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Final Report Geotechnical Engineering Investigation Clinical Lab and Red-Bag Storage Area Martin Luther King Jr. Medical Campus 1670 E. 120 th Street Willowbrook, California Prepared for: County of Los Angeles Department of Public Works Project Number: 60595699 May 30, 2019

Final Report Geotechnical Engineering Investigation

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Final Report

Geotechnical Engineering InvestigationClinical Lab and Red-Bag Storage AreaMartin Luther King Jr. Medical Campus1670 E. 120th StreetWillowbrook, California

Prepared for:County of Los Angeles Department of Public Works

Project Number: 60595699

May 30, 2019

WJouzy
Text Box
Attachment 1-1

AECOMOne California Plaza300 South Grand AvenueLos Angeles, CA 90071

T: +1 (213) 593 8100F: +1 (213) 593 8178aecom.com

May 30, 2019

County of Los AngelesDepartment of Public Works Project Management Division I900 South Fremont Avenue, 5th FloorAlhambra, CA 91803-1331

Attention: Ms. Gillian Tiede, P.E.Project Manager

Subject: Final ReportGeotechnical Engineering InvestigationClinical Lab and Red-Bag Storage AreaMartin Luther King Jr. Medical Campus1670 E. 120th Street Willowbrook, CaliforniaProject No. 60595699

Dear Ms. Tiede:

AECOM Technical Services, Inc. (AECOM) is pleased to present the results of our geotechnical engineering investigation performed for the proposed Clinical Lab and Red-Bag Storage Area Project at the Martin Luther King, Jr. (MLK) Medical Campus located at 12021 S. Wilmington Avenue, Willowbrook, in Los Angeles County, California. This report summarizes the results of our investigation and contains our geotechnical engineering recommendations for design and construction of the subject structure and the associated improvements.

AECOM prepared this report exclusively for the Project Management Division (PMD) of the Los Angeles County Department of Public Works (LACDPW) for its use in project planning, design, and construction. If you have any questions regarding this report, or if we can be of further service, please contact us at 213-593-8100.

Sincerely,

AECOM Technical Services, Inc.

Garry Lay, P.E., G.E.Principal Engineer, Vice President

Table of ContentsSection 1 Introduction .................................................................................................................... 1-1

General .......................................................................................................................... 1-1Project Description ......................................................................................................... 1-1Purpose and Scope of Work ........................................................................................... 1-1

Section 2 Field Investigation and Laboratory Testing ...................................................................... 2-1Review of Existing Data .................................................................................................. 2-1Geotechnical Field Exploration........................................................................................ 2-1

2.2.1 Pre-Feld Activities ............................................................................................. 2-12.2.2 Soil Boring ........................................................................................................ 2-12.2.3 Cone Penetration Test ...................................................................................... 2-1

Geotechnical Laboratory Testing ..................................................................................... 2-2Section 3 Site Conditions ............................................................................................................... 3-1

Regional Geologic and Topographic Setting .................................................................... 3-1Faulting and Seismicity ................................................................................................... 3-1Surface Conditions ......................................................................................................... 3-2Subsurface Conditions .................................................................................................... 3-2Groundwater................................................................................................................... 3-2Generalized Soil Profile .................................................................................................. 3-4Field Infiltration Characteristics ....................................................................................... 3-4

Section 4 Geological and Seismic Hazards Evaluation ................................................................... 4-1General .......................................................................................................................... 4-1Geological Hazards ........................................................................................................ 4-1Seismic Hazards............................................................................................................. 4-1

4.3.1 Ground Rupture ................................................................................................ 4-14.3.2 Ground Motion .................................................................................................. 4-14.3.3 Liquefaction and Seismically-Induced Settlement .............................................. 4-24.3.4 Lateral Spread Displacement ............................................................................ 4-34.3.5 Earthquake-Induced Flooding ........................................................................... 4-34.3.6 Other Seismic Hazards ..................................................................................... 4-4

Section 5 Discussion and Recommendations ................................................................................. 5-1General .......................................................................................................................... 5-1Earthwork ....................................................................................................................... 5-1

5.2.1 Site Preparation ................................................................................................ 5-25.2.2 Over-excavations .............................................................................................. 5-25.2.3 Fill and Backfills ................................................................................................ 5-25.2.4 Grading Factor.................................................................................................. 5-35.2.5 Temporary Excavation ...................................................................................... 5-45.2.6 Temporary Shoring ........................................................................................... 5-45.2.7 Permanent Slopes ............................................................................................ 5-5

Foundation Recommendations ....................................................................................... 5-5Deep Foundation Design - Existing Piles ........................................................................ 5-5

5.4.1 Existing Pile Axial Capacity ............................................................................... 5-55.4.2 Settlement ........................................................................................................ 5-75.4.3 Lateral Capacity - Vertical Piles ......................................................................... 5-75.4.4 Lateral Capacity - Pile Cap ............................................................................... 5-8

Deep Foundation Design - New Piles .............................................................................. 5-85.5.1 Axial Capacity ................................................................................................... 5-8

5.5.2 Settlement ........................................................................................................ 5-95.5.3 Pile Downdrag Consideration ............................................................................ 5-95.5.4 Lateral Capacity ................................................................................................ 5-95.5.5 Lateral Capacity - Pile Cap/Grade Beam ......................................................... 5-105.5.6 Sleeved Pile ................................................................................................... 5-10

Micropile ....................................................................................................................... 5-115.6.1 Axial Capacity ................................................................................................. 5-115.6.2 Lateral Capacity .............................................................................................. 5-12

Retaining Structure ....................................................................................................... 5-125.7.1 Bearing Capacity ............................................................................................ 5-125.7.2 Earth Pressure................................................................................................ 5-125.7.3 Wall Drainage ................................................................................................. 5-13

Floor Slab ..................................................................................................................... 5-13Concrete Flatwork ........................................................................................................ 5-14Site Drainage ................................................................................................................ 5-14Low Impact Development Mitigation Measure ............................................................... 5-14Utilities ......................................................................................................................... 5-14Corrosivity .................................................................................................................... 5-14County Building Code Section 111 Statement ............................................................... 5-15

Section 6 Construction Considerations ........................................................................................... 6-1Excavation ...................................................................................................................... 6-1Groundwater................................................................................................................... 6-1CIDH Installation............................................................................................................. 6-1Micropile Installation ....................................................................................................... 6-1

Section 7 Design Review ............................................................................................................... 7-1Section 8 Construction Monitoring .................................................................................................. 8-1Section 9 References ..................................................................................................................... 9-1Section 10 Uncertainties and Limitations ........................................................................................ 10-1

FiguresFigure 1 Vicinity MapFigure 2 Geotechnical Investigation Plot PlanFigure 3 Regional Geologic MapFigure 4 Regional Fault MapFigure 5 Geologic Cross-Section A-A’ Figure 6 Lateral Earth Pressures for Temporary ShoringFigure 7 Lateral Earth PressuresFigure 8 Axial Pile Capacity: New PilesFigure 9 Vertical Earth Pressures Buried Objects

TablesTable 1 - SUMMARY OF SOIL BORINGS ............................................................................................. 2-2Table 2 - SUMMARY OF CONE PENETRATION TESTS ...................................................................... 2-2Table 3 - MAJOR FAULT CHARACTERIZATION ................................................................................... 3-2Table 4 – GENERALIZED SOIL PROFILE ............................................................................................ 3-4Table 5 – SEISMIC DESIGN PARAMETERS ........................................................................................ 4-2Table 6 - LIQUEFACTION POTENTIAL AND SEISMIC SETTLEMENT ................................................. 4-3Table 7 - IMPORT FILL AND SELECT BACKFILL CRITERIA ............................................................... 5-3Table 8 - PILE AXIAL LOAD-DISPLACEMENT RELATIONSHIP – COOLING TOWER PHASE 1 .......... 5-6Table 9 - PILE AXIAL LOAD-DISPLACEMENT RELATIONSHIP - COOLING TOWER PHASE 2 ........... 5-7Table 10 - PILE lateral LOAD-DISPLACEMENT RELATIONSHIP - COOLING TOWER PHASE 1 ......... 5-8Table 11 - PILE LATERAL LOAD-DISPLACEMENT RELATIONSHIP - COOLING TOWER PHASE 1 .... 5-8Table 12 - SUMMARY OF CIDH PILE AXIAL CAPACITY ...................................................................... 5-9Table 13 - SUMMARY OF CIDH PILE LATERAL CAPACITY ............................................................... 5-10Table 14 – CORROSION POTENTIAL ................................................................................................ 5-15

AppendicesAppendix A Relevant Previous Geotechnical Data Appendix B Field Exploration and Logs of BoringAppendix C Cone Penetration TestAppendix D Geotechnical Laboratory TestingAppendix E Liquefaction and Seismic Settlement AnalysesAppendix F Axial Pile AnalysesAppendix G Lateral Pile Analyses

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Section 1 Introduction

General

This report presents the results of AECOM Technical Services, Inc. (AECOM) geotechnical engineering investigation performed for the proposed Clinical Lab and Red-Bag Storage Area Project (Project) at Martin Luther King, Jr. (MLK) Medical Campus (Campus) located at 12021 South Wilmington Avenue, in Willowbrook area of unincorporated Los Angeles County, California. The location of the Project site relative to the surrounding area is shown on the Vicinity Map, Figure 1. Generally, the Campus is bound by 120th Street to the north, service access road to the south, Wilmington Avenue to the east, and Compton Avenue to the west. The geographic coordinates of the subject improvements are 33.92294° North and 117.244172° West.

This geotechnical investigation was performed for the Project Management Division (PMD) of Los Angeles County Department of Public Works (LACDPW) under the As-needed Geotechnical Engineering, Materials Testing and Inspection Services, Consultant Services Agreement, PW15013, between LACDPW and AECOM.

The report provides the findings from our subsurface explorations and laboratory testing, our interpretation of the geologic and geotechnical conditions encountered, and recommendations for design and construction of the Project. Conclusions and recommendations presented in this report are based on subsurface conditions encountered at our exploration locations. As subsurface conditions may vary at different locations, these conclusions and recommendations should not be extrapolated to other areas, or used for other facilities, without our prior review. This report excludes any discussion of the environmental issues at the Project site. However, a limited Phase II Environmental Site Assessment (ESA) study was conducted by AECOM’s legacy company URS Corporation (URS) in 2009 which addressed the vicinity of the Project (URS, 2009) and significant earthwork was performed to the north, east, and south of the subject site during the previous MLK Impatient Tower (IPT) and Multi-Service Ambulatory Care Center (MACC) projects between 2011 and 2014.

Project Description

The Project is located immediately east of the existing South Support Building, between south of Outpatient Center (formerly known as MLK MACC) and service access road. The Project site is currently occupied by the Cooling Tower as shown on Figure 2. It is our understanding that the Project will consist of demolition of the cooling tower and construction of an at-grade prefabricated steel structure (i.e., “Butler” Building) with a building footprint of approximately 80 feet (east-west dimension) by 210 feet (north-south dimension). The design structural loading information was not available during the preparation of the subject report; however, we anticipated the structure may be lightly loaded by nature. The project will also include construction of an exterior red-bag storage enclosure.

In addition, we understand that site stormwater mitigation measure will mostly follow the nature drainage pattern as follows toward southeast, while field infiltration measure was judged not feasible based on the previous study by URS (URS, 2010).

Purpose and Scope of Work

The purpose of our geotechnical investigation is to explore the subsurface conditions at the proposed Project area and to provide foundation design parameters, earthwork requirements, and construction recommendations for the design and construction of the Project.

Our services were performed in accordance with the requirements of the 2016 California Building Code (CBC)/2017 County of Los Angeles Building Code (CLABC) and American Society of Civil Engineers (ASCE)/Structural Engineering Institute (SEI) 7-10 Standards with the field and laboratory testing

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procedures following the pertinent American Society for Testing and Materials (ASTM) and California Test Method (CTM) Standards. Seismic hazard evaluation will be based on guidelines established by the California Geological Survey (CGS) in the Special Publication (SP) 117A.

The scope of services as outlined in the work authorization No. A15013CP-00013 was followed closely and generally included the following tasks:

1) Reviewed available geologic maps/reports and previous geotechnical information relative to the Project;

2) Obtained a permit from Los Angeles County Department of Environmental Health (EH) for explorations penetrating the groundwater, or deeper than 10 feet;

3) Notified Underground Service Alert (USA) prior to beginning of our field investigation program;4) Explored subsurface conditions by drilling and sampling two geotechnical exploratory borings;5) Explored subsurface conditions by pushing one geotechnical exploratory cone penetration

sounding;6) Performed laboratory testing on selected soil samples obtained from the borings to evaluate soil

index, shear strength, consolidation potential, expansion index, sand equivalent, maximum density, and corrosion potential;

7) Performed geologic/seismic hazard evaluation including liquefaction and seismic-induced settlement analyses based on the updated seismic design criteria, and provide applicable mitigation measures, where required;

8) Performed engineering analyses to develop geotechnical recommendations; and9) Prepared this report containing our findings and recommendations for the proposed improvements

in accordance with the current standards and requirements, including:- Brief description of the Project;- Plan drawn to scale depicting the locations of relevant explorations;- Summary of the relevant field and laboratory testing programs;- Subsurface soil conditions, soil types, groundwater information;- Discussion of the site geologic and subsurface conditions;- One geologic cross section;- Geological and seismic hazards at the site, including subsidence, ground shaking, ground

rupture, seismic-induced settlements, liquefaction, and lateral spreading potential in accordance with 2008 CGS SP 117A, CGS published hazard maps and reports, and 2016 CBC, including seismic design criteria based on the ASCE 7-10;

- Generalized geotechnical design profile and shear strength parameters for foundation design and excavation support, if applicable, based on the field and laboratory data;

- Permanent active, passive and at-rest earth pressure under static and seismic loading conditions for retaining wall;

- Recommended foundation design capacities for spread footings, continuous footings, and/or deep foundation;

- Magnitude of total and differential footing settlements;- Lateral earth pressures: passive, active, at-rest conditions;- Temporary excavation and shoring alternative, and associated design input, as well as the

potential impact to the existing adjacent structure;- Fill material and compaction requirements, including bedding and pipe zone material, and

suitability of on-site soils for utility backfill;- Earthwork recommendations;- Geotechnical consideration for low impact development (LID) mitigation measures;

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- Corrosion potential to steel and concrete will be evaluated based on ACI 318 and Caltrans Corrosion Guideline

- Construction monitoring recommendations; and- Los Angeles County Building Code Section 111 compliance statement.

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Section 2 Field Investigation and Laboratory TestingThe geotechnical investigation included reviewing available geotechnical and geologic data, as-built information and performing subsurface explorations. Geotechnical laboratory testing was conducted on selected soil samples collected during the field exploration program.

Review of Existing Data

Available geologic and geotechnical documents reviewed during the current investigation are listed in Section 9. Pertinent information from these documents was incorporated into the preparation of this report. Relevant field data and previous studies within the project vicinity are attached in Appendix A.

Geotechnical Field Exploration

The field investigation consisted of exploratory two hollow-stem auger borings and one cone penetration test (CPT). The exploration program was developed based on the preliminary site layout prepared by Perkins Eastman.

2.2.1 Pre-Feld ActivitiesAECOM conducted pre-field activities including USA notification prior to commencing soil sampling and testing activities to identify underground utilities in relation to the Project site. We also prepared a site-specific Health and Safety Plan (HASP), which was reviewed and approved by an AECOM Certified Industrial Hygienist (CIH). Our subconsultant, Southwest Geophysics Inc. (SGI), conducted a geophysical survey to further verify the locations of suspected underground utilities utilizing a variety of non-destructive techniques such as ground penetrating radar (GPR), electromagnetic, electrical resistivity, and magnetometer surveys to check for underground utilities.

In addition, AECOM conducted a site kickoff meeting with MLK personnel to discuss logistical matters (i.e. site access, traffic closure, and other site requirements/restrictions) for the field exploration program.

2.2.2 Soil BoringTwo soil borings were completed at the site using hollow-stem auger (HSA) drilling technique between January 23 and 24, 2019, at the locations shown on Figure 2. The borings were drilled to a maximum depth of 60 feet below the existing ground surface (bgs). The boring depths were selected to extend below the anticipated load influence depths and to investigate liquefaction potential. A summary of the soil boring operations is provided in Table 1. Details of the field investigation, including sampling procedures, boring logs, and disposal of investigation-derived wastes (IDW) are presented in Appendix B.

2.2.3 Cone Penetration TestOne cone penetration test was performed on February 14, 2019 at the locations as shown on Figure 2. The CPTs extended to 100 feet bgs. A summary of the CPTs is provided Table 2. Details of the CPT including records and correlations are included in Appendix C.

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TABLE 1 - SUMMARY OF SOIL BORINGS

APPROXIMATELOCATION

BORINGNUMBER

APPROXIMATE COORDINATES APPROXIMATE BORING

DEPTH(feet)

APPROXIMATEBORINGBOTTOM

ELEVATION(feet - MSL)

NORTHING1

(feet)EASTING1

(feet)

SURFACEELEVATION2

(feet MSL)North of the

Cooling Tower B-18-L1 6487581.914 1794445.806 95.0 60 33.58

South of the Cooling Tower B-18-L2 6487550.637 1794184.221 90.0 60 28.5

Notes:1. Approximate locations. Northing and easting based on California Zone 05, NAD83. 2. Based on topo map; MSL=mean sea level.

TABLE 2 - SUMMARY OF CONE PENETRATION TESTS

APPROXIMATELOCATION

BORINGNUMBER

APPROXIMATE COORDINATES APPROXIMATE BORING

DEPTH(feet)

APPROXIMATEBORINGBOTTOM

ELEVATION(feet - MSL)

NORTHING1

(feet)EASTING1

(feet)

SURFACEELEVATION2

(feet MSL)North of the

Cooling Tower C-18-L3 6487581.007 1794447.264 95.0 100 -5

Notes:1. Approximate locations. Northing and easting based on California Zone 05, NAD83. 2. Based on topo map; MSL=mean sea level.

Geotechnical Laboratory Testing

Geotechnical soil samples obtained from the borings were carefully sealed and packaged in the field to reduce moisture loss and disturbance. The samples were delivered to the appropriate testing laboratories, where they were further examined and classified. Laboratory testing was performed on selected samples to confirm (and to modify if necessary) the visual classification of the soils based on the field identification. Geotechnical tests performed included:

· Soil classification (ASTM D2488);· Moisture content test (ASTM D2216);· In-situ density test (ASTM D2937);· Particle size analysis (ASTM D422, D1140);· Atterberg limits (ASTM D4318);· Direct shear test (ASTM D3080);· Maximum dry density and optimum moisture content (ASTM D1557);· Consolidation test (ASTM D2435);· Expansion index (ASTM D4829);· Chemical (Corrosion) Test (Resistivity, Sulfate, pH and Chloride) (California Test Methods 417,

422, 532, & 643).

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A description of the laboratory testing and the test results are presented in Appendix D of this report. For ease of reference, test results of moisture, in-situ density, and fines content of soils tested are also shown on the Log of Boring in Appendix B.

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Section 3 Site ConditionsAECOM’s knowledge of the site geology and subsurface conditions has been developed from a review of the area’s geology, historical information, and relevant field and laboratory programs performed at the Campus.

Regional Geologic and Topographic Setting

The site is located within the northern portion of the Peninsular Ranges Geomorphic Province, which is characterized by a series of generally northwest-trending mountain ranges and intervening valleys. The northern portion of the peninsular Ranges Province, generally referred to as the Los Angeles Basin is a broad sediment filled trough.

The site lies within the central portion of the Los Angeles basin, which is underlain by over 1,000 feet of sediments that have been deposited within this down-warped basin since Pliocene time. Underlying these alluvial deposits is Pliocene age marine sediments deposited during a time when a shallow sea covered much of southern California. The local geology of the site vicinity is shown in Figure 3, Regional Geologic Map.

The hills bordering this area of the Los Angeles Basin are characterized by a complex sequence of Cretaceous to Pleistocene age marine and non-marine sedimentary rocks. Localized igneous intrusive rocks attest to the complex geologic history of the area. Erosion of the hills within the Santa Monica Mountains, located to the north of the site, is the source for the broad alluvial deposits forming much of the Los Angeles Basin to the south.

The site is directly underlain by artificial fill and relatively younger alluvial deposits labeled as map symbol Qya2 on Figure 3, overlying more consolidated older alluvium. These deposits are representative of alluvial outwash associated with transport and deposition of the ancestral Los Angeles River. These soils generally consist of medium dense interbedded clayey silts, silty clays and sandy silts, and silty sands.

Faulting and Seismicity

The Los Angeles Basin, as well as most of Southern California, is located within a complex zone of faults and folds resulting from compressional forces occurring along a bend within the boundary between the Pacific and North American tectonic plates. Numerous generally east-west to northwest trending faults have formed as a result of these north-south compressional forces acting within this area. The major faults within the vicinity of the Los Angeles Basin are characterized by a combination of blind thrusting, right-lateral strike-slip, and reverse faulting.

The Regional Fault Map, as shown on Figure 4, includes the location of active and potentially active faults, within the general vicinity of the site. Most of the larger earthquakes have been associated with larger faults that have been mapped at the ground surface. A number of moderate to large earthquakes in the region have also occurred on deep-seated buried thrust faults in this geological complex region of Southern California. The most recent significant earthquake was the magnitude 6.7 Northridge earthquake, which occurred on a shallowly south-dipping thrust fault that underlies much of the San Fernando Valley.

The closest active fault to site is the Newport-Inglewood fault, located approximately 2.3 miles to the southwest. The historically active San Andreas fault is located approximately 42 miles to the north. The characteristics of the nearby faults are summarized in Table 3.

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TABLE 3 - MAJOR FAULT CHARACTERIZATION

FAULTAPPROXIMATE

DISTANCE1

(kilometers)

APPROXIMATEDISTANCE1

(miles)

TYPE OFFAULT2

MAXIMUMEARTQUAKEMAGNITUDE1

(Mw)Newport-Inglewood 3.7 2.3 Strike Slip 6.99Puente Hills 5.4 3.4 Blind Thrust 6.92Compton 15.2 9.5 Blind Thrust 7.29Elysian Park 16.0 10.0 Thrust 6.72San Vicente 16.3 10.2 Blind Thrust 6.17Anaheim 17.0 10.6 Blind Thrust 6.24Palos Verdes 17.3 10.8 Strike Slip 7.15Redondo Canyon 18.7 11.7 Reverse 6.49Santa Monica 20.8 13.0 Reverse 6.63San Andreas 68.2 42.6 Strike Slip 7.1Notes:

1. Distance to fault, Rx, which is defined as the perpendicular distance from the site to the surface projection of the topof fault.

2. Fault characterization based on Field et al., 2013.3. The maximum earthquake magnitude is estimated using the Leonard 2010 magnitude-area scaling relations.· Fault data based on Uniform California Earthquake Rupture Forecast, Version 3 (Field et al., 2013).

Surface Conditions

The proposed site is currently an existing old cooling tower that services the old hospital. The project site is surrounded by asphalt-concrete paved access road leading to the loading docks of the new MACC building. The general topography of the Project site is relatively level with the existing ground elevations of the Project site ranged from approximately 90 to 95 feet above mean sea level (MSL). The project site has the highest elevation at the north side and slopes towards the south.

Subsurface Conditions

Based on the information from the previous investigations, the proposed Project is underlain by a layer of fill approximately up to 15 feet deep; however, thicker backfill may be anticipated along underground utilities (i.e., storm drains) depending on the depths of respective lines. The fill is primarily of silty sand and sandy clay mixture. The fill is generally medium dense for silty sand, soft to medium stiff for sandy clay mixture. Below the fill, alluvium was encountered to the maximum explored depths of approximately 100 feet bgs. The alluvial soils generally consist of medium dense to very dense sand silty sand and poorly graded sand, and soft to hard sandy silt and sandy lean clay. There is a zone of approximately 15 to 25 feet of loose silty sand and sandy clay mix just below the fill. Overall, the uncorrected standard penetration test (SPT) blow counts are 5 to 19 for coarse grained. The subsurface condition below the proposed structure is presented on Figure 5.

Groundwater

Highest groundwater was encountered at 50.3 feet bgs (corresponding to elevation 44.7 feet MSL) in Boring B-18-L1 during this investigation. This is approximately 14 feet below the consistent high groundwater levels recorded from previous field programs conducted for the construction projects at the campus, as well as the high groundwater level data from the nearby groundwater well located at the northwest corner of E. 120th Street and Compton Avenue. These observed groundwater levels were highly influenced by the area

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groundwater pumping activities and may rise to shallower depths with reduced quantity of extraction or local injection/infiltration actions. According to GS200.2, the highest groundwater level is at elevation 58 feet MSL was recommended for LID design, based on the current borings, the nearby monitoring well, and available modern (in the past 30 years) groundwater level measurements.

For engineering analyses and foundation design, it is recommended to utilize the historically highest groundwater level developed by CGS for conservatism. In accordance with CGS Seismic Hazard Zone Report 034 (SHZR 034; 2001), the contours indicated depths of 8 to 10 feet in the Project vicinity to be used for historically highest groundwater level. Considering the groundwater contours were mainly based on the recorded data from early 20th century (Mendenhall, 1905), it is our opinion that the early 1900’s ground elevation should be used as the reference to the historical high groundwater level, instead of the current grades, since the majority of the Project site has been raised in the past phases of development. Therefore, we utilized the available data based on the fill/native contact elevations in the borings from the initial investigations during mid-1960s to the recent studies at the site to identify the original ground levels and it is judged that an average elevation of 87 feet MSL is considered reasonable to represent the relatively level original ground prior to current grades at the Project site. Accordingly, an average historically highest groundwater elevation of 78 feet MSL is recommended for our liquefaction evaluations and engineering analyses.

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Generalized Soil Profile

For design purposes, the site subsurface conditions were summarized into a generalized profile and the geotechnical parameters of the idealized profile are presented in Table 4.

TABLE 4 – GENERALIZED SOIL PROFILE

SOIL TYPE ELEVATION(feet MSL)

DEPTH1

(feet bgs)

TOTALUNIT

WEIGHT(pcf)

SPT-N2

(bpf)

SHEAR STRENGTHEffective Total

Cohesion(psf)

FrictionAngle

(degrees)

UndrainedShear

Strength(psf)

FILL – loose SiltySand 92.52 to 77.5 0 to 15 125 6 to 13 200 28 --

ALLUVIUM –Medium dense todense Poorly-graded Sand

77.5 to 72.5 15 to 20 130 10 to 18 0 31 --

ALLUVIUM –Medium dense todense Clayey Sandto Silty Sand

72.5 to 62 20 to 30 125 17 to 18 100 30 --

ALLUVIUM –Medium dense todense Well-gradedSand to Poorly-graded Sand

62 to 47.5 30 to 45 110 27 to 50 100 31 --

ALLUVIUM – hardSilt 47.5 to 40 45 to 52.5 120 19 to 23 -- -- 1,500

ALLUVIUM –Medium dense todense Silty Sand

40 to 31 52.5 to 61.5 125 27 to 50 100 31 --

Notes:1. Assumed finished grade at 92.5 feet MSL.2. Range indicating maximum and minimum uncorrected values recorded, while arithmetic average reported in

parentheses.

Field Infiltration Characteristics

A series of field infiltration tests were conducted by URS throughout the campus and the relevant data to the subject Project from the test PT-2 were provided in Appendix A (URS, 2010). Based on the adjusted field infiltration rate of 0.3 inches per hour at the near surface soil (i.e., less than 5 feet from ground surface), the site near-surface soils are not able to meet the minimum requirement for stormwater infiltration within the corresponding test depths once the proper factors of safety are considered in accordance with “Guidelines for Design, Investigation, and Reporting, Low Impact Development Stormwater Infiltration (GS200.2)” by LACDPW Geotechnical and Materials Engineering Division (GMED) dated June 30, 2017. Therefore, infiltration at near surface soils is not considered feasible for the subject project.

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Section 4 Geological and Seismic Hazards EvaluationGeneral

Geological and seismic hazards are those hazards that could impact a site due to the surrounding geologic and seismic conditions. Geological hazards include landsliding, erosion, subsidence, volcanic eruptions, and poor soil conditions. Seismic hazards include phenomena that occur during an earthquake such as ground shaking, ground rupture, and liquefaction. The potential impact of these hazards to the site has been assessed and is summarized in the following sections. Our assessment of these hazards was based on guidelines established by California Geological Survey (CGS; formerly California Division of Mines and Geology [CDMG]) as outlined in its Special Publication 117A (2008) and Note 48 (2007).

Geological Hazards

Geologic hazards such as landsliding, erosion, subsidence, poor soil conditions and volcanic eruptions have a low potential of impacting the site. No significant slopes are present at the subject site, as such, there is minimal risk for landsliding under normal conditions. According to the CGS, the site is not located within a landslide hazard zone. Most of the existing site is landscaped or covered with asphalt or concrete and will not be readily susceptible to erosion. Subsidence beneath the proposed site due to oil or groundwater withdrawal is unlikely to occur because the site is located a considerable distance from such activities. Medium dense soil conditions underlie the site reducing the potential of damage due to poor soil conditions, and laboratory test results indicated that the near surface onsite soil has Expansion Index of approximately 47 near the proposed building footprint, which is considered as having a low expansion potential.

Seismic Hazards

Seismic hazards are those hazards associated with earthquakes such as ground shaking, ground rupture, liquefaction, differential compaction or seismic settlement, and other phenomena. The proposed project site, like most sites in southern California, is most susceptible to ground shaking generated during earthquakes on nearby faults. The intensity of ground shaking, or strong ground motion, is highly dependent upon on the distance of the fault to the site, the magnitude of the earthquake, and the underlying soil conditions. These hazards and how they may affect the site are discussed in the following sections.

4.3.1 Ground Rupture

The site is not located within a currently established Alquist-Priolo Earthquake Fault Zone, therefore, the potential for ground surface rupture was considered low because no known active faults were mapped on the site. The CGS defines an active fault as one that has experienced surface rupture within the last 11,000 years (Holocene time). However, ground rupture or cracking can occur due to earthquakes at locations where faults have not been mapped.

4.3.2 Ground Motion

Like most sites in southern California, is susceptible to strong ground shaking generated during earthquakes on nearby faults. Strong ground motion occurs as energy is released during an earthquake. The intensity of ground motion is dependent upon the distance to the fault rupture, the earthquake magnitude, and the geologic conditions underlying and surrounding the site.

Based on the results obtained from USGS Earthquake Hazards Program - U.S. Seismic Design Maps Version 3.1.0 dated 07-11-2013, a PGAM (Site-Specific Maximum Considered Earthquake Geometric Mean

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(MCEG) peak ground acceleration) of 0.634g (corresponding to 2% probability of exceedance in 50 years; average return period [ARP] of 2475 years) and the corresponding mean moment magnitude of 6.7 (USGS, 2014) shall be considered for geotechnical engineering analyses such as evaluation of liquefaction potential and seismic-induced settlement per 2016 CBC. Under PGAM, the building foundations should not lose the ability to carry gravity loads and the building should not collapse under the design event; otherwise, mitigation should be performed.

The subject project is classified as Site Class F profile due to presence of potential liquefiable soils at the site. However, if the fundamental period for the proposed structure is less than 0.5 seconds, the seismic design can be performed in accordance with the criteria listed in Table 5 based on Site Class D profile following the mapped values of the current CBC and CLABC.

TABLE 5 – SEISMIC DESIGN PARAMETERS

CHARACTERISTIC CRITERIA

Site Class F1

Ss - mapped spectral acceleration at short periods (g) 1.7282

S1 - mapped spectral acceleration at 1-second period (g) 0.6272

Fa - site coefficient 1.0Fv - site coefficient 1.5SMS - risk-targeted maximum considered earthquake (MCER) spectral acceleration at short periods (g) 1.728

SM1 - MCER spectral acceleration at 1-second period (g) 0.94SDS - design spectral acceleration at short periods (g) 1.152SD1 - design spectral acceleration at 1-second period (g) 0.627PGA – mapped maximum considered earthquake geometric mean (MCEG) peak ground acceleration (g) 0.6342

Notes:1. Site Class F due to potential liquefaction. The seismic design parameters were based on Site Class

D considering the proposed structures to be on piles and fundamental period of no greater than 0.5 seconds.

2. ASCE 7-10 mapped values for 2 percent probability exceedance in 50 years.

4.3.3 Liquefaction and Seismically-Induced Settlement

The project site is within the liquefaction zone assigned by the CGS. A site-specific liquefaction analysis was performed in general accordance with the guidelines presented in the California Geological Survey 117A (CGS, 2008), the recommendations provided in Seed et al (2003) and the Manual for Preparation of Geotechnical Reports (LACDPW, 2013). As discussed in Section 3.5, a design groundwater elevation of 78 feet MSL was used in the liquefaction analysis. The peak ground acceleration was based on the mapped maximum considered earthquake geometric mean (MCEG) peak ground acceleration. The corresponding modal moment magnitude of 6.7 and modal distance of 7.0 kilometers using the USGS seismic deaggregation tool were considered. The input parameters were as follows:

Moment Magnitude, Mw: 6.7

Peak Ground Acceleration (PGA): 0.634 g

Design Groundwater Elevation: 78 feet MSL

The site-specific liquefaction analyses were performed assuming the design groundwater at both historicalhigh (i.e., 78 feet MSL) and current groundwater level (greater than 51.5 feet). The evaluation indicates

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that potential for liquefaction at the Project site is moderate and the results are summarized in Table 6.However, the fine-grained silty soils encountered at the MLK Campus are judged unlikely to undergo severestrength loss during ground shaking.

For soils above the groundwater table, dry sand settlement could occur from the sandy soils due to groundshaking. Liquefaction and dry sand settlement evaluation were performed using the relevant boring dataand laboratory testing.

Based on the results of the dry sand and liquefaction-induced settlement analyses, the total seismic-induced settlement is estimated to be up to approximately 2.0 inches and therefore, the impact to thefoundations due to design earthquake is considered moderate. It is also judged that surface expression atthe foundation/ pile cap bottom and potential down drag on piles are unlikely, due to the interbedded andisolated nature of potential liquefiable materials encountered at the site.

TABLE 6 - LIQUEFACTION POTENTIAL AND SEISMIC SETTLEMENT

BORING

DEPTH OFPOTENTIALLYLIQUEFIABLE

LAYER(feet)

POTENTIALLYLIQUEFIABLE

LAYERELEVATION1

(feet MSL)

TOTALTHICKNESS OFPOTENTIALLYLIQUEFIABLE

LAYER1,2

(feet)

TOTALSEISMICALLY-

INDUCEDSETTLEMENT3

(inches)

B-18-L1 22 to 32 72 to 62 10 1.6B-18-L2 18 to 22 72 to 62 10 2.0

Notes:1. Design groundwater at Elevation +78 feet MSL.2. Settlement at level existing ground surface.3. Seismically-induced settlement based on material with factor of safety less than 1.0.

The detailed calculations for dry sand settlement and liquefaction-induced settlement are presented inAppendix E.

4.3.4 Lateral Spread Displacement

According to publications by Bartlett and Youd, 1999, conditions such as free-face, sloping ground surface and liquefiable layers are factors contributing to lateral spread displacement of the ground during strong motion events. As the project site relatively leveled with no sloping ground conditions, the risk of lateral spread displacement is considered low.

4.3.5 Earthquake-Induced Flooding

Earthquake induced flooding occurs when nearby water retaining structures, such as dams or storage tanks, are breached or damaged during an earthquake. According to the Los Angeles County Safety Element (1990), the site is within the inundation zone for several dams and reservoirs located upstream of the site. As presented in planning scenarios for a magnitude 8.3 earthquake on the San Andreas Fault, and a magnitude 7.1 earthquake on the Newport-Inglewood fault, the CGS has determined that the risk for failure of these dams during such an earthquake is unlikely. Therefore, the overall risk for earthquake induced flooding appears to be low.

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4.3.6 Other Seismic HazardsOther seismic hazards include tsunamis, seiches and earthquake-induced landslides. The potential for tsunamis, seiches and earthquake-induced landslides at the proposed site is low due to the sites distance from the Pacific Ocean; absence of oceans, lakes, or large bodies of water in the immediate area; and relatively flat topography of the site.

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Section 5 Discussion and RecommendationsGeneral

The subsurface information and geotechnical recommendations presented in this report are intended to provide general geotechnical information for design and construction of the proposed Clinical Lab and Red-Bag Storage Area. Based on the results of our geotechnical investigation and the anticipated loading conditions, we believe that the proposed Project is feasible from a geotechnical point of view, provided the recommendations in this report are incorporated in the design and implemented during construction of the project.

The Project site is currently occupied by the cooling towers built in early- to mid-1970’s in two phases, which have below grade basin at varying depths to the lowest bottom elevation of approximately 80 feet MSL. Based on the current Project scheme, we understand that the basins will be partially removed as part of the cooling tower demolition prior to the construction of the subject structure.

The overall MLK Medical Center site is located within the liquefaction zone (CGS, 1999). A site-specific liquefaction analysis was performed for the proposed structure. The subject project site has moderate liquefaction potential and the total seismic-induced settlement is up to 2.8 inch, which has low impact to foundation with proper structural mitigation from design earthquake.

Based on our subsurface investigation, there is up to 15 feet of fill overlying 33 feet thick or greater of clayey, silty soils and poorly-graded sands underlain the proposed Project limits. The fill is loose and soft and may be compressible and not considered suitable to support any structural footings. The underlying clayey/silty soil, when subject to structural loadings, could settle over time when it is saturated. The combined load-induced settlements from the fill zone and the clayey/silty layer may be too excessive and not conducive to use of conventional shallow foundation system. Therefore, deep foundation system utilizing cast-in-drilled-hole (CIDH) piles, similar to the majority of the buildings within the MLK campus, is considered feasible foundation scheme for the Project. As an alternative, mat foundation may be considered as viable options, depending on tolerance of total and differential settlement occurred at individual footing location and the total pressure of the building load.

Due to the extensive effort to remove the existing cooling tower basins, it is recommended to consider to keep the existing basins in place and reuse the existing CIDH piles of the cooling tower to support the proposed structure, provided the basin can be backfilled with light weight backfill without exceeding the original design bearing pressure to surcharge the adjacent building foundations, and the structure loads are transferred to the deeper bearing layers through piling. If additional deep foundation elements are required, micropiles may be considered to supplement the existing CIDH piles to support the proposed structure. We can provide further recommendations if this option is considered and the conceptual scheme is provided.

The following subsections contain our geotechnical recommendations pertaining to the design and construction of the project. The project is considered feasible from a geotechnical standpoint, provided that these recommendations are properly implemented and executed.

Earthwork

Earthwork should be performed in accordance with the applicable portion of the State and local building code, as well as the recommendations of this report, and should be performed under the observation and testing of a representative of the Geotechnical Engineer of Record (GEOR).

It is the responsibility of the contractor to select the proper equipment necessary for site excavation and backfilling. All excavations should be observed by the GEOR. Some variations in subsurface conditions are anticipated. However, if conditions encountered during construction appear to differ from those

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encountered in the exploratory borings, AECOM should be notified so as to consider the need for modifications.

5.2.1 Site Preparation

It is the responsibility of the contractor to notify and coordinate with USA before any proposed earthwork. All active or inactive utilities and tunnels within the construction limits should be identified for relocation, abandonment, or protection prior to grading. Any pipes greater than 2 inches in diameter to be abandoned in-place and should be filled with lean-mix concrete after review of their location and approval by the GEOR.

Where excavations are proposed, all existing debris, organic materials, deleterious materials, undocumented fill and loose soils should be removed and disposed of outside the construction limits under observation of the GEOR.

For cooling tower basin demolition, if pursued, over-excavation should reach to the lowest bottom of the entire basin to ensure the uniform subgrade support from the backfill soil. In addition, the backfill placement should not impose higher overburden then the original design bearing capacity (i.e., 1,000 psf, corresponding to 8 feet of soils) to surcharge the adjacent deep foundations and the nearby fuel tanks. If necessary, light weight backfill or geofoam may be considered.

5.2.2 Over-excavationsOver-excavation is not required for the proposed building on deep foundations. However, for any proposed retaining walls to retain soil 5 feet high or less, we recommend that the upper 3 feet of loose fill below the base of the retaining wall footings be overexcavated and replaced with compacted/engineered fill. For the retaining wall greater than 5 feet but less than 8 feet high, overexcavation should be 5 feet of the undocumented old fill below the base of the retaining wall footings or 2 feet below the native soils.

The area of overexcavation should extend at least 3 feet beyond the building edge, or equal to the depth of removal; whichever is greater. For taller retaining walls, locations should be identified and more specific recommendations can be provided where applicable.

For concrete flatwork/hardscape, overexcavation can be further reduced to 2 feet with similar procedure except the shallower over-excavation depth.

Following over-excavations, the upper 8 inches of the exposed subgrade to receive compacted/ engineered fill should be scarified and proof-rolled in place to at least 95 percent of the maximum dry density to secure uniform support. Probing and field density tests should be performed by a field representative of the GEOR to evaluate the extent of any loose or soft zones.

5.2.3 Fill and Backfills

Onsite sandy soils and other onsite fine-grained clayey soils generated from excavation meet the engineered fill criteria and may be used for a general engineered fill and backfill, but not as Select Backfill. Some or most of the near-surface onsite soils (especially beneath the existing lawns) are very moist to wet and may need some drying before being re-use as new fill materials. All new engineered fill and backfill should be free of hazardous, organic, and inorganic debris. All fill and backfill materials should be observed and tested by the GEOR in order to determine their suitability

Engineered fill and backfill should be compacted by:

· Placing in loose lifts/layers less than 8 inches thick.

· Moisture conditioning to above-optimum moisture content.

· Compacting to at least 95 percent relative compaction in accordance with ASTM D1557 standard.

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No compaction by ponding or jetting should be allowed. If specified moisture content (above optimum) and relative compaction are not achieved, additional compaction effort, moisture conditioning of the fill soils, and/or removal and re-compaction of the below-minimum-compaction soils will be required at the expense of the contractor. No fill should be placed, spread or rolled during unfavorable weather. When the work is interrupted by rain, operations should not be resumed until field tests by the GEOR have indicated that conditions will permit satisfactory results.

To fill the area between the existing structure and the proposed structure: soil, lightweight fill, or geofoam may be used. Soil shall follow the recommendations above for engineered fill. However, lightweight fill material or geofoam may be used to reduce the additional stresses and settlement induced by the newly placed fill.

The lightweight fill material must be selected so that the material can withstand the building load. Lightweight fill materials such as Elastizell (approximate unit weight 4 kN/m3 [of 25 pcf]) and Geofoam (approximate unit weight 21.6 kN/m3 [1.35 pcf]) have been used successfully. However, deflections of lightweight fill material will probably impact the performance of the building. For example, Geofoam material may deform 1 percent under a compression loading of 50 kPa (1,150 psf). Lightweight fill material may be more costly in comparison to traditional fill.

Select Backfill is material placed within a horizontal distance of 5 feet or one-half of the wall height, whichever is greater, behind retaining walls. In addition, aggregate base and trench bedding materials should conform to the Greenbook or similar standards. Select Backfill, if required, should meet the criteria in Table 7.

If additional fill is required, then import materials for compacted/engineered fill should meet the criteria in Table 7.

TABLE 7 - IMPORT FILL AND SELECT BACKFILL CRITERIA

CRITERIA IMPORT FILL SELECT BACKFILLMaximum particle size (inches) 3 1

Maximum liquid limit (%) 10 5Maximum plasticity index (%) 5 0

Minimum percentage passing the No. 4 sieve (%) 80 80Maximum percentage passing the No. 200 sieve (%) 20 10

Minimum sand equivalent 20 20Maximum Expansion Index 30 30

Site grading may be accomplished with conventional heavy-duty construction equipment. The soil fill can be compacted using rubber-tired or vibratory soil compactors as defined by the Caterpillar Performance Handbook (2017) or equivalent. However, to avoid overstressing any existing retaining/basement walls, either the backfill should be compacted using lightweight compaction equipment or the walls should be properly braced.

5.2.4 Grading FactorIf the onsite soil is reused for site civil improvements, a grading factor of 0.90 (i.e., the factor is less than unity, indicating shrinkage) may be considered to estimate the net quantity of the soils to be imported or exported during the earthwork, assuming minimum relative compaction of 95 percent per ASTM D1557.

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5.2.5 Temporary ExcavationExcavations during construction should comply with the current California and Federal OSHA requirements. For design purposes, a Cal/OSHA soil type C can be assumed for the onsite soils. It should be noted that this assessment of Cal/OSHA soil type for temporary excavations is based on engineering classifications of the subsurface materials encountered in widely spaced exploratory borings. The Contractor should have a geotechnical professional evaluate the soil/rock conditions encountered during excavation to determine permissible temporary slope inclinations.

Based on Cal/OSHA requirements, unsupported slopes for temporary excavation in the existing undocumented fill may be vertical for cuts of less than 4 feet in depth. For deeper cuts, up to a maximum height of 20 feet, temporary excavation slopes should be made no steeper than 1.5H:1V (horizontal to vertical). In areas where soils with little or no cohesion are encountered, shoring or flatter excavation slopes may be necessary. Overexcavation should not be performed below an imaginary plane projected at 1H:1V below horizontal from any existing building foundations. If temporary excavation is deeper than 20 feet, or there is space limitation to prohibit sloped excavation, braced or cantilevered shoring should be considered in accordance with Section 5.2.6. It should be noted that the contractor and its engineering professional are responsible for detailed shoring design, which requires final review and approval by the GEOR.

Surcharge loads from vehicles and stockpiled material should be kept away from the top of temporary excavations at a distance equal to at least one half of the excavation depth. During wet weather, runoff water should be prevented from entering the excavation, and collected and disposed of outside the construction limits. To prevent runoff from adjacent areas from entering the excavation, a perimeter berm should be constructed at the top of the slope.

5.2.6 Temporary ShoringWhere stability or lack of available set-back will not allow adequate sloping of temporary excavations, shoring may be required. If soldier beam/legging system is used, maximum horizontal spacing between soldier piles should be limited to about 8 feet. Treated timber lagging may be required in sandy zones. Any void space between the back of the lagging and excavation face should be filled with lean concrete with provisions for weep holes to reduce the potential for buildup of hydrostatic pressure.

The temporary shoring system should be designed to resist lateral earth pressures plus additional horizontal pressures imposed by foundations of adjacent structures and/or vehicle traffic load. Temporary tied-back or braced excavations should be designed to resist an earth pressure in accordance with Figure 6.

If tie-back anchor is proposed by the shoring design professional, the following criteria should be considered:

· Anchors should be at least 5 times pile diameter from the adjacent pile, if any.

· Top lateral deflection of the shoring system should be no greater than ¼-inch. Vertical movement should be controlled within ¼-inch. Rotation of the shoring wall should not be greater than 0.1 percent.

· Instrumentation program utilizing baseline survey and periodical monitoring at developed monuments should be included in the shoring design.

· Construction sequence should clearly be identified in the shoring design.

· If pressure grouted anchors are used, real-time monitoring program should be included as part of pressure grout operation for grouting pressure adjustment in order to prevent hydro fracturing or any adverse impact to the exiting adjacent foundation elements.

· Shoring system abandonment after the construction is completed should be included in the shoring design package. The anchors need to be de-tensioned after abandonment.

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5.2.7 Permanent SlopesPermanent compacted fill slopes, if any, should be planned no steeper than 2H:1V. The slopes should be planted and/or protected to reduce surface erosion.

Foundation RecommendationsThe subsurface information and geotechnical recommendations presented in this report are intended to provide general geotechnical information for planning and design of the Project. Based on the pertinent subsurface data and the anticipated loading conditions, we believe the proposed Project is feasible from a geotechnical point of view, provided the recommendations in this report are incorporated in the design and implemented during construction phase of the Project.

The Project site is located within the liquefaction zone assigned by the CGS (CGS, 1999). A site-specific liquefaction analysis was performed for the projects described in this report. The project site is primarily underlain by clayey soil, which does not liquefy. Based on our dry sand settlement and liquefaction analyses, the likelihood of liquefaction is considered moderate and the seismic-induced settlement is approximately 2.0 inch.

Based on our subsurface investigation, there are about 15 to 20 feet of fills underlain the north of the existing cooling towers. The fills are compressible and not considered suitable to support any structural footings. The adjacent buildings are supported on pile foundations and any additional surcharge shall be avoided to prevent settlement and impact to adjacent structure. The bottoms of the existing cooling tower basins are expected to be bearing on the stiff and dense alluvium. The design of the proposed building can rely on the support of the existing CIDH piles, new CIDH piles, or micropiles.

Deep Foundation Design - Existing PilesFor the current work, the three types of existing 24-inch diameter CIDH pile’s vertical soil springs for the existing cooling tower were developed using the computer program SHAFT (Version 6.0) and axial load capacities for the phase I cooling towers and phase II cooling towers were evaluated. phase I cooling towers foundation consist of 24-inch diameter and 35 feet long CIDH piles with only steel reinforcement in the upper 20 feet at two different elevations: 87 feet MSL (5-feet cover) and 81 feet MSL (10-feet cover). phase II cooling towers foundation consists of 24-inch diameter and 29 feet long CIDH piles with full steel reinforcement along the 29-foot length. SHAFT is a commercially available computer program developed to compute the capacity of a drilled shaft under axial loading. The computation procedures are based principally on the recommendations by the Federal Highway Administration (FHWA, 1999). This approach is considered adequate for practice in California based on the past local experience and previous load test studies by the agencies and research institutes. In general, the axial capacity of a drilled shaft is derived from side resistance (skin friction). End bearing of pile is not considered because of unknown pile installation condition (bottom clean up) and some of the pile tips below groundwater level. Both compression (downward) and tension (uplift) capacities were calculated. For compression, full pile length (including unreinforced portion) was considered. However, only upper pile length with reinforcing was used for tensile capacity evaluation. Analyses were also carried out to account for the variations in the axial capacity with different combination of pile cut-off elevations (also refer to as overburden or soil cover). The pile overburden ranges from 5 feet to 10 feet are considered in our model. For the consideration of non-linearity design where discrete soil-structure interaction (SSI) analysis is required, vertical soil springs (expressed in load versus pile head upward and downward movement) were developed and provided for consideration in the retrofit design for the phase I cooling towers and phase II cooling towers .

5.4.1 Existing Pile Axial CapacityAxial capacities were evaluated for 24-inch diameter CIDH piles. Ultimate axial capacities were calculated using computer program SHAFT (Ensoft Inc., 2012). The results are presented in Table 8, Table 9, and

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Appendix F. For pile center-to-center spacing more than 3-pile diameters, group efficiency reduction is not required.

TABLE 8 - PILE AXIAL LOAD-DISPLACEMENT RELATIONSHIP – COOLING TOWER PHASE 1

PILE CUTOFF AT 87 FEET MSL PILE CUTOFF AT 81 FEET MSLCOMPRESSION UPLIFT COMPRESSION UPLIFT

TOPMOVEMEN

T (inch)

TOP LOAD(kips)

TOPMOVEMEN

T (inch)

TOPLOAD(kips)

TOPMOVEMEN

T (inch)

TOP LOAD(kips)

TOPMOVEMEN

T (inch)

TOPLOAD(kips)

0.00 0.02 0.00 0.00 0.00 0.02 0.00 0.000.00 0.10 0.00 0.02 0.00 0.10 0.00 0.020.00 0.20 0.00 0.04 0.00 0.20 0.00 0.040.01 9.99 0.01 2.13 0.01 9.99 0.01 2.110.01 15.03 0.01 3.25 0.01 15.03 0.01 3.160.02 20.06 0.01 4.33 0.02 20.08 0.01 4.210.04 47.76 0.03 10.64 0.04 47.77 0.03 10.380.08 75.99 0.05 17.67 0.08 75.71 0.05 17.260.10 86.68 0.08 20.74 0.10 86.25 0.08 20.260.13 90.65 0.10 21.83 0.13 90.19 0.10 21.320.28 94.71 0.25 23.82 0.28 94.19 0.25 23.240.53 94.71 0.50 24.47 0.53 94.13 0.51 23.870.66 94.71 0.63 24.63 0.66 94.13 0.63 24.020.81 94.71 0.79 24.90 0.81 94.13 0.79 24.281.23 94.71 1.21 25.51 1.23 94.13 1.21 24.85

Notes:· Partially reinforced pile (upper 20 feet).· Pile length of 35 feet.

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TABLE 9 - PILE AXIAL LOAD-DISPLACEMENT RELATIONSHIP - COOLING TOWER PHASE 2

PILE CUTOFF AT 87 FEET MSLCOMPRESSION UPLIFT

TOPMOVEMENT

(inch)TOP LOAD

(kips)TOP

MOVEMENT(inch)

TOPLOAD(kips)

0.00 0.01 0.00 0.010.00 0.07 0.00 0.040.00 0.14 0.00 0.080.01 6.90 0.01 4.060.01 10.38 0.01 6.110.01 13.86 0.01 8.160.03 33.50 0.03 19.920.07 54.30 0.06 32.710.09 62.64 0.09 38.110.12 65.52 0.11 40.050.27 68.75 0.26 43.230.52 68.75 0.51 44.130.64 68.75 0.64 44.350.80 68.75 0.79 44.731.22 68.75 1.21 45.56

Notes:· Full reinforced pile.· Pile length of 29 feet.

5.4.2 SettlementThe settlement of the deep foundations designed and constructed in accordance with the recommendations provided, was estimated to be less than ½-inch under the static loading conditions. Most of this settlement should occur shortly after application of the structural loads. Differential settlement between the pile supports was estimated to be less than ¼-inch.

5.4.3 Lateral Capacity - Vertical PilesLateral load pile analysis was evaluated using the computer program LPILE 2013 (Ensoft Inc, 2013). The lateral capacities of CIDH piles were estimated using soil resistance-pile deflection models (p-y analyses) for sands, clays, and silts.

A range of typical acceptable horizontal top-of-pile deflections of ¼-, ½-, and 1-inch were used to estimate the lateral pile capacity. The analysis assumed a pile length of 20 and 29 feet for 24-inch CIDH respectively, and the top-of-pile is at Elevation 87 feet and 81 feet, respectively. Lateral load evaluations were performed for pinned- and fixed-head conditions for the proposed CIDH piles and the piles were modeled using 50 percent of the gross moment of inertia as the piles may crack. A factor of safety has not been applied to the estimated loads or deflections. If the minimum center-to-center spacing between the piles is greater than six pile diameters, a group efficiency reduction should not be applied. Summaries of the results of laterally-loaded pile capacities are presented in Table 10, Table 11, and Appendix G.

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TABLE 10 - PILE LATERAL LOAD-DISPLACEMENT RELATIONSHIP - COOLING TOWER PHASE 1

PILE CUTOFF AT 87 FEET MSL PILE CUTOFF AT 81 FEET MSLFREE HEAD FIXED HEAD FREE HEAD FIXED HEAD

PILE HEADDEFLECTION (inch)

MAXIMUM SHEAR

(lbs)

PILE HEADDEFLECTION (inch)

MAXIMUM SHEAR

(lbs)

PILE HEADDEFLECTION (inch)

MAXIMUM SHEAR

(lbs)

PILE HEADDEFLECTION (inch)

MAXIMUM SHEAR

(lbs)0.01 1065 0.01 1065 0.01 1550 0.01 36080.1 10619 0.1 17543 0.1 15424 0.1 240860.2 17845 0.2 29166 0.2 21438 0.2 360890.3 21547 0.3 35572 0.3 26558 0.3 433640.5 28963 0.5 45135 0.5 37116 0.5 560350.75 35608 0.75 52468 0.75 46549 0.75 67964

1 39781 1 58133 1 52749 1 76263Note: Partly reinforced pile. Pile reinforced length of 20 feet.

TABLE 11 - PILE LATERAL LOAD-DISPLACEMENT RELATIONSHIP - COOLING TOWER PHASE 1

FREE HEAD FIXED HEADPILE HEAD

DEFLECTION(inch)

MAXIMUMSHEAR

(lbs)

PILE HEADDEFLECTION

(inch)

MAXIMUMSHEAR

(lbs)0.01 1124 0.01 25810.1 11211 0.1 211250.2 19313 0.2 386970.3 25723 0.3 547740.5 40479 0.5 860200.75 55393 0.75 110839

1 68911 1 124021Notes:

· Full reinforced pile.· Pile length of 29 feet.

5.4.4 Lateral Capacity - Pile CapAdditional resistance to lateral loads for pile foundation system may be provided by passive resistance against the sides of pile caps and grade beams. The passive resistance on the side walls of the pile caps and grade beams can also be used in accordance with the recommended passive pressure provided in Section 5.7.2.

Deep Foundation Design - New Piles

The proposed structural addition may also be supported on deep cast-in-drilled-hole (CIDH) foundation system. To account for the uncertainty associated with undocumented fill and the potential time-dependent relative pile-fill settlement, skin friction within the fill (both undocumented and proposed new fill) is ignored for pile axial resistance. The CIDH deep foundation design recommendations are presented below:

5.5.1 Axial CapacityAxial capacities were evaluated for 18-inch and 24-inch diameter CIDH piles. Ultimate axial capacities were calculated using computer program SHAFT 2012 (Ensoft Inc., 2012). End bearing capacity is neglected in the calculation to eliminate pile load test for verification of end bearing capacity. The sample results are presented in Table 12 and the full design chart is provided in Figure 8. Detailed calculation is

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included in Appendix G. For pile center-to-center spacing more than 3-pile diameters, group efficiency reduction is not required.

TABLE 12 - SUMMARY OF CIDH PILE AXIAL CAPACITY

LOCATION PILE TYPEMINIMUM PILE

LENGTH(feet)

ULTIMATECOMPRESSION

CAPACITY(kips)

UPLIFT(kips)

New Support

CIDH Pile(18-inch diameter)

40 109 7650 166 116

CIDH Pile(24-inch diameter)

40 146 10250 211 147

Notes:· Support pile cutoff elevation at 87 feet MSL.· Skin friction above elevation 64 feet MSL was ignored.· A factor of safety of 2.0 can be used to calculate the allowable capacities for static condition.· A factor of safety of 1.5 can be used to calculate the allowable capacities for seismic condition.· Minimum pile length: 40

5.5.2 SettlementThe settlement of the deep foundations designed and constructed in accordance with the recommendations provided, was estimated to be less than ½-inch under the static loading conditions. Most of this settlement should occur shortly after application of the structural loads. Differential settlement between the pile supports was estimated to be less than ¼-inch.

5.5.3 Pile Downdrag ConsiderationPile downdrag occurs when pile’s surrounding subsurface soil compresses relative to pile, causing a negative skin friction. This compression or settlement can be caused by consolidations, dry-sand settlement, or liquefaction. Based on the analysis from Section 4.3.3, seismically-induced settlement has negligible effects on pile downdrag forces, thus we consider pile downdrag effects to be minimal.

5.5.4 Lateral CapacityLateral load pile analysis was evaluated using the computer program LPILE 2013 (Ensoft Inc., 2013). The lateral capacities of CIDH piles were estimated using soil resistance-pile deflection models (p-y analyses) for sands, clays, and silts.

A range of typical acceptable horizontal top-of-pile (cut-off) deflections of ¼-, ½-, and 1-inch were used to estimate the lateral pile capacity. The analysis assumed a pile length of 35 feet for both 18- and 24-inch CIDH and the top-of-pile is 3.5 feet below the proposed finished grade. Lateral load evaluations were performed for pinned- and fixed-head conditions for the proposed CIDH piles and the piles were modeled using 50 percent of the gross moment of inertia as the piles may crack. A factor of safety has not been applied to the estimated loads or deflections. If the minimum center-to-center spacing between the piles is less than six pile diameters, a group efficiency reduction should be applied. Group efficiency factors of 0.5 and 1.0 may be considered for pile center-to-center spacing of 3 and 6 pile diameters, respectively. For other pile center-to-center spacing, group efficiency factor can be estimated based on linear interpolation of the given factors above. Summaries of the results of laterally-loaded pile capacities are presented in Table 13 and Appendix H.

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TABLE 13 - SUMMARY OF CIDH PILE LATERAL CAPACITY

LOCATION PILE TYPE PILE HEADCONNECTION

PILE HEADDISPLACE-

MENT(inches)

AXIALLOAD1

(kips)

ULTIMATELATERALCAPACITY

(kips)

MAX.MOMENT

(kips-inches)/Depth (feet)

MAX. SHEAR(kips)/

Depth (feet)

New Support

CIDH Pile(18-inchdiameter)

Pinned-headcondition

0.25 250 10 671 \ 7.2 10 \ 00.5 250 19 1294 \ 7.2 19 \ 00.75 250 26 1696 \ 7.2 26 \ 0

Fixed-headcondition

0.25 250 24 -1807 \ 0 24 \ 00.5 250 43 -2816 \ 0 43 \ 00.75 250 58 -3585 \ 0 58 \ 0

CIDH Pile(24-inchdiameter)

Pinned-headcondition

0.25 250 5 306 \ 9.2 5 \ 00.5 250 11 610 \ 9.2 11 \ 00.75 250 15 853 \ 8.8 15 \ 0

Fixed-headcondition

0.25 250 15 -884 \ 0 15 \ 00.5 250 24 -1264 \ 0 24 \ 00.75 250 30 -1284 \ 0 30 \ 0

Notes:· Pile cutoff elevation at 87 feet MSL· Minimum pile length of 35 feet, for both 24-inch, 30-inch, and 36-inch CIDH piles, was assumed for the lateral pile analyses.1. Axial loads insensitive to lateral capacities for fully embedded piles.

5.5.5 Lateral Capacity - Pile Cap/Grade BeamIn addition to the lateral resistance provided by the vertical piles discussed in Section 5.5.4, the passive resistance on the side walls of the pile caps and grade beams can also be used in accordance with the recommended passive pressure provided in Section 5.7.2. Sleeve piles will provide zero lateral capacity and lateral capacity will rely on local passive resistance from the pile cap or grade beam. Local passive resistance may load the surrounding end retaining walls. The configuration of the final building detail was not available at the time of this report and additional analysis may be required to evaluate the additional lateral loading.

5.5.6 Sleeved PileDue to the existing underground utilities and , there may be piles required to be placed in oversized sleeves to avoid surcharging to the adjacent settlement- and/or stress-sensitive utilities or other subsurface structures if minimum setback of 5 pile diameters to the face of subsurface structure cannot be met, or the construction sequence leads to completion of piling prior to the adjacent fill placement. Piles installed in proposed lightweight fill, such as Geofoam, must be placed in oversized sleeves to avoid damaging the lightweight fill.

Such sleeved pile should be designed within an oversized sleeve, which has a minimum 2 inches clearance from the pile perimeter and extends one foot below the bottom of adjacent subsurface structures. The actual sleeve should be structurally designed to be able to resist the earth pressure under restrained condition shown in Figure 7. Sleeve piles will provide zero lateral capacity must rely on passive resistance recommended in Section 5.5.5.

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Micropile

Based on our understanding of the Project, battered micropiles in groups are judged the most feasible foundation alternative, which can provide both compression and tension resistance to carry the gravity loads, provide the lateral resistance to resist the seismic loading and to provide the means of transferring such loads to a deeper zone so as to avoid surcharging the existing retaining/basement walls. The proposed micropile is a structural elements that usually consists of a form of steel reinforcement (any types of steel bars and/or tendons) inside grouted drilled holes, and can be installed with smaller equipment in many different types of ground with design loads as small as three tons to as high as 500 tons, depending on installation methods. The installation usually involves gravity grouting, jet grouting, post-grouting, or pressure grouting techniques. The micropiles may be installed in 8-inch to 12-inch diameter holes. Load is mainly (and initially) resisted by the strength of the steel and transferred via the grout to the surrounding soil by high values of interfacial friction with minimal or no end bearing component. The proposed pads will be acting as structural slabs to be supported by micropiles.

5.6.1 Axial CapacityOur recommendations for the micropiles are based on the procedures outlined in the Federal Highway Administration’s (FHWA) Geotechnical Engineering Circular No. 4, Ground anchors and Anchored Systems (FHWA-IF-99-015; FHWA, 1999). Generally, the micropiles are initially installed with a casing throughout its entire length with additional grout injected under gravity or pressure after the primary grout has been tremied as the casing is being withdrawn to a designated length below the ground surface, therefore leaving a permanent casing in the upper zone of the micropile. The lower portion of the micropile without casing, where the grout contacts the surrounding soil is referred to as the bonded length, and the upper portion where the grout is still within the casing is referred to as the un-bonded length, or free length.

For the gravity grouted micropile, ultimate bond strength of 25 pounds per square inch (psi) may be considered for the geotechnical capacities of the system. For post-grouted/pressure grouted micropiles, the aforementioned ultimate bond strength may be increased by another 100 to 150 percent based on field verification. A minimum casing length of 5 feet embedded into the bonded length is required.

If post-grouted/pressure grouted micropiles are considered, the grouting pressure should be adjusted based on the actual monitoring data during installation and should not be greater than 150 psi. Port grout should be injected using adjustable sleeve-port grouting pipes to prevent hydro fracturing. The free length (unbounded) portion outside the upper casing of the micropiles should be backfilled using a lean sand/cement mix. The cased/unbonded portion of the micropiles should be extended to elevation 62 feet MSL; therefore, the grouted micropiles will be installed completely below the bottom of potentially liquefiable layers and . With the cased length well below the adjacent structures, impact due to surcharge from the proposed loads is considered remote. It should be noted that the design engineer retained by specialty micropiles contractor is responsible for the final design, which needs to be submitted for review prior to installation of non-production micropile(s). The installation should also be adjusted accordingly based on actual micropiles performance and ease of construction.

For micropiles installed with center-to-center spacing of at least 3 times their grout diameters, or 5 feet, whichever is greater, no group reduction in uplift capacity is necessary. However, for micropiles with spacing of 2.5 times their grout diameters, a reduction factor of 0.7 should be applied to uplift or download capacity to account for group effects.

In addition, minimum critical edge of 8 times diameter of drilled hole (8d) and 16d for critical spacing for the steel/grout bond failure mode may be considered for the micropile design. For the grout/concrete bond failure mode, the minimum critical edge and critical spacing may be reduced to 5d and 10d, respectively.

A resisting factor of 0.70 for both geotechnical tension and compression resistance should be considered for load and resisting factor design (LRFD) under the strength limit state for axially loaded micropiles,

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provided static load tests to be performed to field verify the design capacities. For extreme limit states, the resisting factor can be 1.0. If allowable stress design (ASD) is considered, a minimum factor of safety (FS) of 2.0 should be considered for both compression and tension load conditions.

The micropile should be installed by a qualified contractor who has prior experience in constructing such system of similar size under similar soil conditions.

Micropiles capacity is generally more realistically evaluated from load tests in the field, as the actual capacity depends on various site-specific, equipment- and method-related factors. Consequently, load tests should be part of the project specifications, and the load tests should be performed under the observation of the GEOR.

5.6.2 Lateral CapacityTo minimize any potential surcharge and induced stress transfer to the existing adjacent walls, minimal lateral resistance is anticipated for the cased portion of the proposed micropile. Instead, horizontal resistance will provided be provided based on horizontal component of axial resistance. To minimize the potential adverse impact due to the stiff response of battered micropiles, high inclination (i.e., 35 to 45 degrees with respect to horizontal) may be considered for soften response to minimize puncture failure between micropile and structural slab.

In addition to micropile horizontal resistance, passive resistance as shown on Figure 7 may be considered in east-west direction when the existing retaining walls are away (i.e., twice the wall retained height or greater).

A FS of at least 1.5 should be considered for ASD. For LRFD, resisting factors of 0.7 and 0.5 may be considered for horizontal component of miropile axial resistance and passive earth pressure, respectively, under the strength limit state. For service or extreme limit states, the resisting factor can be 1.0.

Retaining Structure

The proposed retaining wall along south end of building may be over 5 feet in which case should be supported on piles due to lateral loading combination from the earth pressure and proposed building. However, the elevation and height of the wall was not available at the time of this report and additional analysis may be required.

5.7.1 Bearing CapacityFor the proposed onsite retaining walls less than 5 feet tall where the foundations are founded on compacted/engineered fill placed in accordance with Section 5.2, an allowable bearing pressure of 2,500 pounds per square foot (psf) can be considered with a minimum dimension of 2 feet wide and a minimum embedment depth of 2 feet below the lowest adjacent grade. The recommended bearing pressure can be increased by 20 percent with each additional foot of width or depth, to a maximum value of 4,000 psf. The bearing pressure applies to dead plus live loads and includes a calculated factor of safety of at least 3. The allowable bearing pressure values may be increased by one-third for short-term loading due to wind or seismic forces. The edge pressure of any eccentrically loaded footing should not exceed the allowable bearing value.

5.7.2 Earth PressureMiscellaneous retaining walls should be design based on the earth pressure recommendations of cantilever walls shown in Figure 7. The recommended active earth pressures are based on the requirement of using select backfill behind the retaining wall as stipulated on Figure 7. Lateral pressures resulting from traffic behind the wall should be added as a uniform horizontal pressure of 100 psf along upper 10 feet of the wall. Surcharges that are setback distance behind the wall a horizontal distance greater than the exposed wall

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height do not need to be added to the design pressure. Sliding friction coefficient are summarized on Figure 7.

5.7.3 Wall DrainageAdequate drainage should be provided behind basement and retaining walls, and collector pipes should be installed at the base of the walls to drain the collected water. Retaining wall backdrains should consist of Caltrans Class 2 permeable material at least 18-inches wide that is placed behind the entire wall from three inches below the collector pipe to within 18 inches of the ground surface. The upper 18 inches should be backfilled with a comparatively impermeable material (such as silty or clayey materials) so that the permeable material is protected from direct surface water infiltration. As an alternative to the Caltrans Class 2 permeable material, a geocomposite material (drain plus filter fabric) may be used against the wall.

Floor Slab

Slab-on-grade should be supported on engineered fill placed in accordance with Section 5.2.3. For design of slabs, and for estimating their deflections, a modulus of subgrade reaction (k) of 150 pounds per square inch per inch of deflection (pci) may be used.

Slabs-on-grade should be underlain by a minimum of 6 inches of compacted free-draining granular materials. The free-draining granular material should contain less than 5 percent fines (passing the No. 200 sieve) and should be placed below the moisture vapor barrier.

Moisture vapor will tend to migrate through the slab-on-grade for sensitive flooring. To reduce vapor migration through the building floor/slab, the following is required:

· Minimum 10-mm-thick plastic vapor barrier with joints overlapped by at least 6 inches and taped.

· Sealing the plastic vapor barrier around plumbing, electrical, and other conducts.

· No sand above the plastic vapor barrier.

· Minimum 7-day wet cure with no curing compounds.

· Two-month drying period before floor coverings are placed.

· Concrete mix design, materials, placement, curing, and finishing in conformance with the Greenbook and the American Concrete Institute (ACI; 1996, 1997).

The plastic vapor barrier should satisfy the requirements of American Society for Testing and Materials (ASTM) E 1745 (Class “A”). ACI 302.1R-96 defines a vapor barrier as having a water vapor transmission rate (WVTR) of 0.00, plus a testing tolerance generally of a WVTR of 0.008 or less when tested in accordance with ASTM E 96. Note that commonly used “poly” or "visqueen” does not meet ASTM E 1745 requirements. Vapor barriers should be installed in accordance with ASTM E 1643. Care should be taken to seal the plastic vapor barrier and avoid puncturing the plastic vapor barrier during construction.

The floor slab are founded on compacted/engineered fill placed in accordance with Section 5.2.3, an allowable bearing pressure of 1,000 pounds per square foot (psf) can be considered at the current elevation of the existing mat foundation (approximately Elev. 81 feet). The bearing pressure applies to dead plus live loads and includes a calculated factor of safety of at least 3. The allowable bearing pressure values may be increased by one-third for short-term loading due to wind or seismic forces.

The recommended bearing pressure shall be reduced by 125 psf per foot of fill for soil, 45 psf per foot of fill for lightweight fill, or 90 psf per foot of fill for slurry above the existing foundation

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Concrete Flatwork

Concrete flatwork/hardscape should be supported on compacted/engineered fill placed in accordance with Section 5.2.3. For design of concrete flatwork, and for estimating their deflections, k of 150 pci may be used.

Site Drainage

Site drainage of surface storm water should be provided for during and after construction. The grading plans should account for any alterations in existing surface drainage. During construction, provisions should be made to divert surface water away from open excavations. Any water that collects in open excavations should be pumped out to avoid softening of foundation soils.

It is recommended that the final ground surface around the proposed structures be graded to a slope of at least 2 percent for minimum 10 feet to provide positive drainage away from the structures and existing retaining wall. In cases where this is not feasible, adequate measures should be provided to collect and drain storm water around the structures.

Low Impact Development Mitigation Measure

Based on the field infiltration tests within the near-surface soils, the site is judged not feasible for infiltration for the storm water improvement/best management practices (BMP) design due to a low unfactored infiltration rate of 0.3 inch per hour with associated reduction factors (i.e., RFt of 2; RFv of 2; and RFs of 1 to 2). In addition, due to presence of the existing underground fuel tanks located immediately south of the proposed improvement, as well as the undocumented fills toward the north, infiltration based measure should be avoided. Instead, other measure such as capture and reuse, should be considered for LID design.

Utilities

Utility trenches (either open or backfilled) that parallel structures, pavement, or flatwork should be planned so that they do not extend below a plane with a downward slope of 1H:1V from the bottom edge of footings, pavement, or flatwork. Otherwise, temporary shoring to provide footing, pavement, flatwork, or utility support is recommended unless localized settlements on the order of 1 percent of the trench depth can be tolerated. All excavations should comply with appropriate safety standards outlined in Section 5.2.5.

Utility pipes should be placed on the bottom of a neatly cut trench on a layer of bedding according to the manufacturer's recommendations. Jetting should not be allowed for compaction purposes. We anticipate that the near-surface soils will not be suitable for use as bedding materials.

For pipeline design purposes, the vertical pressure on a pipe can be estimated based on Figure 9. A modulus of soil reaction value of 500 pounds per square inch (psi) may be used for design. The allowable design soil bearing value for associated lightly loaded structures such as manholes is 500 psf for footing with a minimum embedment and width of 1 foot.

Corrosivity

Selected test were conducted on representative soil samples to evaluate if special precautions or considerations should be made with respect to materials in contact with soils. Specifically, the soil sample was tested to assess corrosivity parameters, which include pH, resistivity, sulfate and chloride content. The test results are summarized in Table 14.

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TABLE 14 – CORROSION POTENTIAL

Boring Location and

DepthMaterial pH

Minimum Resistivity (Ohm-cm)

Sulfate Content (ppm)

Chloride Content (mg/L)

B-18-L1 @ 0-5’ Silty SAND 8.3 1,169 294 55

B-18-L2 @ 0-5’ Silty SAND 9.1 3,515 51 37

The test result for pH, which indicates the degree of alkalinity or acidity of an on-site soil, of the bulk sample is between 8.3 and 9.1.

A commonly accepted correlation between electrical resistivity and corrosivity potential for ferrous metals is as the following:

Below 1,000 ohm-cm - Severely corrosive1,000 to 2,000 ohm-cm - Corrosive2,000 to 10,000 ohm-cm - Moderately corrosiveOver 10,000 ohm-cm - Mildly corrosive

The minimum resistivity test result indicates that the surface soil may be corrosive to moderately corrosive to metals.

The current 2016 CBC stipulates that corrosion potential to the foundation element is to be evaluated in accordance with the design procedure following American Concrete Institute (ACI) 318 (ACI, 2014). Based on the test results of corrosion potential, the site is classified as exposure class F0, S1, W0, and C1 using ACI 318 Table 19.3.1.1. Accordingly, the concrete mixture may be designed per ACI 318 Table 19.3.1.1. In addition, a minimum concrete cover of 3 inches should be maintained to provide reinforcement protection in accordance with ACI 318, Section 7.7.1.

County Building Code Section 111 Statement

Based on the findings of this geotechnical investigation, and provided that the recommendations of this report are followed, and the designs and construction are properly and adequately executed, it is our opinion that the proposed construction work within the project site will be safe from landslides, slippage, or settlement. Further, it is our opinion that the proposed construction will not adversely affect the stability of the adjacent properties, with the same provisions listed above.

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Section 6 Construction ConsiderationsExcavation

The project site is primarily underlain by loose to medium dense sand and soft to very stiff clay or silt. Caving should be anticipated in sandy soil layers when drilling CIDH piles or performing other temporary excavations. Proper equipment should be selected for such subsurface materials.

Groundwater

Based on the findings of our field exploration and the available information on groundwater conditions, groundwater could be encountered during construction. Caving should be anticipated with the onsite sandy soil in combination with groundwater. Groundwater level can be as high as 15 feet bgs during construction. Groundwater conditions may change due to various factors such as rainfalls in the area.

CIDH Installation

Steel reinforcement and concrete should be placed after completion of the drilling of each CIDH pile. Pile excavations should not be allowed to stand open overnight. A minimum of 15 hours should be allowed between concrete placement in one shaft before drilling an adjacent shaft within 5 diameters center-to-center. Loose soils and water (if any) at the bottom of the drilled holes should be removed. All drilled pier construction should be performed in accordance with ACI 336.1-91, "Standard Specifications for Construction of Drilled Piers." The shaft borings bottom should be inspected and approved by the Resident Engineer prior to installation of reinforcement.

The contractor should be made aware of the presence of static groundwater at a depth of approximately 40 to 50 feet below the existing grade. It may be necessary to place concrete in water by tremmieing if the pile tips are below this depth. In addition, local ravelling of the boring walls in the sandy stratum may be experienced during pile installation. Use of special installation techniques may be warranted to prevent caving of the soils, and to facilitate advancing the hole to the design depths. To ensure a proper execution during construction, the geotechnical engineer should review the pile installation method proposed by the contractor.

When permanent steel shells are used, the steel shell should be driven in-place using impact hammers, and the GEOR should be contacted for considering the need for a reduction in the given axial capacities. If the casing would be retrieved in accordance with Caltrans Standard Specifications and Special Provisions, its impact on capacities can be neglected. Casing must be removed after placement of concrete to allow mobilization of the estimated skin friction capacity.

Based on the analytical tests performed on the selected soil samples, attention should be directed to the conditions of soil cuttings and water generated in excavation and drilling for the piles. If contamination is encountered in soil cuttings, the excavated soils and groundwater should be removed and disposed of properly in accordance with appropriate environmental protocols.

Micropile Installation

The Contractor should select drilling methods to establish a stable hole. Special care should be exercised in the selection of drilling method when excessive loss of ground may impact the adjacent foundations. The Contractor may use a temporary casing or slurry to stabilize the hole. However, there is a possibility that the excessive use of bentonite or other clay-based drilling fluid may negatively affect the bond strength of grout.

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Grout may be neat cement grout or contain sand. The on-site material should not be used for any grouting purposes. All materials used for grouting and the drill hole backfill should comply with the manufacturer’s recommendations.

Stressing and testing are required for every micropile to stress and lock-off the micropile at its design load. The lock-off load will be same as the unfactored micropile design load. The Contractor is responsible for selecting the equipment and procedures to stress the micropiles. Stressing must begin after the grout has reached adequate strength. All production micropiles should be tested in accordance with Caltrans Specification Section 46-2.01.D(2).

It is recommended that all production micropiles be proof tested to 80% of the ultimate tensile capacity, and at least 2 percent of production micropile should be performance tested with cyclic loading schedule. The location of the performance test micropiles will be determined by a qualified engineer in the field. All failing micropiles should be replaced and bond length or have design load capacities reduced. Modification to the anchor design and/or additional load tests may be required depending on the results of the load testing program.

It is recommended that a geotechnical professional observe and record the installation of the anchors to verify the assumed soil and geologic conditions. It is also recommended that a geotechnical professional observe and record the testing and lock-off of the anchors.

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Section 7 Design ReviewThe geotechnical aspects of the Project should be reviewed by the GEOR during the design process. The scope of services may include:

· Assisting the design team in providing specific recommendations for special cases;· Reviewing the design grading plan to ensure that all geotechnical recommendations contained in

this report have been included in the design;· Reviewing foundation design drawings;· Reviewing the geotechnical portions of the Project for possible cost savings through alternative

approaches;· Reviewing the proposed construction techniques to evaluate if they satisfy the intent of the

recommendations presented in this report.

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Section 8 Construction MonitoringAs a necessary requisite to the proper use of this report, the following should be monitored by a qualified engineer/engineering geologist/technician under the supervision of the GEOR:

· Site preparation including site stripping, removal of subsurface structures, and bottom observation;· Temporary excavation and overexcavation;· All foundation excavations and subgrade preparation;· Placement of all engineered fills and backfills; · CIDH pile construction; and· Installation of the shoring system, if applicable.

To capture any impact on adjacent properties due to the proposed construction activities, some means of monitoring the performance of the shoring system is recommended. If any sign of excessive deformation is observed, immediate action should be taken to correct potential issues occurred, before proceeding further excavation operation.

The GEOR should be notified at least two days in advance of the start of construction. A joint meeting between the contractor and the GEOR is recommended prior to the start of construction to discuss specific procedures and scheduling.

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Section 9 References1) American Concrete Institute, 2011, ACI 318-11, Building Code Requirements for Structure Concrete

and Commentary.

2) American Society for Testing and Materials (ASTM), 1999. Annual Book of ASTM Standards, Section 4 - Construction, Volume 4.08, Soil and Rock (I): D 420 - D 4914, West Conshohocken, PA.

3) Bartlett, S.F. and T. Leslie Youd, "Liquefaction-Induced Lateral Ground Displacement" (April 2, 1995). International Conferences on Recent Advances in Geotechnical Earthquake Engineering and Soil Dynamics. Paper 3.

4) Building News, 2009, “Greenbook,” Standard Specifications for Public Works Construction.

5) California Building Code (CBC), 2016. Title 24, Volume 2, California Building Standards Commission.

6) California Department of Transportation (Caltrans), 2017, Standard Specifications Retaining Wall Type 1 RSP B3-1A.

7) California Department of Transportation, 2012, Corrosion Guidelines, Version 2.0.

8) California Division of Oil, Gas and Geothermal Resources (DOGGR), District 1, Map 117, http://www.conservation.ca.gov/dog/pages/index.aspx.

9) California Department of Transportation (Caltrans), 2010, Standard Specifications.

10) California Department of Water Resources, 2004, Updated 2016, California’s groundwater Bulletin 118 – Coastal Plain of Los Angeles Groundwater Basin, South Basin, http://www.water.ca.gov/pubs/groundwater/bulletin_118/basindescriptions/4-11.03.pdf.

11) California Division of Oil, Gas and Geothermal Resources (DOGGR), http://www.conservation.ca.gov/dog/pages/index.aspx.

12) California Geological Survey (CGS) Seismic Hazard Analysis Website (http://wwwconsrv.ca.gov/cgs/rghm/pshamap/pshamap.asp).

13) CGS, 1994. Fault Activity Map of California and Adjacent Areas, with Locations and Ages of Recent Volcanic Eruptions, Compiled by Jennings, C.W, Geologic Data Map No. 6, Scale 1:750,000.

14) CGS, 1994, Fault Rupture Hazard Zones in California, Special Publication No. 42.

15) CGS, 2001, Alquist-Priolo Earthquake Fault Zone (APEFZ) maps, Geographic Information System data files.

16) CGS, 2008, Special Publication 117A, Guidelines for Evaluating and Mitigating Seismic Hazards in California.

17) Caterpillar Performance Handbook, 2004, Caterpillar, Inc., Edition 35.

18) Department of Conservation, State of California, USGS San Diego County Tsunami Inundation Map, (Inundation & Tsunami Hazard Areas), 2009.

19) Ensoft, Inc., 2012, Computer Program SHAFT v2012.

20) Ensoft, Inc., 2012, Computer Program LPILE v2013.

21) Field, E.H., Biasi, G.P., Bird, P., Dawson, T.E., Felzer, K.R., Jackson, D.D., Johnson, K.M., Jordan, T.H., Madden, C., Michael, A.J., Milner, K.R., Page, M.T., Parsons, T., Powers, P.M., Shaw, B.E., Thatcher, W.R., Weldon, R.J., II, and Zeng, Y., 2013. Uniform California earthquake rupture forecast, version 3 (UCERF3) The time-independent model: U.S. Geological Survey Open-File Report 2013–1165, 97 p., California Geological Survey Special Report 228, and Southern California Earthquake Center Publication 1792, http://pubs.usgs.gov/of/2013/1165/.

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22) Lindvall, S.C., and Rockwell, T.K. (1995), Holocene Activity o f t h e Rose Canyon Fault Zone in San Diego, California: Journal of Geophysical Research, V o l . 100, No. B12, pp. 24,124-24,132.

23) Miller, C.D., 1989, Potential hazards from future volcanic eruptions in California: U.S. Geological Survey Bulletin 1847, 17 p., 2 tables, plate 1, scale 1:500,000.

24) Rockwell, T., Bergmann, M., and Kenney, M., 2000, Holocene slip rate of the Elsinore fault in Temecula Valley, Riverside County, California. In Geology and Enology of the Temecula Valley (B. Birnbaum and K. Cato, eds), p. 105-118.

25) Rockwell, Thomas, Henyey, Thomas, and Forrest, Michael, 1997, The Palos Verdes Fault field trip guide: Southern California Faults, Shattered Crust Series, Southern California Earthquake Center, 54 p.

26) Forrest, M.R., Rockwell, T.K., Grant, L., and Gath, E., 1996, Whittier-Elsinore Newport-Inglewood Faultbook, Southern California Faults, Shattered Crust Series, No. 1, Southern California Earthquake Center, July, 1996.

27) Rockwell, Thomas K., Lindvall, Scott C., Haraden, Colleen C., Hirabayashi, C. Kenji, and Baker, Elizabeth, 1991, Minimum Holocene slip rate for the Rose Canyon fault in San Diego, California: in (Abbott, P.L., ed.) Environmental Perils, San Diego Region: for the Annual Meeting of the Geological Society of America, San Diego Association of Geologists, p. 37-46.

28) Rockwell, T.K., McElwain, R.S., Millman, D.E. and Lamar, D.L., l986, Recurrent late Holocene faulting on the Glen Ivy North strand of the Elsinore fault at Glen Ivy Marsh: in Guidebook and Volume on Neotectonics and Faulting in Southern California (P. Ehlig, ed.), Cordilleran Section, Geological Society of America, p. 167-176.

29) Rockwell, T.K. and Pinault, C.T., l986, Holocene slip events on the southern Elsinore fault, Coyote Mountains, southern Californai: in Guidebook and Volume on Neotectonics and Faulting in Southern California (P. Ehlig, ed.), Cordilleran Section, Geological Society of America, p. 193-196.

30) State of California Water Resources Control Board (SWRCB), GeoTracker.

31) Special Publication 117A, Guidelines for Evaluating and Mitigating Seismic Hazards in California.

32) United States Geological Survey, 2013, Earthquake Ground Motion Tool computer program.

33) Yerkes, R.F. and Campbell, R.H., 2005 Preliminary Geologic Map of the Los Angeles 30' x 60' Quadrangle, Southern California, U.S. Geological Survey Open-File Report 2005-1019, Scale 1:100,000CGS, 2008, Special Publication 117A, Guidelines for Evaluating and Mitigating Seismic Hazards in California.

34) Wesnousky, S.G. (1986), Earthquakes, Quaternary Faults, and Seismic Hazards in California,

Final Geotechnical Engineering Investigation ReportClinical Lab and Red-Bag Storage AreaMartin Luther King Jr. Medical Campus

Willowbrook, CaliforniaMay 30, 2019

10-1

Section 10 Uncertainties and LimitationsAECOM has observed only a very small portion of the pertinent subsurface conditions. The recommendations presented herein are based on the assumption that the soil and geologic conditions do not deviate appreciably from those found during our investigation.

We recommend that AECOM/the GEOR review the design plans to verify that the intent of the recommendations presented herein has been properly interpreted and incorporated into the contract documents. We further recommend that geotechnically-relevant construction be observed by a qualified Geotechnical Engineer or Engineering Geologist to evaluate if the site conditions encountered are as anticipated, or to provide revised recommendations, if necessary. If variations or undesirable geotechnical conditions are encountered during construction, a Geotechnical Engineer should be consulted for further recommendations.

Geotechnical engineering and the geologic sciences are characterized by uncertainty. Professional judgments presented herein are based partly on our understanding of the proposed construction, and partly on our general experience. Our engineering work and judgments rendered meet current professional standards; we do not guarantee the performance of the Project in any respect.

- o0o -

It has been a pleasure to assist you with this Project. We look forward to being of further assistance as construction begins. Should you have any questions regarding this report, please contact us.

Very truly yours,

Dennis H. Nguyen, P.E. Joseph P. Gratzer, P.G., C.E.G.Staff Geotechnical Engineer Senior Geologist

Reviewed by:

S. Neville Su, P.E., G.E. Chi-Hung Lay, P.E., G.E.Project Manager Principal Engineer

FIGURES

Geotechnical Engineering InvestigationMartin Luther King Jr. Medical Campus: DHS Regional Lab & Red Bag Storage

VICINITY MAPDHS Regional Lab & Red Bag StorageMartin Luther King Jr. Medical Campus

Willowbrook, California

Figure 1

Martin Luther King Jr. Medical Campus

AECOM Geotechnical Boring

AECOM CPT SoundingNGEOTECHNICAL INVESTIGATION PLOT PLAN

DHS Regional Lab & Red Bag StorageMartin Luther King Jr. Medical Campus

Willowbrook, California

Figure 2

C-09-14B-18-L2

C-18-L3

B-18-L1

A

A′

B-16-M1

Geotechnical Engineering InvestigationMartin Luther King Jr. Medical Campus: DHS Regional Lab & Red Bag Storage

Building New Lab Building Footprint

New Hazardous Waste Yard Footprint

Geotechnical Engineering InvestigationMartin Luther King Jr. Medical Campus: DHS Regional Lab & Red Bag Storage

REGIONAL GEOLOGIC MAPDHS Regional Lab & Red Bag StorageMartin Luther King Jr. Medical Campus

Willowbrook, California

Figure 3

Martin Luther King Jr. Medical Campus

LegendQoa Older AlluviumQya1, Qya2 Younger Alluvium

REGIONAL FAULTDHS Regional Lab & Red Bag StorageMartin Luther King Jr. Medical Campus

Willowbrook, California

Figure 4

LegendInferred Geology?

Geotechnical Engineering InvestigationMartin Luther King Jr. Medical Campus: DHS Regional Lab & Red Bag Storage

Geotechnical Engineering Investigation

Martin Luther King Jr. Medical Campus

CROSS - SECTION A-A'

DHS Regional Lab & Red Bag Storage

Martin Luther King Jr. Medical Campus

Willowbrook, California

LEGEND

Measured Ground Water Level

Fill: Silty Sand

Alluvium: Poorly-graded Sand with Silt

Alluvium: Silt, Clayey Sand, Silty Sand

Alluvium: Poorly-graded Sand, Silty Sand

Alluvium: Silt

Alluvium: Silty Sand, Poorly-graded Sand

?

?

?

?

?

?

?

?

?

?

?

?

?

?

?

?

?

?

?

?

?

?

?

Well-graded Sand

New Lab BuildingHazardous Waste Yard

existing surface

Inferred Geologic Contact?

Figure 5

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FIGURES

PP = 300 H2<3,000 psf BRACED SHORING P = Pq + Ps

= 0.44 q + 53 H1

(300 psf minimum)

CANTILEVER SHORING P = Pq + Ps

= 0.28 q + 31 H3

Notes:· All values of height (H) in feet, and pressure (P) and surcharge (q) in pounds per square foot (psf).· Values for temporary excavations using flexible walls.· For traffic surcharge, assume no less than a 100 psf uniform horizontal pressure along the top 10 feet.· Earth pressure assumes no hydrostatic pressures. If hydrostatic pressures are allowed to build up, the

incremental earth pressures below groundwater level should be reduced by 50 percent and added tohydrostatic pressure for total lateral pressure.

FIGURE 6 - LATERAL EARTH PRESSURES FOR TEMPORARY SHORING

BRACEDSHORING

q (Surcharge)

Pp

H1

H2P

qP sP

q (Surcharge)

sPq P

CANTILEVERSHORING

3H

FIGURES

3

Drainage Backfill

oa,q P Pp

q (Surcharge)

FeWeep Drain

m

1

1

2

H

H

P

P

0.5H

P

H2H

11

SelectBackfill

Pp = 300 H2 £3,000 psf Cantilever Walls Restrained Wallsµ = 0.40 (Select Backfill) P = Pa + Pq = 31H3 + 0.28q P = Po + Pq = 53H3 + 0.44qµ = 0.55 (Lightweight fill)µ = 0.25 (Slurry fill) Fe = 15H12 Fe = 29H12

Notes:· Select backfill for pressure behind the wall; import sandy fill for passive resistance.· All values of height (H) in feet, pressure (P), and surcharge (q) in pounds per square foot (psf) and force

(F) in pounds.· Pp, Pa, and Po are the passive, active, and at-rest earth pressures, respectively; Fe is the ultimate

incremental seismic force. · Pq is the incremental surcharge pressure; µ is the allowable friction coefficient applied to dead normal

(buoyant) loads. Fe is in addition to the active and at-rest pressures. Below groundwater, active and at-rest pressure should be reduced by 50 percent and hydrostatic pressure should be added to active and at-rest pressures. Pp should be reduced by 50 percent below the groundwater.

· Adjacent bearing pressure should be considered as a surcharge, which applies at the bottom of footing.· For 2H:1V slopes above the wall, increase the active and at-rest pressures by 50 percent; for 1.5H:1V

slope, increase the active and at-rest pressures by 100 percent. · For 5H:1V slopes below the toe of the retaining wall, decrease the passive pressures by 25 percent; for

3H:1V slope, decrease the passive pressures by 50 percent.· Neglect the upper 1 foot for passive pressure unless the surface is contained by a pavement or slab.· Friction and passive resistance may be used in combination, if the passive resistance is reduced by one-

half.· A factor of safety of 1.5 should be considered for ASD.· If proposed pile applies additional lateral loading, additional analysis may be required

FIGURE 7 - LATERAL EARTH PRESSURES

FIGURES

Notes:

1. Assuming pile cutoff elevation approximately at 87 feet MSL, respectively,2. End Bearing ignored.3. Minimum factors of safety of 2.0 and 1.3 for static and seismic loading conditions, respectively.

FIGURE 8 – AXIAL PILE CAPACITY; NEW PILES

0

10

20

30

40

50

60

0 50 100 150 200 250

Pile

Len

gth

(ft)

Ultimate Compression Capacity (kips)

18-inch compression skin friction

18-inch uplift skin friction

24-inch compression skin friction

24-inch uplift skin friction

FIGURES

2b

HC

P=C (YH+Q )

0

0.1

0.2

0.3

0.4

0.5

0.5 1.0 1.5 2.0 2.50

BOU

SSIN

ESQ

CO

EFFI

CIE

NT

C b

H

r

Q

r/H

p

Notes:· P = Vertical soil pressure at the top of the conduit (pounds per square foot [psf]).· Cp = Concentration factor, assume 1.5.· Y = Unit weight of soil (pounds per cubic foot [pcf]), assume 125 pcf.· H = Height of fill above the top of the pipe (feet).· Q = Concentrated surface load (pounds).· Cb = Boussinesq coefficient obtained from figure above.· The effects of more than one load are cumulative.

FIGURE 9 - VERTICAL EARTH PRESSURES BURIED OBJECTS

APPENDIX A RELEVANT PREVIOUS GEOTECHNICAL DATA

B-09-4

A

B-09-5

B-09-6

C-09-1

C-09-3C-09-4

C-09-2

C-09-6

C-09-5

C-09-7

C-09-8

C-09-12

C-09-10

C-09-14C-09-16 C-09-15

C-09-9

B-02-4

B-02-3

B-02-2

B-02-7

B-02-8

B-02-9

C-02-3

C-02-1

C-02-2

B-LC-10

B-LC-11

B-LC-13

B-LC-12

B-LC-14

B-LC-6

B-LC-7

B-LC-5B-LC-4

B-LC-3

B-LC-9

B-LC-8

B-09-3

B-ASE-1

B-LC-1 B-LC-2

B-09-1

HAWKINS BUILDING

EXISTING CENTRALPLANT PHASE I (CP1)

MAIN HOSPITAL BLDGCENTRAL TOWER

MAIN HOSPITAL BLDGSOUTH TOWER

TRAUMA CENTER (IPT)

PEDIATRIC ACUTECARE (MLA)

PLANTMANAGEMENT EXISTING MEDICAL

RECORDS BUILDING(HSB)

C-09-11

SERVICE & SUPPLY BLDG(NORTH)

SERVICE & SUPPLY BLDG(SOUTH)

EXISTINGSTORAGE

NEWCENTRALPLANTPHASE III(CP3)

BB

'

EXPLANATION

B-09-1Previous URS Boring Location (2009)

C-09-1Previous URS CPT Location (2009)

Proposed Buildings and Buildings to beRetrofitted

B-LC-1

C-02-1

B-02-1Previous URS Boring Location (2002)

Previous URS CPT Location (2002)

Previous LeRoy Crandrall and AssociatesBoring Location (1967)

B-ASE-1

Previous Associated Soils EngineeringBoring Location (2008)

A A' Geologic Cross Section

B-LC89-1

Previous LeRoy Crandrall and AssociatesBoring Location (1989)

* The location of the tunnel is only approximate based on the draft proposed siteplan dated 01/30/09 from the HMC Architects

Project Limit

Existing Utility Tunnel Phase 1

Existing Utility Tunnel Phase 2

Maximum depth: 50.24 (ft)

Page 1 of 2

Kehoe Testing & EngineeringOffice: (714) 901-7270Fax: (714) [email protected]@msn.com

CPT Data 30 ton rig Customer: URS CorpJob Site: 29405433

Date: 25/Mar/2009Test ID: C-14Project: LosAngeles

Test ID: C-14

File: Z25M0904C.ECP

0 700

Tip Stress COR

(tsf) 0 8

Sleeve Stress

(tsf) -1 14

Pore Pressure

(tsf) 0 8

Ratio COR

(%) 2 12

SBT FR

(Rob. 1986)

Sand Mix

Sandy Silt

Silt Mix

Sandy Silt

Sand Mix

Silt Mix

Silty Clay

Silty Sand

Silt Mix

Silty Clay

Clay

Silty Clay

Sandy Silt

Sand Mix

Sand

Gr Sand

Sandy Silt

Silt Mix

Sandy Silt

Silt Mix

Depth

(f

t)

0 0

10 10

20 20

30 30

40 40

50 50

FIGURE A-3

FIGURE A-4

FIGURE B-2

FIGURE B-3

Project Name: LACDPW - Mobile PET CT Tech DockProject Number: 60485266Boring No.: B-16-M1Sample No.: BK-1 Depth (ft): 0-5Location: N/ASoil Description: Clayey SandMold Number F D EWater Added, g -15 0 26Compact Moisture(%) 11.3 13.0 15.8Compaction Gage Pressure, psi 350 200 80Exudation Pressure, psi 711 320 120Sample Height, Inches 2.5 2.5 2.6Gross Weight Mold, g 2904 3018 3030Tare Weight Mold, g 1871 1969 1957Net Sample Weight, g 1034 1049 1074Expansion, inchesx10-4 26 9 0Stability 2,000 (160 psi) 17/28 32/81 50/124Turns Displacement 3.65 4.05 4.84R-Value Uncorrected 76 38 13R-Value Corrected 76 38 14Dry Density, pcf 112.5 112.5 108.1Traffic Index 8.0 8.0 8.0G.E. by Stability 0.45 1.19 1.65G.E. by Expansion 0.87 0.30 0.00

Date:

02/03/16

02/08/16Checked By:

STKMAP

R-VALUE TEST DATAASTM D2844

Tested By:Computed By: 02/04/16

Date:Date:

Gf = 1.34, and 2.2 % Retained on the ¾"

Rem

arks

By Exudation:

By Expansion:

At Equilibrium:

(by Exudation)

R-V

ALU

E

36

65

36

0

10

20

30

40

50

60

70

80

90

100

0100200300400500600700800

R-V

ALU

E

EXUDATION PRESSURE - PSI

0.00

1.00

2.00

3.00

4.00

0.00 1.00 2.00 3.00 4.00

CO

VER

TH

ICKN

ESS

BY S

TABI

LOM

ETER

(FT.

)

COVER THICKNESS BY EXPANSION (FT.)FIGURE B-6

CORROSIVITY TEST

Resistivity Test and PH: Califiornia Test Method 643

Sulfate Content: California Test Method 417

Chloride Content: California Test Method 422

Project Name : Location :

Project No. : Tested By :

Date: Data Input By:

Depth Resistivity Sulfate Content Chloride Content

(ft.) (ohm-cm) (ppm) (ppm)

B-16-H1 BK-1 0-5 950 9.2 411 15

B-16-M1 BK-1 0-5 1,250 8.8 399 15

B-16-R1 BK-1 0-5 1,300 8.2 ND* 15Silty SAND (SM)

Boring No. Sample No. PHSoil Description

Lean CLAY with Sand (CL)

Silty SAND (SM)

Los Angeles County, CA

A. D. Camacho

A. D. Camacho

LACDPW - Mobile PET CT Tech Unit

60485266

February 11, 2016

FIGURE B-9

Re

po

rt:

DM

G4

;P

roje

ct

File

:L

:\N

EV

ILL

E\P

RO

JE

CT

\ML

K\M

LK

-2

01

0.G

PJ;

Da

taT

em

pla

te:D

ML

A.G

DT

Pri

nte

d:

7/2

0/1

0

Modified California

Comments

Date(s)Drilled

DrillingMethod

Drill RigType

Approximate GroundSurface Elevation(ft)

N/A

JobNumber

5.5

N 33° 55.339', W 118° 14.638'

29405642

140 lbs Hammer/30-inch drop

SamplingMethod(s)

88.0

Total DepthDrilled (ft)

ASPHALT CONCRETE - 6 inches

ARTIFICIAL FILLS:Silty SANDOlive brown, loose, slightly moist, fine-grained sand

Silty CLAY with Sanddark olive brown, firm, moist, fine-grained sand, low to mediumplasticity

Boring terminate at 5.5 feet below ground surface.No groundwater encountered.Boring backfilled with coarse pond pebbles.Surface patched with cold patch asphalt.

SM

CL-ML

CME 75

Approximate GroundwaterDepth and Date Measured

LoggedBy

No groundwater encountered.

6/7/2010

Hollow-stem Auger, Hand Auger Drill BitSize/Type

HammerData

ADC

MATERIAL DESCRIPTIONOTHER TESTSand REMARKS

Mo

istu

reC

on

ten

t(%

)

Dry

De

nsity

(pcf)

De

pth

(ft)

Ele

va

tio

n(f

t)

US

CS

80

70

0

5

10

15

20

Blo

ws

pe

rfo

ot

This log is part of the report prepared by URS for this project and should beread together with the report. This summary applies only at the location ofthe exploration and at the time of drilling or excavation. Subsurfaceconditions may differ at other locations and may change at this location withtime. Data presented are a simplification of actual conditions encountered.

Figure A-9

LOG OF BORING

Sheet 1 of 1

Gra

ph

icL

og

Nu

mb

er

Typ

e

SAMPLES

Martin Luther King Jr MACC

FOR: Los Angeles County Department of Public Works12021 S. Wilmington Avenue, Willowbrook, CA

Boring PT-2

USBR 7300Calculation of Test Condition

0 ft5 ft5 ft

25 ftft

25 ftBased on the Test Data, Condition I is the most applicable

Calculation of Equivalent Radius of the Well, rw

0.1250 ft

Calculations for k20

5 ft

0.2383 gpm

75.4oF

0.8915 no units6.16E-04 ft/min Equation43.13E-04 cm/sec

Determine Eqivalent Radious of the Well(1 bag =38.5 lbs)

Weight of Gravel 231.00 lbfPour density of gravel 104.00 pcf

Volume of Gravel 2.22 ft^3Drilled Hole Depth 60.00 inchesDepth of Gravel Pack 0.00 inchesGravel Height 60.00 inches Equation 1Equivalent Well Diameter 0.75 ftEquivalent Well Diameter 9.02 inchesEquivalent Well Radius 4.51 inches

Determine Test DurationS-Specific yield of Soil 0.1000 ( fine-0.1, coarse -0.35)Height of Water in well - h 5.0000 ftWell Radius- r 0.3760 fth/r 13.2966

Minimum Volume Requirement 60.6253 ft^3 Equation 2Minimum Volume Requirement 453.4771 gallonsUsed Volume 94.0000 gallonsRequirement Met in the Field 20.7 %

Project Name: MLK JR HOSPITAL

Location: Los Angeles, CA

Test Number: PT-2

Float depth =Borehole depth =

Height of water in test well, h =Depth of water table, ft bgs

Depth to impervious layer, ft bgsUnsaturated distance between water table or

impervious layer and surface of well water, Tu

rw =

Condition I - K20 =

h =

Steady-state discharge rate, q =

Average well water temperature, T =Kinematic viscosity ratio, V =

Page 1

USBR 7300

Project Name: MLK JR HOSPITAL

Location: Los Angeles, CA

Test Number: PT-2

Discharge Rate (PT-2)

0.01

0.1

1

10

0 60 120 180 240 300 360

Time (minutes)

Flo

wR

ate

(gp

m)

Time-Discharge Curve for well Permeameter Test (PT-2)

0

40

80

120

160

200

0 60 120 180 240 300 360

Time (minutes)

Flo

wV

olu

me

(ga

llo

ns

)

Page 2

Date : 6/14/2010 Client: LACDPWDone By : AC Test No. PT-3Checked By : RIT

Clock Difference

Time

Accumulated

Time (mins)

Tank

Reading

(gallons)

Difference

Flow

(gallons)

Accumulated

Flow

(gallons)

Flow Rate

(gpm)

Well Temp

(oF)

Difference

Time (min)

7:36:12 0 0 54.0 0 0.07:54:26 0:18:14 18.23 53.0 1 1.0 0.055 76.0 18.238:16:56 0:22:30 40.73 52.0 1 2.0 0.044 76.0 22.508:39:19 0:22:23 63.12 51.0 1 3.0 0.045 76.0 22.389:03:22 0:24:03 87.17 50.0 1 4.0 0.042 76.0 24.059:29:16 0:25:54 113.07 49.0 1 5.0 0.039 76.0 25.909:56:42 0:27:26 140.50 48.0 1 6.0 0.036 76.0 27.43

10:24:33 0:27:51 168.35 47.0 1 7.0 0.036 76.0 27.8510:52:16 0:27:43 196.07 46.0 1 8.0 0.036 76.0 27.7211:20:19 0:28:03 224.12 45.0 1 9.0 0.036 76.0 28.0511:48:16 0:27:57 252.07 44.0 1 10.0 0.036 77.0 27.9512:16:07 0:27:51 279.92 43.0 1 11.0 0.036 77.0 27.8512:45:08 0:29:01 308.93 42.0 1 12.0 0.034 81.0 29.0213:14:06 0:28:58 337.90 41.0 1 13.0 0.035 79.0 28.9713:44:17 0:30:11 368.08 40.0 1 14.0 0.033 79.0 30.1814:14:48 0:30:31 398.60 39.0 1 15.0 0.033 79.0 30.5214:45:01 0:30:13 428.82 38.0 1 16.0 0.033 78.0 30.2215:14:52 0:29:51 458.67 37.0 1 17.0 0.034 78.0 29.8515:44:28 0:29:36 488.27 36.0 1 18.0 0.034 78.0 29.6016:14:32 0:30:04 518.33 35.0 1 19.0 0.033 77.0 30.0716:45:01 0:30:29 548.82 34.0 1 20.0 0.033 77.0 30.4817:15:19 0:30:18 579.12 33.0 1 21.0 0.033 77.0 30.30

Project Name: MLK Jr Hospital

Location: Los Angeles, CATest Data Interpretation

USBR 7300

Page 1

APPENDIX B FIELD EXPLORATION AND LOGS OF BORING

APPENDIX B FIELD EXPLORATION AND LOGS OF BORING

B-1

This appendix describes the geotechnical boring program conducted by AECOM for the proposed Relocated Red Bag Storage and Future DHS Regional Lab project (Project) within the Martin Luther King, Jr. Medical Center, located at 12021 S. Wilmington Avenue, Los Angeles County, California. The exploratory boring locations were first marked in the field and checked through Underground Services Alert (USA) for clearance of potential conflicts with underground utilities. When necessary, the marked locations were adjusted in order to avoid encountering underground utilities.

Our original exploratory boring program was initiated on January 23, 2019 and completed on January 24, 2019 under the supervision of an AECOM engineer. Subsurface exploration included drilling and sampling two borings to a maximum depth of 61.5 feet below the existing ground surface by our subcontractor, , 2R Drilling Inc. of Chino, California. All borings were drilled using a truck-mounted CME-75 drill rig with hollow stem auger. The borings were backfilled with cement-bentonite grout and the surrounding ground surface was reinstated following borehole completion. The locations of the borings are shown on Figure 4.

AECOM geotechnical representative maintained field boring logs and visually classified the soils according to the Unified Soil Classification System. The boring logs and other pertinent information are presented in following pages. When subsurface conditions permitted, relatively undisturbed samples were recovered with the Modified California Soil Sampler (with 2.42-inch I.D.). Standard Penetration Testing (SPT) and testing with the Modified California Soil Sampler were performed in the subsurface soils using a 140-pound automatic-tripped hammer with a 30-inch drop. The number of blows required to drive the sampler was recorded at 6-inch intervals for each sample taken. SPT was performed in accordance with ASTM D1586 procedures. The total number of blows required to drive the sampler every 6 inches is recorded on the boring logs presented in this Appendix.

Geotechnical samples obtained in the field were carefully sealed and packaged to reduce moisture loss and disturbance and were transported to our laboratory for further testing.

The blow count for the final 12 inches of sampler penetration is commonly referred to as the "N Value". This value generally reflects the resistance to penetration of the soil at the sample depth. The degree of relative density of granular soils and the degree of consistency of cohesive soils are generally described on the boring logs according to the conventional correlation presented in the following table.

The relative density and consistency descriptions on the attached boring log are based on unadjusted blow counts recorded in the field. These numbers are considered useful in providing an estimate of the relative density or consistency of soils. The relative density and consistency descriptions on the log may deviate from the correlation for a number of reasons, including reliance on other test results or the engineer’s judgment based on manual manipulation of the sample.

Granular Soils Cohesive Soils

SPT Blow Count Description SPT Blow Count Description

< 4 Very Loose < 2 Very Soft4 – 10 Loose 2 – 4 Soft11 – 30 Medium Dense 5 – 8 Firm31 – 50 Dense 9 – 15 Stiff

> 50 Very Dense 16 - 30 Very Stiff> 30 Hard

It is widely accepted that the above-listed SPT blow count correlation is overly simplistic. For most applications in non-gravelly soils, the blow count is usually adjusted for the effective vertical pressure at the sampling depth and for other sampling system parameters such as the efficiency of the sampling system

APPENDIX B FIELD EXPLORATION AND LOGS OF BORING

B-2

and/or sampling techniques used. In gravelly soils, it is recognized that the blow counts are higher than would be expected in non-gravelly soils of similar density or consistency. This occurs because the sampler tends to push larger gravel clasts ahead of it. The area of the gravel clast may be significantly greater than that of the sampler, causing increased resistance and higher blow counts.

The blow count obtained from nonstandard penetration tests using a Modified California Soil Sampler, N, may be converted to standard blow count, N60, by the relationship between SPT values and hammer ratios [Rs = f(inner/outer diameter of sampler, weight of hammer, and height of drop)] (Fang, 1991). In this project using a 140-pound hammer and 30-inch drop, N60 is equivalent to approximately 0.5´N for the sampler in sandy soils and 0.6´ N in cohesive soils.

Expansion Index Test

SILTY SANDS, SAND - SILT MIXTURES

CLAYEY SANDS, SAND - CLAY MIXTURES

INORGANIC SILTS AND VERY FINE SANDS, ROCK FLOUR, SILTYOR CLAYEY FINE SANDS OR CLAYEY SILTS WITH SLIGHTPLASTICITY

INORGANIC CLAYS OF LOW TO MEDIUM PLASTICITY,GRAVELLY CLAYS, SANDY CLAYS, SILTY CLAYS, LEANCLAYS

Shelby Tube Sample

Rock Core Sample

Note: Number of blows required to advance driven sample 12"(or length noted) is recorded; blow count recorded for seatinginterval (initial 6" of drive) is indicated by an asterisk.

WELL-GRADED GRAVELS, GRAVEL - SAND MIXTURES, LITTLEOR NO FINES

CL

CORR Corrosion Test

DS Direct Shear Test

(LITTLE OR NO FINES)

GRAVELS WITHFINES

GC

SW

SP

(APPRECIABLEAMOUNT OF FINES)

Disturbed Type-U Sample

Approximate depth of perched water or groundwater

Pitcher Tube Sample

GRAVEL ANDGRAVELLY SOILS

CON

CLAYEY GRAVELS, GRAVEL - SAND - CLAY MIXTURES

POORLY GRADED SANDS, GRAVELLY SANDS, LITTLE OR NOFINES

R-Value Resistance Value Test

SA Sieve Analysis

LIQUID LIMITGREATER THAN 50

GM

Bk

WELL-GRADED SANDS, GRAVELLY SANDS, LITTLE OR NOFINES

GW

GP POORLY GRADED GRAVELS, GRAVEL - SAND MIXTURES,LITTLE OR NO FINES

Torvane Test

SILTY GRAVELS, GRAVEL - SAND - SILT MIXTURES

MORE THAN 50% OFMATERIAL ISLARGER THAN NO.200 SIEVE SIZE

CLEAN GRAVELS

(LITTLE OR NO FINES)

SANDS WITHFINES

(APPRECIABLEAMOUNT OF FINES)

Bulk sample

OL

CLEAN SANDS

EI

PT

ORGANIC SILTS AND ORGANIC SILTY CLAYS OF LOWPLASTICITY

INORGANIC SILTS, MICACEOUS OR DIATOMACEOUS FINESANDY OR SILTY SOILS, ELASTIC SILTS

INORGANIC CLAYS OF HIGH PLASTICITY

ORGANIC CLAYS OF MEDIUM TO HIGH PLASTICITY, ORGANICSILTS

SE Sand Equivalent Test

ML

SYMBOLS TYPICAL DESCRIPTIONS

LIQUID LIMIT LESSTHAN 50

Swell Load Test

Laboratory and Field Test Abbreviations

TV

SILTS AND CLAYS

SILTS AND CLAYS

HIGHLY ORGANIC SOILS

MORE THAN 50% OFCOARSE FRACTIONRETAINED ON NO. 4SIEVE

SAND ANDSANDY SOILS

MORE THAN 50% OFCOARSE FRACTIONPASSING NO. 4 SIEVE

PEAT, HUMUS, SWAMP SOILS WITH HIGH ORGANICCONTENTS

NOTE: Dual symbols are used to indicate gravels or sand with 5-12% fines and soils with fines classifying as CL-ML. Symbols separated by a slash indicateborderline soil classifications.

SOIL CLASSIFICATION CHART

MAJOR DIVISIONS

OH

FINE GRAINEDSOILS

MORE THAN 50% OFMATERIAL ISSMALLER THAN NO.200 SIEVE SIZE

COMP Compaction Test

Consolidation Test

MH

CH

SM

SC

SWELL

KEY TO LOG OF BORING Clinical Lab and Red Bag Storage Area Martin Luther King Jr. Medical Campus

FOR: Los Angeles County, Department of Public Works

Dames & Moore Type-U sample

Standard Penetration Test

No Recovery

COARSEGRAINED SOILS

CBR

COL

California Bearing Ratio Test

Collapse Potential Test

Sampler and Symbol Descriptions

Rock Material Symbols (examples)

Topanga FormationModelo Formation Santa MonicaSlate

FIGURE 3

AC

SM

9-inch Asphalt

5-inch Base Silty SAND (SM) dense; dark olive brown; moist; fine-grained SAND,with little CLAY

becomes medium dense; olive brown

becomes dark olive brown; little calcification;micaceous

Total Depth = 16.5 feet bgsGroundwater not encounteredBorehole backfilled with soil cuttings and capped withconcrete cap with black dye

CORR, R-Value

32

13

15

6

61220667

369

233

1

2

3

4

Total DepthDrilled (ft)

140 lbs, 30-inch drop

SamplingMethod(s)

Approximate GroundwaterDepth and Date Measured Groundwater not encountered

LoggedByJan. 28, 2016

Hollow Stem Auger

Approximate GroundSurface Elevation (ft)

HammerData

Ana Coria

60595699

WGS 1984 87.0 MSL

Drill BitSize

Location(ft and/or °)

16.5

CME 75

Bulk, SPT, Modified California

Long. 118.24382

Date(s)Drilled

DrillingMethod

Drill RigType

8-inch

JobNumber

CoordinateSystem

Lat. 33.92299

Boring B-16-M1

This log is part of the report prepared by URS for this project and shouldbe read together with the report. This summary applies only at thelocation of the exploration and at the time of drilling or excavation.Subsurface conditions may differ at other locations and may change atthis location with time. Data presented are a simplification of actualconditions encountered.

Sheet 1 of 1

Clinical Lab and Red Bag Storage Area Martin Luther King Jr. Medical Campus

FOR: Los Angeles County, Department of Public Works

LOG OF BORING

US

CS

Gra

phi

c Lo

g

Dep

th (

ft)

Typ

e MATERIAL DESCRIPTION

Num

ber

SAMPLES

OTHER TESTS

AND

REMARKS

Ele

vatio

n (f

t)

Moi

stur

eC

onte

nt (

%)

Dry

Den

sity

(p

cf)

Blo

ws

per

foot

Blo

ws

per

6 in

ches

80

70

60

0

5

10

15

20

25

30

Liqu

idLi

mit

(%)

Pla

stic

ityIn

dex

(%)

Poc

ket P

en

(tsf

)

% P

ass

ing

No.

200

Sie

ve

AECOMAECOM

Rep

ort:

DM

G4;

P

roje

ct F

ile: \

\LO

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S.N

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EC

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S\P

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ES

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ION

201

8\B

OR

ING

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LA

B -

GO

BI U

PD

AT

E.G

PJ;

D

ata

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plat

e:U

RS

HS

A L

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S 2

010

.GD

T

Pri

nted

: 3

/16/

19

AC

BASESM

SC

SP

SC

9-inch thick ASPHALT CONCRETE

5.5-inch thick BASESilty SAND loose; olive brown; moist

medium dense

Clayey SANDmedium dense; olive brown; moist

loose to medium dense

Poorly-graded SAND medium dense; light olive brown to grayish brown;moist, fine SAND

Clayey SANDdense; olive brown; moist; fine SAND

COMP, CORR,EI, R-Value

DS

17

25

18

99

5

21

8

30

18

223

6912

235

121713

5711

B-1

S-1

S-2

S-3

S-4

S-5

5

Total DepthDrilled (ft)

140 lbs, 30-inch drop

SamplingMethod(s)

Approximate GroundwaterDepth and Date Measured 50.33' on 1/24/2019

LoggedByJan. 24, 2019

Hollow Stem Auger

Approximate GroundSurface Elevation (ft)

HammerData

S. Denise

60595699

California State PlaneCoord. Zone 5 NAD83 (ft) 95.0 MSL

Drill BitSize

Location(ft and/or °)

61.5

CME 75

Bulk, SPT, Modified California

Long. 1794445.806

Date(s)Drilled

DrillingMethod

Drill RigType

8 inch OD Bullet

JobNumber

CoordinateSystem

Lat. 6487581.914

Boring B-18-L1

This log is part of the report prepared by URS for this project and shouldbe read together with the report. This summary applies only at thelocation of the exploration and at the time of drilling or excavation.Subsurface conditions may differ at other locations and may change atthis location with time. Data presented are a simplification of actualconditions encountered.

Sheet 1 of 2

Clinical Lab and Red Bag Storage Area Martin Luther King Jr. Medical Campus

FOR: Los Angeles County, Department of Public Works

LOG OF BORING

US

CS

Gra

phi

c Lo

g

Dep

th (

ft)

Typ

e MATERIAL DESCRIPTION

Num

ber

SAMPLES

OTHER TESTS

AND

REMARKS

Ele

vatio

n (f

t)

Moi

stur

eC

onte

nt (

%)

Dry

Den

sity

(p

cf)

Blo

ws

per

foot

Blo

ws

per

6 in

ches

90

80

70

0

5

10

15

20

25

30

Liqu

idLi

mit

(%)

Pla

stic

ityIn

dex

(%)

Poc

ket P

en

(tsf

)

% P

ass

ing

No.

200

Sie

ve

AECOMAECOM

Rep

ort:

DM

G4;

P

roje

ct F

ile: \

\LO

SA

NG

ELE

S.N

A.A

EC

OM

NE

T.C

OM

\LO

SA

NG

ELE

S\P

RO

JEC

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\EN

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LEG

AC

Y\G

T\D

A W

U\L

A C

OU

NT

Y G

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CH

ON

-CA

LL\M

LK\F

IELD

INV

ES

TIG

AT

ION

\INV

ES

TIG

AT

ION

201

8\B

OR

ING

LO

GS

\MLK

LA

B -

GO

BI U

PD

AT

E.G

PJ;

D

ata

Tem

plat

e:U

RS

HS

A L

OG

S 2

010

.GD

T

Pri

nted

: 3

/16/

19

SC

SP

ML

SM

SP

olive brown; fine to medium SAND

Silty SANDdense; grayish brown; moist; fine SAND

olive brown

Poorly-graded SANDdense; grayish brown; moist; fine to medium SAND

SILThard; dark grayish brown; moist; fine SAND

very stiff

Silty SANDmedium dense; dark grayish brown; moist; fineSAND

dense; wet

very dense; olive brown

Poorly-graded SANDvery dense; dark gray; wet, fine SANDBottom of borehole at 61.5 feet. Ground waterencountered at 50.33 feet.Borehole backfilled with cement bentonite grout to 5feet above GW, and soil cuttings with concrete cap toexisting grade

CONS, SA

DS

22

15

19

25

101

100

46

27

51

29

33

30

100+

101630

91314

202526

121613

101419

91416

1445

50/5"

NP

NP

NP

NP

S-6

S-7

S-8

S-9

S-11

S-13

S-14

80.9

Martin Luther King Jr. Medical Campus

FOR: Los Angeles County, Department of Public Works

Boring B-18-L1Sheet 2 of 2

LOG OF BORINGClinical Lab and Red Bag Storage Area

US

CS

Gra

phi

c Lo

g

Dep

th (

ft)

Typ

e MATERIAL DESCRIPTION

Num

ber

SAMPLES

OTHER TESTS

AND

REMARKS

Ele

vatio

n (f

t)

Moi

stur

eC

onte

nt (

%)

Dry

Den

sity

(p

cf)

Blo

ws

per

foot

Blo

ws

per

6 in

ches

60

50

40

30

30

35

40

45

50

55

60

65

Liqu

idLi

mit

(%)

Pla

stic

ityIn

dex

(%)

Poc

ket P

en

(tsf

)

% P

ass

ing

No.

200

Sie

ve

AECOMAECOM

Rep

ort:

DM

G4;

P

roje

ct F

ile: \

\LO

SA

NG

ELE

S.N

A.A

EC

OM

NE

T.C

OM

\LO

SA

NG

ELE

S\P

RO

JEC

TS

\EN

V\_

LEG

AC

Y\G

T\D

A W

U\L

A C

OU

NT

Y G

EO

TE

CH

ON

-CA

LL\M

LK\F

IELD

INV

ES

TIG

AT

ION

\INV

ES

TIG

AT

ION

201

8\B

OR

ING

LO

GS

\MLK

LA

B -

GO

BI U

PD

AT

E.G

PJ;

D

ata

Tem

plat

e:U

RS

HS

A L

OG

S 2

010

.GD

T

Pri

nted

: 3

/16/

19

CC

ML

CL

SM

SC

SP

9.5-inch thick CONCRETE

Sandy SILTmedium stiff; olive brown; moist

Lean CLAY with SANDmedium stiff; olive brown; moist

Silty SANDdense; olive brown; moist; fine grained SAND

fine GRAVEL

very dense

Clayey SAND medium dense; dark yellowish brown; moist

dense

Poorly-graded SAND with Graveldense; dark yellowish brown; moist; coarse to fineSAND, fine GRAVEL

COMP, CORR,R-Value

CONS, SA

23

25

15 114

9

7

57

10

29

354

243

112334

346

91217

NP NP

BK-1

S-1

S-3

S-5

S-6

S-7

84.2

32

Total DepthDrilled (ft)

140 lbs, 30-inch drop

SamplingMethod(s)

Approximate GroundwaterDepth and Date Measured 56.5' on 1/23/2019

LoggedByJan. 23, 2019

Hollow Stem Auger

Approximate GroundSurface Elevation (ft)

HammerData

S. Denise

60595699

California State PlaneCoord. Zone 5 NAD83 (ft) 90.0 MSL

Drill BitSize

Location(ft and/or °)

61.5

CME 75

Bulk, SPT, Modified California

Long. 1794184.221

Date(s)Drilled

DrillingMethod

Drill RigType

8 inch OD Bullet

JobNumber

CoordinateSystem

Lat. 6487550.637

Boring B-18-L2

This log is part of the report prepared by URS for this project and shouldbe read together with the report. This summary applies only at thelocation of the exploration and at the time of drilling or excavation.Subsurface conditions may differ at other locations and may change atthis location with time. Data presented are a simplification of actualconditions encountered.

Sheet 1 of 2

Clinical Lab and Red Bag Storage Area Martin Luther King Jr. Medical Campus

FOR: Los Angeles County, Department of Public Works

LOG OF BORING

US

CS

Gra

phi

c Lo

g

Dep

th (

ft)

Typ

e MATERIAL DESCRIPTION

Num

ber

SAMPLES

OTHER TESTS

AND

REMARKS

Ele

vatio

n (f

t)

Moi

stur

eC

onte

nt (

%)

Dry

Den

sity

(p

cf)

Blo

ws

per

foot

Blo

ws

per

6 in

ches

90

80

70

60

0

5

10

15

20

25

30

Liqu

idLi

mit

(%)

Pla

stic

ityIn

dex

(%)

Poc

ket P

en

(tsf

)

% P

ass

ing

No.

200

Sie

ve

AECOMAECOM

Rep

ort:

DM

G4;

P

roje

ct F

ile: \

\LO

SA

NG

ELE

S.N

A.A

EC

OM

NE

T.C

OM

\LO

SA

NG

ELE

S\P

RO

JEC

TS

\EN

V\_

LEG

AC

Y\G

T\D

A W

U\L

A C

OU

NT

Y G

EO

TE

CH

ON

-CA

LL\M

LK\F

IELD

INV

ES

TIG

AT

ION

\INV

ES

TIG

AT

ION

201

8\B

OR

ING

LO

GS

\MLK

LA

B -

GO

BI U

PD

AT

E.G

PJ;

D

ata

Tem

plat

e:U

RS

HS

A L

OG

S 2

010

.GD

T

Pri

nted

: 3

/16/

19

ML

SM

very dense; dark grayish brown; slight petrol smell

very dense

SILT with Sandhard; olive brown; moist; low plasticity; fine SAND

Silty SANDdense; oliver gray; moist; fine SAND

medium dense

dense

Bottom of borehole at 61.5 feet. Ground waterencountered at 56.5 feet.Borehole backfilled with cement bentonite grout to 5feet above GW, and soil cuttings with concrete cap toexisting grade

DS

4

4

16

104

29

100+

49

39

27

30

35

101316

3550/4"

92425

121722

61116

91317

71421

NP NP

S-8

S-9

S-10

S-11

S-12

S-13

S-14

2.6

Martin Luther King Jr. Medical Campus

FOR: Los Angeles County, Department of Public Works

Boring B-18-L2Sheet 2 of 2

LOG OF BORINGClinical Lab and Red Bag Storage Area

US

CS

Gra

phi

c Lo

g

Dep

th (

ft)

Typ

e MATERIAL DESCRIPTION

Num

ber

SAMPLES

OTHER TESTS

AND

REMARKS

Ele

vatio

n (f

t)

Moi

stur

eC

onte

nt (

%)

Dry

Den

sity

(p

cf)

Blo

ws

per

foot

Blo

ws

per

6 in

ches

60

50

40

30

30

35

40

45

50

55

60

65

Liqu

idLi

mit

(%)

Pla

stic

ityIn

dex

(%)

Poc

ket P

en

(tsf

)

% P

ass

ing

No.

200

Sie

ve

AECOMAECOM

Rep

ort:

DM

G4;

P

roje

ct F

ile: \

\LO

SA

NG

ELE

S.N

A.A

EC

OM

NE

T.C

OM

\LO

SA

NG

ELE

S\P

RO

JEC

TS

\EN

V\_

LEG

AC

Y\G

T\D

A W

U\L

A C

OU

NT

Y G

EO

TE

CH

ON

-CA

LL\M

LK\F

IELD

INV

ES

TIG

AT

ION

\INV

ES

TIG

AT

ION

201

8\B

OR

ING

LO

GS

\MLK

LA

B -

GO

BI U

PD

AT

E.G

PJ;

D

ata

Tem

plat

e:U

RS

HS

A L

OG

S 2

010

.GD

T

Pri

nted

: 3

/16/

19

APPENDIX C CONE PENETRATION TEST

SUMMARY

OF

CONE PENETRATION TEST DATA

Prepared by:

KEHOE TESTING & ENGINEERING 5415 Industrial Drive

Huntington Beach, CA 92649-1518 Office (714) 901-7270 / Fax (714) 901-7289

www.kehoetesting.com

Project:

Martin Luther King Jr. Medical Campus Behavior Center Project Los Angeles, CA

February 14, 2019

Prepared for:

Mr. Dennis Nguyen

AECOM 300 S. Grand Avenue

Los Angeles, CA 90071 Office (213) 593-8100 / Fax (213) 593-8178

TABLE OF CONTENTS

1. INTRODUCTION 2. SUMMARY OF FIELD WORK 3. FIELD EQUIPMENT & PROCEDURES 4. CONE PENETRATION TEST DATA & INTERPRETATION

APPENDIX

CPT Plots CPT Classification/Soil Behavior Chart CPT Data Files (sent via email)

SUMMARY

OF CONE PENETRATION TEST DATA

1. INTRODUCTION This report presents the results of a Cone Penetration Test (CPT) program carried out for the Martin Luther King Jr. Medical Campus Behavior Center Project located in Los Angeles, California. The work was performed by Kehoe Testing & Engineering (KTE) on February 14, 2019. The scope of work was performed as directed by AECOM personnel. 2. SUMMARY OF FIELD WORK The fieldwork consisted of performing CPT soundings at two locations to determine the soil lithology. A summary is provided in TABLE 2.1.

LOCATION

DEPTH OF CPT (ft)

COMMENTS/NOTES:

C-BHC2 100 C-LC3 100

TABLE 2.1 - Summary of CPT Soundings

3. FIELD EQUIPMENT & PROCEDURES The CPT soundings were carried out by KTE using an integrated electronic cone system manufactured by Vertek. The CPT soundings were performed in accordance with ASTM standards (D5778). The cone penetrometers were pushed using a 30-ton CPT rig. The cone used during the program was a 15 cm^2 cone and recorded the following parameters at approximately 2.5 cm depth intervals:

Cone Resistance (qc) Inclination Sleeve Friction (fs) Penetration Speed Dynamic Pore Pressure (u)

The above parameters were recorded and viewed in real time using a laptop computer. Data is stored at the KTE office for up to 2 years for future analysis and reference. A complete set of baseline readings was taken prior to each sounding to determine temperature shifts and any zero load offsets. Monitoring base line readings ensures that the cone electronics are operating properly.

4. CONE PENETRATION TEST DATA & INTERPRETATION The Cone Penetration Test data is presented in graphical form in the attached Appendix. These plots were generated using the CPeT-IT program. Penetration depths are referenced to ground surface. The soil classification on the CPT plots is derived from the attached CPT Classification Chart (Robertson) and presents major soil lithologic changes. The stratigraphic interpretation is based on relationships between cone resistance (qc), sleeve friction (fs), and penetration pore pressure (u). The friction ratio (Rf), which is sleeve friction divided by cone resistance, is a calculated parameter that is used along with cone resistance to infer soil behavior type. Generally, cohesive soils (clays) have high friction ratios, low cone resistance and generate excess pore water pressures. Cohesionless soils (sands) have lower friction ratios, high cone bearing and generate little (or negative) excess pore water pressures. The CPT data files have also been provided. These files can be imported in CPeT-IT (software by GeoLogismiki) and other programs to calculate various geotechnical parameters. It should be noted that it is not always possible to clearly identify a soil type based on qc, fs and u. In these situations, experience, judgement and an assessment of the pore pressure data should be used to infer the soil behavior type. If you have any questions regarding this information, please do not hesitate to call our office at (714) 901-7270. Sincerely,

KEHOE TESTING & ENGINEERING

Steven P. Kehoe President 02/18/19-hh-0239

APPENDIX

Project: AECOM / MLK Jr. Medical Campus Behavior Center

Kehoe Testing and Engineering

714-901-7270

[email protected]

www.kehoetesting.comTotal depth: 100.14 ft, Date: 2/14/2019

Surface Elevation: 0.00 ft

Los Angeles, CA Cone Type: Vertek

C-LC3

Location:

CPeT-IT v.2.3.1.8 - CPTU data presentation & interpretation software - Report created on: 2/16/2019, 7:03:17 AM 1

Project file:

APPENDIX D GEOTECHNICAL LABORATORY TESTING

APPENDIX D GEOTECHNICAL LABORATORY TESTING

D-1

Geotechnical soil samples obtained from the borings were carefully packaged in the field to reduce moisture loss and disturbance. The samples were subsequently delivered to our laboratory where they were further examined and classified. Selected representative samples were tested to evaluate moisture content, in-situ dry density, grain-size distribution, plasticity index, shear strength, corrosivity, and R-value. Tests discussed below were performed in accordance with the latest American Society of Testing and Materials (ASTM) and California Test (CT) standards.

Moisture Content and In-situ Density (ASTM D2216 and D2937) TestsThe moisture content and in-situ density tests were performed on selected soil samples obtained from the borings. Moisture content and in-situ density tests were performed in accordance with ASTM Test Method D2216. The test results are presented on the logs of borings (Appendix D-1).

Sieve Analyses (ASTM D6913)Sieve analyses were performed to determine the particle size distribution of representative soils. The tests were performed in accordance with ASTM Test Method D6913. Test results are presented in Appendix D-2 (Grain Size Distribution).

Percent Passing No. 200 SievePercent passing no. 20 sieve were performed to determine the fines content of the representative soils. The tests were performed in accordance with ASTM Test Method D1140. Test results are presented in Appendix D-3.

Atterberg Limits Tests (ASTM D4318)Atterberg Limits tests were performed to aid in classification and to evaluate the plasticity characteristics of fine-grained materials encountered in the borings. The tests were performed in accordance with ASTM Test Method D4318. The results of this test are presented in Appendix D-4 and D-5.

Direct Shear Test (ASTM D3080)One consolidated-drained (saturated) direct shear test was performed on a selected undisturbed sample to evaluate shear-strength parameters of the on-site soils. The direct-shear test was performed in accordance with ASTM Test Method D3080. The results are presented in Appendix D-6 through D-8, respectively.

Expansion Index (ASTM D4829)Expansion index (EI) tests were performed on selected samples to evaluate expansion characteristics of the soils. The test was performed in accordance with ASTM D4829, and the result of the test is presented in Appendix D-9.

Consolidation Test (ASTM D2435)One consolidation tests were performed to determine the magnitude and rate of volume decrease that a laterally confined soil specimen undergoes when subjected to different vertical pressures. The tests were performed in accordance with ASTM Test Method D2435. Test results are presented in Appendix D-10 and D-11.

APPENDIX D GEOTECHNICAL LABORATORY TESTING

D-2

Compaction Test (ASTM D1557)A compaction test was performed on a representative bulk sample of the near-surface soils in order to evaluate compaction characteristics of the soils. The test was performed in accordance with ASTM Test Method D1557. Test results are presented in Figures D-12 and D-13.

R-Value Test (ASTM D2844)R-Value test were performed on selected samples to evaluate bearing characteristics of the soils. The test was performed in accordance with ASTM D2844, and the result of the test is presented in Appendix D-14 through D-15.

Corrosivity Tests (CT 417, CT 422, CT 643)

Selected representative samples obtained from the borings were tested for corrosion. The subject soil samples were processed with the U.S. Standard No. 8 Sieve and tested for pH (CT 643), Sulfate Ion Content (CT 417), Chloride Ion Content (CT 422), and resistivity (CT 643), the result of the test is presented in Appendix D-16.

Client: AECOM AP Lab No.: 19-0206Project Name: MLK BHC Projects Date: 02/07/19

Project No.: 60595699

Boring Sample Sample Moisture Dry DensityNo. No. Depth (ft.) Content (%) (pcf)

B-18-L1 S-1 5 17.4 NA B-18-L1 S-5 25 18.3 NA B-18-L1 S-9 45 14.7 NA B-18-L1 S-13 55 19.2 NA B-18-L2 B-1 0-5 23.1 NA B-18-L2 S-4 11 25.0 NA B-18-L2 S-8 30 3.5 NA B-18-L2 S-12 50 16.1 NA

MOISTURE AND DENSITY TEST RESULTS

Appendix D - 1

GRAIN SIZE DISTRIBUTION CURVEASTM D 6913

Client Name: AECOM Tested by: AM Date: 02/11/19Project Name: MLK BHC Projects Computed by: JP Date: 02/12/19Project Number: 60595699 Checked by: AP Date: 02/12/19

Gravel Sand Silt & Clay

B-18-L1 S-4 20 0 95 5 SP-SM

B-18-L2 S-5 15 0 68 32 SM

Symbol Boring No. Sample No.

Sample Depth (feet)

Percent Soil Type U.S.C.S

Atterberg Limits LL:PL:PI

N/A

N/A

0

10

20

30

40

50

60

70

80

90

100

0.0010.010.1110100

PER

CEN

T PA

SSIN

G B

Y W

EIG

HT

PARTICLE SIZE (mm)

SAND SILT OR CLAY

HYDROMETERSIEVE NUMBER

GRAVEL

COARSE FINE COARSE MEDIUM FINE

SIEVE OPENING

Appendix D - 2

Client: AECOM AP Lab No.: 19-0206

Project Name: MLK BHC Projects Test Date: 02/07/19

Project Number: 60595699

Boring Sample Percent FinesNo. No. (%)

B-18-L1 S-6 30 80.9

B-18-L2 S-2 6.5 84.2

B-18-L2 S-9 35 2.6

PERCENT PASSING NO. 200 SIEVE

Depth (ft)

ASTM D1140

Appendix D - 3

Project Name: MLK BHC Projects Tested By: LS Date: 02/08/19Project No.: 60595699 Checked By: AP Date: 02/12/19

PROCEDURE USED

Wet Preparation

X Dry Preparation

X Procedure A Multipoint Test

Procedure B One-point Test

Symbol Boring Number

Sample Number

Depth (feet) LL PL PI

Plasticity Chart

Symbol

B-18-L1 S-6 30 NP NP NP

B-18-L1 S-14 60 NP NP NP

* NP denotes "non-plastic"

ATTERBERG LIMITSASTM D 4318

CL-ML

CL

ML or OL

CH

MH or OH

0

10

20

30

40

50

60

0 10 20 30 40 50 60 70 80 90 100

PLAS

TIC

ITY

IND

EX (P

I)

LIQUID LIMIT (LL)

30

35

40

45

50

10 100

Moi

stur

e C

onte

nt (%

)

Number of Blows25

Appendix D - 4

Project Name: MLK BHC Projects Tested By: LS Date: 02/08/19Project No.: 60595699 Checked By: AP Date: 02/12/19

PROCEDURE USED

Wet Preparation

X Dry Preparation

X Procedure A Multipoint Test

Procedure B One-point Test

Symbol Boring Number

Sample Number

Depth (feet) LL PL PI

Plasticity Chart

Symbol

B-18-L2 S-5 15 NP NP NP

B-18-L2 S-9 35 NP NP NP

* NP denotes "non-plastic"

ATTERBERG LIMITSASTM D 4318

CL-ML

CL

ML or OL

CH

MH or OH

0

10

20

30

40

50

60

0 10 20 30 40 50 60 70 80 90 100

PLAS

TIC

ITY

IND

EX (P

I)

LIQUID LIMIT (LL)

20

25

30

35

40

10 100

Moi

stur

e C

onte

nt (%

)

Number of Blows25

Appendix D - 5

 Project Name: MLK BHC Projects Tested By: ST Date: 02/11/19

 Project No.: 60595699 Computed By: JP Date: 02/12/19

 Boring No.: L-18-L1 Checked by: AP Date: 02/12/19

 Sample No.: S‐2 Depth (ft): 10

 Sample Type: Mod. Cal. Soil Description: Silty Sand Test Condition: Inundated Shear Type: Regular 

Wet             

Unit Weight   

(pcf)

Dry          

Unit Weight 

(pcf)

Initial 

Moisture 

Content (%)

Final 

Moisture 

Content (%)

Initial Degree 

Saturation 

(%)

Final Degree 

Saturation  

(%)

Normal 

Stress 

(ksf)

Peak    

Shear 

Stress (ksf)

Ultimate    

Shear 

Stress (ksf)

0.5 0.696 0.516

1 1.021 0.781

2 1.608 1.332

100

DIRECT SHEAR TEST RESULTSASTM D 3080

124.2 99.0 25.4 26.1 98

0

1

2

0 0.1 0.2 0.3

Shea

r Stre

ss (k

sf)

Shear Deformation (Inches)

0.5 ksf 1 ksf 2 ksf

0

1

2

3

0 1 2 3 4 5 6

Shea

r Stre

ss (k

sf)

Normal Stress (ksf)

Peak: C=400 psf; ɸ=31˚

Ultimate: C=250 psf; ɸ=28˚

Normal Stress:

Appendix D - 6

 Project Name: MLK BHC Projects Tested By: ST Date: 02/11/19

 Project No.: 60595699 Computed By: JP Date: 02/12/19

 Boring No.: L-18-L1 Checked by: AP Date: 02/12/19

 Sample No.: S‐14 Depth (ft): 60

 Sample Type: Mod. Cal. Soil Description: Silty Sand Test Condition: Inundated Shear Type: Regular 

Wet             

Unit Weight   

(pcf)

Dry          

Unit Weight 

(pcf)

Initial 

Moisture 

Content (%)

Final 

Moisture 

Content (%)

Initial Degree 

Saturation 

(%)

Final Degree 

Saturation  

(%)

Normal 

Stress 

(ksf)

Peak    

Shear 

Stress (ksf)

Ultimate    

Shear 

Stress (ksf)

2 1.968 1.373

4 3.636 2.573

8 6.408 5.004

DIRECT SHEAR TEST RESULTSASTM D 3080

124.5 99.5 25.1 25.7 98 100

0

1

2

3

4

5

6

7

8

0 0.1 0.2 0.3

Shea

r Stre

ss (k

sf)

Shear Deformation (Inches)

2 ksf 4 ksf 8 ksf

0

1

2

3

4

5

6

7

8

0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16

Shea

r Stre

ss (k

sf)

Normal Stress (ksf)

Peak: C=450 psf; ɸ=37˚

Ultimate: C=150 psf; ɸ=31˚

Normal Stress:

Appendix D - 7

 Project Name: MLK BHC Projects Tested By: ST Date: 02/11/19

 Project No.: 60595699 Computed By: JP Date: 02/12/19

 Boring No.: B-18-L2 Checked by: AP Date: 02/12/19

 Sample No.: S‐9 Depth (ft): 35

 Sample Type: Mod. Cal. Soil Description: Well‐Graded Sand Test Condition: Inundated Shear Type: Regular 

Wet             

Unit Weight   

(pcf)

Dry          

Unit Weight 

(pcf)

Initial 

Moisture 

Content (%)

Final 

Moisture 

Content (%)

Initial Degree 

Saturation 

(%)

Final Degree 

Saturation  

(%)

Normal 

Stress 

(ksf)

Peak    

Shear 

Stress (ksf)

Ultimate    

Shear 

Stress (ksf)

2 1.872 1.332

4 3.516 2.496

8 6.348 4.978

92

DIRECT SHEAR TEST RESULTSASTM D 3080

107.7 104.0 3.5 21.1 15

0

1

2

3

4

5

6

7

8

0 0.1 0.2 0.3

Shea

r Stre

ss (k

sf)

Shear Deformation (Inches)

2 ksf 4 ksf 8 ksf

0

1

2

3

4

5

6

7

8

0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16

Shea

r Stre

ss (k

sf)

Normal Stress (ksf)

Peak: C=400 psf; ɸ=36˚

Ultimate: C=150 psf; ɸ=31˚

Normal Stress:

Appendix D - 8

EXPANSION INDEX TEST RESULTSASTM D 4829

Client Name: AECOM AP Job No.: 19-0206 Project Name: MLK BHC Projects Date: 02/11/19 Project No.: 60595699

Boring Sample Depth Soil Description Molded Molded Init. Degree Measured CorrectedNo. No. (ft) Dry Density Moisture Saturation Expansion Expansion

(pcf) Content (%) (%) Index Index

B-18-L1 B-1 0-5 Sandy Clay 112.6 9.3 50.4 46 47

ASTM EXPANSION CLASSIFICATIONExpansion Index Classification

0-20 V. Low21-50 Low51-90 Medium

91-130 High>130 V. High

Appendix D - 9

Initial Dry Unit Weight (pcf): 101.5Boring No. : B-18-L1

Sample No.: S-6 Initial Moisture Content (%): 22.0

Depth (feet): 30 Final Moisture Content (%): 23.6

Sample Type: Mod Cal Assumed Specific Gravity: 2.7

Soil Description: Silt w/sand Initial Void Ratio: 0.66

Remarks: Swell= 0.18% upon inundation

Project Name: MLK BHC ProjectsProject No.: 60595699Date:

AP No: 19-0206 Figure No: 1

CONSOLIDATION CURVEASTM D 2435 2/6/2019

0

1

2

3

4

5

6

7

8

0.1 1 10 100

VERTICAL STRESS (ksf)

CO

NSO

LID

ATI

ON

(Per

cent

of S

ampl

e Th

ickn

ess)

At Field Moisture After Saturation

Appendix D - 10

Boring No. : B-18-L2 Initial Dry Unit Weight (pcf): 113.7

Sample No.: S-5 Initial Moisture Content (%): 14.9

Depth (feet): 15 Final Moisture Content (%): 15.4

Sample Type: Mod Cal Assumed Specific Gravity: 2.7

Soil Description: Silty Sand Initial Void Ratio: 0.48

Remarks: Collapse= 0.01% upon inundation

Project Name: MLK BHC ProjectsProject No.: 60595699Date:

AP No: 19-0206 Figure No: 1

CONSOLIDATION CURVEASTM D 2435 2/6/2019

0

1

2

3

4

5

6

7

8

0.1 1 10 100

VERTICAL STRESS (ksf)

CO

NSO

LID

ATI

ON

(Per

cent

of S

ampl

e Th

ickn

ess)

At Field Moisture After Saturation

Appendix D - 11

COMPACTION TESTClient: AECOM AP Number: 19-0206Project Name: MLK BHC Projects Tested By: AM Date: 02/11/19Project No. : 60595699 Calculated By: JP Date: 02/12/19

Checked By: AP Date: 02/12/19Depth(ft.): 0-5

Boring No.: B-18-L1 Sample No.: B-1 Visual Sample Description: Sandy Clay

Compaction Method X ASTM D1557 ASTM D698

METHOD A Preparation Method MoistMOLD VOLUME (CU.FT) 0.0333 X Dry

Wt. Comp. Soil + Mold (gm.) 3876 3844 3790 3681

Wt. of Mold (gm.) 1837 1837 1837 1837

Net Wt. of Soil (gm.) 2039 2007 1953 1844

Container No.

Wt. of Container (gm.) 149.87 152.15 136.50 132.80

Wet Wt. of Soil + Cont. (gm.) 339.34 371.81 380.46 404.99

Dry Wt. of Soil + Cont. (gm.) 321.34 348.07 362.90 390.66

Moisture Content (%) 10.50 12.12 7.76 5.56

Wet Density (pcf) 134.85 132.71 129.17 121.92

Dry Density (pcf) 122.04 118.36 119.87 115.51

Maximum Dry Density (pcf) 122.2 Optimum Moisture Content (%) 9.9 Maximum Dry Density w/ Rock Correction (pcf) N/A Optimum Moisture Content w/ Rock Correction (%) N/A

PROCEDURE USEDX METHOD A: Percent of Oversize: 3.3%

Soil Passing No. 4 (4.75 mm) Sieve Mold : 4 in. (101.6 mm) diameter Layers : 5 (Five) Blows per layer : 25 (twenty-five)

METHOD B: Percent of Oversize: N/A

Soil Passing 3/8 in. (9.5 mm) Sieve Mold : 4 in. (101.6 mm) diameter Layers : 5 (Five) Blows per layer : 25 (twenty-five)

METHOD C: Percent of Oversize: N/A

Soil Passing 3/4 in. (19.0 mm) Sieve Mold : 6 in. (152.4 mm) diameter Layers : 5 (Five) Blows per layer : 56 (fifty-six)

100

110

120

130

140

0 10 20 30 40

Dry

Den

sity

(pcf

)

Moisture (%)

100% Saturation @ S.G.= 2.6100% Saturation @ S.G.= 2.7100% Saturation @ S.G.= 2.8

Appendix D - 12

COMPACTION TESTClient: AECOM AP Number: 19-0206Project Name: MLK BHC Projects Tested By: AM Date: 02/11/19Project No. : 60595699 Calculated By: JP Date: 02/12/19

Checked By: AP Date: 02/12/19Depth(ft.): 0-5

Boring No.: B-18-L2 Sample No.: B-1 Visual Sample Description: Sandy Silt

Compaction Method X ASTM D1557 ASTM D698

METHOD A Preparation Method MoistMOLD VOLUME (CU.FT) 0.0333 X Dry

Wt. Comp. Soil + Mold (gm.) 3885 3835 3820 3702

Wt. of Mold (gm.) 1837 1837 1837 1837

Net Wt. of Soil (gm.) 2048 1998 1983 1865

Container No.

Wt. of Container (gm.) 151.03 138.85 142.18 135.17

Wet Wt. of Soil + Cont. (gm.) 358.93 366.42 374.78 382.56

Dry Wt. of Soil + Cont. (gm.) 334.46 336.03 352.49 364.22

Moisture Content (%) 13.34 15.41 10.60 8.01

Wet Density (pcf) 135.42 132.14 131.12 123.35

Dry Density (pcf) 119.48 114.50 118.55 114.20

Maximum Dry Density (pcf) 120.1 Optimum Moisture Content (%) 12.2 Maximum Dry Density w/ Rock Correction (pcf) N/A Optimum Moisture Content w/ Rock Correction (%) N/A

PROCEDURE USEDX METHOD A: Percent of Oversize: 1.2%

Soil Passing No. 4 (4.75 mm) Sieve Mold : 4 in. (101.6 mm) diameter Layers : 5 (Five) Blows per layer : 25 (twenty-five)

METHOD B: Percent of Oversize: N/A

Soil Passing 3/8 in. (9.5 mm) Sieve Mold : 4 in. (101.6 mm) diameter Layers : 5 (Five) Blows per layer : 25 (twenty-five)

METHOD C: Percent of Oversize: N/A

Soil Passing 3/4 in. (19.0 mm) Sieve Mold : 6 in. (152.4 mm) diameter Layers : 5 (Five) Blows per layer : 56 (fifty-six)

100

110

120

130

140

0 10 20 30 40

Dry

Den

sity

(pcf

)

Moisture (%)

100% Saturation @ S.G.= 2.6100% Saturation @ S.G.= 2.7100% Saturation @ S.G.= 2.8

Appendix D - 13

Depth (ft.): 0-5

Project Name: MLK BHC Projects Project Number: 60595699 Boring No.: B-18-L1Sample No.: B-1Location: N/ASoil Description: Sandy ClayMold Number D E FWater Added, g 20 -5 -10Compact Moisture(%) 16.7 13.9 13.4Compaction Gage Pressure, psi 60 100 250Exudation Pressure, psi 124 370 500Sample Height, Inches 2.5 2.4 2.3Gross Weight Mold, g 3025 2991 2902Tare Weight Mold, g 1964 1954 1868Net Sample Weight, g 1061 1036 1033Expansion, inchesx10-4 4 20 57Stability 2,000 (160 psi) 50/118 48/114 36/96Turns Displacement 4.39 3.90 3.89R-Value Uncorrected 17 21 30R-Value Corrected 17 20 26Dry Density, pcf 110.2 114.8 120.1Traffic Index 8.0 8.0 8.0G.E. by Stability 1.59 1.53 1.41G.E. by Expansion 0.01 0.07 0.19

Date:

02/06/19

02/12/19Checked By:

STKMAP

R-VALUE TEST DATAASTM D2844

Tested By:Computed By: 02/10/19

Date:Date:

Gf = 1.34, and 0.0 % Retained on the ¾"

*Not ApplicableRem

arks

By Exudation:

By Expansion:

At Equilibrium:

(by Exudation)

R-V

ALU

E

19

*N/A

19

0

10

20

30

40

50

60

70

80

90

100

0100200300400500600700800

R-V

ALU

E

EXUDATION PRESSURE - PSI

0.00

1.00

2.00

3.00

4.00

0.00 1.00 2.00 3.00 4.00

CO

VER

TH

ICKN

ESS

BY S

TABI

LOM

ETER

(FT.

)

COVER THICKNESS BY EXPANSION (FT.)

Appendix D - 14

Depth (ft.): 0-5

Project Name: MLK BHC Projects Project Number: 60595699 Boring No.: B-18-L2Sample No.: B-1Location: N/ASoil Description: Sandy SiltMold Number A B CWater Added, g -5 -10 -30Compact Moisture(%) 22.6 22.0 19.6Compaction Gage Pressure, psi 50 50 150Exudation Pressure, psi 104 212 336Sample Height, Inches 2.5 2.5 2.4Gross Weight Mold, g 2984 2995 2963Tare Weight Mold, g 1967 1966 1968Net Sample Weight, g 1017 1029 995Expansion, inchesx10-4 2 6 8Stability 2,000 (160 psi) 64/140 58/132 50/120Turns Displacement 4.68 4.67 4.52R-Value Uncorrected 7 10 16R-Value Corrected 7 10 15Dry Density, pcf 100.6 102.2 105.0Traffic Index 8.0 8.0 8.0G.E. by Stability 1.78 1.72 1.62G.E. by Expansion 0.01 0.02 0.03

Date:

02/06/19

02/12/19Checked By:

STKMAP

R-VALUE TEST DATAASTM D2844

Tested By:Computed By: 02/10/19

Date:Date:

Gf = 1.34, and 0.0 % Retained on the ¾"

*Not ApplicableRem

arks

By Exudation:

By Expansion:

At Equilibrium:

(by Exudation)

R-V

ALU

E

14

*N/A

14

0

10

20

30

40

50

60

70

80

90

100

0100200300400500600700800

R-V

ALU

E

EXUDATION PRESSURE - PSI

0.00

1.00

2.00

3.00

4.00

0.00 1.00 2.00 3.00 4.00

CO

VER

TH

ICKN

ESS

BY S

TABI

LOM

ETER

(FT.

)

COVER THICKNESS BY EXPANSION (FT.)

Appendix D - 15

CORROSION TEST RESULTS

Client Name: AECOM AP Job No.: 19-0206 Project Name: MLK BHC Projects Date: 02/11/19 Project No.: 60595699

Boring Sample Depth Soil Type pH Sulfate Content Chloride Content No. No. (feet) (ppm) (ppm)

B-18-L1 B-1 0-5 CL 8.3 294 55

B-18-L2 B-1 0-5 ML 9.1 51 37

NOTES: Resistivity Test and pH: California Test Method 643Sulfate Content : California Test Method 417Chloride Content : California Test Method 422ND = Not DetectableNA = Not Sufficient SampleNR = Not Requested

MinimumResistivity (ohm-cm)

1169

3515

Appendix D - 16

APPENDIX E LIQUEFACTION/SEISMIC SETTLEMENT ANALYSES

APPENDIX E LIQUEFACTION/SEISMIC SETTLEMENT ANALYSES

The liquefaction potential evaluation was generally based on the approaches recommended by R. B. Seed, et al. (2003) for a unified and consistent framework to evaluate liquefaction. The comprehensive efforts by Seed et al. (2003) summarized recent advances in the liquefaction engineering topics based on a recent database. This approach meets the requirements in the California Geological Survey (CGS; formerly California Division of Mines and Geology [CDMG]) Special Publication 117A (2008). The simplified liquefaction evaluation procedure involves the following basic steps:

1. An estimate is made of the cyclic stress ratio (CSR) caused by given earthquake ground motions at different depths using a simplified approach. The intensity of ground shaking, the duration of shaking, and the variations of induced shear stresses with depth are incorporated into the evaluation.

2. An estimate is then made of cyclic resistance ratio (CRR), indicative of the liquefaction resistance of the site subsurface soils. Recommendations were provided to estimate CRR from standard penetration test (SPT) blow counts.

The procedure can provide a deterministic index, namely a factor of safety (FS), comparing of the CRR and CSR to evaluate the potential zone of liquefaction in the soil deposit. The FS against liquefaction is defined as FS = CRR/CSR. Potential zones of liquefaction correspond to soil layers where FS is less than 1. In addition to the FS, the procedure can provide the probabilistic evaluation for liquefaction potential.

SIMPLIFIED PROCEDURES BASED ON SPT BLOWCOUNTS

The use of standard penetration test (SPT) blow counts in liquefaction potential evaluation is considered to be appropriate because many factors affecting the liquefaction potential of sandy soils affect the SPT blow count in a similar way. Among several SPT-based approaches, the procedure proposed by Seed, et al. (2003) was adopted in this analysis because it was developed more recently and based on a larger database, which consisted of modern field records, than previous approaches.

Initially, the subsurface soils that consisted of fine-grained materials (silts and clays) were evaluated to screen out the non-liquefiable fine-grained soils. The silts and clays (including the soils containing more than 20 percent fines with plasticity index [PI] higher than 12 percent or soils consisting of fines more than 35 percent fines with PI less than 12 percent) were categorized into three groups based on the following criteria:

· Zone A: soils with PI less than 12 percent and liquid limit (LL) less than 37 percent were considered potentially susceptible to cyclically induced liquefaction if the in-situ moisture content was more than 80 percent of the LL.

· Zone B: soils with PI less than 20 percent and LL less than 47 percent may be liquefiable if the in-situ moisture content was more than 85 percent of the LL.

· Zone C: soils outside zones A and B were generally not considered susceptible to classic cyclic liquefaction, but should be checked for potential loss of strength with remolding or monotonic accumulation of shear deformation.

The liquefaction potential of the soils classified as Zones A or B was then estimated based on the following procedures recommended for the sandy soils. The soils classified as Zone C were not included in this liquefaction analysis; however, other evaluations were performed on those Zone C clays/silts, which may be vulnerable to strength loss during shaking.

The CSR, generally based on the earthquake magnitude, shaking intensity (maximum ground acceleration), and overall soil conditions (average shear wave velocity at depths within approximately 50 feet below the ground surface), was then adjusted by a duration weighting factor (DWFM), which was correlated to the

APPENDIX E LIQUEFACTION/SEISMIC SETTLEMENT ANALYSES

design earthquake magnitude, and an effective overburden stress factor (Ks) to a fully normalized value at a magnitude of 7.5 and effective overburden stress of 1 atmosphere (atm; approximately 1 ton per square foot [tsf]).

Either the CRR or probability of liquefaction potential can be evaluated using the SPT blow count data of potentially liquefiable sandy soils (including the fine-grained material classified as Zones A and B). Normalized clean sand SPT blow counts, N1,60cs, were obtained by modifying the field SPT blow counts. The modifications included normalizing to an overburden pressure of 1 atm and corrections for hammer energy, borehole diameter, rod length, the lining (or lack of lining) of SPT samplers, and fines content (percent passing No. 200 sieve). An expression was presented in the procedure for CRR for a given earthquake magnitude and probability, as a function of (N1)60cs and effective overburden stress. For the deterministic approach, the threshold was set at a probability of 15 percent in this analysis. The FS can be obtained using the pairs of CRR and CSR. In addition to CRR, probabilities at a given earthquake magnitude can be calculated directly as a function of (N1)60cs, CSR, and effective overburden stress.

ANALYSES

Calculations for liquefaction potential evaluation was based on the design event with a peak ground acceleration (PGA) of 0.636g and corresponding moment magnitude of 6.61. The PGA was based on the full mapped maximum considered earthquake geometric mean (MCEG) and the corresponding modal magnitude was the result of deaggregation using USGS online tool (USGS, 2008). The design groundwater level was assumed at elevation 78 feet MSL, which was based on the original historical high data developed for the current State Seismic Hazard Map and Report (CGS, 1999 and 2001b; Mendenhall, 1905).

SEISMIC SETTLEMENT

Liquefaction-induced settlement on level ground at the existing ground surface was estimated based on procedures presented by Tokimatsu and Seed (1987) for the SPT method. The dry sand and liquefaction-induced settlement were based on design high groundwater (more conservative for liquefaction condition) and existing low groundwater level during field exploration (more conservative for dry sand settlement). The total seismic-induced settlement is up to 2 inch for either scenario. The dry sand and liquefaction induced settlement calculations are attached at the end of this appendix.

SHEET 1 1PROJECT NO.DATECOMPUTED BYCHECKED BY

PROJECT: MLK CLINICAL LAB AND RED BAG STORAGE AREA: HIGH GWSUBJECT:

Soil Unit Weight (pcf) = 120Groundwater level for liquefaction analysis (feet) = 12.3Peak Ground Acceleration (g) = 0.634Earthquake Magnitude = 6.7 Total Settlement (inches): 0.000

Equn 16 Equn 15 Equn 14 Equn 12, if Ic <2.6 Equn 14 Equn 12, if Ic >2.6 Equn 14 Equn 19 Equn 18 Equn 11 Reduction Factor

Equn2 Equn 1

Adjust Column "U" by Magnitude scaling factor

CPT Depth Tip Sleeve DEPTH TO DEPTH TOTAL EFFECTIVE F Q Ic qc1N Ic qc1N Ic Kc qc1ncs RESISTANCE rd

EFFECTIVE PRESSURE

DURING DEV DEV. STRESS FACTORResistance Resistance WATER PRESSURE PRESSURE n=1 n=0.5 n=0.7 STRESS LIQUEFACTION STRESS RATIO OF

(No.) (m) (tsf) (tsf) (feet) (feet) (tsf) (tsf) RATIO (tsf) RATIO M=7.5 SAFETY

C-LC3 0.020 7.23 4.6826 17 0.066 0.00 0.00 64.80 1824.76 3.04 Clayey #VALUE! #VALUE! #VALUE! #VALUE! #VALUE! #VALUE! 1.00 0.00 4.120 3.088 Above GroundwaterC-LC3 0.041 56.15 6.0222 17 0.133 0.01 0.01 10.73 7035.34 2.28 628.56 2.35 628.56 2.35 2.11 1329.042 1.000 1.00 0.01 4.120 3.088 Above GroundwaterC-LC3 0.061 122.73 8.3104 17 0.201 0.01 0.01 6.77 10175.62 2.12 1117.58 2.09 1117.58 2.09 1.44 1613.028 1.000 1.00 0.01 4.119 3.087 Above GroundwaterC-LC3 0.081 210.49 11.4474 17 0.265 0.02 0.02 5.44 13237.36 2.06 1669.29 1.97 1669.29 1.97 1.26 2110.036 1.000 1.00 0.02 4.118 3.087 Above GroundwaterC-LC3 0.100 244.25 12.0233 17 0.329 0.02 0.02 4.92 12372.35 2.01 1738.45 1.93 1738.45 1.93 1.21 2111.056 1.000 1.00 0.02 4.118 3.086 Above GroundwaterC-LC3 0.129 244.3 9.2115 17 0.423 0.03 0.03 3.77 9624.69 1.87 1533.48 1.82 1533.48 1.82 1.12 1718.436 1.000 1.00 0.03 4.117 3.086 Above GroundwaterC-LC3 0.140 244.34 8.3686 17 0.46 0.03 0.03 3.43 8851.90 1.82 1470.75 1.78 1470.75 1.78 1.09 1607.175 1.000 1.00 0.03 4.117 3.085 Above GroundwaterC-LC3 0.163 268.97 7.6334 17 0.534 0.03 0.03 2.84 8393.82 1.73 1502.65 1.70 1502.65 1.70 1.04 1558.065 1.000 1.00 0.03 4.116 3.085 Above GroundwaterC-LC3 0.183 330.81 6.42 17 0.601 0.04 0.04 1.94 9172.88 1.59 1742.07 1.53 1742.07 1.53 1.00 1742.071 1.000 1.00 0.04 4.115 3.084 Above GroundwaterC-LC3 0.202 442.78 4.5143 17 0.662 0.04 0.04 1.02 11146.53 1.36 2221.69 1.23 2221.69 1.23 1.00 2221.690 1.000 1.00 0.04 4.115 3.084 Above GroundwaterC-LC3 0.222 538.29 4.2658 17 0.728 0.04 0.04 0.79 12322.49 1.28 2575.58 1.12 2575.58 1.12 1.00 2575.580 1.000 1.00 0.04 4.114 3.083 Above GroundwaterC-LC3 0.244 522.61 3.7815 17 0.8 0.05 0.05 0.72 10886.71 1.22 2385.38 1.08 2385.38 1.08 1.00 2385.377 1.000 1.00 0.05 4.113 3.083 Above GroundwaterC-LC3 0.264 454.14 3.4769 17 0.866 0.05 0.05 0.77 8739.18 1.20 1992.30 1.12 1992.30 1.12 1.00 1992.302 1.000 1.00 0.05 4.113 3.082 Above GroundwaterC-LC3 0.284 390.32 3.1579 17 0.932 0.06 0.06 0.81 6978.97 1.19 1650.58 1.16 1650.58 1.16 1.00 1650.582 1.000 1.00 0.06 4.112 3.082 Above GroundwaterC-LC3 0.302 285.68 2.8889 17 0.992 0.06 0.06 1.01 4798.73 1.24 1170.98 1.29 1170.98 1.29 1.00 1170.977 1.000 1.00 0.06 4.111 3.081 Above GroundwaterC-LC3 0.324 246.49 2.6247 17 1.063 0.06 0.06 1.07 3863.69 1.25 976.02 1.34 976.02 1.34 1.00 976.016 1.000 1.00 0.06 4.111 3.081 Above GroundwaterC-LC3 0.343 201.36 2.5543 17 1.126 0.07 0.07 1.27 2979.46 1.32 774.69 1.45 774.69 1.45 1.00 774.691 1.000 1.00 0.07 4.110 3.080 Above GroundwaterC-LC3 0.365 173.54 2.5533 17 1.196 0.07 0.07 1.47 2417.34 1.39 647.83 1.54 647.83 1.54 1.00 647.826 1.000 1.00 0.07 4.110 3.080 Above GroundwaterC-LC3 0.385 150.2 2.5524 17 1.262 0.08 0.08 1.70 1982.62 1.46 545.84 1.63 545.84 1.63 1.00 545.839 1.000 1.00 0.08 4.109 3.079 Above GroundwaterC-LC3 0.403 130.05 2.6068 17 1.321 0.08 0.08 2.01 1639.80 1.54 461.94 1.72 461.94 1.72 1.05 486.332 1.000 1.00 0.08 4.108 3.079 Above GroundwaterC-LC3 0.423 111.79 2.7697 17 1.387 0.08 0.08 2.48 1342.31 1.65 387.52 1.84 387.52 1.84 1.14 440.446 1.000 1.00 0.08 4.108 3.079 Above GroundwaterC-LC3 0.441 94.31 2.9546 17 1.447 0.09 0.09 3.14 1085.27 1.77 320.07 1.97 320.07 1.97 1.26 403.747 1.000 1.00 0.09 4.107 3.078 Above GroundwaterC-LC3 0.462 81.91 3.0725 17 1.517 0.09 0.09 3.76 898.91 1.87 271.50 2.07 271.50 2.07 1.41 381.931 1.000 1.00 0.09 4.106 3.078 Above GroundwaterC-LC3 0.482 75.36 2.9828 17 1.581 0.09 0.09 3.96 793.43 1.91 244.68 2.12 244.68 2.12 1.48 362.918 1.000 1.00 0.09 4.106 3.077 Above GroundwaterC-LC3 0.503 67.87 2.8012 17 1.649 0.10 0.10 4.13 684.97 1.94 215.77 2.16 215.77 2.16 1.57 339.343 1.000 1.00 0.10 4.105 3.077 Above GroundwaterC-LC3 0.524 60.98 2.6303 17 1.72 0.10 0.10 4.32 589.89 1.98 189.82 2.21 189.82 2.21 1.68 318.849 1.000 1.00 0.10 4.104 3.076 Above GroundwaterC-LC3 0.543 56.58 2.3657 17 1.78 0.11 0.11 4.19 528.78 1.99 173.13 2.22 173.13 2.22 1.71 295.477 1.000 1.00 0.11 4.104 3.076 Above GroundwaterC-LC3 0.562 54 1.9366 17 1.843 0.11 0.11 3.59 487.33 1.94 162.39 2.18 162.39 2.18 1.61 261.761 1.000 1.00 0.11 4.103 3.075 Above GroundwaterC-LC3 0.581 52.45 1.8691 17 1.906 0.11 0.11 3.57 457.64 1.95 155.10 2.19 155.10 2.19 1.63 253.400 1.000 1.00 0.11 4.103 3.075 Above GroundwaterC-LC3 0.600 51.5 1.8414 17 1.969 0.12 0.12 3.58 434.92 1.96 149.83 2.20 149.83 2.20 1.66 248.387 1.000 1.00 0.12 4.102 3.074 Above GroundwaterC-LC3 0.625 51.76 1.7664 17 2.049 0.12 0.12 3.42 420.02 1.95 147.62 2.18 147.62 2.18 1.63 240.342 1.000 1.00 0.12 4.101 3.074 Above GroundwaterC-LC3 0.643 55.29 1.6789 17 2.11 0.13 0.13 3.04 435.73 1.90 155.39 2.13 155.39 2.13 1.51 234.866 1.000 1.00 0.13 4.101 3.073 Above GroundwaterC-LC3 0.665 63.22 1.708 17 2.181 0.13 0.13 2.71 482.11 1.83 174.76 2.06 174.76 2.06 1.38 241.954 1.000 0.99 0.13 4.100 3.073 Above GroundwaterC-LC3 0.685 70.8 1.8198 17 2.247 0.13 0.13 2.58 524.14 1.80 192.82 2.02 192.82 2.02 1.32 254.752 1.000 0.99 0.13 4.099 3.072 Above GroundwaterC-LC3 0.704 80.18 1.9499 17 2.31 0.14 0.14 2.44 577.50 1.76 215.37 1.97 215.37 1.97 1.26 271.496 1.000 0.99 0.14 4.099 3.072 Above GroundwaterC-LC3 0.722 86.47 2.0969 17 2.369 0.14 0.14 2.43 607.34 1.75 229.35 1.95 229.35 1.95 1.24 284.751 1.000 0.99 0.14 4.098 3.071 Above GroundwaterC-LC3 0.745 88.37 2.2892 17 2.445 0.15 0.15 2.59 601.39 1.77 230.72 1.97 230.72 1.97 1.27 292.356 1.000 0.99 0.15 4.098 3.071 Above GroundwaterC-LC3 0.762 85.52 2.4287 17 2.5 0.15 0.15 2.84 569.13 1.82 220.81 2.02 220.81 2.02 1.32 292.254 1.000 0.99 0.15 4.097 3.071 Above GroundwaterC-LC3 0.782 81.82 2.6579 17 2.566 0.15 0.15 3.25 530.44 1.89 208.52 2.08 208.52 2.08 1.42 295.995 1.000 0.99 0.15 4.096 3.070 Above GroundwaterC-LC3 0.801 85.01 2.7936 17 2.627 0.16 0.16 3.29 538.34 1.89 214.12 2.08 214.12 2.08 1.42 303.159 1.000 0.99 0.16 4.096 3.070 Above GroundwaterC-LC3 0.821 84.49 2.9349 17 2.695 0.16 0.16 3.48 521.51 1.92 210.11 2.10 210.11 2.10 1.46 306.587 1.000 0.99 0.16 4.095 3.069 Above GroundwaterC-LC3 0.841 89.74 2.9109 17 2.759 0.17 0.17 3.25 541.10 1.88 220.56 2.07 220.56 2.07 1.40 307.978 1.000 0.99 0.17 4.094 3.069 Above Groundwater

DN

60595699

NS

3/4/2019

LIQUEFACTION POTENTIAL EVALUATION - NCEER PROCEDURE

OF

CPT Liquefaction.xls,liqandset,3/4/2019

Soil Unit Weight (pcf) = 120Groundwater level for liquefaction analysis (feet) = 12.3Peak Ground Acceleration (g) = 0.634Earthquake Magnitude = 6.7 Total Settlement (inches): 0.000

Equn 16 Equn 15 Equn 14 Equn 12, if Ic <2.6 Equn 14 Equn 12, if Ic >2.6 Equn 14 Equn 19 Equn 18 Equn 11 Reduction Factor

Equn2 Equn 1

Adjust Column "U" by Magnitude scaling factor

CPT Depth Tip Sleeve DEPTH TO DEPTH TOTAL EFFECTIVE F Q Ic qc1N Ic qc1N Ic Kc qc1ncs RESISTANCE rd

EFFECTIVE PRESSURE

DURING DEV DEV. STRESS FACTORResistance Resistance WATER PRESSURE PRESSURE n=1 n=0.5 n=0.7 STRESS LIQUEFACTION STRESS RATIO OF

(No.) (m) (tsf) (tsf) (feet) (feet) (tsf) (tsf) RATIO (tsf) RATIO M=7.5 SAFETYC-LC3 0.867 99.82 2.7731 17 2.845 0.17 0.17 2.78 583.77 1.81 241.60 1.99 241.60 1.99 1.28 310.351 1.000 0.99 0.17 4.094 3.068 Above GroundwaterC-LC3 0.886 104.99 2.5853 17 2.908 0.17 0.17 2.47 600.73 1.75 251.35 1.93 251.35 1.93 1.22 307.495 1.000 0.99 0.17 4.093 3.068 Above GroundwaterC-LC3 0.907 109.47 2.3955 17 2.975 0.18 0.18 2.19 612.28 1.70 259.11 1.88 259.11 1.88 1.17 304.406 1.000 0.99 0.18 4.092 3.067 Above GroundwaterC-LC3 0.926 113.34 2.304 17 3.039 0.18 0.18 2.04 620.59 1.67 265.43 1.85 265.43 1.85 1.15 304.459 1.000 0.99 0.18 4.092 3.067 Above GroundwaterC-LC3 0.947 122.3 2.2526 17 3.107 0.19 0.19 1.84 655.05 1.62 283.26 1.80 283.26 1.80 1.11 313.693 1.000 0.99 0.19 4.091 3.066 Above GroundwaterC-LC3 0.965 113.26 2.261 17 3.167 0.19 0.19 2.00 595.04 1.67 259.82 1.85 259.82 1.85 1.15 297.776 1.000 0.99 0.19 4.091 3.066 Above GroundwaterC-LC3 0.985 110.33 2.3426 17 3.23 0.19 0.19 2.13 568.30 1.71 250.62 1.88 250.62 1.88 1.17 293.855 1.000 0.99 0.19 4.090 3.065 Above GroundwaterC-LC3 1.004 107.23 2.4979 17 3.294 0.20 0.20 2.33 541.55 1.75 241.20 1.92 241.20 1.92 1.21 292.607 1.000 0.99 0.20 4.089 3.065 Above GroundwaterC-LC3 1.024 94.22 2.6791 17 3.36 0.20 0.20 2.85 466.36 1.86 209.84 2.03 209.84 2.03 1.34 281.603 1.000 0.99 0.20 4.089 3.064 Above GroundwaterC-LC3 1.043 85.09 2.8389 17 3.422 0.21 0.21 3.34 413.43 1.94 187.79 2.12 187.79 2.12 1.48 278.464 1.000 0.99 0.21 4.088 3.064 Above GroundwaterC-LC3 1.064 80.7 3.0119 17 3.49 0.21 0.21 3.74 384.39 2.00 176.35 2.17 176.35 2.17 1.60 281.850 1.000 0.99 0.21 4.087 3.063 Above GroundwaterC-LC3 1.083 77.43 3.0867 17 3.554 0.21 0.21 4.00 362.11 2.04 167.68 2.21 167.68 2.21 1.68 282.325 1.000 0.99 0.21 4.087 3.063 Above GroundwaterC-LC3 1.103 72.52 3.0868 17 3.62 0.22 0.22 4.27 332.89 2.08 155.61 2.25 155.61 2.25 1.79 279.287 1.000 0.99 0.22 4.086 3.062 Above GroundwaterC-LC3 1.122 64.42 3.0722 17 3.68 0.22 0.22 4.79 290.76 2.15 137.09 2.32 137.09 2.32 2.02 276.599 1.000 0.99 0.22 4.086 3.062 Above GroundwaterC-LC3 1.142 56.76 2.9933 17 3.746 0.22 0.22 5.29 251.54 2.22 119.72 2.39 119.72 2.39 2.27 272.369 1.000 0.99 0.22 4.085 3.062 Above GroundwaterC-LC3 1.162 50.56 2.7635 17 3.811 0.23 0.23 5.49 220.11 2.26 105.73 2.44 105.73 2.44 2.46 260.320 1.000 0.99 0.23 4.084 3.061 Above GroundwaterC-LC3 1.180 44.01 2.5414 17 3.873 0.23 0.23 5.81 188.39 2.32 91.30 2.49 91.30 2.49 2.73 249.469 1.000 0.99 0.23 4.084 3.061 Above GroundwaterC-LC3 1.201 37.29 2.27 17 3.939 0.24 0.24 6.13 156.78 2.38 76.71 2.56 76.71 2.56 3.08 236.042 1.000 0.99 0.24 4.083 3.060 Above GroundwaterC-LC3 1.229 30.4 1.9726 17 4.032 0.24 0.24 6.54 124.66 2.46 61.81 2.64 82.09 2.56 3.10 254.661 1.000 0.99 0.24 4.082 3.060 Above GroundwaterC-LC3 1.249 26.35 1.7358 17 4.097 0.25 0.25 6.65 106.19 2.50 53.15 2.69 70.36 2.61 3.38 237.915 1.000 0.99 0.25 4.082 3.059 Above GroundwaterC-LC3 1.267 23.68 1.2138 17 4.158 0.25 0.25 5.18 93.92 2.45 47.41 2.64 62.58 2.56 3.08 192.647 1.000 0.99 0.25 4.081 3.059 Above GroundwaterC-LC3 1.287 22.13 0.8225 17 4.224 0.25 0.25 3.76 86.32 2.36 43.96 2.56 43.96 2.56 3.10 136.187 0.315 0.99 0.25 4.080 3.058 Above GroundwaterC-LC3 1.305 21.27 0.7809 17 4.283 0.26 0.26 3.72 81.77 2.37 41.96 2.57 41.96 2.57 3.16 132.636 0.297 0.99 0.26 4.080 3.058 Above GroundwaterC-LC3 1.326 20.41 0.7739 17 4.35 0.26 0.26 3.84 77.20 2.40 39.95 2.60 39.95 2.60 3.31 132.302 0.295 0.99 0.26 4.079 3.057 Above GroundwaterC-LC3 1.344 19.21 0.7987 17 4.411 0.26 0.26 4.22 71.58 2.45 37.34 2.65 48.71 2.57 3.12 152.005 0.407 0.99 0.26 4.079 3.057 Above GroundwaterC-LC3 1.363 18.26 0.8208 17 4.473 0.27 0.27 4.56 67.04 2.50 35.25 2.69 45.85 2.61 3.38 154.846 0.425 0.99 0.27 4.078 3.056 Above GroundwaterC-LC3 1.385 16.11 0.8167 17 4.543 0.27 0.27 5.16 58.10 2.58 30.86 2.77 40.02 2.69 3.91 156.305 0.435 0.99 0.27 4.077 3.056 Above GroundwaterC-LC3 1.401 15.59 0.7893 17 4.595 0.28 0.28 5.15 55.55 2.59 29.69 2.78 38.42 2.70 3.99 153.426 0.416 0.99 0.28 4.077 3.055 Above GroundwaterC-LC3 1.424 15.85 0.7317 17 4.672 0.28 0.28 4.70 55.54 2.56 29.94 2.75 38.61 2.67 3.78 145.951 0.369 0.99 0.28 4.076 3.055 Above GroundwaterC-LC3 1.443 16.97 0.6691 17 4.733 0.28 0.28 4.01 58.76 2.49 31.84 2.68 40.96 2.60 3.34 136.974 0.319 0.99 0.28 4.076 3.054 Above GroundwaterC-LC3 1.462 18.86 0.5936 17 4.798 0.29 0.29 3.20 64.51 2.39 35.15 2.58 35.15 2.58 3.23 113.515 0.216 0.99 0.29 4.075 3.054 Above GroundwaterC-LC3 1.482 20.41 0.5227 17 4.861 0.29 0.29 2.60 68.98 2.31 37.79 2.50 37.79 2.50 2.77 104.780 0.187 0.99 0.29 4.074 3.054 Above GroundwaterC-LC3 1.500 21.53 0.4549 17 4.922 0.30 0.30 2.14 71.90 2.24 39.62 2.43 39.62 2.43 2.44 96.811 0.164 0.99 0.30 4.074 3.053 Above Groundwater

CPT Liquefaction.xls,liqandset,3/4/2019

SHEET 1 1PROJECT NO.DATECOMPUTED BYCHECKED BY

PROJECT: MLK CLINICAL LAB AND RED BAG STORAGE: LOW GWSUBJECT:

Soil Unit Weight (pcf) = 120Groundwater level for liquefaction analysis (feet) = 12.3Peak Ground Acceleration (g) = 0.634Earthquake Magnitude = 6.7 Total Settlement (inches): 0.000

Equn 16 Equn 15 Equn 14 Equn 12, if Ic <2.6 Equn 14 Equn 12, if Ic >2.6 Equn 14 Equn 19 Equn 18 Equn 11 Reduction Factor

Equn2 Equn 1

Adjust Column "U" by Magnitude scaling factor

CPT Depth Tip Sleeve DEPTH TO DEPTH TOTAL EFFECTIVE F Q Ic qc1N Ic qc1N Ic Kc qc1ncs RESISTANCE rd

EFFECTIVE PRESSURE

DURING DEV DEV. STRESS FACTORResistance Resistance WATER PRESSURE PRESSURE n=1 n=0.5 n=0.7 STRESS LIQUEFACTION STRESS RATIO OF

(No.) (m) (tsf) (tsf) (feet) (feet) (tsf) (tsf) RATIO (tsf) RATIO M=7.5 SAFETY

C-LC3 0.020 7.23 4.6826 50 0.066 0.00 0.00 64.80 1824.76 3.04 Clayey #VALUE! #VALUE! #VALUE! #VALUE! #VALUE! #VALUE! 1.00 0.00 4.120 3.088 Above GroundwaterC-LC3 0.041 56.15 6.0222 50 0.133 0.01 0.01 10.73 7035.34 2.28 628.56 2.35 628.56 2.35 2.11 1329.042 1.000 1.00 0.01 4.120 3.088 Above GroundwaterC-LC3 0.061 122.73 8.3104 50 0.201 0.01 0.01 6.77 10175.62 2.12 1117.58 2.09 1117.58 2.09 1.44 1613.028 1.000 1.00 0.01 4.119 3.087 Above GroundwaterC-LC3 0.081 210.49 11.4474 50 0.265 0.02 0.02 5.44 13237.36 2.06 1669.29 1.97 1669.29 1.97 1.26 2110.036 1.000 1.00 0.02 4.118 3.087 Above GroundwaterC-LC3 0.100 244.25 12.0233 50 0.329 0.02 0.02 4.92 12372.35 2.01 1738.45 1.93 1738.45 1.93 1.21 2111.056 1.000 1.00 0.02 4.118 3.086 Above GroundwaterC-LC3 0.129 244.3 9.2115 50 0.423 0.03 0.03 3.77 9624.69 1.87 1533.48 1.82 1533.48 1.82 1.12 1718.436 1.000 1.00 0.03 4.117 3.086 Above GroundwaterC-LC3 0.140 244.34 8.3686 50 0.46 0.03 0.03 3.43 8851.90 1.82 1470.75 1.78 1470.75 1.78 1.09 1607.175 1.000 1.00 0.03 4.117 3.085 Above GroundwaterC-LC3 0.163 268.97 7.6334 50 0.534 0.03 0.03 2.84 8393.82 1.73 1502.65 1.70 1502.65 1.70 1.04 1558.065 1.000 1.00 0.03 4.116 3.085 Above GroundwaterC-LC3 0.183 330.81 6.42 50 0.601 0.04 0.04 1.94 9172.88 1.59 1742.07 1.53 1742.07 1.53 1.00 1742.071 1.000 1.00 0.04 4.115 3.084 Above GroundwaterC-LC3 0.202 442.78 4.5143 50 0.662 0.04 0.04 1.02 11146.53 1.36 2221.69 1.23 2221.69 1.23 1.00 2221.690 1.000 1.00 0.04 4.115 3.084 Above GroundwaterC-LC3 0.222 538.29 4.2658 50 0.728 0.04 0.04 0.79 12322.49 1.28 2575.58 1.12 2575.58 1.12 1.00 2575.580 1.000 1.00 0.04 4.114 3.083 Above GroundwaterC-LC3 0.244 522.61 3.7815 50 0.8 0.05 0.05 0.72 10886.71 1.22 2385.38 1.08 2385.38 1.08 1.00 2385.377 1.000 1.00 0.05 4.113 3.083 Above GroundwaterC-LC3 0.264 454.14 3.4769 50 0.866 0.05 0.05 0.77 8739.18 1.20 1992.30 1.12 1992.30 1.12 1.00 1992.302 1.000 1.00 0.05 4.113 3.082 Above GroundwaterC-LC3 0.284 390.32 3.1579 50 0.932 0.06 0.06 0.81 6978.97 1.19 1650.58 1.16 1650.58 1.16 1.00 1650.582 1.000 1.00 0.06 4.112 3.082 Above GroundwaterC-LC3 0.302 285.68 2.8889 50 0.992 0.06 0.06 1.01 4798.73 1.24 1170.98 1.29 1170.98 1.29 1.00 1170.977 1.000 1.00 0.06 4.111 3.081 Above GroundwaterC-LC3 0.324 246.49 2.6247 50 1.063 0.06 0.06 1.07 3863.69 1.25 976.02 1.34 976.02 1.34 1.00 976.016 1.000 1.00 0.06 4.111 3.081 Above GroundwaterC-LC3 0.343 201.36 2.5543 50 1.126 0.07 0.07 1.27 2979.46 1.32 774.69 1.45 774.69 1.45 1.00 774.691 1.000 1.00 0.07 4.110 3.080 Above GroundwaterC-LC3 0.365 173.54 2.5533 50 1.196 0.07 0.07 1.47 2417.34 1.39 647.83 1.54 647.83 1.54 1.00 647.826 1.000 1.00 0.07 4.110 3.080 Above GroundwaterC-LC3 0.385 150.2 2.5524 50 1.262 0.08 0.08 1.70 1982.62 1.46 545.84 1.63 545.84 1.63 1.00 545.839 1.000 1.00 0.08 4.109 3.079 Above GroundwaterC-LC3 0.403 130.05 2.6068 50 1.321 0.08 0.08 2.01 1639.80 1.54 461.94 1.72 461.94 1.72 1.05 486.332 1.000 1.00 0.08 4.108 3.079 Above GroundwaterC-LC3 0.423 111.79 2.7697 50 1.387 0.08 0.08 2.48 1342.31 1.65 387.52 1.84 387.52 1.84 1.14 440.446 1.000 1.00 0.08 4.108 3.079 Above GroundwaterC-LC3 0.441 94.31 2.9546 50 1.447 0.09 0.09 3.14 1085.27 1.77 320.07 1.97 320.07 1.97 1.26 403.747 1.000 1.00 0.09 4.107 3.078 Above GroundwaterC-LC3 0.462 81.91 3.0725 50 1.517 0.09 0.09 3.76 898.91 1.87 271.50 2.07 271.50 2.07 1.41 381.931 1.000 1.00 0.09 4.106 3.078 Above GroundwaterC-LC3 0.482 75.36 2.9828 50 1.581 0.09 0.09 3.96 793.43 1.91 244.68 2.12 244.68 2.12 1.48 362.918 1.000 1.00 0.09 4.106 3.077 Above GroundwaterC-LC3 0.503 67.87 2.8012 50 1.649 0.10 0.10 4.13 684.97 1.94 215.77 2.16 215.77 2.16 1.57 339.343 1.000 1.00 0.10 4.105 3.077 Above GroundwaterC-LC3 0.524 60.98 2.6303 50 1.72 0.10 0.10 4.32 589.89 1.98 189.82 2.21 189.82 2.21 1.68 318.849 1.000 1.00 0.10 4.104 3.076 Above GroundwaterC-LC3 0.543 56.58 2.3657 50 1.78 0.11 0.11 4.19 528.78 1.99 173.13 2.22 173.13 2.22 1.71 295.477 1.000 1.00 0.11 4.104 3.076 Above GroundwaterC-LC3 0.562 54 1.9366 50 1.843 0.11 0.11 3.59 487.33 1.94 162.39 2.18 162.39 2.18 1.61 261.761 1.000 1.00 0.11 4.103 3.075 Above GroundwaterC-LC3 0.581 52.45 1.8691 50 1.906 0.11 0.11 3.57 457.64 1.95 155.10 2.19 155.10 2.19 1.63 253.400 1.000 1.00 0.11 4.103 3.075 Above GroundwaterC-LC3 0.600 51.5 1.8414 50 1.969 0.12 0.12 3.58 434.92 1.96 149.83 2.20 149.83 2.20 1.66 248.387 1.000 1.00 0.12 4.102 3.074 Above GroundwaterC-LC3 0.625 51.76 1.7664 50 2.049 0.12 0.12 3.42 420.02 1.95 147.62 2.18 147.62 2.18 1.63 240.342 1.000 1.00 0.12 4.101 3.074 Above GroundwaterC-LC3 0.643 55.29 1.6789 50 2.11 0.13 0.13 3.04 435.73 1.90 155.39 2.13 155.39 2.13 1.51 234.866 1.000 1.00 0.13 4.101 3.073 Above GroundwaterC-LC3 0.665 63.22 1.708 50 2.181 0.13 0.13 2.71 482.11 1.83 174.76 2.06 174.76 2.06 1.38 241.954 1.000 0.99 0.13 4.100 3.073 Above GroundwaterC-LC3 0.685 70.8 1.8198 50 2.247 0.13 0.13 2.58 524.14 1.80 192.82 2.02 192.82 2.02 1.32 254.752 1.000 0.99 0.13 4.099 3.072 Above GroundwaterC-LC3 0.704 80.18 1.9499 50 2.31 0.14 0.14 2.44 577.50 1.76 215.37 1.97 215.37 1.97 1.26 271.496 1.000 0.99 0.14 4.099 3.072 Above GroundwaterC-LC3 0.722 86.47 2.0969 50 2.369 0.14 0.14 2.43 607.34 1.75 229.35 1.95 229.35 1.95 1.24 284.751 1.000 0.99 0.14 4.098 3.071 Above GroundwaterC-LC3 0.745 88.37 2.2892 50 2.445 0.15 0.15 2.59 601.39 1.77 230.72 1.97 230.72 1.97 1.27 292.356 1.000 0.99 0.15 4.098 3.071 Above GroundwaterC-LC3 0.762 85.52 2.4287 50 2.5 0.15 0.15 2.84 569.13 1.82 220.81 2.02 220.81 2.02 1.32 292.254 1.000 0.99 0.15 4.097 3.071 Above GroundwaterC-LC3 0.782 81.82 2.6579 50 2.566 0.15 0.15 3.25 530.44 1.89 208.52 2.08 208.52 2.08 1.42 295.995 1.000 0.99 0.15 4.096 3.070 Above GroundwaterC-LC3 0.801 85.01 2.7936 50 2.627 0.16 0.16 3.29 538.34 1.89 214.12 2.08 214.12 2.08 1.42 303.159 1.000 0.99 0.16 4.096 3.070 Above GroundwaterC-LC3 0.821 84.49 2.9349 50 2.695 0.16 0.16 3.48 521.51 1.92 210.11 2.10 210.11 2.10 1.46 306.587 1.000 0.99 0.16 4.095 3.069 Above GroundwaterC-LC3 0.841 89.74 2.9109 50 2.759 0.17 0.17 3.25 541.10 1.88 220.56 2.07 220.56 2.07 1.40 307.978 1.000 0.99 0.17 4.094 3.069 Above Groundwater

605956993/4/2019

DNNS

LIQUEFACTION POTENTIAL EVALUATION - NCEER PROCEDURE

OF

CPT Liquefaction.xls,liqandset (2),3/4/2019

Soil Unit Weight (pcf) = 120Groundwater level for liquefaction analysis (feet) = 12.3Peak Ground Acceleration (g) = 0.634Earthquake Magnitude = 6.7 Total Settlement (inches): 0.000

Equn 16 Equn 15 Equn 14 Equn 12, if Ic <2.6 Equn 14 Equn 12, if Ic >2.6 Equn 14 Equn 19 Equn 18 Equn 11 Reduction Factor

Equn2 Equn 1

Adjust Column "U" by Magnitude scaling factor

CPT Depth Tip Sleeve DEPTH TO DEPTH TOTAL EFFECTIVE F Q Ic qc1N Ic qc1N Ic Kc qc1ncs RESISTANCE rd

EFFECTIVE PRESSURE

DURING DEV DEV. STRESS FACTORResistance Resistance WATER PRESSURE PRESSURE n=1 n=0.5 n=0.7 STRESS LIQUEFACTION STRESS RATIO OF

(No.) (m) (tsf) (tsf) (feet) (feet) (tsf) (tsf) RATIO (tsf) RATIO M=7.5 SAFETYC-LC3 0.867 99.82 2.7731 50 2.845 0.17 0.17 2.78 583.77 1.81 241.60 1.99 241.60 1.99 1.28 310.351 1.000 0.99 0.17 4.094 3.068 Above GroundwaterC-LC3 0.886 104.99 2.5853 50 2.908 0.17 0.17 2.47 600.73 1.75 251.35 1.93 251.35 1.93 1.22 307.495 1.000 0.99 0.17 4.093 3.068 Above GroundwaterC-LC3 0.907 109.47 2.3955 50 2.975 0.18 0.18 2.19 612.28 1.70 259.11 1.88 259.11 1.88 1.17 304.406 1.000 0.99 0.18 4.092 3.067 Above GroundwaterC-LC3 0.926 113.34 2.304 50 3.039 0.18 0.18 2.04 620.59 1.67 265.43 1.85 265.43 1.85 1.15 304.459 1.000 0.99 0.18 4.092 3.067 Above GroundwaterC-LC3 0.947 122.3 2.2526 50 3.107 0.19 0.19 1.84 655.05 1.62 283.26 1.80 283.26 1.80 1.11 313.693 1.000 0.99 0.19 4.091 3.066 Above GroundwaterC-LC3 0.965 113.26 2.261 50 3.167 0.19 0.19 2.00 595.04 1.67 259.82 1.85 259.82 1.85 1.15 297.776 1.000 0.99 0.19 4.091 3.066 Above GroundwaterC-LC3 0.985 110.33 2.3426 50 3.23 0.19 0.19 2.13 568.30 1.71 250.62 1.88 250.62 1.88 1.17 293.855 1.000 0.99 0.19 4.090 3.065 Above GroundwaterC-LC3 1.004 107.23 2.4979 50 3.294 0.20 0.20 2.33 541.55 1.75 241.20 1.92 241.20 1.92 1.21 292.607 1.000 0.99 0.20 4.089 3.065 Above GroundwaterC-LC3 1.024 94.22 2.6791 50 3.36 0.20 0.20 2.85 466.36 1.86 209.84 2.03 209.84 2.03 1.34 281.603 1.000 0.99 0.20 4.089 3.064 Above GroundwaterC-LC3 1.043 85.09 2.8389 50 3.422 0.21 0.21 3.34 413.43 1.94 187.79 2.12 187.79 2.12 1.48 278.464 1.000 0.99 0.21 4.088 3.064 Above GroundwaterC-LC3 1.064 80.7 3.0119 50 3.49 0.21 0.21 3.74 384.39 2.00 176.35 2.17 176.35 2.17 1.60 281.850 1.000 0.99 0.21 4.087 3.063 Above GroundwaterC-LC3 1.083 77.43 3.0867 50 3.554 0.21 0.21 4.00 362.11 2.04 167.68 2.21 167.68 2.21 1.68 282.325 1.000 0.99 0.21 4.087 3.063 Above GroundwaterC-LC3 1.103 72.52 3.0868 50 3.62 0.22 0.22 4.27 332.89 2.08 155.61 2.25 155.61 2.25 1.79 279.287 1.000 0.99 0.22 4.086 3.062 Above GroundwaterC-LC3 1.122 64.42 3.0722 50 3.68 0.22 0.22 4.79 290.76 2.15 137.09 2.32 137.09 2.32 2.02 276.599 1.000 0.99 0.22 4.086 3.062 Above GroundwaterC-LC3 1.142 56.76 2.9933 50 3.746 0.22 0.22 5.29 251.54 2.22 119.72 2.39 119.72 2.39 2.27 272.369 1.000 0.99 0.22 4.085 3.062 Above GroundwaterC-LC3 1.162 50.56 2.7635 50 3.811 0.23 0.23 5.49 220.11 2.26 105.73 2.44 105.73 2.44 2.46 260.320 1.000 0.99 0.23 4.084 3.061 Above GroundwaterC-LC3 1.180 44.01 2.5414 50 3.873 0.23 0.23 5.81 188.39 2.32 91.30 2.49 91.30 2.49 2.73 249.469 1.000 0.99 0.23 4.084 3.061 Above GroundwaterC-LC3 1.201 37.29 2.27 50 3.939 0.24 0.24 6.13 156.78 2.38 76.71 2.56 76.71 2.56 3.08 236.042 1.000 0.99 0.24 4.083 3.060 Above GroundwaterC-LC3 1.229 30.4 1.9726 50 4.032 0.24 0.24 6.54 124.66 2.46 61.81 2.64 82.09 2.56 3.10 254.661 1.000 0.99 0.24 4.082 3.060 Above GroundwaterC-LC3 1.249 26.35 1.7358 50 4.097 0.25 0.25 6.65 106.19 2.50 53.15 2.69 70.36 2.61 3.38 237.915 1.000 0.99 0.25 4.082 3.059 Above GroundwaterC-LC3 1.267 23.68 1.2138 50 4.158 0.25 0.25 5.18 93.92 2.45 47.41 2.64 62.58 2.56 3.08 192.647 1.000 0.99 0.25 4.081 3.059 Above GroundwaterC-LC3 1.287 22.13 0.8225 50 4.224 0.25 0.25 3.76 86.32 2.36 43.96 2.56 43.96 2.56 3.10 136.187 0.315 0.99 0.25 4.080 3.058 Above GroundwaterC-LC3 1.305 21.27 0.7809 50 4.283 0.26 0.26 3.72 81.77 2.37 41.96 2.57 41.96 2.57 3.16 132.636 0.297 0.99 0.26 4.080 3.058 Above GroundwaterC-LC3 1.326 20.41 0.7739 50 4.35 0.26 0.26 3.84 77.20 2.40 39.95 2.60 39.95 2.60 3.31 132.302 0.295 0.99 0.26 4.079 3.057 Above GroundwaterC-LC3 1.344 19.21 0.7987 50 4.411 0.26 0.26 4.22 71.58 2.45 37.34 2.65 48.71 2.57 3.12 152.005 0.407 0.99 0.26 4.079 3.057 Above GroundwaterC-LC3 1.363 18.26 0.8208 50 4.473 0.27 0.27 4.56 67.04 2.50 35.25 2.69 45.85 2.61 3.38 154.846 0.425 0.99 0.27 4.078 3.056 Above GroundwaterC-LC3 1.385 16.11 0.8167 50 4.543 0.27 0.27 5.16 58.10 2.58 30.86 2.77 40.02 2.69 3.91 156.305 0.435 0.99 0.27 4.077 3.056 Above GroundwaterC-LC3 1.401 15.59 0.7893 50 4.595 0.28 0.28 5.15 55.55 2.59 29.69 2.78 38.42 2.70 3.99 153.426 0.416 0.99 0.28 4.077 3.055 Above GroundwaterC-LC3 1.424 15.85 0.7317 50 4.672 0.28 0.28 4.70 55.54 2.56 29.94 2.75 38.61 2.67 3.78 145.951 0.369 0.99 0.28 4.076 3.055 Above GroundwaterC-LC3 1.443 16.97 0.6691 50 4.733 0.28 0.28 4.01 58.76 2.49 31.84 2.68 40.96 2.60 3.34 136.974 0.319 0.99 0.28 4.076 3.054 Above GroundwaterC-LC3 1.462 18.86 0.5936 50 4.798 0.29 0.29 3.20 64.51 2.39 35.15 2.58 35.15 2.58 3.23 113.515 0.216 0.99 0.29 4.075 3.054 Above GroundwaterC-LC3 1.482 20.41 0.5227 50 4.861 0.29 0.29 2.60 68.98 2.31 37.79 2.50 37.79 2.50 2.77 104.780 0.187 0.99 0.29 4.074 3.054 Above GroundwaterC-LC3 1.500 21.53 0.4549 50 4.922 0.30 0.30 2.14 71.90 2.24 39.62 2.43 39.62 2.43 2.44 96.811 0.164 0.99 0.30 4.074 3.053 Above Groundwater

CPT Liquefaction.xls,liqandset (2),3/4/2019

PROJECT NO. 60595699DATE 1/11/2016COMPUTED BY DNCHECKED BY NS

PROJECT: MLK CLINICAL LAB AND RED BAG STORAGE

SUBJECT: DRY SAND SETTLEMENT DUE TO EARTHQUAKE SHAKING: B-18-L1 HIGH GW

INPUT

CLAYS (CL,CH) and ELASTIC SILTS (MH) not considered in analyses

Cs for CAL (Sand) = 0.55Cs for CAL (Clay) = 0.7Atmospheric Pressure, Pa (ksf) = 2.116Energy Ratio (%) = 80Ground Surface Elevation (feet) = 100Depth of Groundwater (feet) = 17Peak Ground Acceleration (g) = 0.634Earthquake Magnitude Mw = 6.7

BORING SAMPLE DEPTH UNIT FIELD SOIL PI D50 BOREHOLE SAMPLE LINER TOTAL EFFECTIVE DEPTH ENERGYBORING

DIAMETER ROD SAMPLER MODIFIED RELATIVE REDUCTION φ

EFFECTIVE PRESSURE AT

DESIGN σm' Gmax γeff*Geff/Gmax n(PI) γ ε εm LAYER SETTLEMENT SETTLEMENT

ELEVATION WEIGHT BLOWCOUNT CLASSIF. DIAMETER TYPE USED PRESSURE PRESSURE FACTOR FACTOR FACTOR FACTOR FACTOR PENETR. DENSITY FACTOR (rad) WATER TABLE (kPa) (psf) (%) (%) (%) (%) (feet) LAYER TOTAL(No.) (feet) (feet) (pcf) (bl/ft) (mm) (in) (ksf) (ksf) Cn Ce=ER/60 Cb Cr Cs (N1)60 Dr (%) Rd (ksf) (in) (in)

B-18-L1 95 5 120 5 Sand 0.0 1.000 8 SPT NO 0.600 0.600 1.70 1.33 1.15 0.75 1.10 10.8 42 0.99 0.49 0.60 20 896244 0.03 0.00E+00 0.11 0.26 0.22 5 0.266B-18-L1 85 15 12 8 Sand 0.0 1.000 8 SPT NO 0.720 0.720 1.70 1.33 1.15 0.85 1.10 19.5 57 0.97 0.69 0.72 20 1097818 0.03 0.00E+00 0.10 0.15 0.12 10 0.296B-18-L1 75 25 1 18 Sand 0.0 1.000 8 SPT NO 0.730 0.106 1.70 1.33 1.15 0.95 1.10 49.0 90 0.94 0.70 0.11 3 569735 0.05 0.00E+00 413.27 Below WT Below WT 10B-18-L1 65 35 125 27 Sand 0.0 1.000 8 SPT NO 1.980 0.732 1.70 1.33 1.15 1.00 1.20 84.5 100 0.89 0.70 0.73 20 1794710 0.04 0.00E+00 0.35 Below WT Below WT 10B-18-L1 55 45 125 29 Sand 0.0 1.000 8 SPT NO 3.230 1.358 1.25 1.33 1.15 1.00 1.20 66.6 100 0.81 0.70 1.36 37 2258498 0.05 0.00E+00 0.26 Below WT Below WT 10B-18-L1 45 55 120 30 Sand 0.0 1.000 8 SPT NO 4.430 1.934 1.05 1.33 1.15 1.00 1.20 57.7 98 0.73 0.70 1.93 53 2569881 0.05 0.00E+00 0.22 Below WT Below WT 10 0.6

PROJECT NO. 60595699DATE 1/11/2016COMPUTED BY DNCHECKED BY NS

PROJECT: MLK CLINICAL LAB AND RED BAG STORAGE

SUBJECT: DRY SAND SETTLEMENT DUE TO EARTHQUAKE SHAKING: B-18-L2 HIGH GW

INPUT

CLAYS (CL,CH) and ELASTIC SILTS (MH) not considered in analyses

Cs for CAL (Sand) = 0.55Cs for CAL (Clay) = 0.7Atmospheric Pressure, Pa (ksf) = 2.116Energy Ratio (%) = 80Ground Surface Elevation (feet) = 100Depth of Groundwater (feet) = 12Peak Ground Acceleration (g) = 0.634Earthquake Magnitude Mw = 6.7

BORING SAMPLE DEPTH UNIT FIELD SOIL PI D50 BOREHOLE SAMPLE LINER TOTAL EFFECTIVE DEPTH ENERGYBORING

DIAMETER ROD SAMPLER MODIFIED RELATIVE REDUCTION φ

EFFECTIVE PRESSURE AT

DESIGN σm' Gmax γeff*Geff/Gmax n(PI) γ ε εm LAYER SETTLEMENT SETTLEMENT

ELEVATION WEIGHT BLOWCOUNT CLASSIF. DIAMETER TYPE USED PRESSURE PRESSURE FACTOR FACTOR FACTOR FACTOR FACTOR PENETR. DENSITY FACTOR (rad) WATER TABLE (kPa) (psf) (%) (%) (%) (%) (feet) LAYER TOTAL(No.) (feet) (feet) (pcf) (bl/ft) (mm) (in) (ksf) (ksf) Cn Ce=ER/60 Cb Cr Cs (N1)60 Dr (%) Rd (ksf) (in) (in)

B-18-L2 90 10 120 7 Sand 0.0 1.000 8 SPT NO 1.200 1.200 1.33 1.33 1.15 0.75 1.10 11.8 44 0.98 0.63 1.20 35 1228333 0.04 0.00E+00 0.17 0.39 0.33 10 0.787B-18-L2 80 20 120 10 Sand 0.0 1.000 8 SPT NO 2.400 1.776 1.09 1.33 1.15 0.95 1.10 17.5 54 0.95 0.65 1.78 51 1687613 0.06 0.00E+00 0.28 Below WT Below WT 10B-18-L2 70 30 120 29 Sand 0.0 1.000 8 SPT NO 3.600 2.352 0.95 1.33 1.15 0.95 1.20 48.1 90 0.93 0.70 2.35 64 2666286 0.05 0.00E+00 0.18 Below WT Below WT 10B-18-L2 60 40 120 49 Sand 0.0 1.000 8 SPT NO 4.800 2.928 0.85 1.33 1.15 1.00 1.20 76.6 100 0.85 0.70 2.93 80 3475171 0.05 0.00E+00 0.13 Below WT Below WT 10B-18-L2 50 50 120 27 Sand 0.0 1.000 8 SPT NO 6.000 3.504 0.78 1.33 1.15 1.00 1.20 38.6 80 0.77 0.70 3.50 96 3024798 0.06 0.00E+00 0.20 Below WT Below WT 10B-18-L2 40 60 120 35 Sand 0.0 1.000 8 SPT NO 7.200 4.080 0.72 1.33 1.15 1.00 1.20 46.4 88 0.69 0.70 4.08 112 3469737 0.06 0.00E+00 0.15 Below WT Below WT 10 0.8

PROJECT NO. 60595699DATE 1/11/2016COMPUTED BY DNCHECKED BY NS

PROJECT: MLK CLINICAL LAB AND RED BAG STORAGE

SUBJECT: DRY SAND SETTLEMENT DUE TO EARTHQUAKE SHAKING: B-18-L1 LOW GW

INPUT

CLAYS (CL,CH) and ELASTIC SILTS (MH) not considered in analyses

Cs for CAL (Sand) = 0.55Cs for CAL (Clay) = 0.7Atmospheric Pressure, Pa (ksf) = 2.116Energy Ratio (%) = 80Ground Surface Elevation (feet) = 100Depth of Groundwater (feet) = 50Peak Ground Acceleration (g) = 0.634Earthquake Magnitude Mw = 6.7

BORING SAMPLE DEPTH UNIT FIELD SOIL PI D50 BOREHOLE SAMPLE LINER TOTAL EFFECTIVE DEPTH ENERGYBORING

DIAMETER ROD SAMPLER MODIFIED RELATIVE REDUCTION φ

EFFECTIVE PRESSURE AT

DESIGN σm' Gmax γeff*Geff/Gmax n(PI) γ ε εm LAYER SETTLEMENT SETTLEMENT

ELEVATION WEIGHT BLOWCOUNT CLASSIF. DIAMETER TYPE USED PRESSURE PRESSURE FACTOR FACTOR FACTOR FACTOR FACTOR PENETR. DENSITY FACTOR (rad) WATER TABLE (kPa) (psf) (%) (%) (%) (%) (feet) LAYER TOTAL(No.) (feet) (feet) (pcf) (bl/ft) (mm) (in) (ksf) (ksf) Cn Ce=ER/60 Cb Cr Cs (N1)60 Dr (%) Rd (ksf) (in) (in)

B-18-L1 95 5 120 5 Sand 0.0 1.000 8 SPT NO 0.600 0.600 1.70 1.33 1.15 0.75 1.10 10.8 42 0.99 0.49 0.60 20 896244 0.03 0.00E+00 0.11 0.26 0.22 5 0.266B-18-L1 85 15 12 8 Sand 0.0 1.000 8 SPT NO 0.720 0.720 1.70 1.33 1.15 0.85 1.10 19.5 57 0.97 0.69 0.72 20 1097818 0.03 0.00E+00 0.10 0.15 0.12 10 0.296B-18-L1 75 25 1 18 Sand 0.0 1.000 8 SPT NO 0.730 0.730 1.70 1.33 1.15 0.95 1.10 49.0 90 0.94 0.70 0.73 20 1495139 0.02 0.00E+00 0.05 0.02 0.01 10 0.031B-18-L1 65 35 125 27 Sand 0.0 1.000 8 SPT NO 1.980 1.980 1.03 1.33 1.15 1.00 1.20 51.4 93 0.89 0.70 1.98 54 2500711 0.03 0.00E+00 0.07 0.02 0.02 10 0.041B-18-L1 55 45 125 29 Sand 0.0 1.000 8 SPT NO 3.230 3.230 0.81 1.33 1.15 1.00 1.20 43.2 85 0.81 0.70 3.23 88 3014769 0.04 0.00E+00 0.07 0.02 0.02 10 0.045B-18-L1 45 55 120 30 Sand 0.0 1.000 8 SPT NO 4.430 3.806 0.75 1.33 1.15 1.00 1.20 41.2 83 0.73 0.70 3.81 104 3220454 0.04 0.00E+00 0.09 Below WT Below WT 10 0.7

PROJECT NO. 60595699DATE 1/11/2016COMPUTED BY DNCHECKED BY NS

PROJECT: MLK CLINICAL LAB AND RED BAG STORAGE

SUBJECT: DRY SAND SETTLEMENT DUE TO EARTHQUAKE SHAKING: B-18-L2 LOW GW

INPUT

CLAYS (CL,CH) and ELASTIC SILTS (MH) not considered in analyses

Cs for CAL (Sand) = 0.55Cs for CAL (Clay) = 0.7Atmospheric Pressure, Pa (ksf) = 2.116Energy Ratio (%) = 80Ground Surface Elevation (feet) = 100Depth of Groundwater (feet) = 50Peak Ground Acceleration (g) = 0.634Earthquake Magnitude Mw = 6.7

BORING SAMPLE DEPTH UNIT FIELD SOIL PI D50 BOREHOLE SAMPLE LINER TOTAL EFFECTIVE DEPTH ENERGYBORING

DIAMETER ROD SAMPLER MODIFIED RELATIVE REDUCTION φ

EFFECTIVE PRESSURE AT

DESIGN σm' Gmax γeff*Geff/Gmax n(PI) γ ε εm LAYER SETTLEMENT SETTLEMENT

ELEVATION WEIGHT BLOWCOUNT CLASSIF. DIAMETER TYPE USED PRESSURE PRESSURE FACTOR FACTOR FACTOR FACTOR FACTOR PENETR. DENSITY FACTOR (rad) WATER TABLE (kPa) (psf) (%) (%) (%) (%) (feet) LAYER TOTAL(No.) (feet) (feet) (pcf) (bl/ft) (mm) (in) (ksf) (ksf) Cn Ce=ER/60 Cb Cr Cs (N1)60 Dr (%) Rd (ksf) (in) (in)

B-18-L2 90 10 120 7 Sand 0.0 1.000 8 SPT NO 1.200 1.200 1.33 1.33 1.15 0.75 1.10 11.8 44 0.98 0.63 1.20 35 1228333 0.04 0.00E+00 0.17 0.39 0.33 10 0.787B-18-L2 80 20 120 10 Sand 0.0 1.000 8 SPT NO 2.400 2.400 0.94 1.33 1.15 0.95 1.10 15.0 50 0.95 0.62 2.40 70 1890975 0.05 0.00E+00 0.16 0.23 0.19 10 0.463B-18-L2 70 30 120 29 Sand 0.0 1.000 8 SPT NO 3.600 3.600 0.77 1.33 1.15 0.95 1.20 38.9 80 0.93 0.70 3.60 99 3072759 0.04 0.00E+00 0.10 0.06 0.05 10 0.115B-18-L2 60 40 120 49 Sand 0.0 1.000 8 SPT NO 4.800 4.800 0.66 1.33 1.15 1.00 1.20 59.9 100 0.85 0.70 4.80 131 4097632 0.04 0.00E+00 0.08 0.02 0.02 10 0.045B-18-L2 50 50 120 27 Sand 0.0 1.000 8 SPT NO 6.000 6.000 0.59 1.33 1.15 1.00 1.20 29.5 70 0.77 0.67 6.00 168 3658551 0.05 0.00E+00 0.10 0.09 0.07 10 0.178B-18-L2 40 60 120 35 Sand 0.0 1.000 8 SPT NO 7.200 6.576 0.57 1.33 1.15 1.00 1.20 36.5 78 0.69 0.70 6.58 180 4068151 0.05 0.00E+00 0.09 Below WT Below WT 10 1.6

SHEET 1 1PROJECTDATE

COMPUTED BYCHECKED BY

PROJECT: MLK CLINICAL LAB AND RED BAG STORAGE

SUBJECT: LIQUEFACTION POTENTIAL EVALUATION: B-18-L1 HIGH GW

Reference: Seed, et.al., 2003, Recent Advances in Soil Liquefaction Engineering: A Unified and Consistent FrameworkFAT CLAYS (CH) and ELASTIC SILTS (MH) not considered in analyses

Soil Unit Weight (pcf) = 120Energy Ratio (%) = 80

Design Probability in decimals = 0.15Peak Ground Acceleration (g) = 0.634Earthquake Magnitude = 6.7

BORING DEPTH SPT-N SOIL PERCENT TOTAL EFFECTIVE DEPTH ENERGYBORING

DIAMETER ROD SAMPLER NOR. MODIFIED FINES PENETR.SHEAR MASS

PARTICIPATION

EFFECTIVE PRESSURE

DURING FACTOR VOLUM. LAYER SETTLE SETTLECLASSIF. FINES PRESSURE PRESSURE FACTOR FACTOR FACTOR FACTOR FACTOR PENETR. PENETR. CORRECTION RESIST. FACTOR LIQUEFACTION SOIL TYPE Dr OF STRAIN THICKNESS LAYER TOTAL

B-18-L1 5 5 Clay 80.0 50 8 SPT No 17 500 0.60 0.60 1.70 1.33 1.15 0.75 1.10 9 11 1.3 14 0.96 0.03 0.60 0.397 COARSE 47 1.29 1.46 0.211 0.232 Above Design Ground Water Table 10B-18-L1 15 8 Clay 80.0 50 8 SPT No 17 500 1.80 1.80 1.05 1.33 1.15 0.85 1.10 8 12 1.3 16 0.84 0.07 1.80 0.348 COARSE 46 1.29 1.05 0.256 0.195 Above Design Ground Water Table 10B-18-L1 25 18 Sand 20.0 50 8 SPT No 17 500 3.00 3.00 0.82 1.33 1.15 0.95 1.10 15 24 1.1 26 0.68 0.11 2.50 0.334 COARSE 61 1.29 0.95 0.272 0.289 37 1.06 0.2 10 0.24B-18-L1 35 27 Sand 5.0 50 8 SPT No 17 500 4.20 4.20 0.69 1.33 1.15 1.00 1.20 19 34 1.0 34 0.53 0.15 3.08 0.299 COARSE 69 1.29 0.89 0.259 0.528 0 >1.3 10B-18-L1 45 29 Sand 20.0 50 8 SPT No 17 500 5.40 5.40 0.61 1.33 1.15 1.00 1.20 18 32 1.1 36 0.45 0.17 3.65 0.275 COARSE 67 1.29 0.85 0.251 0.537 0 >1.3 10B-18-L1 55 30 Sand 5.0 50 8 SPT No 17 500 6.60 6.29 0.56 1.33 1.15 1.00 1.20 17 31 1.0 31 0.42 0.17 4.23 0.268 COARSE 66 1.29 0.81 0.256 0.380 0 >1.3 10 0.2

STD DEVIATION

FOR rd

IN-SITU CYCLIC STRESS RATIO

SAMPLE TYPE

LINER USED

LIQUE- FIABLE FINE-

GRAINED SOILS

AVERAGE SHEAR WAVE VELOCITY AT

UPPER 40 FEET (feet/sec)

ADJUSTED CYCLIC STRESS RATIO

CYCLIC RESISTANCE

RATIO

PROBABILITY OF

LIQUEFACTION

3/4/201929405910.0

DNNS

DEPTH TO WATER DURING

DRILLING (feet)

DESIGN WATER

LEVEL IN DEPTH (feet)

BOREHOLE DIAMETER

(inches)

OF

XXX\XXX-XX\Calcs\SPT Liquefaction.xls\B-18-L1

SHEET 1 1PROJECTDATE

COMPUTED BYCHECKED BY

PROJECT: MLK CLINICAL LAB AND RED BAG STORAGE

SUBJECT: LIQUEFACTION POTENTIAL EVALUATION: B-18-l2 HIGH GW

Reference: Seed, et.al., 2003, Recent Advances in Soil Liquefaction Engineering: A Unified and Consistent FrameworkFAT CLAYS (CH) and ELASTIC SILTS (MH) not considered in analyses

Soil Unit Weight (pcf) = 120Energy Ratio (%) = 80

Design Probability in decimals = 0.15Peak Ground Acceleration (g) = 0.634Earthquake Magnitude = 6.7

BORING DEPTH SPT-N SOIL PERCENT TOTAL EFFECTIVE DEPTH ENERGYBORING

DIAMETER ROD SAMPLER NOR. MODIFIED FINES PENETR.SHEAR MASS

PARTICIPATION

EFFECTIVE PRESSURE

DURING FACTOR VOLUM. LAYER SETTLE SETTLECLASSIF. FINES PRESSURE PRESSURE FACTOR FACTOR FACTOR FACTOR FACTOR PENETR. PENETR. CORRECTION RESIST. FACTOR LIQUEFACTION SOIL TYPE Dr OF STRAIN THICKNESS LAYER TOTAL

B-18-L2 10 7 Clay 80.0 50 8 SPT No 12 500 1.20 1.20 1.29 1.33 1.15 0.80 1.10 9 12 1.3 16 0.91 0.05 1.20 0.376 COARSE 48 1.29 1.19 0.245 0.221 Above Design Ground Water Table 10B-18-L2 20 10 Sand 30.0 50 8 SPT No 12 500 2.40 2.40 0.91 1.33 1.15 0.95 1.10 9 15 1.2 18 0.76 0.09 1.90 0.396 COARSE 48 1.29 1.03 0.297 0.164 100 0.55 1.7 10 2.04B-18-L2 30 29 Sand 5.0 50 8 SPT No 12 500 3.60 3.60 0.75 1.33 1.15 0.95 1.20 22 38 1.0 38 0.60 0.13 2.48 0.357 COARSE 74 1.29 0.95 0.290 0.734 0 >1.3 10B-18-L2 40 49 Sand 5.0 50 8 SPT No 12 500 4.80 4.80 0.65 1.33 1.15 1.00 1.20 32 58 1.0 58 0.48 0.17 3.05 0.314 COARSE 90 1.29 0.86 0.281 3.306 0 >1.3 10B-18-L2 50 27 Sand 40.0 50 8 SPT No 12 500 6.00 6.00 0.58 1.33 1.15 1.00 1.20 16 29 1.2 34 0.43 0.17 3.63 0.293 COARSE 63 1.29 0.85 0.267 0.507 0 >1.3 10B-18-L2 60 35 Sand 30.0 50 8 SPT No 12 500 7.20 6.58 0.55 1.33 1.15 1.00 1.20 19 36 1.2 41 0.41 0.17 4.20 0.288 COARSE 70 1.29 0.81 0.274 0.764 0 >1.3 10 2.0

29405910.03/4/2019

DNNS

DEPTH TO WATER DURING

DRILLING (feet)

BOREHOLE DIAMETER

(inches)SAMPLE

TYPELINER USED

DESIGN WATER

LEVEL IN DEPTH (feet)

LIQUE- FIABLE FINE-

GRAINED SOILS

AVERAGE SHEAR WAVE VELOCITY AT

UPPER 40 FEET (feet/sec)

STD DEVIATION

FOR rd

IN-SITU CYCLIC STRESS RATIO

ADJUSTED CYCLIC STRESS RATIO

CYCLIC RESISTANCE

RATIO

PROBABILITY OF

LIQUEFACTION

OF

XXX\XXX-XX\Calcs\SPT Liquefaction.xls\B-18-L2

SHEET 1 1PROJECTDATE

COMPUTED BYCHECKED BY

PROJECT: MLK CLINICAL LAB AND RED BAG STORAGE

SUBJECT: LIQUEFACTION POTENTIAL EVALUATION: B-18-L1 LOW GW

Reference: Seed, et.al., 2003, Recent Advances in Soil Liquefaction Engineering: A Unified and Consistent FrameworkFAT CLAYS (CH) and ELASTIC SILTS (MH) not considered in analyses

Soil Unit Weight (pcf) = 120Energy Ratio (%) = 80

Design Probability in decimals = 0.15Peak Ground Acceleration (g) = 0.634Earthquake Magnitude = 6.7

BORING DEPTH SPT-N SOIL PERCENT TOTAL EFFECTIVE DEPTH ENERGYBORING

DIAMETER ROD SAMPLER NOR. MODIFIED FINES PENETR.SHEAR MASS

PARTICIPATION

EFFECTIVE PRESSURE

DURING FACTOR VOLUM. LAYER SETTLE SETTLECLASSIF. FINES PRESSURE PRESSURE FACTOR FACTOR FACTOR FACTOR FACTOR PENETR. PENETR. CORRECTION RESIST. FACTOR LIQUEFACTION SOIL TYPE Dr OF STRAIN THICKNESS LAYER TOTAL

B-18-L1 5 5 Clay 80.0 50 8 SPT No 50 500 0.60 0.60 1.70 1.33 1.15 0.75 1.10 9 11 1.3 14 0.96 0.03 0.60 0.397 COARSE 47 1.29 1.46 0.211 0.232 Above Design Ground Water Table 10B-18-L1 15 8 Clay 80.0 50 8 SPT No 50 500 1.80 1.80 1.05 1.33 1.15 0.85 1.10 8 12 1.3 16 0.84 0.07 1.80 0.348 COARSE 46 1.29 1.05 0.256 0.195 Above Design Ground Water Table 10B-18-L1 25 18 Sand 20.0 50 8 SPT No 50 500 3.00 3.00 0.82 1.33 1.15 0.95 1.10 15 24 1.1 26 0.68 0.11 3.00 0.279 COARSE 61 1.29 0.90 0.239 0.275 Above Design Ground Water Table 10B-18-L1 35 27 Sand 5.0 50 8 SPT No 50 500 4.20 4.20 0.69 1.33 1.15 1.00 1.20 19 34 1.0 34 0.53 0.15 4.20 0.219 COARSE 69 1.29 0.81 0.208 0.485 Above Design Ground Water Table 10B-18-L1 45 29 Sand 20.0 50 8 SPT No 50 500 5.40 5.40 0.61 1.33 1.15 1.00 1.20 18 32 1.1 36 0.45 0.17 5.40 0.186 COARSE 67 1.29 0.76 0.191 0.482 Above Design Ground Water Table 10B-18-L1 55 30 Sand 5.0 50 8 SPT No 50 500 6.60 6.29 0.56 1.33 1.15 1.00 1.20 17 31 1.0 31 0.42 0.17 6.29 0.180 COARSE 66 1.29 0.72 0.194 0.340 0 >1.3 10 0.0

29405910.03/4/2019

DNNS

DEPTH TO WATER DURING

DRILLING (feet)

BOREHOLE DIAMETER

(inches)SAMPLE

TYPELINER USED

DESIGN WATER

LEVEL IN DEPTH (feet)

LIQUE- FIABLE FINE-

GRAINED SOILS

AVERAGE SHEAR WAVE VELOCITY AT

UPPER 40 FEET (feet/sec)

STD DEVIATION

FOR rd

IN-SITU CYCLIC STRESS RATIO

ADJUSTED CYCLIC STRESS RATIO

CYCLIC RESISTANCE

RATIO

PROBABILITY OF

LIQUEFACTION

OF

XXX\XXX-XX\Calcs\SPT Liquefaction.xls\B-18-L1 (2)

SHEET 1 1PROJECTDATE

COMPUTED BYCHECKED BY

PROJECT: MLK CLINICAL LAB AND RED BAG STORAGE

SUBJECT: LIQUEFACTION POTENTIAL EVALUATION: B-18-L2 LOW GW

Reference: Seed, et.al., 2003, Recent Advances in Soil Liquefaction Engineering: A Unified and Consistent FrameworkFAT CLAYS (CH) and ELASTIC SILTS (MH) not considered in analyses

Soil Unit Weight (pcf) = 120Energy Ratio (%) = 80

Design Probability in decimals = 0.15Peak Ground Acceleration (g) = 0.634Earthquake Magnitude = 6.7

BORING DEPTH SPT-N SOIL PERCENT TOTAL EFFECTIVE DEPTH ENERGYBORING

DIAMETER ROD SAMPLER NOR. MODIFIED FINES PENETR.SHEAR MASS

PARTICIPATION

EFFECTIVE PRESSURE

DURING FACTOR VOLUM. LAYER SETTLE SETTLECLASSIF. FINES PRESSURE PRESSURE FACTOR FACTOR FACTOR FACTOR FACTOR PENETR. PENETR. CORRECTION RESIST. FACTOR LIQUEFACTION SOIL TYPE Dr OF STRAIN THICKNESS LAYER TOTAL

B-18-L2 10 7 Clay 80.0 50 8 SPT No 50 500 1.20 1.20 1.29 1.33 1.15 0.80 1.10 9 12 1.3 16 0.91 0.05 1.20 0.376 COARSE 48 1.29 1.19 0.245 0.221 Above Design Ground Water Table 10B-18-L2 20 10 Sand 30.0 50 8 SPT No 50 500 2.40 2.40 0.91 1.33 1.15 0.95 1.10 9 15 1.2 18 0.76 0.09 2.40 0.314 COARSE 48 1.29 0.96 0.252 0.154 Above Design Ground Water Table 10B-18-L2 30 29 Sand 5.0 50 8 SPT No 50 500 3.60 3.60 0.75 1.33 1.15 0.95 1.20 22 38 1.0 38 0.60 0.13 3.60 0.246 COARSE 74 1.29 0.85 0.223 0.661 Above Design Ground Water Table 10B-18-L2 40 49 Sand 5.0 50 8 SPT No 50 500 4.80 4.80 0.65 1.33 1.15 1.00 1.20 32 58 1.0 58 0.48 0.17 4.80 0.200 COARSE 90 1.29 0.72 0.214 2.915 Above Design Ground Water Table 10B-18-L2 50 27 Sand 40.0 50 8 SPT No 50 500 6.00 6.00 0.58 1.33 1.15 1.00 1.20 16 29 1.2 34 0.43 0.17 6.00 0.177 COARSE 63 1.29 0.73 0.188 0.441 0 >1.3 10B-18-L2 60 35 Sand 30.0 50 8 SPT No 50 500 7.20 6.58 0.55 1.33 1.15 1.00 1.20 19 36 1.2 41 0.41 0.17 6.58 0.184 COARSE 70 1.29 0.71 0.201 0.674 0 >1.3 10 0.0

29405910.03/4/2019

DNNS

DEPTH TO WATER DURING

DRILLING (feet)

BOREHOLE DIAMETER

(inches)SAMPLE

TYPELINER USED

DESIGN WATER

LEVEL IN DEPTH (feet)

LIQUE- FIABLE FINE-

GRAINED SOILS

AVERAGE SHEAR WAVE VELOCITY AT

UPPER 40 FEET (feet/sec)

STD DEVIATION

FOR rd

IN-SITU CYCLIC STRESS RATIO

ADJUSTED CYCLIC STRESS RATIO

CYCLIC RESISTANCE

RATIO

PROBABILITY OF

LIQUEFACTION

OF

XXX\XXX-XX\Calcs\SPT Liquefaction.xls\B-18-L2 (2)

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APPENDIX F AXIAL PILE ANALYSIS

APPENDIX F AXIAL PILE ANALYSIS

Axial pile capacities for cast-in-drilled-hole (CIDH) piles were evaluated using the computer program SHAFT (Ensoft Inc., 2012) following the principles proposed in the book titled “Drilled Shafts: Construction Procedures and Design Methods” by Federal Highway Administration, 1999. The ultimate capacity was obtained by using the formula:

Ultimate axial pile capacity = å incremental side friction + end-bearing

Using conventional notation used by O’Neill & Reese,

RT = pBåDzi fmax,i + pB2qmax/4

RA = RT/F (allowable stress design [ASD]), and

hSgiQi £ SfiRi (load and resistance factor design [LRFD])

RT = nominal ultimate axial resistance of the drilled shaft

RA = allowable resistance (ASD)

F = global factor of safety (ASD)

B = diameter of the drilled shaft

Dzi = layer thickness in layer i

fmax,i = unit side resistance for compression in layer i

qmax = unit base resistance for compression loading

h = ductility/redundancy/operational importance factor (LRFD)

gi = load factor for load component i

Qi = nominal load value for load component i

fi = resistance factor for resistance component I

Ri = nominal value of resistance component i

The subsurface conditions are classified into four types: cohesive, granular, intermediate geomaterials (IGM), and rock. Recommendations are provided in the design manual to estimate the unit side and base resistances for each of the four types of material. The manual provides recommendations for estimating unit resistance as a function of shear strength for cohesive material and based on overburden pressures and SPT blow count for sands and IGM. For settlement analysis, recommendations for t-z and q-z curves were provided in the design manual. Care should be taken to limit the base resistance in large-diameter drilled shaft if the settlement estimates are not performed because the factor of safety (FS) normally used in drilled shaft design might result in excessive settlements for large-diameter drilled shafts

Piles were assumed to develop resistance to axial loads from side friction for normal loading conditions. Pile end-bearing and skin friction contribution from undocumented and new fills were neglected. Generally skin friction of cohesive soils from near surface (5 feet from finish grade) and from bottom one pile diameter was not considered. Idealized soil input parameters are summarized in Table G1. Summaries of the analysis results are provided at the end of this appendix.

Where Allowable Stress Design (ASD) methods were used, a minimum global FS of 2 should be applied to the estimated ultimate pile capacities and the resulting value was checked against the service load demand. Where load and resistance factor design (LRFD) methods were used, a resistance factor, f, of 0.7 was

APPENDIX F AXIAL PILE ANALYSIS

applied to the estimated ultimate pile capacities and the resulting value was checked against the factored load demand.

Pile downdrag may be caused by seismically induced settlement of the soils. Pile downdrag should be considered as an additional load to the allowable pile capacity if ASD method is used; when LRFD is used, nominal resistance should be reduced to include the pile downdrag. For the subject project, pile downdrag is considered remote and does not need to be considered in the capacities.

Settlement analyses can also be performed using the same computer program as for capacity analysis. The program uses recommendations based on Federal Highway Administration (FHWA, 1999) for computing the axial capacity of single pile and employs t-z and q-z curves to compute the load versus pile vertical movement of the drilled shaft.

TABLE F1 - PILE AXIAL CAPACITY ANALYSIS - SOIL INPUT PARAMETERS

SOIL TYPE DEPTH(feet)

SHAFTMODEL

TOTALUNIT

WEIGHT(lb/foot3)

INTERNALFRICTION

ANGLE(degrees)

COHESION(lb/foot2)

qs,max(lb/foot2)

qt,max(lb/foot2)

FILL –Silty Sand 0 to 15 Sand 125 28 -- 4,000 0

ALLUVIUMPoorly-

graded Sand15 to 20 Sand 130 31 -- 4,000 0

ALLUVIUM–Silty Sand 20 to 30 Sand 125 30 -- 4,000 0

ALLUVIUM–

Poorly/Well-graded Sand

30 to 45 Sand 110 31 -- 4,000 0

ALLUVIUM–Silt 45 to 52.5 Clay 120 -- 1,500 4,000 0

ALLUVIUM -Silty Sand 52.5 to 61.5 Sand 125 31 -- 4,000 0

Note:· Pile cutoff at 5 to 10 feet below grade.· End-bearing and skin friction within fills were ignored.· Groundwater at 14.5 bgs (Elevation 78 feet).

Ultimate Axial Capacity (tons)D

epth

(ft

)

0 5 10 15 20 25 30 35 40 45 50 55 60 65 70 75 800

24

68

1012

1416

1820

2224

2628

3032

3436

3840

Skin Friction

Tip Resistance

Total Capacity

Ultimate Axial Capacity (tons)D

epth

(ft

)

0 5 10 15 20 25 30 35 40 45 50 55 60 65 70 75 80

24

68

1012

1416

1820

2224

2628

3032

3436

380

Skin Friction

Tip Resistance

Total Capacity

existing phase1 81 compression.sfo =========================================================================

SHAFT for Windows, Version 2012.7.9

Serial Number : 292734667

VERTICALLY LOADED DRILLED SHAFT ANALYSIS (c) Copyright ENSOFT, Inc., 1987-2012 All Rights Reserved

=========================================================================

Path to file locations : \\losangeles.na.aecomnet.com\LosAngeles\Projects\ENV\_legacy\GT\Da Wu\LA County Geotech On-call\MLK\Report\2019 BHC - Lab\Appendix F and G\ Name of input data file : .sfd Name of output file : .sfo Name of plot output file : .sfp Name of runtime file : .sfr

------------------------------------------------------------------------- Time and Date of Analysis -------------------------------------------------------------------------

Date: March 21, 2019 Time: 13:10:44 MLK Medical Campus: Relocated Red Bag Storage and Future DHS Regional La

PROPOSED DEPTH = 35.0 FT ----------------

NUMBER OF LAYERS = 6 ------------------

WATER TABLE DEPTH = 0.0 FT. -------------------

FACTOR OF SAFETY APPLIED TO THE ULTIMATE SIDE FRICTION CAPACITY = 2.50 ------------------------------------------------------- FACTOR OF SAFETY APPLIED TO THE ULTIMATE BASE CAPACITY = 3.00 ------------------------------------------------------

SOIL INFORMATION ---------------

LAYER NO 1----SAND

AT THE TOP

SKIN FRICTION COEFFICIENT- BETA = 0.120E+01 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.280E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.125E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11

Page 1

existing phase1 81 compression.sfo DEPTH, FT = 0.000E+00

AT THE BOTTOM

SKIN FRICTION COEFFICIENT- BETA = 0.120E+01 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.280E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.125E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11 DEPTH, FT = 0.350E+01

LAYER NO 2----SAND

AT THE TOP

SKIN FRICTION COEFFICIENT- BETA = 0.120E+01 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.310E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.130E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11 DEPTH, FT = 0.350E+01

AT THE BOTTOM

SKIN FRICTION COEFFICIENT- BETA = 0.111E+01 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.310E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.130E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11 DEPTH, FT = 0.850E+01

LAYER NO 3----SAND

AT THE TOP

SKIN FRICTION COEFFICIENT- BETA = 0.111E+01 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.300E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.125E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11 DEPTH, FT = 0.850E+01

AT THE BOTTOM

SKIN FRICTION COEFFICIENT- BETA = 0.919E+00 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.300E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.125E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11 DEPTH, FT = 0.185E+02

LAYER NO 4----SANDPage 2

existing phase1 81 compression.sfo

AT THE TOP

SKIN FRICTION COEFFICIENT- BETA = 0.919E+00 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.310E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.110E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11 DEPTH, FT = 0.185E+02

AT THE BOTTOM

SKIN FRICTION COEFFICIENT- BETA = 0.719E+00 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.310E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.110E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11 DEPTH, FT = 0.335E+02

LAYER NO 5----CLAY

AT THE TOP

STRENGTH REDUCTION FACTOR-ALPHA = 0.550E+00 END BEARING COEFFICIENT-Nc = 0.900E+01 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.150E+04 INTERNAL FRICTION ANGLE, DEG. = 0.000E+00 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.120E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11 DEPTH, FT = 0.335E+02

AT THE BOTTOM

STRENGTH REDUCTION FACTOR-ALPHA = 0.550E+00 END BEARING COEFFICIENT-Nc = 0.900E+01 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.150E+04 INTERNAL FRICTION ANGLE, DEG. = 0.000E+00 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.120E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11 DEPTH, FT = 0.410E+02

LAYER NO 6----SAND

AT THE TOP

SKIN FRICTION COEFFICIENT- BETA = 0.636E+00 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.310E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.125E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11 DEPTH, FT = 0.410E+02

AT THE BOTTOMPage 3

existing phase1 81 compression.sfo

SKIN FRICTION COEFFICIENT- BETA = 0.545E+00 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.310E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.125E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11 DEPTH, FT = 0.500E+02

DRILLED SHAFT INFORMATION -------------------------

DIAMETER OF STEM = 2.000 FT. DIAMETER OF BASE = 2.000 FT. END OF STEM TO BASE = 0.000 FT. ANGLE OF BELL = 0.000 DEG. IGNORED TOP PORTION = 14.000 FT. IGNORED BOTTOM PORTION = 0.000 FT. AREA OF ONE PERCENT STEEL = 4.524 SQ.IN. ELASTIC MODULUS, Ec = 0.350E+07 LB/SQ IN VOLUME OF UNDERREAM = 0.000 CU.YDS.

PREDICTED RESULTS -----------------

QS = ULTIMATE SIDE RESISTANCE; QB = ULTIMATE BASE RESISTANCE; WT = WEIGHT OF DRILLED SHAFT (FOR UPLIFT CAPACITY ONLY); QU = TOTAL ULTIMATE RESISTANCE; QBD = TOTAL ALLOWABLE LOAD USING A FACTOR OF SAFETY APPLIED TO THE ULTIMATE BASE RESISTANCE; QDN = TOTAL ALLOWABLE LOAD USING FACTORS OF SAFETY APPLIED TO THE ULTIMATE SIDE RESISTANCE AND THE ULTIMATE BASE RESISTANCE.

LENGTH VOLUME QS QB QU QBD QDN QU/VOLUME (FEET) (CU.YDS) (TONS) (TONS) (TONS) (TONS) (TONS) (TONS/CU.YDS) 15.0 1.75 2.79 0.00 2.79 2.79 1.11 1.60 16.0 1.86 5.71 0.00 5.71 5.71 2.29 3.07 17.0 1.98 8.78 0.00 8.78 8.78 3.51 4.44 18.0 2.09 11.97 0.00 11.97 11.97 4.79 5.71 19.0 2.21 15.28 0.00 15.28 15.28 6.11 6.91 20.0 2.33 18.70 0.00 18.70 18.70 7.48 8.03 21.0 2.44 22.19 0.00 22.19 22.19 8.88 9.08 22.0 2.56 25.75 0.00 25.75 25.75 10.30 10.06 23.0 2.68 29.39 0.00 29.39 29.39 11.75 10.98 24.0 2.79 33.09 0.00 33.09 33.09 13.23 11.85 25.0 2.91 36.85 0.00 36.85 36.85 14.74 12.67 26.0 3.03 40.67 0.00 40.67 40.67 16.27 13.44 27.0 3.14 44.55 0.00 44.55 44.55 17.82 14.18 28.0 3.26 48.48 0.00 48.48 48.48 19.39 14.88 29.0 3.37 52.47 0.00 52.47 52.47 20.99 15.55 30.0 3.49 56.51 0.00 56.51 56.51 22.60 16.19 31.0 3.61 60.59 0.00 60.59 60.59 24.24 16.80 32.0 3.72 64.72 0.00 64.72 64.72 25.89 17.38 33.0 3.84 68.89 0.00 68.89 68.89 27.56 17.94 34.0 3.96 73.10 0.00 73.10 73.10 29.24 18.48

Page 4

existing phase1 81 compression.sfo 35.0 4.07 75.69 0.00 75.69 75.69 30.28 18.58

RESULT FROM TREND (AVERAGED) LINE

TOP LOAD TOP MOVEMENT TIP LOAD TIP MOVEMENT ton IN. ton IN. 0.1438E-01 0.1467E-04 0.2291E-09 0.1000E-04 0.7191E-01 0.7336E-04 0.1146E-08 0.5000E-04 0.1438E+00 0.1467E-03 0.2291E-08 0.1000E-03 0.7191E+01 0.7336E-02 0.1146E-06 0.5000E-02 0.1082E+02 0.1101E-01 0.1718E-06 0.7500E-02 0.1445E+02 0.1469E-01 0.2291E-06 0.1000E-01 0.3495E+02 0.3644E-01 0.5728E-06 0.2500E-01 0.5807E+02 0.6919E-01 0.1146E-05 0.5000E-01 0.7014E+02 0.9835E-01 0.1718E-05 0.7500E-01 0.7709E+02 0.1257E+00 0.2291E-05 0.1000E+00 0.9041E+02 0.2803E+00 0.5603E-05 0.2500E+00 0.9027E+02 0.5302E+00 0.9040E-05 0.5000E+00 0.9021E+02 0.6552E+00 0.1035E-04 0.6250E+00 0.9014E+02 0.8114E+00 0.1207E-04 0.7812E+00 0.8994E+02 0.1230E+01 0.1595E-04 0.1200E+01

RESULT FROM UPPER-BOUND LINE

TOP LOAD TOP MOVEMENT TIP LOAD TIP MOVEMENT ton IN. ton IN. 0.1990E-01 0.1640E-04 0.3273E-09 0.1000E-04 0.9952E-01 0.8200E-04 0.1636E-08 0.5000E-04 0.1990E+00 0.1640E-03 0.3273E-08 0.1000E-03 0.9987E+01 0.8204E-02 0.1636E-06 0.5000E-02 0.1503E+02 0.1232E-01 0.2455E-06 0.7500E-02 0.2008E+02 0.1644E-01 0.3273E-06 0.1000E-01 0.4777E+02 0.4054E-01 0.8182E-06 0.2500E-01 0.7571E+02 0.7501E-01 0.1636E-05 0.5000E-01 0.8625E+02 0.1038E+00 0.2455E-05 0.7500E-01 0.9019E+02 0.1301E+00 0.3273E-05 0.1000E+00 0.9419E+02 0.2816E+00 0.7790E-05 0.2500E+00 0.9413E+02 0.5315E+00 0.1135E-04 0.5000E+00 0.9413E+02 0.6565E+00 0.1220E-04 0.6250E+00 0.9413E+02 0.8128E+00 0.1368E-04 0.7812E+00 0.9413E+02 0.1232E+01 0.1697E-04 0.1200E+01

RESULT FROM LOWER-BOUND LINE

TOP LOAD TOP MOVEMENT TIP LOAD TIP MOVEMENT ton IN. ton IN. 0.9158E-02 0.1301E-04 0.1309E-09 0.1000E-04 0.4579E-01 0.6503E-04 0.6546E-09 0.5000E-04 0.9158E-01 0.1301E-03 0.1309E-08 0.1000E-03 0.4579E+01 0.6503E-02 0.6546E-07 0.5000E-02 0.6869E+01 0.9754E-02 0.9819E-07 0.7500E-02 0.9168E+01 0.1301E-01 0.1309E-06 0.1000E-01 0.2258E+02 0.3243E-01 0.3273E-06 0.2500E-01 0.4042E+02 0.6336E-01 0.6546E-06 0.5000E-01 0.5364E+02 0.9280E-01 0.9819E-06 0.7500E-01 0.6371E+02 0.1211E+00 0.1309E-05 0.1000E+00 0.8662E+02 0.2790E+00 0.3417E-05 0.2500E+00

Page 5

existing phase1 81 compression.sfo 0.8641E+02 0.5289E+00 0.6729E-05 0.5000E+00 0.8630E+02 0.6539E+00 0.8496E-05 0.6250E+00 0.8615E+02 0.8101E+00 0.1046E-04 0.7812E+00 0.8576E+02 0.1229E+01 0.1492E-04 0.1200E+01

Page 6

Ultimate Axial Capacity (tons)D

epth

(ft

)

0 2 4 6 8 10 12 14 16 18 20 22 24 26 28 30 32 34 36 38 400

24

68

1012

1416

1820

2224

2628

Skin Friction

Tip Resistance

Total Capacity

Ultimate Axial Capacity (tons)D

epth

(ft

)

0 2 4 6 8 10 12 14 16 18 20 22 24 26 28 30 32 34 36 38 40

24

68

1012

1416

1820

2224

2628

Skin Friction

Tip Resistance

Total Capacity

existing phase2 87 compression.sfo =========================================================================

SHAFT for Windows, Version 2012.7.9

Serial Number : 292734667

VERTICALLY LOADED DRILLED SHAFT ANALYSIS (c) Copyright ENSOFT, Inc., 1987-2012 All Rights Reserved

=========================================================================

Path to file locations : \\losangeles.na.aecomnet.com\LosAngeles\Projects\ENV\_legacy\GT\Da Wu\LA County Geotech On-call\MLK\Report\2019 BHC - Lab\Appendix F and G\ Name of input data file : .sfd Name of output file : .sfo Name of plot output file : .sfp Name of runtime file : .sfr

------------------------------------------------------------------------- Time and Date of Analysis -------------------------------------------------------------------------

Date: March 21, 2019 Time: 13:13:17 MLK Medical Campus: Relocated Red Bag Storage and Future DHS Regional La

PROPOSED DEPTH = 29.0 FT ----------------

NUMBER OF LAYERS = 6 ------------------

WATER TABLE DEPTH = 0.0 FT. -------------------

FACTOR OF SAFETY APPLIED TO THE ULTIMATE SIDE FRICTION CAPACITY = 2.50 ------------------------------------------------------- FACTOR OF SAFETY APPLIED TO THE ULTIMATE BASE CAPACITY = 3.00 ------------------------------------------------------

SOIL INFORMATION ---------------

LAYER NO 1----SAND

AT THE TOP

SKIN FRICTION COEFFICIENT- BETA = 0.120E+01 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.280E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.125E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11

Page 1

existing phase2 87 compression.sfo DEPTH, FT = 0.000E+00

AT THE BOTTOM

SKIN FRICTION COEFFICIENT- BETA = 0.107E+01 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.280E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.125E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11 DEPTH, FT = 0.100E+02

LAYER NO 2----SAND

AT THE TOP

SKIN FRICTION COEFFICIENT- BETA = 0.107E+01 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.310E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.130E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11 DEPTH, FT = 0.100E+02

AT THE BOTTOM

SKIN FRICTION COEFFICIENT- BETA = 0.977E+00 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.310E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.130E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11 DEPTH, FT = 0.150E+02

LAYER NO 3----SAND

AT THE TOP

SKIN FRICTION COEFFICIENT- BETA = 0.977E+00 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.300E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.125E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11 DEPTH, FT = 0.150E+02

AT THE BOTTOM

SKIN FRICTION COEFFICIENT- BETA = 0.825E+00 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.300E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.125E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11 DEPTH, FT = 0.250E+02

LAYER NO 4----SANDPage 2

existing phase2 87 compression.sfo

AT THE TOP

SKIN FRICTION COEFFICIENT- BETA = 0.825E+00 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.310E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.110E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11 DEPTH, FT = 0.250E+02

AT THE BOTTOM

SKIN FRICTION COEFFICIENT- BETA = 0.646E+00 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.310E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.110E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11 DEPTH, FT = 0.400E+02

LAYER NO 5----CLAY

AT THE TOP

STRENGTH REDUCTION FACTOR-ALPHA = 0.550E+00 END BEARING COEFFICIENT-Nc = 0.900E+01 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.150E+04 INTERNAL FRICTION ANGLE, DEG. = 0.000E+00 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.120E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11 DEPTH, FT = 0.400E+02

AT THE BOTTOM

STRENGTH REDUCTION FACTOR-ALPHA = 0.550E+00 END BEARING COEFFICIENT-Nc = 0.900E+01 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.150E+04 INTERNAL FRICTION ANGLE, DEG. = 0.000E+00 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.120E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11 DEPTH, FT = 0.470E+02

LAYER NO 6----SAND

AT THE TOP

SKIN FRICTION COEFFICIENT- BETA = 0.574E+00 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.310E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.125E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11 DEPTH, FT = 0.470E+02

AT THE BOTTOMPage 3

existing phase2 87 compression.sfo

SKIN FRICTION COEFFICIENT- BETA = 0.490E+00 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.310E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.125E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11 DEPTH, FT = 0.560E+02

DRILLED SHAFT INFORMATION -------------------------

DIAMETER OF STEM = 2.000 FT. DIAMETER OF BASE = 2.000 FT. END OF STEM TO BASE = 0.000 FT. ANGLE OF BELL = 0.000 DEG. IGNORED TOP PORTION = 20.000 FT. IGNORED BOTTOM PORTION = 0.000 FT. AREA OF ONE PERCENT STEEL = 4.524 SQ.IN. ELASTIC MODULUS, Ec = 0.350E+07 LB/SQ IN VOLUME OF UNDERREAM = 0.000 CU.YDS.

PREDICTED RESULTS -----------------

QS = ULTIMATE SIDE RESISTANCE; QB = ULTIMATE BASE RESISTANCE; WT = WEIGHT OF DRILLED SHAFT (FOR UPLIFT CAPACITY ONLY); QU = TOTAL ULTIMATE RESISTANCE; QBD = TOTAL ALLOWABLE LOAD USING A FACTOR OF SAFETY APPLIED TO THE ULTIMATE BASE RESISTANCE; QDN = TOTAL ALLOWABLE LOAD USING FACTORS OF SAFETY APPLIED TO THE ULTIMATE SIDE RESISTANCE AND THE ULTIMATE BASE RESISTANCE.

LENGTH VOLUME QS QB QU QBD QDN QU/VOLUME (FEET) (CU.YDS) (TONS) (TONS) (TONS) (TONS) (TONS) (TONS/CU.YDS) 21.0 2.44 3.55 0.00 3.55 3.55 1.42 1.45 22.0 2.56 7.22 0.00 7.22 7.22 2.89 2.82 23.0 2.68 10.99 0.00 10.99 10.99 4.40 4.11 24.0 2.79 14.87 0.00 14.87 14.87 5.95 5.32 25.0 2.91 18.84 0.00 18.84 18.84 7.54 6.48 26.0 3.03 22.90 0.00 22.90 22.90 9.16 7.57 27.0 3.14 27.00 0.00 27.00 27.00 10.80 8.59 28.0 3.26 31.16 0.00 31.16 31.16 12.46 9.56 29.0 3.37 35.36 0.00 35.36 35.36 14.15 10.48

RESULT FROM TREND (AVERAGED) LINE

TOP LOAD TOP MOVEMENT TIP LOAD TIP MOVEMENT ton IN. ton IN. 0.1004E-01 0.1284E-04 0.2291E-09 0.1000E-04 0.5018E-01 0.6421E-04 0.1146E-08 0.5000E-04 0.1004E+00 0.1284E-03 0.2291E-08 0.1000E-03 0.5031E+01 0.6423E-02 0.1146E-06 0.5000E-02

Page 4

existing phase2 87 compression.sfo 0.7587E+01 0.9643E-02 0.1718E-06 0.7500E-02 0.1012E+02 0.1286E-01 0.2291E-06 0.1000E-01 0.2472E+02 0.3202E-01 0.5728E-06 0.2500E-01 0.4164E+02 0.6191E-01 0.1146E-05 0.5000E-01 0.5069E+02 0.8956E-01 0.1718E-05 0.7500E-01 0.5576E+02 0.1160E+00 0.2291E-05 0.1000E+00 0.6598E+02 0.2690E+00 0.5603E-05 0.2500E+00 0.6596E+02 0.5190E+00 0.9040E-05 0.5000E+00 0.6592E+02 0.6440E+00 0.1035E-04 0.6250E+00 0.6586E+02 0.8002E+00 0.1207E-04 0.7812E+00 0.6572E+02 0.1219E+01 0.1595E-04 0.1200E+01

RESULT FROM UPPER-BOUND LINE

TOP LOAD TOP MOVEMENT TIP LOAD TIP MOVEMENT ton IN. ton IN. 0.1369E-01 0.1385E-04 0.3273E-09 0.1000E-04 0.6844E-01 0.6927E-04 0.1636E-08 0.5000E-04 0.1369E+00 0.1385E-03 0.3273E-08 0.1000E-03 0.6900E+01 0.6935E-02 0.1636E-06 0.5000E-02 0.1038E+02 0.1041E-01 0.2455E-06 0.7500E-02 0.1386E+02 0.1389E-01 0.3273E-06 0.1000E-01 0.3350E+02 0.3448E-01 0.8182E-06 0.2500E-01 0.5430E+02 0.6553E-01 0.1636E-05 0.5000E-01 0.6264E+02 0.9302E-01 0.2455E-05 0.7500E-01 0.6552E+02 0.1189E+00 0.3273E-05 0.1000E+00 0.6875E+02 0.2698E+00 0.7790E-05 0.2500E+00 0.6875E+02 0.5198E+00 0.1135E-04 0.5000E+00 0.6875E+02 0.6448E+00 0.1220E-04 0.6250E+00 0.6875E+02 0.8011E+00 0.1368E-04 0.7812E+00 0.6875E+02 0.1220E+01 0.1697E-04 0.1200E+01

RESULT FROM LOWER-BOUND LINE

TOP LOAD TOP MOVEMENT TIP LOAD TIP MOVEMENT ton IN. ton IN. 0.6491E-02 0.1185E-04 0.1309E-09 0.1000E-04 0.3246E-01 0.5925E-04 0.6546E-09 0.5000E-04 0.6491E-01 0.1185E-03 0.1309E-08 0.1000E-03 0.3246E+01 0.5925E-02 0.6546E-07 0.5000E-02 0.4876E+01 0.8888E-02 0.9819E-07 0.7500E-02 0.6517E+01 0.1185E-01 0.1309E-06 0.1000E-01 0.1611E+02 0.2959E-01 0.3273E-06 0.2500E-01 0.2897E+02 0.5828E-01 0.6546E-06 0.5000E-01 0.3862E+02 0.8607E-01 0.9819E-06 0.7500E-01 0.4591E+02 0.1132E+00 0.1309E-05 0.1000E+00 0.6320E+02 0.2682E+00 0.3417E-05 0.2500E+00 0.6317E+02 0.5182E+00 0.6729E-05 0.5000E+00 0.6308E+02 0.6432E+00 0.8496E-05 0.6250E+00 0.6298E+02 0.7994E+00 0.1046E-04 0.7812E+00 0.6269E+02 0.1218E+01 0.1492E-04 0.1200E+01

Page 5

Ultimate Axial Capacity (tons)D

epth

(ft

)

0 5 10 15 20 25 30 35 40 45 50 55 60 65 700

24

68

1012

1416

1820

2224

2628

3032

3436

3840

Skin Friction

Tip Resistance

Total Capacity

existing phase1 87 compression.sfo =========================================================================

SHAFT for Windows, Version 2012.7.9

Serial Number : 292734667

VERTICALLY LOADED DRILLED SHAFT ANALYSIS (c) Copyright ENSOFT, Inc., 1987-2012 All Rights Reserved

=========================================================================

Path to file locations : \\losangeles.na.aecomnet.com\LosAngeles\Projects\ENV\_legacy\GT\Da Wu\LA County Geotech On-call\MLK\Report\2019 BHC - Lab\Appendix F and G\ Name of input data file : .sfd Name of output file : .sfo Name of plot output file : .sfp Name of runtime file : .sfr

------------------------------------------------------------------------- Time and Date of Analysis -------------------------------------------------------------------------

Date: March 21, 2019 Time: 13:12:12 MLK Medical Campus: Relocated Red Bag Storage and Future DHS Regional La

PROPOSED DEPTH = 35.0 FT ----------------

NUMBER OF LAYERS = 6 ------------------

WATER TABLE DEPTH = 0.0 FT. -------------------

FACTOR OF SAFETY APPLIED TO THE ULTIMATE SIDE FRICTION CAPACITY = 2.50 ------------------------------------------------------- FACTOR OF SAFETY APPLIED TO THE ULTIMATE BASE CAPACITY = 3.00 ------------------------------------------------------

SOIL INFORMATION ---------------

LAYER NO 1----SAND

AT THE TOP

SKIN FRICTION COEFFICIENT- BETA = 0.120E+01 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.280E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.125E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11

Page 1

existing phase1 87 compression.sfo DEPTH, FT = 0.000E+00

AT THE BOTTOM

SKIN FRICTION COEFFICIENT- BETA = 0.107E+01 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.280E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.125E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11 DEPTH, FT = 0.100E+02

LAYER NO 2----SAND

AT THE TOP

SKIN FRICTION COEFFICIENT- BETA = 0.107E+01 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.310E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.130E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11 DEPTH, FT = 0.100E+02

AT THE BOTTOM

SKIN FRICTION COEFFICIENT- BETA = 0.977E+00 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.310E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.130E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11 DEPTH, FT = 0.150E+02

LAYER NO 3----SAND

AT THE TOP

SKIN FRICTION COEFFICIENT- BETA = 0.977E+00 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.300E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.125E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11 DEPTH, FT = 0.150E+02

AT THE BOTTOM

SKIN FRICTION COEFFICIENT- BETA = 0.825E+00 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.300E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.125E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11 DEPTH, FT = 0.250E+02

LAYER NO 4----SANDPage 2

existing phase1 87 compression.sfo

AT THE TOP

SKIN FRICTION COEFFICIENT- BETA = 0.825E+00 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.310E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.110E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11 DEPTH, FT = 0.250E+02

AT THE BOTTOM

SKIN FRICTION COEFFICIENT- BETA = 0.646E+00 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.310E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.110E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11 DEPTH, FT = 0.400E+02

LAYER NO 5----CLAY

AT THE TOP

STRENGTH REDUCTION FACTOR-ALPHA = 0.550E+00 END BEARING COEFFICIENT-Nc = 0.900E+01 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.150E+04 INTERNAL FRICTION ANGLE, DEG. = 0.000E+00 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.120E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11 DEPTH, FT = 0.400E+02

AT THE BOTTOM

STRENGTH REDUCTION FACTOR-ALPHA = 0.550E+00 END BEARING COEFFICIENT-Nc = 0.900E+01 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.150E+04 INTERNAL FRICTION ANGLE, DEG. = 0.000E+00 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.120E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11 DEPTH, FT = 0.470E+02

LAYER NO 6----SAND

AT THE TOP

SKIN FRICTION COEFFICIENT- BETA = 0.574E+00 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.310E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.125E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11 DEPTH, FT = 0.470E+02

AT THE BOTTOMPage 3

existing phase1 87 compression.sfo

SKIN FRICTION COEFFICIENT- BETA = 0.490E+00 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.310E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.125E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11 DEPTH, FT = 0.560E+02

DRILLED SHAFT INFORMATION -------------------------

DIAMETER OF STEM = 2.000 FT. DIAMETER OF BASE = 2.000 FT. END OF STEM TO BASE = 0.000 FT. ANGLE OF BELL = 0.000 DEG. IGNORED TOP PORTION = 20.000 FT. IGNORED BOTTOM PORTION = 0.000 FT. AREA OF ONE PERCENT STEEL = 4.524 SQ.IN. ELASTIC MODULUS, Ec = 0.350E+07 LB/SQ IN VOLUME OF UNDERREAM = 0.000 CU.YDS.

PREDICTED RESULTS -----------------

QS = ULTIMATE SIDE RESISTANCE; QB = ULTIMATE BASE RESISTANCE; WT = WEIGHT OF DRILLED SHAFT (FOR UPLIFT CAPACITY ONLY); QU = TOTAL ULTIMATE RESISTANCE; QBD = TOTAL ALLOWABLE LOAD USING A FACTOR OF SAFETY APPLIED TO THE ULTIMATE BASE RESISTANCE; QDN = TOTAL ALLOWABLE LOAD USING FACTORS OF SAFETY APPLIED TO THE ULTIMATE SIDE RESISTANCE AND THE ULTIMATE BASE RESISTANCE.

LENGTH VOLUME QS QB QU QBD QDN QU/VOLUME (FEET) (CU.YDS) (TONS) (TONS) (TONS) (TONS) (TONS) (TONS/CU.YDS) 21.0 2.44 3.55 0.00 3.55 3.55 1.42 1.45 22.0 2.56 7.22 0.00 7.22 7.22 2.89 2.82 23.0 2.68 10.99 0.00 10.99 10.99 4.40 4.11 24.0 2.79 14.87 0.00 14.87 14.87 5.95 5.32 25.0 2.91 18.84 0.00 18.84 18.84 7.54 6.48 26.0 3.03 22.90 0.00 22.90 22.90 9.16 7.57 27.0 3.14 27.00 0.00 27.00 27.00 10.80 8.59 28.0 3.26 31.16 0.00 31.16 31.16 12.46 9.56 29.0 3.37 35.36 0.00 35.36 35.36 14.15 10.48 30.0 3.49 39.62 0.00 39.62 39.62 15.85 11.35 31.0 3.61 43.91 0.00 43.91 43.91 17.56 12.17 32.0 3.72 48.25 0.00 48.25 48.25 19.30 12.96 33.0 3.84 52.62 0.00 52.62 52.62 21.05 13.70 34.0 3.96 57.03 0.00 57.03 57.03 22.81 14.41 35.0 4.07 61.48 0.00 61.48 61.48 24.59 15.09

RESULT FROM TREND (AVERAGED) LINE

Page 4

existing phase1 87 compression.sfo TOP LOAD TOP MOVEMENT TIP LOAD TIP MOVEMENT ton IN. ton IN. 0.1434E-01 0.1476E-04 0.2291E-09 0.1000E-04 0.7169E-01 0.7381E-04 0.1146E-08 0.5000E-04 0.1434E+00 0.1476E-03 0.2291E-08 0.1000E-03 0.7196E+01 0.7384E-02 0.1146E-06 0.5000E-02 0.1083E+02 0.1109E-01 0.1718E-06 0.7500E-02 0.1447E+02 0.1479E-01 0.2291E-06 0.1000E-01 0.3498E+02 0.3669E-01 0.5728E-06 0.2500E-01 0.5826E+02 0.6968E-01 0.1146E-05 0.5000E-01 0.7038E+02 0.9894E-01 0.1718E-05 0.7500E-01 0.7742E+02 0.1263E+00 0.2291E-05 0.1000E+00 0.9093E+02 0.2811E+00 0.5603E-05 0.2500E+00 0.9087E+02 0.5311E+00 0.9040E-05 0.5000E+00 0.9081E+02 0.6561E+00 0.1035E-04 0.6250E+00 0.9074E+02 0.8123E+00 0.1207E-04 0.7812E+00 0.9054E+02 0.1231E+01 0.1595E-04 0.1200E+01

RESULT FROM UPPER-BOUND LINE

TOP LOAD TOP MOVEMENT TIP LOAD TIP MOVEMENT ton IN. ton IN. 0.1979E-01 0.1650E-04 0.3273E-09 0.1000E-04 0.9896E-01 0.8252E-04 0.1636E-08 0.5000E-04 0.1979E+00 0.1650E-03 0.3273E-08 0.1000E-03 0.9991E+01 0.8271E-02 0.1636E-06 0.5000E-02 0.1503E+02 0.1242E-01 0.2455E-06 0.7500E-02 0.2006E+02 0.1657E-01 0.3273E-06 0.1000E-01 0.4776E+02 0.4086E-01 0.8182E-06 0.2500E-01 0.7599E+02 0.7567E-01 0.1636E-05 0.5000E-01 0.8668E+02 0.1046E+00 0.2455E-05 0.7500E-01 0.9065E+02 0.1309E+00 0.3273E-05 0.1000E+00 0.9471E+02 0.2825E+00 0.7790E-05 0.2500E+00 0.9471E+02 0.5325E+00 0.1135E-04 0.5000E+00 0.9471E+02 0.6575E+00 0.1220E-04 0.6250E+00 0.9471E+02 0.8137E+00 0.1368E-04 0.7812E+00 0.9471E+02 0.1232E+01 0.1697E-04 0.1200E+01

RESULT FROM LOWER-BOUND LINE

TOP LOAD TOP MOVEMENT TIP LOAD TIP MOVEMENT ton IN. ton IN. 0.9161E-02 0.1307E-04 0.1309E-09 0.1000E-04 0.4580E-01 0.6537E-04 0.6546E-09 0.5000E-04 0.9161E-01 0.1307E-03 0.1309E-08 0.1000E-03 0.4580E+01 0.6537E-02 0.6546E-07 0.5000E-02 0.6882E+01 0.9807E-02 0.9819E-07 0.7500E-02 0.9197E+01 0.1308E-01 0.1309E-06 0.1000E-01 0.2264E+02 0.3261E-01 0.3273E-06 0.2500E-01 0.4053E+02 0.6369E-01 0.6546E-06 0.5000E-01 0.5381E+02 0.9325E-01 0.9819E-06 0.7500E-01 0.6395E+02 0.1217E+00 0.1309E-05 0.1000E+00 0.8714E+02 0.2798E+00 0.3417E-05 0.2500E+00 0.8702E+02 0.5298E+00 0.6729E-05 0.5000E+00 0.8690E+02 0.6548E+00 0.8496E-05 0.6250E+00 0.8676E+02 0.8110E+00 0.1046E-04 0.7812E+00 0.8636E+02 0.1230E+01 0.1492E-04 0.1200E+01

Page 5

existing phase1 81 uplift.sfo =========================================================================

SHAFT for Windows, Version 2012.7.9

Serial Number : 292734667

VERTICALLY LOADED DRILLED SHAFT ANALYSIS (c) Copyright ENSOFT, Inc., 1987-2012 All Rights Reserved

=========================================================================

Path to file locations : \\losangeles.na.aecomnet.com\LosAngeles\Projects\ENV\_legacy\GT\Da Wu\LA County Geotech On-call\MLK\Report\2019 BHC - Lab\Appendix F and G\ Name of input data file : .sfd Name of output file : .sfo Name of plot output file : .sfp Name of runtime file : .sfr

------------------------------------------------------------------------- Time and Date of Analysis -------------------------------------------------------------------------

Date: March 21, 2019 Time: 13:18:21 MLK Medical Campus: Relocated Red Bag Storage and Future DHS Regional La

PROPOSED DEPTH = 20.0 FT ----------------

REDUCTION FACTOR APPLIED FOR UPLIFT FRICTION = 0.600 ----------------------------------------------

NUMBER OF LAYERS = 6 ------------------

WATER TABLE DEPTH = 0.0 FT. -------------------

FACTOR OF SAFETY APPLIED TO THE ULTIMATE SIDE FRICTION CAPACITY = 2.50 ------------------------------------------------------- FACTOR OF SAFETY APPLIED TO THE ULTIMATE BASE CAPACITY = 3.00 ------------------------------------------------------

SOIL INFORMATION ---------------

LAYER NO 1----SAND

AT THE TOP

SKIN FRICTION COEFFICIENT- BETA = 0.120E+01 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00

Page 1

existing phase1 81 uplift.sfo INTERNAL FRICTION ANGLE, DEG. = 0.280E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.125E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11 DEPTH, FT = 0.000E+00

AT THE BOTTOM

SKIN FRICTION COEFFICIENT- BETA = 0.120E+01 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.280E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.125E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11 DEPTH, FT = 0.350E+01

LAYER NO 2----SAND

AT THE TOP

SKIN FRICTION COEFFICIENT- BETA = 0.120E+01 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.310E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.130E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11 DEPTH, FT = 0.350E+01

AT THE BOTTOM

SKIN FRICTION COEFFICIENT- BETA = 0.111E+01 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.310E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.130E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11 DEPTH, FT = 0.850E+01

LAYER NO 3----SAND

AT THE TOP

SKIN FRICTION COEFFICIENT- BETA = 0.111E+01 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.300E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.125E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11 DEPTH, FT = 0.850E+01

AT THE BOTTOM

SKIN FRICTION COEFFICIENT- BETA = 0.919E+00 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.300E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.125E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11

Page 2

existing phase1 81 uplift.sfo DEPTH, FT = 0.185E+02

LAYER NO 4----SAND

AT THE TOP

SKIN FRICTION COEFFICIENT- BETA = 0.919E+00 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.310E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.110E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11 DEPTH, FT = 0.185E+02

AT THE BOTTOM

SKIN FRICTION COEFFICIENT- BETA = 0.719E+00 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.310E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.110E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11 DEPTH, FT = 0.335E+02

LAYER NO 5----CLAY

AT THE TOP

STRENGTH REDUCTION FACTOR-ALPHA = 0.550E+00 END BEARING COEFFICIENT-Nc = 0.900E+01 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.150E+04 INTERNAL FRICTION ANGLE, DEG. = 0.000E+00 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.120E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11 DEPTH, FT = 0.335E+02

AT THE BOTTOM

STRENGTH REDUCTION FACTOR-ALPHA = 0.550E+00 END BEARING COEFFICIENT-Nc = 0.900E+01 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.150E+04 INTERNAL FRICTION ANGLE, DEG. = 0.000E+00 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.120E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11 DEPTH, FT = 0.410E+02

LAYER NO 6----SAND

AT THE TOP

SKIN FRICTION COEFFICIENT- BETA = 0.636E+00 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.310E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.125E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11

Page 3

existing phase1 81 uplift.sfo DEPTH, FT = 0.410E+02

AT THE BOTTOM

SKIN FRICTION COEFFICIENT- BETA = 0.545E+00 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.310E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.125E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11 DEPTH, FT = 0.500E+02

DRILLED SHAFT INFORMATION -------------------------

DIAMETER OF STEM = 2.000 FT. DIAMETER OF BASE = 2.000 FT. END OF STEM TO BASE = 0.000 FT. ANGLE OF BELL = 0.000 DEG. IGNORED TOP PORTION = 14.000 FT. IGNORED BOTTOM PORTION = 0.000 FT. AREA OF ONE PERCENT STEEL = 4.524 SQ.IN. ELASTIC MODULUS, Ec = 0.350E+07 LB/SQ IN VOLUME OF UNDERREAM = 0.000 CU.YDS.

PREDICTED RESULTS -----------------

QS = ULTIMATE SIDE RESISTANCE; QB = ULTIMATE BASE RESISTANCE; WT = WEIGHT OF DRILLED SHAFT (FOR UPLIFT CAPACITY ONLY); QU = TOTAL ULTIMATE RESISTANCE; QBD = TOTAL ALLOWABLE LOAD USING A FACTOR OF SAFETY APPLIED TO THE ULTIMATE BASE RESISTANCE; QDN = TOTAL ALLOWABLE LOAD USING FACTORS OF SAFETY APPLIED TO THE ULTIMATE SIDE RESISTANCE AND THE ULTIMATE BASE RESISTANCE.

LENGTH VOLUME QS WT QU QBD QDN QU/VOLUME (FEET) (CU.YDS) (TONS) (TONS) (TONS) (TONS) (TONS) (TONS/CU.YDS) 15.0 1.75 1.67 2.06 3.74 3.74 2.73 2.14 16.0 1.86 3.43 2.20 5.63 5.63 3.57 3.02 17.0 1.98 5.27 2.34 7.60 7.60 4.45 3.84 18.0 2.09 7.18 2.48 9.66 9.66 5.35 4.61 19.0 2.21 9.17 2.62 11.79 11.79 6.28 5.33 20.0 2.33 11.22 2.75 13.97 13.97 7.24 6.00

RESULT FROM TREND (AVERAGED) LINE

TOP LOAD TOP MOVEMENT TIP LOAD TIP MOVEMENT ton IN. ton IN. 0.3122E-02 0.1062E-04 0.4014E-04 0.1000E-04 0.1561E-01 0.5312E-04 0.2007E-03 0.5000E-04 0.3122E-01 0.1062E-03 0.4014E-03 0.1000E-03

Page 4

existing phase1 81 uplift.sfo 0.1561E+01 0.5312E-02 0.2007E-01 0.5000E-02 0.2342E+01 0.7968E-02 0.3011E-01 0.7500E-02 0.3122E+01 0.1062E-01 0.4014E-01 0.1000E-01 0.7719E+01 0.2654E-01 0.1004E+00 0.2500E-01 0.1321E+02 0.5265E-01 0.2007E+00 0.5000E-01 0.1629E+02 0.7828E-01 0.3011E+00 0.7500E-01 0.1799E+02 0.1036E+00 0.4014E+00 0.1000E+00 0.2197E+02 0.2545E+00 0.9818E+00 0.2500E+00 0.2258E+02 0.5047E+00 0.1584E+01 0.5000E+00 0.2279E+02 0.6297E+00 0.1813E+01 0.6250E+00 0.2308E+02 0.7861E+00 0.2115E+01 0.7812E+00 0.2371E+02 0.1205E+01 0.2794E+01 0.1200E+01

RESULT FROM UPPER-BOUND LINE

TOP LOAD TOP MOVEMENT TIP LOAD TIP MOVEMENT ton IN. ton IN. 0.4211E-02 0.1084E-04 0.5735E-04 0.1000E-04 0.2105E-01 0.5421E-04 0.2867E-03 0.5000E-04 0.4211E-01 0.1084E-03 0.5735E-03 0.1000E-03 0.2105E+01 0.5421E-02 0.2867E-01 0.5000E-02 0.3158E+01 0.8131E-02 0.4301E-01 0.7500E-02 0.4212E+01 0.1084E-01 0.5735E-01 0.1000E-01 0.1038E+02 0.2708E-01 0.1434E+00 0.2500E-01 0.1726E+02 0.5346E-01 0.2867E+00 0.5000E-01 0.2026E+02 0.7908E-01 0.4301E+00 0.7500E-01 0.2132E+02 0.1043E+00 0.5735E+00 0.1000E+00 0.2324E+02 0.2548E+00 0.1365E+01 0.2500E+00 0.2387E+02 0.5050E+00 0.1989E+01 0.5000E+00 0.2402E+02 0.6300E+00 0.2138E+01 0.6250E+00 0.2428E+02 0.7863E+00 0.2397E+01 0.7812E+00 0.2485E+02 0.1205E+01 0.2973E+01 0.1200E+01

RESULT FROM LOWER-BOUND LINE

TOP LOAD TOP MOVEMENT TIP LOAD TIP MOVEMENT ton IN. ton IN. 0.2041E-02 0.1041E-04 0.2294E-04 0.1000E-04 0.1020E-01 0.5204E-04 0.1147E-03 0.5000E-04 0.2041E-01 0.1041E-03 0.2294E-03 0.1000E-03 0.1020E+01 0.5204E-02 0.1147E-01 0.5000E-02 0.1530E+01 0.7806E-02 0.1720E-01 0.7500E-02 0.2041E+01 0.1041E-01 0.2294E-01 0.1000E-01 0.5062E+01 0.2601E-01 0.5735E-01 0.2500E-01 0.9166E+01 0.5184E-01 0.1147E+00 0.5000E-01 0.1231E+02 0.7747E-01 0.1720E+00 0.7500E-01 0.1465E+02 0.1029E+00 0.2294E+00 0.1000E+00 0.2069E+02 0.2542E+00 0.5987E+00 0.2500E+00 0.2128E+02 0.5044E+00 0.1179E+01 0.5000E+00 0.2156E+02 0.6295E+00 0.1489E+01 0.6250E+00 0.2188E+02 0.7858E+00 0.1833E+01 0.7812E+00 0.2257E+02 0.1205E+01 0.2615E+01 0.1200E+01

Page 5

existing phase1 87 uplift.sfo =========================================================================

SHAFT for Windows, Version 2012.7.9

Serial Number : 292734667

VERTICALLY LOADED DRILLED SHAFT ANALYSIS (c) Copyright ENSOFT, Inc., 1987-2012 All Rights Reserved

=========================================================================

Path to file locations : \\losangeles.na.aecomnet.com\LosAngeles\Projects\ENV\_legacy\GT\Da Wu\LA County Geotech On-call\MLK\Report\2019 BHC - Lab\Appendix F and G\ Name of input data file : .sfd Name of output file : .sfo Name of plot output file : .sfp Name of runtime file : .sfr

------------------------------------------------------------------------- Time and Date of Analysis -------------------------------------------------------------------------

Date: March 21, 2019 Time: 13:19:26 MLK Medical Campus: Relocated Red Bag Storage and Future DHS Regional La

PROPOSED DEPTH = 20.0 FT ----------------

REDUCTION FACTOR APPLIED FOR UPLIFT FRICTION = 0.600 ----------------------------------------------

NUMBER OF LAYERS = 6 ------------------

WATER TABLE DEPTH = 0.0 FT. -------------------

FACTOR OF SAFETY APPLIED TO THE ULTIMATE SIDE FRICTION CAPACITY = 2.50 ------------------------------------------------------- FACTOR OF SAFETY APPLIED TO THE ULTIMATE BASE CAPACITY = 3.00 ------------------------------------------------------

SOIL INFORMATION ---------------

LAYER NO 1----SAND

AT THE TOP

SKIN FRICTION COEFFICIENT- BETA = 0.120E+01 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00

Page 1

existing phase1 87 uplift.sfo INTERNAL FRICTION ANGLE, DEG. = 0.280E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.125E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11 DEPTH, FT = 0.000E+00

AT THE BOTTOM

SKIN FRICTION COEFFICIENT- BETA = 0.107E+01 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.280E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.125E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11 DEPTH, FT = 0.100E+02

LAYER NO 2----SAND

AT THE TOP

SKIN FRICTION COEFFICIENT- BETA = 0.107E+01 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.310E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.130E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11 DEPTH, FT = 0.100E+02

AT THE BOTTOM

SKIN FRICTION COEFFICIENT- BETA = 0.977E+00 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.310E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.130E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11 DEPTH, FT = 0.150E+02

LAYER NO 3----SAND

AT THE TOP

SKIN FRICTION COEFFICIENT- BETA = 0.977E+00 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.300E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.125E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11 DEPTH, FT = 0.150E+02

AT THE BOTTOM

SKIN FRICTION COEFFICIENT- BETA = 0.825E+00 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.300E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.125E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11

Page 2

existing phase1 87 uplift.sfo DEPTH, FT = 0.250E+02

LAYER NO 4----SAND

AT THE TOP

SKIN FRICTION COEFFICIENT- BETA = 0.825E+00 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.310E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.110E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11 DEPTH, FT = 0.250E+02

AT THE BOTTOM

SKIN FRICTION COEFFICIENT- BETA = 0.646E+00 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.310E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.110E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11 DEPTH, FT = 0.400E+02

LAYER NO 5----CLAY

AT THE TOP

STRENGTH REDUCTION FACTOR-ALPHA = 0.550E+00 END BEARING COEFFICIENT-Nc = 0.900E+01 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.150E+04 INTERNAL FRICTION ANGLE, DEG. = 0.000E+00 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.120E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11 DEPTH, FT = 0.400E+02

AT THE BOTTOM

STRENGTH REDUCTION FACTOR-ALPHA = 0.550E+00 END BEARING COEFFICIENT-Nc = 0.900E+01 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.150E+04 INTERNAL FRICTION ANGLE, DEG. = 0.000E+00 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.120E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11 DEPTH, FT = 0.470E+02

LAYER NO 6----SAND

AT THE TOP

SKIN FRICTION COEFFICIENT- BETA = 0.574E+00 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.310E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.125E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11

Page 3

existing phase1 87 uplift.sfo DEPTH, FT = 0.470E+02

AT THE BOTTOM

SKIN FRICTION COEFFICIENT- BETA = 0.490E+00 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.310E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.125E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11 DEPTH, FT = 0.560E+02

DRILLED SHAFT INFORMATION -------------------------

DIAMETER OF STEM = 2.000 FT. DIAMETER OF BASE = 2.000 FT. END OF STEM TO BASE = 0.000 FT. ANGLE OF BELL = 0.000 DEG. IGNORED TOP PORTION = 20.000 FT. IGNORED BOTTOM PORTION = 0.000 FT. AREA OF ONE PERCENT STEEL = 4.524 SQ.IN. ELASTIC MODULUS, Ec = 0.350E+07 LB/SQ IN VOLUME OF UNDERREAM = 0.000 CU.YDS.

PREDICTED RESULTS -----------------

QS = ULTIMATE SIDE RESISTANCE; QB = ULTIMATE BASE RESISTANCE; WT = WEIGHT OF DRILLED SHAFT (FOR UPLIFT CAPACITY ONLY); QU = TOTAL ULTIMATE RESISTANCE; QBD = TOTAL ALLOWABLE LOAD USING A FACTOR OF SAFETY APPLIED TO THE ULTIMATE BASE RESISTANCE; QDN = TOTAL ALLOWABLE LOAD USING FACTORS OF SAFETY APPLIED TO THE ULTIMATE SIDE RESISTANCE AND THE ULTIMATE BASE RESISTANCE.

LENGTH VOLUME QS WT QU QBD QDN QU/VOLUME (FEET) (CU.YDS) (TONS) (TONS) (TONS) (TONS) (TONS) (TONS/CU.YDS) 21.0 2.44 2.13 2.89 5.02 5.02 3.74 2.06

RESULT FROM TREND (AVERAGED) LINE

TOP LOAD TOP MOVEMENT TIP LOAD TIP MOVEMENT ton IN. ton IN. 0.3167E-02 0.1051E-04 0.4215E-04 0.1000E-04 0.1583E-01 0.5255E-04 0.2107E-03 0.5000E-04 0.3167E-01 0.1051E-03 0.4215E-03 0.1000E-03 0.1583E+01 0.5255E-02 0.2107E-01 0.5000E-02 0.2375E+01 0.7883E-02 0.3161E-01 0.7500E-02 0.3208E+01 0.1052E-01 0.4215E-01 0.1000E-01 0.7907E+01 0.2628E-01 0.1054E+00 0.2500E-01 0.1353E+02 0.5219E-01 0.2107E+00 0.5000E-01

Page 4

existing phase1 87 uplift.sfo 0.1668E+02 0.7770E-01 0.3161E+00 0.7500E-01 0.1842E+02 0.1030E+00 0.4215E+00 0.1000E+00 0.2250E+02 0.2537E+00 0.1031E+01 0.2500E+00 0.2314E+02 0.5039E+00 0.1663E+01 0.5000E+00 0.2337E+02 0.6290E+00 0.1904E+01 0.6250E+00 0.2367E+02 0.7854E+00 0.2221E+01 0.7812E+00 0.2433E+02 0.1204E+01 0.2934E+01 0.1200E+01

RESULT FROM UPPER-BOUND LINE

TOP LOAD TOP MOVEMENT TIP LOAD TIP MOVEMENT ton IN. ton IN. 0.4258E-02 0.1069E-04 0.6021E-04 0.1000E-04 0.2129E-01 0.5344E-04 0.3011E-03 0.5000E-04 0.4258E-01 0.1069E-03 0.6021E-03 0.1000E-03 0.2129E+01 0.5344E-02 0.3011E-01 0.5000E-02 0.3249E+01 0.8024E-02 0.4516E-01 0.7500E-02 0.4332E+01 0.1070E-01 0.6021E-01 0.1000E-01 0.1064E+02 0.2672E-01 0.1505E+00 0.2500E-01 0.1767E+02 0.5286E-01 0.3011E+00 0.5000E-01 0.2074E+02 0.7837E-01 0.4516E+00 0.7500E-01 0.2183E+02 0.1036E+00 0.6021E+00 0.1000E+00 0.2382E+02 0.2540E+00 0.1433E+01 0.2500E+00 0.2447E+02 0.5042E+00 0.2088E+01 0.5000E+00 0.2463E+02 0.6293E+00 0.2245E+01 0.6250E+00 0.2490E+02 0.7856E+00 0.2516E+01 0.7812E+00 0.2551E+02 0.1205E+01 0.3121E+01 0.1200E+01

RESULT FROM LOWER-BOUND LINE

TOP LOAD TOP MOVEMENT TIP LOAD TIP MOVEMENT ton IN. ton IN. 0.2076E-02 0.1033E-04 0.2409E-04 0.1000E-04 0.1038E-01 0.5167E-04 0.1204E-03 0.5000E-04 0.2076E-01 0.1033E-03 0.2409E-03 0.1000E-03 0.1038E+01 0.5167E-02 0.1204E-01 0.5000E-02 0.1557E+01 0.7751E-02 0.1806E-01 0.7500E-02 0.2076E+01 0.1033E-01 0.2409E-01 0.1000E-01 0.5189E+01 0.2584E-01 0.6021E-01 0.2500E-01 0.9386E+01 0.5151E-01 0.1204E+00 0.5000E-01 0.1260E+02 0.7703E-01 0.1806E+00 0.7500E-01 0.1500E+02 0.1024E+00 0.2409E+00 0.1000E+00 0.2119E+02 0.2535E+00 0.6286E+00 0.2500E+00 0.2181E+02 0.5037E+00 0.1238E+01 0.5000E+00 0.2210E+02 0.6288E+00 0.1563E+01 0.6250E+00 0.2243E+02 0.7851E+00 0.1925E+01 0.7812E+00 0.2316E+02 0.1204E+01 0.2746E+01 0.1200E+01

Page 5

existing phase2 87 uplift.sfo =========================================================================

SHAFT for Windows, Version 2012.7.9

Serial Number : 292734667

VERTICALLY LOADED DRILLED SHAFT ANALYSIS (c) Copyright ENSOFT, Inc., 1987-2012 All Rights Reserved

=========================================================================

Path to file locations : \\losangeles.na.aecomnet.com\LosAngeles\Projects\ENV\_legacy\GT\Da Wu\LA County Geotech On-call\MLK\Report\2019 BHC - Lab\Appendix F and G\ Name of input data file : .sfd Name of output file : .sfo Name of plot output file : .sfp Name of runtime file : .sfr

------------------------------------------------------------------------- Time and Date of Analysis -------------------------------------------------------------------------

Date: March 21, 2019 Time: 13:31:21 MLK Medical Campus: Relocated Red Bag Storage and Future DHS Regional La

PROPOSED DEPTH = 29.0 FT ----------------

REDUCTION FACTOR APPLIED FOR UPLIFT FRICTION = 0.600 ----------------------------------------------

NUMBER OF LAYERS = 6 ------------------

WATER TABLE DEPTH = 0.0 FT. -------------------

FACTOR OF SAFETY APPLIED TO THE ULTIMATE SIDE FRICTION CAPACITY = 2.50 ------------------------------------------------------- FACTOR OF SAFETY APPLIED TO THE ULTIMATE BASE CAPACITY = 3.00 ------------------------------------------------------

SOIL INFORMATION ---------------

LAYER NO 1----SAND

AT THE TOP

SKIN FRICTION COEFFICIENT- BETA = 0.120E+01 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00

Page 1

existing phase2 87 uplift.sfo INTERNAL FRICTION ANGLE, DEG. = 0.280E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.125E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11 DEPTH, FT = 0.000E+00

AT THE BOTTOM

SKIN FRICTION COEFFICIENT- BETA = 0.107E+01 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.280E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.125E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11 DEPTH, FT = 0.100E+02

LAYER NO 2----SAND

AT THE TOP

SKIN FRICTION COEFFICIENT- BETA = 0.107E+01 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.310E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.130E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11 DEPTH, FT = 0.100E+02

AT THE BOTTOM

SKIN FRICTION COEFFICIENT- BETA = 0.977E+00 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.310E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.130E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11 DEPTH, FT = 0.150E+02

LAYER NO 3----SAND

AT THE TOP

SKIN FRICTION COEFFICIENT- BETA = 0.977E+00 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.300E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.125E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11 DEPTH, FT = 0.150E+02

AT THE BOTTOM

SKIN FRICTION COEFFICIENT- BETA = 0.825E+00 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.300E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.125E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11

Page 2

existing phase2 87 uplift.sfo DEPTH, FT = 0.250E+02

LAYER NO 4----SAND

AT THE TOP

SKIN FRICTION COEFFICIENT- BETA = 0.825E+00 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.310E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.110E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11 DEPTH, FT = 0.250E+02

AT THE BOTTOM

SKIN FRICTION COEFFICIENT- BETA = 0.646E+00 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.310E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.110E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11 DEPTH, FT = 0.400E+02

LAYER NO 5----CLAY

AT THE TOP

STRENGTH REDUCTION FACTOR-ALPHA = 0.550E+00 END BEARING COEFFICIENT-Nc = 0.900E+01 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.150E+04 INTERNAL FRICTION ANGLE, DEG. = 0.000E+00 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.120E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11 DEPTH, FT = 0.400E+02

AT THE BOTTOM

STRENGTH REDUCTION FACTOR-ALPHA = 0.550E+00 END BEARING COEFFICIENT-Nc = 0.900E+01 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.150E+04 INTERNAL FRICTION ANGLE, DEG. = 0.000E+00 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.120E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11 DEPTH, FT = 0.470E+02

LAYER NO 6----SAND

AT THE TOP

SKIN FRICTION COEFFICIENT- BETA = 0.574E+00 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.310E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.125E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11

Page 3

existing phase2 87 uplift.sfo DEPTH, FT = 0.470E+02

AT THE BOTTOM

SKIN FRICTION COEFFICIENT- BETA = 0.490E+00 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.310E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.125E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E+11 DEPTH, FT = 0.560E+02

DRILLED SHAFT INFORMATION -------------------------

DIAMETER OF STEM = 2.000 FT. DIAMETER OF BASE = 2.000 FT. END OF STEM TO BASE = 0.000 FT. ANGLE OF BELL = 0.000 DEG. IGNORED TOP PORTION = 20.000 FT. IGNORED BOTTOM PORTION = 0.000 FT. AREA OF ONE PERCENT STEEL = 4.524 SQ.IN. ELASTIC MODULUS, Ec = 0.350E+07 LB/SQ IN VOLUME OF UNDERREAM = 0.000 CU.YDS.

PREDICTED RESULTS -----------------

QS = ULTIMATE SIDE RESISTANCE; QB = ULTIMATE BASE RESISTANCE; WT = WEIGHT OF DRILLED SHAFT (FOR UPLIFT CAPACITY ONLY); QU = TOTAL ULTIMATE RESISTANCE; QBD = TOTAL ALLOWABLE LOAD USING A FACTOR OF SAFETY APPLIED TO THE ULTIMATE BASE RESISTANCE; QDN = TOTAL ALLOWABLE LOAD USING FACTORS OF SAFETY APPLIED TO THE ULTIMATE SIDE RESISTANCE AND THE ULTIMATE BASE RESISTANCE.

LENGTH VOLUME QS WT QU QBD QDN QU/VOLUME (FEET) (CU.YDS) (TONS) (TONS) (TONS) (TONS) (TONS) (TONS/CU.YDS) 21.0 2.44 2.13 2.89 5.02 5.02 3.74 2.06 22.0 2.56 4.33 3.03 7.36 7.36 4.76 2.87 23.0 2.68 6.60 3.17 9.76 9.76 5.80 3.65 24.0 2.79 8.92 3.30 12.22 12.22 6.87 4.38 25.0 2.91 11.31 3.44 14.75 14.75 7.96 5.07 26.0 3.03 13.74 3.58 17.32 17.32 9.07 5.72 27.0 3.14 16.20 3.72 19.92 19.92 10.20 6.34 28.0 3.26 18.70 3.85 22.55 22.55 11.33 6.92 29.0 3.37 21.22 3.99 25.21 25.21 12.48 7.47

RESULT FROM TREND (AVERAGED) LINE

TOP LOAD TOP MOVEMENT TIP LOAD TIP MOVEMENT ton IN. ton IN.

Page 4

existing phase2 87 uplift.sfo 0.5978E-02 0.1171E-04 0.5821E-04 0.1000E-04 0.2989E-01 0.5857E-04 0.2910E-03 0.5000E-04 0.5978E-01 0.1171E-03 0.5821E-03 0.1000E-03 0.2989E+01 0.5857E-02 0.2910E-01 0.5000E-02 0.4487E+01 0.8786E-02 0.4366E-01 0.7500E-02 0.6000E+01 0.1172E-01 0.5821E-01 0.1000E-01 0.1474E+02 0.2923E-01 0.1455E+00 0.2500E-01 0.2505E+02 0.5723E-01 0.2910E+00 0.5000E-01 0.3072E+02 0.8390E-01 0.4366E+00 0.7500E-01 0.3389E+02 0.1098E+00 0.5821E+00 0.1000E+00 0.4100E+02 0.2620E+00 0.1424E+01 0.2500E+00 0.4187E+02 0.5124E+00 0.2297E+01 0.5000E+00 0.4218E+02 0.6376E+00 0.2629E+01 0.6250E+00 0.4259E+02 0.7940E+00 0.3066E+01 0.7812E+00 0.4348E+02 0.1213E+01 0.4051E+01 0.1200E+01

RESULT FROM UPPER-BOUND LINE

TOP LOAD TOP MOVEMENT TIP LOAD TIP MOVEMENT ton IN. ton IN. 0.8111E-02 0.1232E-04 0.8315E-04 0.1000E-04 0.4056E-01 0.6159E-04 0.4158E-03 0.5000E-04 0.8111E-01 0.1232E-03 0.8315E-03 0.1000E-03 0.4056E+01 0.6159E-02 0.4158E-01 0.5000E-02 0.6113E+01 0.9243E-02 0.6236E-01 0.7500E-02 0.8164E+01 0.1233E-01 0.8315E-01 0.1000E-01 0.1992E+02 0.3071E-01 0.2079E+00 0.2500E-01 0.3271E+02 0.5945E-01 0.4158E+00 0.5000E-01 0.3811E+02 0.8607E-01 0.6236E+00 0.7500E-01 0.4005E+02 0.1117E+00 0.8315E+00 0.1000E+00 0.4323E+02 0.2628E+00 0.1979E+01 0.2500E+00 0.4413E+02 0.5132E+00 0.2884E+01 0.5000E+00 0.4435E+02 0.6383E+00 0.3100E+01 0.6250E+00 0.4473E+02 0.7947E+00 0.3475E+01 0.7812E+00 0.4556E+02 0.1214E+01 0.4311E+01 0.1200E+01

RESULT FROM LOWER-BOUND LINE

TOP LOAD TOP MOVEMENT TIP LOAD TIP MOVEMENT ton IN. ton IN. 0.3884E-02 0.1112E-04 0.3326E-04 0.1000E-04 0.1942E-01 0.5559E-04 0.1663E-03 0.5000E-04 0.3884E-01 0.1112E-03 0.3326E-03 0.1000E-03 0.1942E+01 0.5559E-02 0.1663E-01 0.5000E-02 0.2913E+01 0.8338E-02 0.2495E-01 0.7500E-02 0.3884E+01 0.1112E-01 0.3326E-01 0.1000E-01 0.9634E+01 0.2777E-01 0.8315E-01 0.2500E-01 0.1739E+02 0.5502E-01 0.1663E+00 0.5000E-01 0.2328E+02 0.8173E-01 0.2495E+00 0.7500E-01 0.2770E+02 0.1080E+00 0.3326E+00 0.1000E+00 0.3877E+02 0.2613E+00 0.8681E+00 0.2500E+00 0.3961E+02 0.5117E+00 0.1710E+01 0.5000E+00 0.4001E+02 0.6369E+00 0.2159E+01 0.6250E+00 0.4045E+02 0.7933E+00 0.2658E+01 0.7812E+00 0.4141E+02 0.1213E+01 0.3792E+01 0.1200E+01

Page 5

Ultimate Axial Capacity (tons)D

epth

(ft

)

0 10 20 30 40 50 60 70 80 900

510

1520

2530

3540

4550

5560

Skin Friction

Tip Resistance

Total Capacity

Ultimate Axial Capacity (tons)D

epth

(ft

)

0 10 20 30 40 50 60 70 80 90

510

1520

2530

3540

4550

550

Skin Friction

Tip Resistance

Total Capacity

18new.sfo =========================================================================

SHAFT for Windows, Version 2012.7.9

Serial Number : 292734667

VERTICALLY LOADED DRILLED SHAFT ANALYSIS (c) Copyright ENSOFT, Inc., 1987-2012 All Rights Reserved

=========================================================================

Path to file locations : \\losangeles.na.aecomnet.com\LosAngeles\Projects\ENV\_legacy\GT\Da Wu\LA County Geotech On-call\MLK\Report\2019 BHC - Lab\Appendix F and G\ Name of input data file : .sfd Name of output file : .sfo Name of plot output file : .sfp Name of runtime file : .sfr

------------------------------------------------------------------------- Time and Date of Analysis -------------------------------------------------------------------------

Date: April 03, 2019 Time: 16:26:45 MLK Medical Campus: Relocated Red Bag Storage and Future DHS Regional La

PROPOSED DEPTH = 60.0 FT ----------------

NUMBER OF LAYERS = 6 ------------------

WATER TABLE DEPTH = 0.0 FT. -------------------

*********************WARNING********************** PLEASE PROVIDE THE SOIL DEPTH THAT IS TWO-DIAMETER DEEPER THAN THE TIP OF DRILLED SHAFTS

FACTOR OF SAFETY APPLIED TO THE ULTIMATE SIDE FRICTION CAPACITY = 2.50 ------------------------------------------------------- FACTOR OF SAFETY APPLIED TO THE ULTIMATE BASE CAPACITY = 3.00 ------------------------------------------------------

SOIL INFORMATION ---------------

LAYER NO 1----SAND

AT THE TOPPage 1

18new.sfo

SKIN FRICTION COEFFICIENT- BETA = 0.120E+01 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.280E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.125E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E-01 DEPTH, FT = 0.000E+00

AT THE BOTTOM

SKIN FRICTION COEFFICIENT- BETA = 0.107E+01 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.280E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.125E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E-01 DEPTH, FT = 0.100E+02

LAYER NO 2----SAND

AT THE TOP

SKIN FRICTION COEFFICIENT- BETA = 0.107E+01 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.310E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.130E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E-01 DEPTH, FT = 0.100E+02

AT THE BOTTOM

SKIN FRICTION COEFFICIENT- BETA = 0.977E+00 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.310E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.130E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E-01 DEPTH, FT = 0.150E+02

LAYER NO 3----SAND

AT THE TOP

SKIN FRICTION COEFFICIENT- BETA = 0.977E+00 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.300E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.125E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E-01 DEPTH, FT = 0.150E+02

AT THE BOTTOM

SKIN FRICTION COEFFICIENT- BETA = 0.825E+00 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.300E+02

Page 2

18new.sfo BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.125E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E-01 DEPTH, FT = 0.250E+02

LAYER NO 4----SAND

AT THE TOP

SKIN FRICTION COEFFICIENT- BETA = 0.825E+00 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.310E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.110E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.400E+04 DEPTH, FT = 0.250E+02

AT THE BOTTOM

SKIN FRICTION COEFFICIENT- BETA = 0.646E+00 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.310E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.110E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.400E+04 DEPTH, FT = 0.400E+02

LAYER NO 5----CLAY

AT THE TOP

STRENGTH REDUCTION FACTOR-ALPHA = 0.550E+00 END BEARING COEFFICIENT-Nc = 0.900E+01 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.150E+04 INTERNAL FRICTION ANGLE, DEG. = 0.000E+00 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.120E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.400E+04 DEPTH, FT = 0.400E+02

AT THE BOTTOM

STRENGTH REDUCTION FACTOR-ALPHA = 0.550E+00 END BEARING COEFFICIENT-Nc = 0.900E+01 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.150E+04 INTERNAL FRICTION ANGLE, DEG. = 0.000E+00 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.120E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.400E+04 DEPTH, FT = 0.470E+02

LAYER NO 6----SAND

AT THE TOP

SKIN FRICTION COEFFICIENT- BETA = 0.574E+00 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.310E+02

Page 3

18new.sfo BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.125E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.400E+04 DEPTH, FT = 0.470E+02

AT THE BOTTOM

SKIN FRICTION COEFFICIENT- BETA = 0.490E+00 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.310E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.125E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.400E+04 DEPTH, FT = 0.560E+02

DRILLED SHAFT INFORMATION -------------------------

DIAMETER OF STEM = 1.500 FT. DIAMETER OF BASE = 1.500 FT. END OF STEM TO BASE = 0.000 FT. ANGLE OF BELL = 0.000 DEG. IGNORED TOP PORTION = 23.000 FT. IGNORED BOTTOM PORTION = 0.000 FT. AREA OF ONE PERCENT STEEL = 2.545 SQ.IN. ELASTIC MODULUS, Ec = 0.350E+07 LB/SQ IN VOLUME OF UNDERREAM = 0.000 CU.YDS.

PREDICTED RESULTS -----------------

QS = ULTIMATE SIDE RESISTANCE; QB = ULTIMATE BASE RESISTANCE; WT = WEIGHT OF DRILLED SHAFT (FOR UPLIFT CAPACITY ONLY); QU = TOTAL ULTIMATE RESISTANCE; QBD = TOTAL ALLOWABLE LOAD USING A FACTOR OF SAFETY APPLIED TO THE ULTIMATE BASE RESISTANCE; QDN = TOTAL ALLOWABLE LOAD USING FACTORS OF SAFETY APPLIED TO THE ULTIMATE SIDE RESISTANCE AND THE ULTIMATE BASE RESISTANCE.

LENGTH VOLUME QS QB QU QBD QDN QU/VOLUME (FEET) (CU.YDS) (TONS) (TONS) (TONS) (TONS) (TONS) (TONS/CU.YDS) 24.0 1.57 2.91 0.00 2.91 2.91 1.16 1.85 25.0 1.64 5.89 0.00 5.89 5.89 2.36 3.60 26.0 1.70 8.93 0.00 8.93 8.93 3.57 5.25 27.0 1.77 12.01 0.00 12.01 12.01 4.80 6.79 28.0 1.83 15.12 0.00 15.12 15.12 6.05 8.25 29.0 1.90 18.28 0.00 18.28 18.28 7.31 9.63 30.0 1.96 21.47 0.00 21.47 21.47 8.59 10.93 31.0 2.03 24.69 0.00 24.69 24.69 9.88 12.17 32.0 2.09 27.94 0.00 27.94 27.94 11.18 13.34 33.0 2.16 31.22 0.00 31.22 31.22 12.49 14.45 34.0 2.23 34.53 0.00 34.53 34.53 13.81 15.52 35.0 2.29 37.87 0.00 37.87 37.87 15.15 16.53 36.0 2.36 41.22 0.00 41.22 41.22 16.49 17.49

Page 4

18new.sfo 37.0 2.42 44.60 0.00 44.60 44.60 17.84 18.42 38.0 2.49 48.00 0.00 48.00 48.00 19.20 19.30 39.0 2.55 51.42 0.00 51.42 51.42 20.57 20.14 40.0 2.62 54.85 0.00 54.85 54.85 21.94 20.95 41.0 2.68 56.80 0.00 56.80 56.80 22.72 21.16 42.0 2.75 58.74 0.00 58.74 58.74 23.50 21.37 43.0 2.81 60.68 0.00 60.68 60.68 24.27 21.56 44.0 2.88 62.63 0.00 62.63 62.63 25.05 21.74 45.0 2.95 64.57 0.00 64.57 64.57 25.83 21.92 46.0 3.01 66.52 0.00 66.52 66.52 26.61 22.09 47.0 3.08 68.46 0.00 68.46 68.46 27.38 22.25 48.0 3.14 72.07 0.00 72.07 72.07 28.83 22.94 49.0 3.21 75.70 0.00 75.70 75.70 30.28 23.60 50.0 3.27 79.35 0.00 79.35 79.35 31.74 24.24 51.0 3.34 83.02 0.00 83.02 83.02 33.21 24.87 52.0 3.40 86.69 0.00 86.69 86.69 34.68 25.47

RESULT FROM TREND (AVERAGED) LINE

TOP LOAD TOP MOVEMENT TIP LOAD TIP MOVEMENT ton IN. ton IN. 0.3448E-01 0.3591E-04 0.1718E-09 0.1000E-04 0.1724E+00 0.1796E-03 0.8591E-09 0.5000E-04 0.3448E+00 0.3591E-03 0.1718E-08 0.1000E-03 0.1764E+02 0.1817E-01 0.8591E-07 0.5000E-02 0.2635E+02 0.2728E-01 0.1289E-06 0.7500E-02 0.3454E+02 0.3619E-01 0.1718E-06 0.1000E-01 0.6804E+02 0.7907E-01 0.4296E-06 0.2500E-01 0.9316E+02 0.1270E+00 0.8591E-06 0.5000E-01 0.1033E+03 0.1609E+00 0.1289E-05 0.7500E-01 0.1094E+03 0.1918E+00 0.1713E-05 0.1000E+00 0.1132E+03 0.3454E+00 0.4011E-05 0.2500E+00 0.1119E+03 0.5939E+00 0.6097E-05 0.5000E+00 0.1118E+03 0.7188E+00 0.7077E-05 0.6250E+00 0.1117E+03 0.8750E+00 0.8182E-05 0.7812E+00 0.1116E+03 0.9937E+00 0.8969E-05 0.9000E+00

RESULT FROM UPPER-BOUND LINE

TOP LOAD TOP MOVEMENT TIP LOAD TIP MOVEMENT ton IN. ton IN. 0.5328E-01 0.4860E-04 0.2455E-09 0.1000E-04 0.2664E+00 0.2430E-03 0.1227E-08 0.5000E-04 0.5328E+00 0.4860E-03 0.2455E-08 0.1000E-03 0.2744E+02 0.2478E-01 0.1227E-06 0.5000E-02 0.4031E+02 0.3698E-01 0.1841E-06 0.7500E-02 0.5196E+02 0.4864E-01 0.2455E-06 0.1000E-01 0.9159E+02 0.9831E-01 0.6137E-06 0.2500E-01 0.1111E+03 0.1426E+00 0.1227E-05 0.5000E-01 0.1163E+03 0.1726E+00 0.1841E-05 0.7500E-01 0.1185E+03 0.2001E+00 0.2435E-05 0.1000E+00 0.1182E+03 0.3497E+00 0.5548E-05 0.2500E+00 0.1174E+03 0.5988E+00 0.7109E-05 0.5000E+00 0.1174E+03 0.7238E+00 0.7924E-05 0.6250E+00 0.1174E+03 0.8800E+00 0.8844E-05 0.7812E+00 0.1174E+03 0.9988E+00 0.9544E-05 0.9000E+00

Page 5

18new.sfo RESULT FROM LOWER-BOUND LINE

TOP LOAD TOP MOVEMENT TIP LOAD TIP MOVEMENT ton IN. ton IN. 0.1940E-01 0.2513E-04 0.9819E-10 0.1000E-04 0.9701E-01 0.1257E-03 0.4909E-09 0.5000E-04 0.1940E+00 0.2513E-03 0.9819E-09 0.1000E-03 0.9817E+01 0.1262E-01 0.4909E-07 0.5000E-02 0.1477E+02 0.1897E-01 0.7364E-07 0.7500E-02 0.1965E+02 0.2530E-01 0.9819E-07 0.1000E-01 0.4406E+02 0.6004E-01 0.2455E-06 0.2500E-01 0.7168E+02 0.1085E+00 0.4909E-06 0.5000E-01 0.8862E+02 0.1478E+00 0.7364E-06 0.7500E-01 0.9997E+02 0.1832E+00 0.9917E-06 0.1000E+00 0.1080E+03 0.3408E+00 0.2474E-05 0.2500E+00 0.1064E+03 0.5891E+00 0.5086E-05 0.5000E+00 0.1062E+03 0.7139E+00 0.6230E-05 0.6250E+00 0.1060E+03 0.8700E+00 0.7521E-05 0.7812E+00 0.1058E+03 0.9886E+00 0.8395E-05 0.9000E+00

Page 6

Ultimate Axial Capacity (tons)D

epth

(ft

)

0 10 20 30 40 50 60 70 80 90 100 110 1200

510

1520

2530

3540

4550

5560

Skin Friction

Tip Resistance

Total Capacity

24new.sfo =========================================================================

SHAFT for Windows, Version 2012.7.9

Serial Number : 292734667

VERTICALLY LOADED DRILLED SHAFT ANALYSIS (c) Copyright ENSOFT, Inc., 1987-2012 All Rights Reserved

=========================================================================

Path to file locations : \\losangeles.na.aecomnet.com\LosAngeles\Projects\ENV\_legacy\GT\Da Wu\LA County Geotech On-call\MLK\Report\2019 BHC - Lab\Appendix F and G\ Name of input data file : .sfd Name of output file : .sfo Name of plot output file : .sfp Name of runtime file : .sfr

------------------------------------------------------------------------- Time and Date of Analysis -------------------------------------------------------------------------

Date: April 08, 2019 Time: 11:27:32 MLK Medical Campus: Relocated Red Bag Storage and Future DHS Regional La

PROPOSED DEPTH = 60.0 FT ----------------

NUMBER OF LAYERS = 6 ------------------

WATER TABLE DEPTH = 0.0 FT. -------------------

*********************WARNING********************** PLEASE PROVIDE THE SOIL DEPTH THAT IS TWO-DIAMETER DEEPER THAN THE TIP OF DRILLED SHAFTS

FACTOR OF SAFETY APPLIED TO THE ULTIMATE SIDE FRICTION CAPACITY = 2.50 ------------------------------------------------------- FACTOR OF SAFETY APPLIED TO THE ULTIMATE BASE CAPACITY = 3.00 ------------------------------------------------------

SOIL INFORMATION ---------------

LAYER NO 1----SAND

AT THE TOPPage 1

24new.sfo

SKIN FRICTION COEFFICIENT- BETA = 0.120E+01 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.280E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.125E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E-01 DEPTH, FT = 0.000E+00

AT THE BOTTOM

SKIN FRICTION COEFFICIENT- BETA = 0.107E+01 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.280E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.125E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E-01 DEPTH, FT = 0.100E+02

LAYER NO 2----SAND

AT THE TOP

SKIN FRICTION COEFFICIENT- BETA = 0.107E+01 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.310E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.130E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E-01 DEPTH, FT = 0.100E+02

AT THE BOTTOM

SKIN FRICTION COEFFICIENT- BETA = 0.977E+00 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.310E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.130E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E-01 DEPTH, FT = 0.150E+02

LAYER NO 3----SAND

AT THE TOP

SKIN FRICTION COEFFICIENT- BETA = 0.977E+00 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.300E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.125E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E-01 DEPTH, FT = 0.150E+02

AT THE BOTTOM

SKIN FRICTION COEFFICIENT- BETA = 0.825E+00 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.300E+02

Page 2

24new.sfo BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.125E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.100E-01 DEPTH, FT = 0.250E+02

LAYER NO 4----SAND

AT THE TOP

SKIN FRICTION COEFFICIENT- BETA = 0.825E+00 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.310E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.110E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.400E+04 DEPTH, FT = 0.250E+02

AT THE BOTTOM

SKIN FRICTION COEFFICIENT- BETA = 0.646E+00 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.310E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.110E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.400E+04 DEPTH, FT = 0.400E+02

LAYER NO 5----CLAY

AT THE TOP

STRENGTH REDUCTION FACTOR-ALPHA = 0.550E+00 END BEARING COEFFICIENT-Nc = 0.900E+01 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.150E+04 INTERNAL FRICTION ANGLE, DEG. = 0.000E+00 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.120E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.400E+04 DEPTH, FT = 0.400E+02

AT THE BOTTOM

STRENGTH REDUCTION FACTOR-ALPHA = 0.550E+00 END BEARING COEFFICIENT-Nc = 0.900E+01 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.150E+04 INTERNAL FRICTION ANGLE, DEG. = 0.000E+00 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.120E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.400E+04 DEPTH, FT = 0.470E+02

LAYER NO 6----SAND

AT THE TOP

SKIN FRICTION COEFFICIENT- BETA = 0.574E+00 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.310E+02

Page 3

24new.sfo BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.125E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.400E+04 DEPTH, FT = 0.470E+02

AT THE BOTTOM

SKIN FRICTION COEFFICIENT- BETA = 0.490E+00 UNDRAINED SHEAR STRENGTH, LB/SQ FT = 0.000E+00 INTERNAL FRICTION ANGLE, DEG. = 0.310E+02 BLOWS PER FOOT FROM STANDARD PENETRATION TEST = 0.000E+00 SOIL UNIT WEIGHT, LB/CU FT = 0.125E+03 MAXIMUM LOAD TRANSFER FOR SOIL, LB/SQ FT = 0.400E+04 DEPTH, FT = 0.560E+02

DRILLED SHAFT INFORMATION -------------------------

DIAMETER OF STEM = 2.000 FT. DIAMETER OF BASE = 2.000 FT. END OF STEM TO BASE = 0.000 FT. ANGLE OF BELL = 0.000 DEG. IGNORED TOP PORTION = 23.000 FT. IGNORED BOTTOM PORTION = 0.000 FT. AREA OF ONE PERCENT STEEL = 4.524 SQ.IN. ELASTIC MODULUS, Ec = 0.350E+07 LB/SQ IN VOLUME OF UNDERREAM = 0.000 CU.YDS.

PREDICTED RESULTS -----------------

QS = ULTIMATE SIDE RESISTANCE; QB = ULTIMATE BASE RESISTANCE; WT = WEIGHT OF DRILLED SHAFT (FOR UPLIFT CAPACITY ONLY); QU = TOTAL ULTIMATE RESISTANCE; QBD = TOTAL ALLOWABLE LOAD USING A FACTOR OF SAFETY APPLIED TO THE ULTIMATE BASE RESISTANCE; QDN = TOTAL ALLOWABLE LOAD USING FACTORS OF SAFETY APPLIED TO THE ULTIMATE SIDE RESISTANCE AND THE ULTIMATE BASE RESISTANCE.

LENGTH VOLUME QS QB QU QBD QDN QU/VOLUME (FEET) (CU.YDS) (TONS) (TONS) (TONS) (TONS) (TONS) (TONS/CU.YDS) 24.0 2.79 3.88 0.00 3.88 3.88 1.55 1.39 25.0 2.91 7.85 0.00 7.85 7.85 3.14 2.70 26.0 3.03 11.90 0.00 11.90 11.90 4.76 3.93 27.0 3.14 16.01 0.00 16.01 16.01 6.40 5.10 28.0 3.26 20.17 0.00 20.17 20.17 8.07 6.19 29.0 3.37 24.37 0.00 24.37 24.37 9.75 7.22 30.0 3.49 28.62 0.00 28.62 28.62 11.45 8.20 31.0 3.61 32.92 0.00 32.92 32.92 13.17 9.13 32.0 3.72 37.26 0.00 37.26 37.26 14.90 10.00 33.0 3.84 41.63 0.00 41.63 41.63 16.65 10.84 34.0 3.96 46.04 0.00 46.04 46.04 18.42 11.64 35.0 4.07 50.49 0.00 50.49 50.49 20.19 12.40 36.0 4.19 54.96 0.00 54.96 54.96 21.99 13.12

Page 4

24new.sfo 37.0 4.31 59.47 0.00 59.47 59.47 23.79 13.81 38.0 4.42 64.00 0.00 64.00 64.00 25.60 14.47 39.0 4.54 68.56 0.00 68.56 68.56 27.42 15.11 40.0 4.65 73.14 0.00 73.14 73.14 29.25 15.71 41.0 4.77 75.73 0.00 75.73 75.73 30.29 15.87 42.0 4.89 78.32 0.00 78.32 78.32 31.33 16.02 43.0 5.00 80.91 0.00 80.91 80.91 32.37 16.17 44.0 5.12 83.51 0.00 83.51 83.51 33.40 16.31 45.0 5.24 86.10 0.00 86.10 86.10 34.44 16.44 46.0 5.35 88.69 0.00 88.69 88.69 35.48 16.57 47.0 5.47 91.28 0.00 91.28 91.28 36.51 16.69 48.0 5.59 96.10 0.00 96.10 96.10 38.44 17.20 49.0 5.70 100.94 0.00 100.94 100.94 40.37 17.70 50.0 5.82 105.80 0.00 105.80 105.80 42.32 18.18 51.0 5.93 110.69 0.00 110.69 110.69 44.27 18.65

RESULT FROM TREND (AVERAGED) LINE

TOP LOAD TOP MOVEMENT TIP LOAD TIP MOVEMENT ton IN. ton IN. 0.2805E-01 0.2236E-04 0.2291E-09 0.1000E-04 0.1402E+00 0.1118E-03 0.1146E-08 0.5000E-04 0.2805E+00 0.2236E-03 0.2291E-08 0.1000E-03 0.1415E+02 0.1121E-01 0.1146E-06 0.5000E-02 0.2129E+02 0.1684E-01 0.1718E-06 0.7500E-02 0.2842E+02 0.2247E-01 0.2291E-06 0.1000E-01 0.6599E+02 0.5456E-01 0.5728E-06 0.2500E-01 0.1015E+03 0.9632E-01 0.1146E-05 0.5000E-01 0.1197E+03 0.1303E+00 0.1718E-05 0.7500E-01 0.1297E+03 0.1598E+00 0.2291E-05 0.1000E+00 0.1459E+03 0.3177E+00 0.5603E-05 0.2500E+00 0.1437E+03 0.5663E+00 0.9040E-05 0.5000E+00 0.1436E+03 0.6913E+00 0.1035E-04 0.6250E+00 0.1435E+03 0.8475E+00 0.1207E-04 0.7812E+00 0.1433E+03 0.1266E+01 0.1595E-04 0.1200E+01

RESULT FROM UPPER-BOUND LINE

TOP LOAD TOP MOVEMENT TIP LOAD TIP MOVEMENT ton IN. ton IN. 0.4112E-01 0.2775E-04 0.3273E-09 0.1000E-04 0.2056E+00 0.1387E-03 0.1636E-08 0.5000E-04 0.4112E+00 0.2775E-03 0.3273E-08 0.1000E-03 0.2089E+02 0.1397E-01 0.1636E-06 0.5000E-02 0.3141E+02 0.2100E-01 0.2455E-06 0.7500E-02 0.4189E+02 0.2801E-01 0.3273E-06 0.1000E-01 0.9310E+02 0.6643E-01 0.8182E-06 0.2500E-01 0.1305E+03 0.1097E+00 0.1636E-05 0.5000E-01 0.1428E+03 0.1410E+00 0.2455E-05 0.7500E-01 0.1483E+03 0.1686E+00 0.3273E-05 0.1000E+00 0.1524E+03 0.3209E+00 0.7790E-05 0.2500E+00 0.1508E+03 0.5698E+00 0.1135E-04 0.5000E+00 0.1508E+03 0.6948E+00 0.1220E-04 0.6250E+00 0.1508E+03 0.8510E+00 0.1368E-04 0.7812E+00 0.1508E+03 0.1270E+01 0.1697E-04 0.1200E+01

RESULT FROM LOWER-BOUND LINEPage 5

24new.sfo

TOP LOAD TOP MOVEMENT TIP LOAD TIP MOVEMENT ton IN. ton IN. 0.1668E-01 0.1748E-04 0.1309E-09 0.1000E-04 0.8342E-01 0.8740E-04 0.6546E-09 0.5000E-04 0.1668E+00 0.1748E-03 0.1309E-08 0.1000E-03 0.8355E+01 0.8742E-02 0.6546E-07 0.5000E-02 0.1259E+02 0.1313E-01 0.9819E-07 0.7500E-02 0.1681E+02 0.1752E-01 0.1309E-06 0.1000E-01 0.4068E+02 0.4337E-01 0.3273E-06 0.2500E-01 0.7149E+02 0.8259E-01 0.6546E-06 0.5000E-01 0.9319E+02 0.1178E+00 0.9819E-06 0.7500E-01 0.1092E+03 0.1501E+00 0.1309E-05 0.1000E+00 0.1394E+03 0.3145E+00 0.3417E-05 0.2500E+00 0.1367E+03 0.5629E+00 0.6729E-05 0.5000E+00 0.1365E+03 0.6878E+00 0.8496E-05 0.6250E+00 0.1363E+03 0.8440E+00 0.1046E-04 0.7812E+00 0.1358E+03 0.1263E+01 0.1492E-04 0.1200E+01

Page 6

APPENDIX G LATERAL PILE ANALYSIS

APPENDIX G LATERAL PILE ANALYSIS

G-1

Pile lateral performances were estimated using the p-y curve approach.

BACKGROUND

Lateral pile analyses were performed using the computer program LPILE (Ensoft Inc., 2012). The program computes deflection, shear, and bending moments of laterally loaded piles. The program uses nonlinear p-y (lateral load-deflection) curves to model the soil behavior. These p-y curves can be either input or generated by the program. For sloping ground surfaces, a reduction factor is applied to the resisting soil force (p) based on the ratio of the difference between the passive and active earth pressures for a sloping ground surface to the difference between the passive and active earth pressure for a level surface. A movement module was also used in the analyses to evaluate the pile reaction against the moving soil. By using this technique, shear forces from piles to resist the movement can be obtained in order to model the pile pinning effect in other analyses.

Input parameters for the program include applied moments, lateral forces, axial load, head condition (free or fixed), pile geometry and stiffness, initial soil movement along the pile, and soil geometry and strength parameters. The soil parameters include soil type for internal p-y curve generation, unit weight, friction angle, shear strength, initial stiffness, and soil strain at 50 percent of maximum strength.

ANALYSES

Lateral pile analyses were performed for 18-inch and 24-inch cast-in-drilled-hole (CIDH) piles for the proposed tower foundations. Soil profiles and analyses parameters are provided in Table D1. The lateral pile analyses considered a single pile. For piles in a group or pile center-to-center spacing of less than 6 pile diameters, a group reduction factor should be considered. We judge that a factor of safety need not be applied for the results estimated using the p-y curve approach. Detailed analysis outputs are included at the end of this appendix.

TABLE G1 - SOIL INPUT PARAMETERS

SOIL TYPE DEPTH (ft) LPILEMODEL

EFFECTIVEUNIT

WEIGHT(pcf)

K(lb/inch3)

INTERNALFRICTION

ANGLE(degrees)

UNDRAINEDSHEAR

STRENGTH(psf)

e50

FILL –Silty Sand -5.5 to 10 Sand 125.0 90 28 -- --

ALLUVIUMPoorly-

graded Sand10 to 15 Sand 67.6 100 31 -- --

ALLUVIUM–Silty Sand 15 to 25 Sand 62.6 90 30 -- --

ALLUVIUM–

Poorly/Well-graded Sand

25 to 40 Sand 47.6 100 31 1,500 0.01

ALLUVIUM–Silt 40 to 47 Clay 57.6 60 -- -- --

ALLUVIUM- Silty Sand 47 to 56 Sand 62.6 100 31 -- --

Note:· Considering static loading conditions.· Groundwater at 14.5 bgs (Elevation 78 feet).

Lateral Deflection (inches)D

epth

(ft)

-0.1 0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 10

12

34

56

78

910

1112

1314

1516

1718

19

Case 1Case 2Case 3Case 4Case 5Case 6Case 7Case 8Case 9Case 10Case 11Case 12Case 13Case 14

Bending Moment (in-kips)D

epth

(ft)

-1000 -800 -600 -400 -200 0 200 400 600 8000

12

34

56

78

910

1112

1314

1516

1718

19

Case 1Case 2Case 3Case 4Case 5Case 6Case 7Case 8Case 9Case 10Case 11Case 12Case 13Case 14

Shear Force (kips)D

epth

(ft)

-10 0 10 20 30 40 50 60 70 800

12

34

56

78

910

1112

1314

1516

1718

19

Case 1Case 2Case 3Case 4Case 5Case 6Case 7Case 8Case 9Case 10Case 11Case 12Case 13Case 14

existing phase1 81.lp6o================================================================================

LPile Plus for Windows, Version 2012-06.037

Analysis of Individual Piles and Drilled Shafts Subjected to Lateral Loading Using the p-y Method

© 1985-2012 by Ensoft, Inc. All Rights Reserved

================================================================================

This copy of LPile is licensed to:

Dennis NguyenAECOM

Serial Number of Security Device: 160777832Company Name Stored in Security Device: AECOM (URS)

-------------------------------------------------------------------------------- Files Used for Analysis--------------------------------------------------------------------------------

Path to file locations:\\losangeles.na.aecomnet.com\LosAngeles\Projects\ENV\_legacy\GT\Da Wu\LA County Geotech On-call\MLK\Report\2019 BHC - Lab\Appendix F and G\Name of input data file: existing phase1 81.lp6dName of output report file: existing phase1 81.lp6oName of plot output file: existing phase1 81.lp6pName of runtime messeage file: existing phase1 81.lp6r

-------------------------------------------------------------------------------- Date and Time of Analysis--------------------------------------------------------------------------------

Date: March 12, 2019 Time: 13:38:08

-------------------------------------------------------------------------------- Problem Title--------------------------------------------------------------------------------

Project Name: MLK DHS Lab & Red Bag Storage

Job Number: 60595699

Client: LACDPW

Engineer: Dennis Nguyen

Description:

Page 1

existing phase1 81.lp6o

-------------------------------------------------------------------------------- Program Options--------------------------------------------------------------------------------

Engineering units are US Customary Units: pounds, inches, feet

Basic Program Options:

This analysis computes pile response to lateral loading and will compute nonlinear moment-curvature and nominal moment capacity for section types with nonlinear properties.

Computation Options:- Analysis does not use p-y multipliers (individual pile or shaft only)- Analysis assumes no shear resistance at pile tip- Analysis for fixed-length pile or shaft only- No computation of foundation stiffness matrix values- Report pile response for full length of pile- Analysis assumes no loading by soil movements acting on pile- No p-y curves to be computed and reported for user-specified depths

Solution Control Parameters:- Number of pile increments = 100- Maximum number of iterations allowed = 100- Deflection tolerance for convergence = 1.0000E-05 in- Maximum allowable deflection = 100.0000 in

Pile Response Output Options:- Values of pile-head deflection, bending moment, shear force, and soil reaction are printed for full length of pile.- Printing Increment (nodal spacing of output points) = 1

-------------------------------------------------------------------------------- Pile Structural Properties and Geometry--------------------------------------------------------------------------------

Total number of pile sections = 1

Total length of pile = 20.00 ft

Depth of ground surface below top of pile = -9.00 ft

Pile diameter values used for p-y curve computations are defined using 2 points.

p-y curves are computed using pile diameter values interpolated with depth over the length of the pile.

Point Depth Pile X Diameter ft in----- --------- ----------- 1 0.00000 24.0000000 2 20.000000 24.0000000

Input Structural Properties:----------------------------

Page 2

existing phase1 81.lp6oPile Section No. 1:

Section Type = Drilled Shaft (Bored Pile) Section Length = 20.00000000 ft Section Diameter = 24.00000000 in

-------------------------------------------------------------------------------- Ground Slope and Pile Batter Angles--------------------------------------------------------------------------------

Ground Slope Angle = 0.000 degrees = 0.000 radians

Pile Batter Angle = 0.000 degrees = 0.000 radians

-------------------------------------------------------------------------------- Soil and Rock Layering Information--------------------------------------------------------------------------------

The soil profile is modelled using 6 layers

Layer 1 is sand, p-y criteria by Reese et al., 1974

Distance from top of pile to top of layer = -9.00000 ft Distance from top of pile to bottom of layer = 4.00000 ft Effective unit weight at top of layer = 125.00000 pcf Effective unit weight at bottom of layer = 125.00000 pcf Friction angle at top of layer = 28.00000 deg. Friction angle at bottom of layer = 28.00000 deg. Subgrade k at top of layer = 0.0000 pci Subgrade k at bottom of layer = 0.0000 pci

NOTE: Internal default values for subgrade k will be computed for the above soil layer.

Layer 2 is sand, p-y criteria by Reese et al., 1974

Distance from top of pile to top of layer = 4.00000 ft Distance from top of pile to bottom of layer = 9.00000 ft Effective unit weight at top of layer = 67.60000 pcf Effective unit weight at bottom of layer = 67.60000 pcf Friction angle at top of layer = 31.00000 deg. Friction angle at bottom of layer = 31.00000 deg. Subgrade k at top of layer = 0.0000 pci Subgrade k at bottom of layer = 0.0000 pci

NOTE: Internal default values for subgrade k will be computed for the above soil layer.

Layer 3 is sand, p-y criteria by Reese et al., 1974

Distance from top of pile to top of layer = 9.00000 ft Distance from top of pile to bottom of layer = 19.00000 ft Effective unit weight at top of layer = 62.60000 pcf Effective unit weight at bottom of layer = 62.60000 pcf Friction angle at top of layer = 30.00000 deg.

Page 3

existing phase1 81.lp6o Friction angle at bottom of layer = 30.00000 deg. Subgrade k at top of layer = 0.0000 pci Subgrade k at bottom of layer = 0.0000 pci

NOTE: Internal default values for subgrade k will be computed for the above soil layer.

Layer 4 is sand, p-y criteria by Reese et al., 1974

Distance from top of pile to top of layer = 19.00000 ft Distance from top of pile to bottom of layer = 34.00000 ft Effective unit weight at top of layer = 47.60000 pcf Effective unit weight at bottom of layer = 47.60000 pcf Friction angle at top of layer = 31.00000 deg. Friction angle at bottom of layer = 31.00000 deg. Subgrade k at top of layer = 0.0000 pci Subgrade k at bottom of layer = 0.0000 pci

NOTE: Internal default values for subgrade k will be computed for the above soil layer.

Layer 5 is soft clay, p-y criteria by Matlock, 1970

Distance from top of pile to top of layer = 34.00000 ft Distance from top of pile to bottom of layer = 41.00000 ft Effective unit weight at top of layer = 57.60000 pcf Effective unit weight at bottom of layer = 57.60000 pcf Undrained cohesion at top of layer = 1500.00000 psf Undrained cohesion at bottom of layer = 1500.00000 psf Epsilon-50 at top of layer = 0.0000 Epsilon-50 at bottom of layer = 0.0000

NOTE: Internal default values for Epsilon-50 will be computed for the above soil layer.

Layer 6 is sand, p-y criteria by Reese et al., 1974

Distance from top of pile to top of layer = 41.00000 ft Distance from top of pile to bottom of layer = 50.00000 ft Effective unit weight at top of layer = 62.60000 pcf Effective unit weight at bottom of layer = 62.60000 pcf Friction angle at top of layer = 31.00000 deg. Friction angle at bottom of layer = 31.00000 deg. Subgrade k at top of layer = 0.0000 pci Subgrade k at bottom of layer = 0.0000 pci

NOTE: Internal default values for subgrade k will be computed for the above soil layer.

(Depth of lowest soil layer extends 30.00 ft below pile tip)

-------------------------------------------------------------------------------- Summary of Soil Properties--------------------------------------------------------------------------------

Layer Layer Effective UndrainedAngle of Strain

Page 4

existing phase1 81.lp6oLayer Soil Type Depth Unit Wt. CohesionFriction Factor kpy Num. (p-y Curve Criteria) ft pcf psf deg. Epsilon 50 pci----- ---------------------------------- ---------- ---------- -------------------- ---------- ---------- 1 Sand (Reese, et al.) -9.000 125.000 -- 28.000 -- default 4.000 125.000 -- 28.000 -- default 2 Sand (Reese, et al.) 4.000 67.600 -- 31.000 -- default 9.000 67.600 -- 31.000 -- default 3 Sand (Reese, et al.) 9.000 62.600 -- 30.000 -- default 19.000 62.600 -- 30.000 -- default 4 Sand (Reese, et al.) 19.000 47.600 -- 31.000 -- default 34.000 47.600 -- 31.000 -- default 5 Soft Clay 34.000 57.600 1500.000 -- default -- 41.000 57.600 1500.000 -- default -- 6 Sand (Reese, et al.) 41.000 62.600 -- 31.000 -- default 50.000 62.600 -- 31.000 -- default

-------------------------------------------------------------------------------- Loading Type--------------------------------------------------------------------------------

Static loading criteria were used when computing p-y curves for all analyses.

-------------------------------------------------------------------------------- Pile-head Loading and Pile-head Fixity Conditions--------------------------------------------------------------------------------

Number of loads specified = 14

Load Load Condition Condition Axial Thrust Compute No. Type 1 2 Force, lbsTop y vs. Pile Length----- ---- -------------------- ----------------------- ------------------------------------- 1 4 y = 0.01000 in M = 0.0000 in-lbs 10000.00000000 Yes 2 4 y = 0.10000 in M = 0.0000 in-lbs 10000.00000000 Yes 3 4 y = 0.20000 in M = 0.0000 in-lbs 10000.00000000 Yes 4 4 y = 0.30000 in M = 0.0000 in-lbs 10000.00000000 Yes 5 4 y = 0.50000 in M = 0.0000 in-lbs 10000.00000000 No

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existing phase1 81.lp6o 6 4 y = 0.75000 in M = 0.0000 in-lbs 10000.00000000 No 7 4 y = 1.00000 in M = 0.0000 in-lbs 10000.00000000 No 8 5 y = 0.01000 in S = 0.0000 in/in 10000.00000000 No 9 5 y = 0.10000 in S = 0.0000 in/in 10000.00000000 No 10 5 y = 0.20000 in S = 0.0000 in/in 10000.00000000 No 11 5 y = 0.30000 in S = 0.0000 in/in 10000.00000000 No 12 5 y = 0.50000 in S = 0.0000 in/in 10000.00000000 No 13 5 y = 0.75000 in S = 0.0000 in/in 10000.00000000 No 14 5 y = 1.00000 in S = 0.0000 in/in 10000.00000000 No

V = perpendicular shear force applied to pile headM = bending moment applied to pile heady = lateral deflection relative to pile axisS = pile slope relative to original pile batter angleR = rotational stiffness applie to pile headAxial thrust is assumed to be acting axially for all pile batter angles.

-------------------------------------------------------------------------------- Computations of Nominal Moment Capacity and Nonlinear Bending Stiffness--------------------------------------------------------------------------------

Axial thrust force values were determined from pile-head loading conditions

Number of Pile Sections Analyzed = 1

Pile Section No. 1:-------------------

Dimensions and Properties of Drilled Shaft (Bored Pile):--------------------------------------------------------

Length of Section = 20.00000000 ftShaft Diameter = 24.00000000 inConcrete Cover Thickness = 3.00000000 inNumber of Reinforcing Bars = 12 barsYield Stress of Reinforcing Bars = 60.00000000 ksiModulus of Elasticity of Reinforcing Bars = 29000. ksiGross Area of Shaft = 452.38934212 sq. in.Total Area of Reinforcing Steel = 1.32000000 sq. in.Area Ratio of Steel Reinforcement = 0.29 percentEdge-to-Edge Bar Spacing = 4.18668567 inMaximum Concrete Aggregate Size = 0.75000000 inRatio of Bar Spacing to Aggregate Size = 5.58Offset of Rebar Cage Center from Center of Pile = 0.0000000 in

Axial Structural Capacities:----------------------------

Nom. Axial Structural Capacity = 0.85 Fc Ac + Fy As = 1229.427 kipsTensile Load for Cracking of Concrete = -167.736 kipsNominal Axial Tensile Capacity = -79.200 kips

Page 6

existing phase1 81.lp6oReinforcing Bar Dimensions and Positions Used in Computations:

Bar Bar Diam. Bar Area X Y Number inches sq. in. inches inches ---------- ---------- ---------- ---------- ---------- 1 0.37500 0.11000 8.81250 0.00000 2 0.37500 0.11000 7.63185 4.40625 3 0.37500 0.11000 4.40625 7.63185 4 0.37500 0.11000 0.00000 8.81250 5 0.37500 0.11000 -4.40625 7.63185 6 0.37500 0.11000 -7.63185 4.40625 7 0.37500 0.11000 -8.81250 0.00000 8 0.37500 0.11000 -7.63185 -4.40625 9 0.37500 0.11000 -4.40625 -7.63185 10 0.37500 0.11000 0.00000 -8.81250 11 0.37500 0.11000 4.40625 -7.63185 12 0.37500 0.11000 7.63185 -4.40625

NOTE: The positions of the above rebars were computed by LPile

Minimum spacing between any two bars not equal to zero = 4.18669 inches betweenBars 7 and 8

Spacing to aggregate size ratio = 5.58225

Concrete Properties:--------------------

Compressive Strength of Concrete = 3.00000000 ksiModulus of Elasticity of Concrete = 3122.01857778 ksiModulus of Rupture of Concrete = -0.41079191 ksiCompression Strain at Peak Stress = 0.00163356Tensile Strain at Fracture of Concrete = -0.00011596Maximum Coarse Aggregate Size = 0.75000000 in

Number of Axial Thrust Force Values Determined from Pile-head Loadings = 1

Number Axial Thrust Force kips ------ ------------------ 1 10.000

Definitions of Run Messages and Notes:--------------------------------------

C = concrete in section has cracked in tension. Y = stress in reinforcing steel has reached yield stress. T = ACI 318-08 criteria for tension-controlled section met, tensile strain in reinforcement exceeds 0.005 while simultaneously compressive strain in concrete more than than 0.003. See ACI 318-08, Section 10.3.4. Z = depth of tensile zone in concrete section is less than 10 percent of section depth.

Bending Stiffness (EI) = Computed Bending Moment / Curvature.Position of neutral axis is measured from edge of compression side of pile.Compressive stresses and strains are positive in sign.Tensile stresses and strains are negative in sign.

Page 7

existing phase1 81.lp6oAxial Thrust Force = 10.000 kips

Bending Bending Bending Depth to Max Comp Max Tens Max Concrete Max Steel Run Curvature Moment Stiffness N Axis Strain Strain Stress Stress Msg rad/in. in-kip kip-in2 in in/in in/in ksi ksi ------------- ------------- ------------- ------------- ------------- -------------------------- ------------- --- 0.000001250 76.0873440 60869875. 16.7390877 0.0000209 -0.000009076 0.0758165 0.6024419 0.000002500 151.7934938 60717398. 14.3782869 0.0000359 -0.0000241 0.1294969 1.0337258 0.000003750 227.0367332 60543129. 13.5915522 0.0000510 -0.0000390 0.1826828 1.4650313 0.000005000 301.8152914 60363058. 13.1982492 0.0000660 -0.0000540 0.2353724 1.8963461 0.000006250 376.1289456 60180631. 12.9623053 0.0000810 -0.0000690 0.2875655 2.3276679 0.000007500 449.9776413 59997019. 12.8050375 0.0000960 -0.0000840 0.3392620 2.7589957 0.000008750 523.3613581 59812727. 12.6927260 0.0001111 -0.0000989 0.3904617 3.1903293 0.0000100 596.2800896 59628009. 12.6085121 0.0001261 -0.0001139 0.4411647 3.6216685 0.0000113 596.2800896 53002675. 6.8532370 0.0000771 -0.0001929 0.2717723 -5.5549814 C 0.0000125 596.2800896 47702407. 6.6410432 0.0000830 -0.0002170 0.2919246 -6.2491219 C 0.0000138 596.2800896 43365825. 6.4607446 0.0000888 -0.0002412 0.3116826 -6.9459281 C 0.0000150 596.2800896 39752006. 6.3064990 0.0000946 -0.0002654 0.3311606 -7.6444729 C 0.0000163 596.2800896 36694159. 6.1718983 0.0001003 -0.0002897 0.3503387 -8.3449429 C 0.0000175 596.2800896 34073148. 6.0533951 0.0001059 -0.0003141 0.3692591 -9.0470019 C 0.0000188 596.2800896 31801605. 5.9485044 0.0001115 -0.0003385 0.3879711 -9.7502507 C 0.0000200 596.2800896 29814004. 5.8556156 0.0001171 -0.0003629 0.4065405 -10.4541429 C 0.0000213 596.2800896 28060240. 5.7705071 0.0001226 -0.0003874 0.4248161 -11.1599749 C 0.0000225 596.2800896 26501337. 5.6949845 0.0001281 -0.0004119 0.4430370 -11.8657226 C 0.0000238 596.2800896 25106530. 5.6268263 0.0001336 -0.0004364 0.4611462 -12.5718733 C 0.0000250 596.2800896 23851204. 5.5627914 0.0001391 -0.0004609 0.4789643 -13.2799762 C 0.0000263 596.2800896 22715432. 5.5049647 0.0001445 -0.0004855 0.4967294 -13.9879955 C 0.0000275 596.2800896 21682912. 5.4524998 0.0001499 -0.0005101 0.5144414 -14.6959313 C 0.0000288 596.2800896 20740177. 5.4046976 0.0001554 -0.0005346 0.5321000 -15.4037833 C 0.0000300 596.2800896 19876003. 5.3586531 0.0001608 -0.0005592 0.5494741 -16.1135717 C 0.0000313 596.2800896 19080963. 5.3161276 0.0001661 -0.0005839 0.5667697 -16.8235093 C 0.0000325 596.2800896 18347080. 5.2769621 0.0001715 -0.0006085 0.5840137 -17.5333631 C 0.0000338 596.2800896 17667558. 5.2407837 0.0001769 -0.0006331

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existing phase1 81.lp6o 0.6012058 -18.2431328 C 0.0000350 596.2800896 17036574. 5.2072725 0.0001823 -0.0006577 0.6183461 -18.9528183 C 0.0000363 596.2800896 16449106. 5.1761527 0.0001876 -0.0006824 0.6354344 -19.6624194 C 0.0000375 596.2800896 15900802. 5.1463845 0.0001930 -0.0007070 0.6523730 -20.3728068 C 0.0000388 596.2800896 15387873. 5.1176695 0.0001983 -0.0007317 0.6691420 -21.0841687 C 0.0000400 596.2800896 14907002. 5.0908231 0.0002036 -0.0007564 0.6858604 -21.7954451 C 0.0000413 596.2800896 14455275. 5.0656756 0.0002090 -0.0007810 0.7025282 -22.5066355 C 0.0000425 596.2800896 14030120. 5.0420771 0.0002143 -0.0008057 0.7191452 -23.2177398 C 0.0000438 596.2800896 13629259. 5.0198952 0.0002196 -0.0008304 0.7357114 -23.9287578 C 0.0000450 596.2800896 13250669. 4.9990120 0.0002250 -0.0008550 0.7522267 -24.6396892 C 0.0000463 596.2800896 12892542. 4.9793223 0.0002303 -0.0008797 0.7686910 -25.3505338 C 0.0000475 596.2800896 12553265. 4.9607321 0.0002356 -0.0009044 0.7851043 -26.0612913 C 0.0000488 596.2800896 12231386. 4.9431570 0.0002410 -0.0009290 0.8014665 -26.7719616 C 0.0000513 596.2800896 11634733. 4.9101443 0.0002516 -0.0009784 0.8339394 -28.1939480 C 0.0000538 596.2800896 11093583. 4.8790479 0.0002622 -0.0010278 0.8659784 -29.6177339 C 0.0000563 596.2800896 10600535. 4.8509378 0.0002729 -0.0010771 0.8978171 -31.0411575 C 0.0000588 596.2800896 10149448. 4.8254339 0.0002835 -0.0011265 0.9294549 -32.4642168 C 0.0000613 596.2800896 9735185. 4.8022184 0.0002941 -0.0011759 0.9608910 -33.8869094 C 0.0000638 596.2800896 9353413. 4.7810231 0.0003048 -0.0012252 0.9921249 -35.3092333 C 0.0000663 596.2800896 9000454. 4.7616206 0.0003155 -0.0012745 1.0231559 -36.7311862 C 0.0000688 596.2800896 8673165. 4.7438164 0.0003261 -0.0013239 1.0539833 -38.1527659 C 0.0000713 596.2800896 8368843. 4.7274433 0.0003368 -0.0013732 1.0846065 -39.5739700 C 0.0000738 596.2800896 8085154. 4.7123570 0.0003475 -0.0014225 1.1150247 -40.9947963 C 0.0000763 596.2800896 7820067. 4.6984319 0.0003583 -0.0014717 1.1452373 -42.4152423 C 0.0000788 596.2800896 7571811. 4.6855583 0.0003690 -0.0015210 1.1752436 -43.8353059 C 0.0000813 596.2800896 7338832. 4.6731874 0.0003797 -0.0015703 1.2049383 -45.2560520 C 0.0000838 596.2800896 7119762. 4.6613503 0.0003904 -0.0016196 1.2343412 -46.6772951 C 0.0000863 596.2800896 6913392. 4.6503625 0.0004011 -0.0016689 1.2635405 -48.0981306 C 0.0000888 596.2800896 6718649. 4.6401531 0.0004118 -0.0017182 1.2925356 -49.5185556 C 0.0000913 596.2800896 6534576. 4.6306594 0.0004225 -0.0017675 1.3213257 -50.9385674 C 0.0000938 596.2800896 6360321. 4.6218250 0.0004333 -0.0018167 1.3499101 -52.3581630 C 0.0000963 596.2800896 6195118. 4.6135996 0.0004441 -0.0018659 1.3782881 -53.7773397 C

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existing phase1 81.lp6o 0.0000988 596.2800896 6038279. 4.6059381 0.0004548 -0.0019152 1.4064588 -55.1960945 C 0.0001013 596.2800896 5889186. 4.5987996 0.0004656 -0.0019644 1.4344217 -56.6144243 C 0.0001038 596.2800896 5747278. 4.5921474 0.0004764 -0.0020136 1.4621758 -58.0323263 C 0.0001063 596.2800896 5612048. 4.5859480 0.0004873 -0.0020627 1.4897204 -59.4497974 C 0.0001088 596.2800896 5483035. 4.5801713 0.0004981 -0.0021119 1.5170547 -60.0000000 CY 0.0001113 596.2800896 5359821. 4.5747897 0.0005089 -0.0021611 1.5441778 -60.0000000 CY 0.0001138 596.2800896 5242023. 4.5697781 0.0005198 -0.0022102 1.5710892 -60.0000000 CY 0.0001163 605.1262719 5205387. 4.5651137 0.0005307 -0.0022593 1.5977880 -60.0000000 CY 0.0001188 616.2166766 5189193. 4.5607753 0.0005416 -0.0023084 1.6242734 -60.0000000 CY 0.0001213 627.2967561 5173581. 4.5567439 0.0005525 -0.0023575 1.6505444 -60.0000000 CY 0.0001238 638.3664441 5158517. 4.5530017 0.0005634 -0.0024066 1.6766003 -60.0000000 CY 0.0001263 649.3102714 5143052. 4.5492886 0.0005743 -0.0024557 1.7023659 -60.0000000 CY 0.0001288 659.0459991 5118804. 4.5433314 0.0005850 -0.0025050 1.7271428 -60.0000000 CY 0.0001313 667.9088616 5088829. 4.5359197 0.0005953 -0.0025547 1.7511578 -60.0000000 CY 0.0001338 676.7549988 5059850. 4.5288687 0.0006057 -0.0026043 1.7749703 -60.0000000 CY 0.0001363 685.1641051 5028727. 4.5212629 0.0006160 -0.0026540 1.7982959 -60.0000000 CY 0.0001388 691.3993484 4983058. 4.5094436 0.0006257 -0.0027043 1.8199634 -60.0000000 CY 0.0001413 696.2920527 4929501. 4.4953197 0.0006350 -0.0027550 1.8405557 -60.0000000 CY 0.0001438 701.1797625 4877772. 4.4817545 0.0006443 -0.0028057 1.8609887 -60.0000000 CY 0.0001463 706.0624537 4827777. 4.4687196 0.0006536 -0.0028564 1.8812620 -60.0000000 CY 0.0001488 710.9401018 4779429. 4.4561888 0.0006629 -0.0029071 1.9013749 -60.0000000 CY 0.0001588 730.3435779 4600589. 4.4082369 0.0006998 -0.0031102 1.9793984 -60.0000000 CY 0.0001688 749.6077413 4442120. 4.3657018 0.0007367 -0.0033133 2.0544559 -60.0000000 CY 0.0001788 761.4479657 4259849. 4.3120389 0.0007708 -0.0035192 2.1210101 -60.0000000 CY 0.0001888 769.9967030 4079453. 4.2576705 0.0008036 -0.0037264 2.1828247 -60.0000000 CY 0.0001988 778.4996230 3916979. 4.2093895 0.0008366 -0.0039334 2.2426119 -60.0000000 CY 0.0002088 786.8480316 3769332. 4.1631469 0.0008691 -0.0041409 2.2991694 -60.0000000 CY 0.0002188 795.1252195 3634858. 4.1208986 0.0009014 -0.0043486 2.3534458 -60.0000000 CY 0.0002288 803.3586649 3511950. 4.0828946 0.0009340 -0.0045560 2.4057405 -60.0000000 CY 0.0002388 811.5477668 3399153. 4.0486107 0.0009666 -0.0047634 2.4560307 -60.0000000 CY 0.0002488 819.6916977 3295243. 4.0176074 0.0009994 -0.0049706 2.5042925 -60.0000000 CY 0.0002588 826.7932787 3195336. 3.9868321 0.0010316 -0.0051784

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existing phase1 81.lp6o 2.5495145 -60.0000000 CY 0.0002688 830.5391163 3090378. 3.9490801 0.0010613 -0.0053887 2.5891959 -60.0000000 CY 0.0002788 833.3685080 2989663. 3.9094511 0.0010898 -0.0056002 2.6253910 -60.0000000 CY 0.0002888 836.1741864 2895841. 3.8729171 0.0011183 -0.0058117 2.6600421 -60.0000000 CY 0.0002988 838.9557505 2808220. 3.8391717 0.0011470 -0.0060230 2.6931323 -60.0000000 CY 0.0003088 841.7127586 2726195. 3.8079485 0.0011757 -0.0062343 2.7246440 -60.0000000 CY 0.0003188 844.4447587 2649238. 3.7790144 0.0012046 -0.0064454 2.7545595 -60.0000000 CY 0.0003288 847.1512884 2576886. 3.7521652 0.0012335 -0.0066565 2.7828607 -60.0000000 CY 0.0003388 849.8318743 2508729. 3.7272206 0.0012626 -0.0068674 2.8095289 -60.0000000 CY 0.0003488 852.4089989 2444184. 3.7019733 0.0012911 -0.0070789 2.8339284 -60.0000000 CY 0.0003588 854.9293167 2383078. 3.6775697 0.0013193 -0.0072907 2.8564940 -60.0000000 CY 0.0003688 857.4258218 2325223. 3.6547894 0.0013477 -0.0075023 2.8774944 -60.0000000 CY 0.0003788 859.8982795 2270358. 3.6335086 0.0013762 -0.0077138 2.8969109 -60.0000000 CY 0.0003888 862.3462346 2218254. 3.6136169 0.0014048 -0.0079252 2.9147240 -60.0000000 CY 0.0003988 864.7692188 2168700. 3.5950147 0.0014335 -0.0081365 2.9309136 -60.0000000 CY 0.0004088 867.1667493 2121509. 3.5776127 0.0014623 -0.0083477 2.9454593 -60.0000000 CY 0.0004188 869.5383287 2076509. 3.5613301 0.0014913 -0.0085587 2.9583399 -60.0000000 CY 0.0004288 871.8834435 2033547. 3.5460940 0.0015204 -0.0087696 2.9695336 -60.0000000 CY 0.0004388 874.2015639 1992482. 3.5318382 0.0015496 -0.0089804 2.9790181 -60.0000000 CY 0.0004488 876.4921423 1953186. 3.5185030 0.0015789 -0.0091911 2.9867702 -60.0000000 CY 0.0004588 878.7546127 1915541. 3.5060336 0.0016084 -0.0094016 2.9927662 -60.0000000 CY 0.0004688 880.9883893 1879442. 3.4943806 0.0016380 -0.0096120 2.9969814 -60.0000000 CY 0.0004788 883.1928657 1844789. 3.4834988 0.0016677 -0.0098223 2.9993905 -60.0000000 CY 0.0004888 885.0224976 1810788. 3.4709132 0.0016964 -0.0100336 2.9991276 -60.0000000 CY 0.0004988 886.7873237 1778020. 3.4585692 0.0017250 -0.0102450 2.9934460 -60.0000000 CY 0.0005088 887.9821732 1745420. 3.4444561 0.0017524 -0.0104576 2.9953459 -60.0000000 CY 0.0005188 888.6173409 1712997. 3.4286611 0.0017786 -0.0106714 2.9980460 -60.0000000 CY 0.0005288 889.2382922 1681775. 3.4136627 0.0018050 -0.0108850 2.9995970 -60.0000000 CY 0.0005388 889.7845008 1651572. 3.3991749 0.0018313 -0.0110987 2.9992113 -60.0000000 CY 0.0005488 890.3014535 1622417. 3.3854861 0.0018578 -0.0113122 2.9944588 -60.0000000 CY 0.0006088 893.1490543 1467185. 3.3161623 0.0020187 -0.0125913 2.9958655 -60.0000000 CY 0.0006688 895.5530431 1339145. 3.2646906 0.0021833 -0.0138667 2.9998368 60.0000000 CY

Page 11

existing phase1 81.lp6o 0.0007288 897.4916889 1231549. 3.2233026 0.0023490 -0.0151410 2.9942323 60.0000000 CY 0.0007888 899.0579811 1139852. 3.1874194 0.0025141 -0.0164159 2.9940451 60.0000000 CY 0.0008488 900.3958393 1060849. 3.1601255 0.0026822 -0.0176878 2.9942121 60.0000000 CY 0.0009088 901.5573161 992085. 3.1392881 0.0028528 -0.0189572 2.9959040 60.0000000 CY 0.0009688 902.5306344 931645. 3.1239428 0.0030263 -0.0202237 2.9842164 60.0000000 CYT 0.0010288 903.3885835 878142. 3.1123773 0.0032019 -0.0214881 2.9984981 60.0000000 CYT 0.0010888 904.0891823 830392. 3.1045829 0.0033801 -0.0227499 2.9900077 60.0000000 CYT 0.0011488 904.6758641 787531. 3.0995034 0.0035606 -0.0240094 2.9777273 60.0000000 CYT 0.0012088 905.1776403 748854. 3.0964534 0.0037428 -0.0252672 2.9950328 60.0000000 CYT 0.0012688 905.5777865 713756. 3.0954236 0.0039273 -0.0265227 2.9979209 60.0000000 CYT

-------------------------------------------------------------------------------- Summary of Results for Nominal (Unfactored) Moment Capacity for Section 1--------------------------------------------------------------------------------

Moment values interpolated at maximum compressive strain = 0.003or maximum developed moment if pile fails at smaller strains.

Load Axial Thrust Nominal Mom. Cap. Max. Comp. No. kips in-kip Strain ---- ---------------- ------------------ ------------ 1 10.000 902.383 0.00300000

Note note that the values of moment capacity in the table above are not factored by a strength reduction factor (phi-factor).

In ACI 318-08, the value of the strength reduction factor depends on whether the transverse reinforcing steel bars are tied hoops (0.65) or spirals (0.70).

The above values should be multiplied by the appropriate strength reduction factor to compute ultimate moment capacity according to ACI 318-08, Section 9.3.2.2 or the value required by the design standard being followed.

The following table presents factored moment capacities and corresponding bending stiffnesses computed for common resistance factor values used for reinforced concrete sections.

Axial Resistance Nominal Ultimate (Factored) Ultimate (Factored) Bending Stiffness Load Factor Moment Capacity Axial Thrust Moment Capacity at Ult. Mom. Cap. No. for Moment in-kip kipsin-kip kip-in^2 ----- ---------- ------------------- -------------------------------------- ------------------- 1 0.65 902.383 6.500586.549 59652659.965

1 0.70 902.383 7.000631.668 5167632.554

1 0.75 902.383 7.500Page 12

existing phase1 81.lp6o676.787 5059731.157

-------------------------------------------------------------------------------- Computed Values of Pile Loading and Deflection for Lateral Loading for Load Case Number 1--------------------------------------------------------------------------------

Pile-head conditions are Displacement and Moment (Loading Type 4)Displacement of pile head = 0.010000 inchesMoment at pile head = 0.000 in-lbsAxial load at pile head = 10000.000 lbs

Depth Deflect. Bending Shear Slope Total Bending Soil Res. Soil Spr. Distrib. X y Moment Force S Stress Stiffness p Es*h Lat. Load feet inches in-lbs lbs radians psi* lb-in^2 lb/in lb/inch lb/inch ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- 0.00 0.0100 0.000 1549.9660 -0.000116 0.000 6.087E+10-22.7480 2729.7579 0.000 0.200 0.009721 3657.1950 1495.5430 -0.000116 0.000 6.087E+10-22.6045 5580.8384 0.000 0.400 0.009442 7184.1845 1441.4971 -0.000116 0.000 6.087E+10-22.4337 5702.1610 0.000 0.600 0.009164 10582. 1387.8932 -0.000116 0.000 6.087E+10-22.2363 5823.4836 0.000 0.800 0.008887 13852. 1334.7937 -0.000115 0.000 6.087E+10-22.0133 5944.8062 0.000 1.000 0.008611 16994. 1282.2591 -0.000115 0.000 6.087E+10-21.7656 6066.1287 0.000 1.200 0.008337 20012. 1230.3476 -0.000114 0.000 6.087E+10-21.4941 6187.4513 0.000 1.400 0.008065 22906. 1179.1147 -0.000113 0.000 6.087E+10-21.1999 6308.7739 0.000 1.600 0.007795 25677. 1128.6140 -0.000112 0.000 6.087E+10-20.8840 6430.0965 0.000 1.800 0.007527 28328. 1078.8963 -0.000111 0.000 6.087E+10-20.5474 6551.4190 0.000 2.000 0.007262 30861. 1030.0099 -0.000110 0.000 6.087E+10-20.1913 6672.7416 0.000 2.200 0.007000 33278. 982.0005 -0.000109 0.000 6.087E+10-19.8165 6794.0642 0.000 2.400 0.006741 35580. 934.9113 -0.000107 0.000 6.087E+10-19.4244 6915.3868 0.000 2.600 0.006486 37770. 888.7828 -0.000106 0.000 6.087E+10-19.0160 7036.7093 0.000 2.800 0.006234 39851. 843.6527 -0.000104 0.000 6.087E+10-18.5924 7158.0319 0.000 3.000 0.005986 41825. 799.5562 -0.000103 0.000 6.087E+10-18.1548 7279.3545 0.000 3.200 0.005741 43694. 756.5254 -0.000101 0.000 6.087E+10-17.7042 7400.6771 0.000 3.400 0.005501 45461. 714.5900 -9.914E-05 0.000 6.087E+10-17.2420 7521.9996 0.000 3.600 0.005266 47129. 673.7766 -9.732E-05 0.000 6.087E+10-16.7691 7643.3222 0.000 3.800 0.005034 48700. 634.1094 -9.543E-05 0.000 6.087E+10-16.2869 7764.6448 0.000

Page 13

existing phase1 81.lp6o 4.000 0.004807 50177. 588.2926 -9.348E-05 0.000 6.087E+10-21.8938 10930. 0.000 4.200 0.004585 51528. 528.2859 -9.147E-05 0.000 6.087E+10-28.1118 14713. 0.000 4.400 0.004368 52717. 461.9417 -8.942E-05 0.000 6.087E+10-27.1751 14930. 0.000 4.600 0.004156 53750. 397.8548 -8.732E-05 0.000 6.087E+10-26.2307 15147. 0.000 4.800 0.003949 54631. 336.0414 -8.518E-05 0.000 6.087E+10-25.2805 15363. 0.000 5.000 0.003747 55367. 276.5129 -8.301E-05 0.000 6.087E+10-24.3266 15580. 0.000 5.200 0.003551 55962. 219.2762 -8.082E-05 0.000 6.087E+10-23.3707 15796. 0.000 5.400 0.003359 56423. 164.3338 -7.860E-05 0.000 6.087E+10-22.4146 16013. 0.000 5.600 0.003173 56755. 111.6841 -7.637E-05 0.000 6.087E+10-21.4601 16230. 0.000 5.800 0.002993 56963. 61.3213 -7.413E-05 0.000 6.087E+10-20.5089 16446. 0.000 6.000 0.002818 57053. 13.2357 -7.188E-05 0.000 6.087E+10-19.5625 16663. 0.000 6.200 0.002648 57030. -32.5861 -6.963E-05 0.000 6.087E+10-18.6224 16879. 0.000 6.400 0.002483 56900. -76.1611 -6.739E-05 0.000 6.087E+10-17.6901 17096. 0.000 6.600 0.002324 56668. -117.5096 -6.515E-05 0.000 6.087E+10-16.7670 17313. 0.000 6.800 0.002171 56339. -156.6551 -6.292E-05 0.000 6.087E+10-15.8543 17529. 0.000 7.000 0.002022 55919. -193.6242 -6.071E-05 0.000 6.087E+10-14.9533 17746. 0.000 7.200 0.001879 55412. -228.4464 -5.851E-05 0.000 6.087E+10-14.0651 17962. 0.000 7.400 0.001741 54825. -261.1536 -5.634E-05 0.000 6.087E+10-13.1909 18179. 0.000 7.600 0.001609 54162. -291.7804 -5.419E-05 0.000 6.087E+10-12.3315 18396. 0.000 7.800 0.001481 53427. -320.3638 -5.207E-05 0.000 6.087E+10-11.4879 18612. 0.000 8.000 0.001359 52626. -346.9425 -4.998E-05 0.000 6.087E+10-10.6610 18829. 0.000 8.200 0.001241 51764. -371.5576 -4.792E-05 0.000 6.087E+10-9.8515 19045. 0.000 8.400 0.001129 50845. -394.2515 -4.590E-05 0.000 6.087E+10-9.0601 19262. 0.000 8.600 0.001021 49874. -415.0687 -4.391E-05 0.000 6.087E+10-8.2875 19479. 0.000 8.800 0.000918 48855. -434.0546 -4.197E-05 0.000 6.087E+10-7.5341 19695. 0.000 9.000 0.000820 47792. -450.7546 -4.006E-05 0.000 6.087E+10-6.3826 18688. 0.000 9.200 0.000726 46693. -464.6515 -3.820E-05 0.000 6.087E+10-5.1982 17189. 0.000 9.400 0.000636 45564. -476.4153 -3.638E-05 0.000 6.087E+10-4.6050 17369. 0.000 9.600 0.000551 44408. -486.7773 -3.461E-05 0.000 6.087E+10-4.0300 17549. 0.000 9.800 0.000470 43229. -495.7812 -3.288E-05 0.000 6.087E+10-3.4733 17728. 0.000 10.000 0.000393 42030. -503.4710 -3.120E-05 0.000 6.087E+10-2.9349 17908. 0.000 10.200 0.000320 40814. -509.8910 -2.957E-05 0.000 6.087E+10

Page 14

existing phase1 81.lp6o-2.4151 18088. 0.000 10.400 0.000251 39584. -515.0855 -2.798E-05 0.000 6.087E+10-1.9137 18267. 0.000 10.600 0.000186 38343. -519.0988 -2.644E-05 0.000 6.087E+10-1.4307 18447. 0.000 10.800 0.000124 37094. -521.9751 -2.496E-05 0.000 6.087E+10-0.9662 18627. 0.000 11.000 6.635E-05 35839. -523.7584 -2.352E-05 0.000 6.087E+10-0.5199 18807. 0.000 11.200 1.160E-05 34581. -524.4924 -2.213E-05 0.000 6.087E+10-0.0918 18986. 0.000 11.400 -3.988E-05 33322. -524.2204 -2.079E-05 0.000 6.087E+100.3185 19166. 0.000 11.600 -8.820E-05 32065. -522.9850 -1.950E-05 0.000 6.087E+100.7110 19346. 0.000 11.800 -0.000133 30813. -520.8286 -1.826E-05 0.000 6.087E+101.0860 19525. 0.000 12.000 -0.000176 29566. -517.7926 -1.707E-05 0.000 6.087E+101.4440 19705. 0.000 12.200 -0.000215 28328. -513.9178 -1.593E-05 0.000 6.087E+101.7850 19885. 0.000 12.400 -0.000252 27100. -509.2442 -1.484E-05 0.000 6.087E+102.1096 20064. 0.000 12.600 -0.000287 25884. -503.8109 -1.379E-05 0.000 6.087E+102.4181 20244. 0.000 12.800 -0.000319 24683. -497.6561 -1.280E-05 0.000 6.087E+102.7109 20424. 0.000 13.000 -0.000348 23496. -490.8170 -1.185E-05 0.000 6.087E+102.9884 20604. 0.000 13.200 -0.000375 22327. -483.3297 -1.094E-05 0.000 6.087E+103.2511 20783. 0.000 13.400 -0.000401 21177. -475.2291 -1.009E-05 0.000 6.087E+103.4994 20963. 0.000 13.600 -0.000424 20047. -466.5493 -9.274E-06 0.000 6.087E+103.7338 21143. 0.000 13.800 -0.000445 18938. -457.3229 -8.506E-06 0.000 6.087E+103.9549 21322. 0.000 14.000 -0.000465 17852. -447.5814 -7.780E-06 0.000 6.087E+104.1631 21502. 0.000 14.200 -0.000482 16790. -437.3550 -7.097E-06 0.000 6.087E+104.3589 21682. 0.000 14.400 -0.000499 15753. -426.6727 -6.456E-06 0.000 6.087E+104.5430 21862. 0.000 14.600 -0.000513 14742. -415.5622 -5.855E-06 0.000 6.087E+104.7158 22041. 0.000 14.800 -0.000527 13759. -404.0499 -5.293E-06 0.000 6.087E+104.8778 22221. 0.000 15.000 -0.000539 12803. -392.1608 -4.769E-06 0.000 6.087E+105.0298 22401. 0.000 15.200 -0.000550 11876. -379.9185 -4.283E-06 0.000 6.087E+105.1721 22580. 0.000 15.400 -0.000559 10980. -367.3454 -3.832E-06 0.000 6.087E+105.3054 22760. 0.000 15.600 -0.000568 10113. -354.4626 -3.416E-06 0.000 6.087E+105.4303 22940. 0.000 15.800 -0.000576 9278.3081 -341.2897 -3.034E-06 0.000 6.087E+105.5472 23120. 0.000 16.000 -0.000583 8475.2570 -327.8451 -2.684E-06 0.000 6.087E+105.6567 23299. 0.000 16.200 -0.000589 7704.7806 -314.1457 -2.365E-06 0.000 6.087E+105.7594 23479. 0.000 16.400 -0.000594 6967.4712 -300.2073 -2.076E-06 0.000 6.087E+105.8559 23659. 0.000

Page 15

existing phase1 81.lp6o 16.600 -0.000599 6263.8851 -286.0444 -1.815E-06 0.000 6.087E+105.9466 23838. 0.000 16.800 -0.000603 5594.5451 -271.6702 -1.581E-06 0.000 6.087E+106.0320 24018. 0.000 17.000 -0.000606 4959.9442 -257.0965 -1.373E-06 0.000 6.087E+106.1127 24198. 0.000 17.200 -0.000609 4360.5479 -242.3342 -1.189E-06 0.000 6.087E+106.1892 24377. 0.000 17.400 -0.000612 3796.7973 -227.3928 -1.028E-06 0.000 6.087E+106.2619 24557. 0.000 17.600 -0.000614 3269.1118 -212.2809 -8.891E-07 0.000 6.087E+106.3313 24737. 0.000 17.800 -0.000616 2777.8918 -197.0058 -7.699E-07 0.000 6.087E+106.3979 24917. 0.000 18.000 -0.000618 2323.5208 -181.5740 -6.693E-07 0.000 6.087E+106.4620 25096. 0.000 18.200 -0.000619 1906.3687 -165.9908 -5.859E-07 0.000 6.087E+106.5240 25276. 0.000 18.400 -0.000621 1526.7929 -150.2608 -5.182E-07 0.000 6.087E+106.5843 25456. 0.000 18.600 -0.000622 1185.1416 -134.3876 -4.648E-07 0.000 6.087E+106.6433 25635. 0.000 18.800 -0.000623 881.7548 -118.3740 -4.240E-07 0.000 6.087E+106.7013 25815. 0.000 19.000 -0.000624 616.9666 -101.2127 -3.945E-07 0.000 6.087E+107.5998 29231. 0.000 19.200 -0.000625 395.9528 -82.0060 -3.745E-07 0.000 6.087E+108.4058 32283. 0.000 19.400 -0.000626 223.3558 -61.7501 -3.623E-07 0.000 6.087E+108.4741 32500. 0.000 19.600 -0.000627 99.5695 -41.3305 -3.559E-07 0.000 6.087E+108.5423 32716. 0.000 19.800 -0.000627 24.9865 -20.7472 -3.535E-07 0.000 6.087E+108.6105 32933. 0.000 20.000 -0.000628 0.000 0.000 -3.530E-07 0.000 6.087E+108.6788 16575. 0.000

* This analysis makes computations of pile response using nonlinear moment-curvaturerelationships. The above values of total stress are computed for combined axial and bending stress in elastic sections and do not equal actual stresses in concrete and steel in the range of nonlinear bending.

Output Summary for Load Case No. 1:

Pile-head deflection = 0.0100000 inchesComputed slope at pile head = -0.0001163 radiansMaximum bending moment = 57053. inch-lbsMaximum shear force = 1549.9659742 lbsDepth of maximum bending moment = 72.0000000 inches below pile headDepth of maximum shear force = 0.000000 inches below pile headNumber of iterations = 6Number of zero deflection points = 1

-------------------------------------------------------------------------------- Pile-head Deflection vs. Pile Length for Load Case 1--------------------------------------------------------------------------------

Boundary Condition Type 4, Deflection and MomentPage 16

existing phase1 81.lp6o

Deflection = 0.01000 inMoment = 0. in-lbsAxial Load = 10000. lbs

Pile Pile Head Maximum Maximum Length Deflection Moment Shear feet inches ln-lbs lbs ------------ ------------ ------------ ------------ 20.0000 0.0100000 57053. 1549.9659742 19.0000 0.0100000 56065. 1534.1042890 18.0000 0.0100000 54965. 1521.6525963 17.0000 0.0100000 53283. 1501.5849579 16.0000 0.0100000 50696. 1464.5734325 15.0000 0.0100000 47367. 1415.8951192 14.0000 0.0100000 43077. 1347.2493727 13.0000 0.0100000 38179. 1265.1021422 12.0000 0.0100000 32555. 1162.3050452 11.0000 0.0100000 26945. 1053.4541515 10.0000 0.0100000 21593. 941.2362924 9.0000 0.0100000 16880. 832.6272714 8.0000 0.0100000 12396. 713.3756215 7.0000 0.0100000 8890.0157132 603.0010889 6.0000 0.0100000 6201.5001490 501.8547131 5.0000 0.0100000 4150.7197870 408.0114780 4.0000 0.0100000 2270.6062338 297.8771759 3.0000 0.0100000 1219.8233359 215.3823002 2.0000 0.0100000 508.0778715 134.7056638 1.0000 0.0100000 104.0177125 50.0030633

-------------------------------------------------------------------------------- Computed Values of Pile Loading and Deflection for Lateral Loading for Load Case Number 2--------------------------------------------------------------------------------

Pile-head conditions are Displacement and Moment (Loading Type 4)Displacement of pile head = 0.100000 inchesMoment at pile head = 0.000 in-lbsAxial load at pile head = 10000.000 lbs

Depth Deflect. Bending Shear Slope Total Bending Soil Res. Soil Spr. Distrib. X y Moment Force S Stress Stiffness p Es*h Lat. Load feet inches in-lbs lbs radians psi* lb-in^2 lb/in lb/inch lb/inch ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- 0.00 0.1000 0.000 15424. -0.001167 0.000 6.087E+10-227.4798 2729.7579 0.000 0.200 0.0972 36390. 14879. -0.001166 0.000 6.087E+10-226.0245 5580.8384 0.000 0.400 0.0944 71477. 14339. -0.001164 0.000 6.087E+10-224.2942 5702.1610 0.000 0.600 0.0916 105273. 13803. -0.001160 0.000 6.079E+10-222.2977 5823.4836 0.000 0.800 0.0888 137788. 13272. -0.001155 0.000 6.073E+10-220.0438 5944.8062 0.000 1.000 0.0861 169035. 12747. -0.001149 0.000 6.066E+10-217.5419 6066.1287 0.000 1.200 0.0833 199029. 12228. -0.001142 0.000 6.059E+10

Page 17

existing phase1 81.lp6o-214.8017 6187.4513 0.000 1.400 0.0806 227786. 11716. -0.001134 0.000 6.054E+10-211.8332 6308.7739 0.000 1.600 0.0779 255323. 11212. -0.001124 0.000 6.046E+10-208.6466 6430.0965 0.000 1.800 0.0752 281657. 10715. -0.001113 0.000 6.040E+10-205.2523 6551.4190 0.000 2.000 0.0725 306809. 10227. -0.001102 0.000 6.035E+10-201.6613 6672.7416 0.000 2.200 0.0699 330799. 9747.4129 -0.001089 0.000 6.028E+10-197.8843 6794.0642 0.000 2.400 0.0673 353649. 9277.2326 -0.001075 0.000 6.023E+10-193.9326 6915.3868 0.000 2.600 0.0647 375381. 8816.7326 -0.001061 0.000 6.018E+10-189.8174 7036.7093 0.000 2.800 0.0622 396020. 8366.2916 -0.001045 0.000 6.012E+10-185.5501 7158.0319 0.000 3.000 0.0597 415590. 7926.2606 -0.001029 0.000 6.007E+10-181.1423 7279.3545 0.000 3.200 0.0573 434115. 7496.9631 -0.001012 0.000 6.003E+10-176.6056 7400.6771 0.000 3.400 0.0549 451624. 7078.6942 -0.000995 0.000 5.999E+10-171.9518 7521.9996 0.000 3.600 0.0525 468141. 6671.7210 -0.000976 0.000 5.995E+10-167.1925 7643.3222 0.000 3.800 0.0502 483695. 6276.2825 -0.000957 0.000 5.991E+10-162.3396 7764.6448 0.000 4.000 0.0479 498313. 5819.6792 -0.000937 0.000 5.987E+10-218.1631 10930. 0.000 4.200 0.0457 511674. 5221.8385 -0.000917 0.000 5.984E+10-280.0375 14713. 0.000 4.400 0.0435 523422. 4561.0499 -0.000896 0.000 5.981E+10-270.6197 14930. 0.000 4.600 0.0414 533610. 3922.9535 -0.000875 0.000 5.978E+10-261.1273 15147. 0.000 4.800 0.0393 542294. 3307.7046 -0.000854 0.000 5.976E+10-251.5801 15363. 0.000 5.000 0.0373 549528. 2715.4111 -0.000832 0.000 5.974E+10-241.9978 15580. 0.000 5.200 0.0353 555368. 2146.1348 -0.000809 0.000 5.973E+10-232.3991 15796. 0.000 5.400 0.0334 559868. 1599.8931 -0.000787 0.000 5.971E+10-222.8023 16013. 0.000 5.600 0.0315 563085. 1076.6604 -0.000764 0.000 5.971E+10-213.2249 16230. 0.000 5.800 0.0297 565073. 576.3701 -0.000742 0.000 5.970E+10-203.6837 16446. 0.000 6.000 0.0280 565887. 98.9161 -0.000719 0.000 5.970E+10-194.1947 16663. 0.000 6.200 0.0263 565582. -355.8453 -0.000696 0.000 5.970E+10-184.7732 16879. 0.000 6.400 0.0246 564213. -788.0939 -0.000674 0.000 5.970E+10-175.4339 17096. 0.000 6.600 0.0230 561832. -1198.0432 -0.000651 0.000 5.971E+10-166.1905 17313. 0.000 6.800 0.0215 558493. -1585.9391 -0.000628 0.000 5.972E+10-157.0561 17529. 0.000 7.000 0.0200 554250. -1952.0579 -0.000606 0.000 5.973E+10-148.0429 17746. 0.000 7.200 0.0186 549153. -2296.7041 -0.000584 0.000 5.974E+10-139.1623 17962. 0.000 7.400 0.0172 543253. -2620.2089 -0.000562 0.000 5.976E+10-130.4250 18179. 0.000

Page 18

existing phase1 81.lp6o 7.600 0.0159 536603. -2922.9280 -0.000540 0.000 5.978E+10-121.8409 18396. 0.000 7.800 0.0146 529249. -3205.2399 -0.000519 0.000 5.980E+10-113.4190 18612. 0.000 8.000 0.0134 521242. -3467.5440 -0.000498 0.000 5.982E+10-105.1677 18829. 0.000 8.200 0.0122 512629. -3710.2587 -0.000477 0.000 5.984E+10-97.0945 19045. 0.000 8.400 0.0111 503456. -3933.8196 -0.000457 0.000 5.986E+10-89.2062 19262. 0.000 8.600 0.0100 493769. -4138.6778 -0.000437 0.000 5.988E+10-81.5089 19479. 0.000 8.800 0.009018 483611. -4325.2979 -0.000417 0.000 5.991E+10-74.0078 19695. 0.000 9.000 0.008040 473027. -4489.2373 -0.000398 0.000 5.993E+10-62.6084 18688. 0.000 9.200 0.007108 462082. -4625.4560 -0.000379 0.000 5.996E+10-50.9072 17189. 0.000 9.400 0.006220 450843. -4740.5589 -0.000361 0.000 5.999E+10-45.0119 17369. 0.000 9.600 0.005375 439345. -4841.7332 -0.000343 0.000 6.002E+10-39.3000 17549. 0.000 9.800 0.004572 427619. -4929.4208 -0.000326 0.000 6.005E+10-33.7730 17728. 0.000 10.000 0.003810 415699. -5004.0668 -0.000309 0.000 6.007E+10-28.4320 17908. 0.000 10.200 0.003089 403615. -5066.1179 -0.000293 0.000 6.010E+10-23.2772 18088. 0.000 10.400 0.002405 391396. -5116.0211 -0.000277 0.000 6.014E+10-18.3088 18267. 0.000 10.600 0.001760 379071. -5154.2231 -0.000261 0.000 6.017E+10-13.5262 18447. 0.000 10.800 0.001150 366668. -5181.1687 -0.000247 0.000 6.020E+10-8.9285 18627. 0.000 11.000 0.000576 354213. -5197.3004 -0.000232 0.000 6.023E+10-4.5145 18807. 0.000 11.200 3.571E-05 341732. -5203.0569 -0.000218 0.000 6.026E+10-0.2825 18986. 0.000 11.400 -0.000472 329249. -5198.8725 -0.000205 0.000 6.029E+103.7695 19166. 0.000 11.600 -0.000948 316787. -5185.1762 -0.000192 0.000 6.032E+107.6441 19346. 0.000 11.800 -0.001394 304369. -5162.3908 -0.000180 0.000 6.036E+1011.3438 19525. 0.000 12.000 -0.001811 292017. -5130.9320 -0.000168 0.000 6.038E+1014.8718 19705. 0.000 12.200 -0.002200 279749. -5091.2079 -0.000157 0.000 6.041E+1018.2315 19885. 0.000 12.400 -0.002563 267586. -5043.6183 -0.000146 0.000 6.043E+1021.4265 20064. 0.000 12.600 -0.002900 255547. -4988.5537 -0.000135 0.000 6.046E+1024.4606 20244. 0.000 12.800 -0.003212 243648. -4926.3954 -0.000125 0.000 6.049E+1027.3380 20424. 0.000 13.000 -0.003502 231906. -4857.5142 -0.000116 0.000 6.053E+1030.0630 20604. 0.000 13.200 -0.003769 220337. -4782.2702 -0.000107 0.000 6.055E+1032.6403 20783. 0.000 13.400 -0.004016 208956. -4701.0123 -9.852E-05 0.000 6.057E+1035.0746 20963. 0.000 13.600 -0.004242 197777. -4614.0781 -9.046E-05 0.000 6.060E+1037.3706 21143. 0.000 13.800 -0.004450 186813. -4521.7929 -8.285E-05 0.000 6.062E+10

Page 19

existing phase1 81.lp6o39.5336 21322. 0.000 14.000 -0.004640 176076. -4424.4702 -7.566E-05 0.000 6.064E+1041.5687 21502. 0.000 14.200 -0.004813 165579. -4322.4104 -6.891E-05 0.000 6.067E+1043.4811 21682. 0.000 14.400 -0.004971 155332. -4215.9015 -6.256E-05 0.000 6.071E+1045.2763 21862. 0.000 14.600 -0.005113 145346. -4105.2183 -5.662E-05 0.000 6.072E+1046.9597 22041. 0.000 14.800 -0.005242 135630. -3990.6225 -5.107E-05 0.000 6.074E+1048.5368 22221. 0.000 15.000 -0.005358 126193. -3872.3624 -4.589E-05 0.000 6.075E+1050.0132 22401. 0.000 15.200 -0.005463 117045. -3750.6732 -4.109E-05 0.000 6.076E+1051.3945 22580. 0.000 15.400 -0.005556 108192. -3625.7765 -3.664E-05 0.000 6.078E+1052.6861 22760. 0.000 15.600 -0.005638 99643. -3497.8810 -3.254E-05 0.000 6.080E+1053.8936 22940. 0.000 15.800 -0.005712 91404. -3367.1816 -2.877E-05 0.000 6.082E+1055.0226 23120. 0.000 16.000 -0.005777 83482. -3233.8602 -2.532E-05 0.000 6.084E+1056.0785 23299. 0.000 16.200 -0.005833 75882. -3098.0858 -2.218E-05 0.000 6.087E+1057.0668 23479. 0.000 16.400 -0.005883 68612. -2960.0142 -1.933E-05 0.000 6.087E+1057.9929 23659. 0.000 16.600 -0.005926 61675. -2819.7885 -1.676E-05 0.000 6.087E+1058.8619 23838. 0.000 16.800 -0.005963 55078. -2677.5396 -1.446E-05 0.000 6.087E+1059.6789 24018. 0.000 17.000 -0.005995 48824. -2533.3861 -1.241E-05 0.000 6.087E+1060.4490 24198. 0.000 17.200 -0.006023 42918. -2387.4351 -1.060E-05 0.000 6.087E+1061.1769 24377. 0.000 17.400 -0.006046 37365. -2239.7818 -9.017E-06 0.000 6.087E+1061.8674 24557. 0.000 17.600 -0.006066 32168. -2090.5109 -7.646E-06 0.000 6.087E+1062.5250 24737. 0.000 17.800 -0.006083 27331. -1939.6961 -6.473E-06 0.000 6.087E+1063.1540 24917. 0.000 18.000 -0.006097 22857. -1787.4013 -5.484E-06 0.000 6.087E+1063.7584 25096. 0.000 18.200 -0.006109 18751. -1633.6807 -4.664E-06 0.000 6.087E+1064.3422 25276. 0.000 18.400 -0.006120 15016. -1478.5794 -3.998E-06 0.000 6.087E+1064.9089 25456. 0.000 18.600 -0.006129 11654. -1322.1342 -3.472E-06 0.000 6.087E+1065.4621 25635. 0.000 18.800 -0.006136 8669.7967 -1164.3742 -3.072E-06 0.000 6.087E+1066.0047 25815. 0.000 19.000 -0.006143 6065.4618 -995.3820 -2.781E-06 0.000 6.087E+1074.8222 29231. 0.000 19.200 -0.006150 3892.0969 -806.3294 -2.585E-06 0.000 6.087E+1082.7216 32283. 0.000 19.400 -0.006156 2195.2046 -607.0338 -2.465E-06 0.000 6.087E+1083.3581 32500. 0.000 19.600 -0.006162 978.4531 -406.2126 -2.402E-06 0.000 6.087E+1083.9929 32716. 0.000 19.800 -0.006167 245.4996 -203.8682 -2.378E-06 0.000 6.087E+1084.6274 32933. 0.000 20.000 -0.006173 0.000 0.000 -2.373E-06 0.000 6.087E+1085.2627 16575. 0.000

Page 20

existing phase1 81.lp6o

* This analysis makes computations of pile response using nonlinear moment-curvaturerelationships. The above values of total stress are computed for combined axial and bending stress in elastic sections and do not equal actual stresses in concrete and steel in the range of nonlinear bending.

Output Summary for Load Case No. 2:

Pile-head deflection = 0.1000000 inchesComputed slope at pile head = -0.0011666 radiansMaximum bending moment = 565887. inch-lbsMaximum shear force = 15424. lbsDepth of maximum bending moment = 72.0000000 inches below pile headDepth of maximum shear force = 0.000000 inches below pile headNumber of iterations = 6Number of zero deflection points = 1

-------------------------------------------------------------------------------- Pile-head Deflection vs. Pile Length for Load Case 2--------------------------------------------------------------------------------

Boundary Condition Type 4, Deflection and Moment

Deflection = 0.10000 inMoment = 0. in-lbsAxial Load = 10000. lbs

Pile Pile Head Maximum Maximum Length Deflection Moment Shear feet inches ln-lbs lbs ------------ ------------ ------------ ------------ 20.0000 0.1000000 565887. 15424. 19.0000 0.1000000 556372. 15271. 18.0000 0.1000000 545854. 15152. 17.0000 0.1000000 529622. 14960. 16.0000 0.1000000 504432. 14600. 15.0000 0.1000000 471833. 14124. 14.0000 0.1000000 429562. 13449. 13.0000 0.1000000 381082. 12636. 12.0000 0.1000000 325192. 11615. 11.0000 0.1000000 269287. 10531. 10.0000 0.1000000 215871. 9410.7453536 9.0000 0.1000000 168777. 8325.6904097 8.0000 0.1000000 123957. 7133.5994644 7.0000 0.1000000 88900. 6029.9943499 6.0000 0.1000000 62015. 5018.5471318 5.0000 0.1000000 41507. 4080.1147856 4.0000 0.1000000 22706. 2978.7717541 3.0000 0.1000000 12198. 2153.8230023 2.0000 0.1000000 5080.7787044 1347.0566917 1.0000 0.1000000 1040.1771107 500.0310604

-------------------------------------------------------------------------------- Computed Values of Pile Loading and Deflection for Lateral Loading for Load Case Number 3--------------------------------------------------------------------------------

Page 21

existing phase1 81.lp6o

Pile-head conditions are Displacement and Moment (Loading Type 4)Displacement of pile head = 0.200000 inchesMoment at pile head = 0.000 in-lbsAxial load at pile head = 10000.000 lbs

Depth Deflect. Bending Shear Slope Total Bending Soil Res. Soil Spr. Distrib. X y Moment Force S Stress Stiffness p Es*h Lat. Load feet inches in-lbs lbs radians psi* lb-in^2 lb/in lb/inch lb/inch ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- 0.00 0.2000 0.000 21438. -0.002887 0.000 6.087E+10-454.9597 2729.7579 0.000 0.200 0.1931 50210. 20353. -0.002886 0.000 6.087E+10-448.9602 5580.8384 0.000 0.400 0.1861 97833. 19284. -0.002883 0.000 6.080E+10-442.2715 5702.1610 0.000 0.600 0.1792 142909. 18231. -0.002878 0.000 6.073E+10-434.9054 5823.4836 0.000 0.800 0.1723 185480. 17197. -0.002871 0.000 6.062E+10-426.8739 5944.8062 0.000 1.000 0.1655 225592. 16183. -0.002863 0.000 6.055E+10-418.1893 6066.1287 0.000 1.200 0.1586 263295. 15190. -0.002854 0.000 6.044E+10-408.8642 6187.4513 0.000 1.400 0.1518 298643. 14221. -0.002842 0.000 6.037E+10-398.9113 6308.7739 0.000 1.600 0.1449 331692. 13276. -0.002830 0.000 6.028E+10-388.3436 6430.0965 0.000 1.800 0.1382 362504. 12358. -0.002816 0.000 6.021E+10-377.1742 6551.4190 0.000 2.000 0.1314 391144. 11467. -0.002801 0.000 6.014E+10-365.4162 6672.7416 0.000 2.200 0.1247 417678. 10604. -0.002785 0.000 6.007E+10-353.0826 6794.0642 0.000 2.400 0.1181 442179. 9772.4246 -0.002768 0.000 6.001E+10-340.1867 6915.3868 0.000 2.600 0.1114 464719. 8972.1107 -0.002750 0.000 5.996E+10-326.7415 7036.7093 0.000 2.800 0.1049 485377. 8204.7088 -0.002731 0.000 5.990E+10-312.7601 7158.0319 0.000 3.000 0.0983 504233. 7471.4904 -0.002711 0.000 5.986E+10-298.2552 7279.3545 0.000 3.200 0.0919 521370. 6773.6963 -0.002690 0.000 5.982E+10-283.2399 7400.6771 0.000 3.400 0.0854 536875. 6112.5366 -0.002669 0.000 5.977E+10-267.7265 7521.9996 0.000 3.600 0.0790 550838. 5489.1915 -0.002647 0.000 5.974E+10-251.7277 7643.3222 0.000 3.800 0.0727 563351. 4904.8112 -0.002625 0.000 5.971E+10-235.2558 7764.6448 0.000 4.000 0.0664 574507. 4259.3900 -0.002602 0.000 5.968E+10-302.5952 10930. 0.000 4.200 0.0602 583921. 3453.1985 -0.002570 0.000 3.524E+10-369.2310 14713. 0.000 4.400 0.0541 591206. 2606.2161 -0.002506 0.000 1.608E+10-336.5877 14930. 0.000 4.600 0.0482 596551. 1837.2994 -0.002383 0.000 9.055E+09-304.1763 15147. 0.000 4.800 0.0427 600139. 1144.5351 -0.002187 0.000 6.154E+09

Page 22

existing phase1 81.lp6o-273.1273 15363. 0.000 5.000 0.0377 602149. 523.1102 -0.001932 0.000 5.218E+09-244.7268 15580. 0.000 5.200 0.0334 602743. -34.3272 -0.001654 0.000 5.216E+09-219.8044 15796. 0.000 5.400 0.0298 602064. -536.3486 -0.001377 0.000 5.218E+09-198.5467 16013. 0.000 5.600 0.0268 600235. -991.9562 -0.001119 0.000 6.002E+09-181.1263 16230. 0.000 5.800 0.0244 597356. -1409.8475 -0.000911 0.000 8.159E+09-167.1165 16446. 0.000 6.000 0.0224 593511. -1797.1097 -0.000765 0.000 1.234E+10-155.6019 16663. 0.000 6.200 0.0207 588767. -2158.6478 -0.000673 0.000 2.061E+10-145.6798 16879. 0.000 6.400 0.0192 583182. -2497.4114 -0.000621 0.000 3.787E+10-136.6232 17096. 0.000 6.600 0.0177 576809. -2814.8745 -0.000591 0.000 5.967E+10-127.9294 17313. 0.000 6.800 0.0163 569699. -3111.6476 -0.000567 0.000 5.969E+10-119.3815 17529. 0.000 7.000 0.0150 561901. -3388.0924 -0.000545 0.000 5.971E+10-110.9892 17746. 0.000 7.200 0.0137 553462. -3644.5937 -0.000522 0.000 5.973E+10-102.7618 17962. 0.000 7.400 0.0125 544432. -3881.5569 -0.000500 0.000 5.975E+10-94.7075 18179. 0.000 7.600 0.0113 534855. -4099.4068 -0.000479 0.000 5.978E+10-86.8341 18396. 0.000 7.800 0.0102 524777. -4298.5857 -0.000457 0.000 5.981E+10-79.1483 18612. 0.000 8.000 0.009134 514244. -4479.5513 -0.000437 0.000 5.983E+10-71.6564 18829. 0.000 8.200 0.008111 503296. -4642.7754 -0.000416 0.000 5.986E+10-64.3637 19045. 0.000 8.400 0.007136 491978. -4788.7419 -0.000396 0.000 5.988E+10-57.2751 19262. 0.000 8.600 0.006209 480330. -4917.9457 -0.000377 0.000 5.991E+10-50.3947 19479. 0.000 8.800 0.005328 468390. -5030.8904 -0.000358 0.000 5.995E+10-43.7259 19695. 0.000 9.000 0.004492 456198. -5125.3387 -0.000339 0.000 5.998E+10-34.9811 18688. 0.000 9.200 0.003700 443805. -5199.1183 -0.000321 0.000 6.001E+10-26.5019 17189. 0.000 9.400 0.002951 431258. -5256.5462 -0.000304 0.000 6.004E+10-21.3547 17369. 0.000 9.600 0.002243 418588. -5301.8492 -0.000287 0.000 6.007E+10-16.3978 17549. 0.000 9.800 0.001575 405823. -5335.4843 -0.000270 0.000 6.010E+10-11.6314 17728. 0.000 10.000 0.000946 392991. -5357.9083 -0.000254 0.000 6.013E+10-7.0552 17908. 0.000 10.200 0.000354 380117. -5369.5767 -0.000239 0.000 6.017E+10-2.6685 18088. 0.000 10.400 -0.000201 367228. -5370.9430 -0.000224 0.000 6.020E+101.5299 18267. 0.000 10.600 -0.000721 354347. -5362.4576 -0.000210 0.000 6.023E+105.5413 18447. 0.000 10.800 -0.001207 341498. -5344.5670 -0.000196 0.000 6.026E+109.3675 18627. 0.000 11.000 -0.001660 328703. -5317.7132 -0.000182 0.000 6.029E+1013.0107 18807. 0.000

Page 23

existing phase1 81.lp6o 11.200 -0.002082 315982. -5282.3322 -0.000170 0.000 6.032E+1016.4734 18986. 0.000 11.400 -0.002474 303356. -5238.8542 -0.000157 0.000 6.036E+1019.7583 19166. 0.000 11.600 -0.002837 290843. -5187.7020 -0.000145 0.000 6.038E+1022.8685 19346. 0.000 11.800 -0.003172 278462. -5129.2909 -0.000134 0.000 6.041E+1025.8074 19525. 0.000 12.000 -0.003481 266229. -5064.0278 -0.000123 0.000 6.044E+1028.5785 19705. 0.000 12.200 -0.003764 254160. -4992.3111 -0.000113 0.000 6.047E+1031.1855 19885. 0.000 12.400 -0.004023 242271. -4914.5294 -0.000103 0.000 6.050E+1033.6325 20064. 0.000 12.600 -0.004259 230576. -4831.0618 -9.373E-05 0.000 6.053E+1035.9238 20244. 0.000 12.800 -0.004473 219087. -4742.2768 -8.482E-05 0.000 6.056E+1038.0637 20424. 0.000 13.000 -0.004666 207817. -4648.5323 -7.636E-05 0.000 6.058E+1040.0567 20604. 0.000 13.200 -0.004839 196777. -4550.1753 -6.835E-05 0.000 6.060E+1041.9075 20783. 0.000 13.400 -0.004994 185979. -4447.5412 -6.077E-05 0.000 6.062E+1043.6209 20963. 0.000 13.600 -0.005131 175432. -4340.9539 -5.361E-05 0.000 6.065E+1045.2018 21143. 0.000 13.800 -0.005251 165145. -4230.7255 -4.688E-05 0.000 6.067E+1046.6552 21322. 0.000 14.000 -0.005356 155127. -4117.1559 -4.054E-05 0.000 6.071E+1047.9861 21502. 0.000 14.200 -0.005446 145385. -4000.5328 -3.461E-05 0.000 6.072E+1049.1998 21682. 0.000 14.400 -0.005522 135926. -3881.1315 -2.905E-05 0.000 6.074E+1050.3013 21862. 0.000 14.600 -0.005585 126757. -3759.2150 -2.386E-05 0.000 6.075E+1051.2958 22041. 0.000 14.800 -0.005637 117883. -3635.0338 -1.902E-05 0.000 6.076E+1052.1885 22221. 0.000 15.000 -0.005677 109310. -3508.8261 -1.454E-05 0.000 6.078E+1052.9846 22401. 0.000 15.200 -0.005706 101041. -3380.8175 -1.039E-05 0.000 6.079E+1053.6892 22580. 0.000 15.400 -0.005727 93082. -3251.2214 -6.555E-06 0.000 6.081E+1054.3075 22760. 0.000 15.600 -0.005738 85436. -3120.2390 -3.033E-06 0.000 6.084E+1054.8445 22940. 0.000 15.800 -0.005741 78105. -2988.0592 1.924E-07 0.000 6.086E+1055.3053 23120. 0.000 16.000 -0.005737 71093. -2854.8590 3.134E-06 0.000 6.087E+1055.6948 23299. 0.000 16.200 -0.005726 64402. -2720.8036 5.805E-06 0.000 6.087E+1056.0179 23479. 0.000 16.400 -0.005709 58033. -2586.0469 8.219E-06 0.000 6.087E+1056.2793 23659. 0.000 16.600 -0.005687 51988. -2450.7314 1.039E-05 0.000 6.087E+1056.4836 23838. 0.000 16.800 -0.005659 46269. -2314.9887 1.232E-05 0.000 6.087E+1056.6353 24018. 0.000 17.000 -0.005628 40876. -2178.9398 1.404E-05 0.000 6.087E+1056.7388 24198. 0.000 17.200 -0.005592 35809. -2042.6955 1.555E-05 0.000 6.087E+1056.7982 24377. 0.000 17.400 -0.005553 31070. -1906.3566 1.687E-05 0.000 6.087E+10

Page 24

existing phase1 81.lp6o56.8176 24557. 0.000 17.600 -0.005511 26658. -1770.0145 1.801E-05 0.000 6.087E+1056.8008 24737. 0.000 17.800 -0.005466 22573. -1633.7517 1.898E-05 0.000 6.087E+1056.7516 24917. 0.000 18.000 -0.005420 18815. -1497.6417 1.980E-05 0.000 6.087E+1056.6734 25096. 0.000 18.200 -0.005371 15383. -1361.7504 2.047E-05 0.000 6.087E+1056.5694 25276. 0.000 18.400 -0.005321 12278. -1226.1358 2.102E-05 0.000 6.087E+1056.4428 25456. 0.000 18.600 -0.005270 9496.9658 -1090.8490 2.145E-05 0.000 6.087E+1056.2962 25635. 0.000 18.800 -0.005219 7040.5422 -955.9346 2.177E-05 0.000 6.087E+1056.1324 25815. 0.000 19.000 -0.005166 4907.4346 -813.0735 2.201E-05 0.000 6.087E+1062.9185 29231. 0.000 19.200 -0.005113 3136.7330 -655.0409 2.217E-05 0.000 6.087E+1068.7753 32283. 0.000 19.400 -0.005060 1762.1744 -490.2932 2.226E-05 0.000 6.087E+1068.5144 32500. 0.000 19.600 -0.005006 782.2570 -326.1862 2.231E-05 0.000 6.087E+1068.2415 32716. 0.000 19.800 -0.004952 195.4097 -162.7469 2.233E-05 0.000 6.087E+1067.9579 32933. 0.000 20.000 -0.004899 0.000 0.000 2.234E-05 0.000 6.087E+1067.6645 16575. 0.000

* This analysis makes computations of pile response using nonlinear moment-curvaturerelationships. The above values of total stress are computed for combined axial and bending stress in elastic sections and do not equal actual stresses in concrete and steel in the range of nonlinear bending.

Output Summary for Load Case No. 3:

Pile-head deflection = 0.2000000 inchesComputed slope at pile head = -0.0028866 radiansMaximum bending moment = 602743. inch-lbsMaximum shear force = 21438. lbsDepth of maximum bending moment = 62.4000000 inches below pile headDepth of maximum shear force = 0.000000 inches below pile headNumber of iterations = 62Number of zero deflection points = 1

-------------------------------------------------------------------------------- Pile-head Deflection vs. Pile Length for Load Case 3--------------------------------------------------------------------------------

Boundary Condition Type 4, Deflection and Moment

Deflection = 0.20000 inMoment = 0. in-lbsAxial Load = 10000. lbs

Pile Pile Head Maximum Maximum Length Deflection Moment Shear feet inches ln-lbs lbs

Page 25

existing phase1 81.lp6o------------ ------------ ------------ ------------ 20.0000 0.2000000 602743. 21438. 19.0000 0.2000000 603037. 21442. 18.0000 0.2000000 602534. 21457. 17.0000 0.2000000 602564. 21500. 16.0000 0.2000000 602093. 21540. 15.0000 0.2000000 601604. 21610. 14.0000 0.2000000 600100. 21691. 13.0000 0.2000000 598893. 21839. 12.0000 0.2000000 599664. 22109. 11.0000 0.2000000 538053. 21049. 10.0000 0.2000000 431521. 18816. 9.0000 0.2000000 337469. 16649. 8.0000 0.2000000 247890. 14266. 7.0000 0.2000000 177794. 12060. 6.0000 0.2000000 124029. 10037. 5.0000 0.2000000 83014. 8160.2272787 4.0000 0.2000000 45412. 5957.5435082 3.0000 0.2000000 24396. 4307.6460046 2.0000 0.2000000 10162. 2694.1133834 1.0000 0.2000000 2080.3542214 1000.0621207

-------------------------------------------------------------------------------- Computed Values of Pile Loading and Deflection for Lateral Loading for Load Case Number 4--------------------------------------------------------------------------------

Pile-head conditions are Displacement and Moment (Loading Type 4)Displacement of pile head = 0.300000 inchesMoment at pile head = 0.000 in-lbsAxial load at pile head = 10000.000 lbs

Depth Deflect. Bending Shear Slope Total Bending Soil Res. Soil Spr. Distrib. X y Moment Force S Stress Stiffness p Es*h Lat. Load feet inches in-lbs lbs radians psi* lb-in^2 lb/in lb/inch lb/inch ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- 0.00 0.3000 0.000 26558. -0.004891 0.000 6.087E+10-682.4395 2729.7579 0.000 0.200 0.2883 61891. 24935. -0.004890 0.000 6.087E+10-670.3096 5580.8384 0.000 0.400 0.2765 119921. 23342. -0.004886 0.000 6.076E+10-657.0069 5702.1610 0.000 0.600 0.2648 174167. 21782. -0.004880 0.000 6.065E+10-642.5456 5823.4836 0.000 0.800 0.2531 224711. 20259. -0.004872 0.000 6.055E+10-626.9402 5944.8062 0.000 1.000 0.2414 271644. 18775. -0.004863 0.000 6.042E+10-610.2056 6066.1287 0.000 1.200 0.2298 315062. 17331. -0.004851 0.000 6.032E+10-592.3565 6187.4513 0.000 1.400 0.2181 355068. 15933. -0.004838 0.000 6.022E+10-573.4080 6308.7739 0.000 1.600 0.2065 391771. 14580. -0.004823 0.000 6.014E+10-553.3750 6430.0965 0.000 1.800 0.1950 425285. 13278. -0.004806 0.000 6.005E+10-532.2723 6551.4190 0.000 2.000 0.1835 455734. 12027. -0.004789 0.000 5.998E+10-510.1147 6672.7416 0.000

Page 26

existing phase1 81.lp6o 2.200 0.1720 483244. 10830. -0.004770 0.000 5.991E+10-486.9169 6794.0642 0.000 2.400 0.1606 507948. 9690.7672 -0.004750 0.000 5.985E+10-462.6932 6915.3868 0.000 2.600 0.1492 529987. 8610.5861 -0.004729 0.000 5.979E+10-437.4578 7036.7093 0.000 2.800 0.1379 549506. 7592.1673 -0.004708 0.000 5.974E+10-411.2245 7158.0319 0.000 3.000 0.1266 566656. 6637.8894 -0.004685 0.000 5.970E+10-384.0071 7279.3545 0.000 3.200 0.1154 581593. 5750.0986 -0.004649 0.000 2.882E+10-355.8186 7400.6771 0.000 3.400 0.1043 594479. 4930.8837 -0.004562 0.000 1.132E+10-326.8604 7521.9996 0.000 3.600 0.0935 605480. 4181.3594 -0.004360 0.000 5.216E+09-297.7432 7643.3222 0.000 3.800 0.0834 614759. 3500.4306 -0.004079 0.000 5.191E+09-269.6975 7764.6448 0.000 4.000 0.0739 622478. 2772.8542 -0.003792 0.000 5.180E+09-336.6162 10930. 0.000 4.200 0.0652 628251. 1889.5566 -0.003502 0.000 5.172E+09-399.4651 14713. 0.000 4.400 0.0571 631716. 983.9192 -0.003210 0.000 5.167E+09-355.2327 14930. 0.000 4.600 0.0498 633128. 180.8518 -0.002916 0.000 5.166E+09-313.9902 15147. 0.000 4.800 0.0431 632724. -527.0643 -0.002622 0.000 5.166E+09-275.9400 15363. 0.000 5.000 0.0372 630724. -1147.7161 -0.002329 0.000 5.169E+09-241.2698 15580. 0.000 5.200 0.0319 627327. -1689.4243 -0.002037 0.000 5.174E+09-210.1537 15796. 0.000 5.400 0.0274 622712. -2160.9114 -0.001747 0.000 5.180E+09-182.7523 16013. 0.000 5.600 0.0235 617038. -2571.2711 -0.001460 0.000 5.188E+09-159.2142 16230. 0.000 5.800 0.0204 610440. -2929.9397 -0.001176 0.000 5.198E+09-139.6763 16446. 0.000 6.000 0.0179 603031. -3246.6689 -0.000905 0.000 5.538E+09-124.2647 16663. 0.000 6.200 0.0160 594900. -3531.1659 -0.000702 0.000 9.931E+09-112.8161 16879. 0.000 6.400 0.0145 586115. -3790.7334 -0.000593 0.000 1.887E+10-103.4901 17096. 0.000 6.600 0.0132 576733. -4029.1396 -0.000537 0.000 3.789E+10-95.1817 17313. 0.000 6.800 0.0119 566801. -4248.0853 -0.000508 0.000 5.970E+10-87.2730 17529. 0.000 7.000 0.0108 556366. -4448.2656 -0.000485 0.000 5.972E+10-79.5439 17746. 0.000 7.200 0.009620 545473. -4630.1198 -0.000463 0.000 5.975E+10-72.0013 17962. 0.000 7.400 0.008535 534164. -4794.1035 -0.000441 0.000 5.978E+10-64.6517 18179. 0.000 7.600 0.007502 522482. -4940.6865 -0.000420 0.000 5.981E+10-57.5008 18396. 0.000 7.800 0.006519 510469. -5070.3517 -0.000399 0.000 5.984E+10-50.5535 18612. 0.000 8.000 0.005585 498164. -5183.5930 -0.000379 0.000 5.987E+10-43.8143 18829. 0.000 8.200 0.004699 485606. -5280.9142 -0.000359 0.000 5.990E+10-37.2868 19045. 0.000 8.400 0.003859 472832. -5362.8272 -0.000340 0.000 5.993E+10

Page 27

existing phase1 81.lp6o-30.9741 19262. 0.000 8.600 0.003065 459880. -5429.8506 -0.000322 0.000 5.997E+10-24.8787 19479. 0.000 8.800 0.002316 446785. -5482.5082 -0.000303 0.000 6.000E+10-19.0026 19695. 0.000 9.000 0.001609 433579. -5520.3433 -0.000286 0.000 6.003E+10-12.5267 18688. 0.000 9.200 0.000943 420301. -5543.4838 -0.000269 0.000 6.006E+10-6.7571 17189. 0.000 9.400 0.000318 406983. -5554.3580 -0.000252 0.000 6.010E+10-2.3048 17369. 0.000 9.600 -0.000267 393652. -5554.7768 -0.000236 0.000 6.013E+101.9558 17549. 0.000 9.800 -0.000816 380332. -5545.1990 -0.000221 0.000 6.017E+106.0257 17728. 0.000 10.000 -0.001328 367045. -5526.0811 -0.000206 0.000 6.020E+109.9059 17908. 0.000 10.200 -0.001804 353816. -5497.8762 -0.000192 0.000 6.023E+1013.5982 18088. 0.000 10.400 -0.002247 340665. -5461.0333 -0.000178 0.000 6.026E+1017.1042 18267. 0.000 10.600 -0.002657 327612. -5415.9966 -0.000164 0.000 6.029E+1020.4263 18447. 0.000 10.800 -0.003037 314676. -5363.2047 -0.000152 0.000 6.033E+1023.5670 18627. 0.000 11.000 -0.003385 301876. -5303.0897 -0.000139 0.000 6.036E+1026.5289 18807. 0.000 11.200 -0.003706 289228. -5236.0767 -0.000128 0.000 6.039E+1029.3152 18986. 0.000 11.400 -0.003998 276749. -5162.5834 -0.000116 0.000 6.041E+1031.9292 19166. 0.000 11.600 -0.004264 264453. -5083.0193 -0.000106 0.000 6.044E+1034.3743 19346. 0.000 11.800 -0.004505 252355. -4997.7852 -9.540E-05 0.000 6.047E+1036.6542 19525. 0.000 12.000 -0.004722 240468. -4907.2728 -8.563E-05 0.000 6.050E+1038.7728 19705. 0.000 12.200 -0.004916 228804. -4811.8643 -7.632E-05 0.000 6.054E+1040.7343 19885. 0.000 12.400 -0.005089 217375. -4711.9319 -6.748E-05 0.000 6.056E+1042.5428 20064. 0.000 12.600 -0.005240 206190. -4607.8374 -5.909E-05 0.000 6.058E+1044.2027 20244. 0.000 12.800 -0.005372 195260. -4499.9320 -5.114E-05 0.000 6.060E+1045.7185 20424. 0.000 13.000 -0.005486 184593. -4388.5562 -4.362E-05 0.000 6.062E+1047.0947 20604. 0.000 13.200 -0.005582 174197. -4274.0394 -3.652E-05 0.000 6.065E+1048.3360 20783. 0.000 13.400 -0.005661 164080. -4156.6996 -2.982E-05 0.000 6.068E+1049.4472 20963. 0.000 13.600 -0.005725 154246. -4036.8433 -2.353E-05 0.000 6.071E+1050.4331 21143. 0.000 13.800 -0.005774 144704. -3914.7655 -1.762E-05 0.000 6.072E+1051.2985 21322. 0.000 14.000 -0.005809 135456. -3790.7494 -1.209E-05 0.000 6.074E+1052.0482 21502. 0.000 14.200 -0.005832 126509. -3665.0668 -6.911E-06 0.000 6.075E+1052.6873 21682. 0.000 14.400 -0.005843 117864. -3537.9776 -2.085E-06 0.000 6.076E+1053.2204 21862. 0.000 14.600 -0.005842 109527. -3409.7300 2.406E-06 0.000 6.078E+1053.6526 22041. 0.000

Page 28

existing phase1 81.lp6o 14.800 -0.005831 101498. -3280.5608 6.572E-06 0.000 6.079E+1053.9885 22221. 0.000 15.000 -0.005810 93780. -3150.6950 1.043E-05 0.000 6.081E+1054.2330 22401. 0.000 15.200 -0.005781 86374. -3020.3463 1.398E-05 0.000 6.083E+1054.3909 22580. 0.000 15.400 -0.005743 79281. -2889.7171 1.725E-05 0.000 6.086E+1054.4668 22760. 0.000 15.600 -0.005698 72502. -2758.9985 2.024E-05 0.000 6.087E+1054.4653 22940. 0.000 15.800 -0.005646 66037. -2628.3709 2.297E-05 0.000 6.087E+1054.3910 23120. 0.000 16.000 -0.005588 59885. -2498.0037 2.545E-05 0.000 6.087E+1054.2483 23299. 0.000 16.200 -0.005524 54045. -2368.0561 2.770E-05 0.000 6.087E+1054.0414 23479. 0.000 16.400 -0.005455 48517. -2238.6771 2.972E-05 0.000 6.087E+1053.7745 23659. 0.000 16.600 -0.005381 43298. -2110.0058 3.153E-05 0.000 6.087E+1053.4516 23838. 0.000 16.800 -0.005304 38388. -1982.1718 3.314E-05 0.000 6.087E+1053.0767 24018. 0.000 17.000 -0.005222 33782. -1855.2954 3.456E-05 0.000 6.087E+1052.6536 24198. 0.000 17.200 -0.005138 29480. -1729.4881 3.581E-05 0.000 6.087E+1052.1858 24377. 0.000 17.400 -0.005050 25479. -1604.8530 3.690E-05 0.000 6.087E+1051.6768 24557. 0.000 17.600 -0.004961 21775. -1481.4850 3.783E-05 0.000 6.087E+1051.1299 24737. 0.000 17.800 -0.004869 18366. -1359.4714 3.862E-05 0.000 6.087E+1050.5481 24917. 0.000 18.000 -0.004775 15248. -1238.8924 3.928E-05 0.000 6.087E+1049.9344 25096. 0.000 18.200 -0.004680 12418. -1119.8213 3.983E-05 0.000 6.087E+1049.2915 25276. 0.000 18.400 -0.004584 9871.0052 -1002.3251 4.027E-05 0.000 6.087E+1048.6219 25456. 0.000 18.600 -0.004487 7604.4851 -886.4652 4.061E-05 0.000 6.087E+1047.9280 25635. 0.000 18.800 -0.004389 5614.0228 -772.2976 4.087E-05 0.000 6.087E+1047.2117 25815. 0.000 19.000 -0.004291 3895.4949 -652.9313 4.106E-05 0.000 6.087E+1052.2602 29231. 0.000 19.200 -0.004192 2477.9817 -522.5516 4.118E-05 0.000 6.087E+1056.3896 32283. 0.000 19.400 -0.004093 1385.2703 -388.3707 4.126E-05 0.000 6.087E+1055.4279 32500. 0.000 19.600 -0.003994 611.8221 -256.5214 4.130E-05 0.000 6.087E+1054.4465 32716. 0.000 19.800 -0.003895 151.9852 -127.0498 4.131E-05 0.000 6.087E+1053.4465 32933. 0.000 20.000 -0.003796 0.000 0.000 4.132E-05 0.000 6.087E+1052.4283 16575. 0.000

* This analysis makes computations of pile response using nonlinear moment-curvaturerelationships. The above values of total stress are computed for combined axial and bending stress in elastic sections and do not equal actual stresses in concrete and steel in the range of nonlinear bending.

Page 29

existing phase1 81.lp6oOutput Summary for Load Case No. 4:

Pile-head deflection = 0.3000000 inchesComputed slope at pile head = -0.0048909 radiansMaximum bending moment = 633128. inch-lbsMaximum shear force = 26558. lbsDepth of maximum bending moment = 55.2000000 inches below pile headDepth of maximum shear force = 0.000000 inches below pile headNumber of iterations = 42Number of zero deflection points = 1

-------------------------------------------------------------------------------- Pile-head Deflection vs. Pile Length for Load Case 4--------------------------------------------------------------------------------

Boundary Condition Type 4, Deflection and Moment

Deflection = 0.30000 inMoment = 0. in-lbsAxial Load = 10000. lbs

Pile Pile Head Maximum Maximum Length Deflection Moment Shear feet inches ln-lbs lbs ------------ ------------ ------------ ------------ 20.0000 0.3000000 633128. 26558. 19.0000 0.3000000 633820. 26583. 18.0000 0.3000000 635222. 26614. 17.0000 0.3000000 634418. 26615. 16.0000 0.3000000 635704. 26668. 15.0000 0.3000000 635894. 26724. 14.0000 0.3000000 633571. 26739. 13.0000 0.3000000 631116. 26800. 12.0000 0.3000000 624497. 26844. 11.0000 0.3000000 611805. 26840. 10.0000 0.3000000 599082. 26966. 9.0000 0.3000000 506066. 24969. 8.0000 0.3000000 371796. 21398. 7.0000 0.3000000 266680. 18089. 6.0000 0.3000000 186041. 15055. 5.0000 0.3000000 124521. 12240. 4.0000 0.3000000 68118. 8936.3152393 3.0000 0.3000000 36595. 6461.4689978 2.0000 0.3000000 15242. 4041.1696167 1.0000 0.3000000 3120.5313321 1500.0944032

-------------------------------------------------------------------------------- Computed Values of Pile Loading and Deflection for Lateral Loading for Load Case Number 5--------------------------------------------------------------------------------

Pile-head conditions are Displacement and Moment (Loading Type 4)Displacement of pile head = 0.500000 inchesMoment at pile head = 0.000 in-lbsAxial load at pile head = 10000.000 lbs

Depth Deflect. Bending Shear Slope Total Bending Soil Res. Soil Spr. Distrib. X y Moment Force S Stress Stiffness p

Page 30

existing phase1 81.lp6o Es*h Lat. Load feet inches in-lbs lbs radians psi* lb-in^2 lb/in lb/inch lb/inch ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- 0.00 0.5000 0.000 37116. -0.009276 0.000 6.087E+10 -1062.7069 2550.4966 0.000 0.200 0.4777 86240. 34559. -0.009274 0.000 6.087E+10 -1067.8307 5364.4341 0.000 0.400 0.4555 166330. 31993. -0.009269 0.000 6.067E+10 -1070.7652 5641.9900 0.000 0.600 0.4332 240251. 29447. -0.009261 0.000 6.050E+10 -1051.2503 5823.4836 0.000 0.800 0.4110 308118. 26963. -0.009250 0.000 6.034E+10 -1018.1242 5944.8062 0.000 1.000 0.3888 370119. 24562. -0.009237 0.000 6.019E+10-982.8264 6066.1287 0.000 1.200 0.3667 426459. 22248. -0.009221 0.000 6.005E+10-945.3769 6187.4513 0.000 1.400 0.3446 477354. 20027. -0.009203 0.000 5.992E+10-905.7954 6308.7739 0.000 1.600 0.3225 523030. 17903. -0.009183 0.000 5.981E+10-864.1016 6430.0965 0.000 1.800 0.3005 563729. 15882. -0.009161 0.000 5.970E+10-820.3146 6551.4190 0.000 2.000 0.2785 599702. 13968. -0.009072 0.000 9.263E+09-774.4532 6672.7416 0.000 2.200 0.2570 631211. 12166. -0.008848 0.000 5.168E+09-727.4275 6794.0642 0.000 2.400 0.2361 658523. 10477. -0.008547 0.000 5.120E+09-680.2464 6915.3868 0.000 2.600 0.2159 681909. 8900.5014 -0.008230 0.000 5.041E+09-633.1262 7036.7093 0.000 2.800 0.1966 701640. 7437.1977 -0.007895 0.000 4.872E+09-586.2937 7158.0319 0.000 3.000 0.1780 717986. 6085.6219 -0.007539 0.000 4.711E+09-540.0194 7279.3545 0.000 3.200 0.1604 731213. 4844.1046 -0.007165 0.000 4.592E+09-494.5784 7400.6771 0.000 3.400 0.1437 741582. 3710.3384 -0.006777 0.000 4.505E+09-450.2268 7521.9996 0.000 3.600 0.1279 749348. 2681.4232 -0.006377 0.000 4.443E+09-407.2025 7643.3222 0.000 3.800 0.1130 754759. 1753.9110 -0.005967 0.000 4.358E+09-365.7244 7764.6448 0.000 4.000 0.0992 758053. 772.7957 -0.005548 0.000 4.308E+09-451.8717 10930. 0.000 4.200 0.0864 758735. -405.1826 -0.005124 0.000 4.297E+09-529.7769 14713. 0.000 4.400 0.0746 756354. -1597.9909 -0.004703 0.000 4.333E+09-464.2300 14930. 0.000 4.600 0.0638 751290. -2638.5474 -0.004289 0.000 4.412E+09-402.9003 15147. 0.000 4.800 0.0540 743895. -3537.1110 -0.003886 0.000 4.486E+09-345.9026 15363. 0.000 5.000 0.0452 734498. -4304.1965 -0.003494 0.000 4.564E+09-293.3354 15580. 0.000 5.200 0.0373 723403. -4950.5257 -0.003115 0.000 4.661E+09-245.2723 15796. 0.000 5.400 0.0302 710885. -5486.9456 -0.002750 0.000 4.779E+09-201.7443 16013. 0.000 5.600 0.0241 697197. -5924.3292 -0.002401 0.000 4.918E+09-162.7421 16230. 0.000

Page 31

existing phase1 81.lp6o 5.800 0.0187 682564. -6273.4853 -0.002068 0.000 5.038E+09-128.2213 16446. 0.000 6.000 0.0141 667184. -6545.1334 -0.001749 0.000 5.091E+09-98.1521 16663. 0.000 6.200 0.0103 651231. -6749.9954 -0.001439 0.000 5.138E+09-72.5663 16879. 0.000 6.400 0.007229 634853. -6898.8648 -0.001140 0.000 5.163E+09-51.4915 17096. 0.000 6.600 0.004848 618171. -7002.6162 -0.000849 0.000 5.186E+09-34.9681 17313. 0.000 6.800 0.003153 601281. -7072.2131 -0.000568 0.000 5.236E+09-23.0293 17529. 0.000 7.000 0.002120 584252. -7118.6587 -0.000404 0.000 2.617E+10-15.6753 17746. 0.000 7.200 0.001215 567131. -7148.3856 -0.000365 0.000 5.970E+10-9.0972 17962. 0.000 7.400 0.000366 549957. -7162.6265 -0.000343 0.000 5.974E+10-2.7703 18179. 0.000 7.600 -0.000431 532767. -7161.9865 -0.000321 0.000 5.979E+103.3036 18396. 0.000 7.800 -0.001176 515595. -7147.0743 -0.000300 0.000 5.983E+109.1232 18612. 0.000 8.000 -0.001872 498475. -7118.5010 -0.000280 0.000 5.987E+1014.6879 18829. 0.000 8.200 -0.002520 481440. -7076.8784 -0.000260 0.000 5.991E+1019.9976 19045. 0.000 8.400 -0.003122 464519. -7022.8179 -0.000241 0.000 5.996E+1025.0528 19262. 0.000 8.600 -0.003678 447742. -6956.9293 -0.000223 0.000 6.000E+1029.8543 19479. 0.000 8.800 -0.004192 431136. -6879.8197 -0.000206 0.000 6.004E+1034.4037 19695. 0.000 9.000 -0.004665 414728. -6794.9463 -0.000189 0.000 6.008E+1036.3242 18688. 0.000 9.200 -0.005098 398530. -6707.5450 -0.000172 0.000 6.012E+1036.5102 17189. 0.000 9.400 -0.005492 382541. -6616.0357 -0.000157 0.000 6.016E+1039.7476 17369. 0.000 9.600 -0.005850 366780. -6517.0069 -0.000142 0.000 6.020E+1042.7763 17549. 0.000 9.800 -0.006173 351266. -6410.9560 -0.000128 0.000 6.023E+1045.5995 17728. 0.000 10.000 -0.006462 336014. -6298.3722 -0.000114 0.000 6.027E+1048.2203 17908. 0.000 10.200 -0.006720 321039. -6179.7370 -0.000101 0.000 6.031E+1050.6424 18088. 0.000 10.400 -0.006946 306356. -6055.5224 -8.829E-05 0.000 6.035E+1052.8697 18267. 0.000 10.600 -0.007143 291977. -5926.1915 -7.640E-05 0.000 6.038E+1054.9061 18447. 0.000 10.800 -0.007313 277914. -5792.1971 -6.507E-05 0.000 6.041E+1056.7559 18627. 0.000 11.000 -0.007456 264177. -5653.9819 -5.431E-05 0.000 6.044E+1058.4234 18807. 0.000 11.200 -0.007573 250777. -5511.9779 -4.409E-05 0.000 6.047E+1059.9132 18986. 0.000 11.400 -0.007667 237722. -5366.6062 -3.439E-05 0.000 6.051E+1061.2299 19166. 0.000 11.600 -0.007739 225019. -5218.2766 -2.522E-05 0.000 6.055E+1062.3782 19346. 0.000 11.800 -0.007788 212675. -5067.3872 -1.655E-05 0.000 6.057E+1063.3630 19525. 0.000 12.000 -0.007818 200696. -4914.3246 -8.359E-06 0.000 6.059E+10

Page 32

existing phase1 81.lp6o64.1892 19705. 0.000 12.200 -0.007829 189087. -4759.4635 -6.403E-07 0.000 6.061E+1064.8618 19885. 0.000 12.400 -0.007821 177851. -4603.1665 6.623E-06 0.000 6.064E+1065.3857 20064. 0.000 12.600 -0.007797 166991. -4445.7846 1.345E-05 0.000 6.067E+1065.7660 20244. 0.000 12.800 -0.007757 156511. -4287.6561 1.984E-05 0.000 6.070E+1066.0077 20424. 0.000 13.000 -0.007701 146410. -4129.1077 2.583E-05 0.000 6.072E+1066.1160 20604. 0.000 13.200 -0.007633 136690. -3970.4537 3.142E-05 0.000 6.073E+1066.0957 20783. 0.000 13.400 -0.007551 127350. -3811.9967 3.664E-05 0.000 6.075E+1065.9518 20963. 0.000 13.600 -0.007457 118390. -3654.0273 4.149E-05 0.000 6.076E+1065.6894 21143. 0.000 13.800 -0.007351 109809. -3496.8244 4.600E-05 0.000 6.078E+1065.3131 21322. 0.000 14.000 -0.007236 101603. -3340.6553 5.017E-05 0.000 6.079E+1064.8278 21502. 0.000 14.200 -0.007111 93771. -3185.7759 5.403E-05 0.000 6.081E+1064.2383 21682. 0.000 14.400 -0.006977 86309. -3032.4311 5.758E-05 0.000 6.083E+1063.5491 21862. 0.000 14.600 -0.006834 79213. -2880.8544 6.085E-05 0.000 6.086E+1062.7648 22041. 0.000 14.800 -0.006684 72478. -2731.2691 6.384E-05 0.000 6.087E+1061.8897 22221. 0.000 15.000 -0.006528 66100. -2583.8876 6.657E-05 0.000 6.087E+1060.9282 22401. 0.000 15.200 -0.006365 60072. -2438.9125 6.906E-05 0.000 6.087E+1059.8844 22580. 0.000 15.400 -0.006196 54390. -2296.5365 7.131E-05 0.000 6.087E+1058.7623 22760. 0.000 15.600 -0.006023 49045. -2156.9428 7.335E-05 0.000 6.087E+1057.5657 22940. 0.000 15.800 -0.005844 44033. -2020.3058 7.519E-05 0.000 6.087E+1056.2985 23120. 0.000 16.000 -0.005662 39344. -1886.7908 7.683E-05 0.000 6.087E+1054.9640 23299. 0.000 16.200 -0.005475 34972. -1756.5550 7.830E-05 0.000 6.087E+1053.5658 23479. 0.000 16.400 -0.005286 30909. -1629.7475 7.960E-05 0.000 6.087E+1052.1071 23659. 0.000 16.600 -0.005093 27146. -1506.5099 8.074E-05 0.000 6.087E+1050.5910 23838. 0.000 16.800 -0.004898 23674. -1386.9764 8.174E-05 0.000 6.087E+1049.0203 24018. 0.000 17.000 -0.004701 20484. -1271.2747 8.261E-05 0.000 6.087E+1047.3978 24198. 0.000 17.200 -0.004502 17568. -1159.5261 8.336E-05 0.000 6.087E+1045.7261 24377. 0.000 17.400 -0.004301 14915. -1051.8459 8.400E-05 0.000 6.087E+1044.0075 24557. 0.000 17.600 -0.004099 12515. -948.3437 8.454E-05 0.000 6.087E+1042.2443 24737. 0.000 17.800 -0.003895 10359. -849.1244 8.499E-05 0.000 6.087E+1040.4385 24917. 0.000 18.000 -0.003691 8435.0814 -754.2878 8.537E-05 0.000 6.087E+1038.5920 25096. 0.000 18.200 -0.003485 6733.8829 -663.9297 8.566E-05 0.000 6.087E+1036.7064 25276. 0.000

Page 33

existing phase1 81.lp6o 18.400 -0.003279 5244.1070 -578.1419 8.590E-05 0.000 6.087E+1034.7834 25456. 0.000 18.600 -0.003073 3954.6784 -497.0128 8.608E-05 0.000 6.087E+1032.8242 25635. 0.000 18.800 -0.002866 2854.3135 -420.6277 8.622E-05 0.000 6.087E+1030.8301 25815. 0.000 19.000 -0.002659 1931.5271 -344.7669 8.631E-05 0.000 6.087E+1032.3873 29231. 0.000 19.200 -0.002452 1195.2896 -266.3240 8.637E-05 0.000 6.087E+1032.9818 32283. 0.000 19.400 -0.002245 649.0261 -190.2715 8.641E-05 0.000 6.087E+1030.3953 32500. 0.000 19.600 -0.002037 277.8386 -120.4727 8.643E-05 0.000 6.087E+1027.7705 32716. 0.000 19.800 -0.001830 66.6087 -57.0187 8.643E-05 0.000 6.087E+1025.1079 32933. 0.000 20.000 -0.001622 0.000 0.000 8.643E-05 0.000 6.087E+1022.4077 16575. 0.000

* This analysis makes computations of pile response using nonlinear moment-curvaturerelationships. The above values of total stress are computed for combined axial and bending stress in elastic sections and do not equal actual stresses in concrete and steel in the range of nonlinear bending.

Output Summary for Load Case No. 5:

Pile-head deflection = 0.5000000 inchesComputed slope at pile head = -0.0092759 radiansMaximum bending moment = 758735. inch-lbsMaximum shear force = 37116. lbsDepth of maximum bending moment = 50.4000000 inches below pile headDepth of maximum shear force = 0.000000 inches below pile headNumber of iterations = 56Number of zero deflection points = 1

-------------------------------------------------------------------------------- Computed Values of Pile Loading and Deflection for Lateral Loading for Load Case Number 6--------------------------------------------------------------------------------

Pile-head conditions are Displacement and Moment (Loading Type 4)Displacement of pile head = 0.750000 inchesMoment at pile head = 0.000 in-lbsAxial load at pile head = 10000.000 lbs

Depth Deflect. Bending Shear Slope Total Bending Soil Res. Soil Spr. Distrib. X y Moment Force S Stress Stiffness p Es*h Lat. Load feet inches in-lbs lbs radians psi* lb-in^2 lb/in lb/inch lb/inch ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- 0.00 0.7500 0.000 46549. -0.0154 0.000 6.087E+10 -1400.4316 2240.6905 0.000 0.200 0.7130 108054. 43190. -0.0154 0.000 6.087E+10 -1399.0161 4709.0938 0.000 0.400 0.6760 208050. 39838. -0.0154 0.000 6.058E+10

Page 34

existing phase1 81.lp6o-1394.0269 4948.9627 0.000 0.600 0.6391 300016. 36503. -0.0154 0.000 6.037E+10 -1385.3273 5202.4957 0.000 0.800 0.6021 384002. 33193. -0.0154 0.000 6.016E+10 -1372.7809 5471.5595 0.000 1.000 0.5653 460080. 29918. -0.0154 0.000 5.997E+10 -1356.2513 5758.4949 0.000 1.200 0.5284 528346. 26681. -0.0153 0.000 5.980E+10 -1341.7612 6094.2556 0.000 1.400 0.4916 588883. 23520. -0.0153 0.000 1.920E+10 -1292.2623 6308.7739 0.000 1.600 0.4550 641975. 20506. -0.0151 0.000 5.153E+09 -1218.9977 6430.0965 0.000 1.800 0.4191 688038. 17671. -0.0148 0.000 5.007E+09 -1143.9894 6551.4190 0.000 2.000 0.3840 727504. 15017. -0.0144 0.000 4.625E+09 -1067.5516 6672.7416 0.000 2.200 0.3498 760812. 12548. -0.0140 0.000 4.269E+09-990.1285 6794.0642 0.000 2.400 0.3166 788406. 10265. -0.0136 0.000 3.743E+09-912.2051 6915.3868 0.000 2.600 0.2846 810734. 8168.7202 -0.0130 0.000 3.410E+09-834.4844 7036.7093 0.000 2.800 0.2540 828242. 6258.1992 -0.0124 0.000 3.153E+09-757.6165 7158.0319 0.000 3.000 0.2249 841370. 4530.3656 -0.0117 0.000 2.736E+09-682.2449 7279.3545 0.000 3.200 0.1976 850551. 2980.3981 -0.0110 0.000 2.491E+09-609.3947 7400.6771 0.000 3.400 0.1723 856203. 1601.1892 -0.0101 0.000 2.355E+09-539.9460 7521.9996 0.000 3.600 0.1490 858723. 383.7286 -0.009240 0.000 2.298E+09-474.6046 7643.3222 0.000 3.800 0.1279 858488. -682.4484 -0.008344 0.000 2.303E+09-413.8763 7764.6448 0.000 4.000 0.1090 855848. -1774.6399 -0.007462 0.000 2.364E+09-496.2832 10930. 0.000 4.200 0.0921 850328. -3047.7894 -0.006619 0.000 2.499E+09-564.6747 14713. 0.000 4.400 0.0772 841536. -4301.7067 -0.005842 0.000 2.734E+09-480.2564 14930. 0.000 4.600 0.0641 829960. -5363.2182 -0.005152 0.000 3.108E+09-404.3366 15147. 0.000 4.800 0.0525 816040. -6251.4934 -0.004538 0.000 3.341E+09-335.8928 15363. 0.000 5.000 0.0423 800171. -6983.9511 -0.003975 0.000 3.559E+09-274.4886 15580. 0.000 5.200 0.0334 782708. -7577.0608 -0.003461 0.000 3.842E+09-219.7694 15796. 0.000 5.400 0.0257 763967. -8046.3136 -0.002999 0.000 4.207E+09-171.2745 16013. 0.000 5.600 0.0190 744230. -8405.9949 -0.002582 0.000 4.485E+09-128.4599 16230. 0.000 5.800 0.0133 723742. -8669.3361 -0.002196 0.000 4.659E+09-90.9911 16446. 0.000 6.000 0.008455 702722. -8848.9682 -0.001836 0.000 4.862E+09-58.7024 16663. 0.000 6.200 0.004464 681355. -8957.0888 -0.001501 0.000 5.043E+09-31.3981 16879. 0.000 6.400 0.001252 659800. -9005.4677 -0.001184 0.000 5.116E+09-8.9175 17096. 0.000 6.600 -0.001218 638186. -9005.6274 -0.000881 0.000 5.159E+098.7844 17313. 0.000

Page 35

existing phase1 81.lp6o 6.800 -0.002975 616615. -8969.0128 -0.000590 0.000 5.189E+0921.7277 17529. 0.000 7.000 -0.004047 595163. -8907.0276 -0.000375 0.000 9.867E+0929.9267 17746. 0.000 7.200 -0.004772 573880. -8828.2530 -0.000291 0.000 5.968E+1035.7189 17962. 0.000 7.400 -0.005442 552801. -8735.9234 -0.000268 0.000 5.973E+1041.2225 18179. 0.000 7.600 -0.006059 531960. -8630.7304 -0.000246 0.000 5.979E+1046.4383 18396. 0.000 7.800 -0.006624 511386. -8513.3628 -0.000225 0.000 5.984E+1051.3680 18612. 0.000 8.000 -0.007140 491107. -8384.5050 -0.000205 0.000 5.989E+1056.0135 18829. 0.000 8.200 -0.007608 471150. -8244.8360 -0.000186 0.000 5.994E+1060.3773 19045. 0.000 8.400 -0.008032 451540. -8095.0284 -0.000167 0.000 5.999E+1064.4623 19262. 0.000 8.600 -0.008412 432302. -7935.7474 -0.000150 0.000 6.004E+1068.2719 19479. 0.000 8.800 -0.008750 413456. -7767.6495 -0.000133 0.000 6.008E+1071.8097 19695. 0.000 9.000 -0.009049 395023. -7596.9187 -0.000117 0.000 6.013E+1070.4660 18688. 0.000 9.200 -0.009311 376996. -7432.3392 -0.000101 0.000 6.018E+1066.6836 17189. 0.000 9.400 -0.009536 359353. -7269.5076 -8.660E-05 0.000 6.022E+1069.0093 17369. 0.000 9.600 -0.009726 342107. -7101.3556 -7.263E-05 0.000 6.025E+1071.1174 17549. 0.000 9.800 -0.009884 325270. -6928.3999 -5.934E-05 0.000 6.030E+1073.0124 17728. 0.000 10.000 -0.0100 308853. -6751.1459 -4.672E-05 0.000 6.034E+1074.6992 17908. 0.000 10.200 -0.0101 292867. -6570.0874 -3.476E-05 0.000 6.038E+1076.1829 18088. 0.000 10.400 -0.0102 277319. -6385.7059 -2.343E-05 0.000 6.041E+1077.4684 18267. 0.000 10.600 -0.0102 262217. -6198.4704 -1.272E-05 0.000 6.045E+1078.5612 18447. 0.000 10.800 -0.0102 247567. -6008.8373 -2.600E-06 0.000 6.048E+1079.4664 18627. 0.000 11.000 -0.0102 233374. -5817.2501 6.939E-06 0.000 6.052E+1080.1896 18807. 0.000 11.200 -0.0102 219644. -5624.1391 1.592E-05 0.000 6.055E+1080.7363 18986. 0.000 11.400 -0.0102 206378. -5429.9213 2.436E-05 0.000 6.058E+1081.1119 19166. 0.000 11.600 -0.0101 193579. -5235.0004 3.228E-05 0.000 6.060E+1081.3221 19346. 0.000 11.800 -0.0100 181248. -5039.7670 3.970E-05 0.000 6.063E+1081.3724 19525. 0.000 12.000 -0.009898 169386. -4844.5981 4.664E-05 0.000 6.066E+1081.2683 19705. 0.000 12.200 -0.009778 157992. -4649.8575 5.311E-05 0.000 6.070E+1081.0155 19885. 0.000 12.400 -0.009643 147064. -4455.8958 5.914E-05 0.000 6.072E+1080.6193 20064. 0.000 12.600 -0.009494 136601. -4263.0504 6.475E-05 0.000 6.073E+1080.0852 20244. 0.000 12.800 -0.009332 126598. -4071.6458 6.995E-05 0.000 6.075E+1079.4186 20424. 0.000 13.000 -0.009159 117053. -3881.9939 7.476E-05 0.000 6.076E+10

Page 36

existing phase1 81.lp6o78.6247 20604. 0.000 13.200 -0.008974 107961. -3694.3939 7.920E-05 0.000 6.078E+1077.7086 20783. 0.000 13.400 -0.008778 99317. -3509.1329 8.330E-05 0.000 6.080E+1076.6755 20963. 0.000 13.600 -0.008574 91113. -3326.4858 8.705E-05 0.000 6.082E+1075.5303 21143. 0.000 13.800 -0.008361 83345. -3146.7162 9.049E-05 0.000 6.084E+1074.2778 21322. 0.000 14.000 -0.008139 76005. -2970.0757 9.364E-05 0.000 6.087E+1072.9226 21502. 0.000 14.200 -0.007911 69084. -2796.8053 9.650E-05 0.000 6.087E+1071.4694 21682. 0.000 14.400 -0.007676 62575. -2627.1353 9.909E-05 0.000 6.087E+1069.9224 21862. 0.000 14.600 -0.007435 56469. -2461.2855 0.000101 0.000 6.087E+1068.2858 22041. 0.000 14.800 -0.007189 50756. -2299.4660 0.000104 0.000 6.087E+1066.5637 22221. 0.000 15.000 -0.006938 45427. -2141.8776 0.000105 0.000 6.087E+1064.7600 22401. 0.000 15.200 -0.006683 40470. -1988.7118 0.000107 0.000 6.087E+1062.8782 22580. 0.000 15.400 -0.006424 35876. -1840.1518 0.000109 0.000 6.087E+1060.9218 22760. 0.000 15.600 -0.006162 31632. -1696.3724 0.000110 0.000 6.087E+1058.8943 22940. 0.000 15.800 -0.005896 27728. -1557.5411 0.000111 0.000 6.087E+1056.7986 23120. 0.000 16.000 -0.005628 24151. -1423.8177 0.000112 0.000 6.087E+1054.6376 23299. 0.000 16.200 -0.005358 20888. -1295.3555 0.000113 0.000 6.087E+1052.4142 23479. 0.000 16.400 -0.005085 17928. -1172.3016 0.000114 0.000 6.087E+1050.1308 23659. 0.000 16.600 -0.004811 15256. -1054.7971 0.000114 0.000 6.087E+1047.7897 23838. 0.000 16.800 -0.004536 12859. -942.9776 0.000115 0.000 6.087E+1045.3932 24018. 0.000 17.000 -0.004259 10724. -836.9741 0.000115 0.000 6.087E+1042.9431 24198. 0.000 17.200 -0.003982 8836.2293 -736.9128 0.000116 0.000 6.087E+1040.4413 24377. 0.000 17.400 -0.003703 7181.3242 -642.9160 0.000116 0.000 6.087E+1037.8894 24557. 0.000 17.600 -0.003424 5744.6549 -555.1023 0.000116 0.000 6.087E+1035.2887 24737. 0.000 17.800 -0.003144 4511.2432 -473.5872 0.000117 0.000 6.087E+1032.6406 24917. 0.000 18.000 -0.002864 3465.8369 -398.4832 0.000117 0.000 6.087E+1029.9461 25096. 0.000 18.200 -0.002583 2592.9170 -329.9004 0.000117 0.000 6.087E+1027.2062 25276. 0.000 18.400 -0.002303 1876.7023 -267.9469 0.000117 0.000 6.087E+1024.4217 25456. 0.000 18.600 -0.002022 1301.1548 -212.7289 0.000117 0.000 6.087E+1021.5933 25635. 0.000 18.800 -0.001741 849.9833 -164.3514 0.000117 0.000 6.087E+1018.7214 25815. 0.000 19.000 -0.001459 506.6462 -120.5567 0.000117 0.000 6.087E+1017.7742 29231. 0.000 19.200 -0.001178 265.6878 -80.2103 0.000117 0.000 6.087E+1015.8479 32283. 0.000

Page 37

existing phase1 81.lp6o 19.400 -0.000897 116.0127 -46.6176 0.000117 0.000 6.087E+1012.1461 32500. 0.000 19.600 -0.000616 36.2989 -21.9703 0.000117 0.000 6.087E+108.3934 32716. 0.000 19.800 -0.000334 4.9307 -6.3905 0.000117 0.000 6.087E+104.5898 32933. 0.000 20.000 -5.325E-05 0.000 0.000 0.000117 0.000 6.087E+100.7356 16575. 0.000

* This analysis makes computations of pile response using nonlinear moment-curvaturerelationships. The above values of total stress are computed for combined axial and bending stress in elastic sections and do not equal actual stresses in concrete and steel in the range of nonlinear bending.

Output Summary for Load Case No. 6:

Pile-head deflection = 0.7500000 inchesComputed slope at pile head = -0.0154118 radiansMaximum bending moment = 858723. inch-lbsMaximum shear force = 46549. lbsDepth of maximum bending moment = 43.2000000 inches below pile headDepth of maximum shear force = 0.000000 inches below pile headNumber of iterations = 52Number of zero deflection points = 2

-------------------------------------------------------------------------------- Computed Values of Pile Loading and Deflection for Lateral Loading for Load Case Number 7--------------------------------------------------------------------------------

Pile-head conditions are Displacement and Moment (Loading Type 4)Displacement of pile head = 1.000000 inchesMoment at pile head = 0.000 in-lbsAxial load at pile head = 10000.000 lbs

Depth Deflect. Bending Shear Slope Total Bending Soil Res. Soil Spr. Distrib. X y Moment Force S Stress Stiffness p Es*h Lat. Load feet inches in-lbs lbs radians psi* lb-in^2 lb/in lb/inch lb/inch ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- 0.00 1.0000 0.000 52749. -0.0224 0.000 6.087E+10 -1603.0664 1923.6796 0.000 0.200 0.9462 122519. 48831. -0.0224 0.000 6.087E+10 -1662.2326 4216.0805 0.000 0.400 0.8925 235463. 44783. -0.0224 0.000 6.052E+10 -1711.2432 4601.8665 0.000 0.600 0.8387 338550. 40701. -0.0224 0.000 6.026E+10 -1689.7911 4835.3495 0.000 0.800 0.7850 431903. 36678. -0.0224 0.000 6.004E+10 -1662.7446 5083.4884 0.000 1.000 0.7313 515679. 32727. -0.0224 0.000 5.983E+10 -1629.9053 5348.7615 0.000 1.200 0.6777 590066. 28855. -0.0223 0.000 1.486E+10 -1596.5628 5653.8543 0.000 1.400 0.6243 655255. 25070. -0.0221 0.000 5.128E+09

Page 38

existing phase1 81.lp6o-1558.2124 5989.9164 0.000 1.600 0.5717 711460. 21381. -0.0218 0.000 4.774E+09 -1515.6610 6362.9682 0.000 1.800 0.5199 758927. 17859. -0.0214 0.000 4.297E+09 -1419.1620 6551.4190 0.000 2.000 0.4691 798210. 14591. -0.0209 0.000 3.587E+09 -1304.2651 6672.7416 0.000 2.200 0.4196 829967. 11600. -0.0203 0.000 3.104E+09 -1187.8626 6794.0642 0.000 2.400 0.3717 854867. 8889.9551 -0.0196 0.000 2.382E+09 -1070.8941 6915.3868 0.000 2.600 0.3258 873577. 6458.7178 -0.0186 0.000 2.002E+09-955.1370 7036.7093 0.000 2.800 0.2824 886761. 4301.8695 -0.0175 0.000 1.770E+09-842.2366 7158.0319 0.000 3.000 0.2419 895065. 2410.7384 -0.0161 0.000 1.364E+09-733.7059 7279.3545 0.000 3.200 0.2052 899105. 771.0083 -0.0144 0.000 1.171E+09-632.7359 7400.6771 0.000 3.400 0.1729 899456. -638.5664 -0.0125 0.000 1.151E+09-541.9097 7521.9996 0.000 3.600 0.1451 896640. -1843.4419 -0.0107 0.000 1.279E+09-462.1532 7643.3222 0.000 3.800 0.1214 891123. -2869.2054 -0.009203 0.000 1.543E+09-392.6498 7764.6448 0.000 4.000 0.1009 883310. -3892.0332 -0.007934 0.000 1.840E+09-459.7066 10930. 0.000 4.200 0.0833 872822. -5056.3849 -0.006838 0.000 2.015E+09-510.5865 14713. 0.000 4.400 0.0681 859368. -6177.6187 -0.005866 0.000 2.280E+09-423.7751 14930. 0.000 4.600 0.0551 843451. -7103.6634 -0.005035 0.000 2.674E+09-347.9288 15147. 0.000 4.800 0.0440 825512. -7858.8196 -0.004348 0.000 3.212E+09-281.3680 15363. 0.000 5.000 0.0343 805937. -8463.3396 -0.003761 0.000 3.475E+09-222.3987 15580. 0.000 5.200 0.0259 785068. -8934.7841 -0.003235 0.000 3.799E+09-170.4718 15796. 0.000 5.400 0.0187 763205. -9289.3231 -0.002770 0.000 4.221E+09-124.9774 16013. 0.000 5.600 0.0126 740612. -9541.5748 -0.002356 0.000 4.514E+09-85.2324 16230. 0.000 5.800 0.007422 717519. -9704.8831 -0.001977 0.000 4.716E+09-50.8579 16446. 0.000 6.000 0.003116 694124. -9791.8713 -0.001626 0.000 4.953E+09-21.6323 16663. 0.000 6.200 -0.000383 670596. -9814.5982 -0.001299 0.000 5.080E+092.6932 16879. 0.000 6.400 -0.003121 647076. -9784.6860 -0.000990 0.000 5.146E+0922.2337 17096. 0.000 6.600 -0.005135 623677. -9713.5528 -0.000695 0.000 5.179E+0937.0439 17313. 0.000 6.800 -0.006456 600484. -9612.5189 -0.000412 0.000 5.224E+0947.1510 17529. 0.000 7.000 -0.007114 577557. -9492.8162 -0.000263 0.000 5.967E+1052.6012 17746. 0.000 7.200 -0.007716 554931. -9360.3911 -0.000240 0.000 5.973E+1057.7530 17962. 0.000 7.400 -0.008266 532638. -9215.9577 -0.000218 0.000 5.979E+1062.6081 18179. 0.000 7.600 -0.008763 510705. -9060.2251 -0.000197 0.000 5.984E+1067.1691 18396. 0.000

Page 39

existing phase1 81.lp6o 7.800 -0.009212 489159. -8893.8959 -0.000177 0.000 5.989E+1071.4386 18612. 0.000 8.000 -0.009613 468023. -8717.6656 -0.000158 0.000 5.995E+1075.4200 18829. 0.000 8.200 -0.009970 447321. -8532.2212 -0.000140 0.000 6.000E+1079.1170 19045. 0.000 8.400 -0.0103 427075. -8338.2402 -0.000122 0.000 6.005E+1082.5338 19262. 0.000 8.600 -0.0106 407304. -8136.3902 -0.000105 0.000 6.009E+1085.6746 19479. 0.000 8.800 -0.0108 388026. -7927.3276 -8.959E-05 0.000 6.015E+1088.5443 19695. 0.000 9.000 -0.0110 369257. -7718.4184 -7.449E-05 0.000 6.019E+1085.5467 18688. 0.000 9.200 -0.0111 350981. -7519.9564 -6.013E-05 0.000 6.023E+1079.8384 17189. 0.000 9.400 -0.0113 333164. -7326.2351 -4.651E-05 0.000 6.028E+1081.5961 17369. 0.000 9.600 -0.0114 315817. -7128.5517 -3.359E-05 0.000 6.032E+1083.1401 17549. 0.000 9.800 -0.0114 298949. -6927.4128 -2.137E-05 0.000 6.037E+1084.4757 17728. 0.000 10.000 -0.0115 282566. -6723.3121 -9.813E-06 0.000 6.040E+1085.6082 17908. 0.000 10.200 -0.0115 266677. -6516.7303 1.096E-06 0.000 6.043E+1086.5433 18088. 0.000 10.400 -0.0115 251286. -6308.1348 1.138E-05 0.000 6.047E+1087.2863 18267. 0.000 10.600 -0.0114 236398. -6097.9794 2.105E-05 0.000 6.051E+1087.8432 18447. 0.000 10.800 -0.0114 222015. -5886.7043 3.014E-05 0.000 6.055E+1088.2194 18627. 0.000 11.000 -0.0113 208140. -5674.7358 3.866E-05 0.000 6.057E+1088.4210 18807. 0.000 11.200 -0.0112 194774. -5462.4863 4.664E-05 0.000 6.060E+1088.4536 18986. 0.000 11.400 -0.0111 181918. -5250.3546 5.410E-05 0.000 6.063E+1088.3229 19166. 0.000 11.600 -0.0109 169570. -5038.7254 6.106E-05 0.000 6.066E+1088.0348 19346. 0.000 11.800 -0.0108 157729. -4827.9697 6.753E-05 0.000 6.070E+1087.5949 19525. 0.000 12.000 -0.0106 146392. -4618.4449 7.354E-05 0.000 6.072E+1087.0090 19705. 0.000 12.200 -0.0104 135557. -4410.4948 7.911E-05 0.000 6.074E+1086.2827 19885. 0.000 12.400 -0.0102 125218. -4204.4498 8.426E-05 0.000 6.075E+1085.4214 20064. 0.000 12.600 -0.0100 115371. -4000.6274 8.901E-05 0.000 6.077E+1084.4306 20244. 0.000 12.800 -0.009790 106011. -3799.3320 9.339E-05 0.000 6.078E+1083.3155 20424. 0.000 13.000 -0.009561 97130. -3600.8556 9.740E-05 0.000 6.080E+1082.0814 20604. 0.000 13.200 -0.009323 88722. -3405.4779 0.000101 0.000 6.083E+1080.7333 20783. 0.000 13.400 -0.009076 80779. -3213.4666 0.000104 0.000 6.085E+1079.2761 20963. 0.000 13.600 -0.008822 73293. -3025.0777 0.000107 0.000 6.087E+1077.7146 21143. 0.000 13.800 -0.008560 66254. -2840.5561 0.000110 0.000 6.087E+1076.0534 21322. 0.000 14.000 -0.008293 59653. -2660.1358 0.000113 0.000 6.087E+10

Page 40

existing phase1 81.lp6o74.2969 21502. 0.000 14.200 -0.008020 53479. -2484.0405 0.000115 0.000 6.087E+1072.4493 21682. 0.000 14.400 -0.007741 47724. -2312.4838 0.000117 0.000 6.087E+1070.5147 21862. 0.000 14.600 -0.007458 42374. -2145.6699 0.000119 0.000 6.087E+1068.4969 22041. 0.000 14.800 -0.007172 37419. -1983.7941 0.000120 0.000 6.087E+1066.3996 22221. 0.000 15.000 -0.006881 32846. -1827.0429 0.000122 0.000 6.087E+1064.2264 22401. 0.000 15.200 -0.006588 28643. -1675.5947 0.000123 0.000 6.087E+1061.9804 22580. 0.000 15.400 -0.006292 24797. -1529.6205 0.000124 0.000 6.087E+1059.6648 22760. 0.000 15.600 -0.005993 21295. -1389.2840 0.000125 0.000 6.087E+1057.2823 22940. 0.000 15.800 -0.005692 18123. -1254.7422 0.000126 0.000 6.087E+1054.8358 23120. 0.000 16.000 -0.005390 15266. -1126.1461 0.000126 0.000 6.087E+1052.3276 23299. 0.000 16.200 -0.005086 12711. -1003.6410 0.000127 0.000 6.087E+1049.7600 23479. 0.000 16.400 -0.004782 10443. -887.3669 0.000127 0.000 6.087E+1047.1351 23659. 0.000 16.600 -0.004476 8445.6220 -777.4593 0.000128 0.000 6.087E+1044.4546 23838. 0.000 16.800 -0.004169 6704.6821 -674.0492 0.000128 0.000 6.087E+1041.7204 24018. 0.000 17.000 -0.003862 5204.0456 -577.2640 0.000128 0.000 6.087E+1038.9339 24198. 0.000 17.200 -0.003554 3927.6631 -487.2278 0.000128 0.000 6.087E+1036.0963 24377. 0.000 17.400 -0.003246 2859.1916 -404.0617 0.000128 0.000 6.087E+1033.2088 24557. 0.000 17.600 -0.002937 1982.0001 -327.8843 0.000129 0.000 6.087E+1030.2724 24737. 0.000 17.800 -0.002628 1279.1756 -258.8121 0.000129 0.000 6.087E+1027.2878 24917. 0.000 18.000 -0.002320 733.5276 -196.9598 0.000129 0.000 6.087E+1024.2557 25096. 0.000 18.200 -0.002011 327.5920 -142.4409 0.000129 0.000 6.087E+1021.1767 25276. 0.000 18.400 -0.001702 43.6340 -95.3675 0.000129 0.000 6.087E+1018.0511 25456. 0.000 18.600 -0.001393 -136.3499 -55.8512 0.000129 0.000 6.087E+1014.8792 25635. 0.000 18.800 -0.001084 -230.6295 -24.0028 0.000129 0.000 6.087E+1011.6611 25815. 0.000 19.000 -0.000775 -257.7408 1.3213 0.000129 0.000 6.087E+109.4423 29231. 0.000 19.200 -0.000466 -230.4640 20.1812 0.000129 0.000 6.087E+106.2742 32283. 0.000 19.400 -0.000158 -167.0474 30.2718 0.000129 0.000 6.087E+102.1346 32500. 0.000 19.600 0.000151 -91.3351 30.3608 0.000129 0.000 6.087E+10-2.0605 32716. 0.000 19.800 0.000460 -27.4912 20.3147 0.000129 0.000 6.087E+10-6.3112 32933. 0.000 20.000 0.000769 0.000 0.000 0.000129 0.000 6.087E+10-10.6177 16575. 0.000

* This analysis makes computations of pile response using nonlinear moment-curvaturePage 41

existing phase1 81.lp6orelationships. The above values of total stress are computed for combined axial and bending stress in elastic sections and do not equal actual stresses in concrete and steel in the range of nonlinear bending.

Output Summary for Load Case No. 7:

Pile-head deflection = 1.0000000 inchesComputed slope at pile head = -0.0224065 radiansMaximum bending moment = 899456. inch-lbsMaximum shear force = 52749. lbsDepth of maximum bending moment = 40.8000000 inches below pile headDepth of maximum shear force = 0.000000 inches below pile headNumber of iterations = 80Number of zero deflection points = 2

-------------------------------------------------------------------------------- Computed Values of Pile Loading and Deflection for Lateral Loading for Load Case Number 8--------------------------------------------------------------------------------

Pile-head conditions are Displacement and Pile-head Rotation (Loading Type 5)Displacement of pile head = 0.010000 inchesRotation of pile head = 0.000E+00 radiansAxial load on pile head = 10000.000 lbs

Depth Deflect. Bending Shear Slope Total Bending Soil Res. Soil Spr. Distrib. X y Moment Force S Stress Stiffness p Es*h Lat. Load feet inches in-lbs lbs radians psi* lb-in^2 lb/in lb/inch lb/inch ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- 0.00 0.0100 -176928. 3608.1384 0.000 0.000 6.064E+10-22.7480 2729.7579 0.000 0.200 0.009992 -168335. 3552.3770 -6.832E-06 0.000 6.064E+10-23.2340 5580.8384 0.000 0.400 0.009967 -159876. 3496.0789 -1.332E-05 0.000 6.069E+10-23.6811 5702.1610 0.000 0.600 0.009928 -151553. 3438.7549 -1.948E-05 0.000 6.072E+10-24.0889 5823.4836 0.000 0.800 0.009874 -143369. 3380.4995 -2.531E-05 0.000 6.073E+10-24.4572 5944.8062 0.000 1.000 0.009806 -135325. 3321.4082 -3.082E-05 0.000 6.074E+10-24.7856 6066.1287 0.000 1.200 0.009726 -127425. 3261.5766 -3.601E-05 0.000 6.075E+10-25.0741 6187.4513 0.000 1.400 0.009633 -119668. 3201.1004 -4.089E-05 0.000 6.076E+10-25.3227 6308.7739 0.000 1.600 0.009530 -112057. 3140.0753 -4.546E-05 0.000 6.077E+10-25.5316 6430.0965 0.000 1.800 0.009415 -104594. 3078.5963 -4.974E-05 0.000 6.079E+10-25.7010 6551.4190 0.000 2.000 0.009291 -97278. 3016.7577 -5.373E-05 0.000 6.080E+10-25.8312 6672.7416 0.000 2.200 0.009157 -90111. 2954.6529 -5.742E-05 0.000 6.082E+10-25.9228 6794.0642 0.000 2.400 0.009015 -83093. 2892.3739 -6.084E-05 0.000 6.084E+10

Page 42

existing phase1 81.lp6o-25.9763 6915.3868 0.000 2.600 0.008865 -76224. 2830.0115 -6.398E-05 0.000 6.087E+10-25.9924 7036.7093 0.000 2.800 0.008708 -69506. 2767.6544 -6.685E-05 0.000 6.087E+10-25.9718 7158.0319 0.000 3.000 0.008544 -62936. 2705.3898 -6.947E-05 0.000 6.087E+10-25.9154 7279.3545 0.000 3.200 0.008375 -56516. 2643.3025 -7.182E-05 0.000 6.087E+10-25.8240 7400.6771 0.000 3.400 0.008200 -50245. 2581.4752 -7.392E-05 0.000 6.087E+10-25.6988 7521.9996 0.000 3.600 0.008020 -44122. 2519.9879 -7.579E-05 0.000 6.087E+10-25.5406 7643.3222 0.000 3.800 0.007836 -38145. 2458.9181 -7.741E-05 0.000 6.087E+10-25.3509 7764.6448 0.000 4.000 0.007648 -32315. 2386.6999 -7.880E-05 0.000 6.087E+10-34.8310 10930. 0.000 4.200 0.007458 -26685. 2290.0394 -7.996E-05 0.000 6.087E+10-45.7195 14713. 0.000 4.400 0.007264 -21319. 2180.9470 -8.091E-05 0.000 6.087E+10-45.1908 14930. 0.000 4.600 0.007069 -16213. 2073.1804 -8.165E-05 0.000 6.087E+10-44.6146 15147. 0.000 4.800 0.006872 -11364. 1966.8508 -8.219E-05 0.000 6.087E+10-43.9934 15363. 0.000 5.000 0.006675 -6768.2127 1862.0632 -8.255E-05 0.000 6.087E+10-43.3296 15580. 0.000 5.200 0.006476 -2422.0661 1758.9165 -8.273E-05 0.000 6.087E+10-42.6260 15796. 0.000 5.400 0.006278 1678.5573 1657.5034 -8.274E-05 0.000 6.087E+10-41.8850 16013. 0.000 5.600 0.006079 5537.9219 1557.9105 -8.260E-05 0.000 6.087E+10-41.1092 16230. 0.000 5.800 0.005881 9160.4924 1460.2181 -8.231E-05 0.000 6.087E+10-40.3011 16446. 0.000 6.000 0.005684 12551. 1364.5008 -8.188E-05 0.000 6.087E+10-39.4634 16663. 0.000 6.200 0.005488 15714. 1270.8266 -8.133E-05 0.000 6.087E+10-38.5984 16879. 0.000 6.400 0.005294 18655. 1179.2582 -8.065E-05 0.000 6.087E+10-37.7086 17096. 0.000 6.600 0.005101 21378. 1089.8520 -7.986E-05 0.000 6.087E+10-36.7965 17313. 0.000 6.800 0.004910 23890. 1002.6589 -7.897E-05 0.000 6.087E+10-35.8644 17529. 0.000 7.000 0.004722 26195. 917.7240 -7.798E-05 0.000 6.087E+10-34.9146 17746. 0.000 7.200 0.004536 28299. 835.0873 -7.690E-05 0.000 6.087E+10-33.9493 17962. 0.000 7.400 0.004353 30207. 754.7831 -7.575E-05 0.000 6.087E+10-32.9708 18179. 0.000 7.600 0.004172 31925. 676.8408 -7.453E-05 0.000 6.087E+10-31.9811 18396. 0.000 7.800 0.003995 33459. 601.2847 -7.324E-05 0.000 6.087E+10-30.9823 18612. 0.000 8.000 0.003821 34815. 528.1345 -7.189E-05 0.000 6.087E+10-29.9763 18829. 0.000 8.200 0.003650 35998. 457.4049 -7.050E-05 0.000 6.087E+10-28.9650 19045. 0.000 8.400 0.003483 37014. 389.1067 -6.906E-05 0.000 6.087E+10-27.9502 19262. 0.000 8.600 0.003319 37869. 323.2462 -6.758E-05 0.000 6.087E+10-26.9336 19479. 0.000

Page 43

existing phase1 81.lp6o 8.800 0.003158 38569. 259.8258 -6.607E-05 0.000 6.087E+10-25.9168 19695. 0.000 9.000 0.003001 39119. 200.6803 -6.454E-05 0.000 6.087E+10-23.3711 18688. 0.000 9.200 0.002848 39535. 148.1548 -6.299E-05 0.000 6.087E+10-20.4002 17189. 0.000 9.400 0.002699 39833. 100.2350 -6.143E-05 0.000 6.087E+10-19.5330 17369. 0.000 9.600 0.002553 40019. 54.3903 -5.985E-05 0.000 6.087E+10-18.6709 17549. 0.000 9.800 0.002412 40097. 10.6072 -5.827E-05 0.000 6.087E+10-17.8150 17728. 0.000 10.000 0.002274 40073. -31.1302 -5.669E-05 0.000 6.087E+10-16.9662 17908. 0.000 10.200 0.002140 39951. -70.8401 -5.511E-05 0.000 6.087E+10-16.1253 18088. 0.000 10.400 0.002009 39736. -108.5423 -5.354E-05 0.000 6.087E+10-15.2931 18267. 0.000 10.600 0.001883 39432. -144.2585 -5.198E-05 0.000 6.087E+10-14.4703 18447. 0.000 10.800 0.001760 39046. -178.0119 -5.044E-05 0.000 6.087E+10-13.6575 18627. 0.000 11.000 0.001641 38580. -209.8272 -4.890E-05 0.000 6.087E+10-12.8552 18807. 0.000 11.200 0.001525 38041. -239.7303 -4.739E-05 0.000 6.087E+10-12.0640 18986. 0.000 11.400 0.001413 37432. -267.7481 -4.591E-05 0.000 6.087E+10-11.2842 19166. 0.000 11.600 0.001305 36758. -293.9086 -4.444E-05 0.000 6.087E+10-10.5162 19346. 0.000 11.800 0.001200 36023. -318.2403 -4.301E-05 0.000 6.087E+10-9.7602 19525. 0.000 12.000 0.001098 35232. -340.7725 -4.160E-05 0.000 6.087E+10-9.0166 19705. 0.000 12.200 0.001000 34389. -361.5347 -4.023E-05 0.000 6.087E+10-8.2853 19885. 0.000 12.400 0.000905 33499. -380.5570 -3.889E-05 0.000 6.087E+10-7.5666 20064. 0.000 12.600 0.000813 32565. -397.8692 -3.759E-05 0.000 6.087E+10-6.8603 20244. 0.000 12.800 0.000725 31591. -413.5015 -3.633E-05 0.000 6.087E+10-6.1666 20424. 0.000 13.000 0.000639 30582. -427.4837 -3.510E-05 0.000 6.087E+10-5.4852 20604. 0.000 13.200 0.000556 29541. -439.8453 -3.392E-05 0.000 6.087E+10-4.8161 20783. 0.000 13.400 0.000476 28472. -450.6154 -3.277E-05 0.000 6.087E+10-4.1590 20963. 0.000 13.600 0.000399 27379. -459.8225 -3.167E-05 0.000 6.087E+10-3.5136 21143. 0.000 13.800 0.000324 26266. -467.4944 -3.061E-05 0.000 6.087E+10-2.8797 21322. 0.000 14.000 0.000252 25137. -473.6582 -2.960E-05 0.000 6.087E+10-2.2568 21502. 0.000 14.200 0.000182 23994. -478.3401 -2.863E-05 0.000 6.087E+10-1.6447 21682. 0.000 14.400 0.000114 22842. -481.5649 -2.771E-05 0.000 6.087E+10-1.0427 21862. 0.000 14.600 4.905E-05 21684. -483.3568 -2.683E-05 0.000 6.087E+10-0.4505 22041. 0.000 14.800 -1.431E-05 20523. -483.7384 -2.600E-05 0.000 6.087E+100.1325 22221. 0.000 15.000 -7.574E-05 19363. -482.7311 -2.521E-05 0.000 6.087E+10

Page 44

existing phase1 81.lp6o0.7069 22401. 0.000 15.200 -0.000135 18207. -480.3550 -2.447E-05 0.000 6.087E+101.2732 22580. 0.000 15.400 -0.000193 17059. -476.6285 -2.378E-05 0.000 6.087E+101.8322 22760. 0.000 15.600 -0.000249 15921. -471.5688 -2.313E-05 0.000 6.087E+102.3843 22940. 0.000 15.800 -0.000304 14796. -465.1911 -2.252E-05 0.000 6.087E+102.9304 23120. 0.000 16.000 -0.000358 13689. -457.5094 -2.196E-05 0.000 6.087E+103.4711 23299. 0.000 16.200 -0.000410 12601. -448.5356 -2.144E-05 0.000 6.087E+104.0071 23479. 0.000 16.400 -0.000460 11537. -438.2803 -2.096E-05 0.000 6.087E+104.5391 23659. 0.000 16.600 -0.000510 10499. -426.7519 -2.053E-05 0.000 6.087E+105.0679 23838. 0.000 16.800 -0.000559 9489.4973 -413.9573 -2.014E-05 0.000 6.087E+105.5942 24018. 0.000 17.000 -0.000607 8512.5899 -399.9017 -1.978E-05 0.000 6.087E+106.1188 24198. 0.000 17.200 -0.000654 7570.9187 -384.5883 -1.946E-05 0.000 6.087E+106.6424 24377. 0.000 17.400 -0.000700 6667.5003 -368.0187 -1.918E-05 0.000 6.087E+107.1656 24557. 0.000 17.600 -0.000746 5805.3496 -350.1928 -1.894E-05 0.000 6.087E+107.6893 24737. 0.000 17.800 -0.000791 4987.4841 -331.1085 -1.872E-05 0.000 6.087E+108.2142 24917. 0.000 18.000 -0.000836 4216.9277 -310.7624 -1.854E-05 0.000 6.087E+108.7409 25096. 0.000 18.200 -0.000880 3496.7148 -289.1492 -1.839E-05 0.000 6.087E+109.2701 25276. 0.000 18.400 -0.000924 2829.8943 -266.2622 -1.827E-05 0.000 6.087E+109.8024 25456. 0.000 18.600 -0.000968 2219.5328 -242.0933 -1.817E-05 0.000 6.087E+1010.3384 25635. 0.000 18.800 -0.001011 1668.7185 -216.6327 -1.809E-05 0.000 6.087E+1010.8787 25815. 0.000 19.000 -0.001055 1180.5642 -188.1632 -1.803E-05 0.000 6.087E+1012.8459 29231. 0.000 19.200 -0.001098 766.4009 -155.0256 -1.800E-05 0.000 6.087E+1014.7688 32283. 0.000 19.400 -0.001141 437.3050 -118.7605 -1.797E-05 0.000 6.087E+1015.4522 32500. 0.000 19.600 -0.001184 197.2133 -80.8464 -1.796E-05 0.000 6.087E+1016.1429 32716. 0.000 19.800 -0.001227 50.1044 -41.2656 -1.795E-05 0.000 6.087E+1016.8411 32933. 0.000 20.000 -0.001270 0.000 0.000 -1.795E-05 0.000 6.087E+1017.5470 16575. 0.000

* This analysis makes computations of pile response using nonlinear moment-curvaturerelationships. The above values of total stress are computed for combined axial and bending stress in elastic sections and do not equal actual stresses in concrete and steel in the range of nonlinear bending.

Output Summary for Load Case No. 8:

Pile-head deflection = 0.0100000 inchesPage 45

existing phase1 81.lp6oComputed slope at pile head = -0.000000170 radiansMaximum bending moment = -176928. inch-lbsMaximum shear force = 3608.1384462 lbsDepth of maximum bending moment = 0.000000 inches below pile headDepth of maximum shear force = 0.000000 inches below pile headNumber of iterations = 6Number of zero deflection points = 1

-------------------------------------------------------------------------------- Computed Values of Pile Loading and Deflection for Lateral Loading for Load Case Number 9--------------------------------------------------------------------------------

Pile-head conditions are Displacement and Pile-head Rotation (Loading Type 5)Displacement of pile head = 0.100000 inchesRotation of pile head = 0.000E+00 radiansAxial load on pile head = 10000.000 lbs

Depth Deflect. Bending Shear Slope Total Bending Soil Res. Soil Spr. Distrib. X y Moment Force S Stress Stiffness p Es*h Lat. Load feet inches in-lbs lbs radians psi* lb-in^2 lb/in lb/inch lb/inch ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- 0.00 0.1000 -717015. 24086. 0.000 0.000 4.707E+09-227.4798 2729.7579 0.000 0.200 0.0996 -659870. 23531. -0.000351 0.000 4.707E+09-231.5147 5580.8384 0.000 0.400 0.0983 -604051. 22973. -0.000648 0.000 5.620E+09-233.5866 5702.1610 0.000 0.600 0.0964 -549570. 22412. -0.000788 0.000 5.950E+10-234.0304 5823.4836 0.000 0.800 0.0945 -496437. 21850. -0.000809 0.000 5.987E+10-234.1538 5944.8062 0.000 1.000 0.0926 -444652. 21288. -0.000828 0.000 6.001E+10-233.9625 6066.1287 0.000 1.200 0.0906 -394215. 20727. -0.000845 0.000 6.013E+10-233.4624 6187.4513 0.000 1.400 0.0885 -345122. 20168. -0.000860 0.000 6.025E+10-232.6599 6308.7739 0.000 1.600 0.0864 -297368. 19611. -0.000872 0.000 6.037E+10-231.5620 6430.0965 0.000 1.800 0.0843 -250949. 19057. -0.000883 0.000 6.047E+10-230.1765 6551.4190 0.000 2.000 0.0822 -205854. 18506. -0.000892 0.000 6.058E+10-228.5113 6672.7416 0.000 2.200 0.0800 -162076. 17960. -0.000900 0.000 6.068E+10-226.5752 6794.0642 0.000 2.400 0.0779 -119603. 17419. -0.000905 0.000 6.076E+10-224.3772 6915.3868 0.000 2.600 0.0757 -78422. 16883. -0.000909 0.000 6.086E+10-221.9269 7036.7093 0.000 2.800 0.0735 -38519. 16354. -0.000911 0.000 6.087E+10-219.2343 7158.0319 0.000 3.000 0.0713 121.1371 15831. -0.000912 0.000 6.087E+10-216.3096 7279.3545 0.000 3.200 0.0691 37515. 15316. -0.000911 0.000 6.087E+10-213.1635 7400.6771 0.000 3.400 0.0669 73681. 14808. -0.000909 0.000 6.087E+10

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existing phase1 81.lp6o-209.8073 7521.9996 0.000 3.600 0.0648 108639. 14309. -0.000906 0.000 6.078E+10-206.2523 7643.3222 0.000 3.800 0.0626 142409. 13819. -0.000901 0.000 6.073E+10-202.5102 7764.6448 0.000 4.000 0.0604 175012. 13245. -0.000894 0.000 6.065E+10-275.2501 10930. 0.000 4.200 0.0583 206029. 12486. -0.000887 0.000 6.058E+10-357.4219 14713. 0.000 4.400 0.0562 234988. 11638. -0.000878 0.000 6.052E+10-349.5025 14930. 0.000 4.600 0.0541 261933. 10809. -0.000868 0.000 6.045E+10-341.3419 15147. 0.000 4.800 0.0520 286911. 9999.5991 -0.000857 0.000 6.039E+10-332.9626 15363. 0.000 5.000 0.0500 309972. 9210.7795 -0.000846 0.000 6.034E+10-324.3871 15580. 0.000 5.200 0.0480 331164. 8442.7503 -0.000833 0.000 6.028E+10-315.6373 15796. 0.000 5.400 0.0460 350537. 7695.9035 -0.000819 0.000 6.024E+10-306.7350 16013. 0.000 5.600 0.0440 368143. 6970.5796 -0.000805 0.000 6.020E+10-297.7016 16230. 0.000 5.800 0.0421 384034. 6267.0686 -0.000790 0.000 6.016E+10-288.5576 16446. 0.000 6.000 0.0402 398263. 5585.6114 -0.000774 0.000 6.012E+10-279.3234 16663. 0.000 6.200 0.0384 410882. 4926.4008 -0.000758 0.000 6.009E+10-270.0187 16879. 0.000 6.400 0.0366 421946. 4289.5832 -0.000742 0.000 6.006E+10-260.6626 17096. 0.000 6.600 0.0348 431508. 3675.2598 -0.000724 0.000 6.004E+10-251.2736 17313. 0.000 6.800 0.0331 439622. 3083.4883 -0.000707 0.000 6.002E+10-241.8693 17529. 0.000 7.000 0.0314 446343. 2514.2847 -0.000689 0.000 6.000E+10-232.4670 17746. 0.000 7.200 0.0298 451724. 1967.6250 -0.000671 0.000 5.999E+10-223.0828 17962. 0.000 7.400 0.0282 455820. 1443.4469 -0.000653 0.000 5.998E+10-213.7323 18179. 0.000 7.600 0.0267 458684. 941.6515 -0.000635 0.000 5.997E+10-204.4305 18396. 0.000 7.800 0.0252 460370. 462.1052 -0.000617 0.000 5.997E+10-195.1913 18612. 0.000 8.000 0.0237 460931. 4.6421 -0.000598 0.000 5.997E+10-186.0280 18829. 0.000 8.200 0.0223 460421. -430.9350 -0.000580 0.000 5.997E+10-176.9529 19045. 0.000 8.400 0.0209 458891. -844.8517 -0.000561 0.000 5.997E+10-167.9777 19262. 0.000 8.600 0.0196 456393. -1237.3605 -0.000543 0.000 5.998E+10-159.1130 19479. 0.000 8.800 0.0183 452978. -1608.7389 -0.000525 0.000 5.999E+10-150.3689 19695. 0.000 9.000 0.0171 448696. -1948.8337 -0.000507 0.000 6.000E+10-133.0434 18688. 0.000 9.200 0.0159 443647. -2245.0646 -0.000489 0.000 6.001E+10-113.8156 17189. 0.000 9.400 0.0147 437943. -2509.6457 -0.000471 0.000 6.002E+10-106.6687 17369. 0.000 9.600 0.0136 431624. -2757.2359 -0.000454 0.000 6.004E+10-99.6564 17549. 0.000

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existing phase1 81.lp6o 9.800 0.0126 424730. -2988.1643 -0.000437 0.000 6.005E+10-92.7839 17728. 0.000 10.000 0.0115 417302. -3202.7713 -0.000420 0.000 6.007E+10-86.0553 17908. 0.000 10.200 0.0105 409377. -3401.4069 -0.000403 0.000 6.009E+10-79.4744 18088. 0.000 10.400 0.009597 400994. -3584.4292 -0.000387 0.000 6.011E+10-73.0442 18267. 0.000 10.600 0.008687 392190. -3752.2029 -0.000371 0.000 6.013E+10-66.7673 18447. 0.000 10.800 0.007814 383001. -3905.0985 -0.000356 0.000 6.016E+10-60.6457 18627. 0.000 11.000 0.006978 373463. -4043.4901 -0.000341 0.000 6.019E+10-54.6807 18807. 0.000 11.200 0.006178 363609. -4167.7549 -0.000326 0.000 6.021E+10-48.8733 18986. 0.000 11.400 0.005413 353473. -4278.2716 -0.000312 0.000 6.023E+10-43.2239 19166. 0.000 11.600 0.004681 343088. -4375.4191 -0.000298 0.000 6.025E+10-37.7324 19346. 0.000 11.800 0.003982 332486. -4459.5757 -0.000285 0.000 6.028E+10-32.3981 19525. 0.000 12.000 0.003315 321696. -4531.1176 -0.000272 0.000 6.031E+10-27.2201 19705. 0.000 12.200 0.002679 310749. -4590.4178 -0.000259 0.000 6.034E+10-22.1968 19885. 0.000 12.400 0.002072 299674. -4637.8453 -0.000247 0.000 6.037E+10-17.3261 20064. 0.000 12.600 0.001494 288499. -4673.7637 -0.000235 0.000 6.039E+10-12.6059 20244. 0.000 12.800 0.000944 277252. -4698.5306 -0.000224 0.000 6.041E+10-8.0332 20424. 0.000 13.000 0.000420 265957. -4712.4966 -0.000213 0.000 6.044E+10-3.6051 20604. 0.000 13.200 -7.876E-05 254642. -4716.0043 -0.000203 0.000 6.046E+100.6820 20783. 0.000 13.400 -0.000553 243330. -4709.3875 -0.000193 0.000 6.049E+104.8320 20963. 0.000 13.600 -0.001004 232046. -4692.9706 -0.000183 0.000 6.053E+108.8488 21143. 0.000 13.800 -0.001434 220813. -4667.0675 -0.000174 0.000 6.055E+1012.7371 21322. 0.000 14.000 -0.001842 209653. -4631.9813 -0.000166 0.000 6.057E+1016.5014 21502. 0.000 14.200 -0.002230 198587. -4588.0035 -0.000158 0.000 6.059E+1020.1468 21682. 0.000 14.400 -0.002599 187638. -4535.4133 -0.000150 0.000 6.062E+1023.6783 21862. 0.000 14.600 -0.002951 176824. -4474.4776 -0.000143 0.000 6.064E+1027.1015 22041. 0.000 14.800 -0.003286 166167. -4405.4498 -0.000136 0.000 6.067E+1030.4217 22221. 0.000 15.000 -0.003605 155685. -4328.5699 -0.000130 0.000 6.070E+1033.6449 22401. 0.000 15.200 -0.003909 145396. -4244.0639 -0.000124 0.000 6.072E+1036.7768 22580. 0.000 15.400 -0.004199 135319. -4152.1435 -0.000118 0.000 6.074E+1039.8235 22760. 0.000 15.600 -0.004477 125472. -4053.0061 -0.000113 0.000 6.075E+1042.7910 22940. 0.000 15.800 -0.004743 115870. -3946.8343 -0.000108 0.000 6.076E+1045.6855 23120. 0.000 16.000 -0.004997 106532. -3833.7960 -0.000104 0.000 6.078E+10

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existing phase1 81.lp6o48.5131 23299. 0.000 16.200 -0.005242 97473. -3714.0440 -9.999E-05 0.000 6.080E+1051.2802 23479. 0.000 16.400 -0.005477 88709. -3587.7165 -9.632E-05 0.000 6.083E+1053.9928 23659. 0.000 16.600 -0.005704 80257. -3454.9365 -9.298E-05 0.000 6.085E+1056.6572 23838. 0.000 16.800 -0.005924 72130. -3315.8122 -8.998E-05 0.000 6.087E+1059.2796 24018. 0.000 17.000 -0.006136 64345. -3170.4374 -8.729E-05 0.000 6.087E+1061.8661 24198. 0.000 17.200 -0.006342 56916. -3018.8911 -8.490E-05 0.000 6.087E+1064.4225 24377. 0.000 17.400 -0.006544 49858. -2861.2385 -8.279E-05 0.000 6.087E+1066.9547 24557. 0.000 17.600 -0.006740 43186. -2697.5308 -8.096E-05 0.000 6.087E+1069.4684 24737. 0.000 17.800 -0.006932 36914. -2527.8058 -7.938E-05 0.000 6.087E+1071.9691 24917. 0.000 18.000 -0.007121 31057. -2352.0884 -7.804E-05 0.000 6.087E+1074.4621 25096. 0.000 18.200 -0.007307 25628. -2170.3911 -7.692E-05 0.000 6.087E+1076.9523 25276. 0.000 18.400 -0.007490 20642. -1982.7147 -7.601E-05 0.000 6.087E+1079.4447 25456. 0.000 18.600 -0.007672 16114. -1789.0487 -7.529E-05 0.000 6.087E+1081.9437 25635. 0.000 18.800 -0.007852 12059. -1589.3722 -7.473E-05 0.000 6.087E+1084.4534 25815. 0.000 19.000 -0.008030 8489.0631 -1370.6627 -7.433E-05 0.000 6.087E+1097.8045 29231. 0.000 19.200 -0.008208 5482.9294 -1120.8029 -7.405E-05 0.000 6.087E+10110.4120 32283. 0.000 19.400 -0.008386 3112.7636 -852.0414 -7.388E-05 0.000 6.087E+10113.5559 32500. 0.000 19.600 -0.008563 1396.6767 -575.7010 -7.379E-05 0.000 6.087E+10116.7278 32716. 0.000 19.800 -0.008740 352.9406 -291.7119 -7.376E-05 0.000 6.087E+10119.9298 32933. 0.000 20.000 -0.008917 0.000 0.000 -7.375E-05 0.000 6.087E+10123.1634 16575. 0.000

* This analysis makes computations of pile response using nonlinear moment-curvaturerelationships. The above values of total stress are computed for combined axial and bending stress in elastic sections and do not equal actual stresses in concrete and steel in the range of nonlinear bending.

Output Summary for Load Case No. 9:

Pile-head deflection = 0.1000000 inchesComputed slope at pile head = -0.0000146 radiansMaximum bending moment = -717015. inch-lbsMaximum shear force = 24086. lbsDepth of maximum bending moment = 0.000000 inches below pile headDepth of maximum shear force = 0.000000 inches below pile headNumber of iterations = 27Number of zero deflection points = 1

Page 49

existing phase1 81.lp6o-------------------------------------------------------------------------------- Computed Values of Pile Loading and Deflection for Lateral Loading for Load Case Number 10--------------------------------------------------------------------------------

Pile-head conditions are Displacement and Pile-head Rotation (Loading Type 5)Displacement of pile head = 0.200000 inchesRotation of pile head = 0.000E+00 radiansAxial load on pile head = 10000.000 lbs

Depth Deflect. Bending Shear Slope Total Bending Soil Res. Soil Spr. Distrib. X y Moment Force S Stress Stiffness p Es*h Lat. Load feet inches in-lbs lbs radians psi* lb-in^2 lb/in lb/inch lb/inch ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- 0.00 0.2000 -872450. 36089. 0.000 0.000 2.023E+09-454.9597 2729.7579 0.000 0.200 0.1988 -787154. 34980. -0.000984 0.000 2.023E+09-462.1822 5580.8384 0.000 0.400 0.1953 -704498. 33869. -0.001626 0.000 4.844E+09-463.9553 5702.1610 0.000 0.600 0.1910 -624506. 32756. -0.001945 0.000 5.177E+09-463.3434 5823.4836 0.000 0.800 0.1859 -547176. 31647. -0.002101 0.000 5.975E+10-460.5738 5944.8062 0.000 1.000 0.1809 -472498. 30546. -0.002121 0.000 5.993E+10-457.1638 6066.1287 0.000 1.200 0.1758 -400453. 29454. -0.002139 0.000 6.011E+10-453.1243 6187.4513 0.000 1.400 0.1706 -331018. 28372. -0.002153 0.000 6.028E+10-448.4670 6308.7739 0.000 1.600 0.1654 -264165. 27302. -0.002165 0.000 6.044E+10-443.2041 6430.0965 0.000 1.800 0.1602 -199865. 26245. -0.002174 0.000 6.059E+10-437.3485 6551.4190 0.000 2.000 0.1550 -138085. 25203. -0.002181 0.000 6.073E+10-430.9134 6672.7416 0.000 2.200 0.1497 -78786. 24177. -0.002185 0.000 6.086E+10-423.9127 6794.0642 0.000 2.400 0.1445 -21928. 23169. -0.002187 0.000 6.087E+10-416.3607 6915.3868 0.000 2.600 0.1392 32531. 22179. -0.002187 0.000 6.087E+10-408.2721 7036.7093 0.000 2.800 0.1340 84638. 21210. -0.002185 0.000 6.084E+10-399.6618 7158.0319 0.000 3.000 0.1288 134443. 20262. -0.002180 0.000 6.074E+10-390.5454 7279.3545 0.000 3.200 0.1235 181999. 19336. -0.002174 0.000 6.063E+10-380.9385 7400.6771 0.000 3.400 0.1183 227360. 18434. -0.002166 0.000 6.054E+10-370.8575 7521.9996 0.000 3.600 0.1131 270585. 17556. -0.002156 0.000 6.043E+10-360.3187 7643.3222 0.000 3.800 0.1080 311734. 16705. -0.002144 0.000 6.033E+10-349.3389 7764.6448 0.000 4.000 0.1028 350871. 15724. -0.002131 0.000 6.023E+10-468.3776 10930. 0.000 4.200 0.0977 387310. 14442. -0.002117 0.000 6.015E+10-599.2573 14713. 0.000 4.400 0.0927 420296. 13031. -0.002100 0.000 6.006E+10

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existing phase1 81.lp6o-576.5941 14930. 0.000 4.600 0.0877 449961. 11675. -0.002083 0.000 6.000E+10-553.2717 15147. 0.000 4.800 0.0827 476438. 10376. -0.002064 0.000 5.992E+10-529.3196 15363. 0.000 5.000 0.0778 499866. 9135.4829 -0.002045 0.000 5.987E+10-504.7663 15580. 0.000 5.200 0.0729 520387. 7954.1962 -0.002024 0.000 5.982E+10-479.6393 15796. 0.000 5.400 0.0680 538144. 6833.8708 -0.002003 0.000 5.977E+10-453.9652 16013. 0.000 5.600 0.0633 553285. 5775.7895 -0.001981 0.000 5.973E+10-427.7692 16230. 0.000 5.800 0.0585 565963. 4781.1754 -0.001959 0.000 5.970E+10-401.0758 16446. 0.000 6.000 0.0539 576329. 3851.1948 -0.001936 0.000 5.967E+10-373.9080 16663. 0.000 6.200 0.0492 584541. 2986.9597 -0.001912 0.000 5.813E+10-346.2879 16879. 0.000 6.400 0.0447 590758. 2189.5183 -0.001868 0.000 2.183E+10-318.2467 17096. 0.000 6.600 0.0403 595141. 1459.0140 -0.001770 0.000 1.100E+10-290.5068 17313. 0.000 6.800 0.0362 597847. 793.3079 -0.001606 0.000 7.225E+09-264.2483 17529. 0.000 7.000 0.0326 599026. 187.2796 -0.001388 0.000 6.033E+09-240.7753 17746. 0.000 7.200 0.0295 598812. -366.7663 -0.001154 0.000 6.273E+09-220.9297 17962. 0.000 7.400 0.0270 597321. -877.5215 -0.000950 0.000 7.981E+09-204.6997 18179. 0.000 7.600 0.0250 594646. -1352.7493 -0.000799 0.000 1.171E+10-191.3235 18396. 0.000 7.800 0.0232 590866. -1798.1501 -0.000703 0.000 2.049E+10-179.8438 18612. 0.000 8.000 0.0216 586048. -2217.1797 -0.000652 0.000 4.274E+10-169.3475 18829. 0.000 8.200 0.0201 580255. -2611.4226 -0.000624 0.000 5.966E+10-159.1883 19045. 0.000 8.400 0.0186 573543. -2981.4925 -0.000601 0.000 5.968E+10-149.2033 19262. 0.000 8.600 0.0172 565972. -3327.8193 -0.000578 0.000 5.970E+10-139.4023 19479. 0.000 8.800 0.0158 557598. -3650.8552 -0.000555 0.000 5.972E+10-129.7942 19695. 0.000 9.000 0.0145 548475. -3942.1950 -0.000533 0.000 5.974E+10-112.9889 18688. 0.000 9.200 0.0133 538701. -4191.7227 -0.000511 0.000 5.977E+10-94.9509 17189. 0.000 9.400 0.0121 528379. -4410.3650 -0.000490 0.000 5.980E+10-87.2510 17369. 0.000 9.600 0.0109 517554. -4610.7581 -0.000469 0.000 5.983E+10-79.7433 17549. 0.000 9.800 0.009806 506270. -4793.3676 -0.000448 0.000 5.985E+10-72.4314 17728. 0.000 10.000 0.008754 494568. -4958.6673 -0.000428 0.000 5.988E+10-65.3183 17908. 0.000 10.200 0.007750 482489. -5107.1367 -0.000409 0.000 5.991E+10-58.4063 18088. 0.000 10.400 0.006792 470073. -5239.2606 -0.000390 0.000 5.994E+10-51.6969 18267. 0.000 10.600 0.005879 457359. -5355.5265 -0.000371 0.000 5.998E+10-45.1914 18447. 0.000

Page 51

existing phase1 81.lp6o 10.800 0.005011 444384. -5456.4243 -0.000353 0.000 6.001E+10-38.8901 18627. 0.000 11.000 0.004185 431185. -5542.4439 -0.000336 0.000 6.004E+10-32.7929 18807. 0.000 11.200 0.003400 417797. -5614.0747 -0.000319 0.000 6.007E+10-26.8994 18986. 0.000 11.400 0.002656 404253. -5671.8038 -0.000302 0.000 6.010E+10-21.2082 19166. 0.000 11.600 0.001950 390587. -5716.1151 -0.000286 0.000 6.014E+10-15.7179 19346. 0.000 11.800 0.001282 376829. -5747.4879 -0.000271 0.000 6.018E+10-10.4262 19525. 0.000 12.000 0.000649 363012. -5766.3959 -0.000256 0.000 6.021E+10-5.3305 19705. 0.000 12.200 5.164E-05 349163. -5773.3060 -0.000242 0.000 6.024E+10-0.4279 19885. 0.000 12.400 -0.000513 335311. -5768.6774 -0.000228 0.000 6.027E+104.2851 20064. 0.000 12.600 -0.001045 321484. -5752.9605 -0.000215 0.000 6.031E+108.8123 20244. 0.000 12.800 -0.001546 307708. -5726.5964 -0.000203 0.000 6.035E+1013.1578 20424. 0.000 13.000 -0.002018 294006. -5690.0155 -0.000191 0.000 6.038E+1017.3263 20604. 0.000 13.200 -0.002462 280405. -5643.6367 -0.000179 0.000 6.040E+1021.3226 20783. 0.000 13.400 -0.002880 266925. -5587.8672 -0.000169 0.000 6.043E+1025.1519 20963. 0.000 13.600 -0.003271 253591. -5523.1015 -0.000158 0.000 6.047E+1028.8195 21143. 0.000 13.800 -0.003639 240422. -5449.7205 -0.000148 0.000 6.050E+1032.3312 21322. 0.000 14.000 -0.003984 227439. -5368.0915 -0.000139 0.000 6.054E+1035.6930 21502. 0.000 14.200 -0.004307 214662. -5278.5670 -0.000130 0.000 6.056E+1038.9108 21682. 0.000 14.400 -0.004610 202109. -5181.4847 -0.000122 0.000 6.059E+1041.9911 21862. 0.000 14.600 -0.004893 189797. -5077.1671 -0.000114 0.000 6.061E+1044.9402 22041. 0.000 14.800 -0.005159 177744. -4965.9210 -0.000107 0.000 6.064E+1047.7649 22221. 0.000 15.000 -0.005408 165965. -4848.0372 -0.000100 0.000 6.067E+1050.4717 22401. 0.000 15.200 -0.005640 154478. -4723.7903 -9.397E-05 0.000 6.071E+1053.0674 22580. 0.000 15.400 -0.005859 143296. -4593.4384 -8.809E-05 0.000 6.073E+1055.5591 22760. 0.000 15.600 -0.006063 132434. -4457.2232 -8.264E-05 0.000 6.074E+1057.9535 22940. 0.000 15.800 -0.006255 121905. -4315.3698 -7.762E-05 0.000 6.075E+1060.2576 23120. 0.000 16.000 -0.006436 111724. -4168.0867 -7.300E-05 0.000 6.077E+1062.4783 23299. 0.000 16.200 -0.006606 101902. -4015.5659 -6.878E-05 0.000 6.079E+1064.6224 23479. 0.000 16.400 -0.006766 92452. -3857.9829 -6.495E-05 0.000 6.082E+1066.6967 23659. 0.000 16.600 -0.006917 83387. -3695.4971 -6.148E-05 0.000 6.084E+1068.7081 23838. 0.000 16.800 -0.007061 74717. -3528.2515 -5.836E-05 0.000 6.087E+1070.6632 24018. 0.000 17.000 -0.007198 66454. -3356.3735 -5.558E-05 0.000 6.087E+10

Page 52

existing phase1 81.lp6o72.5685 24198. 0.000 17.200 -0.007328 58609. -3179.9749 -5.311E-05 0.000 6.087E+1074.4303 24377. 0.000 17.400 -0.007452 51192. -2999.1525 -5.095E-05 0.000 6.087E+1076.2550 24557. 0.000 17.600 -0.007572 44215. -2813.9885 -4.907E-05 0.000 6.087E+1078.0483 24737. 0.000 17.800 -0.007688 37688. -2624.5511 -4.745E-05 0.000 6.087E+1079.8162 24917. 0.000 18.000 -0.007800 31620. -2430.8947 -4.609E-05 0.000 6.087E+1081.5641 25096. 0.000 18.200 -0.007909 26022. -2233.0610 -4.495E-05 0.000 6.087E+1083.2973 25276. 0.000 18.400 -0.008016 20903. -2031.0794 -4.402E-05 0.000 6.087E+1085.0207 25456. 0.000 18.600 -0.008121 16275. -1824.9678 -4.329E-05 0.000 6.087E+1086.7389 25635. 0.000 18.800 -0.008224 12145. -1614.7335 -4.273E-05 0.000 6.087E+1088.4563 25815. 0.000 19.000 -0.008326 8525.8484 -1386.9040 -4.232E-05 0.000 6.087E+10101.4016 29231. 0.000 19.200 -0.008427 5490.3271 -1129.2001 -4.205E-05 0.000 6.087E+10113.3516 32283. 0.000 19.400 -0.008527 3107.7061 -854.6079 -4.188E-05 0.000 6.087E+10115.4752 32500. 0.000 19.600 -0.008628 1390.2191 -574.9023 -4.179E-05 0.000 6.087E+10117.6129 32716. 0.000 19.800 -0.008728 350.1811 -290.0465 -4.176E-05 0.000 6.087E+10119.7669 32933. 0.000 20.000 -0.008828 0.000 0.000 -4.175E-05 0.000 6.087E+10121.9385 16575. 0.000

* This analysis makes computations of pile response using nonlinear moment-curvaturerelationships. The above values of total stress are computed for combined axial and bending stress in elastic sections and do not equal actual stresses in concrete and steel in the range of nonlinear bending.

Output Summary for Load Case No. 10:

Pile-head deflection = 0.2000000 inchesComputed slope at pile head = -0.0000506 radiansMaximum bending moment = -872450. inch-lbsMaximum shear force = 36089. lbsDepth of maximum bending moment = 0.000000 inches below pile headDepth of maximum shear force = 0.000000 inches below pile headNumber of iterations = 93Number of zero deflection points = 1

-------------------------------------------------------------------------------- Computed Values of Pile Loading and Deflection for Lateral Loading for Load Case Number 11--------------------------------------------------------------------------------

Pile-head conditions are Displacement and Pile-head Rotation (Loading Type 5)Displacement of pile head = 0.300000 inchesRotation of pile head = 0.000E+00 radiansAxial load on pile head = 10000.000 lbs

Page 53

existing phase1 81.lp6o Depth Deflect. Bending Shear Slope Total Bending Soil Res. Soil Spr. Distrib. X y Moment Force S Stress Stiffness p Es*h Lat. Load feet inches in-lbs lbs radians psi* lb-in^2 lb/in lb/inch lb/inch ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- 0.00 0.3000 -901558. 43364. 0.000 0.000 9.905E+08-682.4395 2729.7579 0.000 0.200 0.2974 -799449. 41705. -0.002061 0.000 9.905E+08-691.5094 5580.8384 0.000 0.400 0.2901 -701277. 40048. -0.003202 0.000 4.876E+09-689.2693 5702.1610 0.000 0.600 0.2820 -607066. 38399. -0.003514 0.000 5.202E+09-684.2842 5823.4836 0.000 0.800 0.2732 -516791. 36766. -0.003665 0.000 5.983E+10-676.8155 5944.8062 0.000 1.000 0.2644 -430413. 35152. -0.003684 0.000 6.004E+10-668.3343 6066.1287 0.000 1.200 0.2556 -347885. 33559. -0.003699 0.000 6.024E+10-658.8549 6187.4513 0.000 1.400 0.2467 -269151. 31991. -0.003712 0.000 6.043E+10-648.3921 6308.7739 0.000 1.600 0.2377 -194151. 30448. -0.003721 0.000 6.060E+10-636.9613 6430.0965 0.000 1.800 0.2288 -122821. 28934. -0.003727 0.000 6.075E+10-624.5783 6551.4190 0.000 2.000 0.2199 -55088. 27451. -0.003731 0.000 6.087E+10-611.2591 6672.7416 0.000 2.200 0.2109 9124.7591 26001. -0.003731 0.000 6.087E+10-597.0202 6794.0642 0.000 2.400 0.2019 69898. 24587. -0.003730 0.000 6.087E+10-581.8784 6915.3868 0.000 2.600 0.1930 127320. 23209. -0.003726 0.000 6.075E+10-565.8506 7036.7093 0.000 2.800 0.1841 181483. 21872. -0.003720 0.000 6.063E+10-548.9542 7158.0319 0.000 3.000 0.1751 232483. 20576. -0.003712 0.000 6.053E+10-531.2065 7279.3545 0.000 3.200 0.1662 280423. 19323. -0.003701 0.000 6.040E+10-512.6253 7400.6771 0.000 3.400 0.1574 325410. 18116. -0.003689 0.000 6.030E+10-493.2285 7521.9996 0.000 3.600 0.1485 367557. 16956. -0.003676 0.000 6.020E+10-473.0338 7643.3222 0.000 3.800 0.1397 406977. 15846. -0.003660 0.000 6.010E+10-452.0593 7764.6448 0.000 4.000 0.1310 443794. 14588. -0.003643 0.000 6.001E+10-596.4269 10930. 0.000 4.200 0.1222 477175. 12973. -0.003625 0.000 5.992E+10-749.4151 14713. 0.000 4.400 0.1136 506239. 11226. -0.003605 0.000 5.985E+10-706.4724 14930. 0.000 4.600 0.1049 531233. 9583.5065 -0.003584 0.000 5.979E+10-662.2711 15147. 0.000 4.800 0.0964 552412. 8048.5730 -0.003562 0.000 5.973E+10-616.8401 15363. 0.000 5.000 0.0878 570037. 6624.1166 -0.003540 0.000 5.969E+10-570.2069 15580. 0.000 5.200 0.0794 584377. 5312.9916 -0.003514 0.000 4.887E+10-522.3972 15796. 0.000 5.400 0.0710 595708. 4117.8926 -0.003444 0.000 1.293E+10

Page 54

existing phase1 81.lp6o-473.5186 16013. 0.000 5.600 0.0628 604309. 3039.7684 -0.003250 0.000 5.210E+09-424.9183 16230. 0.000 5.800 0.0554 610455. 2074.5526 -0.002970 0.000 5.198E+09-379.4283 16446. 0.000 6.000 0.0486 614409. 1214.4938 -0.002687 0.000 5.192E+09-337.2874 16663. 0.000 6.200 0.0425 616414. 451.2910 -0.002402 0.000 5.189E+09-298.7149 16879. 0.000 6.400 0.0370 616691. -223.8637 -0.002117 0.000 5.189E+09-263.9140 17096. 0.000 6.600 0.0323 615441. -820.2472 -0.001832 0.000 5.191E+09-233.0723 17313. 0.000 6.800 0.0283 612841. -1347.5702 -0.001548 0.000 5.194E+09-206.3635 17529. 0.000 7.000 0.0249 609047. -1815.9434 -0.001266 0.000 5.200E+09-183.9475 17746. 0.000 7.200 0.0222 604186. -2235.8459 -0.000987 0.000 5.210E+09-165.9713 17962. 0.000 7.400 0.0201 598362. -2618.0915 -0.000763 0.000 8.539E+09-152.5667 18179. 0.000 7.600 0.0185 591655. -2971.4381 -0.000642 0.000 1.883E+10-141.8888 18396. 0.000 7.800 0.0171 584130. -3300.4884 -0.000589 0.000 4.668E+10-132.3199 18612. 0.000 8.000 0.0157 575841. -3606.9382 -0.000562 0.000 5.968E+10-123.0549 18829. 0.000 8.200 0.0144 566844. -3891.3830 -0.000539 0.000 5.970E+10-113.9824 19045. 0.000 8.400 0.0131 557189. -4154.2943 -0.000517 0.000 5.972E+10-105.1103 19262. 0.000 8.600 0.0119 546928. -4396.1616 -0.000495 0.000 5.975E+10-96.4457 19479. 0.000 8.800 0.0107 536111. -4617.4902 -0.000473 0.000 5.978E+10-87.9948 19695. 0.000 9.000 0.009614 524786. -4812.9178 -0.000451 0.000 5.981E+10-74.8615 18688. 0.000 9.200 0.008556 513030. -4976.2837 -0.000431 0.000 5.984E+10-61.2768 17189. 0.000 9.400 0.007547 500921. -5115.3551 -0.000410 0.000 5.986E+10-54.6160 17369. 0.000 9.600 0.006586 488496. -5238.6820 -0.000391 0.000 5.989E+10-48.1565 17549. 0.000 9.800 0.005672 475794. -5346.7501 -0.000371 0.000 5.993E+10-41.9002 17728. 0.000 10.000 0.004804 462850. -5440.0481 -0.000352 0.000 5.996E+10-35.8482 17908. 0.000 10.200 0.003981 449699. -5519.0677 -0.000334 0.000 6.000E+10-30.0014 18088. 0.000 10.400 0.003200 436374. -5584.3013 -0.000316 0.000 6.003E+10-24.3599 18267. 0.000 10.600 0.002462 422909. -5636.2411 -0.000299 0.000 6.006E+10-18.9233 18447. 0.000 10.800 0.001764 409335. -5675.3783 -0.000283 0.000 6.009E+10-13.6910 18627. 0.000 11.000 0.001105 395681. -5702.2013 -0.000267 0.000 6.013E+10-8.6616 18807. 0.000 11.200 0.000485 381977. -5717.1953 -0.000251 0.000 6.016E+10-3.8334 18986. 0.000 11.400 -9.964E-05 368251. -5720.8405 -0.000236 0.000 6.020E+100.7957 19166. 0.000 11.600 -0.000649 354528. -5713.6117 -0.000222 0.000 6.023E+105.2283 19346. 0.000

Page 55

existing phase1 81.lp6o 11.800 -0.001164 340836. -5695.9772 -0.000208 0.000 6.026E+109.4672 19525. 0.000 12.000 -0.001646 327198. -5668.3978 -0.000195 0.000 6.029E+1013.5157 19705. 0.000 12.200 -0.002097 313637. -5631.3259 -0.000182 0.000 6.033E+1017.3775 19885. 0.000 12.400 -0.002519 300176. -5585.2049 -0.000170 0.000 6.037E+1021.0566 20064. 0.000 12.600 -0.002911 286836. -5530.4685 -0.000158 0.000 6.039E+1024.5571 20244. 0.000 12.800 -0.003277 273637. -5467.5397 -0.000147 0.000 6.042E+1027.8836 20424. 0.000 13.000 -0.003616 260599. -5396.8303 -0.000136 0.000 6.045E+1031.0409 20604. 0.000 13.200 -0.003930 247739. -5318.7405 -0.000126 0.000 6.048E+1034.0339 20783. 0.000 13.400 -0.004221 235075. -5233.6583 -0.000116 0.000 6.052E+1036.8679 20963. 0.000 13.600 -0.004489 222623. -5141.9587 -0.000107 0.000 6.055E+1039.5484 21143. 0.000 13.800 -0.004737 210399. -5044.0034 -9.884E-05 0.000 6.057E+1042.0809 21322. 0.000 14.000 -0.004964 198417. -4940.1408 -9.074E-05 0.000 6.059E+1044.4712 21502. 0.000 14.200 -0.005172 186690. -4830.7052 -8.312E-05 0.000 6.062E+1046.7251 21682. 0.000 14.400 -0.005363 175233. -4716.0166 -7.595E-05 0.000 6.065E+1048.8487 21862. 0.000 14.600 -0.005537 164057. -4596.3807 -6.924E-05 0.000 6.068E+1050.8479 22041. 0.000 14.800 -0.005695 153174. -4472.0884 -6.297E-05 0.000 6.071E+1052.7290 22221. 0.000 15.000 -0.005839 142594. -4343.4157 -5.712E-05 0.000 6.073E+1054.4982 22401. 0.000 15.200 -0.005969 132328. -4210.6239 -5.169E-05 0.000 6.074E+1056.1617 22580. 0.000 15.400 -0.006087 122386. -4073.9592 -4.666E-05 0.000 6.075E+1057.7256 22760. 0.000 15.600 -0.006193 112775. -3933.6528 -4.202E-05 0.000 6.077E+1059.1964 22940. 0.000 15.800 -0.006289 103506. -3789.9211 -3.775E-05 0.000 6.079E+1060.5800 23120. 0.000 16.000 -0.006374 94586. -3642.9658 -3.384E-05 0.000 6.081E+1061.8827 23299. 0.000 16.200 -0.006451 86022. -3492.9737 -3.027E-05 0.000 6.083E+1063.1107 23479. 0.000 16.400 -0.006520 77821. -3340.1172 -2.704E-05 0.000 6.086E+1064.2698 23659. 0.000 16.600 -0.006581 69990. -3184.5542 -2.413E-05 0.000 6.087E+1065.3660 23838. 0.000 16.800 -0.006636 62536. -3026.4288 -2.152E-05 0.000 6.087E+1066.4052 24018. 0.000 17.000 -0.006684 55464. -2865.8712 -1.919E-05 0.000 6.087E+1067.3928 24198. 0.000 17.200 -0.006728 48781. -2702.9985 -1.713E-05 0.000 6.087E+1068.3344 24377. 0.000 17.400 -0.006766 42491. -2537.9148 -1.533E-05 0.000 6.087E+1069.2353 24557. 0.000 17.600 -0.006801 36600. -2370.7118 -1.378E-05 0.000 6.087E+1070.1006 24737. 0.000 17.800 -0.006833 31112. -2201.4690 -1.244E-05 0.000 6.087E+1070.9351 24917. 0.000 18.000 -0.006861 26033. -2030.2546 -1.131E-05 0.000 6.087E+10

Page 56

existing phase1 81.lp6o71.7435 25096. 0.000 18.200 -0.006887 21367. -1857.1261 -1.038E-05 0.000 6.087E+1072.5302 25276. 0.000 18.400 -0.006911 17119. -1682.1305 -9.621E-06 0.000 6.087E+1073.2994 25456. 0.000 18.600 -0.006933 13294. -1505.3054 -9.021E-06 0.000 6.087E+1074.0548 25635. 0.000 18.800 -0.006954 9894.4040 -1326.6795 -8.564E-06 0.000 6.087E+1074.8001 25815. 0.000 19.000 -0.006974 6925.9984 -1134.9900 -8.232E-06 0.000 6.087E+1084.9411 29231. 0.000 19.200 -0.006994 4446.8472 -920.1734 -8.008E-06 0.000 6.087E+1094.0727 32283. 0.000 19.400 -0.007013 2509.5504 -693.3327 -7.871E-06 0.000 6.087E+1094.9613 32500. 0.000 19.600 -0.007031 1119.2280 -464.3591 -7.799E-06 0.000 6.087E+1095.8500 32716. 0.000 19.800 -0.007050 281.0008 -233.2502 -7.772E-06 0.000 6.087E+1096.7407 32933. 0.000 20.000 -0.007069 0.000 0.000 -7.766E-06 0.000 6.087E+1097.6344 16575. 0.000

* This analysis makes computations of pile response using nonlinear moment-curvaturerelationships. The above values of total stress are computed for combined axial and bending stress in elastic sections and do not equal actual stresses in concrete and steel in the range of nonlinear bending.

Output Summary for Load Case No. 11:

Pile-head deflection = 0.3000000 inchesComputed slope at pile head = -0.0001237 radiansMaximum bending moment = -901558. inch-lbsMaximum shear force = 43364. lbsDepth of maximum bending moment = 0.000000 inches below pile headDepth of maximum shear force = 0.000000 inches below pile headNumber of iterations = 70Number of zero deflection points = 1

-------------------------------------------------------------------------------- Computed Values of Pile Loading and Deflection for Lateral Loading for Load Case Number 12--------------------------------------------------------------------------------

Pile-head conditions are Displacement and Pile-head Rotation (Loading Type 5)Displacement of pile head = 0.500000 inchesRotation of pile head = 0.000E+00 radiansAxial load on pile head = 10000.000 lbs

Depth Deflect. Bending Shear Slope Total Bending Soil Res. Soil Spr. Distrib. X y Moment Force S Stress Stiffness p Es*h Lat. Load feet inches in-lbs lbs radians psi* lb-in^2 lb/in lb/inch lb/inch ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- 0.00 0.5000 -905605. 56035. 0.000 0.000 4.309E+08 -1062.7069 2550.4966 0.000

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existing phase1 81.lp6o 0.200 0.4939 -774202. 53417. -0.004678 0.000 4.309E+08 -1090.6476 5299.2640 0.000 0.400 0.4775 -648977. 50785. -0.006986 0.000 5.144E+09 -1103.0988 5543.8633 0.000 0.600 0.4604 -530099. 48126. -0.007148 0.000 5.979E+10 -1112.8590 5801.0008 0.000 0.800 0.4432 -417630. 45473. -0.007167 0.000 6.007E+10 -1097.8894 5944.8062 0.000 1.000 0.4260 -311485. 42863. -0.007182 0.000 6.033E+10 -1076.7686 6066.1287 0.000 1.200 0.4088 -211542. 40307. -0.007192 0.000 6.057E+10 -1053.8299 6187.4513 0.000 1.400 0.3915 -117668. 37807. -0.007198 0.000 6.076E+10 -1029.0944 6308.7739 0.000 1.600 0.3742 -29722. 35369. -0.007201 0.000 6.087E+10 -1002.5828 6430.0965 0.000 1.800 0.3569 52449. 32997. -0.007201 0.000 6.087E+10-974.3163 6551.4190 0.000 2.000 0.3396 129008. 30694. -0.007197 0.000 6.074E+10-944.3161 6672.7416 0.000 2.200 0.3224 200127. 28466. -0.007191 0.000 6.059E+10-912.6035 6794.0642 0.000 2.400 0.3051 265990. 26316. -0.007182 0.000 6.044E+10-879.1999 6915.3868 0.000 2.600 0.2879 326789. 24248. -0.007170 0.000 6.029E+10-844.1268 7036.7093 0.000 2.800 0.2707 382724. 22266. -0.007156 0.000 6.016E+10-807.4055 7158.0319 0.000 3.000 0.2536 434009. 20374. -0.007139 0.000 6.003E+10-769.0572 7279.3545 0.000 3.200 0.2364 480864. 18577. -0.007121 0.000 5.991E+10-729.1029 7400.6771 0.000 3.400 0.2194 523519. 16877. -0.007101 0.000 5.981E+10-687.5633 7521.9996 0.000 3.600 0.2024 562212. 15278. -0.007079 0.000 5.971E+10-644.4586 7643.3222 0.000 3.800 0.1854 597193. 13785. -0.006997 0.000 1.008E+10-599.8090 7764.6448 0.000 4.000 0.1688 628716. 12143. -0.006780 0.000 5.172E+09-768.6276 10930. 0.000 4.200 0.1529 655805. 10096. -0.006480 0.000 5.127E+09-937.0916 14713. 0.000 4.400 0.1377 677488. 7943.8032 -0.006166 0.000 5.057E+09-856.4265 14930. 0.000 4.600 0.1233 694231. 5982.6228 -0.005837 0.000 4.952E+09-777.8905 15147. 0.000 4.800 0.1097 706485. 4206.8481 -0.005493 0.000 4.824E+09-701.9217 15363. 0.000 5.000 0.0969 714687. 2609.7745 -0.005137 0.000 4.744E+09-628.9730 15580. 0.000 5.200 0.0850 719258. 1183.6878 -0.004772 0.000 4.701E+09-559.4326 15796. 0.000 5.400 0.0740 720598. -79.9821 -0.004404 0.000 4.688E+09-493.6257 16013. 0.000 5.600 0.0639 719086. -1190.5145 -0.004036 0.000 4.702E+09-431.8179 16230. 0.000 5.800 0.0546 715078. -2157.7576 -0.003672 0.000 4.740E+09-374.2180 16446. 0.000 6.000 0.0462 708905. -2991.9969 -0.003313 0.000 4.801E+09-320.9815 16663. 0.000 6.200 0.0387 700875. -3703.8326 -0.002964 0.000 4.883E+09-272.2149 16879. 0.000 6.400 0.0320 691269. -4304.0658 -0.002625 0.000 4.985E+09

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existing phase1 81.lp6o-227.9795 17096. 0.000 6.600 0.0261 680341. -4803.5972 -0.002297 0.000 5.047E+09-188.2967 17313. 0.000 6.800 0.0210 668322. -5213.4174 -0.001978 0.000 5.088E+09-153.2201 17529. 0.000 7.000 0.0166 655412. -5544.6573 -0.001667 0.000 5.128E+09-122.8131 17746. 0.000 7.200 0.0130 641787. -5808.5862 -0.001364 0.000 5.154E+09-97.1276 17962. 0.000 7.400 0.0101 627596. -6016.6029 -0.001069 0.000 5.173E+09-76.2197 18179. 0.000 7.600 0.007846 612959. -6180.2365 -0.000782 0.000 5.194E+09-60.1416 18396. 0.000 7.800 0.006310 597969. -6311.1286 -0.000557 0.000 8.639E+09-48.9351 18612. 0.000 8.000 0.005172 582692. -6418.5458 -0.000444 0.000 2.345E+10-40.5792 18829. 0.000 8.200 0.004178 567181. -6507.0254 -0.000403 0.000 5.970E+10-33.1538 19045. 0.000 8.400 0.003238 551478. -6577.9957 -0.000381 0.000 5.974E+10-25.9881 19262. 0.000 8.600 0.002351 535625. -6632.0827 -0.000359 0.000 5.978E+10-19.0844 19479. 0.000 8.800 0.001516 519661. -6669.9170 -0.000337 0.000 5.982E+10-12.4442 19695. 0.000 9.000 0.000731 503625. -6691.6845 -0.000317 0.000 5.986E+10-5.6954 18688. 0.000 9.200 -5.092E-06 487556. -6698.4752 -0.000297 0.000 5.990E+100.0365 17189. 0.000 9.400 -0.000695 471487. -6692.3982 -0.000278 0.000 5.994E+105.0277 17369. 0.000 9.600 -0.001339 455446. -6674.6158 -0.000259 0.000 5.998E+109.7909 17549. 0.000 9.800 -0.001940 439461. -6645.6736 -0.000241 0.000 6.002E+1014.3276 17728. 0.000 10.000 -0.002498 423559. -6606.1131 -0.000224 0.000 6.006E+1018.6395 17908. 0.000 10.200 -0.003016 407763. -6556.4712 -0.000208 0.000 6.009E+1022.7288 18088. 0.000 10.400 -0.003495 392097. -6497.2787 -0.000192 0.000 6.014E+1026.5982 18267. 0.000 10.600 -0.003936 376585. -6429.0600 -0.000176 0.000 6.018E+1030.2506 18447. 0.000 10.800 -0.004341 361246. -6352.3320 -0.000162 0.000 6.021E+1033.6894 18627. 0.000 11.000 -0.004711 346102. -6267.6031 -0.000147 0.000 6.025E+1036.9180 18807. 0.000 11.200 -0.005049 331169. -6175.3732 -0.000134 0.000 6.028E+1039.9403 18986. 0.000 11.400 -0.005355 316466. -6076.1322 -0.000121 0.000 6.032E+1042.7605 19166. 0.000 11.600 -0.005630 302009. -5970.3603 -0.000109 0.000 6.036E+1045.3828 19346. 0.000 11.800 -0.005877 287814. -5858.5265 -9.710E-05 0.000 6.039E+1047.8120 19525. 0.000 12.000 -0.006096 273893. -5741.0888 -8.594E-05 0.000 6.042E+1050.0527 19705. 0.000 12.200 -0.006289 260261. -5618.4935 -7.534E-05 0.000 6.045E+1052.1100 19885. 0.000 12.400 -0.006458 246928. -5491.1749 -6.527E-05 0.000 6.048E+1053.9888 20064. 0.000 12.600 -0.006603 233906. -5359.5549 -5.573E-05 0.000 6.052E+1055.6945 20244. 0.000

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existing phase1 81.lp6o 12.800 -0.006725 221205. -5224.0424 -4.671E-05 0.000 6.055E+1057.2325 20424. 0.000 13.000 -0.006827 208833. -5085.0335 -3.819E-05 0.000 6.057E+1058.6082 20604. 0.000 13.200 -0.006909 196798. -4942.9111 -3.016E-05 0.000 6.060E+1059.8272 20783. 0.000 13.400 -0.006972 185108. -4798.0445 -2.260E-05 0.000 6.062E+1060.8950 20963. 0.000 13.600 -0.007017 173769. -4650.7899 -1.549E-05 0.000 6.065E+1061.8172 21143. 0.000 13.800 -0.007046 162785. -4501.4895 -8.836E-06 0.000 6.068E+1062.5997 21322. 0.000 14.000 -0.007060 152162. -4350.4721 -2.610E-06 0.000 6.072E+1063.2481 21502. 0.000 14.200 -0.007059 141903. -4198.0527 3.202E-06 0.000 6.073E+1063.7681 21682. 0.000 14.400 -0.007044 132011. -4044.5327 8.614E-06 0.000 6.074E+1064.1653 21862. 0.000 14.600 -0.007017 122489. -3890.1998 1.364E-05 0.000 6.075E+1064.4454 22041. 0.000 14.800 -0.006979 113338. -3735.3285 1.830E-05 0.000 6.077E+1064.6140 22221. 0.000 15.000 -0.006929 104559. -3580.1799 2.260E-05 0.000 6.079E+1064.6765 22401. 0.000 15.200 -0.006870 96152. -3425.0020 2.656E-05 0.000 6.081E+1064.6384 22580. 0.000 15.400 -0.006802 88117. -3270.0298 3.020E-05 0.000 6.083E+1064.5051 22760. 0.000 15.600 -0.006725 80454. -3115.4855 3.352E-05 0.000 6.085E+1064.2818 22940. 0.000 15.800 -0.006641 73161. -2961.5790 3.655E-05 0.000 6.087E+1063.9736 23120. 0.000 16.000 -0.006550 66237. -2808.5078 3.930E-05 0.000 6.087E+1063.5857 23299. 0.000 16.200 -0.006452 59679. -2656.4578 4.178E-05 0.000 6.087E+1063.1227 23479. 0.000 16.400 -0.006349 53484. -2505.6031 4.401E-05 0.000 6.087E+1062.5895 23659. 0.000 16.600 -0.006241 47650. -2356.1070 4.601E-05 0.000 6.087E+1061.9906 23838. 0.000 16.800 -0.006128 42172. -2208.1219 4.778E-05 0.000 6.087E+1061.3303 24018. 0.000 17.000 -0.006012 37048. -2061.7899 4.934E-05 0.000 6.087E+1060.6130 24198. 0.000 17.200 -0.005892 32273. -1917.2432 5.071E-05 0.000 6.087E+1059.8426 24377. 0.000 17.400 -0.005768 27843. -1774.6047 5.189E-05 0.000 6.087E+1059.0229 24557. 0.000 17.600 -0.005643 23753. -1633.9882 5.291E-05 0.000 6.087E+1058.1576 24737. 0.000 17.800 -0.005514 19997. -1495.4989 5.377E-05 0.000 6.087E+1057.2501 24917. 0.000 18.000 -0.005384 16572. -1359.2343 5.449E-05 0.000 6.087E+1056.3037 25096. 0.000 18.200 -0.005253 13471. -1225.2844 5.508E-05 0.000 6.087E+1055.3213 25276. 0.000 18.400 -0.005120 10688. -1093.7322 5.556E-05 0.000 6.087E+1054.3056 25456. 0.000 18.600 -0.004986 8217.9383 -964.6544 5.593E-05 0.000 6.087E+1053.2593 25635. 0.000 18.800 -0.004852 6054.8081 -838.1219 5.621E-05 0.000 6.087E+1052.1845 25815. 0.000 19.000 -0.004716 4192.2550 -706.5700 5.642E-05 0.000 6.087E+10

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existing phase1 81.lp6o57.4421 29231. 0.000 19.200 -0.004581 2660.5644 -563.6995 5.655E-05 0.000 6.087E+1061.6166 32283. 0.000 19.400 -0.004445 1483.7831 -417.5310 5.663E-05 0.000 6.087E+1060.1904 32500. 0.000 19.600 -0.004309 653.6974 -274.8171 5.668E-05 0.000 6.087E+1058.7378 32716. 0.000 19.800 -0.004173 161.9407 -135.6200 5.669E-05 0.000 6.087E+1057.2598 32933. 0.000 20.000 -0.004037 0.000 0.000 5.669E-05 0.000 6.087E+1055.7569 16575. 0.000

* This analysis makes computations of pile response using nonlinear moment-curvaturerelationships. The above values of total stress are computed for combined axial and bending stress in elastic sections and do not equal actual stresses in concrete and steel in the range of nonlinear bending.

Output Summary for Load Case No. 12:

Pile-head deflection = 0.5000000 inchesComputed slope at pile head = -0.0003660 radiansMaximum bending moment = -905605. inch-lbsMaximum shear force = 56035. lbsDepth of maximum bending moment = 0.000000 inches below pile headDepth of maximum shear force = 0.000000 inches below pile headNumber of iterations = 39Number of zero deflection points = 1

-------------------------------------------------------------------------------- Computed Values of Pile Loading and Deflection for Lateral Loading for Load Case Number 13--------------------------------------------------------------------------------

Pile-head conditions are Displacement and Pile-head Rotation (Loading Type 5)Displacement of pile head = 0.750000 inchesRotation of pile head = 0.000E+00 radiansAxial load on pile head = 10000.000 lbs

Depth Deflect. Bending Shear Slope Total Bending Soil Res. Soil Spr. Distrib. X y Moment Force S Stress Stiffness p Es*h Lat. Load feet inches in-lbs lbs radians psi* lb-in^2 lb/in lb/inch lb/inch ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- 0.00 0.7500 -905613. 67964. 0.000 0.000 2.430E+08 -1400.4316 2240.6905 0.000 0.200 0.7393 -746528. 64518. -0.008158 0.000 2.430E+08 -1435.9755 4661.8277 0.000 0.400 0.7108 -595536. 61061. -0.0120 0.000 5.527E+09 -1445.0456 4878.8650 0.000 0.600 0.6818 -452862. 57586. -0.0121 0.000 5.999E+10 -1450.4781 5105.8336 0.000 0.800 0.6527 -318542. 54102. -0.0121 0.000 6.031E+10 -1452.9543 5342.4876 0.000 1.000 0.6236 -192591. 50615. -0.0121 0.000 6.061E+10 -1452.3640 5589.6903 0.000

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existing phase1 81.lp6o 1.200 0.5945 -75005. 47127. -0.0121 0.000 6.087E+10 -1454.4597 5872.1358 0.000 1.400 0.5653 34203. 43637. -0.0121 0.000 6.087E+10 -1453.9512 6172.7181 0.000 1.600 0.5362 135036. 40169. -0.0121 0.000 6.074E+10 -1436.4991 6430.0965 0.000 1.800 0.5070 227595. 36784. -0.0121 0.000 6.054E+10 -1384.0885 6551.4190 0.000 2.000 0.4779 312182. 33529. -0.0121 0.000 6.033E+10 -1328.7932 6672.7416 0.000 2.200 0.4489 389114. 30409. -0.0121 0.000 6.014E+10 -1270.6394 6794.0642 0.000 2.400 0.4198 458727. 27433. -0.0121 0.000 5.997E+10 -1209.6532 6915.3868 0.000 2.600 0.3908 521372. 24606. -0.0121 0.000 5.982E+10 -1145.8602 7036.7093 0.000 2.800 0.3619 577416. 21936. -0.0120 0.000 5.967E+10 -1079.2854 7158.0319 0.000 3.000 0.3330 627243. 19429. -0.0119 0.000 5.174E+09 -1009.9532 7279.3545 0.000 3.200 0.3048 671246. 17089. -0.0116 0.000 5.078E+09-939.8535 7400.6771 0.000 3.400 0.2774 709828. 14918. -0.0113 0.000 4.790E+09-869.2900 7521.9996 0.000 3.600 0.2508 743394. 12917. -0.0109 0.000 4.491E+09-798.6716 7643.3222 0.000 3.800 0.2252 772350. 11084. -0.0104 0.000 4.033E+09-728.4508 7764.6448 0.000 4.000 0.2006 797099. 9113.4876 -0.009951 0.000 3.604E+09-913.7395 10930. 0.000 4.200 0.1774 816572. 6711.9651 -0.009392 0.000 3.334E+09 -1087.5292 14713. 0.000 4.400 0.1556 829767. 4245.6860 -0.008778 0.000 3.112E+09-967.7034 14930. 0.000 4.600 0.1353 837373. 2060.0853 -0.008107 0.000 2.859E+09-853.6305 15147. 0.000 4.800 0.1166 840044. 139.6984 -0.007392 0.000 2.778E+09-746.6919 15363. 0.000 5.000 0.0998 838398. -1533.5706 -0.006674 0.000 2.830E+09-647.6989 15580. 0.000 5.200 0.0846 833004. -2979.0801 -0.005986 0.000 3.008E+09-556.8924 15796. 0.000 5.400 0.0710 824386. -4216.1427 -0.005347 0.000 3.229E+09-473.9930 16013. 0.000 5.600 0.0589 813023. -5263.2403 -0.004753 0.000 3.381E+09-398.5884 16230. 0.000 5.800 0.0482 799350. -6138.1376 -0.004195 0.000 3.572E+09-330.4927 16446. 0.000 6.000 0.0388 783761. -6858.0246 -0.003681 0.000 3.824E+09-269.4131 16663. 0.000 6.200 0.0306 766608. -7439.2421 -0.003213 0.000 4.152E+09-214.9349 16879. 0.000 6.400 0.0234 748207. -7897.0180 -0.002790 0.000 4.454E+09-166.5450 17096. 0.000 6.600 0.0172 728837. -8245.4796 -0.002399 0.000 4.614E+09-123.8396 17313. 0.000 6.800 0.0119 708744. -8498.0764 -0.002032 0.000 4.802E+09-86.6577 17529. 0.000 7.000 0.007412 688144. -8667.8310 -0.001690 0.000 5.007E+09-54.8046 17746. 0.000 7.200 0.003751 667220. -8767.2830 -0.001368 0.000 5.091E+09-28.0721 17962. 0.000 7.400 0.000844 646126. -8808.6454 -0.001060 0.000 5.148E+09

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existing phase1 81.lp6o-6.3965 18179. 0.000 7.600 -0.001339 624989. -8804.0067 -0.000765 0.000 5.177E+0910.2621 18396. 0.000 7.800 -0.002827 603904. -8765.3860 -0.000481 0.000 5.211E+0921.9219 18612. 0.000 8.000 -0.003647 582938. -8704.7441 -0.000319 0.000 3.109E+1028.6130 18829. 0.000 8.200 -0.004359 562136. -8628.8944 -0.000286 0.000 5.971E+1034.5951 19045. 0.000 8.400 -0.005018 541533. -8539.0557 -0.000263 0.000 5.976E+1040.2705 19262. 0.000 8.600 -0.005624 521161. -8435.9617 -0.000242 0.000 5.982E+1045.6411 19479. 0.000 8.800 -0.006179 501052. -8320.3411 -0.000222 0.000 5.986E+1050.7093 19695. 0.000 9.000 -0.006687 481234. -8197.0077 -0.000202 0.000 5.991E+1052.0686 18688. 0.000 9.200 -0.007148 461716. -8073.0907 -0.000183 0.000 5.996E+1051.1955 17189. 0.000 9.400 -0.007565 442492. -7945.9585 -0.000165 0.000 6.001E+1054.7480 17369. 0.000 9.600 -0.007939 423584. -7810.5980 -0.000148 0.000 6.006E+1058.0524 17549. 0.000 9.800 -0.008273 405009. -7667.6000 -0.000131 0.000 6.010E+1061.1127 17728. 0.000 10.000 -0.008568 386785. -7517.5447 -0.000115 0.000 6.015E+1063.9334 17908. 0.000 10.200 -0.008826 368930. -7361.0017 -0.000100 0.000 6.020E+1066.5191 18088. 0.000 10.400 -0.009049 351457. -7198.5290 -8.577E-05 0.000 6.023E+1068.8748 18267. 0.000 10.600 -0.009238 334381. -7030.6728 -7.211E-05 0.000 6.027E+1071.0054 18447. 0.000 10.800 -0.009395 317714. -6857.9665 -5.914E-05 0.000 6.032E+1072.9164 18627. 0.000 11.000 -0.009522 301466. -6680.9311 -4.682E-05 0.000 6.036E+1074.6132 18807. 0.000 11.200 -0.009620 285647. -6500.0737 -3.515E-05 0.000 6.039E+1076.1013 18986. 0.000 11.400 -0.009691 270267. -6315.8881 -2.411E-05 0.000 6.043E+1077.3866 19166. 0.000 11.600 -0.009735 255332. -6128.8544 -1.368E-05 0.000 6.046E+1078.4748 19346. 0.000 11.800 -0.009756 240849. -5939.4384 -3.831E-06 0.000 6.050E+1079.3719 19525. 0.000 12.000 -0.009754 226823. -5748.0916 5.441E-06 0.000 6.054E+1080.0838 19705. 0.000 12.200 -0.009730 213258. -5555.2512 1.416E-05 0.000 6.057E+1080.6165 19885. 0.000 12.400 -0.009686 200157. -5361.3400 2.235E-05 0.000 6.059E+1080.9761 20064. 0.000 12.600 -0.009623 187523. -5166.7662 3.003E-05 0.000 6.062E+1081.1687 20244. 0.000 12.800 -0.009542 175355. -4971.9238 3.721E-05 0.000 6.065E+1081.2001 20424. 0.000 13.000 -0.009444 163656. -4777.1920 4.392E-05 0.000 6.068E+1081.0764 20604. 0.000 13.200 -0.009331 152423. -4582.9360 5.017E-05 0.000 6.072E+1080.8036 20783. 0.000 13.400 -0.009203 141655. -4389.5068 5.598E-05 0.000 6.073E+1080.3875 20963. 0.000 13.600 -0.009062 131350. -4197.2411 6.137E-05 0.000 6.074E+1079.8339 21143. 0.000

Page 63

existing phase1 81.lp6o 13.800 -0.008909 121505. -4006.4621 6.637E-05 0.000 6.076E+1079.1486 21322. 0.000 14.000 -0.008744 112116. -3817.4794 7.098E-05 0.000 6.077E+1078.3370 21502. 0.000 14.200 -0.008568 103178. -3630.5893 7.523E-05 0.000 6.079E+1077.4048 21682. 0.000 14.400 -0.008383 94686. -3446.0750 7.914E-05 0.000 6.081E+1076.3571 21862. 0.000 14.600 -0.008188 86633. -3264.2072 8.271E-05 0.000 6.083E+1075.1994 22041. 0.000 14.800 -0.007986 79014. -3085.2440 8.598E-05 0.000 6.086E+1073.9366 22221. 0.000 15.000 -0.007776 71820. -2909.4318 8.895E-05 0.000 6.087E+1072.5736 22401. 0.000 15.200 -0.007559 65044. -2737.0052 9.165E-05 0.000 6.087E+1071.1152 22580. 0.000 15.400 -0.007336 58678. -2568.1877 9.409E-05 0.000 6.087E+1069.5660 22760. 0.000 15.600 -0.007107 52712. -2403.1921 9.629E-05 0.000 6.087E+1067.9303 22940. 0.000 15.800 -0.006873 47138. -2242.2209 9.826E-05 0.000 6.087E+1066.2123 23120. 0.000 16.000 -0.006635 41945. -2085.4668 0.000100 0.000 6.087E+1064.4161 23299. 0.000 16.200 -0.006393 37123. -1933.1131 0.000102 0.000 6.087E+1062.5453 23479. 0.000 16.400 -0.006148 32661. -1785.3342 0.000103 0.000 6.087E+1060.6037 23659. 0.000 16.600 -0.005899 28548. -1642.2961 0.000104 0.000 6.087E+1058.5947 23838. 0.000 16.800 -0.005648 24773. -1504.1570 0.000105 0.000 6.087E+1056.5213 24018. 0.000 17.000 -0.005394 21323. -1371.0674 0.000106 0.000 6.087E+1054.3867 24198. 0.000 17.200 -0.005139 18187. -1243.1710 0.000107 0.000 6.087E+1052.1936 24377. 0.000 17.400 -0.004881 15351. -1120.6052 0.000108 0.000 6.087E+1049.9446 24557. 0.000 17.600 -0.004622 12803. -1003.5012 0.000108 0.000 6.087E+1047.6421 24737. 0.000 17.800 -0.004362 10529. -891.9848 0.000109 0.000 6.087E+1045.2882 24917. 0.000 18.000 -0.004101 8515.9394 -786.1770 0.000109 0.000 6.087E+1042.8850 25096. 0.000 18.200 -0.003839 6750.0049 -686.1939 0.000109 0.000 6.087E+1040.4342 25276. 0.000 18.400 -0.003577 5216.9648 -592.1480 0.000109 0.000 6.087E+1037.9374 25456. 0.000 18.600 -0.003314 3902.4392 -504.1480 0.000110 0.000 6.087E+1035.3960 25635. 0.000 18.800 -0.003050 2791.7909 -422.2992 0.000110 0.000 6.087E+1032.8113 25815. 0.000 19.000 -0.002787 1870.1329 -342.1960 0.000110 0.000 6.087E+1033.9415 29231. 0.000 19.200 -0.002523 1143.9759 -260.7414 0.000110 0.000 6.087E+1033.9373 32283. 0.000 19.400 -0.002259 613.2968 -183.3073 0.000110 0.000 6.087E+1030.5912 32500. 0.000 19.600 -0.001995 258.8222 -113.9620 0.000110 0.000 6.087E+1027.1966 32716. 0.000 19.800 -0.001731 60.9996 -52.8213 0.000110 0.000 6.087E+1023.7540 32933. 0.000 20.000 -0.001467 0.000 0.000 0.000110 0.000 6.087E+10

Page 64

existing phase1 81.lp6o20.2637 16575. 0.000

* This analysis makes computations of pile response using nonlinear moment-curvaturerelationships. The above values of total stress are computed for combined axial and bending stress in elastic sections and do not equal actual stresses in concrete and steel in the range of nonlinear bending.

Output Summary for Load Case No. 13:

Pile-head deflection = 0.7500000 inchesComputed slope at pile head = -0.0007855 radiansMaximum bending moment = -905613. inch-lbsMaximum shear force = 67964. lbsDepth of maximum bending moment = 0.000000 inches below pile headDepth of maximum shear force = 0.000000 inches below pile headNumber of iterations = 60Number of zero deflection points = 1

-------------------------------------------------------------------------------- Computed Values of Pile Loading and Deflection for Lateral Loading for Load Case Number 14--------------------------------------------------------------------------------

Pile-head conditions are Displacement and Pile-head Rotation (Loading Type 5)Displacement of pile head = 1.000000 inchesRotation of pile head = 0.000E+00 radiansAxial load on pile head = 10000.000 lbs

Depth Deflect. Bending Shear Slope Total Bending Soil Res. Soil Spr. Distrib. X y Moment Force S Stress Stiffness p Es*h Lat. Load feet inches in-lbs lbs radians psi* lb-in^2 lb/in lb/inch lb/inch ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- 0.00 1.0000 -905583. 76263. 0.000 0.000 1.610E+08 -1603.0664 1923.6796 0.000 0.200 0.9838 -727178. 72274. -0.0122 0.000 1.610E+08 -1662.2304 4055.0456 0.000 0.400 0.9416 -558086. 68212. -0.0176 0.000 5.972E+10 -1722.2922 4389.9532 0.000 0.600 0.8993 -398915. 64007. -0.0176 0.000 6.012E+10 -1782.1938 4756.1601 0.000 0.800 0.8570 -250008. 59736. -0.0176 0.000 6.048E+10 -1776.8970 4976.1356 0.000 1.000 0.8147 -111336. 55483. -0.0176 0.000 6.077E+10 -1767.1916 5206.1244 0.000 1.200 0.7723 17157. 51253. -0.0176 0.000 6.087E+10 -1757.9842 5462.9479 0.000 1.400 0.7300 135524. 47049. -0.0176 0.000 6.074E+10 -1744.8020 5736.4857 0.000 1.600 0.6877 243840. 42883. -0.0176 0.000 6.049E+10 -1727.5372 6029.3486 0.000 1.800 0.6453 342206. 38762. -0.0176 0.000 6.025E+10 -1706.0830 6344.8230 0.000 2.000 0.6031 430745. 34703. -0.0176 0.000 6.004E+10 -1676.7244 6672.7416 0.000

Page 65

existing phase1 81.lp6o 2.200 0.5608 509625. 30786. -0.0176 0.000 5.984E+10 -1587.6565 6794.0642 0.000 2.400 0.5187 579360. 27087. -0.0176 0.000 5.967E+10 -1494.4601 6915.3868 0.000 2.600 0.4765 640486. 23617. -0.0174 0.000 5.155E+09 -1397.1629 7036.7093 0.000 2.800 0.4351 693557. 20383. -0.0171 0.000 4.959E+09 -1297.7408 7158.0319 0.000 3.000 0.3945 739145. 17390. -0.0167 0.000 4.526E+09 -1196.5752 7279.3545 0.000 3.200 0.3548 777832. 14641. -0.0163 0.000 3.929E+09 -1094.2051 7400.6771 0.000 3.400 0.3163 810205. 12138. -0.0158 0.000 3.417E+09-991.3990 7521.9996 0.000 3.600 0.2792 836853. 9881.8303 -0.0151 0.000 2.871E+09-889.0480 7643.3222 0.000 3.800 0.2437 858364. 7868.9256 -0.0143 0.000 2.302E+09-788.3726 7764.6448 0.000 4.000 0.2103 875312. 5773.3324 -0.0134 0.000 1.972E+09-957.9551 10930. 0.000 4.200 0.1796 886717. 3302.7215 -0.0122 0.000 1.775E+09 -1100.8873 14713. 0.000 4.400 0.1517 891752. 849.4059 -0.0109 0.000 1.550E+09-943.5423 14930. 0.000 4.600 0.1271 891319. -1245.3355 -0.009568 0.000 1.584E+09-802.0755 15147. 0.000 4.800 0.1057 886233. -3020.1224 -0.008299 0.000 1.788E+09-676.9136 15363. 0.000 5.000 0.0873 877220. -4512.1391 -0.007161 0.000 1.941E+09-566.4337 15580. 0.000 5.200 0.0714 864919. -5755.5598 -0.006140 0.000 2.166E+09-469.7502 15796. 0.000 5.400 0.0578 849889. -6781.9120 -0.005254 0.000 2.509E+09-385.5433 16013. 0.000 5.600 0.0461 832618. -7619.0596 -0.004517 0.000 3.019E+09-312.0797 16230. 0.000 5.800 0.0361 813534. -8290.4384 -0.003897 0.000 3.374E+09-247.4026 16446. 0.000 6.000 0.0274 793011. -8815.9883 -0.003348 0.000 3.669E+09-190.5557 16663. 0.000 6.200 0.0200 771378. -9213.7374 -0.002860 0.000 4.054E+09-140.9019 16879. 0.000 6.400 0.0137 748922. -9500.0812 -0.002430 0.000 4.448E+09-97.7179 17096. 0.000 6.600 0.008372 725894. -9689.8108 -0.002040 0.000 4.640E+09-60.3901 17313. 0.000 6.800 0.003927 702509. -9796.6934 -0.001679 0.000 4.865E+09-28.6787 17529. 0.000 7.000 0.000313 678950. -9833.8863 -0.001344 0.000 5.052E+09-2.3153 17746. 0.000 7.200 -0.002526 655371. -9813.9770 -0.001030 0.000 5.128E+0918.9064 17962. 0.000 7.400 -0.004629 631893. -9749.2118 -0.000730 0.000 5.167E+0935.0646 18179. 0.000 7.600 -0.006028 608610. -9651.6902 -0.000442 0.000 5.200E+0946.2034 18396. 0.000 7.800 -0.006753 585586. -9533.4057 -0.000280 0.000 3.180E+1052.3670 18612. 0.000 8.000 -0.007371 562863. -9401.1705 -0.000246 0.000 5.971E+1057.8291 18829. 0.000 8.200 -0.007935 540472. -9256.2092 -0.000224 0.000 5.976E+1062.9720 19045. 0.000 8.400 -0.008448 518444. -9099.2845 -0.000203 0.000 5.982E+10

Page 66

existing phase1 81.lp6o67.7986 19262. 0.000 8.600 -0.008910 496805. -8931.1512 -0.000183 0.000 5.987E+1072.3126 19479. 0.000 8.800 -0.009324 475583. -8752.5548 -0.000163 0.000 5.993E+1076.5177 19695. 0.000 9.000 -0.009693 454801. -8570.1616 -0.000145 0.000 5.998E+1075.4766 18688. 0.000 9.200 -0.0100 434453. -8393.4892 -0.000127 0.000 6.003E+1071.7503 17189. 0.000 9.400 -0.0103 414518. -8217.9273 -0.000110 0.000 6.008E+1074.5512 17369. 0.000 9.600 -0.0105 395012. -8035.9411 -9.363E-05 0.000 6.013E+1077.1040 17549. 0.000 9.800 -0.0108 375950. -7848.1199 -7.825E-05 0.000 6.018E+1079.4137 17728. 0.000 10.000 -0.0109 357345. -7655.0407 -6.363E-05 0.000 6.022E+1081.4857 17908. 0.000 10.200 -0.0111 339209. -7457.2673 -4.976E-05 0.000 6.026E+1083.3255 18088. 0.000 10.400 -0.0112 321553. -7255.3499 -3.660E-05 0.000 6.031E+1084.9389 18267. 0.000 10.600 -0.0112 304385. -7049.8252 -2.415E-05 0.000 6.036E+1086.3317 18447. 0.000 10.800 -0.0113 287715. -6841.2153 -1.238E-05 0.000 6.039E+1087.5099 18627. 0.000 11.000 -0.0113 271548. -6630.0280 -1.273E-06 0.000 6.042E+1088.4795 18807. 0.000 11.200 -0.0113 255891. -6416.7565 9.198E-06 0.000 6.046E+1089.2468 18986. 0.000 11.400 -0.0112 240747. -6201.8789 1.905E-05 0.000 6.050E+1089.8179 19166. 0.000 11.600 -0.0112 226121. -5985.8586 2.831E-05 0.000 6.054E+1090.1991 19346. 0.000 11.800 -0.0111 212014. -5769.1437 3.699E-05 0.000 6.057E+1090.3967 19525. 0.000 12.000 -0.0110 198427. -5552.1672 4.512E-05 0.000 6.059E+1090.4170 19705. 0.000 12.200 -0.0109 185361. -5335.3473 5.272E-05 0.000 6.062E+1090.2662 19885. 0.000 12.400 -0.0108 172815. -5119.0871 5.981E-05 0.000 6.065E+1089.9506 20064. 0.000 12.600 -0.0106 160786. -4903.7749 6.641E-05 0.000 6.069E+1089.4762 20244. 0.000 12.800 -0.0104 149273. -4689.7842 7.254E-05 0.000 6.072E+1088.8493 20424. 0.000 13.000 -0.0103 138272. -4477.4741 7.822E-05 0.000 6.073E+1088.0758 20604. 0.000 13.200 -0.0101 127778. -4267.1893 8.347E-05 0.000 6.075E+1087.1616 20783. 0.000 13.400 -0.009859 117786. -4059.2604 8.832E-05 0.000 6.076E+1086.1125 20963. 0.000 13.600 -0.009641 108289. -3854.0046 9.279E-05 0.000 6.078E+1084.9340 21143. 0.000 13.800 -0.009413 99282. -3651.7255 9.689E-05 0.000 6.080E+1083.6319 21322. 0.000 14.000 -0.009176 90756. -3452.7136 0.000101 0.000 6.082E+1082.2113 21502. 0.000 14.200 -0.008930 82704. -3257.2469 0.000104 0.000 6.085E+1080.6776 21682. 0.000 14.400 -0.008677 75116. -3065.5908 0.000107 0.000 6.087E+1079.0358 21862. 0.000 14.600 -0.008416 67984. -2877.9991 0.000110 0.000 6.087E+1077.2906 22041. 0.000

Page 67

existing phase1 81.lp6o 14.800 -0.008149 61297. -2694.7141 0.000113 0.000 6.087E+1075.4469 22221. 0.000 15.000 -0.007876 55044. -2515.9670 0.000115 0.000 6.087E+1073.5090 22401. 0.000 15.200 -0.007598 49215. -2341.9787 0.000117 0.000 6.087E+1071.4812 22580. 0.000 15.400 -0.007315 43797. -2172.9600 0.000119 0.000 6.087E+1069.3676 22760. 0.000 15.600 -0.007028 38779. -2009.1124 0.000120 0.000 6.087E+1067.1721 22940. 0.000 15.800 -0.006737 34147. -1850.6282 0.000122 0.000 6.087E+1064.8981 23120. 0.000 16.000 -0.006443 29890. -1697.6912 0.000123 0.000 6.087E+1062.5493 23299. 0.000 16.200 -0.006146 25993. -1550.4774 0.000124 0.000 6.087E+1060.1288 23479. 0.000 16.400 -0.005847 22442. -1409.1552 0.000125 0.000 6.087E+1057.6397 23659. 0.000 16.600 -0.005546 19223. -1273.8861 0.000126 0.000 6.087E+1055.0846 23838. 0.000 16.800 -0.005243 16321. -1144.8252 0.000127 0.000 6.087E+1052.4662 24018. 0.000 17.000 -0.004938 13721. -1022.1216 0.000127 0.000 6.087E+1049.7868 24198. 0.000 17.200 -0.004632 11409. -905.9191 0.000128 0.000 6.087E+1047.0486 24377. 0.000 17.400 -0.004325 9366.8102 -796.3565 0.000128 0.000 6.087E+1044.2535 24557. 0.000 17.600 -0.004017 7579.9253 -693.5682 0.000128 0.000 6.087E+1041.4034 24737. 0.000 17.800 -0.003708 6031.5166 -597.6846 0.000129 0.000 6.087E+1038.4996 24917. 0.000 18.000 -0.003399 4704.8601 -508.8327 0.000129 0.000 6.087E+1035.5437 25096. 0.000 18.200 -0.003089 3582.9307 -427.1361 0.000129 0.000 6.087E+1032.5368 25276. 0.000 18.400 -0.002779 2648.4097 -352.7162 0.000129 0.000 6.087E+1029.4798 25456. 0.000 18.600 -0.002469 1883.6900 -285.6918 0.000129 0.000 6.087E+1026.3738 25635. 0.000 18.800 -0.002159 1270.8818 -226.1799 0.000129 0.000 6.087E+1023.2194 25815. 0.000 19.000 -0.001848 791.8164 -171.3058 0.000129 0.000 6.087E+1022.5089 29231. 0.000 19.200 -0.001537 442.4017 -119.4780 0.000129 0.000 6.087E+1020.6809 32283. 0.000 19.400 -0.001227 212.1087 -74.7259 0.000129 0.000 6.087E+1016.6125 32500. 0.000 19.600 -0.000916 77.5037 -39.8055 0.000129 0.000 6.087E+1012.4878 32716. 0.000 19.800 -0.000605 14.8282 -14.8520 0.000129 0.000 6.087E+108.3068 32933. 0.000 20.000 -0.000295 0.000 0.000 0.000129 0.000 6.087E+104.0698 16575. 0.000

* This analysis makes computations of pile response using nonlinear moment-curvaturerelationships. The above values of total stress are computed for combined axial and bending stress in elastic sections and do not equal actual stresses in concrete and steel in the range of nonlinear bending.

Page 68

existing phase1 81.lp6oOutput Summary for Load Case No. 14:

Pile-head deflection = 1.0000000 inchesComputed slope at pile head = -0.0013298 radiansMaximum bending moment = -905583. inch-lbsMaximum shear force = 76263. lbsDepth of maximum bending moment = 0.000000 inches below pile headDepth of maximum shear force = 0.000000 inches below pile headNumber of iterations = 73Number of zero deflection points = 2

-------------------------------------------------------------------------------- Summary of Pile Response(s)--------------------------------------------------------------------------------

Definitions of Pile-head Loading Conditions:

Load Type 1: Load 1 = Shear, lbs, and Load 2 = Moment, in-lbsLoad Type 2: Load 1 = Shear, lbs, and Load 2 = Slope, radiansLoad Type 3: Load 1 = Shear, lbs, and Load 2 = Rotational Stiffness, in-lbs/radianLoad Type 4: Load 1 = Top Deflection, inches, and Load 2 = Moment, in-lbsLoad Type 5: Load 1 = Top Deflection, inches, and Load 2 = Slope, radians

Pile-head Pile-head Maximum MaximumLoad Load Condition 1 Condition 2 Axial Pile-head Moment Shear Pile-headCase Type V(lbs) or in-lb, rad., Loading Deflection in Pile in Pile Rotation No. No. y(inches) or in-lb/rad. lbs inches in-lbs lbs radians---- ---- -------------- -------------- ------------- -------------------------- ------------- ------------- 1 4 y = 0.0100 M = 0.000 10000.00000000 0.0100000057053. 1549.9660 -0.00011629 2 4 y = 0.1000 M = 0.000 10000.00000000 0.10000000565887. 15424. -0.00116658 3 4 y = 0.2000 M = 0.000 10000.00000000 0.20000000602743. 21438. -0.00288661 4 4 y = 0.3000 M = 0.000 10000.00000000 0.30000000633128. 26558. -0.00489088 5 4 y = 0.5000 M = 0.000 10000.00000000 0.50000000758735. 37116. -0.00927585 6 4 y = 0.7500 M = 0.000 10000.00000000 0.75000000858723. 46549. -0.01541182 7 4 y = 1.0000 M = 0.000 10000.00000000 1.00000000899456. 52749. -0.02240650 8 5 y = 0.0100 S = 0.000 10000.00000000 0.01000000-176928. 3608.1384 -0.00000017 9 5 y = 0.1000 S = 0.000 10000.00000000 0.10000000-717015. 24086. -0.00001457 10 5 y = 0.2000 S = 0.000 10000.00000000 0.20000000-872450. 36089. -0.00005059 11 5 y = 0.3000 S = 0.000 10000.00000000 0.30000000-901558. 43364. -0.00012370 12 5 y = 0.5000 S = 0.000 10000.00000000 0.50000000-905605. 56035. -0.00036597 13 5 y = 0.7500 S = 0.000 10000.00000000 0.75000000

Page 69

existing phase1 81.lp6o-905613. 67964. -0.00078550 14 5 y = 1.0000 S = 0.000 10000.00000000 1.00000000-905583. 76263. -0.00132981

The analysis ended normally.

Page 70

Lateral Deflection (inches)D

epth

(ft)

-0.1 0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 10

12

34

56

78

910

1112

1314

1516

1718

19

Case 1Case 2Case 3Case 4Case 5Case 6Case 7Case 8Case 9Case 10Case 11Case 12Case 13Case 14

Bending Moment (in-kips)D

epth

(ft)

-1000 -800 -600 -400 -200 0 200 400 600 8000

12

34

56

78

910

1112

1314

1516

1718

19

Case 1Case 2Case 3Case 4Case 5Case 6Case 7Case 8Case 9Case 10Case 11Case 12Case 13Case 14

Shear Force (kips)D

epth

(ft)

-10 -5 0 5 10 15 20 25 30 35 40 45 50 55 600

12

34

56

78

910

1112

1314

1516

1718

19

Case 1Case 2Case 3Case 4Case 5Case 6Case 7Case 8Case 9Case 10Case 11Case 12Case 13Case 14

existing phase1 87.lp6o================================================================================

LPile Plus for Windows, Version 2012-06.037

Analysis of Individual Piles and Drilled Shafts Subjected to Lateral Loading Using the p-y Method

© 1985-2012 by Ensoft, Inc. All Rights Reserved

================================================================================

This copy of LPile is licensed to:

Dennis NguyenAECOM

Serial Number of Security Device: 160777832Company Name Stored in Security Device: AECOM (URS)

-------------------------------------------------------------------------------- Files Used for Analysis--------------------------------------------------------------------------------

Path to file locations:\\losangeles.na.aecomnet.com\LosAngeles\Projects\ENV\_legacy\GT\Da Wu\LA County Geotech On-call\MLK\Report\2019 BHC - Lab\Appendix F and G\Name of input data file: existing phase1 87.lp6dName of output report file: existing phase1 87.lp6oName of plot output file: existing phase1 87.lp6pName of runtime messeage file: existing phase1 87.lp6r

-------------------------------------------------------------------------------- Date and Time of Analysis--------------------------------------------------------------------------------

Date: March 12, 2019 Time: 13:39:30

-------------------------------------------------------------------------------- Problem Title--------------------------------------------------------------------------------

Project Name: MLK DHS Lab & Red Bag Storage

Job Number: 60595699

Client: LACDPW

Engineer: Dennis Nguyen

Description:

Page 1

existing phase1 87.lp6o

-------------------------------------------------------------------------------- Program Options--------------------------------------------------------------------------------

Engineering units are US Customary Units: pounds, inches, feet

Basic Program Options:

This analysis computes pile response to lateral loading and will compute nonlinear moment-curvature and nominal moment capacity for section types with nonlinear properties.

Computation Options:- Analysis does not use p-y multipliers (individual pile or shaft only)- Analysis assumes no shear resistance at pile tip- Analysis for fixed-length pile or shaft only- No computation of foundation stiffness matrix values- Report pile response for full length of pile- Analysis assumes no loading by soil movements acting on pile- p-y curves computed and reported at user-specified depths

Solution Control Parameters:- Number of pile increments = 100- Maximum number of iterations allowed = 100- Deflection tolerance for convergence = 1.0000E-05 in- Maximum allowable deflection = 100.0000 in

Pile Response Output Options:- Values of pile-head deflection, bending moment, shear force, and soil reaction are printed for full length of pile.- Printing Increment (nodal spacing of output points) = 1

-------------------------------------------------------------------------------- Pile Structural Properties and Geometry--------------------------------------------------------------------------------

Total number of pile sections = 1

Total length of pile = 20.00 ft

Depth of ground surface below top of pile = -5.50 ft

Pile diameter values used for p-y curve computations are defined using 2 points.

p-y curves are computed using pile diameter values interpolated with depth over the length of the pile.

Point Depth Pile X Diameter ft in----- --------- ----------- 1 0.00000 24.0000000 2 20.000000 24.0000000

Input Structural Properties:----------------------------

Page 2

existing phase1 87.lp6oPile Section No. 1:

Section Type = Drilled Shaft (Bored Pile) Section Length = 20.00000000 ft Section Diameter = 24.00000000 in

-------------------------------------------------------------------------------- Ground Slope and Pile Batter Angles--------------------------------------------------------------------------------

Ground Slope Angle = 0.000 degrees = 0.000 radians

Pile Batter Angle = 0.000 degrees = 0.000 radians

-------------------------------------------------------------------------------- Soil and Rock Layering Information--------------------------------------------------------------------------------

The soil profile is modelled using 6 layers

Layer 1 is sand, p-y criteria by Reese et al., 1974

Distance from top of pile to top of layer = -5.50000 ft Distance from top of pile to bottom of layer = 10.00000 ft Effective unit weight at top of layer = 125.00000 pcf Effective unit weight at bottom of layer = 125.00000 pcf Friction angle at top of layer = 28.00000 deg. Friction angle at bottom of layer = 28.00000 deg. Subgrade k at top of layer = 0.0000 pci Subgrade k at bottom of layer = 0.0000 pci

NOTE: Internal default values for subgrade k will be computed for the above soil layer.

Layer 2 is sand, p-y criteria by Reese et al., 1974

Distance from top of pile to top of layer = 10.00000 ft Distance from top of pile to bottom of layer = 15.00000 ft Effective unit weight at top of layer = 67.60000 pcf Effective unit weight at bottom of layer = 67.60000 pcf Friction angle at top of layer = 31.00000 deg. Friction angle at bottom of layer = 31.00000 deg. Subgrade k at top of layer = 0.0000 pci Subgrade k at bottom of layer = 0.0000 pci

NOTE: Internal default values for subgrade k will be computed for the above soil layer.

Layer 3 is sand, p-y criteria by Reese et al., 1974

Distance from top of pile to top of layer = 15.00000 ft Distance from top of pile to bottom of layer = 25.00000 ft Effective unit weight at top of layer = 62.60000 pcf Effective unit weight at bottom of layer = 62.60000 pcf Friction angle at top of layer = 30.00000 deg.

Page 3

existing phase1 87.lp6o Friction angle at bottom of layer = 30.00000 deg. Subgrade k at top of layer = 0.0000 pci Subgrade k at bottom of layer = 0.0000 pci

NOTE: Internal default values for subgrade k will be computed for the above soil layer.

Layer 4 is sand, p-y criteria by Reese et al., 1974

Distance from top of pile to top of layer = 25.00000 ft Distance from top of pile to bottom of layer = 40.00000 ft Effective unit weight at top of layer = 47.60000 pcf Effective unit weight at bottom of layer = 47.60000 pcf Friction angle at top of layer = 31.00000 deg. Friction angle at bottom of layer = 31.00000 deg. Subgrade k at top of layer = 0.0000 pci Subgrade k at bottom of layer = 0.0000 pci

NOTE: Internal default values for subgrade k will be computed for the above soil layer.

Layer 5 is soft clay, p-y criteria by Matlock, 1970

Distance from top of pile to top of layer = 40.00000 ft Distance from top of pile to bottom of layer = 49.00000 ft Effective unit weight at top of layer = 57.60000 pcf Effective unit weight at bottom of layer = 57.60000 pcf Undrained cohesion at top of layer = 1500.00000 psf Undrained cohesion at bottom of layer = 1500.00000 psf Epsilon-50 at top of layer = 0.0000 Epsilon-50 at bottom of layer = 0.0000

NOTE: Internal default values for Epsilon-50 will be computed for the above soil layer.

Layer 6 is sand, p-y criteria by Reese et al., 1974

Distance from top of pile to top of layer = 49.00000 ft Distance from top of pile to bottom of layer = 56.00000 ft Effective unit weight at top of layer = 62.60000 pcf Effective unit weight at bottom of layer = 62.60000 pcf Friction angle at top of layer = 31.00000 deg. Friction angle at bottom of layer = 31.00000 deg. Subgrade k at top of layer = 0.0000 pci Subgrade k at bottom of layer = 0.0000 pci

NOTE: Internal default values for subgrade k will be computed for the above soil layer.

(Depth of lowest soil layer extends 36.00 ft below pile tip)

-------------------------------------------------------------------------------- Summary of Soil Properties--------------------------------------------------------------------------------

Layer Layer Effective UndrainedAngle of Strain

Page 4

existing phase1 87.lp6oLayer Soil Type Depth Unit Wt. CohesionFriction Factor kpy Num. (p-y Curve Criteria) ft pcf psf deg. Epsilon 50 pci----- ---------------------------------- ---------- ---------- -------------------- ---------- ---------- 1 Sand (Reese, et al.) -5.500 125.000 -- 28.000 -- default 10.000 125.000 -- 28.000 -- default 2 Sand (Reese, et al.) 10.000 67.600 -- 31.000 -- default 15.000 67.600 -- 31.000 -- default 3 Sand (Reese, et al.) 15.000 62.600 -- 30.000 -- default 25.000 62.600 -- 30.000 -- default 4 Sand (Reese, et al.) 25.000 47.600 -- 31.000 -- default 40.000 47.600 -- 31.000 -- default 5 Soft Clay 40.000 57.600 1500.000 -- default -- 49.000 57.600 1500.000 -- default -- 6 Sand (Reese, et al.) 49.000 62.600 -- 31.000 -- default 56.000 62.600 -- 31.000 -- default

-------------------------------------------------------------------------------- Loading Type--------------------------------------------------------------------------------

Static loading criteria were used when computing p-y curves for all analyses.

-------------------------------------------------------------------------------- Pile-head Loading and Pile-head Fixity Conditions--------------------------------------------------------------------------------

Number of loads specified = 14

Load Load Condition Condition Axial Thrust Compute No. Type 1 2 Force, lbsTop y vs. Pile Length----- ---- -------------------- ----------------------- ------------------------------------- 1 4 y = 0.01000 in M = 0.0000 in-lbs 10000.00000000 No 2 4 y = 0.10000 in M = 0.0000 in-lbs 10000.00000000 No 3 4 y = 0.20000 in M = 0.0000 in-lbs 10000.00000000 No 4 4 y = 0.30000 in M = 0.0000 in-lbs 10000.00000000 No 5 4 y = 0.50000 in M = 0.0000 in-lbs 10000.00000000 No

Page 5

existing phase1 87.lp6o 6 4 y = 0.75000 in M = 0.0000 in-lbs 10000.00000000 No 7 4 y = 1.00000 in M = 0.0000 in-lbs 10000.00000000 No 8 4 y = 0.01000 in M = 0.0000 in-lbs 10000.00000000 No 9 5 y = 0.10000 in S = 0.0000 in/in 10000.00000000 No 10 5 y = 0.20000 in S = 0.0000 in/in 10000.00000000 No 11 5 y = 0.30000 in S = 0.0000 in/in 10000.00000000 No 12 5 y = 0.50000 in S = 0.0000 in/in 10000.00000000 No 13 5 y = 0.75000 in S = 0.0000 in/in 10000.00000000 No 14 5 y = 1.00000 in S = 0.0000 in/in 10000.00000000 No

V = perpendicular shear force applied to pile headM = bending moment applied to pile heady = lateral deflection relative to pile axisS = pile slope relative to original pile batter angleR = rotational stiffness applie to pile headAxial thrust is assumed to be acting axially for all pile batter angles.

-------------------------------------------------------------------------------- Specified Depths for Output of p-y Curves--------------------------------------------------------------------------------

Lateral load-transfer (p-y) curves are computed and output at 5 depths.(Note that these curves are independent from the curves used at nodal point depths)

Depth Depth Below Pile Head Depth Below Ground Surface No. ft ft----- --------------------- -------------------------- 1 1.000 6.500 2 5.000 10.500 3 10.000 15.500 4 15.000 20.500 5 19.000 24.500

Depth of ground surface below top of pile = -5.50 ft

-------------------------------------------------------------------------------- Computations of Nominal Moment Capacity and Nonlinear Bending Stiffness--------------------------------------------------------------------------------

Axial thrust force values were determined from pile-head loading conditions

Number of Pile Sections Analyzed = 1

Pile Section No. 1:-------------------

Dimensions and Properties of Drilled Shaft (Bored Pile):--------------------------------------------------------

Page 6

existing phase1 87.lp6oLength of Section = 20.00000000 ftShaft Diameter = 24.00000000 inConcrete Cover Thickness = 3.00000000 inNumber of Reinforcing Bars = 12 barsYield Stress of Reinforcing Bars = 60.00000000 ksiModulus of Elasticity of Reinforcing Bars = 29000. ksiGross Area of Shaft = 452.38934212 sq. in.Total Area of Reinforcing Steel = 1.32000000 sq. in.Area Ratio of Steel Reinforcement = 0.29 percentEdge-to-Edge Bar Spacing = 4.18668567 inMaximum Concrete Aggregate Size = 0.75000000 inRatio of Bar Spacing to Aggregate Size = 5.58Offset of Rebar Cage Center from Center of Pile = 0.0000000 in

Axial Structural Capacities:----------------------------

Nom. Axial Structural Capacity = 0.85 Fc Ac + Fy As = 1229.427 kipsTensile Load for Cracking of Concrete = -167.736 kipsNominal Axial Tensile Capacity = -79.200 kips

Reinforcing Bar Dimensions and Positions Used in Computations:

Bar Bar Diam. Bar Area X Y Number inches sq. in. inches inches ---------- ---------- ---------- ---------- ---------- 1 0.37500 0.11000 8.81250 0.00000 2 0.37500 0.11000 7.63185 4.40625 3 0.37500 0.11000 4.40625 7.63185 4 0.37500 0.11000 0.00000 8.81250 5 0.37500 0.11000 -4.40625 7.63185 6 0.37500 0.11000 -7.63185 4.40625 7 0.37500 0.11000 -8.81250 0.00000 8 0.37500 0.11000 -7.63185 -4.40625 9 0.37500 0.11000 -4.40625 -7.63185 10 0.37500 0.11000 0.00000 -8.81250 11 0.37500 0.11000 4.40625 -7.63185 12 0.37500 0.11000 7.63185 -4.40625

NOTE: The positions of the above rebars were computed by LPile

Minimum spacing between any two bars not equal to zero = 4.18669 inches betweenBars 7 and 8

Spacing to aggregate size ratio = 5.58225

Concrete Properties:--------------------

Compressive Strength of Concrete = 3.00000000 ksiModulus of Elasticity of Concrete = 3122.01857778 ksiModulus of Rupture of Concrete = -0.41079191 ksiCompression Strain at Peak Stress = 0.00163356Tensile Strain at Fracture of Concrete = -0.00011596Maximum Coarse Aggregate Size = 0.75000000 in

Number of Axial Thrust Force Values Determined from Pile-head Loadings = 1

Number Axial Thrust ForcePage 7

existing phase1 87.lp6o kips ------ ------------------ 1 10.000

Definitions of Run Messages and Notes:--------------------------------------

C = concrete in section has cracked in tension. Y = stress in reinforcing steel has reached yield stress. T = ACI 318-08 criteria for tension-controlled section met, tensile strain in reinforcement exceeds 0.005 while simultaneously compressive strain in concrete more than than 0.003. See ACI 318-08, Section 10.3.4. Z = depth of tensile zone in concrete section is less than 10 percent of section depth.

Bending Stiffness (EI) = Computed Bending Moment / Curvature.Position of neutral axis is measured from edge of compression side of pile.Compressive stresses and strains are positive in sign.Tensile stresses and strains are negative in sign.

Axial Thrust Force = 10.000 kips

Bending Bending Bending Depth to Max Comp Max Tens Max Concrete Max Steel Run Curvature Moment Stiffness N Axis Strain Strain Stress Stress Msg rad/in. in-kip kip-in2 in in/in in/in ksi ksi ------------- ------------- ------------- ------------- ------------- -------------------------- ------------- --- 0.000001250 76.0873440 60869875. 16.7390877 0.0000209 -0.000009076 0.0758165 0.6024419 0.000002500 151.7934938 60717398. 14.3782869 0.0000359 -0.0000241 0.1294969 1.0337258 0.000003750 227.0367332 60543129. 13.5915522 0.0000510 -0.0000390 0.1826828 1.4650313 0.000005000 301.8152914 60363058. 13.1982492 0.0000660 -0.0000540 0.2353724 1.8963461 0.000006250 376.1289456 60180631. 12.9623053 0.0000810 -0.0000690 0.2875655 2.3276679 0.000007500 449.9776413 59997019. 12.8050375 0.0000960 -0.0000840 0.3392620 2.7589957 0.000008750 523.3613581 59812727. 12.6927260 0.0001111 -0.0000989 0.3904617 3.1903293 0.0000100 596.2800896 59628009. 12.6085121 0.0001261 -0.0001139 0.4411647 3.6216685 0.0000113 596.2800896 53002675. 6.8532370 0.0000771 -0.0001929 0.2717723 -5.5549814 C 0.0000125 596.2800896 47702407. 6.6410432 0.0000830 -0.0002170 0.2919246 -6.2491219 C 0.0000138 596.2800896 43365825. 6.4607446 0.0000888 -0.0002412 0.3116826 -6.9459281 C 0.0000150 596.2800896 39752006. 6.3064990 0.0000946 -0.0002654 0.3311606 -7.6444729 C 0.0000163 596.2800896 36694159. 6.1718983 0.0001003 -0.0002897 0.3503387 -8.3449429 C 0.0000175 596.2800896 34073148. 6.0533951 0.0001059 -0.0003141 0.3692591 -9.0470019 C 0.0000188 596.2800896 31801605. 5.9485044 0.0001115 -0.0003385 0.3879711 -9.7502507 C 0.0000200 596.2800896 29814004. 5.8556156 0.0001171 -0.0003629

Page 8

existing phase1 87.lp6o 0.4065405 -10.4541429 C 0.0000213 596.2800896 28060240. 5.7705071 0.0001226 -0.0003874 0.4248161 -11.1599749 C 0.0000225 596.2800896 26501337. 5.6949845 0.0001281 -0.0004119 0.4430370 -11.8657226 C 0.0000238 596.2800896 25106530. 5.6268263 0.0001336 -0.0004364 0.4611462 -12.5718733 C 0.0000250 596.2800896 23851204. 5.5627914 0.0001391 -0.0004609 0.4789643 -13.2799762 C 0.0000263 596.2800896 22715432. 5.5049647 0.0001445 -0.0004855 0.4967294 -13.9879955 C 0.0000275 596.2800896 21682912. 5.4524998 0.0001499 -0.0005101 0.5144414 -14.6959313 C 0.0000288 596.2800896 20740177. 5.4046976 0.0001554 -0.0005346 0.5321000 -15.4037833 C 0.0000300 596.2800896 19876003. 5.3586531 0.0001608 -0.0005592 0.5494741 -16.1135717 C 0.0000313 596.2800896 19080963. 5.3161276 0.0001661 -0.0005839 0.5667697 -16.8235093 C 0.0000325 596.2800896 18347080. 5.2769621 0.0001715 -0.0006085 0.5840137 -17.5333631 C 0.0000338 596.2800896 17667558. 5.2407837 0.0001769 -0.0006331 0.6012058 -18.2431328 C 0.0000350 596.2800896 17036574. 5.2072725 0.0001823 -0.0006577 0.6183461 -18.9528183 C 0.0000363 596.2800896 16449106. 5.1761527 0.0001876 -0.0006824 0.6354344 -19.6624194 C 0.0000375 596.2800896 15900802. 5.1463845 0.0001930 -0.0007070 0.6523730 -20.3728068 C 0.0000388 596.2800896 15387873. 5.1176695 0.0001983 -0.0007317 0.6691420 -21.0841687 C 0.0000400 596.2800896 14907002. 5.0908231 0.0002036 -0.0007564 0.6858604 -21.7954451 C 0.0000413 596.2800896 14455275. 5.0656756 0.0002090 -0.0007810 0.7025282 -22.5066355 C 0.0000425 596.2800896 14030120. 5.0420771 0.0002143 -0.0008057 0.7191452 -23.2177398 C 0.0000438 596.2800896 13629259. 5.0198952 0.0002196 -0.0008304 0.7357114 -23.9287578 C 0.0000450 596.2800896 13250669. 4.9990120 0.0002250 -0.0008550 0.7522267 -24.6396892 C 0.0000463 596.2800896 12892542. 4.9793223 0.0002303 -0.0008797 0.7686910 -25.3505338 C 0.0000475 596.2800896 12553265. 4.9607321 0.0002356 -0.0009044 0.7851043 -26.0612913 C 0.0000488 596.2800896 12231386. 4.9431570 0.0002410 -0.0009290 0.8014665 -26.7719616 C 0.0000513 596.2800896 11634733. 4.9101443 0.0002516 -0.0009784 0.8339394 -28.1939480 C 0.0000538 596.2800896 11093583. 4.8790479 0.0002622 -0.0010278 0.8659784 -29.6177339 C 0.0000563 596.2800896 10600535. 4.8509378 0.0002729 -0.0010771 0.8978171 -31.0411575 C 0.0000588 596.2800896 10149448. 4.8254339 0.0002835 -0.0011265 0.9294549 -32.4642168 C 0.0000613 596.2800896 9735185. 4.8022184 0.0002941 -0.0011759 0.9608910 -33.8869094 C 0.0000638 596.2800896 9353413. 4.7810231 0.0003048 -0.0012252 0.9921249 -35.3092333 C 0.0000663 596.2800896 9000454. 4.7616206 0.0003155 -0.0012745 1.0231559 -36.7311862 C 0.0000688 596.2800896 8673165. 4.7438164 0.0003261 -0.0013239 1.0539833 -38.1527659 C

Page 9

existing phase1 87.lp6o 0.0000713 596.2800896 8368843. 4.7274433 0.0003368 -0.0013732 1.0846065 -39.5739700 C 0.0000738 596.2800896 8085154. 4.7123570 0.0003475 -0.0014225 1.1150247 -40.9947963 C 0.0000763 596.2800896 7820067. 4.6984319 0.0003583 -0.0014717 1.1452373 -42.4152423 C 0.0000788 596.2800896 7571811. 4.6855583 0.0003690 -0.0015210 1.1752436 -43.8353059 C 0.0000813 596.2800896 7338832. 4.6731874 0.0003797 -0.0015703 1.2049383 -45.2560520 C 0.0000838 596.2800896 7119762. 4.6613503 0.0003904 -0.0016196 1.2343412 -46.6772951 C 0.0000863 596.2800896 6913392. 4.6503625 0.0004011 -0.0016689 1.2635405 -48.0981306 C 0.0000888 596.2800896 6718649. 4.6401531 0.0004118 -0.0017182 1.2925356 -49.5185556 C 0.0000913 596.2800896 6534576. 4.6306594 0.0004225 -0.0017675 1.3213257 -50.9385674 C 0.0000938 596.2800896 6360321. 4.6218250 0.0004333 -0.0018167 1.3499101 -52.3581630 C 0.0000963 596.2800896 6195118. 4.6135996 0.0004441 -0.0018659 1.3782881 -53.7773397 C 0.0000988 596.2800896 6038279. 4.6059381 0.0004548 -0.0019152 1.4064588 -55.1960945 C 0.0001013 596.2800896 5889186. 4.5987996 0.0004656 -0.0019644 1.4344217 -56.6144243 C 0.0001038 596.2800896 5747278. 4.5921474 0.0004764 -0.0020136 1.4621758 -58.0323263 C 0.0001063 596.2800896 5612048. 4.5859480 0.0004873 -0.0020627 1.4897204 -59.4497974 C 0.0001088 596.2800896 5483035. 4.5801713 0.0004981 -0.0021119 1.5170547 -60.0000000 CY 0.0001113 596.2800896 5359821. 4.5747897 0.0005089 -0.0021611 1.5441778 -60.0000000 CY 0.0001138 596.2800896 5242023. 4.5697781 0.0005198 -0.0022102 1.5710892 -60.0000000 CY 0.0001163 605.1262719 5205387. 4.5651137 0.0005307 -0.0022593 1.5977880 -60.0000000 CY 0.0001188 616.2166766 5189193. 4.5607753 0.0005416 -0.0023084 1.6242734 -60.0000000 CY 0.0001213 627.2967561 5173581. 4.5567439 0.0005525 -0.0023575 1.6505444 -60.0000000 CY 0.0001238 638.3664441 5158517. 4.5530017 0.0005634 -0.0024066 1.6766003 -60.0000000 CY 0.0001263 649.3102714 5143052. 4.5492886 0.0005743 -0.0024557 1.7023659 -60.0000000 CY 0.0001288 659.0459991 5118804. 4.5433314 0.0005850 -0.0025050 1.7271428 -60.0000000 CY 0.0001313 667.9088616 5088829. 4.5359197 0.0005953 -0.0025547 1.7511578 -60.0000000 CY 0.0001338 676.7549988 5059850. 4.5288687 0.0006057 -0.0026043 1.7749703 -60.0000000 CY 0.0001363 685.1641051 5028727. 4.5212629 0.0006160 -0.0026540 1.7982959 -60.0000000 CY 0.0001388 691.3993484 4983058. 4.5094436 0.0006257 -0.0027043 1.8199634 -60.0000000 CY 0.0001413 696.2920527 4929501. 4.4953197 0.0006350 -0.0027550 1.8405557 -60.0000000 CY 0.0001438 701.1797625 4877772. 4.4817545 0.0006443 -0.0028057 1.8609887 -60.0000000 CY 0.0001463 706.0624537 4827777. 4.4687196 0.0006536 -0.0028564 1.8812620 -60.0000000 CY 0.0001488 710.9401018 4779429. 4.4561888 0.0006629 -0.0029071

Page 10

existing phase1 87.lp6o 1.9013749 -60.0000000 CY 0.0001588 730.3435779 4600589. 4.4082369 0.0006998 -0.0031102 1.9793984 -60.0000000 CY 0.0001688 749.6077413 4442120. 4.3657018 0.0007367 -0.0033133 2.0544559 -60.0000000 CY 0.0001788 761.4479657 4259849. 4.3120389 0.0007708 -0.0035192 2.1210101 -60.0000000 CY 0.0001888 769.9967030 4079453. 4.2576705 0.0008036 -0.0037264 2.1828247 -60.0000000 CY 0.0001988 778.4996230 3916979. 4.2093895 0.0008366 -0.0039334 2.2426119 -60.0000000 CY 0.0002088 786.8480316 3769332. 4.1631469 0.0008691 -0.0041409 2.2991694 -60.0000000 CY 0.0002188 795.1252195 3634858. 4.1208986 0.0009014 -0.0043486 2.3534458 -60.0000000 CY 0.0002288 803.3586649 3511950. 4.0828946 0.0009340 -0.0045560 2.4057405 -60.0000000 CY 0.0002388 811.5477668 3399153. 4.0486107 0.0009666 -0.0047634 2.4560307 -60.0000000 CY 0.0002488 819.6916977 3295243. 4.0176074 0.0009994 -0.0049706 2.5042925 -60.0000000 CY 0.0002588 826.7932787 3195336. 3.9868321 0.0010316 -0.0051784 2.5495145 -60.0000000 CY 0.0002688 830.5391163 3090378. 3.9490801 0.0010613 -0.0053887 2.5891959 -60.0000000 CY 0.0002788 833.3685080 2989663. 3.9094511 0.0010898 -0.0056002 2.6253910 -60.0000000 CY 0.0002888 836.1741864 2895841. 3.8729171 0.0011183 -0.0058117 2.6600421 -60.0000000 CY 0.0002988 838.9557505 2808220. 3.8391717 0.0011470 -0.0060230 2.6931323 -60.0000000 CY 0.0003088 841.7127586 2726195. 3.8079485 0.0011757 -0.0062343 2.7246440 -60.0000000 CY 0.0003188 844.4447587 2649238. 3.7790144 0.0012046 -0.0064454 2.7545595 -60.0000000 CY 0.0003288 847.1512884 2576886. 3.7521652 0.0012335 -0.0066565 2.7828607 -60.0000000 CY 0.0003388 849.8318743 2508729. 3.7272206 0.0012626 -0.0068674 2.8095289 -60.0000000 CY 0.0003488 852.4089989 2444184. 3.7019733 0.0012911 -0.0070789 2.8339284 -60.0000000 CY 0.0003588 854.9293167 2383078. 3.6775697 0.0013193 -0.0072907 2.8564940 -60.0000000 CY 0.0003688 857.4258218 2325223. 3.6547894 0.0013477 -0.0075023 2.8774944 -60.0000000 CY 0.0003788 859.8982795 2270358. 3.6335086 0.0013762 -0.0077138 2.8969109 -60.0000000 CY 0.0003888 862.3462346 2218254. 3.6136169 0.0014048 -0.0079252 2.9147240 -60.0000000 CY 0.0003988 864.7692188 2168700. 3.5950147 0.0014335 -0.0081365 2.9309136 -60.0000000 CY 0.0004088 867.1667493 2121509. 3.5776127 0.0014623 -0.0083477 2.9454593 -60.0000000 CY 0.0004188 869.5383287 2076509. 3.5613301 0.0014913 -0.0085587 2.9583399 -60.0000000 CY 0.0004288 871.8834435 2033547. 3.5460940 0.0015204 -0.0087696 2.9695336 -60.0000000 CY 0.0004388 874.2015639 1992482. 3.5318382 0.0015496 -0.0089804 2.9790181 -60.0000000 CY 0.0004488 876.4921423 1953186. 3.5185030 0.0015789 -0.0091911 2.9867702 -60.0000000 CY 0.0004588 878.7546127 1915541. 3.5060336 0.0016084 -0.0094016 2.9927662 -60.0000000 CY

Page 11

existing phase1 87.lp6o 0.0004688 880.9883893 1879442. 3.4943806 0.0016380 -0.0096120 2.9969814 -60.0000000 CY 0.0004788 883.1928657 1844789. 3.4834988 0.0016677 -0.0098223 2.9993905 -60.0000000 CY 0.0004888 885.0224976 1810788. 3.4709132 0.0016964 -0.0100336 2.9991276 -60.0000000 CY 0.0004988 886.7873237 1778020. 3.4585692 0.0017250 -0.0102450 2.9934460 -60.0000000 CY 0.0005088 887.9821732 1745420. 3.4444561 0.0017524 -0.0104576 2.9953459 -60.0000000 CY 0.0005188 888.6173409 1712997. 3.4286611 0.0017786 -0.0106714 2.9980460 -60.0000000 CY 0.0005288 889.2382922 1681775. 3.4136627 0.0018050 -0.0108850 2.9995970 -60.0000000 CY 0.0005388 889.7845008 1651572. 3.3991749 0.0018313 -0.0110987 2.9992113 -60.0000000 CY 0.0005488 890.3014535 1622417. 3.3854861 0.0018578 -0.0113122 2.9944588 -60.0000000 CY 0.0006088 893.1490543 1467185. 3.3161623 0.0020187 -0.0125913 2.9958655 -60.0000000 CY 0.0006688 895.5530431 1339145. 3.2646906 0.0021833 -0.0138667 2.9998368 60.0000000 CY 0.0007288 897.4916889 1231549. 3.2233026 0.0023490 -0.0151410 2.9942323 60.0000000 CY 0.0007888 899.0579811 1139852. 3.1874194 0.0025141 -0.0164159 2.9940451 60.0000000 CY 0.0008488 900.3958393 1060849. 3.1601255 0.0026822 -0.0176878 2.9942121 60.0000000 CY 0.0009088 901.5573161 992085. 3.1392881 0.0028528 -0.0189572 2.9959040 60.0000000 CY 0.0009688 902.5306344 931645. 3.1239428 0.0030263 -0.0202237 2.9842164 60.0000000 CYT 0.0010288 903.3885835 878142. 3.1123773 0.0032019 -0.0214881 2.9984981 60.0000000 CYT 0.0010888 904.0891823 830392. 3.1045829 0.0033801 -0.0227499 2.9900077 60.0000000 CYT 0.0011488 904.6758641 787531. 3.0995034 0.0035606 -0.0240094 2.9777273 60.0000000 CYT 0.0012088 905.1776403 748854. 3.0964534 0.0037428 -0.0252672 2.9950328 60.0000000 CYT 0.0012688 905.5777865 713756. 3.0954236 0.0039273 -0.0265227 2.9979209 60.0000000 CYT

-------------------------------------------------------------------------------- Summary of Results for Nominal (Unfactored) Moment Capacity for Section 1--------------------------------------------------------------------------------

Moment values interpolated at maximum compressive strain = 0.003or maximum developed moment if pile fails at smaller strains.

Load Axial Thrust Nominal Mom. Cap. Max. Comp. No. kips in-kip Strain ---- ---------------- ------------------ ------------ 1 10.000 902.383 0.00300000

Note note that the values of moment capacity in the table above are not factored by a strength reduction factor (phi-factor).

In ACI 318-08, the value of the strength reduction factor depends on whether the transverse reinforcing steel bars are tied hoops (0.65) or spirals (0.70).

The above values should be multiplied by the appropriate strength reduction Page 12

existing phase1 87.lp6ofactor to compute ultimate moment capacity according to ACI 318-08, Section 9.3.2.2 or the value required by the design standard being followed.

The following table presents factored moment capacities and corresponding bending stiffnesses computed for common resistance factor values used for reinforced concrete sections.

Axial Resistance Nominal Ultimate (Factored) Ultimate (Factored) Bending Stiffness Load Factor Moment Capacity Axial Thrust Moment Capacity at Ult. Mom. Cap. No. for Moment in-kip kipsin-kip kip-in^2 ----- ---------- ------------------- -------------------------------------- ------------------- 1 0.65 902.383 6.500586.549 59652659.965

1 0.70 902.383 7.000631.668 5167632.554

1 0.75 902.383 7.500676.787 5059731.157

-------------------------------------------------------------------------------- p-y Curves Reported for Specified Depths--------------------------------------------------------------------------------

p-y Curve in Sand Computed Using Reese Criteria for Static Loading Conditions

Soil Layer Number = 1Depth below pile head = 1.000 ftDepth below ground surface = 6.500 ftEquivalent Depth (see note) = 6.500 ftGround Slope Angle = 0.000 degreesPile Batter = 0.000 degreesEffective Slope = 0.000 degreesPile Diameter, b = 24.000 inAngle of Friction = 28.000 degreesAvg. Eff. Unit Weight = 125.00000 pcfkpy = 21.063 pciK active = 0.361K passive = 2.770K0 = 0.400Pst = 1030.122 lbs/inPsd = 3049.664 lbs/inPs = Pst (shallow controls) = 1030.122 lbs/inA (static) = 1.0200B (static) = 0.6650C = Pm/(Ym^(1/n)) = 1013.1127n = Pm/(m Ym) = 2.3415m = (Pu-Pm)/(Yu-Ym) = 731.3868Yk = [c/(kx)]^(n/(n-1)) = 0.4301 inPk = 706.570 lbs/inYm = b/60 = 0.4000 inPm = B ps = 685.031 lbs/inYu = 3b/80 = 0.9000 inPu = A Ps = 1050.725 lbs/inEs,lim = 1642.910 lbs/in/inp-multiplier = 1.00000y-multiplier = 1.00000

Page 13

existing phase1 87.lp6o

This p-y curve is computed using the equivalent depth.

This curve has a tri-linear shape for a Reese sand p-y curve because Ym < Yk < Yu.

y, in p, lbs/in---------------- ----------------- 0.0000 0.0000 0.43007 706.56994 * 0.46622 733.46420 0.50237 759.90258 0.53852 786.34097 0.57467 812.77935 0.61081 839.21773 0.64696 865.65611 0.68311 892.09450 0.71926 918.53288 0.75541 944.97126 0.79156 971.40964 0.82770 997.84803 0.86385 1024.28641 0.90000 1050.72479 0.92250 1050.72479 0.94500 1050.72479

* p value(s) computed using p = k * Eff x * y

The above p-y curve was computed using internal default values of k.

p-y Curve in Sand Computed Using Reese Criteria for Static Loading Conditions

Soil Layer Number = 1Depth below pile head = 5.000 ftDepth below ground surface = 10.500 ftEquivalent Depth (see note) = 10.500 ftGround Slope Angle = 0.000 degreesPile Batter = 0.000 degreesEffective Slope = 0.000 degreesPile Diameter, b = 24.000 inAngle of Friction = 28.000 degreesAvg. Eff. Unit Weight = 125.00000 pcfkpy = 21.063 pciK active = 0.361K passive = 2.770K0 = 0.400Pst = 2363.810 lbs/inPsd = 4926.380 lbs/inPs = Pst (shallow controls) = 2363.810 lbs/inA (static) = 0.8800B (static) = 0.5000C = Pm/(Ym^(1/n)) = 2063.1469n = Pm/(m Ym) = 1.6447m = (Pu-Pm)/(Yu-Ym) = 1796.4958Yk = [c/(kx)]^(n/(n-1)) = 0.5260 inPk = 1396.083 lbs/inYm = b/60 = 0.4000 inPm = B ps = 1181.905 lbs/inYu = 3b/80 = 0.9000 inPu = A Ps = 2080.153 lbs/inEs,lim = 2653.931 lbs/in/inp-multiplier = 1.00000

Page 14

existing phase1 87.lp6oy-multiplier = 1.00000

This p-y curve is computed using the equivalent depth.

This curve has a tri-linear shape for a Reese sand p-y curve because Ym < Yk < Yu.

y, in p, lbs/in---------------- ----------------- 0.0000 0.0000 0.52604 1396.08316 * 0.55481 1460.01946 0.58358 1511.69726 0.61234 1563.37506 0.64111 1615.05286 0.66987 1666.73066 0.69864 1718.40846 0.72740 1770.08626 0.75617 1821.76406 0.78494 1873.44186 0.81370 1925.11966 0.84247 1976.79746 0.87123 2028.47526 0.90000 2080.15306 0.92250 2080.15306 0.94500 2080.15306

* p value(s) computed using p = k * Eff x * y

The above p-y curve was computed using internal default values of k.

p-y Curve in Sand Computed Using Reese Criteria for Static Loading Conditions

Soil Layer Number = 2Depth below pile head = 10.000 ftDepth below ground surface = 15.500 ftEquivalent Depth (see note) = 16.240 ftGround Slope Angle = 0.000 degreesPile Batter = 0.000 degreesEffective Slope = 0.000 degreesPile Diameter, b = 24.000 inAngle of Friction = 29.500 degreesAvg. Eff. Unit Weight = 125.00000 pcfkpy = 28.352 pciK active = 0.340K passive = 2.940K0 = 0.400Pst = 5903.800 lbs/inPsd = 8730.440 lbs/inPs = Pst (shallow controls) = 5903.800 lbs/inA (static) = 0.8800B (static) = 0.5000C = Pm/(Ym^(1/n)) = 5152.8701n = Pm/(m Ym) = 1.6447m = (Pu-Pm)/(Yu-Ym) = 4486.8883Yk = [c/(kx)]^(n/(n-1)) = 0.8369 inPk = 4624.300 lbs/inYm = b/60 = 0.4000 inPm = B ps = 2951.900 lbs/in

Page 15

existing phase1 87.lp6oYu = 3b/80 = 0.9000 inPu = A Ps = 5195.344 lbs/inEs,lim = 5525.275 lbs/in/inp-multiplier = 1.00000y-multiplier = 1.00000

This p-y curve is computed using the equivalent depth.

This curve has a tri-linear shape for a Reese sand p-y curve because Ym < Yk < Yu.

y, in p, lbs/in---------------- ----------------- 0.0000 0.0000 0.83694 4624.29955 * 0.84179 4651.10325 * 0.84664 4677.90695 * 0.85149 4704.71066 * 0.85634 4731.51436 * 0.86119 4758.31806 * 0.86604 4785.12177 * 0.87089 4811.92547 * 0.87574 4838.72917 * 0.88060 4865.53288 * 0.88545 4892.33658 * 0.89030 4919.14028 * 0.89515 4945.94398 * 0.90000 4972.74769 * 0.94029 5195.34435 0.94500 5195.34435

* p value(s) computed using p = k * Eff x * y

The above p-y curve was computed using internal default values of k.

p-y Curve in Sand Computed Using Reese Criteria for Static Loading Conditions

Soil Layer Number = 3Depth below pile head = 15.000 ftDepth below ground surface = 20.500 ftEquivalent Depth (see note) = 21.749 ftGround Slope Angle = 0.000 degreesPile Batter = 0.000 degreesEffective Slope = 0.000 degreesPile Diameter, b = 24.000 inAngle of Friction = 30.500 degreesAvg. Eff. Unit Weight = 111.00000 pcfkpy = 34.279 pciK active = 0.327K passive = 3.061K0 = 0.400Pst = 9843.496 lbs/inPsd = 11593.113 lbs/inPs = Pst (shallow controls) = 9843.496 lbs/inA (static) = 0.8800B (static) = 0.5000C = Pm/(Ym^(1/n)) = 8591.4584n = Pm/(m Ym) = 1.6447m = (Pu-Pm)/(Yu-Ym) = 7481.0568

Page 16

existing phase1 87.lp6oYk = [c/(kx)]^(n/(n-1)) = 0.9019 inPk = 8068.909 lbs/inYm = b/60 = 0.4000 inPm = B ps = 4921.748 lbs/inYu = 3b/80 = 0.9000 inPu = A Ps = 8662.276 lbs/inEs,lim = 8946.173 lbs/in/inp-multiplier = 1.00000y-multiplier = 1.00000

This p-y curve is computed using the equivalent depth.

This curve has a bi-linear shape for a Reese sand p-y curve because Ym < Yu < Yk.

y, in p, lbs/in---------------- ----------------- 0.0000 0.0000 0.06916 618.73402 * 0.13832 1237.46805 * 0.20749 1856.20207 * 0.27665 2474.93610 * 0.34581 3093.67012 * 0.41497 3712.40415 * 0.48413 4331.13817 * 0.55329 4949.87220 * 0.62246 5568.60622 * 0.69162 6187.34025 * 0.76078 6806.07427 * 0.82994 7424.80829 * 0.89910 8043.54232 * 0.96827 8662.27634 0.99247 8662.27634 1.01668 8662.27634

* p value(s) computed using p = k * Eff x * y

The above p-y curve was computed using internal default values of k.

p-y Curve in Sand Computed Using Reese Criteria for Static Loading Conditions

Soil Layer Number = 3Depth below pile head = 19.000 ftDepth below ground surface = 24.500 ftEquivalent Depth (see note) = 25.749 ftGround Slope Angle = 0.000 degreesPile Batter = 0.000 degreesEffective Slope = 0.000 degreesPile Diameter, b = 24.000 inAngle of Friction = 30.000 degreesAvg. Eff. Unit Weight = 103.09796 pcfkpy = 31.199 pciK active = 0.333K passive = 3.000K0 = 0.400Pst = 12069.180 lbs/inPsd = 12101.220 lbs/inPs = Pst (shallow controls) = 12069.180 lbs/inA (static) = 0.8800B (static) = 0.5000C = Pm/(Ym^(1/n)) = 10534.0482n = Pm/(m Ym) = 1.6447

Page 17

existing phase1 87.lp6om = (Pu-Pm)/(Yu-Ym) = 9172.5769Yk = [c/(kx)]^(n/(n-1)) = 1.2539 inPk = 12087.370 lbs/inYm = b/60 = 0.4000 inPm = B ps = 6034.590 lbs/inYu = 3b/80 = 0.9000 inPu = A Ps = 10620.879 lbs/inEs,lim = 9640.087 lbs/in/inp-multiplier = 1.00000y-multiplier = 1.00000

This p-y curve is computed using the equivalent depth.

This curve has a bi-linear shape for a Reese sand p-y curve because Ym < Yu < Yk.

y, in p, lbs/in---------------- ----------------- 0.0000 0.0000 0.07870 758.63418 * 0.15739 1517.26837 * 0.23609 2275.90255 * 0.31478 3034.53674 * 0.39348 3793.17092 * 0.47217 4551.80511 * 0.55087 5310.43929 * 0.62957 6069.07348 * 0.70826 6827.70766 * 0.78696 7586.34185 * 0.86565 8344.97603 * 0.94435 9103.61022 * 1.02305 9862.24440 * 1.10174 10621. * 1.12928 10621. 1.15683 10621.

* p value(s) computed using p = k * Eff x * y

The above p-y curve was computed using internal default values of k.

-------------------------------------------------------------------------------- Computed Values of Pile Loading and Deflection for Lateral Loading for Load Case Number 1--------------------------------------------------------------------------------

Pile-head conditions are Displacement and Moment (Loading Type 4)Displacement of pile head = 0.010000 inchesMoment at pile head = 0.000 in-lbsAxial load at pile head = 10000.000 lbs

Depth Deflect. Bending Shear Slope Total Bending Soil Res. Soil Spr. Distrib. X y Moment Force S Stress Stiffness p Es*h Lat. Load feet inches in-lbs lbs radians psi* lb-in^2 lb/in lb/inch lb/inch ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- 0.00 0.0100 0.000 1064.8147 -9.980E-05 0.000 6.087E+10

Page 18

existing phase1 87.lp6o-13.9015 1668.1854 0.000 0.200 0.009760 2517.9140 1031.2585 -9.975E-05 0.000 6.087E+10-14.0620 3457.6934 0.000 0.400 0.009521 4954.8285 997.3458 -9.960E-05 0.000 6.087E+10-14.1986 3579.0160 0.000 0.600 0.009282 7309.9545 963.1335 -9.936E-05 0.000 6.087E+10-14.3117 3700.3385 0.000 0.800 0.009044 9582.6383 928.6773 -9.902E-05 0.000 6.087E+10-14.4018 3821.6611 0.000 1.000 0.008807 11772. 894.0321 -9.860E-05 0.000 6.087E+10-14.4693 3942.9837 0.000 1.200 0.008571 13879. 859.2514 -9.810E-05 0.000 6.087E+10-14.5146 4064.3063 0.000 1.400 0.008336 15901. 824.3877 -9.751E-05 0.000 6.087E+10-14.5385 4185.6288 0.000 1.600 0.008103 17840. 789.4920 -9.685E-05 0.000 6.087E+10-14.5412 4306.9514 0.000 1.800 0.007871 19696. 754.6143 -9.611E-05 0.000 6.087E+10-14.5236 4428.2740 0.000 2.000 0.007642 21467. 719.8029 -9.529E-05 0.000 6.087E+10-14.4860 4549.5966 0.000 2.200 0.007414 23155. 685.1047 -9.441E-05 0.000 6.087E+10-14.4291 4670.9191 0.000 2.400 0.007188 24760. 650.5654 -9.347E-05 0.000 6.087E+10-14.3536 4792.2417 0.000 2.600 0.006965 26283. 616.2288 -9.246E-05 0.000 6.087E+10-14.2602 4913.5643 0.000 2.800 0.006745 27723. 582.1374 -9.140E-05 0.000 6.087E+10-14.1493 5034.8869 0.000 3.000 0.006527 29081. 548.3321 -9.028E-05 0.000 6.087E+10-14.0218 5156.2094 0.000 3.200 0.006311 30359. 514.8519 -8.911E-05 0.000 6.087E+10-13.8783 5277.5320 0.000 3.400 0.006099 31557. 481.7345 -8.789E-05 0.000 6.087E+10-13.7195 5398.8546 0.000 3.600 0.005889 32675. 449.0158 -8.662E-05 0.000 6.087E+10-13.5461 5520.1772 0.000 3.800 0.005683 33716. 416.7300 -8.531E-05 0.000 6.087E+10-13.3588 5641.4997 0.000 4.000 0.005480 34680. 384.9096 -8.396E-05 0.000 6.087E+10-13.1583 5762.8223 0.000 4.200 0.005280 35568. 353.5854 -8.258E-05 0.000 6.087E+10-12.9452 5884.1449 0.000 4.400 0.005084 36381. 322.7866 -8.116E-05 0.000 6.087E+10-12.7204 6005.4675 0.000 4.600 0.004890 37121. 292.5406 -7.971E-05 0.000 6.087E+10-12.4846 6126.7900 0.000 4.800 0.004701 37789. 262.8731 -7.823E-05 0.000 6.087E+10-12.2383 6248.1126 0.000 5.000 0.004515 38387. 233.8083 -7.673E-05 0.000 6.087E+10-11.9824 6369.4352 0.000 5.200 0.004333 38915. 205.3685 -7.521E-05 0.000 6.087E+10-11.7175 6490.7578 0.000 5.400 0.004154 39376. 177.5744 -7.367E-05 0.000 6.087E+10-11.4443 6612.0803 0.000 5.600 0.003979 39771. 150.4451 -7.210E-05 0.000 6.087E+10-11.1635 6733.4029 0.000 5.800 0.003808 40102. 123.9980 -7.053E-05 0.000 6.087E+10-10.8757 6854.7255 0.000 6.000 0.003640 40369. 98.2491 -6.894E-05 0.000 6.087E+10-10.5817 6976.0480 0.000 6.200 0.003477 40576. 73.2126 -6.735E-05 0.000 6.087E+10-10.2821 7097.3706 0.000

Page 19

existing phase1 87.lp6o 6.400 0.003317 40724. 48.9011 -6.575E-05 0.000 6.087E+10-9.9774 7218.6932 0.000 6.600 0.003161 40814. 25.3261 -6.414E-05 0.000 6.087E+10-9.6685 7340.0158 0.000 6.800 0.003009 40849. 2.4971 -6.253E-05 0.000 6.087E+10-9.3557 7461.3383 0.000 7.000 0.002861 40829. -19.5776 -6.092E-05 0.000 6.087E+10-9.0398 7582.6609 0.000 7.200 0.002717 40758. -40.8909 -5.931E-05 0.000 6.087E+10-8.7213 7703.9835 0.000 7.400 0.002577 40636. -61.4376 -5.770E-05 0.000 6.087E+10-8.4009 7825.3061 0.000 7.600 0.002440 40466. -81.2133 -5.611E-05 0.000 6.087E+10-8.0789 7946.6286 0.000 7.800 0.002307 40249. -100.2153 -5.451E-05 0.000 6.087E+10-7.7560 8067.9512 0.000 8.000 0.002178 39987. -118.4418 -5.293E-05 0.000 6.087E+10-7.4327 8189.2738 0.000 8.200 0.002053 39683. -135.8924 -5.136E-05 0.000 6.087E+10-7.1095 8310.5964 0.000 8.400 0.001932 39337. -152.5680 -4.980E-05 0.000 6.087E+10-6.7868 8431.9189 0.000 8.600 0.001814 38953. -168.4702 -4.826E-05 0.000 6.087E+10-6.4651 8553.2415 0.000 8.800 0.001700 38531. -183.6021 -4.673E-05 0.000 6.087E+10-6.1448 8674.5641 0.000 9.000 0.001590 38074. -197.9675 -4.522E-05 0.000 6.087E+10-5.8264 8795.8867 0.000 9.200 0.001483 37583. -211.5714 -4.373E-05 0.000 6.087E+10-5.5102 8917.2092 0.000 9.400 0.001380 37060. -224.4195 -4.226E-05 0.000 6.087E+10-5.1966 9038.5318 0.000 9.600 0.001280 36508. -236.5184 -4.081E-05 0.000 6.087E+10-4.8859 9159.8544 0.000 9.800 0.001184 35927. -247.8757 -3.938E-05 0.000 6.087E+10-4.5785 9281.1770 0.000 10.000 0.001091 35320. -260.6046 -3.798E-05 0.000 6.087E+10-6.0288 13261. 0.000 10.200 0.001002 34678. -276.7564 -3.660E-05 0.000 6.087E+10-7.4310 17805. 0.000 10.400 0.000915 33993. -293.9227 -3.524E-05 0.000 6.087E+10-6.8742 18021. 0.000 10.600 0.000832 33269. -309.7632 -3.392E-05 0.000 6.087E+10-6.3263 18238. 0.000 10.800 0.000753 32508. -324.2999 -3.262E-05 0.000 6.087E+10-5.7876 18455. 0.000 11.000 0.000676 31714. -337.5550 -3.135E-05 0.000 6.087E+10-5.2584 18671. 0.000 11.200 0.000602 30889. -349.5519 -3.012E-05 0.000 6.087E+10-4.7390 18888. 0.000 11.400 0.000531 30037. -360.3141 -2.892E-05 0.000 6.087E+10-4.2295 19104. 0.000 11.600 0.000463 29161. -369.8657 -2.775E-05 0.000 6.087E+10-3.7302 19321. 0.000 11.800 0.000398 28263. -378.2311 -2.662E-05 0.000 6.087E+10-3.2410 19538. 0.000 12.000 0.000336 27347. -385.4348 -2.552E-05 0.000 6.087E+10-2.7621 19754. 0.000 12.200 0.000276 26414. -391.5014 -2.446E-05 0.000 6.087E+10-2.2934 19971. 0.000 12.400 0.000218 25469. -396.4553 -2.344E-05 0.000 6.087E+10-1.8349 20187. 0.000 12.600 0.000163 24513. -400.3211 -2.246E-05 0.000 6.087E+10

Page 20

existing phase1 87.lp6o-1.3865 20404. 0.000 12.800 0.000110 23548. -403.1227 -2.151E-05 0.000 6.087E+10-0.9482 20621. 0.000 13.000 5.985E-05 22579. -404.8841 -2.060E-05 0.000 6.087E+10-0.5196 20837. 0.000 13.200 1.148E-05 21606. -405.6285 -1.973E-05 0.000 6.087E+10-0.1007 21054. 0.000 13.400 -3.484E-05 20633. -405.3788 -1.890E-05 0.000 6.087E+100.3088 21270. 0.000 13.600 -7.922E-05 19661. -404.1571 -1.810E-05 0.000 6.087E+100.7092 21487. 0.000 13.800 -0.000122 18693. -401.9850 -1.734E-05 0.000 6.087E+101.1008 21704. 0.000 14.000 -0.000162 17732. -398.8833 -1.663E-05 0.000 6.087E+101.4839 21920. 0.000 14.200 -0.000202 16780. -394.8719 -1.595E-05 0.000 6.087E+101.8589 22137. 0.000 14.400 -0.000239 15838. -389.9698 -1.530E-05 0.000 6.087E+102.2262 22353. 0.000 14.600 -0.000275 14909. -384.1950 -1.470E-05 0.000 6.087E+102.5861 22570. 0.000 14.800 -0.000310 13994. -377.5648 -1.413E-05 0.000 6.087E+102.9391 22787. 0.000 15.000 -0.000343 13097. -370.3577 -1.359E-05 0.000 6.087E+103.0668 21471. 0.000 15.200 -0.000375 12217. -362.9816 -1.309E-05 0.000 6.087E+103.0800 19722. 0.000 15.400 -0.000406 11355. -355.2490 -1.263E-05 0.000 6.087E+103.3638 19901. 0.000 15.600 -0.000435 10513. -346.8404 -1.220E-05 0.000 6.087E+103.6433 20081. 0.000 15.800 -0.000464 9690.9510 -337.7657 -1.180E-05 0.000 6.087E+103.9189 20261. 0.000 16.000 -0.000492 8891.8784 -328.0339 -1.143E-05 0.000 6.087E+104.1910 20441. 0.000 16.200 -0.000519 8116.9372 -317.6528 -1.110E-05 0.000 6.087E+104.4600 20620. 0.000 16.400 -0.000545 7367.6777 -306.6292 -1.079E-05 0.000 6.087E+104.7263 20800. 0.000 16.600 -0.000571 6645.6350 -294.9689 -1.052E-05 0.000 6.087E+104.9906 20980. 0.000 16.800 -0.000596 5952.3317 -282.6766 -1.027E-05 0.000 6.087E+105.2531 21159. 0.000 17.000 -0.000620 5289.2804 -269.7557 -1.005E-05 0.000 6.087E+105.5143 21339. 0.000 17.200 -0.000644 4657.9867 -256.2088 -9.851E-06 0.000 6.087E+105.7747 21519. 0.000 17.400 -0.000667 4059.9508 -242.0376 -9.679E-06 0.000 6.087E+106.0347 21699. 0.000 17.600 -0.000691 3496.6710 -227.2423 -9.530E-06 0.000 6.087E+106.2947 21878. 0.000 17.800 -0.000713 2969.6453 -211.8226 -9.403E-06 0.000 6.087E+106.5551 22058. 0.000 18.000 -0.000736 2480.3740 -195.7769 -9.295E-06 0.000 6.087E+106.8163 22238. 0.000 18.200 -0.000758 2030.3622 -179.1030 -9.206E-06 0.000 6.087E+107.0786 22417. 0.000 18.400 -0.000780 1621.1214 -161.7976 -9.134E-06 0.000 6.087E+107.3425 22597. 0.000 18.600 -0.000802 1254.1720 -143.8567 -9.078E-06 0.000 6.087E+107.6082 22777. 0.000 18.800 -0.000823 931.0448 -125.2756 -9.035E-06 0.000 6.087E+107.8761 22957. 0.000

Page 21

existing phase1 87.lp6o 19.000 -0.000845 653.2830 -106.0487 -9.003E-06 0.000 6.087E+108.1463 23136. 0.000 19.200 -0.000867 422.4434 -86.1700 -8.982E-06 0.000 6.087E+108.4192 23316. 0.000 19.400 -0.000888 240.0983 -65.6329 -8.969E-06 0.000 6.087E+108.6950 23496. 0.000 19.600 -0.000910 107.8359 -44.4305 -8.962E-06 0.000 6.087E+108.9737 23675. 0.000 19.800 -0.000931 27.2619 -22.5554 -8.959E-06 0.000 6.087E+109.2556 23855. 0.000 20.000 -0.000953 0.000 0.000 -8.959E-06 0.000 6.087E+109.5406 12017. 0.000

* This analysis makes computations of pile response using nonlinear moment-curvaturerelationships. The above values of total stress are computed for combined axial and bending stress in elastic sections and do not equal actual stresses in concrete and steel in the range of nonlinear bending.

Output Summary for Load Case No. 1:

Pile-head deflection = 0.0100000 inchesComputed slope at pile head = -0.0000998 radiansMaximum bending moment = 40849. inch-lbsMaximum shear force = 1064.8147015 lbsDepth of maximum bending moment = 81.6000000 inches below pile headDepth of maximum shear force = 0.000000 inches below pile headNumber of iterations = 6Number of zero deflection points = 1

-------------------------------------------------------------------------------- Computed Values of Pile Loading and Deflection for Lateral Loading for Load Case Number 2--------------------------------------------------------------------------------

Pile-head conditions are Displacement and Moment (Loading Type 4)Displacement of pile head = 0.100000 inchesMoment at pile head = 0.000 in-lbsAxial load at pile head = 10000.000 lbs

Depth Deflect. Bending Shear Slope Total Bending Soil Res. Soil Spr. Distrib. X y Moment Force S Stress Stiffness p Es*h Lat. Load feet inches in-lbs lbs radians psi* lb-in^2 lb/in lb/inch lb/inch ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- 0.00 0.1000 0.000 10619. -0.001000 0.000 6.087E+10-139.0155 1668.1854 0.000 0.200 0.0976 25109. 10283. -0.001000 0.000 6.087E+10-140.6123 3457.6934 0.000 0.400 0.0952 49407. 9944.0731 -0.000998 0.000 6.087E+10-141.9700 3579.0160 0.000 0.600 0.0928 72888. 9601.9981 -0.000996 0.000 6.087E+10-143.0925 3700.3385 0.000 0.800 0.0904 95545. 9257.5063 -0.000992 0.000 6.081E+10-143.9840 3821.6611 0.000 1.000 0.0880 117372. 8911.1467 -0.000988 0.000 6.076E+10

Page 22

existing phase1 87.lp6o-144.6490 3942.9837 0.000 1.200 0.0857 138366. 8563.4567 -0.000983 0.000 6.073E+10-145.0926 4064.3063 0.000 1.400 0.0833 158523. 8214.9618 -0.000977 0.000 6.070E+10-145.3198 4185.6288 0.000 1.600 0.0810 177844. 7866.1746 -0.000971 0.000 6.064E+10-145.3361 4306.9514 0.000 1.800 0.0787 196328. 7517.5946 -0.000963 0.000 6.060E+10-145.1472 4428.2740 0.000 2.000 0.0764 213975. 7169.7072 -0.000955 0.000 6.056E+10-144.7590 4549.5966 0.000 2.200 0.0741 230788. 6822.9833 -0.000946 0.000 6.053E+10-144.1776 4670.9191 0.000 2.400 0.0718 246771. 6477.8790 -0.000937 0.000 6.048E+10-143.4093 4792.2417 0.000 2.600 0.0696 261927. 6134.8351 -0.000927 0.000 6.045E+10-142.4606 4913.5643 0.000 2.800 0.0674 276262. 5794.2765 -0.000916 0.000 6.041E+10-141.3382 5034.8869 0.000 3.000 0.0652 289783. 5456.6124 -0.000905 0.000 6.039E+10-140.0487 5156.2094 0.000 3.200 0.0630 302498. 5122.2352 -0.000893 0.000 6.036E+10-138.5990 5277.5320 0.000 3.400 0.0609 314413. 4791.5210 -0.000881 0.000 6.033E+10-136.9961 5398.8546 0.000 3.600 0.0588 325539. 4464.8292 -0.000868 0.000 6.030E+10-135.2470 5520.1772 0.000 3.800 0.0567 335886. 4142.5022 -0.000855 0.000 6.027E+10-133.3589 5641.4997 0.000 4.000 0.0547 345464. 3824.8651 -0.000841 0.000 6.025E+10-131.3387 5762.8223 0.000 4.200 0.0527 354286. 3512.2261 -0.000827 0.000 6.023E+10-129.1937 5884.1449 0.000 4.400 0.0507 362363. 3204.8764 -0.000813 0.000 6.021E+10-126.9310 6005.4675 0.000 4.600 0.0488 369708. 2903.0898 -0.000799 0.000 6.019E+10-124.5578 6126.7900 0.000 4.800 0.0469 376336. 2607.1231 -0.000784 0.000 6.018E+10-122.0811 6248.1126 0.000 5.000 0.0450 382260. 2317.2160 -0.000769 0.000 6.016E+10-119.5081 6369.4352 0.000 5.200 0.0432 387495. 2033.5915 -0.000753 0.000 6.015E+10-116.8457 6490.7578 0.000 5.400 0.0414 392057. 1756.4556 -0.000738 0.000 6.014E+10-114.1009 6612.0803 0.000 5.600 0.0397 395962. 1485.9978 -0.000722 0.000 6.012E+10-111.2806 6733.4029 0.000 5.800 0.0380 399225. 1222.3912 -0.000706 0.000 6.012E+10-108.3916 6854.7255 0.000 6.000 0.0363 401863. 965.7928 -0.000690 0.000 6.011E+10-105.4405 6976.0480 0.000 6.200 0.0346 403894. 716.3436 -0.000674 0.000 6.010E+10-102.4339 7097.3706 0.000 6.400 0.0330 405334. 474.1690 -0.000658 0.000 6.010E+10-99.3782 7218.6932 0.000 6.600 0.0315 406201. 239.3794 -0.000642 0.000 6.010E+10-96.2798 7340.0158 0.000 6.800 0.0300 406514. 12.0698 -0.000625 0.000 6.010E+10-93.1448 7461.3383 0.000 7.000 0.0285 406289. -207.6790 -0.000609 0.000 6.010E+10-89.9792 7582.6609 0.000 7.200 0.0270 405546. -419.8006 -0.000593 0.000 6.010E+10-86.7888 7703.9835 0.000

Page 23

existing phase1 87.lp6o 7.400 0.0256 404303. -624.2424 -0.000577 0.000 6.010E+10-83.5793 7825.3061 0.000 7.600 0.0243 402577. -820.9651 -0.000561 0.000 6.011E+10-80.3562 7946.6286 0.000 7.800 0.0229 400389. -1009.9424 -0.000545 0.000 6.011E+10-77.1249 8067.9512 0.000 8.000 0.0217 397756. -1191.1606 -0.000529 0.000 6.012E+10-73.8903 8189.2738 0.000 8.200 0.0204 394697. -1364.6181 -0.000513 0.000 6.013E+10-70.6575 8310.5964 0.000 8.400 0.0192 391230. -1530.3245 -0.000497 0.000 6.014E+10-67.4312 8431.9189 0.000 8.600 0.0180 387375. -1688.3011 -0.000482 0.000 6.015E+10-64.2159 8553.2415 0.000 8.800 0.0169 383149. -1838.5795 -0.000466 0.000 6.016E+10-61.0160 8674.5641 0.000 9.000 0.0158 378572. -1981.2013 -0.000451 0.000 6.017E+10-57.8355 8795.8867 0.000 9.200 0.0147 373661. -2116.2180 -0.000436 0.000 6.019E+10-54.6784 8917.2092 0.000 9.400 0.0137 368435. -2243.6901 -0.000421 0.000 6.020E+10-51.5483 9038.5318 0.000 9.600 0.0127 362912. -2363.6867 -0.000407 0.000 6.021E+10-48.4488 9159.8544 0.000 9.800 0.0117 357109. -2476.2852 -0.000392 0.000 6.022E+10-45.3832 9281.1770 0.000 10.000 0.0108 351045. -2602.4256 -0.000378 0.000 6.023E+10-59.7338 13261. 0.000 10.200 0.009920 344636. -2762.4187 -0.000364 0.000 6.025E+10-73.5937 17805. 0.000 10.400 0.009062 337802. -2932.3867 -0.000351 0.000 6.026E+10-68.0463 18021. 0.000 10.600 0.008236 330577. -3089.1496 -0.000337 0.000 6.028E+10-62.5894 18238. 0.000 10.800 0.007442 322991. -3232.9283 -0.000324 0.000 6.030E+10-57.2263 18455. 0.000 11.000 0.006679 315074. -3363.9516 -0.000312 0.000 6.032E+10-51.9598 18671. 0.000 11.200 0.005946 306859. -3482.4543 -0.000299 0.000 6.035E+10-46.7924 18888. 0.000 11.400 0.005242 298373. -3588.6760 -0.000287 0.000 6.037E+10-41.7258 19104. 0.000 11.600 0.004566 289647. -3682.8604 -0.000276 0.000 6.039E+10-36.7612 19321. 0.000 11.800 0.003919 280709. -3765.2536 -0.000264 0.000 6.040E+10-31.8997 19538. 0.000 12.000 0.003298 271586. -3836.1032 -0.000253 0.000 6.042E+10-27.1416 19754. 0.000 12.200 0.002702 262307. -3895.6573 -0.000243 0.000 6.045E+10-22.4868 19971. 0.000 12.400 0.002132 252899. -3944.1633 -0.000233 0.000 6.047E+10-17.9349 20187. 0.000 12.600 0.001586 243387. -3981.8669 -0.000223 0.000 6.049E+10-13.4848 20404. 0.000 12.800 0.001063 233797. -4009.0110 -0.000213 0.000 6.052E+10-9.1353 20621. 0.000 13.000 0.000563 224154. -4025.8348 -0.000204 0.000 6.055E+10-4.8846 20837. 0.000 13.200 8.328E-05 214482. -4032.5729 -0.000195 0.000 6.056E+10-0.7305 21054. 0.000 13.400 -0.000376 204807. -4029.4544 -0.000187 0.000 6.058E+103.3292 21270. 0.000 13.600 -0.000815 195150. -4016.7024 -0.000179 0.000 6.060E+10

Page 24

existing phase1 87.lp6o7.2975 21487. 0.000 13.800 -0.001236 185535. -3994.5327 -0.000172 0.000 6.062E+1011.1773 21704. 0.000 14.000 -0.001639 175984. -3963.1535 -0.000165 0.000 6.064E+1014.9721 21920. 0.000 14.200 -0.002026 166520. -3922.7644 -0.000158 0.000 6.067E+1018.6855 22137. 0.000 14.400 -0.002397 157163. -3873.5561 -0.000151 0.000 6.070E+1022.3214 22353. 0.000 14.600 -0.002752 147934. -3815.7096 -0.000145 0.000 6.072E+1025.8840 22570. 0.000 14.800 -0.003094 138854. -3749.3956 -0.000140 0.000 6.073E+1029.3776 22787. 0.000 15.000 -0.003423 129944. -3677.3970 -0.000134 0.000 6.074E+1030.6212 21471. 0.000 15.200 -0.003739 121209. -3603.7804 -0.000129 0.000 6.076E+1030.7260 19722. 0.000 15.400 -0.004044 112652. -3526.6690 -0.000125 0.000 6.077E+1033.5336 19901. 0.000 15.600 -0.004338 104287. -3442.8717 -0.000120 0.000 6.079E+1036.2975 20081. 0.000 15.800 -0.004622 96132. -3352.4882 -0.000117 0.000 6.081E+1039.0220 20261. 0.000 16.000 -0.004897 88201. -3255.6079 -0.000113 0.000 6.083E+1041.7116 20441. 0.000 16.200 -0.005164 80510. -3152.3093 -0.000110 0.000 6.085E+1044.3706 20620. 0.000 16.400 -0.005423 73075. -3042.6604 -0.000107 0.000 6.087E+1047.0035 20800. 0.000 16.600 -0.005676 65911. -2926.7185 -0.000104 0.000 6.087E+1049.6148 20980. 0.000 16.800 -0.005922 59032. -2804.5301 -0.000101 0.000 6.087E+1052.2088 21159. 0.000 17.000 -0.006162 52454. -2676.1314 -9.915E-05 0.000 6.087E+1054.7901 21339. 0.000 17.200 -0.006398 46191. -2541.5480 -9.720E-05 0.000 6.087E+1057.3628 21519. 0.000 17.400 -0.006629 40259. -2400.7950 -9.550E-05 0.000 6.087E+1059.9313 21699. 0.000 17.600 -0.006856 34672. -2253.8778 -9.402E-05 0.000 6.087E+1062.4997 21878. 0.000 17.800 -0.007080 29445. -2100.7919 -9.276E-05 0.000 6.087E+1065.0719 22058. 0.000 18.000 -0.007301 24593. -1941.5233 -9.169E-05 0.000 6.087E+1067.6519 22238. 0.000 18.200 -0.007520 20130. -1776.0490 -9.081E-05 0.000 6.087E+1070.2433 22417. 0.000 18.400 -0.007737 16072. -1604.3376 -9.010E-05 0.000 6.087E+1072.8495 22597. 0.000 18.600 -0.007953 12433. -1426.3496 -8.954E-05 0.000 6.087E+1075.4738 22777. 0.000 18.800 -0.008167 9229.6732 -1242.0380 -8.911E-05 0.000 6.087E+1078.1191 22957. 0.000 19.000 -0.008380 6475.8993 -1051.3494 -8.880E-05 0.000 6.087E+1080.7881 23136. 0.000 19.200 -0.008593 4187.4587 -854.2239 -8.859E-05 0.000 6.087E+1083.4831 23316. 0.000 19.400 -0.008806 2379.8767 -650.5969 -8.846E-05 0.000 6.087E+1086.2061 23496. 0.000 19.600 -0.009018 1068.8395 -440.3993 -8.839E-05 0.000 6.087E+1088.9586 23675. 0.000 19.800 -0.009230 270.2030 -223.5586 -8.837E-05 0.000 6.087E+1091.7420 23855. 0.000

Page 25

existing phase1 87.lp6o 20.000 -0.009442 0.000 0.000 -8.836E-05 0.000 6.087E+1094.5568 12017. 0.000

* This analysis makes computations of pile response using nonlinear moment-curvaturerelationships. The above values of total stress are computed for combined axial and bending stress in elastic sections and do not equal actual stresses in concrete and steel in the range of nonlinear bending.

Output Summary for Load Case No. 2:

Pile-head deflection = 0.1000000 inchesComputed slope at pile head = -0.0010002 radiansMaximum bending moment = 406514. inch-lbsMaximum shear force = 10619. lbsDepth of maximum bending moment = 81.6000000 inches below pile headDepth of maximum shear force = 0.000000 inches below pile headNumber of iterations = 6Number of zero deflection points = 1

For Analysis Case 3, Iteration 96, Y(top) = 2.0000E-01, dYmax = 1.8162E-05, Node32, Delta dYmax = 3.3952E-06For Analysis Case 3, Iteration 97, Y(top) = 2.0000E-01, dYmax = 1.4763E-05, Node32, Delta dYmax = 3.3988E-06For Analysis Case 3, Iteration 98, Y(top) = 2.0000E-01, dYmax = 1.2372E-05, Node32, Delta dYmax = 2.3911E-06For Analysis Case 3, Iteration 99, Y(top) = 2.0000E-01, dYmax = 1.0753E-05, Node32, Delta dYmax = 1.6187E-06For Analysis Case 3, Iteration 100, Y(top) = 2.0000E-01, dYmax = 9.6550E-06, Node32, Delta dYmax = 1.0984E-06

-------------------------------------------------------------------------------- Computed Values of Pile Loading and Deflection for Lateral Loading for Load Case Number 3--------------------------------------------------------------------------------

Pile-head conditions are Displacement and Moment (Loading Type 4)Displacement of pile head = 0.200000 inchesMoment at pile head = 0.000 in-lbsAxial load at pile head = 10000.000 lbs

Depth Deflect. Bending Shear Slope Total Bending Soil Res. Soil Spr. Distrib. X y Moment Force S Stress Stiffness p Es*h Lat. Load feet inches in-lbs lbs radians psi* lb-in^2 lb/in lb/inch lb/inch ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- 0.00 0.2000 0.000 17845. -0.002271 0.000 6.087E+10-278.0309 1668.1854 0.000 0.200 0.1945 42083. 17175. -0.002270 0.000 6.087E+10-280.2886 3457.6934 0.000 0.400 0.1891 82551. 16501. -0.002268 0.000 6.085E+10-282.0011 3579.0160 0.000 0.600 0.1837 121395. 15822. -0.002264 0.000 6.076E+10-283.1750 3700.3385 0.000 0.800 0.1782 158607. 15142. -0.002258 0.000 6.069E+10-283.8174 3821.6611 0.000 1.000 0.1728 194185. 14461. -0.002251 0.000 6.060E+10

Page 26

existing phase1 87.lp6o-283.9358 3942.9837 0.000 1.200 0.1674 228127. 13780. -0.002243 0.000 6.054E+10-283.5383 4064.3063 0.000 1.400 0.1621 260436. 13100. -0.002233 0.000 6.045E+10-282.6334 4185.6288 0.000 1.600 0.1567 291116. 12424. -0.002222 0.000 6.038E+10-281.2298 4306.9514 0.000 1.800 0.1514 320176. 11751. -0.002210 0.000 6.031E+10-279.3369 4428.2740 0.000 2.000 0.1461 347627. 11084. -0.002197 0.000 6.024E+10-276.9641 4549.5966 0.000 2.200 0.1408 373482. 10422. -0.002182 0.000 6.019E+10-274.1214 4670.9191 0.000 2.400 0.1356 397758. 9768.2696 -0.002167 0.000 6.012E+10-270.8186 4792.2417 0.000 2.600 0.1304 420474. 9122.8079 -0.002151 0.000 6.006E+10-267.0662 4913.5643 0.000 2.800 0.1253 441651. 8486.8792 -0.002133 0.000 6.001E+10-262.8744 5034.8869 0.000 3.000 0.1202 461314. 7861.5252 -0.002115 0.000 5.996E+10-258.2539 5156.2094 0.000 3.200 0.1152 479488. 7247.7621 -0.002097 0.000 5.992E+10-253.2153 5277.5320 0.000 3.400 0.1101 496203. 6646.5805 -0.002077 0.000 5.987E+10-247.7694 5398.8546 0.000 3.600 0.1052 511491. 6058.9449 -0.002057 0.000 5.984E+10-241.9269 5520.1772 0.000 3.800 0.1003 525385. 5485.7943 -0.002036 0.000 5.981E+10-235.6986 5641.4997 0.000 4.000 0.0954 537921. 4928.0418 -0.002015 0.000 5.977E+10-229.0952 5762.8223 0.000 4.200 0.0906 549136. 4386.5748 -0.001993 0.000 5.974E+10-222.1274 5884.1449 0.000 4.400 0.0858 559072. 3862.2548 -0.001971 0.000 5.972E+10-214.8059 6005.4675 0.000 4.600 0.0811 567770. 3355.9184 -0.001948 0.000 5.969E+10-207.1412 6126.7900 0.000 4.800 0.0765 575274. 2868.3766 -0.001925 0.000 5.968E+10-199.1437 6248.1126 0.000 5.000 0.0719 581630. 2400.4158 -0.001902 0.000 5.966E+10-190.8237 6369.4352 0.000 5.200 0.0674 586887. 1952.7979 -0.001878 0.000 5.965E+10-182.1912 6490.7578 0.000 5.400 0.0629 591094. 1526.2608 -0.001844 0.000 3.113E+10-173.2564 6612.0803 0.000 5.600 0.0585 594302. 1121.3425 -0.001781 0.000 1.784E+10-164.1755 6733.4029 0.000 5.800 0.0543 596562. 738.0909 -0.001681 0.000 1.202E+10-155.2008 6854.7255 0.000 6.000 0.0504 597925. 375.8886 -0.001546 0.000 9.432E+09-146.6344 6976.0480 0.000 6.200 0.0469 598440. 33.4220 -0.001386 0.000 8.540E+09-138.7544 7097.3706 0.000 6.400 0.0438 598152. -291.1613 -0.001220 0.000 8.858E+09-131.7317 7218.6932 0.000 6.600 0.0411 597101. -599.9388 -0.001071 0.000 1.045E+10-125.5828 7340.0158 0.000 6.800 0.0387 595324. -894.8544 -0.000951 0.000 1.396E+10-120.1802 7461.3383 0.000 7.000 0.0365 592852. -1177.4429 -0.000866 0.000 2.101E+10-115.3102 7582.6609 0.000 7.200 0.0345 589714. -1448.7075 -0.000812 0.000 3.547E+10-110.7436 7703.9835 0.000

Page 27

existing phase1 87.lp6o 7.400 0.0326 585937. -1709.1447 -0.000781 0.000 5.965E+10-106.2873 7825.3061 0.000 7.600 0.0308 581547. -1958.8809 -0.000757 0.000 5.966E+10-101.8262 7946.6286 0.000 7.800 0.0290 576571. -2197.9129 -0.000734 0.000 5.967E+10-97.3672 8067.9512 0.000 8.000 0.0272 571033. -2426.2543 -0.000711 0.000 5.969E+10-92.9173 8189.2738 0.000 8.200 0.0256 564959. -2643.9344 -0.000688 0.000 5.970E+10-88.4829 8310.5964 0.000 8.400 0.0239 558375. -2850.9984 -0.000665 0.000 5.972E+10-84.0704 8431.9189 0.000 8.600 0.0224 551306. -3047.5057 -0.000643 0.000 5.974E+10-79.6857 8553.2415 0.000 8.800 0.0208 543778. -3233.5298 -0.000621 0.000 5.976E+10-75.3344 8674.5641 0.000 9.000 0.0194 535815. -3409.1574 -0.000599 0.000 5.978E+10-71.0219 8795.8867 0.000 9.200 0.0180 527442. -3574.4874 -0.000578 0.000 5.980E+10-66.7532 8917.2092 0.000 9.400 0.0166 518685. -3729.6308 -0.000557 0.000 5.982E+10-62.5330 9038.5318 0.000 9.600 0.0153 509567. -3874.7092 -0.000536 0.000 5.984E+10-58.3657 9159.8544 0.000 9.800 0.0140 500112. -4009.8547 -0.000516 0.000 5.987E+10-54.2555 9281.1770 0.000 10.000 0.0128 490344. -4159.9301 -0.000496 0.000 5.989E+10-70.8074 13261. 0.000 10.200 0.0116 480168. -4348.5916 -0.000477 0.000 5.991E+10-86.4105 17805. 0.000 10.400 0.0105 469494. -4547.1345 -0.000458 0.000 5.994E+10-79.0419 18021. 0.000 10.600 0.009450 458364. -4728.1611 -0.000439 0.000 5.997E+10-71.8136 18238. 0.000 10.800 0.008418 446820. -4892.0130 -0.000421 0.000 6.000E+10-64.7297 18455. 0.000 11.000 0.007429 434903. -5039.0403 -0.000404 0.000 6.003E+10-57.7931 18671. 0.000 11.200 0.006481 422652. -5169.5995 -0.000386 0.000 6.006E+10-51.0063 18888. 0.000 11.400 0.005574 410107. -5284.0526 -0.000370 0.000 6.009E+10-44.3712 19104. 0.000 11.600 0.004706 397306. -5382.7646 -0.000354 0.000 6.012E+10-37.8889 19321. 0.000 11.800 0.003877 384287. -5466.1030 -0.000338 0.000 6.016E+10-31.5598 19538. 0.000 12.000 0.003084 371085. -5534.4353 -0.000323 0.000 6.019E+10-25.3838 19754. 0.000 12.200 0.002327 357737. -5588.1282 -0.000308 0.000 6.022E+10-19.3602 19971. 0.000 12.400 0.001604 344277. -5627.5457 -0.000294 0.000 6.025E+10-13.4877 20187. 0.000 12.600 0.000913 330739. -5653.0485 -0.000281 0.000 6.028E+10-7.7646 20404. 0.000 12.800 0.000255 317156. -5664.9920 -0.000268 0.000 6.032E+10-2.1884 20621. 0.000 13.000 -0.000374 303560. -5663.7255 -0.000256 0.000 6.036E+103.2438 20837. 0.000 13.200 -0.000973 289982. -5649.5908 -0.000244 0.000 6.039E+108.5352 21054. 0.000 13.400 -0.001545 276453. -5622.9209 -0.000233 0.000 6.041E+1013.6897 21270. 0.000 13.600 -0.002090 263003. -5584.0397 -0.000222 0.000 6.044E+10

Page 28

existing phase1 87.lp6o18.7113 21487. 0.000 13.800 -0.002610 249661. -5533.2603 -0.000212 0.000 6.048E+1023.6048 21704. 0.000 14.000 -0.003107 236454. -5470.8846 -0.000202 0.000 6.051E+1028.3750 21920. 0.000 14.200 -0.003581 223410. -5397.2020 -0.000193 0.000 6.055E+1033.0272 22137. 0.000 14.400 -0.004033 210557. -5312.4890 -0.000184 0.000 6.057E+1037.5670 22353. 0.000 14.600 -0.004466 197919. -5217.0084 -0.000176 0.000 6.059E+1042.0002 22570. 0.000 14.800 -0.004880 185523. -5111.0087 -0.000169 0.000 6.062E+1046.3329 22787. 0.000 15.000 -0.005276 173394. -4998.7663 -0.000162 0.000 6.065E+1047.2024 21471. 0.000 15.200 -0.005656 161537. -4886.3496 -0.000155 0.000 6.069E+1046.4782 19722. 0.000 15.400 -0.006021 149947. -4770.6671 -0.000149 0.000 6.072E+1049.9239 19901. 0.000 15.600 -0.006371 138645. -4646.7922 -0.000143 0.000 6.073E+1053.3052 20081. 0.000 15.800 -0.006708 127650. -4514.8725 -0.000138 0.000 6.075E+1056.6279 20261. 0.000 16.000 -0.007033 116980. -4375.0414 -0.000133 0.000 6.076E+1059.8980 20441. 0.000 16.200 -0.007347 106656. -4227.4178 -0.000129 0.000 6.078E+1063.1216 20620. 0.000 16.400 -0.007651 96695. -4072.1065 -0.000125 0.000 6.080E+1066.3045 20800. 0.000 16.600 -0.007945 87116. -3909.1977 -0.000121 0.000 6.083E+1069.4529 20980. 0.000 16.800 -0.008232 77936. -3738.7671 -0.000118 0.000 6.086E+1072.5726 21159. 0.000 17.000 -0.008511 69175. -3560.8764 -0.000115 0.000 6.087E+1075.6697 21339. 0.000 17.200 -0.008783 60850. -3375.5730 -0.000112 0.000 6.087E+1078.7498 21519. 0.000 17.400 -0.009050 52978. -3182.8908 -0.000110 0.000 6.087E+1081.8187 21699. 0.000 17.600 -0.009311 45577. -2982.8501 -0.000108 0.000 6.087E+1084.8818 21878. 0.000 17.800 -0.009569 38665. -2775.4584 -0.000106 0.000 6.087E+1087.9445 22058. 0.000 18.000 -0.009822 32260. -2560.7108 -0.000105 0.000 6.087E+1091.0119 22238. 0.000 18.200 -0.0101 26379. -2338.5902 -0.000104 0.000 6.087E+1094.0887 22417. 0.000 18.400 -0.0103 21040. -2109.0684 -0.000103 0.000 6.087E+1097.1795 22597. 0.000 18.600 -0.0106 16260. -1872.1066 -0.000102 0.000 6.087E+10100.2886 22777. 0.000 18.800 -0.0108 12059. -1627.6565 -0.000102 0.000 6.087E+10103.4199 22957. 0.000 19.000 -0.0111 8452.5455 -1375.6605 -0.000101 0.000 6.087E+10106.5768 23136. 0.000 19.200 -0.0113 5460.3282 -1116.0536 -0.000101 0.000 6.087E+10109.7623 23316. 0.000 19.400 -0.0115 3100.3369 -848.7637 -0.000101 0.000 6.087E+10112.9792 23496. 0.000 19.600 -0.0118 1391.1030 -573.7133 -0.000101 0.000 6.087E+10116.2295 23675. 0.000 19.800 -0.0120 351.3495 -290.8204 -0.000101 0.000 6.087E+10119.5146 23855. 0.000

Page 29

existing phase1 87.lp6o 20.000 -0.0123 0.000 0.000 -0.000101 0.000 6.087E+10122.8357 12017. 0.000

* This analysis makes computations of pile response using nonlinear moment-curvaturerelationships. The above values of total stress are computed for combined axial and bending stress in elastic sections and do not equal actual stresses in concrete and steel in the range of nonlinear bending.

Output Summary for Load Case No. 3:

Pile-head deflection = 0.2000000 inchesComputed slope at pile head = -0.0022710 radiansMaximum bending moment = 598440. inch-lbsMaximum shear force = 17845. lbsDepth of maximum bending moment = 74.4000000 inches below pile headDepth of maximum shear force = 0.000000 inches below pile headNumber of iterations = 100Number of zero deflection points = 1

-------------------------------------------------------------------------------- Computed Values of Pile Loading and Deflection for Lateral Loading for Load Case Number 4--------------------------------------------------------------------------------

Pile-head conditions are Displacement and Moment (Loading Type 4)Displacement of pile head = 0.300000 inchesMoment at pile head = 0.000 in-lbsAxial load at pile head = 10000.000 lbs

Depth Deflect. Bending Shear Slope Total Bending Soil Res. Soil Spr. Distrib. X y Moment Force S Stress Stiffness p Es*h Lat. Load feet inches in-lbs lbs radians psi* lb-in^2 lb/in lb/inch lb/inch ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- 0.00 0.3000 0.000 21547. -0.004020 0.000 6.087E+10-417.0464 1668.1854 0.000 0.200 0.2904 50609. 20545. -0.004019 0.000 6.087E+10-418.3132 3457.6934 0.000 0.400 0.2807 98809. 19541. -0.004016 0.000 6.080E+10-418.6119 3579.0160 0.000 0.600 0.2711 144597. 18537. -0.004011 0.000 6.073E+10-417.9501 3700.3385 0.000 0.800 0.2615 187977. 17536. -0.004004 0.000 6.062E+10-416.3363 3821.6611 0.000 1.000 0.2519 228960. 16539. -0.003996 0.000 6.054E+10-413.7793 3942.9837 0.000 1.200 0.2423 267559. 15551. -0.003986 0.000 6.043E+10-410.2885 4064.3063 0.000 1.400 0.2327 303794. 14571. -0.003975 0.000 6.036E+10-405.8737 4185.6288 0.000 1.600 0.2232 337691. 13603. -0.003962 0.000 6.026E+10-400.5450 4306.9514 0.000 1.800 0.2137 369281. 12650. -0.003948 0.000 6.019E+10-394.3128 4428.2740 0.000 2.000 0.2042 398599. 11712. -0.003933 0.000 6.012E+10

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existing phase1 87.lp6o-387.1879 4549.5966 0.000 2.200 0.1948 425686. 10792. -0.003916 0.000 6.005E+10-379.1812 4670.9191 0.000 2.400 0.1855 450590. 9892.8266 -0.003899 0.000 6.000E+10-370.3036 4792.2417 0.000 2.600 0.1761 473359. 9015.7824 -0.003880 0.000 5.993E+10-360.5665 4913.5643 0.000 2.800 0.1668 494052. 8163.1253 -0.003861 0.000 5.988E+10-349.9810 5034.8869 0.000 3.000 0.1576 512727. 7336.8779 -0.003841 0.000 5.984E+10-338.5585 5156.2094 0.000 3.200 0.1484 529453. 6539.0357 -0.003820 0.000 5.980E+10-326.3100 5277.5320 0.000 3.400 0.1393 544298. 5771.5673 -0.003798 0.000 5.975E+10-313.2469 5398.8546 0.000 3.600 0.1302 557339. 5036.4147 -0.003776 0.000 5.972E+10-299.3803 5520.1772 0.000 3.800 0.1211 568654. 4335.4932 -0.003753 0.000 5.969E+10-284.7210 5641.4997 0.000 4.000 0.1121 578329. 3670.6920 -0.003730 0.000 5.967E+10-269.2800 5762.8223 0.000 4.200 0.1032 586453. 3043.8745 -0.003699 0.000 3.592E+10-253.0679 5884.1449 0.000 4.400 0.0944 593117. 2456.7664 -0.003634 0.000 1.554E+10-236.1888 6005.4675 0.000 4.600 0.0858 598420. 1910.5662 -0.003498 0.000 8.011E+09-218.9781 6126.7900 0.000 4.800 0.0776 602456. 1405.3722 -0.003270 0.000 5.217E+09-202.0169 6248.1126 0.000 5.000 0.0701 605322. 939.7590 -0.002992 0.000 5.205E+09-185.9940 6369.4352 0.000 5.200 0.0632 607110. 511.3387 -0.002712 0.000 5.203E+09-171.0229 6490.7578 0.000 5.400 0.0571 607907. 117.4574 -0.002432 0.000 5.201E+09-157.2115 6612.0803 0.000 5.600 0.0516 607791. -244.7939 -0.002152 0.000 5.202E+09-144.6646 6733.4029 0.000 5.800 0.0467 606835. -578.5722 -0.001871 0.000 5.203E+09-133.4840 6854.7255 0.000 6.000 0.0426 605104. -887.2745 -0.001592 0.000 5.206E+09-123.7680 6976.0480 0.000 6.200 0.0391 602653. -1174.5302 -0.001314 0.000 5.216E+09-115.6117 7097.3706 0.000 6.400 0.0363 599529. -1444.1899 -0.001072 0.000 7.004E+09-109.1048 7218.6932 0.000 6.600 0.0339 595772. -1699.7003 -0.000906 0.000 1.128E+10-103.8206 7340.0158 0.000 6.800 0.0319 591414. -1943.3816 -0.000807 0.000 1.966E+10-99.2471 7461.3383 0.000 7.000 0.0301 586483. -2176.4981 -0.000752 0.000 3.701E+10-95.0167 7582.6609 0.000 7.200 0.0283 581003. -2399.5888 -0.000721 0.000 5.966E+10-90.8922 7703.9835 0.000 7.400 0.0266 574999. -2612.7869 -0.000698 0.000 5.968E+10-86.7729 7825.3061 0.000 7.600 0.0250 568495. -2816.1126 -0.000675 0.000 5.969E+10-82.6652 7946.6286 0.000 7.800 0.0234 561514. -3009.6013 -0.000652 0.000 5.971E+10-78.5754 8067.9512 0.000 8.000 0.0218 554080. -3193.3031 -0.000630 0.000 5.973E+10-74.5094 8189.2738 0.000 8.200 0.0204 546217. -3367.2821 -0.000608 0.000 5.975E+10-70.4731 8310.5964 0.000

Page 31

existing phase1 87.lp6o 8.400 0.0189 537946. -3531.6157 -0.000586 0.000 5.977E+10-66.4716 8431.9189 0.000 8.600 0.0175 529293. -3686.3937 -0.000564 0.000 5.980E+10-62.5101 8553.2415 0.000 8.800 0.0162 520279. -3831.7180 -0.000543 0.000 5.982E+10-58.5934 8674.5641 0.000 9.000 0.0149 510927. -3967.7012 -0.000523 0.000 5.984E+10-54.7259 8795.8867 0.000 9.200 0.0137 501259. -4094.4666 -0.000502 0.000 5.986E+10-50.9119 8917.2092 0.000 9.400 0.0125 491297. -4212.1472 -0.000482 0.000 5.989E+10-47.1552 9038.5318 0.000 9.600 0.0114 481064. -4320.8847 -0.000463 0.000 5.991E+10-43.4594 9159.8544 0.000 9.800 0.0103 470579. -4420.8293 -0.000444 0.000 5.994E+10-39.8278 9281.1770 0.000 10.000 0.009256 459865. -4529.9947 -0.000425 0.000 5.997E+10-51.1434 13261. 0.000 10.200 0.008258 448856. -4664.8803 -0.000407 0.000 6.000E+10-61.2613 17805. 0.000 10.400 0.007302 437493. -4804.1922 -0.000389 0.000 6.002E+10-54.8320 18021. 0.000 10.600 0.006389 425814. -4928.2500 -0.000372 0.000 6.005E+10-48.5494 18238. 0.000 10.800 0.005516 413855. -5037.4083 -0.000355 0.000 6.008E+10-42.4159 18455. 0.000 11.000 0.004683 401652. -5132.0278 -0.000339 0.000 6.011E+10-36.4336 18671. 0.000 11.200 0.003889 389238. -5212.4728 -0.000323 0.000 6.014E+10-30.6039 18888. 0.000 11.400 0.003132 376647. -5279.1103 -0.000308 0.000 6.018E+10-24.9275 19104. 0.000 11.600 0.002410 363913. -5332.3088 -0.000293 0.000 6.021E+10-19.4046 19321. 0.000 11.800 0.001724 351066. -5372.4363 -0.000279 0.000 6.023E+10-14.0350 19538. 0.000 12.000 0.001071 338139. -5399.8597 -0.000265 0.000 6.026E+10-8.8178 19754. 0.000 12.200 0.000451 325160. -5414.9432 -0.000252 0.000 6.030E+10-3.7518 19971. 0.000 12.400 -0.000138 312159. -5418.0474 -0.000239 0.000 6.033E+101.1650 20187. 0.000 12.600 -0.000698 299165. -5409.5278 -0.000227 0.000 6.037E+105.9347 20404. 0.000 12.800 -0.001229 286204. -5389.7338 -0.000216 0.000 6.039E+1010.5603 20621. 0.000 13.000 -0.001733 273304. -5359.0079 -0.000204 0.000 6.042E+1015.0446 20837. 0.000 13.200 -0.002210 260491. -5317.6848 -0.000194 0.000 6.045E+1019.3914 21054. 0.000 13.400 -0.002663 247789. -5266.0899 -0.000184 0.000 6.048E+1023.6043 21270. 0.000 13.600 -0.003093 235222. -5204.5394 -0.000174 0.000 6.052E+1027.6878 21487. 0.000 13.800 -0.003499 222815. -5133.3386 -0.000165 0.000 6.055E+1031.6462 21704. 0.000 14.000 -0.003885 210590. -5052.7817 -0.000157 0.000 6.057E+1035.4845 21920. 0.000 14.200 -0.004251 198570. -4963.1510 -0.000148 0.000 6.059E+1039.2077 22137. 0.000 14.400 -0.004598 186774. -4864.7164 -0.000141 0.000 6.062E+1042.8211 22353. 0.000 14.600 -0.004927 175226. -4757.7347 -0.000134 0.000 6.065E+10

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existing phase1 87.lp6o46.3302 22570. 0.000 14.800 -0.005239 163944. -4642.4497 -0.000127 0.000 6.068E+1049.7407 22787. 0.000 15.000 -0.005536 152948. -4523.3323 -0.000121 0.000 6.071E+1049.5238 21471. 0.000 15.200 -0.005818 142237. -4406.5327 -0.000115 0.000 6.073E+1047.8093 19722. 0.000 15.400 -0.006087 131802. -4288.5927 -0.000109 0.000 6.074E+1050.4740 19901. 0.000 15.600 -0.006343 121657. -4164.3347 -0.000104 0.000 6.076E+1053.0744 20081. 0.000 15.800 -0.006588 111818. -4033.9064 -9.978E-05 0.000 6.077E+1055.6158 20261. 0.000 16.000 -0.006822 102299. -3897.4431 -9.556E-05 0.000 6.079E+1058.1036 20441. 0.000 16.200 -0.007047 93115. -3755.0669 -9.170E-05 0.000 6.081E+1060.5432 20620. 0.000 16.400 -0.007262 84280. -3606.8870 -8.820E-05 0.000 6.084E+1062.9400 20800. 0.000 16.600 -0.007470 75806. -3452.9999 -8.504E-05 0.000 6.087E+1065.2993 20980. 0.000 16.800 -0.007671 67709. -3293.4889 -8.221E-05 0.000 6.087E+1067.6265 21159. 0.000 17.000 -0.007865 60002. -3128.4250 -7.970E-05 0.000 6.087E+1069.9268 21339. 0.000 17.200 -0.008053 52697. -2957.8667 -7.747E-05 0.000 6.087E+1072.2052 21519. 0.000 17.400 -0.008236 45808. -2781.8604 -7.553E-05 0.000 6.087E+1074.4667 21699. 0.000 17.600 -0.008416 39347. -2600.4409 -7.385E-05 0.000 6.087E+1076.7162 21878. 0.000 17.800 -0.008591 33329. -2413.6315 -7.242E-05 0.000 6.087E+1078.9583 22058. 0.000 18.000 -0.008763 27765. -2221.4446 -7.122E-05 0.000 6.087E+1081.1975 22238. 0.000 18.200 -0.008933 22669. -2023.8822 -7.022E-05 0.000 6.087E+1083.4379 22417. 0.000 18.400 -0.009100 18054. -1820.9367 -6.942E-05 0.000 6.087E+1085.6835 22597. 0.000 18.600 -0.009266 13932. -1612.5910 -6.879E-05 0.000 6.087E+1087.9379 22777. 0.000 18.800 -0.009430 10317. -1398.8200 -6.831E-05 0.000 6.087E+1090.2046 22957. 0.000 19.000 -0.009594 7221.2298 -1179.5907 -6.797E-05 0.000 6.087E+1092.4865 23136. 0.000 19.200 -0.009757 4658.2008 -954.8635 -6.773E-05 0.000 6.087E+1094.7862 23316. 0.000 19.400 -0.009919 2641.1361 -724.5928 -6.759E-05 0.000 6.087E+1097.1060 23496. 0.000 19.600 -0.0101 1183.3994 -488.7285 -6.751E-05 0.000 6.087E+1099.4476 23675. 0.000 19.800 -0.0102 298.4800 -247.2164 -6.748E-05 0.000 6.087E+10101.8124 23855. 0.000 20.000 -0.0104 0.000 0.000 -6.748E-05 0.000 6.087E+10104.2012 12017. 0.000

* This analysis makes computations of pile response using nonlinear moment-curvaturerelationships. The above values of total stress are computed for combined axial and bending stress in elastic sections and do not equal actual stresses in concrete and steel in the range of nonlinear bending.

Page 33

existing phase1 87.lp6o

Output Summary for Load Case No. 4:

Pile-head deflection = 0.3000000 inchesComputed slope at pile head = -0.0040196 radiansMaximum bending moment = 607907. inch-lbsMaximum shear force = 21547. lbsDepth of maximum bending moment = 64.8000000 inches below pile headDepth of maximum shear force = 0.000000 inches below pile headNumber of iterations = 73Number of zero deflection points = 1

-------------------------------------------------------------------------------- Computed Values of Pile Loading and Deflection for Lateral Loading for Load Case Number 5--------------------------------------------------------------------------------

Pile-head conditions are Displacement and Moment (Loading Type 4)Displacement of pile head = 0.500000 inchesMoment at pile head = 0.000 in-lbsAxial load at pile head = 10000.000 lbs

Depth Deflect. Bending Shear Slope Total Bending Soil Res. Soil Spr. Distrib. X y Moment Force S Stress Stiffness p Es*h Lat. Load feet inches in-lbs lbs radians psi* lb-in^2 lb/in lb/inch lb/inch ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- 0.00 0.5000 0.000 28963. -0.007926 0.000 6.087E+10-668.4651 1604.3162 0.000 0.200 0.4810 67775. 27354. -0.007925 0.000 6.087E+10-672.3618 3354.9819 0.000 0.400 0.4620 131678. 25739. -0.007921 0.000 6.074E+10-673.3531 3498.2416 0.000 0.600 0.4430 191702. 24118. -0.007915 0.000 6.061E+10-677.1069 3668.6675 0.000 0.800 0.4240 247826. 22496. -0.007906 0.000 6.048E+10-675.1114 3821.6611 0.000 1.000 0.4050 300061. 20887. -0.007895 0.000 6.037E+10-665.3898 3942.9837 0.000 1.200 0.3861 348462. 19304. -0.007882 0.000 6.024E+10-653.7995 4064.3063 0.000 1.400 0.3672 393098. 17751. -0.007867 0.000 6.013E+10-640.3531 4185.6288 0.000 1.600 0.3483 434045. 16233. -0.007851 0.000 6.003E+10-625.0633 4306.9514 0.000 1.800 0.3295 471391. 14753. -0.007833 0.000 5.994E+10-607.9433 4428.2740 0.000 2.000 0.3107 505235. 13317. -0.007813 0.000 5.985E+10-589.0064 4549.5966 0.000 2.200 0.2920 535685. 11928. -0.007792 0.000 5.978E+10-568.2657 4670.9191 0.000 2.400 0.2733 562862. 10591. -0.007770 0.000 5.971E+10-545.7347 4792.2417 0.000 2.600 0.2547 586895. 9310.4371 -0.007730 0.000 2.457E+10-521.4268 4913.5643 0.000 2.800 0.2362 607924. 8090.0951 -0.007561 0.000 5.203E+09-495.5249 5034.8869 0.000 3.000 0.2184 626091. 6932.4252 -0.007276 0.000 5.175E+09

Page 34

existing phase1 87.lp6o-469.2000 5156.2094 0.000 3.200 0.2013 641548. 5838.2570 -0.006981 0.000 5.154E+09-442.6068 5277.5320 0.000 3.400 0.1849 654449. 4808.0534 -0.006679 0.000 5.130E+09-415.8962 5398.8546 0.000 3.600 0.1692 664948. 3841.9165 -0.006369 0.000 5.099E+09-389.2179 5520.1772 0.000 3.800 0.1543 673196. 2939.5888 -0.006054 0.000 5.071E+09-362.7218 5641.4997 0.000 4.000 0.1402 679348. 2100.4576 -0.005733 0.000 5.050E+09-336.5542 5762.8223 0.000 4.200 0.1268 683554. 1323.5654 -0.005409 0.000 5.035E+09-310.8560 5884.1449 0.000 4.400 0.1142 685961. 607.6230 -0.005082 0.000 5.023E+09-285.7627 6005.4675 0.000 4.600 0.1024 686714. -48.9781 -0.004754 0.000 5.017E+09-261.4049 6126.7900 0.000 4.800 0.0914 685954. -648.1514 -0.004425 0.000 5.023E+09-237.9063 6248.1126 0.000 5.000 0.0812 683816. -1192.0971 -0.004099 0.000 5.034E+09-215.3818 6369.4352 0.000 5.200 0.0717 680429. -1683.2826 -0.003774 0.000 5.046E+09-193.9395 6490.7578 0.000 5.400 0.0630 675917. -2124.4283 -0.003452 0.000 5.063E+09-173.6820 6612.0803 0.000 5.600 0.0551 670397. -2518.4933 -0.003133 0.000 5.081E+09-154.7056 6733.4029 0.000 5.800 0.0480 663979. -2868.6615 -0.002819 0.000 5.102E+09-137.1013 6854.7255 0.000 6.000 0.0416 656763. -3178.3278 -0.002509 0.000 5.125E+09-120.9540 6976.0480 0.000 6.200 0.0360 648843. -3451.0850 -0.002204 0.000 5.144E+09-106.3437 7097.3706 0.000 6.400 0.0310 640303. -3690.7142 -0.001903 0.000 5.156E+09-93.3474 7218.6932 0.000 6.600 0.0268 631219. -3901.1800 -0.001608 0.000 5.168E+09-82.0408 7340.0158 0.000 6.800 0.0233 621655. -4086.6239 -0.001317 0.000 5.182E+09-72.4957 7461.3383 0.000 7.000 0.0205 611666. -4251.3542 -0.001032 0.000 5.196E+09-64.7795 7582.6609 0.000 7.200 0.0184 601298. -4399.8359 -0.000784 0.000 6.782E+09-58.9553 7703.9835 0.000 7.400 0.0167 590585. -4536.0782 -0.000632 0.000 1.536E+10-54.5800 7825.3061 0.000 7.600 0.0153 579555. -4662.5026 -0.000566 0.000 3.626E+10-50.7736 7946.6286 0.000 7.800 0.0140 568232. -4779.9926 -0.000536 0.000 5.969E+10-47.1347 8067.9512 0.000 8.000 0.0128 556637. -4888.8144 -0.000513 0.000 5.972E+10-43.5501 8189.2738 0.000 8.200 0.0116 544790. -4989.1036 -0.000491 0.000 5.975E+10-40.0242 8310.5964 0.000 8.400 0.0104 532713. -5081.0059 -0.000469 0.000 5.979E+10-36.5610 8431.9189 0.000 8.600 0.009306 520424. -5164.6762 -0.000448 0.000 5.982E+10-33.1643 8553.2415 0.000 8.800 0.008255 507944. -5240.2782 -0.000428 0.000 5.985E+10-29.8374 8674.5641 0.000 9.000 0.007253 495291. -5307.9831 -0.000407 0.000 5.988E+10-26.5834 8795.8867 0.000 9.200 0.006299 482485. -5367.9694 -0.000388 0.000 5.991E+10-23.4052 8917.2092 0.000

Page 35

existing phase1 87.lp6o 9.400 0.005392 469544. -5420.4219 -0.000369 0.000 5.994E+10-20.3052 9038.5318 0.000 9.600 0.004529 456485. -5465.5310 -0.000350 0.000 5.998E+10-17.2857 9159.8544 0.000 9.800 0.003710 443326. -5503.4920 -0.000332 0.000 6.001E+10-14.3485 9281.1770 0.000 10.000 0.002934 430084. -5540.1646 -0.000315 0.000 6.004E+10-16.2121 13261. 0.000 10.200 0.002199 416748. -5579.1977 -0.000298 0.000 6.007E+10-16.3155 17805. 0.000 10.400 0.001504 403318. -5612.3310 -0.000282 0.000 6.011E+10-11.2956 18021. 0.000 10.600 0.000848 389822. -5633.6185 -0.000266 0.000 6.014E+10-6.4440 18238. 0.000 10.800 0.000229 376289. -5643.4644 -0.000250 0.000 6.018E+10-1.7609 18455. 0.000 11.000 -0.000354 362746. -5642.2732 -0.000236 0.000 6.021E+102.7536 18671. 0.000 11.200 -0.000902 349218. -5630.4485 -0.000221 0.000 6.024E+107.1003 18888. 0.000 11.400 -0.001417 335730. -5608.3920 -0.000208 0.000 6.027E+1011.2801 19104. 0.000 11.600 -0.001900 322308. -5576.5025 -0.000195 0.000 6.030E+1015.2945 19321. 0.000 11.800 -0.002352 308972. -5535.1745 -0.000182 0.000 6.034E+1019.1455 19538. 0.000 12.000 -0.002774 295747. -5484.7975 -0.000170 0.000 6.037E+1022.8353 19754. 0.000 12.200 -0.003169 282654. -5425.7553 -0.000159 0.000 6.040E+1026.3666 19971. 0.000 12.400 -0.003536 269711. -5358.4247 -0.000148 0.000 6.043E+1029.7423 20187. 0.000 12.600 -0.003878 256940. -5283.1752 -0.000137 0.000 6.046E+1032.9657 20404. 0.000 12.800 -0.004195 244359. -5200.3677 -0.000127 0.000 6.049E+1036.0405 20621. 0.000 13.000 -0.004489 231985. -5110.3546 -0.000118 0.000 6.053E+1038.9705 20837. 0.000 13.200 -0.004760 219835. -5013.4782 -0.000109 0.000 6.055E+1041.7599 21054. 0.000 13.400 -0.005011 207925. -4910.0708 -0.000100 0.000 6.058E+1044.4130 21270. 0.000 13.600 -0.005242 196271. -4800.4539 -9.241E-05 0.000 6.060E+1046.9344 21487. 0.000 13.800 -0.005455 184887. -4684.9382 -8.486E-05 0.000 6.062E+1049.3288 21704. 0.000 14.000 -0.005650 173788. -4563.8224 -7.777E-05 0.000 6.065E+1051.6011 21920. 0.000 14.200 -0.005828 162985. -4437.3935 -7.110E-05 0.000 6.068E+1053.7563 22137. 0.000 14.400 -0.005991 152491. -4305.9263 -6.487E-05 0.000 6.072E+1055.7997 22353. 0.000 14.600 -0.006139 142319. -4169.6830 -5.904E-05 0.000 6.073E+1057.7364 22570. 0.000 14.800 -0.006274 132480. -4028.9133 -5.361E-05 0.000 6.074E+1059.5717 22787. 0.000 15.000 -0.006397 122983. -3888.7553 -4.856E-05 0.000 6.075E+1057.2266 21471. 0.000 15.200 -0.006507 113816. -3755.9137 -4.389E-05 0.000 6.077E+1053.4747 19722. 0.000 15.400 -0.006607 104957. -3625.9951 -3.957E-05 0.000 6.079E+1054.7907 19901. 0.000 15.600 -0.006697 96413. -3493.0002 -3.559E-05 0.000 6.081E+10

Page 36

existing phase1 87.lp6o56.0384 20081. 0.000 15.800 -0.006778 88192. -3357.0871 -3.195E-05 0.000 6.083E+1057.2225 20261. 0.000 16.000 -0.006851 80301. -3218.4029 -2.863E-05 0.000 6.085E+1058.3476 20441. 0.000 16.200 -0.006916 72745. -3077.0839 -2.561E-05 0.000 6.087E+1059.4182 20620. 0.000 16.400 -0.006974 65532. -2933.2553 -2.288E-05 0.000 6.087E+1060.4389 20800. 0.000 16.600 -0.007026 58667. -2787.0317 -2.044E-05 0.000 6.087E+1061.4141 20980. 0.000 16.800 -0.007072 52155. -2638.5171 -1.825E-05 0.000 6.087E+1062.3481 21159. 0.000 17.000 -0.007113 46003. -2487.8052 -1.632E-05 0.000 6.087E+1063.2451 21339. 0.000 17.200 -0.007150 40215. -2334.9799 -1.462E-05 0.000 6.087E+1064.1093 21519. 0.000 17.400 -0.007183 34796. -2180.1151 -1.314E-05 0.000 6.087E+1064.9447 21699. 0.000 17.600 -0.007213 29751. -2023.2755 -1.186E-05 0.000 6.087E+1065.7549 21878. 0.000 17.800 -0.007240 25084. -1864.5170 -1.078E-05 0.000 6.087E+1066.5438 22058. 0.000 18.000 -0.007265 20801. -1703.8867 -9.879E-06 0.000 6.087E+1067.3148 22238. 0.000 18.200 -0.007288 16906. -1541.4237 -9.136E-06 0.000 6.087E+1068.0710 22417. 0.000 18.400 -0.007309 13403. -1377.1597 -8.538E-06 0.000 6.087E+1068.8156 22597. 0.000 18.600 -0.007329 10296. -1211.1193 -8.071E-06 0.000 6.087E+1069.5514 22777. 0.000 18.800 -0.007348 7590.0994 -1043.3209 -7.718E-06 0.000 6.087E+1070.2807 22957. 0.000 19.000 -0.007366 5288.7195 -873.7768 -7.464E-06 0.000 6.087E+1071.0060 23136. 0.000 19.200 -0.007383 3396.3292 -702.4946 -7.293E-06 0.000 6.087E+1071.7292 23316. 0.000 19.400 -0.007401 1917.0956 -529.4774 -7.189E-06 0.000 6.087E+1072.4518 23496. 0.000 19.600 -0.007418 855.1826 -354.7250 -7.134E-06 0.000 6.087E+1073.1752 23675. 0.000 19.800 -0.007435 214.7581 -178.2342 -7.113E-06 0.000 6.087E+1073.9005 23855. 0.000 20.000 -0.007452 0.000 0.000 -7.109E-06 0.000 6.087E+1074.6280 12017. 0.000

* This analysis makes computations of pile response using nonlinear moment-curvaturerelationships. The above values of total stress are computed for combined axial and bending stress in elastic sections and do not equal actual stresses in concrete and steel in the range of nonlinear bending.

Output Summary for Load Case No. 5:

Pile-head deflection = 0.5000000 inchesComputed slope at pile head = -0.0079264 radiansMaximum bending moment = 686714. inch-lbsMaximum shear force = 28963. lbsDepth of maximum bending moment = 55.2000000 inches below pile headDepth of maximum shear force = 0.000000 inches below pile headNumber of iterations = 45

Page 37

existing phase1 87.lp6oNumber of zero deflection points = 1

-------------------------------------------------------------------------------- Computed Values of Pile Loading and Deflection for Lateral Loading for Load Case Number 6--------------------------------------------------------------------------------

Pile-head conditions are Displacement and Moment (Loading Type 4)Displacement of pile head = 0.750000 inchesMoment at pile head = 0.000 in-lbsAxial load at pile head = 10000.000 lbs

Depth Deflect. Bending Shear Slope Total Bending Soil Res. Soil Spr. Distrib. X y Moment Force S Stress Stiffness p Es*h Lat. Load feet inches in-lbs lbs radians psi* lb-in^2 lb/in lb/inch lb/inch ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- 0.00 0.7500 0.000 35608. -0.0130 0.000 6.087E+10-808.8662 1294.1858 0.000 0.200 0.7189 83441. 33662. -0.0130 0.000 6.087E+10-812.5077 2712.5707 0.000 0.400 0.6878 162202. 31712. -0.0130 0.000 6.068E+10-812.6210 2835.6635 0.000 0.600 0.6567 236282. 29758. -0.0130 0.000 6.051E+10-816.0490 2982.4646 0.000 0.800 0.6256 305661. 27791. -0.0129 0.000 6.035E+10-823.2718 3158.3043 0.000 1.000 0.5946 370298. 25810. -0.0129 0.000 6.019E+10-827.3342 3339.6019 0.000 1.200 0.5636 430170. 23823. -0.0129 0.000 6.004E+10-828.0489 3526.3944 0.000 1.400 0.5326 485271. 21840. -0.0129 0.000 5.990E+10-825.2276 3718.7153 0.000 1.600 0.5017 535618. 19867. -0.0129 0.000 5.978E+10-818.6809 3916.5930 0.000 1.800 0.4708 581250. 17915. -0.0128 0.000 3.902E+10-808.2187 4120.0501 0.000 2.000 0.4400 622225. 15992. -0.0127 0.000 5.181E+09-793.6761 4328.9541 0.000 2.200 0.4099 658622. 14109. -0.0124 0.000 5.120E+09-775.4740 4540.1487 0.000 2.400 0.3806 690544. 12275. -0.0121 0.000 4.989E+09-753.3329 4750.6483 0.000 2.600 0.3520 718120. 10506. -0.0117 0.000 4.711E+09-720.7119 4913.5643 0.000 2.800 0.3244 741535. 8824.5233 -0.0113 0.000 4.506E+09-680.4506 5034.8869 0.000 3.000 0.2976 761021. 7240.6695 -0.0109 0.000 4.267E+09-639.4276 5156.2094 0.000 3.200 0.2719 776814. 5755.8023 -0.0105 0.000 3.949E+09-597.9617 5277.5320 0.000 3.400 0.2474 789152. 4370.5125 -0.009982 0.000 3.732E+09-556.4464 5398.8546 0.000 3.600 0.2240 798272. 3084.4781 -0.009461 0.000 3.588E+09-515.2490 5520.1772 0.000 3.800 0.2019 804411. 1896.5350 -0.008918 0.000 3.498E+09-474.7036 5641.4997 0.000 4.000 0.1812 807803. 804.7613 -0.008361 0.000 3.451E+09

Page 38

existing phase1 87.lp6o-435.1079 5762.8223 0.000 4.200 0.1618 808676. -193.4334 -0.007798 0.000 3.439E+09-396.7210 5884.1449 0.000 4.400 0.1438 807249. -1101.2141 -0.007236 0.000 3.458E+09-359.7629 6005.4675 0.000 4.600 0.1271 803737. -1922.2254 -0.006681 0.000 3.508E+09-324.4132 6126.7900 0.000 4.800 0.1117 798343. -2660.4947 -0.006139 0.000 3.587E+09-290.8112 6248.1126 0.000 5.000 0.0976 791261. -3320.3365 -0.005615 0.000 3.698E+09-259.0569 6369.4352 0.000 5.200 0.0848 782675. -3906.2576 -0.005114 0.000 3.844E+09-229.2107 6490.7578 0.000 5.400 0.0731 772757. -4422.8648 -0.004640 0.000 4.028E+09-201.2953 6612.0803 0.000 5.600 0.0625 761668. -4874.7771 -0.004195 0.000 4.258E+09-175.2983 6733.4029 0.000 5.800 0.0529 749559. -5266.5439 -0.003778 0.000 4.443E+09-151.1740 6854.7255 0.000 6.000 0.0443 736570. -5602.6429 -0.003381 0.000 4.548E+09-128.9085 6976.0480 0.000 6.200 0.0367 722829. -5887.5740 -0.003001 0.000 4.668E+09-108.5341 7097.3706 0.000 6.400 0.0299 708454. -6125.8981 -0.002638 0.000 4.805E+09-90.0693 7218.6932 0.000 6.600 0.0240 693551. -6322.2038 -0.002293 0.000 4.961E+09-73.5188 7340.0158 0.000 6.800 0.0189 678217. -6481.0761 -0.001964 0.000 5.055E+09-58.8748 7461.3383 0.000 7.000 0.0146 662536. -6607.1141 -0.001648 0.000 5.107E+09-46.1569 7582.6609 0.000 7.200 0.0110 646582. -6704.9824 -0.001341 0.000 5.147E+09-35.4000 7703.9835 0.000 7.400 0.008171 630417. -6779.4308 -0.001044 0.000 5.169E+09-26.6404 7825.3061 0.000 7.600 0.006015 614091. -6835.3006 -0.000756 0.000 5.192E+09-19.9177 7946.6286 0.000 7.800 0.004542 597644. -6877.5225 -0.000530 0.000 8.513E+09-15.2672 8067.9512 0.000 8.000 0.003472 581104. -6910.0603 -0.000421 0.000 2.806E+10-11.8476 8189.2738 0.000 8.200 0.002522 564496. -6934.7569 -0.000385 0.000 5.970E+10-8.7329 8310.5964 0.000 8.400 0.001626 547836. -6952.0927 -0.000362 0.000 5.975E+10-5.7136 8431.9189 0.000 8.600 0.000783 531143. -6962.2992 -0.000341 0.000 5.979E+10-2.7919 8553.2415 0.000 8.800 -8.326E-06 514433. -6965.6134 -0.000320 0.000 5.983E+100.0301 8674.5641 0.000 9.000 -0.000751 497723. -6962.2765 -0.000299 0.000 5.987E+102.7506 8795.8867 0.000 9.200 -0.001445 481029. -6952.5339 -0.000280 0.000 5.991E+105.3682 8917.2092 0.000 9.400 -0.002093 464365. -6936.6338 -0.000261 0.000 5.996E+107.8819 9038.5318 0.000 9.600 -0.002696 447745. -6914.8265 -0.000242 0.000 6.000E+1010.2908 9159.8544 0.000 9.800 -0.003257 431185. -6887.3641 -0.000225 0.000 6.004E+1012.5945 9281.1770 0.000 10.000 -0.003776 414697. -6847.2153 -0.000208 0.000 6.008E+1020.8628 13261. 0.000 10.200 -0.004255 398328. -6784.2982 -0.000192 0.000 6.012E+1031.5681 17805. 0.000

Page 39

existing phase1 87.lp6o 10.400 -0.004696 382141. -6704.0985 -0.000176 0.000 6.016E+1035.2649 18021. 0.000 10.600 -0.005101 366157. -6615.2646 -0.000161 0.000 6.020E+1038.7633 18238. 0.000 10.800 -0.005471 350396. -6518.2703 -0.000147 0.000 6.024E+1042.0653 18455. 0.000 11.000 -0.005807 334877. -6413.5839 -0.000133 0.000 6.027E+1045.1734 18671. 0.000 11.200 -0.006111 319617. -6301.6676 -0.000120 0.000 6.031E+1048.0902 18888. 0.000 11.400 -0.006384 304634. -6182.9767 -0.000108 0.000 6.035E+1050.8189 19104. 0.000 11.600 -0.006629 289944. -6057.9583 -9.609E-05 0.000 6.039E+1053.3630 19321. 0.000 11.800 -0.006845 275561. -5927.0515 -8.486E-05 0.000 6.042E+1055.7260 19538. 0.000 12.000 -0.007036 261498. -5790.6859 -7.419E-05 0.000 6.045E+1057.9120 19754. 0.000 12.200 -0.007201 247769. -5649.2817 -6.408E-05 0.000 6.048E+1059.9249 19971. 0.000 12.400 -0.007343 234385. -5503.2486 -5.452E-05 0.000 6.052E+1061.7693 20187. 0.000 12.600 -0.007463 221356. -5352.9858 -4.549E-05 0.000 6.055E+1063.4497 20404. 0.000 12.800 -0.007562 208693. -5198.8814 -3.697E-05 0.000 6.057E+1064.9707 20621. 0.000 13.000 -0.007641 196403. -5041.3118 -2.894E-05 0.000 6.060E+1066.3373 20837. 0.000 13.200 -0.007701 184496. -4880.6420 -2.140E-05 0.000 6.062E+1067.5543 21054. 0.000 13.400 -0.007743 172977. -4717.2247 -1.433E-05 0.000 6.065E+1068.6268 21270. 0.000 13.600 -0.007770 161854. -4551.4007 -7.703E-06 0.000 6.068E+1069.5599 21487. 0.000 13.800 -0.007780 151131. -4383.4982 -1.516E-06 0.000 6.072E+1070.3588 21704. 0.000 14.000 -0.007777 140813. -4213.8331 4.253E-06 0.000 6.073E+1071.0288 21920. 0.000 14.200 -0.007760 130904. -4042.7087 9.622E-06 0.000 6.074E+1071.5749 22137. 0.000 14.400 -0.007731 121407. -3870.4161 1.461E-05 0.000 6.076E+1072.0023 22353. 0.000 14.600 -0.007690 112325. -3697.2339 1.922E-05 0.000 6.077E+1072.3162 22570. 0.000 14.800 -0.007638 103660. -3523.4285 2.349E-05 0.000 6.079E+1072.5217 22787. 0.000 15.000 -0.007577 95412. -3355.0596 2.742E-05 0.000 6.081E+1067.7857 21471. 0.000 15.200 -0.007507 87554. -3199.6936 3.103E-05 0.000 6.083E+1061.6860 19722. 0.000 15.400 -0.007428 80052. -3051.7550 3.433E-05 0.000 6.085E+1061.5962 19901. 0.000 15.600 -0.007342 72904. -2904.1219 3.735E-05 0.000 6.087E+1061.4313 20081. 0.000 15.800 -0.007249 66110. -2756.9700 4.009E-05 0.000 6.087E+1061.1953 20261. 0.000 16.000 -0.007150 59669. -2610.4653 4.257E-05 0.000 6.087E+1060.8920 20441. 0.000 16.200 -0.007045 53578. -2464.7646 4.480E-05 0.000 6.087E+1060.5253 20620. 0.000 16.400 -0.006934 47836. -2320.0154 4.680E-05 0.000 6.087E+1060.0990 20800. 0.000 16.600 -0.006820 42440. -2176.3566 4.858E-05 0.000 6.087E+10

Page 40

existing phase1 87.lp6o59.6166 20980. 0.000 16.800 -0.006701 37387. -2033.9186 5.015E-05 0.000 6.087E+1059.0817 21159. 0.000 17.000 -0.006579 32674. -1892.8235 5.153E-05 0.000 6.087E+1058.4975 21339. 0.000 17.200 -0.006454 28299. -1753.1857 5.274E-05 0.000 6.087E+1057.8674 21519. 0.000 17.400 -0.006326 24257. -1615.1118 5.377E-05 0.000 6.087E+1057.1942 21699. 0.000 17.600 -0.006196 20544. -1478.7015 5.466E-05 0.000 6.087E+1056.4810 21878. 0.000 17.800 -0.006064 17156. -1344.0478 5.540E-05 0.000 6.087E+1055.7304 22058. 0.000 18.000 -0.005930 14090. -1211.2372 5.601E-05 0.000 6.087E+1054.9450 22238. 0.000 18.200 -0.005795 11340. -1080.3506 5.652E-05 0.000 6.087E+1054.1271 22417. 0.000 18.400 -0.005659 8901.2796 -951.4634 5.691E-05 0.000 6.087E+1053.2789 22597. 0.000 18.600 -0.005522 6769.8404 -824.6460 5.722E-05 0.000 6.087E+1052.4023 22777. 0.000 18.800 -0.005384 4940.2319 -699.9645 5.745E-05 0.000 6.087E+1051.4990 22957. 0.000 19.000 -0.005246 3407.2530 -577.4810 5.762E-05 0.000 6.087E+1050.5706 23136. 0.000 19.200 -0.005107 2165.5576 -457.2541 5.773E-05 0.000 6.087E+1049.6184 23316. 0.000 19.400 -0.004969 1209.6622 -339.3399 5.780E-05 0.000 6.087E+1048.6435 23496. 0.000 19.600 -0.004830 533.9520 -223.7917 5.783E-05 0.000 6.087E+1047.6466 23675. 0.000 19.800 -0.004691 132.6860 -110.6616 5.784E-05 0.000 6.087E+1046.6285 23855. 0.000 20.000 -0.004552 0.000 0.000 5.785E-05 0.000 6.087E+1045.5895 12017. 0.000

* This analysis makes computations of pile response using nonlinear moment-curvaturerelationships. The above values of total stress are computed for combined axial and bending stress in elastic sections and do not equal actual stresses in concrete and steel in the range of nonlinear bending.

Output Summary for Load Case No. 6:

Pile-head deflection = 0.7500000 inchesComputed slope at pile head = -0.0129658 radiansMaximum bending moment = 808676. inch-lbsMaximum shear force = 35608. lbsDepth of maximum bending moment = 50.4000000 inches below pile headDepth of maximum shear force = 0.000000 inches below pile headNumber of iterations = 42Number of zero deflection points = 1

-------------------------------------------------------------------------------- Computed Values of Pile Loading and Deflection for Lateral Loading for Load Case Number 7--------------------------------------------------------------------------------

Pile-head conditions are Displacement and Moment (Loading Type 4)Page 41

existing phase1 87.lp6oDisplacement of pile head = 1.000000 inchesMoment at pile head = 0.000 in-lbsAxial load at pile head = 10000.000 lbs

Depth Deflect. Bending Shear Slope Total Bending Soil Res. Soil Spr. Distrib. X y Moment Force S Stress Stiffness p Es*h Lat. Load feet inches in-lbs lbs radians psi* lb-in^2 lb/in lb/inch lb/inch ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- 0.00 1.0000 0.000 39781. -0.0185 0.000 6.087E+10-893.1068 1071.7282 0.000 0.200 0.9557 93346. 37607. -0.0185 0.000 6.087E+10-919.2012 2308.3573 0.000 0.400 0.9114 181398. 35371. -0.0185 0.000 6.063E+10-943.5108 2484.5673 0.000 0.600 0.8671 264014. 33096. -0.0184 0.000 6.044E+10-952.8558 2637.3091 0.000 0.800 0.8229 341142. 30801. -0.0184 0.000 6.026E+10-959.3908 2798.2086 0.000 1.000 0.7786 412744. 28495. -0.0184 0.000 6.008E+10-961.9641 2965.0627 0.000 1.200 0.7345 478804. 26189. -0.0184 0.000 5.992E+10-960.3383 3138.1197 0.000 1.400 0.6903 539332. 23891. -0.0184 0.000 5.977E+10-954.2746 3317.6792 0.000 1.600 0.6462 594363. 21614. -0.0183 0.000 1.093E+10-943.5321 3504.1085 0.000 1.800 0.6025 643957. 19368. -0.0181 0.000 5.151E+09-928.1006 3697.2236 0.000 2.000 0.5594 688197. 17164. -0.0178 0.000 5.006E+09-908.1588 3896.2017 0.000 2.200 0.5172 727198. 15014. -0.0174 0.000 4.628E+09-883.6279 4100.7406 0.000 2.400 0.4758 761101. 12928. -0.0170 0.000 4.264E+09-854.4911 4310.1908 0.000 2.600 0.4355 790071. 10905. -0.0165 0.000 3.714E+09-831.9649 4585.1832 0.000 2.800 0.3964 814237. 8924.8589 -0.0160 0.000 3.363E+09-817.8137 4951.8175 0.000 3.000 0.3587 833678. 7018.8100 -0.0154 0.000 2.968E+09-770.5605 5156.2094 0.000 3.200 0.3226 848665. 5242.9376 -0.0146 0.000 2.536E+09-709.3332 5277.5320 0.000 3.400 0.2884 859547. 3613.1865 -0.0138 0.000 2.280E+09-648.7927 5398.8546 0.000 3.600 0.2564 866670. 2126.8830 -0.0128 0.000 2.134E+09-589.7935 5520.1772 0.000 3.800 0.2268 870372. 779.4606 -0.0118 0.000 2.064E+09-533.0585 5641.4997 0.000 4.000 0.1996 870980. -435.1981 -0.0108 0.000 2.053E+09-479.1570 5762.8223 0.000 4.200 0.1748 868803. -1524.3794 -0.009826 0.000 2.093E+09-428.4941 5884.1449 0.000 4.400 0.1524 864135. -2496.1422 -0.008853 0.000 2.184E+09-381.3083 6005.4675 0.000 4.600 0.1323 857247. -3358.9249 -0.007937 0.000 2.331E+09-337.6773 6126.7900 0.000 4.800 0.1143 848393. -4121.1725 -0.007096 0.000 2.544E+09-297.5289 6248.1126 0.000 5.000 0.0982 837806. -4790.9993 -0.006341 0.000 2.838E+09

Page 42

existing phase1 87.lp6o-260.6601 6369.4352 0.000 5.200 0.0838 825700. -5375.9108 -0.005678 0.000 3.209E+09-226.7661 6490.7578 0.000 5.400 0.0710 812274. -5882.6330 -0.005082 0.000 3.389E+09-195.5023 6612.0803 0.000 5.600 0.0595 797708. -6317.4057 -0.004528 0.000 3.595E+09-166.8083 6733.4029 0.000 5.800 0.0492 782168. -6686.2970 -0.004018 0.000 3.851E+09-140.6011 6854.7255 0.000 6.000 0.0402 765806. -6995.1307 -0.003554 0.000 4.167E+09-116.7603 6976.0480 0.000 6.200 0.0322 748762. -7249.4039 -0.003131 0.000 4.449E+09-95.1340 7097.3706 0.000 6.400 0.0251 731159. -7454.3027 -0.002738 0.000 4.594E+09-75.6150 7218.6932 0.000 6.600 0.0190 713113. -7614.8677 -0.002367 0.000 4.758E+09-58.1892 7340.0158 0.000 6.800 0.0138 694722. -7736.0894 -0.002019 0.000 4.947E+09-42.8290 7461.3383 0.000 7.000 0.009335 676076. -7822.8767 -0.001690 0.000 5.062E+09-29.4938 7582.6609 0.000 7.200 0.005663 657253. -7880.0840 -0.001376 0.000 5.123E+09-18.1790 7703.9835 0.000 7.400 0.002730 638318. -7912.5816 -0.001074 0.000 5.159E+09-8.9023 7825.3061 0.000 7.600 0.000510 619324. -7925.2914 -0.000782 0.000 5.185E+09-1.6891 7946.6286 0.000 7.800 -0.001022 600314. -7923.1956 -0.000517 0.000 5.950E+093.4356 8067.9512 0.000 8.000 -0.001973 581318. -7910.9940 -0.000361 0.000 1.962E+106.7324 8189.2738 0.000 8.200 -0.002753 562358. -7891.4738 -0.000314 0.000 5.971E+109.5344 8310.5964 0.000 8.400 -0.003480 543454. -7865.3630 -0.000292 0.000 5.976E+1012.2247 8431.9189 0.000 8.600 -0.004153 524619. -7832.9313 -0.000270 0.000 5.981E+1014.8017 8553.2415 0.000 8.800 -0.004777 505869. -7794.4522 -0.000250 0.000 5.985E+1017.2642 8674.5641 0.000 9.000 -0.005351 487217. -7750.2015 -0.000230 0.000 5.990E+1019.6113 8795.8867 0.000 9.200 -0.005879 468679. -7700.4570 -0.000210 0.000 5.994E+1021.8424 8917.2092 0.000 9.400 -0.006361 450265. -7645.4973 -0.000192 0.000 6.000E+1023.9573 9038.5318 0.000 9.600 -0.006801 431989. -7585.6014 -0.000174 0.000 6.004E+1025.9560 9159.8544 0.000 9.800 -0.007199 413863. -7521.0477 -0.000158 0.000 6.008E+1027.8388 9281.1770 0.000 10.000 -0.007557 395896. -7437.5354 -0.000141 0.000 6.012E+1041.7549 13261. 0.000 10.200 -0.007877 378169. -7317.3014 -0.000126 0.000 6.017E+1058.4401 17805. 0.000 10.400 -0.008162 360779. -7173.6314 -0.000111 0.000 6.021E+1061.2849 18021. 0.000 10.600 -0.008411 343741. -7023.3872 -9.718E-05 0.000 6.025E+1063.9186 18238. 0.000 10.800 -0.008628 327071. -6867.0711 -8.382E-05 0.000 6.029E+1066.3448 18455. 0.000 11.000 -0.008814 310783. -6705.1770 -7.113E-05 0.000 6.034E+1068.5669 18671. 0.000 11.200 -0.008969 294890. -6538.1898 -5.909E-05 0.000 6.038E+1070.5891 18888. 0.000

Page 43

existing phase1 87.lp6o 11.400 -0.009097 279403. -6366.5842 -4.768E-05 0.000 6.041E+1072.4155 19104. 0.000 11.600 -0.009198 264333. -6190.8252 -3.688E-05 0.000 6.044E+1074.0504 19321. 0.000 11.800 -0.009274 249689. -6011.3664 -2.668E-05 0.000 6.048E+1075.4985 19538. 0.000 12.000 -0.009326 235479. -5828.6506 -1.705E-05 0.000 6.052E+1076.7646 19754. 0.000 12.200 -0.009356 221712. -5643.1088 -7.988E-06 0.000 6.055E+1077.8536 19971. 0.000 12.400 -0.009365 208393. -5455.1598 5.337E-07 0.000 6.057E+1078.7706 20187. 0.000 12.600 -0.009354 195527. -5265.2104 8.534E-06 0.000 6.060E+1079.5206 20404. 0.000 12.800 -0.009324 183119. -5073.6549 1.603E-05 0.000 6.063E+1080.1089 20621. 0.000 13.000 -0.009277 171173. -4880.8752 2.304E-05 0.000 6.066E+1080.5409 20837. 0.000 13.200 -0.009213 159690. -4687.2402 2.958E-05 0.000 6.069E+1080.8217 21054. 0.000 13.400 -0.009135 148673. -4493.1061 3.568E-05 0.000 6.072E+1080.9567 21270. 0.000 13.600 -0.009042 138121. -4298.8165 4.135E-05 0.000 6.073E+1080.9513 21487. 0.000 13.800 -0.008936 128036. -4104.7020 4.661E-05 0.000 6.075E+1080.8107 21704. 0.000 14.000 -0.008818 118417. -3911.0810 5.147E-05 0.000 6.076E+1080.5401 21920. 0.000 14.200 -0.008689 109261. -3718.2592 5.597E-05 0.000 6.078E+1080.1447 22137. 0.000 14.400 -0.008550 100566. -3526.5300 6.011E-05 0.000 6.080E+1079.6296 22353. 0.000 14.600 -0.008400 92331. -3336.1749 6.392E-05 0.000 6.082E+1078.9996 22570. 0.000 14.800 -0.008243 84550. -3147.4637 6.741E-05 0.000 6.084E+1078.2598 22787. 0.000 15.000 -0.008077 77219. -2966.8429 7.060E-05 0.000 6.087E+1072.2575 21471. 0.000 15.200 -0.007904 70305. -2802.1951 7.351E-05 0.000 6.087E+1064.9490 19722. 0.000 15.400 -0.007724 63765. -2647.3960 7.615E-05 0.000 6.087E+1064.0503 19901. 0.000 15.600 -0.007538 57594. -2494.8465 7.854E-05 0.000 6.087E+1063.0742 20081. 0.000 15.800 -0.007347 51786. -2344.7282 8.070E-05 0.000 6.087E+1062.0243 20261. 0.000 16.000 -0.007151 46336. -2197.2141 8.263E-05 0.000 6.087E+1060.9041 20441. 0.000 16.200 -0.006950 41236. -2052.4692 8.436E-05 0.000 6.087E+1059.7168 20620. 0.000 16.400 -0.006746 36480. -1910.6503 8.589E-05 0.000 6.087E+1058.4656 20800. 0.000 16.600 -0.006538 32061. -1771.9072 8.724E-05 0.000 6.087E+1057.1536 20980. 0.000 16.800 -0.006327 27970. -1636.3823 8.843E-05 0.000 6.087E+1055.7838 21159. 0.000 17.000 -0.006114 24202. -1504.2110 8.946E-05 0.000 6.087E+1054.3589 21339. 0.000 17.200 -0.005898 20746. -1375.5227 9.034E-05 0.000 6.087E+1052.8814 21519. 0.000 17.400 -0.005680 17595. -1250.4403 9.110E-05 0.000 6.087E+1051.3539 21699. 0.000 17.600 -0.005461 14739. -1129.0813 9.173E-05 0.000 6.087E+10

Page 44

existing phase1 87.lp6o49.7786 21878. 0.000 17.800 -0.005240 12171. -1011.5579 9.227E-05 0.000 6.087E+1048.1576 22058. 0.000 18.000 -0.005018 9879.5423 -897.9775 9.270E-05 0.000 6.087E+1046.4928 22238. 0.000 18.200 -0.004795 7856.0661 -788.4428 9.305E-05 0.000 6.087E+1044.7861 22417. 0.000 18.400 -0.004571 6090.5503 -683.0528 9.332E-05 0.000 6.087E+1043.0390 22597. 0.000 18.600 -0.004347 4572.9331 -581.9026 9.353E-05 0.000 6.087E+1041.2529 22777. 0.000 18.800 -0.004122 3292.9280 -485.0843 9.369E-05 0.000 6.087E+1039.4290 22957. 0.000 19.000 -0.003897 2240.0312 -392.6872 9.380E-05 0.000 6.087E+1037.5686 23136. 0.000 19.200 -0.003672 1403.5272 -304.7981 9.387E-05 0.000 6.087E+1035.6724 23316. 0.000 19.400 -0.003447 772.4947 -221.5019 9.391E-05 0.000 6.087E+1033.7411 23496. 0.000 19.600 -0.003221 335.8102 -142.8822 9.394E-05 0.000 6.087E+1031.7754 23675. 0.000 19.800 -0.002996 82.1515 -69.0210 9.394E-05 0.000 6.087E+1029.7756 23855. 0.000 20.000 -0.002770 0.000 0.000 9.395E-05 0.000 6.087E+1027.7419 12017. 0.000

* This analysis makes computations of pile response using nonlinear moment-curvaturerelationships. The above values of total stress are computed for combined axial and bending stress in elastic sections and do not equal actual stresses in concrete and steel in the range of nonlinear bending.

Output Summary for Load Case No. 7:

Pile-head deflection = 1.0000000 inchesComputed slope at pile head = -0.0184609 radiansMaximum bending moment = 870980. inch-lbsMaximum shear force = 39781. lbsDepth of maximum bending moment = 48.0000000 inches below pile headDepth of maximum shear force = 0.000000 inches below pile headNumber of iterations = 39Number of zero deflection points = 1

-------------------------------------------------------------------------------- Computed Values of Pile Loading and Deflection for Lateral Loading for Load Case Number 8--------------------------------------------------------------------------------

Pile-head conditions are Displacement and Moment (Loading Type 4)Displacement of pile head = 0.010000 inchesMoment at pile head = 0.000 in-lbsAxial load at pile head = 10000.000 lbs

Depth Deflect. Bending Shear Slope Total Bending Soil Res. Soil Spr. Distrib. X y Moment Force S Stress Stiffness p Es*h Lat. Load feet inches in-lbs lbs radians psi* lb-in^2 lb/in lb/inch lb/inch

Page 45

existing phase1 87.lp6o---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- 0.00 0.0100 0.000 1064.8147 -9.980E-05 0.000 6.087E+10-13.9015 1668.1854 0.000 0.200 0.009760 2517.9140 1031.2585 -9.975E-05 0.000 6.087E+10-14.0620 3457.6934 0.000 0.400 0.009521 4954.8285 997.3458 -9.960E-05 0.000 6.087E+10-14.1986 3579.0160 0.000 0.600 0.009282 7309.9545 963.1335 -9.936E-05 0.000 6.087E+10-14.3117 3700.3385 0.000 0.800 0.009044 9582.6383 928.6773 -9.902E-05 0.000 6.087E+10-14.4018 3821.6611 0.000 1.000 0.008807 11772. 894.0321 -9.860E-05 0.000 6.087E+10-14.4693 3942.9837 0.000 1.200 0.008571 13879. 859.2514 -9.810E-05 0.000 6.087E+10-14.5146 4064.3063 0.000 1.400 0.008336 15901. 824.3877 -9.751E-05 0.000 6.087E+10-14.5385 4185.6288 0.000 1.600 0.008103 17840. 789.4920 -9.685E-05 0.000 6.087E+10-14.5412 4306.9514 0.000 1.800 0.007871 19696. 754.6143 -9.611E-05 0.000 6.087E+10-14.5236 4428.2740 0.000 2.000 0.007642 21467. 719.8029 -9.529E-05 0.000 6.087E+10-14.4860 4549.5966 0.000 2.200 0.007414 23155. 685.1047 -9.441E-05 0.000 6.087E+10-14.4291 4670.9191 0.000 2.400 0.007188 24760. 650.5654 -9.347E-05 0.000 6.087E+10-14.3536 4792.2417 0.000 2.600 0.006965 26283. 616.2288 -9.246E-05 0.000 6.087E+10-14.2602 4913.5643 0.000 2.800 0.006745 27723. 582.1374 -9.140E-05 0.000 6.087E+10-14.1493 5034.8869 0.000 3.000 0.006527 29081. 548.3321 -9.028E-05 0.000 6.087E+10-14.0218 5156.2094 0.000 3.200 0.006311 30359. 514.8519 -8.911E-05 0.000 6.087E+10-13.8783 5277.5320 0.000 3.400 0.006099 31557. 481.7345 -8.789E-05 0.000 6.087E+10-13.7195 5398.8546 0.000 3.600 0.005889 32675. 449.0158 -8.662E-05 0.000 6.087E+10-13.5461 5520.1772 0.000 3.800 0.005683 33716. 416.7300 -8.531E-05 0.000 6.087E+10-13.3588 5641.4997 0.000 4.000 0.005480 34680. 384.9096 -8.396E-05 0.000 6.087E+10-13.1583 5762.8223 0.000 4.200 0.005280 35568. 353.5854 -8.258E-05 0.000 6.087E+10-12.9452 5884.1449 0.000 4.400 0.005084 36381. 322.7866 -8.116E-05 0.000 6.087E+10-12.7204 6005.4675 0.000 4.600 0.004890 37121. 292.5406 -7.971E-05 0.000 6.087E+10-12.4846 6126.7900 0.000 4.800 0.004701 37789. 262.8731 -7.823E-05 0.000 6.087E+10-12.2383 6248.1126 0.000 5.000 0.004515 38387. 233.8083 -7.673E-05 0.000 6.087E+10-11.9824 6369.4352 0.000 5.200 0.004333 38915. 205.3685 -7.521E-05 0.000 6.087E+10-11.7175 6490.7578 0.000 5.400 0.004154 39376. 177.5744 -7.367E-05 0.000 6.087E+10-11.4443 6612.0803 0.000 5.600 0.003979 39771. 150.4451 -7.210E-05 0.000 6.087E+10-11.1635 6733.4029 0.000 5.800 0.003808 40102. 123.9980 -7.053E-05 0.000 6.087E+10-10.8757 6854.7255 0.000 6.000 0.003640 40369. 98.2491 -6.894E-05 0.000 6.087E+10

Page 46

existing phase1 87.lp6o-10.5817 6976.0480 0.000 6.200 0.003477 40576. 73.2126 -6.735E-05 0.000 6.087E+10-10.2821 7097.3706 0.000 6.400 0.003317 40724. 48.9011 -6.575E-05 0.000 6.087E+10-9.9774 7218.6932 0.000 6.600 0.003161 40814. 25.3261 -6.414E-05 0.000 6.087E+10-9.6685 7340.0158 0.000 6.800 0.003009 40849. 2.4971 -6.253E-05 0.000 6.087E+10-9.3557 7461.3383 0.000 7.000 0.002861 40829. -19.5776 -6.092E-05 0.000 6.087E+10-9.0398 7582.6609 0.000 7.200 0.002717 40758. -40.8909 -5.931E-05 0.000 6.087E+10-8.7213 7703.9835 0.000 7.400 0.002577 40636. -61.4376 -5.770E-05 0.000 6.087E+10-8.4009 7825.3061 0.000 7.600 0.002440 40466. -81.2133 -5.611E-05 0.000 6.087E+10-8.0789 7946.6286 0.000 7.800 0.002307 40249. -100.2153 -5.451E-05 0.000 6.087E+10-7.7560 8067.9512 0.000 8.000 0.002178 39987. -118.4418 -5.293E-05 0.000 6.087E+10-7.4327 8189.2738 0.000 8.200 0.002053 39683. -135.8924 -5.136E-05 0.000 6.087E+10-7.1095 8310.5964 0.000 8.400 0.001932 39337. -152.5680 -4.980E-05 0.000 6.087E+10-6.7868 8431.9189 0.000 8.600 0.001814 38953. -168.4702 -4.826E-05 0.000 6.087E+10-6.4651 8553.2415 0.000 8.800 0.001700 38531. -183.6021 -4.673E-05 0.000 6.087E+10-6.1448 8674.5641 0.000 9.000 0.001590 38074. -197.9675 -4.522E-05 0.000 6.087E+10-5.8264 8795.8867 0.000 9.200 0.001483 37583. -211.5714 -4.373E-05 0.000 6.087E+10-5.5102 8917.2092 0.000 9.400 0.001380 37060. -224.4195 -4.226E-05 0.000 6.087E+10-5.1966 9038.5318 0.000 9.600 0.001280 36508. -236.5184 -4.081E-05 0.000 6.087E+10-4.8859 9159.8544 0.000 9.800 0.001184 35927. -247.8757 -3.938E-05 0.000 6.087E+10-4.5785 9281.1770 0.000 10.000 0.001091 35320. -260.6046 -3.798E-05 0.000 6.087E+10-6.0288 13261. 0.000 10.200 0.001002 34678. -276.7564 -3.660E-05 0.000 6.087E+10-7.4310 17805. 0.000 10.400 0.000915 33993. -293.9227 -3.524E-05 0.000 6.087E+10-6.8742 18021. 0.000 10.600 0.000832 33269. -309.7632 -3.392E-05 0.000 6.087E+10-6.3263 18238. 0.000 10.800 0.000753 32508. -324.2999 -3.262E-05 0.000 6.087E+10-5.7876 18455. 0.000 11.000 0.000676 31714. -337.5550 -3.135E-05 0.000 6.087E+10-5.2584 18671. 0.000 11.200 0.000602 30889. -349.5519 -3.012E-05 0.000 6.087E+10-4.7390 18888. 0.000 11.400 0.000531 30037. -360.3141 -2.892E-05 0.000 6.087E+10-4.2295 19104. 0.000 11.600 0.000463 29161. -369.8657 -2.775E-05 0.000 6.087E+10-3.7302 19321. 0.000 11.800 0.000398 28263. -378.2311 -2.662E-05 0.000 6.087E+10-3.2410 19538. 0.000 12.000 0.000336 27347. -385.4348 -2.552E-05 0.000 6.087E+10-2.7621 19754. 0.000 12.200 0.000276 26414. -391.5014 -2.446E-05 0.000 6.087E+10-2.2934 19971. 0.000

Page 47

existing phase1 87.lp6o 12.400 0.000218 25469. -396.4553 -2.344E-05 0.000 6.087E+10-1.8349 20187. 0.000 12.600 0.000163 24513. -400.3211 -2.246E-05 0.000 6.087E+10-1.3865 20404. 0.000 12.800 0.000110 23548. -403.1227 -2.151E-05 0.000 6.087E+10-0.9482 20621. 0.000 13.000 5.985E-05 22579. -404.8841 -2.060E-05 0.000 6.087E+10-0.5196 20837. 0.000 13.200 1.148E-05 21606. -405.6285 -1.973E-05 0.000 6.087E+10-0.1007 21054. 0.000 13.400 -3.484E-05 20633. -405.3788 -1.890E-05 0.000 6.087E+100.3088 21270. 0.000 13.600 -7.922E-05 19661. -404.1571 -1.810E-05 0.000 6.087E+100.7092 21487. 0.000 13.800 -0.000122 18693. -401.9850 -1.734E-05 0.000 6.087E+101.1008 21704. 0.000 14.000 -0.000162 17732. -398.8833 -1.663E-05 0.000 6.087E+101.4839 21920. 0.000 14.200 -0.000202 16780. -394.8719 -1.595E-05 0.000 6.087E+101.8589 22137. 0.000 14.400 -0.000239 15838. -389.9698 -1.530E-05 0.000 6.087E+102.2262 22353. 0.000 14.600 -0.000275 14909. -384.1950 -1.470E-05 0.000 6.087E+102.5861 22570. 0.000 14.800 -0.000310 13994. -377.5648 -1.413E-05 0.000 6.087E+102.9391 22787. 0.000 15.000 -0.000343 13097. -370.3577 -1.359E-05 0.000 6.087E+103.0668 21471. 0.000 15.200 -0.000375 12217. -362.9816 -1.309E-05 0.000 6.087E+103.0800 19722. 0.000 15.400 -0.000406 11355. -355.2490 -1.263E-05 0.000 6.087E+103.3638 19901. 0.000 15.600 -0.000435 10513. -346.8404 -1.220E-05 0.000 6.087E+103.6433 20081. 0.000 15.800 -0.000464 9690.9510 -337.7657 -1.180E-05 0.000 6.087E+103.9189 20261. 0.000 16.000 -0.000492 8891.8784 -328.0339 -1.143E-05 0.000 6.087E+104.1910 20441. 0.000 16.200 -0.000519 8116.9372 -317.6528 -1.110E-05 0.000 6.087E+104.4600 20620. 0.000 16.400 -0.000545 7367.6777 -306.6292 -1.079E-05 0.000 6.087E+104.7263 20800. 0.000 16.600 -0.000571 6645.6350 -294.9689 -1.052E-05 0.000 6.087E+104.9906 20980. 0.000 16.800 -0.000596 5952.3317 -282.6766 -1.027E-05 0.000 6.087E+105.2531 21159. 0.000 17.000 -0.000620 5289.2804 -269.7557 -1.005E-05 0.000 6.087E+105.5143 21339. 0.000 17.200 -0.000644 4657.9867 -256.2088 -9.851E-06 0.000 6.087E+105.7747 21519. 0.000 17.400 -0.000667 4059.9508 -242.0376 -9.679E-06 0.000 6.087E+106.0347 21699. 0.000 17.600 -0.000691 3496.6710 -227.2423 -9.530E-06 0.000 6.087E+106.2947 21878. 0.000 17.800 -0.000713 2969.6453 -211.8226 -9.403E-06 0.000 6.087E+106.5551 22058. 0.000 18.000 -0.000736 2480.3740 -195.7769 -9.295E-06 0.000 6.087E+106.8163 22238. 0.000 18.200 -0.000758 2030.3622 -179.1030 -9.206E-06 0.000 6.087E+107.0786 22417. 0.000 18.400 -0.000780 1621.1214 -161.7976 -9.134E-06 0.000 6.087E+107.3425 22597. 0.000 18.600 -0.000802 1254.1720 -143.8567 -9.078E-06 0.000 6.087E+10

Page 48

existing phase1 87.lp6o7.6082 22777. 0.000 18.800 -0.000823 931.0448 -125.2756 -9.035E-06 0.000 6.087E+107.8761 22957. 0.000 19.000 -0.000845 653.2830 -106.0487 -9.003E-06 0.000 6.087E+108.1463 23136. 0.000 19.200 -0.000867 422.4434 -86.1700 -8.982E-06 0.000 6.087E+108.4192 23316. 0.000 19.400 -0.000888 240.0983 -65.6329 -8.969E-06 0.000 6.087E+108.6950 23496. 0.000 19.600 -0.000910 107.8359 -44.4305 -8.962E-06 0.000 6.087E+108.9737 23675. 0.000 19.800 -0.000931 27.2619 -22.5554 -8.959E-06 0.000 6.087E+109.2556 23855. 0.000 20.000 -0.000953 0.000 0.000 -8.959E-06 0.000 6.087E+109.5406 12017. 0.000

* This analysis makes computations of pile response using nonlinear moment-curvaturerelationships. The above values of total stress are computed for combined axial and bending stress in elastic sections and do not equal actual stresses in concrete and steel in the range of nonlinear bending.

Output Summary for Load Case No. 8:

Pile-head deflection = 0.0100000 inchesComputed slope at pile head = -0.0000998 radiansMaximum bending moment = 40849. inch-lbsMaximum shear force = 1064.8147015 lbsDepth of maximum bending moment = 81.6000000 inches below pile headDepth of maximum shear force = 0.000000 inches below pile headNumber of iterations = 6Number of zero deflection points = 1

-------------------------------------------------------------------------------- Computed Values of Pile Loading and Deflection for Lateral Loading for Load Case Number 9--------------------------------------------------------------------------------

Pile-head conditions are Displacement and Pile-head Rotation (Loading Type 5)Displacement of pile head = 0.100000 inchesRotation of pile head = 0.000E+00 radiansAxial load on pile head = 10000.000 lbs

Depth Deflect. Bending Shear Slope Total Bending Soil Res. Soil Spr. Distrib. X y Moment Force S Stress Stiffness p Es*h Lat. Load feet inches in-lbs lbs radians psi* lb-in^2 lb/in lb/inch lb/inch ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- 0.00 0.1000 -680688. 17543. 0.000 0.000 5.046E+09-139.0155 1668.1854 0.000 0.200 0.0996 -638993. 17199. -0.000314 0.000 5.046E+09-143.5108 3457.6934 0.000 0.400 0.0985 -598118. 16850. -0.000513 0.000 1.529E+10-146.8791 3579.0160 0.000 0.600 0.0972 -558086. 16494. -0.000571 0.000 5.970E+10-149.7871 3700.3385 0.000

Page 49

existing phase1 87.lp6o 0.800 0.0958 -518917. 16132. -0.000593 0.000 5.982E+10-152.4736 3821.6611 0.000 1.000 0.0943 -480625. 15763. -0.000613 0.000 5.991E+10-154.9367 3942.9837 0.000 1.200 0.0928 -443225. 15388. -0.000631 0.000 6.001E+10-157.1753 4064.3063 0.000 1.400 0.0913 -406731. 15009. -0.000648 0.000 6.010E+10-159.1887 4185.6288 0.000 1.600 0.0897 -371152. 14625. -0.000664 0.000 6.019E+10-160.9769 4306.9514 0.000 1.800 0.0881 -336501. 14236. -0.000678 0.000 6.027E+10-162.5404 4428.2740 0.000 2.000 0.0864 -302786. 13845. -0.000690 0.000 6.036E+10-163.8800 4549.5966 0.000 2.200 0.0848 -270014. 13450. -0.000702 0.000 6.043E+10-164.9974 4670.9191 0.000 2.400 0.0831 -238192. 13053. -0.000712 0.000 6.051E+10-165.8945 4792.2417 0.000 2.600 0.0814 -207326. 12654. -0.000721 0.000 6.058E+10-166.5735 4913.5643 0.000 2.800 0.0796 -177419. 12254. -0.000728 0.000 6.064E+10-167.0373 5034.8869 0.000 3.000 0.0779 -148474. 11852. -0.000735 0.000 6.072E+10-167.2890 5156.2094 0.000 3.200 0.0761 -120492. 11451. -0.000740 0.000 6.076E+10-167.3322 5277.5320 0.000 3.400 0.0743 -93474. 11049. -0.000744 0.000 6.081E+10-167.1707 5398.8546 0.000 3.600 0.0725 -67419. 10649. -0.000747 0.000 6.087E+10-166.8087 5520.1772 0.000 3.800 0.0707 -42325. 10249. -0.000750 0.000 6.087E+10-166.2507 5641.4997 0.000 4.000 0.0689 -18188. 9850.8825 -0.000751 0.000 6.087E+10-165.5014 5762.8223 0.000 4.200 0.0671 4995.2723 9454.8019 -0.000751 0.000 6.087E+10-164.5657 5884.1449 0.000 4.400 0.0653 27231. 9061.1842 -0.000750 0.000 6.087E+10-163.4490 6005.4675 0.000 4.600 0.0635 48525. 8670.4573 -0.000749 0.000 6.087E+10-162.1567 6126.7900 0.000 4.800 0.0617 68885. 8283.0361 -0.000747 0.000 6.087E+10-160.6943 6248.1126 0.000 5.000 0.0599 88319. 7899.3216 -0.000744 0.000 6.083E+10-159.0678 6369.4352 0.000 5.200 0.0582 106837. 7519.7007 -0.000740 0.000 6.078E+10-157.2830 6490.7578 0.000 5.400 0.0564 124449. 7144.5457 -0.000735 0.000 6.075E+10-155.3462 6612.0803 0.000 5.600 0.0546 141167. 6774.2142 -0.000730 0.000 6.073E+10-153.2634 6733.4029 0.000 5.800 0.0529 157001. 6409.0486 -0.000724 0.000 6.070E+10-151.0412 6854.7255 0.000 6.000 0.0512 171965. 6049.3761 -0.000717 0.000 6.066E+10-148.6859 6976.0480 0.000 6.200 0.0494 186072. 5695.5084 -0.000710 0.000 6.062E+10-146.2039 7097.3706 0.000 6.400 0.0477 199337. 5347.7415 -0.000703 0.000 6.059E+10-143.6018 7218.6932 0.000 6.600 0.0461 211775. 5006.3558 -0.000695 0.000 6.057E+10-140.8863 7340.0158 0.000 6.800 0.0444 223401. 4671.6157 -0.000686 0.000 6.055E+10-138.0638 7461.3383 0.000 7.000 0.0428 234232. 4343.7702 -0.000677 0.000 6.052E+10

Page 50

existing phase1 87.lp6o-135.1409 7582.6609 0.000 7.200 0.0412 244284. 4023.0521 -0.000667 0.000 6.049E+10-132.1242 7703.9835 0.000 7.400 0.0396 253574. 3709.6788 -0.000658 0.000 6.047E+10-129.0202 7825.3061 0.000 7.600 0.0380 262122. 3403.8519 -0.000647 0.000 6.045E+10-125.8355 7946.6286 0.000 7.800 0.0365 269944. 3105.7577 -0.000637 0.000 6.043E+10-122.5764 8067.9512 0.000 8.000 0.0349 277060. 2815.5670 -0.000626 0.000 6.041E+10-119.2493 8189.2738 0.000 8.200 0.0335 283489. 2533.4354 -0.000615 0.000 6.040E+10-115.8604 8310.5964 0.000 8.400 0.0320 289250. 2259.5036 -0.000603 0.000 6.039E+10-112.4161 8431.9189 0.000 8.600 0.0306 294363. 1993.8976 -0.000592 0.000 6.038E+10-108.9222 8553.2415 0.000 8.800 0.0292 298849. 1736.7291 -0.000580 0.000 6.037E+10-105.3849 8674.5641 0.000 9.000 0.0278 302727. 1488.0953 -0.000568 0.000 6.036E+10-101.8099 8795.8867 0.000 9.200 0.0264 306019. 1248.0799 -0.000556 0.000 6.035E+10-98.2030 8917.2092 0.000 9.400 0.0251 308745. 1016.7527 -0.000544 0.000 6.034E+10-94.5697 9038.5318 0.000 9.600 0.0238 310926. 794.1706 -0.000531 0.000 6.034E+10-90.9154 9159.8544 0.000 9.800 0.0226 312582. 580.3774 -0.000519 0.000 6.033E+10-87.2456 9281.1770 0.000 10.000 0.0213 313736. 334.2570 -0.000506 0.000 6.033E+10-117.8548 13261. 0.000 10.200 0.0201 314211. 13.6296 -0.000494 0.000 6.033E+10-149.3347 17805. 0.000 10.400 0.0190 313826. -336.4060 -0.000481 0.000 6.033E+10-142.3616 18021. 0.000 10.600 0.0178 312620. -669.7260 -0.000469 0.000 6.033E+10-135.4050 18238. 0.000 10.800 0.0167 310633. -986.3784 -0.000457 0.000 6.034E+10-128.4720 18455. 0.000 11.000 0.0156 307907. -1286.4279 -0.000444 0.000 6.034E+10-121.5692 18671. 0.000 11.200 0.0146 304480. -1569.9541 -0.000432 0.000 6.035E+10-114.7026 18888. 0.000 11.400 0.0136 300392. -1837.0501 -0.000420 0.000 6.037E+10-107.8774 19104. 0.000 11.600 0.0126 295682. -2087.8211 -0.000408 0.000 6.037E+10-101.0984 19321. 0.000 11.800 0.0116 290390. -2322.3828 -0.000397 0.000 6.038E+10-94.3697 19538. 0.000 12.000 0.0107 284554. -2540.8599 -0.000385 0.000 6.040E+10-87.6946 19754. 0.000 12.200 0.009743 278212. -2743.3845 -0.000374 0.000 6.041E+10-81.0760 19971. 0.000 12.400 0.008859 271403. -2930.0950 -0.000363 0.000 6.042E+10-74.5161 20187. 0.000 12.600 0.008000 264165. -3101.1340 -0.000352 0.000 6.044E+10-68.0165 20404. 0.000 12.800 0.007167 256535. -3256.6477 -0.000342 0.000 6.046E+10-61.5782 20621. 0.000 13.000 0.006358 248550. -3396.7837 -0.000332 0.000 6.048E+10-55.2018 20837. 0.000 13.200 0.005573 240246. -3521.6902 -0.000322 0.000 6.050E+10-48.8869 21054. 0.000

Page 51

existing phase1 87.lp6o 13.400 0.004810 231661. -3631.5142 -0.000313 0.000 6.053E+10-42.6331 21270. 0.000 13.600 0.004070 222830. -3726.4006 -0.000304 0.000 6.055E+10-36.4390 21487. 0.000 13.800 0.003351 213789. -3806.4909 -0.000295 0.000 6.056E+10-30.3029 21704. 0.000 14.000 0.002652 204573. -3871.9217 -0.000287 0.000 6.058E+10-24.2228 21920. 0.000 14.200 0.001973 195218. -3922.8241 -0.000279 0.000 6.060E+10-18.1959 22137. 0.000 14.400 0.001312 185757. -3959.3223 -0.000272 0.000 6.062E+10-12.2192 22353. 0.000 14.600 0.000669 176226. -3981.5324 -0.000264 0.000 6.064E+10-6.2892 22570. 0.000 14.800 4.235E-05 166658. -3989.5620 -0.000258 0.000 6.067E+10-0.4021 22787. 0.000 15.000 -0.000568 157088. -3983.9442 -0.000251 0.000 6.070E+105.0836 21471. 0.000 15.200 -0.001164 147547. -3966.3664 -0.000245 0.000 6.072E+109.5646 19722. 0.000 15.400 -0.001746 138061. -3937.5185 -0.000240 0.000 6.073E+1014.4753 19901. 0.000 15.600 -0.002314 128659. -3896.9119 -0.000234 0.000 6.074E+1019.3636 20081. 0.000 15.800 -0.002871 119368. -3844.5948 -0.000229 0.000 6.076E+1024.2340 20261. 0.000 16.000 -0.003416 110216. -3780.6043 -0.000225 0.000 6.078E+1029.0914 20441. 0.000 16.200 -0.003950 101231. -3704.9658 -0.000221 0.000 6.079E+1033.9407 20620. 0.000 16.400 -0.004475 92443. -3617.6927 -0.000217 0.000 6.082E+1038.7869 20800. 0.000 16.600 -0.004992 83877. -3518.7862 -0.000213 0.000 6.084E+1043.6352 20980. 0.000 16.800 -0.005500 75563. -3408.2349 -0.000210 0.000 6.087E+1048.4908 21159. 0.000 17.000 -0.006001 67528. -3286.0151 -0.000208 0.000 6.087E+1053.3590 21339. 0.000 17.200 -0.006496 59800. -3152.0904 -0.000205 0.000 6.087E+1058.2449 21519. 0.000 17.400 -0.006985 52407. -3006.4120 -0.000203 0.000 6.087E+1063.1538 21699. 0.000 17.600 -0.007469 45379. -2848.9185 -0.000201 0.000 6.087E+1068.0907 21878. 0.000 17.800 -0.007949 38742. -2679.5368 -0.000199 0.000 6.087E+1073.0607 22058. 0.000 18.000 -0.008426 32526. -2498.1818 -0.000198 0.000 6.087E+1078.0685 22238. 0.000 18.200 -0.008899 26760. -2304.7567 -0.000197 0.000 6.087E+1083.1190 22417. 0.000 18.400 -0.009369 21473. -2099.1542 -0.000196 0.000 6.087E+1088.2164 22597. 0.000 18.600 -0.009838 16694. -1881.2564 -0.000195 0.000 6.087E+1093.3651 22777. 0.000 18.800 -0.0103 12452. -1650.9358 -0.000194 0.000 6.087E+1098.5688 22957. 0.000 19.000 -0.0108 8778.6656 -1408.0560 -0.000194 0.000 6.087E+10103.8311 23136. 0.000 19.200 -0.0112 5703.0147 -1152.4727 -0.000194 0.000 6.087E+10109.1550 23316. 0.000 19.400 -0.0117 3256.0914 -884.0346 -0.000193 0.000 6.087E+10114.5434 23496. 0.000 19.600 -0.0122 1468.9348 -602.5847 -0.000193 0.000 6.087E+10

Page 52

existing phase1 87.lp6o119.9982 23675. 0.000 19.800 -0.0126 372.9665 -307.9614 -0.000193 0.000 6.087E+10125.5212 23855. 0.000 20.000 -0.0131 0.000 0.000 -0.000193 0.000 6.087E+10131.1133 12017. 0.000

* This analysis makes computations of pile response using nonlinear moment-curvaturerelationships. The above values of total stress are computed for combined axial and bending stress in elastic sections and do not equal actual stresses in concrete and steel in the range of nonlinear bending.

Output Summary for Load Case No. 9:

Pile-head deflection = 0.1000000 inchesComputed slope at pile head = -0.000009916 radiansMaximum bending moment = -680688. inch-lbsMaximum shear force = 17543. lbsDepth of maximum bending moment = 0.000000 inches below pile headDepth of maximum shear force = 0.000000 inches below pile headNumber of iterations = 22Number of zero deflection points = 1

-------------------------------------------------------------------------------- Computed Values of Pile Loading and Deflection for Lateral Loading for Load Case Number 10--------------------------------------------------------------------------------

Pile-head conditions are Displacement and Pile-head Rotation (Loading Type 5)Displacement of pile head = 0.200000 inchesRotation of pile head = 0.000E+00 radiansAxial load on pile head = 10000.000 lbs

Depth Deflect. Bending Shear Slope Total Bending Soil Res. Soil Spr. Distrib. X y Moment Force S Stress Stiffness p Es*h Lat. Load feet inches in-lbs lbs radians psi* lb-in^2 lb/in lb/inch lb/inch ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- 0.00 0.2000 -831680. 29166. 0.000 0.000 3.087E+09-278.0309 1668.1854 0.000 0.200 0.1992 -762501. 28477. -0.000620 0.000 3.087E+09-287.0233 3457.6934 0.000 0.400 0.1970 -694961. 27780. -0.001085 0.000 4.946E+09-293.8156 3579.0160 0.000 0.600 0.1940 -629105. 27069. -0.001399 0.000 5.171E+09-299.1377 3700.3385 0.000 0.800 0.1903 -564964. 26346. -0.001558 0.000 5.310E+10-303.0399 3821.6611 0.000 1.000 0.1865 -502569. 25614. -0.001581 0.000 5.986E+10-306.4665 3942.9837 0.000 1.200 0.1827 -441939. 24875. -0.001600 0.000 6.001E+10-309.4300 4064.3063 0.000 1.400 0.1789 -383091. 24130. -0.001616 0.000 6.016E+10-311.9335 4185.6288 0.000 1.600 0.1750 -326038. 23379. -0.001630 0.000 6.029E+10-313.9809 4306.9514 0.000

Page 53

existing phase1 87.lp6o 1.800 0.1710 -270795. 22623. -0.001642 0.000 6.043E+10-315.5768 4428.2740 0.000 2.000 0.1671 -217368. 21864. -0.001652 0.000 6.056E+10-316.7265 4549.5966 0.000 2.200 0.1631 -165766. 21103. -0.001660 0.000 6.067E+10-317.4362 4670.9191 0.000 2.400 0.1591 -115992. 20341. -0.001665 0.000 6.076E+10-317.7126 4792.2417 0.000 2.600 0.1551 -68048. 19579. -0.001669 0.000 6.087E+10-317.5630 4913.5643 0.000 2.800 0.1511 -21933. 18817. -0.001671 0.000 6.087E+10-316.9953 5034.8869 0.000 3.000 0.1471 22356. 18058. -0.001671 0.000 6.087E+10-316.0179 5156.2094 0.000 3.200 0.1431 64825. 17301. -0.001669 0.000 6.087E+10-314.6397 5277.5320 0.000 3.400 0.1391 105482. 16548. -0.001665 0.000 6.078E+10-312.8700 5398.8546 0.000 3.600 0.1351 144336. 15800. -0.001661 0.000 6.073E+10-310.7187 5520.1772 0.000 3.800 0.1311 181400. 15057. -0.001654 0.000 6.063E+10-308.1961 5641.4997 0.000 4.000 0.1272 216689. 14321. -0.001646 0.000 6.056E+10-305.3125 5762.8223 0.000 4.200 0.1232 250219. 13592. -0.001637 0.000 6.048E+10-302.0790 5884.1449 0.000 4.400 0.1193 282009. 12871. -0.001626 0.000 6.040E+10-298.5068 6005.4675 0.000 4.600 0.1154 312079. 12160. -0.001615 0.000 6.033E+10-294.6072 6126.7900 0.000 4.800 0.1115 340452. 11458. -0.001602 0.000 6.026E+10-290.3919 6248.1126 0.000 5.000 0.1077 367153. 10766. -0.001587 0.000 6.020E+10-285.8727 6369.4352 0.000 5.200 0.1039 392206. 10086. -0.001572 0.000 6.013E+10-281.0616 6490.7578 0.000 5.400 0.1002 415639. 9417.2658 -0.001556 0.000 6.007E+10-275.9706 6612.0803 0.000 5.600 0.0965 437483. 8761.3671 -0.001539 0.000 6.002E+10-270.6117 6733.4029 0.000 5.800 0.0928 457768. 8118.6364 -0.001521 0.000 5.997E+10-264.9972 6854.7255 0.000 6.000 0.0892 476526. 7489.6728 -0.001503 0.000 5.992E+10-259.1391 6976.0480 0.000 6.200 0.0856 493790. 6875.0464 -0.001483 0.000 5.988E+10-253.0496 7097.3706 0.000 6.400 0.0820 509597. 6275.2981 -0.001463 0.000 5.984E+10-246.7407 7218.6932 0.000 6.600 0.0785 523982. 5690.9401 -0.001442 0.000 5.981E+10-240.2243 7340.0158 0.000 6.800 0.0751 536983. 5122.4563 -0.001421 0.000 5.977E+10-233.5123 7461.3383 0.000 7.000 0.0717 548638. 4570.3019 -0.001399 0.000 5.974E+10-226.6164 7582.6609 0.000 7.200 0.0684 558987. 4034.9045 -0.001377 0.000 5.972E+10-219.5481 7703.9835 0.000 7.400 0.0651 568072. 3516.6643 -0.001354 0.000 5.969E+10-212.3188 7825.3061 0.000 7.600 0.0619 575932. 3015.9544 -0.001331 0.000 5.967E+10-204.9396 7946.6286 0.000 7.800 0.0587 582612. 2533.1212 -0.001308 0.000 5.966E+10-197.4214 8067.9512 0.000 8.000 0.0556 588154. 2068.4855 -0.001283 0.000 5.434E+10

Page 54

existing phase1 87.lp6o-189.7750 8189.2738 0.000 8.200 0.0526 592602. 1622.3196 -0.001253 0.000 4.173E+10-182.0299 8310.5964 0.000 8.400 0.0496 596001. 1194.7669 -0.001215 0.000 3.387E+10-174.2640 8431.9189 0.000 8.600 0.0467 598396. 785.7787 -0.001169 0.000 2.915E+10-166.5594 8553.2415 0.000 8.800 0.0440 599829. 395.1164 -0.001118 0.000 2.653E+10-158.9925 8674.5641 0.000 9.000 0.0414 600346. 22.3752 -0.001062 0.000 2.546E+10-151.6251 8795.8867 0.000 9.200 0.0389 599988. -332.9723 -0.001006 0.000 2.569E+10-144.4978 8917.2092 0.000 9.400 0.0365 598796. -671.5213 -0.000951 0.000 2.720E+10-137.6263 9038.5318 0.000 9.600 0.0343 596810. -993.8748 -0.000901 0.000 3.015E+10-131.0016 9159.8544 0.000 9.800 0.0322 594069. -1300.5886 -0.000857 0.000 3.494E+10-124.5933 9281.1770 0.000 10.000 0.0302 590608. -1650.4059 -0.000820 0.000 4.225E+10-166.9212 13261. 0.000 10.200 0.0283 586186. -2102.4997 -0.000790 0.000 5.410E+10-209.8236 17805. 0.000 10.400 0.0264 580554. -2592.3352 -0.000765 0.000 5.966E+10-198.3727 18021. 0.000 10.600 0.0246 573779. -3054.7956 -0.000742 0.000 5.968E+10-187.0110 18238. 0.000 10.800 0.0229 565927. -3490.1072 -0.000719 0.000 5.970E+10-175.7487 18455. 0.000 11.000 0.0212 557061. -3898.5191 -0.000697 0.000 5.972E+10-164.5946 18671. 0.000 11.200 0.0195 547247. -4280.3008 -0.000674 0.000 5.975E+10-153.5568 18888. 0.000 11.400 0.0179 536548. -4635.7392 -0.000653 0.000 5.978E+10-142.6419 19104. 0.000 11.600 0.0164 525027. -4965.1366 -0.000631 0.000 5.981E+10-131.8559 19321. 0.000 11.800 0.0149 512746. -5268.8076 -0.000611 0.000 5.984E+10-121.2034 19538. 0.000 12.000 0.0134 499766. -5547.0775 -0.000590 0.000 5.987E+10-110.6882 19754. 0.000 12.200 0.0121 486148. -5800.2789 -0.000571 0.000 5.990E+10-100.3130 19971. 0.000 12.400 0.0107 471952. -6028.7501 -0.000551 0.000 5.994E+10-90.0797 20187. 0.000 12.600 0.009409 457237. -6232.8326 -0.000533 0.000 5.998E+10-79.9891 20404. 0.000 12.800 0.008152 442060. -6412.8687 -0.000515 0.000 6.001E+10-70.0410 20621. 0.000 13.000 0.006938 426480. -6569.1991 -0.000497 0.000 6.005E+10-60.2344 20837. 0.000 13.200 0.005764 410552. -6702.1614 -0.000481 0.000 6.009E+10-50.5675 21054. 0.000 13.400 0.004630 394333. -6812.0876 -0.000465 0.000 6.013E+10-41.0377 21270. 0.000 13.600 0.003534 377876. -6899.3024 -0.000449 0.000 6.018E+10-31.6413 21487. 0.000 13.800 0.002474 361237. -6964.1211 -0.000434 0.000 6.021E+10-22.3742 21704. 0.000 14.000 0.001449 344469. -7006.8479 -0.000420 0.000 6.025E+10-13.2314 21920. 0.000 14.200 0.000456 327625. -7027.7743 -0.000407 0.000 6.029E+10-4.2073 22137. 0.000

Page 55

existing phase1 87.lp6o 14.400 -0.000505 310756. -7027.1775 -0.000394 0.000 6.034E+104.7045 22353. 0.000 14.600 -0.001437 293913. -7005.3191 -0.000382 0.000 6.038E+1013.5108 22570. 0.000 14.800 -0.002340 277148. -6962.4433 -0.000371 0.000 6.041E+1022.2191 22787. 0.000 15.000 -0.003217 260511. -6901.2411 -0.000360 0.000 6.045E+1028.7828 21471. 0.000 15.200 -0.004070 244040. -6826.5716 -0.000350 0.000 6.049E+1033.4417 19722. 0.000 15.400 -0.004899 227761. -6737.6961 -0.000341 0.000 6.054E+1040.6212 19901. 0.000 15.600 -0.005706 211715. -6631.6585 -0.000332 0.000 6.057E+1047.7435 20081. 0.000 15.800 -0.006493 195945. -6508.5863 -0.000324 0.000 6.060E+1054.8167 20261. 0.000 16.000 -0.007262 180490. -6368.5871 -0.000317 0.000 6.063E+1061.8492 20441. 0.000 16.200 -0.008013 165391. -6211.7486 -0.000310 0.000 6.067E+1068.8495 20620. 0.000 16.400 -0.008749 150688. -6038.1376 -0.000304 0.000 6.072E+1075.8263 20800. 0.000 16.600 -0.009471 136422. -5847.8001 -0.000298 0.000 6.073E+1082.7883 20980. 0.000 16.800 -0.0102 122633. -5640.7611 -0.000293 0.000 6.075E+1089.7443 21159. 0.000 17.000 -0.0109 109360. -5417.0244 -0.000288 0.000 6.078E+1096.7030 21339. 0.000 17.200 -0.0116 96645. -5176.5731 -0.000284 0.000 6.080E+10103.6731 21519. 0.000 17.400 -0.0122 84527. -4919.3694 -0.000281 0.000 6.084E+10110.6633 21699. 0.000 17.600 -0.0129 73045. -4645.3551 -0.000277 0.000 6.087E+10117.6820 21878. 0.000 17.800 -0.0136 62242. -4354.4519 -0.000275 0.000 6.087E+10124.7374 22058. 0.000 18.000 -0.0142 52157. -4046.5622 -0.000273 0.000 6.087E+10131.8374 22238. 0.000 18.200 -0.0149 42832. -3721.5698 -0.000271 0.000 6.087E+10138.9897 22417. 0.000 18.400 -0.0155 34307. -3379.3405 -0.000269 0.000 6.087E+10146.2013 22597. 0.000 18.600 -0.0162 26624. -3019.7239 -0.000268 0.000 6.087E+10153.4792 22777. 0.000 18.800 -0.0168 19825. -2642.5535 -0.000267 0.000 6.087E+10160.8295 22957. 0.000 19.000 -0.0175 13952. -2247.6488 -0.000266 0.000 6.087E+10168.2578 23136. 0.000 19.200 -0.0181 9049.0039 -1834.8166 -0.000266 0.000 6.087E+10175.7691 23316. 0.000 19.400 -0.0187 5158.0370 -1403.8525 -0.000266 0.000 6.087E+10183.3676 23496. 0.000 19.600 -0.0194 2323.2628 -954.5430 -0.000265 0.000 6.087E+10191.0569 23675. 0.000 19.800 -0.0200 588.9741 -486.6675 -0.000265 0.000 6.087E+10198.8394 23855. 0.000 20.000 -0.0206 0.000 0.000 -0.000265 0.000 6.087E+10206.7168 12017. 0.000

* This analysis makes computations of pile response using nonlinear moment-curvaturerelationships. The above values of total stress are computed for combined axial and bending stress in elastic

Page 56

existing phase1 87.lp6o sections and do not equal actual stresses in concrete and steel in the range of nonlinear bending.

Output Summary for Load Case No. 10:

Pile-head deflection = 0.2000000 inchesComputed slope at pile head = -0.0000269 radiansMaximum bending moment = -831680. inch-lbsMaximum shear force = 29166. lbsDepth of maximum bending moment = 0.000000 inches below pile headDepth of maximum shear force = 0.000000 inches below pile headNumber of iterations = 36Number of zero deflection points = 1

-------------------------------------------------------------------------------- Computed Values of Pile Loading and Deflection for Lateral Loading for Load Case Number 11--------------------------------------------------------------------------------

Pile-head conditions are Displacement and Pile-head Rotation (Loading Type 5)Displacement of pile head = 0.300000 inchesRotation of pile head = 0.000E+00 radiansAxial load on pile head = 10000.000 lbs

Depth Deflect. Bending Shear Slope Total Bending Soil Res. Soil Spr. Distrib. X y Moment Force S Stress Stiffness p Es*h Lat. Load feet inches in-lbs lbs radians psi* lb-in^2 lb/in lb/inch lb/inch ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- 0.00 0.3000 -893560. 35572. 0.000 0.000 1.443E+09-417.0464 1668.1854 0.000 0.200 0.2982 -809406. 34541. -0.001417 0.000 1.443E+09-429.6417 3457.6934 0.000 0.400 0.2932 -727694. 33501. -0.002279 0.000 4.623E+09-437.2375 3579.0160 0.000 0.600 0.2873 -648492. 32445. -0.002619 0.000 5.144E+09-442.9285 3700.3385 0.000 0.800 0.2806 -571834. 31377. -0.002782 0.000 5.968E+10-446.8645 3821.6611 0.000 1.000 0.2739 -497749. 30301. -0.002803 0.000 5.987E+10-450.0377 3942.9837 0.000 1.200 0.2672 -426256. 29218. -0.002822 0.000 6.005E+10-452.4520 4064.3063 0.000 1.400 0.2604 -357369. 28130. -0.002837 0.000 6.022E+10-454.1125 4185.6288 0.000 1.600 0.2536 -291097. 27039. -0.002850 0.000 6.038E+10-455.0250 4306.9514 0.000 1.800 0.2467 -227446. 25947. -0.002860 0.000 6.054E+10-455.1960 4428.2740 0.000 2.000 0.2398 -166416. 24855. -0.002868 0.000 6.067E+10-454.6331 4549.5966 0.000 2.200 0.2329 -108005. 23765. -0.002874 0.000 6.078E+10-453.3443 4670.9191 0.000 2.400 0.2260 -52205. 22680. -0.002877 0.000 6.087E+10-451.3383 4792.2417 0.000 2.600 0.2191 994.9661 21600. -0.002878 0.000 6.087E+10-448.6244 4913.5643 0.000

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existing phase1 87.lp6o 2.800 0.2122 51611. 20527. -0.002877 0.000 6.087E+10-445.2124 5034.8869 0.000 3.000 0.2053 99663. 19463. -0.002874 0.000 6.080E+10-441.1127 5156.2094 0.000 3.200 0.1984 145174. 18410. -0.002869 0.000 6.072E+10-436.3359 5277.5320 0.000 3.400 0.1915 188171. 17370. -0.002862 0.000 6.062E+10-430.8933 5398.8546 0.000 3.600 0.1847 228686. 16343. -0.002854 0.000 6.054E+10-424.7964 5520.1772 0.000 3.800 0.1778 266754. 15332. -0.002844 0.000 6.043E+10-418.0570 5641.4997 0.000 4.000 0.1710 302414. 14337. -0.002833 0.000 6.036E+10-410.6872 5762.8223 0.000 4.200 0.1643 335708. 13361. -0.002820 0.000 6.027E+10-402.6993 5884.1449 0.000 4.400 0.1575 366682. 12405. -0.002806 0.000 6.020E+10-394.1058 6005.4675 0.000 4.600 0.1508 395386. 11470. -0.002791 0.000 6.013E+10-384.9191 6126.7900 0.000 4.800 0.1441 421872. 10558. -0.002775 0.000 6.006E+10-375.1519 6248.1126 0.000 5.000 0.1375 446197. 9669.9716 -0.002757 0.000 6.001E+10-364.8168 6369.4352 0.000 5.200 0.1309 468421. 8807.4798 -0.002739 0.000 5.995E+10-353.9263 6490.7578 0.000 5.400 0.1243 488605. 7971.7768 -0.002720 0.000 5.989E+10-342.4929 6612.0803 0.000 5.600 0.1178 506816. 7164.1505 -0.002700 0.000 5.985E+10-330.5290 6733.4029 0.000 5.800 0.1114 523122. 6385.8595 -0.002679 0.000 5.981E+10-318.0468 6854.7255 0.000 6.000 0.1050 537596. 5638.1333 -0.002658 0.000 5.977E+10-305.0584 6976.0480 0.000 6.200 0.0986 550313. 4922.1726 -0.002636 0.000 5.974E+10-291.5756 7097.3706 0.000 6.400 0.0923 561349. 4239.1498 -0.002614 0.000 5.971E+10-277.6101 7218.6932 0.000 6.600 0.0861 570786. 3590.2099 -0.002591 0.000 5.969E+10-263.1732 7340.0158 0.000 6.800 0.0799 578707. 2976.4708 -0.002568 0.000 5.967E+10-248.2761 7461.3383 0.000 7.000 0.0737 585197. 2399.0241 -0.002542 0.000 4.810E+10-232.9295 7582.6609 0.000 7.200 0.0677 590344. 1858.8835 -0.002494 0.000 2.113E+10-217.1876 7703.9835 0.000 7.400 0.0618 594239. 1356.6297 -0.002397 0.000 1.139E+10-201.3572 7825.3061 0.000 7.600 0.0562 596971. 891.8913 -0.002238 0.000 7.406E+09-185.9248 7946.6286 0.000 7.800 0.0510 598628. 462.9975 -0.002016 0.000 5.723E+09-171.4867 8067.9512 0.000 8.000 0.0465 599290. 66.9114 -0.001753 0.000 5.231E+09-158.5850 8189.2738 0.000 8.200 0.0426 599033. -300.4022 -0.001483 0.000 5.450E+09-147.5097 8310.5964 0.000 8.400 0.0394 597919. -643.3336 -0.001242 0.000 6.576E+09-138.2665 8431.9189 0.000 8.600 0.0366 596004. -965.9277 -0.001054 0.000 9.037E+09-130.5618 8553.2415 0.000 8.800 0.0343 593334. -1271.3481 -0.000923 0.000 1.359E+10-123.9552 8674.5641 0.000 9.000 0.0322 589946. -1561.7344 -0.000839 0.000 2.250E+10

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existing phase1 87.lp6o-118.0334 8795.8867 0.000 9.200 0.0303 585878. -1838.3284 -0.000791 0.000 4.199E+10-112.4616 8917.2092 0.000 9.400 0.0284 581160. -2101.6781 -0.000762 0.000 5.966E+10-106.9965 9038.5318 0.000 9.600 0.0266 575826. -2351.9431 -0.000739 0.000 5.968E+10-101.5577 9159.8544 0.000 9.800 0.0249 569906. -2589.1945 -0.000716 0.000 5.969E+10-96.1518 9281.1770 0.000 10.000 0.0232 563432. -2858.2209 -0.000693 0.000 5.971E+10-128.0368 13261. 0.000 10.200 0.0215 556220. -3203.5923 -0.000671 0.000 5.972E+10-159.7727 17805. 0.000 10.400 0.0200 548087. -3575.1175 -0.000648 0.000 5.974E+10-149.8316 18021. 0.000 10.600 0.0184 539091. -3922.9231 -0.000627 0.000 5.977E+10-140.0064 18238. 0.000 10.800 0.0169 529287. -4247.2962 -0.000605 0.000 5.980E+10-130.3045 18455. 0.000 11.000 0.0155 518733. -4548.5406 -0.000584 0.000 5.982E+10-120.7325 18671. 0.000 11.200 0.0141 507482. -4826.9748 -0.000564 0.000 5.985E+10-111.2960 18888. 0.000 11.400 0.0128 495590. -5082.9297 -0.000543 0.000 5.988E+10-101.9997 19104. 0.000 11.600 0.0115 483110. -5316.7464 -0.000524 0.000 5.991E+10-92.8475 19321. 0.000 11.800 0.0103 470095. -5528.7742 -0.000505 0.000 5.994E+10-83.8423 19538. 0.000 12.000 0.009110 456597. -5719.3685 -0.000486 0.000 5.998E+10-74.9862 19754. 0.000 12.200 0.007965 442666. -5888.8884 -0.000468 0.000 6.001E+10-66.2804 19971. 0.000 12.400 0.006863 428352. -6037.6951 -0.000451 0.000 6.004E+10-57.7252 20187. 0.000 12.600 0.005801 413706. -6166.1499 -0.000434 0.000 6.008E+10-49.3204 20404. 0.000 12.800 0.004779 398776. -6274.6122 -0.000418 0.000 6.012E+10-41.0648 20621. 0.000 13.000 0.003796 383608. -6363.4378 -0.000402 0.000 6.016E+10-32.9565 20837. 0.000 13.200 0.002849 368250. -6432.9771 -0.000387 0.000 6.020E+10-24.9929 21054. 0.000 13.400 0.001937 352748. -6483.5732 -0.000373 0.000 6.023E+10-17.1706 21270. 0.000 13.600 0.001060 337147. -6515.5609 -0.000359 0.000 6.027E+10-9.4858 21487. 0.000 13.800 0.000214 321491. -6529.2646 -0.000346 0.000 6.031E+10-1.9340 21704. 0.000 14.000 -0.000601 305823. -6524.9972 -0.000333 0.000 6.035E+105.4901 21920. 0.000 14.200 -0.001387 290187. -6503.0588 -0.000322 0.000 6.039E+1012.7920 22137. 0.000 14.400 -0.002145 274624. -6463.7348 -0.000310 0.000 6.042E+1019.9779 22353. 0.000 14.600 -0.002877 259176. -6407.2960 -0.000300 0.000 6.045E+1027.0545 22570. 0.000 14.800 -0.003584 243883. -6333.9962 -0.000290 0.000 6.049E+1034.0287 22787. 0.000 15.000 -0.004268 228787. -6247.3424 -0.000280 0.000 6.054E+1038.1828 21471. 0.000 15.200 -0.004930 213910. -6152.9062 -0.000272 0.000 6.056E+1040.5141 19722. 0.000

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existing phase1 87.lp6o 15.400 -0.005572 199266. -6048.8423 -0.000264 0.000 6.059E+1046.2059 19901. 0.000 15.600 -0.006195 184888. -5931.1929 -0.000256 0.000 6.062E+1051.8353 20081. 0.000 15.800 -0.006800 170808. -5800.0989 -0.000249 0.000 6.066E+1057.4097 20261. 0.000 16.000 -0.007390 157059. -5655.6834 -0.000242 0.000 6.070E+1062.9366 20441. 0.000 16.200 -0.007964 143673. -5498.0510 -0.000236 0.000 6.073E+1068.4237 20620. 0.000 16.400 -0.008524 130680. -5327.2880 -0.000231 0.000 6.074E+1073.8787 20800. 0.000 16.600 -0.009073 118113. -5143.4624 -0.000226 0.000 6.076E+1079.3093 20980. 0.000 16.800 -0.009610 106002. -4946.6231 -0.000222 0.000 6.078E+1084.7233 21159. 0.000 17.000 -0.0101 94380. -4736.8009 -0.000218 0.000 6.081E+1090.1285 21339. 0.000 17.200 -0.0107 83276. -4514.0080 -0.000214 0.000 6.084E+1095.5324 21519. 0.000 17.400 -0.0112 72723. -4278.2381 -0.000211 0.000 6.087E+10100.9425 21699. 0.000 17.600 -0.0117 62751. -4029.4674 -0.000208 0.000 6.087E+10106.3664 21878. 0.000 17.800 -0.0122 53391. -3767.6545 -0.000206 0.000 6.087E+10111.8110 22058. 0.000 18.000 -0.0127 44676. -3492.7412 -0.000204 0.000 6.087E+10117.2833 22238. 0.000 18.200 -0.0131 36636. -3204.6533 -0.000203 0.000 6.087E+10122.7899 22417. 0.000 18.400 -0.0136 29303. -2903.3012 -0.000201 0.000 6.087E+10128.3369 22597. 0.000 18.600 -0.0141 22710. -2588.5807 -0.000200 0.000 6.087E+10133.9301 22777. 0.000 18.800 -0.0146 16888. -2260.3746 -0.000200 0.000 6.087E+10139.5750 22957. 0.000 19.000 -0.0151 11870. -1918.5530 -0.000199 0.000 6.087E+10145.2763 23136. 0.000 19.200 -0.0155 7688.1495 -1562.9756 -0.000199 0.000 6.087E+10151.0382 23316. 0.000 19.400 -0.0160 4376.7604 -1193.4923 -0.000198 0.000 6.087E+10156.8645 23496. 0.000 19.600 -0.0165 1968.9068 -809.9453 -0.000198 0.000 6.087E+10162.7580 23675. 0.000 19.800 -0.0170 498.5374 -412.1706 -0.000198 0.000 6.087E+10168.7209 23855. 0.000 20.000 -0.0175 0.000 0.000 -0.000198 0.000 6.087E+10174.7546 12017. 0.000

* This analysis makes computations of pile response using nonlinear moment-curvaturerelationships. The above values of total stress are computed for combined axial and bending stress in elastic sections and do not equal actual stresses in concrete and steel in the range of nonlinear bending.

Output Summary for Load Case No. 11:

Pile-head deflection = 0.3000000 inchesComputed slope at pile head = -0.0000700 radiansMaximum bending moment = -893560. inch-lbsMaximum shear force = 35572. lbs

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existing phase1 87.lp6oDepth of maximum bending moment = 0.000000 inches below pile headDepth of maximum shear force = 0.000000 inches below pile headNumber of iterations = 94Number of zero deflection points = 1

-------------------------------------------------------------------------------- Computed Values of Pile Loading and Deflection for Lateral Loading for Load Case Number 12--------------------------------------------------------------------------------

Pile-head conditions are Displacement and Pile-head Rotation (Loading Type 5)Displacement of pile head = 0.500000 inchesRotation of pile head = 0.000E+00 radiansAxial load on pile head = 10000.000 lbs

Depth Deflect. Bending Shear Slope Total Bending Soil Res. Soil Spr. Distrib. X y Moment Force S Stress Stiffness p Es*h Lat. Load feet inches in-lbs lbs radians psi* lb-in^2 lb/in lb/inch lb/inch ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- 0.00 0.5000 -905598. 45135. 0.000 0.000 5.868E+08-668.4651 1604.3162 0.000 0.200 0.4956 -799192. 43500. -0.003486 0.000 5.868E+08-680.9493 3297.8731 0.000 0.400 0.4833 -696629. 41859. -0.005290 0.000 4.925E+09-686.4920 3409.2673 0.000 0.600 0.4702 -598012. 40202. -0.005597 0.000 5.235E+09-694.7917 3546.6584 0.000 0.800 0.4564 -503391. 38520. -0.005744 0.000 5.986E+10-706.5051 3715.2026 0.000 1.000 0.4426 -412839. 36813. -0.005763 0.000 6.008E+10-716.1786 3883.5918 0.000 1.200 0.4287 -326412. 35085. -0.005778 0.000 6.029E+10-723.6852 4051.0741 0.000 1.400 0.4149 -244153. 33349. -0.005789 0.000 6.049E+10-723.5121 4185.6288 0.000 1.600 0.4010 -166061. 31617. -0.005797 0.000 6.067E+10-719.5301 4306.9514 0.000 1.800 0.3870 -92113. 29897. -0.005802 0.000 6.082E+10-714.1132 4428.2740 0.000 2.000 0.3731 -22278. 28191. -0.005804 0.000 6.087E+10-707.2723 4549.5966 0.000 2.200 0.3592 43482. 26503. -0.005804 0.000 6.087E+10-699.0190 4670.9191 0.000 2.400 0.3452 105217. 24837. -0.005801 0.000 6.079E+10-689.3653 4792.2417 0.000 2.600 0.3313 162980. 23196. -0.005796 0.000 6.068E+10-678.3241 4913.5643 0.000 2.800 0.3174 216836. 21583. -0.005788 0.000 6.056E+10-665.9081 5034.8869 0.000 3.000 0.3035 266856. 20001. -0.005779 0.000 6.043E+10-652.1310 5156.2094 0.000 3.200 0.2897 313120. 18454. -0.005767 0.000 6.033E+10-637.0063 5277.5320 0.000 3.400 0.2759 355714. 16945. -0.005754 0.000 6.022E+10-620.5481 5398.8546 0.000 3.600 0.2621 394734. 15477. -0.005739 0.000 6.013E+10-602.7702 5520.1772 0.000

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existing phase1 87.lp6o 3.800 0.2483 430281. 14054. -0.005722 0.000 6.004E+10-583.6868 5641.4997 0.000 4.000 0.2346 462466. 12677. -0.005704 0.000 5.996E+10-563.3119 5762.8223 0.000 4.200 0.2209 491406. 11351. -0.005685 0.000 5.989E+10-541.6596 5884.1449 0.000 4.400 0.2073 517225. 10079. -0.005665 0.000 5.983E+10-518.7436 6005.4675 0.000 4.600 0.1937 540056. 8862.7864 -0.005644 0.000 5.977E+10-494.5776 6126.7900 0.000 4.800 0.1802 560037. 7706.2834 -0.005622 0.000 5.971E+10-469.1750 6248.1126 0.000 5.000 0.1668 577316. 6612.2148 -0.005596 0.000 4.891E+10-442.5489 6369.4352 0.000 5.200 0.1534 592044. 5583.4619 -0.005531 0.000 1.383E+10-414.7453 6490.7578 0.000 5.400 0.1402 604382. 4622.2479 -0.005341 0.000 5.223E+09-386.2664 6612.0803 0.000 5.600 0.1277 614488. 3728.7347 -0.005060 0.000 5.192E+09-358.3279 6733.4029 0.000 5.800 0.1159 622523. 2901.4522 -0.004774 0.000 5.180E+09-331.0743 6854.7255 0.000 6.000 0.1048 628644. 2138.5957 -0.004483 0.000 5.172E+09-304.6394 6976.0480 0.000 6.200 0.0944 633003. 1438.0464 -0.004191 0.000 5.166E+09-279.1517 7097.3706 0.000 6.400 0.0847 635747. 797.3828 -0.003896 0.000 5.162E+09-254.7345 7218.6932 0.000 6.600 0.0757 637017. 213.8945 -0.003600 0.000 5.160E+09-231.5057 7340.0158 0.000 6.800 0.0674 636947. -315.4060 -0.003304 0.000 5.160E+09-209.5781 7461.3383 0.000 7.000 0.0598 635662. -793.7705 -0.003008 0.000 5.162E+09-189.0590 7582.6609 0.000 7.200 0.0530 633281. -1224.7027 -0.002713 0.000 5.165E+09-170.0511 7703.9835 0.000 7.400 0.0468 629914. -1611.9463 -0.002419 0.000 5.170E+09-152.6518 7825.3061 0.000 7.600 0.0414 625660. -1959.4730 -0.002128 0.000 5.176E+09-136.9537 7946.6286 0.000 7.800 0.0366 620610. -2271.4709 -0.001839 0.000 5.183E+09-123.0446 8067.9512 0.000 8.000 0.0325 614845. -2552.3335 -0.001554 0.000 5.191E+09-111.0076 8189.2738 0.000 8.200 0.0291 608434. -2806.6486 -0.001271 0.000 5.201E+09-100.9216 8310.5964 0.000 8.400 0.0264 601434. -3039.1871 -0.000997 0.000 5.399E+09-92.8606 8431.9189 0.000 8.600 0.0244 593894. -3254.7943 -0.000796 0.000 1.054E+10-86.8120 8553.2415 0.000 8.800 0.0226 585850. -3457.0408 -0.000696 0.000 2.207E+10-81.7267 8674.5641 0.000 9.000 0.0210 577333. -3647.5427 -0.000650 0.000 4.939E+10-77.0249 8795.8867 0.000 9.200 0.0195 568373. -3826.8671 -0.000625 0.000 5.969E+10-72.4121 8917.2092 0.000 9.400 0.0180 558994. -3995.1834 -0.000602 0.000 5.972E+10-67.8514 9038.5318 0.000 9.600 0.0166 549225. -4152.6222 -0.000580 0.000 5.974E+10-63.3476 9159.8544 0.000 9.800 0.0152 539089. -4299.3255 -0.000558 0.000 5.977E+10-58.9052 9281.1770 0.000 10.000 0.0139 528615. -4462.2952 -0.000537 0.000 5.980E+10

Page 62

existing phase1 87.lp6o-76.9029 13261. 0.000 10.200 0.0127 517696. -4667.2435 -0.000516 0.000 5.983E+10-93.8873 17805. 0.000 10.400 0.0114 506237. -4883.0135 -0.000495 0.000 5.985E+10-85.9210 18021. 0.000 10.600 0.0103 494282. -5079.8459 -0.000475 0.000 5.988E+10-78.1060 18238. 0.000 10.800 0.009161 481876. -5258.1089 -0.000456 0.000 5.991E+10-70.4465 18455. 0.000 11.000 0.008091 469064. -5418.1796 -0.000437 0.000 5.994E+10-62.9458 18671. 0.000 11.200 0.007066 455890. -5560.4425 -0.000418 0.000 5.998E+10-55.6066 18888. 0.000 11.400 0.006084 442394. -5685.2874 -0.000400 0.000 6.001E+10-48.4308 19104. 0.000 11.600 0.005145 428620. -5793.1081 -0.000383 0.000 6.004E+10-41.4197 19321. 0.000 11.800 0.004247 414606. -5884.3004 -0.000366 0.000 6.008E+10-34.5738 19538. 0.000 12.000 0.003389 400393. -5959.2606 -0.000350 0.000 6.011E+10-27.8931 19754. 0.000 12.200 0.002569 386018. -6018.3842 -0.000334 0.000 6.015E+10-21.3766 19971. 0.000 12.400 0.001786 371520. -6062.0638 -0.000319 0.000 6.019E+10-15.0231 20187. 0.000 12.600 0.001039 356936. -6090.6882 -0.000304 0.000 6.022E+10-8.8305 20404. 0.000 12.800 0.000325 342300. -6104.6404 -0.000290 0.000 6.025E+10-2.7964 20621. 0.000 13.000 -0.000355 327647. -6104.2972 -0.000277 0.000 6.029E+103.0824 20837. 0.000 13.200 -0.001004 313012. -6090.0271 -0.000264 0.000 6.033E+108.8094 21054. 0.000 13.400 -0.001624 298428. -6062.1894 -0.000252 0.000 6.037E+1014.3887 21270. 0.000 13.600 -0.002214 283926. -6021.1330 -0.000241 0.000 6.040E+1019.8249 21487. 0.000 13.800 -0.002778 269538. -5967.1958 -0.000230 0.000 6.043E+1025.1228 21704. 0.000 14.000 -0.003316 255294. -5900.7029 -0.000219 0.000 6.046E+1030.2879 21920. 0.000 14.200 -0.003830 241225. -5821.9665 -0.000209 0.000 6.050E+1035.3257 22137. 0.000 14.400 -0.004321 227359. -5731.2848 -0.000200 0.000 6.054E+1040.2424 22353. 0.000 14.600 -0.004790 213725. -5628.9408 -0.000191 0.000 6.057E+1045.0442 22570. 0.000 14.800 -0.005239 200349. -5515.2023 -0.000183 0.000 6.059E+1049.7378 22787. 0.000 15.000 -0.005668 187260. -5394.6644 -0.000175 0.000 6.062E+1050.7105 21471. 0.000 15.200 -0.006080 174463. -5273.8540 -0.000168 0.000 6.065E+1049.9649 19722. 0.000 15.400 -0.006476 161954. -5149.4573 -0.000162 0.000 6.068E+1053.6990 19901. 0.000 15.600 -0.006856 149754. -5016.1821 -0.000155 0.000 6.072E+1057.3637 20081. 0.000 15.800 -0.007222 137884. -4874.1872 -0.000150 0.000 6.073E+1060.9654 20261. 0.000 16.000 -0.007574 126365. -4723.6161 -0.000144 0.000 6.075E+1064.5105 20441. 0.000 16.200 -0.007915 115217. -4564.5970 -0.000140 0.000 6.077E+1068.0055 20620. 0.000

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existing phase1 87.lp6o 16.400 -0.008245 104461. -4397.2422 -0.000135 0.000 6.079E+1071.4568 20800. 0.000 16.600 -0.008565 94117. -4221.6487 -0.000131 0.000 6.081E+1074.8711 20980. 0.000 16.800 -0.008876 84204. -4037.8979 -0.000128 0.000 6.084E+1078.2546 21159. 0.000 17.000 -0.009179 74741. -3846.0558 -0.000125 0.000 6.087E+1081.6139 21339. 0.000 17.200 -0.009475 65749. -3646.1731 -0.000122 0.000 6.087E+1084.9551 21519. 0.000 17.400 -0.009765 57245. -3438.2858 -0.000120 0.000 6.087E+1088.2844 21699. 0.000 17.600 -0.0100 49251. -3222.4153 -0.000118 0.000 6.087E+1091.6077 21878. 0.000 17.800 -0.0103 41784. -2998.5692 -0.000116 0.000 6.087E+1094.9307 22058. 0.000 18.000 -0.0106 34863. -2766.7415 -0.000114 0.000 6.087E+1098.2590 22238. 0.000 18.200 -0.0109 28509. -2526.9133 -0.000113 0.000 6.087E+10101.5978 22417. 0.000 18.400 -0.0111 22739. -2279.0535 -0.000112 0.000 6.087E+10104.9520 22597. 0.000 18.600 -0.0114 17575. -2023.1197 -0.000111 0.000 6.087E+10108.3262 22777. 0.000 18.800 -0.0117 13034. -1759.0589 -0.000111 0.000 6.087E+10111.7245 22957. 0.000 19.000 -0.0119 9136.3734 -1486.8086 -0.000110 0.000 6.087E+10115.1507 23136. 0.000 19.200 -0.0122 5902.3052 -1206.2978 -0.000110 0.000 6.087E+10118.6082 23316. 0.000 19.400 -0.0125 3351.4149 -917.4482 -0.000110 0.000 6.087E+10122.0998 23496. 0.000 19.600 -0.0127 1503.8162 -620.1753 -0.000110 0.000 6.087E+10125.6276 23675. 0.000 19.800 -0.0130 379.8312 -314.3900 -0.000109 0.000 6.087E+10129.1934 23855. 0.000 20.000 -0.0133 0.000 0.000 -0.000109 0.000 6.087E+10132.7982 12017. 0.000

* This analysis makes computations of pile response using nonlinear moment-curvaturerelationships. The above values of total stress are computed for combined axial and bending stress in elastic sections and do not equal actual stresses in concrete and steel in the range of nonlinear bending.

Output Summary for Load Case No. 12:

Pile-head deflection = 0.5000000 inchesComputed slope at pile head = -0.0002176 radiansMaximum bending moment = -905598. inch-lbsMaximum shear force = 45135. lbsDepth of maximum bending moment = 0.000000 inches below pile headDepth of maximum shear force = 0.000000 inches below pile headNumber of iterations = 56Number of zero deflection points = 1

-------------------------------------------------------------------------------- Computed Values of Pile Loading and Deflection for Lateral Loading for Load Case Number 13

Page 64

existing phase1 87.lp6o--------------------------------------------------------------------------------

Pile-head conditions are Displacement and Pile-head Rotation (Loading Type 5)Displacement of pile head = 0.750000 inchesRotation of pile head = 0.000E+00 radiansAxial load on pile head = 10000.000 lbs

Depth Deflect. Bending Shear Slope Total Bending Soil Res. Soil Spr. Distrib. X y Moment Force S Stress Stiffness p Es*h Lat. Load feet inches in-lbs lbs radians psi* lb-in^2 lb/in lb/inch lb/inch ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- 0.00 0.7500 -905599. 52468. 0.000 0.000 3.133E+08-808.8662 1294.1858 0.000 0.200 0.7417 -781972. 50486. -0.006463 0.000 3.133E+08-825.9348 2672.6539 0.000 0.400 0.7190 -662959. 48496. -0.009614 0.000 5.105E+09-831.8651 2776.8293 0.000 0.600 0.6955 -548729. 46488. -0.009781 0.000 5.974E+10-841.3052 2903.0133 0.000 0.800 0.6720 -439345. 44452. -0.009800 0.000 6.002E+10-855.3051 3054.5253 0.000 1.000 0.6485 -334887. 42386. -0.009816 0.000 6.027E+10-866.7708 3207.8479 0.000 1.200 0.6249 -235421. 40295. -0.009827 0.000 6.052E+10-875.5407 3362.5414 0.000 1.400 0.6013 -140998. 38187. -0.009835 0.000 6.073E+10-881.4527 3518.0886 0.000 1.600 0.5777 -51653. 36068. -0.009838 0.000 6.087E+10-884.3442 3673.8792 0.000 1.800 0.5541 32599. 33946. -0.009839 0.000 6.087E+10-884.0519 3829.1902 0.000 2.000 0.5305 111759. 31828. -0.009836 0.000 6.077E+10-880.4124 3983.1618 0.000 2.200 0.5069 185848. 29724. -0.009830 0.000 6.062E+10-873.2615 4134.7661 0.000 2.400 0.4833 254906. 27641. -0.009821 0.000 6.046E+10-862.4348 4282.7670 0.000 2.600 0.4597 318997. 25576. -0.009810 0.000 6.031E+10-858.9249 4483.9143 0.000 2.800 0.4362 378140. 23508. -0.009796 0.000 6.017E+10-864.1206 4754.3600 0.000 3.000 0.4127 432305. 21430. -0.009780 0.000 6.004E+10-867.2816 5043.3690 0.000 3.200 0.3893 481474. 19362. -0.009762 0.000 5.991E+10-855.9812 5277.5320 0.000 3.400 0.3659 525712. 17347. -0.009741 0.000 5.981E+10-823.0093 5398.8546 0.000 3.600 0.3425 565209. 15415. -0.009720 0.000 5.970E+10-787.7876 5520.1772 0.000 3.800 0.3192 600168. 13569. -0.009570 0.000 5.231E+09-750.3330 5641.4997 0.000 4.000 0.2966 630799. 11814. -0.009286 0.000 5.169E+09-712.1096 5762.8223 0.000 4.200 0.2746 657321. 10151. -0.008986 0.000 5.123E+09-673.3209 5884.1449 0.000 4.400 0.2534 679957. 8582.3437 -0.008670 0.000 5.048E+09-634.1637 6005.4675 0.000 4.600 0.2330 698932. 7107.5342 -0.008338 0.000 4.901E+09-594.8442 6126.7900 0.000

Page 65

existing phase1 87.lp6o 4.800 0.2134 714473. 5727.0026 -0.007986 0.000 4.744E+09-555.5988 6248.1126 0.000 5.000 0.1947 726805. 4440.2755 -0.007617 0.000 4.631E+09-516.6739 6369.4352 0.000 5.200 0.1769 736152. 3246.3069 -0.007234 0.000 4.550E+09-478.2999 6490.7578 0.000 5.400 0.1600 742734. 2143.5179 -0.006842 0.000 4.496E+09-440.6909 6612.0803 0.000 5.600 0.1440 746769. 1129.8368 -0.006443 0.000 4.464E+09-404.0433 6733.4029 0.000 5.800 0.1290 748467. 202.7418 -0.006040 0.000 4.451E+09-368.5359 6854.7255 0.000 6.000 0.1150 748032. -640.6966 -0.005637 0.000 4.454E+09-334.3295 6976.0480 0.000 6.200 0.1020 745662. -1403.7727 -0.005235 0.000 4.473E+09-301.5672 7097.3706 0.000 6.400 0.0899 741545. -2090.1027 -0.004838 0.000 4.506E+09-270.3744 7218.6932 0.000 6.600 0.0788 735862. -2703.5829 -0.004446 0.000 4.553E+09-240.8591 7340.0158 0.000 6.800 0.0685 728782. -3248.3486 -0.004063 0.000 4.614E+09-213.1122 7461.3383 0.000 7.000 0.0593 720465. -3728.7331 -0.003689 0.000 4.688E+09-187.2082 7582.6609 0.000 7.200 0.0508 711061. -4149.2296 -0.003326 0.000 4.778E+09-163.2056 7703.9835 0.000 7.400 0.0433 700708. -4514.4539 -0.002975 0.000 4.882E+09-141.1479 7825.3061 0.000 7.600 0.0366 689534. -4829.1078 -0.002637 0.000 4.996E+09-121.0638 7946.6286 0.000 7.800 0.0306 677655. -5097.9505 -0.002311 0.000 5.056E+09-102.9718 8067.9512 0.000 8.000 0.0255 665175. -5325.8137 -0.001993 0.000 5.098E+09-86.9142 8189.2738 0.000 8.200 0.0211 652187. -5517.6357 -0.001684 0.000 5.136E+09-72.9374 8310.5964 0.000 8.400 0.0174 638771. -5678.4623 -0.001383 0.000 5.158E+09-61.0848 8431.9189 0.000 8.600 0.0144 624996. -5813.4471 -0.001090 0.000 5.177E+09-51.4026 8553.2415 0.000 8.800 0.0122 610919. -5927.8514 -0.000804 0.000 5.197E+09-43.9343 8674.5641 0.000 9.000 0.0106 596581. -6027.0345 -0.000584 0.000 9.056E+09-38.7183 8795.8867 0.000 9.200 0.009353 582017. -6115.1982 -0.000493 0.000 5.966E+10-34.7514 8917.2092 0.000 9.400 0.008198 567252. -6193.9483 -0.000470 0.000 5.970E+10-30.8736 9038.5318 0.000 9.600 0.007097 552309. -6263.5022 -0.000447 0.000 5.973E+10-27.0880 9159.8544 0.000 9.800 0.006050 537209. -6324.0842 -0.000426 0.000 5.977E+10-23.3970 9281.1770 0.000 10.000 0.005055 521974. -6385.6751 -0.000404 0.000 5.982E+10-27.9288 13261. 0.000 10.200 0.004110 506577. -6455.7744 -0.000384 0.000 5.985E+10-30.4874 17805. 0.000 10.400 0.003213 491004. -6521.3116 -0.000364 0.000 5.989E+10-24.1270 18021. 0.000 10.600 0.002364 475292. -6571.8204 -0.000344 0.000 5.993E+10-17.9637 18238. 0.000 10.800 0.001560 459476. -6607.7748 -0.000326 0.000 5.997E+10-11.9984 18455. 0.000 11.000 0.000801 443590. -6629.6505 -0.000308 0.000 6.001E+10

Page 66

existing phase1 87.lp6o-6.2313 18671. 0.000 11.200 8.416E-05 427668. -6637.9229 -0.000290 0.000 6.005E+10-0.6623 18888. 0.000 11.400 -0.000592 411742. -6633.0663 -0.000273 0.000 6.008E+104.7095 19104. 0.000 11.600 -0.001228 395843. -6615.5523 -0.000257 0.000 6.012E+109.8855 19321. 0.000 11.800 -0.001826 380000. -6585.8485 -0.000242 0.000 6.017E+1014.8677 19538. 0.000 12.000 -0.002388 364242. -6544.4171 -0.000227 0.000 6.020E+1019.6585 19754. 0.000 12.200 -0.002916 348598. -6491.7142 -0.000213 0.000 6.024E+1024.2607 19971. 0.000 12.400 -0.003409 333092. -6428.1881 -0.000199 0.000 6.028E+1028.6777 20187. 0.000 12.600 -0.003871 317752. -6354.2789 -0.000186 0.000 6.032E+1032.9132 20404. 0.000 12.800 -0.004303 302601. -6270.4173 -0.000174 0.000 6.036E+1036.9715 20621. 0.000 13.000 -0.004706 287662. -6177.0233 -0.000162 0.000 6.039E+1040.8569 20837. 0.000 13.200 -0.005081 272959. -6074.5058 -0.000151 0.000 6.042E+1044.5743 21054. 0.000 13.400 -0.005431 258512. -5963.2619 -0.000140 0.000 6.045E+1048.1289 21270. 0.000 13.600 -0.005755 244342. -5843.6761 -0.000130 0.000 6.049E+1051.5260 21487. 0.000 13.800 -0.006057 230469. -5716.1193 -0.000121 0.000 6.053E+1054.7713 21704. 0.000 14.000 -0.006336 216910. -5580.9488 -0.000112 0.000 6.056E+1057.8707 21920. 0.000 14.200 -0.006595 203685. -5438.5075 -0.000104 0.000 6.058E+1060.8303 22137. 0.000 14.400 -0.006835 190811. -5289.1237 -9.602E-05 0.000 6.061E+1063.6563 22353. 0.000 14.600 -0.007056 178302. -5133.1103 -8.871E-05 0.000 6.064E+1066.3549 22570. 0.000 14.800 -0.007260 166176. -4970.7652 -8.189E-05 0.000 6.067E+1068.9327 22787. 0.000 15.000 -0.007449 154446. -4808.0781 -7.556E-05 0.000 6.071E+1066.6399 21471. 0.000 15.200 -0.007623 143101. -4652.9407 -6.967E-05 0.000 6.073E+1062.6412 19722. 0.000 15.400 -0.007783 132116. -4500.3204 -6.424E-05 0.000 6.074E+1064.5424 19901. 0.000 15.600 -0.007931 121502. -4343.2344 -5.923E-05 0.000 6.076E+1066.3627 20081. 0.000 15.800 -0.008068 111271. -4181.8696 -5.463E-05 0.000 6.077E+1068.1079 20261. 0.000 16.000 -0.008194 101432. -4016.3995 -5.043E-05 0.000 6.079E+1069.7838 20441. 0.000 16.200 -0.008310 91995. -3846.9839 -4.661E-05 0.000 6.082E+1071.3959 20620. 0.000 16.400 -0.008417 82969. -3673.7689 -4.316E-05 0.000 6.084E+1072.9499 20800. 0.000 16.600 -0.008517 74363. -3496.8873 -4.006E-05 0.000 6.087E+1074.4514 20980. 0.000 16.800 -0.008610 66185. -3316.4588 -3.729E-05 0.000 6.087E+1075.9057 21159. 0.000 17.000 -0.008696 58445. -3132.5901 -3.483E-05 0.000 6.087E+1077.3182 21339. 0.000 17.200 -0.008777 51151. -2945.3752 -3.267E-05 0.000 6.087E+1078.6941 21519. 0.000

Page 67

existing phase1 87.lp6o 17.400 -0.008853 44309. -2754.8963 -3.079E-05 0.000 6.087E+1080.0383 21699. 0.000 17.600 -0.008925 37929. -2561.2234 -2.917E-05 0.000 6.087E+1081.3557 21878. 0.000 17.800 -0.008993 32017. -2364.4156 -2.779E-05 0.000 6.087E+1082.6508 22058. 0.000 18.000 -0.009058 26581. -2164.5208 -2.663E-05 0.000 6.087E+1083.9281 22238. 0.000 18.200 -0.009121 21628. -1961.5770 -2.568E-05 0.000 6.087E+1085.1917 22417. 0.000 18.400 -0.009181 17166. -1755.6126 -2.492E-05 0.000 6.087E+1086.4453 22597. 0.000 18.600 -0.009240 13203. -1546.6470 -2.432E-05 0.000 6.087E+1087.6927 22777. 0.000 18.800 -0.009298 9743.7577 -1334.6916 -2.387E-05 0.000 6.087E+1088.9369 22957. 0.000 19.000 -0.009355 6797.2042 -1119.7504 -2.354E-05 0.000 6.087E+1090.1808 23136. 0.000 19.200 -0.009411 4370.0858 -901.8209 -2.332E-05 0.000 6.087E+1091.4271 23316. 0.000 19.400 -0.009467 2469.5832 -680.8953 -2.319E-05 0.000 6.087E+1092.6776 23496. 0.000 19.600 -0.009522 1102.9014 -456.9610 -2.312E-05 0.000 6.087E+1093.9343 23675. 0.000 19.800 -0.009578 277.2800 -230.0020 -2.309E-05 0.000 6.087E+1095.1982 23855. 0.000 20.000 -0.009633 0.000 0.000 -2.308E-05 0.000 6.087E+1096.4701 12017. 0.000

* This analysis makes computations of pile response using nonlinear moment-curvaturerelationships. The above values of total stress are computed for combined axial and bending stress in elastic sections and do not equal actual stresses in concrete and steel in the range of nonlinear bending.

Output Summary for Load Case No. 13:

Pile-head deflection = 0.7500000 inchesComputed slope at pile head = -0.0004735 radiansMaximum bending moment = -905599. inch-lbsMaximum shear force = 52468. lbsDepth of maximum bending moment = 0.000000 inches below pile headDepth of maximum shear force = 0.000000 inches below pile headNumber of iterations = 94Number of zero deflection points = 1

-------------------------------------------------------------------------------- Computed Values of Pile Loading and Deflection for Lateral Loading for Load Case Number 14--------------------------------------------------------------------------------

Pile-head conditions are Displacement and Pile-head Rotation (Loading Type 5)Displacement of pile head = 1.000000 inchesRotation of pile head = 0.000E+00 radiansAxial load on pile head = 10000.000 lbs

Depth Deflect. Bending Shear Slope Total Bending Soil Res. Soil Spr. Distrib. X y Moment Force S Stress Stiffness p

Page 68

existing phase1 87.lp6o Es*h Lat. Load feet inches in-lbs lbs radians psi* lb-in^2 lb/in lb/inch lb/inch ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- 0.00 1.0000 -905573. 58133. 0.000 0.000 2.120E+08-893.1068 1071.7282 0.000 0.200 0.9877 -768578. 55927. -0.009477 0.000 2.120E+08-919.2008 2233.5623 0.000 0.400 0.9545 -636670. 53691. -0.0140 0.000 5.161E+09-943.5102 2372.3445 0.000 0.600 0.9206 -510189. 51390. -0.0141 0.000 5.984E+10-974.2336 2539.7921 0.000 0.800 0.8867 -389318. 49017. -0.0142 0.000 6.014E+10 -1003.4183 2716.0282 0.000 1.000 0.8527 -274228. 46594. -0.0142 0.000 6.042E+10 -1016.1155 2860.0167 0.000 1.200 0.8187 -164990. 44144. -0.0142 0.000 6.068E+10 -1025.5245 3006.4163 0.000 1.400 0.7846 -61658. 41675. -0.0142 0.000 6.087E+10 -1031.4447 3154.8989 0.000 1.600 0.7506 35732. 39197. -0.0142 0.000 6.087E+10 -1033.6743 3305.0689 0.000 1.800 0.7166 127168. 36718. -0.0142 0.000 6.075E+10 -1032.0106 3456.4465 0.000 2.000 0.6826 212660. 34248. -0.0142 0.000 6.057E+10 -1026.2498 3608.4481 0.000 2.200 0.6486 292240. 31797. -0.0142 0.000 6.038E+10 -1016.1871 3760.3584 0.000 2.400 0.6146 365967. 29376. -0.0141 0.000 6.020E+10 -1001.6171 3911.2957 0.000 2.600 0.5807 433924. 26982. -0.0141 0.000 6.003E+10-993.3093 4105.5307 0.000 2.800 0.5468 496159. 24599. -0.0141 0.000 5.987E+10-992.6357 4357.0565 0.000 3.000 0.5129 552677. 22221. -0.0141 0.000 5.973E+10-989.0087 4627.5736 0.000 3.200 0.4791 603497. 19855. -0.0139 0.000 5.212E+09-982.3043 4920.3478 0.000 3.400 0.4460 648652. 17509. -0.0137 0.000 5.144E+09-973.2037 5236.7949 0.000 3.600 0.4136 688194. 15199. -0.0133 0.000 5.007E+09-951.3503 5520.1772 0.000 3.800 0.3820 722249. 12980. -0.0130 0.000 4.673E+09-897.9655 5641.4997 0.000 4.000 0.3513 751122. 10890. -0.0126 0.000 4.418E+09-843.5231 5762.8223 0.000 4.200 0.3216 775127. 8932.1122 -0.0122 0.000 3.980E+09-788.3761 5884.1449 0.000 4.400 0.2929 794580. 7106.4249 -0.0117 0.000 3.644E+09-733.0299 6005.4675 0.000 4.600 0.2656 809798. 5413.1922 -0.0111 0.000 3.423E+09-677.9973 6126.7900 0.000 4.800 0.2396 821097. 3851.0998 -0.0105 0.000 3.275E+09-623.7464 6248.1126 0.000 5.000 0.2150 828788. 2417.7645 -0.009913 0.000 3.137E+09-570.6997 6369.4352 0.000 5.200 0.1920 833178. 1109.7809 -0.009262 0.000 2.992E+09-519.2867 6490.7578 0.000 5.400 0.1706 834560. -77.3199 -0.008587 0.000 2.945E+09-469.9640 6612.0803 0.000 5.600 0.1508 833219. -1148.9419 -0.007913 0.000 2.991E+09-423.0543 6733.4029 0.000

Page 69

existing phase1 87.lp6o 5.800 0.1326 829425. -2111.0791 -0.007260 0.000 3.119E+09-378.7268 6854.7255 0.000 6.000 0.1159 823434. -2969.9664 -0.006636 0.000 3.242E+09-337.0126 6976.0480 0.000 6.200 0.1007 815488. -3731.9109 -0.006039 0.000 3.348E+09-297.9412 7097.3706 0.000 6.400 0.0870 805811. -4403.3046 -0.005468 0.000 3.477E+09-261.5536 7218.6932 0.000 6.600 0.0745 794614. -4990.5937 -0.004928 0.000 3.643E+09-227.8540 7340.0158 0.000 6.800 0.0633 782093. -5500.1804 -0.004423 0.000 3.851E+09-196.8015 7461.3383 0.000 7.000 0.0533 768426. -5938.3168 -0.003955 0.000 4.110E+09-168.3122 7582.6609 0.000 7.200 0.0443 753778. -6311.0099 -0.003524 0.000 4.375E+09-142.2654 7703.9835 0.000 7.400 0.0364 738302. -6623.9871 -0.003122 0.000 4.533E+09-118.5489 7825.3061 0.000 7.600 0.0293 722133. -6882.8068 -0.002741 0.000 4.673E+09-97.1341 7946.6286 0.000 7.800 0.0232 705396. -7092.9691 -0.002380 0.000 4.834E+09-78.0012 8067.9512 0.000 8.000 0.0179 688201. -7259.9099 -0.002040 0.000 5.006E+09-61.1161 8189.2738 0.000 8.200 0.0134 670646. -7388.9746 -0.001717 0.000 5.080E+09-46.4378 8310.5964 0.000 8.400 0.009671 652816. -7485.4715 -0.001406 0.000 5.134E+09-33.9762 8431.9189 0.000 8.600 0.006663 634784. -7554.7388 -0.001106 0.000 5.163E+09-23.7466 8553.2415 0.000 8.800 0.004364 616607. -7602.1616 -0.000815 0.000 5.189E+09-15.7724 8674.5641 0.000 9.000 0.002749 598332. -7633.1777 -0.000536 0.000 5.235E+09-10.0744 8795.8867 0.000 9.200 0.001792 579993. -7653.2579 -0.000387 0.000 5.967E+10-6.6591 8917.2092 0.000 9.400 0.000892 561615. -7665.2783 -0.000364 0.000 5.971E+10-3.3579 9038.5318 0.000 9.600 4.519E-05 543217. -7669.5148 -0.000342 0.000 5.976E+10-0.1725 9159.8544 0.000 9.800 -0.000749 524818. -7666.2465 -0.000320 0.000 5.981E+102.8961 9281.1770 0.000 10.000 -0.001492 506435. -7652.8759 -0.000300 0.000 5.985E+108.2460 13261. 0.000 10.200 -0.002187 488099. -7623.5091 -0.000280 0.000 5.989E+1016.2263 17805. 0.000 10.400 -0.002835 469855. -7578.4916 -0.000261 0.000 5.994E+1021.2884 18021. 0.000 10.600 -0.003438 451734. -7521.5965 -0.000242 0.000 5.999E+1026.1243 18238. 0.000 10.800 -0.003997 433763. -7453.3648 -0.000224 0.000 6.003E+1030.7355 18455. 0.000 11.000 -0.004515 415969. -7374.3336 -0.000207 0.000 6.007E+1035.1239 18671. 0.000 11.200 -0.004993 398376. -7285.0348 -0.000191 0.000 6.012E+1039.2918 18888. 0.000 11.400 -0.005432 381010. -7185.9941 -0.000176 0.000 6.017E+1043.2421 19104. 0.000 11.600 -0.005835 363892. -7077.7297 -0.000161 0.000 6.021E+1046.9782 19321. 0.000 11.800 -0.006204 347045. -6960.7515 -0.000147 0.000 6.024E+1050.5036 19538. 0.000 12.000 -0.006539 330488. -6835.5602 -0.000133 0.000 6.028E+10

Page 70

existing phase1 87.lp6o53.8224 19754. 0.000 12.200 -0.006843 314240. -6702.6465 -0.000120 0.000 6.033E+1056.9390 19971. 0.000 12.400 -0.007116 298321. -6562.4903 -0.000108 0.000 6.037E+1059.8579 20187. 0.000 12.600 -0.007361 282745. -6415.5596 -9.652E-05 0.000 6.040E+1062.5843 20404. 0.000 12.800 -0.007580 267531. -6262.3107 -8.560E-05 0.000 6.043E+1065.1232 20621. 0.000 13.000 -0.007772 252690. -6103.1866 -7.527E-05 0.000 6.047E+1067.4801 20837. 0.000 13.200 -0.007941 238239. -5938.6176 -6.553E-05 0.000 6.051E+1069.6607 21054. 0.000 13.400 -0.008087 224188. -5769.0200 -5.636E-05 0.000 6.055E+1071.6707 21270. 0.000 13.600 -0.008211 210550. -5594.7959 -4.775E-05 0.000 6.057E+1073.5161 21487. 0.000 13.800 -0.008316 197336. -5416.3331 -3.967E-05 0.000 6.060E+1075.2029 21704. 0.000 14.000 -0.008402 184554. -5234.0049 -3.211E-05 0.000 6.062E+1076.7373 21920. 0.000 14.200 -0.008470 172214. -5048.1697 -2.505E-05 0.000 6.065E+1078.1254 22137. 0.000 14.400 -0.008522 160324. -4859.1710 -1.847E-05 0.000 6.069E+1079.3735 22353. 0.000 14.600 -0.008559 148891. -4667.3372 -1.236E-05 0.000 6.072E+1080.4879 22570. 0.000 14.800 -0.008581 137921. -4472.9819 -6.689E-06 0.000 6.073E+1081.4749 22787. 0.000 15.000 -0.008591 127421. -4282.9858 -1.447E-06 0.000 6.075E+1076.8552 21471. 0.000 15.200 -0.008588 117363. -4106.0715 3.388E-06 0.000 6.076E+1070.5734 19722. 0.000 15.400 -0.008575 107711. -3936.0600 7.833E-06 0.000 6.078E+1071.1029 19901. 0.000 15.600 -0.008551 98469. -3764.8827 1.190E-05 0.000 6.080E+1071.5449 20081. 0.000 15.800 -0.008517 89639. -3592.7432 1.561E-05 0.000 6.082E+1071.9046 20261. 0.000 16.000 -0.008476 81223. -3419.8332 1.899E-05 0.000 6.085E+1072.1871 20441. 0.000 16.200 -0.008426 73223. -3246.3320 2.203E-05 0.000 6.087E+1072.3972 20620. 0.000 16.400 -0.008370 65640. -3072.4074 2.477E-05 0.000 6.087E+1072.5399 20800. 0.000 16.600 -0.008307 58475. -2898.2157 2.721E-05 0.000 6.087E+1072.6199 20980. 0.000 16.800 -0.008239 51727. -2723.9018 2.939E-05 0.000 6.087E+1072.6417 21159. 0.000 17.000 -0.008166 45398. -2549.6001 3.130E-05 0.000 6.087E+1072.6098 21339. 0.000 17.200 -0.008089 39488. -2375.4343 3.298E-05 0.000 6.087E+1072.5284 21519. 0.000 17.400 -0.008008 33995. -2201.5181 3.442E-05 0.000 6.087E+1072.4017 21699. 0.000 17.600 -0.007924 28919. -2027.9559 3.566E-05 0.000 6.087E+1072.2335 21878. 0.000 17.800 -0.007837 24259. -1854.8426 3.671E-05 0.000 6.087E+1072.0276 22058. 0.000 18.000 -0.007748 20014. -1682.2646 3.759E-05 0.000 6.087E+1071.7874 22238. 0.000 18.200 -0.007656 16182. -1510.3005 3.830E-05 0.000 6.087E+1071.5161 22417. 0.000

Page 71

existing phase1 87.lp6o 18.400 -0.007564 12762. -1339.0212 3.887E-05 0.000 6.087E+1071.2167 22597. 0.000 18.600 -0.007470 9753.0036 -1168.4907 3.931E-05 0.000 6.087E+1070.8920 22777. 0.000 18.800 -0.007375 7151.8467 -998.7670 3.965E-05 0.000 6.087E+1070.5444 22957. 0.000 19.000 -0.007280 4957.0190 -829.9023 3.989E-05 0.000 6.087E+1070.1761 23136. 0.000 19.200 -0.007184 3166.4012 -661.9442 4.005E-05 0.000 6.087E+1069.7890 23316. 0.000 19.400 -0.007087 1777.7647 -494.9360 4.014E-05 0.000 6.087E+1069.3845 23496. 0.000 19.600 -0.006991 788.7813 -328.9179 4.019E-05 0.000 6.087E+1068.9640 23675. 0.000 19.800 -0.006894 197.0294 -163.9273 4.021E-05 0.000 6.087E+1068.5282 23855. 0.000 20.000 -0.006798 0.000 0.000 4.022E-05 0.000 6.087E+1068.0779 12017. 0.000

* This analysis makes computations of pile response using nonlinear moment-curvaturerelationships. The above values of total stress are computed for combined axial and bending stress in elastic sections and do not equal actual stresses in concrete and steel in the range of nonlinear bending.

Output Summary for Load Case No. 14:

Pile-head deflection = 1.0000000 inchesComputed slope at pile head = -0.0007755 radiansMaximum bending moment = -905573. inch-lbsMaximum shear force = 58133. lbsDepth of maximum bending moment = 0.000000 inches below pile headDepth of maximum shear force = 0.000000 inches below pile headNumber of iterations = 93Number of zero deflection points = 1

-------------------------------------------------------------------------------- Summary of Pile Response(s)--------------------------------------------------------------------------------

Definitions of Pile-head Loading Conditions:

Load Type 1: Load 1 = Shear, lbs, and Load 2 = Moment, in-lbsLoad Type 2: Load 1 = Shear, lbs, and Load 2 = Slope, radiansLoad Type 3: Load 1 = Shear, lbs, and Load 2 = Rotational Stiffness, in-lbs/radianLoad Type 4: Load 1 = Top Deflection, inches, and Load 2 = Moment, in-lbsLoad Type 5: Load 1 = Top Deflection, inches, and Load 2 = Slope, radians

Pile-head Pile-head Maximum MaximumLoad Load Condition 1 Condition 2 Axial Pile-head Moment Shear Pile-headCase Type V(lbs) or in-lb, rad., Loading Deflection in Pile in Pile Rotation No. No. y(inches) or in-lb/rad. lbs inches in-lbs lbs radians

Page 72

existing phase1 87.lp6o---- ---- -------------- -------------- ------------- -------------------------- ------------- ------------- 1 4 y = 0.0100 M = 0.000 10000.00000000 0.0100000040849. 1064.8147 -0.00009980 2 4 y = 0.1000 M = 0.000 10000.00000000 0.10000000406514. 10619. -0.00100016 3 4 y = 0.2000 M = 0.000 10000.00000000 0.20000000598440. 17845. -0.00227104 4 4 y = 0.3000 M = 0.000 10000.00000000 0.30000000607907. 21547. -0.00401958 5 4 y = 0.5000 M = 0.000 10000.00000000 0.50000000686714. 28963. -0.00792636 6 4 y = 0.7500 M = 0.000 10000.00000000 0.75000000808676. 35608. -0.01296578 7 4 y = 1.0000 M = 0.000 10000.00000000 1.00000000870980. 39781. -0.01846090 8 4 y = 0.0100 M = 0.000 10000.00000000 0.0100000040849. 1064.8147 -0.00009980 9 5 y = 0.1000 S = 0.000 10000.00000000 0.10000000-680688. 17543. -0.00000992 10 5 y = 0.2000 S = 0.000 10000.00000000 0.20000000-831680. 29166. -0.00002689 11 5 y = 0.3000 S = 0.000 10000.00000000 0.30000000-893560. 35572. -0.00007000 12 5 y = 0.5000 S = 0.000 10000.00000000 0.50000000-905598. 45135. -0.00021761 13 5 y = 0.7500 S = 0.000 10000.00000000 0.75000000-905599. 52468. -0.00047347 14 5 y = 1.0000 S = 0.000 10000.00000000 1.00000000-905573. 58133. -0.00077552

The analysis ended normally.

Page 73

Lateral Deflection (inches)D

epth

(ft)

-0.1 0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 10

24

68

1012

1416

1820

2224

2628

Case 1Case 2Case 3Case 4Case 5Case 6Case 7Case 8Case 9Case 10Case 11Case 12Case 13Case 14

Bending Moment (in-kips)D

epth

(ft)

-5000 -4000 -3000 -2000 -1000 0 1000 2000 30000

24

68

1012

1416

1820

2224

2628

Case 1Case 2Case 3Case 4Case 5Case 6Case 7Case 8Case 9Case 10Case 11Case 12Case 13Case 14

Shear Force (kips)D

epth

(ft)

-20 0 20 40 60 80 100 1200

24

68

1012

1416

1820

2224

2628

Case 1Case 2Case 3Case 4Case 5Case 6Case 7Case 8Case 9Case 10Case 11Case 12Case 13Case 14

existing phase2 87.lp6o================================================================================

LPile Plus for Windows, Version 2012-06.037

Analysis of Individual Piles and Drilled Shafts Subjected to Lateral Loading Using the p-y Method

© 1985-2012 by Ensoft, Inc. All Rights Reserved

================================================================================

This copy of LPile is licensed to:

Dennis NguyenAECOM

Serial Number of Security Device: 160777832Company Name Stored in Security Device: AECOM (URS)

-------------------------------------------------------------------------------- Files Used for Analysis--------------------------------------------------------------------------------

Path to file locations:\\losangeles.na.aecomnet.com\LosAngeles\Projects\ENV\_legacy\GT\Da Wu\LA County Geotech On-call\MLK\Report\2019 BHC - Lab\Appendix F and G\Name of input data file: existing phase2 87.lp6dName of output report file: existing phase2 87.lp6oName of plot output file: existing phase2 87.lp6pName of runtime messeage file: existing phase2 87.lp6r

-------------------------------------------------------------------------------- Date and Time of Analysis--------------------------------------------------------------------------------

Date: March 12, 2019 Time: 13:36:13

-------------------------------------------------------------------------------- Problem Title--------------------------------------------------------------------------------

Project Name: MLK DHS Lab & Red Bag Storage

Job Number: 60595699

Client: LACDPW

Engineer: Dennis Nguyen

Description:

Page 1

existing phase2 87.lp6o

-------------------------------------------------------------------------------- Program Options--------------------------------------------------------------------------------

Engineering units are US Customary Units: pounds, inches, feet

Basic Program Options:

This analysis computes pile response to lateral loading and will compute nonlinear moment-curvature and nominal moment capacity for section types with nonlinear properties.

Computation Options:- Analysis does not use p-y multipliers (individual pile or shaft only)- Analysis assumes no shear resistance at pile tip- Analysis for fixed-length pile or shaft only- No computation of foundation stiffness matrix values- Report pile response for full length of pile- Analysis assumes no loading by soil movements acting on pile- No p-y curves to be computed and reported for user-specified depths

Solution Control Parameters:- Number of pile increments = 100- Maximum number of iterations allowed = 100- Deflection tolerance for convergence = 1.0000E-05 in- Maximum allowable deflection = 100.0000 in

Pile Response Output Options:- Values of pile-head deflection, bending moment, shear force, and soil reaction are printed for full length of pile.- Printing Increment (nodal spacing of output points) = 1

-------------------------------------------------------------------------------- Pile Structural Properties and Geometry--------------------------------------------------------------------------------

Total number of pile sections = 1

Total length of pile = 29.00 ft

Depth of ground surface below top of pile = -5.50 ft

Pile diameter values used for p-y curve computations are defined using 2 points.

p-y curves are computed using pile diameter values interpolated with depth over the length of the pile.

Point Depth Pile X Diameter ft in----- --------- ----------- 1 0.00000 24.0000000 2 29.000000 24.0000000

Input Structural Properties:----------------------------

Page 2

existing phase2 87.lp6oPile Section No. 1:

Section Type = Drilled Shaft (Bored Pile) Section Length = 29.00000000 ft Section Diameter = 24.00000000 in

-------------------------------------------------------------------------------- Ground Slope and Pile Batter Angles--------------------------------------------------------------------------------

Ground Slope Angle = 0.000 degrees = 0.000 radians

Pile Batter Angle = 0.000 degrees = 0.000 radians

-------------------------------------------------------------------------------- Soil and Rock Layering Information--------------------------------------------------------------------------------

The soil profile is modelled using 6 layers

Layer 1 is sand, p-y criteria by Reese et al., 1974

Distance from top of pile to top of layer = -5.50000 ft Distance from top of pile to bottom of layer = 10.00000 ft Effective unit weight at top of layer = 125.00000 pcf Effective unit weight at bottom of layer = 125.00000 pcf Friction angle at top of layer = 28.00000 deg. Friction angle at bottom of layer = 28.00000 deg. Subgrade k at top of layer = 0.0000 pci Subgrade k at bottom of layer = 0.0000 pci

NOTE: Internal default values for subgrade k will be computed for the above soil layer.

Layer 2 is sand, p-y criteria by Reese et al., 1974

Distance from top of pile to top of layer = 10.00000 ft Distance from top of pile to bottom of layer = 15.00000 ft Effective unit weight at top of layer = 67.60000 pcf Effective unit weight at bottom of layer = 67.60000 pcf Friction angle at top of layer = 31.00000 deg. Friction angle at bottom of layer = 31.00000 deg. Subgrade k at top of layer = 0.0000 pci Subgrade k at bottom of layer = 0.0000 pci

NOTE: Internal default values for subgrade k will be computed for the above soil layer.

Layer 3 is sand, p-y criteria by Reese et al., 1974

Distance from top of pile to top of layer = 15.00000 ft Distance from top of pile to bottom of layer = 25.00000 ft Effective unit weight at top of layer = 62.60000 pcf Effective unit weight at bottom of layer = 62.60000 pcf Friction angle at top of layer = 30.00000 deg.

Page 3

existing phase2 87.lp6o Friction angle at bottom of layer = 30.00000 deg. Subgrade k at top of layer = 0.0000 pci Subgrade k at bottom of layer = 0.0000 pci

NOTE: Internal default values for subgrade k will be computed for the above soil layer.

Layer 4 is sand, p-y criteria by Reese et al., 1974

Distance from top of pile to top of layer = 25.00000 ft Distance from top of pile to bottom of layer = 40.00000 ft Effective unit weight at top of layer = 47.60000 pcf Effective unit weight at bottom of layer = 47.60000 pcf Friction angle at top of layer = 31.00000 deg. Friction angle at bottom of layer = 31.00000 deg. Subgrade k at top of layer = 0.0000 pci Subgrade k at bottom of layer = 0.0000 pci

NOTE: Internal default values for subgrade k will be computed for the above soil layer.

Layer 5 is soft clay, p-y criteria by Matlock, 1970

Distance from top of pile to top of layer = 40.00000 ft Distance from top of pile to bottom of layer = 49.00000 ft Effective unit weight at top of layer = 57.60000 pcf Effective unit weight at bottom of layer = 57.60000 pcf Undrained cohesion at top of layer = 1500.00000 psf Undrained cohesion at bottom of layer = 1500.00000 psf Epsilon-50 at top of layer = 0.0000 Epsilon-50 at bottom of layer = 0.0000

NOTE: Internal default values for Epsilon-50 will be computed for the above soil layer.

Layer 6 is sand, p-y criteria by Reese et al., 1974

Distance from top of pile to top of layer = 49.00000 ft Distance from top of pile to bottom of layer = 56.00000 ft Effective unit weight at top of layer = 62.60000 pcf Effective unit weight at bottom of layer = 62.60000 pcf Friction angle at top of layer = 31.00000 deg. Friction angle at bottom of layer = 31.00000 deg. Subgrade k at top of layer = 0.0000 pci Subgrade k at bottom of layer = 0.0000 pci

NOTE: Internal default values for subgrade k will be computed for the above soil layer.

(Depth of lowest soil layer extends 27.00 ft below pile tip)

-------------------------------------------------------------------------------- Summary of Soil Properties--------------------------------------------------------------------------------

Layer Layer Effective UndrainedAngle of Strain

Page 4

existing phase2 87.lp6oLayer Soil Type Depth Unit Wt. CohesionFriction Factor kpy Num. (p-y Curve Criteria) ft pcf psf deg. Epsilon 50 pci----- ---------------------------------- ---------- ---------- -------------------- ---------- ---------- 1 Sand (Reese, et al.) -5.500 125.000 -- 28.000 -- default 10.000 125.000 -- 28.000 -- default 2 Sand (Reese, et al.) 10.000 67.600 -- 31.000 -- default 15.000 67.600 -- 31.000 -- default 3 Sand (Reese, et al.) 15.000 62.600 -- 30.000 -- default 25.000 62.600 -- 30.000 -- default 4 Sand (Reese, et al.) 25.000 47.600 -- 31.000 -- default 40.000 47.600 -- 31.000 -- default 5 Soft Clay 40.000 57.600 1500.000 -- default -- 49.000 57.600 1500.000 -- default -- 6 Sand (Reese, et al.) 49.000 62.600 -- 31.000 -- default 56.000 62.600 -- 31.000 -- default

-------------------------------------------------------------------------------- Loading Type--------------------------------------------------------------------------------

Static loading criteria were used when computing p-y curves for all analyses.

-------------------------------------------------------------------------------- Pile-head Loading and Pile-head Fixity Conditions--------------------------------------------------------------------------------

Number of loads specified = 14

Load Load Condition Condition Axial Thrust Compute No. Type 1 2 Force, lbsTop y vs. Pile Length----- ---- -------------------- ----------------------- ------------------------------------- 1 4 y = 0.01000 in M = 0.0000 in-lbs 10000.00000000 No 2 4 y = 0.10000 in M = 0.0000 in-lbs 10000.00000000 No 3 4 y = 0.20000 in M = 0.0000 in-lbs 10000.00000000 No 4 4 y = 0.30000 in M = 0.0000 in-lbs 10000.00000000 No 5 4 y = 0.50000 in M = 0.0000 in-lbs 10000.00000000 No

Page 5

existing phase2 87.lp6o 6 4 y = 0.75000 in M = 0.0000 in-lbs 10000.00000000 No 7 4 y = 1.00000 in M = 0.0000 in-lbs 10000.00000000 No 8 5 y = 0.01000 in S = 0.0000 in/in 10000.00000000 No 9 5 y = 0.10000 in S = 0.0000 in/in 10000.00000000 No 10 5 y = 0.20000 in S = 0.0000 in/in 10000.00000000 No 11 5 y = 0.30000 in S = 0.0000 in/in 10000.00000000 No 12 5 y = 0.50000 in S = 0.0000 in/in 10000.00000000 No 13 5 y = 0.75000 in S = 0.0000 in/in 10000.00000000 No 14 5 y = 1.00000 in S = 0.0000 in/in 10000.00000000 No

V = perpendicular shear force applied to pile headM = bending moment applied to pile heady = lateral deflection relative to pile axisS = pile slope relative to original pile batter angleR = rotational stiffness applie to pile headAxial thrust is assumed to be acting axially for all pile batter angles.

-------------------------------------------------------------------------------- Computations of Nominal Moment Capacity and Nonlinear Bending Stiffness--------------------------------------------------------------------------------

Axial thrust force values were determined from pile-head loading conditions

Number of Pile Sections Analyzed = 1

Pile Section No. 1:-------------------

Dimensions and Properties of Drilled Shaft (Bored Pile):--------------------------------------------------------

Length of Section = 29.00000000 ftShaft Diameter = 24.00000000 inConcrete Cover Thickness = 3.00000000 inNumber of Reinforcing Bars = 8 barsYield Stress of Reinforcing Bars = 60.00000000 ksiModulus of Elasticity of Reinforcing Bars = 29000. ksiGross Area of Shaft = 452.38934212 sq. in.Total Area of Reinforcing Steel = 10.16000000 sq. in.Area Ratio of Steel Reinforcement = 2.25 percentEdge-to-Edge Bar Spacing = 5.13229382 inMaximum Concrete Aggregate Size = 0.75000000 inRatio of Bar Spacing to Aggregate Size = 6.84Offset of Rebar Cage Center from Center of Pile = 0.0000000 in

Axial Structural Capacities:----------------------------

Nom. Axial Structural Capacity = 0.85 Fc Ac + Fy As = 1737.285 kipsTensile Load for Cracking of Concrete = -194.263 kipsNominal Axial Tensile Capacity = -609.600 kips

Page 6

existing phase2 87.lp6oReinforcing Bar Dimensions and Positions Used in Computations:

Bar Bar Diam. Bar Area X Y Number inches sq. in. inches inches ---------- ---------- ---------- ---------- ---------- 1 1.27000 1.27000 8.36500 0.00000 2 1.27000 1.27000 5.91495 5.91495 3 1.27000 1.27000 0.00000 8.36500 4 1.27000 1.27000 -5.91495 5.91495 5 1.27000 1.27000 -8.36500 0.00000 6 1.27000 1.27000 -5.91495 -5.91495 7 1.27000 1.27000 0.00000 -8.36500 8 1.27000 1.27000 5.91495 -5.91495

NOTE: The positions of the above rebars were computed by LPile

Minimum spacing between any two bars not equal to zero = 5.13229 inches betweenBars 1 and 2

Spacing to aggregate size ratio = 6.84306

Concrete Properties:--------------------

Compressive Strength of Concrete = 3.00000000 ksiModulus of Elasticity of Concrete = 3122.01857778 ksiModulus of Rupture of Concrete = -0.41079191 ksiCompression Strain at Peak Stress = 0.00163356Tensile Strain at Fracture of Concrete = -0.00011596Maximum Coarse Aggregate Size = 0.75000000 in

Number of Axial Thrust Force Values Determined from Pile-head Loadings = 1

Number Axial Thrust Force kips ------ ------------------ 1 10.000

Definitions of Run Messages and Notes:--------------------------------------

C = concrete in section has cracked in tension. Y = stress in reinforcing steel has reached yield stress. T = ACI 318-08 criteria for tension-controlled section met, tensile strain in reinforcement exceeds 0.005 while simultaneously compressive strain in concrete more than than 0.003. See ACI 318-08, Section 10.3.4. Z = depth of tensile zone in concrete section is less than 10 percent of section depth.

Bending Stiffness (EI) = Computed Bending Moment / Curvature.Position of neutral axis is measured from edge of compression side of pile.Compressive stresses and strains are positive in sign.Tensile stresses and strains are negative in sign.

Axial Thrust Force = 10.000 kips

Bending Bending Bending Depth to Max Comp Max Tens Max Concrete Max Steel Run

Page 7

existing phase2 87.lp6o Curvature Moment Stiffness N Axis Strain Strain Stress Stress Msg rad/in. in-kip kip-in2 in in/in in/in ksi ksi ------------- ------------- ------------- ------------- ------------- -------------------------- ------------- --- 0.000001250 85.7732986 68618639. 16.1837180 0.0000202 -0.000009770 0.0732985 0.5823098 0.000002500 171.1554179 68462167. 14.0986495 0.0000352 -0.0000248 0.1269847 1.0134521 0.000003750 256.0814434 68288385. 13.4037508 0.0000503 -0.0000397 0.1801755 1.4446079 0.000005000 340.5502909 68110058. 13.0563425 0.0000653 -0.0000547 0.2328701 1.8757697 0.000006250 424.5618236 67929892. 12.8479221 0.0000803 -0.0000697 0.2850682 2.3069359 0.000007500 508.1160095 67748801. 12.7089936 0.0000953 -0.0000847 0.3367698 2.7381061 0.000008750 591.2128359 67567181. 12.6097739 0.0001103 -0.0000997 0.3879747 3.1692801 0.0000100 673.8522999 67385230. 12.5353721 0.0001254 -0.0001146 0.4386831 3.6004577 0.0000113 673.8522999 59897982. 8.6707401 0.0000975 -0.0001725 0.3429206 -4.9620211 C 0.0000125 673.8522999 53908184. 8.5648989 0.0001071 -0.0001929 0.3751951 -5.5517241 C 0.0000138 673.8522999 49007440. 8.4777783 0.0001166 -0.0002134 0.4072479 -6.1416359 C 0.0000150 673.8522999 44923487. 8.4047160 0.0001261 -0.0002339 0.4390802 -6.7317485 C 0.0000163 673.8522999 41467834. 8.3433605 0.0001356 -0.0002544 0.4707415 -7.3216413 C 0.0000175 673.8522999 38505846. 8.2912050 0.0001451 -0.0002749 0.5022314 -7.9113134 C 0.0000188 673.8522999 35938789. 8.2455214 0.0001546 -0.0002954 0.5334939 -8.5012477 C 0.0000200 673.8522999 33692615. 8.2056791 0.0001641 -0.0003159 0.5645682 -9.0911061 C 0.0000213 673.8522999 31710696. 8.1708929 0.0001736 -0.0003364 0.5954712 -9.6807372 C 0.0000225 673.8522999 29948991. 8.1403216 0.0001832 -0.0003568 0.6262027 -10.2701401 C 0.0000238 673.8522999 28372728. 8.1133010 0.0001927 -0.0003773 0.6567621 -10.8593139 C 0.0000250 673.8522999 26954092. 8.0892999 0.0002022 -0.0003978 0.6871492 -11.4482575 C 0.0000263 673.8522999 25670564. 8.0678883 0.0002118 -0.0004182 0.7173635 -12.0369700 C 0.0000275 673.8522999 24503720. 8.0487142 0.0002213 -0.0004387 0.7474046 -12.6254504 C 0.0000288 674.6021397 23464422. 8.0312543 0.0002309 -0.0004591 0.7772510 -13.2138916 C 0.0000300 701.6085999 23386953. 8.0153066 0.0002405 -0.0004795 0.8069037 -13.8022832 C 0.0000313 728.5837059 23314679. 8.0008998 0.0002500 -0.0005000 0.8363831 -14.3904345 C 0.0000325 755.5273370 23246995. 7.9878573 0.0002596 -0.0005204 0.8656889 -14.9783444 C 0.0000338 782.4392737 23183386. 7.9760287 0.0002692 -0.0005408 0.8948204 -15.5660127 C 0.0000350 809.3196005 23123417. 7.9652849 0.0002788 -0.0005612 0.9237775 -16.1534365 C 0.0000363 836.1680835 23066706. 7.9555147 0.0002884 -0.0005816

Page 8

existing phase2 87.lp6o 0.9525597 -16.7406158 C 0.0000375 862.9845987 23012923. 7.9466219 0.0002980 -0.0006020 0.9811665 -17.3275492 C 0.0000388 889.7690206 22961781. 7.9385224 0.0003076 -0.0006224 1.0095976 -17.9142359 C 0.0000400 916.5212234 22913031. 7.9311429 0.0003172 -0.0006428 1.0378524 -18.5006746 C 0.0000413 943.2410797 22866450. 7.9244189 0.0003269 -0.0006631 1.0659306 -19.0868642 C 0.0000425 969.9284615 22821846. 7.9182935 0.0003365 -0.0006835 1.0938316 -19.6728036 C 0.0000438 996.5832397 22779045. 7.9127162 0.0003462 -0.0007038 1.1215552 -20.2584916 C 0.0000450 1023.2052842 22737895. 7.9076422 0.0003558 -0.0007242 1.1491008 -20.8439270 C 0.0000463 1049.7944639 22698259. 7.9030317 0.0003655 -0.0007445 1.1764680 -21.4291088 C 0.0000475 1076.3506467 22660014. 7.8988489 0.0003752 -0.0007648 1.2036563 -22.0140357 C 0.0000488 1102.8736992 22623050. 7.8950618 0.0003849 -0.0007851 1.2306653 -22.5987065 C 0.0000513 1155.8198243 22552582. 7.8885618 0.0004043 -0.0008257 1.2841436 -23.7672755 C 0.0000538 1208.6318712 22486174. 7.8833329 0.0004237 -0.0008663 1.3368993 -24.9348051 C 0.0000563 1261.3086661 22423265. 7.8792118 0.0004432 -0.0009068 1.3889285 -26.1012860 C 0.0000588 1313.8490883 22363389. 7.8760627 0.0004627 -0.0009473 1.4402277 -27.2667081 C 0.0000613 1366.2519985 22306155. 7.8737726 0.0004823 -0.0009877 1.4907928 -28.4310613 C 0.0000638 1418.5162391 22251235. 7.8722460 0.0005019 -0.0010281 1.5406202 -29.5943351 C 0.0000663 1470.6406333 22198349. 7.8714020 0.0005215 -0.0010685 1.5897058 -30.7565188 C 0.0000688 1522.6239850 22147258. 7.8711714 0.0005411 -0.0011089 1.6380456 -31.9176018 C 0.0000713 1574.4650780 22097755. 7.8714951 0.0005608 -0.0011492 1.6856357 -33.0775730 C 0.0000738 1626.1626759 22049663. 7.8723219 0.0005806 -0.0011894 1.7324720 -34.2364213 C 0.0000763 1677.7155213 22002827. 7.8736075 0.0006004 -0.0012296 1.7785502 -35.3941352 C 0.0000788 1729.1223351 21957109. 7.8753133 0.0006202 -0.0012698 1.8238662 -36.5507031 C 0.0000813 1780.3818166 21912392. 7.8774054 0.0006400 -0.0013100 1.8684156 -37.7061134 C 0.0000838 1831.4926424 21868569. 7.8798543 0.0006599 -0.0013501 1.9121942 -38.8603538 C 0.0000863 1882.4534661 21825547. 7.8826338 0.0006799 -0.0013901 1.9551975 -40.0134122 C 0.0000888 1933.2629173 21783244. 7.8857209 0.0006999 -0.0014301 1.9974211 -41.1652761 C 0.0000913 1983.9196016 21741585. 7.8890950 0.0007199 -0.0014701 2.0388603 -42.3159326 C 0.0000938 2034.4220994 21700502. 7.8927380 0.0007399 -0.0015101 2.0795105 -43.4653690 C 0.0000963 2084.7689656 21659937. 7.8966337 0.0007601 -0.0015499 2.1193671 -44.6135719 C 0.0000988 2134.9587286 21619835. 7.9007675 0.0007802 -0.0015898 2.1584253 -45.7605278 C 0.0001013 2184.9898900 21580147. 7.9051266 0.0008004 -0.0016296 2.1966802 -46.9062229 C

Page 9

existing phase2 87.lp6o 0.0001038 2234.8609234 21540828. 7.9096993 0.0008206 -0.0016694 2.2341268 -48.0506434 C 0.0001063 2284.5702740 21501838. 7.9144752 0.0008409 -0.0017091 2.2707602 -49.1937747 C 0.0001088 2334.1163575 21463139. 7.9194448 0.0008612 -0.0017488 2.3065753 -50.3356024 C 0.0001113 2383.4975596 21424697. 7.9245998 0.0008816 -0.0017884 2.3415668 -51.4761115 C 0.0001138 2432.7122350 21386481. 7.9299326 0.0009020 -0.0018280 2.3757295 -52.6152869 C 0.0001163 2481.7587062 21348462. 7.9354362 0.0009225 -0.0018675 2.4090580 -53.7531129 C 0.0001188 2530.6352634 21310613. 7.9411045 0.0009430 -0.0019070 2.4415469 -54.8895738 C 0.0001213 2579.3401625 21272909. 7.9469319 0.0009636 -0.0019464 2.4731906 -56.0246534 C 0.0001238 2627.8716249 21235326. 7.9529134 0.0009842 -0.0019858 2.5039834 -57.1583351 C 0.0001263 2676.2281536 21197847. 7.9590444 0.0010048 -0.0020252 2.5339199 -58.2905982 C 0.0001288 2724.4072894 21160445. 7.9653209 0.0010255 -0.0020645 2.5629936 -59.4214328 C 0.0001313 2772.4074348 21123104. 7.9717391 0.0010463 -0.0021037 2.5911989 -60.0000000 CY 0.0001338 2820.2266616 21085807. 7.9782957 0.0010671 -0.0021429 2.6185296 -60.0000000 CY 0.0001363 2867.8630011 21048536. 7.9849879 0.0010880 -0.0021820 2.6449796 -60.0000000 CY 0.0001388 2915.3144431 21011275. 7.9918129 0.0011089 -0.0022211 2.6705426 -60.0000000 CY 0.0001413 2962.5789346 20974010. 7.9987684 0.0011298 -0.0022602 2.6952120 -60.0000000 CY 0.0001438 3009.6543785 20936726. 8.0058523 0.0011508 -0.0022992 2.7189814 -60.0000000 CY 0.0001463 3056.5386320 20899409. 8.0130627 0.0011719 -0.0023381 2.7418441 -60.0000000 CY 0.0001488 3103.2295051 20862047. 8.0203982 0.0011930 -0.0023770 2.7637932 -60.0000000 CY 0.0001588 3288.0308662 20712005. 8.0506145 0.0012780 -0.0025320 2.8422658 -60.0000000 CY 0.0001688 3457.9366570 20491476. 8.0727358 0.0013623 -0.0026877 2.9044499 -60.0000000 CY 0.0001788 3591.8432935 20094228. 8.0712528 0.0014427 -0.0028473 2.9493432 -60.0000000 CY 0.0001888 3714.1761680 19677755. 8.0670657 0.0015227 -0.0030073 2.9799488 -60.0000000 CY 0.0001988 3833.6003798 19288555. 8.0670581 0.0016033 -0.0031667 2.9967120 -60.0000000 CY 0.0002088 3933.4425138 18842838. 8.0562567 0.0016817 -0.0033283 2.9991826 -60.0000000 CY 0.0002188 3993.9920055 18258249. 8.0165222 0.0017536 -0.0034964 2.9998591 -60.0000000 CY 0.0002288 4028.8576130 17612492. 7.9601236 0.0018209 -0.0036691 2.9999738 -60.0000000 CY 0.0002388 4061.0035215 17009439. 7.9092390 0.0018883 -0.0038417 2.9999894 -60.0000000 CY 0.0002488 4092.1909964 16451019. 7.8645808 0.0019563 -0.0040137 2.9999648 -60.0000000 CY 0.0002588 4122.4922615 15932337. 7.8253444 0.0020248 -0.0041852 2.9998271 -60.0000000 CY 0.0002688 4151.9345383 15449059. 7.7903709 0.0020937 -0.0043563 2.9993714 -60.0000000 CY 0.0002788 4180.5325552 14997426. 7.7584149 0.0021627 -0.0045273

Page 10

existing phase2 87.lp6o 2.9982415 60.0000000 CY 0.0002888 4208.4810849 14574826. 7.7302049 0.0022321 -0.0046979 2.9980292 60.0000000 CY 0.0002988 4235.8038861 14178423. 7.7053463 0.0023020 -0.0048680 2.9998176 60.0000000 CY 0.0003088 4262.5488688 13805826. 7.6834551 0.0023723 -0.0050377 2.9982600 60.0000000 CY 0.0003188 4288.8097589 13455089. 7.6641015 0.0024429 -0.0052071 2.9987280 60.0000000 CY 0.0003288 4314.5525336 13124114. 7.6471324 0.0025140 -0.0053760 2.9991857 60.0000000 CY 0.0003388 4339.8743971 12811437. 7.6321817 0.0025854 -0.0055446 2.9964911 60.0000000 CY 0.0003488 4364.7808407 12515501. 7.6190760 0.0026572 -0.0057128 2.9994230 60.0000000 CY 0.0003588 4389.3091377 12235008. 7.6076107 0.0027292 -0.0058808 2.9959658 60.0000000 CY 0.0003688 4413.4854701 11968774. 7.5976129 0.0028016 -0.0060484 2.9991992 60.0000000 CY 0.0003788 4437.3469127 11715767. 7.5889124 0.0028743 -0.0062157 2.9971767 60.0000000 CY 0.0003888 4460.8836898 11474942. 7.5814346 0.0029473 -0.0063827 2.9982790 60.0000000 CY 0.0003988 4484.1845721 11245604. 7.5749331 0.0030205 -0.0065495 2.9999994 60.0000000 CYT 0.0004088 4507.1520075 11026672. 7.5695265 0.0030940 -0.0067160 2.9959441 60.0000000 CYT 0.0004188 4528.8296459 10815116. 7.5633867 0.0031672 -0.0068828 2.9993449 60.0000000 CYT 0.0004288 4549.9306149 10612083. 7.5574613 0.0032403 -0.0070497 2.9975587 60.0000000 CYT 0.0004388 4567.7180744 10410753. 7.5475239 0.0033115 -0.0072185 2.9960156 60.0000000 CYT 0.0004488 4584.6393212 10216466. 7.5372890 0.0033824 -0.0073876 2.9991028 60.0000000 CYT 0.0004588 4597.9326428 10022741. 7.5225605 0.0034510 -0.0075590 2.9998409 60.0000000 CYT 0.0004688 4609.7249399 9834080. 7.5076368 0.0035192 -0.0077308 2.9938940 60.0000000 CYT 0.0004788 4618.5626625 9647128. 7.4889183 0.0035853 -0.0079047 2.9960881 60.0000000 CYT 0.0004888 4625.5523880 9464046. 7.4683027 0.0036501 -0.0080799 2.9985288 60.0000000 CYT 0.0004988 4630.2285845 9283666. 7.4477359 0.0037146 -0.0082554 2.9997874 60.0000000 CYT 0.0005088 4632.4929137 9105637. 7.4244391 0.0037772 -0.0084328 2.9985720 60.0000000 CYT 0.0005188 4634.5866438 8934143. 7.4020464 0.0038398 -0.0086102 2.9942872 60.0000000 CYT

-------------------------------------------------------------------------------- Summary of Results for Nominal (Unfactored) Moment Capacity for Section 1--------------------------------------------------------------------------------

Moment values interpolated at maximum compressive strain = 0.003or maximum developed moment if pile fails at smaller strains.

Load Axial Thrust Nominal Mom. Cap. Max. Comp. No. kips in-kip Strain ---- ---------------- ------------------ ------------ 1 10.000 4477.660 0.00300000

Page 11

existing phase2 87.lp6oNote note that the values of moment capacity in the table above are not factored by a strength reduction factor (phi-factor).

In ACI 318-08, the value of the strength reduction factor depends on whether the transverse reinforcing steel bars are tied hoops (0.65) or spirals (0.70).

The above values should be multiplied by the appropriate strength reduction factor to compute ultimate moment capacity according to ACI 318-08, Section 9.3.2.2 or the value required by the design standard being followed.

The following table presents factored moment capacities and corresponding bending stiffnesses computed for common resistance factor values used for reinforced concrete sections.

Axial Resistance Nominal Ultimate (Factored) Ultimate (Factored) Bending Stiffness Load Factor Moment Capacity Axial Thrust Moment Capacity at Ult. Mom. Cap. No. for Moment in-kip kipsin-kip kip-in^2 ----- ---------- ------------------- -------------------------------------- ------------------- 1 0.65 4477.660 6.5002910.479 21015072.538

1 0.70 4477.660 7.0003134.362 20836770.682

1 0.75 4477.660 7.5003358.245 20620871.565

-------------------------------------------------------------------------------- Computed Values of Pile Loading and Deflection for Lateral Loading for Load Case Number 1--------------------------------------------------------------------------------

Pile-head conditions are Displacement and Moment (Loading Type 4)Displacement of pile head = 0.010000 inchesMoment at pile head = 0.000 in-lbsAxial load at pile head = 10000.000 lbs

Depth Deflect. Bending Shear Slope Total Bending Soil Res. Soil Spr. Distrib. X y Moment Force S Stress Stiffness p Es*h Lat. Load feet inches in-lbs lbs radians psi* lb-in^2 lb/in lb/inch lb/inch ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- 0.00 0.0100 0.000 1124.2771 -9.863E-05 0.000 6.862E+10-13.9015 2418.8688 0.000 0.290 0.009657 3831.7399 1075.4983 -9.853E-05 0.000 6.862E+10-14.1322 5092.8184 0.000 0.580 0.009314 7492.3261 1026.0025 -9.825E-05 0.000 6.862E+10-14.3136 5347.8991 0.000 0.870 0.008973 10980. 975.9590 -9.778E-05 0.000 6.862E+10-14.4470 5602.9798 0.000 1.160 0.008634 14292. 925.5330 -9.714E-05 0.000 6.862E+10-14.5335 5858.0605 0.000 1.450 0.008297 17428. 874.8846 -9.633E-05 0.000 6.862E+10

Page 12

existing phase2 87.lp6o-14.5748 6113.1412 0.000 1.740 0.007963 20388. 824.1687 -9.537E-05 0.000 6.862E+10-14.5723 6368.2219 0.000 2.030 0.007633 23171. 773.5348 -9.427E-05 0.000 6.862E+10-14.5277 6623.3027 0.000 2.320 0.007307 25778. 723.1260 -9.303E-05 0.000 6.862E+10-14.4428 6878.3834 0.000 2.610 0.006986 28210. 673.0796 -9.166E-05 0.000 6.862E+10-14.3195 7133.4641 0.000 2.900 0.006669 30469. 623.5260 -9.017E-05 0.000 6.862E+10-14.1596 7388.5448 0.000 3.190 0.006358 32556. 574.5889 -8.857E-05 0.000 6.862E+10-13.9651 7643.6255 0.000 3.480 0.006053 34474. 526.3854 -8.687E-05 0.000 6.862E+10-13.7381 7898.7062 0.000 3.770 0.005753 36226. 479.0250 -8.508E-05 0.000 6.862E+10-13.4805 8153.7869 0.000 4.060 0.005461 37814. 432.6104 -8.320E-05 0.000 6.862E+10-13.1945 8408.8677 0.000 4.350 0.005174 39243. 387.2368 -8.125E-05 0.000 6.862E+10-12.8822 8663.9484 0.000 4.640 0.004895 40515. 342.9921 -7.923E-05 0.000 6.862E+10-12.5457 8919.0291 0.000 4.930 0.004623 41636. 299.9569 -7.714E-05 0.000 6.862E+10-12.1871 9174.1098 0.000 5.220 0.004358 42608. 258.2043 -7.501E-05 0.000 6.862E+10-11.8086 9429.1905 0.000 5.510 0.004101 43438. 217.8004 -7.282E-05 0.000 6.862E+10-11.4121 9684.2712 0.000 5.800 0.003851 44129. 178.8037 -7.060E-05 0.000 6.862E+10-10.9998 9939.3519 0.000 6.090 0.003609 44687. 141.2657 -6.835E-05 0.000 6.862E+10-10.5737 10194. 0.000 6.380 0.003376 45117. 105.2309 -6.607E-05 0.000 6.862E+10-10.1359 10450. 0.000 6.670 0.003150 45424. 70.7368 -6.378E-05 0.000 6.862E+10-9.6883 10705. 0.000 6.960 0.002932 45614. 37.8142 -6.147E-05 0.000 6.862E+10-9.2328 10960. 0.000 7.250 0.002722 45692. 6.4872 -5.915E-05 0.000 6.862E+10-8.7713 11215. 0.000 7.540 0.002520 45663. -23.2265 -5.684E-05 0.000 6.862E+10-8.3056 11470. 0.000 7.830 0.002326 45534. -51.3153 -5.453E-05 0.000 6.862E+10-7.8374 11725. 0.000 8.120 0.002140 45310. -77.7736 -5.222E-05 0.000 6.862E+10-7.3685 11980. 0.000 8.410 0.001963 44996. -102.6018 -4.993E-05 0.000 6.862E+10-6.9005 12235. 0.000 8.700 0.001793 44599. -125.8057 -4.766E-05 0.000 6.862E+10-6.4350 12490. 0.000 8.990 0.001631 44124. -147.3963 -4.541E-05 0.000 6.862E+10-5.9734 12745. 0.000 9.280 0.001477 43576. -167.3898 -4.319E-05 0.000 6.862E+10-5.5171 13000. 0.000 9.570 0.001330 42962. -185.8072 -4.099E-05 0.000 6.862E+10-5.0676 13255. 0.000 9.860 0.001192 42286. -202.6740 -3.883E-05 0.000 6.862E+10-4.6260 13510. 0.000 10.150 0.001060 41554. -223.8219 -3.670E-05 0.000 6.862E+10-7.5280 24711. 0.000 10.440 0.000936 40731. -248.6996 -3.462E-05 0.000 6.862E+10-6.7695 25166. 0.000

Page 13

existing phase2 87.lp6o 10.730 0.000819 39826. -270.9735 -3.258E-05 0.000 6.862E+10-6.0315 25622. 0.000 11.020 0.000709 38847. -290.7174 -3.058E-05 0.000 6.862E+10-5.3156 26077. 0.000 11.310 0.000606 37804. -308.0108 -2.864E-05 0.000 6.862E+10-4.6232 26533. 0.000 11.600 0.000510 36705. -322.9378 -2.675E-05 0.000 6.862E+10-3.9555 26988. 0.000 11.890 0.000420 35559. -335.5864 -2.491E-05 0.000 6.862E+10-3.3138 27443. 0.000 12.180 0.000337 34371. -346.0484 -2.314E-05 0.000 6.862E+10-2.6988 27899. 0.000 12.470 0.000259 33152. -354.4183 -2.143E-05 0.000 6.862E+10-2.1114 28354. 0.000 12.760 0.000187 31906. -360.7930 -1.978E-05 0.000 6.862E+10-1.5522 28810. 0.000 13.050 0.000121 30642. -365.2714 -1.819E-05 0.000 6.862E+10-1.0216 29265. 0.000 13.340 6.087E-05 29365. -367.9534 -1.667E-05 0.000 6.862E+10-0.5198 29720. 0.000 13.630 5.440E-06 28082. -368.9400 -1.522E-05 0.000 6.862E+10-0.0472 30176. 0.000 13.920 -4.503E-05 26798. -368.3324 -1.382E-05 0.000 6.862E+100.3964 30631. 0.000 14.210 -9.077E-05 25519. -366.2318 -1.250E-05 0.000 6.862E+100.8109 31087. 0.000 14.500 -0.000132 24250. -362.7389 -1.123E-05 0.000 6.862E+101.1965 31542. 0.000 14.790 -0.000169 22996. -357.9537 -1.004E-05 0.000 6.862E+101.5536 31997. 0.000 15.080 -0.000202 21760. -352.3798 -8.902E-06 0.000 6.862E+101.6498 28440. 0.000 15.370 -0.000231 20544. -346.1818 -7.829E-06 0.000 6.862E+101.9123 28818. 0.000 15.660 -0.000256 19351. -339.1120 -6.818E-06 0.000 6.862E+102.1508 29196. 0.000 15.950 -0.000278 18184. -331.2533 -5.866E-06 0.000 6.862E+102.3657 29574. 0.000 16.240 -0.000297 17046. -322.6863 -4.973E-06 0.000 6.862E+102.5578 29952. 0.000 16.530 -0.000313 15938. -313.4893 -4.136E-06 0.000 6.862E+102.7278 30329. 0.000 16.820 -0.000326 14864. -303.7381 -3.355E-06 0.000 6.862E+102.8764 30707. 0.000 17.110 -0.000336 13825. -293.5056 -2.628E-06 0.000 6.862E+103.0044 31085. 0.000 17.400 -0.000344 12821. -282.8622 -1.952E-06 0.000 6.862E+103.1125 31463. 0.000 17.690 -0.000350 11856. -271.8754 -1.326E-06 0.000 6.862E+103.2017 31841. 0.000 17.980 -0.000353 10929. -260.6099 -7.485E-07 0.000 6.862E+103.2727 32219. 0.000 18.270 -0.000355 10042. -249.1273 -2.167E-07 0.000 6.862E+103.3265 32597. 0.000 18.560 -0.000355 9195.3494 -237.4862 2.711E-07 0.000 6.862E+103.3638 32974. 0.000 18.850 -0.000353 8389.2481 -225.7425 7.170E-07 0.000 6.862E+103.3855 33352. 0.000 19.140 -0.000350 7624.1319 -213.9487 1.123E-06 0.000 6.862E+103.3925 33730. 0.000 19.430 -0.000345 6900.0869 -202.1548 1.491E-06 0.000 6.862E+103.3856 34108. 0.000 19.720 -0.000340 6217.0306 -190.4077 1.824E-06 0.000 6.862E+10

Page 14

existing phase2 87.lp6o3.3656 34486. 0.000 20.010 -0.000333 5574.7227 -178.7513 2.123E-06 0.000 6.862E+103.3334 34864. 0.000 20.300 -0.000325 4972.7740 -167.2269 2.390E-06 0.000 6.862E+103.2898 35241. 0.000 20.590 -0.000316 4410.6569 -155.8732 2.628E-06 0.000 6.862E+103.2354 35619. 0.000 20.880 -0.000307 3887.7138 -144.7259 2.839E-06 0.000 6.862E+103.1711 35997. 0.000 21.170 -0.000296 3403.1667 -133.8186 3.024E-06 0.000 6.862E+103.0975 36375. 0.000 21.460 -0.000286 2956.1256 -123.1822 3.185E-06 0.000 6.862E+103.0154 36753. 0.000 21.750 -0.000274 2545.5967 -112.8454 3.324E-06 0.000 6.862E+102.9253 37131. 0.000 22.040 -0.000262 2170.4902 -102.8346 3.444E-06 0.000 6.862E+102.8280 37508. 0.000 22.330 -0.000250 1829.6278 -93.1744 3.546E-06 0.000 6.862E+102.7239 37886. 0.000 22.620 -0.000238 1521.7498 -83.8871 3.630E-06 0.000 6.862E+102.6136 38264. 0.000 22.910 -0.000225 1245.5211 -74.9935 3.701E-06 0.000 6.862E+102.4977 38642. 0.000 23.200 -0.000212 999.5377 -66.5125 3.758E-06 0.000 6.862E+102.3764 39020. 0.000 23.490 -0.000199 782.3323 -58.4618 3.803E-06 0.000 6.862E+102.2504 39398. 0.000 23.780 -0.000185 592.3789 -50.8574 3.838E-06 0.000 6.862E+102.1200 39775. 0.000 24.070 -0.000172 428.0979 -43.7141 3.864E-06 0.000 6.862E+101.9854 40153. 0.000 24.360 -0.000159 287.8600 -37.0456 3.882E-06 0.000 6.862E+101.8470 40531. 0.000 24.650 -0.000145 169.9901 -30.8648 3.893E-06 0.000 6.862E+101.7052 40909. 0.000 24.940 -0.000131 72.7701 -25.1834 3.899E-06 0.000 6.862E+101.5600 41287. 0.000 25.230 -0.000118 -5.5579 -19.5326 3.901E-06 0.000 6.862E+101.6876 49806. 0.000 25.520 -0.000104 -63.4485 -13.9741 3.899E-06 0.000 6.862E+101.5069 50261. 0.000 25.810 -9.077E-05 -103.0893 -9.0502 3.895E-06 0.000 6.862E+101.3229 50717. 0.000 26.100 -7.723E-05 -126.7089 -4.7724 3.889E-06 0.000 6.862E+101.1356 51172. 0.000 26.390 -6.370E-05 -136.5757 -1.1520 3.883E-06 0.000 6.862E+100.9451 51628. 0.000 26.680 -5.020E-05 -134.9969 1.7999 3.876E-06 0.000 6.862E+100.7514 52083. 0.000 26.970 -3.673E-05 -124.3184 4.0721 3.869E-06 0.000 6.862E+100.5545 52538. 0.000 27.260 -2.327E-05 -106.9245 5.6536 3.863E-06 0.000 6.862E+100.3544 52994. 0.000 27.550 -9.840E-06 -85.2382 6.5333 3.858E-06 0.000 6.862E+100.1511 53449. 0.000 27.840 3.580E-06 -61.7216 6.6997 3.855E-06 0.000 6.862E+10-0.0555 53905. 0.000 28.130 1.699E-05 -38.8764 6.1415 3.852E-06 0.000 6.862E+10-0.2654 54360. 0.000 28.420 3.039E-05 -19.2451 4.8467 3.851E-06 0.000 6.862E+10-0.4787 54815. 0.000 28.710 4.379E-05 -5.4112 2.8036 3.850E-06 0.000 6.862E+10-0.6955 55271. 0.000

Page 15

existing phase2 87.lp6o 29.000 5.719E-05 0.000 0.000 3.850E-06 0.000 6.862E+10-0.9158 27863. 0.000

* This analysis makes computations of pile response using nonlinear moment-curvaturerelationships. The above values of total stress are computed for combined axial and bending stress in elastic sections and do not equal actual stresses in concrete and steel in the range of nonlinear bending.

Output Summary for Load Case No. 1:

Pile-head deflection = 0.0100000 inchesComputed slope at pile head = -0.0000986 radiansMaximum bending moment = 45692. inch-lbsMaximum shear force = 1124.2770768 lbsDepth of maximum bending moment = 87.0000000 inches below pile headDepth of maximum shear force = 0.000000 inches below pile headNumber of iterations = 6Number of zero deflection points = 2

-------------------------------------------------------------------------------- Computed Values of Pile Loading and Deflection for Lateral Loading for Load Case Number 2--------------------------------------------------------------------------------

Pile-head conditions are Displacement and Moment (Loading Type 4)Displacement of pile head = 0.100000 inchesMoment at pile head = 0.000 in-lbsAxial load at pile head = 10000.000 lbs

Depth Deflect. Bending Shear Slope Total Bending Soil Res. Soil Spr. Distrib. X y Moment Force S Stress Stiffness p Es*h Lat. Load feet inches in-lbs lbs radians psi* lb-in^2 lb/in lb/inch lb/inch ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- 0.00 0.1000 0.000 11211. -0.000988 0.000 6.862E+10-139.0155 2418.8688 0.000 0.290 0.0966 38208. 10724. -0.000987 0.000 6.862E+10-141.3135 5092.8184 0.000 0.580 0.0931 74705. 10229. -0.000984 0.000 6.862E+10-143.1179 5347.8991 0.000 0.870 0.0897 109468. 9728.2909 -0.000980 0.000 6.855E+10-144.4404 5602.9798 0.000 1.160 0.0863 142482. 9224.1525 -0.000973 0.000 6.849E+10-145.2943 5858.0605 0.000 1.450 0.0829 173736. 8717.8325 -0.000965 0.000 6.845E+10-145.6942 6113.1412 0.000 1.740 0.0796 203225. 8210.8837 -0.000956 0.000 6.838E+10-145.6557 6368.2219 0.000 2.030 0.0763 230950. 7704.8023 -0.000944 0.000 6.833E+10-145.1957 6623.3027 0.000 2.320 0.0730 256916. 7201.0247 -0.000932 0.000 6.829E+10-144.3317 6878.3834 0.000 2.610 0.0698 281134. 6700.9244 -0.000918 0.000 6.822E+10-143.0823 7133.4641 0.000 2.900 0.0666 303618. 6205.8092 -0.000903 0.000 6.818E+10

Page 16

existing phase2 87.lp6o-141.4667 7388.5448 0.000 3.190 0.0635 324389. 5716.9189 -0.000887 0.000 6.814E+10-139.5047 7643.6255 0.000 3.480 0.0605 343470. 5235.4236 -0.000870 0.000 6.810E+10-137.2167 7898.7062 0.000 3.770 0.0575 360888. 4762.4219 -0.000852 0.000 6.806E+10-134.6233 8153.7869 0.000 4.060 0.0545 376676. 4298.9399 -0.000833 0.000 6.802E+10-131.7456 8408.8677 0.000 4.350 0.0517 390867. 3845.9303 -0.000814 0.000 6.799E+10-128.6048 8663.9484 0.000 4.640 0.0489 403500. 3404.2716 -0.000793 0.000 6.797E+10-125.2221 8919.0291 0.000 4.930 0.0461 414616. 2974.7685 -0.000773 0.000 6.795E+10-121.6188 9174.1098 0.000 5.220 0.0435 424258. 2558.1514 -0.000751 0.000 6.793E+10-117.8163 9429.1905 0.000 5.510 0.0409 432473. 2155.0771 -0.000729 0.000 6.791E+10-113.8356 9684.2712 0.000 5.800 0.0384 439308. 1766.1296 -0.000707 0.000 6.789E+10-109.6975 9939.3519 0.000 6.090 0.0360 444814. 1391.8205 -0.000684 0.000 6.788E+10-105.4227 10194. 0.000 6.380 0.0336 449043. 1032.5904 -0.000661 0.000 6.787E+10-101.0314 10450. 0.000 6.670 0.0314 452047. 688.8104 -0.000638 0.000 6.786E+10-96.5433 10705. 0.000 6.960 0.0292 453882. 360.7834 -0.000615 0.000 6.786E+10-91.9779 10960. 0.000 7.250 0.0271 454601. 48.7458 -0.000592 0.000 6.786E+10-87.3540 11215. 0.000 7.540 0.0251 454262. -247.1302 -0.000568 0.000 6.786E+10-82.6897 11470. 0.000 7.830 0.0232 452921. -526.7351 -0.000545 0.000 6.786E+10-78.0027 11725. 0.000 8.120 0.0213 450634. -790.0194 -0.000522 0.000 6.787E+10-73.3101 11980. 0.000 8.410 0.0195 447458. -1036.9917 -0.000499 0.000 6.787E+10-68.6280 12235. 0.000 8.700 0.0178 443451. -1267.7161 -0.000476 0.000 6.788E+10-63.9722 12490. 0.000 8.990 0.0162 438668. -1482.3100 -0.000453 0.000 6.789E+10-59.3576 12745. 0.000 9.280 0.0147 433166. -1680.9410 -0.000431 0.000 6.791E+10-54.7982 13000. 0.000 9.570 0.0132 426999. -1863.8249 -0.000409 0.000 6.792E+10-50.3075 13255. 0.000 9.860 0.0118 420222. -2031.2229 -0.000387 0.000 6.794E+10-45.8982 13510. 0.000 10.150 0.0105 412889. -2240.9688 -0.000366 0.000 6.795E+10-74.6455 24711. 0.000 10.440 0.009276 404650. -2487.5681 -0.000345 0.000 6.797E+10-67.0783 25166. 0.000 10.730 0.008111 395599. -2708.1943 -0.000325 0.000 6.798E+10-59.7183 25622. 0.000 11.020 0.007017 385824. -2903.5964 -0.000305 0.000 6.800E+10-52.5817 26077. 0.000 11.310 0.005992 375411. -3074.5762 -0.000285 0.000 6.803E+10-45.6826 26533. 0.000 11.600 0.005033 364445. -3221.9820 -0.000266 0.000 6.805E+10-39.0334 26988. 0.000 11.890 0.004140 353005. -3346.7021 -0.000248 0.000 6.808E+10-32.6448 27443. 0.000

Page 17

existing phase2 87.lp6o 12.180 0.003309 341169. -3449.6590 -0.000230 0.000 6.811E+10-26.5258 27899. 0.000 12.470 0.002539 329011. -3531.8034 -0.000213 0.000 6.813E+10-20.6836 28354. 0.000 12.760 0.001827 316602. -3594.1087 -0.000196 0.000 6.815E+10-15.1240 28810. 0.000 13.050 0.001171 304010. -3637.5657 -0.000181 0.000 6.817E+10-9.8513 29265. 0.000 13.340 0.000570 291297. -3663.1775 -0.000165 0.000 6.820E+10-4.8682 29720. 0.000 13.630 2.032E-05 278526. -3671.9547 -0.000151 0.000 6.823E+10-0.1762 30176. 0.000 13.920 -0.000480 265751. -3664.9107 -0.000137 0.000 6.826E+104.2245 30631. 0.000 14.210 -0.000933 253027. -3643.0572 -0.000124 0.000 6.829E+108.3350 31087. 0.000 14.500 -0.001341 240404. -3607.4006 -0.000111 0.000 6.831E+1012.1573 31542. 0.000 14.790 -0.001707 227928. -3558.9381 -9.926E-05 0.000 6.833E+1015.6947 31997. 0.000 15.080 -0.002032 215641. -3502.7316 -8.797E-05 0.000 6.835E+1016.6079 28440. 0.000 15.370 -0.002319 203555. -3440.4165 -7.730E-05 0.000 6.838E+1019.2054 28818. 0.000 15.660 -0.002570 191701. -3369.4798 -6.724E-05 0.000 6.841E+1021.5628 29196. 0.000 15.950 -0.002787 180108. -3290.7463 -5.779E-05 0.000 6.844E+1023.6863 29574. 0.000 16.240 -0.002972 168801. -3205.0184 -4.892E-05 0.000 6.846E+1025.5826 29952. 0.000 16.530 -0.003128 157804. -3113.0743 -4.062E-05 0.000 6.848E+1027.2589 30329. 0.000 16.820 -0.003255 147137. -3015.6665 -3.287E-05 0.000 6.849E+1028.7226 30707. 0.000 17.110 -0.003356 136818. -2913.5212 -2.566E-05 0.000 6.850E+1029.9816 31085. 0.000 17.400 -0.003434 126861. -2807.3368 -1.896E-05 0.000 6.852E+1031.0439 31463. 0.000 17.690 -0.003488 117280. -2697.7833 -1.276E-05 0.000 6.853E+1031.9179 31841. 0.000 17.980 -0.003522 108085. -2585.5017 -7.040E-06 0.000 6.855E+1032.6118 32219. 0.000 18.270 -0.003537 99285. -2471.1035 -1.777E-06 0.000 6.858E+1033.1343 32597. 0.000 18.560 -0.003535 90886. -2355.1704 3.047E-06 0.000 6.860E+1033.4939 32974. 0.000 18.850 -0.003516 82893. -2238.2544 7.454E-06 0.000 6.862E+1033.6992 33352. 0.000 19.140 -0.003483 75308. -2120.8779 1.147E-05 0.000 6.862E+1033.7586 33730. 0.000 19.430 -0.003436 68131. -2003.5338 1.510E-05 0.000 6.862E+1033.6805 34108. 0.000 19.720 -0.003378 61362. -1886.6862 1.839E-05 0.000 6.862E+1033.4732 34486. 0.000 20.010 -0.003308 54998. -1770.7710 2.134E-05 0.000 6.862E+1033.1447 34864. 0.000 20.300 -0.003229 49036. -1656.1964 2.398E-05 0.000 6.862E+1032.7028 35241. 0.000 20.590 -0.003142 43469. -1543.3436 2.632E-05 0.000 6.862E+1032.1551 35619. 0.000 20.880 -0.003046 38292. -1432.5679 2.839E-05 0.000 6.862E+1031.5091 35997. 0.000 21.170 -0.002944 33497. -1324.1995 3.021E-05 0.000 6.862E+10

Page 18

existing phase2 87.lp6o30.7716 36375. 0.000 21.460 -0.002836 29074. -1218.5446 3.180E-05 0.000 6.862E+1029.9496 36753. 0.000 21.750 -0.002723 25014. -1115.8866 3.317E-05 0.000 6.862E+1029.0493 37131. 0.000 22.040 -0.002605 21305. -1016.4872 3.435E-05 0.000 6.862E+1028.0768 37508. 0.000 22.330 -0.002484 17936. -920.5876 3.534E-05 0.000 6.862E+1027.0379 37886. 0.000 22.620 -0.002359 14895. -828.4100 3.618E-05 0.000 6.862E+1025.9378 38264. 0.000 22.910 -0.002232 12168. -740.1586 3.686E-05 0.000 6.862E+1024.7814 38642. 0.000 23.200 -0.002102 9741.1657 -656.0212 3.742E-05 0.000 6.862E+1023.5734 39020. 0.000 23.490 -0.001971 7599.6426 -576.1706 3.786E-05 0.000 6.862E+1022.3178 39398. 0.000 23.780 -0.001839 5728.3832 -500.7657 3.819E-05 0.000 6.862E+1021.0184 39775. 0.000 24.070 -0.001706 4111.6546 -429.9531 3.844E-05 0.000 6.862E+1019.6786 40153. 0.000 24.360 -0.001571 2733.2341 -363.8681 3.862E-05 0.000 6.862E+1018.3013 40531. 0.000 24.650 -0.001437 1576.4451 -302.6364 3.873E-05 0.000 6.862E+1016.8893 40909. 0.000 24.940 -0.001302 624.1894 -246.3752 3.878E-05 0.000 6.862E+1015.4447 41287. 0.000 25.230 -0.001167 -141.0257 -190.4448 3.880E-05 0.000 6.862E+1016.6992 49806. 0.000 25.520 -0.001032 -704.0064 -135.4583 3.877E-05 0.000 6.862E+1014.9022 50261. 0.000 25.810 -0.000897 -1086.5144 -86.7838 3.873E-05 0.000 6.862E+1013.0716 50717. 0.000 26.100 -0.000762 -1310.7175 -44.5362 3.867E-05 0.000 6.862E+1011.2086 51172. 0.000 26.390 -0.000628 -1399.1773 -8.8272 3.860E-05 0.000 6.862E+109.3138 51628. 0.000 26.680 -0.000494 -1374.8411 20.2330 3.853E-05 0.000 6.862E+107.3875 52083. 0.000 26.970 -0.000360 -1261.0373 42.5348 3.846E-05 0.000 6.862E+105.4297 52538. 0.000 27.260 -0.000226 -1081.4760 57.9683 3.840E-05 0.000 6.862E+103.4402 52994. 0.000 27.550 -9.237E-05 -860.2505 66.4228 3.835E-05 0.000 6.862E+101.4187 53449. 0.000 27.840 4.102E-05 -621.8429 67.7855 3.832E-05 0.000 6.862E+10-0.6355 53905. 0.000 28.130 0.000174 -391.1300 61.9421 3.829E-05 0.000 6.862E+10-2.7228 54360. 0.000 28.420 0.000308 -193.3906 48.7760 3.827E-05 0.000 6.862E+10-4.8439 54815. 0.000 28.710 0.000441 -54.3127 28.1687 3.827E-05 0.000 6.862E+10-6.9994 55271. 0.000 29.000 0.000574 0.000 0.000 3.827E-05 0.000 6.862E+10-9.1895 27863. 0.000

* This analysis makes computations of pile response using nonlinear moment-curvaturerelationships. The above values of total stress are computed for combined axial and bending stress in elastic sections and do not equal actual stresses in concrete and steel in the range of nonlinear bending.

Page 19

existing phase2 87.lp6o

Output Summary for Load Case No. 2:

Pile-head deflection = 0.1000000 inchesComputed slope at pile head = -0.0009880 radiansMaximum bending moment = 454601. inch-lbsMaximum shear force = 11211. lbsDepth of maximum bending moment = 87.0000000 inches below pile headDepth of maximum shear force = 0.000000 inches below pile headNumber of iterations = 6Number of zero deflection points = 2

-------------------------------------------------------------------------------- Computed Values of Pile Loading and Deflection for Lateral Loading for Load Case Number 3--------------------------------------------------------------------------------

Pile-head conditions are Displacement and Moment (Loading Type 4)Displacement of pile head = 0.200000 inchesMoment at pile head = 0.000 in-lbsAxial load at pile head = 10000.000 lbs

Depth Deflect. Bending Shear Slope Total Bending Soil Res. Soil Spr. Distrib. X y Moment Force S Stress Stiffness p Es*h Lat. Load feet inches in-lbs lbs radians psi* lb-in^2 lb/in lb/inch lb/inch ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- 0.00 0.2000 0.000 19313. -0.002169 0.000 6.862E+10-278.0309 2418.8688 0.000 0.290 0.1925 65601. 18339. -0.002168 0.000 6.862E+10-281.6419 5092.8184 0.000 0.580 0.1849 127790. 17355. -0.002163 0.000 6.852E+10-284.1639 5347.8991 0.000 0.870 0.1774 186539. 16363. -0.002155 0.000 6.842E+10-285.6171 5602.9798 0.000 1.160 0.1699 241827. 15368. -0.002144 0.000 6.831E+10-286.0241 5858.0605 0.000 1.450 0.1625 293652. 14374. -0.002130 0.000 6.820E+10-285.4096 6113.1412 0.000 1.740 0.1551 342020. 13384. -0.002114 0.000 6.811E+10-283.7997 6368.2219 0.000 2.030 0.1478 386950. 12401. -0.002096 0.000 6.800E+10-281.2227 6623.3027 0.000 2.320 0.1405 428474. 11428. -0.002075 0.000 6.792E+10-277.7077 6878.3834 0.000 2.610 0.1333 466633. 10469. -0.002052 0.000 6.783E+10-273.2853 7133.4641 0.000 2.900 0.1262 501483. 9527.4929 -0.002027 0.000 6.776E+10-267.9871 7388.5448 0.000 3.190 0.1192 533086. 8605.5850 -0.002000 0.000 6.769E+10-261.8451 7643.6255 0.000 3.480 0.1123 561517. 7706.4622 -0.001972 0.000 6.763E+10-254.8921 7898.7062 0.000 3.770 0.1055 586860. 6832.8892 -0.001943 0.000 6.758E+10-247.1613 8153.7869 0.000 4.060 0.0988 609209. 5987.5150 -0.001912 0.000 6.752E+10-238.6859 8408.8677 0.000 4.350 0.0922 628666. 5172.8728 -0.001880 0.000 6.748E+10

Page 20

existing phase2 87.lp6o-229.4993 8663.9484 0.000 4.640 0.0857 645343. 4391.3801 -0.001847 0.000 6.744E+10-219.6345 8919.0291 0.000 4.930 0.0793 659359. 3645.3396 -0.001811 0.000 5.820E+10-209.1244 9174.1098 0.000 5.220 0.0731 670841. 2936.8519 -0.001761 0.000 3.922E+10-198.0524 9429.1905 0.000 5.510 0.0671 679922. 2267.4816 -0.001690 0.000 2.876E+10-186.6432 9684.2712 0.000 5.800 0.0613 686740. 1637.9294 -0.001598 0.000 2.343E+10-175.1684 9939.3519 0.000 6.090 0.0559 691433. 1047.9640 -0.001496 0.000 2.342E+10-163.8922 10194. 0.000 6.380 0.0509 694138. 496.7448 -0.001393 0.000 2.341E+10-152.9005 10450. 0.000 6.670 0.0463 694987. -16.8632 -0.001289 0.000 2.341E+10-142.2766 10705. 0.000 6.960 0.0419 694110. -494.2800 -0.001186 0.000 2.341E+10-132.1009 10960. 0.000 7.250 0.0380 691630. -937.2006 -0.001083 0.000 2.342E+10-122.4511 11215. 0.000 7.540 0.0344 687663. -1347.5841 -0.000981 0.000 2.343E+10-113.4015 11470. 0.000 7.830 0.0312 682319. -1727.6429 -0.000881 0.000 2.446E+10-105.0231 11725. 0.000 8.120 0.0283 675700. -2079.7430 -0.000794 0.000 3.014E+10-97.3333 11980. 0.000 8.410 0.0256 667899. -2406.0041 -0.000725 0.000 3.873E+10-90.1731 12235. 0.000 8.700 0.0232 659004. -2707.9824 -0.000672 0.000 5.179E+10-83.3777 12490. 0.000 8.990 0.0210 649098. -2986.6779 -0.000634 0.000 6.743E+10-76.7922 12745. 0.000 9.280 0.0188 638261. -3242.6364 -0.000600 0.000 6.746E+10-70.3104 13000. 0.000 9.570 0.0168 626571. -3476.2502 -0.000568 0.000 6.748E+10-63.9504 13255. 0.000 9.860 0.0149 614106. -3687.9725 -0.000536 0.000 6.751E+10-57.7291 13510. 0.000 10.150 0.0131 600940. -3949.7893 -0.000504 0.000 6.754E+10-92.7404 24711. 0.000 10.440 0.0114 586650. -4254.0886 -0.000474 0.000 6.758E+10-82.1443 25166. 0.000 10.730 0.009762 571365. -4522.0857 -0.000444 0.000 6.761E+10-71.8770 25622. 0.000 11.020 0.008268 555208. -4754.9600 -0.000415 0.000 6.764E+10-61.9588 26077. 0.000 11.310 0.006874 538299. -4953.9574 -0.000387 0.000 6.768E+10-52.4075 26533. 0.000 11.600 0.005575 520755. -5120.3809 -0.000360 0.000 6.772E+10-43.2382 26988. 0.000 11.890 0.004370 502686. -5255.5819 -0.000333 0.000 6.776E+10-34.4635 27443. 0.000 12.180 0.003255 484199. -5360.9514 -0.000308 0.000 6.779E+10-26.0937 27899. 0.000 12.470 0.002226 465396. -5437.9121 -0.000284 0.000 6.783E+10-18.1366 28354. 0.000 12.760 0.001280 446371. -5487.9107 -0.000260 0.000 6.788E+10-10.5982 28810. 0.000 13.050 0.000414 427218. -5512.4101 -0.000238 0.000 6.792E+10-3.4819 29265. 0.000 13.340 -0.000376 408021. -5512.8825 -0.000217 0.000 6.796E+103.2105 29720. 0.000

Page 21

existing phase2 87.lp6o 13.630 -0.001093 388863. -5490.8025 -0.000196 0.000 6.800E+109.4792 30176. 0.000 13.920 -0.001741 369819. -5447.6417 -0.000177 0.000 6.804E+1015.3260 30631. 0.000 14.210 -0.002323 350960. -5384.8619 -0.000158 0.000 6.808E+1020.7543 31087. 0.000 14.500 -0.002843 332351. -5303.9109 -0.000141 0.000 6.812E+1025.7693 31542. 0.000 14.790 -0.003304 314054. -5206.2164 -0.000124 0.000 6.816E+1030.3770 31997. 0.000 15.080 -0.003709 296125. -5100.6233 -0.000109 0.000 6.819E+1030.3087 28440. 0.000 15.370 -0.004061 278562. -4989.3723 -9.412E-05 0.000 6.823E+1033.6286 28818. 0.000 15.660 -0.004364 261405. -4867.1570 -8.036E-05 0.000 6.827E+1036.6101 29196. 0.000 15.950 -0.004620 244692. -4735.1372 -6.746E-05 0.000 6.830E+1039.2633 29574. 0.000 16.240 -0.004833 228454. -4594.4369 -5.541E-05 0.000 6.833E+1041.5989 29952. 0.000 16.530 -0.005006 212718. -4446.1425 -4.418E-05 0.000 6.836E+1043.6278 30329. 0.000 16.820 -0.005141 197511. -4291.3008 -3.374E-05 0.000 6.839E+1045.3617 30707. 0.000 17.110 -0.005241 182853. -4130.9178 -2.407E-05 0.000 6.843E+1046.8125 31085. 0.000 17.400 -0.005308 168762. -3965.9574 -1.513E-05 0.000 6.846E+1047.9923 31463. 0.000 17.690 -0.005346 155251. -3797.3408 -6.893E-06 0.000 6.848E+1048.9138 31841. 0.000 17.980 -0.005356 142333. -3625.9457 6.675E-07 0.000 6.849E+1049.5892 32219. 0.000 18.270 -0.005341 130015. -3452.6064 7.585E-06 0.000 6.851E+1050.0311 32597. 0.000 18.560 -0.005303 118302. -3278.1137 1.389E-05 0.000 6.853E+1050.2520 32974. 0.000 18.850 -0.005245 107198. -3103.2152 1.962E-05 0.000 6.856E+1050.2644 33352. 0.000 19.140 -0.005167 96702. -2928.6152 2.479E-05 0.000 6.858E+1050.0804 33730. 0.000 19.430 -0.005072 86813. -2754.9761 2.944E-05 0.000 6.862E+1049.7122 34108. 0.000 19.720 -0.004962 77526. -2582.9183 3.361E-05 0.000 6.862E+1049.1716 34486. 0.000 20.010 -0.004838 68834. -2413.0221 3.732E-05 0.000 6.862E+1048.4699 34864. 0.000 20.300 -0.004702 60729. -2245.8283 4.061E-05 0.000 6.862E+1047.6184 35241. 0.000 20.590 -0.004556 53200. -2081.8402 4.350E-05 0.000 6.862E+1046.6277 35619. 0.000 20.880 -0.004399 46236. -1921.5242 4.602E-05 0.000 6.862E+1045.5079 35997. 0.000 21.170 -0.004235 39823. -1765.3123 4.820E-05 0.000 6.862E+1044.2690 36375. 0.000 21.460 -0.004064 33946. -1613.6029 5.007E-05 0.000 6.862E+1042.9202 36753. 0.000 21.750 -0.003887 28589. -1466.7634 5.166E-05 0.000 6.862E+1041.4703 37131. 0.000 22.040 -0.003704 23734. -1325.1310 5.298E-05 0.000 6.862E+1039.9276 37508. 0.000 22.330 -0.003518 19362. -1189.0158 5.408E-05 0.000 6.862E+1038.2996 37886. 0.000 22.620 -0.003328 15454. -1058.7017 5.496E-05 0.000 6.862E+10

Page 22

existing phase2 87.lp6o36.5936 38264. 0.000 22.910 -0.003135 11990. -934.4491 5.566E-05 0.000 6.862E+1034.8160 38642. 0.000 23.200 -0.002941 8946.7968 -816.4964 5.619E-05 0.000 6.862E+1032.9729 39020. 0.000 23.490 -0.002744 6303.0838 -705.0624 5.657E-05 0.000 6.862E+1031.0696 39398. 0.000 23.780 -0.002547 4035.6253 -600.3480 5.684E-05 0.000 6.862E+1029.1110 39775. 0.000 24.070 -0.002349 2120.7059 -502.5385 5.699E-05 0.000 6.862E+1027.1013 40153. 0.000 24.360 -0.002150 533.9905 -411.8053 5.706E-05 0.000 6.862E+1025.0442 40531. 0.000 24.650 -0.001952 -749.4302 -328.3076 5.705E-05 0.000 6.862E+1022.9429 40909. 0.000 24.940 -0.001753 -1755.0016 -252.1948 5.699E-05 0.000 6.862E+1020.8001 41287. 0.000 25.230 -0.001555 -2508.6727 -177.2777 5.688E-05 0.000 6.862E+1022.2558 49806. 0.000 25.520 -0.001357 -2992.8131 -104.4425 5.674E-05 0.000 6.862E+1019.6035 50261. 0.000 25.810 -0.001160 -3239.5416 -40.9138 5.658E-05 0.000 6.862E+1016.9072 50717. 0.000 26.100 -0.000963 -3281.5114 13.1565 5.642E-05 0.000 6.862E+1014.1677 51172. 0.000 26.390 -0.000767 -3151.8990 57.6187 5.626E-05 0.000 6.862E+1011.3853 51628. 0.000 26.680 -0.000572 -2884.4004 92.3234 5.610E-05 0.000 6.862E+108.5599 52083. 0.000 26.970 -0.000377 -2513.2326 117.1202 5.597E-05 0.000 6.862E+105.6911 52538. 0.000 27.260 -0.000182 -2073.1391 131.8563 5.585E-05 0.000 6.862E+102.7779 52994. 0.000 27.550 1.175E-05 -1599.4000 136.3759 5.576E-05 0.000 6.862E+10-0.1805 53449. 0.000 27.840 0.000206 -1127.8437 130.5193 5.569E-05 0.000 6.862E+10-3.1854 53905. 0.000 28.130 0.000399 -694.8613 114.1229 5.564E-05 0.000 6.862E+10-6.2379 54360. 0.000 28.420 0.000593 -337.4207 87.0189 5.561E-05 0.000 6.862E+10-9.3391 54815. 0.000 28.710 0.000786 -93.0802 49.0360 5.560E-05 0.000 6.862E+10-12.4901 55271. 0.000 29.000 0.000980 0.000 0.000 5.560E-05 0.000 6.862E+10-15.6915 27863. 0.000

* This analysis makes computations of pile response using nonlinear moment-curvaturerelationships. The above values of total stress are computed for combined axial and bending stress in elastic sections and do not equal actual stresses in concrete and steel in the range of nonlinear bending.

Output Summary for Load Case No. 3:

Pile-head deflection = 0.2000000 inchesComputed slope at pile head = -0.0021695 radiansMaximum bending moment = 694987. inch-lbsMaximum shear force = 19313. lbsDepth of maximum bending moment = 80.0400000 inches below pile headDepth of maximum shear force = 0.000000 inches below pile headNumber of iterations = 23

Page 23

existing phase2 87.lp6oNumber of zero deflection points = 2

-------------------------------------------------------------------------------- Computed Values of Pile Loading and Deflection for Lateral Loading for Load Case Number 4--------------------------------------------------------------------------------

Pile-head conditions are Displacement and Moment (Loading Type 4)Displacement of pile head = 0.300000 inchesMoment at pile head = 0.000 in-lbsAxial load at pile head = 10000.000 lbs

Depth Deflect. Bending Shear Slope Total Bending Soil Res. Soil Spr. Distrib. X y Moment Force S Stress Stiffness p Es*h Lat. Load feet inches in-lbs lbs radians psi* lb-in^2 lb/in lb/inch lb/inch ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- 0.00 0.3000 0.000 25723. -0.003553 0.000 6.862E+10-417.0464 2418.8688 0.000 0.290 0.2876 87113. 24265. -0.003551 0.000 6.862E+10-420.9414 5092.8184 0.000 0.580 0.2753 169129. 22796. -0.003544 0.000 6.846E+10-423.0474 5347.8991 0.000 0.870 0.2630 246020. 21323. -0.003534 0.000 6.830E+10-423.3913 5602.9798 0.000 1.160 0.2507 317784. 19852. -0.003519 0.000 6.815E+10-422.0026 5858.0605 0.000 1.450 0.2385 384437. 18389. -0.003501 0.000 6.801E+10-418.9136 6113.1412 0.000 1.740 0.2263 446016. 16940. -0.003480 0.000 6.788E+10-414.1585 6368.2219 0.000 2.030 0.2143 502578. 15509. -0.003456 0.000 6.776E+10-407.7737 6623.3027 0.000 2.320 0.2023 554201. 14104. -0.003429 0.000 6.764E+10-399.7968 6878.3834 0.000 2.610 0.1904 600982. 12729. -0.003399 0.000 6.754E+10-390.2670 7133.4641 0.000 2.900 0.1786 643035. 11391. -0.003367 0.000 6.745E+10-379.2240 7388.5448 0.000 3.190 0.1670 680494. 10093. -0.003300 0.000 2.345E+10-366.7085 7643.6255 0.000 3.480 0.1556 713509. 8839.8377 -0.003196 0.000 2.335E+10-353.2817 7898.7062 0.000 3.770 0.1447 742242. 7635.1561 -0.003087 0.000 2.328E+10-339.0641 8153.7869 0.000 4.060 0.1342 766865. 6481.1182 -0.002974 0.000 2.322E+10-324.1761 8408.8677 0.000 4.350 0.1240 787557. 5379.8492 -0.002858 0.000 2.317E+10-308.7371 8663.9484 0.000 4.640 0.1143 804507. 4333.0616 -0.002738 0.000 2.313E+10-292.8649 8919.0291 0.000 4.930 0.1050 817906. 3342.0618 -0.002616 0.000 2.310E+10-276.6752 9174.1098 0.000 5.220 0.0961 827950. 2407.7581 -0.002492 0.000 2.308E+10-260.2810 9429.1905 0.000 5.510 0.0876 834838. 1530.6706 -0.002367 0.000 2.307E+10-243.7923 9684.2712 0.000 5.800 0.0796 838768. 710.9425 -0.002240 0.000 2.306E+10

Page 24

existing phase2 87.lp6o-227.3158 9939.3519 0.000 6.090 0.0720 839942. -51.6475 -0.002114 0.000 2.306E+10-210.9543 10194. 0.000 6.380 0.0649 838556. -757.6718 -0.001987 0.000 2.306E+10-194.8068 10450. 0.000 6.670 0.0582 834807. -1408.0393 -0.001861 0.000 2.307E+10-178.9676 10705. 0.000 6.960 0.0519 828886. -2003.9802 -0.001735 0.000 2.308E+10-163.5272 10960. 0.000 7.250 0.0461 820980. -2547.0309 -0.001611 0.000 2.310E+10-148.5709 11215. 0.000 7.540 0.0407 811270. -3039.0174 -0.001488 0.000 2.312E+10-134.1799 11470. 0.000 7.830 0.0357 799932. -3482.0391 -0.001367 0.000 2.314E+10-120.4303 11725. 0.000 8.120 0.0312 787130. -3878.4525 -0.001248 0.000 2.317E+10-107.3935 11980. 0.000 8.410 0.0271 773025. -4230.8542 -0.001131 0.000 2.321E+10-95.1362 12235. 0.000 8.700 0.0233 757762. -4542.0650 -0.001016 0.000 2.324E+10-83.7205 12490. 0.000 8.990 0.0200 741483. -4815.1130 -0.000904 0.000 2.328E+10-73.2036 12745. 0.000 9.280 0.0170 724312. -5053.2177 -0.000794 0.000 2.333E+10-63.6381 13000. 0.000 9.570 0.0145 706367. -5259.7736 -0.000688 0.000 2.337E+10-55.0722 13255. 0.000 9.860 0.0122 687752. -5438.3349 -0.000584 0.000 2.343E+10-47.5493 13510. 0.000 10.150 0.0104 668557. -5649.4751 -0.000511 0.000 5.380E+10-73.7957 24711. 0.000 10.440 0.008688 648467. -5887.2004 -0.000473 0.000 6.744E+10-62.8281 25166. 0.000 10.730 0.007100 627615. -6087.4741 -0.000440 0.000 6.748E+10-52.2717 25622. 0.000 11.020 0.005624 606129. -6251.7570 -0.000408 0.000 6.753E+10-42.1437 26077. 0.000 11.310 0.004257 584131. -6381.5646 -0.000378 0.000 6.758E+10-32.4583 26533. 0.000 11.600 0.002995 561740. -6478.4569 -0.000348 0.000 6.763E+10-23.2269 26988. 0.000 11.890 0.001833 539066. -6544.0296 -0.000320 0.000 6.767E+10-14.4585 27443. 0.000 12.180 0.000768 516216. -6579.9047 -0.000293 0.000 6.773E+10-6.1594 27899. 0.000 12.470 -0.000205 493290. -6587.7225 -0.000267 0.000 6.778E+101.6664 28354. 0.000 12.760 -0.001089 470384. -6569.1331 -0.000242 0.000 6.782E+109.0171 28810. 0.000 13.050 -0.001890 447586. -6525.7894 -0.000219 0.000 6.787E+1015.8931 29265. 0.000 13.340 -0.002611 424979. -6459.3396 -0.000196 0.000 6.793E+1022.2965 29720. 0.000 13.630 -0.003256 402642. -6371.4205 -0.000175 0.000 6.797E+1028.2317 30176. 0.000 13.920 -0.003829 380646. -6263.6522 -0.000155 0.000 6.801E+1033.7042 30631. 0.000 14.210 -0.004335 359058. -6137.6320 -0.000136 0.000 6.806E+1038.7213 31087. 0.000 14.500 -0.004776 337938. -5994.9295 -0.000118 0.000 6.811E+1043.2916 31542. 0.000 14.790 -0.005158 317342. -5837.0823 -0.000102 0.000 6.815E+1047.4252 31997. 0.000

Page 25

existing phase2 87.lp6o 15.080 -0.005483 297319. -5676.5922 -8.586E-05 0.000 6.819E+1044.8105 28440. 0.000 15.370 -0.005755 277838. -5515.6909 -7.119E-05 0.000 6.823E+1047.6615 28818. 0.000 15.660 -0.005979 258935. -5345.4853 -5.750E-05 0.000 6.828E+1050.1578 29196. 0.000 15.950 -0.006156 240638. -5167.1873 -4.477E-05 0.000 6.831E+1052.3123 29574. 0.000 16.240 -0.006290 222974. -4981.9636 -3.297E-05 0.000 6.834E+1054.1381 29952. 0.000 16.530 -0.006385 205966. -4790.9345 -2.205E-05 0.000 6.837E+1055.6487 30329. 0.000 16.820 -0.006444 189631. -4595.1726 -1.198E-05 0.000 6.841E+1056.8581 30707. 0.000 17.110 -0.006469 173984. -4395.7018 -2.738E-06 0.000 6.845E+1057.7803 31085. 0.000 17.400 -0.006463 159037. -4193.4967 5.726E-06 0.000 6.847E+1058.4296 31463. 0.000 17.690 -0.006429 144797. -3989.4819 1.345E-05 0.000 6.849E+1058.8203 31841. 0.000 17.980 -0.006369 131269. -3784.5328 2.046E-05 0.000 6.851E+1058.9665 32219. 0.000 18.270 -0.006286 118455. -3579.4755 2.680E-05 0.000 6.853E+1058.8825 32597. 0.000 18.560 -0.006183 106354. -3375.0869 3.251E-05 0.000 6.856E+1058.5822 32974. 0.000 18.850 -0.006060 94962. -3172.0960 3.761E-05 0.000 6.859E+1058.0793 33352. 0.000 19.140 -0.005921 84274. -2971.1843 4.216E-05 0.000 6.862E+1057.3872 33730. 0.000 19.430 -0.005767 74280. -2772.9872 4.618E-05 0.000 6.862E+1056.5192 34108. 0.000 19.720 -0.005599 64971. -2578.0952 4.971E-05 0.000 6.862E+1055.4877 34486. 0.000 20.010 -0.005421 56333. -2387.0557 5.279E-05 0.000 6.862E+1054.3051 34864. 0.000 20.300 -0.005232 48353. -2200.3745 5.544E-05 0.000 6.862E+1052.9829 35241. 0.000 20.590 -0.005035 41014. -2018.5177 5.771E-05 0.000 6.862E+1051.5325 35619. 0.000 20.880 -0.004830 34300. -1841.9131 5.962E-05 0.000 6.862E+1049.9644 35997. 0.000 21.170 -0.004620 28191. -1670.9531 6.120E-05 0.000 6.862E+1048.2885 36375. 0.000 21.460 -0.004404 22666. -1505.9959 6.249E-05 0.000 6.862E+1046.5145 36753. 0.000 21.750 -0.004185 17705. -1347.3682 6.352E-05 0.000 6.862E+1044.6509 37131. 0.000 22.040 -0.003962 13284. -1195.3671 6.430E-05 0.000 6.862E+1042.7060 37508. 0.000 22.330 -0.003737 9380.2967 -1050.2627 6.488E-05 0.000 6.862E+1040.6873 37886. 0.000 22.620 -0.003511 5969.4864 -912.3001 6.527E-05 0.000 6.862E+1038.6015 38264. 0.000 22.910 -0.003283 3026.1452 -781.7021 6.549E-05 0.000 6.862E+1036.4548 38642. 0.000 23.200 -0.003055 524.2810 -658.6711 6.558E-05 0.000 6.862E+1034.2527 39020. 0.000 23.490 -0.002827 -1562.7702 -543.3914 6.556E-05 0.000 6.862E+1032.0000 39398. 0.000 23.780 -0.002599 -3262.2860 -436.0320 6.544E-05 0.000 6.862E+1029.7009 39775. 0.000 24.070 -0.002371 -4602.1070 -336.7481 6.524E-05 0.000 6.862E+10

Page 26

existing phase2 87.lp6o27.3589 40153. 0.000 24.360 -0.002145 -5610.5931 -245.6838 6.498E-05 0.000 6.862E+1024.9769 40531. 0.000 24.650 -0.001919 -6316.5887 -162.9740 6.467E-05 0.000 6.862E+1022.5574 40909. 0.000 24.940 -0.001694 -6749.3936 -88.7463 6.434E-05 0.000 6.862E+1020.1022 41287. 0.000 25.230 -0.001471 -6938.7412 -17.1347 6.400E-05 0.000 6.862E+1021.0539 49806. 0.000 25.520 -0.001249 -6873.1050 50.8866 6.365E-05 0.000 6.862E+1018.0387 50261. 0.000 25.810 -0.001028 -6589.0002 108.3446 6.330E-05 0.000 6.862E+1014.9831 50717. 0.000 26.100 -0.000808 -6123.4325 155.0981 6.298E-05 0.000 6.862E+1011.8867 51172. 0.000 26.390 -0.000590 -5513.9009 191.0041 6.269E-05 0.000 6.862E+108.7489 51628. 0.000 26.680 -0.000372 -4798.4067 215.9163 6.243E-05 0.000 6.862E+105.5684 52083. 0.000 26.970 -0.000155 -4015.4684 229.6834 6.220E-05 0.000 6.862E+102.3437 52538. 0.000 27.260 6.087E-05 -3204.1393 232.1488 6.202E-05 0.000 6.862E+10-0.9269 52994. 0.000 27.550 0.000276 -2404.0295 223.1490 6.188E-05 0.000 6.862E+10-4.2454 53449. 0.000 27.840 0.000492 -1655.3288 202.5141 6.177E-05 0.000 6.862E+10-7.6137 53905. 0.000 28.130 0.000706 -998.8305 170.0674 6.171E-05 0.000 6.862E+10-11.0338 54360. 0.000 28.420 0.000921 -475.9545 125.6258 6.167E-05 0.000 6.862E+10-14.5074 54815. 0.000 28.710 0.001136 -128.7674 69.0008 6.165E-05 0.000 6.862E+10-18.0357 55271. 0.000 29.000 0.001350 0.000 0.000 6.165E-05 0.000 6.862E+10-21.6199 27863. 0.000

* This analysis makes computations of pile response using nonlinear moment-curvaturerelationships. The above values of total stress are computed for combined axial and bending stress in elastic sections and do not equal actual stresses in concrete and steel in the range of nonlinear bending.

Output Summary for Load Case No. 4:

Pile-head deflection = 0.3000000 inchesComputed slope at pile head = -0.0035530 radiansMaximum bending moment = 839942. inch-lbsMaximum shear force = 25723. lbsDepth of maximum bending moment = 73.0800000 inches below pile headDepth of maximum shear force = 0.000000 inches below pile headNumber of iterations = 54Number of zero deflection points = 2

-------------------------------------------------------------------------------- Computed Values of Pile Loading and Deflection for Lateral Loading for Load Case Number 5--------------------------------------------------------------------------------

Pile-head conditions are Displacement and Moment (Loading Type 4)Page 27

existing phase2 87.lp6oDisplacement of pile head = 0.500000 inchesMoment at pile head = 0.000 in-lbsAxial load at pile head = 10000.000 lbs

Depth Deflect. Bending Shear Slope Total Bending Soil Res. Soil Spr. Distrib. X y Moment Force S Stress Stiffness p Es*h Lat. Load feet inches in-lbs lbs radians psi* lb-in^2 lb/in lb/inch lb/inch ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- 0.00 0.5000 0.000 40479. -0.006175 0.000 6.862E+10-668.4651 2326.2585 0.000 0.290 0.4785 137035. 38138. -0.006171 0.000 6.862E+10-676.8395 4922.3546 0.000 0.580 0.4570 265872. 35770. -0.006161 0.000 6.826E+10-684.1516 5209.2020 0.000 0.870 0.4356 386424. 33364. -0.006145 0.000 6.800E+10-698.9015 5583.1393 0.000 1.160 0.4143 498511. 30934. -0.006122 0.000 6.777E+10-697.3790 5858.0605 0.000 1.450 0.3930 602152. 28519. -0.006094 0.000 6.754E+10-690.3997 6113.1412 0.000 1.740 0.3719 697431. 26134. -0.006026 0.000 2.340E+10-680.5014 6368.2219 0.000 2.030 0.3511 784464. 23787. -0.005915 0.000 2.318E+10-668.1893 6623.3027 0.000 2.320 0.3307 863402. 21487. -0.005791 0.000 2.301E+10-653.6394 6878.3834 0.000 2.610 0.3108 934420. 19242. -0.005655 0.000 2.288E+10-637.0332 7133.4641 0.000 2.900 0.2913 997717. 17057. -0.005508 0.000 2.278E+10-618.5558 7388.5448 0.000 3.190 0.2724 1053519. 14939. -0.005351 0.000 2.269E+10-598.3948 7643.6255 0.000 3.480 0.2541 1102068. 12895. -0.005185 0.000 2.262E+10-576.7391 7898.7062 0.000 3.770 0.2363 1143626. 10928. -0.005012 0.000 2.257E+10-553.7771 8153.7869 0.000 4.060 0.2192 1178472. 9042.2920 -0.004833 0.000 2.252E+10-529.6960 8408.8677 0.000 4.350 0.2027 1206897. 7242.4770 -0.004649 0.000 2.249E+10-504.6804 8663.9484 0.000 4.640 0.1869 1229203. 5531.0273 -0.004460 0.000 2.246E+10-478.9114 8919.0291 0.000 4.930 0.1717 1245703. 3910.2572 -0.004268 0.000 2.244E+10-452.5657 9174.1098 0.000 5.220 0.1572 1256716. 2381.8752 -0.004074 0.000 2.243E+10-425.8148 9429.1905 0.000 5.510 0.1433 1262565. 947.0038 -0.003879 0.000 2.242E+10-398.8240 9684.2712 0.000 5.800 0.1302 1263577. -393.7989 -0.003683 0.000 2.242E+10-371.7523 9939.3519 0.000 6.090 0.1177 1260080. -1640.5149 -0.003487 0.000 2.242E+10-344.7512 10194. 0.000 6.380 0.1059 1252401. -2793.6408 -0.003292 0.000 2.243E+10-317.9648 10450. 0.000 6.670 0.0948 1240865. -3854.1605 -0.003098 0.000 2.245E+10-291.5293 10705. 0.000 6.960 0.0843 1225792. -4823.5172 -0.002907 0.000 2.247E+10-265.5723 10960. 0.000 7.250 0.0745 1207496. -5703.5837 -0.002719 0.000 2.249E+10

Page 28

existing phase2 87.lp6o-240.2131 11215. 0.000 7.540 0.0654 1186284. -6496.6332 -0.002534 0.000 2.251E+10-215.5625 11470. 0.000 7.830 0.0569 1162456. -7205.3088 -0.002352 0.000 2.254E+10-191.7224 11725. 0.000 8.120 0.0490 1136299. -7832.5935 -0.002175 0.000 2.258E+10-168.7861 11980. 0.000 8.410 0.0418 1108092. -8381.7801 -0.002002 0.000 2.262E+10-146.8384 12235. 0.000 8.700 0.0351 1078101. -8856.4411 -0.001834 0.000 2.266E+10-125.9553 12490. 0.000 8.990 0.0290 1046579. -9260.3994 -0.001671 0.000 2.270E+10-106.2047 12745. 0.000 9.280 0.0235 1013765. -9597.6996 -0.001514 0.000 2.275E+10-87.6460 13000. 0.000 9.570 0.0185 979885. -9872.5798 -0.001361 0.000 2.281E+10-70.3311 13255. 0.000 9.860 0.0140 945147. -10089. -0.001215 0.000 2.286E+10-54.3037 13510. 0.000 10.150 0.0100 909747. -10308. -0.001074 0.000 2.293E+10-71.0877 24711. 0.000 10.440 0.006515 873481. -10513. -0.000938 0.000 2.299E+10-47.1179 25166. 0.000 10.730 0.003480 836639. -10640. -0.000809 0.000 2.307E+10-25.6204 25622. 0.000 11.020 0.000883 799483. -10696. -0.000686 0.000 2.314E+10-6.6200 26077. 0.000 11.310 -0.001295 762243. -10690. -0.000569 0.000 2.323E+109.8704 26533. 0.000 11.600 -0.003075 725118. -10632. -0.000458 0.000 2.332E+1023.8493 26988. 0.000 11.890 -0.004479 688279. -10529. -0.000352 0.000 2.342E+1035.3251 27443. 0.000 12.180 -0.005528 651863. -10390. -0.000284 0.000 6.742E+1044.3157 27899. 0.000 12.470 -0.006459 615984. -10221. -0.000252 0.000 6.751E+1052.6267 28354. 0.000 12.760 -0.007280 580740. -10025. -0.000221 0.000 6.759E+1060.2666 28810. 0.000 13.050 -0.007996 546225. -9803.1128 -0.000192 0.000 6.766E+1067.2463 29265. 0.000 13.340 -0.008615 512524. -9558.0778 -0.000165 0.000 6.774E+1073.5785 29720. 0.000 13.630 -0.009143 479712. -9292.1073 -0.000139 0.000 6.780E+1079.2781 30176. 0.000 13.920 -0.009584 447860. -9007.3742 -0.000115 0.000 6.787E+1084.3616 30631. 0.000 14.210 -0.009946 417029. -8705.9915 -9.326E-05 0.000 6.794E+1088.8468 31087. 0.000 14.500 -0.0102 387273. -8390.0078 -7.267E-05 0.000 6.800E+1092.7530 31542. 0.000 14.790 -0.0105 358640. -8061.4034 -5.359E-05 0.000 6.806E+1096.1002 31997. 0.000 15.080 -0.0106 331169. -7743.3656 -3.596E-05 0.000 6.813E+1086.6801 28440. 0.000 15.370 -0.0107 304748. -7438.3359 -1.972E-05 0.000 6.817E+1088.6243 28818. 0.000 15.660 -0.0107 279400. -7127.2947 -4.821E-06 0.000 6.823E+1090.1350 29196. 0.000 15.950 -0.0107 255143. -6811.7138 8.805E-06 0.000 6.829E+1091.2333 29574. 0.000 16.240 -0.0107 231990. -6492.9913 2.121E-05 0.000 6.832E+1091.9405 29952. 0.000

Page 29

existing phase2 87.lp6o 16.530 -0.0106 209950. -6172.4517 3.247E-05 0.000 6.837E+1092.2777 30329. 0.000 16.820 -0.0105 189027. -5851.3452 4.262E-05 0.000 6.841E+1092.2662 30707. 0.000 17.110 -0.0103 169222. -5530.8485 5.173E-05 0.000 6.846E+1091.9273 31085. 0.000 17.400 -0.0101 150529. -5212.0644 5.985E-05 0.000 6.848E+1091.2819 31463. 0.000 17.690 -0.009875 132941. -4896.0238 6.705E-05 0.000 6.851E+1090.3506 31841. 0.000 17.980 -0.009630 116448. -4583.6864 7.338E-05 0.000 6.854E+1089.1536 32219. 0.000 18.270 -0.009364 101034. -4275.9424 7.891E-05 0.000 6.857E+1087.7107 32597. 0.000 18.560 -0.009080 86682. -3973.6144 8.367E-05 0.000 6.862E+1086.0410 32974. 0.000 18.850 -0.008782 73372. -3677.4592 8.773E-05 0.000 6.862E+1084.1631 33352. 0.000 19.140 -0.008470 61081. -3388.1704 9.113E-05 0.000 6.862E+1082.0948 33730. 0.000 19.430 -0.008147 49784. -3106.3808 9.395E-05 0.000 6.862E+1079.8532 34108. 0.000 19.720 -0.007816 39454. -2832.6655 9.621E-05 0.000 6.862E+1077.4544 34486. 0.000 20.010 -0.007478 30062. -2567.5444 9.797E-05 0.000 6.862E+1074.9140 34864. 0.000 20.300 -0.007134 21577. -2311.4854 9.928E-05 0.000 6.862E+1072.2464 35241. 0.000 20.590 -0.006787 13967. -2064.9074 0.000100 0.000 6.862E+1069.4651 35619. 0.000 20.880 -0.006437 7198.0377 -1828.1837 0.000101 0.000 6.862E+1066.5830 35997. 0.000 21.170 -0.006086 1235.6202 -1601.6452 0.000101 0.000 6.862E+1063.6116 36375. 0.000 21.460 -0.005734 -3956.4380 -1385.5839 0.000101 0.000 6.862E+1060.5616 36753. 0.000 21.750 -0.005384 -8415.0640 -1180.2563 0.000101 0.000 6.862E+1057.4428 37131. 0.000 22.040 -0.005035 -12178. -985.8868 0.000100 0.000 6.862E+1054.2638 37508. 0.000 22.330 -0.004688 -15284. -802.6712 9.933E-05 0.000 6.862E+1051.0325 37886. 0.000 22.620 -0.004343 -17772. -630.7803 9.849E-05 0.000 6.862E+1047.7554 38264. 0.000 22.910 -0.004002 -19681. -470.3630 9.754E-05 0.000 6.862E+1044.4384 38642. 0.000 23.200 -0.003664 -21052. -321.5501 9.651E-05 0.000 6.862E+1041.0863 39020. 0.000 23.490 -0.003330 -21926. -184.4571 9.542E-05 0.000 6.862E+1037.7028 39398. 0.000 23.780 -0.003000 -22343. -59.1877 9.430E-05 0.000 6.862E+1034.2911 39775. 0.000 24.070 -0.002674 -22344. 54.1635 9.317E-05 0.000 6.862E+1030.8532 40153. 0.000 24.360 -0.002352 -21972. 155.5074 9.204E-05 0.000 6.862E+1027.3904 40531. 0.000 24.650 -0.002033 -21268. 244.7582 9.095E-05 0.000 6.862E+1023.9032 40909. 0.000 24.940 -0.001719 -20275. 321.8309 8.989E-05 0.000 6.862E+1020.3914 41287. 0.000 25.230 -0.001408 -19034. 392.3686 8.890E-05 0.000 6.862E+1020.1475 49806. 0.000 25.520 -0.001100 -17550. 455.0702 8.797E-05 0.000 6.862E+10

Page 30

existing phase2 87.lp6o15.8880 50261. 0.000 25.810 -0.000795 -15873. 502.8873 8.712E-05 0.000 6.862E+1011.5931 50717. 0.000 26.100 -0.000494 -14056. 535.6911 8.636E-05 0.000 6.862E+107.2597 51172. 0.000 26.390 -0.000194 -12151. 553.3412 8.570E-05 0.000 6.862E+102.8841 51628. 0.000 26.680 0.000103 -10211. 555.6838 8.513E-05 0.000 6.862E+10-1.5378 52083. 0.000 26.970 0.000398 -8289.2880 542.5504 8.466E-05 0.000 6.862E+10-6.0102 52538. 0.000 27.260 0.000692 -6440.5440 513.7574 8.429E-05 0.000 6.862E+10-10.5376 52994. 0.000 27.550 0.000985 -4719.4028 469.1055 8.400E-05 0.000 6.862E+10-15.1244 53449. 0.000 27.840 0.001277 -3181.4164 408.3804 8.380E-05 0.000 6.862E+10-19.7750 53905. 0.000 28.130 0.001568 -1882.9080 331.3535 8.367E-05 0.000 6.862E+10-24.4933 54360. 0.000 28.420 0.001859 -881.0195 237.7837 8.360E-05 0.000 6.862E+10-29.2825 54815. 0.000 28.710 0.002150 -233.7524 127.4190 8.358E-05 0.000 6.862E+10-34.1455 55271. 0.000 29.000 0.002441 0.000 0.000 8.357E-05 0.000 6.862E+10-39.0839 27863. 0.000

* This analysis makes computations of pile response using nonlinear moment-curvaturerelationships. The above values of total stress are computed for combined axial and bending stress in elastic sections and do not equal actual stresses in concrete and steel in the range of nonlinear bending.

Output Summary for Load Case No. 5:

Pile-head deflection = 0.5000000 inchesComputed slope at pile head = -0.0061750 radiansMaximum bending moment = 1263577. inch-lbsMaximum shear force = 40479. lbsDepth of maximum bending moment = 69.6000000 inches below pile headDepth of maximum shear force = 0.000000 inches below pile headNumber of iterations = 24Number of zero deflection points = 2

-------------------------------------------------------------------------------- Computed Values of Pile Loading and Deflection for Lateral Loading for Load Case Number 6--------------------------------------------------------------------------------

Pile-head conditions are Displacement and Moment (Loading Type 4)Displacement of pile head = 0.750000 inchesMoment at pile head = 0.000 in-lbsAxial load at pile head = 10000.000 lbs

Depth Deflect. Bending Shear Slope Total Bending Soil Res. Soil Spr. Distrib. X y Moment Force S Stress Stiffness p Es*h Lat. Load feet inches in-lbs lbs radians psi* lb-in^2 lb/in lb/inch lb/inch

Page 31

existing phase2 87.lp6o---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- 0.00 0.7500 0.000 55393. -0.009301 0.000 6.862E+10-808.8662 1876.5695 0.000 0.290 0.7176 188193. 52557. -0.009297 0.000 6.862E+10-820.6724 3979.6753 0.000 0.580 0.6853 366446. 49682. -0.009282 0.000 6.805E+10-831.6425 4223.1619 0.000 0.870 0.6530 534628. 46753. -0.009259 0.000 6.768E+10-852.0299 4540.5006 0.000 1.160 0.6209 692490. 43761. -0.009194 0.000 2.341E+10-867.2909 4861.3451 0.000 1.450 0.5890 839845. 40726. -0.009079 0.000 2.306E+10-877.1740 5182.3161 0.000 1.740 0.5577 976573. 37666. -0.008941 0.000 2.281E+10-881.3323 5499.8345 0.000 2.030 0.5268 1102622. 34602. -0.008782 0.000 2.262E+10-879.4370 5809.4600 0.000 2.320 0.4965 1218015. 31556. -0.008603 0.000 2.247E+10-871.1781 6105.6943 0.000 2.610 0.4669 1322852. 28529. -0.008406 0.000 2.235E+10-868.5520 6473.3158 0.000 2.900 0.4380 1417162. 25483. -0.008192 0.000 2.225E+10-882.0954 7007.9056 0.000 3.190 0.4099 1500783. 22394. -0.007963 0.000 2.217E+10-892.9673 7580.9876 0.000 3.480 0.3826 1573581. 19329. -0.007722 0.000 2.210E+10-868.4220 7898.7062 0.000 3.770 0.3562 1635853. 16366. -0.007469 0.000 2.204E+10-834.5167 8153.7869 0.000 4.060 0.3306 1688010. 13524. -0.007206 0.000 2.199E+10-798.9071 8408.8677 0.000 4.350 0.3060 1730483. 10808. -0.006935 0.000 2.196E+10-761.8674 8663.9484 0.000 4.640 0.2824 1763719. 8223.6034 -0.006658 0.000 2.193E+10-723.6659 8919.0291 0.000 4.930 0.2597 1788182. 5773.2827 -0.006376 0.000 2.191E+10-684.5644 9174.1098 0.000 5.220 0.2380 1804345. 3460.1607 -0.006091 0.000 2.189E+10-644.8161 9429.1905 0.000 5.510 0.2173 1812689. 1286.0630 -0.005803 0.000 2.188E+10-604.6653 9684.2712 0.000 5.800 0.1976 1813700. -748.0154 -0.005515 0.000 2.188E+10-564.3453 9939.3519 0.000 6.090 0.1789 1807867. -2641.8732 -0.005227 0.000 2.189E+10-524.0787 10194. 0.000 6.380 0.1612 1795676. -4396.0618 -0.004940 0.000 2.190E+10-484.0757 10450. 0.000 6.670 0.1445 1777614. -6011.8427 -0.004657 0.000 2.191E+10-444.5340 10705. 0.000 6.960 0.1288 1754158. -7491.1429 -0.004376 0.000 2.193E+10-405.6385 10960. 0.000 7.250 0.1141 1725780. -8836.5087 -0.004100 0.000 2.196E+10-367.5603 11215. 0.000 7.540 0.1003 1692941. -10051. -0.003830 0.000 2.199E+10-330.4573 11470. 0.000 7.830 0.0874 1656091. -11138. -0.003565 0.000 2.202E+10-294.4735 11725. 0.000 8.120 0.0755 1615666. -12103. -0.003307 0.000 2.206E+10-259.7395 11980. 0.000 8.410 0.0644 1572086. -12949. -0.003055 0.000 2.210E+10-226.3720 12235. 0.000 8.700 0.0542 1525756. -13681. -0.002812 0.000 2.214E+10

Page 32

existing phase2 87.lp6o-194.4746 12490. 0.000 8.990 0.0448 1477063. -14305. -0.002576 0.000 2.219E+10-164.1375 12745. 0.000 9.280 0.0363 1426374. -14826. -0.002349 0.000 2.224E+10-135.4383 13000. 0.000 9.570 0.0285 1374037. -15250. -0.002130 0.000 2.230E+10-108.4420 13255. 0.000 9.860 0.0214 1320379. -15584. -0.001920 0.000 2.236E+10-83.2018 13510. 0.000 10.150 0.0151 1265706. -15915. -0.001719 0.000 2.242E+10-107.2751 24711. 0.000 10.440 0.009467 1209728. -16221. -0.001527 0.000 2.248E+10-68.4662 25166. 0.000 10.730 0.004479 1152913. -16398. -0.001344 0.000 2.256E+10-32.9783 25622. 0.000 11.020 0.000110 1095693. -16456. -0.001171 0.000 2.263E+10-0.8233 26077. 0.000 11.310 -0.003673 1038458. -16409. -0.001008 0.000 2.272E+1028.0053 26533. 0.000 11.600 -0.006903 981556. -16267. -0.000853 0.000 2.280E+1053.5304 26988. 0.000 11.890 -0.009611 925296. -16042. -0.000708 0.000 2.290E+1075.7898 27443. 0.000 12.180 -0.0118 869950. -15745. -0.000572 0.000 2.300E+1094.8347 27899. 0.000 12.470 -0.0136 815748. -15388. -0.000445 0.000 2.311E+10110.7280 28354. 0.000 12.760 -0.0149 762883. -14980. -0.000326 0.000 2.323E+10123.5432 28810. 0.000 13.050 -0.0159 711509. -14533. -0.000216 0.000 2.336E+10133.3626 29265. 0.000 13.340 -0.0164 661747. -14057. -0.000144 0.000 6.271E+10140.2768 29720. 0.000 13.630 -0.0169 613683. -13558. -0.000110 0.000 6.751E+10146.2311 30176. 0.000 13.920 -0.0172 567388. -13041. -7.986E-05 0.000 6.761E+10151.3313 30631. 0.000 14.210 -0.0174 522926. -12507. -5.182E-05 0.000 6.771E+10155.6098 31087. 0.000 14.500 -0.0176 480346. -11959. -2.605E-05 0.000 6.780E+10159.1000 31542. 0.000 14.790 -0.0176 439693. -11401. -2.458E-06 0.000 6.789E+10161.8363 31997. 0.000 15.080 -0.0176 400998. -10869. 1.908E-05 0.000 6.797E+10143.5946 28440. 0.000 15.370 -0.0175 364042. -10368. 3.865E-05 0.000 6.805E+10144.6567 28818. 0.000 15.660 -0.0173 328838. -9863.2905 5.636E-05 0.000 6.813E+10145.1532 29196. 0.000 15.950 -0.0171 295390. -9358.2211 7.229E-05 0.000 6.819E+10145.1166 29574. 0.000 16.240 -0.0168 263699. -8854.1496 8.655E-05 0.000 6.827E+10144.5796 29952. 0.000 16.530 -0.0165 233759. -8352.7611 9.922E-05 0.000 6.832E+10143.5747 30329. 0.000 16.820 -0.0161 205557. -7855.6289 0.000110 0.000 6.837E+10142.1336 30707. 0.000 17.110 -0.0157 179076. -7364.2157 0.000120 0.000 6.844E+10140.2878 31085. 0.000 17.400 -0.0153 154294. -6879.8765 0.000129 0.000 6.848E+10138.0681 31463. 0.000 17.690 -0.0148 131183. -6403.8601 0.000136 0.000 6.851E+10135.5045 31841. 0.000

Page 33

existing phase2 87.lp6o 17.980 -0.0143 109714. -5937.3129 0.000142 0.000 6.855E+10132.6261 32219. 0.000 18.270 -0.0138 89850. -5481.2818 0.000147 0.000 6.860E+10129.4608 32597. 0.000 18.560 -0.0133 71554. -5036.7177 0.000151 0.000 6.862E+10126.0358 32974. 0.000 18.850 -0.0128 54784. -4604.4794 0.000154 0.000 6.862E+10122.3770 33352. 0.000 19.140 -0.0122 39496. -4185.3383 0.000157 0.000 6.862E+10118.5087 33730. 0.000 19.430 -0.0117 25643. -3779.9823 0.000158 0.000 6.862E+10114.4545 34108. 0.000 19.720 -0.0111 13176. -3389.0205 0.000159 0.000 6.862E+10110.2362 34486. 0.000 20.010 -0.0106 2044.1076 -3012.9883 0.000160 0.000 6.862E+10105.8743 34864. 0.000 20.300 -0.0100 -7805.5648 -2652.3518 0.000160 0.000 6.862E+10101.3881 35241. 0.000 20.590 -0.009457 -16427. -2307.5129 0.000159 0.000 6.862E+1096.7952 35619. 0.000 20.880 -0.008905 -23877. -1978.8150 0.000158 0.000 6.862E+1092.1117 35997. 0.000 21.170 -0.008357 -30211. -1666.5473 0.000157 0.000 6.862E+1087.3525 36375. 0.000 21.460 -0.007815 -35487. -1370.9508 0.000155 0.000 6.862E+1082.5306 36753. 0.000 21.750 -0.007278 -39764. -1092.2233 0.000153 0.000 6.862E+1077.6577 37131. 0.000 22.040 -0.006749 -43100. -830.5245 0.000151 0.000 6.862E+1072.7440 37508. 0.000 22.330 -0.006228 -45554. -585.9810 0.000149 0.000 6.862E+1067.7982 37886. 0.000 22.620 -0.005714 -47188. -358.6922 0.000146 0.000 6.862E+1062.8276 38264. 0.000 22.910 -0.005209 -48061. -148.7344 0.000144 0.000 6.862E+1057.8379 38642. 0.000 23.200 -0.004712 -48234. 43.8339 0.000142 0.000 6.862E+1052.8336 39020. 0.000 23.490 -0.004224 -47766. 218.9673 0.000139 0.000 6.862E+1047.8178 39398. 0.000 23.780 -0.003744 -46719. 376.6290 0.000137 0.000 6.862E+1042.7923 39775. 0.000 24.070 -0.003272 -45154. 516.7863 0.000134 0.000 6.862E+1037.7578 40153. 0.000 24.360 -0.002809 -43132. 639.4069 0.000132 0.000 6.862E+1032.7138 40531. 0.000 24.650 -0.002353 -40713. 744.4546 0.000130 0.000 6.862E+1027.6585 40909. 0.000 24.940 -0.001904 -37959. 831.8861 0.000128 0.000 6.862E+1022.5895 41287. 0.000 25.230 -0.001462 -34932. 907.5985 0.000126 0.000 6.862E+1020.9234 49806. 0.000 25.520 -0.001026 -31651. 969.7895 0.000124 0.000 6.862E+1014.8186 50261. 0.000 25.810 -0.000596 -28191. 1010.6791 0.000123 0.000 6.862E+108.6811 50717. 0.000 26.100 -0.000170 -24625. 1030.1416 0.000122 0.000 6.862E+102.5042 51172. 0.000 26.390 0.000251 -21030. 1028.0270 0.000120 0.000 6.862E+10-3.7195 51628. 0.000 26.680 0.000668 -17479. 1004.1585 0.000119 0.000 6.862E+10-9.9980 52083. 0.000 26.970 0.001082 -14049. 958.3321 0.000119 0.000 6.862E+10

Page 34

existing phase2 87.lp6o-16.3390 52538. 0.000 27.260 0.001494 -10817. 890.3159 0.000118 0.000 6.862E+10-22.7508 52994. 0.000 27.550 0.001904 -7860.6154 799.8504 0.000118 0.000 6.862E+10-29.2409 53449. 0.000 27.840 0.002312 -5258.2802 686.6498 0.000117 0.000 6.862E+10-35.8169 53905. 0.000 28.130 0.002720 -3089.6922 550.4043 0.000117 0.000 6.862E+10-42.4852 54360. 0.000 28.420 0.003127 -1435.6115 390.7822 0.000117 0.000 6.862E+10-49.2516 54815. 0.000 28.710 0.003534 -377.9851 207.4347 0.000117 0.000 6.862E+10-56.1205 55271. 0.000 29.000 0.003940 0.000 0.000 0.000117 0.000 6.862E+10-63.0948 27863. 0.000

* This analysis makes computations of pile response using nonlinear moment-curvaturerelationships. The above values of total stress are computed for combined axial and bending stress in elastic sections and do not equal actual stresses in concrete and steel in the range of nonlinear bending.

Output Summary for Load Case No. 6:

Pile-head deflection = 0.7500000 inchesComputed slope at pile head = -0.0093013 radiansMaximum bending moment = 1813700. inch-lbsMaximum shear force = 55393. lbsDepth of maximum bending moment = 69.6000000 inches below pile headDepth of maximum shear force = 0.000000 inches below pile headNumber of iterations = 34Number of zero deflection points = 2

-------------------------------------------------------------------------------- Computed Values of Pile Loading and Deflection for Lateral Loading for Load Case Number 7--------------------------------------------------------------------------------

Pile-head conditions are Displacement and Moment (Loading Type 4)Displacement of pile head = 1.000000 inchesMoment at pile head = 0.000 in-lbsAxial load at pile head = 10000.000 lbs

Depth Deflect. Bending Shear Slope Total Bending Soil Res. Soil Spr. Distrib. X y Moment Force S Stress Stiffness p Es*h Lat. Load feet inches in-lbs lbs radians psi* lb-in^2 lb/in lb/inch lb/inch ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- 0.00 1.0000 0.000 68911. -0.0123 0.000 6.862E+10-893.1068 1554.0058 0.000 0.290 0.9572 234830. 65738. -0.0123 0.000 6.862E+10-930.3695 3382.5842 0.000 0.580 0.9144 458393. 62431. -0.0123 0.000 6.785E+10-970.3824 3693.1848 0.000 0.870 0.8717 670203. 58992. -0.0122 0.000 4.570E+10 -1006.0280 4016.4721 0.000

Page 35

existing phase2 87.lp6o 1.160 0.8291 869828. 55455. -0.0122 0.000 2.300E+10 -1026.7068 4309.3203 0.000 1.450 0.7870 1057014. 51856. -0.0120 0.000 2.269E+10 -1041.4019 4604.6868 0.000 1.740 0.7455 1231583. 48218. -0.0118 0.000 2.246E+10 -1049.7260 4899.9473 0.000 2.030 0.7047 1393433. 44562. -0.0116 0.000 2.228E+10 -1051.3154 5191.8409 0.000 2.320 0.6646 1542544. 40913. -0.0114 0.000 2.213E+10 -1045.8309 5476.3257 0.000 2.610 0.6253 1678980. 37275. -0.0111 0.000 2.200E+10 -1044.9843 5815.3212 0.000 2.900 0.5870 1802752. 33614. -0.0109 0.000 2.189E+10 -1059.1299 6278.8358 0.000 3.190 0.5497 1913688. 29909. -0.0106 0.000 2.180E+10 -1069.8525 6773.0803 0.000 3.480 0.5134 2011657. 26173. -0.0103 0.000 2.172E+10 -1077.1425 7300.8731 0.000 3.770 0.4783 2096569. 22418. -0.009930 0.000 2.165E+10 -1081.0134 7865.4625 0.000 4.060 0.4443 2168379. 18669. -0.009586 0.000 2.159E+10 -1073.6179 8408.8677 0.000 4.350 0.4116 2227174. 15018. -0.009232 0.000 2.155E+10 -1024.6435 8663.9484 0.000 4.640 0.3801 2273549. 11540. -0.008868 0.000 2.151E+10-974.0760 8919.0291 0.000 4.930 0.3498 2308113. 8240.8548 -0.008497 0.000 2.148E+10-922.2650 9174.1098 0.000 5.220 0.3209 2331496. 5123.0984 -0.008121 0.000 2.147E+10-869.5490 9429.1905 0.000 5.510 0.2933 2344335. 2189.8011 -0.007742 0.000 2.146E+10-816.2541 9684.2712 0.000 5.800 0.2670 2347276. -557.5647 -0.007362 0.000 2.145E+10-762.6918 9939.3519 0.000 6.090 0.2421 2340967. -3118.5842 -0.006981 0.000 2.146E+10-709.1585 10194. 0.000 6.380 0.2184 2326057. -5493.8450 -0.006603 0.000 2.147E+10-655.9339 10450. 0.000 6.670 0.1961 2303190. -7684.8781 -0.006228 0.000 2.149E+10-603.2805 10705. 0.000 6.960 0.1751 2273003. -9694.0968 -0.005858 0.000 2.151E+10-551.4429 10960. 0.000 7.250 0.1554 2236126. -11525. -0.005493 0.000 2.154E+10-500.6470 11215. 0.000 7.540 0.1369 2193174. -13181. -0.005136 0.000 2.157E+10-451.1002 11470. 0.000 7.830 0.1196 2144746. -14667. -0.004786 0.000 2.161E+10-402.9913 11725. 0.000 8.120 0.1036 2091425. -15988. -0.004445 0.000 2.165E+10-356.4898 11980. 0.000 8.410 0.0887 2033776. -17151. -0.004114 0.000 2.170E+10-311.7470 12235. 0.000 8.700 0.0749 1972340. -18161. -0.003793 0.000 2.175E+10-268.8956 12490. 0.000 8.990 0.0623 1907636. -19026. -0.003483 0.000 2.180E+10-228.0504 12745. 0.000 9.280 0.0507 1840160. -19752. -0.003185 0.000 2.186E+10-189.3085 13000. 0.000 9.570 0.0401 1770382. -20348. -0.002898 0.000 2.192E+10-152.7500 13255. 0.000 9.860 0.0305 1698743. -20819. -0.002623 0.000 2.198E+10-118.4388 13510. 0.000 10.150 0.0218 1625661. -21295. -0.002360 0.000 2.205E+10

Page 36

existing phase2 87.lp6o-155.1399 24711. 0.000 10.440 0.0141 1550692. -21743. -0.002110 0.000 2.212E+10-101.8351 25166. 0.000 10.730 0.007164 1474480. -22012. -0.001872 0.000 2.219E+10-52.7484 25622. 0.000 11.020 0.001052 1397622. -22117. -0.001647 0.000 2.227E+10-7.8800 26077. 0.000 11.310 -0.004301 1320660. -22074. -0.001435 0.000 2.236E+1032.7942 26533. 0.000 11.600 -0.008939 1244089. -21896. -0.001236 0.000 2.244E+1069.3213 26988. 0.000 11.890 -0.0129 1168350. -21598. -0.001049 0.000 2.254E+10101.7682 27443. 0.000 12.180 -0.0162 1093838. -21195. -0.000875 0.000 2.264E+10130.2197 27899. 0.000 12.470 -0.0190 1020897. -20699. -0.000713 0.000 2.274E+10154.7768 28354. 0.000 12.760 -0.0212 949824. -20124. -0.000563 0.000 2.286E+10175.5537 28810. 0.000 13.050 -0.0229 880873. -19483. -0.000424 0.000 2.298E+10192.6766 29265. 0.000 13.340 -0.0242 814251. -18789. -0.000296 0.000 2.311E+10206.2812 29720. 0.000 13.630 -0.0250 750122. -18053. -0.000178 0.000 2.326E+10216.5113 30176. 0.000 13.920 -0.0254 688611. -17288. -7.089E-05 0.000 2.342E+10223.5173 30631. 0.000 14.210 -0.0255 629804. -16503. -3.496E-06 0.000 6.745E+10227.4541 31087. 0.000 14.500 -0.0254 573750. -15706. 2.752E-05 0.000 6.760E+10230.3840 31542. 0.000 14.790 -0.0253 520486. -14901. 5.566E-05 0.000 6.772E+10232.3572 31997. 0.000 15.080 -0.0250 470034. -14141. 8.109E-05 0.000 6.782E+10204.5631 28440. 0.000 15.370 -0.0247 422059. -13429. 0.000104 0.000 6.793E+10204.5963 28818. 0.000 15.660 -0.0243 376560. -12718. 0.000124 0.000 6.802E+10203.9279 29196. 0.000 15.950 -0.0238 333531. -12011. 0.000143 0.000 6.812E+10202.6031 29574. 0.000 16.240 -0.0233 292955. -11309. 0.000159 0.000 6.820E+10200.6666 29952. 0.000 16.530 -0.0227 254808. -10615. 0.000173 0.000 6.829E+10198.1626 30329. 0.000 16.820 -0.0221 219061. -9930.8800 0.000185 0.000 6.835E+10195.1344 30707. 0.000 17.110 -0.0215 185676. -9257.9201 0.000195 0.000 6.842E+10191.6242 31085. 0.000 17.400 -0.0208 154612. -8597.9426 0.000204 0.000 6.848E+10187.6732 31463. 0.000 17.690 -0.0200 125820. -7952.4123 0.000211 0.000 6.852E+10183.3212 31841. 0.000 17.980 -0.0193 99249. -7322.6582 0.000216 0.000 6.858E+10178.6065 32219. 0.000 18.270 -0.0185 74840. -6709.8780 0.000221 0.000 6.862E+10173.5660 32597. 0.000 18.560 -0.0178 52533. -6115.1441 0.000224 0.000 6.862E+10168.2350 32974. 0.000 18.850 -0.0170 32263. -5539.4096 0.000226 0.000 6.862E+10162.6469 33352. 0.000 19.140 -0.0162 13962. -4983.5141 0.000227 0.000 6.862E+10156.8333 33730. 0.000

Page 37

existing phase2 87.lp6o 19.430 -0.0154 -2438.4117 -4448.1906 0.000228 0.000 6.862E+10150.8239 34108. 0.000 19.720 -0.0146 -17013. -3934.0714 0.000227 0.000 6.862E+10144.6468 34486. 0.000 20.010 -0.0138 -29835. -3441.6954 0.000226 0.000 6.862E+10138.3279 34864. 0.000 20.300 -0.0130 -40983. -2971.5148 0.000224 0.000 6.862E+10131.8909 35241. 0.000 20.590 -0.0122 -50533. -2523.9022 0.000222 0.000 6.862E+10125.3578 35619. 0.000 20.880 -0.0115 -58564. -2099.1576 0.000219 0.000 6.862E+10118.7483 35997. 0.000 21.170 -0.0107 -65158. -1697.5161 0.000216 0.000 6.862E+10112.0802 36375. 0.000 21.460 -0.009977 -70394. -1319.1542 0.000212 0.000 6.862E+10105.3691 36753. 0.000 21.750 -0.009244 -74354. -964.1980 0.000209 0.000 6.862E+1098.6287 37131. 0.000 22.040 -0.008524 -77120. -632.7294 0.000205 0.000 6.862E+1091.8705 37508. 0.000 22.330 -0.007817 -78772. -324.7937 0.000201 0.000 6.862E+1085.1041 37886. 0.000 22.620 -0.007125 -79394. -40.4060 0.000197 0.000 6.862E+1078.3371 38264. 0.000 22.910 -0.006446 -79067. 220.4415 0.000193 0.000 6.862E+1071.5753 38642. 0.000 23.200 -0.005781 -77873. 457.7740 0.000189 0.000 6.862E+1064.8226 39020. 0.000 23.490 -0.005130 -75894. 671.6267 0.000185 0.000 6.862E+1058.0812 39398. 0.000 23.780 -0.004493 -73212. 862.0397 0.000181 0.000 6.862E+1051.3516 39775. 0.000 24.070 -0.003868 -69907. 1029.0521 0.000178 0.000 6.862E+1044.6326 40153. 0.000 24.360 -0.003256 -66062. 1172.6963 0.000174 0.000 6.862E+1037.9216 40531. 0.000 24.650 -0.002655 -61757. 1292.9937 0.000171 0.000 6.862E+1031.2148 40909. 0.000 24.940 -0.002066 -57074. 1389.9493 0.000168 0.000 6.862E+1024.5068 41287. 0.000 25.230 -0.001486 -52095. 1469.5973 0.000165 0.000 6.862E+1021.2679 49806. 0.000 25.520 -0.000916 -46858. 1529.6127 0.000163 0.000 6.862E+1013.2236 50261. 0.000 25.810 -0.000353 -41460. 1561.5837 0.000160 0.000 6.862E+105.1506 50717. 0.000 26.100 0.000201 -36000. 1565.3917 0.000159 0.000 6.862E+10-2.9621 51172. 0.000 26.390 0.000750 -30576. 1540.8792 0.000157 0.000 6.862E+10-11.1256 51628. 0.000 26.680 0.001293 -25287. 1487.8482 0.000155 0.000 6.862E+10-19.3520 52083. 0.000 26.970 0.001832 -20231. 1406.0593 0.000154 0.000 6.862E+10-27.6531 52538. 0.000 27.260 0.002367 -15511. 1295.2318 0.000153 0.000 6.862E+10-36.0408 52994. 0.000 27.550 0.002899 -11227. 1155.0446 0.000153 0.000 6.862E+10-44.5266 53449. 0.000 27.840 0.003429 -7482.6217 985.1380 0.000152 0.000 6.862E+10-53.1209 53905. 0.000 28.130 0.003958 -4381.2896 785.1174 0.000152 0.000 6.862E+10-61.8334 54360. 0.000 28.420 0.004487 -2028.7775 554.5575 0.000152 0.000 6.862E+10

Page 38

existing phase2 87.lp6o-70.6723 54815. 0.000 28.710 0.005015 -532.1311 293.0078 0.000152 0.000 6.862E+10-79.6436 55271. 0.000 29.000 0.005542 0.000 0.000 0.000152 0.000 6.862E+10-88.7517 27863. 0.000

* This analysis makes computations of pile response using nonlinear moment-curvaturerelationships. The above values of total stress are computed for combined axial and bending stress in elastic sections and do not equal actual stresses in concrete and steel in the range of nonlinear bending.

Output Summary for Load Case No. 7:

Pile-head deflection = 1.0000000 inchesComputed slope at pile head = -0.0123094 radiansMaximum bending moment = 2347276. inch-lbsMaximum shear force = 68911. lbsDepth of maximum bending moment = 69.6000000 inches below pile headDepth of maximum shear force = 0.000000 inches below pile headNumber of iterations = 15Number of zero deflection points = 2

-------------------------------------------------------------------------------- Computed Values of Pile Loading and Deflection for Lateral Loading for Load Case Number 8--------------------------------------------------------------------------------

Pile-head conditions are Displacement and Pile-head Rotation (Loading Type 5)Displacement of pile head = 0.010000 inchesRotation of pile head = 0.000E+00 radiansAxial load on pile head = 10000.000 lbs

Depth Deflect. Bending Shear Slope Total Bending Soil Res. Soil Spr. Distrib. X y Moment Force S Stress Stiffness p Es*h Lat. Load feet inches in-lbs lbs radians psi* lb-in^2 lb/in lb/inch lb/inch ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- 0.00 0.0100 -147576. 2581.1069 0.000 0.000 6.849E+10-13.9015 2418.8688 0.000 0.290 0.009987 -138682. 2530.2451 -7.273E-06 0.000 6.849E+10-14.6154 5092.8184 0.000 0.580 0.009949 -129965. 2478.2101 -1.410E-05 0.000 6.851E+10-15.2897 5347.8991 0.000 0.870 0.009889 -121433. 2423.9025 -2.048E-05 0.000 6.853E+10-15.9215 5602.9798 0.000 1.160 0.009807 -113093. 2367.4745 -2.644E-05 0.000 6.854E+10-16.5083 5858.0605 0.000 1.450 0.009705 -104954. 2309.0864 -3.197E-05 0.000 6.856E+10-17.0480 6113.1412 0.000 1.740 0.009584 -97020. 2248.9053 -3.709E-05 0.000 6.858E+10-17.5388 6368.2219 0.000 2.030 0.009447 -89299. 2187.1037 -4.182E-05 0.000 6.861E+10-17.9794 6623.3027 0.000 2.320 0.009293 -81795. 2123.8584 -4.616E-05 0.000 6.862E+10-18.3685 6878.3834 0.000

Page 39

existing phase2 87.lp6o 2.610 0.009125 -74513. 2059.3493 -5.012E-05 0.000 6.862E+10-18.7057 7133.4641 0.000 2.900 0.008944 -67458. 1993.7585 -5.372E-05 0.000 6.862E+10-18.9902 7388.5448 0.000 3.190 0.008751 -60633. 1927.2690 -5.697E-05 0.000 6.862E+10-19.2221 7643.6255 0.000 3.480 0.008548 -54040. 1860.0639 -5.988E-05 0.000 6.862E+10-19.4015 7898.7062 0.000 3.770 0.008335 -47683. 1792.3257 -6.246E-05 0.000 6.862E+10-19.5286 8153.7869 0.000 4.060 0.008113 -41562. 1724.2347 -6.472E-05 0.000 6.862E+10-19.6041 8408.8677 0.000 4.350 0.007884 -35678. 1655.9692 -6.668E-05 0.000 6.862E+10-19.6289 8663.9484 0.000 4.640 0.007649 -30031. 1587.7038 -6.835E-05 0.000 6.862E+10-19.6041 8919.0291 0.000 4.930 0.007409 -24622. 1519.6093 -6.973E-05 0.000 6.862E+10-19.5307 9174.1098 0.000 5.220 0.007164 -19450. 1451.8519 -7.085E-05 0.000 6.862E+10-19.4103 9429.1905 0.000 5.510 0.006915 -14513. 1384.5924 -7.171E-05 0.000 6.862E+10-19.2445 9684.2712 0.000 5.800 0.006665 -9808.2472 1317.9861 -7.233E-05 0.000 6.862E+10-19.0350 9939.3519 0.000 6.090 0.006412 -5334.3906 1252.1817 -7.271E-05 0.000 6.862E+10-18.7836 10194. 0.000 6.380 0.006159 -1088.0018 1187.3214 -7.288E-05 0.000 6.862E+10-18.4924 10450. 0.000 6.670 0.005905 2934.4388 1123.5404 -7.283E-05 0.000 6.862E+10-18.1634 10705. 0.000 6.960 0.005652 6736.9080 1060.9660 -7.258E-05 0.000 6.862E+10-17.7989 10960. 0.000 7.250 0.005400 10324. 999.7182 -7.215E-05 0.000 6.862E+10-17.4010 11215. 0.000 7.540 0.005149 13700. 939.9086 -7.154E-05 0.000 6.862E+10-16.9723 11470. 0.000 7.830 0.004902 16871. 881.6408 -7.077E-05 0.000 6.862E+10-16.5150 11725. 0.000 8.120 0.004657 19841. 825.0097 -6.984E-05 0.000 6.862E+10-16.0316 11980. 0.000 8.410 0.004416 22617. 770.1017 -6.876E-05 0.000 6.862E+10-15.5247 12235. 0.000 8.700 0.004178 25206. 716.9945 -6.755E-05 0.000 6.862E+10-14.9967 12490. 0.000 8.990 0.003946 27612. 665.7568 -6.621E-05 0.000 6.862E+10-14.4502 12745. 0.000 9.280 0.003718 29844. 616.4485 -6.475E-05 0.000 6.862E+10-13.8878 13000. 0.000 9.570 0.003495 31907. 569.1206 -6.318E-05 0.000 6.862E+10-13.3121 13255. 0.000 9.860 0.003278 33810. 523.8152 -6.152E-05 0.000 6.862E+10-12.7255 13510. 0.000 10.150 0.003067 35557. 463.7819 -5.976E-05 0.000 6.862E+10-21.7764 24711. 0.000 10.440 0.002862 37042. 389.8791 -5.792E-05 0.000 6.862E+10-20.6965 25166. 0.000 10.730 0.002664 38275. 319.7439 -5.601E-05 0.000 6.862E+10-19.6111 25622. 0.000 11.020 0.002472 39271. 253.3880 -5.404E-05 0.000 6.862E+10-18.5245 26077. 0.000 11.310 0.002287 40042. 190.8089 -5.203E-05 0.000 6.862E+10-17.4405 26533. 0.000 11.600 0.002110 40603. 131.9906 -4.999E-05 0.000 6.862E+10

Page 40

existing phase2 87.lp6o-16.3631 26988. 0.000 11.890 0.001940 40965. 76.9043 -4.792E-05 0.000 6.862E+10-15.2957 27443. 0.000 12.180 0.001776 41141. 25.5092 -4.583E-05 0.000 6.862E+10-14.2417 27899. 0.000 12.470 0.001621 41145. -22.2466 -4.375E-05 0.000 6.862E+10-13.2041 28354. 0.000 12.760 0.001472 40989. -66.4252 -4.167E-05 0.000 6.862E+10-12.1859 28810. 0.000 13.050 0.001331 40686. -107.0986 -3.959E-05 0.000 6.862E+10-11.1896 29265. 0.000 13.340 0.001196 40247. -144.3472 -3.754E-05 0.000 6.862E+10-10.2176 29720. 0.000 13.630 0.001069 39684. -178.2594 -3.552E-05 0.000 6.862E+10-9.2721 30176. 0.000 13.920 0.000949 39009. -208.9307 -3.352E-05 0.000 6.862E+10-8.3550 30631. 0.000 14.210 0.000836 38232. -236.4627 -3.156E-05 0.000 6.862E+10-7.4680 31087. 0.000 14.500 0.000730 37365. -260.9626 -2.964E-05 0.000 6.862E+10-6.6124 31542. 0.000 14.790 0.000630 36418. -282.5424 -2.777E-05 0.000 6.862E+10-5.7897 31997. 0.000 15.080 0.000536 35400. -300.2419 -2.595E-05 0.000 6.862E+10-4.3825 28440. 0.000 15.370 0.000449 34330. -314.3379 -2.418E-05 0.000 6.862E+10-3.7187 28818. 0.000 15.660 0.000368 33214. -326.1793 -2.247E-05 0.000 6.862E+10-3.0868 29196. 0.000 15.950 0.000293 32061. -335.8777 -2.082E-05 0.000 6.862E+10-2.4871 29574. 0.000 16.240 0.000223 30878. -343.5454 -1.922E-05 0.000 6.862E+10-1.9197 29952. 0.000 16.530 0.000159 29672. -349.2952 -1.768E-05 0.000 6.862E+10-1.3847 30329. 0.000 16.820 9.996E-05 28448. -353.2394 -1.621E-05 0.000 6.862E+10-0.8821 30707. 0.000 17.110 4.606E-05 27214. -355.4900 -1.480E-05 0.000 6.862E+10-0.4114 31085. 0.000 17.400 -3.042E-06 25975. -356.1580 -1.345E-05 0.000 6.862E+100.0275 31463. 0.000 17.690 -4.756E-05 24736. -355.3530 -1.216E-05 0.000 6.862E+100.4351 31841. 0.000 17.980 -8.771E-05 23503. -353.1830 -1.094E-05 0.000 6.862E+100.8120 32219. 0.000 18.270 -0.000124 22279. -349.7538 -9.781E-06 0.000 6.862E+101.1588 32597. 0.000 18.560 -0.000156 21069. -345.1692 -8.681E-06 0.000 6.862E+101.4761 32974. 0.000 18.850 -0.000184 19877. -339.5302 -7.643E-06 0.000 6.862E+101.7647 33352. 0.000 19.140 -0.000209 18706. -332.9352 -6.665E-06 0.000 6.862E+102.0255 33730. 0.000 19.430 -0.000231 17560. -325.4796 -5.745E-06 0.000 6.862E+102.2593 34108. 0.000 19.720 -0.000249 16441. -317.2556 -4.883E-06 0.000 6.862E+102.4671 34486. 0.000 20.010 -0.000265 15352. -308.3521 -4.077E-06 0.000 6.862E+102.6499 34864. 0.000 20.300 -0.000277 14296. -298.8545 -3.325E-06 0.000 6.862E+102.8085 35241. 0.000 20.590 -0.000288 13273. -288.8449 -2.626E-06 0.000 6.862E+102.9441 35619. 0.000

Page 41

existing phase2 87.lp6o 20.880 -0.000296 12285. -278.4016 -1.978E-06 0.000 6.862E+103.0578 35997. 0.000 21.170 -0.000301 11335. -267.5992 -1.379E-06 0.000 6.862E+103.1505 36375. 0.000 21.460 -0.000305 10423. -256.5089 -8.270E-07 0.000 6.862E+103.2233 36753. 0.000 21.750 -0.000307 9549.8959 -245.1977 -3.205E-07 0.000 6.862E+103.2773 37131. 0.000 22.040 -0.000307 8716.4554 -233.7295 1.427E-07 0.000 6.862E+103.3136 37508. 0.000 22.330 -0.000306 7923.1289 -222.1640 5.646E-07 0.000 6.862E+103.3332 37886. 0.000 22.620 -0.000304 7170.1549 -210.5575 9.474E-07 0.000 6.862E+103.3372 38264. 0.000 22.910 -0.000300 6457.5828 -198.9627 1.293E-06 0.000 6.862E+103.3265 38642. 0.000 23.200 -0.000295 5785.2845 -187.4288 1.603E-06 0.000 6.862E+103.3022 39020. 0.000 23.490 -0.000288 5152.9665 -176.0016 1.881E-06 0.000 6.862E+103.2652 39398. 0.000 23.780 -0.000281 4560.1824 -164.7234 2.127E-06 0.000 6.862E+103.2165 39775. 0.000 24.070 -0.000274 4006.3436 -153.6335 2.344E-06 0.000 6.862E+103.1570 40153. 0.000 24.360 -0.000265 3490.7304 -142.7679 2.534E-06 0.000 6.862E+103.0876 40531. 0.000 24.650 -0.000256 3012.5029 -132.1597 2.699E-06 0.000 6.862E+103.0091 40909. 0.000 24.940 -0.000246 2570.7113 -121.8391 2.841E-06 0.000 6.862E+102.9223 41287. 0.000 25.230 -0.000236 2164.3049 -110.8723 2.961E-06 0.000 6.862E+103.3805 49806. 0.000 25.520 -0.000226 1798.8341 -99.3181 3.061E-06 0.000 6.862E+103.2598 50261. 0.000 25.810 -0.000215 1472.8382 -88.1966 3.144E-06 0.000 6.862E+103.1318 50717. 0.000 26.100 -0.000204 1184.7671 -77.5323 3.212E-06 0.000 6.862E+102.9971 51172. 0.000 26.390 -0.000193 932.9901 -67.3471 3.265E-06 0.000 6.862E+102.8564 51628. 0.000 26.680 -0.000181 715.8038 -57.6610 3.307E-06 0.000 6.862E+102.7103 52083. 0.000 26.970 -0.000170 531.4391 -48.4919 3.339E-06 0.000 6.862E+102.5593 52538. 0.000 27.260 -0.000158 378.0675 -39.8561 3.362E-06 0.000 6.862E+102.4038 52994. 0.000 27.550 -0.000146 253.8064 -31.7685 3.378E-06 0.000 6.862E+102.2443 53449. 0.000 27.840 -0.000134 156.7238 -24.2426 3.388E-06 0.000 6.862E+102.0810 53905. 0.000 28.130 -0.000123 84.8421 -17.2912 3.395E-06 0.000 6.862E+101.9141 54360. 0.000 28.420 -0.000111 36.1411 -10.9261 3.398E-06 0.000 6.862E+101.7440 54815. 0.000 28.710 -9.889E-05 8.5601 -5.1587 3.399E-06 0.000 6.862E+101.5706 55271. 0.000 29.000 -8.706E-05 0.000 0.000 3.399E-06 0.000 6.862E+101.3941 27863. 0.000

* This analysis makes computations of pile response using nonlinear moment-curvaturerelationships. The above values of total stress are computed for combined axial and bending stress in elastic

Page 42

existing phase2 87.lp6o sections and do not equal actual stresses in concrete and steel in the range of nonlinear bending.

Output Summary for Load Case No. 8:

Pile-head deflection = 0.0100000 inchesComputed slope at pile head = -0.000000226 radiansMaximum bending moment = -147576. inch-lbsMaximum shear force = 2581.1068770 lbsDepth of maximum bending moment = 0.000000 inches below pile headDepth of maximum shear force = 0.000000 inches below pile headNumber of iterations = 6Number of zero deflection points = 1

-------------------------------------------------------------------------------- Computed Values of Pile Loading and Deflection for Lateral Loading for Load Case Number 9--------------------------------------------------------------------------------

Pile-head conditions are Displacement and Pile-head Rotation (Loading Type 5)Displacement of pile head = 0.100000 inchesRotation of pile head = 0.000E+00 radiansAxial load on pile head = 10000.000 lbs

Depth Deflect. Bending Shear Slope Total Bending Soil Res. Soil Spr. Distrib. X y Moment Force S Stress Stiffness p Es*h Lat. Load feet inches in-lbs lbs radians psi* lb-in^2 lb/in lb/inch lb/inch ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- 0.00 0.1000 -974916. 21125. 0.000 0.000 2.281E+10-139.0155 2418.8688 0.000 0.290 0.0997 -902283. 20617. -0.000143 0.000 2.281E+10-145.9667 5092.8184 0.000 0.580 0.0990 -831413. 20098. -0.000275 0.000 2.308E+10-152.1439 5347.8991 0.000 0.870 0.0978 -762381. 19559. -0.000394 0.000 2.323E+10-157.5105 5602.9798 0.000 1.160 0.0963 -695253. 19003. -0.000494 0.000 2.828E+10-162.0359 5858.0605 0.000 1.450 0.0944 -630084. 18433. -0.000557 0.000 5.447E+10-165.8080 6113.1412 0.000 1.740 0.0924 -566921. 17850. -0.000592 0.000 6.761E+10-169.0496 6368.2219 0.000 2.030 0.0903 -505805. 17257. -0.000620 0.000 6.775E+10-171.8034 6623.3027 0.000 2.320 0.0881 -446768. 16655. -0.000644 0.000 6.788E+10-174.0691 6878.3834 0.000 2.610 0.0858 -389839. 16046. -0.000665 0.000 6.799E+10-175.8487 7133.4641 0.000 2.900 0.0834 -335039. 15432. -0.000684 0.000 6.812E+10-177.1465 7388.5448 0.000 3.190 0.0810 -282383. 14814. -0.000700 0.000 6.822E+10-177.9688 7643.6255 0.000 3.480 0.0786 -231882. 14194. -0.000713 0.000 6.832E+10-178.3241 7898.7062 0.000 3.770 0.0761 -183541. 13574. -0.000723 0.000 6.843E+10-178.2225 8153.7869 0.000

Page 43

existing phase2 87.lp6o 4.060 0.0735 -137357. 12955. -0.000732 0.000 6.850E+10-177.6757 8408.8677 0.000 4.350 0.0710 -93325. 12338. -0.000737 0.000 6.859E+10-176.6969 8663.9484 0.000 4.640 0.0684 -51432. 11726. -0.000741 0.000 6.862E+10-175.3010 8919.0291 0.000 4.930 0.0658 -11663. 11119. -0.000743 0.000 6.862E+10-173.5037 9174.1098 0.000 5.220 0.0632 26006. 10519. -0.000742 0.000 6.862E+10-171.3221 9429.1905 0.000 5.510 0.0606 61599. 9926.9602 -0.000740 0.000 6.862E+10-168.7743 9684.2712 0.000 5.800 0.0581 95149. 9344.6634 -0.000736 0.000 6.859E+10-165.8791 9939.3519 0.000 6.090 0.0555 126689. 8773.0118 -0.000730 0.000 6.852E+10-162.6563 10194. 0.000 6.380 0.0530 156260. 8213.1096 -0.000723 0.000 6.848E+10-159.1265 10450. 0.000 6.670 0.0505 183903. 7665.9889 -0.000715 0.000 6.843E+10-155.3107 10705. 0.000 6.960 0.0480 209665. 7132.6075 -0.000705 0.000 6.837E+10-151.2303 10960. 0.000 7.250 0.0456 233595. 6613.8477 -0.000693 0.000 6.832E+10-146.9075 11215. 0.000 7.540 0.0432 255745. 6110.5146 -0.000681 0.000 6.829E+10-142.3644 11470. 0.000 7.830 0.0408 276171. 5623.3359 -0.000667 0.000 6.824E+10-137.6234 11725. 0.000 8.120 0.0385 294930. 5152.9610 -0.000653 0.000 6.819E+10-132.7070 11980. 0.000 8.410 0.0363 312082. 4699.9607 -0.000637 0.000 6.816E+10-127.6380 12235. 0.000 8.700 0.0341 327686. 4264.8271 -0.000621 0.000 6.813E+10-122.4388 12490. 0.000 8.990 0.0320 341808. 3847.9742 -0.000604 0.000 6.811E+10-117.1319 12745. 0.000 9.280 0.0299 354510. 3449.7381 -0.000586 0.000 6.807E+10-111.7395 13000. 0.000 9.570 0.0279 365859. 3070.3779 -0.000568 0.000 6.805E+10-106.2837 13255. 0.000 9.860 0.0260 375920. 2710.0760 -0.000549 0.000 6.802E+10-100.7863 13510. 0.000 10.150 0.0241 384759. 2237.1324 -0.000529 0.000 6.801E+10-171.0203 24711. 0.000 10.440 0.0223 391527. 1659.2400 -0.000509 0.000 6.799E+10-161.1017 25166. 0.000 10.730 0.0205 396343. 1115.7942 -0.000489 0.000 6.798E+10-151.2235 25622. 0.000 11.020 0.0189 399327. 606.5952 -0.000469 0.000 6.798E+10-141.4196 26077. 0.000 11.310 0.0173 400598. 131.3293 -0.000448 0.000 6.797E+10-131.7218 26533. 0.000 11.600 0.0158 400272. -310.4246 -0.000428 0.000 6.797E+10-122.1598 26988. 0.000 11.890 0.0143 398467. -719.1871 -0.000407 0.000 6.798E+10-112.7612 27443. 0.000 12.180 0.0129 395295. -1095.5708 -0.000387 0.000 6.798E+10-103.5513 27899. 0.000 12.470 0.0116 390869. -1440.2732 -0.000367 0.000 6.799E+10-94.5535 28354. 0.000 12.760 0.0104 385296. -1754.0685 -0.000347 0.000 6.800E+10-85.7886 28810. 0.000 13.050 0.009189 378684. -2037.8005 -0.000328 0.000 6.802E+10

Page 44

existing phase2 87.lp6o-77.2757 29265. 0.000 13.340 0.008083 371136. -2292.3749 -0.000308 0.000 6.803E+10-69.0314 29720. 0.000 13.630 0.007043 362751. -2518.7524 -0.000290 0.000 6.805E+10-61.0705 30176. 0.000 13.920 0.006067 353626. -2717.9408 -0.000271 0.000 6.808E+10-53.4056 30631. 0.000 14.210 0.005155 343853. -2890.9889 -0.000253 0.000 6.810E+10-46.0473 31087. 0.000 14.500 0.004303 333522. -3038.9789 -0.000236 0.000 6.812E+10-39.0044 31542. 0.000 14.790 0.003511 322718. -3163.0203 -0.000219 0.000 6.814E+10-32.2838 31997. 0.000 15.080 0.002776 311523. -3258.6740 -0.000203 0.000 6.816E+10-22.6896 28440. 0.000 15.370 0.002097 300052. -3328.3678 -0.000188 0.000 6.818E+10-17.3643 28818. 0.000 15.660 0.001471 288370. -3380.0510 -0.000173 0.000 6.821E+10-12.3386 29196. 0.000 15.950 0.000896 276539. -3414.7652 -0.000158 0.000 6.824E+10-7.6121 29574. 0.000 16.240 0.000370 264614. -3433.5490 -0.000144 0.000 6.827E+10-3.1831 29952. 0.000 16.530 -0.000109 252651. -3437.4330 -0.000131 0.000 6.829E+100.9509 30329. 0.000 16.820 -0.000543 240699. -3427.4376 -0.000119 0.000 6.831E+104.7936 30707. 0.000 17.110 -0.000935 228805. -3404.5688 -0.000107 0.000 6.833E+108.3494 31085. 0.000 17.400 -0.001286 217011. -3369.8158 -9.531E-05 0.000 6.835E+1011.6236 31463. 0.000 17.690 -0.001598 205357. -3324.1482 -8.456E-05 0.000 6.837E+1014.6222 31841. 0.000 17.980 -0.001874 193880. -3268.5134 -7.441E-05 0.000 6.840E+1017.3518 32219. 0.000 18.270 -0.002116 182614. -3203.8345 -6.483E-05 0.000 6.843E+1019.8199 32597. 0.000 18.560 -0.002325 171586. -3131.0080 -5.583E-05 0.000 6.846E+1022.0343 32974. 0.000 18.850 -0.002505 160826. -3050.9026 -4.738E-05 0.000 6.847E+1024.0033 33352. 0.000 19.140 -0.002655 150355. -2964.3572 -3.947E-05 0.000 6.848E+1025.7354 33730. 0.000 19.430 -0.002779 140196. -2872.1805 -3.209E-05 0.000 6.850E+1027.2397 34108. 0.000 19.720 -0.002879 130367. -2775.1495 -2.522E-05 0.000 6.851E+1028.5253 34486. 0.000 20.010 -0.002955 120883. -2674.0088 -1.884E-05 0.000 6.853E+1029.6015 34864. 0.000 20.300 -0.003010 111757. -2569.4704 -1.293E-05 0.000 6.855E+1030.4780 35241. 0.000 20.590 -0.003045 103001. -2462.2127 -7.480E-06 0.000 6.857E+1031.1643 35619. 0.000 20.880 -0.003062 94621. -2352.8808 -2.466E-06 0.000 6.859E+1031.6701 35997. 0.000 21.170 -0.003062 86625. -2242.0863 2.131E-06 0.000 6.862E+1032.0049 36375. 0.000 21.460 -0.003047 79016. -2130.4076 6.332E-06 0.000 6.862E+1032.1783 36753. 0.000 21.750 -0.003018 71797. -2018.3901 1.016E-05 0.000 6.862E+1032.1996 37131. 0.000 22.040 -0.002976 64967. -1906.5471 1.362E-05 0.000 6.862E+1032.0780 37508. 0.000

Page 45

existing phase2 87.lp6o 22.330 -0.002923 58526. -1795.3599 1.676E-05 0.000 6.862E+1031.8226 37886. 0.000 22.620 -0.002860 52470. -1685.2794 1.957E-05 0.000 6.862E+1031.4421 38264. 0.000 22.910 -0.002787 46795. -1576.7261 2.209E-05 0.000 6.862E+1030.9449 38642. 0.000 23.200 -0.002706 41495. -1470.0915 2.433E-05 0.000 6.862E+1030.3394 39020. 0.000 23.490 -0.002618 36562. -1365.7391 2.631E-05 0.000 6.862E+1029.6333 39398. 0.000 23.780 -0.002523 31987. -1264.0054 2.804E-05 0.000 6.862E+1028.8343 39775. 0.000 24.070 -0.002422 27762. -1165.2013 2.956E-05 0.000 6.862E+1027.9496 40153. 0.000 24.360 -0.002317 23875. -1069.6132 3.087E-05 0.000 6.862E+1026.9861 40531. 0.000 24.650 -0.002208 20316. -977.5042 3.199E-05 0.000 6.862E+1025.9501 40909. 0.000 24.940 -0.002094 17070. -889.1158 3.294E-05 0.000 6.862E+1024.8478 41287. 0.000 25.230 -0.001978 14125. -796.6160 3.373E-05 0.000 6.862E+1028.3130 49806. 0.000 25.520 -0.001860 11523. -700.6173 3.438E-05 0.000 6.862E+1026.8587 50261. 0.000 25.810 -0.001739 9246.3180 -609.7852 3.490E-05 0.000 6.862E+1025.3437 50717. 0.000 26.100 -0.001617 7276.5039 -524.3219 3.532E-05 0.000 6.862E+1023.7731 51172. 0.000 26.390 -0.001493 5594.5791 -444.4130 3.565E-05 0.000 6.862E+1022.1515 51628. 0.000 26.680 -0.001369 4180.9081 -370.2293 3.590E-05 0.000 6.862E+1020.4828 52083. 0.000 26.970 -0.001243 3015.2844 -301.9290 3.608E-05 0.000 6.862E+1018.7703 52538. 0.000 27.260 -0.001117 2076.9711 -239.6592 3.621E-05 0.000 6.862E+1017.0169 52994. 0.000 27.550 -0.000991 1344.7360 -183.5583 3.630E-05 0.000 6.862E+1015.2250 53449. 0.000 27.840 -0.000865 796.8793 -133.7571 3.635E-05 0.000 6.862E+1013.3964 53905. 0.000 28.130 -0.000738 411.2563 -90.3811 3.638E-05 0.000 6.862E+1011.5324 54360. 0.000 28.420 -0.000612 165.2949 -53.5511 3.640E-05 0.000 6.862E+109.6342 54815. 0.000 28.710 -0.000485 36.0077 -23.3853 3.640E-05 0.000 6.862E+107.7024 55271. 0.000 29.000 -0.000358 0.000 0.000 3.640E-05 0.000 6.862E+105.7374 27863. 0.000

* This analysis makes computations of pile response using nonlinear moment-curvaturerelationships. The above values of total stress are computed for combined axial and bending stress in elastic sections and do not equal actual stresses in concrete and steel in the range of nonlinear bending.

Output Summary for Load Case No. 9:

Pile-head deflection = 0.1000000 inchesComputed slope at pile head = -0.000005540 radiansMaximum bending moment = -974916. inch-lbsMaximum shear force = 21125. lbs

Page 46

existing phase2 87.lp6oDepth of maximum bending moment = 0.000000 inches below pile headDepth of maximum shear force = 0.000000 inches below pile headNumber of iterations = 8Number of zero deflection points = 1

-------------------------------------------------------------------------------- Computed Values of Pile Loading and Deflection for Lateral Loading for Load Case Number 10--------------------------------------------------------------------------------

Pile-head conditions are Displacement and Pile-head Rotation (Loading Type 5)Displacement of pile head = 0.200000 inchesRotation of pile head = 0.000E+00 radiansAxial load on pile head = 10000.000 lbs

Depth Deflect. Bending Shear Slope Total Bending Soil Res. Soil Spr. Distrib. X y Moment Force S Stress Stiffness p Es*h Lat. Load feet inches in-lbs lbs radians psi* lb-in^2 lb/in lb/inch lb/inch ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- 0.00 0.2000 -1648585. 38697. 0.000 0.000 2.203E+10-278.0309 2418.8688 0.000 0.290 0.1995 -1515684. 37680. -0.000250 0.000 2.203E+10-292.0275 5092.8184 0.000 0.580 0.1983 -1386312. 36642. -0.000478 0.000 2.228E+10-304.6773 5347.8991 0.000 0.870 0.1962 -1260622. 35562. -0.000684 0.000 2.242E+10-315.9254 5602.9798 0.000 1.160 0.1935 -1138751. 34446. -0.000870 0.000 2.257E+10-325.7285 5858.0605 0.000 1.450 0.1902 -1020819. 33298. -0.001035 0.000 2.274E+10-334.0596 6113.1412 0.000 1.740 0.1863 -906927. 32123. -0.001182 0.000 2.293E+10-340.9075 6368.2219 0.000 2.030 0.1819 -797158. 30928. -0.001311 0.000 2.315E+10-346.2757 6623.3027 0.000 2.320 0.1772 -691579. 29716. -0.001422 0.000 2.342E+10-350.1814 6878.3834 0.000 2.610 0.1720 -590237. 28493. -0.001489 0.000 6.757E+10-352.6544 7133.4641 0.000 2.900 0.1668 -493165. 27263. -0.001517 0.000 6.778E+10-354.1510 7388.5448 0.000 3.190 0.1615 -400381. 26030. -0.001540 0.000 6.797E+10-354.6866 7643.6255 0.000 3.480 0.1561 -311892. 24796. -0.001558 0.000 6.816E+10-354.2800 7898.7062 0.000 3.770 0.1506 -227692. 23565. -0.001572 0.000 6.833E+10-352.9528 8153.7869 0.000 4.060 0.1451 -147767. 22341. -0.001581 0.000 6.849E+10-350.7292 8408.8677 0.000 4.350 0.1396 -72089. 21126. -0.001587 0.000 6.862E+10-347.6358 8663.9484 0.000 4.640 0.1341 -620.3732 19923. -0.001589 0.000 6.862E+10-343.7012 8919.0291 0.000 4.930 0.1286 66686. 18735. -0.001587 0.000 6.862E+10-338.9557 9174.1098 0.000 5.220 0.1231 129887. 17565. -0.001582 0.000 6.851E+10-333.4317 9429.1905 0.000

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existing phase2 87.lp6o 5.510 0.1176 189049. 16416. -0.001574 0.000 6.841E+10-327.1627 9684.2712 0.000 5.800 0.1121 244250. 15289. -0.001563 0.000 6.831E+10-320.1840 9939.3519 0.000 6.090 0.1067 295572. 14188. -0.001549 0.000 6.819E+10-312.5315 10194. 0.000 6.380 0.1013 343109. 13115. -0.001533 0.000 6.810E+10-304.2426 10450. 0.000 6.670 0.0960 386961. 12072. -0.001514 0.000 6.800E+10-295.3548 10705. 0.000 6.960 0.0908 427235. 11061. -0.001493 0.000 6.792E+10-285.9066 10960. 0.000 7.250 0.0856 464046. 10083. -0.001470 0.000 6.784E+10-275.9364 11215. 0.000 7.540 0.0805 497515. 9140.8777 -0.001446 0.000 6.777E+10-265.4830 11470. 0.000 7.830 0.0756 527767. 8235.9592 -0.001419 0.000 6.770E+10-254.5851 11725. 0.000 8.120 0.0707 554936. 7369.6721 -0.001392 0.000 6.764E+10-243.2811 11980. 0.000 8.410 0.0659 579157. 6543.3632 -0.001362 0.000 6.759E+10-231.6091 12235. 0.000 8.700 0.0612 600573. 5758.2471 -0.001332 0.000 6.754E+10-219.6070 12490. 0.000 8.990 0.0566 619327. 5015.4084 -0.001301 0.000 6.750E+10-207.3118 12745. 0.000 9.280 0.0521 635570. 4315.8036 -0.001268 0.000 6.746E+10-194.7600 13000. 0.000 9.570 0.0478 649454. 3660.2633 -0.001235 0.000 6.743E+10-181.9874 13255. 0.000 9.860 0.0435 661132. 3049.4949 -0.001201 0.000 6.739E+10-169.0289 13510. 0.000 10.150 0.0394 670762. 2268.3673 -0.001155 0.000 4.062E+10-279.8950 24711. 0.000 10.440 0.0355 677000. 1334.6975 -0.001086 0.000 2.871E+10-256.6968 25166. 0.000 10.730 0.0319 680127. 479.8846 -0.000995 0.000 2.389E+10-234.5749 25622. 0.000 11.020 0.0286 680409. -300.7836 -0.000895 0.000 2.345E+10-214.0849 26077. 0.000 11.310 0.0256 678096. -1013.3100 -0.000798 0.000 2.525E+10-195.4130 26533. 0.000 11.600 0.0230 673412. -1663.9090 -0.000714 0.000 3.140E+10-178.4945 26988. 0.000 11.890 0.0207 666564. -2258.0055 -0.000650 0.000 4.378E+10-162.9403 27443. 0.000 12.180 0.0185 657742. -2799.4734 -0.000607 0.000 6.740E+10-148.2481 27899. 0.000 12.470 0.0164 647122. -3290.5000 -0.000573 0.000 6.744E+10-133.9511 28354. 0.000 12.760 0.0145 634880. -3732.5124 -0.000540 0.000 6.747E+10-120.0791 28810. 0.000 13.050 0.0127 621182. -4127.0364 -0.000507 0.000 6.750E+10-106.6588 29265. 0.000 13.340 0.0110 606191. -4475.6847 -0.000476 0.000 6.753E+10-93.7138 29720. 0.000 13.630 0.009372 590064. -4780.1456 -0.000445 0.000 6.757E+10-81.2638 30176. 0.000 13.920 0.007876 572952. -5042.1710 -0.000415 0.000 6.760E+10-69.3255 30631. 0.000 14.210 0.006483 554999. -5263.5654 -0.000386 0.000 6.764E+10-57.9127 31087. 0.000 14.500 0.005189 536344. -5446.1759 -0.000358 0.000 6.768E+10

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existing phase2 87.lp6o-47.0359 31542. 0.000 14.790 0.003992 517119. -5591.8817 -0.000331 0.000 6.773E+10-36.7030 31997. 0.000 15.080 0.002887 497448. -5696.7927 -0.000305 0.000 6.777E+10-23.5907 28440. 0.000 15.370 0.001870 477490. -5764.7898 -0.000280 0.000 6.781E+10-15.4881 28818. 0.000 15.660 0.000939 457344. -5805.4508 -0.000256 0.000 6.785E+10-7.8803 29196. 0.000 15.950 8.991E-05 437102. -5820.4921 -0.000233 0.000 6.790E+10-0.7641 29574. 0.000 16.240 -0.000682 416850. -5811.6154 -0.000211 0.000 6.794E+105.8656 29952. 0.000 16.530 -0.001379 396668. -5780.5027 -0.000190 0.000 6.798E+1012.0152 30329. 0.000 16.820 -0.002005 376631. -5728.8109 -0.000170 0.000 6.802E+1017.6927 30707. 0.000 17.110 -0.002564 356807. -5658.1669 -0.000152 0.000 6.807E+1022.9073 31085. 0.000 17.400 -0.003060 337261. -5570.1635 -0.000134 0.000 6.812E+1027.6694 31463. 0.000 17.690 -0.003496 318048. -5466.3552 -0.000117 0.000 6.815E+1031.9905 31841. 0.000 17.980 -0.003876 299223. -5348.2552 -0.000101 0.000 6.818E+1035.8831 32219. 0.000 18.270 -0.004202 280832. -5217.3320 -8.660E-05 0.000 6.822E+1039.3602 32597. 0.000 18.560 -0.004479 262916. -5075.0069 -7.274E-05 0.000 6.827E+1042.4358 32974. 0.000 18.850 -0.004708 245515. -4922.6519 -5.978E-05 0.000 6.830E+1045.1245 33352. 0.000 19.140 -0.004895 228659. -4761.5876 -4.770E-05 0.000 6.833E+1047.4412 33730. 0.000 19.430 -0.005040 212377. -4593.0821 -3.648E-05 0.000 6.836E+1049.4011 34108. 0.000 19.720 -0.005148 196694. -4418.3497 -2.607E-05 0.000 6.839E+1051.0198 34486. 0.000 20.010 -0.005222 181627. -4238.5505 -1.644E-05 0.000 6.843E+1052.3131 34864. 0.000 20.300 -0.005263 167194. -4054.7892 -7.577E-06 0.000 6.847E+1053.2968 35241. 0.000 20.590 -0.005275 153407. -3868.1159 5.704E-07 0.000 6.848E+1053.9867 35619. 0.000 20.880 -0.005259 140272. -3679.5255 8.032E-06 0.000 6.850E+1054.3986 35997. 0.000 21.170 -0.005219 127797. -3489.9589 1.484E-05 0.000 6.852E+1054.5478 36375. 0.000 21.460 -0.005156 115981. -3300.3033 2.103E-05 0.000 6.854E+1054.4497 36753. 0.000 21.750 -0.005072 104825. -3111.3934 2.664E-05 0.000 6.856E+1054.1193 37131. 0.000 22.040 -0.004970 94324. -2924.0121 3.169E-05 0.000 6.859E+1053.5711 37508. 0.000 22.330 -0.004852 84472. -2738.8922 3.622E-05 0.000 6.862E+1052.8196 37886. 0.000 22.620 -0.004718 75259. -2556.7179 4.027E-05 0.000 6.862E+1051.8783 38264. 0.000 22.910 -0.004571 66674. -2378.1261 4.387E-05 0.000 6.862E+1050.7606 38642. 0.000 23.200 -0.004413 58704. -2203.7090 4.705E-05 0.000 6.862E+1049.4791 39020. 0.000 23.490 -0.004244 51333. -2034.0157 4.984E-05 0.000 6.862E+1048.0458 39398. 0.000

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existing phase2 87.lp6o 23.780 -0.004066 44544. -1869.5541 5.227E-05 0.000 6.862E+1046.4723 39775. 0.000 24.070 -0.003880 38317. -1710.7933 5.437E-05 0.000 6.862E+1044.7695 40153. 0.000 24.360 -0.003687 32633. -1558.1656 5.617E-05 0.000 6.862E+1042.9475 40531. 0.000 24.650 -0.003489 27469. -1412.0690 5.770E-05 0.000 6.862E+1041.0161 40909. 0.000 24.940 -0.003286 22801. -1272.8689 5.897E-05 0.000 6.862E+1038.9840 41287. 0.000 25.230 -0.003079 18605. -1128.3688 6.002E-05 0.000 6.862E+1044.0621 49806. 0.000 25.520 -0.002868 14943. -979.6224 6.087E-05 0.000 6.862E+1041.4244 50261. 0.000 25.810 -0.002655 11783. -840.2176 6.155E-05 0.000 6.862E+1038.6933 50717. 0.000 26.100 -0.002440 9091.0543 -710.4675 6.208E-05 0.000 6.862E+1035.8757 51172. 0.000 26.390 -0.002223 6833.6938 -590.6619 6.248E-05 0.000 6.862E+1032.9781 51628. 0.000 26.680 -0.002005 4975.6989 -481.0702 6.278E-05 0.000 6.862E+1030.0056 52083. 0.000 26.970 -0.001786 3481.0752 -381.9452 6.300E-05 0.000 6.862E+1026.9628 52538. 0.000 27.260 -0.001566 2312.9758 -293.5250 6.314E-05 0.000 6.862E+1023.8534 52994. 0.000 27.550 -0.001346 1433.7461 -216.0366 6.324E-05 0.000 6.862E+1020.6802 53449. 0.000 27.840 -0.001126 804.9593 -149.6979 6.330E-05 0.000 6.862E+1017.4455 53905. 0.000 28.130 -0.000906 387.4435 -94.7199 6.333E-05 0.000 6.862E+1014.1510 54360. 0.000 28.420 -0.000686 141.3015 -51.3090 6.334E-05 0.000 6.862E+1010.7978 54815. 0.000 28.710 -0.000465 25.9245 -19.6685 6.334E-05 0.000 6.862E+107.3864 55271. 0.000 29.000 -0.000245 0.000 0.000 6.334E-05 0.000 6.862E+103.9173 27863. 0.000

* This analysis makes computations of pile response using nonlinear moment-curvaturerelationships. The above values of total stress are computed for combined axial and bending stress in elastic sections and do not equal actual stresses in concrete and steel in the range of nonlinear bending.

Output Summary for Load Case No. 10:

Pile-head deflection = 0.2000000 inchesComputed slope at pile head = -0.0000105 radiansMaximum bending moment = -1648585. inch-lbsMaximum shear force = 38697. lbsDepth of maximum bending moment = 0.000000 inches below pile headDepth of maximum shear force = 0.000000 inches below pile headNumber of iterations = 35Number of zero deflection points = 1

-------------------------------------------------------------------------------- Computed Values of Pile Loading and Deflection for Lateral Loading for Load Case Number 11

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existing phase2 87.lp6o--------------------------------------------------------------------------------

Pile-head conditions are Displacement and Pile-head Rotation (Loading Type 5)Displacement of pile head = 0.300000 inchesRotation of pile head = 0.000E+00 radiansAxial load on pile head = 10000.000 lbs

Depth Deflect. Bending Shear Slope Total Bending Soil Res. Soil Spr. Distrib. X y Moment Force S Stress Stiffness p Es*h Lat. Load feet inches in-lbs lbs radians psi* lb-in^2 lb/in lb/inch lb/inch ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- 0.00 0.3000 -2353486. 54774. 0.000 0.000 2.145E+10-417.0464 2418.8688 0.000 0.290 0.2993 -2165518. 53250. -0.000367 0.000 2.145E+10-438.0637 5092.8184 0.000 0.580 0.2974 -1982843. 51692. -0.000701 0.000 2.174E+10-457.1046 5347.8991 0.000 0.870 0.2945 -1805693. 50072. -0.001003 0.000 2.189E+10-474.0906 5602.9798 0.000 1.160 0.2905 -1634274. 48396. -0.001276 0.000 2.204E+10-488.9564 5858.0605 0.000 1.450 0.2856 -1468768. 46672. -0.001520 0.000 2.220E+10-501.6600 6113.1412 0.000 1.740 0.2799 -1309329. 44908. -0.001737 0.000 2.237E+10-512.1807 6368.2219 0.000 2.030 0.2735 -1156085. 43111. -0.001928 0.000 2.255E+10-520.5181 6623.3027 0.000 2.320 0.2665 -1009139. 41289. -0.002094 0.000 2.276E+10-526.6904 6878.3834 0.000 2.610 0.2589 -868566. 39449. -0.002237 0.000 2.300E+10-530.7330 7133.4641 0.000 2.900 0.2509 -734416. 37599. -0.002358 0.000 2.330E+10-532.6969 7388.5448 0.000 3.190 0.2425 -606714. 35745. -0.002428 0.000 6.753E+10-532.6476 7643.6255 0.000 3.480 0.2340 -485460. 33894. -0.002456 0.000 6.779E+10-531.1206 7898.7062 0.000 3.770 0.2254 -370638. 32051. -0.002478 0.000 6.804E+10-528.1436 8153.7869 0.000 4.060 0.2168 -262212. 30221. -0.002494 0.000 6.827E+10-523.7479 8408.8677 0.000 4.350 0.2080 -160127. 28408. -0.002505 0.000 6.847E+10-517.9673 8663.9484 0.000 4.640 0.1993 -64315. 26618. -0.002511 0.000 6.862E+10-510.8381 8919.0291 0.000 4.930 0.1906 25310. 24855. -0.002512 0.000 6.862E+10-502.3990 9174.1098 0.000 5.220 0.1818 108851. 23124. -0.002508 0.000 6.855E+10-492.6903 9429.1905 0.000 5.510 0.1731 186426. 21428. -0.002501 0.000 6.842E+10-481.7540 9684.2712 0.000 5.800 0.1644 258165. 19773. -0.002490 0.000 6.828E+10-469.6338 9939.3519 0.000 6.090 0.1558 324217. 18161. -0.002475 0.000 6.814E+10-456.3742 10194. 0.000 6.380 0.1472 384742. 16598. -0.002457 0.000 6.801E+10-442.0210 10450. 0.000 6.670 0.1387 439912. 15087. -0.002435 0.000 6.789E+10-426.6203 10705. 0.000

Page 51

existing phase2 87.lp6o 6.960 0.1303 489916. 13631. -0.002412 0.000 6.778E+10-410.2185 10960. 0.000 7.250 0.1219 534950. 12233. -0.002385 0.000 6.768E+10-392.8621 11215. 0.000 7.540 0.1137 575226. 10898. -0.002357 0.000 6.760E+10-374.5973 11470. 0.000 7.830 0.1055 610965. 9627.7001 -0.002326 0.000 6.752E+10-355.4698 11725. 0.000 8.120 0.0975 642397. 8425.3693 -0.002294 0.000 6.745E+10-335.5249 11980. 0.000 8.410 0.0895 669765. 7293.7921 -0.002255 0.000 5.289E+10-314.8068 12235. 0.000 8.700 0.0818 693319. 6235.3774 -0.002182 0.000 2.341E+10-293.4775 12490. 0.000 8.990 0.0744 713315. 5250.8856 -0.002077 0.000 2.336E+10-272.3224 12745. 0.000 9.280 0.0673 730009. 4339.5001 -0.001969 0.000 2.331E+10-251.4624 13000. 0.000 9.570 0.0606 743655. 3499.9903 -0.001859 0.000 2.328E+10-231.0145 13255. 0.000 9.860 0.0544 754499. 2730.7254 -0.001747 0.000 2.325E+10-211.0918 13510. 0.000 10.150 0.0485 762782. 1764.3214 -0.001634 0.000 2.323E+10-344.3128 24711. 0.000 10.440 0.0430 766892. 624.1041 -0.001519 0.000 2.322E+10-310.9846 25166. 0.000 10.730 0.0379 767232. -402.7569 -0.001404 0.000 2.322E+10-279.1654 25622. 0.000 11.020 0.0332 764187. -1321.7885 -0.001289 0.000 2.323E+10-249.0137 26077. 0.000 11.310 0.0289 758122. -2139.0442 -0.001175 0.000 2.324E+10-220.6735 26533. 0.000 11.600 0.0251 749381. -2861.0543 -0.001062 0.000 2.326E+10-194.2748 26988. 0.000 11.890 0.0215 738283. -3494.7774 -0.000951 0.000 2.329E+10-169.9339 27443. 0.000 12.180 0.0184 725123. -4047.5544 -0.000842 0.000 2.332E+10-147.7540 27899. 0.000 12.470 0.0157 710170. -4527.0630 -0.000735 0.000 2.336E+10-127.8256 28354. 0.000 12.760 0.0133 693666. -4941.2748 -0.000631 0.000 2.341E+10-110.2271 28810. 0.000 13.050 0.0113 675823. -5298.4134 -0.000540 0.000 3.049E+10-95.0250 29265. 0.000 13.340 0.009553 656827. -5605.7202 -0.000485 0.000 6.740E+10-81.5881 29720. 0.000 13.630 0.007925 636841. -5867.2518 -0.000452 0.000 6.746E+10-68.7174 30176. 0.000 13.920 0.006411 616022. -6085.0028 -0.000419 0.000 6.751E+10-56.4268 30631. 0.000 14.210 0.005007 594519. -6261.0107 -0.000388 0.000 6.756E+10-44.7271 31087. 0.000 14.500 0.003710 572472. -6397.3452 -0.000358 0.000 6.760E+10-33.6260 31542. 0.000 14.790 0.002515 550018. -6496.0979 -0.000329 0.000 6.765E+10-23.1284 31997. 0.000 15.080 0.001419 527282. -6556.5247 -0.000301 0.000 6.770E+10-11.5997 28440. 0.000 15.370 0.000418 504406. -6582.7258 -0.000275 0.000 6.776E+10-3.4584 28818. 0.000 15.660 -0.000494 481486. -6581.5326 -0.000250 0.000 6.780E+104.1441 29196. 0.000 15.950 -0.001320 458615. -6554.8100 -0.000225 0.000 6.785E+10

Page 52

existing phase2 87.lp6o11.2137 29574. 0.000 16.240 -0.002063 435880. -6504.3994 -0.000203 0.000 6.790E+1017.7580 29952. 0.000 16.530 -0.002729 413359. -6432.1126 -0.000181 0.000 6.795E+1023.7862 30329. 0.000 16.820 -0.003322 391125. -6339.7269 -0.000160 0.000 6.799E+1029.3090 30707. 0.000 17.110 -0.003844 369246. -6228.9810 -0.000141 0.000 6.804E+1034.3381 31085. 0.000 17.400 -0.004301 347781. -6101.5701 -0.000122 0.000 6.809E+1038.8865 31463. 0.000 17.690 -0.004696 326787. -5959.1429 -0.000105 0.000 6.813E+1042.9682 31841. 0.000 17.980 -0.005033 306313. -5803.2979 -8.901E-05 0.000 6.817E+1046.5979 32219. 0.000 18.270 -0.005316 286402. -5635.5811 -7.389E-05 0.000 6.821E+1049.7911 32597. 0.000 18.560 -0.005547 267094. -5457.4837 -5.978E-05 0.000 6.826E+1052.5638 32974. 0.000 18.850 -0.005732 248422. -5270.4399 -4.664E-05 0.000 6.830E+1054.9327 33352. 0.000 19.140 -0.005872 230415. -5075.8256 -3.444E-05 0.000 6.833E+1056.9146 33730. 0.000 19.430 -0.005971 213097. -4874.9576 -2.315E-05 0.000 6.836E+1058.5268 34108. 0.000 19.720 -0.006033 196487. -4669.0927 -1.273E-05 0.000 6.839E+1059.7864 34486. 0.000 20.010 -0.006060 180601. -4459.4274 -3.137E-06 0.000 6.843E+1060.7109 34864. 0.000 20.300 -0.006055 165450. -4247.0978 5.660E-06 0.000 6.847E+1061.3176 35241. 0.000 20.590 -0.006021 151041. -4033.1802 1.370E-05 0.000 6.848E+1061.6236 35619. 0.000 20.880 -0.005960 137378. -3818.6913 2.103E-05 0.000 6.850E+1061.6459 35997. 0.000 21.170 -0.005874 124461. -3604.5895 2.768E-05 0.000 6.852E+1061.4011 36375. 0.000 21.460 -0.005767 112288. -3391.7761 3.369E-05 0.000 6.854E+1060.9054 36753. 0.000 21.750 -0.005640 100852. -3181.0966 3.910E-05 0.000 6.857E+1060.1748 37131. 0.000 22.040 -0.005495 90145. -2973.3417 4.395E-05 0.000 6.860E+1059.2246 37508. 0.000 22.330 -0.005334 80155. -2769.2498 4.826E-05 0.000 6.862E+1058.0696 37886. 0.000 22.620 -0.005159 70868. -2569.5087 5.209E-05 0.000 6.862E+1056.7242 38264. 0.000 22.910 -0.004971 62267. -2374.7574 5.547E-05 0.000 6.862E+1055.2018 38642. 0.000 23.200 -0.004773 54335. -2185.5891 5.843E-05 0.000 6.862E+1053.5156 39020. 0.000 23.490 -0.004565 47052. -2002.5529 6.100E-05 0.000 6.862E+1051.6776 39398. 0.000 23.780 -0.004348 40393. -1826.1565 6.321E-05 0.000 6.862E+1049.6996 39775. 0.000 24.070 -0.004125 34337. -1656.8686 6.511E-05 0.000 6.862E+1047.5923 40153. 0.000 24.360 -0.003895 28857. -1495.1215 6.671E-05 0.000 6.862E+1045.3659 40531. 0.000 24.650 -0.003660 23926. -1341.3131 6.805E-05 0.000 6.862E+1043.0297 40909. 0.000 24.940 -0.003421 19517. -1195.8105 6.915E-05 0.000 6.862E+1040.5925 41287. 0.000

Page 53

existing phase2 87.lp6o 25.230 -0.003179 15599. -1046.0102 7.004E-05 0.000 6.862E+1045.4996 49806. 0.000 25.520 -0.002934 12232. -893.1079 7.075E-05 0.000 6.862E+1042.3753 50261. 0.000 25.810 -0.002687 9377.8163 -751.2445 7.130E-05 0.000 6.862E+1039.1554 50717. 0.000 26.100 -0.002438 6998.0900 -620.7413 7.171E-05 0.000 6.862E+1035.8464 51172. 0.000 26.390 -0.002188 5052.4658 -501.8986 7.202E-05 0.000 6.862E+1032.4540 51628. 0.000 26.680 -0.001937 3499.8634 -394.9988 7.223E-05 0.000 6.862E+1028.9827 52083. 0.000 26.970 -0.001685 2298.2470 -300.3095 7.238E-05 0.000 6.862E+1025.4364 52538. 0.000 27.260 -0.001433 1404.6715 -218.0868 7.248E-05 0.000 6.862E+1021.8180 52994. 0.000 27.550 -0.001180 775.3189 -148.5773 7.253E-05 0.000 6.862E+1018.1299 53449. 0.000 27.840 -0.000928 365.5252 -92.0212 7.256E-05 0.000 6.862E+1014.3736 53905. 0.000 28.130 -0.000675 129.8010 -48.6538 7.257E-05 0.000 6.862E+1010.5502 54360. 0.000 28.420 -0.000423 21.8439 -18.7074 7.258E-05 0.000 6.862E+106.6604 54815. 0.000 28.710 -0.000170 -5.4535 -2.4127 7.258E-05 0.000 6.862E+102.7044 55271. 0.000 29.000 8.229E-05 0.000 0.000 7.258E-05 0.000 6.862E+10-1.3177 27863. 0.000

* This analysis makes computations of pile response using nonlinear moment-curvaturerelationships. The above values of total stress are computed for combined axial and bending stress in elastic sections and do not equal actual stresses in concrete and steel in the range of nonlinear bending.

Output Summary for Load Case No. 11:

Pile-head deflection = 0.3000000 inchesComputed slope at pile head = -0.0000152 radiansMaximum bending moment = -2353486. inch-lbsMaximum shear force = 54774. lbsDepth of maximum bending moment = 0.000000 inches below pile headDepth of maximum shear force = 0.000000 inches below pile headNumber of iterations = 29Number of zero deflection points = 2

-------------------------------------------------------------------------------- Computed Values of Pile Loading and Deflection for Lateral Loading for Load Case Number 12--------------------------------------------------------------------------------

Pile-head conditions are Displacement and Pile-head Rotation (Loading Type 5)Displacement of pile head = 0.500000 inchesRotation of pile head = 0.000E+00 radiansAxial load on pile head = 10000.000 lbs

Depth Deflect. Bending Shear Slope Total Bending Soil Res. Soil Spr. Distrib. X y Moment Force S Stress Stiffness p

Page 54

existing phase2 87.lp6o Es*h Lat. Load feet inches in-lbs lbs radians psi* lb-in^2 lb/in lb/inch lb/inch ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- 0.00 0.5000 -3727400. 86020. 0.000 0.000 1.963E+10-668.4651 2326.2585 0.000 0.290 0.4989 -3432210. 83622. -0.000635 0.000 1.963E+10-689.0738 4807.0063 0.000 0.580 0.4956 -3145344. 81190. -0.001202 0.000 2.083E+10-709.0538 4978.9926 0.000 0.870 0.4905 -2867047. 78673. -0.001701 0.000 2.105E+10-737.5429 5232.8501 0.000 1.160 0.4837 -2597665. 76063. -0.002151 0.000 2.126E+10-762.3445 5484.2377 0.000 1.450 0.4755 -2337500. 73374. -0.002553 0.000 2.146E+10-783.0236 5730.4359 0.000 1.740 0.4660 -2086805. 70621. -0.002910 0.000 2.166E+10-799.1519 5968.2590 0.000 2.030 0.4553 -1845777. 67820. -0.003225 0.000 2.186E+10-810.3103 6193.9697 0.000 2.320 0.4435 -1614551. 64990. -0.003499 0.000 2.206E+10-816.0895 6403.1795 0.000 2.610 0.4309 -1393200. 62129. -0.003735 0.000 2.228E+10-828.4393 6690.4474 0.000 2.900 0.4175 -1181874. 59195. -0.003935 0.000 2.252E+10-857.7358 7148.9846 0.000 3.190 0.4035 -980929. 56163. -0.004102 0.000 2.280E+10-884.8803 7631.3492 0.000 3.480 0.3890 -790695. 53087. -0.004236 0.000 2.316E+10-882.8927 7898.7062 0.000 3.770 0.3740 -611149. 50026. -0.004311 0.000 6.752E+10-876.3824 8153.7869 0.000 4.060 0.3590 -442215. 46992. -0.004338 0.000 6.789E+10-867.4160 8408.8677 0.000 4.350 0.3438 -283785. 43993. -0.004357 0.000 6.822E+10-856.0458 8663.9484 0.000 4.640 0.3287 -135722. 41038. -0.004367 0.000 6.850E+10-842.3276 8919.0291 0.000 4.930 0.3134 2140.2196 38134. -0.004371 0.000 6.862E+10-826.3199 9174.1098 0.000 5.220 0.2982 129996. 35290. -0.004367 0.000 6.851E+10-808.0834 9429.1905 0.000 5.510 0.2830 248065. 32514. -0.004358 0.000 6.830E+10-787.6811 9684.2712 0.000 5.800 0.2679 356594. 29812. -0.004342 0.000 6.807E+10-765.1780 9939.3519 0.000 6.090 0.2528 455856. 27192. -0.004322 0.000 6.785E+10-740.6409 10194. 0.000 6.380 0.2378 546148. 24660. -0.004296 0.000 6.766E+10-714.1374 10450. 0.000 6.670 0.2229 627790. 22224. -0.004266 0.000 6.748E+10-685.7359 10705. 0.000 6.960 0.2081 701127. 19891. -0.004197 0.000 2.339E+10-655.5049 10960. 0.000 7.250 0.1937 766522. 17664. -0.004088 0.000 2.322E+10-624.2760 11215. 0.000 7.540 0.1797 824352. 15547. -0.003968 0.000 2.309E+10-592.2501 11470. 0.000 7.830 0.1661 875006. 13543. -0.003840 0.000 2.299E+10-559.6248 11725. 0.000 8.120 0.1530 918878. 11653. -0.003704 0.000 2.291E+10-526.5936 11980. 0.000

Page 55

existing phase2 87.lp6o 8.410 0.1403 956367. 9878.1512 -0.003561 0.000 2.284E+10-493.3452 12235. 0.000 8.700 0.1282 987878. 8219.2216 -0.003413 0.000 2.279E+10-460.0626 12490. 0.000 8.990 0.1166 1013811. 6675.8669 -0.003260 0.000 2.275E+10-426.9228 12745. 0.000 9.280 0.1055 1034568. 5247.2935 -0.003103 0.000 2.272E+10-394.0964 13000. 0.000 9.570 0.0950 1050548. 3932.1263 -0.002943 0.000 2.270E+10-361.7468 13255. 0.000 9.860 0.0850 1062141. 2728.4332 -0.002781 0.000 2.268E+10-330.0308 13510. 0.000 10.150 0.0756 1069731. 1219.9384 -0.002618 0.000 2.267E+10-536.9202 24711. 0.000 10.440 0.0668 1070814. -554.7294 -0.002453 0.000 2.267E+10-483.0039 25166. 0.000 10.730 0.0585 1066041. -2145.0790 -0.002289 0.000 2.267E+10-430.9902 25622. 0.000 11.020 0.0509 1056043. -3558.0870 -0.002127 0.000 2.269E+10-381.0834 26077. 0.000 11.310 0.0437 1041425. -4801.3985 -0.001966 0.000 2.271E+10-333.4635 26533. 0.000 11.600 0.0372 1022763. -5883.2446 -0.001808 0.000 2.274E+10-288.2872 26988. 0.000 11.890 0.0312 1000603. -6812.3628 -0.001653 0.000 2.277E+10-245.6888 27443. 0.000 12.180 0.0257 975464. -7597.9205 -0.001502 0.000 2.281E+10-205.7811 27899. 0.000 12.470 0.0207 947826. -8249.4421 -0.001356 0.000 2.286E+10-168.6566 28354. 0.000 12.760 0.0162 918142. -8776.7414 -0.001214 0.000 2.291E+10-134.3889 28810. 0.000 13.050 0.0123 886825. -9189.8567 -0.001077 0.000 2.297E+10-103.0336 29265. 0.000 13.340 0.008739 854255. -9498.9913 -0.000945 0.000 2.303E+10-74.6299 29720. 0.000 13.630 0.005674 820778. -9714.4586 -0.000819 0.000 2.310E+10-49.2019 30176. 0.000 13.920 0.003040 786700. -9846.6314 -0.000698 0.000 2.317E+10-26.7595 30631. 0.000 14.210 0.000817 752294. -9905.8955 -0.000582 0.000 2.325E+10-7.3003 31087. 0.000 14.500 -0.001014 717795. -9902.6081 -0.000473 0.000 2.334E+109.1897 31542. 0.000 14.790 -0.002473 683404. -9847.0592 -0.000368 0.000 2.344E+1022.7349 31997. 0.000 15.080 -0.003578 649285. -9756.6171 -0.000301 0.000 6.743E+1029.2433 28440. 0.000 15.370 -0.004567 615519. -9639.9237 -0.000268 0.000 6.751E+1037.8219 28818. 0.000 15.660 -0.005446 582210. -9494.6148 -0.000237 0.000 6.758E+1045.6890 29196. 0.000 15.950 -0.006220 549453. -9323.1391 -0.000208 0.000 6.765E+1052.8602 29574. 0.000 16.240 -0.006896 517336. -9127.8880 -0.000181 0.000 6.773E+1059.3531 29952. 0.000 16.530 -0.007479 485936. -8911.1893 -0.000155 0.000 6.779E+1065.1864 30329. 0.000 16.820 -0.007976 455324. -8675.3028 -0.000131 0.000 6.786E+1070.3805 30707. 0.000 17.110 -0.008391 425565. -8422.4165 -0.000108 0.000 6.793E+1074.9565 31085. 0.000 17.400 -0.008731 396712. -8154.6423 -8.739E-05 0.000 6.798E+10

Page 56

existing phase2 87.lp6o78.9367 31463. 0.000 17.690 -0.009000 368815. -7874.0138 -6.781E-05 0.000 6.804E+1082.3440 31841. 0.000 17.980 -0.009203 341914. -7582.4838 -4.964E-05 0.000 6.811E+1085.2020 32219. 0.000 18.270 -0.009345 316044. -7281.9223 -3.284E-05 0.000 6.815E+1087.5345 32597. 0.000 18.560 -0.009431 291234. -6974.1157 -1.734E-05 0.000 6.820E+1089.3659 32974. 0.000 18.850 -0.009466 267505. -6660.7658 -3.088E-06 0.000 6.826E+1090.7203 33352. 0.000 19.140 -0.009453 244875. -6343.4899 9.969E-06 0.000 6.830E+1091.6222 33730. 0.000 19.430 -0.009396 223354. -6023.8208 2.189E-05 0.000 6.834E+1092.0957 34108. 0.000 19.720 -0.009300 202948. -5703.2075 3.274E-05 0.000 6.838E+1092.1648 34486. 0.000 20.010 -0.009169 183657. -5383.0166 4.258E-05 0.000 6.843E+1091.8529 34864. 0.000 20.300 -0.009004 165479. -5064.5337 5.145E-05 0.000 6.847E+1091.1833 35241. 0.000 20.590 -0.008810 148405. -4748.9645 5.943E-05 0.000 6.849E+1090.1783 35619. 0.000 20.880 -0.008590 132422. -4437.4382 6.656E-05 0.000 6.851E+1088.8598 35997. 0.000 21.170 -0.008347 117515. -4131.0089 7.291E-05 0.000 6.853E+1087.2489 36375. 0.000 21.460 -0.008083 103665. -3830.6592 7.853E-05 0.000 6.856E+1085.3659 36753. 0.000 21.750 -0.007801 90848. -3537.3023 8.346E-05 0.000 6.860E+1083.2301 37131. 0.000 22.040 -0.007502 79040. -3251.7854 8.777E-05 0.000 6.862E+1080.8601 37508. 0.000 22.330 -0.007190 68210. -2974.8929 9.150E-05 0.000 6.862E+1078.2735 37886. 0.000 22.620 -0.006865 58328. -2707.3504 9.471E-05 0.000 6.862E+1075.4866 38264. 0.000 22.910 -0.006531 49360. -2449.8275 9.744E-05 0.000 6.862E+1072.5150 38642. 0.000 23.200 -0.006187 41270. -2202.9423 9.974E-05 0.000 6.862E+1069.3730 39020. 0.000 23.490 -0.005836 34021. -1967.2644 0.000102 0.000 6.862E+1066.0740 39398. 0.000 23.780 -0.005480 27571. -1743.3190 0.000103 0.000 6.862E+1062.6302 39775. 0.000 24.070 -0.005118 21880. -1531.5906 0.000104 0.000 6.862E+1059.0528 40153. 0.000 24.360 -0.004753 16904. -1332.5264 0.000105 0.000 6.862E+1055.3519 40531. 0.000 24.650 -0.004384 12598. -1146.5405 0.000106 0.000 6.862E+1051.5365 40909. 0.000 24.940 -0.004013 8916.7708 -974.0171 0.000107 0.000 6.862E+1047.6148 41287. 0.000 25.230 -0.003641 5811.7859 -800.4923 0.000107 0.000 6.862E+1052.1121 49806. 0.000 25.520 -0.003268 3337.8889 -627.6939 0.000107 0.000 6.862E+1047.1974 50261. 0.000 25.810 -0.002894 1435.5650 -472.1836 0.000107 0.000 6.862E+1042.1764 50717. 0.000 26.100 -0.002520 44.0111 -334.3232 0.000108 0.000 6.862E+1037.0538 51172. 0.000 26.390 -0.002146 -898.8069 -214.4599 0.000107 0.000 6.862E+1031.8332 51628. 0.000

Page 57

existing phase2 87.lp6o 26.680 -0.001772 -1456.1111 -112.9307 0.000107 0.000 6.862E+1026.5170 52083. 0.000 26.970 -0.001398 -1692.2812 -30.0652 0.000107 0.000 6.862E+1021.1068 52538. 0.000 27.260 -0.001025 -1672.8361 33.8107 0.000107 0.000 6.862E+1015.6034 52994. 0.000 27.550 -0.000652 -1464.4243 78.3725 0.000107 0.000 6.862E+1010.0068 53449. 0.000 27.840 -0.000279 -1134.8235 103.2951 0.000107 0.000 6.862E+104.3165 53905. 0.000 28.130 9.399E-05 -752.9456 108.2513 0.000107 0.000 6.862E+10-1.4682 54360. 0.000 28.420 0.000467 -388.8466 92.9105 0.000107 0.000 6.862E+10-7.3483 54815. 0.000 28.710 0.000839 -113.7384 56.9390 0.000107 0.000 6.862E+10-13.3249 55271. 0.000 29.000 0.001211 0.000 0.000 0.000107 0.000 6.862E+10-19.3987 27863. 0.000

* This analysis makes computations of pile response using nonlinear moment-curvaturerelationships. The above values of total stress are computed for combined axial and bending stress in elastic sections and do not equal actual stresses in concrete and steel in the range of nonlinear bending.

Output Summary for Load Case No. 12:

Pile-head deflection = 0.5000000 inchesComputed slope at pile head = -0.0000262 radiansMaximum bending moment = -3727400. inch-lbsMaximum shear force = 86020. lbsDepth of maximum bending moment = 0.000000 inches below pile headDepth of maximum shear force = 0.000000 inches below pile headNumber of iterations = 24Number of zero deflection points = 2

-------------------------------------------------------------------------------- Computed Values of Pile Loading and Deflection for Lateral Loading for Load Case Number 13--------------------------------------------------------------------------------

Pile-head conditions are Displacement and Pile-head Rotation (Loading Type 5)Displacement of pile head = 0.750000 inchesRotation of pile head = 0.000E+00 radiansAxial load on pile head = 10000.000 lbs

Depth Deflect. Bending Shear Slope Total Bending Soil Res. Soil Spr. Distrib. X y Moment Force S Stress Stiffness p Es*h Lat. Load feet inches in-lbs lbs radians psi* lb-in^2 lb/in lb/inch lb/inch ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- 0.00 0.7500 -4631828. 110839. 0.000 0.000 9.187E+09-808.8662 1876.5695 0.000 0.290 0.7469 -4251153. 107922. -0.001682 0.000 9.187E+09-838.3062 3905.6379 0.000 0.580 0.7383 -3880575. 104957. -0.002841 0.000 1.907E+10

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existing phase2 87.lp6o-865.8868 4081.4350 0.000 0.870 0.7272 -3520458. 101876. -0.003497 0.000 2.030E+10-904.2553 4327.4700 0.000 1.160 0.7139 -3171271. 98670. -0.004064 0.000 2.080E+10-938.5510 4574.7718 0.000 1.450 0.6989 -2833432. 95352. -0.004563 0.000 2.108E+10-968.2817 4821.4358 0.000 1.740 0.6822 -2507303. 91940. -0.005002 0.000 2.133E+10-992.9510 5065.2717 0.000 2.030 0.6641 -2193185. 88451. -0.005383 0.000 2.157E+10 -1012.0745 5303.6878 0.000 2.320 0.6447 -1891311. 84906. -0.005711 0.000 2.182E+10 -1025.1825 5533.6173 0.000 2.610 0.6243 -1601841. 81306. -0.005988 0.000 2.207E+10 -1043.8488 5818.4731 0.000 2.900 0.6030 -1325005. 77614. -0.006218 0.000 2.235E+10 -1078.1729 6221.8529 0.000 3.190 0.5810 -1061218. 73807. -0.006402 0.000 2.268E+10 -1109.5319 6645.2049 0.000 3.480 0.5585 -810863. 69897. -0.006545 0.000 2.312E+10 -1137.7564 7089.5446 0.000 3.770 0.5355 -574282. 65894. -0.006620 0.000 6.760E+10 -1162.6996 7555.9797 0.000 4.060 0.5124 -351781. 61810. -0.006644 0.000 6.808E+10 -1184.5239 8044.6949 0.000 4.350 0.4893 -143624. 57655. -0.006657 0.000 6.849E+10 -1203.0454 8557.1384 0.000 4.640 0.4661 49964. 53484. -0.006659 0.000 6.862E+10 -1194.5184 8919.0291 0.000 4.930 0.4429 229085. 49373. -0.006652 0.000 6.833E+10 -1167.6004 9174.1098 0.000 5.220 0.4198 394066. 45363. -0.006636 0.000 6.799E+10 -1137.3958 9429.1905 0.000 5.510 0.3967 545272. 41463. -0.006612 0.000 6.766E+10 -1103.9958 9684.2712 0.000 5.800 0.3738 683107. 37684. -0.006547 0.000 2.344E+10 -1067.4942 9939.3519 0.000 6.090 0.3511 808011. 34037. -0.006436 0.000 2.313E+10 -1028.6604 10194. 0.000 6.380 0.3290 920453. 30528. -0.006305 0.000 2.291E+10-987.7829 10450. 0.000 6.670 0.3073 1020928. 27165. -0.006157 0.000 2.274E+10-945.1499 10705. 0.000 6.960 0.2861 1109951. 23953. -0.005994 0.000 2.261E+10-901.0481 10960. 0.000 7.250 0.2655 1188056. 20896. -0.005816 0.000 2.251E+10-855.7608 11215. 0.000 7.540 0.2456 1255792. 17998. -0.005627 0.000 2.243E+10-809.5658 11470. 0.000 7.830 0.2264 1313716. 15262. -0.005427 0.000 2.236E+10-762.7349 11725. 0.000 8.120 0.2079 1362396. 12690. -0.005219 0.000 2.231E+10-715.5320 11980. 0.000 8.410 0.1901 1402403. 10283. -0.005003 0.000 2.227E+10-668.2124 12235. 0.000 8.700 0.1730 1434311. 8039.2872 -0.004781 0.000 2.223E+10-621.0220 12490. 0.000 8.990 0.1568 1458690. 5959.6078 -0.004555 0.000 2.221E+10-574.1961 12745. 0.000 9.280 0.1413 1476107. 4041.8568 -0.004325 0.000 2.219E+10-527.9596 13000. 0.000 9.570 0.1267 1487122. 2283.6122 -0.004092 0.000 2.218E+10-482.5258 13255. 0.000

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existing phase2 87.lp6o 9.860 0.1128 1492286. 681.7288 -0.003859 0.000 2.218E+10-438.0969 13510. 0.000 10.150 0.0998 1492135. -1313.9268 -0.003625 0.000 2.218E+10-708.8317 24711. 0.000 10.440 0.0876 1483393. -3649.8015 -0.003391 0.000 2.219E+10-633.6250 25166. 0.000 10.730 0.0762 1466969. -5728.7721 -0.003160 0.000 2.220E+10-561.1856 25622. 0.000 11.020 0.0656 1443741. -7560.8970 -0.002932 0.000 2.223E+10-491.7597 26077. 0.000 11.310 0.0558 1414549. -9157.0307 -0.002708 0.000 2.226E+10-425.5585 26533. 0.000 11.600 0.0468 1380196. -10529. -0.002490 0.000 2.229E+10-362.7595 26988. 0.000 11.890 0.0385 1341443. -11688. -0.002278 0.000 2.233E+10-303.5078 27443. 0.000 12.180 0.0309 1299006. -12647. -0.002072 0.000 2.238E+10-247.9182 27899. 0.000 12.470 0.0241 1253560. -13420. -0.001874 0.000 2.243E+10-196.0768 28354. 0.000 12.760 0.0179 1205733. -14019. -0.001683 0.000 2.249E+10-148.0427 28810. 0.000 13.050 0.0123 1156106. -14457. -0.001501 0.000 2.255E+10-103.8505 29265. 0.000 13.340 0.007437 1105216. -14748. -0.001327 0.000 2.262E+10-63.5122 29720. 0.000 13.630 0.003116 1053551. -14906. -0.001161 0.000 2.269E+10-27.0190 30176. 0.000 13.920 -0.000643 1001552. -14943. -0.001004 0.000 2.277E+105.6560 30631. 0.000 14.210 -0.003868 949617. -14873. -0.000855 0.000 2.286E+1034.5565 31087. 0.000 14.500 -0.006591 898095. -14709. -0.000714 0.000 2.295E+1059.7407 31542. 0.000 14.790 -0.008840 847292. -14464. -0.000582 0.000 2.304E+1081.2793 31997. 0.000 15.080 -0.0106 797469. -14171. -0.000458 0.000 2.315E+1086.9820 28440. 0.000 15.370 -0.0120 748695. -13846. -0.000342 0.000 2.326E+1099.6171 28818. 0.000 15.660 -0.0130 701124. -13483. -0.000234 0.000 2.339E+10109.2833 29196. 0.000 15.950 -0.0137 654872. -13091. -0.000165 0.000 6.742E+10116.0807 29574. 0.000 16.240 -0.0142 610026. -12676. -0.000133 0.000 6.752E+10122.0032 29952. 0.000 16.530 -0.0146 566655. -12243. -0.000102 0.000 6.762E+10127.0842 30329. 0.000 16.820 -0.0149 524823. -11793. -7.413E-05 0.000 6.771E+10131.3578 30707. 0.000 17.110 -0.0151 484580. -11330. -4.821E-05 0.000 6.779E+10134.8592 31085. 0.000 17.400 -0.0152 445970. -10856. -2.434E-05 0.000 6.788E+10137.6237 31463. 0.000 17.690 -0.0153 409025. -10373. -2.430E-06 0.000 6.796E+10139.6873 31841. 0.000 17.980 -0.0152 373772. -9884.7408 1.760E-05 0.000 6.803E+10141.0858 32219. 0.000 18.270 -0.0151 340226. -9392.4241 3.585E-05 0.000 6.811E+10141.8549 32597. 0.000 18.560 -0.0150 308398. -8898.4639 5.242E-05 0.000 6.817E+10142.0303 32974. 0.000 18.850 -0.0148 278289. -8404.8654 6.739E-05 0.000 6.823E+10

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existing phase2 87.lp6o141.6469 33352. 0.000 19.140 -0.0145 249895. -7913.5134 8.085E-05 0.000 6.830E+10140.7393 33730. 0.000 19.430 -0.0142 223206. -7426.1736 9.290E-05 0.000 6.834E+10139.3410 34108. 0.000 19.720 -0.0139 198203. -6944.4965 0.000104 0.000 6.839E+10137.4849 34486. 0.000 20.010 -0.0135 174865. -6470.0201 0.000113 0.000 6.845E+10135.2027 34864. 0.000 20.300 -0.0131 153164. -6004.1739 0.000121 0.000 6.848E+10132.5250 35241. 0.000 20.590 -0.0127 133067. -5548.2829 0.000129 0.000 6.851E+10129.4813 35619. 0.000 20.880 -0.0122 114539. -5103.5722 0.000135 0.000 6.854E+10126.0995 35997. 0.000 21.170 -0.0117 97537. -4671.1718 0.000140 0.000 6.858E+10122.4064 36375. 0.000 21.460 -0.0112 82017. -4252.1214 0.000145 0.000 6.862E+10118.4272 36753. 0.000 21.750 -0.0107 67932. -3847.3752 0.000149 0.000 6.862E+10114.1855 37131. 0.000 22.040 -0.0102 55229. -3457.8082 0.000152 0.000 6.862E+10109.7036 37508. 0.000 22.330 -0.009645 43855. -3084.2209 0.000154 0.000 6.862E+10105.0018 37886. 0.000 22.620 -0.009104 33752. -2727.3454 0.000156 0.000 6.862E+10100.0991 38264. 0.000 22.910 -0.008557 24862. -2387.8510 0.000158 0.000 6.862E+1095.0127 38642. 0.000 23.200 -0.008005 17122. -2066.3495 0.000159 0.000 6.862E+1089.7583 39020. 0.000 23.490 -0.007451 10469. -1763.4011 0.000160 0.000 6.862E+1084.3500 39398. 0.000 23.780 -0.006894 4837.5645 -1479.5198 0.000160 0.000 6.862E+1078.8001 39775. 0.000 24.070 -0.006337 160.4141 -1215.1795 0.000160 0.000 6.862E+1073.1196 40153. 0.000 24.360 -0.005780 -3631.2287 -970.8183 0.000160 0.000 6.862E+1067.3178 40531. 0.000 24.650 -0.005223 -6607.6196 -746.8450 0.000160 0.000 6.862E+1061.4025 40909. 0.000 24.940 -0.004668 -8840.3901 -543.6432 0.000159 0.000 6.862E+1055.3802 41287. 0.000 25.230 -0.004114 -10402. -344.8293 0.000159 0.000 6.862E+1058.8807 49806. 0.000 25.520 -0.003562 -11251. -152.8604 0.000158 0.000 6.862E+1051.4463 50261. 0.000 25.810 -0.003012 -11477. 13.0359 0.000158 0.000 6.862E+1043.8964 50717. 0.000 26.100 -0.002464 -11172. 152.4599 0.000157 0.000 6.862E+1036.2323 51172. 0.000 26.390 -0.001918 -10427. 265.0142 0.000157 0.000 6.862E+1028.4541 51628. 0.000 26.680 -0.001374 -9338.1148 350.2994 0.000156 0.000 6.862E+1020.5604 52083. 0.000 26.970 -0.000831 -8000.0009 407.9102 0.000156 0.000 6.862E+1012.5493 52538. 0.000 27.260 -0.000290 -6509.8963 437.4326 0.000155 0.000 6.862E+104.4176 52994. 0.000 27.550 0.000250 -4966.2815 438.4409 0.000155 0.000 6.862E+10-3.8381 53449. 0.000 27.840 0.000789 -3469.1384 410.4974 0.000155 0.000 6.862E+10-12.2215 53905. 0.000

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existing phase2 87.lp6o 28.130 0.001327 -2119.9959 353.1507 0.000155 0.000 6.862E+10-20.7364 54360. 0.000 28.420 0.001866 -1021.9759 265.9370 0.000155 0.000 6.862E+10-29.3864 54815. 0.000 28.710 0.002404 -279.8349 148.3814 0.000155 0.000 6.862E+10-38.1743 55271. 0.000 29.000 0.002941 0.000 0.000 0.000155 0.000 6.862E+10-47.1023 27863. 0.000

* This analysis makes computations of pile response using nonlinear moment-curvaturerelationships. The above values of total stress are computed for combined axial and bending stress in elastic sections and do not equal actual stresses in concrete and steel in the range of nonlinear bending.

Output Summary for Load Case No. 13:

Pile-head deflection = 0.7500000 inchesComputed slope at pile head = -0.0000721 radiansMaximum bending moment = -4631828. inch-lbsMaximum shear force = 110839. lbsDepth of maximum bending moment = 0.000000 inches below pile headDepth of maximum shear force = 0.000000 inches below pile headNumber of iterations = 66Number of zero deflection points = 2

-------------------------------------------------------------------------------- Computed Values of Pile Loading and Deflection for Lateral Loading for Load Case Number 14--------------------------------------------------------------------------------

Pile-head conditions are Displacement and Pile-head Rotation (Loading Type 5)Displacement of pile head = 1.000000 inchesRotation of pile head = 0.000E+00 radiansAxial load on pile head = 10000.000 lbs

Depth Deflect. Bending Shear Slope Total Bending Soil Res. Soil Spr. Distrib. X y Moment Force S Stress Stiffness p Es*h Lat. Load feet inches in-lbs lbs radians psi* lb-in^2 lb/in lb/inch lb/inch ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- 0.00 1.0000 -4634792. 124021. 0.000 0.000 4.108E+09-893.1068 1554.0058 0.000 0.290 0.9932 -4208765. 120783. -0.003746 0.000 4.108E+09-930.3686 3259.9542 0.000 0.580 0.9739 -3793881. 117476. -0.005869 0.000 1.941E+10-970.3801 3467.3201 0.000 0.870 0.9523 -3390725. 114002. -0.006495 0.000 2.058E+10 -1025.9908 3749.2006 0.000 1.160 0.9287 -2999974. 110336. -0.007031 0.000 2.094E+10 -1080.9577 4050.4464 0.000 1.450 0.9034 -2622297. 106480. -0.007495 0.000 2.124E+10 -1135.0856 4372.5572 0.000 1.740 0.8766 -2258351. 102474. -0.007893 0.000 2.152E+10 -1167.1657 4633.7648 0.000 2.030 0.8484 -1908527. 98372. -0.008228 0.000 2.180E+10

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existing phase2 87.lp6o-1190.2364 4881.8727 0.000 2.320 0.8193 -1573107. 94202. -0.008504 0.000 2.210E+10 -1206.6065 5125.1770 0.000 2.610 0.7893 -1252290. 89966. -0.008725 0.000 2.243E+10 -1227.5511 5412.4947 0.000 2.900 0.7586 -946333. 85633. -0.008894 0.000 2.286E+10 -1262.9728 5794.0526 0.000 3.190 0.7274 -655667. 81183. -0.008983 0.000 6.742E+10 -1294.6848 6194.3278 0.000 3.480 0.6960 -380678. 76628. -0.009010 0.000 6.801E+10 -1322.8104 6613.6751 0.000 3.770 0.6647 -121708. 71982. -0.009023 0.000 6.853E+10 -1347.1124 7053.2408 0.000 4.060 0.6332 120948. 67259. -0.009023 0.000 6.853E+10 -1367.3598 7514.3547 0.000 4.350 0.6019 347044. 62473. -0.009011 0.000 6.809E+10 -1383.3286 7998.5739 0.000 4.640 0.5705 556388. 57632. -0.008987 0.000 6.764E+10 -1398.9379 8532.9618 0.000 4.930 0.5393 748788. 52735. -0.008917 0.000 2.326E+10 -1415.2399 9132.2255 0.000 5.220 0.5085 924046. 47876. -0.008791 0.000 2.290E+10 -1377.7083 9429.1905 0.000 5.510 0.4781 1082613. 43163. -0.008638 0.000 2.265E+10 -1330.5251 9684.2712 0.000 5.800 0.4483 1225062. 38620. -0.008459 0.000 2.247E+10 -1280.5461 9939.3519 0.000 6.090 0.4192 1351997. 34255. -0.008259 0.000 2.232E+10 -1228.1375 10194. 0.000 6.380 0.3909 1464051. 30076. -0.008039 0.000 2.220E+10 -1173.6643 10450. 0.000 6.670 0.3633 1561883. 26089. -0.007801 0.000 2.211E+10 -1117.4875 10705. 0.000 6.960 0.3366 1646174. 22300. -0.007548 0.000 2.203E+10 -1059.9623 10960. 0.000 7.250 0.3108 1717619. 18713. -0.007282 0.000 2.197E+10 -1001.4359 11215. 0.000 7.540 0.2859 1776926. 15331. -0.007005 0.000 2.192E+10-942.2459 11470. 0.000 7.830 0.2620 1824813. 12156. -0.006719 0.000 2.187E+10-882.7184 11725. 0.000 8.120 0.2391 1862000. 9187.7920 -0.006426 0.000 2.184E+10-823.1671 11980. 0.000 8.410 0.2173 1889208. 6426.3099 -0.006127 0.000 2.182E+10-763.8916 12235. 0.000 8.700 0.1965 1907154. 3870.1305 -0.005824 0.000 2.180E+10-705.1771 12490. 0.000 8.990 0.1767 1916549. 1516.8322 -0.005519 0.000 2.180E+10-647.2932 12745. 0.000 9.280 0.1581 1918095. -636.9174 -0.005212 0.000 2.180E+10-590.4939 13000. 0.000 9.570 0.1405 1912479. -2595.3061 -0.004907 0.000 2.180E+10-535.0168 13255. 0.000 9.860 0.1239 1900373. -4363.3202 -0.004602 0.000 2.181E+10-481.0833 13510. 0.000 10.150 0.1084 1882430. -6540.0824 -0.004301 0.000 2.183E+10-769.9294 24711. 0.000 10.440 0.0940 1855153. -9062.3703 -0.004003 0.000 2.185E+10-679.6613 25166. 0.000 10.730 0.0806 1819635. -11277. -0.003710 0.000 2.188E+10-593.1838 25622. 0.000 11.020 0.0682 1776923. -13198. -0.003425 0.000 2.192E+10-510.7425 26077. 0.000

Page 63

existing phase2 87.lp6o 11.310 0.0567 1728016. -14839. -0.003147 0.000 2.196E+10-432.5400 26533. 0.000 11.600 0.0463 1673861. -16216. -0.002877 0.000 2.201E+10-358.7379 26988. 0.000 11.890 0.0367 1615352. -17344. -0.002618 0.000 2.206E+10-289.4588 27443. 0.000 12.180 0.0280 1553329. -18239. -0.002368 0.000 2.212E+10-224.7890 27899. 0.000 12.470 0.0202 1488575. -18917. -0.002129 0.000 2.218E+10-164.7810 28354. 0.000 12.760 0.0132 1421818. -19394. -0.001901 0.000 2.225E+10-109.4561 28810. 0.000 13.050 0.006993 1353727. -19687. -0.001684 0.000 2.232E+10-58.8070 29265. 0.000 13.340 0.001499 1284916. -19811. -0.001479 0.000 2.240E+10-12.8008 29720. 0.000 13.630 -0.003300 1215944. -19784. -0.001285 0.000 2.248E+1028.6184 30176. 0.000 13.920 -0.007445 1147312. -19620. -0.001102 0.000 2.256E+1065.5271 30631. 0.000 14.210 -0.0110 1079467. -19335. -0.000931 0.000 2.266E+1098.0196 31087. 0.000 14.500 -0.0139 1012803. -18945. -0.000771 0.000 2.275E+10126.2055 31542. 0.000 14.790 -0.0163 947663. -18464. -0.000621 0.000 2.286E+10150.2075 31997. 0.000 15.080 -0.0182 884336. -17943. -0.000482 0.000 2.297E+10149.1201 28440. 0.000 15.370 -0.0197 822811. -17400. -0.000353 0.000 2.309E+10163.0589 28818. 0.000 15.660 -0.0207 763256. -16814. -0.000234 0.000 2.323E+10173.6913 29196. 0.000 15.950 -0.0213 705801. -16197. -0.000124 0.000 2.338E+10181.1618 29574. 0.000 16.240 -0.0216 650536. -15559. -5.474E-05 0.000 6.743E+10185.6186 29952. 0.000 16.530 -0.0217 597517. -14906. -2.256E-05 0.000 6.755E+10189.1112 30329. 0.000 16.820 -0.0217 546788. -14244. 6.893E-06 0.000 6.766E+10191.6872 30707. 0.000 17.110 -0.0217 498379. -13574. 3.375E-05 0.000 6.777E+10193.3944 31085. 0.000 17.400 -0.0215 452312. -12899. 5.815E-05 0.000 6.786E+10194.2805 31463. 0.000 17.690 -0.0212 408596. -12223. 8.020E-05 0.000 6.796E+10194.3929 31841. 0.000 17.980 -0.0209 367234. -11548. 0.000100 0.000 6.804E+10193.7785 32219. 0.000 18.270 -0.0205 328218. -10875. 0.000118 0.000 6.813E+10192.4834 32597. 0.000 18.560 -0.0201 291532. -10209. 0.000134 0.000 6.820E+10190.5527 32974. 0.000 18.850 -0.0196 257154. -9550.2747 0.000148 0.000 6.829E+10188.0306 33352. 0.000 19.140 -0.0191 225052. -8901.2716 0.000160 0.000 6.834E+10184.9597 33730. 0.000 19.430 -0.0185 195190. -8263.8379 0.000171 0.000 6.840E+10181.3815 34108. 0.000 19.720 -0.0179 167524. -7639.6703 0.000180 0.000 6.847E+10177.3356 34486. 0.000 20.010 -0.0173 142005. -7030.3298 0.000188 0.000 6.849E+10172.8601 34864. 0.000 20.300 -0.0166 118580. -6437.2484 0.000194 0.000 6.853E+10

Page 64

existing phase2 87.lp6o167.9913 35241. 0.000 20.590 -0.0159 97189. -5861.7353 0.000200 0.000 6.858E+10162.7634 35619. 0.000 20.880 -0.0152 77768. -5304.9837 0.000204 0.000 6.862E+10157.2088 35997. 0.000 21.170 -0.0145 60252. -4768.0773 0.000208 0.000 6.862E+10151.3580 36375. 0.000 21.460 -0.0138 44568. -4251.9985 0.000210 0.000 6.862E+10145.2390 36753. 0.000 21.750 -0.0130 30643. -3757.6349 0.000212 0.000 6.862E+10138.8780 37131. 0.000 22.040 -0.0123 18400. -3285.7872 0.000214 0.000 6.862E+10132.2988 37508. 0.000 22.330 -0.0115 7759.2649 -2837.1768 0.000214 0.000 6.862E+10125.5233 37886. 0.000 22.620 -0.0108 -1361.5034 -2412.4529 0.000214 0.000 6.862E+10118.5709 38264. 0.000 22.910 -0.0100 -9046.3278 -2012.2004 0.000214 0.000 6.862E+10111.4592 38642. 0.000 23.200 -0.009293 -15381. -1636.9472 0.000213 0.000 6.862E+10104.2035 39020. 0.000 23.490 -0.008552 -20454. -1287.1719 0.000213 0.000 6.862E+1096.8168 39398. 0.000 23.780 -0.007814 -24355. -963.3104 0.000211 0.000 6.862E+1089.3104 39775. 0.000 24.070 -0.007080 -27174. -665.7639 0.000210 0.000 6.862E+1081.6933 40153. 0.000 24.360 -0.006351 -29003. -394.9048 0.000209 0.000 6.862E+1073.9728 40531. 0.000 24.650 -0.005628 -29937. -151.0838 0.000207 0.000 6.862E+1066.1542 40909. 0.000 24.940 -0.004909 -30069. 65.3639 0.000206 0.000 6.862E+1058.2411 41287. 0.000 25.230 -0.004196 -29496. 271.1931 0.000204 0.000 6.862E+1060.0516 49806. 0.000 25.520 -0.003488 -28196. 463.3362 0.000203 0.000 6.862E+1050.3755 50261. 0.000 25.810 -0.002785 -26285. 621.6102 0.000201 0.000 6.862E+1040.5866 50717. 0.000 26.100 -0.002087 -23883. 745.6174 0.000200 0.000 6.862E+1030.6819 51172. 0.000 26.390 -0.001392 -21110. 834.9472 0.000199 0.000 6.862E+1020.6570 51628. 0.000 26.680 -0.000702 -18086. 889.1711 0.000198 0.000 6.862E+1010.5062 52083. 0.000 26.970 -1.476E-05 -14935. 907.8397 0.000197 0.000 6.862E+100.2229 52538. 0.000 27.260 0.000670 -11781. 890.4791 0.000196 0.000 6.862E+10-10.2002 52994. 0.000 27.550 0.001352 -8750.9442 836.5901 0.000196 0.000 6.862E+10-20.7705 53449. 0.000 27.840 0.002033 -5972.1898 745.6473 0.000196 0.000 6.862E+10-31.4955 53905. 0.000 28.130 0.002713 -3574.8479 617.1000 0.000195 0.000 6.862E+10-42.3823 54360. 0.000 28.420 0.003392 -1690.7658 450.3744 0.000195 0.000 6.862E+10-53.4370 54815. 0.000 28.710 0.004071 -453.8246 244.8771 0.000195 0.000 6.862E+10-64.6649 55271. 0.000 29.000 0.004750 0.000 0.000 0.000195 0.000 6.862E+10-76.0691 27863. 0.000

* This analysis makes computations of pile response using nonlinear moment-curvaturePage 65

existing phase2 87.lp6orelationships. The above values of total stress are computed for combined axial and bending stress in elastic sections and do not equal actual stresses in concrete and steel in the range of nonlinear bending.

Output Summary for Load Case No. 14:

Pile-head deflection = 1.0000000 inchesComputed slope at pile head = -0.0001805 radiansMaximum bending moment = -4634792. inch-lbsMaximum shear force = 124021. lbsDepth of maximum bending moment = 0.000000 inches below pile headDepth of maximum shear force = 0.000000 inches below pile headNumber of iterations = 57Number of zero deflection points = 2

-------------------------------------------------------------------------------- Summary of Pile Response(s)--------------------------------------------------------------------------------

Definitions of Pile-head Loading Conditions:

Load Type 1: Load 1 = Shear, lbs, and Load 2 = Moment, in-lbsLoad Type 2: Load 1 = Shear, lbs, and Load 2 = Slope, radiansLoad Type 3: Load 1 = Shear, lbs, and Load 2 = Rotational Stiffness, in-lbs/radianLoad Type 4: Load 1 = Top Deflection, inches, and Load 2 = Moment, in-lbsLoad Type 5: Load 1 = Top Deflection, inches, and Load 2 = Slope, radians

Pile-head Pile-head Maximum MaximumLoad Load Condition 1 Condition 2 Axial Pile-head Moment Shear Pile-headCase Type V(lbs) or in-lb, rad., Loading Deflection in Pile in Pile Rotation No. No. y(inches) or in-lb/rad. lbs inches in-lbs lbs radians---- ---- -------------- -------------- ------------- -------------------------- ------------- ------------- 1 4 y = 0.0100 M = 0.000 10000.00000000 0.0100000045692. 1124.2771 -0.00009863 2 4 y = 0.1000 M = 0.000 10000.00000000 0.10000000454601. 11211. -0.00098803 3 4 y = 0.2000 M = 0.000 10000.00000000 0.20000000694987. 19313. -0.00216949 4 4 y = 0.3000 M = 0.000 10000.00000000 0.30000000839942. 25723. -0.00355299 5 4 y = 0.5000 M = 0.000 10000.00000000 0.500000001263577. 40479. -0.00617496 6 4 y = 0.7500 M = 0.000 10000.00000000 0.750000001813700. 55393. -0.00930132 7 4 y = 1.0000 M = 0.000 10000.00000000 1.000000002347276. 68911. -0.01230938 8 5 y = 0.0100 S = 0.000 10000.00000000 0.01000000-147576. 2581.1069 -0.00000023 9 5 y = 0.1000 S = 0.000 10000.00000000 0.10000000-974916. 21125. -0.00000554

Page 66

existing phase2 87.lp6o 10 5 y = 0.2000 S = 0.000 10000.00000000 0.20000000-1648585. 38697. -0.00001050 11 5 y = 0.3000 S = 0.000 10000.00000000 0.30000000-2353486. 54774. -0.00001525 12 5 y = 0.5000 S = 0.000 10000.00000000 0.50000000-3727400. 86020. -0.00002616 13 5 y = 0.7500 S = 0.000 10000.00000000 0.75000000-4631828. 110839. -0.00007210 14 5 y = 1.0000 S = 0.000 10000.00000000 1.00000000-4634792. 124021. -0.00018045

The analysis ended normally.

Page 67

Lateral Deflection (inches)D

epth

(ft)

-0.1 0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.80

24

68

1012

1416

1820

2224

2628

3032

3436

38

Case 1Case 2Case 3Case 4Case 5Case 6

Lateral Deflection (inches)D

epth

(ft)

-0.1 0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.0

24

68

1012

1416

1820

2224

2628

3032

3436

38

Case 1Case 2Case 3Case 4Case 5Case 6

Bending Moment (in-kips)

Dep

th (f

t)

-1200 -1000 -800 -600 -400 -200 0 200 400 600 800

02

46

810

1214

1618

2022

2426

2830

3234

3638

Case 1Case 2Case 3Case 4Case 5Case 6

Bending Moment (in-kips)

Dep

th (f

t)

-1200 -1000 -800 -600 -400 -200 0 200 400 600 800

02

46

810

1214

1618

2022

2426

2830

3234

3638

Case 1Case 2Case 3Case 4Case 5Case 6

Shear Force (kips)

Dep

th (f

t)

-10 -5 0 5 10 15 20 25 30

02

46

810

1214

1618

2022

2426

2830

3234

3638

Case 1Case 2Case 3Case 4Case 5Case 6

Shear Force (kips)

Dep

th (f

t)

-10 -5 0 5 10 15 20 25 3

02

46

810

1214

1618

2022

2426

2830

3234

3638

Case 1Case 2Case 3Case 4Case 5Case 6

18new.lp6o================================================================================

LPile Plus for Windows, Version 2012-06.037

Analysis of Individual Piles and Drilled Shafts Subjected to Lateral Loading Using the p-y Method

© 1985-2012 by Ensoft, Inc. All Rights Reserved

================================================================================

This copy of LPile is licensed to:

Dennis NguyenAECOM

Serial Number of Security Device: 294790092Company Name Stored in Security Device: URS Corporation

-------------------------------------------------------------------------------- Files Used for Analysis--------------------------------------------------------------------------------

Path to file locations:\\losangeles.na.aecomnet.com\LosAngeles\Projects\ENV\_legacy\GT\Da Wu\LA County Geotech On-call\MLK\Report\2019 BHC - Lab\Appendix F and G\Name of input data file: 18new.lp6dName of output report file: 18new.lp6oName of plot output file: 18new.lp6pName of runtime messeage file: 18new.lp6r

-------------------------------------------------------------------------------- Date and Time of Analysis--------------------------------------------------------------------------------

Date: April 8, 2019 Time: 15:09:00

-------------------------------------------------------------------------------- Problem Title--------------------------------------------------------------------------------

Project Name: MLK DHS Lab & Red Bag Storage

Job Number: 60595699

Client: LACDPW

Engineer: Dennis Nguyen

Description:

Page 1

18new.lp6o

-------------------------------------------------------------------------------- Program Options--------------------------------------------------------------------------------

Engineering units are US Customary Units: pounds, inches, feet

Basic Program Options:

This analysis computes pile response to lateral loading and will compute nonlinear moment-curvature and nominal moment capacity for section types with nonlinear properties.

Computation Options:- Analysis does not use p-y multipliers (individual pile or shaft only)- Analysis assumes no shear resistance at pile tip- Analysis for fixed-length pile or shaft only- No computation of foundation stiffness matrix values- Report pile response for full length of pile- Analysis assumes no loading by soil movements acting on pile- No p-y curves to be computed and reported for user-specified depths

Solution Control Parameters:- Number of pile increments = 100- Maximum number of iterations allowed = 100- Deflection tolerance for convergence = 1.0000E-05 in- Maximum allowable deflection = 100.0000 in

Pile Response Output Options:- Values of pile-head deflection, bending moment, shear force, and soil reaction are printed for full length of pile.- Printing Increment (nodal spacing of output points) = 1

-------------------------------------------------------------------------------- Pile Structural Properties and Geometry--------------------------------------------------------------------------------

Total number of pile sections = 1

Total length of pile = 40.00 ft

Depth of ground surface below top of pile = 0.00 ft

Pile diameter values used for p-y curve computations are defined using 2 points.

p-y curves are computed using pile diameter values interpolated with depth over the length of the pile.

Point Depth Pile X Diameter ft in----- --------- ----------- 1 0.00000 18.0000000 2 40.000000 18.0000000

Input Structural Properties:----------------------------

Page 2

18new.lp6oPile Section No. 1:

Section Type = Drilled Shaft (Bored Pile) Section Length = 40.00000000 ft Section Diameter = 18.00000000 in

-------------------------------------------------------------------------------- Ground Slope and Pile Batter Angles--------------------------------------------------------------------------------

Ground Slope Angle = 0.000 degrees = 0.000 radians

Pile Batter Angle = 0.000 degrees = 0.000 radians

-------------------------------------------------------------------------------- Soil and Rock Layering Information--------------------------------------------------------------------------------

The soil profile is modelled using 5 layers

Layer 1 is sand, p-y criteria by Reese et al., 1974

Distance from top of pile to top of layer = 0.0000 ft Distance from top of pile to bottom of layer = 23.00000 ft Effective unit weight at top of layer = 125.00000 pcf Effective unit weight at bottom of layer = 125.00000 pcf Friction angle at top of layer = 26.00000 deg. Friction angle at bottom of layer = 26.00000 deg. Subgrade k at top of layer = 0.0000 pci Subgrade k at bottom of layer = 0.0000 pci

NOTE: Internal default values for subgrade k will be computed for the above soil layer.

Layer 2 is sand, p-y criteria by Reese et al., 1974

Distance from top of pile to top of layer = 23.00000 ft Distance from top of pile to bottom of layer = 30.00000 ft Effective unit weight at top of layer = 62.60000 pcf Effective unit weight at bottom of layer = 62.60000 pcf Friction angle at top of layer = 30.00000 deg. Friction angle at bottom of layer = 30.00000 deg. Subgrade k at top of layer = 0.0000 pci Subgrade k at bottom of layer = 0.0000 pci

NOTE: Internal default values for subgrade k will be computed for the above soil layer.

Layer 3 is sand, p-y criteria by Reese et al., 1974

Distance from top of pile to top of layer = 30.00000 ft Distance from top of pile to bottom of layer = 45.00000 ft Effective unit weight at top of layer = 47.60000 pcf Effective unit weight at bottom of layer = 47.60000 pcf Friction angle at top of layer = 31.00000 deg.

Page 3

18new.lp6o Friction angle at bottom of layer = 31.00000 deg. Subgrade k at top of layer = 0.0000 pci Subgrade k at bottom of layer = 0.0000 pci

NOTE: Internal default values for subgrade k will be computed for the above soil layer.

Layer 4 is soft clay, p-y criteria by Matlock, 1970

Distance from top of pile to top of layer = 45.00000 ft Distance from top of pile to bottom of layer = 54.00000 ft Effective unit weight at top of layer = 57.60000 pcf Effective unit weight at bottom of layer = 57.60000 pcf Undrained cohesion at top of layer = 1500.00000 psf Undrained cohesion at bottom of layer = 1500.00000 psf Epsilon-50 at top of layer = 0.0000 Epsilon-50 at bottom of layer = 0.0000

NOTE: Internal default values for Epsilon-50 will be computed for the above soil layer.

Layer 5 is sand, p-y criteria by Reese et al., 1974

Distance from top of pile to top of layer = 54.00000 ft Distance from top of pile to bottom of layer = 61.50000 ft Effective unit weight at top of layer = 62.60000 pcf Effective unit weight at bottom of layer = 62.60000 pcf Friction angle at top of layer = 31.00000 deg. Friction angle at bottom of layer = 31.00000 deg. Subgrade k at top of layer = 0.0000 pci Subgrade k at bottom of layer = 0.0000 pci

NOTE: Internal default values for subgrade k will be computed for the above soil layer.

(Depth of lowest soil layer extends 21.50 ft below pile tip)

-------------------------------------------------------------------------------- Summary of Soil Properties--------------------------------------------------------------------------------

Layer Layer Effective UndrainedAngle of StrainLayer Soil Type Depth Unit Wt. CohesionFriction Factor kpy Num. (p-y Curve Criteria) ft pcf psf deg. Epsilon 50 pci----- ---------------------------------- ---------- ---------- -------------------- ---------- ---------- 1 Sand (Reese, et al.) 0.00 125.000 -- 26.000 -- default 23.000 125.000 -- 26.000 -- default 2 Sand (Reese, et al.) 23.000 62.600 -- 30.000 -- default 30.000 62.600 -- 30.000 -- default 3 Sand (Reese, et al.) 30.000 47.600 --

Page 4

18new.lp6o 31.000 -- default 45.000 47.600 -- 31.000 -- default 4 Soft Clay 45.000 57.600 1500.000 -- default -- 54.000 57.600 1500.000 -- default -- 5 Sand (Reese, et al.) 54.000 62.600 -- 31.000 -- default 61.500 62.600 -- 31.000 -- default

-------------------------------------------------------------------------------- Loading Type--------------------------------------------------------------------------------

Static loading criteria were used when computing p-y curves for all analyses.

-------------------------------------------------------------------------------- Pile-head Loading and Pile-head Fixity Conditions--------------------------------------------------------------------------------

Number of loads specified = 6

Load Load Condition Condition Axial Thrust Compute No. Type 1 2 Force, lbsTop y vs. Pile Length----- ---- -------------------- ----------------------- ------------------------------------- 1 4 y = 0.25000 in M = 0.0000 in-lbs 250000. No 2 4 y = 0.50000 in M = 0.0000 in-lbs 250000. No 3 4 y = 0.75000 in M = 0.0000 in-lbs 250000. No 4 5 y = 0.25000 in S = 0.0000 in/in 250000. No 5 5 y = 0.50000 in S = 0.0000 in/in 250000. No 6 5 y = 0.75000 in S = 0.0000 in/in 250000. No

V = perpendicular shear force applied to pile headM = bending moment applied to pile heady = lateral deflection relative to pile axisS = pile slope relative to original pile batter angleR = rotational stiffness applie to pile headAxial thrust is assumed to be acting axially for all pile batter angles.

-------------------------------------------------------------------------------- Computations of Nominal Moment Capacity and Nonlinear Bending Stiffness--------------------------------------------------------------------------------

Axial thrust force values were determined from pile-head loading conditions

Number of Pile Sections Analyzed = 1

Page 5

18new.lp6oPile Section No. 1:-------------------

Dimensions and Properties of Drilled Shaft (Bored Pile):--------------------------------------------------------

Length of Section = 40.00000000 ftShaft Diameter = 18.00000000 inConcrete Cover Thickness = 3.00000000 inNumber of Reinforcing Bars = 2 barsYield Stress of Reinforcing Bars = 60.00000000 ksiModulus of Elasticity of Reinforcing Bars = 29000. ksiGross Area of Shaft = 254.46900494 sq. in.Total Area of Reinforcing Steel = 2.54000000 sq. in.Area Ratio of Steel Reinforcement = 1.00 percentEdge-to-Edge Bar Spacing = 9.46000000 inMaximum Concrete Aggregate Size = 0.75000000 inRatio of Bar Spacing to Aggregate Size = 12.61Offset of Rebar Cage Center from Center of Pile = 0.0000000 in

Axial Structural Capacities:----------------------------

Nom. Axial Structural Capacity = 0.85 Fc Ac + Fy As = 794.819 kipsTensile Load for Cracking of Concrete = -99.745 kipsNominal Axial Tensile Capacity = -152.400 kips

Reinforcing Bar Dimensions and Positions Used in Computations:

Bar Bar Diam. Bar Area X Y Number inches sq. in. inches inches ---------- ---------- ---------- ---------- ---------- 1 1.27000 1.27000 5.36500 0.00000 2 1.27000 1.27000 -5.36500 0.00000

NOTE: The positions of the above rebars were computed by LPile

Minimum spacing between any two bars not equal to zero = 9.46000 inches betweenBars 1 and 2

Spacing to aggregate size ratio = 12.61333

Concrete Properties:--------------------

Compressive Strength of Concrete = 3.00000000 ksiModulus of Elasticity of Concrete = 3122.01857778 ksiModulus of Rupture of Concrete = -0.41079191 ksiCompression Strain at Peak Stress = 0.00163356Tensile Strain at Fracture of Concrete = -0.00011596Maximum Coarse Aggregate Size = 0.75000000 in

Number of Axial Thrust Force Values Determined from Pile-head Loadings = 1

Number Axial Thrust Force kips ------ ------------------ 1 250.000

Page 6

18new.lp6o

Definitions of Run Messages and Notes:--------------------------------------

C = concrete in section has cracked in tension. Y = stress in reinforcing steel has reached yield stress. T = ACI 318-08 criteria for tension-controlled section met, tensile strain in reinforcement exceeds 0.005 while simultaneously compressive strain in concrete more than than 0.003. See ACI 318-08, Section 10.3.4. Z = depth of tensile zone in concrete section is less than 10 percent of section depth.

Bending Stiffness (EI) = Computed Bending Moment / Curvature.Position of neutral axis is measured from edge of compression side of pile.Compressive stresses and strains are positive in sign.Tensile stresses and strains are negative in sign.

Axial Thrust Force = 250.000 kips

Bending Bending Bending Depth to Max Comp Max Tens Max Concrete Max Steel Run Curvature Moment Stiffness N Axis Strain Strain Stress Stress Msg rad/in. in-kip kip-in2 in in/in in/in ksi ksi ------------- ------------- ------------- ------------- ------------- -------------------------- ------------- --- 0.000001250 19.7286821 15782946. 225.8796679 0.0002823 0.0002598 0.9470934 8.1848755 0.000002500 39.4709055 15788362. 117.4527150 0.0002936 0.0002486 0.9808908 8.5087968 0.000003750 59.2112643 15789670. 81.3161086 0.0003049 0.0002374 1.0144717 8.8333393 0.000005000 78.9488281 15789766. 63.2520891 0.0003163 0.0002263 1.0478344 9.1585028 0.000006250 98.6826654 15789226. 52.4171050 0.0003276 0.0002151 1.0809775 9.4842877 0.000007500 118.4118453 15788246. 45.1966392 0.0003390 0.0002040 1.1138991 9.8106939 0.000008750 138.1354362 15786907. 40.0416128 0.0003504 0.0001929 1.1465978 10.1377217 0.0000100 157.8525063 15785251. 36.1774869 0.0003618 0.0001818 1.1790719 10.4653712 0.0000113 177.5621232 15783300. 33.1739617 0.0003732 0.0001707 1.2113198 10.7936425 0.0000125 197.2633539 15781068. 30.7728578 0.0003847 0.0001597 1.2433399 11.1225359 0.0000138 216.9552647 15778565. 28.8098790 0.0003961 0.0001486 1.2751306 11.4520518 0.0000150 236.6369217 15775795. 27.1754948 0.0004076 0.0001376 1.3066902 11.7821903 0.0000163 256.3073900 15772762. 25.7938762 0.0004192 0.0001267 1.3380172 12.1129517 0.0000175 275.9657336 15769470. 24.6108599 0.0004307 0.0001157 1.3691099 12.4443364 0.0000188 295.6110160 15765921. 23.5867260 0.0004423 0.0001048 1.3999666 12.7763448 0.0000200 315.2422996 15762115. 22.6916849 0.0004538 0.0000938 1.4305858 13.1089773 0.0000213 334.8586459 15758054. 21.9029560 0.0004654 0.0000829 1.4609659 13.4422342 0.0000225 354.4591151 15753738. 21.2028214 0.0004771 0.0000721

Page 7

18new.lp6o 1.4911052 13.7761160 0.0000238 374.0427664 15749169. 20.5772932 0.0004887 0.0000612 1.5210020 14.1106233 0.0000250 393.6086579 15744346. 20.0151811 0.0005004 0.0000504 1.5506548 14.4457564 0.0000263 413.1558462 15739270. 19.5074264 0.0005121 0.0000396 1.5800619 14.7815159 0.0000275 432.6833865 15733941. 19.0466174 0.0005238 0.0000288 1.6092217 15.1179024 0.0000288 452.1903328 15728359. 18.6266314 0.0005355 0.0000180 1.6381325 15.4549165 0.0000300 471.6757374 15722525. 18.2423663 0.0005473 0.000007271 1.6667927 15.7925588 0.0000313 491.1386478 15716437. 17.8895362 0.0005590 -0.000003452 1.6952006 16.1308298 0.0000325 510.5766679 15710051. 17.5645086 0.0005708 -0.0000142 1.7233541 16.4697244 0.0000338 529.9837372 15703222. 17.2641728 0.0005827 -0.0000248 1.7512498 16.8092217 0.0000350 549.3523698 15695782. 16.9858560 0.0005945 -0.0000355 1.7788839 17.1492939 0.0000363 568.6750118 15687587. 16.7272521 0.0006064 -0.0000461 1.8062522 17.4899113 0.0000375 587.9446771 15678525. 16.4863637 0.0006182 -0.0000568 1.8333513 17.8310457 0.0000388 607.1549530 15668515. 16.2614527 0.0006301 -0.0000674 1.8601774 18.1726700 0.0000400 626.2999505 15657499. 16.0509990 0.0006420 -0.0000780 1.8867274 18.5147590 0.0000413 645.3745057 15645443. 15.8536694 0.0006540 -0.0000885 1.9129982 18.8572896 0.0000425 664.3740039 15632330. 15.6682888 0.0006659 -0.0000991 1.9389870 19.2002410 0.0000438 683.2943347 15618156. 15.4938179 0.0006779 -0.0001096 1.9646912 19.5435941 0.0000450 683.2943347 15184319. 15.2066103 0.0006843 -0.0001257 1.9783053 19.7271766 C 0.0000463 683.2943347 14773932. 15.0315845 0.0006952 -0.0001373 2.0013254 20.0404004 C 0.0000475 694.0106912 14610751. 14.8641528 0.0007060 -0.0001490 2.0239221 20.3513955 C 0.0000488 705.9536424 14481100. 14.7038269 0.0007168 -0.0001607 2.0461108 20.6602979 C 0.0000513 728.6703929 14217959. 14.4027074 0.0007381 -0.0001844 2.0893153 21.2722614 C 0.0000538 750.0290422 13954029. 14.1251971 0.0007592 -0.0002083 2.1310510 21.8773636 C 0.0000563 769.9671621 13688305. 13.8675226 0.0007800 -0.0002325 2.1712831 22.4745840 C 0.0000588 788.8160480 13426656. 13.6283115 0.0008007 -0.0002568 2.2101779 23.0658983 C 0.0000613 806.6233164 13169360. 13.4052867 0.0008211 -0.0002814 2.2477616 23.6512780 C 0.0000638 823.3845869 12915837. 13.1962827 0.0008413 -0.0003062 2.2840321 24.2302404 C 0.0000663 839.2898995 12668527. 13.0003570 0.0008613 -0.0003312 2.3190940 24.8040236 C 0.0000688 854.4037844 12427691. 12.8162104 0.0008811 -0.0003564 2.3529860 25.3728822 C 0.0000713 868.7903856 12193549. 12.6427473 0.0009008 -0.0003817 2.3857478 25.9371143 C 0.0000738 882.5131510 11966280. 12.4790424 0.0009203 -0.0004072 2.4174195 26.4970646 C

Page 8

18new.lp6o 0.0000763 895.6345421 11746027. 12.3243140 0.0009397 -0.0004328 2.4480417 27.0531270 C 0.0000788 908.1069632 11531517. 12.1773568 0.0009590 -0.0004585 2.4775895 27.6045012 C 0.0000813 920.0430423 11323607. 12.0378613 0.0009781 -0.0004844 2.5061329 28.1521482 C 0.0000838 931.5243117 11122678. 11.9054686 0.0009971 -0.0005104 2.5337260 28.6968196 C 0.0000863 942.6086036 10928795. 11.7797904 0.0010160 -0.0005365 2.5604095 29.2390885 C 0.0000888 953.1430044 10739639. 11.6594279 0.0010348 -0.0005627 2.5860931 29.7768153 C 0.0000913 963.3197860 10556929. 11.5447856 0.0010535 -0.0005890 2.6108981 30.3122266 C 0.0000938 973.2091127 10380897. 11.4357378 0.0010721 -0.0006154 2.6348742 30.8462249 C 0.0000963 982.5845955 10208671. 11.3306410 0.0010906 -0.0006419 2.6578834 31.3754392 C 0.0000988 991.7732763 10043274. 11.2307747 0.0011090 -0.0006685 2.6801331 31.9043939 C 0.0001013 1000.5344098 9881821. 11.1345091 0.0011274 -0.0006951 2.7014786 32.4294400 C 0.0001038 1009.0968770 9726235. 11.0426812 0.0011457 -0.0007218 2.7220637 32.9538798 C 0.0001063 1017.2967077 9574557. 10.9541218 0.0011639 -0.0007486 2.7417929 33.4750757 C 0.0001088 1025.3281845 9428305. 10.8695534 0.0011821 -0.0007754 2.7607868 33.9960168 C 0.0001113 1032.9945105 9285344. 10.7876651 0.0012001 -0.0008024 2.7789309 34.5133424 C 0.0001138 1040.5854742 9148004. 10.7097648 0.0012182 -0.0008293 2.7964018 35.0319496 C 0.0001163 1047.7457153 9012866. 10.6336856 0.0012362 -0.0008563 2.8129905 35.5454005 C 0.0001188 1054.8330413 8882805. 10.5611837 0.0012541 -0.0008834 2.8289134 36.0601393 C 0.0001213 1061.6624758 8755979. 10.4910222 0.0012720 -0.0009105 2.8440620 36.5725945 C 0.0001238 1068.2720741 8632502. 10.4232524 0.0012899 -0.0009376 2.8584648 37.0834600 C 0.0001263 1074.8091518 8513340. 10.3585178 0.0013078 -0.0009647 2.8722034 37.5956110 C 0.0001288 1081.0088140 8396185. 10.2951561 0.0013255 -0.0009920 2.8851352 38.1035018 C 0.0001313 1087.0960502 8282637. 10.2343163 0.0013433 -0.0010192 2.8973870 38.6118042 C 0.0001338 1093.1112726 8172795. 10.1760823 0.0013611 -0.0010464 2.9089764 39.1213923 C 0.0001363 1098.8043570 8064619. 10.1188728 0.0013787 -0.0010738 2.9197805 39.6265836 C 0.0001388 1104.3969712 7959618. 10.0638736 0.0013964 -0.0011011 2.9299139 40.1323743 C 0.0001413 1109.9181658 7857828. 10.0111361 0.0014141 -0.0011284 2.9393865 40.6394543 C 0.0001438 1115.2182469 7758040. 9.9596564 0.0014317 -0.0011558 2.9481317 41.1441305 C 0.0001463 1120.3432387 7660467. 9.9096272 0.0014493 -0.0011832 2.9561758 41.6474944 C 0.0001488 1125.3974613 7565697. 9.8615804 0.0014669 -0.0012106 2.9635607 42.1521553 C 0.0001588 1144.2463557 7207851. 9.6834824 0.0015373 -0.0013202 2.9862498 44.1659941 C 0.0001688 1161.1758526 6881042. 9.5261670 0.0016075 -0.0014300

Page 9

18new.lp6o 2.9980912 46.1782421 C 0.0001788 1176.3905204 6581206. 9.3872856 0.0016780 -0.0015395 2.9999834 48.1948047 C 0.0001888 1189.9934556 6304601. 9.2651927 0.0017488 -0.0016487 2.9999849 50.2227108 C 0.0001988 1201.8997718 6047294. 9.1562324 0.0018198 -0.0017577 2.9998756 52.2554967 C 0.0002088 1212.5618774 5808680. 9.0605786 0.0018914 -0.0018661 2.9993538 54.3056408 C 0.0002188 1221.9564695 5586087. 8.9751783 0.0019633 -0.0019742 2.9999727 -56.6802747 C 0.0002288 1230.3813916 5378716. 8.9001358 0.0020359 -0.0020816 2.9989889 -59.7691860 C 0.0002388 1237.7427656 5184263. 8.8322057 0.0021087 -0.0021888 2.9995906 60.0000000 CY 0.0002488 1244.3645401 5002471. 8.7724100 0.0021821 -0.0022954 2.9998613 60.0000000 CY 0.0002588 1250.2672206 4831951. 8.7192873 0.0022561 -0.0024014 2.9999567 60.0000000 CY 0.0002688 1255.4116645 4671299. 8.6708657 0.0023303 -0.0025072 2.9999752 60.0000000 CY 0.0002788 1259.9992389 4520177. 8.6280221 0.0024051 -0.0026124 2.9999566 60.0000000 CY 0.0002888 1264.0739336 4377745. 8.5900891 0.0024804 -0.0027171 2.9998699 60.0000000 CY 0.0002988 1267.6763517 4243268. 8.5564914 0.0025563 -0.0028212 2.9996207 60.0000000 CY 0.0003088 1270.7725048 4115862. 8.5256430 0.0026323 -0.0029252 2.9990280 60.0000000 CY 0.0003188 1273.4635973 3995180. 8.4980040 0.0027087 -0.0030288 2.9978597 60.0000000 CY 0.0003288 1275.7987115 3880757. 8.4734880 0.0027857 -0.0031318 2.9999963 60.0000000 CY 0.0003388 1277.7718953 3772020. 8.4518653 0.0028631 -0.0032344 2.9995286 60.0000000 CY 0.0003488 1279.4407787 3668647. 8.4327339 0.0029409 -0.0033366 2.9979880 60.0000000 CY 0.0003588 1280.8284374 3570253. 8.4158293 0.0030192 -0.0034383 2.9999915 60.0000000 CY 0.0003688 1281.9106230 3476368. 8.4010696 0.0030979 -0.0035396 2.9990479 60.0000000 CY 0.0003788 1282.7556123 3386813. 8.3880891 0.0031770 -0.0036405 2.9980282 60.0000000 CY 0.0003888 1283.3418881 3301201. 8.3768330 0.0032565 -0.0037410 2.9994814 60.0000000 CY 0.0003988 1283.6990504 3219308. 8.3669023 0.0033363 -0.0038412 2.9966701 60.0000000 CY 0.0004088 1283.8286922 3140865. 8.3580187 0.0034163 -0.0039412 2.9995590 60.0000000 CY 0.0004188 1283.8286922 3065860. 8.3504621 0.0034968 -0.0040407 2.9965706 60.0000000 CY 0.0004288 1283.8286922 2994353. 8.3441235 0.0035775 -0.0041400 2.9993536 60.0000000 CY 0.0004388 1283.8286922 2926105. 8.3388706 0.0036587 -0.0042388 2.9976615 60.0000000 CY 0.0004488 1283.8286922 2860900. 8.3346874 0.0037402 -0.0043373 2.9987077 60.0000000 CY 0.0004588 1283.8286922 2798537. 8.3313383 0.0038220 -0.0044355 2.9999573 60.0000000 CY

-------------------------------------------------------------------------------- Summary of Results for Nominal (Unfactored) Moment Capacity for Section 1

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18new.lp6o--------------------------------------------------------------------------------

Moment values interpolated at maximum compressive strain = 0.003or maximum developed moment if pile fails at smaller strains.

Load Axial Thrust Nominal Mom. Cap. Max. Comp. No. kips in-kip Strain ---- ---------------- ------------------ ------------ 1 250.000 1280.488 0.00300000

Note note that the values of moment capacity in the table above are not factored by a strength reduction factor (phi-factor).

In ACI 318-08, the value of the strength reduction factor depends on whether the transverse reinforcing steel bars are tied hoops (0.65) or spirals (0.70).

The above values should be multiplied by the appropriate strength reduction factor to compute ultimate moment capacity according to ACI 318-08, Section 9.3.2.2 or the value required by the design standard being followed.

The following table presents factored moment capacities and corresponding bending stiffnesses computed for common resistance factor values used for reinforced concrete sections.

Axial Resistance Nominal Ultimate (Factored) Ultimate (Factored) Bending Stiffness Load Factor Moment Capacity Axial Thrust Moment Capacity at Ult. Mom. Cap. No. for Moment in-kip kipsin-kip kip-in^2 ----- ---------- ------------------- -------------------------------------- ------------------- 1 0.65 1280.488 162.500832.317 12776941.079

1 0.70 1280.488 175.000896.342 11733861.925

1 0.75 1280.488 187.500960.366 10609955.215

-------------------------------------------------------------------------------- Computed Values of Pile Loading and Deflection for Lateral Loading for Load Case Number 1--------------------------------------------------------------------------------

Pile-head conditions are Displacement and Moment (Loading Type 4)Displacement of pile head = 0.250000 inchesMoment at pile head = 0.000 in-lbsAxial load at pile head = 250000.000 lbs

Depth Deflect. Bending Shear Slope Total Bending Soil Res. Soil Spr. Distrib. X y Moment Force S Stress Stiffness p Es*h Lat. Load feet inches in-lbs lbs radians psi* lb-in^2 lb/in lb/inch lb/inch ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- 0.00 0.2500 0.000 5474.6247 -0.002607 0.000 1.578E+10

Page 11

18new.lp6o0.000 0.000 0.000 0.400 0.2375 29406. 5436.8379 -0.002602 0.000 1.578E+10-15.7445 318.2196 0.000 0.800 0.2250 58439. 5327.4455 -0.002589 0.000 1.579E+10-29.8357 636.4393 0.000 1.200 0.2126 86763. 5154.3423 -0.002567 0.000 1.579E+10-42.2907 954.6589 0.000 1.600 0.2004 114080. 4925.3153 -0.002536 0.000 1.579E+10-53.1372 1272.8785 0.000 2.000 0.1883 140132. 4647.9926 -0.002498 0.000 1.579E+10-62.4139 1591.0981 0.000 2.400 0.1764 164695. 4329.7943 -0.002451 0.000 1.578E+10-70.1688 1909.3178 0.000 2.800 0.1648 187581. 3977.8870 -0.002398 0.000 1.578E+10-76.4593 2227.5374 0.000 3.200 0.1534 208637. 3599.1425 -0.002337 0.000 1.578E+10-81.3509 2545.7570 0.000 3.600 0.1423 227743. 3200.1004 -0.002271 0.000 1.578E+10-84.9166 2863.9766 0.000 4.000 0.1316 244808. 2786.9358 -0.002199 0.000 1.577E+10-87.2354 3182.1963 0.000 4.400 0.1212 259775. 2365.4311 -0.002122 0.000 1.577E+10-88.3916 3500.4159 0.000 4.800 0.1112 272610. 1940.9541 -0.002041 0.000 1.577E+10-88.4738 3818.6355 0.000 5.200 0.1016 283307. 1518.4398 -0.001957 0.000 1.577E+10-87.5738 4136.8551 0.000 5.600 0.0924 291883. 1102.3781 -0.001869 0.000 1.577E+10-85.7852 4455.0748 0.000 6.000 0.0837 298376. 696.8065 -0.001779 0.000 1.577E+10-83.2030 4773.2944 0.000 6.400 0.0753 302843. 305.3068 -0.001688 0.000 1.576E+10-79.9219 5091.5140 0.000 6.800 0.0675 305357. -68.9927 -0.001595 0.000 1.576E+10-76.0362 5409.7336 0.000 7.200 0.0600 306009. -423.4116 -0.001502 0.000 1.576E+10-71.6383 5727.9533 0.000 7.600 0.0530 304898. -755.7070 -0.001409 0.000 1.576E+10-66.8181 6046.1729 0.000 8.000 0.0465 302136. -1064.0605 -0.001317 0.000 1.576E+10-61.6625 6364.3925 0.000 8.400 0.0404 297843. -1347.0610 -0.001225 0.000 1.577E+10-56.2544 6682.6121 0.000 8.800 0.0347 292145. -1603.6853 -0.001135 0.000 1.577E+10-50.6724 7000.8318 0.000 9.200 0.0295 285172. -1833.2762 -0.001048 0.000 1.577E+10-44.9905 7319.0514 0.000 9.600 0.0247 277059. -2035.5185 -0.000962 0.000 1.577E+10-39.2771 7637.2710 0.000 10.000 0.0203 267940. -2210.4130 -0.000879 0.000 1.577E+10-33.5956 7955.4906 0.000 10.400 0.0162 257949. -2358.2505 -0.000799 0.000 1.577E+10-28.0034 8273.7103 0.000 10.800 0.0126 247219. -2479.5834 -0.000722 0.000 1.577E+10-22.5520 8591.9299 0.000 11.200 0.009313 235879. -2575.1982 -0.000649 0.000 1.578E+10-17.2874 8910.1495 0.000 11.600 0.006371 224054. -2646.0866 -0.000579 0.000 1.578E+10-12.2494 9228.3691 0.000 12.000 0.003757 211865. -2693.4183 -0.000512 0.000 1.578E+10-7.4721 9546.5888 0.000 12.400 0.001452 199427. -2718.5129 -0.000450 0.000 1.578E+10-2.9840 9864.8084 0.000

Page 12

18new.lp6o 12.800 -0.000562 186847. -2722.8133 -0.000391 0.000 1.578E+101.1921 10183. 0.000 13.200 -0.002303 174227. -2707.8598 -0.000336 0.000 1.578E+105.0385 10501. 0.000 13.600 -0.003790 161659. -2675.2655 -0.000285 0.000 1.578E+108.5424 10819. 0.000 14.000 -0.005041 149229. -2626.6932 -0.000238 0.000 1.579E+1011.6960 11138. 0.000 14.400 -0.006074 137013. -2563.8332 -0.000194 0.000 1.579E+1014.4956 11456. 0.000 14.800 -0.006907 125082. -2488.3837 -0.000155 0.000 1.579E+1016.9417 11774. 0.000 15.200 -0.007557 113496. -2402.0317 -0.000118 0.000 1.579E+1019.0383 12092. 0.000 15.600 -0.008042 102307. -2306.4364 -8.547E-05 0.000 1.579E+1020.7930 12411. 0.000 16.000 -0.008378 91559. -2203.2145 -5.600E-05 0.000 1.579E+1022.2161 12729. 0.000 16.400 -0.008580 81290. -2093.9265 -2.972E-05 0.000 1.579E+1023.3205 13047. 0.000 16.800 -0.008663 71529. -1980.0657 -6.497E-06 0.000 1.579E+1024.1215 13365. 0.000 17.200 -0.008642 62297. -1863.0479 1.384E-05 0.000 1.579E+1024.6359 13683. 0.000 17.600 -0.008530 53610. -1744.2039 3.146E-05 0.000 1.579E+1024.8824 14002. 0.000 18.000 -0.008340 45477. -1624.7724 4.652E-05 0.000 1.579E+1024.8807 14320. 0.000 18.400 -0.008083 37901. -1505.8954 5.920E-05 0.000 1.579E+1024.6514 14638. 0.000 18.800 -0.007772 30879. -1388.6144 6.965E-05 0.000 1.579E+1024.2157 14956. 0.000 19.200 -0.007415 24403. -1273.8678 7.806E-05 0.000 1.579E+1023.5953 15275. 0.000 19.600 -0.007022 18462. -1162.4906 8.458E-05 0.000 1.578E+1022.8119 15593. 0.000 20.000 -0.006603 13040. -1055.2131 8.937E-05 0.000 1.578E+1021.8871 15911. 0.000 20.400 -0.006164 8117.6175 -952.6627 9.258E-05 0.000 1.578E+1020.8423 16229. 0.000 20.800 -0.005714 3672.3576 -855.3648 9.438E-05 0.000 1.578E+1019.6985 16547. 0.000 21.200 -0.005258 -320.3893 -763.7456 9.489E-05 0.000 1.578E+1018.4762 16866. 0.000 21.600 -0.004803 -3887.3283 -678.1346 9.425E-05 0.000 1.578E+1017.1951 17184. 0.000 22.000 -0.004354 -7056.6738 -598.7679 9.258E-05 0.000 1.578E+1015.8744 17502. 0.000 22.400 -0.003914 -9857.6988 -525.7921 9.001E-05 0.000 1.578E+1014.5322 17820. 0.000 22.800 -0.003489 -12320. -459.2676 8.664E-05 0.000 1.578E+1013.1863 18139. 0.000 23.200 -0.003083 -14475. -371.8472 8.256E-05 0.000 1.578E+1023.2389 36186. 0.000 23.600 -0.002697 -16088. -266.3104 7.792E-05 0.000 1.578E+1020.7348 36905. 0.000 24.000 -0.002335 -17218. -172.6288 7.285E-05 0.000 1.578E+1018.2992 37623. 0.000 24.400 -0.001998 -17920. -90.4163 6.751E-05 0.000 1.578E+1015.9560 38342. 0.000 24.800 -0.001687 -18248. -19.1829 6.201E-05 0.000 1.578E+1013.7246 39061. 0.000 25.200 -0.001402 -18253. 41.6463 5.646E-05 0.000 1.578E+10

Page 13

18new.lp6o11.6209 39780. 0.000 25.600 -0.001145 -17984. 92.7128 5.095E-05 0.000 1.578E+109.6568 40499. 0.000 26.000 -0.000913 -17485. 134.7076 4.555E-05 0.000 1.578E+107.8410 41217. 0.000 26.400 -0.000707 -16800. 168.3554 4.034E-05 0.000 1.578E+106.1789 41936. 0.000 26.800 -0.000526 -15966. 194.4001 3.536E-05 0.000 1.578E+104.6731 42655. 0.000 27.200 -0.000368 -15019. 213.5919 3.065E-05 0.000 1.578E+103.3235 43374. 0.000 27.600 -0.000232 -13989. 226.6755 2.624E-05 0.000 1.578E+102.1280 44093. 0.000 28.000 -0.000116 -12906. 234.3804 2.215E-05 0.000 1.578E+101.0824 44812. 0.000 28.400 -1.906E-05 -11792. 237.4121 1.839E-05 0.000 1.578E+100.1808 45530. 0.000 28.800 6.060E-05 -10671. 236.4445 1.497E-05 0.000 1.578E+10-0.5839 46249. 0.000 29.200 0.000125 -9558.3172 232.1148 1.190E-05 0.000 1.578E+10-1.2201 46968. 0.000 29.600 0.000175 -8470.7554 225.0181 9.157E-06 0.000 1.578E+10-1.7369 47687. 0.000 30.000 0.000213 -7420.1195 215.3085 6.740E-06 0.000 1.578E+10-2.3088 52128. 0.000 30.400 0.000240 -6419.9702 202.8147 4.636E-06 0.000 1.578E+10-2.8969 58052. 0.000 30.800 0.000257 -5484.2234 188.2882 2.825E-06 0.000 1.578E+10-3.1558 58918. 0.000 31.200 0.000267 -4619.1843 172.7434 1.289E-06 0.000 1.578E+10-3.3212 59785. 0.000 31.600 0.000269 -3828.9809 156.6005 4.409E-09 0.000 1.578E+10-3.4050 60651. 0.000 32.000 0.000267 -3115.8303 140.2253 -1.052E-06 0.000 1.578E+10-3.4180 61518. 0.000 32.400 0.000259 -2480.2944 123.9315 -1.903E-06 0.000 1.578E+10-3.3710 62384. 0.000 32.800 0.000248 -1921.5218 107.9843 -2.572E-06 0.000 1.578E+10-3.2736 63250. 0.000 33.200 0.000235 -1437.4727 92.6039 -3.083E-06 0.000 1.578E+10-3.1348 64117. 0.000 33.600 0.000219 -1025.1259 77.9698 -3.457E-06 0.000 1.578E+10-2.9627 64983. 0.000 34.000 0.000201 -680.6651 64.2252 -3.717E-06 0.000 1.578E+10-2.7643 65850. 0.000 34.400 0.000183 -399.6444 51.4811 -3.881E-06 0.000 1.578E+10-2.5458 66716. 0.000 34.800 0.000164 -177.1323 39.8214 -3.969E-06 0.000 1.578E+10-2.3124 67582. 0.000 35.200 0.000145 -7.8343 29.3069 -3.997E-06 0.000 1.578E+10-2.0686 68449. 0.000 35.600 0.000126 113.8061 19.9799 -3.981E-06 0.000 1.578E+10-1.8177 69315. 0.000 36.000 0.000107 193.5259 11.8681 -3.934E-06 0.000 1.578E+10-1.5622 70182. 0.000 36.400 8.811E-05 237.1810 4.9888 -3.868E-06 0.000 1.578E+10-1.3041 71048. 0.000 36.800 6.971E-05 250.7027 -0.6477 -3.794E-06 0.000 1.578E+10-1.0444 71914. 0.000 37.200 5.168E-05 240.0691 -5.0351 -3.720E-06 0.000 1.578E+10-0.7836 72781. 0.000 37.600 3.400E-05 211.2928 -8.1680 -3.651E-06 0.000 1.578E+10-0.5217 73647. 0.000

Page 14

18new.lp6o 38.000 1.663E-05 170.4188 -10.0398 -3.593E-06 0.000 1.578E+10-0.2582 74514. 0.000 38.400 -4.875E-07 123.5332 -10.6412 -3.548E-06 0.000 1.578E+100.007656 75380. 0.000 38.800 -1.743E-05 76.7789 -9.9584 -3.518E-06 0.000 1.578E+100.2768 76246. 0.000 39.200 -3.426E-05 36.3752 -7.9731 -3.500E-06 0.000 1.578E+100.5504 77113. 0.000 39.600 -5.103E-05 8.6383 -4.6625 -3.494E-06 0.000 1.578E+100.8291 77979. 0.000 40.000 -6.780E-05 0.000 0.000 -3.492E-06 0.000 1.578E+101.1136 39423. 0.000

* This analysis makes computations of pile response using nonlinear moment-curvaturerelationships. The above values of total stress are computed for combined axial and bending stress in elastic sections and do not equal actual stresses in concrete and steel in the range of nonlinear bending.

Output Summary for Load Case No. 1:

Pile-head deflection = 0.2500000 inchesComputed slope at pile head = -0.0026066 radiansMaximum bending moment = 306009. inch-lbsMaximum shear force = 5474.6246686 lbsDepth of maximum bending moment = 86.4000000 inches below pile headDepth of maximum shear force = 0.000000 inches below pile headNumber of iterations = 6Number of zero deflection points = 3

-------------------------------------------------------------------------------- Computed Values of Pile Loading and Deflection for Lateral Loading for Load Case Number 2--------------------------------------------------------------------------------

Pile-head conditions are Displacement and Moment (Loading Type 4)Displacement of pile head = 0.500000 inchesMoment at pile head = 0.000 in-lbsAxial load at pile head = 250000.000 lbs

Depth Deflect. Bending Shear Slope Total Bending Soil Res. Soil Spr. Distrib. X y Moment Force S Stress Stiffness p Es*h Lat. Load feet inches in-lbs lbs radians psi* lb-in^2 lb/in lb/inch lb/inch ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- 0.00 0.5000 0.000 10928. -0.005217 0.000 1.578E+100.000 0.000 0.000 0.400 0.4750 58714. 10852. -0.005208 0.000 1.578E+10-31.4876 318.2196 0.000 0.800 0.4500 116681. 10633. -0.005182 0.000 1.579E+10-59.6661 636.4393 0.000 1.200 0.4252 173231. 10287. -0.005138 0.000 1.578E+10-84.5692 954.6589 0.000 1.600 0.4007 227769. 9829.2604 -0.005077 0.000 1.578E+10-106.2528 1272.8785 0.000 2.000 0.3765 279776. 9274.7488 -0.004999 0.000 1.577E+10

Page 15

18new.lp6o-124.7937 1591.0981 0.000 2.400 0.3527 328805. 8638.5524 -0.004907 0.000 1.576E+10-140.2881 1909.3178 0.000 2.800 0.3294 374482. 7935.0186 -0.004800 0.000 1.575E+10-152.8509 2227.5374 0.000 3.200 0.3066 416501. 7177.9044 -0.004679 0.000 1.574E+10-162.6133 2545.7570 0.000 3.600 0.2845 454620. 6380.3019 -0.004546 0.000 1.573E+10-169.7211 2863.9766 0.000 4.000 0.2630 488662. 5554.5725 -0.004402 0.000 1.572E+10-174.3329 3182.1963 0.000 4.400 0.2422 518509. 4712.2910 -0.004248 0.000 1.571E+10-176.6178 3500.4159 0.000 4.800 0.2222 544096. 3864.1997 -0.004086 0.000 1.570E+10-176.7536 3818.6355 0.000 5.200 0.2030 565412. 3020.1732 -0.003916 0.000 1.569E+10-174.9242 4136.8551 0.000 5.600 0.1846 582489. 2189.1920 -0.003741 0.000 1.568E+10-171.3180 4455.0748 0.000 6.000 0.1671 595405. 1379.3279 -0.003560 0.000 1.567E+10-166.1254 4773.2944 0.000 6.400 0.1504 604275. 597.7376 -0.003377 0.000 1.567E+10-159.5372 5091.5140 0.000 6.800 0.1346 609247. -149.3339 -0.003191 0.000 1.567E+10-151.7425 5409.7336 0.000 7.200 0.1198 610499. -856.5406 -0.003004 0.000 1.567E+10-142.9269 5727.9533 0.000 7.600 0.1058 608234. -1519.4152 -0.002817 0.000 1.567E+10-133.2709 6046.1729 0.000 8.000 0.0927 602674. -2134.3417 -0.002632 0.000 1.567E+10-122.9485 6364.3925 0.000 8.400 0.0805 594060. -2698.5209 -0.002448 0.000 1.568E+10-112.1261 6682.6121 0.000 8.800 0.0692 582645. -3209.9302 -0.002268 0.000 1.568E+10-100.9611 7000.8318 0.000 9.200 0.0588 568689. -3667.2793 -0.002092 0.000 1.569E+10-89.6010 7319.0514 0.000 9.600 0.0491 552460. -4069.9607 -0.001921 0.000 1.569E+10-78.1829 7637.2710 0.000 10.000 0.0403 534227. -4417.9989 -0.001755 0.000 1.570E+10-66.8329 7955.4906 0.000 10.400 0.0323 514258. -4711.9952 -0.001594 0.000 1.571E+10-55.6655 8273.7103 0.000 10.800 0.0250 492818. -4953.0731 -0.001440 0.000 1.572E+10-44.7836 8591.9299 0.000 11.200 0.0185 470166. -5142.8212 -0.001293 0.000 1.572E+10-34.2781 8910.1495 0.000 11.600 0.0126 446551. -5283.2367 -0.001154 0.000 1.573E+10-24.2284 9228.3691 0.000 12.000 0.007392 422215. -5376.6696 -0.001021 0.000 1.574E+10-14.7020 9546.5888 0.000 12.400 0.002800 397386. -5425.7669 -0.000896 0.000 1.574E+10-5.7552 9864.8084 0.000 12.800 -0.001210 372278. -5433.4196 -0.000779 0.000 1.575E+102.5666 10183. 0.000 13.200 -0.004675 347094. -5402.7111 -0.000669 0.000 1.576E+1010.2286 10501. 0.000 13.600 -0.007633 322018. -5336.8677 -0.000567 0.000 1.576E+1017.2061 10819. 0.000 14.000 -0.0101 297221. -5239.2127 -0.000473 0.000 1.577E+1023.4835 11138. 0.000 14.400 -0.0122 272857. -5113.1229 -0.000386 0.000 1.577E+1029.0540 11456. 0.000

Page 16

18new.lp6o 14.800 -0.0138 249062. -4961.9884 -0.000307 0.000 1.577E+1033.9188 11774. 0.000 15.200 -0.0151 225958. -4789.1757 -0.000234 0.000 1.578E+1038.0865 12092. 0.000 15.600 -0.0161 203649. -4597.9952 -0.000169 0.000 1.578E+1041.5721 12411. 0.000 16.000 -0.0167 182223. -4391.6702 -0.000110 0.000 1.578E+1044.3966 12729. 0.000 16.400 -0.0171 161754. -4173.3121 -5.814E-05 0.000 1.578E+1046.5860 13047. 0.000 16.800 -0.0173 142299. -3945.8963 -1.191E-05 0.000 1.579E+1048.1706 13365. 0.000 17.200 -0.0173 123902. -3712.2441 2.855E-05 0.000 1.579E+1049.1845 13683. 0.000 17.600 -0.0170 106593. -3475.0057 6.359E-05 0.000 1.579E+1049.6648 14002. 0.000 18.000 -0.0166 90389. -3236.6479 9.353E-05 0.000 1.579E+1049.6509 14320. 0.000 18.400 -0.0161 75296. -2999.4441 0.000119 0.000 1.579E+1049.1840 14638. 0.000 18.800 -0.0155 61309. -2765.4669 0.000139 0.000 1.579E+1048.3065 14956. 0.000 19.200 -0.0148 48413. -2536.5840 0.000156 0.000 1.579E+1047.0614 15275. 0.000 19.600 -0.0140 36583. -2314.4555 0.000169 0.000 1.579E+1045.4922 15593. 0.000 20.000 -0.0132 25788. -2100.5338 0.000179 0.000 1.579E+1043.6419 15911. 0.000 20.400 -0.0123 15990. -1896.0657 0.000185 0.000 1.578E+1041.5532 16229. 0.000 20.800 -0.0114 7142.4174 -1702.0953 0.000188 0.000 1.578E+1039.2679 16547. 0.000 21.200 -0.0105 -802.6950 -1519.4684 0.000189 0.000 1.578E+1036.8267 16866. 0.000 21.600 -0.009572 -7899.0279 -1348.8386 0.000188 0.000 1.578E+1034.2691 17184. 0.000 22.000 -0.008675 -14203. -1190.6735 0.000185 0.000 1.578E+1031.6331 17502. 0.000 22.400 -0.007799 -19773. -1045.2620 0.000180 0.000 1.578E+1028.9551 17820. 0.000 22.800 -0.006952 -24668. -912.7217 0.000173 0.000 1.579E+1026.2700 18139. 0.000 23.200 -0.006140 -28950. -738.5754 0.000165 0.000 1.579E+1046.2910 36186. 0.000 23.600 -0.005371 -32154. -528.3639 0.000155 0.000 1.579E+1041.2972 36905. 0.000 24.000 -0.004649 -34395. -341.7926 0.000145 0.000 1.579E+1036.4408 37623. 0.000 24.400 -0.003977 -35784. -178.0887 0.000135 0.000 1.579E+1031.7691 38342. 0.000 24.800 -0.003357 -36427. -36.2721 0.000124 0.000 1.579E+1027.3211 39061. 0.000 25.200 -0.002791 -36428. 84.8059 0.000113 0.000 1.579E+1023.1280 39780. 0.000 25.600 -0.002277 -35883. 186.4262 0.000102 0.000 1.579E+1019.2138 40499. 0.000 26.000 -0.001816 -34882. 269.9682 9.076E-05 0.000 1.579E+1015.5954 41217. 0.000 26.400 -0.001406 -33509. 336.8780 8.036E-05 0.000 1.579E+1012.2837 41936. 0.000 26.800 -0.001045 -31841. 388.6396 7.043E-05 0.000 1.579E+109.2837 42655. 0.000 27.200 -0.000730 -29947. 426.7492 6.103E-05 0.000 1.579E+10

Page 17

18new.lp6o6.5954 43374. 0.000 27.600 -0.000459 -27891. 452.6922 5.224E-05 0.000 1.579E+104.2142 44093. 0.000 28.000 -0.000228 -25727. 467.9231 4.409E-05 0.000 1.579E+102.1320 44812. 0.000 28.400 -3.551E-05 -23505. 473.8483 3.660E-05 0.000 1.578E+100.3369 45530. 0.000 28.800 0.000123 -21266. 471.8118 2.980E-05 0.000 1.578E+10-1.1854 46249. 0.000 29.200 0.000251 -19047. 463.0834 2.367E-05 0.000 1.578E+10-2.4514 46968. 0.000 29.600 0.000350 -16877. 448.8493 1.820E-05 0.000 1.578E+10-3.4794 47687. 0.000 30.000 0.000425 -14781. 429.4139 1.339E-05 0.000 1.578E+10-4.6186 52128. 0.000 30.400 0.000479 -12787. 404.4325 9.198E-06 0.000 1.578E+10-5.7903 58052. 0.000 30.800 0.000514 -10921. 375.4060 5.592E-06 0.000 1.578E+10-6.3041 58918. 0.000 31.200 0.000532 -9196.3595 344.3599 2.533E-06 0.000 1.578E+10-6.6318 59785. 0.000 31.600 0.000538 -7621.1924 312.1313 -2.395E-08 0.000 1.578E+10-6.7968 60651. 0.000 32.000 0.000532 -6199.8415 279.4484 -2.126E-06 0.000 1.578E+10-6.8211 61518. 0.000 32.400 0.000517 -4933.3858 246.9360 -3.819E-06 0.000 1.578E+10-6.7257 62384. 0.000 32.800 0.000496 -3820.0909 215.1219 -5.150E-06 0.000 1.578E+10-6.5302 63250. 0.000 33.200 0.000468 -2855.8569 184.4442 -6.165E-06 0.000 1.578E+10-6.2522 64117. 0.000 33.600 0.000436 -2034.6314 155.2600 -6.908E-06 0.000 1.578E+10-5.9079 64983. 0.000 34.000 0.000402 -1348.7803 127.8540 -7.423E-06 0.000 1.578E+10-5.5113 65850. 0.000 34.400 0.000365 -789.4179 102.4470 -7.748E-06 0.000 1.578E+10-5.0749 66716. 0.000 34.800 0.000327 -346.6938 79.2054 -7.921E-06 0.000 1.578E+10-4.6091 67582. 0.000 35.200 0.000289 -10.0364 58.2498 -7.975E-06 0.000 1.578E+10-4.1224 68449. 0.000 35.600 0.000251 231.6448 39.6641 -7.941E-06 0.000 1.578E+10-3.6217 69315. 0.000 36.000 0.000213 389.7983 23.5031 -7.847E-06 0.000 1.578E+10-3.1121 70182. 0.000 36.400 0.000175 476.1075 9.8009 -7.715E-06 0.000 1.578E+10-2.5972 71048. 0.000 36.800 0.000139 502.4037 -1.4225 -7.566E-06 0.000 1.578E+10-2.0792 71914. 0.000 37.200 0.000103 480.6111 -10.1546 -7.417E-06 0.000 1.578E+10-1.5591 72781. 0.000 37.600 6.758E-05 422.7204 -16.3850 -7.280E-06 0.000 1.578E+10-1.0369 73647. 0.000 38.000 3.294E-05 340.7864 -20.1008 -7.164E-06 0.000 1.578E+10-0.5114 74514. 0.000 38.400 -1.192E-06 246.9451 -21.2832 -7.074E-06 0.000 1.578E+100.0187 75380. 0.000 38.800 -3.497E-05 153.4451 -19.9052 -7.013E-06 0.000 1.578E+100.5555 76246. 0.000 39.200 -6.852E-05 72.6868 -15.9303 -6.979E-06 0.000 1.578E+101.1008 77113. 0.000 39.600 -0.000102 17.2638 -9.3128 -6.965E-06 0.000 1.578E+101.6565 77979. 0.000

Page 18

18new.lp6o 40.000 -0.000135 0.000 0.000 -6.963E-06 0.000 1.578E+102.2239 39423. 0.000

* This analysis makes computations of pile response using nonlinear moment-curvaturerelationships. The above values of total stress are computed for combined axial and bending stress in elastic sections and do not equal actual stresses in concrete and steel in the range of nonlinear bending.

Output Summary for Load Case No. 2:

Pile-head deflection = 0.5000000 inchesComputed slope at pile head = -0.0052174 radiansMaximum bending moment = 610499. inch-lbsMaximum shear force = 10928. lbsDepth of maximum bending moment = 86.4000000 inches below pile headDepth of maximum shear force = 0.000000 inches below pile headNumber of iterations = 6Number of zero deflection points = 3

-------------------------------------------------------------------------------- Computed Values of Pile Loading and Deflection for Lateral Loading for Load Case Number 3--------------------------------------------------------------------------------

Pile-head conditions are Displacement and Moment (Loading Type 4)Displacement of pile head = 0.750000 inchesMoment at pile head = 0.000 in-lbsAxial load at pile head = 250000.000 lbs

Depth Deflect. Bending Shear Slope Total Bending Soil Res. Soil Spr. Distrib. X y Moment Force S Stress Stiffness p Es*h Lat. Load feet inches in-lbs lbs radians psi* lb-in^2 lb/in lb/inch lb/inch ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- 0.00 0.7500 0.000 15453. -0.008002 0.000 1.578E+100.000 0.000 0.000 0.400 0.7116 83777. 15353. -0.007989 0.000 1.578E+10-41.7415 281.5652 0.000 0.800 0.6733 166563. 15041. -0.007951 0.000 1.578E+10-88.3661 629.9655 0.000 1.200 0.6353 247251. 14525. -0.007888 0.000 1.577E+10-126.3447 954.6589 0.000 1.600 0.5976 324938. 13842. -0.007801 0.000 1.576E+10-158.4666 1272.8785 0.000 2.000 0.5604 398855. 13016. -0.007691 0.000 1.574E+10-185.7494 1591.0981 0.000 2.400 0.5237 468347. 12070. -0.007559 0.000 1.572E+10-208.3309 1909.3178 0.000 2.800 0.4878 532867. 11027. -0.007406 0.000 1.570E+10-226.3748 2227.5374 0.000 3.200 0.4526 591976. 9907.1525 -0.007234 0.000 1.568E+10-240.0683 2545.7570 0.000 3.600 0.4184 645337. 8731.9020 -0.007044 0.000 1.565E+10-249.6194 2863.9766 0.000 4.000 0.3850 692708. 7520.2047 -0.006831 0.000 1.463E+10

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18new.lp6o-255.2545 3182.1963 0.000 4.400 0.3528 733926. 6290.1579 -0.006593 0.000 1.415E+10-257.2650 3500.4159 0.000 4.800 0.3217 768918. 5058.4399 -0.006334 0.000 1.370E+10-255.9508 3818.6355 0.000 5.200 0.2920 797689. 3840.2365 -0.006055 0.000 1.330E+10-251.6339 4136.8551 0.000 5.600 0.2636 820317. 2649.1442 -0.005760 0.000 1.296E+10-244.6545 4455.0748 0.000 6.000 0.2367 836944. 1497.1024 -0.005450 0.000 1.270E+10-235.3629 4773.2944 0.000 6.400 0.2113 847768. 394.3619 -0.005129 0.000 1.253E+10-224.1123 5091.5140 0.000 6.800 0.1874 853039. -650.5092 -0.004802 0.000 1.245E+10-211.2506 5409.7336 0.000 7.200 0.1652 853049. -1630.5787 -0.004473 0.000 1.245E+10-197.1117 5727.9533 0.000 7.600 0.1445 848122. -2540.4694 -0.004146 0.000 1.253E+10-182.0095 6046.1729 0.000 8.000 0.1254 838612. -3376.2519 -0.003825 0.000 1.268E+10-166.2332 6364.3925 0.000 8.400 0.1078 824890. -4135.3144 -0.003513 0.000 1.289E+10-150.0429 6682.6121 0.000 8.800 0.0916 807344. -4816.2231 -0.003212 0.000 1.316E+10-133.6691 7000.8318 0.000 9.200 0.0769 786364. -5418.5796 -0.002925 0.000 1.346E+10-117.3128 7319.0514 0.000 9.600 0.0636 762345. -5942.8848 -0.002652 0.000 1.379E+10-101.1477 7637.2710 0.000 10.000 0.0515 735676. -6390.4118 -0.002394 0.000 1.413E+10-85.3219 7955.4906 0.000 10.400 0.0406 706742. -6763.0904 -0.002152 0.000 1.447E+10-69.9609 8273.7103 0.000 10.800 0.0308 675915. -7063.4039 -0.001931 0.000 1.562E+10-55.1697 8591.9299 0.000 11.200 0.0221 643568. -7294.0528 -0.001728 0.000 1.565E+10-40.9340 8910.1495 0.000 11.600 0.0142 610040. -7457.9520 -0.001536 0.000 1.567E+10-27.3574 9228.3691 0.000 12.000 0.007305 575658. -7558.4768 -0.001355 0.000 1.568E+10-14.5279 9546.5888 0.000 12.400 0.001225 540730. -7599.3876 -0.001184 0.000 1.570E+10-2.5182 9864.8084 0.000 12.800 -0.004060 505545. -7584.7579 -0.001024 0.000 1.571E+108.6140 10183. 0.000 13.200 -0.008605 470374. -7518.9041 -0.000875 0.000 1.572E+1018.8251 10501. 0.000 13.600 -0.0125 435464. -7406.3195 -0.000737 0.000 1.573E+1028.0851 10819. 0.000 14.000 -0.0157 401041. -7251.6112 -0.000609 0.000 1.574E+1036.3766 11138. 0.000 14.400 -0.0183 367310. -7059.4420 -0.000492 0.000 1.575E+1043.6939 11456. 0.000 14.800 -0.0204 334452. -6834.4762 -0.000385 0.000 1.576E+1050.0419 11774. 0.000 15.200 -0.0220 302624. -6581.3302 -0.000288 0.000 1.576E+1055.4356 12092. 0.000 15.600 -0.0232 271962. -6304.5287 -0.000201 0.000 1.577E+1059.8984 12411. 0.000 16.000 -0.0239 242582. -6008.4647 -0.000122 0.000 1.577E+1063.4616 12729. 0.000 16.400 -0.0243 214575. -5697.3655 -5.282E-05 0.000 1.578E+1066.1631 13047. 0.000

Page 20

18new.lp6o 16.800 -0.0244 188014. -5375.2623 8.408E-06 0.000 1.578E+1068.0466 13365. 0.000 17.200 -0.0243 162952. -5045.9654 6.178E-05 0.000 1.578E+1069.1605 13683. 0.000 17.600 -0.0238 139424. -4713.0435 0.000108 0.000 1.579E+1069.5570 14002. 0.000 18.000 -0.0232 117448. -4379.8075 0.000147 0.000 1.579E+1069.2914 14320. 0.000 18.400 -0.0224 97026. -4049.2979 0.000179 0.000 1.579E+1068.4210 14638. 0.000 18.800 -0.0215 78144. -3724.2763 0.000206 0.000 1.579E+1067.0047 14956. 0.000 19.200 -0.0205 60778. -3407.2204 0.000227 0.000 1.579E+1065.1019 15275. 0.000 19.600 -0.0193 44890. -3100.3219 0.000243 0.000 1.579E+1062.7724 15593. 0.000 20.000 -0.0181 30431. -2805.4872 0.000255 0.000 1.579E+1060.0753 15911. 0.000 20.400 -0.0169 17346. -2524.3408 0.000262 0.000 1.578E+1057.0690 16229. 0.000 20.800 -0.0156 5569.2227 -2258.2306 0.000265 0.000 1.578E+1053.8103 16547. 0.000 21.200 -0.0143 -4969.8873 -2008.2348 0.000265 0.000 1.578E+1050.3547 16866. 0.000 21.600 -0.0131 -14347. -1775.1703 0.000263 0.000 1.578E+1046.7555 17184. 0.000 22.000 -0.0118 -22642. -1559.6026 0.000257 0.000 1.578E+1043.0643 17502. 0.000 22.400 -0.0106 -29936. -1361.8561 0.000249 0.000 1.579E+1039.3301 17820. 0.000 22.800 -0.009421 -36313. -1182.0248 0.000239 0.000 1.579E+1035.5996 18139. 0.000 23.200 -0.008301 -41857. -946.4031 0.000227 0.000 1.579E+1062.5761 36186. 0.000 23.600 -0.007242 -45943. -662.5948 0.000214 0.000 1.579E+1055.6773 36905. 0.000 24.000 -0.006250 -48730. -411.4008 0.000199 0.000 1.579E+1048.9868 37623. 0.000 24.400 -0.005329 -50371. -191.6710 0.000184 0.000 1.579E+1042.5673 38342. 0.000 24.800 -0.004482 -51012. -1.9815 0.000169 0.000 1.579E+1036.4700 39061. 0.000 25.200 -0.003709 -50795. 159.3127 0.000153 0.000 1.579E+1030.7359 39780. 0.000 25.600 -0.003010 -49851. 294.0285 0.000138 0.000 1.579E+1025.3957 40499. 0.000 26.000 -0.002384 -48303. 404.1081 0.000123 0.000 1.579E+1020.4708 41217. 0.000 26.400 -0.001828 -46267. 491.5763 0.000109 0.000 1.579E+1015.9743 41936. 0.000 26.800 -0.001340 -43845. 558.5016 9.501E-05 0.000 1.579E+1011.9113 42655. 0.000 27.200 -0.000916 -41133. 606.9615 8.209E-05 0.000 1.579E+108.2803 43374. 0.000 27.600 -0.000552 -38215. 639.0111 7.003E-05 0.000 1.579E+105.0737 44093. 0.000 28.000 -0.000244 -35167. 656.6568 5.887E-05 0.000 1.579E+102.2787 44812. 0.000 28.400 1.284E-05 -32053. 661.8334 4.865E-05 0.000 1.579E+10-0.1218 45530. 0.000 28.800 0.000223 -28930. 656.3846 3.938E-05 0.000 1.579E+10-2.1485 46249. 0.000 29.200 0.000391 -25846. 642.0480 3.105E-05 0.000 1.579E+10

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18new.lp6o-3.8251 46968. 0.000 29.600 0.000521 -22841. 620.4428 2.365E-05 0.000 1.578E+10-5.1771 47687. 0.000 30.000 0.000618 -19946. 591.9109 1.715E-05 0.000 1.578E+10-6.7112 52128. 0.000 30.400 0.000686 -17200. 555.9006 1.150E-05 0.000 1.578E+10-8.2931 58052. 0.000 30.800 0.000728 -14637. 514.5406 6.656E-06 0.000 1.578E+10-8.9402 58918. 0.000 31.200 0.000750 -12276. 470.6764 2.564E-06 0.000 1.578E+10-9.3365 59785. 0.000 31.600 0.000753 -10125. 425.4348 -8.426E-07 0.000 1.578E+10-9.5141 60651. 0.000 32.000 0.000742 -8189.7150 379.7926 -3.628E-06 0.000 1.578E+10-9.5035 61518. 0.000 32.400 0.000718 -6470.3433 334.5842 -5.857E-06 0.000 1.578E+10-9.3333 62384. 0.000 32.800 0.000685 -4963.6504 290.5115 -7.596E-06 0.000 1.578E+10-9.0303 63250. 0.000 33.200 0.000645 -3663.2037 248.1542 -8.907E-06 0.000 1.578E+10-8.6186 64117. 0.000 33.600 0.000600 -2559.9922 207.9816 -9.854E-06 0.000 1.578E+10-8.1200 64983. 0.000 34.000 0.000551 -1642.9317 170.3645 -1.049E-05 0.000 1.578E+10-7.5538 65850. 0.000 34.400 0.000499 -899.3108 135.5878 -1.088E-05 0.000 1.578E+10-6.9365 66716. 0.000 34.800 0.000446 -315.1781 103.8634 -1.106E-05 0.000 1.578E+10-6.2821 67582. 0.000 35.200 0.000393 124.3312 75.3417 -1.109E-05 0.000 1.578E+10-5.6020 68449. 0.000 35.600 0.000340 434.7251 50.1242 -1.101E-05 0.000 1.578E+10-4.9053 69315. 0.000 36.000 0.000287 631.9425 28.2746 -1.085E-05 0.000 1.578E+10-4.1987 70182. 0.000 36.400 0.000236 732.1915 9.8295 -1.064E-05 0.000 1.578E+10-3.4868 71048. 0.000 36.800 0.000185 751.8382 -5.1921 -1.041E-05 0.000 1.578E+10-2.7722 71914. 0.000 37.200 0.000136 707.3380 -16.7802 -1.019E-05 0.000 1.578E+10-2.0561 72781. 0.000 37.600 8.720E-05 615.2067 -24.9260 -9.990E-06 0.000 1.578E+10-1.3380 73647. 0.000 38.000 3.970E-05 492.0238 -29.6163 -9.821E-06 0.000 1.578E+10-0.6163 74514. 0.000 38.400 -7.081E-06 354.4611 -30.8286 -9.693E-06 0.000 1.578E+100.1112 75380. 0.000 38.800 -5.335E-05 219.3312 -28.5280 -9.605E-06 0.000 1.578E+100.8474 76246. 0.000 39.200 -9.929E-05 103.6453 -22.6659 -9.556E-06 0.000 1.578E+101.5952 77113. 0.000 39.600 -0.000145 24.6740 -13.1806 -9.537E-06 0.000 1.578E+102.3570 77979. 0.000 40.000 -0.000191 0.000 0.000 -9.533E-06 0.000 1.578E+103.1349 39423. 0.000

* This analysis makes computations of pile response using nonlinear moment-curvaturerelationships. The above values of total stress are computed for combined axial and bending stress in elastic sections and do not equal actual stresses in concrete and steel in the range of nonlinear bending.

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18new.lp6o

Output Summary for Load Case No. 3:

Pile-head deflection = 0.7500000 inchesComputed slope at pile head = -0.0080021 radiansMaximum bending moment = 853049. inch-lbsMaximum shear force = 15453. lbsDepth of maximum bending moment = 86.4000000 inches below pile headDepth of maximum shear force = 0.000000 inches below pile headNumber of iterations = 11Number of zero deflection points = 3

-------------------------------------------------------------------------------- Computed Values of Pile Loading and Deflection for Lateral Loading for Load Case Number 4--------------------------------------------------------------------------------

Pile-head conditions are Displacement and Pile-head Rotation (Loading Type 5)Displacement of pile head = 0.250000 inchesRotation of pile head = 0.000E+00 radiansAxial load on pile head = 250000.000 lbs

Depth Deflect. Bending Shear Slope Total Bending Soil Res. Soil Spr. Distrib. X y Moment Force S Stress Stiffness p Es*h Lat. Load feet inches in-lbs lbs radians psi* lb-in^2 lb/in lb/inch lb/inch ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- 0.00 0.2500 -883668. 14746. 0.000 0.000 1.196E+100.000 0.000 0.000 0.400 0.2491 -812863. 14667. -0.000341 0.000 1.196E+10-16.5175 318.2196 0.000 0.800 0.2467 -742048. 14549. -0.000631 0.000 1.405E+10-32.7144 636.4393 0.000 1.200 0.2431 -671681. 14354. -0.000860 0.000 1.563E+10-48.3486 954.6589 0.000 1.600 0.2385 -602182. 14086. -0.001056 0.000 1.567E+10-63.2381 1272.8785 0.000 2.000 0.2330 -533917. 13749. -0.001230 0.000 1.570E+10-77.2209 1591.0981 0.000 2.400 0.2267 -467237. 13348. -0.001383 0.000 1.572E+10-90.1614 1909.3178 0.000 2.800 0.2197 -402462. 12887. -0.001515 0.000 1.574E+10-101.9496 2227.5374 0.000 3.200 0.2121 -339889. 12372. -0.001628 0.000 1.576E+10-112.5000 2545.7570 0.000 3.600 0.2041 -279784. 11810. -0.001723 0.000 1.577E+10-121.7505 2863.9766 0.000 4.000 0.1956 -222381. 11206. -0.001799 0.000 1.578E+10-129.6605 3182.1963 0.000 4.400 0.1868 -167885. 10568. -0.001859 0.000 1.578E+10-136.2102 3500.4159 0.000 4.800 0.1777 -116466. 9901.9452 -0.001902 0.000 1.579E+10-141.3984 3818.6355 0.000 5.200 0.1685 -68262. 9214.0109 -0.001930 0.000 1.579E+10-145.2409 4136.8551 0.000 5.600 0.1592 -23380. 8510.7860 -0.001944 0.000 1.578E+10-147.7694 4455.0748 0.000 6.000 0.1499 18107. 7798.4696 -0.001945 0.000 1.578E+10

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18new.lp6o-149.0291 4773.2944 0.000 6.400 0.1405 56153. 7083.0138 -0.001933 0.000 1.579E+10-149.0775 5091.5140 0.000 6.800 0.1313 90743. 6370.0703 -0.001911 0.000 1.579E+10-147.9823 5409.7336 0.000 7.200 0.1222 121892. 5664.9443 -0.001879 0.000 1.579E+10-145.8202 5727.9533 0.000 7.600 0.1133 149636. 4972.5566 -0.001837 0.000 1.579E+10-142.6747 6046.1729 0.000 8.000 0.1046 174038. 4297.4138 -0.001788 0.000 1.578E+10-138.6349 6364.3925 0.000 8.400 0.0961 195182. 3643.5849 -0.001732 0.000 1.578E+10-133.7938 6682.6121 0.000 8.800 0.0879 213173. 3014.6863 -0.001670 0.000 1.578E+10-128.2472 7000.8318 0.000 9.200 0.0801 228131. 2413.8726 -0.001603 0.000 1.578E+10-122.0918 7319.0514 0.000 9.600 0.0725 240193. 1843.8338 -0.001532 0.000 1.578E+10-115.4243 7637.2710 0.000 10.000 0.0654 249508. 1306.7988 -0.001457 0.000 1.577E+10-108.3403 7955.4906 0.000 10.400 0.0586 256235. 804.5432 -0.001380 0.000 1.577E+10-100.9329 8273.7103 0.000 10.800 0.0521 260544. 338.4024 -0.001301 0.000 1.577E+10-93.2924 8591.9299 0.000 11.200 0.0461 262607. -90.7111 -0.001222 0.000 1.577E+10-85.5049 8910.1495 0.000 11.600 0.0404 262605. -482.2873 -0.001142 0.000 1.577E+10-77.6519 9228.3691 0.000 12.000 0.0351 260718. -836.1949 -0.001062 0.000 1.577E+10-69.8096 9546.5888 0.000 12.400 0.0302 257127. -1152.6552 -0.000983 0.000 1.577E+10-62.0488 9864.8084 0.000 12.800 0.0257 252013. -1432.2139 -0.000906 0.000 1.577E+10-54.4340 10183. 0.000 13.200 0.0215 245552. -1675.7119 -0.000830 0.000 1.577E+10-47.0235 10501. 0.000 13.600 0.0177 237919. -1884.2543 -0.000757 0.000 1.578E+10-39.8692 10819. 0.000 14.000 0.0142 229280. -2059.1799 -0.000686 0.000 1.578E+10-33.0165 11138. 0.000 14.400 0.0111 219796. -2202.0300 -0.000617 0.000 1.578E+10-26.5043 11456. 0.000 14.800 0.008302 209622. -2314.5171 -0.000552 0.000 1.578E+10-20.3653 11774. 0.000 15.200 0.005806 198902. -2398.4955 -0.000490 0.000 1.578E+10-14.6257 12092. 0.000 15.600 0.003599 187772. -2455.9311 -0.000431 0.000 1.578E+10-9.3058 12411. 0.000 16.000 0.001667 176359. -2488.8740 -0.000376 0.000 1.578E+10-4.4204 12729. 0.000 16.400 -7.916E-06 164781. -2499.4313 -0.000324 0.000 1.578E+100.0215 13047. 0.000 16.800 -0.001442 153142. -2489.7418 -0.000276 0.000 1.579E+104.0158 13365. 0.000 17.200 -0.002653 141540. -2461.9528 -0.000231 0.000 1.579E+107.5630 13683. 0.000 17.600 -0.003657 130061. -2418.1980 -0.000189 0.000 1.579E+1010.6682 14002. 0.000 18.000 -0.004472 118780. -2360.5776 -0.000152 0.000 1.579E+1013.3403 14320. 0.000 18.400 -0.005113 107764. -2291.1408 -0.000117 0.000 1.579E+1015.5917 14638. 0.000

Page 24

18new.lp6o 18.800 -0.005597 97067. -2211.8690 -8.604E-05 0.000 1.579E+1017.4382 14956. 0.000 19.200 -0.005939 86736. -2124.6619 -5.810E-05 0.000 1.579E+1018.8981 15275. 0.000 19.600 -0.006154 76809. -2031.3253 -3.324E-05 0.000 1.579E+1019.9922 15593. 0.000 20.000 -0.006258 67315. -1933.5601 -1.134E-05 0.000 1.579E+1020.7434 15911. 0.000 20.400 -0.006263 58274. -1832.9532 7.753E-06 0.000 1.579E+1021.1761 16229. 0.000 20.800 -0.006183 49700. -1730.9709 2.417E-05 0.000 1.579E+1021.3165 16547. 0.000 21.200 -0.006031 41599. -1628.9517 3.804E-05 0.000 1.579E+1021.1915 16866. 0.000 21.600 -0.005818 33971. -1528.1028 4.953E-05 0.000 1.579E+1020.8289 17184. 0.000 22.000 -0.005556 26810. -1429.4957 5.877E-05 0.000 1.579E+1020.2574 17502. 0.000 22.400 -0.005254 20107. -1334.0643 6.590E-05 0.000 1.578E+1019.5057 17820. 0.000 22.800 -0.004923 13845. -1242.6029 7.107E-05 0.000 1.578E+1018.6032 18139. 0.000 23.200 -0.004572 8007.1937 -1115.2397 7.439E-05 0.000 1.578E+1034.4648 36186. 0.000 23.600 -0.004209 2960.3484 -954.8620 7.606E-05 0.000 1.578E+1032.3592 36905. 0.000 24.000 -0.003842 -1342.0212 -804.9335 7.630E-05 0.000 1.578E+1030.1110 37623. 0.000 24.400 -0.003476 -4950.1435 -666.0228 7.535E-05 0.000 1.578E+1027.7685 38342. 0.000 24.800 -0.003118 -7916.6738 -538.4777 7.339E-05 0.000 1.578E+1025.3753 39061. 0.000 25.200 -0.002772 -10296. -422.4473 7.062E-05 0.000 1.578E+1022.9707 39780. 0.000 25.600 -0.002440 -12142. -317.9037 6.721E-05 0.000 1.578E+1020.5891 40499. 0.000 26.000 -0.002127 -13509. -224.6646 6.331E-05 0.000 1.578E+1018.2605 41217. 0.000 26.400 -0.001833 -14450. -142.4152 5.906E-05 0.000 1.578E+1016.0101 41936. 0.000 26.800 -0.001560 -15018. -70.7289 5.458E-05 0.000 1.578E+1013.8592 42655. 0.000 27.200 -0.001309 -15260. -9.0878 4.997E-05 0.000 1.578E+1011.8246 43374. 0.000 27.600 -0.001080 -15225. 43.0979 4.534E-05 0.000 1.578E+109.9195 44093. 0.000 28.000 -0.000873 -14955. 86.4725 4.075E-05 0.000 1.578E+108.1533 44812. 0.000 28.400 -0.000689 -14493. 121.7182 3.627E-05 0.000 1.578E+106.5324 45530. 0.000 28.800 -0.000525 -13874. 149.5400 3.196E-05 0.000 1.578E+105.0600 46249. 0.000 29.200 -0.000382 -13134. 170.6526 2.785E-05 0.000 1.578E+103.7369 46968. 0.000 29.600 -0.000258 -12303. 185.7680 2.398E-05 0.000 1.578E+102.5613 47687. 0.000 30.000 -0.000152 -11408. 195.8684 2.038E-05 0.000 1.578E+101.6472 52128. 0.000 30.400 -6.220E-05 -10471. 201.6272 1.705E-05 0.000 1.578E+100.7523 58052. 0.000 30.800 1.199E-05 -9513.1904 203.0794 1.401E-05 0.000 1.578E+10-0.1472 58918. 0.000 31.200 7.229E-05 -8555.1801 200.5653 1.126E-05 0.000 1.578E+10

Page 25

18new.lp6o-0.9004 59785. 0.000 31.600 0.000120 -7614.7931 194.7620 8.803E-06 0.000 1.578E+10-1.5176 60651. 0.000 32.000 0.000157 -6706.5929 186.2966 6.626E-06 0.000 1.578E+10-2.0096 61518. 0.000 32.400 0.000184 -5842.2470 175.7432 4.717E-06 0.000 1.578E+10-2.3876 62384. 0.000 32.800 0.000202 -5030.7801 163.6217 3.064E-06 0.000 1.578E+10-2.6630 63250. 0.000 33.200 0.000213 -4278.8323 150.3981 1.648E-06 0.000 1.578E+10-2.8469 64117. 0.000 33.600 0.000218 -3590.9148 136.4852 4.516E-07 0.000 1.578E+10-2.9502 64983. 0.000 34.000 0.000217 -2969.6585 122.2449 -5.460E-07 0.000 1.578E+10-2.9833 65850. 0.000 34.400 0.000213 -2416.0532 107.9907 -1.365E-06 0.000 1.578E+10-2.9560 66716. 0.000 34.800 0.000204 -1929.6720 93.9908 -2.026E-06 0.000 1.578E+10-2.8773 67582. 0.000 35.200 0.000193 -1508.8793 80.4723 -2.549E-06 0.000 1.578E+10-2.7554 68449. 0.000 35.600 0.000180 -1151.0211 67.6247 -2.953E-06 0.000 1.578E+10-2.5977 69315. 0.000 36.000 0.000165 -852.5949 55.6045 -3.258E-06 0.000 1.578E+10-2.4107 70182. 0.000 36.400 0.000149 -609.3996 44.5394 -3.480E-06 0.000 1.578E+10-2.1998 71048. 0.000 36.800 0.000131 -416.6644 34.5328 -3.636E-06 0.000 1.578E+10-1.9697 71914. 0.000 37.200 0.000114 -269.1580 25.6677 -3.740E-06 0.000 1.578E+10-1.7241 72781. 0.000 37.600 9.556E-05 -161.2774 18.0110 -3.806E-06 0.000 1.578E+10-1.4662 73647. 0.000 38.000 7.717E-05 -87.1185 11.6170 -3.844E-06 0.000 1.578E+10-1.1980 74514. 0.000 38.400 5.866E-05 -40.5298 6.5309 -3.863E-06 0.000 1.578E+10-0.9212 75380. 0.000 38.800 4.009E-05 -15.1508 2.7917 -3.872E-06 0.000 1.578E+10-0.6368 76246. 0.000 39.200 2.149E-05 -4.4374 0.4348 -3.875E-06 0.000 1.578E+10-0.3453 77113. 0.000 39.600 2.892E-06 -1.6778 -0.5066 -3.875E-06 0.000 1.578E+10-0.0470 77979. 0.000 40.000 -1.571E-05 0.000 0.000 -3.876E-06 0.000 1.578E+100.2581 39423. 0.000

* This analysis makes computations of pile response using nonlinear moment-curvaturerelationships. The above values of total stress are computed for combined axial and bending stress in elastic sections and do not equal actual stresses in concrete and steel in the range of nonlinear bending.

Output Summary for Load Case No. 4:

Pile-head deflection = 0.2500000 inchesComputed slope at pile head = -0.0000142 radiansMaximum bending moment = -883668. inch-lbsMaximum shear force = 14746. lbsDepth of maximum bending moment = 0.000000 inches below pile headDepth of maximum shear force = 0.000000 inches below pile headNumber of iterations = 9

Page 26

18new.lp6oNumber of zero deflection points = 3

-------------------------------------------------------------------------------- Computed Values of Pile Loading and Deflection for Lateral Loading for Load Case Number 5--------------------------------------------------------------------------------

Pile-head conditions are Displacement and Pile-head Rotation (Loading Type 5)Displacement of pile head = 0.500000 inchesRotation of pile head = 0.000E+00 radiansAxial load on pile head = 250000.000 lbs

Depth Deflect. Bending Shear Slope Total Bending Soil Res. Soil Spr. Distrib. X y Moment Force S Stress Stiffness p Es*h Lat. Load feet inches in-lbs lbs radians psi* lb-in^2 lb/in lb/inch lb/inch ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- 0.00 0.5000 -1264467. 24423. 0.000 0.000 4.375E+090.000 0.000 0.000 0.400 0.4967 -1146785. 24265. -0.001323 0.000 4.375E+09-32.9272 318.2196 0.000 0.800 0.4873 -1028352. 24031. -0.002215 0.000 9.369E+09-64.6121 636.4393 0.000 1.200 0.4754 -910775. 23649. -0.002669 0.000 1.148E+10-94.5519 954.6589 0.000 1.600 0.4617 -794919. 23128. -0.003002 0.000 1.334E+10-122.4297 1272.8785 0.000 2.000 0.4466 -681542. 22479. -0.003253 0.000 1.516E+10-148.0324 1591.0981 0.000 2.400 0.4304 -571316. 21713. -0.003449 0.000 1.569E+10-171.2211 1909.3178 0.000 2.800 0.4135 -464825. 20841. -0.003607 0.000 1.572E+10-191.8812 2227.5374 0.000 3.200 0.3958 -362584. 19877. -0.003733 0.000 1.575E+10-209.9295 2545.7570 0.000 3.600 0.3776 -265048. 18832. -0.003829 0.000 1.577E+10-225.3205 2863.9766 0.000 4.000 0.3591 -172607. 17720. -0.003895 0.000 1.578E+10-238.0437 3182.1963 0.000 4.400 0.3402 -85587. 16553. -0.003935 0.000 1.579E+10-248.1207 3500.4159 0.000 4.800 0.3213 -4252.2501 15344. -0.003948 0.000 1.578E+10-255.6025 3818.6355 0.000 5.200 0.3023 71195. 14106. -0.003938 0.000 1.579E+10-260.5664 4136.8551 0.000 5.600 0.2835 140612. 12849. -0.003906 0.000 1.579E+10-263.1135 4455.0748 0.000 6.000 0.2648 203916. 11585. -0.003854 0.000 1.578E+10-263.3652 4773.2944 0.000 6.400 0.2465 261078. 10326. -0.003783 0.000 1.577E+10-261.4603 5091.5140 0.000 6.800 0.2285 312120. 9079.9281 -0.003696 0.000 1.576E+10-257.5526 5409.7336 0.000 7.200 0.2110 357115. 7857.4653 -0.003594 0.000 1.575E+10-251.8070 5727.9533 0.000 7.600 0.1940 396177. 6666.5745 -0.003479 0.000 1.574E+10-244.3975 6046.1729 0.000 8.000 0.1776 429463. 5514.8101 -0.003353 0.000 1.573E+10

Page 27

18new.lp6o-235.5043 6364.3925 0.000 8.400 0.1618 457166. 4408.8534 -0.003218 0.000 1.573E+10-225.3110 6682.6121 0.000 8.800 0.1467 479510. 3354.5017 -0.003075 0.000 1.572E+10-214.0022 7000.8318 0.000 9.200 0.1323 496748. 2356.6682 -0.002926 0.000 1.571E+10-201.7617 7319.0514 0.000 9.600 0.1186 509156. 1419.3929 -0.002772 0.000 1.571E+10-188.7697 7637.2710 0.000 10.000 0.1057 517027. 545.8617 -0.002615 0.000 1.571E+10-175.2016 7955.4906 0.000 10.400 0.0935 520673. -261.5645 -0.002457 0.000 1.571E+10-161.2260 8273.7103 0.000 10.800 0.0821 520412. -1001.3152 -0.002298 0.000 1.571E+10-147.0035 8591.9299 0.000 11.200 0.0715 516574. -1672.5678 -0.002139 0.000 1.571E+10-132.6851 8910.1495 0.000 11.600 0.0616 509489. -2275.2006 -0.001982 0.000 1.571E+10-118.4119 9228.3691 0.000 12.000 0.0524 499490. -2809.7417 -0.001828 0.000 1.571E+10-104.3135 9546.5888 0.000 12.400 0.0440 486904. -3277.3140 -0.001678 0.000 1.572E+10-90.5083 9864.8084 0.000 12.800 0.0363 472054. -3679.5789 -0.001531 0.000 1.572E+10-77.1021 10183. 0.000 13.200 0.0293 455254. -4018.6777 -0.001390 0.000 1.573E+10-64.1890 10501. 0.000 13.600 0.0230 436810. -4297.1730 -0.001254 0.000 1.573E+10-51.8506 10819. 0.000 14.000 0.0173 417010. -4517.9896 -0.001123 0.000 1.574E+10-40.1563 11138. 0.000 14.400 0.0122 396133. -4684.3574 -0.000999 0.000 1.574E+10-29.1636 11456. 0.000 14.800 0.007713 374439. -4799.7544 -0.000882 0.000 1.575E+10-18.9185 11774. 0.000 15.200 0.003753 352172. -4867.8526 -0.000771 0.000 1.575E+10-9.4558 12092. 0.000 15.600 0.000309 329558. -4892.4658 -0.000667 0.000 1.576E+10-0.7998 12411. 0.000 16.000 -0.002653 306806. -4877.5007 -0.000570 0.000 1.576E+107.0352 12729. 0.000 16.400 -0.005167 284103. -4826.9103 -0.000480 0.000 1.577E+1014.0441 13047. 0.000 16.800 -0.007266 261620. -4744.6516 -0.000397 0.000 1.577E+1020.2304 13365. 0.000 17.200 -0.008982 239508. -4634.6456 -0.000321 0.000 1.578E+1025.6055 13683. 0.000 17.600 -0.0103 217899. -4500.7419 -0.000252 0.000 1.578E+1030.1877 14002. 0.000 18.000 -0.0114 196905. -4346.6864 -0.000189 0.000 1.578E+1034.0020 14320. 0.000 18.400 -0.0122 176623. -4176.0929 -0.000132 0.000 1.578E+1037.0786 14638. 0.000 18.800 -0.0127 157131. -3992.4174 -8.096E-05 0.000 1.579E+1039.4528 14956. 0.000 19.200 -0.0129 138490. -3798.9373 -3.601E-05 0.000 1.579E+1041.1639 15275. 0.000 19.600 -0.0130 120747. -3598.7328 3.397E-06 0.000 1.579E+1042.2547 15593. 0.000 20.000 -0.0129 103934. -3394.6713 3.755E-05 0.000 1.579E+1042.7709 15911. 0.000 20.400 -0.0126 88068. -3189.3958 6.674E-05 0.000 1.579E+1042.7605 16229. 0.000

Page 28

18new.lp6o 20.800 -0.0123 73156. -2985.3150 9.124E-05 0.000 1.579E+1042.2731 16547. 0.000 21.200 -0.0118 59190. -2784.5962 0.000111 0.000 1.579E+1041.3597 16866. 0.000 21.600 -0.0112 46156. -2589.1604 0.000127 0.000 1.579E+1040.0719 17184. 0.000 22.000 -0.0105 34029. -2400.6791 0.000140 0.000 1.579E+1038.4619 17502. 0.000 22.400 -0.009854 22775. -2220.5736 0.000148 0.000 1.578E+1036.5821 17820. 0.000 22.800 -0.009126 12355. -2050.0140 0.000154 0.000 1.578E+1034.4844 18139. 0.000 23.200 -0.008380 2726.1325 -1815.6402 0.000156 0.000 1.578E+1063.1713 36186. 0.000 23.600 -0.007630 -5448.7011 -1523.2448 0.000155 0.000 1.578E+1058.6601 36905. 0.000 24.000 -0.006888 -12270. -1252.8930 0.000153 0.000 1.578E+1053.9865 37623. 0.000 24.400 -0.006164 -17843. -1005.1641 0.000148 0.000 1.578E+1049.2338 38342. 0.000 24.800 -0.005465 -22275. -780.2600 0.000142 0.000 1.578E+1044.4762 39061. 0.000 25.200 -0.004800 -25674. -578.0476 0.000135 0.000 1.579E+1039.7790 39780. 0.000 25.600 -0.004172 -28148. -398.1015 0.000127 0.000 1.579E+1035.1986 40499. 0.000 26.000 -0.003585 -29800. -239.7462 0.000118 0.000 1.579E+1030.7828 41217. 0.000 26.400 -0.003041 -30732. -102.0965 0.000109 0.000 1.579E+1026.5712 41936. 0.000 26.800 -0.002543 -31041. 15.9035 9.917E-05 0.000 1.579E+1022.5954 42655. 0.000 27.200 -0.002089 -30817. 115.4437 8.976E-05 0.000 1.579E+1018.8796 43374. 0.000 27.600 -0.001681 -30148. 197.8138 8.049E-05 0.000 1.579E+1015.4412 44093. 0.000 28.000 -0.001317 -29111. 264.3717 7.149E-05 0.000 1.579E+1012.2912 44812. 0.000 28.400 -0.000995 -27781. 316.5151 6.284E-05 0.000 1.579E+109.4352 45530. 0.000 28.800 -0.000713 -26224. 355.6555 5.463E-05 0.000 1.579E+106.8734 46249. 0.000 29.200 -0.000470 -24498. 383.1959 4.691E-05 0.000 1.579E+104.6018 46968. 0.000 29.600 -0.000263 -22658. 400.5107 3.974E-05 0.000 1.578E+102.6127 47687. 0.000 30.000 -8.875E-05 -20749. 409.0944 3.314E-05 0.000 1.578E+100.9638 52128. 0.000 30.400 5.519E-05 -18810. 409.8055 2.713E-05 0.000 1.578E+10-0.6675 58052. 0.000 30.800 0.000172 -16880. 403.1459 2.170E-05 0.000 1.578E+10-2.1073 58918. 0.000 31.200 0.000264 -14992. 390.2110 1.685E-05 0.000 1.578E+10-3.2823 59785. 0.000 31.600 0.000333 -13174. 372.2204 1.257E-05 0.000 1.578E+10-4.2138 60651. 0.000 32.000 0.000384 -11449. 350.2893 8.828E-06 0.000 1.578E+10-4.9242 61518. 0.000 32.400 0.000418 -9832.4806 325.4259 5.591E-06 0.000 1.578E+10-5.4356 62384. 0.000 32.800 0.000438 -8337.9699 298.5320 2.828E-06 0.000 1.578E+10-5.7702 63250. 0.000 33.200 0.000445 -6973.3612 270.4053 5.001E-07 0.000 1.578E+10

Page 29

18new.lp6o-5.9493 64117. 0.000 33.600 0.000443 -5743.2789 241.7432 -1.434E-06 0.000 1.578E+10-5.9933 64983. 0.000 34.000 0.000432 -4649.1854 213.1484 -3.014E-06 0.000 1.578E+10-5.9213 65850. 0.000 34.400 0.000414 -3689.8210 185.1352 -4.282E-06 0.000 1.578E+10-5.7509 66716. 0.000 34.800 0.000391 -2861.6113 158.1370 -5.278E-06 0.000 1.578E+10-5.4983 67582. 0.000 35.200 0.000363 -2159.0381 132.5145 -6.042E-06 0.000 1.578E+10-5.1777 68449. 0.000 35.600 0.000333 -1574.9718 108.5639 -6.609E-06 0.000 1.578E+10-4.8017 69315. 0.000 36.000 0.000300 -1100.9624 86.5251 -7.016E-06 0.000 1.578E+10-4.3811 70182. 0.000 36.400 0.000265 -727.4913 66.5911 -7.294E-06 0.000 1.578E+10-3.9248 71048. 0.000 36.800 0.000230 -444.1814 48.9154 -7.473E-06 0.000 1.578E+10-3.4401 71914. 0.000 37.200 0.000193 -239.9693 33.6205 -7.577E-06 0.000 1.578E+10-2.9328 72781. 0.000 37.600 0.000157 -103.2408 20.8050 -7.629E-06 0.000 1.578E+10-2.4070 73647. 0.000 38.000 0.000120 -21.9320 10.5505 -7.648E-06 0.000 1.578E+10-1.8657 74514. 0.000 38.400 8.346E-05 16.3990 2.9273 -7.649E-06 0.000 1.578E+10-1.3107 75380. 0.000 38.800 4.676E-05 24.5265 -2.0009 -7.642E-06 0.000 1.578E+10-0.7427 76246. 0.000 39.200 1.009E-05 15.5326 -4.1725 -7.636E-06 0.000 1.578E+10-0.1621 77113. 0.000 39.600 -2.655E-05 2.7977 -3.5264 -7.634E-06 0.000 1.578E+100.4313 77979. 0.000 40.000 -6.319E-05 0.000 0.000 -7.633E-06 0.000 1.578E+101.0380 39423. 0.000

* This analysis makes computations of pile response using nonlinear moment-curvaturerelationships. The above values of total stress are computed for combined axial and bending stress in elastic sections and do not equal actual stresses in concrete and steel in the range of nonlinear bending.

Output Summary for Load Case No. 5:

Pile-head deflection = 0.5000000 inchesComputed slope at pile head = -0.0000646 radiansMaximum bending moment = -1264467. inch-lbsMaximum shear force = 24423. lbsDepth of maximum bending moment = 0.000000 inches below pile headDepth of maximum shear force = 0.000000 inches below pile headNumber of iterations = 28Number of zero deflection points = 3

-------------------------------------------------------------------------------- Computed Values of Pile Loading and Deflection for Lateral Loading for Load Case Number 6--------------------------------------------------------------------------------

Pile-head conditions are Displacement and Pile-head Rotation (Loading Type 5)Page 30

18new.lp6oDisplacement of pile head = 0.750000 inchesRotation of pile head = 0.000E+00 radiansAxial load on pile head = 250000.000 lbs

Depth Deflect. Bending Shear Slope Total Bending Soil Res. Soil Spr. Distrib. X y Moment Force S Stress Stiffness p Es*h Lat. Load feet inches in-lbs lbs radians psi* lb-in^2 lb/in lb/inch lb/inch ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- 0.00 0.7500 -1284040. 29903. 0.000 0.000 1.821E+090.000 0.000 0.000 0.400 0.7419 -1138957. 29702. -0.003193 0.000 1.821E+09-41.7414 270.0694 0.000 0.800 0.7193 -991233. 29390. -0.004931 0.000 1.003E+10-88.4707 590.3376 0.000 1.200 0.6945 -844979. 28849. -0.005329 0.000 1.257E+10-137.1118 947.5790 0.000 1.600 0.6682 -701497. 28094. -0.005606 0.000 1.453E+10-177.1931 1272.8785 0.000 2.000 0.6407 -561820. 27159. -0.005808 0.000 1.569E+10-212.3870 1591.0981 0.000 2.400 0.6124 -426829. 26065. -0.005959 0.000 1.574E+10-243.6109 1909.3178 0.000 2.800 0.5835 -297295. 24830. -0.006069 0.000 1.577E+10-270.7937 2227.5374 0.000 3.200 0.5542 -173892. 23475. -0.006141 0.000 1.578E+10-293.9121 2545.7570 0.000 3.600 0.5246 -57197. 22018. -0.006176 0.000 1.579E+10-312.9874 2863.9766 0.000 4.000 0.4949 52308. 20480. -0.006177 0.000 1.579E+10-328.0820 3182.1963 0.000 4.400 0.4653 154235. 18878. -0.006146 0.000 1.579E+10-339.2960 3500.4159 0.000 4.800 0.4359 248288. 17232. -0.006084 0.000 1.577E+10-346.7629 3818.6355 0.000 5.200 0.4069 334261. 15558. -0.005996 0.000 1.576E+10-350.6459 4136.8551 0.000 5.600 0.3783 412033. 13874. -0.005882 0.000 1.574E+10-351.1343 4455.0748 0.000 6.000 0.3504 481564. 12195. -0.005746 0.000 1.572E+10-348.4389 4773.2944 0.000 6.400 0.3232 542891. 10536. -0.005589 0.000 1.570E+10-342.7888 5091.5140 0.000 6.800 0.2967 596120. 8910.3349 -0.005415 0.000 1.567E+10-334.4267 5409.7336 0.000 7.200 0.2712 641425. 7331.0563 -0.005225 0.000 1.565E+10-323.6060 5727.9533 0.000 7.600 0.2466 679039. 5808.9933 -0.005022 0.000 1.562E+10-310.5869 6046.1729 0.000 8.000 0.2230 709245. 4354.0662 -0.004800 0.000 1.444E+10-295.6328 6364.3925 0.000 8.400 0.2005 732358. 2974.6502 -0.004558 0.000 1.417E+10-279.1239 6682.6121 0.000 8.800 0.1792 748742. 1677.4606 -0.004306 0.000 1.397E+10-261.3717 7000.8318 0.000 9.200 0.1592 758795. 467.7357 -0.004045 0.000 1.383E+10-242.6804 7319.0514 0.000 9.600 0.1404 762941. -650.7162 -0.003781 0.000 1.378E+10-223.3413 7637.2710 0.000 10.000 0.1229 761623. -1675.4368 -0.003515 0.000 1.380E+10

Page 31

18new.lp6o-203.6257 7955.4906 0.000 10.400 0.1066 755294. -2605.2120 -0.003252 0.000 1.388E+10-183.7807 8273.7103 0.000 10.800 0.0916 744418. -3439.9494 -0.002994 0.000 1.402E+10-164.0266 8591.9299 0.000 11.200 0.0779 729457. -4180.5485 -0.002744 0.000 1.421E+10-144.5564 8910.1495 0.000 11.600 0.0653 710870. -4828.7698 -0.002502 0.000 1.442E+10-125.5358 9228.3691 0.000 12.000 0.0539 689107. -5387.1106 -0.002271 0.000 1.468E+10-107.1062 9546.5888 0.000 12.400 0.0435 664605. -5858.6807 -0.002057 0.000 1.563E+10-89.3814 9864.8084 0.000 12.800 0.0341 637799. -6246.8621 -0.001857 0.000 1.565E+10-72.3609 10183. 0.000 13.200 0.0257 609091. -6555.2895 -0.001666 0.000 1.567E+10-56.1505 10501. 0.000 13.600 0.0181 578866. -6788.0661 -0.001484 0.000 1.568E+10-40.8397 10819. 0.000 14.000 0.0114 547487. -6949.6851 -0.001311 0.000 1.570E+10-26.5015 11138. 0.000 14.400 0.005528 515297. -7044.9525 -0.001149 0.000 1.571E+10-13.1933 11456. 0.000 14.800 0.000390 482613. -7078.9145 -0.000997 0.000 1.572E+10-0.9576 11774. 0.000 15.200 -0.004040 449731. -7056.7873 -0.000854 0.000 1.573E+1010.1773 12092. 0.000 15.600 -0.007811 416919. -6983.8910 -0.000722 0.000 1.574E+1020.1962 12411. 0.000 16.000 -0.0110 384419. -6865.5880 -0.000600 0.000 1.575E+1029.0967 12729. 0.000 16.400 -0.0136 352449. -6707.2262 -0.000488 0.000 1.575E+1036.8874 13047. 0.000 16.800 -0.0157 321200. -6514.0864 -0.000385 0.000 1.576E+1043.5875 13365. 0.000 17.200 -0.0173 290838. -6291.3359 -0.000292 0.000 1.577E+1049.2252 13683. 0.000 17.600 -0.0185 261504. -6043.9863 -0.000208 0.000 1.577E+1053.8371 14002. 0.000 18.000 -0.0193 233314. -5776.8563 -0.000133 0.000 1.578E+1057.4670 14320. 0.000 18.400 -0.0197 206364. -5494.5401 -6.567E-05 0.000 1.578E+1060.1647 14638. 0.000 18.800 -0.0199 180724. -5201.3799 -6.798E-06 0.000 1.578E+1061.9854 14956. 0.000 19.200 -0.0198 156447. -4901.4432 4.447E-05 0.000 1.579E+1062.9883 15275. 0.000 19.600 -0.0195 133564. -4598.5045 8.856E-05 0.000 1.579E+1063.2362 15593. 0.000 20.000 -0.0189 112089. -4296.0305 0.000126 0.000 1.579E+1062.7946 15911. 0.000 20.400 -0.0183 92020. -3997.1699 0.000157 0.000 1.579E+1061.7307 16229. 0.000 20.800 -0.0174 73339. -3704.7456 0.000182 0.000 1.579E+1060.1128 16547. 0.000 21.200 -0.0165 56017. -3421.2502 0.000202 0.000 1.579E+1058.0102 16866. 0.000 21.600 -0.0155 40011. -3148.8449 0.000216 0.000 1.579E+1055.4920 17184. 0.000 22.000 -0.0144 25269. -2889.3590 0.000226 0.000 1.579E+1052.6271 17502. 0.000 22.400 -0.0133 11730. -2644.2931 0.000232 0.000 1.578E+1049.4837 17820. 0.000

Page 32

18new.lp6o 22.800 -0.0122 -672.6194 -2414.8221 0.000234 0.000 1.578E+1046.1292 18139. 0.000 23.200 -0.0111 -12012. -2103.5239 0.000232 0.000 1.578E+1083.5784 36186. 0.000 23.600 -0.009984 -21422. -1718.7162 0.000227 0.000 1.578E+1076.7581 36905. 0.000 24.000 -0.008912 -29056. -1366.8506 0.000219 0.000 1.579E+1069.8526 37623. 0.000 24.400 -0.007882 -35069. -1048.0890 0.000209 0.000 1.579E+1062.9647 38342. 0.000 24.800 -0.006904 -39619. -762.1294 0.000198 0.000 1.579E+1056.1851 39061. 0.000 25.200 -0.005984 -42860. -508.2652 0.000185 0.000 1.579E+1049.5916 39780. 0.000 25.600 -0.005126 -44943. -285.4447 0.000172 0.000 1.579E+1043.2502 40499. 0.000 26.000 -0.004334 -46013. -92.3281 0.000158 0.000 1.579E+1037.2150 41217. 0.000 26.400 -0.003609 -46209. 72.6582 0.000144 0.000 1.579E+1031.5292 41936. 0.000 26.800 -0.002951 -45661. 211.2694 0.000130 0.000 1.579E+1026.2254 42655. 0.000 27.200 -0.002360 -44493. 325.3947 0.000116 0.000 1.579E+1021.3268 43374. 0.000 27.600 -0.001834 -42817. 417.0130 0.000103 0.000 1.579E+1016.8475 44093. 0.000 28.000 -0.001370 -40737. 488.1527 9.039E-05 0.000 1.579E+1012.7940 44812. 0.000 28.400 -0.000966 -38348. 540.8556 7.837E-05 0.000 1.579E+109.1655 45530. 0.000 28.800 -0.000618 -35733. 577.1453 6.711E-05 0.000 1.579E+105.9552 46249. 0.000 29.200 -0.000322 -32968. 598.9997 5.667E-05 0.000 1.579E+103.1508 46968. 0.000 29.600 -7.406E-05 -30119. 608.3275 4.708E-05 0.000 1.579E+100.7358 47687. 0.000 30.000 0.000130 -27241. 606.7069 3.836E-05 0.000 1.579E+10-1.4110 52128. 0.000 30.400 0.000294 -24386. 594.7823 3.051E-05 0.000 1.579E+10-3.5576 58052. 0.000 30.800 0.000423 -21604. 573.7892 2.351E-05 0.000 1.578E+10-5.1896 58918. 0.000 31.200 0.000520 -18934. 545.7936 1.735E-05 0.000 1.578E+10-6.4753 59785. 0.000 31.600 0.000589 -16406. 512.3809 1.198E-05 0.000 1.578E+10-7.4467 60651. 0.000 32.000 0.000635 -14044. 474.9815 7.345E-06 0.000 1.578E+10-8.1363 61518. 0.000 32.400 0.000660 -11864. 434.8722 3.405E-06 0.000 1.578E+10-8.5759 62384. 0.000 32.800 0.000668 -9877.5481 393.1791 9.912E-08 0.000 1.578E+10-8.7963 63250. 0.000 33.200 0.000661 -8089.9381 350.8837 -2.633E-06 0.000 1.578E+10-8.8268 64117. 0.000 33.600 0.000642 -6502.7454 308.8312 -4.852E-06 0.000 1.578E+10-8.6950 64983. 0.000 34.000 0.000614 -5113.5132 267.7399 -6.618E-06 0.000 1.578E+10-8.4263 65850. 0.000 34.400 0.000579 -3916.5577 228.2116 -7.992E-06 0.000 1.578E+10-8.0438 66716. 0.000 34.800 0.000538 -2903.5015 190.7436 -9.029E-06 0.000 1.578E+10-7.5679 67582. 0.000 35.200 0.000492 -2063.7499 155.7406 -9.784E-06 0.000 1.578E+10

Page 33

18new.lp6o-7.0167 68449. 0.000 35.600 0.000444 -1384.9097 123.5272 -1.031E-05 0.000 1.578E+10-6.4056 69315. 0.000 36.000 0.000393 -853.1483 94.3601 -1.065E-05 0.000 1.578E+10-5.7474 70182. 0.000 36.400 0.000341 -453.4955 68.4402 -1.085E-05 0.000 1.578E+10-5.0526 71048. 0.000 36.800 0.000289 -170.0880 45.9242 -1.094E-05 0.000 1.578E+10-4.3291 71914. 0.000 37.200 0.000236 13.6386 26.9351 -1.097E-05 0.000 1.578E+10-3.5830 72781. 0.000 37.600 0.000184 114.8079 11.5723 -1.095E-05 0.000 1.578E+10-2.8182 73647. 0.000 38.000 0.000131 151.0041 -0.0801 -1.091E-05 0.000 1.578E+10-2.0370 74514. 0.000 38.400 7.898E-05 140.2133 -7.9456 -1.086E-05 0.000 1.578E+10-1.2403 75380. 0.000 38.800 2.694E-05 100.7951 -11.9495 -1.083E-05 0.000 1.578E+10-0.4280 76246. 0.000 39.200 -2.494E-05 51.4790 -12.0149 -1.080E-05 0.000 1.578E+100.4007 77113. 0.000 39.600 -7.676E-05 11.3768 -8.0605 -1.079E-05 0.000 1.578E+101.2469 77979. 0.000 40.000 -0.000129 0.000 0.000 -1.079E-05 0.000 1.578E+102.1116 39423. 0.000

* This analysis makes computations of pile response using nonlinear moment-curvaturerelationships. The above values of total stress are computed for combined axial and bending stress in elastic sections and do not equal actual stresses in concrete and steel in the range of nonlinear bending.

Output Summary for Load Case No. 6:

Pile-head deflection = 0.7500000 inchesComputed slope at pile head = -0.0001912 radiansMaximum bending moment = -1284040. inch-lbsMaximum shear force = 29903. lbsDepth of maximum bending moment = 0.000000 inches below pile headDepth of maximum shear force = 0.000000 inches below pile headNumber of iterations = 24Number of zero deflection points = 3

-------------------------------------------------------------------------------- Summary of Pile Response(s)--------------------------------------------------------------------------------

Definitions of Pile-head Loading Conditions:

Load Type 1: Load 1 = Shear, lbs, and Load 2 = Moment, in-lbsLoad Type 2: Load 1 = Shear, lbs, and Load 2 = Slope, radiansLoad Type 3: Load 1 = Shear, lbs, and Load 2 = Rotational Stiffness, in-lbs/radianLoad Type 4: Load 1 = Top Deflection, inches, and Load 2 = Moment, in-lbsLoad Type 5: Load 1 = Top Deflection, inches, and Load 2 = Slope, radians

Pile-head Pile-head MaximumPage 34

18new.lp6o MaximumLoad Load Condition 1 Condition 2 Axial Pile-head Moment Shear Pile-headCase Type V(lbs) or in-lb, rad., Loading Deflection in Pile in Pile Rotation No. No. y(inches) or in-lb/rad. lbs inches in-lbs lbs radians---- ---- -------------- -------------- ------------- -------------------------- ------------- ------------- 1 4 y = 0.2500 M = 0.000 250000. 0.25000000306009. 5474.6247 -0.00260658 2 4 y = 0.5000 M = 0.000 250000. 0.50000000610499. 10928. -0.00521735 3 4 y = 0.7500 M = 0.000 250000. 0.75000000853049. 15453. -0.00800208 4 5 y = 0.2500 S = 0.000 250000. 0.25000000-883668. 14746. -0.00001421 5 5 y = 0.5000 S = 0.000 250000. 0.50000000-1264467. 24423. -0.00006456 6 5 y = 0.7500 S = 0.000 250000. 0.75000000-1284040. 29903. -0.00019117

The analysis ended normally.

Page 35

Lateral Deflection (inches)

Dep

th (f

t)

-0.1 0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8

02

46

810

1214

1618

2022

2426

2830

3234

3638

Case 1Case 2Case 3Case 4Case 5Case 6

Lateral Deflection (inches)

Dep

th (f

t)

-0.1 0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.

02

46

810

1214

1618

2022

2426

2830

3234

3638

Case 1Case 2Case 3Case 4Case 5Case 6

Bending Moment (in-kips)

Dep

th (f

t)

-4000 -3500 -3000 -2500 -2000 -1500 -1000 -500 0 500 1000 1500 2000

02

46

810

1214

1618

2022

2426

2830

3234

3638

Case 1Case 2Case 3Case 4Case 5Case 6

Bending Moment (in-kips)

Dep

th (f

t)

-4000 -3500 -3000 -2500 -2000 -1500 -1000 -500 0 500 1000 1500 20

02

46

810

1214

1618

2022

2426

2830

3234

3638

Case 1Case 2Case 3Case 4Case 5Case 6

Shear Force (kips)D

epth

(ft)

-8 -6 -4 -2 0 2 4 60

24

68

1012

1416

1820

2224

2628

3032

3436

38

Case 1Case 2Case 3Case 4Case 5Case 6

24new.lp6o================================================================================

LPile Plus for Windows, Version 2012-06.037

Analysis of Individual Piles and Drilled Shafts Subjected to Lateral Loading Using the p-y Method

© 1985-2012 by Ensoft, Inc. All Rights Reserved

================================================================================

This copy of LPile is licensed to:

Dennis NguyenAECOM

Serial Number of Security Device: 294790092Company Name Stored in Security Device: URS Corporation

-------------------------------------------------------------------------------- Files Used for Analysis--------------------------------------------------------------------------------

Path to file locations:\\losangeles.na.aecomnet.com\LosAngeles\Projects\ENV\_legacy\GT\Da Wu\LA County Geotech On-call\MLK\Report\2019 BHC - Lab\Appendix F and G\Name of input data file: 24new.lp6dName of output report file: 24new.lp6oName of plot output file: 24new.lp6pName of runtime messeage file: 24new.lp6r

-------------------------------------------------------------------------------- Date and Time of Analysis--------------------------------------------------------------------------------

Date: April 8, 2019 Time: 15:09:01

-------------------------------------------------------------------------------- Problem Title--------------------------------------------------------------------------------

Project Name: MLK DHS Lab & Red Bag Storage

Job Number: 60595699

Client: LACDPW

Engineer: Dennis Nguyen

Description:

Page 1

24new.lp6o

-------------------------------------------------------------------------------- Program Options--------------------------------------------------------------------------------

Engineering units are US Customary Units: pounds, inches, feet

Basic Program Options:

This analysis computes pile response to lateral loading and will compute nonlinear moment-curvature and nominal moment capacity for section types with nonlinear properties.

Computation Options:- Analysis does not use p-y multipliers (individual pile or shaft only)- Analysis assumes no shear resistance at pile tip- Analysis for fixed-length pile or shaft only- No computation of foundation stiffness matrix values- Report pile response for full length of pile- Analysis assumes no loading by soil movements acting on pile- No p-y curves to be computed and reported for user-specified depths

Solution Control Parameters:- Number of pile increments = 100- Maximum number of iterations allowed = 100- Deflection tolerance for convergence = 1.0000E-05 in- Maximum allowable deflection = 100.0000 in

Pile Response Output Options:- Values of pile-head deflection, bending moment, shear force, and soil reaction are printed for full length of pile.- Printing Increment (nodal spacing of output points) = 1

-------------------------------------------------------------------------------- Pile Structural Properties and Geometry--------------------------------------------------------------------------------

Total number of pile sections = 1

Total length of pile = 40.00 ft

Depth of ground surface below top of pile = 0.00 ft

Pile diameter values used for p-y curve computations are defined using 2 points.

p-y curves are computed using pile diameter values interpolated with depth over the length of the pile.

Point Depth Pile X Diameter ft in----- --------- ----------- 1 0.00000 24.0000000 2 40.000000 24.0000000

Input Structural Properties:----------------------------

Page 2

24new.lp6oPile Section No. 1:

Section Type = Drilled Shaft (Bored Pile) Section Length = 40.00000000 ft Section Diameter = 24.00000000 in

-------------------------------------------------------------------------------- Ground Slope and Pile Batter Angles--------------------------------------------------------------------------------

Ground Slope Angle = 0.000 degrees = 0.000 radians

Pile Batter Angle = 0.000 degrees = 0.000 radians

-------------------------------------------------------------------------------- Soil and Rock Layering Information--------------------------------------------------------------------------------

The soil profile is modelled using 5 layers

Layer 1 is sand, p-y criteria by Reese et al., 1974

Distance from top of pile to top of layer = 0.0000 ft Distance from top of pile to bottom of layer = 23.00000 ft Effective unit weight at top of layer = 125.00000 pcf Effective unit weight at bottom of layer = 125.00000 pcf Friction angle at top of layer = 26.00000 deg. Friction angle at bottom of layer = 26.00000 deg. Subgrade k at top of layer = 0.0000 pci Subgrade k at bottom of layer = 0.0000 pci

NOTE: Internal default values for subgrade k will be computed for the above soil layer.

Layer 2 is sand, p-y criteria by Reese et al., 1974

Distance from top of pile to top of layer = 23.00000 ft Distance from top of pile to bottom of layer = 30.00000 ft Effective unit weight at top of layer = 62.60000 pcf Effective unit weight at bottom of layer = 62.60000 pcf Friction angle at top of layer = 30.00000 deg. Friction angle at bottom of layer = 30.00000 deg. Subgrade k at top of layer = 0.0000 pci Subgrade k at bottom of layer = 0.0000 pci

NOTE: Internal default values for subgrade k will be computed for the above soil layer.

Layer 3 is sand, p-y criteria by Reese et al., 1974

Distance from top of pile to top of layer = 30.00000 ft Distance from top of pile to bottom of layer = 45.00000 ft Effective unit weight at top of layer = 47.60000 pcf Effective unit weight at bottom of layer = 47.60000 pcf Friction angle at top of layer = 31.00000 deg.

Page 3

24new.lp6o Friction angle at bottom of layer = 31.00000 deg. Subgrade k at top of layer = 0.0000 pci Subgrade k at bottom of layer = 0.0000 pci

NOTE: Internal default values for subgrade k will be computed for the above soil layer.

Layer 4 is soft clay, p-y criteria by Matlock, 1970

Distance from top of pile to top of layer = 45.00000 ft Distance from top of pile to bottom of layer = 54.00000 ft Effective unit weight at top of layer = 57.60000 pcf Effective unit weight at bottom of layer = 57.60000 pcf Undrained cohesion at top of layer = 1500.00000 psf Undrained cohesion at bottom of layer = 1500.00000 psf Epsilon-50 at top of layer = 0.0000 Epsilon-50 at bottom of layer = 0.0000

NOTE: Internal default values for Epsilon-50 will be computed for the above soil layer.

Layer 5 is sand, p-y criteria by Reese et al., 1974

Distance from top of pile to top of layer = 54.00000 ft Distance from top of pile to bottom of layer = 61.50000 ft Effective unit weight at top of layer = 62.60000 pcf Effective unit weight at bottom of layer = 62.60000 pcf Friction angle at top of layer = 31.00000 deg. Friction angle at bottom of layer = 31.00000 deg. Subgrade k at top of layer = 0.0000 pci Subgrade k at bottom of layer = 0.0000 pci

NOTE: Internal default values for subgrade k will be computed for the above soil layer.

(Depth of lowest soil layer extends 21.50 ft below pile tip)

-------------------------------------------------------------------------------- Summary of Soil Properties--------------------------------------------------------------------------------

Layer Layer Effective UndrainedAngle of StrainLayer Soil Type Depth Unit Wt. CohesionFriction Factor kpy Num. (p-y Curve Criteria) ft pcf psf deg. Epsilon 50 pci----- ---------------------------------- ---------- ---------- -------------------- ---------- ---------- 1 Sand (Reese, et al.) 0.00 125.000 -- 26.000 -- default 23.000 125.000 -- 26.000 -- default 2 Sand (Reese, et al.) 23.000 62.600 -- 30.000 -- default 30.000 62.600 -- 30.000 -- default 3 Sand (Reese, et al.) 30.000 47.600 --

Page 4

24new.lp6o 31.000 -- default 45.000 47.600 -- 31.000 -- default 4 Soft Clay 45.000 57.600 1500.000 -- default -- 54.000 57.600 1500.000 -- default -- 5 Sand (Reese, et al.) 54.000 62.600 -- 31.000 -- default 61.500 62.600 -- 31.000 -- default

-------------------------------------------------------------------------------- Loading Type--------------------------------------------------------------------------------

Static loading criteria were used when computing p-y curves for all analyses.

-------------------------------------------------------------------------------- Pile-head Loading and Pile-head Fixity Conditions--------------------------------------------------------------------------------

Number of loads specified = 6

Load Load Condition Condition Axial Thrust Compute No. Type 1 2 Force, lbsTop y vs. Pile Length----- ---- -------------------- ----------------------- ------------------------------------- 1 4 y = 0.25000 in M = 0.0000 in-lbs 250000. No 2 4 y = 0.50000 in M = 0.0000 in-lbs 250000. No 3 4 y = 0.75000 in M = 0.0000 in-lbs 250000. No 4 5 y = 0.25000 in S = 0.0000 in/in 250000. No 5 5 y = 0.50000 in S = 0.0000 in/in 250000. No 6 5 y = 0.75000 in S = 0.0000 in/in 250000. No

V = perpendicular shear force applied to pile headM = bending moment applied to pile heady = lateral deflection relative to pile axisS = pile slope relative to original pile batter angleR = rotational stiffness applie to pile headAxial thrust is assumed to be acting axially for all pile batter angles.

-------------------------------------------------------------------------------- Computations of Nominal Moment Capacity and Nonlinear Bending Stiffness--------------------------------------------------------------------------------

Axial thrust force values were determined from pile-head loading conditions

Number of Pile Sections Analyzed = 1

Page 5

24new.lp6oPile Section No. 1:-------------------

Dimensions and Properties of Drilled Shaft (Bored Pile):--------------------------------------------------------

Length of Section = 40.00000000 ftShaft Diameter = 24.00000000 inConcrete Cover Thickness = 3.00000000 inNumber of Reinforcing Bars = 5 barsYield Stress of Reinforcing Bars = 60.00000000 ksiModulus of Elasticity of Reinforcing Bars = 29000. ksiGross Area of Shaft = 452.38934212 sq. in.Total Area of Reinforcing Steel = 5.00000000 sq. in.Area Ratio of Steel Reinforcement = 1.11 percentEdge-to-Edge Bar Spacing = 8.78911278 inMaximum Concrete Aggregate Size = 0.75000000 inRatio of Bar Spacing to Aggregate Size = 11.72Offset of Rebar Cage Center from Center of Pile = 0.0000000 in

Axial Structural Capacities:----------------------------

Nom. Axial Structural Capacity = 0.85 Fc Ac + Fy As = 1440.843 kipsTensile Load for Cracking of Concrete = -178.779 kipsNominal Axial Tensile Capacity = -300.000 kips

Reinforcing Bar Dimensions and Positions Used in Computations:

Bar Bar Diam. Bar Area X Y Number inches sq. in. inches inches ---------- ---------- ---------- ---------- ---------- 1 1.12800 1.00000 8.43600 0.00000 2 1.12800 1.00000 2.60687 8.02311 3 1.12800 1.00000 -6.82487 4.95856 4 1.12800 1.00000 -6.82487 -4.95856 5 1.12800 1.00000 2.60687 -8.02311

NOTE: The positions of the above rebars were computed by LPile

Minimum spacing between any two bars not equal to zero = 8.78911 inches betweenBars 1 and 2

Spacing to aggregate size ratio = 11.71882

Concrete Properties:--------------------

Compressive Strength of Concrete = 3.00000000 ksiModulus of Elasticity of Concrete = 3122.01857778 ksiModulus of Rupture of Concrete = -0.41079191 ksiCompression Strain at Peak Stress = 0.00163356Tensile Strain at Fracture of Concrete = -0.00011596Maximum Coarse Aggregate Size = 0.75000000 in

Number of Axial Thrust Force Values Determined from Pile-head Loadings = 1

Number Axial Thrust Force kips

Page 6

24new.lp6o ------ ------------------ 1 250.000

Definitions of Run Messages and Notes:--------------------------------------

C = concrete in section has cracked in tension. Y = stress in reinforcing steel has reached yield stress. T = ACI 318-08 criteria for tension-controlled section met, tensile strain in reinforcement exceeds 0.005 while simultaneously compressive strain in concrete more than than 0.003. See ACI 318-08, Section 10.3.4. Z = depth of tensile zone in concrete section is less than 10 percent of section depth.

Bending Stiffness (EI) = Computed Bending Moment / Curvature.Position of neutral axis is measured from edge of compression side of pile.Compressive stresses and strains are positive in sign.Tensile stresses and strains are negative in sign.

Axial Thrust Force = 250.000 kips

Bending Bending Bending Depth to Max Comp Max Tens Max Concrete Max Steel Run Curvature Moment Stiffness N Axis Strain Strain Stress Stress Msg rad/in. in-kip kip-in2 in in/in in/in ksi ksi ------------- ------------- ------------- ------------- ------------- -------------------------- ------------- --- 0.000001250 73.8222443 59057795. 128.6371374 0.0001608 0.0001308 0.5610353 4.6587462 0.000002500 147.6432366 59057295. 70.3392622 0.0001758 0.0001158 0.6101366 5.0908965 0.000003750 221.4548595 59054629. 50.9158320 0.0001909 0.0001009 0.6588505 5.5240467 0.000005000 295.2524284 59050486. 41.2110142 0.0002061 0.0000861 0.7071735 5.9581971 0.000006250 369.0312572 59045001. 35.3936425 0.0002212 0.0000712 0.7551022 6.3933477 0.000007500 442.7866580 59038221. 31.5199952 0.0002364 0.0000564 0.8026331 6.8294990 0.000008750 516.5139403 59030165. 28.7570490 0.0002516 0.0000416 0.8497627 7.2666512 0.0000100 590.2084106 59020841. 26.6882923 0.0002669 0.0000269 0.8964876 7.7048048 0.0000113 663.8653719 59010255. 25.0823301 0.0002822 0.0000122 0.9428044 8.1439602 0.0000125 737.4801036 58998408. 23.8003255 0.0002975 -0.000002496 0.9887095 8.5841180 0.0000138 811.0324659 58984179. 22.7538672 0.0003129 -0.0000171 1.0341970 9.0252546 0.0000150 884.4512395 58963416. 21.8838189 0.0003283 -0.0000317 1.0792523 9.4672612 0.0000163 957.6596929 58932904. 21.1491981 0.0003437 -0.0000463 1.1238597 9.9100097 0.0000175 1030.5971523 58891266. 20.5207680 0.0003591 -0.0000609 1.1680055 10.3533898 0.0000188 1103.2183551 58838312. 19.9771279 0.0003746 -0.0000754 1.2116788 10.7973134 0.0000200 1175.4906758 58774534. 19.5022629 0.0003900 -0.0000900 1.2548712 11.2417125

Page 7

24new.lp6o 0.0000213 1247.3897108 58700692. 19.0839484 0.0004055 -0.0001045 1.2975759 11.6865333 0.0000225 1247.3897108 55439543. 18.2901435 0.0004115 -0.0001285 1.3137080 11.8560186 C 0.0000238 1247.3897108 52521672. 17.8818585 0.0004247 -0.0001453 1.3493599 12.2334801 C 0.0000250 1254.1902342 50167609. 17.5059928 0.0004376 -0.0001624 1.3840642 12.6048446 C 0.0000263 1289.9977873 49142773. 17.1600519 0.0004505 -0.0001795 1.4179888 12.9717395 C 0.0000275 1324.0044233 48145615. 16.8390677 0.0004631 -0.0001969 1.4510822 13.3334564 C 0.0000288 1356.6594849 47188156. 16.5412691 0.0004756 -0.0002144 1.4834711 13.6912332 C 0.0000300 1388.0401257 46268004. 16.2638230 0.0004879 -0.0002321 1.5151717 14.0451261 C 0.0000313 1418.2197666 45383033. 16.0043530 0.0005001 -0.0002499 1.5462004 14.3951949 C 0.0000325 1447.2935912 44532110. 15.7609593 0.0005122 -0.0002678 1.5765821 14.7416042 C 0.0000338 1475.3615764 43714417. 15.5320732 0.0005242 -0.0002858 1.6063455 15.0845667 C 0.0000350 1502.5218065 42929194. 15.3163759 0.0005361 -0.0003039 1.6355205 15.4243216 C 0.0000363 1528.8701179 42175727. 15.1127569 0.0005478 -0.0003222 1.6641383 15.7611358 C 0.0000375 1554.4997572 41453327. 14.9202813 0.0005595 -0.0003405 1.6922317 16.0953060 C 0.0000388 1579.5010497 40761317. 14.7381630 0.0005711 -0.0003589 1.7198350 16.4271608 C 0.0000400 1603.7597545 40093994. 14.5648299 0.0005826 -0.0003774 1.7468973 16.7560028 C 0.0000413 1627.4207447 39452624. 14.3999694 0.0005940 -0.0003960 1.7734736 17.0824134 C 0.0000425 1650.6624604 38839117. 14.2435500 0.0006054 -0.0004146 1.7996410 17.4072755 C 0.0000438 1673.3113705 38247117. 14.0940379 0.0006166 -0.0004334 1.8253220 17.7295606 C 0.0000450 1695.4919357 37677599. 13.9512860 0.0006278 -0.0004522 1.8505672 18.0498284 C 0.0000463 1717.3705581 37132336. 13.8154598 0.0006390 -0.0004710 1.8754559 18.3690356 C 0.0000475 1738.6415567 36602980. 13.6845835 0.0006500 -0.0004900 1.8998398 18.6852138 C 0.0000488 1759.7899894 36098256. 13.5603793 0.0006611 -0.0005089 1.9239523 19.0013364 C 0.0000513 1800.7546042 35136675. 13.3257398 0.0006829 -0.0005471 1.9708899 19.6270305 C 0.0000538 1840.4420933 34240783. 13.1091022 0.0007046 -0.0005854 2.0163484 20.2467628 C 0.0000563 1879.0219160 33404834. 12.9085115 0.0007261 -0.0006239 2.0604091 20.8612593 C 0.0000588 1916.6547602 32623911. 12.7223986 0.0007474 -0.0006626 2.1031542 21.4713366 C 0.0000613 1953.4933799 31893769. 12.5495136 0.0007687 -0.0007013 2.1446682 22.0779237 C 0.0000638 1989.5286670 31208293. 12.3881314 0.0007897 -0.0007403 2.1849474 22.6807081 C 0.0000663 2024.7393666 30562104. 12.2366392 0.0008107 -0.0007793 2.2239719 23.2790929 C 0.0000688 2059.5080847 29956481. 12.0956077 0.0008316 -0.0008184 2.2619694 23.8763681 C 0.0000713 2093.5133533 29382644. 11.9623763 0.0008523 -0.0008577

Page 8

24new.lp6o 2.2987478 -24.6247897 C 0.0000738 2127.1285612 28842421. 11.8377413 0.0008730 -0.0008970 2.3345305 -25.7553807 C 0.0000763 2160.1485286 28329817. 11.7198735 0.0008936 -0.0009364 2.3691958 -26.8890796 C 0.0000788 2192.8384038 27845567. 11.6092699 0.0009142 -0.0009758 2.4029056 -28.0232796 C 0.0000813 2224.9377739 27383850. 11.5039929 0.0009347 -0.0010153 2.4354982 -29.1609665 C 0.0000838 2256.8762439 26947776. 11.4055666 0.0009552 -0.0010548 2.4672495 -30.2972798 C 0.0000863 2288.1393784 26529152. 11.3108422 0.0009756 -0.0010944 2.4978220 -31.4386062 C 0.0000888 2319.2126137 26131973. 11.2218307 0.0009959 -0.0011341 2.5275399 -32.5789629 C 0.0000913 2349.9970729 25753393. 11.1375485 0.0010163 -0.0011737 2.5563324 -33.7197121 C 0.0000938 2380.2693222 25389539. 11.0564752 0.0010365 -0.0012135 2.5840549 -34.8639577 C 0.0000963 2410.3848747 25042960. 10.9801058 0.0010568 -0.0012532 2.6109457 -36.0068293 C 0.0000988 2440.2708666 24711604. 10.9077074 0.0010771 -0.0012929 2.6369512 -37.1494027 C 0.0001013 2469.6523953 24391629. 10.8375406 0.0010973 -0.0013327 2.6618895 -38.2959211 C 0.0001038 2498.8784068 24085575. 10.7712168 0.0011175 -0.0013725 2.6859974 -39.4410512 C 0.0001063 2527.9470745 23792443. 10.7084688 0.0011378 -0.0014122 2.7092690 -40.5847802 C 0.0001088 2556.6701450 23509611. 10.6480236 0.0011580 -0.0014520 2.7315751 -41.7303453 C 0.0001113 2585.0703336 23236587. 10.5898314 0.0011781 -0.0014919 2.7529368 -42.8774061 C 0.0001138 2613.3142483 22974191. 10.5346288 0.0011983 -0.0015317 2.7734623 -44.0230430 C 0.0001163 2641.4000589 22721721. 10.4822271 0.0012186 -0.0015714 2.7931457 -45.1672415 C 0.0001188 2669.2809115 22478155. 10.4321910 0.0012388 -0.0016112 2.8119521 -46.3108920 C 0.0001213 2696.7582656 22241305. 10.3832304 0.0012590 -0.0016510 2.8297576 -47.4580156 C 0.0001238 2724.0783321 22012754. 10.3366582 0.0012792 -0.0016908 2.8467198 -48.6036675 C 0.0001263 2751.2392381 21791994. 10.2923367 0.0012994 -0.0017306 2.8628324 -49.7478317 C 0.0001288 2778.2390763 21578556. 10.2501393 0.0013197 -0.0017703 2.8780888 -50.8904919 C 0.0001313 2805.0759043 21372007. 10.2099490 0.0013401 -0.0018099 2.8924826 -52.0316311 C 0.0001338 2831.5808022 21170698. 10.1706140 0.0013603 -0.0018497 2.9059161 -53.1752808 C 0.0001363 2857.8670011 20975171. 10.1327643 0.0013806 -0.0018894 2.9184569 -54.3187645 C 0.0001388 2883.9904825 20785517. 10.0966691 0.0014009 -0.0019291 2.9301315 -55.4606773 C 0.0001413 2909.9492446 20601411. 10.0622398 0.0014213 -0.0019687 2.9409328 -56.6009999 C 0.0001438 2935.7412310 20422548. 10.0293942 0.0014417 -0.0020083 2.9508538 -57.7397127 C 0.0001463 2961.3643425 20248645. 9.9980557 0.0014622 -0.0020478 2.9598872 -58.8767957 C 0.0001488 2986.8164360 20079438. 9.9681533 0.0014828 -0.0020872 2.9680256 -60.0000000 CY

Page 9

24new.lp6o 0.0001588 3086.3134890 19441345. 9.8577105 0.0015649 -0.0022451 2.9913539 -60.0000000 CY 0.0001688 3182.9437928 18861889. 9.7658819 0.0016480 -0.0024020 2.9999620 -60.0000000 CY 0.0001788 3276.3245800 18329089. 9.6890250 0.0017319 -0.0025581 2.9999110 -60.0000000 CY 0.0001888 3366.3265745 17834843. 9.6246728 0.0018167 -0.0027133 2.9995159 -60.0000000 CY 0.0001988 3443.1632611 17324092. 9.5630393 0.0019007 -0.0028693 2.9990143 -60.0000000 CY 0.0002088 3494.5201384 16740216. 9.4908605 0.0019812 -0.0030288 2.9991128 -60.0000000 CY 0.0002188 3537.0952415 16169578. 9.4200018 0.0020606 -0.0031894 2.9995863 -60.0000000 CY 0.0002288 3578.1681706 15642265. 9.3583089 0.0021407 -0.0033493 2.9997670 60.0000000 CY 0.0002388 3617.9351397 15153655. 9.3049653 0.0022216 -0.0035084 2.9997906 60.0000000 CY 0.0002488 3656.5094366 14699535. 9.2588196 0.0023031 -0.0036669 2.9996760 60.0000000 CY 0.0002588 3691.8163231 14267889. 9.2151766 0.0023844 -0.0038256 2.9992757 60.0000000 CY 0.0002688 3718.0467643 13834593. 9.1664086 0.0024635 -0.0039865 2.9981253 60.0000000 CY 0.0002788 3734.9699282 13398995. 9.1124132 0.0025401 -0.0041499 2.9992986 60.0000000 CY 0.0002888 3746.9001414 12976278. 9.0582911 0.0026156 -0.0043144 2.9994142 60.0000000 CY 0.0002988 3757.8596149 12578610. 9.0083317 0.0026912 -0.0044788 2.9967618 60.0000000 CY 0.0003088 3768.1367140 12204491. 8.9600965 0.0027664 -0.0046436 2.9997236 60.0000000 CY 0.0003188 3778.0446140 11852689. 8.9154700 0.0028418 -0.0048082 2.9967215 60.0000000 CY 0.0003288 3787.7078569 11521545. 8.8745371 0.0029175 -0.0049725 2.9996396 60.0000000 CY 0.0003388 3797.1226807 11209218. 8.8369973 0.0029935 -0.0051365 2.9961522 60.0000000 CY 0.0003488 3806.3157890 10914167. 8.8024865 0.0030699 -0.0053001 2.9990906 60.0000000 CYT 0.0003588 3815.3238476 10635049. 8.7706568 0.0031465 -0.0054635 2.9987195 60.0000000 CYT 0.0003688 3823.9388308 10370004. 8.7398769 0.0032228 -0.0056272 2.9974121 60.0000000 CYT 0.0003788 3832.3373474 10118382. 8.7104719 0.0032991 -0.0057909 2.9997080 60.0000000 CYT 0.0003888 3840.5636913 9879264. 8.6833079 0.0033756 -0.0059544 2.9966709 60.0000000 CYT 0.0003988 3848.6370712 9651754. 8.6581583 0.0034524 -0.0061176 2.9974882 60.0000000 CYT 0.0004088 3856.0910652 9433862. 8.6359961 0.0035300 -0.0062800 2.9996923 60.0000000 CYT 0.0004188 3863.3329564 9225870. 8.6156793 0.0036078 -0.0064422 2.9969866 60.0000000 CYT 0.0004288 3869.7886533 9025746. 8.5985272 0.0036866 -0.0066034 2.9964252 60.0000000 CYT 0.0004388 3875.5848854 8833242. 8.5839973 0.0037662 -0.0067638 2.9992412 60.0000000 CYT 0.0004488 3881.2519657 8649029. 8.5706662 0.0038461 -0.0069239 2.9990283 60.0000000 CYT

--------------------------------------------------------------------------------Page 10

24new.lp6o Summary of Results for Nominal (Unfactored) Moment Capacity for Section 1--------------------------------------------------------------------------------

Moment values interpolated at maximum compressive strain = 0.003or maximum developed moment if pile fails at smaller strains.

Load Axial Thrust Nominal Mom. Cap. Max. Comp. No. kips in-kip Strain ---- ---------------- ------------------ ------------ 1 250.000 3797.902 0.00300000

Note note that the values of moment capacity in the table above are not factored by a strength reduction factor (phi-factor).

In ACI 318-08, the value of the strength reduction factor depends on whether the transverse reinforcing steel bars are tied hoops (0.65) or spirals (0.70).

The above values should be multiplied by the appropriate strength reduction factor to compute ultimate moment capacity according to ACI 318-08, Section 9.3.2.2 or the value required by the design standard being followed.

The following table presents factored moment capacities and corresponding bending stiffnesses computed for common resistance factor values used for reinforced concrete sections.

Axial Resistance Nominal Ultimate (Factored) Ultimate (Factored) Bending Stiffness Load Factor Moment Capacity Axial Thrust Moment Capacity at Ult. Mom. Cap. No. for Moment in-kip kipsin-kip kip-in^2 ----- ---------- ------------------- -------------------------------------- ------------------- 1 0.65 3797.902 162.5002468.636 24402698.479

1 0.70 3797.902 175.0002658.531 22572065.516

1 0.75 3797.902 187.5002848.426 21045395.330

-------------------------------------------------------------------------------- Computed Values of Pile Loading and Deflection for Lateral Loading for Load Case Number 1--------------------------------------------------------------------------------

Pile-head conditions are Displacement and Moment (Loading Type 4)Displacement of pile head = 0.250000 inchesMoment at pile head = 0.000 in-lbsAxial load at pile head = 250000.000 lbs

Depth Deflect. Bending Shear Slope Total Bending Soil Res. Soil Spr. Distrib. X y Moment Force S Stress Stiffness p Es*h Lat. Load feet inches in-lbs lbs radians psi* lb-in^2 lb/in lb/inch lb/inch ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ----------

Page 11

24new.lp6o 0.00 0.2500 0.000 9780.5455 -0.001987 0.000 5.906E+100.000 0.000 0.000 0.400 0.2405 49331. 9742.2854 -0.001985 0.000 5.906E+10-15.9417 318.2196 0.000 0.800 0.2309 98289. 9630.5336 -0.001979 0.000 5.906E+10-30.6215 636.4393 0.000 1.200 0.2215 146533. 9451.3289 -0.001969 0.000 5.906E+10-44.0471 954.6589 0.000 1.600 0.2120 193747. 9210.6615 -0.001955 0.000 5.906E+10-56.2310 1272.8785 0.000 2.000 0.2027 239647. 8914.4493 -0.001937 0.000 5.905E+10-67.1907 1591.0981 0.000 2.400 0.1934 283976. 8568.5153 -0.001916 0.000 5.905E+10-76.9484 1909.3178 0.000 2.800 0.1843 326503. 8178.5652 -0.001891 0.000 5.905E+10-85.5308 2227.5374 0.000 3.200 0.1753 367029. 7750.1669 -0.001863 0.000 5.905E+10-92.9685 2545.7570 0.000 3.600 0.1664 405376. 7288.7307 -0.001832 0.000 5.904E+10-99.2965 2863.9766 0.000 4.000 0.1577 441397. 6799.4914 -0.001797 0.000 5.904E+10-104.5532 3182.1963 0.000 4.400 0.1492 474965. 6287.4913 -0.001760 0.000 5.903E+10-108.7802 3500.4159 0.000 4.800 0.1408 505981. 5757.5656 -0.001720 0.000 5.903E+10-112.0222 3818.6355 0.000 5.200 0.1327 534366. 5214.3285 -0.001678 0.000 5.903E+10-114.3266 4136.8551 0.000 5.600 0.1247 560065. 4662.1616 -0.001633 0.000 5.902E+10-115.7429 4455.0748 0.000 6.000 0.1170 583043. 4105.2042 -0.001587 0.000 5.902E+10-116.3227 4773.2944 0.000 6.400 0.1095 603283. 3547.3447 -0.001539 0.000 5.902E+10-116.1188 5091.5140 0.000 6.800 0.1022 620790. 2992.2143 -0.001489 0.000 5.902E+10-115.1855 5409.7336 0.000 7.200 0.0952 635582. 2443.1823 -0.001438 0.000 5.901E+10-113.5778 5727.9533 0.000 7.600 0.0884 647695. 1903.3525 -0.001386 0.000 5.901E+10-111.3512 6046.1729 0.000 8.000 0.0819 657179. 1375.5623 -0.001332 0.000 5.901E+10-108.5614 6364.3925 0.000 8.400 0.0756 664098. 862.3822 -0.001279 0.000 5.901E+10-105.2637 6682.6121 0.000 8.800 0.0696 668527. 366.1179 -0.001225 0.000 5.901E+10-101.5131 7000.8318 0.000 9.200 0.0639 670552. -111.1870 -0.001170 0.000 5.901E+10-97.3639 7319.0514 0.000 9.600 0.0584 670268. -567.7467 -0.001116 0.000 5.901E+10-92.8693 7637.2710 0.000 10.000 0.0531 667779. -1002.0275 -0.001061 0.000 5.901E+10-88.0811 7955.4906 0.000 10.400 0.0482 663195. -1412.7412 -0.001007 0.000 5.901E+10-83.0496 8273.7103 0.000 10.800 0.0435 656633. -1798.8371 -0.000953 0.000 5.901E+10-77.8237 8591.9299 0.000 11.200 0.0390 648214. -2159.4935 -0.000900 0.000 5.901E+10-72.4499 8910.1495 0.000 11.600 0.0348 638063. -2494.1081 -0.000848 0.000 5.901E+10-66.9729 9228.3691 0.000 12.000 0.0309 626306. -2802.2876 -0.000797 0.000 5.902E+10-61.4352 9546.5888 0.000 12.400 0.0272 613072. -3083.8368 -0.000746 0.000 5.902E+10

Page 12

24new.lp6o-55.8769 9864.8084 0.000 12.800 0.0237 598492. -3338.7470 -0.000697 0.000 5.902E+10-50.3357 10183. 0.000 13.200 0.0205 582693. -3567.1843 -0.000649 0.000 5.902E+10-44.8466 10501. 0.000 13.600 0.0175 565804. -3769.4771 -0.000602 0.000 5.902E+10-39.4422 10819. 0.000 14.000 0.0147 547951. -3946.1040 -0.000557 0.000 5.903E+10-34.1524 11138. 0.000 14.400 0.0122 529257. -4097.6806 -0.000513 0.000 5.903E+10-29.0045 11456. 0.000 14.800 0.009794 509844. -4224.9472 -0.000471 0.000 5.903E+10-24.0232 11774. 0.000 15.200 0.007633 489828. -4328.7558 -0.000430 0.000 5.903E+10-19.2304 12092. 0.000 15.600 0.005664 469321. -4410.0577 -0.000391 0.000 5.904E+10-14.6454 12411. 0.000 16.000 0.003878 448430. -4469.8909 -0.000354 0.000 5.904E+10-10.2851 12729. 0.000 16.400 0.002268 427259. -4509.3679 -0.000318 0.000 5.904E+10-6.1637 13047. 0.000 16.800 0.000823 405904. -4529.6637 -0.000284 0.000 5.904E+10-2.2929 13365. 0.000 17.200 -0.000462 384456. -4532.0041 -0.000252 0.000 5.904E+101.3178 13683. 0.000 17.600 -0.001598 363002. -4517.6544 -0.000222 0.000 5.905E+104.6613 14002. 0.000 18.000 -0.002592 341619. -4487.9084 -0.000193 0.000 5.905E+107.7328 14320. 0.000 18.400 -0.003453 320382. -4444.0783 -0.000166 0.000 5.905E+1010.5297 14638. 0.000 18.800 -0.004189 299355. -4387.4843 -0.000141 0.000 5.905E+1013.0511 14956. 0.000 19.200 -0.004808 278601. -4319.4452 -0.000118 0.000 5.905E+1015.2985 15275. 0.000 19.600 -0.005318 258171. -4241.2695 -9.581E-05 0.000 5.905E+1017.2748 15593. 0.000 20.000 -0.005727 238114. -4154.2466 -7.564E-05 0.000 5.905E+1018.9848 15911. 0.000 20.400 -0.006044 218472. -4059.6390 -5.708E-05 0.000 5.905E+1020.4350 16229. 0.000 20.800 -0.006275 199279. -3958.6748 -4.011E-05 0.000 5.906E+1021.6334 16547. 0.000 21.200 -0.006429 180565. -3852.5403 -2.467E-05 0.000 5.906E+1022.5893 16866. 0.000 21.600 -0.006512 162354. -3742.3741 -1.073E-05 0.000 5.906E+1023.3133 17184. 0.000 22.000 -0.006532 144664. -3629.2602 1.742E-06 0.000 5.906E+1023.8175 17502. 0.000 22.400 -0.006495 127509. -3514.2230 1.280E-05 0.000 5.906E+1024.1147 17820. 0.000 22.800 -0.006409 110896. -3398.2219 2.249E-05 0.000 5.906E+1024.2191 18139. 0.000 23.200 -0.006280 94832. -3223.7078 3.085E-05 0.000 5.906E+1048.4951 37069. 0.000 23.600 -0.006113 79875. -2991.8218 3.795E-05 0.000 5.906E+1048.1240 37788. 0.000 24.000 -0.005915 66019. -2762.4366 4.388E-05 0.000 5.906E+1047.4531 38507. 0.000 24.400 -0.005692 53250. -2536.9191 4.873E-05 0.000 5.906E+1046.5125 39226. 0.000 24.800 -0.005447 41548. -2316.4923 5.258E-05 0.000 5.906E+1045.3320 39944. 0.000

Page 13

24new.lp6o 25.200 -0.005187 30886. -2102.2367 5.552E-05 0.000 5.906E+1043.9411 40663. 0.000 25.600 -0.004914 21233. -1895.0942 5.764E-05 0.000 5.906E+1042.3683 41382. 0.000 26.000 -0.004634 12554. -1695.8715 5.901E-05 0.000 5.906E+1040.6412 42101. 0.000 26.400 -0.004348 4810.9428 -1505.2457 5.972E-05 0.000 5.906E+1038.7863 42820. 0.000 26.800 -0.004060 -2039.3174 -1323.7698 5.983E-05 0.000 5.906E+1036.8287 43539. 0.000 27.200 -0.003773 -8040.8446 -1151.8790 5.942E-05 0.000 5.906E+1034.7924 44257. 0.000 27.600 -0.003490 -13240. -989.8981 5.856E-05 0.000 5.906E+1032.6996 44976. 0.000 28.000 -0.003211 -17684. -838.0487 5.730E-05 0.000 5.906E+1030.5710 45695. 0.000 28.400 -0.002940 -21423. -696.4566 5.571E-05 0.000 5.906E+1028.4257 46414. 0.000 28.800 -0.002676 -24504. -565.1604 5.385E-05 0.000 5.906E+1026.2811 47133. 0.000 29.200 -0.002423 -26978. -444.1187 5.175E-05 0.000 5.906E+1024.1530 47852. 0.000 29.600 -0.002180 -28892. -333.2187 4.948E-05 0.000 5.906E+1022.0553 48570. 0.000 30.000 -0.001948 -30295. -227.0248 4.708E-05 0.000 5.906E+1022.1921 54690. 0.000 30.400 -0.001728 -31184. -121.1882 4.458E-05 0.000 5.906E+1021.9064 60862. 0.000 30.800 -0.001520 -31566. -21.7057 4.203E-05 0.000 5.906E+1019.5446 61729. 0.000 31.200 -0.001324 -31494. 66.6457 3.947E-05 0.000 5.906E+1017.2684 62595. 0.000 31.600 -0.001141 -31021. 144.2917 3.693E-05 0.000 5.906E+1015.0841 63461. 0.000 32.000 -0.000970 -30197. 211.6830 3.444E-05 0.000 5.906E+1012.9957 64328. 0.000 32.400 -0.000810 -29071. 269.2859 3.203E-05 0.000 5.906E+1011.0055 65194. 0.000 32.800 -0.000662 -27689. 317.5725 2.972E-05 0.000 5.906E+109.1139 66061. 0.000 33.200 -0.000525 -26094. 357.0125 2.754E-05 0.000 5.906E+107.3194 66927. 0.000 33.600 -0.000398 -24327. 388.0652 2.549E-05 0.000 5.906E+105.6192 67793. 0.000 34.000 -0.000280 -22429. 411.1725 2.359E-05 0.000 5.906E+104.0088 68660. 0.000 34.400 -0.000171 -20437. 426.7523 2.185E-05 0.000 5.906E+102.4828 69526. 0.000 34.800 -7.053E-05 -18385. 435.1933 2.027E-05 0.000 5.906E+101.0343 70393. 0.000 35.200 2.318E-05 -16308. 436.8499 1.886E-05 0.000 5.906E+10-0.3441 71259. 0.000 35.600 0.000111 -14237. 432.0385 1.762E-05 0.000 5.906E+10-1.6607 72125. 0.000 36.000 0.000192 -12202. 421.0343 1.654E-05 0.000 5.906E+10-2.9244 72992. 0.000 36.400 0.000269 -10234. 404.0695 1.563E-05 0.000 5.906E+10-4.1443 73858. 0.000 36.800 0.000342 -8360.7466 381.3312 1.488E-05 0.000 5.906E+10-5.3299 74725. 0.000 37.200 0.000412 -6609.2012 352.9620 1.427E-05 0.000 5.906E+10-6.4906 75591. 0.000 37.600 0.000479 -5006.5535 319.0600 1.380E-05 0.000 5.906E+10

Page 14

24new.lp6o-7.6353 76457. 0.000 38.000 0.000545 -3579.3344 279.6806 1.345E-05 0.000 5.906E+10-8.7728 77324. 0.000 38.400 0.000608 -2353.8916 234.8392 1.321E-05 0.000 5.906E+10-9.9111 78190. 0.000 38.800 0.000671 -1356.5718 184.5147 1.305E-05 0.000 5.906E+10-11.0574 79057. 0.000 39.200 0.000734 -613.8818 128.6549 1.297E-05 0.000 5.906E+10-12.2175 79923. 0.000 39.600 0.000796 -152.6242 67.1819 1.294E-05 0.000 5.906E+10-13.3962 80789. 0.000 40.000 0.000858 0.000 0.000 1.294E-05 0.000 5.906E+10-14.5963 40828. 0.000

* This analysis makes computations of pile response using nonlinear moment-curvaturerelationships. The above values of total stress are computed for combined axial and bending stress in elastic sections and do not equal actual stresses in concrete and steel in the range of nonlinear bending.

Output Summary for Load Case No. 1:

Pile-head deflection = 0.2500000 inchesComputed slope at pile head = -0.0019867 radiansMaximum bending moment = 670552. inch-lbsMaximum shear force = 9780.5455231 lbsDepth of maximum bending moment = 110.4000000 inches below pile headDepth of maximum shear force = 0.000000 inches below pile headNumber of iterations = 6Number of zero deflection points = 2

-------------------------------------------------------------------------------- Computed Values of Pile Loading and Deflection for Lateral Loading for Load Case Number 2--------------------------------------------------------------------------------

Pile-head conditions are Displacement and Moment (Loading Type 4)Displacement of pile head = 0.500000 inchesMoment at pile head = 0.000 in-lbsAxial load at pile head = 250000.000 lbs

Depth Deflect. Bending Shear Slope Total Bending Soil Res. Soil Spr. Distrib. X y Moment Force S Stress Stiffness p Es*h Lat. Load feet inches in-lbs lbs radians psi* lb-in^2 lb/in lb/inch lb/inch ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- 0.00 0.5000 0.000 19050. -0.004015 0.000 5.906E+100.000 0.000 0.000 0.400 0.4807 96259. 18974. -0.004011 0.000 5.906E+10-31.8704 318.2196 0.000 0.800 0.4615 191775. 18751. -0.003999 0.000 5.906E+10-61.1908 636.4393 0.000 1.200 0.4423 285862. 18393. -0.003979 0.000 5.905E+10-87.9760 954.6589 0.000 1.600 0.4233 377895. 17912. -0.003952 0.000 5.904E+10-112.2507 1272.8785 0.000

Page 15

24new.lp6o 2.000 0.4044 467304. 17321. -0.003918 0.000 5.904E+10-134.0490 1591.0981 0.000 2.400 0.3857 553579. 16631. -0.003877 0.000 5.903E+10-153.4142 1909.3178 0.000 2.800 0.3672 636266. 15854. -0.003828 0.000 5.901E+10-170.3980 2227.5374 0.000 3.200 0.3489 714964. 15001. -0.003773 0.000 5.900E+10-185.0606 2545.7570 0.000 3.600 0.3310 789329. 14083. -0.003712 0.000 5.899E+10-197.4699 2863.9766 0.000 4.000 0.3133 859067. 13110. -0.003645 0.000 5.897E+10-207.7006 3182.1963 0.000 4.400 0.2960 923936. 12094. -0.003572 0.000 5.895E+10-215.8339 3500.4159 0.000 4.800 0.2790 983742. 11043. -0.003495 0.000 5.892E+10-221.9570 3818.6355 0.000 5.200 0.2624 1038337. 9967.6191 -0.003412 0.000 5.889E+10-226.1620 4136.8551 0.000 5.600 0.2462 1087620. 8876.3216 -0.003326 0.000 5.885E+10-228.5453 4455.0748 0.000 6.000 0.2305 1131531. 7777.7153 -0.003235 0.000 5.881E+10-229.2073 4773.2944 0.000 6.400 0.2152 1170051. 6679.8151 -0.003141 0.000 5.878E+10-228.2511 5091.5140 0.000 6.800 0.2003 1203197. 5590.1352 -0.003044 0.000 5.874E+10-225.7822 5409.7336 0.000 7.200 0.1860 1231022. 4515.6795 -0.002945 0.000 5.872E+10-221.9077 5727.9533 0.000 7.600 0.1721 1253615. 3462.9362 -0.002836 0.000 5.144E+10-216.7354 6046.1729 0.000 8.000 0.1587 1271073. 2437.6543 -0.002716 0.000 4.967E+10-210.4654 6364.3925 0.000 8.400 0.1460 1283535. 1444.7408 -0.002592 0.000 4.932E+10-203.2486 6682.6121 0.000 8.800 0.1338 1291164. 488.4241 -0.002467 0.000 4.910E+10-195.2167 7000.8318 0.000 9.200 0.1223 1294143. -427.6928 -0.002340 0.000 4.901E+10-186.4986 7319.0514 0.000 9.600 0.1114 1292674. -1300.6147 -0.002214 0.000 4.906E+10-177.2188 7637.2710 0.000 10.000 0.1011 1286970. -2127.9305 -0.002088 0.000 4.922E+10-167.4961 7955.4906 0.000 10.400 0.0913 1277256. -2907.7849 -0.001963 0.000 4.949E+10-157.4432 8273.7103 0.000 10.800 0.0822 1263766. -3638.8469 -0.001840 0.000 4.988E+10-147.1660 8591.9299 0.000 11.200 0.0737 1246740. -4320.2749 -0.001724 0.000 5.426E+10-136.7624 8910.1495 0.000 11.600 0.0657 1226430. -4951.4907 -0.001619 0.000 5.872E+10-126.2441 9228.3691 0.000 12.000 0.0581 1203091. -5531.9663 -0.001520 0.000 5.875E+10-115.6207 9546.5888 0.000 12.400 0.0511 1176970. -6061.3804 -0.001422 0.000 5.877E+10-104.9685 9864.8084 0.000 12.800 0.0445 1148315. -6539.7673 -0.001328 0.000 5.880E+10-94.3593 10183. 0.000 13.200 0.0383 1117374. -6967.4933 -0.001235 0.000 5.883E+10-83.8598 10501. 0.000 13.600 0.0326 1084391. -7345.2331 -0.001145 0.000 5.885E+10-73.5318 10819. 0.000 14.000 0.0273 1049608. -7673.9456 -0.001058 0.000 5.888E+10-63.4318 11138. 0.000 14.400 0.0225 1013261. -7954.8489 -0.000974 0.000 5.890E+10

Page 16

24new.lp6o-53.6113 11456. 0.000 14.800 0.0180 975580. -8189.3965 -0.000893 0.000 5.892E+10-44.1168 11774. 0.000 15.200 0.0139 936787. -8379.2521 -0.000815 0.000 5.894E+10-34.9897 12092. 0.000 15.600 0.0102 897096. -8526.2661 -0.000741 0.000 5.896E+10-26.2662 12411. 0.000 16.000 0.006779 856712. -8632.4515 -0.000669 0.000 5.897E+10-17.9778 12729. 0.000 16.400 0.003735 815830. -8699.9606 -0.000601 0.000 5.898E+10-10.1511 13047. 0.000 16.800 0.001008 774635. -8731.0623 -0.000536 0.000 5.899E+10-2.8080 13365. 0.000 17.200 -0.001415 733299. -8728.1197 -0.000475 0.000 5.900E+104.0341 13683. 0.000 17.600 -0.003552 691985. -8693.5687 -0.000417 0.000 5.901E+1010.3621 14002. 0.000 18.000 -0.005419 650842. -8629.8976 -0.000362 0.000 5.901E+1016.1675 14320. 0.000 18.400 -0.007032 610008. -8539.6266 -0.000311 0.000 5.902E+1021.4455 14638. 0.000 18.800 -0.008407 569609. -8425.2888 -0.000263 0.000 5.902E+1026.1953 14956. 0.000 19.200 -0.009559 529757. -8289.4128 -0.000219 0.000 5.903E+1030.4198 15275. 0.000 19.600 -0.0105 490555. -8134.5044 -0.000177 0.000 5.903E+1034.1254 15593. 0.000 20.000 -0.0113 452091. -7963.0313 -0.000139 0.000 5.904E+1037.3217 15911. 0.000 20.400 -0.0118 414443. -7777.4075 -0.000104 0.000 5.904E+1040.0215 16229. 0.000 20.800 -0.0123 377676. -7579.9789 -7.132E-05 0.000 5.904E+1042.2404 16547. 0.000 21.200 -0.0125 341846. -7373.0102 -4.207E-05 0.000 5.905E+1043.9966 16866. 0.000 21.600 -0.0127 306996. -7158.6725 -1.570E-05 0.000 5.905E+1045.3108 17184. 0.000 22.000 -0.0127 273161. -6939.0314 7.882E-06 0.000 5.905E+1046.2063 17502. 0.000 22.400 -0.0126 240363. -6716.0370 2.875E-05 0.000 5.905E+1046.7081 17820. 0.000 22.800 -0.0124 208618. -6491.5134 4.700E-05 0.000 5.905E+1046.8434 18139. 0.000 23.200 -0.0121 177931. -6154.2668 6.271E-05 0.000 5.906E+1093.6760 37069. 0.000 23.600 -0.0118 149386. -5706.6053 7.601E-05 0.000 5.906E+1092.8496 37788. 0.000 24.000 -0.0114 122966. -5264.2738 8.708E-05 0.000 5.906E+1091.4552 38507. 0.000 24.400 -0.0110 98640. -4829.8598 9.608E-05 0.000 5.906E+1089.5507 39226. 0.000 24.800 -0.0105 76368. -4405.6737 0.000103 0.000 5.906E+1087.1936 39944. 0.000 25.200 -0.009968 56098. -3993.7529 0.000109 0.000 5.906E+1084.4401 40663. 0.000 25.600 -0.009435 37768. -3595.8680 0.000112 0.000 5.906E+1081.3452 41382. 0.000 26.000 -0.008889 21308. -3213.5313 0.000115 0.000 5.906E+1077.9617 42101. 0.000 26.400 -0.008333 6642.2424 -2848.0066 0.000116 0.000 5.906E+1074.3402 42820. 0.000 26.800 -0.007776 -6311.2310 -2500.3205 0.000116 0.000 5.906E+1070.5290 43539. 0.000

Page 17

24new.lp6o 27.200 -0.007220 -17639. -2171.2749 0.000115 0.000 5.906E+1066.5734 44257. 0.000 27.600 -0.006672 -27431. -1861.4606 0.000113 0.000 5.906E+1062.5159 44976. 0.000 28.000 -0.006134 -35781. -1571.2718 0.000111 0.000 5.906E+1058.3961 45695. 0.000 28.400 -0.005610 -42781. -1300.9208 0.000107 0.000 5.906E+1054.2502 46414. 0.000 28.800 -0.005103 -48527. -1050.4534 0.000104 0.000 5.906E+1050.1113 47133. 0.000 29.200 -0.004615 -53114. -819.7642 9.954E-05 0.000 5.906E+1046.0092 47852. 0.000 29.600 -0.004148 -56636. -608.6124 9.508E-05 0.000 5.906E+1041.9707 48570. 0.000 30.000 -0.003702 -59185. -406.6393 9.037E-05 0.000 5.906E+1042.1848 54690. 0.000 30.400 -0.003280 -60756. -205.5751 8.550E-05 0.000 5.906E+1041.5920 60862. 0.000 30.800 -0.002882 -61364. -16.8130 8.053E-05 0.000 5.906E+1037.0589 61729. 0.000 31.200 -0.002507 -61111. 150.5944 7.556E-05 0.000 5.906E+1032.6942 62595. 0.000 31.600 -0.002156 -60099. 297.4829 7.063E-05 0.000 5.906E+1028.5094 63461. 0.000 32.000 -0.001829 -58425. 424.7347 6.581E-05 0.000 5.906E+1024.5122 64328. 0.000 32.400 -0.001525 -56180. 533.2595 6.116E-05 0.000 5.906E+1020.7065 65194. 0.000 32.800 -0.001242 -53452. 623.9768 5.670E-05 0.000 5.906E+1017.0924 66061. 0.000 33.200 -0.000980 -50326. 697.7996 5.248E-05 0.000 5.906E+1013.6671 66927. 0.000 33.600 -0.000738 -46879. 755.6198 4.853E-05 0.000 5.906E+1010.4246 67793. 0.000 34.000 -0.000514 -43188. 798.2941 4.487E-05 0.000 5.906E+107.3563 68660. 0.000 34.400 -0.000307 -39323. 826.6325 4.152E-05 0.000 5.906E+104.4513 69526. 0.000 34.800 -0.000116 -35352. 841.3873 3.849E-05 0.000 5.906E+101.6965 70393. 0.000 35.200 6.215E-05 -31339. 843.2446 3.578E-05 0.000 5.906E+10-0.9227 71259. 0.000 35.600 0.000228 -27343. 832.8166 3.339E-05 0.000 5.906E+10-3.4223 72125. 0.000 36.000 0.000383 -23424. 810.6359 3.133E-05 0.000 5.906E+10-5.8196 72992. 0.000 36.400 0.000529 -19636. 777.1515 2.958E-05 0.000 5.906E+10-8.1322 73858. 0.000 36.800 0.000667 -16034. 732.7267 2.813E-05 0.000 5.906E+10-10.3782 74725. 0.000 37.200 0.000799 -12669. 677.6380 2.696E-05 0.000 5.906E+10-12.5755 75591. 0.000 37.600 0.000925 -9593.3238 612.0768 2.606E-05 0.000 5.906E+10-14.7417 76457. 0.000 38.000 0.001049 -6855.9799 536.1526 2.539E-05 0.000 5.906E+10-16.8934 77324. 0.000 38.400 0.001169 -4507.1919 449.8978 2.493E-05 0.000 5.906E+10-19.0461 78190. 0.000 38.800 0.001288 -2596.7858 353.2754 2.464E-05 0.000 5.906E+10-21.2133 79057. 0.000 39.200 0.001406 -1174.8801 246.1880 2.448E-05 0.000 5.906E+10-23.4065 79923. 0.000 39.600 0.001523 -292.1451 128.4897 2.443E-05 0.000 5.906E+10

Page 18

24new.lp6o-25.6345 80789. 0.000 40.000 0.001640 0.000 0.000 2.441E-05 0.000 5.906E+10-27.9029 40828. 0.000

* This analysis makes computations of pile response using nonlinear moment-curvaturerelationships. The above values of total stress are computed for combined axial and bending stress in elastic sections and do not equal actual stresses in concrete and steel in the range of nonlinear bending.

Output Summary for Load Case No. 2:

Pile-head deflection = 0.5000000 inchesComputed slope at pile head = -0.0040145 radiansMaximum bending moment = 1294143. inch-lbsMaximum shear force = 19050. lbsDepth of maximum bending moment = 110.4000000 inches below pile headDepth of maximum shear force = 0.000000 inches below pile headNumber of iterations = 15Number of zero deflection points = 2

-------------------------------------------------------------------------------- Computed Values of Pile Loading and Deflection for Lateral Loading for Load Case Number 3--------------------------------------------------------------------------------

Pile-head conditions are Displacement and Moment (Loading Type 4)Displacement of pile head = 0.750000 inchesMoment at pile head = 0.000 in-lbsAxial load at pile head = 250000.000 lbs

Depth Deflect. Bending Shear Slope Total Bending Soil Res. Soil Spr. Distrib. X y Moment Force S Stress Stiffness p Es*h Lat. Load feet inches in-lbs lbs radians psi* lb-in^2 lb/in lb/inch lb/inch ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- 0.00 0.7500 0.000 25874. -0.006279 0.000 5.906E+100.000 0.000 0.000 0.400 0.7199 131730. 25759. -0.006274 0.000 5.906E+10-47.7237 318.2196 0.000 0.800 0.6898 262347. 25425. -0.006258 0.000 5.905E+10-91.4581 636.4393 0.000 1.200 0.6598 390831. 24891. -0.006231 0.000 5.904E+10-131.2236 954.6589 0.000 1.600 0.6300 516254. 24175. -0.006194 0.000 5.903E+10-167.0537 1272.8785 0.000 2.000 0.6003 637778. 23297. -0.006147 0.000 5.901E+10-198.9950 1591.0981 0.000 2.400 0.5709 754655. 22274. -0.006091 0.000 5.899E+10-227.1066 1909.3178 0.000 2.800 0.5419 866225. 21125. -0.006025 0.000 5.897E+10-251.4591 2227.5374 0.000 3.200 0.5131 971917. 19869. -0.005950 0.000 5.892E+10-272.1344 2545.7570 0.000 3.600 0.4847 1071244. 18521. -0.005866 0.000 5.886E+10-289.2246 2863.9766 0.000

Page 19

24new.lp6o 4.000 0.4568 1163803. 17101. -0.005775 0.000 5.878E+10-302.8313 3182.1963 0.000 4.400 0.4293 1249270. 15622. -0.005669 0.000 5.117E+10-313.0648 3500.4159 0.000 4.800 0.4024 1327384. 14103. -0.005544 0.000 4.804E+10-320.1004 3818.6355 0.000 5.200 0.3761 1397963. 12557. -0.005405 0.000 4.597E+10-324.1139 4136.8551 0.000 5.600 0.3505 1460900. 10998. -0.005253 0.000 4.413E+10-325.2913 4455.0748 0.000 6.000 0.3256 1516151. 9440.2055 -0.005088 0.000 4.253E+10-323.8337 4773.2944 0.000 6.400 0.3016 1563736. 7895.1127 -0.004911 0.000 4.119E+10-319.9550 5091.5140 0.000 6.800 0.2785 1603730. 6373.9125 -0.004724 0.000 4.010E+10-313.8785 5409.7336 0.000 7.200 0.2563 1636263. 4886.6022 -0.004528 0.000 3.922E+10-305.8342 5727.9533 0.000 7.600 0.2350 1661508. 3442.0670 -0.004324 0.000 3.855E+10-296.0555 6046.1729 0.000 8.000 0.2148 1679684. 2048.0727 -0.004115 0.000 3.808E+10-284.7755 6364.3925 0.000 8.400 0.1955 1691045. 711.2738 -0.003902 0.000 3.779E+10-272.2240 6682.6121 0.000 8.800 0.1773 1695876. -562.7635 -0.003686 0.000 3.767E+10-258.6248 7000.8318 0.000 9.200 0.1601 1694489. -1769.5248 -0.003470 0.000 3.771E+10-244.1924 7319.0514 0.000 9.600 0.1440 1687217. -2905.4991 -0.003255 0.000 3.789E+10-229.1302 7637.2710 0.000 10.000 0.1289 1674410. -3968.1200 -0.003043 0.000 3.822E+10-213.6285 7955.4906 0.000 10.400 0.1148 1656428. -4955.6992 -0.002836 0.000 3.869E+10-197.8628 8273.7103 0.000 10.800 0.1017 1633640. -5867.3522 -0.002633 0.000 3.929E+10-181.9927 8591.9299 0.000 11.200 0.0895 1606420. -6702.9228 -0.002437 0.000 4.002E+10-166.1617 8910.1495 0.000 11.600 0.0783 1575141. -7462.9025 -0.002248 0.000 4.088E+10-150.4965 9228.3691 0.000 12.000 0.0679 1540172. -8148.3516 -0.002067 0.000 4.185E+10-135.1073 9546.5888 0.000 12.400 0.0584 1501878. -8760.8219 -0.001895 0.000 4.295E+10-120.0887 9864.8084 0.000 12.800 0.0497 1460616. -9302.2822 -0.001732 0.000 4.414E+10-105.5198 10183. 0.000 13.200 0.0418 1416732. -9775.0489 -0.001577 0.000 4.543E+10-91.4663 10501. 0.000 13.600 0.0346 1370561. -10182. -0.001432 0.000 4.677E+10-77.9810 10819. 0.000 14.000 0.0281 1322425. -10525. -0.001296 0.000 4.819E+10-65.1059 11138. 0.000 14.400 0.0222 1272631. -10808. -0.001169 0.000 4.963E+10-52.8731 11456. 0.000 14.800 0.0168 1221470. -11034. -0.001057 0.000 5.873E+10-41.3065 11774. 0.000 15.200 0.0120 1169239. -11206. -0.000960 0.000 5.878E+10-30.2426 12092. 0.000 15.600 0.007628 1116195. -11326. -0.000866 0.000 5.883E+10-19.7226 12411. 0.000 16.000 0.003689 1062589. -11397. -0.000777 0.000 5.887E+10-9.7816 12729. 0.000 16.400 0.000165 1008652. -11421. -0.000693 0.000 5.890E+10

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24new.lp6o-0.4487 13047. 0.000 16.800 -0.002964 954607. -11403. -0.000613 0.000 5.893E+108.2528 13365. 0.000 17.200 -0.005720 900659. -11344. -0.000537 0.000 5.896E+1016.3053 13683. 0.000 17.600 -0.008124 846998. -11248. -0.000466 0.000 5.897E+1023.6965 14002. 0.000 18.000 -0.0102 793801. -11118. -0.000400 0.000 5.899E+1030.4193 14320. 0.000 18.400 -0.0120 741227. -10957. -0.000337 0.000 5.900E+1036.4713 14638. 0.000 18.800 -0.0134 689420. -10769. -0.000279 0.000 5.901E+1041.8551 14956. 0.000 19.200 -0.0146 638511. -10557. -0.000225 0.000 5.901E+1046.5777 15275. 0.000 19.600 -0.0156 588613. -10324. -0.000175 0.000 5.902E+1050.6501 15593. 0.000 20.000 -0.0163 539824. -10072. -0.000129 0.000 5.903E+1054.0875 15911. 0.000 20.400 -0.0168 492229. -9805.8905 -8.716E-05 0.000 5.903E+1056.9086 16229. 0.000 20.800 -0.0172 445897. -9527.3846 -4.902E-05 0.000 5.904E+1059.1356 16547. 0.000 21.200 -0.0173 400884. -9239.5539 -1.460E-05 0.000 5.904E+1060.7939 16866. 0.000 21.600 -0.0173 357232. -8945.0602 1.621E-05 0.000 5.905E+1061.9118 17184. 0.000 22.000 -0.0171 314972. -8646.4228 4.354E-05 0.000 5.905E+1062.5204 17502. 0.000 22.400 -0.0169 274122. -8346.0062 6.748E-05 0.000 5.905E+1062.6532 17820. 0.000 22.800 -0.0165 234689. -8046.0084 8.816E-05 0.000 5.905E+1062.3459 18139. 0.000 23.200 -0.0160 196669. -7599.2749 0.000106 0.000 5.906E+10123.7930 37069. 0.000 23.600 -0.0155 161482. -7009.6170 0.000120 0.000 5.906E+10121.8978 37788. 0.000 24.000 -0.0149 129088. -6430.6617 0.000132 0.000 5.906E+10119.3337 38507. 0.000 24.400 -0.0142 99431. -5865.4392 0.000141 0.000 5.906E+10116.1757 39226. 0.000 24.800 -0.0135 72440. -5316.6234 0.000148 0.000 5.906E+10112.4976 39944. 0.000 25.200 -0.0128 48035. -4786.5389 0.000153 0.000 5.906E+10108.3710 40663. 0.000 25.600 -0.0120 26122. -4277.1716 0.000156 0.000 5.906E+10103.8654 41382. 0.000 26.000 -0.0113 6599.3417 -3790.1811 0.000158 0.000 5.906E+1099.0473 42101. 0.000 26.400 -0.0105 -10642. -3326.9153 0.000157 0.000 5.906E+1093.9801 42820. 0.000 26.800 -0.009782 -25717. -2888.4260 0.000156 0.000 5.906E+1088.7237 43539. 0.000 27.200 -0.009038 -38745. -2475.4872 0.000153 0.000 5.906E+1083.3341 44257. 0.000 27.600 -0.008310 -49849. -2088.6129 0.000150 0.000 5.906E+1077.8635 44976. 0.000 28.000 -0.007601 -59155. -1728.0766 0.000145 0.000 5.906E+1072.3599 45695. 0.000 28.400 -0.006915 -66788. -1393.9316 0.000140 0.000 5.906E+1066.8672 46414. 0.000 28.800 -0.006256 -72873. -1086.0308 0.000134 0.000 5.906E+1061.4249 47133. 0.000

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24new.lp6o 29.200 -0.005624 -77536. -804.0471 0.000128 0.000 5.906E+1056.0684 47852. 0.000 29.600 -0.005023 -80900. -547.4936 0.000122 0.000 5.906E+1050.8289 48570. 0.000 30.000 -0.004454 -83085. -303.7172 0.000115 0.000 5.906E+1050.7446 54690. 0.000 30.400 -0.003917 -84092. -62.7415 0.000108 0.000 5.906E+1049.6619 60862. 0.000 30.800 -0.003412 -83947. 161.7693 0.000102 0.000 5.906E+1043.8842 61729. 0.000 31.200 -0.002941 -82783. 359.1349 9.486E-05 0.000 5.906E+1038.3515 62595. 0.000 31.600 -0.002502 -80727. 530.5598 8.822E-05 0.000 5.906E+1033.0756 63461. 0.000 32.000 -0.002094 -77902. 677.2928 8.177E-05 0.000 5.906E+1028.0632 64328. 0.000 32.400 -0.001717 -74422. 800.6036 7.558E-05 0.000 5.906E+1023.3164 65194. 0.000 32.800 -0.001368 -70397. 901.7619 6.970E-05 0.000 5.906E+1018.8329 66061. 0.000 33.200 -0.001048 -65932. 982.0169 6.416E-05 0.000 5.906E+1014.6067 66927. 0.000 33.600 -0.000752 -61124. 1042.5800 5.899E-05 0.000 5.906E+1010.6279 67793. 0.000 34.000 -0.000481 -56065. 1084.6080 5.423E-05 0.000 5.906E+106.8837 68660. 0.000 34.400 -0.000232 -50842. 1109.1891 4.989E-05 0.000 5.906E+103.3584 69526. 0.000 34.800 -2.316E-06 -45536. 1117.3309 4.597E-05 0.000 5.906E+100.0340 70393. 0.000 35.200 0.000209 -40226. 1109.9493 4.249E-05 0.000 5.906E+10-3.1096 71259. 0.000 35.600 0.000406 -34983. 1087.8610 3.943E-05 0.000 5.906E+10-6.0938 72125. 0.000 36.000 0.000588 -29877. 1051.7766 3.679E-05 0.000 5.906E+10-8.9413 72992. 0.000 36.400 0.000759 -24974. 1002.2966 3.456E-05 0.000 5.906E+10-11.6753 73858. 0.000 36.800 0.000920 -20338. 939.9095 3.272E-05 0.000 5.906E+10-14.3193 74725. 0.000 37.200 0.001073 -16029. 864.9917 3.125E-05 0.000 5.906E+10-16.8965 75591. 0.000 37.600 0.001220 -12109. 777.8100 3.010E-05 0.000 5.906E+10-19.4293 76457. 0.000 38.000 0.001362 -8634.7414 678.5261 2.926E-05 0.000 5.906E+10-21.9390 77324. 0.000 38.400 0.001501 -5665.2432 567.2041 2.868E-05 0.000 5.906E+10-24.4452 78190. 0.000 38.800 0.001637 -3258.4091 443.8197 2.832E-05 0.000 5.906E+10-26.9650 79057. 0.000 39.200 0.001772 -1472.5314 308.2724 2.812E-05 0.000 5.906E+10-29.5130 79923. 0.000 39.600 0.001907 -366.4898 160.4008 2.805E-05 0.000 5.906E+10-32.1002 80789. 0.000 40.000 0.002042 0.000 0.000 2.803E-05 0.000 5.906E+10-34.7335 40828. 0.000

* This analysis makes computations of pile response using nonlinear moment-curvaturerelationships. The above values of total stress are computed for combined axial and bending stress in elastic sections and do not equal actual stresses in concrete and steel in the range of nonlinear bending.

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24new.lp6o

Output Summary for Load Case No. 3:

Pile-head deflection = 0.7500000 inchesComputed slope at pile head = -0.0062789 radiansMaximum bending moment = 1695876. inch-lbsMaximum shear force = 25874. lbsDepth of maximum bending moment = 105.6000000 inches below pile headDepth of maximum shear force = 0.000000 inches below pile headNumber of iterations = 13Number of zero deflection points = 2

-------------------------------------------------------------------------------- Computed Values of Pile Loading and Deflection for Lateral Loading for Load Case Number 4--------------------------------------------------------------------------------

Pile-head conditions are Displacement and Pile-head Rotation (Loading Type 5)Displacement of pile head = 0.250000 inchesRotation of pile head = 0.000E+00 radiansAxial load on pile head = 250000.000 lbs

Depth Deflect. Bending Shear Slope Total Bending Soil Res. Soil Spr. Distrib. X y Moment Force S Stress Stiffness p Es*h Lat. Load feet inches in-lbs lbs radians psi* lb-in^2 lb/in lb/inch lb/inch ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- 0.00 0.2500 -1807120. 24268. 0.000 0.000 3.501E+100.000 0.000 0.000 0.400 0.2494 -1690677. 24188. -0.000240 0.000 3.501E+10-16.5345 318.2196 0.000 0.800 0.2477 -1574336. 24070. -0.000448 0.000 4.093E+10-32.8427 636.4393 0.000 1.200 0.2451 -1458531. 23874. -0.000619 0.000 4.422E+10-48.7483 954.6589 0.000 1.600 0.2418 -1343659. 23603. -0.000766 0.000 4.758E+10-64.1085 1272.8785 0.000 2.000 0.2377 -1230101. 23260. -0.000884 0.000 5.871E+10-78.8084 1591.0981 0.000 2.400 0.2333 -1118238. 22848. -0.000980 0.000 5.882E+10-92.7854 1909.3178 0.000 2.800 0.2283 -1008404. 22371. -0.001067 0.000 5.890E+10-105.9642 2227.5374 0.000 3.200 0.2230 -900912. 21833. -0.001145 0.000 5.896E+10-118.2809 2545.7570 0.000 3.600 0.2173 -796058. 21238. -0.001214 0.000 5.899E+10-129.6822 2863.9766 0.000 4.000 0.2114 -694114. 20591. -0.001275 0.000 5.901E+10-140.1254 3182.1963 0.000 4.400 0.2051 -595330. 19895. -0.001327 0.000 5.902E+10-149.5779 3500.4159 0.000 4.800 0.1986 -499935. 19157. -0.001371 0.000 5.903E+10-158.0163 3818.6355 0.000 5.200 0.1919 -408132. 18381. -0.001408 0.000 5.904E+10-165.4266 4136.8551 0.000 5.600 0.1851 -320100. 17571. -0.001438 0.000 5.905E+10-171.8033 4455.0748 0.000

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24new.lp6o 6.000 0.1781 -235995. 16734. -0.001461 0.000 5.905E+10-177.1489 4773.2944 0.000 6.400 0.1711 -155949. 15873. -0.001477 0.000 5.906E+10-181.4733 5091.5140 0.000 6.800 0.1640 -80069. 14994. -0.001486 0.000 5.906E+10-184.7935 5409.7336 0.000 7.200 0.1568 -8438.1373 14102. -0.001490 0.000 5.906E+10-187.1326 5727.9533 0.000 7.600 0.1497 58882. 13200. -0.001488 0.000 5.906E+10-188.5197 6046.1729 0.000 8.000 0.1425 121852. 12294. -0.001480 0.000 5.906E+10-188.9889 6364.3925 0.000 8.400 0.1355 180456. 11388. -0.001468 0.000 5.906E+10-188.5791 6682.6121 0.000 8.800 0.1284 234698. 10486. -0.001451 0.000 5.905E+10-187.3329 7000.8318 0.000 9.200 0.1215 284601. 9591.2964 -0.001430 0.000 5.905E+10-185.2967 7319.0514 0.000 9.600 0.1147 330207. 8708.5372 -0.001405 0.000 5.905E+10-182.5197 7637.2710 0.000 10.000 0.1080 371575. 7840.7618 -0.001377 0.000 5.904E+10-179.0534 7955.4906 0.000 10.400 0.1015 408782. 6991.1504 -0.001345 0.000 5.904E+10-174.9514 8273.7103 0.000 10.800 0.0951 441918. 6162.6231 -0.001310 0.000 5.904E+10-170.2684 8591.9299 0.000 11.200 0.0889 471088. 5357.8344 -0.001273 0.000 5.903E+10-165.0602 8910.1495 0.000 11.600 0.0829 496408. 4579.1705 -0.001234 0.000 5.903E+10-159.3831 9228.3691 0.000 12.000 0.0771 518009. 3828.7475 -0.001193 0.000 5.903E+10-153.2932 9546.5888 0.000 12.400 0.0715 536027. 3108.4124 -0.001150 0.000 5.903E+10-146.8464 9864.8084 0.000 12.800 0.0660 550609. 2419.7459 -0.001106 0.000 5.903E+10-140.0980 10183. 0.000 13.200 0.0608 561909. 1764.0663 -0.001060 0.000 5.902E+10-133.1019 10501. 0.000 13.600 0.0559 570088. 1142.4360 -0.001014 0.000 5.902E+10-125.9108 10819. 0.000 14.000 0.0511 575311. 555.6680 -0.000968 0.000 5.902E+10-118.5759 11138. 0.000 14.400 0.0466 577745. 4.3352 -0.000921 0.000 5.902E+10-111.1461 11456. 0.000 14.800 0.0423 577562. -511.2204 -0.000874 0.000 5.902E+10-103.6687 11774. 0.000 15.200 0.0382 574935. -990.8767 -0.000827 0.000 5.902E+10-96.1881 12092. 0.000 15.600 0.0343 570035. -1434.7200 -0.000780 0.000 5.902E+10-88.7466 12411. 0.000 16.000 0.0307 563034. -1843.0330 -0.000734 0.000 5.902E+10-81.3838 12729. 0.000 16.400 0.0273 554104. -2216.2817 -0.000689 0.000 5.903E+10-74.1365 13047. 0.000 16.800 0.0241 543411. -2555.1017 -0.000644 0.000 5.903E+10-67.0386 13365. 0.000 17.200 0.0211 531121. -2860.2853 -0.000601 0.000 5.903E+10-60.1213 13683. 0.000 17.600 0.0183 517394. -3132.7667 -0.000558 0.000 5.903E+10-53.4127 14002. 0.000 18.000 0.0157 502386. -3373.6086 -0.000516 0.000 5.903E+10-46.9381 14320. 0.000 18.400 0.0134 486247. -3583.9874 -0.000476 0.000 5.903E+10

Page 24

24new.lp6o-40.7198 14638. 0.000 18.800 0.0112 469123. -3765.1796 -0.000437 0.000 5.904E+10-34.7770 14956. 0.000 19.200 0.009153 451151. -3918.5478 -0.000400 0.000 5.904E+10-29.1264 15275. 0.000 19.600 0.007321 432465. -4045.5264 -0.000364 0.000 5.904E+10-23.7814 15593. 0.000 20.000 0.005657 413188. -4147.6088 -0.000330 0.000 5.904E+10-18.7529 15911. 0.000 20.400 0.004155 393439. -4226.3336 -0.000297 0.000 5.904E+10-14.0491 16229. 0.000 20.800 0.002807 373328. -4283.2721 -0.000266 0.000 5.904E+10-9.6753 16547. 0.000 21.200 0.001604 352957. -4320.0161 -0.000236 0.000 5.905E+10-5.6346 16866. 0.000 21.600 0.000538 332423. -4338.1652 -0.000208 0.000 5.905E+10-1.9275 17184. 0.000 22.000 -0.000397 311811. -4339.3161 -0.000182 0.000 5.905E+101.4479 17502. 0.000 22.400 -0.001211 291203. -4325.0513 -0.000158 0.000 5.905E+104.4957 17820. 0.000 22.800 -0.001911 270669. -4296.9287 -0.000135 0.000 5.905E+107.2221 18139. 0.000 23.200 -0.002506 250276. -4233.1519 -0.000114 0.000 5.905E+1019.3516 37069. 0.000 23.600 -0.003003 230304. -4129.9737 -9.418E-05 0.000 5.905E+1023.6393 37788. 0.000 24.000 -0.003410 210854. -4007.5874 -7.625E-05 0.000 5.905E+1027.3550 38507. 0.000 24.400 -0.003735 192014. -3868.6865 -5.987E-05 0.000 5.906E+1030.5204 39226. 0.000 24.800 -0.003985 173858. -3715.8545 -4.501E-05 0.000 5.906E+1033.1596 39944. 0.000 25.200 -0.004167 156450. -3551.5534 -3.158E-05 0.000 5.906E+1035.2992 40663. 0.000 25.600 -0.004288 139839. -3378.1145 -1.954E-05 0.000 5.906E+1036.9670 41382. 0.000 26.000 -0.004354 124067. -3197.7313 -8.817E-06 0.000 5.906E+1038.1926 42101. 0.000 26.400 -0.004373 109162. -3012.4537 6.610E-07 0.000 5.906E+1039.0064 42820. 0.000 26.800 -0.004348 95146. -2824.1841 8.964E-06 0.000 5.906E+1039.4393 43539. 0.000 27.200 -0.004286 82029. -2634.6756 1.616E-05 0.000 5.906E+1039.5226 44257. 0.000 27.600 -0.004193 69814. -2445.5311 2.233E-05 0.000 5.906E+1039.2876 44976. 0.000 28.000 -0.004072 58498. -2258.2042 2.755E-05 0.000 5.906E+1038.7653 45695. 0.000 28.400 -0.003928 48069. -2074.0007 3.188E-05 0.000 5.906E+1037.9861 46414. 0.000 28.800 -0.003766 38511. -1894.0825 3.540E-05 0.000 5.906E+1036.9798 47133. 0.000 29.200 -0.003589 29801. -1719.4708 3.817E-05 0.000 5.906E+1035.7751 47852. 0.000 29.600 -0.003400 21912. -1551.0518 4.028E-05 0.000 5.906E+1034.3995 48570. 0.000 30.000 -0.003202 14814. -1380.9355 4.177E-05 0.000 5.906E+1036.4823 54690. 0.000 30.400 -0.002999 8555.1806 -1202.1280 4.272E-05 0.000 5.906E+1038.0209 60862. 0.000 30.800 -0.002792 3171.2885 -1024.7088 4.319E-05 0.000 5.906E+1035.9038 61729. 0.000

Page 25

24new.lp6o 31.200 -0.002584 -1385.6900 -857.6696 4.327E-05 0.000 5.906E+1033.6959 62595. 0.000 31.600 -0.002377 -5166.1802 -701.3913 4.300E-05 0.000 5.906E+1031.4201 63461. 0.000 32.000 -0.002171 -8222.2477 -556.1517 4.246E-05 0.000 5.906E+1029.0964 64328. 0.000 32.400 -0.001969 -10607. -422.1391 4.169E-05 0.000 5.906E+1026.7422 65194. 0.000 32.800 -0.001771 -12375. -299.4654 4.076E-05 0.000 5.906E+1024.3719 66061. 0.000 33.200 -0.001578 -13580. -188.1791 3.970E-05 0.000 5.906E+1021.9974 66927. 0.000 33.600 -0.001390 -14277. -88.2780 3.857E-05 0.000 5.906E+1019.6280 67793. 0.000 34.000 -0.001207 -14520. 0.2783 3.740E-05 0.000 5.906E+1017.2705 68660. 0.000 34.400 -0.001031 -14364. 77.5573 3.623E-05 0.000 5.906E+1014.9291 69526. 0.000 34.800 -0.000860 -13862. 143.6419 3.508E-05 0.000 5.906E+1012.6062 70393. 0.000 35.200 -0.000694 -13069. 198.6209 3.399E-05 0.000 5.906E+1010.3017 71259. 0.000 35.600 -0.000533 -12037. 242.5789 3.296E-05 0.000 5.906E+108.0141 72125. 0.000 36.000 -0.000377 -10819. 275.5885 3.204E-05 0.000 5.906E+105.7399 72992. 0.000 36.400 -0.000226 -9468.2893 297.7029 3.121E-05 0.000 5.906E+103.4744 73858. 0.000 36.800 -7.783E-05 -8036.2824 308.9494 3.050E-05 0.000 5.906E+101.2116 74725. 0.000 37.200 6.700E-05 -6575.5752 309.3250 2.991E-05 0.000 5.906E+10-1.0552 75591. 0.000 37.600 0.000209 -5138.5374 298.7926 2.943E-05 0.000 5.906E+10-3.3334 76457. 0.000 38.000 0.000350 -3777.7993 277.2789 2.907E-05 0.000 5.906E+10-5.6307 77324. 0.000 38.400 0.000488 -2546.4233 244.6743 2.881E-05 0.000 5.906E+10-7.9546 78190. 0.000 38.800 0.000626 -1498.0723 200.8340 2.865E-05 0.000 5.906E+10-10.3122 79057. 0.000 39.200 0.000763 -687.1690 145.5808 2.856E-05 0.000 5.906E+10-12.7099 79923. 0.000 39.600 0.000900 -169.0349 78.7109 2.852E-05 0.000 5.906E+10-15.1526 80789. 0.000 40.000 0.001037 0.000 0.000 2.852E-05 0.000 5.906E+10-17.6436 40828. 0.000

* This analysis makes computations of pile response using nonlinear moment-curvaturerelationships. The above values of total stress are computed for combined axial and bending stress in elastic sections and do not equal actual stresses in concrete and steel in the range of nonlinear bending.

Output Summary for Load Case No. 4:

Pile-head deflection = 0.2500000 inchesComputed slope at pile head = -0.000007981 radiansMaximum bending moment = -1807120. inch-lbsMaximum shear force = 24268. lbsDepth of maximum bending moment = 0.000000 inches below pile headDepth of maximum shear force = 0.000000 inches below pile head

Page 26

24new.lp6oNumber of iterations = 14Number of zero deflection points = 2

-------------------------------------------------------------------------------- Computed Values of Pile Loading and Deflection for Lateral Loading for Load Case Number 5--------------------------------------------------------------------------------

Pile-head conditions are Displacement and Pile-head Rotation (Loading Type 5)Displacement of pile head = 0.500000 inchesRotation of pile head = 0.000E+00 radiansAxial load on pile head = 250000.000 lbs

Depth Deflect. Bending Shear Slope Total Bending Soil Res. Soil Spr. Distrib. X y Moment Force S Stress Stiffness p Es*h Lat. Load feet inches in-lbs lbs radians psi* lb-in^2 lb/in lb/inch lb/inch ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- 0.00 0.5000 -2815732. 42628. 0.000 0.000 2.129E+100.000 0.000 0.000 0.400 0.4985 -2611118. 42469. -0.000612 0.000 2.129E+10-33.0469 318.2196 0.000 0.800 0.4941 -2406560. 42233. -0.001136 0.000 2.509E+10-65.5172 636.4393 0.000 1.200 0.4876 -2202958. 41843. -0.001557 0.000 2.770E+10-96.9713 954.6589 0.000 1.600 0.4792 -2001133. 41305. -0.001903 0.000 3.100E+10-127.0699 1272.8785 0.000 2.000 0.4693 -1801863. 40627. -0.002181 0.000 3.512E+10-155.5628 1591.0981 0.000 2.400 0.4582 -1605882. 39816. -0.002401 0.000 4.004E+10-182.2757 1909.3178 0.000 2.800 0.4463 -1413870. 38881. -0.002571 0.000 4.551E+10-207.0933 2227.5374 0.000 3.200 0.4336 -1226450. 37832. -0.002696 0.000 5.872E+10-229.9421 2545.7570 0.000 3.600 0.4204 -1044208. 36679. -0.002789 0.000 5.888E+10-250.8198 2863.9766 0.000 4.000 0.4068 -867642. 35429. -0.002867 0.000 5.897E+10-269.6788 3182.1963 0.000 4.400 0.3929 -697205. 34095. -0.002930 0.000 5.900E+10-286.4887 3500.4159 0.000 4.800 0.3787 -533301. 32684. -0.002980 0.000 5.903E+10-301.2350 3818.6355 0.000 5.200 0.3642 -376285. 31208. -0.003017 0.000 5.904E+10-313.9190 4136.8551 0.000 5.600 0.3497 -226465. 29675. -0.003042 0.000 5.905E+10-324.5560 4455.0748 0.000 6.000 0.3350 -84101. 28097. -0.003054 0.000 5.906E+10-333.1751 4773.2944 0.000 6.400 0.3204 50595. 26482. -0.003056 0.000 5.906E+10-339.8176 5091.5140 0.000 6.800 0.3057 177456. 24839. -0.003047 0.000 5.906E+10-344.5362 5409.7336 0.000 7.200 0.2911 296363. 23179. -0.003027 0.000 5.905E+10-347.3939 5727.9533 0.000 7.600 0.2766 407236. 21509. -0.002999 0.000 5.904E+10-348.4628 6046.1729 0.000

Page 27

24new.lp6o 8.000 0.2623 510041. 19837. -0.002961 0.000 5.903E+10-347.8235 6364.3925 0.000 8.400 0.2482 604783. 18173. -0.002916 0.000 5.902E+10-345.5634 6682.6121 0.000 8.800 0.2343 691503. 16524. -0.002863 0.000 5.901E+10-341.7761 7000.8318 0.000 9.200 0.2207 770282. 14896. -0.002804 0.000 5.899E+10-336.5602 7319.0514 0.000 9.600 0.2074 841231. 13296. -0.002738 0.000 5.898E+10-330.0186 7637.2710 0.000 10.000 0.1944 904494. 11730. -0.002667 0.000 5.895E+10-322.2571 7955.4906 0.000 10.400 0.1818 960245. 10205. -0.002591 0.000 5.893E+10-313.3839 8273.7103 0.000 10.800 0.1696 1008680. 8724.3365 -0.002511 0.000 5.890E+10-303.5086 8591.9299 0.000 11.200 0.1577 1050025. 7293.3364 -0.002427 0.000 5.888E+10-292.7414 8910.1495 0.000 11.600 0.1463 1084522. 5915.8958 -0.002340 0.000 5.885E+10-281.1922 9228.3691 0.000 12.000 0.1352 1112434. 4595.5071 -0.002251 0.000 5.883E+10-268.9698 9546.5888 0.000 12.400 0.1247 1134040. 3335.1438 -0.002159 0.000 5.881E+10-256.1816 9864.8084 0.000 12.800 0.1145 1149633. 2137.2702 -0.002066 0.000 5.880E+10-242.9324 10183. 0.000 13.200 0.1048 1159516. 1003.8541 -0.001971 0.000 5.879E+10-229.3243 10501. 0.000 13.600 0.0956 1164001. -63.6176 -0.001877 0.000 5.878E+10-215.4556 10819. 0.000 14.000 0.0868 1163409. -1064.1214 -0.001782 0.000 5.878E+10-201.4210 11138. 0.000 14.400 0.0785 1158061. -1997.0768 -0.001687 0.000 5.879E+10-187.3105 11456. 0.000 14.800 0.0706 1148285. -2862.3252 -0.001593 0.000 5.880E+10-173.2097 11774. 0.000 15.200 0.0632 1134405. -3660.1058 -0.001499 0.000 5.881E+10-159.1989 12092. 0.000 15.600 0.0562 1116747. -4391.0317 -0.001408 0.000 5.883E+10-145.3535 12411. 0.000 16.000 0.0497 1095630. -5056.0636 -0.001317 0.000 5.884E+10-131.7431 12729. 0.000 16.400 0.0436 1071370. -5656.4835 -0.001229 0.000 5.886E+10-118.4319 13047. 0.000 16.800 0.0379 1044277. -6193.8681 -0.001143 0.000 5.888E+10-105.4784 13365. 0.000 17.200 0.0326 1014652. -6670.0610 -0.001059 0.000 5.890E+10-92.9353 13683. 0.000 17.600 0.0277 982786. -7087.1455 -0.000977 0.000 5.892E+10-80.8499 14002. 0.000 18.000 0.0232 948961. -7447.4174 -0.000899 0.000 5.894E+10-69.2634 14320. 0.000 18.400 0.0191 913448. -7753.3574 -0.000823 0.000 5.895E+10-58.2116 14638. 0.000 18.800 0.0153 876504. -8007.6048 -0.000750 0.000 5.897E+10-47.7248 14956. 0.000 19.200 0.0119 838375. -8212.9310 -0.000680 0.000 5.898E+10-37.8278 15275. 0.000 19.600 0.008786 799293. -8372.2135 -0.000614 0.000 5.899E+10-28.5400 15593. 0.000 20.000 0.005996 759474. -8488.4114 -0.000550 0.000 5.899E+10-19.8758 15911. 0.000 20.400 0.003503 719124. -8564.5406 -0.000490 0.000 5.900E+10

Page 28

24new.lp6o-11.8447 16229. 0.000 20.800 0.001291 678431. -8603.6505 -0.000433 0.000 5.901E+10-4.4511 16547. 0.000 21.200 -0.000656 637569. -8608.8010 -0.000380 0.000 5.901E+102.3050 16866. 0.000 21.600 -0.002354 596698. -8583.0411 -0.000330 0.000 5.902E+108.4282 17184. 0.000 22.000 -0.003820 555963. -8529.3880 -0.000283 0.000 5.902E+1013.9272 17502. 0.000 22.400 -0.005068 515494. -8450.8070 -0.000239 0.000 5.903E+1018.8148 17820. 0.000 22.800 -0.006115 475409. -8350.1931 -0.000199 0.000 5.903E+1023.1076 18139. 0.000 23.200 -0.006977 435810. -8165.4276 -0.000162 0.000 5.904E+1053.8780 37069. 0.000 23.600 -0.007668 397409. -7891.2410 -0.000128 0.000 5.904E+1060.3664 37788. 0.000 24.000 -0.008204 360361. -7588.3988 -9.710E-05 0.000 5.905E+1065.8179 38507. 0.000 24.400 -0.008600 324794. -7261.7619 -6.925E-05 0.000 5.905E+1070.2808 39226. 0.000 24.800 -0.008869 290814. -6915.9493 -4.423E-05 0.000 5.905E+1073.8077 39944. 0.000 25.200 -0.009025 258507. -6555.3211 -2.191E-05 0.000 5.905E+1076.4540 40663. 0.000 25.600 -0.009080 227935. -6183.9660 -2.137E-06 0.000 5.905E+1078.2773 41382. 0.000 26.000 -0.009045 199146. -5805.6918 1.522E-05 0.000 5.906E+1079.3370 42101. 0.000 26.400 -0.008933 172164. -5424.0191 3.031E-05 0.000 5.906E+1079.6933 42820. 0.000 26.800 -0.008754 147002. -5042.1786 4.328E-05 0.000 5.906E+1079.4069 43539. 0.000 27.200 -0.008518 123655. -4663.1108 5.428E-05 0.000 5.906E+1078.5380 44257. 0.000 27.600 -0.008233 102106. -4289.4682 6.345E-05 0.000 5.906E+1077.1464 44976. 0.000 28.000 -0.007909 82324. -3923.6204 7.095E-05 0.000 5.906E+1075.2902 45695. 0.000 28.400 -0.007552 64269. -3567.6607 7.691E-05 0.000 5.906E+1073.0263 46414. 0.000 28.800 -0.007170 47890. -3223.4150 8.146E-05 0.000 5.906E+1070.4094 47133. 0.000 29.200 -0.006770 33129. -2892.4519 8.476E-05 0.000 5.906E+1067.4919 47852. 0.000 29.600 -0.006357 19919. -2576.0944 8.691E-05 0.000 5.906E+1064.3237 48570. 0.000 30.000 -0.005936 8189.7168 -2259.4042 8.805E-05 0.000 5.906E+1067.6306 54690. 0.000 30.400 -0.005512 -1982.3840 -1929.3696 8.831E-05 0.000 5.906E+1069.8838 60862. 0.000 30.800 -0.005088 -10544. -1604.6102 8.780E-05 0.000 5.906E+1065.4326 61729. 0.000 31.200 -0.004669 -17597. -1301.4550 8.665E-05 0.000 5.906E+1060.8821 62595. 0.000 31.600 -0.004256 -23246. -1020.2878 8.499E-05 0.000 5.906E+1056.2709 63461. 0.000 32.000 -0.003853 -27596. -761.3196 8.293E-05 0.000 5.906E+1051.6324 64328. 0.000 32.400 -0.003460 -30754. -524.6149 8.056E-05 0.000 5.906E+1046.9945 65194. 0.000 32.800 -0.003079 -32826. -310.1161 7.797E-05 0.000 5.906E+1042.3800 66061. 0.000

Page 29

24new.lp6o 33.200 -0.002711 -33918. -117.6685 7.526E-05 0.000 5.906E+1037.8065 66927. 0.000 33.600 -0.002357 -34136. 52.9565 7.250E-05 0.000 5.906E+1033.2872 67793. 0.000 34.000 -0.002016 -33584. 202.0387 6.974E-05 0.000 5.906E+1028.8304 68660. 0.000 34.400 -0.001687 -32364. 329.8876 6.706E-05 0.000 5.906E+1024.4401 69526. 0.000 34.800 -0.001372 -30578. 436.8232 6.451E-05 0.000 5.906E+1020.1164 70393. 0.000 35.200 -0.001068 -28325. 523.1569 6.211E-05 0.000 5.906E+1015.8560 71259. 0.000 35.600 -0.000775 -25704. 589.1759 5.992E-05 0.000 5.906E+1011.6519 72125. 0.000 36.000 -0.000493 -22813. 635.1279 5.794E-05 0.000 5.906E+107.4948 72992. 0.000 36.400 -0.000219 -19746. 661.2094 5.621E-05 0.000 5.906E+103.3725 73858. 0.000 36.800 4.680E-05 -16600. 667.5547 5.474E-05 0.000 5.906E+10-0.7286 74725. 0.000 37.200 0.000306 -13469. 654.2290 5.352E-05 0.000 5.906E+10-4.8238 75591. 0.000 37.600 0.000561 -10448. 621.2226 5.254E-05 0.000 5.906E+10-8.9289 76457. 0.000 38.000 0.000811 -7631.5042 568.4489 5.181E-05 0.000 5.906E+10-13.0601 77324. 0.000 38.400 0.001058 -5115.2012 495.7449 5.129E-05 0.000 5.906E+10-17.2332 78190. 0.000 38.800 0.001303 -2995.4526 402.8748 5.096E-05 0.000 5.906E+10-21.4627 79057. 0.000 39.200 0.001547 -1369.9115 289.5376 5.078E-05 0.000 5.906E+10-25.7612 79923. 0.000 39.600 0.001791 -337.7738 155.3778 5.071E-05 0.000 5.906E+10-30.1388 80789. 0.000 40.000 0.002034 0.000 0.000 5.070E-05 0.000 5.906E+10-34.6020 40828. 0.000

* This analysis makes computations of pile response using nonlinear moment-curvaturerelationships. The above values of total stress are computed for combined axial and bending stress in elastic sections and do not equal actual stresses in concrete and steel in the range of nonlinear bending.

Output Summary for Load Case No. 5:

Pile-head deflection = 0.5000000 inchesComputed slope at pile head = -0.0000231 radiansMaximum bending moment = -2815732. inch-lbsMaximum shear force = 42628. lbsDepth of maximum bending moment = 0.000000 inches below pile headDepth of maximum shear force = 0.000000 inches below pile headNumber of iterations = 15Number of zero deflection points = 2

-------------------------------------------------------------------------------- Computed Values of Pile Loading and Deflection for Lateral Loading for Load Case Number 6--------------------------------------------------------------------------------

Page 30

24new.lp6oPile-head conditions are Displacement and Pile-head Rotation (Loading Type 5)Displacement of pile head = 0.750000 inchesRotation of pile head = 0.000E+00 radiansAxial load on pile head = 250000.000 lbs

Depth Deflect. Bending Shear Slope Total Bending Soil Res. Soil Spr. Distrib. X y Moment Force S Stress Stiffness p Es*h Lat. Load feet inches in-lbs lbs radians psi* lb-in^2 lb/in lb/inch lb/inch ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- ---------- 0.00 0.7500 -3585322. 57559. 0.000 0.000 1.555E+100.000 0.000 0.000 0.400 0.7473 -3308946. 57321. -0.001064 0.000 1.555E+10-49.5458 318.2196 0.000 0.800 0.7398 -3032486. 56967. -0.001943 0.000 1.978E+10-98.0894 636.4393 0.000 1.200 0.7287 -2757403. 56384. -0.002615 0.000 2.174E+10-144.9283 954.6589 0.000 1.600 0.7147 -2484928. 55581. -0.003165 0.000 2.423E+10-189.5219 1272.8785 0.000 2.000 0.6983 -2216230. 54570. -0.003605 0.000 2.751E+10-231.4742 1591.0981 0.000 2.400 0.6801 -1952400. 53366. -0.003945 0.000 3.191E+10-270.5168 1909.3178 0.000 2.800 0.6604 -1694451. 51981. -0.004200 0.000 3.770E+10-306.4879 2227.5374 0.000 3.200 0.6398 -1443305. 50431. -0.004385 0.000 4.464E+10-339.3056 2545.7570 0.000 3.600 0.6183 -1199789. 48731. -0.004512 0.000 5.875E+10-368.9372 2863.9766 0.000 4.000 0.5964 -964657. 46897. -0.004600 0.000 5.893E+10-395.4165 3182.1963 0.000 4.400 0.5742 -738540. 44943. -0.004670 0.000 5.900E+10-418.7181 3500.4159 0.000 4.800 0.5516 -521999. 42885. -0.004721 0.000 5.903E+10-438.8374 3818.6355 0.000 5.200 0.5289 -315518. 40738. -0.004755 0.000 5.905E+10-455.7902 4136.8551 0.000 5.600 0.5060 -119507. 38517. -0.004773 0.000 5.906E+10-469.6107 4455.0748 0.000 6.000 0.4830 65695. 36237. -0.004775 0.000 5.906E+10-480.3505 4773.2944 0.000 6.400 0.4601 239824. 33912. -0.004762 0.000 5.905E+10-488.0769 5091.5140 0.000 6.800 0.4373 402684. 31558. -0.004736 0.000 5.904E+10-492.8718 5409.7336 0.000 7.200 0.4147 554150. 29188. -0.004697 0.000 5.903E+10-494.8294 5727.9533 0.000 7.600 0.3922 694160. 26814. -0.004647 0.000 5.901E+10-494.0556 6046.1729 0.000 8.000 0.3701 822719. 24451. -0.004585 0.000 5.898E+10-490.6661 6364.3925 0.000 8.400 0.3482 939893. 22110. -0.004513 0.000 5.894E+10-484.7847 6682.6121 0.000 8.800 0.3267 1045806. 19803. -0.004432 0.000 5.888E+10-476.5426 7000.8318 0.000 9.200 0.3057 1140637. 17540. -0.004343 0.000 5.880E+10-466.0765 7319.0514 0.000 9.600 0.2850 1224618. 15333. -0.004246 0.000 5.872E+10-453.5279 7637.2710 0.000

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24new.lp6o 10.000 0.2649 1298029. 13191. -0.004133 0.000 4.890E+10-439.0412 7955.4906 0.000 10.400 0.2454 1361172. 11123. -0.003999 0.000 4.705E+10-422.9380 8273.7103 0.000 10.800 0.2265 1414404. 9134.4167 -0.003855 0.000 4.549E+10-405.4383 8591.9299 0.000 11.200 0.2084 1458116. 7233.1239 -0.003702 0.000 4.421E+10-386.7671 8910.1495 0.000 11.600 0.1910 1492726. 5423.7215 -0.003540 0.000 4.321E+10-367.1506 9228.3691 0.000 12.000 0.1744 1518678. 3710.2118 -0.003371 0.000 4.246E+10-346.8118 9546.5888 0.000 12.400 0.1586 1536434. 2095.5440 -0.003197 0.000 4.196E+10-325.9665 9864.8084 0.000 12.800 0.1437 1546469. 581.6555 -0.003020 0.000 4.168E+10-304.8204 10183. 0.000 13.200 0.1296 1549266. -830.4715 -0.002842 0.000 4.160E+10-283.5659 10501. 0.000 13.600 0.1164 1545316. -2140.7417 -0.002663 0.000 4.171E+10-262.3801 10819. 0.000 14.000 0.1040 1535107. -3349.8699 -0.002487 0.000 4.200E+10-241.4233 11138. 0.000 14.400 0.0925 1519126. -4459.2973 -0.002313 0.000 4.245E+10-220.8381 11456. 0.000 14.800 0.0818 1497850. -5471.1050 -0.002144 0.000 4.306E+10-200.7485 11774. 0.000 15.200 0.0720 1471748. -6387.9259 -0.001980 0.000 4.382E+10-181.2603 12092. 0.000 15.600 0.0628 1441277. -7212.8586 -0.001822 0.000 4.470E+10-162.4617 12411. 0.000 16.000 0.0545 1406877. -7949.3848 -0.001670 0.000 4.571E+10-144.4242 12729. 0.000 16.400 0.0468 1368972. -8601.2929 -0.001526 0.000 4.682E+10-127.2042 13047. 0.000 16.800 0.0398 1327968. -9172.6080 -0.001390 0.000 4.803E+10-110.8438 13365. 0.000 17.200 0.0335 1284250. -9667.5273 -0.001261 0.000 4.930E+10-95.3726 13683. 0.000 17.600 0.0277 1238186. -10090. -0.001148 0.000 5.871E+10-80.8099 14002. 0.000 18.000 0.0224 1190138. -10445. -0.001049 0.000 5.876E+10-66.9340 14320. 0.000 18.400 0.0176 1140431. -10735. -0.000953 0.000 5.880E+10-53.7829 14638. 0.000 18.800 0.0133 1089373. -10963. -0.000863 0.000 5.885E+10-41.3876 14956. 0.000 19.200 0.009356 1037256. -11134. -0.000776 0.000 5.889E+10-29.7724 15275. 0.000 19.600 0.005835 984350. -11251. -0.000693 0.000 5.892E+10-18.9548 15593. 0.000 20.000 0.002699 930912. -11318. -0.000615 0.000 5.894E+10-8.9464 15911. 0.000 20.400 -7.319E-05 877177. -11339. -0.000542 0.000 5.897E+100.2475 16229. 0.000 20.800 -0.002503 823361. -11317. -0.000473 0.000 5.898E+108.6273 16547. 0.000 21.200 -0.004610 769664. -11258. -0.000408 0.000 5.899E+1016.1992 16866. 0.000 21.600 -0.006417 716265. -11164. -0.000347 0.000 5.900E+1022.9744 17184. 0.000 22.000 -0.007945 663326. -11039. -0.000291 0.000 5.901E+1028.9694 17502. 0.000 22.400 -0.009213 610989. -10887. -0.000239 0.000 5.902E+10

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24new.lp6o34.2053 17820. 0.000 22.800 -0.0102 559381. -10712. -0.000192 0.000 5.902E+1038.7081 18139. 0.000 23.200 -0.0111 508610. -10415. -0.000148 0.000 5.903E+1085.3743 37069. 0.000 23.600 -0.0117 459756. -9989.3225 -0.000109 0.000 5.904E+1091.8562 37788. 0.000 24.000 -0.0121 412974. -9535.8698 -7.355E-05 0.000 5.904E+1097.0824 38507. 0.000 24.400 -0.0124 368388. -9060.1805 -4.179E-05 0.000 5.905E+10101.1214 39226. 0.000 24.800 -0.0125 326097. -8567.7790 -1.357E-05 0.000 5.905E+10104.0459 39944. 0.000 25.200 -0.0125 286170. -8063.8348 1.132E-05 0.000 5.905E+10105.9309 40663. 0.000 25.600 -0.0124 248657. -7553.1516 3.306E-05 0.000 5.905E+10106.8538 41382. 0.000 26.000 -0.0122 213581. -7040.1599 5.184E-05 0.000 5.905E+10106.8927 42101. 0.000 26.400 -0.0119 180947. -6528.9142 6.788E-05 0.000 5.906E+10106.1263 42820. 0.000 26.800 -0.0115 150740. -6023.0931 8.135E-05 0.000 5.906E+10104.6325 43539. 0.000 27.200 -0.0111 122930. -5526.0030 9.248E-05 0.000 5.906E+10102.4884 44257. 0.000 27.600 -0.0106 97469. -5040.5852 0.000101 0.000 5.906E+1099.7690 44976. 0.000 28.000 -0.0101 74297. -4569.4253 0.000108 0.000 5.906E+1096.5476 45695. 0.000 28.400 -0.009607 53342. -4114.7645 0.000114 0.000 5.906E+1092.8944 46414. 0.000 28.800 -0.009051 34522. -3678.5141 0.000117 0.000 5.906E+1088.8766 47133. 0.000 29.200 -0.008482 17747. -3262.2706 0.000119 0.000 5.906E+1084.5581 47852. 0.000 29.600 -0.007906 2918.2244 -2867.3331 0.000120 0.000 5.906E+1079.9992 48570. 0.000 30.000 -0.007329 -10068. -2474.9307 0.000120 0.000 5.906E+1083.5018 54690. 0.000 30.400 -0.006755 -21129. -2068.9501 0.000119 0.000 5.906E+1085.6567 60862. 0.000 30.800 -0.006190 -30214. -1672.3111 0.000116 0.000 5.906E+1079.6095 61729. 0.000 31.200 -0.005637 -37462. -1304.8193 0.000114 0.000 5.906E+1073.5121 62595. 0.000 31.600 -0.005099 -43013. -966.6109 0.000110 0.000 5.906E+1067.4081 63461. 0.000 32.000 -0.004577 -47007. -657.6284 0.000107 0.000 5.906E+1061.3346 64328. 0.000 32.400 -0.004073 -49583. -377.6533 0.000103 0.000 5.906E+1055.3217 65194. 0.000 32.800 -0.003589 -50879. -126.3370 9.880E-05 0.000 5.906E+1049.3934 66061. 0.000 33.200 -0.003125 -51033. 96.7676 9.466E-05 0.000 5.906E+1043.5669 66927. 0.000 33.600 -0.002680 -50178. 292.1781 9.055E-05 0.000 5.906E+1037.8541 67793. 0.000 34.000 -0.002255 -48445. 460.4539 8.654E-05 0.000 5.906E+1032.2608 68660. 0.000 34.400 -0.001849 -45965. 602.1709 8.270E-05 0.000 5.906E+1026.7879 69526. 0.000 34.800 -0.001461 -42863. 717.8976 7.909E-05 0.000 5.906E+1021.4315 70393. 0.000

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24new.lp6o 35.200 -0.001090 -39263. 808.1729 7.576E-05 0.000 5.906E+1016.1832 71259. 0.000 35.600 -0.000734 -35286. 873.4872 7.273E-05 0.000 5.906E+1011.0311 72125. 0.000 36.000 -0.000392 -31052. 914.2652 7.003E-05 0.000 5.906E+105.9598 72992. 0.000 36.400 -6.183E-05 -26678. 930.8518 6.769E-05 0.000 5.906E+100.9513 73858. 0.000 36.800 0.000258 -22278. 923.5006 6.570E-05 0.000 5.906E+10-4.0143 74725. 0.000 37.200 0.000569 -17970. 892.3662 6.406E-05 0.000 5.906E+10-8.9584 75591. 0.000 37.600 0.000873 -13865. 837.4985 6.277E-05 0.000 5.906E+10-13.9031 76457. 0.000 38.000 0.001171 -10080. 758.8419 6.179E-05 0.000 5.906E+10-18.8705 77324. 0.000 38.400 0.001466 -6728.8400 656.2372 6.111E-05 0.000 5.906E+10-23.8815 78190. 0.000 38.800 0.001758 -3927.0205 529.4280 6.068E-05 0.000 5.906E+10-28.9557 79057. 0.000 39.200 0.002049 -1791.9569 378.0709 6.044E-05 0.000 5.906E+10-34.1098 79923. 0.000 39.600 0.002338 -442.6078 201.7507 6.035E-05 0.000 5.906E+10-39.3570 80789. 0.000 40.000 0.002628 0.000 0.000 6.034E-05 0.000 5.906E+10-44.7058 40828. 0.000

* This analysis makes computations of pile response using nonlinear moment-curvaturerelationships. The above values of total stress are computed for combined axial and bending stress in elastic sections and do not equal actual stresses in concrete and steel in the range of nonlinear bending.

Output Summary for Load Case No. 6:

Pile-head deflection = 0.7500000 inchesComputed slope at pile head = -0.0000426 radiansMaximum bending moment = -3585322. inch-lbsMaximum shear force = 57559. lbsDepth of maximum bending moment = 0.000000 inches below pile headDepth of maximum shear force = 0.000000 inches below pile headNumber of iterations = 24Number of zero deflection points = 2

-------------------------------------------------------------------------------- Summary of Pile Response(s)--------------------------------------------------------------------------------

Definitions of Pile-head Loading Conditions:

Load Type 1: Load 1 = Shear, lbs, and Load 2 = Moment, in-lbsLoad Type 2: Load 1 = Shear, lbs, and Load 2 = Slope, radiansLoad Type 3: Load 1 = Shear, lbs, and Load 2 = Rotational Stiffness, in-lbs/radianLoad Type 4: Load 1 = Top Deflection, inches, and Load 2 = Moment, in-lbsLoad Type 5: Load 1 = Top Deflection, inches, and Load 2 = Slope, radians

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24new.lp6o Pile-head Pile-head Maximum MaximumLoad Load Condition 1 Condition 2 Axial Pile-head Moment Shear Pile-headCase Type V(lbs) or in-lb, rad., Loading Deflection in Pile in Pile Rotation No. No. y(inches) or in-lb/rad. lbs inches in-lbs lbs radians---- ---- -------------- -------------- ------------- -------------------------- ------------- ------------- 1 4 y = 0.2500 M = 0.000 250000. 0.25000000670552. 9780.5455 -0.00198675 2 4 y = 0.5000 M = 0.000 250000. 0.500000001294143. 19050. -0.00401451 3 4 y = 0.7500 M = 0.000 250000. 0.750000001695876. 25874. -0.00627892 4 5 y = 0.2500 S = 0.000 250000. 0.25000000-1807120. 24268. -0.00000798 5 5 y = 0.5000 S = 0.000 250000. 0.50000000-2815732. 42628. -0.00002306 6 5 y = 0.7500 S = 0.000 250000. 0.75000000-3585322. 57559. -0.00004265

The analysis ended normally.

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Geotechnical Investigation Report

Project number: 60561395

Prepared for: City of Santa Monica AECOM

81 kg 81 kg

211

kg 211

kg

274

kg 274

kg

215

kg 215

kg

71 kg 71 kg

UP

90

DI

SCO

SCO

S

D

FDC

FDC

PIV

E

E

DI

DN

UPUP

(E) SOUTH SUPPORT BUILDING

122'-3"

2

AS001

RED BAG STORAGE

64'-0"

3

AS001

SERVICE

ROAD

7

AS0121

3

9

10

TRASH COMPACTOR

9

4

4

5

6

8

NEW LAB BUILDING

2 2 2 9

1

NEW

STORAGE

BUILDING

DEMOLITION CONCEPTUAL LIMITS

Clinical Lab and Red Bag Storage Area

Willowbrook, California

Figure 1

Geotechnical Investigation

Martin Luther King Jr. Medical Campus

LEGEND

Proposed Building Layout

Existing Building LayoutArea 3: Sump Location

2

Area 2: Complete Demolition

Area 1: Partial Demolition

1

Note:

1

Depth of demolition to approximately 6 feet below

adjacent grade and to be finalized upon field

verification by contractor & review by Engineer.

2

Field verification by contractor & review by

Engineer required before demolition.

· Backfill requirements per Geotechnical Report.

· Limits are for information only.

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6"TREE
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