B757-200PCF ASL AIRLINES BELGIUM (ASLB) LOW …Unpublished Work . THIS INFORMATION CONTAINED HEREIN IS PROPRIETARY TO PRECISION . CONVERSIONS, LLC, AND SHALL NOT BE REPRODUCED OR DISCLOSED

B757-200PCF ASL AIRLINES BELGIUM (ASLB) LOW UTILIZATION MAINTENANCE PROGRAM (LUMP) SUPPLEMENT

PC-0118-351

Original Issue: Rev IR (5th May 2017)

Compiled and Published by: Precision Conversions, LLC

4900 SW Griffith Drive, Suite 133 Beaverton, Oregon 97005

PRECISION CONVERSIONS CONFIDENTIAL, AND/OR TRADE SECRET

Copyright © 2004 Precision Conversions Unpublished Work – All Rights Reserved

THIS INFORMATION CONTAINED HEREIN IS PROPRIETARY TO PRECISION CONVERSIONS, LLC, AND SHALL NOT BE REPRODUCED OR DISCLOSED IN WHOLE OR IN PART OR USED FOR ANY DESIGN OR MANUFACTURE EXCEPT WHEN SUCH USER POSSESSES DIRECT, WRITTEN AUTHORIZATION FROM PRECISION CONVERSIONS, LLC.

ASLB Low Utilization Maintenance Program Supplement Aircraft Utilization Parameter: 1200 Flight Hours/Year

PC-0118-351 Rev IR PRECISION CONVERSIONS LLC PROPRIETARY INFORMATION. SEE FRONT SHEET FOR FULL DISCLOSURE STATEMENT Page 2

A. Introduction

1. This ASLB Low Utilization Maintenance Program (LUMP) Supplement is to be used in conjunction with the Precision PC-0118-05 Maintenance Planning Document Supplement. It is not a stand-alone maintenance program. It describes only task interval changes that may be made to certain items in the Precision MPD Supplement under a low-utilization maintenance program.

2. This ASLB LUMP Supplement is specifically designed for ASL Airlines Belgium, based on anticipated annual aircraft utilization of 1200 flight hours/year.

3. This ASLB LUMP Supplement is usage limited for ASL Airlines Belgium airplanes, converted to the freighter configuration per Precision Conversions STC ST01529SE.

B. ASL LUMP Supplement Development

The following guidelines were applied to develop the ASLB Low Utilization Maintenance Program (LUMP) Supplement.

1. For OEM tasks, the Boeing LUMP intervals are assumed to be applicable.

2. For Conversion-Added tasks, interval escalation substantiation is completed.

3. Intervals for Section 9 Supplement related tasks such as Certification Maintenance Requirements (CMR) and Airworthiness Limitation (AWL) tasks will remain at MPD Supplement recommended intervals.

4. Precision MPD Supplement tasks not listed in this document continue to apply as published in the latest revision of the Precision MPD Supplement.

C. Reference Documents

The ASLB LUMP Supplement was developed based on the following documents:

1. Boeing Low Utilization Maintenance Program (LUMP) TNT Airways (TNB) B757-28A (S/N: 25622) (10 May 2012)

2. Precision Maintenance Planning Data Document Supplement (PC-0118-05, Rev Feb 23, 2017)

3. Precision Supplemental Maintenance Manual for B757-200 Cargo Conversion (PC-0118-06 Rev N, Dec 23, 2015 and Temporary Revisions 44 - 56)

4. Precision Smoke Detection and Penetration Ground Test Plan and Results (PC-0118-26 Rev A, Jan 3, 2005)

5. Precision System Safety Analysis of Crew Entry Door (PC-0118-48 Rev B, Dec 18, 2012)

6. Precision System Safety Analysis of Flight Deck Window (PC-0118-49 Rev D, Aug 1, 2016)

7. Precision Mechanical System Substantiation Report/System Safety Analysis of Environmental Control Systems (PC-0118-54 Rev C, Sep 12, 2007)



D. Interval Escalation Substantiation

OEM Tasks:

For the following OEM tasks changed due to the conversion, the Boeing TNT LUMP intervals are assumed to be applicable, except as noted in the Interval Escalation table.

Section 1 Systems Section 2 Structures Section 3 Zonal PC-21-003-00 PC-52-414-00 PC-52-816-00 PC-21-025-00 PC-53-102-00 PC-52-818-00 PC-21-026-00 PC-53-106-00 PC-52-822-00 PC-21-030-01 PC-53-118-00 PC-52-828-00 PC-23-001-00 PC-53-236-00 PC-52-830-00 PC-23-005-02 PC-52-832-00 PC-27-001-05 PC-52-834-00 PC-31-001-02 PC-52-840-00 PC-31-002-00 PC-52-842-00 PC-31-007-01 PC-52-846-00 PC-32-001-05 PC-53-858-20 PC-33-007-01 PC-53-860-10 PC-35-005-00 PC-53-862-10 PC-35-015-01 PC-53-864-00 PC-52-005-00 PC-53-866-00 PC-52-005-01 PC-53-870-00

PC-53-874-10

Section 1 Systems Interval Escalation Substantiation PC-52-005-03 Boeing TNT LUMP interval is 16 MO for PASS airplanes (No. 2 doors operational). The No. 2 doors are

deactivated on 757PCF. PC MPD gives an interval of 6000 FH/18 MO, same as No. 2 door locking mechanism lubricate task PC-52-005-01. PC-52-005-01 LUMP interval is 24 MO. Since tasks are similar and intervals are based on experience, the same interval will be applied to PC-52-005-03.



D. Interval Escalation Substantiation (cont’d)

Conversion-Added Tasks:

Section 1 Systems Interval Escalation Substantiation PC-21-2000-00 Similar to task 21-002-00 from Boeing TNT LUMP. Boeing TNT LUMP interval applicable.

PC-21-2004-00 PC-0118-54 SSA of Environmental Control Systems has no restrictions to calendar time. Therefore threshold can be converted using utilization parameters.




PC-25-2000-00 PC AMM 25-11-00/1 states there are no changes to the remove/install procedure except for relocation of the seat from the passenger compartment to the flight compartment. Therefore inspection interval should be same as for passenger seats: 25-001-00 / 25-002-00 / 25-005-00 in Boeing TNT LUMP.

PC-26-2010-00 There is no calendar time restriction. Intervals are converted to calendar time by taking into account utilization parameters. Precision references 4 and 7.

PC-26-2014-00 There is no calendar time restriction. Intervals are converted to calendar time by taking into account utilization parameters. Precision references 4 and 7.

PC-26-2016-00 There is no calendar time restriction. Intervals are converted to calendar time by taking into account utilization parameters. References 4 and 7.



PC-52-2000-00 Similar to Boeing TNT LUMP tasks: 52-005-01; 52-005-06; 52-013-00. Original MPD Interval = 6000 FH / 18 MO converted to 24 MO in Boeing TNT LUMP document. Since tasks are similar and intervals are based on experience, it is acceptable to use same interval for PC task.



Section 1 Systems Interval Escalation Substantiation PC-52-2002-00 Similar to Boeing TNT LUMP tasks: 52-005-01; 52-005-06; 52-013-00. Original MPD Interval = 6000

FH / 18 MO converted to 24 MO in Boeing TNT LUMP document. Since tasks are similar and intervals are based on experience, it is acceptable to use same interval for PC task.












Section 1 Systems Interval Escalation Substantiation PC-52-2022-00 Similar to Boeing TNT LUMP tasks: 52-005-01; 52-005-06; 52-013-00. Original MPD Interval = 6000

FH / 18 MO converted to 24 MO in Boeing TNT LUMP document. Since tasks are similar and intervals are based on experience, it is acceptable to use same interval for PC task.

PC-52-2068-00 Per PC-0118-48 SSA of Crew Entry Door. Any failure will be detected during door operational test/inspection every 5000 cycles. No restrictions to calendar length are applied. Therefore calendar interval can be set 24 MO.

PC-52-2070-00 Per PC-0118-48 SSA of Crew Entry Door. Any failure will be detected during door operational test/inspection every 5000 cycles. No restrictions to calendar length are applied. Therefore, calendar interval can be set to 24 MO.

PC-56-2000-00 Per PC-0118-49 SSA of Flight Deck Window. Any failure will be detected during door operational test/inspection every 5000 cycles. No restrictions to calendar length are applied. Therefore, calendar interval can be set to 24 MO.

Section 2 Structures Interval Escalation Substantiation PC-52-1204-00 Task is similar to Boeing package freighter task 52-444-00. Boeing MPD interval is 375 FC. In the

Boeing TNT LUMP document, this interval is escalated to 4 MO.

PC-52-1252-00 Task is similar to Boeing package freighter task 52-452-00. Boeing MPD interval is 375 FC. In the Boeing TNT LUMP document, this interval is escalated to 4 MO.

Section 3 Zonal Interval Escalation Substantiation No conversion-added tasks in Precision MPD Supplement.

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REVISION LOG

REV LEVEL DESCRIPTION

RevlR ASLB Low Utilization Maintenance Program (LUMP) Supplement

PC-0118-351


APPROVAL DATE

~ ~-- ~ 65-31-1( .._ -

RevlR PRECISION CONVERSIONS LLC PROPRIETARY INFORMATION. SEE FRONT SHEET FOR FULL DISCLOSURE STATEMENT Page 7



Section 1: Systems and Powerplant Maintenance Requirements

SEC MPD ITEM NUMBER

AMM REFERENCE

C A T

T A S K

LUMP INTERVAL

THRES REPEAT ZONE ACCESS

APPLICABILITY

APL ENG MAN

HOURS TASK DESCRIPTION

ATA 21: AIR CONDITIONING

1 PC-21-003-00 6 DIS 16 MO 16 MO NOTE NOTE PCF NOTE

ALL 0.60 Change recirculation air prefilter (left side only). ACCESS NOTE: Task is the same as OEM maintenance manual 21-003-00, but right recirculation fan is deleted. AIRPLANE NOTE: If installed.

1 PC-21-025-00 6 DIS 12 MO 12 MO NOTE NOTE PCF ALL 0.40 Change cabin zone temperature sensor filters. ZONE/ACCESS NOTE: Component has been relocated, but procedure is the same as passenger aircraft. See PC AMM 21-61-11/401 for new location. See OEM maintenance manual 21-61-11/401 for procedure.

1 PC-21-026-00 9 FNC 96 MO 96 MO NOTE NOTE PCF ALL 0.40 Check (off-aircraft) switch setting of zone duct overheat switches and circuit verification. ZONE/ACCESS NOTE: Component has been relocated, but procedure is the same as passenger aircraft. See PC AMM 21-61-01/1 for new location. See OEM maintenance manual 21-61-01/501 for procedure.

1 PC-21-030-01 9 OPC 4 MO 4 MO NOTE NOTE PCF ALL 0.30 Check operation of E/E cooling smoke/low flow detection system with test switch. AIRPLANE NOTE: Right side recirculation system is deactivated. This task does not require pushing R RECIRC FAN switch-light.

1 PC-21-2000-00 7 RST 24 MO 24 MO NOTE NOTE PCF ALL 3.00 Clean return air grilles in the cargo compartment. ACCESS NOTE: Remove return air grilles.

1 PC-21-2004-00 VCK 24 MO 24 MO NOTE NOTE PCF ALL 0.50 Visually check flight deck lavatory vent duct for condition ZONE/ACCESS NOTE: see PC AMM 21-58-00 for component location.




SEC MPD ITEM NUMBER

AMM REFERENCE

C A T

T A S K

LUMP INTERVAL


APPLICABILITY

APL ENG MAN



1 PC-21-2006-00 VCK 24 MO 24 MO NOTE NOTE PCF ALL 0.50 Visually check alternate forward equipment cooling duct for condition. ZONE/ACCESS NOTE: see PC AMM 21-58-00 for component location.




SEC MPD ITEM NUMBER

AMM REFERENCE

C A T

T A S K

LUMP INTERVAL


APPLICABILITY

APL ENG MAN



1 PC-21-2008-00 VCK 24 MO 24 MO NOTE NOTE PCF ALL 0.50 Visually check main deck riser duct restrictor plate for condition. ZONE/ACCESS NOTE: see PC AMM 21-58-00 for component location.

1 PC-21-2012-00 VCK 24 MO 24 MO NOTE NOTE PCF ALL 0.50 Visually check mix manifold riser duct caps (2) for condition. ZONE/ACCESS NOTE: see PC AMM 21-58-00 for component location.

ATA 23: COMMUNICATIONS

1 PC-23-001-00 9 OPC 48 MO 48 MO NOTE NOTE PCF ALL 0.50 Operationally check lavatory address speaker. ZONE/ACCESS NOTE: Component has been relocated, but procedure is the same as passenger aircraft. See PC AMM 23-31-00/1 for new location. See OEM maintenance manual 23-31-00/501 for procedure.

1 PC-23-005-02 9 OPC 24 MO 24 MO NOTE NOTE PCF ALL 0.50 Operationally check the voice recorder Underwater Locator Beacon (ULB). ZONE/ACCESS NOTE: Component has been relocated, but procedure is the same as passenger aircraft. See PC AMM 23-71-00/1 for new location. See OEM maintenance manual 23-71-03/201 for procedure.

ATA 25: EQUIPMENT AND FURNISHINGS

1 PC-25-2000-00 8 OPC 24 MO 24 MO NOTE NOTE PCF ALL 0.10 Check supernumerary seat restraint attachment (and inertia reel if installed). ZONE/ACCESS NOTE: Double attendant seat has been relocated to flight compartment and is referred to as supernumerary seat. See PC AMM 25-11-00/1 for new location. See OEM maintenance manual 25-25-02/401 for procedure




SEC MPD ITEM NUMBER

AMM REFERENCE

C A T

T A S K

LUMP INTERVAL


APPLICABILITY

APL ENG MAN


ATA 26: FIRE PROTECTION

1 PC-26-2010-00 GVI 6 MO 6 MO NOTE NOTE PCF ALL Perform a GVI inspection of detectors for cleanliness. If cleaning required, remove detectors from airplane as per PC AMM 26-10-00. Service detectors as per component maintenance manual. Reinstall detectors. ZONE/ACCESS NOTE: See PC AMM 26-10-00 for component locations.

1 PC-26-2014-00 FNC 8 MO 8 MO NOTE NOTE PCF ALL Perform a functional check of the smoke detectors using the CFMU test switch as per PC AMM 26-10-00. ZONE/ACCESS NOTE: CFMU panel located in E/E bay

1 PC-26-2016-00 GVI 72 MO 72 MO NOTE NOTE PCF ALL Perform a general visual inspection of the FiDS system identification placards. ZONE/ACCESS NOTE: placards are located in the E/E bay for the CFMU and at each smoke detector. NOTE: Task satisfied by E/E zonal and cabin zonal inspections.

1 PC-26-2018-00 DET 72 MO 72 MO NOTE NOTE PCF ALL Perform a detailed inspection of the smoke detector units, visible wiring, pans and attachment hardware for damage. NOTE: With detector pan removed. ZONE/ACCESS NOTE: See PC AMM 26-10-00 for component location

1 PC-26-2020-00 GVI 96 MO 96 MO NOTE NOTE PCF ALL Perform a general visual inspection of the FiDS system wiring. ZONE/ACCESS NOTE: Main deck cargo compartment and E/E compartment. NOTE: Task satisfied by interior E/E zonal and cabin zonal inspections.




SEC MPD ITEM NUMBER

AMM REFERENCE

C A T

T A S K

LUMP INTERVAL


APPLICABILITY

APL ENG MAN


ATA 27: FLIGHT CONTROLS

1 PC-27-001-05 9 DET 48 MO 48 MO 118 119BL PCF ALL 1.00 Detailed visual inspection of flight control cables under galleys and lavatories for wear, broken strands, corrosion, kinks and bird caging. Check end fittings, turnbuckles, pulleys, brackets, fairleads and quadrants for wear, corrosion, cracks and security

ATA 31: INDICATING/RECORDING SYSTEMS

1 PC-31-001-02 9 OPC 24 MO 24 MO NOTE NOTE PCF ALL 0.50

Operationally check the digital flight data recorder Underwater Locator Beacon (ULB). ZONE/ACCESS NOTE: Component has been relocated, but procedure is the same as passenger aircraft. See PC AMM 31-31-00/1 for new location. See OEM maintenance manual 31-31-02/201 for procedure.

1 PC-31-002-00 9 OPC 24 MO 24 MO NOTE NOTE PCF ALL 0.50 Verify all required aircraft parameters are recorded properly on the flight data recorder. ZONE/ACCESS NOTE: Component has been relocated, but procedure is the same as passenger aircraft. See PC AMM 31-31-00/1 for new location. See OEM maintenance manual 31-31-01/201 for procedure.

1 PC-31-007-01 OPC 24 MO 24 MO NOTE NOTE PCF ALL 2.00 Check take-off configuration warning system. NOTE: Task is the same as in OEM Maintenance Manual EXCEPT: For PCF aircraft, prior to procedure, ensure main deck cargo door (MDCD) is closed.




SEC MPD ITEM NUMBER

AMM REFERENCE

C A T

T A S K

LUMP INTERVAL


APPLICABILITY

APL ENG MAN


ATA 32: LANDING GEAR

1 PC-32-001-05 9 DET 48 MO 48 MO 118 119BL PCF ALL 0.25 Detailed visual inspection of landing gear cables under galleys and lavatories for wear, broken strands, corrosion, kinks and bird caging. Check end fittings, turnbuckles, pulleys, brackets, fairleads and quadrants for wear, corrosion, cracks, and security. AIRPLANE NOTE: 10% of operator’s fleet.

ATA 33: LIGHTS

1 PC-33-007-01 OPC 4 MO 4MO 200 PCF ALL 0.50 Operationally check emergency lights using pilot’s control switch.




SEC MPD ITEM NUMBER

AMM REFERENCE

C A T

T A S K

LUMP INTERVAL


APPLICABILITY

APL ENG MAN


ATA 35: OXYGEN

1 PC-35-005-00 6 DET 24 MO 24 MO 211 212

PCF ALL 0.50 Visually check crew/supernumerary oxygen mask/regulator assembly for condition and verify operation of crew mask microphone, if present.

1 PC-35-015-01 OPC 16 MO 16 MO 211 212

PCF ALL 0.60 Operationally check the crew/supernumerary oxygen mask/regulator.

ATA 52: DOORS

1 PC-52-005-00 6 LUB 48 MO 48 MO 832 842

231AL 232AR

PCF ALL 0.20 Lubricate the No. 2 left and right passenger doors hinge mechanism. Some airplanes may not have lube points on lower hinge(s). NOTE: No. 2 doors are deactivated.

1 PC-52-005-01 6 LUB 24 MO 24 MO 832 842

231AL 232AR 8321 8421

PCF ALL 0.40 Lubricate the No. 2 left and right passenger doors hinge torque tubes (Door and Body). NOTE: No. 2 doors are deactivated.

1 PC-52-005-03 LUB 24 MO 24MO 832 842

231AL 232AR

PCF ALL 0.30 Lubricate the No. 2 left and right passenger door rollers and latch crank bearings.

NOTE: No. 2 doors are deactivated.

1 PC-52-2000-00 LUB 24 MO 24 MO 837 837 PCF ALL 0.20 Lubricate crew entry door latch rods.

1 PC-52-2002-00 LUB 24 MO 24 MO 837 837 PCF ALL 0.20 Lubricate crew entry door handle connecting rod.

1 PC-52-2004-00 LUB 24 MO 24 MO 837 837 PCF ALL 0.20 Lubricate crew entry door outer latch yoke bearing.

1 PC-52-2006-00 LUB 24 MO 24 MO 837 837 PCF ALL 0.20 Lubricate crew entry door hinge.

1 PC-52-2008-00 LUB 24 MO 24 MO 838 838 PCF ALL 0.20 Lubricate main cargo door hinges. 1 PC-52-2010-00 LUB 24 MO 24 MO 838 838 PCF ALL 0.20 Lubricate main cargo door lift actuator. 1 PC-52-2012-00 LUB 24 MO 24 MO 838 838 PCF ALL 0.20 Lubricate main cargo door link assemblies. 1 PC-52-2014-00 LUB 24 MO 24 MO 838 838 PCF ALL 0.20 Lubricate main cargo door micro switches.




SEC MPD ITEM NUMBER

AMM REFERENCE

C A T

T A S K

LUMP INTERVAL


APPLICABILITY

APL ENG MAN


ATA 52: DOORS

1 PC-52-2016-00 LUB 24 MO 24 MO 838 838 PCF ALL 0.20 Lubricate main cargo door latch assemblies.

1 PC-52-2018-00 LUB 24 MO 24 MO 838 838 PCF ALL 0.20 Lubricate main cargo door latch spools.

1 PC-52-2020-00 LUB 24 MO 24 MO 838 838 PCF ALL 0.20 Lubricate main cargo door locking mechanism gang bar.

1 PC-52-2022-00 LUB 24 MO 24 MO 838 838 PCF ALL 0.20 Lubricate main cargo door vent door. 1 PC-52-2068-00 OPC 24 MO 24 MO 830 830 PCF ALL 0.10 Operationally test latch/lock system of crew

entry door.

1 PC-52-2070-00 OPC 24 MO 24 MO 830 830 PCF ALL 0.10 Operationally test crew entry door.

ATA 56: WINDOWS

1 PC-56-2000-00 OPC 24 MO 24 MO NOTE NOTE PCF ALL Operationally check the No. 2 right-hand flight deck window external opening mechanism. ZONE/ACCESS NOTE: See PC AMM 56-11-04/1 to locate external opening mechanism.



Section 2: Structural Maintenance Requirements

SEC MPD ITEM NUMBER

AMM REF PGM ZONE ACCESS

LUMP INTERVAL APPLICABILITY MAN HOURS TASK DESCRIPTION

THRES REPEAT APL ENG

ATA 52: DOORS

2 PC-52-414-00 S 832 842

NOTE 4 MO 4 MO PCF ALL 0.10 EXTERNAL – GENERAL VISUAL: Passenger Door Exterior. Passenger door external skin. ACCESS NOTE: As viewed from the ground.

2 PC-52-1204-00 S 837 NOTE 4 MO 4 MO PCF ALL 0.20 EXTERNAL - GENERAL VISUAL: Crew entry door, external skin, frames and stops. ACCESS NOTE: As viewed from the airplane.

2 PC-52-1252-00 S 838 NOTE 4 MO 4 MO PCF ALL 0.20 EXTERNAL - GENERAL VISUAL: Main deck cargo door, external skin, frames and stops. ACCESS NOTE: As viewed from the airplane.

ATA 53: FUSELAGE

2 PC-53-102-00 S 118 119BL 48 MO 48 MO PCF ALL 1.00 INTERNAL - DETAILED: Floor Beams and Seat Tracks Floor beams and seat tracks immediately below and adjacent to galleys and lavatories if installed.

2 PC-53-106-00 S 100 113AL 119BL

821/822 823

832/833 834/835 842/843 844/845

24 MO 24 MO PCF ALL 3.00 EXTERNAL - DETAILED: Door stops and adjacent visible cutout structure within aircraft contour at all body openings (passenger, cargo, emergency, including overwing escape; and Section 41 access and electronic equipment doors).

2 PC-53-118-00 S 118 48 MO 48 MO PCF ALL 0.10 INTERNAL - DETAILED: No. 1 passenger door lower sills.



Section 2: Structural Maintenance Requirements

SEC MPD ITEM NUMBER

AMM REF PGM ZONE ACCESS

LUMP INTERVAL APPLICABILITY MAN HOURS TASK DESCRIPTION

THRES REPEAT APL ENG

ATA 53: FUSELAGE

2 PC-53-236-00 S 837 838

NOTE 4 MO 4 MO PCF ALL 0.25 EXTERNAL – GENERAL VISUAL: Upper lobe skin body external skin including door cutouts and stops. ACCESS NOTE: As viewed from the ground.



Section 3: Zonal Inspection Requirements

SEC MPD ITEM NUMBER

AMM REF ZONE ACCESS

LUMP INTERVAL

THRES REPEAT

APPLICABILITY

APL ENG MAN


ATA 52: DOORS

3 PC-52-816-00 832 24 MO 24 MO PCF ALL 0.40 EXTERNAL - ZONAL (GV): No. 2 Door - Entry Perform External General Visual Inspection of the zone with the door closed. CPC NOTE: Corrosion Prevention and Control Basic Task Required. TASK NOTE: The No. 2 doors are deactivated.

3 PC-52-818-00 832 96 MO 96 MO PCF ALL 0.50 INTERNAL - ZONAL (GV): No. 2 Door - Entry Perform Internal General Visual Inspection of the zone with the door closed. TASK NOTE: The No. 2 doors are deactivated.

3 PC-52-822-00 835 96 MO 96 MO PCF ALL 0.50 INTERNAL - ZONAL (GV): No. 3 Doors – Emergency Exit Perform an Internal General Visual Inspection of the zone with the door closed. TASK NOTE: The No. 3 doors are deactivated.

3 PC-52-828-00 837 24 MO 24 MO PCF ALL 0.40 EXTERNAL - ZONAL (GV): Crew Entry Door Perform an External General Visual Inspection of the zone with the door closed. CPC NOTE: Corrosion Prevention and Control Basic Task Required.

3 PC-52-830-00 837 96 MO 96 MO PCF ALL 0.70 INTERNAL - ZONAL (GV): Crew Entry Door Perform Internal General Visual Inspection of the zone with the door closed.

3 PC-52-832-00 838 24 MO 24 MO PCF ALL 0.80 EXTERNAL - ZONAL (GV): Main Deck Cargo Door Perform an External General Visual Inspection of the zone with the door closed. CPC NOTE: Corrosion Prevention and Control Basic Task Required.




SEC MPD ITEM NUMBER

AMM REF ZONE ACCESS

LUMP INTERVAL

THRES REPEAT

APPLICABILITY

APL ENG MAN


ATA 52: DOORS

3 PC-52-834-00 838 96 MO 96 MO PCF ALL 1.40 INTERNAL - ZONAL (GV): Main Deck Cargo Door Perform Internal General Visual Inspection of the zone with the door open.

3 PC-52-840-00 842 24 MO 24 MO PCF ALL 0.40 EXTERNAL - ZONAL (GV): No. 2 Door - Service Perform an External General Visual Inspection of the zone with the door closed. CPC NOTE: Corrosion Prevention and Control Basic Task Required. TASK NOTE: The No. 2 doors are deactivated.

3 PC-52-842-00 842 96 MO 96 MO PCF ALL 0.50 INTERNAL - ZONAL (GV): No. 2 Door - Service Perform Internal General Visual Inspection of the zone with the door closed. TASK NOTE: The No. 2 doors are deactivated.

3 PC-52-846-00 845 96 MO 96 MO PCF ALL 0.50 INTERNAL - ZONAL (GV): No. 3 Doors – Emergency Exit Perform Internal General Visual Inspection of the zone with the door closed. TASK NOTE: The No. 3 doors are deactivated.




SEC MPD ITEM NUMBER

AMM REF ZONE ACCESS

LUMP INTERVAL

THRES REPEAT

APPLICABILITY

APL ENG MAN


ATA 53: FUSELAGE

3 PC-53-858-20 221 96 MO 96 MO PCF ALL 0.40 INTERNAL - ZONAL (GV): Crew Entry Door - Section 41 Perform Internal General Visual Inspection of the crew entry door (Zone 837) operating mechanism in fuselage.

3 PC-53-860-10 223 224

96 MO 96 MO PCF ALL 1.00 INTERNAL - ZONAL (GV): Areas Above Ceiling – Section 41 Perform Internal General Visual Inspection of the zones. (EZAP) ACCESS NOTE: Between Body Station (BS) 297 and BS 440.

3 PC-53-862-10 231 232

96 MO 96 MO PCF ALL 0.70 INTERNAL - ZONAL (GV): Main Deck - Section 43 Perform Internal General Visual Inspection of No. 2 door (Zones 832/842) operating mechanism in fuselage area. TASK NOTE: The No. 2 doors are deactivated.

3 PC-53-864-00 231 233

24 MO 24 MO PCF ALL 0.70 INTERNAL - ZONAL (GV): Main Deck - Section 43 Perform Internal General Visual Inspection of main deck cargo door (Zone 838) operating mechanism in fuselage area.

3 PC-53-866-00 233 234

96 MO 96 MO PCF ALL 2.00 INTERNAL - ZONAL (GV): Areas Above Ceiling - Section 43 Perform Internal General Visual Inspection of the zones. (EZAP) ACCESS NOTE: Between Body Station (BS) 440 and BS 900.




SEC MPD ITEM NUMBER

AMM REF ZONE ACCESS

LUMP INTERVAL

THRES REPEAT

APPLICABILITY

APL ENG MAN


ATA 53: FUSELAGE

3 PC-53-870-00 243 244


3 PC-53-874-10 253 254
