MAINTENANCE/INSPECTION ENTRIES

25 MAINTENANCE/INSPECTION ENTRIES

~TEVENS AVIATION INC. GREENVILLE, SC

N800TS

1/3/2007

BB-1032 ACTT 8,857 .2 HM 359.0

FLIGHT CYCLES 7 ,826

Performed a Phase 1,2,3,4 /200 Hour Inspection using the Ray_theo~/Beech King Air_ 82?0 Maintenance Manual 200 Hour Phase Inspection Guide.Complied with 200 ho~r l~bncat1on items. Complied with an annual weight and pressure check of cabin and cockpit fire bottles.

~ ~ STEVENS AVIATION INC.

' .. GREENVILLE, SC

1/3/2007 N800TS SN BB-1032 ACTT 8857.2

HM 359 FLIGHT CYCLES 7826

AIRFRAME INSPECTIONS 102 Complied with annual wing bolt lube and annual wing spar cap inspection. 103 Complied with annual pilots fuel control panel and lower edge lighted panel inspection and copilots edge

lighted circuit breaker panel inspection. No defects noted at this time. 151 Complied with 24 month passenger shut off valve overhaul using new overhaul kit PIN 446-0102-1. Operational

and leak check satisfactory. 203 Complied with left and right engine 3600 hour isolator mount inspections. Within service limits at this time. NOTE: Complied with 200, 400, 600 and 800 hour lubrication items.

AIRWORTHINESS DIRECTIVES AND SERVICE BULLETINS 106 Complied with AD 2004-23-02 in accordance with SB 32-2102 R 7 detection and correction of cracks in

nose landing gear fork. No defects noted. I 08 SB 27-3038 Rudder torque shaft support bearing retention unit inspection previously complied with. 109 Complied with SB 27-3459 flight control gust lock inspection. Correct gust lock installed. 110 Complied with SB 28-2156 inspection of left and right fuel boost pumps. Check satisfactory. 111 Complied with SB 32-2220 inspection of nose gear steering link. No defects noted. 112 Complied with SB 35-3020 Puritan Bennett oxygen inspection. No defects noted. 113 Complied with SB 55-2254 Rl sealing of horizontal stabilizer and dorsal fin. 114 SB 55-2422 Rl Modification of rudder torque shaft PCW. 115 Repaired left wing upper fuel bay panel in accordance with AD89-19-04 and SB 2040R3. Installed new fuel tanks

PIN 101-381001-7 SIN 06-27081 and PIN 101-381001-1SIN06-26418. Installed using all new gaskets, seals and new fuel quantity pr~be kit P -5051-5 SIN 28>Jl318...y~~~~a;JST ,,

SA-0505

I I I I I


STEVENS AVIATION INC. GREENVILLE, SC N800TS SN BB-1032 ACTT 8857.2

HM 359 FLIGHT CYCLES 7826

COMPONENTS INSPECTED, TESTED OR CALIBRATED 104 Replaced EL T battery with a new battery PIN JE2- l 978-3 and inspected ELT in accordance with FAR

91.207(c)&(d). Battery expires 1-10-2008. MAINTENANCE EVENTS, PARTS REMOVED OR REPLACED

118 Repaired aft center floorboard. 120 Installed "INOP" placard on switch for deactivated brake deice system. 122 Replaced vent blower with an overhauled vent blower PIN 101-384176-1 SIN 1203 from Stevens Aviation Inc.

in Vandalia, OH CRS#VIB4368K on work order No. DAY 27082 dated Oct 09, 2006. Operational check satisfactory.

123 Replaced right bleed air pressure switch for bleed air fail light with a new switch PIN 90-380002 SIN 19311. Operational checks satisfactory.

124 Stop drilled crack and fabricated doubler for left aft upper stub wing inboard of nacel le from 2024T3 .032. Alodined, primed and installed doubler.

125 Removed No. 2 left and right aft facing seats. Adjusted right seat recline actuators. Replaced left seat inboard actuator with an overhauled actuator PIN 106-384001-3 SIN 30387 from Aviation Fabricators in Clinton, MO CRS# GVRR304K overhauled on work order No. 20636 dated 9/8/2006. Reinstalled seats. Operational check of both seats was satisfactory.

126 Installed new left seat belt placard PIN 101-384087-1. 127 Repositioned cabin door seal. 128 Replaced several rivets in left lower fairing outboard of nacelle with new rivets. I 30 Resealed loose section on left hand stub wing boot and touched up conductive cement. 131 Removed corrosion on belly between spar and a te . ated · ed and painted.

Page 2of4 J _ I J L

SA-0505

~-... STEVENS AVIATION INC.

' .. GREENVILLE, SC

1/3/2007

ACTT 8857.2 HM 359

FLIGHT CYCLES 7826 MAINTENANCE EVENTS, PARTS REMOVED OR REPLACED(CONT.)

N800TS SN BB-1032

133 Repositioned both wiper blades. 134 Serviced all landing gear struts to proper height with nitrogen. . 135 Inspected aft "No Smoking/Fasten Seat Belts" sign. Repaired wiring harness and replaced bulbs with new

bulbs PIN 1202-300. Operational check satisfactory. 136 Inspected coffee light and galley door light switch. Adjusted gal~ey door light switch and replaced Mapco

light socket terminals with new terminals. Operational check satisfactory. . · ,] 37 Disabled emergency lighting system. Optional equipment that dose not affect type design. 138 Adjusted right inboard flap rigging. Operational check satisfactory. I 39 Adjusted nose gear down lock tension. Operational check satisf~ctory. . 140 Removed left and right outboard fuel hinged panels and stop dnlled cracks. Fabncated 2 each doubler

repairs from 2024-T3 .040. Alodined, primed and installed doublers. 141 Resealed windshield hump seal" 142 Secured velcro and installed new velcro to left 3 radiant heat panels. 144 Resealed loose sealant on right outboard lower wing deice boot. Touched up conductive cement.

145 Installed velcro strips to #2 right seat lower cover. 149 Removed interior to gain access to left divider and removed partition. Removed " D" ~indow and. cleaned

and inspected frame. Inspected new "D" window PIN LAI 01-420081-9 SIN 1341 and mstalled with new seal PIN 101-384246-3. Reinstalled interior. Sealed outer part of"D" window.

152 Replaced right inboard gear doo tor hinge bra" ith w br et PIN 81-3705-1 08.

SA-0505

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REMARKS

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The aircraft and/or component identified on the reverse side was inspected in accordance with current FAA regulations and was found airworthy for return to service.

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Pertinent details on file at this agency under:

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FRAKES AVIATION Cleburne Municipal Airport CLEBURNE, TEXAS 76031

FOR

The aircraft and/or component identified on the reverse side was inspected in accordance with current FAA regulations and was found airworthy for return to service.

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1. Approving National Aviation Authority/Country:

FANUNITED STATES

AUTHORIZED RELEASE CERTIFICATE FAA FORM 8130-3, AIRWORTHINESS APPROVAL TAG

4.oRo•'"""o" Cessna Aircraft Company Cessna Parts Distribution Dept. 702

5800 E Pawnee, Wichita, KS 67218

3. FonnTrackingNumber:

911546

Part Number. Eligibil ity:' 10.Quantity: 11.SeriaVBatchNumbet: 12. StatusJWork:

22FH524 01 1 N/A New

~;~W~RTHINESS APPROVAL - PARTS. THIS FORM IS NOT AN EXPORT APPROVAL.

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14. Certifies the items Identified above were manufactured In conformity to:

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17. Name (Typed or Printed): 18. Date {m/dly):

KENNETH E. WYSOCKI .SR., DARF 01/26/2005 User/Installer Responsibilities

It is important to understand that the existence of this document alone does not automatic~lly cons Mute authority _to install the parV~mpo~ent/assem~ly. Where the user/installer performs work In accordance with the national regulations of an a 1 rworth~ness authority different than the a1rwo~mess autho_nty oft.he country specified ln Block 1, ii is essentia~ that the userflnstaller ensures that his/her airworthiness authonty accepts parts/components/assemblies from the a11worthmess authority of the country speafied in Block 1 , . . . . . . . Statements in Blocks 14 and 19 do not constitute installation certification. In all cases, aircraft maintenance records must contain an installation certification issued m accordance with the national regulations by the userflnstaller before the aircraft may be flown.

FAA Form 8130-3 (6-01) Installer must cross-check eligibility with applicable technical data. NSN: 0052-00-012-9005

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Part Number. Eligibility:• 10.Quantity: 11.Serial/BatchNumber: 12. Status.Work:

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Part Number. Eligibility:•

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10.Quantity; 11.Serial/BatchNumber:

1 N/A 12. SlatuSIWork;

13.Remarks:

17. Name (Typed or Printed):

ENNETH E. WYSOCKI SR., 18. Date{m/d/y):

ARF 01/26/2005 It is important to understand that the existence fth· d User/Installer Responsibilities

Whe~e th~ user/installer performs work in acco~an: =~ent almle does n~t automatic~lly constitute authority to install the parVcom onenUass

!~~~~ ~~ ~~~~~~ss~5;er,~~Jn~~ke 1userlinstaller ensu~e~8j;~~~:~~~1:;:n~:n~ns: 1~fh~h~e!~c~~~o;~~~rent tha~~he airwa;iness au~~~~-of the country Statements in_ Blocks 1~ and 19 do not COllStitute installation ce . . . . . mponen assemb!Jes from the airworthiness

accordance with the national regulations by the user/installer be%~~~~nai~~~ ~~6ea~~~ maintenance records must contain an installation certification issued in

FAA Form 8130-3 (6·01) Installer must cross-check eligibility with applicable technical data



FANUNITED STATES . _ . . . .. 1 f. n 4.o•o•NIZATIO• Cessna Airc_r-aft_ Company ;:;'Ye·',()/'\

Cessna Parts Distr1but1on Dept. 702 - C 5800 E Pawnee, Wichita, KS 67218

NSN· 0052-00-012-9005

3. FormTracklngNumber:

911546

5. WorkO..der/Contractllnvoice

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Part Number: Eligibility:' 10.Quantity: 11.SeriaVBatcllNumbet: 12. StatusJWork:

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;;RW~RTHINESS APPROVAL - PARTS. THIS FORM IS NOT AN EXPORT APPROVAL.

Ol,02,208,310,335,340,401,402,404,414,421,425,441,500,525,550,560

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17. Name (Typed or Printed): 18. Date (mfdly):

KENNETH E. WYSOCKI SR., DARF 01/26/2005 User/Installer Responsibilities

It is important to understand that the existence of this document alone does not automatically constitute authority to install the part/componenUassembly. Where the user/installer performs work in accordance with the national regulations of an airworthiness authority different than the airworthiness authority of the country specified in Block 1, it is essential that the userflnstaller ensures that his/her aiiworthiness authority accepts parts/components/assemblies from the aiiworthiness authority of the country specified in Block 1

Statements in Blocks 14 and 19 do not constitute installation certification. In all cases, aircraft maintenance records must contain an installation certification issued in accordance with the national regulations by the userflnsta!ler before the aircraft may be flown.

FAA Form 8130-3 (6-01) Installer must cross-check eligibility with applicable technical data. NSN 0052-00-012-9005

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17. Name (Typed or Printed): 18. Date (m/dfy):

KENNETH E. WYSOCKI SR., DARF 01/26/2005 User/Installer Responsibilities

It is important to understand that the existence of this document alone does not automatically constitute auth~rity ~o install the part/~mpo~enUassemb_ly. · ark· rdance with the national regulations of an airworthiness authority different than the a11Worthmess autho_nty of l_he country

~'::~;~~n u~~~1~~~i1i~; ~~~:i ~at~~ au1:flnstal\er ensures that his/her aiiworthiness authority accepts parts/components/assemblies from the a1iworthmess

~::~Zn: ~es~:1~s~::~~~d~~ ~~~~slitute installation certification._ln all cases, aircraft maintenance records must contain an installation certification issued in accordance with the national regulations by the userflnstaller before the aircraft may be flown.

FAA Form 8130-3 (6-01) Installer must cross-check eligibility with applicable technical data NSN: 0052-00-012-9005

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17. Name (Typed or Printed)·

JAMES A. SCHiLD, ODARF 18. Date {mfdfy):

JUN/22/20 22. Name {Typed or Printed); rrr ,_. l> It is importanl to understand that the existence of !hrs d Us!;!r/lnstaUer Respons1bJ11tres

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FAA FORM 8130-3. AIRWORTHINESS APPROVAL TAG 3. Form Tracking Humbel":

911546 f--'= FAA/UNITED STATES ~ 4 .oRGAN1ZAr10• Cessn-a-Air·craft-Company · ~= Cessna Parts Distribut ion Dept. 702 °'.... 5800 E Pawnee, Wichita, KS 67218

PartNumb!lr: Eligibility:•

22FH524 01 13. Remarb:

5. Work Order/Contract/Invoice

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10. Quantity: 11. S.rlaVBatchNumber: 12. S!BlutJWork:

1 N/ A New

IRWORTHINESS APPROVAL - PARTS. TH IS FORM IS NOT AN EX PORT APPROVAL.

l,02,208,310,335,340,401,402, 404,414,421,425,441 ,500 ,525,550,560

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User/Installer Responsibilities ti is important to understand that the existence of this document alone does 001 automatically constitute authority to install the parUcomponenUassembly. Where the user/installer performs wOl'k in accordance with the national regulations of an airworthiness authority different than the airworthiness authority of the country specified in Block 1, it is essential that the user/installer ensures that his/her airworthiness authority accepts parts/components/assemblies from the airworthiness authority of the country specified in.Block 1

Statements in Blocks 14 and 19 do not constitute installation certification. In all cases, aircraft maintenance records must contain an installation certification issued in accordance with the national regulations by the user/installer before the aircraft may be flown.

FAA Form 8130-3 (6-01) Installer must cross-check eligibility with applicable technical data NSN: 0052-00-012-9005

1 . .,Approving National Aviation Authority/Country: AUTHORIZED RELEASE CERTIFICATE

FAA FORM 8130-3, AIRWORTHINESS APPROVAL TAG J. FormTracidngNumber:

911546 FAA/UNITED STATES

•oRoANIZATION Cessna Aircraft Company Cessna Parts Distribution Dept. 702


'· """81 ~UT '""'~''"' Part Num~ier: Eligibility: .

22FH524 01 13. Remaru:

5. WorkOrder/Cootractflnvolce ••• ,,,, 4 77397

10.Quantity: 11.SeriaVBatch Number: 12. Status/Work:

N/A New

AIRWORTHINESS APPROVAL - PARTS. THIS FORM IS NOT AN EXPORT APPROVAL.

Ol,02,208,310,335,340,401,402,404 ,414,421,425, 441 , 500 ,525,550, 560

PO# 50588100 14. Certifies the items Identified above were manufactured In conformity to: 19;

~ Approv&ddeslgndata and areinacondiUon fOfsafeoperatioo.

0 Non-approv&ddeslgndata specifledloSlock13.

17. Name (Typed or Printed): 18. Date (mld/y):

KENNETH E. WYSOCKI SR., DARF 01/26/2005 User/Installer Resoonslbilities

Z3.n.w!mldly):

It is important to understand that the existence of this document alone does not automatically constitute authority to install the part/component/assembly. Where th~ user/installer performs work in accordance with the national regulations of an airworthiness authority different than the airworthiness authority of the country specified rn Block 1, it is essential that the user/installer ensures that his/her airworthiness authority accepts parts/components/assemblies from the airworthiness authority of the country specified in Block 1

Statements in Blocks 14 and 19 do not constitute installation certification. In all cases, aircraft maintenance records must contain an installation cenifica!ion issued in accordance with the national regulations by the user/installer before the aircraft may be flown.

FAA Fonn 8130-3 (6-01) Installer must cross-check eligibility with applicable technical data. NSN: 0052-00-012-9005

T FECON CR~ST ~.iJIA.'l'IOa

3520 N.W. S& TH STREET SliTTE 30: FT . LAUDERDALE, FL 33319

ORDER DATE: 2 16/07 SHI~ D~TE : 2 16/31

YOUi ORDER IS 100 ~COMPLETED. TIMF 12:0~:52

SHIP TO: BA!IYAS ?.IR sm1ICES I T\1 f1 lHv 1

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stJ Le> J J7oco7 THANK YOU FOR ~ 1HE ORDER

CERTIFICATE OF CO~PL!ANC3

Falc0~ Crest Avi tic~ Supp ly certifies tha! tt~ pa rts and /or ~a~e:ials co~er?~ by this Certlftcat? ar·~ i:! ~ocd ord9r , a11d t~

1t ~hf ir co~form ~y :o appro1 a~ design data, ls fJbst~~tiated by docu~ent3£f e7ld~ Lc~ c~ ~~ !s tr0e ste origtrr2! ~ a ;~~f ~ctu:a~

<:pp~c·'.it-~ ~.1 ·~1 the ivil Avia!i·:~! Z~cthorit.~~. (F1-.A ilppr:)\'?.l , ?.M.A.t P.C . . T'.S C.. 1

I i .

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UPS SHIPPE?. NO "' : L

per:;:; EY: __ . ____ .. _____ _

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CH).RGE2: $---··----------

W~.YBILL NO.: _____ . _______ _

?RC~: f~LCCN CfSST AV:ATIOX

C~ST.PO~:

TO: BANYAN AIR SE?~ICES, INC. 5 3 2 0 !i'f. 30TH TERRACE FT. LAUOERC~LE, FL 33309~0 0G

T0: BANYAN AIR SEkVICES, INC . 5320 NW JITH TERRACE FT. L~UDEROALE, FL 333&~Z000

Approving National Aviation

Authority /Country:

2. 3. Form Tracking Number:

AUTHORIZED RELEASE CERTIFICATE

FAA/United States FAA Form 8130-3, AIRWORTHINESS APPROVAL TAG

4 · Organization

Name and Address

6. 7.

RAYTHEON AIRCRAFT PARTS INVENTORY AND DISTRIBUTION (RAPID)

DALLAS DISTRIBUTION CENTER 801 INDUSTRIAL BLVD, SUITE 100

GRAPEVINE, TX 76051 PCS

8. 10. 11.

0071100794-00001

5. Work Order/Contract/ Invoice Number

0001188075-000030

Item Description Part Number

9.

Eligibility * Quantity Serial/Batch Nbr

12.

Status/Work

0001 WASHER, PLAIN, HIG H STRENGTH

MS20002-5

13.Remark AIRWORTHINESS APPROVAL - PARTS.

Total time of 00.00 hours

14. Certifies the items identified above were manufactured in conformity to:

~ Approved design data and are in a condition for safe operation

D Non-approved design data specified in Block 13.

17.Name (Typed or Printed):

Darwin Enlow

16. Approval/ Authorization No:

ODARF230339CE

18. Date (m/d/y):

FEB/13 /2 007

NIA 4.000 NIA

USER/INST ALLER RESPONSIBILITIES

NEW

It is important to understand that the existence of this Document alone does not automatically constitute authority to install the part/component/assembly.

Where the user/installer work in accordance with the national regulations of an Airworthiness Authority different than the Airworthiness Authority of the country specified in block I it is essential that the user/installer ensure that his/her Airworthiness Authority accepts pans/components/assemblies from the Airworthiness Authority of the country specified in block 1.

Statements in block 14 and 19 do not constitute installation certification. In all cases aircraft maintenance records must contain an installation certification issued in accordance with the national regulations by the user/installer before the aircraft may be flown.

FAA Form 8130-3 (06-01) * Installer must cross check eligibility with applicable technical data.

1. Approving Natioriai -.,,, 1ion

Authority/Country:

2.

Authorized Release Certificate 3. Form Tracking Number:

58896628- 00 3

FAA Fonn 8130-3, Airworthiness Approval Tag

c} './-C f d _/ :J--FAA/UNITED STATES

4. Organization Name And Address

6. 7. Item Description

GOODYEAR TIRE & RUBBER CO. 100 Business Center Drive Stockbridge, GA 30281

8. Part Number

9.

GOODYEAR TIRE & RUBBER CO. 1901 Goodyear Blvd Danville, VA 24541 (PT2066NE )

10. 11.

5. Work Order, Contract, or Invoice Number:

5003207

12. Quanti Serial/Batch Number Status/Work

1 22x6. 75-10 265K08-l "TSO ARTICLE N/A " 15 SEE BLOCK 1 3 - REMARK "NEW MFG"

13. Remarks

70090348 70130268

TSOC62d

AIRCRAFT TIRES FOR EXPORT 70100307 70100312 70100329 70130441

70100332


~ Approved design data and are in a condition for safe operation. D Non-Approved design data specified in Block 13.

7 01 302 0 9 70130213 70130 219 7013 0224 70130226 70 1 30252 7013 02 55 7013 026 3

19. D 14 CFR 43.9 Return to Service D Other regulation specified in Block 13 .

Certifies that unless otherwise specified in Block 13, the work identified in Block 12 . and described in Block 13 was accomplished in accordance with Title 14, Code of -Federal Regulations, part43 and in respect to that work,'the items are approved for return to service.

16.Approval/Authorization No.: 20.d \uthorized Signature: 21. Approval/Certificate No ..

DARF 510258 CE

18. Date:

BOB W MINNIS JAN/2 5/2007

It is important to understand that the existence of this document alone does not automatically constitute authority to install the part/componenUassembly.

Where the user/installer performs work .in .accordance with the national regulations of an airworthiness authority different than the airworthiness authority of the country specified in Block 1, it is essential that the user/installer ensures that his/her airworthiness authority accepts parts/components/assemblies from the airworthiness authority of the country specified in Block 1.

Statements in Blocks 14 and 19 do not constitute installation certification. In all cases, aircraft maintenance records must contain an installation certification issued in accordance with the national regulations by the user/installer before the aircraft may be flown.

FAA Form 8130-3 (6-01) • lristaller must cross check eligibility with applicable technical" data. NSN: 0052-00-012-9005

Approving National Aviation 2. 3. Form Tracking Number:

Authority/Country: AUTHORIZED RELEASE CERTIFICATE

FAA/United States FAA Form 8130-3, AIRWORTIIlNESS APPROVAL TAG

4. Organization

Name and Address

6. 7.



GRAPEVINE, TX 76051 PC 8

8. 10. 11.

007110 0795 -00001

5. Work Order/Contract/ Invoice Numbe'

0001188075-000040


9.


12.

Status/Work

0001 BOLT MS20005-25 . NIA

13 . Remark AIRWORTHINESS APPROVAL - PARTS .

Total time of 00.00 hours


IKJ Approved design data and are in a condition for safe operationmtm~~

0 Non-approved design data specified in Block 13.


Darwin Enlow


ODARF2 30339CE

18. Date (m/d/y):

FEB/ 13 / 2 007

8.000 NIA

USER/INST ALLER RESPONSIBILITIES

NEW

It is important to understand that the ex istence of this Document a lone does not automatica lly constitute authority to install the part/component/assembly .

Where the user/installer work in accordance with the national regulations of an Airworthiness Authority different than the Airworthiness Authority of the country specified in block I it is essential that the user/ insta lle r ensure that his/her Airworthiness Authority accepts parts/components/assemblies from the Airworthiness Authori ty of the country specified in block I .

Statements in block 14 and 19 do not constitute insta llation certification. In all cases aircraft maintenance records must contain an insta llation certification issued in accordance with the national regulations by the user/ installer before the a ircraft may be flown.


Approving National Aviation 2. 3. Form Tracking Number:

Authority/Country: AUTHORIZED RELEASE CERTIFICATE

FAA/United States FAA Form 8130-3, AIRWORTHINESS APPROVAL TAG

4 · Organization

Name and Address

6. 7.



GRAPEVINE, TX 76051 PCS

8. 10. 11.

0071100793-00001

5. Work Order/Contract/ Invoice Number

0001188075 - 000020


9.


12.

Status/Work

0001 NUT 22FH524

13 . Remark AIRWORTHINESS APPROVAL - PARTS.

Total time of 00 . 00 hours

14.

Certifies the items identified above were manufactured in conformity to:

NIA

[X] Approved design data and are in a condition for safe operationV)1~~~

D Non-approved design data specified in Block 13.


Darwin Enlow


ODARF230339CE

18. Date (m/d/y):

FEB /13 /2007

8.000 NIA

USER/INSTALLER RESPONSIBILITIES

NEW

It is important to understand that the ex istence o f this Document a lone does not automatically constitute authority to insta ll the pa rt/component/assembly.

Where the user/installe r work in accordance with the national regulations of an Airworthiness Authority different than the Airworthiness Authority of the country specified in block 1 it is essential that the user/ installer ensure that his/her Airworthiness Authority accepts parts/components/assemblies from the Airworthiness Authority of the country specified in block 1.

Statements in block 14 and 19 do not constitute installation certification . In a ll cases aircraft maintenance records must contain an installation certification issued in accordance with the national regulations by the user/ insta lle r before the aircraft may be flown.


API 8655 Commerce Drive, Suite Southaven MS 38671 ~~ 11111111111111111

BANYAN AIR SERVICE

5360 NW 20TH TERRACE

FORT LAUDERDALE Fl 33309

Shipping Instructions

Document Number Document Date Purchase Order No. Purchase Order Date

Sales Order Number Sales Order Date Customer Number Shipping Conditions lncoterms Cust Ship Acct Delivery Date

Detailed Shipping Instructions at the end of the document

Bill of Lading Total Weight

Packing Instructions Detailed Packing Instructions at the end of the document

10

20

50-910373-3 B/C

Batches

3533531014

50-910373-4 B/C

Batches

3533531014

DECAL-INSTRUCTION ENO cow ...

I \.i

4 EA

DECAL-INSTRUCTION E,NG cow

4 EA

Shipping and Packing Instructions

0.004 LB

0.040 LB

Page 1 of 1 02/14/2007 16:30:46

Pack List

80204672 02/14/2007 50347940 02/14/2007 185309 02/14/2007 5000252 FXPri 1 D (Intl 1-3D) CPF 106419183

02/15/2007

0.044 LB

The Export Classification Control Number (ECCN) for this product is 9A991 (d) 'Aircraft parts and components, n.e.s.' United States law prohibits

disposition of these commodities to the Balkans, Burma, Cuba, Iran, Ivory Coast, Liberia, Libya, North Korea, Rwanda, Syria, Sudan, Zimbabwe

and certain parties within Iraq unless otherwise authorized by the United States.

See http://www.treas.gov/offices/enforcement/ofac/sanctions/.

These Commodities, technology or software were exported from the United States in accordance w ith the Export Administration Regulations.

Diversion contrary to U.S. law is prohibited. The Buyer agrees and certifies if knowledge that the commodity may be used in violation of U.S.

laws or U.N. resolutions related to proliferation of weapons of mass destruction (missiles, nuclear, chemical or biological), terrorist or narcotics

activities the Seller shall be given immediate notice.

**CERTIFICATE OF CONFORMANCE** API certifies that the parts/materials covered by this document have been manufactured under one of the follow ing approvals: (1) Parts produced under a Type Certificate #TC#, (2) Parts

produced under a Technical Standard Order #TSO#, (3) Parts manufactured under a Parts Manufacturer Approval #PMA# , or (4) Industry Standards. This is substantiated by satisfactory

documentary evidence at API or t he original source of supply. These items are new. rebuilt. overhauled, or repaired unless otherwise noted. With the above statement being true and factual, t he

parts/materials supplied under this certificate are considered in compliance with the FAR#s or Industry Standards when they were shipped from API.

~vrm~ Signature - - - ------- - - --- --- -----

Victor Froemel, Quality Assurance Manager

CustPO#

WHSE

Sold To

SAP Order# Terms Code TennsDesc Waybill# Acct# Created By

PIO Raytheon A1lcratt Palf5 lnwntorr & Distribution Co.

API STOCK PACKAGE 3

Warehouse 8201

0000530346 Aerospace Products Intrntl 3778 Distriplex Drive North MEMPHIS TN 38118

0000964650 009 Within 60 days Due net

TS06960

Pa:e# Delivery#

Order#

Ship To

Pack Date Weight

Ttl# ofCtns Carton#

Route

111 0082353353 494208

0000530346 Aerospace Products Intrntl 3778 ·Distriplex Drive North 901-365-3470 MEMPHIS TN 38118

09/25/05 4,329.0000 LBS 1 of 1 1 MANUAL SHIPMENT

Line# Part Number Val Type Description Serial#/ Lot# Quantity UOM

000480 35-921503

004500 720-200-2

000180 35-815115

002570 50-430177-5

003680 50-910373-3 B/C ---001820 50-380044

004530 7232MSE-160-P3

003730 5100CW28B -

003970 58-910021-1

GASKET

RUBBER GRIP-RH

SPRING

BOLT-MAIN ACCESS

DECAL-INSTRUCTION

BEARING

RING

LIGHT

COVER-AIR FILTER

Certificate of Compliance

16 EA

2 EA

109 EA

DOOR 41 EA

ENG CO 204 EA

129 EA

33 EA

29 EA

1 EA

Seller hereby certifies that the Raytheon Aircraft Company manufactured item(s) ideotified on this sales order were i!lllpe<::t.,(f under an FAA-Approved Qua.I ity control system. , Where items or service have been procured from a local supplier. the seUer further certifies or l:es on file the suppliers certi.fication:s that those items were detennined to be in

conformance with applicable specification and are cc:nsidered airworthy.

Please gee Return Policiell on Reverne Side

Raytlleon Aircraft Parts hwentOI)' & DistrilMl'an Co.

Cost PO# API STOCK PACKAGE 3

WHSR Warehouse 8201

Sold To 0000530346 Aerospace Products Intrntl 3778 Distriplex Drive North MEMPHIS TN 38118

0000964650 009

SAP Order# Terms Code Terms Desc Waybill# Acct# Created By

Within 60 days Due net

TS06960

Lint'# Part Number Val Type

003640 50-910274-529

003650.50-910274-593

003660 50-910274-594

003670 50-910275-265

003690 ~910}13-4 B/C /

003700 50-910482

003710 50-921582-1

003720 50-944076-7

003730 5100CW28B

/ ,/

,/

Description

SPRING ASSEM

SEAL STRIP ASSEM FWD

SEAL STRIP ASSEM FWD

WOVEN PYLE SEAL

DECAL-INSTRUCTION

PLATE

GASKET FUEL CELL

LEVER ARM

LIGHT

Page# Delivery#

Order#

Ship To

Pack Date Weight

'ftl# of Ctns Carton#

Route

COWL

CONL

ENG CO

Certificate of Compliance

41 0082353353 494208

0000530346 Aerospace Products Intrntl 3778 Distriplex Drive North 901 .. 365-3470 MEMPHIS TN 38118

09/25/05 4,329.0000 LBS 1 of 1 1 MANUAL SHIPMENT

Serial#/Lot# Quantity UO.M

3 EA

1 EA

3 EA

5 EA

119 EA

6 EA

529 EA

12 EA

18 EA

... _. ~. · ~: ,f

-1-iy certifies that the Raytheon Aircraft Company manufactured item(s) identified on this sales order were inspected under an FAA-Approved Q11ality control ~)'R!.l!m . . ,, ~ervicc have lJ<Jen procured from a local supplier, the seller further certifies or Im on file the !lllpp!iers certifications that those itbm were detcnuincd to be in

conformance wi1h applicoole specification and are comidered ailworthy.

Please sec Rerum Policies on Reverse Side

/

-~-----

MAINTENANCE/INSPEC_I_ION ENIRIES 27

..-~ STEVENS AVIATION INC. ' .. GREENVILLE, SC

1/3/2007

N800TS SN BB-1032 ACTT 8857.2 HM 359

FLIGHT CYCLES 7826 MAINTENANCE EVENTS, PARTS REMOVED OR REPLACED(CONT.)

204 Replaced left prop RPM gauge with an overhauled gauge PIN RCA42-01 SIN 890184 from Precision Avionics and Instruments in Atlanta, GA CRS# ZV4R714M overhauled on work order number X4747 dated Aug 11, 2006. Operational check satisfactory.~ .•.. . . ·> .·.. . .

205 Adjusted left fuel flow transmitt~r 'within tolerance. Found right fuel flow with ill limits. R~~~mnected and leak checked all lines. Leak check satisfactory. , :;. '

207 Replaced left and right engine lower forward cowling latch placards with new placards PIN 50-910373-3-B/C 208 Installed new weld assembly PIN 101-910049-105 in left engine lower aft cowling and fabricated a repair

doubler from 2024T3 .040 for forward attach stiffener. 209 Repaired left engine outboard exhaust shield. 210 Repaired right engine upper forward cowling air inlet scoops. 212 Installed Butterfield Industries Inc. flow thrnugh anti-ice system in left and right engine cowlings in accordance

with STC SA2905RM and Butterfield Industries Inc. installation instructions Drawing No. Bll 003 Rev F dated 11/08/06 using kit PIN BI 1001-1.

213 Replaced left and right engine torque manifold hoses with new hoses PIN330997F4-0074 and 330995F4-0314. Leak check satisfactory.

214 Applied PRC to right propeller deice boot wiring and applied conductive cement. 799 Resaftied left and right prop shaft seal cover bolts to prevent chaffmg beta collar. Replaced missing nut

on left prop de-ice brush block. 950 Service oxygen system to 1850 PSJ. THE MAINTENANCE IDENTIFIED IN THIS WORK ORDER PACKAGE HAS BEEN INSPECTED AND THE ITEM(S) ARE APPROVED FOR RETURN TO SERVICE. PERT DETAILS OF THE REPAIR(S) ARE ON FILE AT THIS A NCY WORK ORD'JEJld#.~f3~ SIGNED1~---:;~~~~~::=__,,~~~;::::;;;;~~~~~::__~~~~

. 05, CRS VJBR368K Page 4 of 4

J

Make:

Model:

Raytheon Beechcraft

8200

Serial No.: 88·1032

Hours: 8868.3 Lndgs:

· BANYAN Airframe Maintenance Record

Description of Work Accomplished.

I

Reg. No.:

Date:

W/ONo.:

Page:

NBOOTS

2/1512007

24082

Hobbs:

SA-0505

370.1

. Removed existing Beechcraft engine exhaust stacks and Raisbeck Engineering Exhaust Stack Fairings. Installed Frakes Aviation engine exhaust stacks P/N FA5726 in accordance with STC SA8703SW and Frakes Aviation installation instructions. Fonm 337 completed. Weight and balance revised. (Installed P/N FA5726-7L S/N 0721085 Left engine, S/N 0721087 Right engine). (P/N FA5726-8R, S/N 0721086 Left engine, SIN 0721088 Right engine). . Jacked aircraft and removed Left side# 1 and# 2 Wheel and Tire assemblies. Disassembled wheels and removed tires. Cleaned and NDT inspected# 1 and# 2 wheel assemblies. Cleaned, treated and painted areas of minor corrosion on# 1 wheel. Reassembled# 1 wheel with new tire P/N 265K08· 1 S/N 70130268 with new seal P/N MS28775-267, and new hardware 8 ea. bolts P/N MS20005-25, 4ea. washers P/N MS20002-5, 4 ea. washers P/N MS20002C5, and 8 ea. nuts P/N 22FH524. Serviced with dry nitrogen. Wheel and tire assembly leak checked. No defects noted. Wheel and tire assembly installed on aircraft. Reassembled# 2 wheel with new tire P/N 265K08-1 S/N 30901308, with new seal P/N MS28775-267, and new hardware 8 ea. bolts P/N MS20005-25. 4ea. washers P/N MS20002-5, 4 ea. washers P/N MS20002C5, and 8 ea. nuts P/N 22FH524. Serviced with dry nitrogen. Wheel and tire assembly leak checked. No defects noted. Wheel and tire assembly installed on aircraft. Removed aircraft from jacks. . Removed# 4 Main Wheel assembly. Disassembled and removed tire. Wheel assembly and bolts cleaned and NDT inspected. Reassembled with new tire P/N 301-392-641 , S/N 61170007 and seal PIN MS28775-267. Serviced with dry nitrogen. Wheel and tire assembly leak checked. No defects noted. Wheel and tire assembly installed on aircraft with two new bearings P/N 13600LA902A3. . Installed missing screws for Rosen Sun Visors aft mount attachment.

Approval for Return to Service

The article(s) identified above was repaired and inspected in accordance with current FAA regulations and is approved for return to service. Pertinent details of the repair are on file at this agu this wor1< o~

Authorized Signature: '-- .<..v~..LJ.. · .;':._/7 /:?-~ Paul J. Baran, Inspector

Raytheon Factory Authorized Service Center 7Z_ = J FAA Certificated Repair Station WD4R618M

5360 NW 20~ Terrace Fort Lauderdale, Florida 33309 Phone 954 491 3170 Fax 954 4911612


Aircraft Model---------- Serial Number ________________ _

Reg# ____________ _ Owner's Name-----------------

DA TE ENTRIES MAY BE ON MULTIPLE INSPECTOR'S LICENSE Y M D HOURS LINES IF REQUIRED SIGNATURE NUMBER

Reg #: N800TS Model: Beech B200 Serial#: BB-1032 Work Order#: 20172

e•A1R <JRE INC. Aviation Services

Hobbs: 378.4 Tach: Total Time: Date: 316107

Replaced cabin altitude differential pressure indicator. Installed overhauled indicator (CRS# NU2R044L WO# 0296372) pin 101-380026-3 sin Wl 7757G. Ops check normal. F her details see WO# 20172 on file this station. ~

-Fof:,bfr; re, 1TI . FAA Repair Station

ACOR030C

t---+----+--+---+-----+------------------~~~.,---~~-·

Reg#: N800TS Model: Beech 8200 Serial#: BB-l 032 Work Order#: 20186

e•AIR (JRE 1Nc Aviation Services

Hobbs: 385.3 Tach: Total Time: Date: 3/15107

Replaced pressurization controller. Installed overhauled controller (CRS# HZ3R571L WO# 4501967274) pin 130346-12 sin 45-2602. Ops check normal. For further.details s # 20186 on file this station.

~ Fo · · re, c. F A Repair Station

ACOR030C

1 1 ~1 ~~ ~ ~----~~~~~--~---------+------,-;

Reg #: N800TS Model: Beech B200 Serial #: BB-1032 Work Order#: 20213

INC.

Aviation Services

Hobbs: 396.0 Tach: Total Time: Date: 412107

Replaced outflow valve vacuum line drain valve pin 101-384184-1. Replaced LH volt/load meter and installed overhauled (CRS# OL2R061L WO# 0093457) pin 101-384106-9sin123846. Acft test flown. System ops check normal. For further details see WO# 20213 on file this statio

~ re, fu . FAA Repair Station

ACOR030C

MAINTENANCE/INSPECTION ENTRIES

Aircraft Model ~~~~~~~~~~

DATE ENTRIES MAY BE ON MULTIPLE INSPECTOR'S Y M D HOURS LINES IF REQUIRED SIGNATURE


--AIR 01RE me. Aviation Services

Hobbs: 4 15.7 Tach: Total Time: Date: 4123107

29

Replaced pilot's winds.hie!~. Instal.led overhauled windshield (CRS# P9AR279J WO# GF67463) pin 101-384025-21. sl~ 99294Hl800 usmg mstallation kit pin I 01-504 l-3S sin 27711. Replaced seal pin 50-410015-121 on LH av10mcs bay access d?or. Resealed fastener receptacles for door. Resealed top OB edge sealer on RH win deice boot. For further dctatls see WO# 2024~~/I~ g

JVC l\llAl<E:

A/C l\/IC)Dl::L:

JVC S/N:

For:~~~~ FAA Repair Station

ACOR030C

BEECHCRAFT SPARKCl-IASERS 8200 KING AIR ---Air<:raft S<irvi<:<-!S, ln<:.---88-1032 All~FRAME ux;13()()1{ ENTl~Y

T ACli (I.Ii):

liC>EH3S: JVC Rl::G. tt:

0421.0 N800TS

Replaced defective and dry-rotted radome nose cone gasket above radar sensor with Beech PIN 50-410054-21 . Replaced defective LH table lighter with Beech PIN 211746. Repaired Marker Beacon System coaxial cable connector. Removed defective AD500A Attitude Indicator for repair. Reinstalled AD500A PIN 7000836-902 sin 81101055 repaired by Duncan Aviation under WOE ESA5A, dated 511712007. Replaced several sections of removable seat rails with Beech PIN 130433-09600. Cut, drilled and

. countersunk rails accordingly. Removed copilots DME indicator for repair. Reinstalled Collins 339F-12 DME Indicator sin 12695 repaired by Duncan Aviation under WO# ESA7A, dated 5114107. Repaired stripped cabin door support rail mounts. Replaced stripped screws with proper structural screws upon repair of mounting. Repaired sidetone issues with #2 and #3 VHF Comm Systems. Removed and replaced defective strobe power pack with Symbolic Displays Part# 701571 sin APS-22345 overhauled by Kelly Aerospace Turbine Rotables, FAA CRS# NV2R045L under WO# APS-28844 dated 512412007. Pertinent details of above work found 0 98526, o fil at Spa chasers Aircraft Services, Inc.

Date_6_ 6-1£-'/0_· '7_,,__,,/%LJ"'--><==--"--J.--


Aircraft Model Bi= /;:L/t 132DO Serial Number lJfJ J{J J :J..

Reg #_____.N~fj~Q~(J......._rs:__ ___ _

~ ~I l ENTRIES MAY BE ON MULTIPLE

LINES IF REQUIRED INSPECTOR'S SIGNATURE

JVC l\llAl<I::: 8EECHCRAFT SPARKCliASEl~S T ACli (I.Ii):

liC)l313S: WC MODEL: 8200 KING AIR Airc:rcift S<-!rvic:es, lnc: .. ---

JVC S/N: 88-1032 All~FRAl\llE ux;BC>C>I< ENTl~Y JVC l~EG. ti=:

30

LICENSE NUMBER

0421.0 N800TS

Removed the following equipment: 1 ea. Garmin GA56 Antenna at 137.0 in.; 1 ea. Garmin GNC420 Comm/GPS Transceiver at 100.0 in .; 1 ea. Garmin-AT MX20 MFD at 101.0 in. ; 1 ea. Sensor Systems LNA/Diplexer at 326.0 in .; 1 ea. N.A.T. LCM01-001 GPS Receiver at 374.0 in. ; 1 ea. Garmin GA56 Antenna at 176.5 in. ; 1 ea. Sensor Systems 68-8282-101 at 301.56 in. ; 2 ea. Sensor Systems 65-8282-101 Antennas at 331 .75 in. ; 1 ea. Comant Cl-177-20 Antenna at 363.0 in.; 1 ea. King KA 92 GPS Antenna at 130.8 in. and 1 ea. L-3 Communications NY163 Stormscope® Antenna at 395.0 in.

Installed the following equipment: 1 ea. Garmin GNC420W WAAS Enabled GPS I Comm P/N 011-01058-40 sin 97203232 at 100.0 in. ; 1 ea. Garmin GA 35 WAAS GPS Antenna P/N 013-00235-00 sin 17242 at 137.0 in .; 1 ea. L3 Communications TRC899 Skywatch Processor P/N 805-11901-001 sin 81677 at 61.0 in. ; 1 ea. L-3 Communications NY164 Skywatch Antenna P/N 805-10890-001 sin 85628 at 171.5 in. ; 1 ea. Garmin GMX200 Multi-Function Display P/N 011-01467-00 s/n 17000899 at 101.0 in.; and 1 ea. N.A.T. 247-001 Audio Summing Amp sin 1775 at 83.0 in. The above Garmin GNC 420W upgraded was completed in accordance with the Garmin STC Upgrade Installation Manual (Doc.# 190-00357-06, Rev. B) and STC# SA01933LA with attached AML. The location of the Garmin GNC 420W was determined to meet the field-of-view requirements without the need for external annunciation. Removed the Aircraft Flight Manual Supplement for the GNC 420 and installed the FAA Approved Flight Manual Supplement for the Garmin 400W Series GPS-WAAS Navigation System (Doc. # 190-00356-63, Rev. B). The above Garmin GMX-200 Multi Function Display was installed in accordance with the Garmin GMX-200 Installation Manual (Doc.# 190-00607-04, Rev. D) and STC# SA01692SE containing an AML that includes this model aircraft. The above L-3 Communications SKYWATCH® HP Traffic Advisory System was installed in accordance with the L-3 Communications Avionics Systems SKY899 Installation Manual P/N009-11900-001 , Rev. B and with reference to STC# ST01552CH-D. Installed patch plates on removed antenna systems as needed. Structural substantiation for the NY-164 antenna and patch plate installations were provided by FAA Approved Engineering Data provided by DER Services, FT. Lauderdale, FL under Document # MDL-2007-054-1 , dated 5/16/2007. Copies of DER Services Drawings and FAA Form 8110-3, dated 5/17/2007, have been placed in the permanent aircraft records. All applicable ICA Instructions have been placed in the permanent aircraft records. A complete functional ground and flight test was performed and all above systems found to function normally. Reference above installations to FAA Forms 337 dated 610512007 and 610612007 . Detailed description of all work performed can be found on WO# 98402 and 98526 on file at Sparkchasers Aircraft Services, Inc., FAA CRS# XSPR699K.

Aircraft New Empty Weight: 8292.00 lbs. Aircraft New Empty Weight CG: 184.78 in.

:::~:"({)7)'Ji ~dtit'"'"'· Date CRS# XSPR699K

{)6/05/ 2007-, '

1. Approving National Aviation 2. Authority/Country AUTHORIZED RELEASE CERTIFICATE

3. Fonn Tracking Number:

FAA/UNITED STATES FAA Form 8130-3, AIRWORTHINESS APPROVAL TAG ESD2A0001001001 4. Organization Name and Address:

Duncan Aviation/Lincoln Airport/Lincoln, NE 68524

6. Item: 7. Description:

1 ALTITUDE INDICATOR

13. Remarks:

8. Part Number:

4016341-905

Customer:SPARKCHASERS AIRCRAFT SERVICE

Discrepancy: Altitude hold always reads 40 feet low.

5. Work Order/Contract/Invoice Number:

ESD2A

9. Eligibility: • 10. Quantity: 11 . Serial/Batch Number: 12. Status/Work:

N/A 1 98108996 REPAIRED

Preliminary Findings: Bench tested and inspected. Could not duplicate discrepancy. Troubleshot and found the R.2 course potentiometer and the C1 synchro to be misaligned.

Corrective Action: Repaired. Cleaned assembly. Replaced defective component. Aligned and calibrated. Unit functional tested per Honeywell maintenance manual for model BA-141. Revised May 15, 1999. Recertified altitude indicator per Honeywell Technical Newsletter, 23-1980-04, revision 10 and 14CFR, 91.411, Part 43, Appendix E. Paragraph (b} to an altitude of 50,000 feet. No current U.S. Airworthiness Directives apply.

Duncan Aviation certifies that the work specified in Blocks 12 and 13 was performed l.A.W. EASA Implementation Rule part 145 approval, and with respect to that work, the aircraft component is considered ready for release to service under EASA approval number 145.4392.

All EASA/FAA Airworthiness Directives are the responsibility of the installer.

Technician: JAMES B. KUHL

This document constitutes a signed copy of the work order.

Approval for return to service

See attached parts list

User/Installer

19· 18114 CFR 43.9 Return to Service 181 Other regulations specified in Block 13

Certifies that unless otherwise specified in Block 13, the work identified in Block 12 and described in Block 13 was accomplished in accordance with Title 14, Code of Federal Regulations, part 43 and in respect to that work, the items are approved for return to service.

21. Approval/Certificate No.: D\!Nf;~.N

f1 '''l(i JGVR194F 23. Date (m/d/y):

Ma 18 2007

It Is Important to understand that the existence of this document alone does not automatically constitute authority to Install the part/component/assembly.

Whem the userflnstaller perfonns work in accordance with the national regulations of an airworthiness authority different than the airworthiness authority of the country specified in Block 1, it is essential

that the user~nstaller ensures that his/her airworthiness authority accepts parts/components/assemblies from the airworthiness authority of the country specified In Block 1.

Staternenls in blocks 14 and 19 do not constitute installations certification. In all cases, aircraft maintenance records must contain an installation certification issued in accordance with the national

regulations by the usernnstaller before the aircraft may be flown.

FAA Form 8130-3 (6-01) • Installer must cross-check eligibility with applicable technical data. NSN-0052-00-012-9005

FMLNK Page 1of2

Part Number 4006068

Part Description GASKET

Parts List Serial Number Quantity

Page 2 of 2

·1. Approving Na11onai Av1auon 2. Autnority/Counuy AUTHOR[ZED RELEASE CERT[F~CA TE

FM/UNITED STATES FL>...A. Form 8130-3, AIRW:::>RTHINESS APPROVAL IAG 4. Organization Name and Address ·

Duncan Aviation/Lincoln Airport/Lincoln, NE 68524 6. Item: 7. Descnpt1on:

AIR DATA COMPUTER

13. Remarks:

8. Part Number:

4013241-931


9. ::11gioility: •

N/A

Discrepancy: Biannual certification. Altitude preselect is 40 feet low.

10. Quantity:

:.:.. Forrr 1ro.ctung t-.l umbe:--.

::SD3A0001001001 I ~~o~;;ar/Comract/invoice Numoer:

Preliminary Findings: Bench checked and inspecte unit. Could not duplicate discrepancy. Found unit in serviceable condition.

Corrective Actions: Cleaned and painted. Function tested unit per Sperry AZ-241 Air Data Computer component maintenance manual, Revision 3, September 15, 1983. Certified air data computer per FAR 43, appendix E, paragraph (b) (2) to an altitude of 50,000 feet.



No current U.S. Airworthiness Directives apply.

Technician: BARRY A. BURKEY



·.o : . A 19 · ~ 14 CFR 43.9 Return tc Service~ Other regulations spe:::ifled in Block 13

sa1'e :;p;:1ra1tior1'.+/ Certifies that unless otnerwise so cified in Block 13, the work identified in Block 12 and described in Block 1 s accomplished in accordance with Title 14,

s, pan 43 and in respec'. to that work, the items are

21. Approval/Certificate No. :

JGVR194F 2:i . Date (m/dly):

, Ma 17 2007 User/Installer Responsibilities

It 1s important to understand that the existence of this document alone does not automatically constitute authority to install the particomponent/assembly.

Where the user/installer performs work in accordance with the national regulations of an airworthiness authori ty different than the airworthiness authority of the country specified in Block 1, i~ is essential

tnat the user/lnstallei ensures that hisfher airworthiness authority accepts parts/components/assemblies from the a1rworth1ness autnority of the country specified in Block 1.

t Statements rn blocks 1~ and 19 do not constitute rnstallatt0ns certifl::::at1on In all cases, aircraft maintenance re:::ords mus~ contain an rnstallat1on cert1ficatron issued m acco~dance with the national

regulations by the user/insta ller before the aircraft may be fiown

FAA. Form 8130-3 (6-01) • lnstalle- mus cross-oheok el1g1b1ht) wit~ aool1cable techn1ca• data NSl\-0052-00-012-9005

FAALNK 8 age ~ of 1

i. Approving National Aviation I 2. Authority/Counuy

FAA/UN[TED STATES

~- Form TracK1ng Number: AUTHOR[Z:ED RELEASE CERTIFICATE FAA Form 8130-3 . AIRW:::>RTHINESS APPROVAL TAG ESA A0001001001

4. Organization Name and Address: 5. Work Oraar/Contract/lnvo1ce Numbe:-:

Duncan Aviation/Lincoln Airport/Lincoln, NE 68524 I ESA7A I 8. Part Numoer:

622-1234-016

6. hem. 7. Description: I S. Eligibility:.

I N/A

10. Quantity: 11. Senal/Batch Number. 12. Status/Work:

INDICATOR 12695 REPAIRED 1 13. Remarks:


Discrepancy: Several segments missing in the lower window.

Preliminary Findings: Bench checked and duplicated the discrepancy. Troubleshot and found DSS and DS6 to be defective. Potentiometer R145 is intermittent.

Corrective Action: Replaced defective parts. Cleaned, inspected, and aligned. Function tested per Collins 339F-12/12() maintenance manual 4th Edition, 1 December 1988.

Duncan Aviation certifies that the work specified in Blocks 12 and 13 was performed I.AW. EASA Implementation Rule part 145 approval , and with respect to that work, the aircraft component is considered ready for release to service under EASA approval number 145.4392.



Technician: ERIC M BUZZELL



19· ~ 14 CFR 43.9 Return to Service [gj Other regulations specified in Block 13

Certifies that unless otherwise specified in Block 13, the work identified in Block 12 and described in Block 13 was accomplished in accordance with Title 14, Code of Federal Regulations, part 43 and in respect to that work, the items are

return to service. 2~1 . Approval/Certificate No. :

23. Date (mldly):

Mav 14. 2007

It is important to undersiand that the existence of this document alone does not automatically constitute authority to install the part/component/assembly.

Where the user/installer performs work in accordance with the national regulations of an alrworth1ness authority different than the airworthiness authority of the country specified in Bicek i, it is essentia!

that the user/installer ensures that hisfner aiMorthiness authority accepts parts/components/assemblies from the airworthiness autho;tty of the country specified tn Block 1

Statements in blocks 14 and 19 do not constitute installations certification . In a!I cases j aircraft maintenance records must contain a'l 1nstaliation certification issued in a~cordance with tne nationa:

regu1at1ons by the user/installei before the a1rcrat: may be fiown

FM Form 8130-3 (6-01) • lnstalle~ must cros~ -check el 1 gi:Jil it~· witn app!i:able technica 1 aato NStv-0052-00-0'1~-9305

0 age o' 2

Part Number 262-1375-030

382-0027-390

Part Description DISPLAY

POT

Parts List Serial Number Quantity

2

1

::)ags 2 o- 2

1 ".Approving Nat1ona1 Aviation I 2.

Autnority/Country AUTHORtZED RELEASE CERTiF~CA TE i 2. F-onr TracKtng Numoer

I ESA5A0001001 OOi FAA/UNITED STATES FAA. Form 8130-3 , AIRW'.JRTH!N:::ss .APPROVAL TAG ~. Organization Name and Address·

Duncan Aviation/Lincoln Airport/Lincoln, NE 68524

6. ltem:

1 7. Description:

ATTITUDE DIRECTOR IND

13. Remarks:

I e. Part Number:

17000836-902


Discrepancy: LOC inop.

5. Wort~ Order/Contractl!nvo1ce Number:

ESA5A

10. Quantity. 111. Serial/Batch Numoer:

81101055

9. E11gioility: • 12. StaiusNvork:

REPAIRED N/A

Preliminary findings: Bench checked unit and duplicated discrepancy. LOC servo is railing to left or right stop and not adjusting. FD and ATT flag motors are loose. Case glass is loose. Power supply capacitors are leaking.

Corrective Action: Troubleshot unit and replaced defective parts. Cleaned geartrain. Aligned flags, servos, and command bars. Resealed case glass. Unit functional tested per Honeywell AD-500A maintenance manual, REVISION NO. 1 DATED 15 September 1983.


Ali EASA/FAA Airworthiness Directives are the responsibility of the installer.


Technician: TRENT M. FULLER


Approvai for return to service


1f ~ 14 CFR. 43.S Return to Service [g! Otner regulations specified in Bio::k 13

Certifies that unless otherwise specified in Block 13, the work identified in Block ~ 2 and described ir. Block 13 was accomplished in accordance with Title 'i4, Code of Federal Regulations, part 43 and in respec: to that work, the items are a ppr

prova11:.;ertif1~i& No.:

2007

It is important to unoerstand that the existence of this document alone does not automatically constitute authority to install tne oartlcomponentiassembly.

Where ttle user/1nsial1er pertonns work in accordance with the national regulations of an airworthiness autnority different than tn£ airworthiness authority of the country specified in Block 1, it is essentia'

that the user/installei ensures that hisfher airworthiness authority accepts parts/components/assemblles from the a1rworth1ness authority of the country specified in Blo::k 1.

Statements m blocks 1.t; and 19 do not constitute installations certification. In a l: cases, aircraft maintenance records must contain an installation certification issued in accordance with tne national

regulations by the user/1nsialler before the aircraf:. may be flown .

FAA Form 8130-3 (6-01) '* lnsta!le :-- mus: cross-::neck el!gib!Hty witr appl!~ble le::nnicai data NSN-0052-0~-012-9005

FAA~NK Page 1 of 2

Part Number 2N2222A 2N2432A

2500263-3 2504649-2 7000041-32 7000041-45 7000262-448 7002117-217 7002131-217

Parts List Part Description TRANSISTOR (248-1005) TRANSISTOR

TRANSISTOR TRANSISTOR CAPACITOR

CAPACITOR

IC

IC MICRO CIRCUIT

Serial Number

J ~. Forrr TracK1ng fll!umoe:-:

I ESA5A0001001 001

Quantitv 1

4

2 1

MAINTENANCE/INSPECTION ENTRIES 31

Aircraft Model 'Be tt,,fl '82 Q6 Reg # __ N~8_00----'--"T5...._~ __ _

Serial Number ____ 1] __ {} __ -........ /LJ""--"'"-3 .._2 ______ _

JVC l\llAl<I:::

A/C l\llC>Dl::L:

JVC S/N:

Date: 06/05/2007

8EECHCRAFT SPARKCHASEl~S 8200 KING AIR Airc:retft Servic:c-!s, lnc:.---

88-1032 AIRFl~AMI:: ux;1~C>C>I< l::NTl~Y

Ti\Cli (I.Ii):

liC>l313S: JVC l~l::G. ti=:

0421 .0 N800TS

Removed Sperry BA-141 Altitude Indicator and AZ-241 Air Date Computer and shipped to Duncan Aviation for certification to FAR Part 43, Appendix E. Reinstalled BA-141 P/N 40216341905 s/n 98108996 repaired by Duncan Aviation under WO# ESD2A dated 5/18/07. Reinstalled AZ-241A Air Data Computer PIN 4013241-931 sin 85042803 inspected and certified by Duncan Aviation under WO# ESD3A dated 5/17/07. Removed RH altimeter PIN U.I 5934A-1 and replaced with new United Instruments 5934PAD-3 Altimeter certified to FAR Part 43, Appendix E. Repaired leaks to LH static system that were located aft of pressure bulkhead. Performed correlation of altitude reporting systems. Transponders, Altitude Reporter and Altimeters checked through altitude operating envelope of aircraft and found to comply with FAR Part 43, Appendix E (c).

I certify that the altimeter and static system tests and inspections required by FAR 91.411 have been performed. The LH Altimeter/Air Data Computer BA141 , P/N 4016341-905 S/N 98108996 I AZ241, P/N 4013241-931 SIN 85042803 certified to FAR Part 43, Appendix E by Duncan Aviation, Inc., CRS# JGVR194F on WO# ESD2A & ESD3A were tested to 50,000 ft. on 05/18/2007. The associated altitude reporting system was tested to 30,000 ft. Details related to certification are on file under WO# 98526, dated 05/30/2007.

I certify that the altimeter and static system tests and inspections required by FAR 91.41 1 have been performed. The RH Altimeter, P/N LI.I. 5934PAD-3 S/N 462200 certified to FAR Part 43, Appendix E by Sparkchasers Aircraft Services, Inc., CRS# XSPR699K on WO# 98402 was tested to 35,000 ft. on 05/17/200?.

I certify the below transponder(s) has(have) been inspected and found to comply with the requirements of FAR Part 91.413 on Work Order No. 98526, dated 05/30/2007.

#1 Transponder: Make Garmin, Model GTX-330, SIN 84119812. #2 Transponder: Make Collins, Model TDR-90, SIN 26753.

s;goed CZJA .. dc:-------------Sparkchasers Aircraft ServicE FAA CRS# XSPR699K

I I

Serial No. l<oo1o1 .

Remarks: -r;_s ~c

'-/ 3. er,ep x Cbmp)'1

Owner

Altimeter S~a!~A¥ Correction=-

·1000 0

600 1000 1600 2000 3000

60000

SERVICEABLE CONDITION Part Name un.~·f-ed 1-JJf; ·me. -kv

Part No. 6<13'f PAD -3

Serial No. Lfb(};)OO Acft No. J600 T.S

Remarks: ·-r:;.s 1-c c1 a I+,· n~r I A v.J FA (2_

Cbm p!'1 f-D 35, VOl'

Owner ~r>'-f Ha le s WO. No. --=CJ--=8"-_t.../::......0_ :2::...--__ Date __ 5__,/c_:__I 7~/::_o~7 __

Inspect0r ~~JJM= Cert. #- fl ~J}{JJ-

TESTED WITH SETRA MOOEL 370 DIGITAL PRESSURE GAGE


Aircraft Model f:J f w 13 2DCJ Serial Number __ B_.. ....... Uf_.--'-) Q"'--'<-?_2-_____ _

Reg# N ~00 \ /

DATE ENTRIES MAY BE ON MULTIPLE INSPECTOR'S LICENSE Y M D HOURS LINES IF REQUIRED SIGNATURE NUMBER

A/C l\llAICI::: BEECHCRAFT SPARKCliASEl~S JVC l\llC>Dl::L: 8200 Kl NG Al R Air<:rClft S<·H"\fi<:es, 111<:.---JVC S/N: BB-1032 All~FRAl\111:: L()(;l:J()()I< ENTl~Y

T ACM (LI-I):

l-IC>l313S: 0445.60 JVC REG. ti=: NBOOTS

Removed the following equipment: 1 ea. Beechcraft Nose Cone I Radome at 20.0 in. Installed the following equipment: 1 ea. Norton I Saint-Gobain Performance Plastics PIN 2090XS Radome sin 603 with erosion boot at 20.0 in . The above radome was installed in accordance with STC# SA37GL containing the FAA Approved Model List that lists this model aircraft. The above radome was installed in accordance wit the Saint-Gobain Installation Document No. Nl-2090, dated 0312512002. The Norton Radome was prepared and finished using Sherwin-Williams JetGlo CM0570535 Matterhorn White paint and Sherwin-Williams AcryGlo H10656 Silver Platinum trim. The above radome meets the electromagnetic performance requirements of RTCA D0-213, Class A for radar transmission efficiency. FAA Form 337, dated 711612007 detail documentation of this installation. WO# 98552 on file at Sparkchasers Aircraft Services, Inc.

Aircraft New Empty Weight: Aircraft New Empty Weight CG: Aircraft New Useful Load:

8293.00 lbs. 184.75 in.

4297.00 lbs.

Signed cff/rvt <? ;jJg A&P3078378

Date 0 J..11/(/;?fO h

Reg #: N800TS Model: Beech 200 Serial#: BB-1032 Work Order#: 20513

e•AIR OIRE fNC. Aviation Services

Hobbs: 458.4 Tach: Total Time: Date: 9/14107

Replaced LH O/B MLG tire with new Goodyear Flight Special II 22 x 6. 75 - 10 1 Oply sin 70390391. Replaced LH landing light with new pin 4594 and re-~plice~roun wire. All ops normal. For further details see WO# 20513 on file this station. · ~

F . . Air Care, Inc.


FAA Repair Station ACOR030C

e•AIR OIRE fNC. Aviation Services

Hobbs: 475 .3 Tach · Total Time· Date: l 0129/07

Replaced l foot of EVA tubing in LH stub wing with new pin 44EVA-BU. Ops check normal. For further details see WO# 20584 on file this station. 4

'7L -, or '.f\.ir Care, Inc.



Aircraft Model--------- Serial Number ________________ _

Reg# ___________ _ Owner's Name------------------

Make: Hawker Beechcraft

Model: 8200

Serial No.: BB-1032

TSN: Ldgs:

BANYAN Airframe Maintenance Record

Description of Work Accomplished.

Reg. No.:

Date:

W/ONo.:

Page:

N800TS

10/29/2007

24978

1 Hobbs: 478.0

Repaired Bleed Air Warning System tubing in area of left Air to Air Heat Exchanger. Aircraft ground run for leaks and operation of system. No defects noted.

Approval for Return to Service

he article(s) identified above was repaired and inspected in accordance with current FAA regulations and is approved for return to service. Pertinent details f the repair are on file at this agency under this work .

Authorized Si nature:

Hawker Beechcraft Factory Authorized Service Center

Reg #: N800TS Model: Beech B200 Serial #: BB-1032 Work Order #: 20618

5360 NW 20th Terrace Fort Lauderdale. Florida 33309 Phone 954 491 3170 Fax 954 4911612

INC.

Aviation Services

Paul J. Baran, Ins ector

FAA Certificated Repair Station WD4R618M

Hobbs: 4931-Tac::: Total Time Date: i '11191c7

Replaced RH flow pack with overhauled unit pin 101-380013-13 sin 3232. Unit overhauled by Aerospace Control Corporation CRS# OJ2R059L WO# 2380 l. Replaced pneumostat with overhauled unit pin 101-380013-3 sm 2955. Unit overhauled by Aerospace Control Corporation CRS# OJR059L WO# 23683. Replaced cabin pressurization controller with overhauled unit pin 130346-12 sin 65-885. Unit overhauled by Professional Aircraft CRS# P8IR813N WO# WOl46028. Ground ran acft and all ops check normal at this time. For further details see WO# 20618 on file this station. ~

, 0---r: . tr Care, Inc.

FA: Repair Station ACOR030C

) )

)

l


Aircraft Model - -------- Serial Number ________________ _

Reg# ____________ ~ Owner's Name----------------

Re!! #: N800TS Model: Beech B200 Serial #: BB-1032 Work Order #: 20592

t~AR <JRE TNc Aviation Services

Hobbs: 481.3 Tact Total Tin::; Date: 10/3l!Q7

Replaced emergency exit door seal with new pin 115-430000-101 . Replaced cabin door seal with new pin 50-430061-27. Replaced outflow and safety gaskets with new p/n 101 -540023-1. Replaced cabin door cushion with new p/n 50-430043-1211. Replaced fuselage cushion with new pin 50-430043-1213 . Replaced cabin door thresh hold with new pin 50-430182-5. Replaced RH prop heat brush block assembly with new p/n 3E2090- l. Ground

ran acft and all ops check normal. For further~et~a· i s e 0# 2 .. 0592 on file this station. A ~··

: . ir Care, Inc. F Repair Station

ACOR030C

'--A/C Maint. Log entry

Serial# 91..2.. 0323 Z.

Updated Main Software Version to .5 0 IA W Manufacturers Instructions. SB o 7<(o & C l A

Updated GPS Software Version to --=3'--,_u ____ IA W Manufacturers Instructions. SB 0'7 l(o te cyf/ _.

Details on file work order# '1 &-WV Sparkchasers A/C Services CRS XSPR699K

Signed f>ayiµ) rJ . i J:+f J</&nwDat~ _ _.:..;:12+/-'-z.._i>+}c=q;+-----CRS XSPR699K 9-"- r '

N# ~ -rr Tac~s 5/5"· z_ AJC Maint. Log entry

UNIT 6 D Uo] A Serial# !./'/15"0~ 9(

Updated Main Software Version to 3 . Z. IA W Manufacturers Instructions. SB 0 1 v 2 :2rrtl

Updated GPS Software Version to __.N~r-/~;4 ____ IAW Manufacturers Instructions. SB __________ . I

Details on file work order#3__'6J1/f/ Sparkchasers A/C Services. CRS XSPR699K '

SignedWadrl . W t!:!&M/ ft?)&JI>ate __ n+/-=2-..;;;..iol'-', cJ'--',2'------CRS XSPR699K I 1 I


Aircraft Model--------- Serial Number ________________ _

Reg# ____________ _ Owner's Name _______________ _

Reg #: N800TS Model: Beech B200 Serial #: BB-1032


~-AIR <JRE INC. Aviation Services

INC.

Hobbs: 506.3 Tach: Total Time:

Hobbs: 4813 Tact

Date: 11/28/07

. h / LP1982SP Ops check normal. For further details see WO# 20642 on file R placed RH recog lamp wit new p n . . 1 t ts station. k:' r 7 !I;-----------

..;, orAi; Care, Inc. FAA Repair Station

ACOR030C

."'(/-"' I.:::. • All:WflUUU:li ~ I~ • L.. N\.. IYtamL LOg entry

Hobbs: 512. l

Reg #: N800TS ~~AIR Ql~ INC Model: Beech B200 ... ,.,.l'I Total Time: Jrial #: BB- l 032 Aviation Services Date: 12/17 /07

Tach:

ork Order#: 20664

- . . · h I 130~21-~10 For further details see WO# 20664 on file th~s station. Replaced LH wmg stall stnp wit new P n rA._------

, l. /~ T r: ir Care, Inc.


N# ~ {~ Tac~s 51~· 2_ A/C Maint. Log entry

UNIT @, D Lh'l A Serial# 1./11~0~ 9(

Updated Main Software Version to 3 . l IA W Manufacturers Instructions. SB 0 ·7 v 2. 1Z CVA

v pin 5utshion with foorthresh 1. Ground

IDS.

Updated GPS Software Version to -"-'f'i'-1-/_..;4-'--___ IA W Manufacturers Instructions. SB _________ . I

Details on file work order#!}_?J1/.t/ Sparkcbasers A/C Services. CRS XSPR699K

Signed(fJa,,J,.J . W,'3:Y.M.J {t12~nDate __ n _,../ -=-z_-to/_· cJ_.'2..__ __ CRS XSPR699K I r I

- ---.--1 . Approving National Aviation 2. 3. Form Tracking Number.

Authority I Country: AUTHORIZED RELEASE CERTIFICATE

FAA I UNITED STATES 104947-1 FAA FORM 8130-3, AIRWORTHINESS APPROVAL TAG

4. Organization Name and Address: 5. Work Order, Contract, or Invoice

ACCESSORY OVERHAUL GROUP, INC. Number:

1454 WILLIAMSON RD

GRIFFIN, GA 30224 104947-1

6. Item: 7. Descrigtion: 8. Part Number: 9. Eligibili!}': * 10. ~: 11. Serial/Batch Number: 12. Status/Work:

1 STARTER GENERATOR 23048-016 VARIOUS 1 15676 FAR 43.9

OVERHAUL

13. REMARKS: OVERHAULED IN ACCORDANCE WITH MANUFACTURER'S MAINTENANCE MANUALS. UNIT BENCH TESTED AND MEETS OR EXCEEDS MANUFACTURER'S SPECIFICATIONS. CERTIFIES THAT THE WORK SPECIFIED IN BLOCK 12/13 WAS CARRIED OUT IN ACCORDANCE WITH JAR 145 AND WITH RESPECT TO THAT WORK THE AIRCRAFT COMPONENT IS CONSIDERED READY FOR RELEASE TO SERVICE UNDER JAA ACCEPTANCE CERTIFICATE NUMBER: JAA.5387

14. Certifies the items identified above were manufactured in conformity to: 19. 00 D Other regulation specified in Block 13 14 CFR 43.9 Return to Service

D Approved design data and are in a condition for safe operation. Certifies that unless otherwise specified in Block 13, the work identified in Block

D Non-approved design data specified in Block 13 12 and described in Block 13 was accomplished with Title 14, Code of F~deral Regulations, part 43 anz~t to that work, the items are approved ~r return to_Eice. _/""""") >.

15. Authorized Signature: 16. Approval Authorization No: 20.Auth1edSig~..- 21 . Approval/Certificate No:

G4ZR155X

17. Name (Typed or Printed): 18. Date (m/d/y): 22. Name (Typ9dor Prv 23. Date (m/d/y): BARRY JONES October-21 -2002

User/Installer Responsibilities / v


Where the user/installer performs work in accordance with the national regulations of an Airworthiness Authority different than the Airworthiness Authority

of the country specified in Block 1, it is essential that the user/installer ensures that his/her airworthiness authority accepts parts/components/assemblies

from the airworthiness authority of the country specified in Block 1.

Statements in Blocks 14 and 19 do not constitute installation certification. In all cases, aircraft maintenance records must contain an installation certification issued in accordance with the national regulation by the user/installer before the aircraft may be flown.

FAA Form 8130-3 (6-01) • Installer must cross check eligibility with applicable technical data. 24779 NSN: 0052-00-012-9005 by CTI

1. Approving National Aviation 2. AUTHORIZED RELEASE CERTIFICATE 3. Form Tracking Number

Authority I Country 47535786 FAA / United states FAA Form 8130-3, Airworthiness Approval Tag

4. Organization Name and Address: Aviall Wheel and Brake Services, 3200 W Prospect Rd, Ste 140,. Ft Laud., FL 33309 5. Work Order I Contract I Invoice Number

47535786 AAC No. XVLR346L EASA Reference No. 145,(;!190

6. 7. 8. 9. 10. 11 . 12. Item Description Part Number Eligibility• Quantity Serial Batch Number Status/Work

BRAKE ASSEMBLY 101-8002-3 N/A 5752 OVERHAULED

13. Remarks: WORK ORDER# 47535786 :lescribing the actual work performed is on file at ihis Air Agency. RETURN TO SERVICE

Technical Data Ref: ABS 073-04 (32-44-09) REV. 7 06/03/03

NOTE: The following statements apply only when this form is used for the purpose of a dual release. Aviall Wheel and Brake's work order certifies that the work specified in Block 12/13 was carrieq out in accordance with EASA 145 and with respect to that work the

~I

aircraft component is considered ready for release to service under EASA Acceptance Certificate# EASA: 145.41 90 Only FAA Airworthiness Directives have been com lied with.

19. ~ 14 CFR 43.9 Return to Service Other Regulation Specified in Block 13

Certifies that unless otherwise specified in Block 13, the work identified in Block 12 and described in Block 13 was accomplished in accordance with Title 14, Code of Federal Regulations, Part 43 and in respect to that work, the items are approved for return to service.

20. Authorized Signature: 21 . Approval/Certificate Number:

XVLR346L

22. Name: (Typed or Printed) 23. Date (m/d/y):

Jose Botero NOV 12, 2007

User/Installer Responsibiliti~s

It is important to understand that the existence of this Document alone does not automatically constitute authority to install the part/componenUassembly.

Where the user/installer performs work in accordance with the national regulations of an Airworthiness Authortty different than the Airworthiness Authority of the country specified in block 1 it is essential that the user/installer ensures that his/her Airworthiness Authority accepts parts/components/assemblies from the Airworthiness Authortty of the country specified in block 1.

Statements in block 14 and 19 do not constitute installation certification In all cases aircraft maintenance records must contain an installation certification issued in accordance with the national regulations by the user /installer before the aircraft may be flown.

FAA Form 8130-3 (6-01) • Installer must cross check eligibility with applicable technical data. Computer Generated Form NSN: 0052-00-01 2-9005

------------~------------~ --


Authority I Country 47536779 FAA/ United states FAA Form 8130-3, Airworthines:? Approval Tag

4. Organization Name and Address: Aviall Wheel and Brake Services, 3200 W Prospect Rd ,1 Ste140, Ft Laud., FL 33309 5. Work Order I Contract I Invoice Number

47536779 AAC No. XVLR346L EASA Reference No. 145.4190

6. 7. 8. 9. 10. 11. 12. Item Description Part Number Eligibility* Quantity Serial Batch Number Status/Work

BRAKE ASS EMBLY 101-8002-3 N/A JUN96-145 OVERHAULED

13. Remarks: WORK ORDER #47536779 :lescribing the actual work performed is on file at this Air Agency. RETURN TO SERVICE


NOTE: The following statements apply only when this form is used for the purpose of a dual release. Aviall Wheel and Brake's work order certifies that the work specified in Block 12/13 was carried out in accordance with EASA 145 and with respect to that work the aircraft component is considered ready for release to service under EASA Acceptance Certific,9te # EASA: 145.4190 Only FAA Airworthiness Directives have been com lied with.

19. ~ }4 CFR 43.9 Return to Service Other Regulation Specified in Block 13

Certifies that unless otherwise specified in Block 13, the work identified in Block 12 and described in I Block 13 was accomplished in accordance with Title 14, Code of Federal Regulations, Part 43 and in :1

respect to that work, the items are approved for return to service.

20. Authonized Signature: Approval/Certificate Number:

XVLR346L

22. Name. (Typed or Printed) 23. Date (m/d/y):


User/Installer Responsibilities



Statements in block 14 and 19 do not constitute installation certification In all cases aircraft maintenance records must contain an installation certification issued in accordance with the national regulations by the user flnstaller before thri aircraft may be flown.

FAA Form 8130-3 (6-01) * Installer must cross check eligibility with applicable technical data. Computer Generated Form NSN: 0052-00-012-9005


Authority I Country

FAA I United States FAA Form 8130-3, Airworthiness Approval Tag 47536777

4. Organization Name and Address: Aviall Wheel and Brake Services, 3200 W Prospect Rd , Ste 140, Ft Laud ., FL 33309 5. Work Order I Contract I Invoice Number


6. 7. 8. 9. 10. 11 . 12. Item Description Part Number Eligibility* Quantity Serial Batch Number Status/Work

BRAKE ASS EMBLY 101-8002-3 N/A S-FEB04-714 OVERHAULED

13. Remarks: WORK ORDER #47536777 :lescribing the actual work performed is on file at this Air Agency. RETURN TO SERVICE

Technical Data Ref: ABS Q73-04 (32-44-09) REV. i 06/03/03

NOTE: The following statements apply only when this form is used for the purpose of a dual release. Aviall Wheel and Brake's work order certifies that the work specified in Block 12113 was carried out in accordance with EASA 145 and with respect to that work the aircraft component is considered ready for release to service under EASA Acceptance Certificate# EASA: 145.4190 Only FAA Airworthiness Directives have been com lied with.


Certifies that unless otherwise specified in Block 13, the work identified in Block 12 and described in Block 13 was accomplished in accordance with Title 14, Code of Federal Regulations, Part 43 and in respect to that work, the items are approved for return to service.

20. Authorized Signature: 21 . Approval/Certificate Number:

-.::::;:a;~~~iJ XVLR346L

22. Name: (Typed or Printed) 23. Date (m/d/y):


User/Installer Responsibilities '

It is important to understand that the existence of this Document alone does not auto(natically constitute authority to install the part/component/assembly.

Where the user/installer performs work in accordance with the national regulations of an Ai rworthiness AGthortty different than the Airworthiness Authority of the country specified in block 1 it is essential that the user/installer ensures that his/her Airworthiness Authority accepts parts/components/assemblies from the Airworthiness Authortty of the country specified in block 1.

Statements in block 14 and 19 do not constitute installation certification In all cases aircraft maintenance records must contain an installation certification issued in accordance with the national regulations by the user flnstaller before the aircraft may be flown .

FAA Form 8130-3 (6-01) * Installer must cross check eligibility with applicable technical data. Computer Generated Form NSN: 0052-00-012-9005


Authority I Country 47535788 FAA / United States FAA Form 8130-3, Airworthiness Approval Tag

4. Organization Name and Address: Aviall Wheel and Brake Services, 3200 W Prospect Rd, Ste 140, Ft Laud. , FL 33309 5. Work Order I Contract I Invoice Number


6. 7. 8. 9. 10. 11. 12. Item Description Part Number Eligibility* Quantity Serial Batch Number Status/Work

BRAKE ASSEMBLY 101 -8002-3 NIA APR97-173 OVERHAULED

13. Remarks: WORK ORDER #47535788 jescribing the actual work performed is on file at this Air Agency. RETURN TO SERVICE


NOTE: The following statements apply only when this form is used for the purpose of a dual release. Aviall Wheel and Brake's work order certifies that the work specified in Block 12/13 was carried out in accordance with EASA 145 and with respect to that work the aircraft component is considered ready for release to service under EASA Acceptance Certificate# EASA: 145.4190 Only FAA Airworthiness Directives have been complied with .


Certifies th::t unless otherwise specified in Block 13, the work identified in Block 12 and described in Block 13 was accomplished in accordance with Title 14, Code of Federal Regulations, Part 43 and in respect to that work, the items are approved for return to service.

20.

22.

Authorized Signature~~ . _

~ Name: (Typed or Printed)

Jose Botero

User/Installer Responsibilities

21 . Approval/Certificate Number:

XVLR346L

23. Date (m/d/y):

NOV 12, 2007



Statements in block 14 and 19 do not constitute installation certification In all cases aircraft maintenance records must contain an installation certification issued in accordance with the national regulations by the user flnstaller before the aircraft may be flown.

FAA Form 8130-3 (6-01) * Installer must cross check eligibility with applicable technical data. Computer Generated Form NSN : 0052-00-012-9005

l. Approving National Aviation 2. 3. Form Tracking Number: Authority/Country: AUTHORIZED RELEASE CERTIFICATE FAA/United States FAA Form 8130-3, AIRWORTHINESS APPROVAL TAG 4801470

4. Organization Name and Address: Precision Electronics, LLC. • 5000-A Clark Howell Hwy. • Atlanta, GA 30349 5. Work order/Contract/Invoice F.A.A. C.R.S. PRZR073K Number:

E.A.S.A. Approval 145.4780 Phone 404-767-4667 • Fax 404-765-1722 • E-mail [email protected] 4801470 6. Item: 7. Description 8. Part Number: 9. Eligibility:* 10. Quantity 11. Serial/Batch Number: 12. Status/Work

1 FLAME DETECTOR 30-215-8 NIA 1 PT2037 Inspected

13. Remarks : Certifies that the work specified in block 12/13 was carried out in accordance with EASA 145 and with respect to that work the aircraft component is considered ready for release to service under EASA Approval Certificate Number: EASA.145.4780. Rcturnin:~ 10 service utilizing approved data as listed on Service Or,der as referenced in Block 5 .

.

AIR CARE, INC , 14. Certifies the items identified above were manufactured in conformity to: 19. ~ 14 CFR 43.9 Return to Service ~ Other regulation specified in Block 13

D Approved design data and are in a condition for safe operation. Certifies that unless otherwise specified in Block 13, the identified in Block 12 and described

D Non-approved design data specified in Block 13. t in Block 13 was accomplished in accordance with Title 14, Code of Federal Regulations, part

l 43 and in[J_ct to that work, the items are approved for return to service.

15. Authorized Signature 16. Approval/Authorization No. : :20. A"thorip~ 21. Approval/Certificate No.:

NIA NIA PRZR073K 17. Name (Typed or Printed): 18. Date (m/d/y):

1. 22:z±IM'Wi1..soN 23. Date (m/d/y):

NIA NIA Jan/30/2008

User/Installer R~sibilities It is important to understand that the existence of this document alone does not automatically constitute authority to install the part/coinponent/assembly.

Where the user/installer performs work in accordance with the national regulations of an airworthiness authority different than the airworthiness authority of the country specified in Block ·l, it is essential that the user/installer ensures that his/her airworthiness authority accepts parts/components/assemblies from the airworthiness authority of the country specified in Block 1.

Statements in Blocks 14 and 19 do not constitute installation certification. In all cases, aircraft maintenance records must contain an installation certifa.:ation issued in accordance with the national regulations by the user/installer before the aircraft may be flown.

I

FAA Forms 8130-3 (6-01) *Installers must cross-check eligibility with applicable technical data. NSN: 0052-00-012-9005

---------



AFTC: 7988

etA1R om INC Aviation Services

Hobbs: 546.5 Tach: Total Time: 9044.7 Date: 214108

35

Performed Phase 1,2,3, and 4 inspections ila/w Raytheon Aircraft King Air 200 Series Maintenance Manual Scheduled Inspection Program. Performed allllual inspection ofELT ila!w FAR 91.207(d). No corrosion or defects noted. ELT ops check normal. Performed annual inspection of fire extinguishers. No defects noted. Performed allllual inspection of wing spar caps. No defects noted. Performed allllual wing bolt lube. Performed allllual inspection of cabin altitude warning pressure switch. No defects noted. Performed allllual insp of oxygen system barometric pressure switch. No defects noted. Performed allllual insp of pilot' s edgelighted fuel panel and co-pilot's circuit breaker panel. No corrosion noted. Replaced lamps pin D-158-100-5tl and necessary. Performed 200, 400, 600, and 800 hour lubrication items. Performed battery capacity check. No defects noted. Performed flaps flex shaft 5000 cycle inspection. No defects noted. CIW AD 90-08-17 by inspection. No defects noted. CIW AD 2004-23-02by visual and FPI inspection. No defects noted. Due next at AFTT: 9244.7. C/W AD 2005-01 -04 by logbook review. PICIW as AD 98-15-13 .and no suspect hose installed up to effective date of AD 2005-01-04. C/W AD 2005-01-08 by visual inspection. No defects noted. AD 2007-12-06 NIA by acft sin. Replaced rudder boost filter pin AA2J4-7. Resealed edges of wing surface deice boots. Replaced RH starter generator. Installed overhauled unit (CRS# G4ZR155X WO# 104947-1) pin 23048-016 sin 15676. Cleaned and inspected QAD mount. No defects noted. Replaced brakes. Installed overhauled brakes (CRS# XVLR346L WO# 47535786, 47536779, 47536777, 47535788) pin 101-8002-3 #1 sin 5752, #2 sin JUN96-145, #3 sin S-FEB04-714, #4) APR97-l 73. Bled brakes. Replaced instrument air filter pin 101-380038-1. Replaced RH ice light lamp pin 7079B-24. Installed gaskets pin 101-120108-77, 101-120108-127 and 101-120108-151 on LH and RH aux tank panels. Replaced shimmy damper outer barrel pin 50-820007-3 . Replaced shimmy damper seals and serviced with 5606. Replaced following items in cabin door : fwd latch hook bolts pin NAS6203-2 ID, aft latch hook bolt pin NAS6203-21D, step intercollllect rod ends pin 21254-3LS, pins pin MS20392-2Cl5, MS20392-2Cl5, spring p/n 50-384066-BSL, step cable p/n 50-430043-437. Remarked bayonets. Replaced MLG tires. Installed new tires (Michelin Air 22 x 6.75 - 10 lOPR) #1 s/n 7180QW00454, #2) s/n 7182W00339, #3) s/n 7180W00461 , #4) s/n 7 l 80W00346. Replaced LH # 1, LH #2 and RH #4 window light lamps p/n 5108WW. Replaced diode p/n 101-361045-3 on FSB/No Smoking light switch. Replaced nut insert pin DI 71SE395-10-6 on RH aux panel cover. Replaced cabin door entry light switch p/n l tp J-2. Replaced RH engine upper forward flame detector. Installed inspected detector (CRS# PRZR073K WO# 4810470) p/n 30-215-8 s/n PT2037. Replaced oxygen bottle capillary line p/n 800438-14. Replace RH #2 cabin seat lateral tracking handle shaft p/n 101-530444-3. Ground ran acft. Systems ops check normal and no leaks noted at this time. For further details see WO# 20716 on file this station. I certify that this acft has been inspected i/a/w a _:has_:.2;},3 and~ctions and is approyed for return to service.

?trorf~e,~

L I I J__

Reg#: N800TS Model: Beech B200 Serial #: BB-1032 Work Order#: 20716

I_


etAR OIRE INC Aviation Services

1

Hobbs: 546.5 Tach: Total Time: 9044. 7 Date: 215108

l

Replaced pilot's oxygen mask adapter pin 101-384211 -1. Ops check normal and no leaks noted at this time. For further details see WO# 20716 on file this station. ~

~ar~ FAA epair Station

ACOR030C


Aircraft Model ~~~~~~~~~


ttAR OIRE INC. Aviation Services

Hobbs: 557.8 Tach: Total Time: Date: 3/17/08

Installed new LH wing stall strip p/n I3~017~s see WO# 20792 on file this station.

~~~~

I I I ~ I_ Reg #: N800TS Model:Beech B200 Serial #:BB-1032 Work Order #:20846


ttAR OIRE INC. Aviation Services

Hobbs:559.l Tach: Total Time: Date:4/8/08

Replaced RH forward fireshield fire detector.Installed new detector p/n 30-215-8 s/n 4918.Tested detector.Ops

check normal.For further details see WO# 20846 on file this s ·

~~,EJ/.·e,~I ~


FAA epair Station ACOR030C

ttAR 01RE INC. Aviation Services

Hobbs: 575.8 Tach: Total Time: Date: 4/29/08

36

Replaced LH ice vane actuator. lristalled overhauled actuator (CRS# PX2R099L(RS) WO# R081387) p/n 101-389006-11 s/n 2206. Ops check normal. For ::~ ~on file this station.

~~«~ FAA Repair Station

ACOR030C

Documents

MAINTENANCE/INSPECTION ENTRIES