Chat with us, powered by LiveChat

Search results for: 'Engine'

Avref Search Results for: Engine

Description:

LUBRICATING OIL,ENGINE

Manufacturer:

IMPERIAL OIL LTD

PartNum:

ENGINE0IL229-74A

UnitMeasure:

NA

Description:

KIT,REPAIR,ENGINE CHANGE

Manufacturer:

COMTORGAGE CORPORATI

PartNum:

ENGINECHGKT

UnitMeasure:

KT

Description:

ENGINE CVR SET, REFURBISHMEN

Manufacturer:

TEXTRON AVIATION

PartNum:

ENGINECVRREFURB

UnitMeasure:

EA

Description:

NRP,D3-110I

Manufacturer:

VOLVO PENTA OF THE A

PartNum:

ENGINE, DIESEL

UnitMeasure:

EA

Description:

POWER UNIT MOBILE 2

Manufacturer:

BEBCO INDUSTRIES INC

PartNum:

ENGINE,DIESEL

UnitMeasure:

EA

Description:

ENGINEERING-87

Manufacturer:

PARKER HANNIFIN

PartNum:

ENGINEERING-87

UnitMeasure:

EA

Description:

ENGINE,GASOLINE

Manufacturer:

BRIGGS AND STRATTON

PartNum:

ENGINEMOD170452-01TYPE1262

UnitMeasure:

EA

Description:

LUBRICATING OIL,ENGINE

Description:

POWER UNIT MOBILE 2

Description:

KIT,REPAIR,ENGINE CHANGE

Description:

KIT,REPAIR,ENGINE CHANGE

Description:

NRP,D3-110I

Description:

INTERFACE UNIT,DATA TRANSFER

Description:

PISTON,INTERNAL COMBUSTION ENGIN

Description:

LUBRICATING OIL,ENGINE

Description:

LUBRICATING OIL,ENGINE

Description:

LUBRICATING OIL,ENGINE

Description:

LUBRICATING OIL,ENGINE

Description:

LUBRICATING OIL,ENGINE

Description:

LUBRICATING OIL,ENGINE

Description:

LUBRICATING OIL,ENGINE

Description:

LUBRICATING OIL,ENGINE

Description:

LUBRICATING OIL,ENGINE

Description:

LUBRICATING OIL,ENGINE

Description:

LUBRICATING OIL,ENGINE

Description:

LUBRICATING OIL,ENGINE

Description:

LUBRICATING OIL,ENGINE

Description:

LUBRICATING OIL,ENGINE

Description:

LUBRICATING OIL,ENGINE

Description:

LUBRICATING OIL,ENGINE

Description:

POWER UNIT MOBILE 2

Description:

INTERFACE UNIT,DATA TRANSFER

Description:

INTERFACE UNIT,DATA TRANSFER

ReplacedPartNumber:

Honeywell P/N 3502132-8 installed in Honeywell Air Turbine Engine Starter P/N s 3505436-6-1, 3505436-7

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No.: P00812 Rev.: A14 Date: 10/13/2006 or later FAA approved revisions

Models:

747-400 Series, 747-400F Series, 767-300 Series

ReplacedPartNumber:

Honeywell P/N 1-300-077-01 as used for Engines P/N: 1-000-060-13 1-000-060-21 1-000-060-29 1-000-060-30

ApprovalBasis:

Identicality per 14 CFR 21.303 DWG No: 5-1422-700 Rev: None Date: 10/23/2007 or later FAA-approved revisions

Models:

T5313B, T5317A, T5317A-1, T5317B

ReplacedPartNumber:

Honeywell P/N 1-300-174-03 as used for Engine P/N 1-000-060-13

ApprovalBasis:

Identicality per 14 CFR 21.303 DWG No: 15-3058-701 Rev: None Date: 10/24/2007 or later FAA-approved revisions

Models:

T5313B

ReplacedPartNumber:

Honeywell P/N 1-300-588-01 as used for Engines P/N: 1-000-060-13 1-000-060-21 1-000-060-29 1-000-060-30

ApprovalBasis:

Identicality per 14 CFR 21.303 DWG No: 28-1971-700 Rev: None Date: 10/23/2007 or later FAA-approved revisions

Models:

T5313B, T5317A, T5317A-1, T5317B

ReplacedPartNumber:

Honeywell P/N 1-300-173-03 as used for Engines P/N: 1-000-060-13 1-000-060-21 1-000-060-29 1-000-060-30

ApprovalBasis:

Identicality per 14 CFR 21.303 DWG No: 11-2883-700 Rev: None Date: 10/23/2007 or later FAA-approved revisions

Models:

T5313B, T5317A, T5317A-1, T5317B

ReplacedPartNumber:

International Aero Engines AG (IAE) P/N 6A4211C01

ApprovalBasis:

Test and Computations Per 14 CFR 21.303, Dwg No. CGAM10123 Rev. E Dated 6/12/08 or later FAA Approval

Models:

V2522-A5, V2524-A5, V2527-A5 V2527E-A5, V2527M-A5, V2530-A5, V2525-D5, V2528-D5, V2533-A5

ReplacedPartNumber:

International Aero Engines 2A2373

ApprovalBasis:

Identicality per 14 CFR 21.303 (c) (4)

Models:

V2500-A1, V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, V2533-A5, V2525-D5, V2528-D5

ReplacedPartNumber:

International Aero Engines 2A3155

ApprovalBasis:

Identicality per 14 CFR 21.303 (c) (4)

Models:

V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, V2533-A5, V2525-D5, V2528-D5

ReplacedPartNumber:

Modification Part

ApprovalBasis:

STC SA01114NY-D

Models:

Model 208B Caravan

ReplacedPartNumber:

International Aero Engines 2A2374

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, V2525-D5, V2528-D5

ReplacedPartNumber:

International Aero Engines 2A3155

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, V2533-A5, V2525-D5, V2528-D5

ReplacedPartNumber:

Delta Engineering 126-11380-1A

ApprovalBasis:

Identicality per 14 CFR 21.303, licensing agreement, STC ST01363NY

Models:

757-200 series

ReplacedPartNumber:

International Aero Engines 2A1961

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

V2500-A1

ReplacedPartNumber:

International Aero Engines 2A1961

ApprovalBasis:

Identicality per 14 CFR 21.303 (c) (4)

Models:

V2500-A1

ReplacedPartNumber:

International Aero Engines 2A2374

ApprovalBasis:

Identicality per 14 CFR 21.303 (c) (4)

Models:

V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, V2525-D5, V2528-D5

ReplacedPartNumber:

International Aero Engines 2A2373

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

V2500-A1, V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, V2533-A5, V2525-D5, V2528-D5

ReplacedPartNumber:

GE Aircraft Engines 1646M80P02

ApprovalBasis:

Licensing Agreement

Models:

CF6-80E (TC E41NE)

ReplacedPartNumber:

GE Aircraft Engines 1374M96P02

ApprovalBasis:

Licensing Agreement

Models:

CF6-80E, -80A, -80C2 (TC E41NE)

ReplacedPartNumber:

GE Aircraft Engines 1303M21P02

ApprovalBasis:

Licensing Agreement

Models:

CF6-80E (TC E41NE)

ReplacedPartNumber:

GE Aircraft Engines 1383M18P03

ApprovalBasis:

Licensing Agreement

Models:

CF6-80E (TC E41NE)

ReplacedPartNumber:

GE Aircraft Engines 1663M88P01

ApprovalBasis:

Licensing Agreement

Models:

CF6-80E (TC E41NE)

ReplacedPartNumber:

International Aero Engines 2A1380

ApprovalBasis:

-

Models:

V2500-A1 (TC E31NE)

ReplacedPartNumber:

Allison Engine P/N 23062387, AND UNISON P/N 420860A

ApprovalBasis:

Identicality per 14 CFR Part 21, Section 21.303, (c)(4), approval per FAA Form 8110-3, dated 5/9/03 & HLI Dwg 27024-000, Rev IR Dated 11/26/03 or later FAA approved revision

Models:

AE3007A Series Engines

ReplacedPartNumber:

Allison Engine P/N 23066759, AND UNISON P/N 421038

ApprovalBasis:

Identicality per 14 CFR Part 21, Section 21.303, (c)(4), approval per FAA Form 8110-3, dated 5/9/03 & HLI Dwg 23037-000, Rev IR Dated 11/26/03 or later FAA approved revision

Models:

AE3007A Series Engines

ReplacedPartNumber:

Allison Engine P/N 23070216 and Unison P/N 421183

ApprovalBasis:

Identicality per 14 CFR Part 21, Section 21.303, (c)(4), approval per FAA Form 8110-3, dated 5/9/03 & HLI Dwg 27045-000, Rev IR Dated 11/26/03 or later FAA approved revision

Models:

AE3007A Series Engines

ReplacedPartNumber:

ALLISON ENGINE P/N 23061469, AND UNISON P/N 420512-C

ApprovalBasis:

Identicality per 14 CFR Part 21, Section 21.303, (c)(4), approval per FAA Form 8110-3, dated 5/9/03 & HLI Dwg 27026-000, Rev IR Dated 11/26/03 or later FAA approved revision

Models:

AE3007A Series Engines

ReplacedPartNumber:

ALLISON ENGINE P/N 23061470, AND UNISON P/N 420513B

ApprovalBasis:

Identicality per 14 CFR Part 21, Section 21.303, (c)(4), approval per FAA Form 8110-3, dated 5/9/03 & HLI Dwg 27025-000, Rev IR Dated 11/26/03 or later FAA approved revision

Models:

AE3007A Series Engines

ReplacedPartNumber:

Modification Part

ApprovalBasis:

Test Report and/ or computations IAW FAR 21.303 (c)4

Models:

TCM/Bendix S4-1200 series magnetos where used on Lycoming TIO-360 series

ReplacedPartNumber:

Modification Part

ApprovalBasis:

Test Report and/ or computations IAW FAR 21.303 (c)4

Models:

TCM/Bendix S4-1200 series magnetos where used on Lycoming TIO-360 series

ReplacedPartNumber:

Modification Part

ApprovalBasis:

Test Report and/ or computations IAW FAR 21.303 (c)4

Models:

TCM/Bendix S4-1200 series magnetos where used on Lycoming TIO-360 series

ReplacedPartNumber:

International Aero Engines 5L0026

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

V2500-A1

ReplacedPartNumber:

Allied Engine 2-193-303-08

ApprovalBasis:

Identicality per FAR 21.303(c)

Models:

LF507-1F

ReplacedPartNumber:

Allison Engine 23061824

ApprovalBasis:

Identicality per FAR 21.303(c)

Models:

250-C20, -C20B, -C20J

ReplacedPartNumber:

Allied Engine 2-193-303-06

ApprovalBasis:

Identicality per FAR 21.303(c)

Models:

LF507-1F

ReplacedPartNumber:

Internationa Aero Engines (IAE) 2A2480

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

V2500-A1

ReplacedPartNumber:

Allied Engine 2-193-303-08

ApprovalBasis:

Identicality per FAR 21.303(c)

Models:

LF507-1F

ReplacedPartNumber:

Allison Engine 23064693

ApprovalBasis:

Identicality per FAR 21.303(c)

Models:

250-C47B

ReplacedPartNumber:

Allison Engine 23065132

ApprovalBasis:

Identicality per FAR 21.303(c)

Models:

250C-18A, C18B, C18C, B15, B17 Series, B17F Series, C20 Series, C20R Series

ReplacedPartNumber:

2A2159, 2A2160, 2A2224 (International Aero Engines)

ApprovalBasis:

per 14 CFR 21.303 DWG. No: 190130 Rev: Date: 5-28-03 or later FAA approved revision

Models:

V2500- A1, V2500-A5, V2500-D5

ReplacedPartNumber:

5W8201 (International Aero Engines)

ApprovalBasis:

Test and computations per 14 CFR 21.303 DWG. No: 5W8201PI Rev.: Date: 2-2-06 or later FAA approved revision

Models:

V2500-A1, V2500-A5, V2500-D5

ReplacedPartNumber:

Allison Engine 23057883

ApprovalBasis:

Identicality per FAR 21.303(c)

Models:

250-C40B, 250-C47B

ReplacedPartNumber:

Allison Engine 23064684

ApprovalBasis:

Identicality per FAR 21.303(c)

Models:

250-C40B

ReplacedPartNumber:

Allison Engine 23064650

ApprovalBasis:

Identicality per FAR 21.303(c)

Models:

250-C47B

ReplacedPartNumber:

Allison Engine Company 23066750 Dwg. 23066750 Revision -

ApprovalBasis:

Identicality per FAR 21.303(c)

Models:

250-C30R/3, C40B, C47B, C47M

ReplacedPartNumber:

5W8201 (International Aero Engines)

ApprovalBasis:

Test and computations per 14 CFR 21.303 DWG. No 5W8201P1 Rev. Date 2-2-06 or later FAA approved revision

Models:

V2500-AI, V2500-A5, V2500-D5

ReplacedPartNumber:

Allison Engine 23064686

ApprovalBasis:

Identicality per FAR 21.303(c)

Models:

250-C47B

ReplacedPartNumber:

2A2224 (International Aero Engines)

ApprovalBasis:

Tests and Computations per 14 CFR 21.303 DWG. No: 190130 Rev: Date: 5-28-03 or later FAA approved revision

Models:

V2500

ReplacedPartNumber:

Allison Engine 23064684

ApprovalBasis:

Identicality per FAR 21.303(c)

Models:

250-C40B

ReplacedPartNumber:

Allison Engine 23064699

ApprovalBasis:

Identicality per FAR 21.303(c)

Models:

250-C40B

ReplacedPartNumber:

Allied Engine 2-193-303-07

ApprovalBasis:

Identicality per FAR 21.303(c)

Models:

LF507-1F

ReplacedPartNumber:

Allison Engine 23064686

ApprovalBasis:

Identicality per FAR 21.303(c)

Models:

250-C47B

ReplacedPartNumber:

Allison Engine 23057336

ApprovalBasis:

Identicality per FAR 21.303(c)

Models:

250-C20R/2

ReplacedPartNumber:

Allied Engine 2-193-303-04

ApprovalBasis:

Identicality per FAR 21.303(c)

Models:

LF507-1F

ReplacedPartNumber:

Allison Engine 23065134

ApprovalBasis:

Identicality per FAR 21.303(c)

Models:

250-C30, -C30M, -C30S, -C30R

ReplacedPartNumber:

Allied Engine 2-193-303-05

ApprovalBasis:

Identicality per FAR 21.303(c)

Models:

LF507-1F

ReplacedPartNumber:

5W8204 (International Aero Engines)

ApprovalBasis:

Test and computations per 14 CFR 21.303 DWG. No 5W8204PI Rev. Date 2-2-06 or later FAA approved revision

Models:

V2500-A1, V2500-A5

ReplacedPartNumber:

2A2159, 2A2160, 2A2224 (International Aero Engines)

ApprovalBasis:

per 14 CFR 21.303 DWG. No: 190130 Rev: Date: 5-28-03 or later FAA approved revision

Models:

V2500- A1, V2500-A5, V2500-D5

ReplacedPartNumber:

5W8204 (International Aero Engines)

ApprovalBasis:

Test and computations per 14 CFR 21.303 DWG. No: 5W8204PI Rev.: Date: 2-2-06 or later FAA approved revision

Models:

V2500-A1, V2500-A5

ReplacedPartNumber:

Allison Engine 23065133

ApprovalBasis:

Identicality per FAR 21.303(c)

Models:

250-C28, C28B, C28C, C30G, C30L, C30P, C30U, C30G2, C30R1

ReplacedPartNumber:

Allison Engine 23064650

ApprovalBasis:

Identicality per FAR 21.303(c)

Models:

250-C47B

ReplacedPartNumber:

Allison Engine 23057337

ApprovalBasis:

Identicality per FAR 21.303(c)

Models:

250-C20R/2

ReplacedPartNumber:

Allison Engine 23064693

ApprovalBasis:

Identicality per FAR 21.303(c)

Models:

250-C47B

ReplacedPartNumber:

Internationa Aero Engines (IAE) 2A2392

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

V2500-A1

ReplacedPartNumber:

Allied Engine 2-193-303-06

ApprovalBasis:

Identicality per FAR 21.303(c)

Models:

LF507-1F

ReplacedPartNumber:

Allison Engine 23064699

ApprovalBasis:

Identicality per FAR 21.303(c)

Models:

250-C40B

ReplacedPartNumber:

Allied Engine 2-193-303-04

ApprovalBasis:

Identicality per FAR 21.303(c)

Models:

LF507-1F

ReplacedPartNumber:

Allied Engine 2-193-303-06

ApprovalBasis:

Identicality per FAR 21.303(c)

Models:

LF507-1F

ReplacedPartNumber:

GE/Gates P/N 41BO04AD07G3, Grimes P/N MISC-060, Grimes P/N MISC-0615, Engineered Magnetics P/N 803911-1, Saft P/N 16623-1, Marathon Power S103 P/N 25503-025

ApprovalBasis:

Identicality per FAR 21.303(c) as verified by DER, Drawing. No. A-1165A, Rev. Orig., dated 04-07-97, or Later FAA Approval

Models:

DC-9, MD-80 Series

ReplacedPartNumber:

Aeronautical Engineers, Inc., AE727-1-025-11 Piston Rod as shown on Aero- nautical Engineers, Inc., Dwg. AE727-1-025 Rev. F, dated February 7, 1985.

ApprovalBasis:

Testing as required by FAR 21.303C(4) as outlined in Aero Accessories Inc., Report No. 120189, dated January 10, 1991, and Test Report No. 70191, dated July 1, 1991.

Models:

Eligible for installation in Monarch/ Aeronautical Engineers Latch Lock Cylinder, P/N AE-727-1-100 when installed on 727 Series and 727-100 Series Air- craft with STC SA1368SO Incorporated.

ReplacedPartNumber:

Grumman Aircraft Engineering Corp., Clips, Wing Center Section Box, 12317-7

ApprovalBasis:

Test and computations per CFR part 21.303(c)

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp., Clips, Wing Center Section Box, 12317-6

ApprovalBasis:

Test and computations per CFR part 21.303(c)

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp. Stringer 12303-4

ApprovalBasis:

Identicality per 14 CFR 21.303(c)

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp., Clips, Wing Center Section Box, 12317-26

ApprovalBasis:

Test and computations per CFR part 21.303(c)

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp Bulkhead 12377

ApprovalBasis:

Test and computation per CFR part 21.303 (c), Dwg. No. 12377, Rev. 0, dated 03/30/02, or later FAA approval

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp., Clips, Wing Center Section Box, 12317-22

ApprovalBasis:

Test and computations per CFR part 21.303(c)

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp. Stringer 12303-5

ApprovalBasis:

Identicality per 14 CFR 21.303(c)

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp Hand Hole, Tapping Ring 12427-1

ApprovalBasis:

Test and computation per CFR part 21.303 (c), Dwg. No. 12427, Rev. 0, dated 09/18/03 or later FAA approval

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp Bulkhead 12374

ApprovalBasis:

Test and computation per CFR part 21.303 (c), Dwg. No. 12374F, Rev. 0, dated 03/22/02, or later FAA approval

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp., Clips, Wing Center Section Box, 12317-14

ApprovalBasis:

Test and computations per CFR part 21.303(c)

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp Brackets, Wing Flap 12339-2

ApprovalBasis:

Identicality per CFR part 21.303 (c) 4, Dwg. No. 12339, Rev. 0, Dated 11/03/03 or later FAA approval

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp. Stringer 12303-2

ApprovalBasis:

Identicality per 14 CFR 21.303(c)

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp Bulkhead 12375

ApprovalBasis:

Test and computation per CFR part 21.303 (c), Dwg. No. 12375, Rev. 0, dated 03/30/02, or later FAA approval

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp., Clips, Wing Center Section Box, 12317-3

ApprovalBasis:

Test and computations per CFR part 21.303(c)

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp Bulkhead 12307-8

ApprovalBasis:

Test and computation per CFR part 21.303 (c)

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp Bulkhead 12307-6

ApprovalBasis:

Test and computation per CFR part 21.303 (c)

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp Bulkhead 12373

ApprovalBasis:

Test and computation per CFR part 21.303 (c), Dwg. No. 12373, Rev. 0, dated 03/10/02, or later FAA approval

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp., Clips, Wing Center Section Box, 12317-25

ApprovalBasis:

Test and computations per CFR part 21.303(c)

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp Bulkhead 12378

ApprovalBasis:

Test and computation per CFR part 21.303 (c), Dwg. No. 12378, Rev. 0, dated 03/30/02, or later FAA approval

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp. Stringer 12003-35

ApprovalBasis:

Identicality per 14 CFR 21.303(c)

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp Bulkhead 12307-9

ApprovalBasis:

Test and computation per CFR part 21.303 (c)

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp Fuel Tank Outlet Valve 12338-2

ApprovalBasis:

Test and computation per 14 CFR part 21.303 (c) 4, Dwg. No. 12338-2, Rev. 0, dated 09/22/03 or later FAA approval

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp Bulkhead 12314

ApprovalBasis:

Test and computation per CFR part 21.303 (c)

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp Bulkhead 12307-6

ApprovalBasis:

Test and computation per CFR part 21.303 (c)

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp., Clips, Wing Center Section Box, 12317-1

ApprovalBasis:

Test and computations per CFR part 21.303(c)

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp., Clips, Wing Center Section Box, 12317-10

ApprovalBasis:

Test and computations per CFR part 21.303(c)

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp. Sringer 12003-34

ApprovalBasis:

Identicality per 14 CFR 21.303(c)

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp Brackets, Wing Flap 12339-3

ApprovalBasis:

Identicality per CFR part 21.303 (c) 4, Dwg. No. 12339, Rev. 0, Dated 11/03/03 or later FAA approval

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp., Clips, Wing Center Section Box, 12317-16

ApprovalBasis:

Test and computations per CFR part 21.303(c)

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp., Clips, Wing Center Section Box, 12317-15

ApprovalBasis:

Test and computations per CFR part 21.303(c)

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp Bulkhead 12372

ApprovalBasis:

Test and computation per CFR part 21.303 (c), Dwg. No. 12372, Rev. 0, dated 03/08/02, or later FAA approval

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp., Clips, Wing Center Section Box, 12317-2

ApprovalBasis:

Test and computations per CFR part 21.303(c)

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp Bulkhead 12312

ApprovalBasis:

Test and computation per CFR part 21.303 (c)

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp., Clips, Wing Center Section Box, 12317-31

ApprovalBasis:

Test and computations per CFR part 21.303(c)

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp. Stringer 12303-11

ApprovalBasis:

Identicality per 14 CFR 21.303(c)

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp Brackets, Wing Flap 12339-1

ApprovalBasis:

Identicality per CFR part 21.303 (c) 4, Dwg. No. 12339, Rev. 0, Dated 11/03/03 or later FAA approval

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp. Stringer 12303-3

ApprovalBasis:

Identicality per 14 CFR 21.303(c)

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp., Clips, Wing Center Section Box, 12317-12

ApprovalBasis:

Test and computations per CFR part 21.303(c)

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp., Clips, Wing Center Section Box, 12317-39

ApprovalBasis:

Test and computations per CFR part 21.303(c)

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp Beam Assembly, Wing Flap 12340-1

ApprovalBasis:

Test and computation per CFR part 21.303 (c) 4, Dwg. No. 12340-1, Rev. 0, dated11/03/03 or later FAA approval

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp., Clips, Wing Center Section Box, 12317-27

ApprovalBasis:

Test and computations per CFR part 21.303(c)

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp Bulkhead 12311,

ApprovalBasis:

Test and computation per CFR part 21.303 (c)

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp. Stringer 12303-9

ApprovalBasis:

Identicality per 14 CFR 21.303(c)

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp Bulkhead 12370

ApprovalBasis:

Test and computation per CFR part 21.303 (c), Dwg. No. 12370, Rev. 0, dated 03/07/02,or later FAA approval

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp Bulkhead 12316

ApprovalBasis:

Test and computation per CFR part 21.303 (c)

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp Hand Hole, Tapping Ring 12350

ApprovalBasis:

Test and computation per CFR part 21.303 (c), Dwg. No. 12350, Rev. 0, dated 09/18/03 or later FAA approval

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Aeronautical Engineers, Inc. AE727-1-025-11 Piston Rod as shown on Dwg AE727-1-025

ApprovalBasis:

Test IAW FAR 21.303(c)(4)

Models:

Eligible for installation in Monarch/Aeronautical Engineers Latch Lock Cylinder AE727-1-100 when installed on 727 Series and 727-100 Series Aircraft with STC SA1368SO Incorporated

ReplacedPartNumber:

Grumman Aircraft Engineering Corp Bulkhead 12307-5

ApprovalBasis:

Test and computation per CFR part 21.303 (c)

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp., Clips, Wing Center Section Box, 12317-13

ApprovalBasis:

Test and computations per CFR part 21.303(c)

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp., Clips, Wing Center Section Box, 12317-38

ApprovalBasis:

Test and computations per CFR part 21.303(c)

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp. Stringer 12303-8

ApprovalBasis:

Identicality per 14 CFR 21.303(c)

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp., Clips, Wing Center Section Box, 12317-5

ApprovalBasis:

Test and computations per CFR part 21.303(c)

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp., Clips, Wing Center Section Box, 12317-4

ApprovalBasis:

Test and computations per CFR part 21.303(c)

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp Bulkhead 12307-8

ApprovalBasis:

Test and computation per CFR part 21.303 (c)

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp Bulkhead 12307-5

ApprovalBasis:

Test and computation per CFR part 21.303 (c)

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp. Stringer 12303-6

ApprovalBasis:

Identicality per 14 CFR 21.303(c)

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp Fuel Tank Vent Fitting 12TG-D

ApprovalBasis:

Test and computation per 14 CFR part 21.303 (c) 4, Dwg. No. 12TG-D, Rev. 0, dated 09/22/03 or later FAA approval

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp., Clips, Wing Center Section Box, 12317-11

ApprovalBasis:

Test and computations per CFR part 21.303(c)

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Modification Part

ApprovalBasis:

Identicality per 14 CFR 21.303, STC SA4837NM

Models:

TS-2A (S2F-1T)

ReplacedPartNumber:

Grumman Aircraft Engineering Corp Bulkhead 12374

ApprovalBasis:

Test and computation per CFR part 21.303 (c), Dwg. No. 12374, Rev. 0, dated 03/22/02, or later FAA approval

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

GE Aircraft Engines 683L307G09

ApprovalBasis:

Licensing Agreement

Models:

CF6-80A, CF6-80C2

ReplacedPartNumber:

Grumman Aircraft Engineering Corp Bulkhead, partial, 12353

ApprovalBasis:

Test and computation per CFR part 21.303 (c)

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Ge Aircraft Engines 683L307G12

ApprovalBasis:

Licensing Agreement

Models:

CF6-80A, CF6-80C2

ReplacedPartNumber:

GE Aircraft Engines 4121T67P04

ApprovalBasis:

Identicality per 14 CFR 21.303, licensing agreement between Honeywell International Inc. and GE Aircraft Engines, letter dated 7/23/03 DWG No: 3291552 Rev: C Dated: 11/20/02 or later FAA approved revisions

Models:

CF34-8C1, CF34-8C5 (All Models)

ReplacedPartNumber:

Grumman Aircraft Engineering Corp., Clips, Wing Center Section Box, 12317-21

ApprovalBasis:

Test and computations per CFR part 21.303(c)

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp Bulkhead 12307-9

ApprovalBasis:

Test and computation per CFR part 21.303 (c)

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp Bulkhead 12379

ApprovalBasis:

Test and computation per CFR part 21.303 (c), Dwg. No. 12379, Rev. 0, dated 05/12/02, or later FAA approval

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp Bulkhead 12380

ApprovalBasis:

Test and computation per CFR part 21.303 (c), Dwg. No. 12380, Rev. 0, dated 05/12/02, or later FAA approval

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

GE Aircraft Engines 683L307G08

ApprovalBasis:

Licensing Agreement

Models:

CF6-80A, CF6-80C2

ReplacedPartNumber:

Grumman Aircraft Engineering Corp. Stringer 12303-1

ApprovalBasis:

Identicality per 14 CFR 21.303(c)

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

GE Aircraft Engines 4121T67P03

ApprovalBasis:

Identicality per 14 CFR 21.303, licensing agreement between Honeywell International Inc. and GE Aircraft Engines, letter dated 7/23/03 DWG No: 3291552 Rev: C Dated: 11/20/02 or later FAA approved revisions

Models:

CF34-8D, CF34-8E (All Models)

ReplacedPartNumber:

Grumman Aircraft Engineering Corp., Clips, Wing Center Section Box, 12317-20

ApprovalBasis:

Test and computations per CFR part 21.303(c)

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp Bulkhead 12307-7

ApprovalBasis:

Test and computation per CFR part 21.303 (c)

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp., Clips, Wing Center Section Box, 12317-30

ApprovalBasis:

Test and computations per CFR part 21.303(c)

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp. Stringer 12303-12

ApprovalBasis:

Identicality per 14 CFR 21.303(c)

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp Bulkhead 12307-7

ApprovalBasis:

Test and computation per CFR part 21.303 (c)

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp., Clips, Wing Center Section Box, 12317-23

ApprovalBasis:

Test and computations per CFR part 21.303(c)

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp. Stringer 12303-10

ApprovalBasis:

Identicality per 14 CFR 21.303(c)

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp Bulkhead 12371

ApprovalBasis:

Test and computation per CFR part 21.303 (c), Dwg. No. 12371, Rev. 0, dated 03/08/02, or later FAA approval

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp., Clips, Wing Center Section Box, 12317-24

ApprovalBasis:

Test and computations per CFR part 21.303(c)

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp., Clips, Wing Center Section Box, 12317-36

ApprovalBasis:

Test and computations per CFR part 21.303(c)

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Modification Part

ApprovalBasis:

STC SA2069CE-D

Models:

250

ReplacedPartNumber:

Grumman Aircraft Engineering Corp., Clips, Wing Center Section Box, 12317-8

ApprovalBasis:

Test and computations per CFR part 21.303(c)

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp. Stringer 12303-7

ApprovalBasis:

Identicality per 14 CFR 21.303(c)

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp Bulkhead 12376

ApprovalBasis:

Test and computation per CFR part 21.303 (c), Dwg. No. 12376, Rev. 0, dated 03/30/02, or later FAA approval

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp Fuel Filler Assembly 13452

ApprovalBasis:

Test and computation per 14 CFR part 21.303 (c) 4, Dwg. No. 13452, Rev. 0, dated 09/22/03 or later FAA approval

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

GE Aircraft Engines 1853M56P09

ApprovalBasis:

Identicality per 14 CFR 21.303, licensing agreement

Models:

CFM56-7B18, -7B20, -7B20/2, -7B22, -7B22/B1, -7B22/2, -7B24, -7B24/B1, -7B24/2, -7B26, -7B26/B1, -7B26/2, -7B27, -7B27/B1, -7B27/B3, -7B27/2, -7B27A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp Bulkhead 12313

ApprovalBasis:

Test and computation per CFR part 21.303 (c)

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp., Clips, Wing Center Section Box, 12317-9

ApprovalBasis:

Test and computations per CFR part 21.303(c)

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp Brackets, Wing Flap 12339-4

ApprovalBasis:

Identicality per CFR part 21.303 (c) 4, Dwg. No. 12339, Rev. 0, Dated 11/03/03 or later FAA approval

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

GE Aircraft Engines 1583M30P05

ApprovalBasis:

Identicality per 14 CFR 21.303, licensing agreement between Honeywell International Inc. and GE Aircraft Engines, letter dated 8/11/03 DWG No: 50E40 Rev: W Dated: 3/14/03 or later FAA approved revisions

Models:

CF6-80C2 (All Models)

ReplacedPartNumber:

Grumman Aircraft Engineering Corp., Clips, Wing Center Section Box, 12317-37

ApprovalBasis:

Test and computations per CFR part 21.303(c)

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Grumman Aircraft Engineering Corp Hand Hole, Tapping Ring 12427-2

ApprovalBasis:

Test and computation per CFR part 21.303 (c), Dwg. No. 12427, Rev. 0, dated 09/18/03 or later FAA approval

Models:

JRF-1, JRF-2, JRF-3, JRF-4, JRF-5, JRF-6B, G21A

ReplacedPartNumber:

Woodward Aircraft Engine Systems 180312

ApprovalBasis:

Test & Computation per 14 CFR 21.303(c)(4) Dwg No 6137 Rev N/C Date 1/27/04 or later FAA approved revisions

Models:

A300-100, -200, -600 series, A310-200, -300 series | 737-300, -400, -500 series, 747SR, 747-200B, -200F, -200C, -300, -400, -400D, -400F series, 757-200, -200CB, -200PF, -300 series, 767-200, -300, -300F, -400ER series | CFM56-2, -2A, -2B series, CFM56-3, -3B, 3C | CF6-6D, 6K series, CF6-45 series, CF6-50A, -50C, -50E series, CF6-80A series, CF6-80C2A series, CF6-80C2B series | DC-10-10, -10F, -15, -30, -30F series, MD-10-10F & -30F series | RB211-535C, -535E series

ReplacedPartNumber:

Pratt & Whitney Engines 1A4828

ApprovalBasis:

Test and Computations per 14 CFR 21.303(c)

Models:

PW2037, PW2040, PW2240, PW2337, PW4050, PW4050-3, PW4052, PW4052-3, PW4056, PW4056-3, PW4060, PW4060-3, PW4060A, PW4060A-3, PW4060C, PW4060C-3,PW4062-3, PW4152, PW4152-3, PW4156, PW4156-3, PW4156A, PW4156A-3, PW4158, PW4158-3,, PW4460, PW4460-3, PW4462, PW4462-3

ReplacedPartNumber:

Pratt & Whitney Engines 596955

ApprovalBasis:

Test and Computations per 14 CFR 21.303(c)

Models:

JT8D -1, -1A, -1B, -7, -7A, -7B, -9, -9A, -11, -15, -15A, -17, -17A, -17R, -17AR, -209, -217, -217A, -217C and -219, JT8D-1, 1B, 1A, 7, 7A, 7B, 9, 9A, 11, 15, 15A, 17, 17A, 17AR, 209, 217, 217A, 217C, 219

ReplacedPartNumber:

CFM International Engines 1522M55P04

ApprovalBasis:

Test and Computations per 14 CFR 21.303(c)

Models:

Engine Models: CFM56 -2-C1/-C2/-C3/-C5/-C6/CFM-2A-2/-3, CMF-2B-1, CFM56-3-B1, CFM56-3B-2, & CFM56-3C1, CFM56 -2-C1/-C2/-C3/-C5/-C6/CFM-2A-2/-3, CMF-2B-1, CFM56-3-B1, CFM56-3B-2, & CFM56-3C1

ReplacedPartNumber:

Pratt & Whitney Engines 781981

ApprovalBasis:

Test and Computations per 14 CFR 21.303(c)

Models:

JT8D -1, -1A, -1B, -7, -7A, -7B, -9, -9A, -11, -15A, -17, -17A, -17AR, -209, -217, -217A, -217C, and -219**, JT8D-1, -1A, -1B, -7, -7A, -7B, -9, -9A, -11, -15, -15A, -17, -17A, -17R, -17AR, -209, -217, -217A, -217C, -219

ReplacedPartNumber:

Pratt & Whitney Engines 789362

ApprovalBasis:

Test and Computations per 14 CFR 21.303(c)

Models:

JT8D-209, -217, and -217A

ReplacedPartNumber:

Pratt & Whitney Engines 5002918-01

ApprovalBasis:

Test and Computations per 14 CFR 21.303(c)

Models:

JT8D -1, -1A, -1B, -7, -7A, -7B, -9, -9A

ReplacedPartNumber:

Pratt & Whitney Engines 50J537

ApprovalBasis:

Test and Computations per 14 CFR 21.303(c)

Models:

PW4050, PW4052, PW4052(-3), PW4056, PW4056(-3), PW4060, PW4060(-3), PW4060A, PW4060A(-3), PW4060C, PW4060C(-3),, PW4062(-3), PW4152, PW4152(-3), PW4156, PW4156A, PW4156A(-3), PW4158, PW4158(-3), PW4460, PW4460(-3), PW4462, PW4462(-3)

ReplacedPartNumber:

Pratt & Whitney Engines 652311

ApprovalBasis:

Test and Computations per 14 CFR 21.303(c)

Models:

JT9D-3A, -7,-7A,-7H,-7ASP,-7AH,-7F,-7J,-20,-20J,-7R4D1,-7R4E1, -7R4H1,-7R4D,-7R4E,-7R4E4,-7R4G2,,-7Q,-7Q3,-59A,-70A, JT9D -3A, -7, -7A, -7F, -7H, -7AH, -7J, -20, -20J, -7R4D, -7R4E, -7R4E4, -7R4D1, -7R4E1, -7R4H1, -7Q, -7Q3, -59A, -70A, and -7R4G2

ReplacedPartNumber:

Pratt & Whitney Engines 740291

ApprovalBasis:

Test and Computations per 14 CFR 21.303(c)

Models:

JT9D -3A, -7, -7A, -7F, -7H, -7AH, -7J, -20, -20J, -7R4D, -7R4E, -7R4E4, -7R4D1, and -7R4E1

ReplacedPartNumber:

Pratt & Whitney Engines 652309

ApprovalBasis:

Test and Computations per 14 CFR 21.303(c)

Models:

JT9D -3A, -7, -7A, -7F, -7H, -7AH, -7J, -20, -20J, -7R4D, -7R4E, -7R4E4, -7R4D1, -7R4E1, -7R4H1, -7Q, -7Q3, -59A, -70A, and -7R4G2, JT9D-3A, -7,-7A,-7H,-7ASP,-7AH,-7F,-7J,-20,-20J,-7R4D1,-7R4E1, -7R4H1,-7R4D,-7R4E,-7R4E4,-7R4G2,,-7Q,-7Q3,-59A,-70A

ReplacedPartNumber:

Pratt & Whitney Engines 50H765

ApprovalBasis:

Test and Computations per 14 CFR 21.303(c)

Models:

PW4050, PW4050-3, PW4052, PW4052-3, PW4056, PW4056-3, PW4060, PW4060-3, PW4060A, PW4060A-3, PW4060C, PW4062-3, PW4152, PW4152-3, PW4156, PW4156-3, PW4156A, PW4156A-3, PW4158, PW4158-3, PW4460, PW4460-3, PW4462, PW4462-3, PW4164, PW4168

ReplacedPartNumber:

Pratt & Whitney Engines 438674

ApprovalBasis:

Test and Computations per 14 CFR 21.303(c)

Models:

JT8D-1, -1A, -1B, -7,-7A, and -7B

ReplacedPartNumber:

Pratt & Whitney Engines 776610

ApprovalBasis:

Test and Computations per 14 CFR 21.303(c)

Models:

JT8D -1, -1A, -1B, -7, -7A, -7B, -9, -9A, -11, -15, -15A, -17, -17A, --17AR., JT8D -1, -1A, -1B, -7, -7A, -7B, -9, -9A, -11, -15, -15A, -17, -17A, -17R, -17AR.

ReplacedPartNumber:

Pratt & Whitney Engines 1B5427

ApprovalBasis:

Test and Computations per 14 CFR 21.303(c)

Models:

PW2037, PW2040, PW2037, PW2040, PW2240, PW2337

ReplacedPartNumber:

Pratt & Whitney Engines 54H727

ApprovalBasis:

Test and Computations per 14 CFR 21.303(c)

Models:

PW4000: PW4050, PW4052, PW4052(-3), PW4056, PW4060, PW4060(-3), PW4060A, PW4060C (-3), PW4060C, PW4152, PW4152(-3), PW4156, PW4156A, PW4156A (-3), PW4158, PW4158 (-3), PW4164, PW4168, PW4460, PW4460(-3), PW4462, PW4462(-3)

ReplacedPartNumber:

Pratt & Whitney Engines 761025

ApprovalBasis:

Test and Computations per 14 CFR 21.303(c)

Models:

JT9D -3A, -7, -7A, -7F, -7H, -7AH, -7J, -20, -20J, 7R4D, -7R4E, and -7R4E4

ReplacedPartNumber:

Pratt & Whitney Engines 776615

ApprovalBasis:

Test and Computations per 14 CFR 21.303(c)

Models:

JT8D -1, -1A, -1B, -7, -7A, -7B, -9, -9A, -11, -15, -15A, -17, -17A, -17R, -17AR., JT8D -1, -1A, -1B, -7, -7A, -7B, -9, -9A, -11, -15, -15A, -17, -17A, --17AR

ReplacedPartNumber:

Pratt & Whitney Engines 50J536

ApprovalBasis:

Test and Computations per 14 CFR 21.303(c)

Models:

PW4062(-3), PW4152, PW4152(-3), PW4156, PW4156A, PW4156A(-3), PW4158, PW4158(-3), PW4460, PW4460(-3), PW4462, PW4462(-3, PW4050, PW4052, PW4052(-3), PW4056, PW4056(-3), PW4060, PW4060(-3), PW4060A, PW4060A(-3), PW4060C, PW4060C(-3), )

ReplacedPartNumber:

Pratt & Whitney Engines 50J538

ApprovalBasis:

Test and Computations per 14 CFR 21.303(c)

Models:

PW4050, PW4052, PW4052(-3), PW4056, PW4056(-3), PW4060, PW4060(-3), PW4060A, PW4060A(-3), PW4060C, PW4060C(-3), PW4062(-3), PW4152, PW4152(-3), PW4156, PW4156A, PW4156A(-3), PW4158, PW4158(-3), PW4460, PW4460(-3), PW4462, PW4462(-3), PW4164, PW4168

ReplacedPartNumber:

Pratt & Whitney Engines 50J439

ApprovalBasis:

Test and Computations per 14 CFR 21.303(c)

Models:

PW4152, PW4152(-3), PW4156, PW4156A, PW4156A(-3), PW4158, PW4158(-3), PW4460, PW4460(-3), PW4462, PW4462(-3)., PW4052, PW4052(-3), PW4056, PW4056(-3), PW4060, PW4060(-3), PW4060A, PW4060A(-3), PW4060C, PW4060C(-3),

ReplacedPartNumber:

Pratt & Whitney Engines 676769

ApprovalBasis:

Test and Computations per 14 CFR 21.303(c)

Models:

JT8D -1, -1A, -1B, -7, -7A, -7B, -9 and -9A

ReplacedPartNumber:

Pratt & Whitney Engines 453778

ApprovalBasis:

Test and Computations per 14 CFR 21.303(c)

Models:

JT8D-1, 1B, 1A, 7, 7A, 7B, 9, 9A, 11, 15, 15A, 17A, 17R, 17AR, 209, 217, 217A, 217C, 219, JT8D -1, -1A, -1B, -7, -7A, -7B, -9, -9A, -11, -15, -15A, -17, -17A, -17R, -17AR, -209, -217, -217A, -217C and -219

ReplacedPartNumber:

Pratt & Whitney Engines 674160

ApprovalBasis:

Test and Computations per 14 CFR 21.303(c)

Models:

JT8D -1, -1A, -1B, -7, -7A, -7B, -9, -9A and -11

ReplacedPartNumber:

Pratt & Whitney Engines 761680

ApprovalBasis:

Test and Computations per 14 CFR 21.303(c)

Models:

JT9D -3A, -7, -7A, -7A(SP), -7F, -7H, -7AH, -7J, -20, -20J, -7R4D, -7R4E, -7R4E4, -7R4D1, -7R4E1, 7R4G2 and -7R4H1

ReplacedPartNumber:

Pratt & Whitney Engines 761024

ApprovalBasis:

Test and Computations per 14 CFR 21.303(c)

Models:

JT9D -3A, -7, -7A, -7F, -7H, -7AH, -7J, -20, -20J, 7R4D, -7R4E, and -7R4E4

ReplacedPartNumber:

Pratt & Whitney Engines 789359

ApprovalBasis:

Test and Computations per 14 CFR 21.303(c)

Models:

JT8D-209, -217, and -217A

ReplacedPartNumber:

Pratt & Whitney Engines 50J106

ApprovalBasis:

Test and Computations per 14 CFR 21.303(c)

Models:

PW4062(-3), PW4152, PW4152(-3), PW4156, PW4156(-3), PW4156A, PW4156A(-3), PW4158, PW4158(-3), PW4460, PW4460(-3), PW4462, PW4462(-3), PW4050, PW4052, PW4052(-3), PW4056, PW4056(-3), PW4060, PW4060(-3), PW4060A, PW4060A(-3), PW4060C, PW4060C(-3),

ReplacedPartNumber:

Pratt & Whitney Engines 715930

ApprovalBasis:

Test and Computations per 14 CFR 21.303(c)

Models:

JT8D -1, -1A, -1B, -7, -7A and -7B

ReplacedPartNumber:

Pratt & Whitney Engines 522887

ApprovalBasis:

Test and Computations per 14 CFR 21.303(c)

Models:

JT8D-1, 1A, 1B, 7, 7A, 7B, 9, 9A, 11, 15, 17, 17R, JT8D -1, -1A, -1B, -7, -7A, -7B, -9, -9A and -11

ReplacedPartNumber:

Pratt & Whitney Engines 51H147-01

ApprovalBasis:

Test and Computations per 14 CFR 21.303(c)

Models:

PW4050, PW4050-3, PW4052, PW4052-3, PW4056, PW4056-3, PW4060, PW4060-3, PW4060A, PW4060A-3, PW4060C, PW4062-3, PW4152, PW4152-3, PW4156, PW4156-3, PW4156A, PW4156A-3, PW4158, PW4158-3, PW4460, PW4460-3, PW4462, PW4462-3, PW4164, PW4168

ReplacedPartNumber:

Pratt & Whitney Engines 5002917-01

ApprovalBasis:

Test and Computations per 14 CFR 21.303(c)

Models:

JT8D -1, -1A, -1B, -7, -7A, -7B, -9, -9A

ReplacedPartNumber:

Pratt & Whitney Engines 629714

ApprovalBasis:

Test and Computations per 14 CFR 21.303(c)

Models:

JT9D-3A,-7,-7A, -7AH,-7F,-7H,-7J,-20,-20J, -7R4D,-7R4E, and -7R4E4.

ReplacedPartNumber:

Pratt & Whitney Engines 567888

ApprovalBasis:

Test and Computations per 14 CFR 21.303(c)

Models:

JT8D -1, -1A, -1B, -7, -7A, -7B, -9, -9A, -11, -15, -17 and -17R

ReplacedPartNumber:

Pratt & Whitney Engines 50J539

ApprovalBasis:

Test and Computations per 14 CFR 21.303(c)

Models:

PW4050, PW4052, PW4052(-3), PW4056, PW4056(-3), PW4060, PW4060(-3), PW4060A, PW4060A(-3), PW4060C, PW4060C(-3), PW4062(-3), PW4152, PW4152(-3), PW4156, PW4156A, PW4156A(-3), PW4158, PW4158(-3), PW4460, PW4460(-3), PW4462, PW4462(-3), PW4164, PW4168

ReplacedPartNumber:

Pratt & Whitney Engines 705357

ApprovalBasis:

Test and Computations per 14 CFR 21.303(c)

Models:

JT9D -3A, -7, -7A, -7F, -7H, -7AH, -7J, -20, -20J, -7R4D, -7R4E, -7R4E4, -7R4D1, and -7R4E1

ReplacedPartNumber:

Pratt & Whitney Engines 789360

ApprovalBasis:

Test and Computations per 14 CFR 21.303(c)

Models:

JT8D -209, -217, and -217A

ReplacedPartNumber:

Pratt & Whitney Engines 51H779

ApprovalBasis:

Test and Computations per 14 CFR 21.303(c)

Models:

PW4060, PW4060(-3), PW4060A,PW4060A(-3), PW4060C, PW4060C(-3), PW4062(-3), PW4152, PW4152(-3), PW4156, PW4156(-3), PW4156A, PW4156A(-3), PW4158, PW4158(-3), PW4460, PW4460(-3), PW4462, PW4462(-3), PW4164, PW4168, PW2037, 2040, 4050, 4052, 4056, 4060, 4060A, 4152, 4156, 4158, 4460, JT9D-3A, 7, 7H, 7AH, 7A, 7A(SP), 7F, 7J, 20, 20J, 59A, 70A, 7Q, 7Q3, 7R4D, 7R4D1, 7R4E, 7R4E1, 7R4E4, 7R4G2, 7R4H1, PW2037, PW2040, PW2240, PW2337, PW4050, PW4050(-3), PW4052, PW4052(-3), PW4056, PW4056(-3), Engine Model JT9D -3A, -7, -7H, -7AH, -7A, -7A(SP), -7F, -7J, -20, -20J, -59A, -70A, -7Q, -7Q3, -7R4D, -7R4D1, -7R4E, -7R4E1, -7R4E4, -7R4G2, -7R4H1

ReplacedPartNumber:

Pratt & Whitney Engines 697359

ApprovalBasis:

Test and Computations per 14 CFR 21.303(c)

Models:

JT9D-3A,-7,-7A, -7AH,-7F,-7H,-7J,-20,-20J, -7R4D,-7R4D1,-7R4E, -7R4E1,-7R4E4,-7R4G2, and -7R4H1., JT9D -3A, -7, -7A, -7F, -7H, -7AH, -7J, -20, -20J, -7R4D, -7R4E, -7R4E4, -7R4D1, and -7R4E1

ReplacedPartNumber:

Allied Signal Electric Engine Starter Retainer Clutch 371455-1 and 371455

ApprovalBasis:

Tests and Computations per 14 CFR 21.303 (c)(4), Dwg No. 371455-1AFI, Rev. B, Date 05/06/05, or later FAA approved revisions.

Models:

Allied Signal Electric Engine Starter Models 3605812-1, -2-1, -3, -4, -9, -10-1, -11, -12, -13-1, -14-1, -16, -17, -18, -19, -21, -22, 372697-6, -9, -10, -13, -15, -16, -18-1, -21-1, -22, -24 and 375322-7, -8, -9, -10, used on 707, 727-100, 727-200, 737, 737-300) McDonnell Douglas (Allied Signal Electric Engine Starter Models 3605812-1, -2-1, -3, -4, -9, -10-1, -11, -12, -13-1, -14-1, -16, -17, -18, -19, -21, -22, 372697-6, -9, -10, -13, -15, -16, -18-1, -21-1, -22, -24 and 375322-7, -8, -9, -10, used on McDonnell Douglas DC8-70, DC9-10/30, DC9 (TWA), DC9-50, DC9-80, MD80) airbus (Allied Signal Electric Engine Starter Models 3605812-1, -2-1, -3, -4, -9, -10-1, -11, -12, -13-1, -14-1, -16, -17, -18, -19, -21, -22, 372697-6, -9, -10, -13, -15, -16, -18-1, -21-1, -22, -24 and 375322-7, -8, -9, -10, used on BAC 1-11

ReplacedPartNumber:

Allied Signal Electric Engine Starter Clutch Housing 372695-1 and 372695

ApprovalBasis:

Tests and Computations per 14 CFR 21.303 (c)(4), Dwg No. 372695-1AFI, Rev. A, Date 05/06/05, or later FAA approved revisions.

Models:

Allied Signal Electric Engine Starter Models 3605812-1, -2-1, -3, -4, -9, -10-1, -11, -12, -13-1, -14-1, -16, -17, -18, -19, -21, -22, 372697-6, -9, -10, -13, -15, -16, -18-1, -21-1, -22, -24 and 375322-7, -8, -9, -10, used on 707, 727-100, 727-200, 737, 737-300.) McDonnell Douglas (Allied Signal Electric Engine Starter Models 3605812-1, -2-1, -3, -4, -9, -10-1, -11, -12, -13-1, -14-1, -16, -17, -18, -19, -21, -22, 372697-6, -9, -10, -13, -15, -16, -18-1, -21-1, -22, -24 and 375322-7, -8, -9, -10, used on McDonnell Douglas DC8-70, DC9-10/30, DC9 (TWA), DC9-50, DC9-80, MD80) airbus (Allied Signal Electric Engine Starter Models 3605812-1, -2-1, -3, -4, -9, -10-1, -11, -12, -13-1, -14-1, -16, -17, -18, -19, -21, -22, 372697-6, -9, -10, -13, -15, -16, -18-1, -21-1, -22, -24 and 375322-7, -8, -9, -10, used on BAC 1-11

ReplacedPartNumber:

International Aero Engines AS42714

ApprovalBasis:

Tests and Computations per 14 CFR 21.303 (c)(4), Dwg No. AS42714AFI, Rev. N/C, Date 09/18/06, or later FAA approved revisions.

Models:

V2500-A1, V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, V2533-A5, V2525-D5, V2528-D5

ReplacedPartNumber:

Allison Engine Company 6897962

ApprovalBasis:

Analysis and Test per 21.303(d)

Models:

T56/501 Series, T15, 15L, T14, T16, 14L, 423, 425, 22A, 22C, 25W, 25A, 22G, 4AL, 4BL, K17

ReplacedPartNumber:

Teledyne Continental Engine 653701

ApprovalBasis:

Test and computations according to 14 CFR 21.303(c)

Models:

J3C: C-65, A-75-8, A-75-9, C-85-8, C-85-12, C-90-8F, PA-11: C-65, C-85-8FJ, C-85-12, C-90-8F, engines model | A-75-8, A-75-9, C-65, C-85-8, C-85-8FJ, C-85-12, C-90-8F, J3C: C-65, A-75-8, A-75-9, C-85-8, C-85-12, C-90-8F, PA-11: C-65, C-85-8FJ, C-85-12, C-90-8F, engines model

ReplacedPartNumber:

G.E. or Gates 41BO04AD07G3 & 41BO04AA15N, Grimes MISC-060 & MISC-0615, EAC EA1D131D3, Engineered Magnetics 803911-1, Saft 16623-1 & 16624-1, Marathon Power 25503-025

ApprovalBasis:

Test and Computions per 14 CFR 21.303

Models:

Falcon 50, Falcon 900 | F28 | DC-9 Series, MD-80 Series

ReplacedPartNumber:

Emergency Power Supply, Inc. and/or EM Engineered Magnetics Inc. 803949-1

ApprovalBasis:

Test and Computations per 14 CFR Part 21.303 (c)4, Aero Design, Inc. s Dwg No A-1280A, Rev Orig., Date 06/09/03, or later FAA Approved Revision

Models:

717 Series | MD-90 Series

ReplacedPartNumber:

International Aero Engines 5L0040

ApprovalBasis:

T.C.D.S. E40NE Identicality per International Aero Engines letter dated November 17, 1995

Models:

V2500-Al, V2500-A5 (All)

ReplacedPartNumber:

International Aero Engines 5L0045

ApprovalBasis:

T.C.D.S. E40NE Identicality per International Aero Engines letter dated November 17, 1995

Models:

V2500-D5 (All)

ReplacedPartNumber:

International Aero Engines P/N 775963

ApprovalBasis:

Test and Computations per 14 CFR , Part 21.303 DWG NO 775963SD REV IR DATE 05/04/07 or later FAA Approved revisions

Models:

V2500 Series Engine

ReplacedPartNumber:

Cross Manufacturing S13631-17 used on IAE V2500 A5 Enginers

ApprovalBasis:

Test and Computations per 14 CFR 21.303, DWG NO S13631-17SD REV IR DATE 12/20/07 or later FAA Approved revisions

Models:

A319 Series, A320 Series, A321 Series

ReplacedPartNumber:

Flight Equipment & Engineering Limited B38406-9

ApprovalBasis:

Test and Computations per FAR 21.303(c)

Models:

747SP Series

ReplacedPartNumber:

Flight Equipment & Engineering Limited B311105-7941-1

ApprovalBasis:

Test and Computations per FAR 21.303(c)

Models:

767-300 Series

ReplacedPartNumber:

Flight Equipment & Engineering Limited C311116-6107

ApprovalBasis:

Test and Computations per FAR 21.303(c)

Models:

757-200 Series

ReplacedPartNumber:

Flight Equipment & Engineering Limited B311105-7941-2

ApprovalBasis:

Test and Computations per FAR 21.303(c)

Models:

767-300 Series

ReplacedPartNumber:

Flight Equipment & Engineering Limited B311106/29

ApprovalBasis:

Test and Computations per FAR 21.303(c)

Models:

767-200 Series

ReplacedPartNumber:

Modification Part

ApprovalBasis:

STC SH7 95GL dtd 7/2/85

Models:

Model A109A

ReplacedPartNumber:

Modification Part

ApprovalBasis:

STC SH673GL dtd 9/17/85

Models:

Models AS355E, AS355F and AS355F-1

ReplacedPartNumber:

Modification Part

ApprovalBasis:

STC SH795GL dtd 7/2/85

Models:

Model A109AII

ReplacedPartNumber:

International Aero Engines 5R5030, Pall Aerospace QA05954, PTI Technologies, Inc. PIN 7594068101 and Western Filter Corp. PIN WF337020,SoFrance CA00080A.

ApprovalBasis:

Test and Computations per 14 CFR 21.303 Dwg. 1763483, Rev. A dated 2/20/09 or later FAAapproved reVISIOns

Models:

V2500-A1, V2500A5, V2522-A5, V2524-A5, V2527A5, V2527E-A5, V2527M-A5, V2530A5, V2533-A5, V2500-D5, V2525D5, V2528-D5 Series Engines.

ReplacedPartNumber:

GE Aircraft Engines P/N 2043M10P05

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4). Licensing Agreement between Woodward Governor Company and GE Aircraft Engines, File No. None dated: September 7, 2005 DWG No: 8063-884 Rev: A Date: 8/13/2003

Models:

GE Aircraft Engines CF34-10

ReplacedPartNumber:

International Aero Engines 8910-620

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4), Licensing agreement

Models:

V2522-A5, V2524-A5, V2527M-A5, V2527-A5, V2527E-A5, V2530-A5, V2533-A5

ReplacedPartNumber:

GE Aircraft Engines 1851M65P06

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

GE90-76B, GE90-77B, GE90-85B, GE90-90B, GE90-92B

ReplacedPartNumber:

AlliedSignal Engines 3105716-2

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4), Licensing Agreement

Models:

TPE331-14GR, TPE331-14HR

ReplacedPartNumber:

BMW Rolls Royce Aero Engine 8910-214

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

BR700-710A2-20

ReplacedPartNumber:

BMW Rolls Royce Engines 8100-010

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

BR700-715A1-30, BR700-715B1-30, BR700-715C1-30

ReplacedPartNumber:

General Electric Aircraft Engines 6078T55P16

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

CF34-3B, CF34-3B1

ReplacedPartNumber:

General Electric Aircraft Engines 6078T55P10

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

CF34-3B, CF34-3B1

ReplacedPartNumber:

GARRETTENGINE DIVISION P/N 897375-14

ApprovalBasis:

IDENTIAL DESIGN PER FAR 21.303(C)

Models:

TPE 331-10-501K, TPE 331-10-511K

ReplacedPartNumber:

GARRETTENGINE DIVISION P/N 803561-15

ApprovalBasis:

IDENTIAL DESIGN PER FAR 21.303(C)

Models:

TPE 331-5-252M

ReplacedPartNumber:

GARRETTENGINE DIVISION P/N 893561-13

ApprovalBasis:

IDENTIAL DESIGN PER FAR 21.303(C)

Models:

TPE 331-5-252K

ReplacedPartNumber:

BMW Rolls Royce Aero Engine 8061-614

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

BR700-710A2-20

ReplacedPartNumber:

GE Aircraft Engines P/N 2043M18P02

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4). Licensing Agreement between Woodward Governor Company and GE Aircraft Engines, File No. None dated: October 24, 2005 DWG No: 8100-151 Rev: A Date: 6/23/2004

Models:

CF34-10E

ReplacedPartNumber:

GE Aircraft Engines 6078T55P19

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

CF34-3A1

ReplacedPartNumber:

BMW Rolls Royce Engines 8100-113

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

BR700-715A1-30, BR700-715B1-30, BR700-715C1-30

ReplacedPartNumber:

AlliedSignal Engines 3105716-5

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4), Licensing Agreement

Models:

TPE331-14GR, TPE331-14HR

ReplacedPartNumber:

BMW Rolls Royce Engines 8910-214

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

BR700-715A1-30, BR700-715B1-30, BR700-715C1-30

ReplacedPartNumber:

GE Aircraft Engines P/N 1348M79P13

ApprovalBasis:

Identicality per 14 CFR 21.303 (c)(4). Licensing agreement between Woodward Governor Company and GE Aircraft Engines, dated 1/5/2005. Woodward Governor Dwg. 8061-535 Revision New, dated 07/14/04 Or later FAA Approved Revision

Models:

CFM56-5

ReplacedPartNumber:

GARRETTENGINE DIVISION P/N 897375-26

ApprovalBasis:

IDENTIAL DESIGN PER FAR 21.303(C)

Models:

TPE 331-10

ReplacedPartNumber:

GE Aircraft Engines P/N 1348M79P13

ApprovalBasis:

Identicality per 14 CFR 21.303, DWG No: 8061-535 Rev: New Date: 7/14/2004 or later FAA approved Revisions

Models:

CFM56-5

ReplacedPartNumber:

GE Aircraft Engines 1851M65P07

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4), Licensing agreement

Models:

GE90

ReplacedPartNumber:

International Aero Engines 8061-633

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

V2522-A5, V2524-A5, V2527M-A5, V2527-A5, V2527E-A5

ReplacedPartNumber:

GE Aircraft Engines 6078T55P20

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

CF34-3A1

ReplacedPartNumber:

AlliedSignal Engines 3105501-6

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4), Licensing Agreement

Models:

TPE331-14GR, TPE331-14HR

ReplacedPartNumber:

BMW Rolls Royce Aero Engines 8061-964

ApprovalBasis:

Identicality per 14 CFR 21.303, Licensing Agreement

Models:

BR700-715A1-30, BR700-715B1-30, BR700-715C1-30

ReplacedPartNumber:

GE Aircraft Engines 6078T55P18

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

CF34-3B, CF34-3B1

ReplacedPartNumber:

General Electric Aircraft Engines 1851M65P04

ApprovalBasis:

Identicality per FAR 21.303(c)(4)

Models:

90-76B, GE 90-77B, GE 90-85B, GE 90-90B, GE 90-92B

ReplacedPartNumber:

General Electric Aircraft Engines 6068T72P11

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4), Licensing Agreement

Models:

CT7-9B, CT7-9C

ReplacedPartNumber:

General Electric Aircraft Engines 6078T55P12

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

CF34-3A1

ReplacedPartNumber:

GE Aircraft Engines P/N 2043M17P03

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4). Licensing Agreement between Woodward Governor Company and GE Aircraft Engines, File No. None dated: October 24, 2005 DWG No: 8100-052 Rev: A Date: 6/23/2004

Models:

CF34-10E

ReplacedPartNumber:

General Electric Aircraft Engines 6047T74P11

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

CF34-1A, CF34-3A

ReplacedPartNumber:

GE Engines 4120T01P02

ApprovalBasis:

Identicality per 14 CFR 21.303, Licensing Agreement

Models:

CF34-8C1

ReplacedPartNumber:

AlliedSignal Engines 3105500-10

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4), Licensing Agreement

Models:

TPE331-14A, TPE331-14F

ReplacedPartNumber:

AlliedSignal Engines 3105501-4

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4), Licensing Agreement

Models:

TPE331-14A, TPE331-14F, TPE331-14GR, TPE331-14HR, TPE331-15AW

ReplacedPartNumber:

AlliedSignal Engine 3105800-1

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4), Licensing Agreement

Models:

TPE331-14A, TPE331-15AW

ReplacedPartNumber:

BMW Rolls Royce Engines 8910-512

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

BR700-710A1-10 BR700-710A2-20 BR700-715A1-30 BR700-715B1-30 BR700-715C1-30

ReplacedPartNumber:

International Aero Engines 8061-636

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4), Licensing agreement

Models:

V2522-A5, V2524-A5, V2527M-A5, V2527-A5, V2527E-A5

ReplacedPartNumber:

General Electric Aircraft Engines 6078T55P14

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

CF34-3A1

ReplacedPartNumber:

GE Aricraft Engines 6078T55P17

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

CF34-3A1

ReplacedPartNumber:

General Electric Aircraft Engines 1348M79P10

ApprovalBasis:

Identicality per FAR 21.303(c)(4)

Models:

CFM56-5A, CFM56-5B, CFM56-5C

ReplacedPartNumber:

International Aero Engines 8061-637

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4), Licensing agreement

Models:

V2530-A5, V2533-A5

ReplacedPartNumber:

General Electric Aircraft Engines 6068T72P12

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4), Licensing Agreement

Models:

CT7-9B, CT7-9B1, CT7-9B2, CT7-9C, CT7-9D

ReplacedPartNumber:

General Electric Engines 6068T72P18

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

CT7-9B, CT7-9B1, CT7-9B2, CT7-9C, CT7-9D

ReplacedPartNumber:

General Electric Aircraft Engines 1959M18P03

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

CFM56-7

ReplacedPartNumber:

AlliedSignal Engines 3105900-6

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4), Licensing Agreement

Models:

TPE331-14GR, TPE331-14HR

ReplacedPartNumber:

General Electric Engines 6068T72P17

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

CT7-9B, CT7-9C

ReplacedPartNumber:

General Electric Aircraft Engines 6068T72P07

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4), Licensing Agreement

Models:

CT7-9B, CT7-9C

ReplacedPartNumber:

BMW Rolls-Royce Engines 8061-615

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

BR700-710A1-10, BR700-710A2-20

ReplacedPartNumber:

General Electric Engines 6068T72P23

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

CT7-9B, CT7-9B1, CT7-9B2, CT7-9C, CT7-9D

ReplacedPartNumber:

General Electric Aircraft Engines 6068T72P10

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4), Licensing Agreement

Models:

CT7-9B, CT7-9C

ReplacedPartNumber:

General Electric Aircraft Engines 6068T72P08

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4), Licensing Agreement

Models:

CT7-9B, CT7-9B1, CT7-9B2, CT7-9C, CT7-9D

ReplacedPartNumber:

BMW Rolls Royce Engines 8100-114

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

BR700-715A1-30 BR700-715B1-30 BR700-715C1-30

ReplacedPartNumber:

GARRETTENGINE DIVISION P/N 897375-24

ApprovalBasis:

IDENTIAL DESIGN PER FAR 21.303(C)

Models:

TPE 331-11

ReplacedPartNumber:

GARRETTENGINE DIVISION P/N 897375-15

ApprovalBasis:

IDENTIAL DESIGN PER FAR 21.303(C)

Models:

TPE 331-11-UA-601W, TPE 331-11-UA-611W

ReplacedPartNumber:

GE Aircraft Engines P/N 6068T72P25

ApprovalBasis:

Identicality per 14 CFR 21.303, DWG No: 8061-491 Rev: C Date: 9/11/2000 or later FAA approved revisions

Models:

CT7

ReplacedPartNumber:

AlliedSignal Engines 869169-1

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

TPE331-1, -2, -2UA, -3U, -5, -5A, -5AB, -6, -6A, -9, -10, -10A, -10U, -10UF, -10UG, -10UGR, -10UK, -10R, -11U, -11UA, -11UW, -12, -12UA, -12UAR, -12UHR

ReplacedPartNumber:

General Electric Aircraft Engines 6078T55P15

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

CF34-3A1

ReplacedPartNumber:

International Aero Engines 8061-626

ApprovalBasis:

Identicality per FAR 21.303(c)(4)

Models:

V2525-D5, V2528-D5

ReplacedPartNumber:

General Electric Aircraft Engines 6078T55P09

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

CF34-3A1

ReplacedPartNumber:

BMW Rolls Royce Engines 8061-963

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

BR700-715A1-30, BR700-715B1-30, BR700-715C1-30

ReplacedPartNumber:

General Electric Aircraft Engines 6078T55P08

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

CF34-3A1

ReplacedPartNumber:

International Aero Engines 8061-632

ApprovalBasis:

Identicality per FAR 21.303(c)(4)

Models:

V2527-A5, V2530-A5, V2533-A5

ReplacedPartNumber:

General Electric Engines 6068T72P22

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

CT7-9B, CT7-9C

ReplacedPartNumber:

AlliedSignal Engines 897711-4

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4), Licensing Agreement

Models:

TPE331-12B

ReplacedPartNumber:

BMW Rolls Royce Engines 8910-418

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

BR700-715A1-30, BR700-715B1-30, BR700-715C1-30

ReplacedPartNumber:

BMW Rolls Royce Aero Engine 8910-213

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

BR700-710A2-20

ReplacedPartNumber:

GARRETTENGINE DIVISION P/N 892561-16

ApprovalBasis:

IDENTIAL DESIGN PER FAR 21.303(C)

Models:

TPE 331-5

ReplacedPartNumber:

GARRETTENGINE DIVISION P/N 897375-19

ApprovalBasis:

IDENTICAL DESIGN PER FAR 21.303(C)

Models:

TPE 331-10-DG-513H, TPE 331-10-UGR-513K

ReplacedPartNumber:

GARRETTENGINE DIVISION P/N 893561-26

ApprovalBasis:

IDENTIAL DESIGN PER FAR 21.303(C)

Models:

TPE 331-5

ReplacedPartNumber:

GARRETTENGINE DIVISION P/N 897375-16

ApprovalBasis:

IDENTICAL DESIGN PER FAR 21.303(C)

Models:

TPE 331-10-R511C, TPE 331-10-R512C

ReplacedPartNumber:

GARRETTENGINE DIVISION P/N 897375-27

ApprovalBasis:

IDENTIAL DESIGN PER FAR 21.303(C)

Models:

TPE 331-12

ReplacedPartNumber:

GE Aircraft Engines P/N 1962M80P03

ApprovalBasis:

Identicality per 14 CFR 21.303, DWG No: 8061-693 Rev: New Date: 11/22/2005 or later FAA approved revisions

Models:

GE90

ReplacedPartNumber:

GENERAL ELECTRIC CO ENGINE MAIN CONTROL P/N 1323M36P01 DWG NO 1323M36 NO REV DTD 10/25/84

ApprovalBasis:

IDENTICAL DESIGN APPROVAL PER FAR 21.303(C)

Models:

CFM56-2G

ReplacedPartNumber:

AlliedSignal Engines 3105716-4

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4), Licensing Agreement

Models:

TPE331-14A, TPE331-14B, TPE331-14F, TPE331-15AW

ReplacedPartNumber:

General Electric Aircraft Engines 6068T72P06

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4), Licensing Agreement

Models:

CT7-9B, CT7-9C

ReplacedPartNumber:

General Electric Aircraft Engines 6091T07P02

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

CF34-3A2

ReplacedPartNumber:

International Aero Engines 8061-627

ApprovalBasis:

Identicality per FAR 21.303(c)(4)

Models:

V2522-A5, V2524-A5

ReplacedPartNumber:

AlliedSignal Engines 3105900-5

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4), Licensing Agreement

Models:

TPE331-14GR, TPE331-14HR

ReplacedPartNumber:

GE Aircraft Engines P/N 4120T01P02

ApprovalBasis:

Identicality per 14 CFR 21.303, DWG No 8061-926 Rev New Date 2/25/2000 or later FAA approved revisions

Models:

CF34-8C1, CF34-8C5, CF34-8C5A1, CF34-8C5A2, CF34-8C5A3, CF34-8C5B1, CF34-8D1, CF34-8D3, CF34-8D5, CF34-8D6, CF34-8E2, CF34-8E2A1, CF34-8E5, CF34-8E5A1, CF34-8E5A2, CF34-8E6, CF34-8E6A1

ReplacedPartNumber:

GARRETTENGINE DIVISION P/N 897375-25

ApprovalBasis:

IDENTIAL DESIGN PER FAR 21.303(C)

Models:

TPE 331-10

ReplacedPartNumber:

BMW Rolls Royce Engines 8061-976

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

BR700-710A1-10, BR700-710A2-20

ReplacedPartNumber:

General Electric Aircraft Engines 6078T55P13

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

CF34-3B, CF34-3B1

ReplacedPartNumber:

General Electric Aircraft Engines 6068T72P09

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4), Licensing Agreement

Models:

CT7-9B, CT7-9C

ReplacedPartNumber:

AlliedSignal Engines 3105501-7

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4), Licensing Agreement

Models:

TPE331-14GR, TPE331-14HR

ReplacedPartNumber:

General Electric Aircraft Engines 1851M65P05

ApprovalBasis:

Identicality per FAR 21.303(c)(4)

Models:

GE90-76B, GE90-77B, GE90-85B, GE90-90B, GE90-92B

ReplacedPartNumber:

General Electric Aircraft Engines 1693M75P09

ApprovalBasis:

Identicality per FAR 21.303(c)(4)

Models:

GE90-76B, -77B, -85B, -90B, -92B

ReplacedPartNumber:

AlliedSignal Engine 3105500-9

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4), Licensing Agreement

Models:

TPE331-14A, TPR331-15AW, TPE331-14A

ReplacedPartNumber:

GE Aircraft Engines 6078T55P21

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

CF34-3B, CF34-3B1

ReplacedPartNumber:

BMW Rolls Royce Aero Engine 8100-114

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

BR700-710A1-10, BR700-710A2-20

ReplacedPartNumber:

BMW Rolls Royce Aero Engine 8061-612

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

BR700-710A2-20

ReplacedPartNumber:

GE Aircraft Engines 1348M79P07

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4), Licensing agreement

Models:

CFM56-5

ReplacedPartNumber:

AlliedSignal Engines 3105900-1

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4), Licensing Agreement

Models:

TPE331-14GR, TPE331-14HR

ReplacedPartNumber:

General Electric Aircraft Engines 6068T72P13

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4), Licensing Agreement

Models:

CT7-9C

ReplacedPartNumber:

GE Aircraft Engines 9363M11P18

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4), Licensing Agreement

Models:

CF6-80A

ReplacedPartNumber:

GE Aircraft Engines 4147T69P02

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4), Licensing Agreement

Models:

CF34-3

ReplacedPartNumber:

GE Aircraft Engines 9363M11P17

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4), Licensing Agreement

Models:

CF6-80A

ReplacedPartNumber:

GE Aircraft Engines 9238M79P32

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4), Licensing Agreement

Models:

CF6-80A

ReplacedPartNumber:

GE Aircraft Engines 9238M79P33

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4), Licensing Agreement

Models:

CF6-80A

ReplacedPartNumber:

GE Aircraft Engines 9238M79P31

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4), Licensing Agreement

Models:

CF6-80A

ReplacedPartNumber:

International Aero Engines 8061-637

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

V2522-A5, V2524-A5, V2527M-A5, V2527-A5, V2527E-A5

ReplacedPartNumber:

GE Aircraft Engines 4147T70P02

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4), Licensing Agreement

Models:

CF34-3

ReplacedPartNumber:

GE Aircraft Engines 9363M11P19

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4), Licensing Agreement

Models:

CF6-80A

ReplacedPartNumber:

GE Aircraft Engines 1348M79P12

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4), Licensing Agreement

Models:

CFM56-5

ReplacedPartNumber:

GE Aircraft Engines 1348M79P11

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4), Licensing Agreement

Models:

CFM56-5

ReplacedPartNumber:

GE Aircraft Engines 9238M79P30

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4), Licensing Agreement

Models:

CF6-80A

ReplacedPartNumber:

International Aero Engines 8061-636

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

V2522-A5, V2524-A5, V2527M-A5, V2527-A5, V2527E-A5

ReplacedPartNumber:

GE Aircraft Engines 9238M79P36

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4), Licensing Agreement

Models:

CF6-80A

ReplacedPartNumber:

GE Aircraft Engines 9238M79P34

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4), Licensing Agreement

Models:

CF6-80A

ReplacedPartNumber:

GE Aircraft Engines 9238M79P35

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4), Licensing Agreement

Models:

CF6-80A

ReplacedPartNumber:

General Electric Aircraft Engines 6047T74P12

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

CF34-1A, CF34-3A

ReplacedPartNumber:

GE Aircraft Engines P/N 1317M47G14

ApprovalBasis:

Identicality Per 14 CFR 21.303 DWG No 6840023E18 Rev None Date 10/27/2006 or later FAA-approved revisions

Models:

GE Aircraft Engines) (CFM56-7B18, CFM56-7B20, CFM56-7B20/2, CFM56-7B22/B2, CFM56-7B22, CFM56-7B22/2, CFM56-7B22/B1, CFM56-7B24, CFM56-7B24/2, CFM56-7B24/B1, CFM56-7B26, CFM56-7B26/2, CFM56-7B26/B1, CFM56-7B26/B2, CFM56-7B27, CFM56-7B27A, CFM56-7B27/B1, CFM56-7B27/B3, CFM56-7B27/2, CFM56-7B18/3, CFM56-7B20/3, CFM56-7B22/3B1, CFM56-7B22/3B2, CFM56-7B24/3, CFM56-7B24/3B1, CFM56-7B26/3, CFM56-7B26/3B2, CFM56-7B26/3F, CFM56-7B27/3, CFM56-7B27/3B3, CFM56-7B27/3F

ReplacedPartNumber:

EM Engineered Magnetics Inc. P/N 803949-1, Aero Design, Inc. P/N AD-803949-1

ApprovalBasis:

Test and Computation per 14 CFR 21.303 Dwg. No. ABS-1030A Rev. Orig. Date May 15, 2008 or later FAA-approved revisions

Models:

717-200

ReplacedPartNumber:

Flight Equipment & Engineering, Ltd. 113175-01

ApprovalBasis:

Identicality per FAR 21.303(c)(4)

Models:

A300, A310, A319, A320, A330 Series | 707, 727, 737, 747, 757, 767, 777 Series | L1011 Series | DC8, DC9, DC10, MD11, MD88, MD90 Series

ReplacedPartNumber:

Flight Equipment & Engineering, Ltd. A38405-21

ApprovalBasis:

Identicality per FAR 21.303(c)(4)

Models:

A300, A310, A319, A320, A330 Series | 707, 727, 737, 747, 757, 767, 777 Series | L1011 Series | DC8, DC9, DC10, MD11, MD88, MD90 Series

ReplacedPartNumber:

Flight Equipment and Engineering, Ltd. A315106-127-2

ApprovalBasis:

Identicality per FAR 21.303(c)(4)

Models:

A300, A310, A319, A320, A330 Series | 707, 727, 737, 747, 757, 767, 777 Series | L1011 Series | DC-8, DC-9, DC-10, MD-11, MD-88, MD-90 Series

ReplacedPartNumber:

Vlier Engineering VQ-147

ApprovalBasis:

Identicality per FAR 21.303(c)(4)

Models:

A300, A310, A320 Series | 707, 727, 737, 747, 757, 767 Series | L1011 Series | DC-8, DC-9, DC-10, MD-88, MD-11 Series

ReplacedPartNumber:

Flight Equipment & Engineering, Ltd. 113175-03

ApprovalBasis:

Identicality per FAR 21.303(c)(4)

Models:

A300, A310, A319, A320, A330 Series | 707, 727, 737, 747, 757, 767, 777 Series | L1011 Series | DC8, DC9, DC10, MD11, MD88, MD90 Series

ReplacedPartNumber:

Vlier Engineering VQ-147

ApprovalBasis:

Identicality per FAR 21.303(c)(4)

Models:

A300, A310, A319, A320, A330 Series | 707, 727, 737, 747, 757, 767, 777 Series | L1011 Series | DC8, DC9, DC10, MD11, MD88, MD90 Series

ReplacedPartNumber:

International Aero Engines P/N 3A2050

ApprovalBasis:

14 CFR FAR Part 21.303(c)4 Test and Computations, FAA Letter dated 1/13/99 and Dwg. No. M8003 Rev, NC dated 9/8/98 or later FAA Approval

Models:

V2500-A1

ReplacedPartNumber:

International Aero Engines P/N 3A0137

ApprovalBasis:

14 CFR FAR Part 21.303(c)4 Test and Computations, FAA Letter dated 1/7/99 and Dwg. No. M8001 Rev, NC dated 10/12/98 or later FAA Approval

Models:

V2500-A1

ReplacedPartNumber:

International Aero Engines P/N 3A0727

ApprovalBasis:

14 CFR FAR Part 21.303(c)4 Test and Computations, FAA Letter dated 1/7/99 and Dwg. No. M8005 Rev, NC dated 10/12/98 or later FAA Approval

Models:

V2500-A1

ReplacedPartNumber:

Gables Engineering P/N 245-0033

ApprovalBasis:

Identicality Per 14 CFR Part 21, Section 21.303(c)(4) FAA Design Data Approval per FAA 8110-3 dated 1/15/04, Dwg No. 245-0033ATS, Rev N/C, Date 01/15/04 or later FAA approved revision

Models:

757 767-200 767-300

ReplacedPartNumber:

Gables Engineering P/N 245-0025

ApprovalBasis:

Identicality Per 14 CFR Part 21, Section 21.303(c)(4) FAA Design Data Approval per FAA 8110-3 dated 1/15/04, Dwg No. 245-0025ATS, Rev N/C, Date 01/15/04 or later FAA approved revision

Models:

MD88 MD90

ReplacedPartNumber:

Aeronautical Engineering P/N ADCPA5280MRS

ApprovalBasis:

Test and computation approved per 14 CFR 21.303 (c)(4), Dwg. A5280, dated 04/28/09 no Revision, or later FAA approved revision

Models:

727, 737 SERIES

ReplacedPartNumber:

Aeronautical Engineering AE505811

ApprovalBasis:

Identicality approved per 14 CFR Part 21, section 21.303(c)(4) Dwg. 4299 no revision dated 6/5/98 and EO 4299-2 dated 2/18/05 or later FAA approved revision

Models:

DC9 series

ReplacedPartNumber:

GE Aircraft Engines P/N: 2162M48P02

ApprovalBasis:

Identicality per 14 CFR 21.303 (c)(4), Licensing Agreement between GE Aircraft Engines and Rosemount Aerospace Inc. dated 8/22/03, File No. 03-75159-A. GE Aircraft Engines TC #E00063EN. Rosemount Aerospace Inc. Spec. Dwg. 0510HT2, Rev. A, dtd 10/18/02*, F/A Dwg. 00510-1410, Rev. H, dtd 6/2/03*, BOM 00510-1410-0002, Rev. H, dtd 6/2/03*.

Models:

CF34-8C5, -8C5A1, -8C5A2, -8C5A3, -8C5B1, -8D1, -8D3, -8D5, -8D6, -8E2, -8E2A1, -8E5, -8E5A1, -8E5A2, -8E6, -8E6A1

ReplacedPartNumber:

GE Aircraft Engines P/N: 1687M90P02

ApprovalBasis:

Identicality per 14 CFR 21.303 (c)(4), Licensing Agreement between GE Aircraft Engines and Rosemount Aerospace Inc. dated 8/22/03, File No. 03-75159-A. GE Aircraft Engines TC #E00049EN. Rosemount Aerospace Inc. Spec. Dwg. 132ABK, Rev. G, dtd 02/15/01*, F/A Dwg. 00132-0953, Rev. G, dtd 04/05/00*, BOM 00132-0953-0001, Rev. G, dtd 7/9/99*.

Models:

GE90-110B1, -113B, -115B, -77B, -90B, -94B

ReplacedPartNumber:

GE Aircraft Engines P/N: 1325M60P09

ApprovalBasis:

Identicality per 14 CFR 21.303 (c)(4), Licensing Agreement between GE Aircraft Engines and Rosemount Aerospace Inc. dated 8/22/03, File No. 03-75159-A. GE Aircraft Engines TC #E00049EN. Rosemount Aerospace Inc. Spec. Dwg. 154DN9 Rev. G, dtd 02/15/01*, F/A Dwg. 00154-1361, Rev. G, dtd 09/09/99*, BOM 00154-1361-0001, Rev. G, dtd 8/31/99*.

Models:

GE90-110B1, -113B, -115B, -77B, -90B, -94B

ReplacedPartNumber:

Garrett Engine P/N 32-54004-2049-3

ApprovalBasis:

Identical Design Approval per FAR 21.303(c)

Models:

TFE731

ReplacedPartNumber:

Garrett Engine P/N 32-62315-1002-2

ApprovalBasis:

Identical Design Approval per FAR 21.303(c)

Models:

TFE731

ReplacedPartNumber:

Garrett Engine P/N 3071949-9

ApprovalBasis:

Identical Design Approval per FAR 21.303(c)

Models:

TFE731

ReplacedPartNumber:

Garrett Engine P/N 35-59001-0012-1

ApprovalBasis:

Identical Design Approval per FAR 21.303(c)

Models:

TFE731

ReplacedPartNumber:

Garrett Engine P/N 32-82501-0002-1

ApprovalBasis:

Identical Design Approval per FAR 21.303(c)

Models:

TFE731

ReplacedPartNumber:

GE Aircraft Engines 1374M96P02

ApprovalBasis:

Licensing Agreement

Models:

CF6-80E, -80A, -80C2 (TC E41NE)

ReplacedPartNumber:

Garrett Engine P/N 35-87521-0014-1

ApprovalBasis:

Identical Design Approval per FAR 21.303(c)

Models:

TFE731

ReplacedPartNumber:

Garrett Engine P/N 24-45164-0003-1

ApprovalBasis:

Identical Design Approval per FAR 21.303(c)

Models:

TFE731

ReplacedPartNumber:

Garrett Engine P/N 32-62315-1004-2

ApprovalBasis:

Identical Design Approval per FAR 21.303(c)

Models:

TFE731

ReplacedPartNumber:

Garrett Engine P/N 35-87521-0012-1

ApprovalBasis:

Identical Design Approval per FAR 21.303(c)

Models:

TFE731

ReplacedPartNumber:

Garrett Engine P/N 32-62315-1003-2

ApprovalBasis:

Identical Design Approval per FAR 21.303(c)

Models:

TFE731

ReplacedPartNumber:

Garrett Engine P/N 35-56002-0029-1

ApprovalBasis:

Identical Design Approval per FAR 21.303(c)

Models:

TFE731

ReplacedPartNumber:

Garrett Engine P/N 35-59011-0009-1

ApprovalBasis:

Identical Design Approval per FAR 21.303(c)

Models:

TFE731

ReplacedPartNumber:

Garrett Engine P/N 35-79501-2080-3

ApprovalBasis:

Identical Design Approval per FAR 21.303(c)

Models:

TFE731

ReplacedPartNumber:

Garrett Engine P/N 24-45100-0113 -1

ApprovalBasis:

Identical Design Approval per FAR 21.303(c)

Models:

TFE731

ReplacedPartNumber:

GE Aircraft Engines 1383M18P03

ApprovalBasis:

Licensing Agreement

Models:

CF6-80E (TC E41NE)

ReplacedPartNumber:

Garrett Engine P/N 35-56002-0030-1

ApprovalBasis:

Identical Design Approval per FAR 21.303(c)

Models:

TFE731

ReplacedPartNumber:

Garrett Engine P/N 32-62315-1009-2

ApprovalBasis:

Identical Design Approval per FAR 21.303(c)

Models:

TFE731

ReplacedPartNumber:

Garrett Engine P/N 24-45100-0098-1

ApprovalBasis:

Identical Design Approval per FAR 21.303(c)

Models:

TFE731

ReplacedPartNumber:

Garrett Engine P/N 32-62315-1010-2

ApprovalBasis:

Identical Design Approval per FAR 21.303(c)

Models:

TFE731

ReplacedPartNumber:

GE Aircraft Engines 1663M88P01

ApprovalBasis:

Licensing Agreement

Models:

CF6-80E (TC E41NE)

ReplacedPartNumber:

Garrett Engine P/N 38-79004-0021-1

ApprovalBasis:

Identical Design Approval per FAR 21.303(c)

Models:

TFE731

ReplacedPartNumber:

Garrett Engine P/N 32-61801-1008-2

ApprovalBasis:

Identical Design Approval per FAR 21.303(c)

Models:

TFE731

ReplacedPartNumber:

Garrett Engine P/N 32-53005-1023-2

ApprovalBasis:

Identical Design Approval per FAR 21.303(c)

Models:

TFE731

ReplacedPartNumber:

GE Aircraft Engines 1646M80P02

ApprovalBasis:

Licensing Agreement

Models:

CF6-80E (TC E41NE)

ReplacedPartNumber:

Garrett Engine P/N 865101-3

ApprovalBasis:

Identical Design Approval per FAR 21.303(c)

Models:

TPE331, refer to Page 2 for Engine Model Applicability

ReplacedPartNumber:

Garrett Engine P/N 32-62315-1005-2

ApprovalBasis:

Identical Design Approval per FAR 21.303(c)

Models:

TFE731

ReplacedPartNumber:

Garrett Engine P/N 32-62315-2082-3

ApprovalBasis:

Identical Design Approval per FAR 21.303(c)

Models:

TFE731

ReplacedPartNumber:

Garrett Engine P/N 35-78510-1004-2

ApprovalBasis:

Identical Design Approval per FAR 21.303(c)

Models:

TFE731

ReplacedPartNumber:

Garrett Engine P/N 35-62320-0013-1

ApprovalBasis:

Identical Design Approval per FAR 21.303(c)

Models:

TFE731

ReplacedPartNumber:

Garrett Engine P/N 35-62320-0015-1

ApprovalBasis:

Identical Design Approval per FAR 21.303(c)

Models:

TFE731

ReplacedPartNumber:

Garrett Engine P/N 35-80005-2002-3

ApprovalBasis:

Identical Design Approval per FAR 21.303(c)

Models:

TFE731

ReplacedPartNumber:

Garrett Engine P/N 35-62320-0021-1

ApprovalBasis:

Identical Design Approval per FAR 21.303(c)

Models:

TFE731

ReplacedPartNumber:

Garrett Engine P/N 24-45164-0004-1

ApprovalBasis:

Identical Design Approval per FAR 21.303(c)

Models:

TFE731

ReplacedPartNumber:

Garrett Engine P/N 24-45900-0095-1

ApprovalBasis:

Identical Design Approval per FAR 21.303(c)

Models:

TFE731

ReplacedPartNumber:

Garrett Engine P/N 35-87521-0016-1

ApprovalBasis:

Identical Design Approval per FAR 21.303(c)

Models:

TFE731

ReplacedPartNumber:

Garrett Engine P/N 35-61801-1005-2

ApprovalBasis:

Identical Design Approval per FAR 21.303(c)

Models:

TFE731

ReplacedPartNumber:

Garrett Engine P/N 35-56002-0031-1

ApprovalBasis:

Identical Design Approval per FAR 21.303(c)

Models:

TFE731

ReplacedPartNumber:

Garrett Engine P/N 3071949-7

ApprovalBasis:

Identical Design Approval per FAR 21.303(c)

Models:

TFE731

ReplacedPartNumber:

Garrett Engine P/N 24-45100-0099 -1

ApprovalBasis:

Identical Design Approval per FAR 21.303(c)

Models:

TFE731

ReplacedPartNumber:

GE Aircraft Engines 1303M21P02

ApprovalBasis:

Licensing Agreement

Models:

CF6-80E (TC E41NE)

ReplacedPartNumber:

Garrett Engine P/N 32-62315-1006-2

ApprovalBasis:

Identical Design Approval per FAR 21.303(c)

Models:

TFE731

ReplacedPartNumber:

Allison Engine 35-62315-2464-3

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

AE2100A, AE2100C, AE2100D3

ReplacedPartNumber:

Allison Engine 25-48644-1021-2

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

AE2100A, AE2100C, AE2100D3

ReplacedPartNumber:

Allison Engine 35-54004-2069-3

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

AE2100A, AE2100C, AE2100D3

ReplacedPartNumber:

Allison Engine 35-56055-4190-1

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

AE2100A, AE2100C, AE2100D3

ReplacedPartNumber:

Allison Engine 35-62315-2544-3

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

AE2100A, AE2100C, AE2100D3

ReplacedPartNumber:

Allison Engine 25-48644-1017-2

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

AE2100A, AE2100C, AE2100D3

ReplacedPartNumber:

Allison Engine 35-62315-2460-3

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

AE2100A, AE2100C, AE2100D3

ReplacedPartNumber:

Allison Engine 24-48600-1017-2

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

AE2100A, AE2100C, AE2100D3

ReplacedPartNumber:

Allison Engine 38-79004-0082-1

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

AE2100A, AE2100C, AE2100D3

ReplacedPartNumber:

Allison Engine 24-48613-1021-4

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

AE2100A, AE2100C, AE2100D3

ReplacedPartNumber:

Allison Engine 35-62315-2455-3

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

AE2100A, AE2100C, AE2100D3

ReplacedPartNumber:

Allison Engine 32-62315-0267-1

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

AE2100A, AE2100C, AE2100D3

ReplacedPartNumber:

Allison Engine 35-56024-0095-1

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

AE2100A, AE2100C, AE2100D3

ReplacedPartNumber:

Allison Engine 38-18432-0005-1

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

AE2100A, AE2100C, AE2100D3

ReplacedPartNumber:

Allison Engine 25-48644-1019-2

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

AE2100A, AE2100C, AE2100D3

ReplacedPartNumber:

Allison Engine 32-54004-3077-4

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

AE2100A, AE2100C, AE2100D3

ReplacedPartNumber:

Allison Engine 35-62010-1047-2

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

AE2100A, AE2100C, AE2100D3

ReplacedPartNumber:

Allison Engine 35-62315-2589-3

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

AE2100A, AE2100C, AE2100D3

ReplacedPartNumber:

Allison Engine 32-62315-0257-1

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

AE2100A, AE2100C, AE2100D3

ReplacedPartNumber:

Allison Engine 35-62315-2462-3

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

AE2100A, AE2100C, AE2100D3

ReplacedPartNumber:

Allison Engine 32-62315-0259-1

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

AE2100A, AE2100C, AE2100D3

ReplacedPartNumber:

Allison Engine 24-48600-1007-2

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

AE2100A, AE2100C, AE2100D3

ReplacedPartNumber:

Allison Engine 35-62315-2454-3

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

AE2100A, AE2100C, AE2100D3

ReplacedPartNumber:

Allison Engine 23062456

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

AE2100/A, AE2100/C, AE2100D3

ReplacedPartNumber:

Allison Engine 32-54004-2078-3

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

AE2100A, AE2100C, AE2100D3

ReplacedPartNumber:

Allison Engine 24-48600-1008-2

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

AE2100A, AE2100C, AE2100D3

ReplacedPartNumber:

Allison Engine 32-79501-1031-2

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

AE2100A, AE2100C, AE2100D3

ReplacedPartNumber:

Allison Engine 25-48644-1018-2

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

AE2100A, AE2100C, AE2100D3

ReplacedPartNumber:

Allison Engine 25-48644-1022-2

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

AE2100A, AE2100C, AE2100D3

ReplacedPartNumber:

Allison Engine 32-62315-0256-1

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

AE2100A, AE2100C, AE2100D3

ReplacedPartNumber:

Allison Engine 24-48600-1020-3

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

AE2100A, AE2100C, AE2100D3

ReplacedPartNumber:

Allison Engine 23069439

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

AE2100A, AE2100C, AE2100D3

ReplacedPartNumber:

Allison Engine 24-48600-1006-2

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

AE2100A, AE2100C, AE2100D3

ReplacedPartNumber:

Allison Engine 35-56045-0890-1

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

AE2100A, AE2100C, AE2100D3

ReplacedPartNumber:

Allison Engine 35-87509-1002-2

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

AE2100A, AE2100C, AE2100D3

ReplacedPartNumber:

Allison Engine 24-48600-1009-2

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

AE2100A, AE2100C, AE2100D3

ReplacedPartNumber:

Allison Engine 35-62315-2458-3

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

AE2100A, AE2100C, AE2100D3

ReplacedPartNumber:

Allison Engine 25-48644-1020-2

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

AE2100A, AE2100C, AE2100D3

ReplacedPartNumber:

Allison Engine 38-87006-2008-3

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

AE2100A, AE2100C, AE2100D3

ReplacedPartNumber:

Allison Engine 35-56030-0540-1

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

AE2100A, AE2100C, AE2100D3

ReplacedPartNumber:

Allison Engine 38-87003-2009-3

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

AE2100A, AE2100C, AE2100D3

ReplacedPartNumber:

Allison Engine 35-79501-3052-4

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

AE2100A, AE2100C, AE2100D3

ReplacedPartNumber:

Allison Engine 25-48623-1021-3

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

AE2100A, AE2100C, AE2100D3

ReplacedPartNumber:

Allison Engine 35-13001-0001-1

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

AE2100A, AE2100C, AE2100D3

ReplacedPartNumber:

Allison Engine 35-62315-2463-3

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

AE2100A, AE2100C, AE2100D3

ReplacedPartNumber:

Allison Engine 35-54004-4121-5

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

AE2100A, AE2100C, AE2100D3

ReplacedPartNumber:

Allison Engine 36-04503-0453-1

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

AE2100A, AE2100C, AE2100D3

ReplacedPartNumber:

Allison Engine 36-04503-0481-1

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

AE2100A, AE2100C, AE2100D3

ReplacedPartNumber:

Allison Engine 35-62315-2457-3

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

AE2100A, AE2100C, AE2100D3

ReplacedPartNumber:

Allison Engine 32-82004-1005-2

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

AE2100A, AE2100C, AE2100D3

ReplacedPartNumber:

Allison Engine 36-04503-0514-1

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

AE2100A, AE2100C, AE2100D3

ReplacedPartNumber:

Allison Engine 32-62315-0262-1

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

AE2100A, AE2100C, AE2100D3

ReplacedPartNumber:

Allison Engine 35-62315-2456-3

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

AE2100A, AE2100C, AE2100D3

ReplacedPartNumber:

Engine Alliance P/N 2411M18P02

ApprovalBasis:

Identicality per 14 CFR 21.303 Licensing Agreement between Engine Alliance and Hamilton Sundstrand, dated 10/20/2009 DWG No 1706305 Rev G Date 10/07/2009 or later FAA-approved revisions.

Models:

GP7270, GP7277

ReplacedPartNumber:

International Aero Engines AG (IAE) P/N 6A4211C02

ApprovalBasis:

Test and Computations Per 14 CFR 21.303, Dwg No. CGAM10123 Rev. E Dated 6/12/08 or later FAA Approval

Models:

V2522-A5, V2524-A5, V2527-A5 V2527E-A5, V2527M-A5, V2530-A5, V2525-D5, V2528-D5, V2533-A5

ReplacedPartNumber:

International Aero Engines AG (IAE) P/N 6A6566

ApprovalBasis:

Test and Computations Per 14 CFR 21.303, Dwg No. CGAM10123 Rev. E Dated 6/12/08 or later FAA Approval

Models:

V2522-A5, V2524-A5, V2527-A5 V2527E-A5, V2527M-A5, V2530-A5, V2525-D5, V2528-D5, V2533-A5

ReplacedPartNumber:

International Aero Engines AG (IAE) P/N 6A6545

ApprovalBasis:

Test and Computations Per 14 CFR 21.303, Dwg No. CGAM10123 Rev. E Dated 6/12/08 or later FAA Approval

Models:

V2522-A5, V2524-A5, V2527-A5 V2527E-A5, V2527M-A5, V2530-A5, V2525-D5, V2528-D5, V2533-A5

ReplacedPartNumber:

International Aero Engines P/N 2A1701

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG NO: ADP72176 REV: N/C DATE: 09/12/07 or later FAA Approved revisions

Models:

V2500-1A, V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2533-A5

ReplacedPartNumber:

Aero Design, Inc. P/N AD-4002P GE/Gates P/N 41BO04AD07G3 Grimes P/N MISC-060 and MISC-0615 Engineered Magnetics P/N 803911-1 Saft P/N 16623-1 and 16624-1 Marathon S103 P/N 25503-025

ApprovalBasis:

Test and Computation per 14 CFR 21.303 Dwg. No ABS-1002A Rev. Orig. Date April 20, 2008 or later FAA-approved revision.

Models:

DC-9-11, DC-9-12, DC-9-13, DC-9-14, DC-9-15, DC-9-15F, DC-9-21, DC-9-31, DC-9-32, DC-9-32F, DC-9-33F, DC-9-34, DC-9-34F, DC-9-41, DC-9-51, DC-9-81(MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83), DC-9-87, (MD-87)

ReplacedPartNumber:

International Aero Engines P/N 3A1818

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG NO ADP72180 REV N/C DATE 09/12/07 or later FAA Approved revisions

Models:

V2500-A1, V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2533-A5

ReplacedPartNumber:

International Aero Engines P/N 3A0710

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG NO ADP72179 REV N/C DATE 09/12/07 or later FAA Approved revisions

Models:

V2500-A1, V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, V2533-A5

ReplacedPartNumber:

International Aero Engines P/N 6A4139

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG NO ADP72186 REV N/C DATE 10/08/07 or later FAA Approved revisions

Models:

V2500-A1, V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, V2533-A5

ReplacedPartNumber:

General Electric Aircraft Engines, SPAD for P/N 4902T04G01

ApprovalBasis:

Test and Computations per 14 CFR 21.303 (c) (4) DWG No TSG4902T04G01-2 Rev A Date Nov.17, 2000 or Later FAA approved Revisions

Models:

CJ610-1, -4, -5, -6, -8, -9, CF700-2D, -2D -2

ReplacedPartNumber:

International Aero Engines P/N 2A0333

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG NO ADP72175 REV NC DATE 12/3/07 or later FAA Approved revisions

Models:

V2500-A1, V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, V2533-A5, V2525-D5, V2528-D5

ReplacedPartNumber:

General Electric Aircraft Engines, P/N 4902T04G01 (W/ Cover Plate SPAD)

ApprovalBasis:

Test and Computations per 14 CFR 21.303 (c) (4) DWG No TSG4902T04G01 Rev A Date Nov.17, 2000 or Later FAA approved Revisions

Models:

CJ610-1, -4, -5, -6, -8, -9, CF700-2D, -2D-2

ReplacedPartNumber:

Aero Design, Inc. P/N AD-4002P GE/Gates P/N 41BO04AD07G3 Grimes P/N MISC-060 and MISC-0615 Engineered Magnetics P/N 803911-1 Saft P/N 16623-1 and 16624-1 Marathon S103 P/N 25503-025

ApprovalBasis:

Test and Computation per 14 CFR 21.303 Dwg. No ABS-1002A Rev Orig. Date April 20, 2008 or later FAA-approved revision.

Models:

Mystere Falcon 50, Mystere Falcon 900) Fokker (F.28 Mark 0070, F.28 Mark 0100, F.28 Mark 1000, F.28 Mark 2000 F.28 Mark 3000, F.28 Mark 4000

ReplacedPartNumber:

Boeing 65B90686-4, Hook - Roller Hinge, Engine Side Cowl

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

747

ReplacedPartNumber:

International Aero Engines P/N 5A1837

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG NO ADP72182 REV NC DATE 10/30/07 or later FAA Approved revisions

Models:

V2500-A1, V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, V2533-A5, V2525-D5, V2528-D5

ReplacedPartNumber:

General Electric Aircraft Engines, P/N 4902T04G01

ApprovalBasis:

Test and Computations per CFR 21.303 (c) (4) DWG No TSG4902T04G01 Rev None Date Sept 9, 1999 or Later FAA approved Revisions

Models:

CJ610-1, -4, -5, -6, -8, -9, CF700-2D, -2D-2

ReplacedPartNumber:

International Aero Engines P/N 6A4139

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG NO: ADP72186 REV: N/C DATE: 10/08/07 or later FAA Approved revisions

Models:

V2500-1A, V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, V2533-A5

ReplacedPartNumber:

International Aero Engines P/N 6A1069

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG NO: ADP72184 REV: N/C DATE: 09/18/07 or later FAA Approved revisions

Models:

V2500-1A, V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, V2533-A5

ReplacedPartNumber:

International Aero Engines P/N 2A1701

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG NO ADP72176 REV N/C DATE 09/12/07 or later FAA Approved revisions

Models:

V2500-A1, V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2533-A5

ReplacedPartNumber:

International Aero Engines P/N 3A2425

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG NO ADP72181 REV N/C DATE 09/12/07 or later FAA Approved revisions

Models:

V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, V2533-A5

ReplacedPartNumber:

International Aero Engines P/N 5R0255

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG NO ADP72183 REV NC DATE 10/30/07 or later FAA Approved revisions

Models:

V2500-A1, V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, V2533-A5, V2525-D5, V2528-D5

ReplacedPartNumber:

International Aero Engines P/N 2A2191

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG NO ADP72177 REV N/C DATE 11/29/07 or later FAA Approved revisions

Models:

V2500-1A, V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, V2533-A5

ReplacedPartNumber:

International Aero Engines P/N 3A2425

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG NO: ADP72181 REV: N/C DATE: 09/12/07 or later FAA Approved revisions

Models:

V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, V2533-A5

ReplacedPartNumber:

Boeing 65B90687-4, Hook - Roller Hinge, Engine Side Cowl

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

747

ReplacedPartNumber:

International Aero Engines P/N 6A4354

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG NO ADP72188 REV NC DATE 10/24/07 or later FAA Approved revisions

Models:

V2500-A1, V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, V2533-A5, V2525-D5, V2528-D5

ReplacedPartNumber:

International Aero Engines P/N 6A1069

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG NO ADP72184 REV N/C DATE 09/18/07 or later FAA Approved revisions

Models:

V2500-A1, V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, V2533-A5

ReplacedPartNumber:

International Aero Engines P/N 3A1818

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG NO: ADP72180 REV: N/C DATE: 09/12/07 or later FAA Approved revisions

Models:

V2500-1A, V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2533-A5

ReplacedPartNumber:

Boeing 65B90676-602, Hook - Roller Hinge, Engine Side Cowl

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

747

ReplacedPartNumber:

International Aero Engines P/N 3A0710

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG NO: ADP72179 REV: N/C DATE: 09/12/07 or later FAA Approved revisions

Models:

V2500-1A, V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, V2533-A5

ReplacedPartNumber:

General Electric Aircraft Engines, P/N 4902T04G01 (W/ O Cover Plate SPAD)

ApprovalBasis:

Test and Computations per 14 CFR 21.303 (c) (4) DWG No TSG4902T04G01-1 Rev A Date Nov.17, 2000 or Later FAA approved Revisions

Models:

CJ610-1, -4, -5, -6, -8, -9, CF700-2D, -2D-2

ReplacedPartNumber:

Aero Design, Inc. P/N AD-4002P, GE/Gates P/N 41BO04AD07G3, Grimes P/N MISC-060 and MISC-0615, Engineered Magnetics P/N 803911-1, Saft P/N 16623-1 and 16624-1, Marathon S103 P/N 25503-025

ApprovalBasis:

Test and Computation per 14 CFR Part 21.303 (c)(4) Dwg No ABS-1002A, Rev Orig, Date April 20, 2008 or later FAA-approved revisions

Models:

DC-9, MD-80 Series) Dassault Aviation (Falcon 50 Series, Falcon 900 Series) Fokker (F28 Series

ReplacedPartNumber:

International Aero Engines P/N 2A3803

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG NO ADP72178 REV N/C DATE 12/3/07 or later FAA Approved revisions

Models:

V2500-A1, V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, V2533-A5, V2525-D5 V2528-D5

ReplacedPartNumber:

Piper 488-098, 71028-3, -5, 461-712, Engineered Fabrics Corp. 2F1-6-40556-6, -10

ApprovalBasis:

Identicality per 14 CFR 21.303 ( c) (4), licensing agreement between Floats & Fuel Cells and FFC Manufacturing, updated 4/11/05 and STC SA02918AT-D dated 4/11/05 Dwg. No. MDL 25-2810-003 Rev. I/R Date: 04/08/05 or later FAA approved revisions

Models:

PA-31, PA31-300, Serial Series 31-2 through 31-900, 31-7300901 and after with STC SA02918AT-D installed, PA 31-350, Serial Series 31-5001 through 31-5004, 31-7305005 and after with STC SA02918AT-D installed, PA-31-325C/R, Serial Series 31-7400990 and 31-7512001 and after with STC SA02918AT-D installed, PA-31-T1020, All serial numbers with STC SA02918AT-D installed

ReplacedPartNumber:

Piper 488-098, 71028-3, -5, 461-712, Engineered Fabrics Corp. 2F1-6-40556-6, -10

ApprovalBasis:

Identicality per 14 CFR 21.303 ( c) (4), licensing agreement between Floats & Fuel Cells and FFC Manufacturing, updated 4/11/05 and STC SA022918AT-D dated 4/11/05 Dwg. No. MDL 05-2810-003 Rev. I/R Date 04/08/05 or later FAA approved revisions

Models:

PA-31-325C/R, Serial Series 31-7400990 and 31-7512001 and after with STC SA022918AT-D installed, PA-31, PA31-300, Serial Series 31-2 through 31-900, 31-7300901 and after with STC SA022918AT-D installed, PA-31-T1020, All serial numbers with STC SA022918AT-D installed, PA 31-350, Serial Series 31-5001 through 31-5004, 31-7305005 and after with STC SA022918AT-D installed

ReplacedPartNumber:

Piper 488-100, 71027-3, -5, 461-715, Engineered Fabrics Corp. 2F1-6-33571-4, -6

ApprovalBasis:

Identicality per 14 CFR 21.303 ( c) (4), licensing agreement between Floats & Fuel Cells and FFC Manufacturing, updated 4/11/05 and STC SA022918AT-D dated 4/11/05 Dwg. No. MDL 05-2810-003 Rev. I/R Date 04/08/05 or later FAA approved revisions

Models:

PA 31-350, Serial Series 31-5001 through 31-5004, 31-7305005 and after with STC SA022918AT-D installed, PA-31-325C/R, Serial Series 31-7400990 and 31-7512001 and after with STC SA022918AT-D installed, PA-31-T1020, All serial numbers with STC SA022918AT-D installed, PA-31, PA31-300, Serial Series 31-2 through 31-900, 31-7300901 and after with STC SA022918AT-D installed

ReplacedPartNumber:

International Aero Engines 3A0137

ApprovalBasis:

Test and Computations per 14 CFR 21.303(c)(4)

Models:

V2500-A1

ReplacedPartNumber:

International Aero Engines P/N 3A0137

ApprovalBasis:

14 CFR FAR Part 21.303(c)4 Test and Computations, FAA Letter dated 1/7/99 and Dwg. No. M8001 Rev, NC dated 10/12/98 or later FAA Approval

Models:

V2500-A1

ReplacedPartNumber:

Allison Engine Co. 23060817

ApprovalBasis:

Identicality per FAR 21.303(c)(4)

Models:

250-C28B, -C28C

ReplacedPartNumber:

International Aero Engines 3A2050

ApprovalBasis:

Test and Computations per 14 CFR 21.303(c)(4)

Models:

V2500-A1

ReplacedPartNumber:

International Aero Engines 2A0127

ApprovalBasis:

Test and Computation per 14 CFR 21.303(c)(4), Dwg. No DEC47-008, Rev. A, Date 12/09/04, or later FAA Approved revisions

Models:

V2500-A1, V2522-A5, V2524-A5, V2525-D5, V2527-A5, V2527E-A5, V2528-D5, V2530-A5, V2533-A5

ReplacedPartNumber:

International Aero Engines 5A1821

ApprovalBasis:

Test and Computation per 14 CFR 21.303(c)(4), Dwg. No DEC47-005, Rev. No Revision, Date 07/02/04, or later FAA Approved revisions

Models:

V2522-A5, V2524-A5, V2525-D5, V2527-A5, V2527E-A5, V2528-D5, V2530-A5, V2533-A5

ReplacedPartNumber:

Piper 488-099, 71028-2, -4, 461-713, Engineered Fabrics Corp. 2F1-6-40556-5, -9

ApprovalBasis:

Identicality per 14 CFR 21.303 ( c) (4), licensing agreement between Floats & Fuel Cells and FFC Manufacturing, updated 4/11/05 and STC SA022918AT-D dated 4/11/05 Dwg. No. MDL 05-2810-003 Rev. I/R Date 04/08/05 or later FAA approved revisions

Models:

PA-31, PA31-300, Serial Series 31-2 through 31-900, 31-7300901 and after with STC SA022918AT-D installed, PA 31-350, Serial Series 31-5001 through 31-5004, 31-7305005 and after with STC SA022918AT-D installed, PA-31-T1020, All serial numbers with STC SA022918AT-D installed, PA-31-325C/R, Serial Series 31-7400990 and 31-7512001 and after with STC SA022918AT-D installed

ReplacedPartNumber:

Piper 488-100, 71027-3, -5, 461-715, Engineered Fabrics Corp. 2F1-6-33571-4, -6

ApprovalBasis:

Identicality per 14 CFR 21.303 ( c) (4), licensing agreement between Floats & Fuel Cells and FFC Manufacturing, updated 4/11/05 and STC SA02918AT-D dated 4/11/05 Dwg. No. MDL 25-2810-003 Rev. I/R Date: 04/08/05 or later FAA approved revisions

Models:

PA-31, PA31-300, Serial Series 31-2 through 31-900, 31-7300901 and after with STC SA02918AT-D installed, PA 31-350, Serial Series 31-5001 through 31-5004, 31-7305005 and after with STC SA02918AT-D installed, PA-31-325C/R, Serial Series 31-7400990 and 31-7512001 and after with STC SA02918AT-D installed, PA-31-T1020, All serial numbers with STC SA02918AT-D installed

ReplacedPartNumber:

International Aero Engines 3A0723

ApprovalBasis:

Test and Computations per 14 CFR 21.303(c)(4)

Models:

V2500-A1

ReplacedPartNumber:

Allison Engine Co. 23060816

ApprovalBasis:

Identicality per FAR 21.303(c)(4)

Models:

250-C20W, -C30 (All), -C30G, -C30L, -C30M, -C30P, -C30R, -C30R/1, -C30S, -C30U, -C47B, -C47M

ReplacedPartNumber:

Franklin Engine 17864

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

6A-350 Series, 6A4-150-B3, -B4, A64-165-B3, -B4, -B6, 6A4-200-C6, 6AS-335 Series, 6AS-350 Series

ReplacedPartNumber:

Allied-Signal Aerospace, Co. (Garrett Engine Div.) 3001436-1

ApprovalBasis:

Test and Computations per 14 CFR FAR 21.303(c)(4)

Models:

TPE331-1, -2, -2UA, -3U, -3UW, -5, -5A, -5AB, -5B, -6, -6A, -8, -10, -10N, -10R, -10U, -10UA, -10UF, -10UG, -10UGR, -10UR, 11U, 12UA, 12UAR, 12UHR, -25AA, -25AB, -25DA, -25DB, -25FA, -43-A,-47-A, -55-B, -61-A Series Engines

ReplacedPartNumber:

International Aero Engines P/N 3A2050

ApprovalBasis:

14 CFR FAR Part 21.303(c)4 Test and Computations, FAA Letter dated 1/13/99 and Dwg. No. M8003 Rev, NC dated 9/8/98 or later FAA Approval

Models:

V2500-A1

ReplacedPartNumber:

Allison Engine Co. 23060814

ApprovalBasis:

Identicality per FAR 21.303(c)(4)

Models:

250-C18, -C18A, -C18B, -C18C, -C20, -C20B (All), -C20C (T63-A-720), -C20J (All), -C20R/1 (All), -C20R/2 (All), -C20R/4

ReplacedPartNumber:

Franklin Engine 17794

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

6A-350 Series, 4A-235 Series, 6A4-165-B3, -B4, -B6 6A4-200, 6AS-335 Series, 6AS-350 Series

ReplacedPartNumber:

Piper 488-099, 71028-2, -4, 461-713, Engineered Fabrics Corp. 2F1-6-40556-5, -9

ApprovalBasis:

Identicality per 14 CFR 21.303 ( c) (4), licensing agreement between Floats & Fuel Cells and FFC Manufacturing, updated 4/11/05 and STC SA02918AT-D dated 4/11/05 Dwg. No. MDL 25-2810-003 Rev. I/R Date: 04/08/05 or later FAA approved revisions

Models:

PA-31, PA31-300, Serial Series 31-2 through 31-900, 31-7300901 and after with STC SA02918AT-D installed, PA 31-350, Serial Series 31-5001 through 31-5004, 31-7305005 and after with STC SA02918AT-D installed, PA-31-325C/R, Serial Series 31-7400990 and 31-7512001 and after with STC SA02918AT-D installed, PA-31-T1020, All serial numbers with STC SA02918AT-D installed

ReplacedPartNumber:

International Aero Engines 3A0727

ApprovalBasis:

Test and Computations per 14 CFR 21.303(c)(4)

Models:

V2500-A1

ReplacedPartNumber:

Allied-Signal Aerospace Co. (Garrett Engine Division) 897513-1

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

TPE331 and TFE731 Series

ReplacedPartNumber:

Piper 488-101, 71027-2, -4, 461-714, Engineered Fabrics Corp. 2F1-6-33571-3, -5

ApprovalBasis:

Identicality per 14 CFR 21.303 ( c) (4), licensing agreement between Floats & Fuel Cells and FFC Manufacturing, updated 4/11/05 and STC SA02918AT-D dated 4/11/05 Dwg. No. MDL 25-2810-003 Rev. I/R Date: 04/08/05 or later FAA approved revisions

Models:

PA-31, PA31-300, Serial Series 31-2 through 31-900, 31-7300901 and after with STC SA02918AT-D installed, PA 31-350, Serial Series 31-5001 through 31-5004, 31-7305005 and after with STC SA02918AT-D installed, PA-31-325C/R, Serial Series 31-7400990 and 31-7512001 and after with STC SA02918AT-D installed, PA-31-T1020, All serial numbers with STC SA02918AT-D installed

ReplacedPartNumber:

Allison Engine Co. 23060815

ApprovalBasis:

Identicality per FAR 21.303(c)(4)

Models:

250-C30 (All), -C30G, -C30G/2, -C30M, -C30S, -C40B

ReplacedPartNumber:

Piper 488-101, 71027-2, -4, 461-714, Engineered Fabrics Corp. 2F1-6-33571-3, -5

ApprovalBasis:

Identicality per 14 CFR 21.303 ( c) (4), licensing agreement between Floats & Fuel Cells and FFC Manufacturing, updated 4/11/05 and STC SA022918AT-D dated 4/11/05 Dwg. No. MDL 05-2810-003 Rev. I/R Date 04/08/05 or later FAA approved revisions

Models:

PA-31-325C/R, Serial Series 31-7400990 and 31-7512001 and after with STC SA022918AT-D installed, PA-31, PA31-300, Serial Series 31-2 through 31-900, 31-7300901 and after with STC SA022918AT-D installed, PA 31-350, Serial Series 31-5001 through 31-5004, 31-7305005 and after with STC SA022918AT-D installed, PA-31-T1020, All serial numbers with STC SA022918AT-D installed

ReplacedPartNumber:

International Aero Engines P/N 3A0727

ApprovalBasis:

14 CFR FAR Part 21.303(c)4 Test and Computations, FAA Letter dated 1/7/99 and Dwg. No. M8005 Rev, NC dated 10/12/98 or later FAA Approval

Models:

V2500-A1

ReplacedPartNumber:

Franklin Engine 14724

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

6A8-215-B8F, -B9F

ReplacedPartNumber:

Unison P/N 9045405-1, P/N 9045405-3, P/N 9045405-5, P/N 9045405-7, International Aero Engines P/N 5U0006, P/N 5U0052, P/N 5U0068, P/N 5U0072

ApprovalBasis:

Test and Computation per 14 CFR 21.303 (c) 4 Drwg. No. CH53564, Revision NR, Dated 8/16/04 Parts List No. 53564PP Revision NR, Dated 8/16/04 Or later FAA approved revisions

Models:

V2500-A1, V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, V2533-A5

ReplacedPartNumber:

Allison Engine Co. 23060813

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

250-B17C (All), -B17D (All), -B17E, -B17F, -B17F/1, -B17F/2, -C20S

ReplacedPartNumber:

Allison Engine Co. 23060818

ApprovalBasis:

Identicality per FAR 21.303(c)(4)

Models:

250-C20F, -C20R (All)

ReplacedPartNumber:

General Electric Engines, 4902T04G01

ApprovalBasis:

Test and Computations per CFR 21.303(c)(4)

Models:

CJ610-1, -4, -5, -6, -8, -9, CF700-2D, -2D-2

ReplacedPartNumber:

3870108-1 APU Engine Mount Only

ApprovalBasis:

Test and Computation per 14 CFR 21.303(c)(4), Dwg No DEC39-220, Rev. No Revision, Date 11/12/2002, or later FAA approved revisions.

Models:

737-600, 737-700, 737-800, 737-900

ReplacedPartNumber:

Engine Alliance P/N: 2121M15P01

ApprovalBasis:

Identicality per 14 CFR 21.303 (c), Licensing Agreement between AeroControlex Group and Engine Alliance dtd. 01/16/08 TC: E00072EN AeroControlex Group Dwg. No: AA5116-01, Rev. 4 dtd. 01/24/05 or later FAA Approved Revision

Models:

GP7270, GP7277

ReplacedPartNumber:

Honeywell P/N 3502093-2 installed in Honeywell Air Turbine Engine Starter P/Ns 3505526-3-1, 3505526-4-1, 3505526-5-1, 3505526-6-1, 3505526-7-1, 3505526-8-1, 3505526-9-1

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No.: P00815 Rev.: A Date: 4/17/2006 or later FAA approved revisions

Models:

737-300 Series, 737-400 Series, 737-500 Series

ReplacedPartNumber:

IAE International Aero Engines P/N 44066 installed in IAE International Aero Engines Chip Detector P/Ns: VB3521-2, 1A6794

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No: 44066FS Rev: A Date: 4/17/2006 or later FAA-approved revisions

Models:

V2527-A5, V2527E-A5) Airbus (A319 Model -131, A319 Model -132, A319 Model -133, A320 Model -231, A320 Model -232, A320 Model -233, A321 Model -131, A321 Model -231

ReplacedPartNumber:

Honeywell P/N 361753-1 installed in Honeywell Air Turbine Engine Starter P/N 3505188-9

ApprovalBasis:

Test and computations per 14 CFR 21.303 DWG No.: P00811 Rev.: A3 Date: 7/18/2007 or later FAA approved revisions

Models:

CL-600-2B19

ReplacedPartNumber:

Honeywell P/N 3164893-1 installed in Honeywell Engine Air Start Valve P/Ns 898930-8, -10 & Honeywell Pressure Regulating Shutoff Valve P/Ns 3215622-1, -2, 3213876-11

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No.: P00774 Rev.: C6 Date: 05/01/2007 or later FAA approved revisions

Models:

CL-600-2B19 (Regional Jet Series 100 & 400)

ReplacedPartNumber:

Garret Tur- bine Engine Co. P/N 3103235-8 Parker OEM

ApprovalBasis:

Identical Design Approval per FAR 21.303(c)

Models:

TPE331-10, -10A, -10B, -10G, -10GR, -10U, -10UA, -10UG, -10UGR, -10R, -10UF, -10UR, -11U, & -11UA

ReplacedPartNumber:

Garrett Tur- bine Engine Co. P/N 868752-1 Parker OEM

ApprovalBasis:

Identical Design Approval per FAR 21.303(c)

Models:

TPE331-3U, -3UW, -5, -6, -6A, -8, -10, -10R, -10U, -10UA, -10UF, -11U, & -11UA

ReplacedPartNumber:

Garrett Tur- bine Engine Co. P/N 868242-1 Parker OEM

ApprovalBasis:

Identical Design Approval per FAR 21.303(C)

Models:

TPE331-3U, -3UW, -5, -6, -6A, -8, -10, -10R, -10U, -10UA, -10UF, -11U, & -11UA

ReplacedPartNumber:

GE Aircraft Engines 2043M12PO3

ApprovalBasis:

Identicality per 14 CFR 21.303, licensing agreement between Argo-Tech Corp. and GE Aircraft Engines Dtd. 1-14-05 TC E0-00070EN Dwg. No 837600-3 Rev B, Dtd 1/13/04 Dwg. No. 837601-3 Rev. E, Dtd 1-13-04 or later FAA Approved Revision

Models:

CF34-10-E5, CF34-10E5A1, CF34-10E6, CF34-10E6A1

ReplacedPartNumber:

Allied-Signal 364435-10 installed in Allied-Signal Air Turbine Engine Starter 384022-1-3, 384022-2-1, 384022-3-1, 384022-4-1, 384022-4-2, 384022-5-1

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No. P00042 Rev. D Date 04/22/02 or later FAA approved revisions

Models:

747-200B Series, 747-200C Series, 747-200F Series, 747-300 Series

ReplacedPartNumber:

GE Aircraft Engines 5079T04P02

ApprovalBasis:

Identicality per 14 CFR 21.303, Licensing Agreement between Allen Aircraft Products, Inc. and GE Aircraft Engines dtd 10/20/04. TC E00063EN Allen Aircraft Products, Inc. Dwg. No 2009051.02, Rev. A dtd. 8/7/03 or later FAA Approved Revision

Models:

CF34-8E, All Models

ReplacedPartNumber:

GE Aircraft Engines 1689M10P09

ApprovalBasis:

Licensing Agreement

Models:

GE90-76B, GE90-77B, GE90-85B, GE90-90B, GE90-92B

ReplacedPartNumber:

Allied-Signal 364435-10 installed in Allied-Signal Air Turbine Engine Starter 384022-5-1

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No. P00042 Rev. D Date 04/22/02 or later FAA approved revisions

Models:

CF6-80A1, CF6-80A3, CF6-45A, CF6-45A2

ReplacedPartNumber:

General Electric Aircraft Engines 9033M17P04

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

CF6-6D, -6D1, -6D1A, -6K, -6K2, CF6-50A, -50C, -50CA, -50C1, -50C2, -50C2B, -50C2D, -50E, -50E1, -50E2, -50E2B., CF6-80A1, -80A3, -80C2A2, -80C2A3, -80C2A5, -80C2B4, -80C2B6, -80C2B1F, -80C2B1F1, -80C2B2F, -80C2B3F, -80C2B4F, -80C2B6F, -80C2D1F

ReplacedPartNumber:

Allison Engine 23061016

ApprovalBasis:

Licensing Agreement

Models:

AE2100 A, AE2100 C, AE2100 D3

ReplacedPartNumber:

General Electric Aircraft Engines 9386M93P01

ApprovalBasis:

Identicality per 14 CFR 21.303(c), Licensing Agreement

Models:

CFM56-2, CFM56-2A, CFM56-2B, CFM56-3, CFM56-3B, CFM56-3C, CFM56-5, CFM56-5-A1/F, CFM56-5A3, CFM56-5C4 DEV

ReplacedPartNumber:

Allied-Signal 364435-10 installed in Allied-Signal Air Turbine Engine Starter 3505448-5-1

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No. P00042 Rev. D Date 04/22/02 or later FAA approved revisions

Models:

747-200B Series, 747-200C Series, 747-200F Series, 747-300 Series, 767-200 Series, 767-300 Series | CF6-80A, CF6-80A1, CF6-80A2, CF6-80A3, CF6-80C2A1, CF6-80C2A5, CF6-80C2A8, CF6-80C2D1F | MD-11F

ReplacedPartNumber:

GE Aircraft Engines 5079T04P03

ApprovalBasis:

Identicality per 14 CFR 21.303, Licensing Agreement between Allen Aircraft Products, Inc. and GE Aircraft Engines dtd 2/17/05. TC E00070EN Allen Aircraft Products, Inc. Dwg. No 2009081.02, Rev. A dtd. 10/18/04 or later FAA Approved Revision

Models:

CF34-10E, All Models

ReplacedPartNumber:

Allied-Signal 364435-10 installed in Allied-Signal Air Turbine Engine Starter 3505448-3-1

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No. P00042 Rev. D Date 04/22/02 or later FAA approved revisions

Models:

767-200 Series | CF6-80A, CF6-80A2

ReplacedPartNumber:

Allied-Signal 364435-10 installed in Allied-Signal Air Turbine Engine Starter 384022-4-2

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No. P00042 Rev. D Date 04/22/02 or later FAA approved revisions

Models:

CF6-45A, CF6-45A2

ReplacedPartNumber:

Boeing 310T3152-13 installed in PW2000 Engine Mount INSTL 310N3020-6, 310N3020-14, 310N3020-16, & 310N3020-122

ApprovalBasis:

Test and Computations per 14 CFR 21.303 FSCC DWG No. 310T3152-13FS Rev B Date 09/01/04 or later FAA approved revisions

Models:

757-200 Series

ReplacedPartNumber:

GE Aircraft Engines 1689M10P09

ApprovalBasis:

Licensing Agreement

Models:

GE90-76B, GE90-77B, GE90-85B, GE90-90B, GE90-92B

ReplacedPartNumber:

GE Aircraft Engines 5071T99P02

ApprovalBasis:

Identicality per 14 CFR 21.303, Licensing Agreement between Allen Aircraft Products, Inc. and GE Aircraft Engines dtd 10/20/04. TC E00063EN Allen Aircraft Products, Inc. Dwg. No 3009051.02, Rev. D dtd. 8/7/03 or later FAA Approved Revision

Models:

CF34-8E, All Models

ReplacedPartNumber:

Allison Engine 23061016

ApprovalBasis:

Licensing Agreement

Models:

AE2100 A, AE2100 C, AE2100 D3

ReplacedPartNumber:

Nash Engineering Company P/N K-2407-2

ApprovalBasis:

Test and Computations per 14 CFR 21.303, DWG No. K-2407TMT Rev -, Dated 12/10/07 or later FAA approved revision

Models:

S-64E, S-64F when Nash Engineering Company Fuel Booster Pump P/N 65-5045-3 is installed.

ReplacedPartNumber:

Nash Engineering Company P/N K-2407-1

ApprovalBasis:

Test and Computations per 14 CFR 21.303, DWG No. K-2407TMT Rev -, Dated 12/10/07 or later FAA approved revision

Models:

S-64E, S-64F when Nash Engineering Company Fuel Booster Pump P/N 65-5045-3 is installed.

ReplacedPartNumber:

Nash Engineering Company P/N K-2407-3

ApprovalBasis:

Test and Computations per 14 CFR 21.303, DWG No. K-2407TMT Rev -, Dated 12/10/07 or later FAA approved revision

Models:

S-64E, S-64F when Nash Engineering Company Fuel Booster Pump P/N 65-5045-3 is installed.

ReplacedPartNumber:

Nash Engineering Company P/N 64-0226

ApprovalBasis:

Test and Computations per 14 CFR 21.303, DWG No. 64-0226TMT, Rev -, Date 8/07/07 or later FAA approved revision

Models:

S-64E, S-64F when Nash Engineering Company Fuel Booster Pump P/N 65-5045-3 is installed.

ReplacedPartNumber:

Nash Engineering Company P/N AS51986

ApprovalBasis:

Test and Computations per 14 CFR 21.303, DWG No. AS51986TMT, Rev -, Date 12/21/07 or later FAA approved revision

Models:

S-64E, S-64F when Nash Engineering Company Fuel Booster Pump P/N 65-5045-3 is installed.

ReplacedPartNumber:

Nash Engineering Company P/N 61-1574

ApprovalBasis:

Test and Computations per 14 CFR 21.303, DWG No. 61-1574TMT, Rev -, Date 1/07/07 or later FAA approved revision

Models:

S-64E, S-64F when Nash Engineering Company Fuel Booster Pump P/N 65-5045-3 is installed.

ReplacedPartNumber:

Nash Engineering Company P/N K-2407

ApprovalBasis:

Test and Computations per 14 CFR 21.303, DWG No. K-2407TMT Rev -, Dated 12/10/07 or later FAA approved revision

Models:

S-64E, S-64F when Nash Engineering Company Fuel Booster Pump P/N 65-5045-3 is installed.

ReplacedPartNumber:

Nash Engineering Company P/N K-2407-4

ApprovalBasis:

Test and Computations per 14 CFR 21.303, DWG No. K-2407TMT Rev -, Dated 12/10/07 or later FAA approved revision

Models:

S-64E, S-64F when Nash Engineering Company Fuel Booster Pump P/N 65-5045-3 is installed.

ReplacedPartNumber:

Franklin Bushing, Engine Mount P/N F10246

ApprovalBasis:

FAA Engineering Letter of design approval dated 5/4/95 and drawing Number AEF10246, Rev. I/R, dated 11/17/94 or ,later FAA approved revisions

Models:

2A-120-A, -B, -C, -D, 6A-350-C1, -C1A, -C2, -C2A, -D, -D1, -D1A, -D1B, 4A-235-B, -B2, -B3, -B4, -B6, 6AS-335-A, -B, 6A-335-A, -B, -B1, -B1A, -D

ReplacedPartNumber:

Engine Alliance 2405M25P01

ApprovalBasis:

Identicality Per 14 CFR Part 21, Section 21.303(e)(4), per licensing agreement between Engine Alliance and Pall Aeropower dated September 2, 2008 and DWG No. 2405M25P01 Rev. '--' dated 8/21/2008 or later FAA approved revision.

Models:

GP7270, GP7277

ReplacedPartNumber:

International Aero Engines (IAE) , P/N 740-1094-5

ApprovalBasis:

Testing and Computation per 14 CFR Part 21, section 21.303(c)(4) approval per Seal Dynamics, Inc. Dwg. No. SD740-1094-5 Rev. IR dated 7/27/04 or later FAA approval

Models:

V2500-A1 & -A5 Series Engines

ReplacedPartNumber:

Engine Alliance PN 2045M18P08

ApprovalBasis:

Identicality Per 14 CFR 21.303 (c) (4), per licensing agreement between Unison File No. 07011 dated 11/06/08, and Engine Alliance Company, Unison drawing 502977-8, Rev. A dated August 18, 2008 or later FAA approved revision.

Models:

GP7270, GP7277

ReplacedPartNumber:

International Aero Engines (IAE), P/N 740-1118-1

ApprovalBasis:

Testing and Computation per 14 CFR Part 21, section 21.303(c)(4) approval per Seal Dynamics, Inc. Dwg. No. SD740-1118-1 Rev. IR dated 7/27/04 or later FAA approval

Models:

V2500-A1 & -A5 series engines

ReplacedPartNumber:

Eagle Engineering 411T1233-5

ApprovalBasis:

Identicality per 14 CFR 21.303

Models:

767-200, and 767-300 Series

ReplacedPartNumber:

Eagle Engineering E9-64838-12

ApprovalBasis:

Identicality per 14 CFR 21.303

Models:

707 Series, 720

ReplacedPartNumber:

Eagle Engineering E411N1114-7A

ApprovalBasis:

Identicality per 14 CFR 21.303

Models:

737-100, 737-200, 737-200C, 737-300, 737-400, 737-500 Series, 757-200, 757-200PF, 757-200CB Series

ReplacedPartNumber:

Lewis Engineering 56B17S3

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No 102-00122 Rev B Date 04/05/00 or later FAA approved revisions

Models:

747-100, 747-200B

ReplacedPartNumber:

Engine Alliance P/N 2045M40P04

ApprovalBasis:

Identicality Per 14 CFR 21.303 (c) (4), per licensing agreement between Unison, File No. 07007 dated 05/28/08, and Unison Industries, Unison drawing 503001-4, Revision A dated January 7, 2008 or later FAA approved revision.

Models:

GP7270, GP7277

ReplacedPartNumber:

Engine Alliance P/N 2045M36P09

ApprovalBasis:

Identicality Per 14 CFR 21.303 (c) (4), per licensing agreement between Unison, File No. 07007 dated 05/28/08, and Unison Industries, Unison drawing 502996-9, Revision A, dated January 7, 2008 or later FAA approved revision.

Models:

GP7270, GP7277

ReplacedPartNumber:

Engine Alliance P/N 2045M56P03

ApprovalBasis:

Identicality Per 14 CFR 21.303 (c) (4), per licensing agreement between Engine Alliance, File No. 07008, dated 04/08/08, and Unison Industries, Unison drawing 501170-3, Revision A, dated May 12, 2008 or later FAA approved revision.

Models:

GP7270, GP7277

ReplacedPartNumber:

Engine Alliance P/N 2045M19P07

ApprovalBasis:

Identicality Per 14 CFR 21.303 (c) (4), per licensing agreement between Unison, File No. 07007 dated 05/28/08, and Unison Industries, Unison drawing 502978-7, Revision B, dated March 12, 2008 or later FAA approved revision.

Models:

GP7270, GP7277

ReplacedPartNumber:

Engine Alliance P/N 2045M37P07

ApprovalBasis:

Identicality Per 14 CFR 21.303 (c) (4), per licensing agreement between Engine Alliance, File No. 07006 dated 05/30/08, and Unison Industries, Unison drawing 502997-5, Revision A, dated April 17, 2008 or later FAA approved revision.

Models:

GP7270, GP7277

ReplacedPartNumber:

Engine Alliance P/N 2045M46P05

ApprovalBasis:

Identicality Per 14 CFR 21.303 (c) (4), per licensing agreement between Engine Alliance, File No. 07006 dated 05/30/08, and Unison Industries, Unison drawing 501425-5, Revision B, dated March 12, 2008 or later FAA approved revision.

Models:

GP7270, GP7277

ReplacedPartNumber:

Engine Alliance P/N 2045M18P07

ApprovalBasis:

Identicality Per 14 CFR 21.303 (c) (4), per licensing agreement between Unison, File No. 07007 dated 05/28/08, and Unison Industries, Unison drawing 502997-7, Revision B, dated March 12, 2008 or later FAA approved revision.

Models:

GP7270, GP7277

ReplacedPartNumber:

International Aero Engines PN 1023018

ApprovalBasis:

Identicality by Licensing Agreement with IAE letter dated 7/23/97 and previous approved PAL -Supplement No. 75.

Models:

V2500-A1f-A5,-D5

ReplacedPartNumber:

International Aero Engines PN L500101

ApprovalBasis:

Identicality by Licensing Agreement with IAE letter dated 7/23/97 and previous approved PAL -Supplement No. 75.

Models:

V2500-A1 ,-A5,-D5

ReplacedPartNumber:

International Aero Engines PN L500301

ApprovalBasis:

Identicality by Licensing Agreement with IAE letter dated 7/23/97 and previous approved PAL -Supplement No. 103.

Models:

V2525-D5 V2528-D5

ReplacedPartNumber:

International Aero Engines PN L500103

ApprovalBasis:

Identicality by Licensing Agreement with IAE letter dated 7/23/97 and previous approved PAL -Supplement No. 75.

Models:

V2500-A1.-A5.-D5

ReplacedPartNumber:

Engine Alliance P/N 2045M23P03

ApprovalBasis:

Identically Per 14 CFR 21.303 (c) (4), per licensing agreement between EA, File No. Unison 07004, Unison Industries, based on Unison Drawing 503004-3, Revision C, Dated 10/26/2007 or later FAA Approved revision

Models:

GP7270, GP7277

ReplacedPartNumber:

Engine Alliance P/N 2045M27P02

ApprovalBasis:

Identically Per 14 CFR 21.303 (c) (4), per licensing agreement between EA, File No. Unison 07004, Unison Industries, based on Unison Drawing 502988-2, Revision D, Dated 10/26/2007 or later FAA Approved revision

Models:

GP7270, GP7277

ReplacedPartNumber:

Engine Alliance P/N 2045M19P06

ApprovalBasis:

Identically Per 14 CFR 21.303 (c) (4), per licensing agreement between EA, File No. Unison 07004, Unison Industries, based on Unison Drawing 502978-6, Revision E, Dated 11/14/2007 or later FAA Approved revision

Models:

GP7270, GP7277

ReplacedPartNumber:

Engine Alliance P/N 2121M18P06

ApprovalBasis:

Identically Per 14 CFR 21.303 (c) (4), per licensing agreement between EA, File No. Unison 07004, Unison Industries, based on Unison Drawing 506519-2, Revision D, Dated 4/2/2007 or later FAA Approved revision

Models:

GP7270, GP7277

ReplacedPartNumber:

Engine Alliance P/N 2045M51P03

ApprovalBasis:

Identically Per 14 CFR 21.303 (c) (4), per licensing agreement between EA, File No. Unison 07004, Unison Industries, based on Unison Drawing 501445-3, Revision D, Dated 10/26/2007 or later FAA Approved revision

Models:

GP7270, GP7277

ReplacedPartNumber:

Engine Alliance P/N 2045M32P03

ApprovalBasis:

Identically Per 14 CFR 21.303 (c) (4), per licensing agreement between EA, File No. Unison 07004, Unison Industries, based on Unison Drawing 502992-3 , Revision C, Dated 10/24/2007 or later FAA Approved revision

Models:

GP7270, GP7277

ReplacedPartNumber:

Engine Alliance ACC496F3035

ApprovalBasis:

Identicality Per 14 CFR Part 21, Section 21.303(e)(4), per licensing agreement between Engine Alliance and Pall Aeropower dated November 29, 2007 and DWG No. 2045M92P01 Rev. 'N/A' dated 3/11/2005 or later FAA approved revision.

Models:

GP7270, GP7277

ReplacedPartNumber:

Engine Alliance P/N 2045M52P03

ApprovalBasis:

Identically Per 14 CFR 21.303 (c) (4), per licensing agreement between EA, File No. Unison 07004, Unison Industries, based on Unison Drawing 501450-3, Revision D, Dated 10/25/2007 or later FAA Approved revision

Models:

GP7270, GP7277

ReplacedPartNumber:

Engine Alliance P/N 175484P02

ApprovalBasis:

Identically Per 14 CFR 21.303 (c) (4), per licensing agreement between EA, File No. Unison 07004, Unison Industries, based on Unison Drawing 9044650-2 , Revision K, Dated 3/18/1997 or later FAA Approved revision

Models:

GP7270, GP7277

ReplacedPartNumber:

Engine Alliance P/N 2045M18P06

ApprovalBasis:

Identically Per 14 CFR 21.303 (c) (4), per licensing agreement between EA, File No. Unison 07004, Unison Industries, based on Unison Drawing 502977-6, Revision E, Dated 11/14/2007 or later FAA Approved revision

Models:

GP7270, GP7277

ReplacedPartNumber:

Engine Alliance P/N 2045M20P03

ApprovalBasis:

Identically Per 14 CFR 21.303 (c) (4), per licensing agreement between EA, File No. Unison 07004, Unison Industries, based on Unison Drawing 502979-3, Revision G, Dated 11/14/2007 or later FAA Approved revision

Models:

GP7270, GP7277

ReplacedPartNumber:

Engine Alliance P/N 2121M16P04

ApprovalBasis:

Identically Per 14 CFR 21.303 (c) (4), per licensing agreement between EA, File No. Unison 07004, Unison Industries, based on Unison Drawing 502982-4, Revision D, Dated 10/25/2007 or later FAA Approved revision

Models:

GP7270, GP7277

ReplacedPartNumber:

Engine Alliance ACC496F3035

ApprovalBasis:

Identicality Per 14 CFR Part 21, Section 21.303(e)(4), per licensing agreement between Engine Alliance and Pall Aeropower dated November 29, 2007 and DWG No. 2045M92P01 Rev. 'N/A' dated 3/11/2007 or later FAA approved revision.

Models:

GP7270, GP7277

ReplacedPartNumber:

Engine Alliance P/N 2045M29P02

ApprovalBasis:

Identically Per 14 CFR 21.303 (c) (4), per licensing agreement between EA, File No. Unison 07004, Unison Industries, based on Unison Drawing 502993-2, Revision E, Dated 10/26/2007 or later FAA Approved revision

Models:

GP7270, GP7277

ReplacedPartNumber:

Engine Alliance P/N 2045M40P03

ApprovalBasis:

Identically Per 14 CFR 21.303 (c) (4), per licensing agreement between EA, File No. Unison 07004, Unison Industries, based on Unison Drawing 503001-3, Revision D, Dated 10/26/2007 or later FAA Approved revision

Models:

GP7270, GP7277

ReplacedPartNumber:

Engine Alliance P/N 2045M37P06

ApprovalBasis:

Identically Per 14 CFR 21.303 (c) (4), per licensing agreement between EA, File No. Unison 07004, Unison Industries, based on Unison Drawing 506510-2, Revision D, Dated 4/2/2007 or later FAA Approved revision

Models:

GP7270, GP7277

ReplacedPartNumber:

Engine Alliance P/N 2121M17P04

ApprovalBasis:

Identically Per 14 CFR 21.303 (c) (4), per licensing agreement between EA, File No. Unison 07004, Unison Industries, based on Unison Drawing 502983-4, Revision E, Dated 10/25/2007 or later FAA Approved revision

Models:

GP7270, GP7277

ReplacedPartNumber:

Engine Alliance P/N 2045M49P04

ApprovalBasis:

Identically Per 14 CFR 21.303 (c) (4), per licensing agreement between EA, File No. Unison 07004, Unison Industries, based on Unison Drawing 501440-4, Revision E, Dated 11/14/2007 or later FAA Approved revision

Models:

GP7270, GP7277

ReplacedPartNumber:

Engine Alliance P/N 9238M66P10

ApprovalBasis:

Identically Per 14 CFR 21.303 (c) (4), per licensing agreement between EA, File No. Unison 07004, Unison Industries, based on Unison Drawing 503306-2, Revision AE, Dated 1/29/2005 or later FAA Approved revision

Models:

GP7270, GP7277

ReplacedPartNumber:

Engine Alliance PN 2045M55P02

ApprovalBasis:

Identically Per 14 CFR 21.303 (c) (4), per licensing agreement between EA, File No. Unison 07004, Unison Industries, based on Unison Drawing 501175-2, Revision B, Dated 3/14/2005 or later FAA Approved revision

Models:

GP7270, GP7277

ReplacedPartNumber:

Engine Alliance P/N 2045M31P03

ApprovalBasis:

Identically Per 14 CFR 21.303 (c) (4), per licensing agreement between EA, File No. Unison 07004, Unison Industries, based on Unison Drawing 502991-3, Revision D, Dated 10/25/2007 or later FAA Approved revision

Models:

GP7270, GP7277

ReplacedPartNumber:

Engine Alliance P/N 2045M88P06

ApprovalBasis:

Identically Per 14 CFR 21.303 (c) (4), per licensing agreement between EA, File No. Unison 07004, Unison Industries, based on Unison Drawing 503002-6, Revision F, Dated 10/25/2007 or later FAA Approved revision

Models:

GP7270, GP7277

ReplacedPartNumber:

Engine Alliance P/N 2045M38P06

ApprovalBasis:

Identically Per 14 CFR 21.303 (c) (4), per licensing agreement between EA, File No. Unison 07004, Unison Industries, based on Unison Drawing 506511-2, Revision D, Dated 4/2/2007 or later FAA Approved revision

Models:

GP7270, GP7277

ReplacedPartNumber:

Engine Alliance (EA) P/N 2411M18P01

ApprovalBasis:

Identicality per 14CFR 21.303(c) (4) Licensing Agreement between Engine Alliance and Hamilton Sundstrand, Ltr No. 775-L-0070-08 dated 3-12-08 TC E00072EN Dwg. 1706305 Rev F dated 2-28-08, or later FAA-approved revision.

Models:

GP7270, GP7277

ReplacedPartNumber:

Engine Alliance P/N 2045M43P04

ApprovalBasis:

Identically Per 14 CFR 21.303 (c) (4), per licensing agreement between EA, File No. Unison 07004, Unison Industries, based on Unison Drawing 503006-4, Revision F, Dated 11/29/2007 or later FAA Approved revision

Models:

GP7270, GP7277

ReplacedPartNumber:

Engine Alliance P/N 2045M21P02

ApprovalBasis:

Identically Per 14 CFR 21.303 (c) (4), per licensing agreement between EA, File No. Unison 07004, Unison Industries, based on Unison Drawing 502981-2, Revision E, Dated 11/14/2007 or later FAA Approved revision

Models:

GP7270, GP7277

ReplacedPartNumber:

Engine Alliance P/N 2045M76P04

ApprovalBasis:

Identically Per 14 CFR 21.303 (c) (4), per licensing agreement between EA, File No. Unison 07004, Unison Industries, based on Unison Drawing 502575-4, Revision F, Dated 9/26/2007 or later FAA Approved revision

Models:

GP7270, GP7277

ReplacedPartNumber:

Engine Alliance P/N 2045M47P03

ApprovalBasis:

Identically Per 14 CFR 21.303 (c) (4), per licensing agreement between EA, File No. Unison 07004, Unison Industries, based on Unison Drawing 501430-3, Revision F, Dated 11/14/2007 or later FAA Approved revision

Models:

GP7270, GP7277

ReplacedPartNumber:

Engine Alliance P/N 2045M36P08

ApprovalBasis:

Identically Per 14 CFR 21.303 (c) (4), per licensing agreement between EA, File No. Unison 07004, Unison Industries, based on Unison Drawing 502996-8, Revision H, Dated 10/26/2007 or later FAA Approved revision

Models:

GP7270, GP7277

ReplacedPartNumber:

Engine Alliance P/N 2045M39P04

ApprovalBasis:

Identically Per 14 CFR 21.303 (c) (4), per licensing agreement between EA, File No. Unison 07004, Unison Industries, based on Unison Drawing 502999-4, Revision C, Dated 10/26/2007 or later FAA Approved revision

Models:

GP7270, GP7277

ReplacedPartNumber:

Engine Alliance 2045M92P01

ApprovalBasis:

Identicality Per 14 CFR Part 21, Section 21.303(e)(4), per licensing agreement between Engine Alliance and Pall Aeropower dated November 29, 2007 and DWG No. 2045M92P01 Rev. 'N/A' dated 3/11/2005 or later FAA approved revision.

Models:

GP7270, GP7277

ReplacedPartNumber:

Engine Alliance P/N 2045M26P02

ApprovalBasis:

Identically Per 14 CFR 21.303 (c) (4), per licensing agreement between EA, File No. Unison 07004, Unison Industries, based on Unison Drawing 502987-2 , Revision C, Dated 3/1/2007 or later FAA Approved revision

Models:

GP7270, GP7277

ReplacedPartNumber:

Engine Alliance PN 2045M53P02

ApprovalBasis:

Identically Per 14 CFR 21.303 (c) (4), per licensing agreement between EA, File No. Unison 07004, Unison Industries, based on Unison Drawing 430252-1, Revision B, Dated 7/12/2005 or later FAA Approved revision

Models:

GP7270, GP7277

ReplacedPartNumber:

Engine Alliance P/N 2045M22P03

ApprovalBasis:

Identically Per 14 CFR 21.303 (c) (4), per licensing agreement between EA, File No. Unison 07004, Unison Industries, based on Unison Drawing 503003-3, Revision D, Dated 11/14/2007 or later FAA Approved revision

Models:

GP7270, GP7277

ReplacedPartNumber:

Engine Alliance P/N 2045M35P07

ApprovalBasis:

Identically Per 14 CFR 21.303 (c) (4), per licensing agreement between EA, File No. Unison 07004, Unison Industries, based on Unison Drawing 502994-7, Revision G, Dated 10/26/2007 or later FAA Approved revision

Models:

GP7270, GP7277

ReplacedPartNumber:

Engine Alliance P/N 2045M28P05

ApprovalBasis:

Identically Per 14 CFR 21.303 (c) (4), per licensing agreement between EA, File No. Unison 07004, Unison Industries, based on Unison Drawing 502989-5, Revision D, Dated 10/25/2007 or later FAA Approved revision

Models:

GP7270, GP7277

ReplacedPartNumber:

Engine Alliance P/N 2045M46P04

ApprovalBasis:

Identically Per 14 CFR 21.303 (c) (4), per licensing agreement between EA, File No. Unison 07004, Unison Industries, based on Unison Drawing 501425-4, Revision F, Dated 11/14/2007 or later FAA Approved revision

Models:

GP7270, GP7277

ReplacedPartNumber:

Engine Alliance PN 2045M54P01

ApprovalBasis:

Identically Per 14 CFR 21.303 (c) (4), per licensing agreement between EA, File No. Unison 07004, Unison Industries, based on Unison Drawing 430251, Revision N/A, Dated 11/18/2003 or later FAA Approved revision

Models:

GP7270, GP7277

ReplacedPartNumber:

Engine Alliance P/N 2121M19P06

ApprovalBasis:

Identically Per 14 CFR 21.303 (c) (4), per licensing agreement between EA, File No. Unison 07004, Unison Industries, based on Unison Drawing 506520-2, Revision D, Dated 4/2/2007 or later FAA Approved revision

Models:

GP7270, GP7277

ReplacedPartNumber:

Flight Equipment & Engineering Ltd B26201-903

ApprovalBasis:

Dwg No 903

Models:

340A, 340B, SF340A

ReplacedPartNumber:

Flight Equipment & Engineering Ltd B26201-904

ApprovalBasis:

Dwg No 904

Models:

340A, 340B, SF340A

ReplacedPartNumber:

Flight Equipment & Engineering Ltd. C26201-902

ApprovalBasis:

Dwg No 001

Models:

340A, 340B, SF340A

ReplacedPartNumber:

Flight Equipment & Engineering Ltd. C26201-901

ApprovalBasis:

Dwg No 002

Models:

340A, 340B, SF340A

ReplacedPartNumber:

The Young Engineers Corporation TYE 1000-1SHD

ApprovalBasis:

Test and Computation per 14 CFR 21.303 Dwg.: PE1000 Rev.: C Dated: 5/18/98 or later FAA approved revision

Models:

188A (S/N 1035 and up), 188C) McDonnell Douglas (DC-8-61F/-62F, DC-8-63/-63F, DC-8-71/-71F, DC-8-73F, DC-9-32) Boeing (727-100C Series, 727-200 Series, 737-200 Series, 737-300 Series

ReplacedPartNumber:

Pemco Engineers 80100

ApprovalBasis:

Identicality per 14 CFR 21.303 Dwg.: 80100 Rev.: A Dated: 10/05/78 or later FAA approved revision

Models:

DC-9-11, DC-9-12, DC-9-13, DC-9-14, DC-9-15, DC-9-15F, DC-9-21, DC-9-31, DC-9-32, DC-9-32F, DC-9-33F, DC-9-34, DC-9-34F, DC-9-41, DC-9-51, DC-9-81, DC-9-82, DC-9-83, DC-9-87, MD-88 MD-90-30

ReplacedPartNumber:

Hamilton Standard 814858-1 and 814858-3 (Used in Hamilton Sundstrand Engine Anti-ice Valve, 810502)

ApprovalBasis:

Test and Computation Per 14 CFR Part 21.303 Dwg AIR23017 Rev - Date 7/19/01 or later FAA approved revisions.

Models:

777-200 Series and 777-300 Series when Hamilton Standard Engine Anti-Ice Valve, P/N 810502 is installed.

ReplacedPartNumber:

Hamilton Standard P/Ns 808612-2 and 808612-3 (Used in Hamilton Sundstrand Engine Anti-Ice valve, P/N 810502)

ApprovalBasis:

Test and Computation Per 14 CFR Part 21.303 Dwg: AIR23018 Rev: - Date: 7/19/01 or later FAA approved revisions.

Models:

777-200 Series and 777-300 Series when Hamilton Standard Engine Anti-Ice Valve, P/N 810502 is installed.

ReplacedPartNumber:

Hamilton Standard P/Ns 814858-1 and 814858-3 (Used in Hamilton Sundstrand Engine Anti-ice Valve, P/N 810502)

ApprovalBasis:

Test and Computation Per 14 CFR Part 21.303 Dwg: AIR23017 Rev: - Date: 7/19/01 or later FAA approved revisions.

Models:

777-200 Series and 777-300 Series when Hamilton Standard Engine Anti-Ice Valve, P/N 810502 is installed.

ReplacedPartNumber:

Hamilton Standard 808612-2 and 808612-3, (Used in Hamilton Sundstrand Engine Anti-Ice valve, 810502)

ApprovalBasis:

Test and Computation Per 14 CFR Part 21.303

Models:

777-200 Series and 777-300 Series when Hamilton Standard Engine Anti-Ice Valve, P/N 810502 is installed.

ReplacedPartNumber:

Hamilton Standard 814858-1 and 814858-3 (Used in Hamilton Sundstrand Engine Anti-ice Valve, 810502)

ApprovalBasis:

Test and Computation Per 14 CFR Part 21.303

Models:

777-200 Series and 777-300 Series when Hamilton Standard Engine Anti-Ice Valve, P/N 810502 is installed.

ReplacedPartNumber:

Hamilton Standard 808612-2 and 808612-3 (Used in Hamilton Sundstrand Engine Anti-Ice valve, 810502)

ApprovalBasis:

Test and Computation Per 14 CFR Part 21.303

Models:

777-200 Series and 777-300 Series when Hamilton Standard Engine Anti-Ice Valve, P/N 810502 is installed.

ReplacedPartNumber:

Hamilton Standard 814858-1 and 814858-3, (Used in Hamilton Sundstrand Engine Anti-ice Valve, 810502)

ApprovalBasis:

Test and Computation Per 14 CFR Part 21.303

Models:

777-200 Series and 777-300 Series when Hamilton Standard Engine Anti-Ice Valve, P/N 810502 is installed.

ReplacedPartNumber:

McDonnell Douglas S4750950C26-29, McDonnell Douglas S3892972C26-29, Pemco Engineers 16100-503-26-29, Ancra 80928-10, AAR 47360-101

ApprovalBasis:

Tests and Computations per 14 CFR 21.303. Dwg: RK2001- 2 Rev. A, Dated 8/15/01 or later FAA approved revision

Models:

DC-8-11, -12, -21, -31, -32, -33, -41, -42, -43, -51, -52, -53, -61, -61F, -71, -71F, -73, -73F, DC-8F-54, DC-8F-55) Boeing (727-100 Series, 727-100C Series, 727-200 Series, 727-200F Series

ReplacedPartNumber:

Hamilton Standard 808612-2 and 808612-3 (Used in Hamilton Sundstrand Engine Anti-Ice valve, 810502)

ApprovalBasis:

Test and Computation Per 14 CFR Part 21.303 Dwg AIR23018 Rev - Date 7/19/01 or later FAA approved revisions.

Models:

777-200 Series and 777-300 Series when Hamilton Standard Engine Anti-Ice Valve, P/N 810502 is installed.

ReplacedPartNumber:

GE Aircraft Engines P/N 1326M38G01

ApprovalBasis:

Test & Computation per 14 CFR 21.303(c)(4) Dwg No: 1326M38G01ATS, Rev: NC, Date: 09/09/05, or later FAA-approved revisions

Models:

CF6-80C2A1, A2, A3, A5, A5F, A8, CF6-80C2B1, B1F, B1F1, B2, B2F, B4, B4F, B5F, B6, B6F, B6FA, B7F, B8F

ReplacedPartNumber:

GE Aircraft Engines P/N 1326M38G01

ApprovalBasis:

Test & Computation per 14 CFR 21.303(c)(4) Dwg No: 1326M38G01ATS, Rev: NC, Date: 09/09/05, or later FAA-approved revisions

Models:

CF6-80C2A1, A2, A3, A5, A5F, A8, CF6-80C2B1, B1F, B1F1, B2, B2F, B4, B4F, B5F, B6, B6F, B6FA, B7F, B8F

ReplacedPartNumber:

GE Aircraft Engines P/N 1326M37G01

ApprovalBasis:

Test & Computation per 14 CFR 21.303(c)(4) Dwg No: 1326M37G01ATS, Rev: NC, Date: 09/09/05, or later FAA-approved revisions

Models:

CF6-80C2A1, A2, A3, A5, A5F, A8, CF6-80C2B1, B1F, B1F1, B2, B2F, B4, B4F, B5F, B6, B6F, B6FA, B7F, B8F

ReplacedPartNumber:

GE Aircraft Engines P/N 1326M37G01

ApprovalBasis:

Test & Computation per 14 CFR 21.303(c)(4) Dwg No: 1326M37G01ATS, Rev: NC, Date: 09/09/05, or later FAA-approved revisions

Models:

CF6-80C2A1, A2, A3, A5, A5F, A8, CF6-80C2B1, B1F, B1F1, B2, B2F, B4, B4F, B5F, B6, B6F, B6FA, B7F, B8F

ReplacedPartNumber:

Engine Oil Screen

ApprovalBasis:

STC SE8409SW DWG #: C6SC-2 and C6SC-3 Date: 05/26/05 or later FAA approved revisions

Models:

GO-300, O-300, C-125, C-145, IO-360, TSIO-360

ReplacedPartNumber:

Modification Parts

ApprovalBasis:

FAA STC ST02219NY-D Master Data List 0125-05893-2132 Revision - dated Nov. 2, 206

Models:

MD-11( )

ReplacedPartNumber:

International Aero Engines P/N AS42714

ApprovalBasis:

Test and Computation per 14 CFR 21.303 (c)(4), Dwg. No. AS42714AFI Rev. NC dated 9/18/06 or later FAA approval

Models:

V2500-A1, V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, V2533-A5, V2525-D5, V2528-D5

ReplacedPartNumber:

Aeronautical Engineers Inc. 44550-101

ApprovalBasis:

STC SA1993SO

Models:

DC-9-15F

ReplacedPartNumber:

Franklin Engine Co

ApprovalBasis:

Surrendered

Models:

4-A-235-B

ReplacedPartNumber:

Franklin Engine Co

ApprovalBasis:

Surrendered

Models:

6A-335-B, -D, 6A-350-C1A, -C2, -D1, 6AS-350-A, -A1

ReplacedPartNumber:

Franklin Engine Co

ApprovalBasis:

Surrendered

Models:

6V4-200-C32, 6V5-335A, 6V-335A, -A1A

ReplacedPartNumber:

Franklin Engine Co

ApprovalBasis:

Surrendered

Models:

6V4-200-C33, 6V-335-A1B, -B, 6V5-335-B

ReplacedPartNumber:

Franklin Engine Co

ApprovalBasis:

Surrendered

Models:

6V4-178-B32, -B33, 6V4-200-C32, -C33, 6V-335-1, -B

ReplacedPartNumber:

Franklin Engine Co

ApprovalBasis:

Surrendered

Models:

6A4-150-B3

ReplacedPartNumber:

Franklin Engine Co

ApprovalBasis:

Surrendered

Models:

6A4-150-B3, 6A4-165-B3, 6A-335-A

ReplacedPartNumber:

International Aero Engines P/N 5A0803

ApprovalBasis:

Tests and Computations per 14 CFR 21.303 (c)(4), PTMI Dwg. No.: 5A0803PT, Rev.: N/C, Dated: 12-19-05, or later FAA approved revisions.

Models:

V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, V2533-A5, V2525-D5, V2528-D5

ReplacedPartNumber:

The Young Engineers Corporation TYE 1000-1SHD

ApprovalBasis:

Test and Computation per 14 CFR 21.303 Dwg No: PE1000 Rev: C Dated: 5/18/98 or later FAA approved revision

Models:

188C and 188A (S/N 1035 and up)) McDonnell Douglas (DC-8-61F/-62F, DC-8-63/-63F, DC-8-71/-71F, DC-8-73F, DC-9-32) Boeing (727-100C Series, 727-200 Series, 737-200 Series, 737-300 Series

ReplacedPartNumber:

Pemco Engineers 80100

ApprovalBasis:

Identicality per 14 CFR 21.303 Dwg No: 80100 Rev: A Dated: 10/05/78 or later FAA approved revision

Models:

DC-9-11/-12/-13, DC-9-14/-15, DC-9-15F/-21, DC-9-31/-32, DC-9-32F/-33F, DC-9-34/-34F, DC-9-41/-51/-81, DC-9-82/-83/-87, MD-88, MD-90-30

ReplacedPartNumber:

G.E. aircraft Engines 9387M17P10

ApprovalBasis:

Identicality per 14 CFR 21.303, licensing agreement between Pacific Scientific Electro Kinetics Division and GE Aircraft Engines, dated 1/13/04. Dwg. No: 87006-10 Rev: W Date: 8/24/00 or later FAA approved revisions

Models:

CF6-80E1A1 -80E1A4, -80E1A2, -80E1A3

ReplacedPartNumber:

GE Aircraft Engines P/N: 1962M36P01

ApprovalBasis:

Identicality per 14 CFR 21.303 licensing agreement between Triumph Thermal Systems, Inc. and GE Aircraft Engines dated October 14, 2003 TC: E13NE, E41NE DWG. NO.: UA538950-8 REV.: None DATE: 08/12/00 Or later FAA approved revisions.

Models:

CF6-80A, CF6-80A2, CF6-80C2, CF6-80C2B1, CF6-80C2B1F, CF6-80C2B1F1, CF6-80C2B1F2, CF6-80C2B2, CF6-80C2B2F2, CF6-80C2B3F, CF6-80C2B4, CF6-80C2B4F, CF6-80C2B5F, CF6-80C2B6, CF6-80C2B6F, CF6-80C2B6FA, CF6-80C2B7F, CF6-80C2B7F1, CF6-80C2B8F, CF6-80E1A1, CF6-80E1A2, CF6-80E1A3, CF6-80E1A4

ReplacedPartNumber:

GE Aircraft Engines P/N: 5034T31P02

ApprovalBasis:

Identicality per 14 CFR 21.303 licensing agreement between Triumph Thermal Systems, Inc. and GE Aircraft Engines dated October 14, 2003 TC: E8NE DWG. NO.: UA536190-3 REV.: N DATE: 12/06/95 Or later FAA approved revisions.

Models:

CT7-2A, CT7-2D, CT7-2D1, CT7-5A2, CT7-5A3, CT7-6, CT7-6A, CT7-6D, CT7-6E, CT7-7A, CT7-7A1, CT7-8, CT7-9B, CT7-9B1, CT7-9B2, CT7-9C, CT7-9C3, CT7-9D, CT7-9D2

ReplacedPartNumber:

GE Aircraft Engines P/N: 9377M44P01

ApprovalBasis:

Identicality per 14 CFR 21.303 licensing agreement between Triumph Thermal Systems, Inc. and GE Aircraft Engines dated October 14, 2003 TC: E13NE DWG. NO.: UA538728-1 REV.: C DATE: 05/06/01 Or later FAA approved revisions.

Models:

CF6-80C2, CF6-80C2A1, CF6-80C2A2, CF6-80C2A3, CF6-80C2A5, CF6-80C2A5F, CF6-80C2A8, CF6-80C2A9F, CF6-80C2B1, CF6-80C2B1F, CF6-80C2B1F1, CF6-80C2B1F2, CF6-80C2B2, CF6-80C2B2F, CF6-80C2B3F, CF6-80C2B4, CF6-80C2B4F, CF6-80C2B5F, CF6-80C2B6, CF6-80C2B6F, CF6-80C2B6FA, CF6-80C2B7F, CF6-80C2B7F1, CF6-80C2B8F, CF6-80C2D1F, CF6-80C2D2F

ReplacedPartNumber:

GE Aircraft Engines P/N: 1838M88P03

ApprovalBasis:

Identicality per 14 CFR 21.303 licensing agreement between Triumph Thermal Systems, Inc. and GE Aircraft Engines dated October 14, 2003 TC: E00049EN DWG. NO.: UA541461-4 REV.: L DATE: 02/10/02 Or later FAA approved revisions.

Models:

GE90

ReplacedPartNumber:

GE Aircraft Engines P/N: 1306M13P02

ApprovalBasis:

Identicality per 14 CFR 21.303 licensing agreement between Triumph Thermal Systems, Inc. and GE Aircraft Engines dated October 14, 2003 TC: E41NE DWG. NO.: UA538950-7 REV.: F DATE: 09/18/92 Or later FAA approved revisions.

Models:

CF6-80C2B1F, CF6-80C2B6FA

ReplacedPartNumber:

GE Aircraft Engines P/N: 5044T42P02

ApprovalBasis:

Identicality per 14 CFR 21.303 licensing agreement between Triumph Thermal Systems, Inc. and GE Aircraft Engines dated October 14, 2003 TC: E8NE DWG. NO.: UA537628-1 REV.: J DATE: 01/28/88 Or later FAA approved revisions.

Models:

CT7-2D1, CT7-5A2, CT7-5A3, CT7-5FLT, CT7-7A, CT7-7A1, CT7-7FLT

ReplacedPartNumber:

GE Aircraft Engines P/N: 9268M48P02

ApprovalBasis:

Identicality per 14 CFR 21.303 licensing agreement between Triumph Thermal Systems, Inc. and GE Aircraft Engines dated October 14, 2003 TC: E13NE DWG. NO.: UA538728-2 REV.: E DATE: 09/12/83 Or later FAA approved revisions.

Models:

CF6-80C2

ReplacedPartNumber:

GE Aircraft Engines P/N: 1838M88P11

ApprovalBasis:

Identicality per 14 CFR 21.303 licensing agreement between Triumph Thermal Systems, Inc. and GE Aircraft Engines dated October 14, 2003 TC: E00049EN DWG. NO.: UA541461-12 REV.: L DATE: 02/10/02 Or later FAA approved revisions.

Models:

GE90-76B, GE90-77B, GE90-85B, GE90-90B, GE90-94B, GE90-110B1, GE90-113B, GE90-115B

ReplacedPartNumber:

GE Aircraft Engines P/N: 1838M91P07

ApprovalBasis:

Identicality per 14 CFR 21.303 licensing agreement between Triumph Thermal Systems, Inc. and GE Aircraft Engines dated October 14, 2003 TC: E00049EN DWG. NO.: UA541462-8 REV.: D DATE: 08/09/98 Or later FAA approved revisions.

Models:

GE90-76B, GE90-77B, GE90-85B, GE90-90B, GE90-94B

ReplacedPartNumber:

GE Aircraft Engines P/N: 9268M48P02

ApprovalBasis:

Identicality per 14 CFR 21.303 licensing agreement between Triumph Thermal Systems, Inc. and GE Aircraft Engines dated October 14, 2003 TC: E13NE DWG. NO.: UA538283-2 REV.: E DATE: 09/12/83 Or later FAA approved revisions.

Models:

CF6-80C2

ReplacedPartNumber:

GE Aircraft Engines P/N: 1838M91P05

ApprovalBasis:

Identicality per 14 CFR 21.303 licensing agreement between Triumph Thermal Systems, Inc. and GE Aircraft Engines dated October 14, 2003 TC: E00049EN DWG. N O.: UA541462-6 REV.: D DATE: 08/09/98 Or later FAA approved revisions.

Models:

GE90-76B, GE90-77B, GE90-85B, GE90-90B, GE90-94B

ReplacedPartNumber:

GE Aircraft Engines P/N: 1838M91P08

ApprovalBasis:

Identicality per 14 CFR 21.303 licensing agreement between Triumph Thermal Systems, Inc. and GE Aircraft Engines dated October 14, 2003 TC: E00049EN DWG. NO.: UA541462-9 REV.: D DATE: 08/09/98 Or later FAA approved revisions.

Models:

GE90-76B, GE90-77B, GE90-85B, GE90-90B, GE90-94B

ReplacedPartNumber:

GE Aircraft Engines 1691M44P03

ApprovalBasis:

Identicality per 14 CFR Part 21 21.303(c)(4), Licensing agreement

Models:

GE90-94B

ReplacedPartNumber:

GE Aircraft Engines P/N: 1838M90P03

ApprovalBasis:

Identicality per 14 CFR 21.303 licensing agreement between Triumph Thermal Systems, Inc. and GE Aircraft Engines dated October 14, 2003 TC: E00049EN DWG. NO.: UA541463-4 REV.: B DATE: 10/31/94 Or later FAA approved revisions.

Models:

GE90-76B, GE90-77B, GE90-85B, GE90-90B, GE90-94B, GE90-110B1, GE90-113B, GE90-115B

ReplacedPartNumber:

GE Aircraft Engines P/N: 1838M91P06

ApprovalBasis:

Identicality per 14 CFR 21.303 licensing agreement between Triumph Thermal Systems, Inc. and GE Aircraft Engines dated October 14, 2003 TC: E00049EN DWG. NO.: UA541462-7 REV.: D DATE: 08/09/98 Or later FAA approved revisions.

Models:

GE90-76B, GE90-77B, GE90-85B, GE90-90B, GE90-94B

ReplacedPartNumber:

GE Aircraft Engines P/N: 1306M13P02

ApprovalBasis:

Identicality per 14 CFR 21.303 licensing agreement between Triumph Thermal Systems, Inc. and GE Aircraft Engines dated October 14, 2003 TC: E13NE DWG. NO.: UA538950-4 REV.: F DATE: 09/18/92 Or later FAA approved revisions.

Models:

CF6-80C2B1F, CF6-80C2B6FA

ReplacedPartNumber:

GE Aircraft Engines P/N: 9280M60P02

ApprovalBasis:

Identicality per 14 CFR 21.303 licensing agreement between Triumph Thermal Systems, Inc. and GE Aircraft Engines dated October 14, 2003 TC: E13NE DWG. NO.: UA538342-2 REV.: A DATE: 05/03/81 Or later FAA approved revisions.

Models:

CF6-80A1, CF6-80A3

ReplacedPartNumber:

GE Aircraft Engines P/N: 1838M89P04

ApprovalBasis:

Identicality per 14 CFR 21.303 licensing agreement between Triumph Thermal Systems, Inc. and GE Aircraft Engines dated October 14, 2003 TC: E00049EN DWG. NO.: UA541464-5 REV.: D DATE: 09/21/01 Or later FAA approved revisions.

Models:

GE90-76B, GE90-77B, GE90-85B, GE90-90B, GE90-94B, GE90-110B1, GE90-113B, GE90-115B

ReplacedPartNumber:

GE Aircraft Engines P/N: 1838M89P03

ApprovalBasis:

Identicality per 14 CFR 21.303 licensing agreement between Triumph Thermal Systems, Inc. and GE Aircraft Engines dated October 14, 2003 TC: E00049EN DWG. NO.: UA541464-4 REV.: D DATE: 09/21/01 Or later FAA approved revisions.

Models:

GE90-76B, GE90-77B, GE90-85B, GE90-90B, GE90-94B, GE90-110B1, GE90-113B, GE90-115B

ReplacedPartNumber:

Pemco Engineers 80100

ApprovalBasis:

Identicality per 14 CFR 21.303

Models:

DC-9-11, -12, -13, -14, -15, -15F, -21, -31, -32, -32F, -33F, -34, -34F, -41, -51, -81, -82, -83, -87, MD-88, MD-90-30

ReplacedPartNumber:

GE Aircraft Engine 9227M70P01

ApprovalBasis:

Identicality per 14 CFR 21.303, Licensing Agreement

Models:

CF6-80A

ReplacedPartNumber:

GE Aircraft Engine 9227M69P01

ApprovalBasis:

Identicality per 14 CFR 21.303, Licensing Agreement

Models:

CF6-80A

ReplacedPartNumber:

GE Aircraft Engine 9210M41P01

ApprovalBasis:

Identicality per 14 CFR 21.303, Licensing Agreement

Models:

CF6-80A

ReplacedPartNumber:

GE Aircraft Engine 9210M42P05

ApprovalBasis:

Identicality per 14 CFR 21.303, Licensing Agreement

Models:

CF6-80A

ReplacedPartNumber:

Teledyne Continental Motor Engine 642066

ApprovalBasis:

Test and Computation per 14 CFR 21.303

Models:

TSIO-520-L/-LB/-WB

ReplacedPartNumber:

Teledyne Continental Motor Engine 640704, 640705

ApprovalBasis:

Test and Computation per 14 CFR 21.303

Models:

TSIO-520-L/-LB/-WB

ReplacedPartNumber:

Teledyne Continental Motor (TCM) Engine 640706, 640707, 640677

ApprovalBasis:

Test and Computation per 14 CFR 21.303

Models:

TSIO-520-L/-LB/-WB

ReplacedPartNumber:

Lycoming Engine LW-16825

ApprovalBasis:

Test and Computation per 14 CFR 21.303

Models:

TIO-540-J2B/-J2BD/ -N2BD/-R2AD, LTIO-540-J2B/-J2BD/-R2AD

ReplacedPartNumber:

Lycoming Engine LW-16826

ApprovalBasis:

Test and Computation per 14 CFR 21.303

Models:

TIO-540-J2B/-J2BD/ -R2AD, LTIO-540-J2B/-J2BD/-R2AD

ReplacedPartNumber:

Teledyne Continental Motor Engine 640711

ApprovalBasis:

Test and Computation per 14 CFR 21.303

Models:

TSIO-520-L/-LB/-WB

ReplacedPartNumber:

Teledyne Continental Motor Engine 640710

ApprovalBasis:

Test and Computation per 14 CFR 21.303

Models:

TSIO-520-L/-LB/-WB

ReplacedPartNumber:

Lycoming Engine LW-16826

ApprovalBasis:

Test and Computation per 14 CFR 21.303

Models:

TIO-540-J2B/-J2BD/ -R2AD, LTIO-540-J2B/-J2BD/-R2AD

ReplacedPartNumber:

Teledyne Continental Motor Engine 643882

ApprovalBasis:

Test and Computation per 14 CFR 21.303

Models:

T188C (S/N's T18803798T, T18803803T, T18803804T, T18803811T, T18803817T & On)

ReplacedPartNumber:

Teledyne Continental Motor Engine 642067

ApprovalBasis:

Test and Computation per 14 CFR 21.303

Models:

TSIO-520-L/-LB/-WB

ReplacedPartNumber:

Lycoming Engine LW-16825

ApprovalBasis:

Test and Computation per 14 CFR 21.303

Models:

TIO-540-J2B/-J2BD/ -N2BD/-R2AD, LTIO-540-J2B/-J2BD/-R2AD

ReplacedPartNumber:

Dick Wilson Aero Engineering Co. DW-1

ApprovalBasis:

Identicality per 14 CFR 21.303, licensing agreement

Models:

Raytheon) (35-33, 35-A33, 35-B33, 35-C33, 35-C33A, E33, E33A, E33C, F33, F33A, F33C, G33, 36, A36, A36TC, B36TC

ReplacedPartNumber:

Dick Wilson Aero Engineering Co. DW-1

ApprovalBasis:

Identicality per 14 CFR 21.303, licensing agreement

Models:

Raytheon) (35-33, 35-A33, 35-B33, 35-C33, 35-C33A, E33, E33A, E33C, F33, F33A, F33C, G33, 36, A36, A36TC, B36TC

ReplacedPartNumber:

Modification Part

ApprovalBasis:

STC SA1704CE, SA1602CE, SA1178CE, SA1583CE

Models:

Raytheon) (65,A65,A65-8200, 65-80,65-A80, 65-A80-8800, 65-B80,65-88, 65-90,65-A90, 65-A90-1, 65-A90-2, 65-A90-3, 65-A90-4, 70,B90,C90, E90, 99,99A,99A(FACH), A99,A99A,B99,C99, 100,A100,A100A, A100C,B100, 200,200C,200CT, 200T,A200,A200C, A200CT, F90

ReplacedPartNumber:

International Aero Engines 5L0072

ApprovalBasis:

Identicality per FAR 21.303(c)

Models:

V2500-D5

ReplacedPartNumber:

GE Aircraft Engines 1752M18P07

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4), Licensing Agreement

Models:

CF6-80E1

ReplacedPartNumber:

McDonnell Douglas S4750950C26-29, S3892972C26-29, Pemco Engineers 16100-503-26-29, Ancra 80928-10, AAR 47360-101

ApprovalBasis:

Tests and Computations per 14 CFR 21.303

Models:

DC-8-11, -12, -21,-31, -32, -33, -41, -42, -43, -51, -52, -53, -61, -61F, -71, -71F, -73, -73F, DC-8F-54, DC-8F-55

ReplacedPartNumber:

The Young Engineers Corporation TYE 1000-1SHD

ApprovalBasis:

Test and Computation per 14 CFR 21.303 Dwg No: PE1000 Rev: C Dated: 5/18/98 or later FAA approved revision

Models:

188C and 188A (S/N 1035 and up) | DC-8-61F/-62F, DC-8-63/-63F, DC-8-71/-71F, DC-8-73F, DC-9-32 | 727-100C Series, 727-200 Series, 737-200 Series, 737-300 Series

ReplacedPartNumber:

Pemco Engineers 80100

ApprovalBasis:

Identicality per 14 CFR 21.303 Dwg No: 80100 Rev: A Dated: 10/05/78 or later FAA approved revision

Models:

DC-9-11/-12/-13, DC-9-14/-15, DC-9-15F/-21, DC-9-31/-32, DC-9-32F/-33F, DC-9-34/-34F, DC-9-41/-51/-81, DC-9-82/-83/-87, MD-88, MD-90-30

ReplacedPartNumber:

McDonnell Douglas S4750950C26-29, S3892972C26-29, Pemco Engineers 16100-503-26-29, Ancra 80928-10, AAR 47360-101

ApprovalBasis:

Tests and Computations per 14 CFR 21.303

Models:

727-100 Series, 727-100C Series, 727-200 Series, 727-200F Series

ReplacedPartNumber:

International Aero Engines, 5U0019

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

V2500-A1, V2522-A5, V2524-A5, V2527-A5, V2530-A5, V2533-A5, V2525-D5, V2528-D5

ReplacedPartNumber:

BMW Rolls Royce Aero Engines 9060440-1

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4), Licensing Agreement

Models:

BR700-715A1-30, 715B1-30, 715C1-30

ReplacedPartNumber:

International Aero Engines, 5U0028

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

V2500-A1, V2522-A5, V2524-A5, V2527-A5, V2530-A5, V2533-A5, V2525-D5, V2528-D5, V2500-A1

ReplacedPartNumber:

International Aero Engines 4P0220

ApprovalBasis:

Test and computations per 14 CFR 21.303(c), Jesse Industries DWG No 4P0220JI Rev N/C Date 03/10/04 Or later FAA approved revisions.

Models:

V2500-A1, V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, V2533-A5, V2525-D5, V2528-D5

ReplacedPartNumber:

International Aero Engines 4P0223

ApprovalBasis:

Test and omputations per 14 CFR 21.303(c), Jesse Industries DWG No 4P0223JI Rev N/C Date 03/10/04 Or later FAA approved revisions.

Models:

V2500-A1, V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, V2533-A5, V2525-D5, V2528-D5

ReplacedPartNumber:

BMW Rolls Royce Aero Engines 83311-430973-10

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4), Licensing Agreement

Models:

BR700-710A2-20

ReplacedPartNumber:

BMW Rolls Royce Aero Engines 83311-430973-11

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4), Licensing Agreement

Models:

BR700-710A2-20

ReplacedPartNumber:

General Electric Aircraft Engines 4095T13P04-1

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

CFE738

ReplacedPartNumber:

BMW Rolls Royce Aero Engines 83311-430143

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4), Licensing Agreement

Models:

BR700-710A2-20

ReplacedPartNumber:

BMW Rolls Royce Aero Engines 83311-430973-12

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4), Licensing Agreement

Models:

BR700-710A1-10

ReplacedPartNumber:

Light Helicopter Turbine Engine LH70001-04 Ignition Unit

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

CT800-0

ReplacedPartNumber:

Godfrey Engineering GE16731-2

ApprovalBasis:

Test and Computation per 14 CFR 21.303(c)(4)

Models:

717 Series | DC-9, MD-80, and MD-90 Series

ReplacedPartNumber:

International Aero Engines, 5U0012

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

V2500-A1, V2522-A5, V2524-A5, V2527-A5, V2530-A5, V2533-A5, V2525-D5, V2528-D5

ReplacedPartNumber:

International Aero Engines 5U0073

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

V2500-D5

ReplacedPartNumber:

AVITAS Engineering AV31-001

ApprovalBasis:

Licensing Agreement

Models:

737-100,-200

ReplacedPartNumber:

AVITAS Engineering AV31-001

ApprovalBasis:

Licensing Agreement

Models:

727-100, -200

ReplacedPartNumber:

BMW Rolls Royce Aero Engines 83311-430973-6

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4), Licensing Agreement

Models:

BR700-710A2-20

ReplacedPartNumber:

BMW Rolls Royce Aero Engines 83311-430973-13

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4), Licensing Agreement

Models:

BR700-710A1-10

ReplacedPartNumber:

BMW Rolls Royce Aero Engines 83311-430973-7

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4), Licensing Agreement

Models:

BR700-710A2-20

ReplacedPartNumber:

International Aero Engines 5U0072

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

V2500-A1 and -A5

ReplacedPartNumber:

Allied Signal Garrett Auxiliary Engine Division, 3051402-1

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

CFE738

ReplacedPartNumber:

BMW Rolls Royce Aero Engines 83311-431017-2

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4), Licensing Agreement

Models:

BR700-715A1-30, 715B1-30, 715C1-30

ReplacedPartNumber:

International Aero Engines, 5U0014

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

V2500-A1, V2522-A5, V2524-A5, V2527-A5, V2530-A5, V2533-A5, V2525-D5, V2528-D5

ReplacedPartNumber:

Allied Signal Garrett Auxiliary Engine Division, 3051401-2

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

CFE738

ReplacedPartNumber:

International Aero Engines 5U0071

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

V2500-A1, -A5, and -D5

ReplacedPartNumber:

Allied Signal Electric Engine Starter Clutch Housing, 372695-1

ApprovalBasis:

Test and Computations per 14 CFR Part 21 21.303(c)(4)

Models:

Allied Signal Electric Engine Starter Models 3605812-16, -17, -18, -19, -21, and -22 used on 707, 727-100, 727-200, 737, 737-300 | Allied Signal Electric Engine Starter Models 3605812-16, -17, -18, -19, -21, and -22 used on 1-11 | Allied Signal Electric Engine Starter Models 3605812-16, -17, -18, -19, -21, and -22 used on DC8-70, DC9-10/30, DC9-50, DC9-80, MD80 | Allied Signal Electric Engine Starter Models 3605812-16, -17, -18, -19, -21, and -22 used on Trident 1, 2E, 3B and Mercure

ReplacedPartNumber:

Allied Signal Electric Engine Starter Retainer Clutch, 371455-1

ApprovalBasis:

Test and Computations per 14 CFR Part 21 21.303(c)(4)

Models:

Allied Signal Electric Engine Starter Models 3605812-16, -17, -18, -19, -21, and -22 used on 707, 727-100, 727-200, 737, 737-300 | Allied Signal Electric Engine Starter Models 3605812-16, -17, -18, -19, -21, and -22 used on 1-11 | Allied Signal Electric Engine Starter Models 3605812-16, -17, -18, -19, -21, and -22 used on DC8-70, DC9-10/30, DC9-50, DC9-80, MD80 | Allied Signal Electric Engine Starter Models 3605812-16, -17, -18, -19, -21, and -22 used on Trident 1, 2E, 3B and Mercure aircraft

ReplacedPartNumber:

Allied Signal Electric Engine Starter Clutch Housing 372695-1

ApprovalBasis:

Test and Computations per 14 CFR Part 21 21.303(c)(4)

Models:

Allied Signal Electric Engine Starter Models: 3605812-1, -2-1, -3, -4, -9, -10-1, -11, -12, -13-1, -14-1, 372697-6, -9, -10, -13, -15, -16, -18-1, -21-1, -22, -24 and 375322-7, -8, -9, -10 where used on airplane models: MD80, DC9 (TWA), Allied Signal Electric Engine Starter Models: 3605812-1, -2-1, -3, -4, -9, -10-1, -11, -12, -13-1, -14-1, 372697-6, -9, -10, -13, -15, -16, -18-1, -21-1, -22, -24 and 375322-7, -8, -9, -10 where used on airplane models 707, 727-100, 727-200, 737, 737-3, Allied Signal Electric Engine Starter Models: 3605812-1, -2-1, -3, -4, -9, -10-1, -11, -12, -13-1, -14-1, 372697-6, -9, -10, -13, -15, -16, -18-1, -21-1, -22, -24 and 375322-7, -8, -9, -10 where used on airplane models: DC-8-70, DC9-10/30, DC9-50/80, Allied Signal Electric Engine Starter Models: 3605812-1, -2-1, -3, -4, -9, -10-1, -11, -12, -13-1, -14-1, 372697-6, -9, -10, -13, -15, -16, -18-1, -21-1, -22, -24 and 375322-7, -8, -9, -10 where used on airplane models: 1-11, Trident 1, 2E,3B and Mercu

ReplacedPartNumber:

Allied Signal Electric Engine Starter Retainer Clutch 371455-1 and 371455

ApprovalBasis:

Test and Computations per 14 CFR Part 21 21.303(c)(4)

Models:

Allied Signal Electric Engine Starter Models: 3605812-1, -2-1, -3, -4, -9, -10-1, -11, -12, -13-1, -14-1, 372697-6, -9, -10, -13, -15, -16, -18-1, -21-1, -22, -24 and 375322-7, -8, -9, -10 where used on airplane models 707, 727-100, 727-200, 737, 737-3, Allied Signal Electric Engine Starter Models: 3605812-1, -2-1, -3, -4, -9, -10-1, -11, -12, -13-1, -14-1, 372697-6, -9, -10, -13, -15, -16, -18-1, -21-1, -22, -24 and 375322-7, -8, -9, -10 where used on airplane models: DC-8-70, DC9-10/30 DC9-50/80, Allied Signal Electric Engine Starter Models: 3605812-1, -2-1, -3, -4, -9, -10-1, -11, -12, -13-1, -14-1, 372697-6, -9, -10, -13, -15, -16, -18-1, -21-1, -22, -24 and 375322-7, -8, -9, -10 where used on airplane models: MD80, DC9 (TWA), Allied Signal Electric Engine Starter Models: 3605812-1, -2-1, -3, -4, -9, -10-1, -11, -12, -13-1, -14-1, 372697-6, -9, -10, -13, -15, -16, -18-1, -21-1, -22, -24 and 375322-7, -8, -9, -10 where used on airplane models: 1-11, Trident 1, 2E,3B and Mercu

ReplacedPartNumber:

Allied Signal Garrett Auxiliary Engine Division, 3051400-1

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

CFE738

ReplacedPartNumber:

IAE Int l Aero Engines VTB12350E

ApprovalBasis:

Identicality per 14 CFR 21.303, Licensing Agreement

Models:

V2500-A1, and V2500-A5 Series

ReplacedPartNumber:

Aero Products Engineering AP-2009

ApprovalBasis:

Licensing Agreement, STC SA2-983

Models:

RC-3

ReplacedPartNumber:

International Aero Engines, 5U0020

ApprovalBasis:

Identicality per 14 CFR 21.303(c)(4)

Models:

V2500-A1, V2522-A5, V2524-A5, V2527-A5, V2530-A5, V2533-A5, V2525-D5, V2528-D5

ReplacedPartNumber:

Aero Products Engineering AP-2008

ApprovalBasis:

Licensing Agreement, STC SA2-983

Models:

RC-3

ReplacedPartNumber:

Garrett Engine Div Plug, Machine 572-510-9002

ApprovalBasis:

Identicality per FAR 21.303(c)

Models:

747-200 (starter)

ReplacedPartNumber:

Pratt & Whitney Engine 234223

ApprovalBasis:

Identicality per 14 CFR 21.303

Models:

R-985 Wasp Jr. Series AN-1, -3, -4, -6,-6B, -10 -12, -12B, -14B, B3, B4, and B5

ReplacedPartNumber:

Pratt & Whitney Engine 34749

ApprovalBasis:

Identicality per 14 CFR 21.303

Models:

R-985 Wasp Jr. Series B4, only. Engine Models: R-1340 Wasp Series S3H1, S1H1, S1H2, and S3H1G .

ReplacedPartNumber:

Pratt & Whitney Engine 80485

ApprovalBasis:

Identicality per 14 CFR 21.303

Models:

R-985 Wasp Jr. Series B4, only.

ReplacedPartNumber:

Pratt & Whitney Engine 234222

ApprovalBasis:

Identicality per 14 CFR 21.303

Models:

R-1340 Wasp . Series S3H1, S1H1, S1H2, and S3H1G

ReplacedPartNumber:

Modification Part

ApprovalBasis:

STC SH321NW, SH322NW

Models:

UH-12D - limited to models modified by STC SH177WE | UH-12E - limited to models modified by STC SH178WE

ReplacedPartNumber:

Installed vacuum pump on engines listed in Sigma Tek FAA approved installation procedure

ApprovalBasis:

FAA Approval Letter

Models:

Various Continental engines listed in Sigma Tek installation procedure rev. 4 dtd 6/10/74 FAA approved 7/3/74 | Various Textron engines listed in Sigma Tek installation procedure rev. 4 dtd 6/10/74 FAA approved 7/3/74

ReplacedPartNumber:

Installed vacuum pump on engines listed in Sigma Tek FAA approved installation procedure

ApprovalBasis:

FAA Approval Letter

Models:

Various Lycoming engines listed in Sigma Tek installation procedure rev. 6 dtd 6/10/74 FAA approved 7/3/74

ReplacedPartNumber:

Installed vacuum pump on engines listed in Sigma Tek FAA approved installation procedure

ApprovalBasis:

FAA Approval Letter

Models:

Various Continental engines listed in Sigma Tek installation procedure Rev 15 dtd 2/1/86 FAA approved 2/27/86. | Various Lycoming engines listed in Sigma Tek installation procedure Rev 15 dtd 2/1/86 FAA approved 2/27/86.

ReplacedPartNumber:

Installed Vcuum pump on engines listed in FAA approved Sigma Tek Installation Procedures

ApprovalBasis:

FAA Approval Letter

Models:

Various Lycoming engines listed in Sigma Tek Installation Procedures Rev 16 dated 10/20/92 FAA approed 11/17/92

ReplacedPartNumber:

Installed vacuum pump on engines listed in Sigma Tek FAA approved installation procedure

ApprovalBasis:

FAA Approval Letter

Models:

Various Continental engines listed in Sigma Tek installation procedure rev. 14 dtd 3/29/82 FAA approved 5/27/82 | Various Lycoming engines listed in Sigma Tek installation procedure rev. 14 dtd 3/29/82 FAA approved 5/27/82

ReplacedPartNumber:

Installed vacuum pump on engines listed in Sigma Tek FAA approved installation procedure

ApprovalBasis:

FAA Approval Letter

Models:

Various Continental engines listed in Sigma Tek installation procedure rev. 6 dtd 6/10/74 FAA approved 7/3/74

ReplacedPartNumber:

Installed vacuum pump on engines listed in Sigma Tek FAA approved installation procedure

ApprovalBasis:

FAA Approval Letter

Models:

Various Continental engines listed in Sigma Tek installation procedure Rev 15 dtd 2/1/86 FAA approved 2/27/86. | Various Lycoming engines listed in Sigma Tek installation procedure Rev 15 dtd 2/1/86 FAA approved 2/27/86.

ReplacedPartNumber:

Flight Systems Engineering Inc. P-5a(A100)

ApprovalBasis:

Licensing Agreement

Models:

727-100, 200 Series

ReplacedPartNumber:

Franklin Engine 17794

ApprovalBasis:

Design Approval per 14 CFR Part 21 21.303

Models:

6A-350 Series, 4A-235 Series, 6A4-165-B3, -B4, and -B6, 6A4-200, 6AS-335 Series, 6AS-350 Series

ReplacedPartNumber:

Franklin Engine 17864

ApprovalBasis:

Design Approval per 14 CFR Part 21 21.303

Models:

6A-350 Series, 6A4-150-B3, -B4, 6A4-165-B3, -B4, -B6: 6A4-200-C6, 6AS-335 Series, 6AS-350 Series

ReplacedPartNumber:

Flight Systems Engineering Inc. P-5a(A162)

ApprovalBasis:

Licensing Agreement

Models:

727-100, 200 Series

ReplacedPartNumber:

Franklin Engine 14724

ApprovalBasis:

Design Approval per 14 CFR Part 21 21.303

Models:

6A8-215-B8F, -B9F

ReplacedPartNumber:

Modification Part

ApprovalBasis:

STC SA5489NM dtd 10-30-91 Reissued 1-24-92

Models:

G-1159 S/N's 1 thru 300 except those with Aircraft Service Change 285 incorporated.

ReplacedPartNumber:

Flight Systems Engineering Inc. MP-10A

ApprovalBasis:

Licensing Agreement

Models:

727-100, 200 Series

ReplacedPartNumber:

Flight Systems Engineering Inc. MP-20A

ApprovalBasis:

Licensing Agreement

Models:

727-100, 200 Series

ReplacedPartNumber:

International Aero Engines 5950041-107

ApprovalBasis:

Identicality per 14 CFR 21.303, Licensing Agreement

Models:

V2500-D5 Series

ReplacedPartNumber:

International Aero Engines 5R5025, Pall Aerospace QA06249

ApprovalBasis:

Test and Computation per 14 CFR 21.303

Models:

V2500-A1, V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, V2525-D5, V2528-D5, V2533-A5

ReplacedPartNumber:

International Aero Engines 5R5030, Pall AerospaceQA05954

ApprovalBasis:

Test and Computation per 14 CFR 21.303

Models:

V2500-A1, V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, V2525-D5, V2528-D5, V2533-A5

ReplacedPartNumber:

International Aero Engines 5950041-105

ApprovalBasis:

Identicality per 14 CFR 21.303, Licensing Agreement

Models:

V2500-D5 Series

ReplacedPartNumber:

Modification Parts

ApprovalBasis:

STC SR01113NY-D

Models:

S-76A, S-76B, S-76C

ReplacedPartNumber:

Modification Part

ApprovalBasis:

STC SA2069CE-D

Models:

Lake Model 250 (S/N 36 and after)

ReplacedPartNumber:

Modification Parts

ApprovalBasis:

STC SE3353NM

Models:

Continental engines as listed on MEL SE3353NM dated 6/24/86

ReplacedPartNumber:

GE Aircraft Engines 1694M66P05

ApprovalBasis:

Identicality per 14 CFR 21.303

Models:

GE90

ReplacedPartNumber:

Modification Part

ApprovalBasis:

Design Approval per FAR 21.303(c)

Models:

JT3D, JT8D, JT9D (See MDL for interchangeable with part numbers)

ReplacedPartNumber:

International Aero Engines 6A3789

ApprovalBasis:

Test reports and Computations per 14 Code of Federal Regulations (14CFR) 21.303(c)

Models:

V2500-A1, V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, V2533-A5, V2525-D5, V2528-D5

ReplacedPartNumber:

Modification Part

ApprovalBasis:

Design Approval per FAR 21.303(c)

Models:

CF6 Series (See MDL for interchangeable with part numbers)

ReplacedPartNumber:

Modification Part

ApprovalBasis:

Design Approval per FAR 21.303(c)

Models:

CF6 Series (See MDL for interchangeable with part numbers)

ReplacedPartNumber:

International Aero Engines 6A3790

ApprovalBasis:

Test reports and Computations per 14 CFR 21.303(c)

Models:

V2500-A1, V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, V2533-A5, V2525-D5, V2528-D5

ReplacedPartNumber:

International Aero Engines UP10815

ApprovalBasis:

Test reports and Computations per 14 CFR 21.303(c)

Models:

V2500-A1, V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, V2533-A5, V2525-D5, V2528-D5

ReplacedPartNumber:

Modification Part

ApprovalBasis:

Design Approval per FAR 21.303(c)

Models:

CF6 Series (See MDL for interchangeable with part numbers)

ReplacedPartNumber:

Modification Part

ApprovalBasis:

Design Approval per FAR 21.303(c)

Models:

JT3D, JT8D, JT9D (See MDL for interchangeable with part numbers)

ReplacedPartNumber:

Modification Part

ApprovalBasis:

Design Approval per FAR 21.303(c)

Models:

CF6 Series (See MDL for interchangeable with part numbers)

ReplacedPartNumber:

International Aero Engines 6A2543

ApprovalBasis:

Test reports and Computations per 14 CFR 21.303(c)

Models:

V2500-A1, V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, V2533-A5

ReplacedPartNumber:

ApprovalBasis:

Licensing Agreement, STC SH7853SW

Models:

222, 222B, 222U

ReplacedPartNumber:

Modification Part

ApprovalBasis:

Design Approval per FAR 21.303(c)

Models:

JT3D, JT8D and JT9D (See MDL for interchangeable with part numbers)

ReplacedPartNumber:

CFMI Engine 301-384-321-0

ApprovalBasis:

Identicality per 14 CFR 21.303

Models:

CFM56-2, -2-C1, -2-C3, -3-B1 -3B-2, -3C-1

ReplacedPartNumber:

International Aero Engines UP11069

ApprovalBasis:

Test reports and Computations per 14 CFR 21.303(c)

Models:

V2500-A1, V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, V2533-A5, V2525-D5, V2528-D5

ReplacedPartNumber:

Modification Part

ApprovalBasis:

Design Approval per FAR 21.303(c)

Models:

CF6 Series (See MDL for interchangeable with part numbers)

ReplacedPartNumber:

Modification Part

ApprovalBasis:

Design Approval per FAR 21.303(c)

Models:

CF6 Series (See MDL for interchangeable with part numbers)

ReplacedPartNumber:

Modification Part

ApprovalBasis:

Design Approval per FAR 21.303(c)

Models:

JT3D, JT8D, JT9D (See MDL for interchangeable with part numbers)

ReplacedPartNumber:

International Aero Engines 6A3791

ApprovalBasis:

Test reports and Computations per 14 CFR 21.303(c)

Models:

V2500-A1, V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, V2533-A5, V2525-D5, V2528-D5

ReplacedPartNumber:

Modification Part

ApprovalBasis:

Design Approval per FAR 21.303(c)

Models:

JT3D, JT8D, JT9D (See MDL for interchangeable with part numbers)

ReplacedPartNumber:

Modification Part

ApprovalBasis:

Design Approval per FAR 21.303(c)

Models:

JT3D, JT8D, JT9D (See MDL for interchangeable with numbers)

ReplacedPartNumber:

International Aero Engines 6A2512

ApprovalBasis:

Test reports and Computations per 14 CFR 21.303(c)

Models:

V2500-A1, V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, V2533-A5, V2525-D5, V2528-D5

ReplacedPartNumber:

AlliedSignal Inc., AlliedSignal Engines 160450-2

ApprovalBasis:

Identicality per 14 CFR 21.303, Licensing Agreement

Models:

CFE738-1

ReplacedPartNumber:

GE Aircraft Engines 9037M23P11

ApprovalBasis:

Identicality per 14 CFR 21.303, Licensing Agreement

Models:

CF6-80A1, CF6-80A3

ReplacedPartNumber:

AlliedSignal Inc., AlliedSignal Engines 160448-2

ApprovalBasis:

Identicality per 14 CFR 21.303, Licensing Agreement

Models:

CFE738-1

ReplacedPartNumber:

GE Aircraft Engines General Electric Company 9250M97P04, 9250M97P02

ApprovalBasis:

Identicality per 14 CFR 21.303, Licensing Agreement

Models:

CF6-80C, CF6-80A, -A2, -C2

ReplacedPartNumber:

GE Aircraft Engines 9250M97P08

ApprovalBasis:

Identicality per 14 CFR 21.303, Licensing Agreement

Models:

CF6-80A, CF6-80A2, CF6-80C2A1, CF6-80C2A2, CF6-80C2A3, CF6-80C2A5, CF6-80C2A8, CF6-80C2B1, CF6-80C2B1F, CF6-80C2B1F1, CF6-80C2B2, CF6-80C2B2F, CF6-80C2B4, CF6-80C2B4F, CF6-80C2B6, CF6-80C2B6F, CF6-80C2D1F

ReplacedPartNumber:

GE Aircraft Engines General Electric Company 9250M97P07

ApprovalBasis:

Identicality per 14 CFR 21.303, Licensing Agreement

Models:

CF6-80C

ReplacedPartNumber:

Flight Equipment & Engineering LTD. B/E Aerospace, Seat Product Division C311109/503-1114

ApprovalBasis:

Test and Computations per 14 CFR 21.303

Models:

747-400 Series

ReplacedPartNumber:

Modification Parts

ApprovalBasis:

Licensing Agreement

Models:

757-200

ReplacedPartNumber:

Internat l Aero Engines (IAE) 108603

ApprovalBasis:

Identicality per 14 CFR 21.303, Licensing Agreement

Models:

V2525-D5, V2528-D5

ReplacedPartNumber:

Internat l Aero Engines (IAE) 6222SM8

ApprovalBasis:

Identicality per 14 CFR 21.303, Licensing Agreement

Models:

V2525-D5, V2528-D5

ReplacedPartNumber:

Aerocon Engineering Co. Parts as listed on MDL AC26-2200

ApprovalBasis:

Identicality per 14 CFR 21.303, Licensing Agreement

Models:

727-100 Series

ReplacedPartNumber:

Modification Part

ApprovalBasis:

Identicality per 14 CFR 21.303, Licensing Agreement

Models:

707-300, 707-300B, and 707-300C Series

ReplacedPartNumber:

Flight Systems Engineering Inc. P-5A (A162)

ApprovalBasis:

Identicality per 14 CFR 21.303, Licensing Agreement

Models:

727-100, -200 Series | 382E, 382G | DC-9, All Series

ReplacedPartNumber:

Flight Systems Engineering Inc. MP-2A

ApprovalBasis:

Identicality per 14 CFR 21.303, Licensing Agreement

Models:

727-100, -200 Series | DC-8-50, -60, -70 All Series

ReplacedPartNumber:

Flight Systems Engineering Inc. MP-20A

ApprovalBasis:

Identicality per 14 CFR 21.303, Licensing Agreement

Models:

727-100, -200 Series | DC-8-50, -60, -70 All Series

ReplacedPartNumber:

Flight Systems Engineering Inc. MP-10A

ApprovalBasis:

Identicality per 14 CFR 21.303, Licensing Agreement

Models:

727-100, -200 Series | DC-8-50, -60, -70 All Series

ReplacedPartNumber:

Flight Systems Engineering Inc. MP-5A

ApprovalBasis:

Identicality per 14 CFR 21.303, Licensing Agreement

Models:

727-100, -200 Series | DC-8-50, -60, -70 All Series

ReplacedPartNumber:

Engine 250-C20F

ApprovalBasis:

STC SH7961SW-D, dated 8-1-97 in accordance with AHC drawing list 355A82-1753 Rev. H, dated 11/5/90, or later approved revision.

Models:

AS355F1

ReplacedPartNumber:

Engine 250-C20R

ApprovalBasis:

STC SH7962SW-D, dated 8-1-97 in accordance with AHC drawing list 355A82-1755 Rev. D, dated 11/5/90, or later FAA approved revision.

Models:

AS355F2

ReplacedPartNumber:

Engine 250-C20R

ApprovalBasis:

STC SH7962SW-D, dated 8-1-97 in accordance with AHC drawing list 355A82-1755 Rev. D, dated 11/5/90, or later FAA approved revision.

Models:

AS355F2

ReplacedPartNumber:

Engine 250-C20F

ApprovalBasis:

STC SH7961SW-D, dated 8-1-97 in accordance with AHC drawing list 355A82-1753 Rev. H, dated 11/5/90, or later approved revision.

Models:

AS355F1

ReplacedPartNumber:

Honeywell P/N 1-300-336-01 as used on Engines P/N: 1-000-060-13, 1-000-060-21, 1-000-060-29, 1-000-060-30

ApprovalBasis:

Identicality per14 CFR § 21.303 DWG No: 6-2825-700Rev: NoneDate: 01/25/2008or later FAA-approved revisions

Models:

T5313B | T5317A | T5317A-1 | T5317B

ReplacedPartNumber:

Allied Signal Engines: 3104110

ApprovalBasis:

Identicality per 14 CFR 21.303,DWG No: 58260,Rev: A,Date: 12/10/1992 or later FAA?approved revisions

Models:

TPE331-14GR | TPE331-14HR

ReplacedPartNumber:

Lycoming Engines LW-14371

ApprovalBasis:

Identicality per licensing agreement between Lycoming Engines and Hartzell Engine Technologies LLC, Dated 03-Dec-18. DWG No. LW-14351 thru LW-14375 Rev - T Date 27-Sep-14 or later FAA-approved revision (CONT'D FROM PG. 8)

Models:

AEIO-320-D2B, AEIO-320-E1B, AEIO-320-E2B, AEIO-360-A1A, AEIO-360-A1B6, AEIO-360-A1D, AEIO-360-B1B, AEIO-360-B1F, AEIO-360-B1G6, AEIO-360-B2F, AEIO-360-H1A, AEIO-360-H1B, AEIO-540-D4A5, AEIO-540-L1B5, AEIO-540-L1B5D, AEIO-540-L1D5, HIO-360-C1B, HIO-360-G1A, IO-320-E1A, IO-320-E1B, IO-320-E2A, IO-320-E2B, IO-360-A1A, IO-360-A1B, IO-360-A1B6, IO-360-A2B, IO-360-B1B, IO-360-B1F, IO-360-L2A, IO-360-M1A, IO-540-C4B5, IO-540-K1E5, IO-540-M1C5, IO-540-W1A5, O-235-C1, O-235-C1B, O-235-C2A, O-235-F2B, O-235-H2C, O-235-J2A, O-235-K2B, O-235-K2C, O-235-N2A, O-235-L2C, O-235-L2A, O-320-A2A, 0-320-A2B, O-320-B2B, 0-320-B2C, O-320-B2D, O-320-D1A, O-320-D1F, O-320-D2A, O-320-E1C, O-320-E2A, O-320-E2C, O-320-E2D, O-360-A1A, O-360-A1D, O-360-A1LD, O-360-A1P, O-360-A2A, O-360-A2G, O-360-A3A, O-360-A3AD, O-360-A4M, O-360-A5AD, O-360-C1E, O-360-C1F, O-360-C1G, O-360-C2E, O-360-C4F, O-360-J2A, O-540-J1A5D, O-540-B4B5, O-540-J3A5

ReplacedPartNumber:

Lycoming Engines 32B19549

ApprovalBasis:

Identicality per licensing agreement between Lycoming Engines and Hartzell Engine Technologies LLC, Dated 03-Dec-18. DWG No. 32X19549 thru 32X19599 Rev - AG Date 27-Sep-14 or later FAA-approved revisions (CONT'D FROM PG. 7)

Models:

O-540-B4B5, O-360-A1A, O-360-A1F6, IO-540-M1C5, IO-360-A3B6, O-320-E2A, HIO-360-B1A, O-320-E1F, O-540-F1B5, IO-540-L1C5, O-360-A4M, IO-360-A1B6, IO-540-K1H5, O-360-C4P, TIO-540-J2B, LTIO-540-J2B, HIO-360-E1AD, TIO-540-AB1AD, IO-540-C4B5, HIO-360-F1AD, IO-360-B1E, O-320-A2D, O-235-N2C, O-235-C2A, O-320-E2D, IVO-360-A1A, O-320-D1F, O-540-A4A5, AEIO-360-A1E, IO-320-B1A, IO-320-C1A, IO-320-D1B, TIO-540-C1A, TO-360-C1A6D, O-540-E4B5, O-540-A4D5, O-540-J3A5D, IO-540-K1G5D, IO-540-K1G5, IO-540-C4D5D, IO-540-D4A5, IO-540-J4A5, IO-540-N1A5, IO-540-R1A5, IO-540-T4A5D, IO-540-T4B5, IO-540-T4B5D, IO-540-W1A5, IO-540-V4A5, HIO-360-C1A, HIO-360-E1BD, O-360-A1AD, O-360-A1P, O-360-A3AD, O-360-C1G, IO-360-A1D6, IO-360-B1B, O-540-J3A5D, IO-360-B1F6, IO-360-C1A, IO-360-C1B, IO-360-C1C, IO-360-C1C6, IO-360-C1D6, IO-360-C1F, IO-360-L2A, O-320-A2C, O-320-D3G, O-320-D2A, O-320-B2C, O-320-D1A, O-320-H2AD, AEIO-320-D1B, AEIO-320-D2B, AEIO-360-A1D, AEIO-360-A1E6, AEIO-360-B2F, AEIO-540-D4A5, AEIO-540-L1B5, IO-390-A1A6, LIO-320-B1A, LIO-320-C1A, AEIO-580-B1A

ReplacedPartNumber:

Lycoming Engines 32C19553

ApprovalBasis:

Identicality per licensing agreement between Lycoming Engines and Hartzell Engine Technologies LLC, Dated 03-Dec-18. DWG No. 32X19549 thru 32X19599 Rev - AG Date 27-Sep-14 or later FAA-approved revisions (CONT'D FROM PG. 1)

Models:

, IO-360-A1B6, HIO-360-F1AD, AEIO-360-A1B6, IO-360-A1A, IO-360-C1E6, IO-360-M1A, AEIO-360-A1E, IO-360-A1B6D, AEIO-360-A1E6, IO-360-A1B, HIO-360-G1A, IO-360-B1B, IO-360-A3B6, AEIO-360-B1F, LIO-360-M1A, HIO-360-B1A, IO-360-L2A, AEIO-320-D1B, IO-320-B1A, LIO-320-B1A, IO-320-D1A, IO-720-A1B, IO-720-D1B, IO-720-D1CD, IO-720-D1C, AEIO-540-D4A5, IO-540-C4D5D, IO-540-K1K5, IO-540-K1B5, IO-540-C4B5, AEIO-540-L1B5, IO-540-M1A5, IO-540-K1F5, IO-540-D4A5, IO-540-K1D5, IO-540-E1B5, IO-540-K1J5, IO-540-L1C5, AEIO-540-D4B5, IO-540-T4B5, IO-540-AA1B5, IO-540-J4A5, IO-540-K1J5D, IO-540-AE1A5, IO-540-L1B5D, IO-540-C4D5, IO-540-S1A5, IO-540-M1C5, IO-540-M1B5D, IO-540-V4A5, IO-540-G1D5, AEIO-540-L1B5D, IO-540-W1A5, IO-540-AA1A5, IO-580-B1A, IO-390-A1B6, TIO-540-C1A, TIO-540-J2B, TIO-540-J2BD, TIO-540-AA1AD, TIO-540-AB1AD, TIO-540-U2A, TIO-540-A2B, TIO-540-A2C, TIO-540-F2BD, TIO-540-W2A, TIO-540-V2AD, TIO-540-AH1A, TIO-360-C1A6D, O-235-L2C, TO-360-C1A6D, O-320-D2A, O-320-E2A, O-320-D3G, O-320-D1A, O-360-A1AD, O-360-A1A, HO-360-C1A, O-360-A4K, O-360-A4M, O-360-B2C, O-360-C1F, O-360-C4F, O-540-E4A5, O-540-E4C5, O-540-J3A5, O-540-E4B5, O-540-B4B5, O-540-A4D5

ReplacedPartNumber:

General Electric 4587, Q5587, Grimes 55-2477-1, Whelan Engineering 34-0750707-00

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No IFE360-LED-02 Rev A Date 03/24/2017 or later FAA-approved revisions

Models:

DHC-8-101, DHC-8-102, DHC-8-103, DHC-8-106, DHC-8-201, DHC-8-202, DHC-8-301, DHC-8-311, DHC-8-315, DHC-8-400, DHC-8-401, DHC-8-402

ReplacedPartNumber:

International Aero Engines P/N 6B1335

ApprovalBasis:

Tests and Computations per 14 CFR 21.303, Dwg No. 6B1335JA, Rev. -, Dated 2018/07/25, or later FAA approved revisions.

Models:

IAE) c/o IAE Airworthiness (V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, V2525-D5, V2528-D5, V2533-A5

ReplacedPartNumber:

International Aero Engines P/N 6B1143

ApprovalBasis:

Tests and Computations per 14 CFR 21.303, Dwg No. 6B1143JA, Rev. -, Dated 2018/07/20, or later FAA approved revisions.

Models:

IAE) c/o IAE Airworthiness (V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, V2533-A5

ReplacedPartNumber:

International Aero Engines P/N 6B1139

ApprovalBasis:

Tests and Computations per 14 CFR 21.303, Dwg No. 6B1139JA, Rev. -, Dated 2018/07/20, or later FAA approved revisions.

Models:

IAE) c/o IAE Airworthiness (V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, V2533-A5

ReplacedPartNumber:

International Aero Engines P/N 6B1142

ApprovalBasis:

Tests and Computations per 14 CFR 21.303, Dwg No. 6B1142JA, Rev. -, Dated 2018/07/20, or later FAA approved revisions.

Models:

IAE) c/o IAE Airworthiness (V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, V2533-A5

ReplacedPartNumber:

International Aero Engines P/N 2A0364

ApprovalBasis:

Tests and Computations per 14 CFR 21.303, Dwg No. 2A0364JA, Rev. A, Dated 2018/12/13, or later FAA approved revisions.

Models:

IAE) (IAE) c/o IAE Airworthiness (V2500-A1, V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, V2525-D5, V2528-D5, V2533-A5

ReplacedPartNumber:

International Aero Engines P/N BLT5654

ApprovalBasis:

Tests and Computations per 14 CFR 21.303, Dwg No. DNBLT5654, Rev. A, Dated 7/8/2008, or later FAA approved revisions.

Models:

IAE) c/o IAE Airworthiness (V2522-A5, V2524-A5, V2527M-A5, V2525-D5, V2528-D5

ReplacedPartNumber:

International Aero Engines P/N BRR12496

ApprovalBasis:

Tests and Computations per 14 CFR 21.303, Dwg No. BRR12496JA, Rev. A, Dated 2018/10/11, or later FAA approved revisions.

Models:

IAE) (IAE) c/o IAE Airworthiness (V2500-A1, V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, V2525-D5, V2528-D5, V2533-A5

ReplacedPartNumber:

International Aero Engines P/N 2A0696

ApprovalBasis:

Tests and Computations per 14 CFR 21.303, Dwg No. 2A0696JA, Rev. A, Dated 2018/10/26, or later FAA approved revisions.

Models:

IAE) (IAE) c/o IAE Airworthiness (V2500-A1, V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, V2525-D5, V2528-D5, V2533-A5

ReplacedPartNumber:

International Aero Engines P/N 2A1470

ApprovalBasis:

Tests and Computations per 14 CFR 21.303, Dwg No. 2A1470JA, Rev. -, Dated 2018/10/30, or later FAA approved revisions.

Models:

IAE) (IAE) c/o IAE Airworthiness (V2500-A1, V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, V2525-D5, V2528-D5, V2533-A5

ReplacedPartNumber:

Honeywell P/N 1-300-662-01 as used on Engine Subassembly P/N 1-000-060-30

ApprovalBasis:

Test and Computation per 14 CFR 21.303 DWG No 6-2825-701 Rev None Date 01/19/2009 or later FAA-approved revisions

Models:

T5317B

ReplacedPartNumber:

3883841-1 Used on engine P/N 3882500-17

ApprovalBasis:

Test and Computation per 14 CFR 21.303 DWG No 3-460-700 Rev A Date 10/17/2008 or later FAA-approved revisions

Models:

747-200B Series, 757-200 Series, 757-200PF Series, 757-200CB Series, 757-300 Series, 767-200 Series, 767-300 Series, 767-300F Series, 767-400ER Series) Airbus (A300, Model B4-601, A300, Model B4-603, A300, Model B4-620, A300, Model B4-605R, A300, Model B4-622R, A300, Model F4-605R, A300, Model F4-622R, A300, Model C4-605R, Variant F, A300, Model B4-622

ReplacedPartNumber:

Honeywell P/N 1-300-662-01 as used on Engine Subassembly P/N 1-000-060-29

ApprovalBasis:

Test and Computation per 14 CFR 21.303 DWG No 6-2825-701 Rev None Date 01/19/2009 or later FAA-approved revisions

Models:

T5317A-1

ReplacedPartNumber:

3883841-1 Used on engine P/N 3883600-2

ApprovalBasis:

Test and Computation per 14 CFR 21.303 DWG No 3-460-700 Rev A Date 10/17/2008 or later FAA-approved revisions

Models:

MD90-30

ReplacedPartNumber:

3883841-1 Used on engine P/N 3883240-6

ApprovalBasis:

Test and Computation per 14 CFR 21.303 DWG No 3-460-700 Rev A Date 10/17/2008 or later FAA-approved revisions

Models:

A330-201, A330-202, A330-203, A330-223, A330-243, A330-301, A330-302, A330-303, A330-321, A330-322, A330-323, A330-341, A330-342) (A330-343, A340-211, A340-212, A340-213, A340-311, A340-312, A340-313, A340-541, A340-642

ReplacedPartNumber:

Honeywell P/N 1-300-662-01 as used on Engine Subassembly P/N 1-000-060-13

ApprovalBasis:

Test and Computation per 14 CFR 21.303 DWG No 6-2825-701 Rev None Date 01/19/2009 or later FAA-approved revisions

Models:

T5313B

ReplacedPartNumber:

Honeywell P/N 1-300-662-01 as used on Engine Subassembly P/N 1-000-060-21

ApprovalBasis:

Test and Computation per 14 CFR 21.303 DWG No 6-2825-701 Rev None Date 01/19/2009 or later FAA-approved revisions

Models:

T5317A

ReplacedPartNumber:

Honeywell P/N 895506-1 as used on Engine Subassembly P/N See below

ApprovalBasis:

Test and Computation per 14 CFR 21.303 DWG No 28-2562-701 Rev None Date 06/25/2008 or later FAA-approved revisions.

Models:

TPE331-5-251K TPE331-5-255K TPE331-5-251C TPE331-5-252M TPE331-5-252K TPE331-5-254K TPE331-5-252C TPE331-6-251M TPE331-6-252M TPE331-6A-252M TPE331-6-252B TPE331-6-253B TPE331-6A-251M TPE331-10AV-511B TPE331-10AV-511M TPE331-10AU-511G

ReplacedPartNumber:

International Aero Engines P/N U780603

ApprovalBasis:

Tests and Computations per 14 CFR 21.303, Dwg No. U780603KT, Rev. A, Dated 2018/01/15, or later FAA approved revisions.

Models:

IAE) c/o IAE Airworthiness (V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, V2525-D5, V2528-D5, V2533-A5

ReplacedPartNumber:

Honeywell P/N 1-300-616-01 as used on Engines P/N 1-000-060-21, 1-000-060-29, 1-000-060-30

ApprovalBasis:

Identicality per 14 CFR 21.303 DWG No 15-3058-700 Rev None Date 11/15/2012 or later FAA-approved revisions

Models:

T5317A, T5317A-1, T5317B

ReplacedPartNumber:

Honeywell P/N 1-300-616-01 as used on Engines P/N 1-000-060-21, 1-000-060-29 1-000-060-30

ApprovalBasis:

Identicality per 14 CFR 21.303 DWG No 15-3058-700 Rev None Date 11/15/2007 or later FAA-approved revisions

Models:

T5317A, T5317A-1, T5317B

ReplacedPartNumber:

International Aero Engines P/N 5A0906

ApprovalBasis:

Tests and Computations per 14 CFR 21.303, Dwg No. JA5A0906, Rev. -, Date 2017/01/31, or later FAA approved revisions.

Models:

IAE) (V2500-A1

ReplacedPartNumber:

International Aero Engines P/N 5A1711

ApprovalBasis:

Tests and Computations per 14 CFR 21.303, Dwg No. M0C36921, Rev. A, Date 11/10/08, or later FAA approved revisions.

Models:

IAE) (V2500-A1

ReplacedPartNumber:

Hamilton Sundstrand 814858-1 and 814858-3, installed on Hamilton Sundstrand Engine Anti-ice Valve 810502

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No AIR23017 Rev - Date 07/19/2001 or later FAA-approved revisions

Models:

777-232LR

ReplacedPartNumber:

Hamilton Sundstrand 814858-1 and 814858-3, installed on Hamilton Sundstrand Engine Anti-ice Valve 810502

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No AIR23017 Rev - Date 07/19/2001 or later FAA-approved revisions

Models:

777-232LR

ReplacedPartNumber:

Harper Engineering H3-1898-14, Boeing S832Z610-5

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No ADP25011 Rev N/C Date 05/14/2018 or later FAA-approved revisions

Models:

737-8, 737-9, 737-700 Series, 737-800 Series, 737-900ER Series, 747-8 Series, 777-300ER Series, 787-8, 787-9

ReplacedPartNumber:

International Aero Engines, LLC P/N 5326910

ApprovalBasis:

Identicality per 14 CFR Sec. 21.303 (c), licensing agreement between International Aero Engines, LLC and Lear Romec Division Crane Co. Dwg. No. 5326910 Rev. - Date 13 April, 2017 or later FAA-approved revisions.

Models:

PW1133G-JM, PW1124G-JM, PW1127G-JM, PW1130G-JM, PW1124G1-JM, PW1122G-JM, PW1127G1-JM PW1127GA-JM, PW1133GA-JM

ReplacedPartNumber:

90-876, as used in Kelly Aerospace / Hartzell Engine Technologies MZ-4205, -4206, -4208, -4216 & -4218 thru -4226 starter motors

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No 90-876-AC Rev IR Date 08/22/2017 or later FAA-approved revisions

Models:

O-320-A, -B, -C, -D, IO-320-A, -B, -C, -D, -E, -F, LIO-320-B, -C, AIO-320-A, -B, -C, AEIO-320-D, -E, O-340-A, -B, O-360-A, -B, -C, -D, -E, -F, -G, -J, IO-360-A, -B, -C, -D, -E, -F, -J, -K, -L, -M, AEIO-360-A, -B, -H, HO-360-A, -B, -C, IVO-360-A, LHIO-360-C, -F, LTO-360-A, -E, TO-360-A, -C, -E, -F, AEIO-390-A, HIO-360-A, -B, -C, -D, -E, -G, IO-390-A, IO-540-A, -B, -C, -D, -E, -G, -J, -K, -L, -M, N, -P, -R, -S, -T, -U, -V, -W, AEIO-540-D, -L, IGO-540-A, -B, IGSO-540-A, -B, HIO-540-A, LTIO-540-F, -J, -K, -N, -R, -U, -V, -W, TIO-540-A, -C, -E, -F, -G, -H, -J, -K, N, -R, -S, -T, -U, -V, -W, TIVO-540-A, VO-540-A, -B, -C, VSO-580-A, IO-580-A, -B, AEIO-580-B, TIO-541-A, -E

ReplacedPartNumber:

EBB-75A, as used in Kelly Aerospace / Hartzell Engine Technologies MHB-4001, -4002, -4003, -4007, -4011, -4012, -4013, -6016, -6018 & MZ-4205, -4206, - 4207, -4217, -4218, -4219, -6222, -6224, -6226 starter motors

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No EBB-75A-AC Rev IR Date 12/22/2015 or later FAA-approved revisions

Models:

O-320-A, -B, -C, -D, IO-320-A, -B, -C, -D, -E, -F, LIO-320-B, -C, AIO-320-A, -B, -C, AEIO-320-D, -E, O-340-A, -B, O-360-A, -B, -C, -D, -E, -F, -G, -J, IO-360-A, -B, -C, -D, -E, -F, -J, -K, -L, -M, AEIO-360-A, -B, -H, HO-360-A, -B, -C, IVO-360-A, LHIO-360-C, -F, LTO-360-A, -E, TO-360-A, -C, -E, -F, AEIO-390-A, HIO-360-A, -B, -C, -D, -E, -G, IO-390-A, O-435-A, -c, GO-435-C, IO-540-A, -B, -C, -D, -E, -G, -J, -K, -L, -M, N, -P, -R, -S, -T, -U, -V, -W, AEIO-540-D, -L, IGO-540-A, -B, IGSO-540-A, -B, HIO-540-A, LTIO-540-F, -J, -K, -N, -R, -U, -V, -W, TIO-540-A, -C, -E, -F, -G, -H, -J, -K, N, -R, -S, -T, -U, -V, -W, TIVO-540-A, VO-540-A, -B, -C, VSO-580-A, IO-580-A, -B, AEIO-580-B, TIO-541-A, -E

ReplacedPartNumber:

MHD-2012S, as used in Kelly Aerospace/ Hartzell Engine Technologies MCL-6501 thru -6503 starter motors

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No 2012-AC Rev IR Date 01/26/2016 or later FAA-approved revisions

Models:

O-300-D, -E, IO-360-A, -B, -C, -D, -E, -F, -G, -H, -J, -K, -AB, -AF, -DB, -GB, -HB, -JB, -KB, -ES, TSIO-360-A, -AB, -B, -C, -CB, -D, -DB, -E, -F, -G, -GB, -H, -HB, -EB, -FB, -JB, -KB, -LB, -BB, -MB, -NB, -PB, -RB, -SB, LTSIO-360-E, -EB, -KB, -RB, IO-E46-A, -B, O-470-A, -B, -E, -G, -H, -J, -K, -L, -M, -N, -P, -R, -S, -T, -U, IO-470-A, -C, -D, -E, -F, -G, -H, -J, -K, -L, -LO, -M, -N, -P, -R, -S, -T, -U, -V, -VO, TSIO-470-B, -C, -D, O-520-A, -B, -BA, -BB, -C, -CB, -D, -E, -F, -J, -K, -L, -M, -MB, -N, -NB, -P, L/IO-520-P, IO-520-A, -D, -E, -F, -J, -L, TSIO-520-A, -B, -C, -D, -E, -G, -H, -J, -K, -L, -M, -N, -P, -R, -BB, -DB, -EB, -JB, -KB, -LB, -NB, -T, -U, -UB, -VB, -WB, -AE, -AF, LTSIO-520-AE, TSIO-520-BE, -CE, GTSIO-520-C, -D, -E, -F, -H, -K, -L, -M, -N, IO-550-A, -B, -C, -D, -E, -F, -G, -L, -N, -P, -R, IOF-550-B, -C, -D, -E, -F, -L, -N, -P, -R, TSIO-550-A, -B, -C, -E, -G, -K, -N, TSIOF-550-D, -J, -K, -P, TSIOL-550-A, -B, -C

ReplacedPartNumber:

EBB-124A, as used in Kelly Aerospace / Hartzell Engine Technologies MZ 4204 & MMU series starter motors

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No EBB-124A-AC Rev IR Date 12/22/2015 or later FAA-approved revisions

Models:

O-235-A, -B, -AP, -BP, -C, -G, -H, -J, -K, -L, -M, -N, -P, O-320-A, -B, -C, -D, IO-320-A, -B, - C, -D, -E, -F, LIO-320-B, -C, AIO-320-A, -B, -C, AEIO-320-D, -E) Textron Lycoming (O-290-A, -AP, -B, -C, -CP, -D

ReplacedPartNumber:

MDL-2012ES, as used in Kelly Aerospace / Hartzell Engine Technologies MHJ-4002 & -4003 starter motors

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No MDL-2012ES-AC Rev IR Date 01/12/2016 or later FAA-approved revisions

Models:

O-300-D, -E, IO-360-A, -B, -C, -D, -E, -F, -G, -H, -J, -K, -AB, -AF, -DB, -GB, -HB, -JB, -KB, -ES, TSIO-360-A, -AB, -B, -C, -CB, -D, -DB, -E, -F, -G, -GB, -H, -HB, -EB, -FB, -JB, -KB, -LB, -BB, -MB, -NB, -PB, -RB, -SB, LTSIO-360-E, -EB, -KB, -RB, IO-E46-A, -B, O-470-A, -B, -E, -G, -H, -J, -K, -L, -M, -N, -P, -R, -S, -T, -U, IO-470-A, -C, -D, -E, -F, -G, -H, -J, -K, -L, -LO, -M, -N, -P, -R, -S, -T, -U, -V, -VO, TSIO-470-B, -C, -D, O-520-A, -B, -BA, -BB, -C, -CB, -D, -E, -F, -J, -K, -L, -M, -MB, -N, -NB, -P, L/IO-520-P, IO-520-A, -D, -E, -F, -J, -L, TSIO-520-A, -B, -C, -D, -E, -G, -H, -J, -K, -L, -M, -N, -P, -R, -BB, -DB, -EB, -JB, -KB, -LB, -NB, -T, -U, -UB, -VB, -WB, -AE, -AF, LTSIO-520-AE, TSIO-520-BE, -CE, GTSIO-520-C, -D, -E, -F, -H, -K, -L, -M, -N, IO-550-A, -B, -C, -D, -E, -F, -G, -L, -N, -P, -R, IOF-550-B, -C, -D, -E, -F, -L, -N, -P, -R, TSIO-550-A, -B, -C, -E, -G, -K, -N, TSIOF-550-D, -J, -K, -P, TSIOL-550-A, -B, -C

ReplacedPartNumber:

EBB-131A, as used in Kelly Aerospace / Hartzell Engine Technologies MHB-4016, -4017, -4018, -4019, -4020 & MZ-4221, -4222, -4223, -4224, -4225 starter motors

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No EBB-131A-AC Rev IR Date 12/22/2015 or later FAA-approved revisions

Models:

O-320-A, -B, -C, -D, IO-320-A, -B, -C, -D, -E, -F, LIO-320-B, -C, AIO-320-A, -B, -C, AEIO-320-D, -E, O-340-A, -B, O-360-A, -B, -C, -D, -E, -F, -G, -J, IO-360-A, -B, -C, -D, -E, -F, -J, -K, -L, -M, AEIO-360-A, -B, -H, HO-360-A, -B, -C, IVO-360-A, LHIO-360-C, -F, LTO-360-A, -E, TO-360-A, -C, -E, -F, AEIO-390-A, HIO-360-A, -B, -C, -D, -E, -G, IO-390-A, IO-540-A, -B, -C, -D, -E, -G, -J, -K, -L, -M, N, -P, -R, -S, -T, -U, -V, -W, AEIO-540-D, -L, IGO-540-A, -B, IGSO-540-A, -B, HIO-540-A, LTIO-540-F, -J, -K, -N, -R, -U, -V, -W, TIO-540-A, -C, -E, -F, -G, -H, -J, -K, N, -R, -S, -T, -U, -V, -W, TIVO-540-A, VO-540-A, -B, -C, VSO-580-A, IO-580-A, -B, AEIO-580-B, TIO-541-A, -E

ReplacedPartNumber:

EBB-142A, as used in Kelly Aerospace / Hartzell Engine Technologies MHB-4009, -4014, -6014 & MZ-4216, -4220, -6220 starter motors

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No EBB-142A-AC Rev IR Date 12/22/2015 or later FAA-approved revisions

Models:

O-320-A, -B, -C, -D, IO-320-A, -B, -C, -D, -E, -F, LIO-320-B, -C, AIO-320-A, -B, -C, AEIO-320-D, -E, O-340-A, -B, O-360-A, -B, -C, -D, -E, -F, -G, -J, IO-360-A, -B, -C, -D, -E, -F, -J, -K, -L, -M, AEIO-360-A, -B, -H, HO-360-A, -B, -C, IVO-360-A, LHIO-360-C, -F, LTO-360-A, -E, TO-360-A, -C, -E, -F, AEIO-390-A, HIO-360-A, -B, -C, -D, -E, -G, IO-390-A, IO-540-A, -B, -C, -D, -E, -G, -J, -K, -L, -M, N, -P, -R, -S, -T, -U, -V, -W, AEIO-540-D, -L, IGO-540-A, -B, IGSO-540-A, -B, HIO-540-A, LTIO-540-F, -J, -K, -N, -R, -U, -V, -W, TIO-540-A, -C, -E, -F, -G, -H, -J, -K, N, -R, -S, -T, -U, -V, -W, TIVO-540-A, VO-540-A, -B, -C, VSO-580-A, IO-580-A, -B, AEIO-580-B, TIO-541-A, -E

ReplacedPartNumber:

90-726, as used in Kelly Aerospace / Hartzell Engine Technologies MCL, MDB, MHJ & ES 646 series & MHP-4004 starter motors

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No 90-726-AC Rev IR Date 09/13/2017 or later FAA-approved revisions

Models:

O-300-D, -E, IO-360-A, -B, -C, -D, -E, -F, -G, -H, -J, -K, -AB, -AF, -DB, -GB, -HB, -JB, -KB, -ES, TSIO-360-A, -AB, -B, -C, -CB, -D, -DB, -E, -F, -G, -GB, -H, -HB, -EB, -FB, -JB, -KB, -LB, -BB, -MB, -NB, -PB, -RB, -SB, LTSIO-360-E, -EB, -KB, -RB, IO-E46-A, -B, O-470-A, -B, -E, -G, -H, -J, -K, -L, -M, -N, -P, -R, -S, -T, -U, IO-470-A, -C, -D, -E, -F, -G, -H, -J, -K, -L, -LO, -M, -N, -P, -R, -S, -T, -U, -V, -VO, TSIO-470-B, -C, -D, O-520-A, -B, -BA, -BB, -C, -CB, -D, -E, -F, -J, -K, -L, -M, -MB, -N, -NB, -P, L/IO-520-P, IO-520-A, -D, -E, -F, -J, -L, TSIO-520-A, -B, -C, -D, -E, -G, -H, -J, -K, -L, -M, -N, -P, -R, -BB, -DB, -EB, -JB, -KB, -LB, -NB, -T, -U, -UB, -VB, -WB, -AE, -AF, LTSIO-520-AE, TSIO-520-BE, -CE, GTSIO-520-C, -D, -E, -F, -H, -K, -L, -M, -N, IO-550-A, -B, -C, -D, -E, -F, -G, -L, -N, -P, -R, IOF-550-B, -C, -D, -E, -F, -L, -N, -P, -R, TSIO-550-A, -B, -C, -E, -G, -K, -N, TSIOF-550-D, -J, -K, -P, TSIOL-550-A, -B, -C

ReplacedPartNumber:

MDL-1064E, as used in Hartzell Engine Technologies ES646 series starter motors

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No 1064-AC Rev IR Date 01/26/2016 or later FAA-approved revisions

Models:

O-300-D, -E, IO-360-A, -B, -C, -D, -E, -F, -G, -H, -J, -K, -AB, -AF, -DB, -GB, -HB, -JB, -KB, -ES, TSIO-360-A, -AB, -B, -C, -CB, -D, -DB, -E, -F, -G, -GB, -H, -HB, -EB, -FB, -JB, -KB, -LB, -BB, -MB, -NB, -PB, -RB, -SB, LTSIO-360-E, -EB, -KB, -RB, IO-E46-A, -B, O-470-A, -B, -E, -G, -H, -J, -K, -L, -M, -N, -P, -R, -S, -T, -U, IO-470-A, -C, -D, -E, -F, -G, -H, -J, -K, -L, -LO, -M, -N, -P, -R, -S, -T, -U, -V, -VO, TSIO-470-B, -C, -D, O-520-A, -B, -BA, -BB, -C, -CB, -D, -E, -F, -J, -K, -L, -M, -MB, -N, -NB, -P, L/IO-520-P, IO-520-A, -D, -E, -F, -J, -L, TSIO-520-A, -B, -C, -D, -E, -G, -H, -J, -K, -L, -M, -N, -P, -R, -BB, -DB, -EB, -JB, -KB, -LB, -NB, -T, -U, -UB, -VB, -WB, -AE, -AF, LTSIO-520-AE, TSIO-520-BE, -CE, GTSIO-520-C, -D, -E, -F, -H, -K, -L, -M, -N, IO-550-A, -B, -C, -D, -E, -F, -G, -L, -N, -P, -R, IOF-550-B, -C, -D, -E, -F, -L, -N, -P, -R, TSIO-550-A, -B, -C, -E, -G, -K, -N, TSIOF-550-D, -J, -K, -P, TSIOL-550-A, -B, -C

ReplacedPartNumber:

MHB-3005S, as used in Kelly Aerospace / Hartzell Engine Technologies MHB-4001, -4002, -4003, -4007, -4008, -4010 thru -4013 & -4016 thru -4020 starter motors

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No MHB-3005S-AC Rev IR Date 06/14/2015 or later FAA-approved revisions

Models:

O-320-A, -B, -C, -D, IO-320-A, -B, -C, -D, -E, -F, LIO-320-B, -C, AIO-320-A, -B, -C, AEIO-320-D, -E, O-340-A, -B, O-360-A, -B, -C, -D, -E, -F, -G, -J, IO-360-A, -B, -C, -D, -E, -F, -J, -K, -L, -M, AEIO-360-A, -B, -H, HO-360-A, -B, -C, IVO-360-A, LHIO-360-C, -F, LTO-360-A, -E, TO-360-A, -C, -E, -F, AEIO-390-A, HIO-360-A, -B, -C, -D, -E, -G, IO-390-A, IO-540-A, -B, -C, -D, -E, -G, -J, -K, -L, -M, N, -P, -R, -S, -T, -U, -V, -W, AEIO-540-D, -L, IGO-540-A, -B, IGSO-540-A, -B, HIO-540-A, LTIO-540-F, -J, -K, -N, -R, -U, -V, -W, TIO-540-A, -C, -E, -F, -G, -H, -J, -K, N, -R, -S, -T, -U, -V, -W, TIVO-540-A, VO-540-A, -B, -C, VSO-580-A, IO-580-A, -B, AEIO-580-B, TIO-541-A, -E

ReplacedPartNumber:

MFX-1064S, as used in Kelly Aerospace/ Hartzell Engine Technologies MCL-6501 thru -6503 starter motors

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No 1064-AC Rev IR Date 01/26/2016 or later FAA-approved revisions

Models:

O-300-D, -E, IO-360-A, -B, -C, -D, -E, -F, -G, -H, -J, -K, -AB, -AF, -DB, -GB, -HB, -JB, -KB, -ES, TSIO-360-A, -AB, -B, -C, -CB, -D, -DB, -E, -F, -G, -GB, -H, -HB, -EB, -FB, -JB, -KB, -LB, -BB, -MB, -NB, -PB, -RB, -SB, LTSIO-360-E, -EB, -KB, -RB, IO-E46-A, -B, O-470-A, -B, -E, -G, -H, -J, -K, -L, -M, -N, -P, -R, -S, -T, -U, IO-470-A, -C, -D, -E, -F, -G, -H, -J, -K, -L, -LO, -M, -N, -P, -R, -S, -T, -U, -V, -VO, TSIO-470-B, -C, -D, O-520-A, -B, -BA, -BB, -C, -CB, -D, -E, -F, -J, -K, -L, -M, -MB, -N, -NB, -P, L/IO-520-P, IO-520-A, -D, -E, -F, -J, -L, TSIO-520-A, -B, -C, -D, -E, -G, -H, -J, -K, -L, -M, -N, -P, -R, -BB, -DB, -EB, -JB, -KB, -LB, -NB, -T, -U, -UB, -VB, -WB, -AE, -AF, LTSIO-520-AE, TSIO-520-BE, -CE, GTSIO-520-C, -D, -E, -F, -H, -K, -L, -M, -N, IO-550-A, -B, -C, -D, -E, -F, -G, -L, -N, -P, -R, IOF-550-B, -C, -D, -E, -F, -L, -N, -P, -R, TSIO-550-A, -B, -C, -E, -G, -K, -N, TSIOF-550-D, -J, -K, -P, TSIOL-550-A, -B, -C

ReplacedPartNumber:

MZ-298, as used in Kelly Aerospace / Hartzell Engine Technologies MHB series & MZ series starter motors

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No MZ-298-AC Rev IR Date 12/18/2015 or later FAA-approved revisions

Models:

O-320-A, -B, -C, -D, IO-320-A, -B, -C, -D, -E, -F, LIO-320-B, -C, AIO-320-A, -B, -C, AEIO-320-D, -E, O-340-A, -B, O-360-A, -B, -C, -D, -E, -F, -G, -J, IO-360-A, -B, -C, -D, -E, -F, -J, -K, -L, -M, AEIO-360-A, -B, -H, HO-360-A, -B, -C, IVO-360-A, LHIO-360-C, -F, LTO-360-A, -E, TO-360-A, -C, -E, -F, AEIO-390-A, HIO-360-A, -B, -C, -D, -E, -G, IO-390-A, IO-540-A, -B, -C, -D, -E, -G, -J, -K, -L, -M, N, -P, -R, -S, -T, -U, -V, -W, AEIO-540-D, -L, IGO-540-A, -B, IGSO-540-A, -B, HIO-540-A, LTIO-540-F, -J, -K, -N, -R, -U, -V, -W, TIO-540-A, -C, -E, -F, -G, -H, -J, -K, N, -R, -S, -T, -U, -V, -W, TIVO-540-A, VO-540-A, -B, -C, VSO-580-A, IO-580-A, -B, AEIO-580-B, TIO-541-A, -E

ReplacedPartNumber:

EBB-75A, as used in Kelly Aerospace/ Hartzell Engine Technologies MHB-4001, -4002, -4003, -4007, -4011, -4012, -4013, -6016, -6018 & MZ-4205, -4206, - 4207, -4217, -4218, -4219, -6222, -6224, -6226 starter motors

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No EBB-75A-AC Rev IR Date 12/22/2015 or later FAA-approved revisions

Models:

O-290-A, -AP, -B, -C, -CP, -D, IO-720-A, -B, -C, -D

ReplacedPartNumber:

MZ-1005RSS, as used in Kelly Aerospace / Hartzell Engine Technologies MZ-4214 starter motor

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No MZ-1005RSS-AC Rev IR Date 12/22/2015 or later FAA-approved revisions

Models:

O-290-A, -AP, -B, -C, -CP, -D

ReplacedPartNumber:

MHB-3005S, as used in Kelly Aerospace/ Hartzell Engine Technologies MHB-4001, -4002, -4003, -4007, -4008, -4010 thru -4013 & -4016 thru -4020 starter motors

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No MHB-3005S-AC Rev IR Date 06/14/2015 or later FAA-approved revisions

Models:

IO-720-A, -B, -C, -D

ReplacedPartNumber:

MCL-1005PS-1, as used in Kelly Aerospace / Hartzell Engine Technologies MCL-6501 & -6502 starter motors

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No MCL-1005PS-1-AC Rev IR Date 12/22/2015 or later FAA-approved revisions

Models:

O-300-D, -E, IO-360-A, -B, -C, -D, -E, -F, -G, -H, -J, -K, -AB, -AF, -DB, -GB, -HB, -JB, -KB, -ES, TSIO-360-A, -AB, -B, -C, -CB, -D, -DB, -E, -F, -G, -GB, -H, -HB, -EB, -FB, -JB, -KB, -LB, -BB, -MB, -NB, -PB, -RB, -SB, LTSIO-360-E, -EB, -KB, -RB, IO-E46-A, -B, O-470-A, -B, -E, -G, -H, -J, -K, -L, -M, -N, -P, -R, -S, -T, -U, IO-470-A, -C, -D, -E, -F, -G, -H, -J, -K, -L, -LO, -M, -N, -P, -R, -S, -T, -U, -V, -VO, TSIO-470-B, -C, -D, O-520-A, -B, -BA, -BB, -C, -CB, -D, -E, -F, -J, -K, -L, -M, -MB, -N, -NB, -P, L/IO-520-P, IO-520-A, -D, -E, -F, -J, -L, TSIO-520-A, -B, -C, -D, -E, -G, -H, -J, -K, -L, -M, -N, -P, -R, -BB, -DB, -EB, -JB, -KB, -LB, -NB, -T, -U, -UB, -VB, -WB, -AE, -AF, LTSIO-520-AE, TSIO-520-BE, -CE, GTSIO-520-C, -D, -E, -F, -H, -K, -L, -M, -N, IO-550-A, -B, -C, -D, -E, -F, -G, -L, -N, -P, -R, IOF-550-B, -C, -D, -E, -F, -L, -N, -P, -R, TSIO-550-A, -B, -C, -E, -G, -K, -N, TSIOF-550-D, -J, -K, -P, TSIOL-550-A, -B, -C) Franklin Sp. z.o.o. (6A-350-C1, 6A-350-C2A

ReplacedPartNumber:

MZ-3005GS, as used in Kelly Aerospace / Hartzell Engine Technologies MZ-4205 thru -4208 & -4216 thru -4260 starter motors

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No MZ-3005GS-AC Rev IR Date 12/22/2015 or later FAA-approved revisions

Models:

O-320-A, -B, -C, -D, IO-320-A, -B, -C, -D, -E, -F, LIO-320-B, -C, AIO-320-A, -B, -C, AEIO-320-D, -E, O-340-A, -B, O-360-A, -B, -C, -D, -E, -F, -G, -J, IO-360-A, -B, -C, -D, -E, -F, -J, -K, -L, -M, AEIO-360-A, -B, -H, HO-360-A, -B, -C, IVO-360-A, LHIO-360-C, -F, LTO-360-A, -E, TO-360-A, -C, -E, -F, AEIO-390-A, HIO-360-A, -B, -C, -D, -E, -G, IO-390-A, IO-540-A, -B, -C, -D, -E, -G, -J, -K, -L, -M, N, -P, -R, -S, -T, -U, -V, -W, AEIO-540-D, -L, IGO-540-A, -B, IGSO-540-A, -B, HIO-540-A, LTIO-540-F, -J, -K, -N, -R, -U, -V, -W, TIO-540-A, -C, -E, -F, -G, -H, -J, -K, N, -R, -S, -T, -U, -V, -W, TIVO-540-A, VO-540-A, -B, -C, VSO-580-A, IO-580-A, -B, AEIO-580-B, TIO-541-A, -E) Textron Lycoming (IO-720-A, -B, -C, -D

ReplacedPartNumber:

MHB-2012S, as used in Kelly Aerospace / Hartzell Engine Technologies MHB-4001 thru -4003, -4007, -4008, -4010 thru -4013, -4016 thru -4020 starter motors

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No MHB-2012S-AC Rev IR Date 01/26/2016 or later FAA-approved revisions

Models:

O-320-A, -B, -C, -D, IO-320-A, -B, -C, -D, -E, -F, LIO-320-B, -C, AIO-320-A, -B, -C, AEIO-320-D, -E, O-340-A, -B, O-360-A, -B, -C, -D, -E, -F, -G, -J, IO-360-A, -B, -C, -D, -E, -F, -J, -K, -L, -M, AEIO-360-A, -B, -H, HO-360-A, -B, -C, IVO-360-A, LHIO-360-C, -F, LTO-360-A, -E, TO-360-A, -C, -E, -F, AEIO-390-A, HIO-360-A, -B, -C, -D, -E, -G, IO-390-A, O-435-A, -C, GO-435-C, IO-540-A, -B, -C, -D, -E, -G, -J, -K, -L, -M, N, -P, -R, -S, -T, -U, -V, -W, AEIO-540-D, -L, IGO-540-A, -B, IGSO-540-A, -B, HIO-540-A, LTIO-540-F, -J, -K, -N, -R, -U, -V, -W, TIO-540-A, -C, -E, -F, -G, -H, -J, -K, N, -R, -S, -T, -U, -V, -W, TIVO-540-A, VO-540-A, -B, -C, VSO-580-A, IO-580-A, -B, AEIO-580-B, TIO-541-A, -E

ReplacedPartNumber:

MHB-2012S, as used in Kelly Aerospace/ Hartzell Engine Technologies MHB-4001 thru -4003, -4007, -4008, -4010 thru -4013, -4016 thru -4020 starter motors

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No MHB-2012S-AC Rev IR Date 01/26/2016 or later FAA-approved revisions

Models:

IO-720-A, -B, -C, -D

ReplacedPartNumber:

MDL-1064-ES, as used in Kelly Aerospace / Hartzell Engine Technologies MHJ-4002, -4003 & MHP-4004, -4101 starter motors

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No 1064-AC Rev IR Date 01/26/2016 or later FAA-approved revisions

Models:

O-300-D, -E, IO-360-A, -B, -C, -D, -E, -F, -G, -H, -J, -K, -AB, -AF, -DB, -GB, -HB, -JB, -KB, -ES, TSIO-360-A, -AB, -B, -C, -CB, -D, -DB, -E, -F, -G, -GB, -H, -HB, -EB, -FB, -JB, -KB, -LB, -BB, -MB, -NB, -PB, -RB, -SB, LTSIO-360-E, -EB, -KB, -RB, IO-E46-A, -B, O-470-A, -B, -E, -G, -H, -J, -K, -L, -M, -N, -P, -R, -S, -T, -U, IO-470-A, -C, -D, -E, -F, -G, -H, -J, -K, -L, -LO, -M, -N, -P, -R, -S, -T, -U, -V, -VO, TSIO-470-B, -C, -D, O-520-A, -B, -BA, -BB, -C, -CB, -D, -E, -F, -J, -K, -L, -M, -MB, -N, -NB, -P, L/IO-520-P, IO-520-A, -D, -E, -F, -J, -L, TSIO-520-A, -B, -C, -D, -E, -G, -H, -J, -K, -L, -M, -N, -P, -R, -BB, -DB, -EB, -JB, -KB, -LB, -NB, -T, -U, -UB, -VB, -WB, -AE, -AF, LTSIO-520-AE, TSIO-520-BE, -CE, GTSIO-520-C, -D, -E, -F, -H, -K, -L, -M, -N, IO-550-A, -B, -C, -D, -E, -F, -G, -L, -N, -P, -R, IOF-550-B, -C, -D, -E, -F, -L, -N, -P, -R, TSIO-550-A, -B, -C, -E, -G, -K, -N, TSIOF-550-D, -J, -K, -P, TSIOL-550-A, -B, -C

ReplacedPartNumber:

MBG-2012S, as used in Kelly Aerospace / Hartzell Engine Technologies MZ-4204 thru -4208 & -4216 thru -4226 starter motors

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No 2012-AC Rev IR Date 01/26/2016 or later FAA-approved revisions

Models:

O-320-A, -B, -C, -D, IO-320-A, -B, -C, -D, -E, -F, LIO-320-B, -C, AIO-320-A, -B, -C, AEIO-320-D, -E, O-340-A, -B, O-360-A, -B, -C, -D, -E, -F, -G, -J, IO-360-A, -B, -C, -D, -E, -F, -J, -K, -L, -M, AEIO-360-A, -B, -H, HO-360-A, -B, -C, IVO-360-A, LHIO-360-C, -F, LTO-360-A, -E, TO-360-A, -C, -E, -F, AEIO-390-A, HIO-360-A, -B, -C, -D, -E, -G, IO-390-A, IO-540-A, -B, -C, -D, -E, -G, -J, -K, -L, -M, N, -P, -R, -S, -T, -U, -V, -W, AEIO-540-D, -L, IGO-540-A, -B, IGSO-540-A, -B, HIO-540-A, LTIO-540-F, -J, -K, -N, -R, -U, -V, -W, TIO-540-A, -C, -E, -F, -G, -H, -J, -K, N, -R, -S, -T, -U, -V, -W, TIVO-540-A, VO-540-A, -B, -C, VSO-580-A, IO-580-A, -B, AEIO-580-B, TIO-541-A, -E) Textron Lycoming (IO-720-A, -B, -C, -D

ReplacedPartNumber:

90-2502, as used in Kelly Aerospace / Hartzell Engine Technologies MHB-4001 thru -4003, -4007, -4008, -4010 thru -4013, -4016 thru -4020 starter motors

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No 90-2502-AC Rev IR Date 09/13/2017 or later FAA-approved revisions

Models:

O-320-A, -B, -C, -D, IO-320-A, -B, -C, -D, -E, -F, LIO-320-B, -C, AIO-320-A, -B, -C, AEIO-320-D, -E, O-340-A, -B, O-360-A, -B, -C, -D, -E, -F, -G, -J, IO-360-A, -B, -C, -D, -E, -F, -J, -K, -L, -M, AEIO-360-A, -B, -H, HO-360-A, -B, -C, IVO-360-A, LHIO-360-C, -F, LTO-360-A, -E, TO-360-A, -C, -E, -F, AEIO-390-A, HIO-360-A, -B, -C, -D, -E, -G, IO-390-A, IO-540-A, -B, -C, -D, -E, -G, -J, -K, -L, -M, N, -P, -R, -S, -T, -U, -V, -W, AEIO-540-D, -L, IGO-540-A, -B, IGSO-540-A, -B, HIO-540-A, LTIO-540-F, -J, -K, -N, -R, -U, -V, -W, TIO-540-A, -C, -E, -F, -G, -H, -J, -K, N, -R, -S, -T, -U, -V, -W, TIVO-540-A, VO-540-A, -B, -C, VSO-580-A, IO-580-A, -B, AEIO-580-B, TIO-541-A, -E

ReplacedPartNumber:

ML-18A, as used in Kelly Aerospace / Hartzell Engine Technologies ES 646 series, MCL series & MHJ series starter motors

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No ML-18A-AC Rev A Date 03/05/2015 or later FAA-approved revisions

Models:

O-300-D, -E, IO-360-A, -B, -C, -D, -E, -F, -G, -H, -J, -K, -AB, -AF, -DB, -GB, -HB, -JB, -KB, -ES, TSIO-360-A, -AB, -B, -C, -CB, -D, -DB, -E, -F, -G, -GB, -H, -HB, -EB, -FB, -JB, -KB, -LB, -BB, -MB, -NB, -PB, -RB, -SB, LTSIO-360-E, -EB, -KB, -RB, IO-E46-A, -B, O-470-A, -B, -E, -G, -H, -J, -K, -L, -M, -N, -P, -R, -S, -T, -U, IO-470-A, -C, -D, -E, -F, -G, -H, -J, -K, -L, -LO, -M, -N, -P, -R, -S, -T, -U, -V, -VO, TSIO-470-B, -C, -D, O-520-A, -B, -BA, -BB, -C, -CB, -D, -E, -F, -J, -K, -L, -M, -MB, -N, -NB, -P, L/IO-520-P, IO-520-A, -D, -E, -F, -J, -L, TSIO-520-A, -B, -C, -D, -E, -G, -H, -J, -K, -L, -M, -N, -P, -R, -BB, -DB, -EB, -JB, -KB, -LB, -NB, -T, -U, -UB, -VB, -WB, -AE, -AF, LTSIO-520-AE, TSIO-520-BE, -CE, GTSIO-520-C, -D, -E, -F, -H, -K, -L, -M, -N, IO-550-A, -B, -C, -D, -E, -F, -G, -L, -N, -P, -R, IOF-550-B, -C, -D, -E, -F, -L, -N, -P, -R, TSIO-550-A, -B, -C, -E, -G, -K, -N, TSIOF-550-D, -J, -K, -P, TSIOL-550-A, -B, -C

ReplacedPartNumber:

MDL-1005FS, as used in Kelly Aerospace / Hartzell Engine Technologies MHJ-4002 & -4003 starter motors

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No MDL-1005FS-AC Rev IR Date 12/22/2015 or later FAA-approved revisions

Models:

O-300-D, -E, IO-360-A, -B, -C, -D, -E, -F, -G, -H, -J, -K, -AB, -AF, -DB, -GB, -HB, -JB, -KB, -ES, TSIO-360-A, -AB, -B, -C, -CB, -D, -DB, -E, -F, -G, -GB, -H, -HB, -EB, -FB, -JB, -KB, -LB, -BB, -MB, -NB, -PB, -RB, -SB, LTSIO-360-E, -EB, -KB, -RB, IO-E46-A, -B, O-470-A, -B, -E, -G, -H, -J, -K, -L, -M, -N, -P, -R, -S, -T, -U, IO-470-A, -C, -D, -E, -F, -G, -H, -J, -K, -L, -LO, -M, -N, -P, -R, -S, -T, -U, -V, -VO, TSIO-470-B, -C, -D, O-520-A, -B, -BA, -BB, -C, -CB, -D, -E, -F, -J, -K, -L, -M, -MB, -N, -NB, -P, L/IO-520-P, IO-520-A, -D, -E, -F, -J, -L, TSIO-520-A, -B, -C, -D, -E, -G, -H, -J, -K, -L, -M, -N, -P, -R, -BB, -DB, -EB, -JB, -KB, -LB, -NB, -T, -U, -UB, -VB, -WB, -AE, -AF, LTSIO-520-AE, TSIO-520-BE, -CE, GTSIO-520-C, -D, -E, -F, -H, -K, -L, -M, -N, IO-550-A, -B, -C, -D, -E, -F, -G, -L, -N, -P, -R, IOF-550-B, -C, -D, -E, -F, -L, -N, -P, -R, TSIO-550-A, -B, -C, -E, -G, -K, -N, TSIOF-550-D, -J, -K, -P, TSIOL-550-A, -B, -C

ReplacedPartNumber:

MDC-0034, as used in Kelly Aerospace / Hartzell Engine Technologies MCL-6501, MHJ -4002, -4003, -4004, -4005 & MCL-6502, -6503 starter motors

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No MDC-0034-AC Rev A Date 03/05/2017 or later FAA-approved revisions

Models:

O-300-D, -E, IO-360-A, -B, -C, -D, -E, -F, -G, -H, -J, -K, -AB, -AF, -DB, -GB, -HB, -JB, -KB, -ES, TSIO-360-A, -AB, -B, -C, -CB, -D, -DB, -E, -F, -G, -GB, -H, -HB, -EB, -FB, -JB, -KB, -LB, -BB, -MB, -NB, -PB, -RB, -SB, LTSIO-360-E, -EB, -KB, -RB, IO-E46-A, -B, O-470-A, -B, -E, -G, -H, -J, -K, -L, -M, -N, -P, -R, -S, -T, -U, IO-470-A, -C, -D, -E, -F, -G, -H, -J, -K, -L, -LO, -M, -N, -P, -R, -S, -T, -U, -V, -VO, TSIO-470-B, -C, -D, O-520-A, -B, -BA, -BB, -C, -CB, -D, -E, -F, -J, -K, -L, -M, -MB, -N, -NB, -P, L/IO-520-P, IO-520-A, -D, -E, -F, -J, -L, TSIO-520-A, -B, -C, -D, -E, -G, -H, -J, -K, -L, -M, -N, -P, -R, -BB, -DB, -EB, -JB, -KB, -LB, -NB, -T, -U, -UB, -VB, -WB, -AE, -AF, LTSIO-520-AE, TSIO-520-BE, -CE, GTSIO-520-C, -D, -E, -F, -H, -K, -L, -M, -N, IO-550-A, -B, -C, -D, -E, -F, -G, -L, -N, -P, -R, IOF-550-B, -C, -D, -E, -F, -L, -N, -P, -R, TSIO-550-A, -B, -C, -E, -G, -K, -N, TSIOF-550-D, -J, -K, -P, TSIOL-550-A, -B, -C

ReplacedPartNumber:

Hartzell Engine Technologies ES646376

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No ES646376-AC Rev IR Date 12/22/2015 or later FAA-approved revisions

Models:

O-300-D, -E, IO-360-A, -B, -C, -D, -E, -F, -G, -H, -J, -K, -AB, -AF, -DB, -GB, -HB, -JB, -KB, -ES, TSIO-360-A, -AB, -B, -C, -CB, -D, -DB, -E, -F, -G, -GB, -H, -HB, -EB, -FB, -JB, -KB, -LB, -BB, -MB, -NB, -PB, -RB, -SB, LTSIO-360-E, -EB, -KB, -RB, IO-E46-A, -B, O-470-A, -B, -E, -G, -H, -J, -K, -L, -M, -N, -P, -R, -S, -T, -U, IO-470-A, -C, -D, -E, -F, -G, -H, -J, -K, -L, -LO, -M, -N, -P, -R, -S, -T, -U, -V, -VO, TSIO-470-B, -C, -D, O-520-A, -B, -BA, -BB, -C, -CB, -D, -E, -F, -J, -K, -L, -M, -MB, -N, -NB, -P, L/IO-520-P, IO-520-A, -D, -E, -F, -J, -L, TSIO-520-A, -B, -C, -D, -E, -G, -H, -J, -K, -L, -M, -N, -P, -R, -BB, -DB, -EB, -JB, -KB, -LB, -NB, -T, -U, -UB, -VB, -WB, -AE, -AF, LTSIO-520-AE, TSIO-520-BE, -CE, GTSIO-520-C, -D, -E, -F, -H, -K, -L, -M, -N, IO-550-A, -B, -C, -D, -E, -F, -G, -L, -N, -P, -R, IOF-550-B, -C, -D, -E, -F, -L, -N, -P, -R, TSIO-550-A, -B, -C, -E, -G, -K, -N, TSIOF-550-D, -J, -K, -P, TSIOL-550-A, -B, -C

ReplacedPartNumber:

MHB-3005AS, as used in Kelly Aerospace / Hartzell Engine Technologies MMU-4001 starter motor

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No MHB-3005AS-AC Rev IR Date 12/22/2015 or later FAA-approved revisions

Models:

O-235-A, -B, -AP, -BP, -C, -G, -H, -J, -K, -L, -M, -N, -P

ReplacedPartNumber:

Hartzell Engine Technologies ES646351

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No ES646351-AC Rev IR Date 12/22/2015 or later FAA-approved revisions

Models:

O-300-D, -E, IO-360-A, -B, -C, -D, -E, -F, -G, -H, -J, -K, -AB, -AF, -DB, -GB, -HB, -JB, -KB, -ES, TSIO-360-A, -AB, -B, -C, -CB, -D, -DB, -E, -F, -G, -GB, -H, -HB, -EB, -FB, -JB, -KB, -LB, -BB, -MB, -NB, -PB, -RB, -SB, LTSIO-360-E, -EB, -KB, -RB, IO-E46-A, -B, O-470-A, -B, -E, -G, -H, -J, -K, -L, -M, -N, -P, -R, -S, -T, -U, IO-470-A, -C, -D, -E, -F, -G, -H, -J, -K, -L, -LO, -M, -N, -P, -R, -S, -T, -U, -V, -VO, TSIO-470-B, -C, -D, O-520-A, -B, -BA, -BB, -C, -CB, -D, -E, -F, -J, -K, -L, -M, -MB, -N, -NB, -P, L/IO-520-P, IO-520-A, -D, -E, -F, -J, -L, TSIO-520-A, -B, -C, -D, -E, -G, -H, -J, -K, -L, -M, -N, -P, -R, -BB, -DB, -EB, -JB, -KB, -LB, -NB, -T, -U, -UB, -VB, -WB, -AE, -AF, LTSIO-520-AE, TSIO-520-BE, -CE, GTSIO-520-C, -D, -E, -F, -H, -K, -L, -M, -N, IO-550-A, -B, -C, -D, -E, -F, -G, -L, -N, -P, -R, IOF-550-B, -C, -D, -E, -F, -L, -N, -P, -R, TSIO-550-A, -B, -C, -E, -G, -K, -N, TSIOF-550-D, -J, -K, -P, TSIOL-550-A, -B, -C

ReplacedPartNumber:

MZ-1005RSS as used in Kelly Aerospace / Hartzell Engine Technologies MZ-4214 starter motor

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No MZ-1005RSS-AC Rev IR Date 12/22/2015 or later FAA-approved revisions

Models:

O-235-A, -B, -AP, -BP, -C, -G, -H, -J, -K, -L, -M, -N, -P, O-320-A, -B, -C, -D, IO-320-A, -B, -C, -D, -E, -F, LIO-320-B, -C, AIO-320-A, -B, -C, AEIO-320-D, -E

ReplacedPartNumber:

International Aero Engines P/N 5A1711

ApprovalBasis:

Tests and Computations per 14 CFR 21.303 (c)(4), Dwg No. M0C36921, Rev. A, Date 11/10/08, or later FAA approved revisions.

Models:

IAE) (V2500-A1

ReplacedPartNumber:

International Aero Engines P/N 5A0906

ApprovalBasis:

Tests and Computations per 14 CFR 21.303 (c)(4), Dwg No. JA5A0906, Rev. -, Date 2017/01/31, or later FAA approved revisions.

Models:

IAE) (V2500-A1

ReplacedPartNumber:

Lycoming Engines 66GP-0SANN

ApprovalBasis:

Identicality Per 14 CFR 21.303 DWG No 4370 Rev F Date 09/10/08 or later FAA approved revisions

Models:

IO-360-P1A

ReplacedPartNumber:

Lycoming Engines 66GC25RFNN

ApprovalBasis:

Identicality Per 14 CFR 21.303 DWG No 4330 Rev E Date 01/17/05 or later FAA approved revisions

Models:

LIO-360-B1G6

ReplacedPartNumber:

Lycoming Engines 1182-E7

ApprovalBasis:

Identicality Per 14 CFR 21.303 DWG No REM38E[F] Rev NR Date 07/12/13 Parts List No REM38E[F]PP Rev NR Date 07/12/13 or later FAA approved revisions

Models:

LIO-360-B

ReplacedPartNumber:

Lycoming Engines LW-M-2463 LW-M-2464

ApprovalBasis:

Identicality Per 14 CFR 21.303 DWG No 503099 - ( ) Rev A Date 02/17/04 or later FAA approved revisions

Models:

IO-540-AE1A5

ReplacedPartNumber:

Lycoming Engines 1182-F7

ApprovalBasis:

Identicality Per 14 CFR 21.303 DWG No RHM38E[F] Rev NR Date 08/29/13 Parts List No RHM38E[F]PP Rev NR Date 08/29/13 or later FAA approved revisions

Models:

LIO-360-B

ReplacedPartNumber:

Lycoming Engines 66GP-0RANN

ApprovalBasis:

Identicality Per 14 CFR 21.303 DWG No 4302 Rev E Date 01/17/05 or later FAA approved revisions

Models:

LIO-360-B1G6

ReplacedPartNumber:

Lycoming Engines 66GC05SFNN

ApprovalBasis:

Identicality Per 14 CFR 21.303 DWG No 4381 Rev E Date 01/17/05 or later FAA approved revisions

Models:

O-235-F2A

ReplacedPartNumber:

Lycoming Engines 1182-K7

ApprovalBasis:

Identicality Per 14 CFR 21.303 DWG No RHM38S[C] Rev NR Date 10/02/13 Parts List No RHM38S[C]PP Rev NR Date 10/02/13 or later FAA approved revisions

Models:

LIO-360-B

ReplacedPartNumber:

Lycoming Engines 1182-J7

ApprovalBasis:

Identicality Per 14 CFR 21.303 DWG No REM38S[C] Rev NR Date 10/02/13 Parts List No REM38S[C]PP Rev NR Date 10/02/13 or later FAA approved revisions

Models:

LIO-360-B

ReplacedPartNumber:

Lycoming Engines 1182-B3

ApprovalBasis:

Identicality Per 14 CFR 21.303 DWG No REM40E[F] Rev NR Date 07/12/13 Parts List No REM40E[F]PP Rev NR Date 07/11/13 or later FAA approved revisions

Models:

LIO-360-B

ReplacedPartNumber:

Lycoming Engines 67P20406 67P20407

ApprovalBasis:

Identicality Per 14 CFR 21.303 DWG No 503099 - ( ) Rev B Date 04/08/09 or later FAA approved revisions

Models:

IO-360-P1A

ReplacedPartNumber:

Lycoming Engines 1182-B7

ApprovalBasis:

Identicality Per 14 CFR 21.303 DWG No REM37BY[E] Rev NR Date 07/17/13 Parts List No REM37BY[E]PP Rev NR Date 07/17/13 or later FAA approved revisions

Models:

LIO-360-B

ReplacedPartNumber:

Lycoming Engines 66GC20SFNN

ApprovalBasis:

Identicality Per 14 CFR 21.303 DWG No 4371 Rev D Date 01/17/05 or later FAA approved revisions

Models:

AEIO-320-H1A, AEIO-320-H1B, IO-360-P1A

ReplacedPartNumber:

Lycoming Engines 66GC25SFNN

ApprovalBasis:

Identicality Per 14 CFR 21.303 DWG No 4373 Rev D Date 01/17/05 or later FAA approved revisions

Models:

IO-360-B1F6, IO-360-P1A

ReplacedPartNumber:

Harper Engineering H3-1898-334A, Boeing S412A100-334A

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No ADP25007 Rev A Date 10/26/2017 or later FAA-approved revisions

Models:

737-700 Series, 737-800 Series, 737-900ER Series

ReplacedPartNumber:

Harper Engineering H3-1898-203A, Boeing S413U100-203

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No ADP25007 Rev A Date 10/26/2017 or later FAA-approved revisions

Models:

747-8 Series

ReplacedPartNumber:

Harper Engineering H3-1898-360A, Boeing S412A100-360A

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No ADP25007 Rev A Date 10/26/2017 or later FAA-approved revisions

Models:

737-700 Series, 737-800 Series, 737-900 Series, 737-900ER Series

ReplacedPartNumber:

Harper Engineering H3-1898-403A, Boeing S832Z610-13

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No ADP25007 Rev A Date 10/26/2017 or later FAA-approved revisions

Models:

787-8, 787-9

ReplacedPartNumber:

Harper Engineering H3-1898-323A, Boeing S412A100-323A

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No ADP25007 Rev A Date 10/26/2017 or later FAA-approved revisions

Models:

737-800 Series

ReplacedPartNumber:

Harper Engineering H3-1898-357A, Boeing S412A100-357A

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No ADP25007 Rev A Date 10/26/2017 or later FAA-approved revisions

Models:

737-800 Series, 737-900 Series, 737-900ER Series

ReplacedPartNumber:

Harper Engineering H3-1898-353A, Boeing S412A100-353A

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No ADP25007 Rev A Date 10/26/2017 or later FAA-approved revisions

Models:

737-800 Series

ReplacedPartNumber:

Harper Engineering H3-1898-342A, Boeing S412A100-342A

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No ADP25007 Rev A Date 10/26/2017 or later FAA-approved revisions

Models:

737-900ER Series

ReplacedPartNumber:

Harper Engineering H3-1898-401A, Boeing S832Z610-11

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No ADP25007 Rev A Date 10/26/2017 or later FAA-approved revisions

Models:

787-8, 787-9

ReplacedPartNumber:

Harper Engineering H3-1898-343A, Boeing S412A100-343A

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No ADP25007 Rev A Date 10/26/2017 or later FAA-approved revisions

Models:

737-900ER Series

ReplacedPartNumber:

Harper Engineering H3-1898-205A, Boeing S413U100-205

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No ADP25007 Rev A Date 10/26/2017 or later FAA-approved revisions

Models:

747-8 Series

ReplacedPartNumber:

Harper Engineering H3-1898-402A, Boeing S832Z610-12

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No ADP25007 Rev A Date 10/26/2017 or later FAA-approved revisions

Models:

787-8, 787-9

ReplacedPartNumber:

Harper Engineering H3-1898-404A, Boeing S832Z610-14

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No ADP25007 Rev A Date 10/26/2017 or later FAA-approved revisions

Models:

787-8, 787-9

ReplacedPartNumber:

Harper Engineering H3-1898-330A, Boeing S412A100-330A

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No ADP25007 Rev A Date 10/26/2017 or later FAA-approved revisions

Models:

737-700 Series, 737-800 Series, 737-900 Series, 737-900ER Series

ReplacedPartNumber:

Harper Engineering H3-1898-204A, Boeing S413U100-204

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No ADP25007 Rev A Date 10/26/2017 or later FAA-approved revisions

Models:

747-8 Series

ReplacedPartNumber:

Harper Engineering H3-1898-335A, Boeing S412A100-335A

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No ADP25007 Rev A Date 10/26/2017 or later FAA-approved revisions

Models:

737-900ER Series

ReplacedPartNumber:

Harper Engineering H3-1898-358A, Boeing S412A100-358A

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No ADP25007 Rev A Date 10/26/2017 or later FAA-approved revisions

Models:

737-700 Series, 737-800 Series, 737-900ER Series

ReplacedPartNumber:

Harper Engineering H3-1898-328A, Boeing S412A100-328A

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No ADP25007 Rev A Date 10/26/2017 or later FAA-approved revisions

Models:

737-800 Series, 737-900ER Series

ReplacedPartNumber:

Harper Engineering H3-1898-347A, Boeing S412A100-347A

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No ADP25007 Rev A Date 10/26/2017 or later FAA-approved revisions

Models:

737-700 Series, 737-800 Series, 737-900ER Series

ReplacedPartNumber:

Harper Engineering H3-1898-327A, Boeing S412A100-327A

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No ADP25007 Rev A Date 10/26/2017 or later FAA-approved revisions

Models:

737-800 Series, 737-900ER Series

ReplacedPartNumber:

Harper Engineering H3-1898-202A, Boeing S413U100-202

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No ADP25007 Rev A Date 10/26/2017 or later FAA-approved revisions

Models:

747-8 Series

ReplacedPartNumber:

Harper Engineering H3-1898-318A, Boeing S412A100-318A

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No ADP25007 Rev A Date 10/26/2017 or later FAA-approved revisions

Models:

737-800 Series, 737-900ER Series

ReplacedPartNumber:

Lycoming Engines 66GC25SFNN

ApprovalBasis:

Identicality Per 14 CFR 21.303 DWG No 4373 Rev D Date 01/17/05 or later FAA approved revisions

Models:

AEIO-360-A1E, AEIO-360-B1H, IO-360-A1D6, IO-360-B1G6, IO-360-M1B, O-290-D2, O-290-D2B, O-290-D2C, O-320-B2D, O-320-B2E, O-360-A1D, O-360-A1H6, O-360-A1P, O-360-A4M, O-360-B2C, O-360-C4P

ReplacedPartNumber:

Lycoming Engines 66GR25RANN

ApprovalBasis:

Identicality Per 14 CFR 21.303 DWG No 4348 Rev D Date 01/17/05 or later FAA approved revisions

Models:

LIO-360-M1A

ReplacedPartNumber:

Lycoming Engines 67P20403 67P20400

ApprovalBasis:

Identicality Per 14 CFR 21.303 DWG No 503099 - ( ) Rev B Date 04/08/09 or later FAA approved revisions

Models:

IO-360-C1G6

ReplacedPartNumber:

Continental Motors 628325 Lycoming Engines 1182-E7 Champion REM38E[E]

ApprovalBasis:

Identicality Per 14 CFR 21.303 DWG No REM38E[F] Rev NR Date 07/12/13 Parts List No REM38E[F]PP Rev NR Date 07/12/13 or later FAA approved revisions

Models:

C-145, O-300-A, B, C, D, GO-300-A, B, C, D, E, F, IO-240-A, B, IOF-240-B, IO-346-A, IO-360-A, AB, C, CB, D, DB, E, ES, G, GB, H, HB, J, JB, K, KB, L/TSIO-360-A, AB, B, BB, C, CB, D, DB, E, EB, F, FB, G, GB, H, HB, JB, KB, LB, MB, RB, SB, E-165, E-185, O-470-2, B, G, H, M, N, P, IO-470-C, G, J, K, R, P, T) Lycoming Engines (O-235-C, E, H, K, L, M, N, P, O-290, O-320-A, B, C, D, E, H, IO-320-A, B, C, D, E, F, LIO-320-B, AEIO-320-A, D, E, O-360-A, B, C, D, F, J, IO-360-A, B, C, D, E, F, J, L, M, N, HO-360-A, B, C, LO-360-A, HIO-360-A, B, C, D, G, LIO-360-C, M, LHIO-360-C, AIO-360-A, B, AEIO-360-A, B, H, VO-360-A, B, GO-435-C, VO-435-A, GO-480-B, D, F, GSO-480-A, B, IGSO-480, O-540-A, B, E, F, G, H, J, IO-540-A, B, C, D, E, G, J, K, L, N, R, T, V, W, AB, AE, AEIO-540-D, L, VO-540-C2A

ReplacedPartNumber:

Continental Motors 655707 Lycoming Engines 1182-B7 Champion REM37BY[D]

ApprovalBasis:

Identicality Per 14 CFR 21.303 DWG No REM37BY[E] Rev NR Date 07/17/13 Parts List No REM37BY[E]PP Rev NR Date 07/17/13 or later FAA approved revisions

Models:

A-40, A-50, A-65, A-75, A-80, C-75, C-85, C-90, O-200-A, B, C, D, X, C-115, C-125, C-145, O-300-A, B, C, D, GO-300-A, B, C, D, E, F, E-165, E-185, E-225) Lycoming Engines (O-235-C, E, H, K, L, M, N, P, O-290, O-320-A, B, C, D, E, H, IO-320-A, B, C, D, E, F, LIO-320-B, AEIO-320-A, D, E, O-360-A, B, C, D, F, J, IO-360-A, B, C, D, E, F, J, L, M, N, HO-360-A, B, C, LO-360-A, HIO-360-A, B, G, LIO-360-C, M, AIO-360-A, B, AEIO-360-A, B, H, VO-360-A, B, O-540-A, B, E, F, G, H, J, IO-540-A, B, C, D, E, G, J, K, L, N, R, T, V, W, AB, AE, AEIO-540-D, L, VO-540-C2A

ReplacedPartNumber:

Lycoming Engines 66LP-0SCEN

ApprovalBasis:

Identicality Per 14 CFR 21.303 DWG No 6390 Rev G Date 07/28/08 or later FAA approved revisions

Models:

O-540-F1A5

ReplacedPartNumber:

Lycoming Engines 66GP-0SAEN

ApprovalBasis:

Identicality Per 14 CFR 21.303 DWG No 4342 Rev E Date 01/17/05 or later FAA approved revisions

Models:

O-360-A1F6

ReplacedPartNumber:

Continental Motors 646631 Lycoming Engines 1182-L7 Champion RHB36S[B]

ApprovalBasis:

Identicality Per 14 CFR 21.303 DWG No RHB36S[C] Rev NR Date 10/02/13 Parts List No RHB36S[C]PP Rev NR Date 10/02/13 or later FAA approved revisions

Models:

O-470-U, T, IO-470-D, E, F, H, L, M, N, S, U, V, GIO-470-A, TSIO-470-B, C, D, GTSIO-520-D, F, G, H, K, L, M, N, IO-520-A, B, BA, BB, C, CB, D, F, J, K, L, M, MB, N, NB, L/IO-520-P, L/TSIO-520-B, C, D, DB, E, EB, G, H, J, JB, K, KB, L, LB, M, N, NB, P, R, T, U, UB, VB, WB, AE, BE, CE, IO-550-A, B, C, D, E, F, L, N, P, R, IOF-550-B, C, D, E, F, L.N, P, R, TSIO-550-A, B, C, E, G, K, N, TSIO-550-D, J, K) Lycoming Engines (, IO-360-A, C, IVO-360, TO-360-C, E, F, LTO-360-E, TIO-360-A, C, IO-390-A, C, AEIO-390-A, TVO-435-A, B, C, D, E, F, G, VO-435-A, B, GO-480-G1, G2, IGO-480-A, GSO-480, IGSO-480, O-540-9, L, IO-540-E, G, J, K, M, P, R, S, AA, AC, IGO-540-A, B, IGSO-540-A, B, IVO-540-A, AEIO-540-L, TIO-540-A, C, E, F, G, H, J, K, N, R, S, T, U, V, W, AA, AB, AE, AF, AG, AH, AJ, AK, LTIO-540-F, J, N, R, U, V, TIVO-540-A, VO-540-A, B, C, TIO-541-A, E, TIGO-541-E, IO-580, AEIO-580, IO-720-A, B, D

ReplacedPartNumber:

Lycoming Engines 67P20428 67P20429

ApprovalBasis:

Identicality Per 14 CFR 21.303 DWG No 503099 - ( ) Rev B Date 04/08/09 or later FAA approved revisions

Models:

IO-360-M1A, IO-360-M1B, LIO-360-M1A

ReplacedPartNumber:

Continental Motors 634675 Lycoming Engines 1182-U5 Champion RHB32E[E]

ApprovalBasis:

Identicality Per 14 CFR 21.303 DWG No RHB32E[F] Rev NR Date 10/12/12 Parts List No RHB32E[F]PP Rev NR Date 05/08/13 or later FAA approved revisions

Models:

O-470-U, T, IO-470-D, E, F, H, L, M, N, S, U, V, GIO-470-A, TSIO-470-B, C, D, GTSIO-520-D, F, G, H, K, L, M, N, IO-520-A, B, BA, BB, C, CB, D, F, J, K, L, M, MB, N, NB, L/IO-520-P, L/TSIO-520-B, C, D, DB, E, EB, G, H, J, JB, K, KB, L, LB, M, N, NB, P, R, T, U, UB, VB, WB, AE, BE, CE, IO-550-A, B, C, D, E, F, L, N, P, R, IOF-550-B, C, D, E, F, L.N, P, R, TSIO-550-A, B, C, E, G, K, N, TSIO-550-D, J, K) Lycoming Engines (IO-360-A, C, HIO-360-E, F, LHIO-360-F, TO-360-C, E, F, LTO-360-E, TIO-360-A, C, TVO-435-A, B, C, D, E, F, G, VO-435-A, B, GO-480-G1, G2, IGO-480-A, GSO-480, IGSO-480, O-540-L, IO-540-E, G, J, K, M, P, R, S, AA, AC, IGO-540-A, B, IGSO-540-A, B, AEIO-540-L, TIO-540-A, C, E, F, G, H, J, K, N, R, S, T, U, V, W, AA, AB, AE, AF, AG, AH, AJ, AK, LTIO-540-F, J, N, R, U, V, TIVO-540-A, TIO-541-A, E, TIGO-541-E, IO-720-A, B, D

ReplacedPartNumber:

Lycoming Engines 66LC35SDNN

ApprovalBasis:

Identicality Per 14 CFR 21.303 DWG No 6351 Rev D Date 01/18/05 or later FAA approved revisions

Models:

AEIO-540-L1D5, IO-540-A1B5, IO-540-AC1A5, IO-540-AF1A5, IO-540-C4D5, IO-540-M1A5, IO-540-M1C5, IO-540-T4B5, IO-540-V4A5, IO-540-W1A5, O-540-A1B5, O-540-A4A5, O-540-A4B5, O-540-A4E5, O-540-F1A5, O-540-H2A5

ReplacedPartNumber:

Lycoming Engines 66GR25SANN

ApprovalBasis:

Identicality Per 14 CFR 21.303 DWG No 4347 Rev D Date 01/17/05 or later FAA approved revisions

Models:

AEIO-320-D1B, AEIO-360-B1F, HIO-360-G1A, IO-360-B4A, IO-360-M1A, IO-360-N1A, O-360-A4M, O-360-J2A

ReplacedPartNumber:

Lycoming Engines 1182-A7 Champion REB32E[C]

ApprovalBasis:

Identicality Per 14 CFR 21.303 DWG No REB32E[D] Rev NR Date 07/07/13 Parts List No REB32E[D]PP Rev NR Date 07/07/13 or later FAA approved revisions

Models:

IO-540-E, J, K, P, R, AE, AEIO-540-L, TIO-540-C1A, E, H

ReplacedPartNumber:

Lycoming Engines 67P20406 67P20407

ApprovalBasis:

Identicality Per 14 CFR 21.303 DWG No 503099 - ( ) Rev B Date 04/08/09 or later FAA approved revisions

Models:

AEIO-360-H1B, O-360-A4P

ReplacedPartNumber:

Continental Motors 646632 Lycoming Engines 1182-M7 Champion RHB32S[B]

ApprovalBasis:

Identicality Per 14 CFR 21.303 DWG No RHB32S[C] Rev NR Date 05/08/13 Parts List No RHB32S[C]PP Rev A Date 05/16/16 or later FAA approved revisions

Models:

O-470-U, T, IO-470-D, E, F, H, L, M, N, S, U, V, GIO-470-A, TSIO-470-B, C, D, GTSIO-520-D, F, G, H, K, L, M, N, IO-520-A, B, BA, BB, C, CB, D, F, J, K, L, M, MB, N, NB, L/IO-520-P, L/TSIO-520-B, C, D, DB, E, EB, G, H, J, JB, K, KB, L, LB, M, N, NB, P, R, T, U, UB, VB, WB, AE, BE, CE, IO-550-A, B, C, D, E, F, L, N, P, R, IOF-550-B, C, D, E, F, L.N, P, R, TSIO-550-A, B, C, E, G, K, N, TSIO-550-D, J, K) Lycoming Engines (IO-360-A, C, HIO-360-E, F, LHIO-360-F, TO-360-C, F, TIO-360-A, C, TVO-435-A, B, C, D, E, F, G, VO-435-A, B, GO-480-G1, G2, IGO-480-A, GSO-480, IGSO-480, O-540-9, L, IO-540-E, G, J, K, M, P, R, S, AA, AC, IGO-540-A, B, IGSO-540-A, B, IVO-540-A, AEIO-540-L, TIO-540-A, C, E, F, G, H, J, K, N, R, S, T, U, V, W, AA, AB, AE, AF, AG, AH, AJ, AK, LTIO-540-F, J, N, R, U, V, TIVO-540-A, VO-540-A, B, C, TIO-541-A, E, TIGO-541-E, IO-720-A, B, D

ReplacedPartNumber:

Lycoming Engines 66GC20SFNN

ApprovalBasis:

Identicality Per 14 CFR 21.303 DWG No 4371 Rev D Date 01/17/05 or later FAA approved revisions

Models:

AEIO-360-A1B6, AEIO-360-H1B, IO-360-B4A, IO-360-C1A, IO-360-C1C, IO-360-L2A, IO-360-M1B, O-320-B2B, O-320-D1A, O-320-E1F, O-360-A4P, O-360-C1G, O-360-C4F, O-360-C4P

ReplacedPartNumber:

Lycoming Engines 66GP-0SANN

ApprovalBasis:

Identicality Per 14 CFR 21.303 DWG No 4370 Rev F Date 09/10/08 or later FAA approved revisions

Models:

AEIO-360-A1E6, AEIO-360-A2C, AEIO-360-B1F, AEIO-360-B1H, AEIO-360-B2F, AEIO-360-H1B, AEIO-390-A1A6, AEIO-390-A3A6, AEIO-390-A1B6, AEIO-390-A3B6, HIO-360-G1A, IO-360-A2D, IO-360-A3B6, IO-360-B1F, IO-360-B1G6, IO-360-B2E, IO-360-M1A, IO-360-M1B, IO-360-N1A, IO-390-A1A6, IO-390-A1B6, IO-390-A3A6, IO-390-A3B6, IO-390-C1A6, IO-390-C1B6, IO-390-C3A6, IO-390-C3B6, O-290-D2, O-290-D2B, O-290-D2C, O-320-B2E, O-360-A1H6, O-360-A1P, O-360-A4P, O-360-B2C, O-360-C4F, O-360-C4P, O-360-J2A

ReplacedPartNumber:

Lycoming Engines 66LR30SCNP

ApprovalBasis:

Identicality Per 14 CFR 21.303 DWG No 6363 Rev G Date 01/18/05 or later FAA approved revisions

Models:

IO-540-AG1A5

ReplacedPartNumber:

Lycoming Engines 66LP-0SCNP

ApprovalBasis:

Identicality Per 14 CFR 21.303 DWG No 6360 Rev G Date 01/18/05 or later FAA approved revisions

Models:

IO-540-AA1B5, IO-540-AG1A5, TIO-540-AF1B, TIO-540-AH1A, TIO-540-AJ1A

ReplacedPartNumber:

Lycoming Engines 67J20609-P 67J20608-P

ApprovalBasis:

Identicality per 14 CFR 21.303 DWG No 503099 - ( ) Rev B Date 04/08/09 or later FAA approved revisions

Models:

IO-580-B1A, TIO-540-AF1B, TIO-540-AH1A, TIO-540-AJ1A, TIO-540-AK1A

ReplacedPartNumber:

Lycoming Engines 1182-H7 Champion RHB37E[E]

ApprovalBasis:

Identicality Per 14 CFR 21.303 DWG No RHB37E[F] Rev NR Date 09/04/13 Parts List No RHB37E[F]PP Rev A Date 08/08/14 or later FAA approved revisions

Models:

IO-360-A, C, IVO-360, HIO-360-E, F, LHIO-360-F, TO-360-C, E, F, LTO-360-E, TIO-360-A, C, IO-390-A, C, AEIO-390-A, TVO-435-A, B, C, D, E, F, G, VO-435-A, B, GO-480-G1, G2, IGO-480-A, GSO-480, IGSO-480, O-540-9, L, IO-540-E, G, J, K, M, P, R, S, AA, AC, IGO-540-A, B, IGSO-540-A, B, IVO-540-A, AEIO-540-L, TIO-540-A, C, E, F, G, H, J, K, N, R, S, T, U, V, W, AA, AB, AE, AF, AG, AH, AJ, AK, LTIO-540-F, J, N, R, U, V, TIVO-540-A, VO-540-A, B, C, TIO-541-A, E, TIGO-541-E, IO-580, AEIO-580, IO-720-A, B, D

ReplacedPartNumber:

Lycoming Engines 67U20608 67U20609

ApprovalBasis:

Identicality per 14 CFR 21.303 DWG No 503099 - ( ) Rev B Date 04/08/09 or later FAA approved revisions

Models:

IO-540-V4A5

ReplacedPartNumber:

Lycoming Engines 66LP-0SCNN

ApprovalBasis:

Identicality Per 14 CFR 21.303 DWG No 6350 Rev E Date 01/11/05 or later FAA approved revisions

Models:

AEIO-540-D4D5, AEIO-540-L1D5, AEIO-580-B1A, IO-540-AC1A5, IO-540-AF1A5, IO-540-C4D5, IO-540-M1C5, IO-540-T4B5, IO-540-V4A5, IO-540-W1A5, IO-580-B1A

ReplacedPartNumber:

Lycoming Engines 1182-N8 Champion REB36S

ApprovalBasis:

Identicality Per 14 CFR 21.303 DWG No REB36S[A] Rev NR Date 10/02/13 Parts List No REB36S[A]PP Rev NR Date 10/02/13 or later FAA approved revisions

Models:

IO-390-A, C, AEIO-390-A, IO-580, AEIO-580

ReplacedPartNumber:

Continental Motors 646630 Lycoming Engines 1182-K7 Champion RHM38S[B]

ApprovalBasis:

Identicality Per 14 CFR 21.303 DWG No RHM38S[C] Rev NR Date 10/02/13 Parts List No RHM38S[C]PP Rev NR Date 10/02/13 or later FAA approved revisions

Models:

A-65, A-75, C-75, C-85, C-90, O-200-A, B, C, D, X, C-115, C-125, C-145, O-300-A, B, C, D, GO-300-A, B, C, D, E, F, IO-346-A, IO-360-A, AB, B, BB, C, CB, D, DB, E, EB, F, FB, G, GB, H, HB, JB, KB, LB, MB, RB, SB, L/TSIO-360-A, AB, B, BB, C, CB, D, DB, E, EB, F, FB, G, GB, H, HB, JB, KB, LB, MB, RB, SB, E-165, E-185, E-225, O-470-2, 4, 11, 13, 13A, 15, A, B, E, G, H, J, K, L, M, N, R, S, P, IO-470-C, G, J, K, R, P, T) Lycoming Engines (O-320-H, O-360-A, C, E, F, J, IO-360-A, B, C, D, E, F, J, L, M, N, LO-360-A, E, LIO-360-A, AEIO-360-A, GO-435-C, GO-480-B, D, F, O-540-A, B, E, F, G, H, J, IO-540-A, B, C, D, E, G, K, J, L, N, L, T, V, W, AB, AE, AF, AEIO-540-L, IO-720-A, B, C, D

ReplacedPartNumber:

Lycoming Engines 1182-G7 Champion REB37E[D]

ApprovalBasis:

Identicality Per 14 CFR 21.303 DWG No REB37E[E] Rev NR Date 09/04/13 Parts List No REB37E[E]PP Rev NR Date 09/04/13 or later FAA approved revisions

Models:

O-360-C4P, IO-320-C1A, C1B, F1A, LIO-320-C1A, IO-360-A1B6, C1A, C1F, F1A, IO-390-A, C, AEIO-390-A, O-540-E4A5, IO-540-E, J, K, M, P, R, AE, AEIO-540-L, TIO-540-C1A, E, H, IO-580, AEIO-580

ReplacedPartNumber:

Lycoming Engines 66GC25RFNN

ApprovalBasis:

Identicality Per 14 CFR 21.303 DWG No 4330 Rev E Date 01/17/05 or later FAA approved revisions

Models:

LO-360-A1H6

ReplacedPartNumber:

Lycoming Engines 66GR15SANN

ApprovalBasis:

Identicality Per 14 CFR 21.303 DWG No 4345 Rev D Date 01/17/05 or later FAA approved revisions

Models:

AEIO-360-A2C, AEIO-390-A1A6, AEIO-390-A3A6, AEIO-390-A1B6, AEIO-390-A3B6, IO-360-A1A, IO-360-A2D, IO-390-A1A6, IO-390-A1B6, IO-390-A3A6, IO-390-A3B6, IO-390-C1A6, IO-390-C1B6, IO-390-C3A6, IO-390-C3B6

ReplacedPartNumber:

Lycoming Engines 66LC35SDNP

ApprovalBasis:

Identicality Per 14 CFR 21.303 DWG No 6361 Rev F Date 01/18/05 or later FAA approved revisions

Models:

IO-540-AA1B5, TIO-540-AF1B, TIO-540-AH1A, TIO-540-AJ1A, TIO-540-AK1A

ReplacedPartNumber:

Lycoming Engines 66GP-0SAGN

ApprovalBasis:

Identicality Per 14 CFR 21.303 DWG No 4353 Rev D Date 01/17/05 or later FAA approved revisions

Models:

AEIO-360-A1B6, AEIO-390-A1A6

ReplacedPartNumber:

Continental Motors 630049 Lycoming Engines 1182-F7 Champion RHM38E[E]

ApprovalBasis:

Identicality Per 14 CFR 21.303 DWG No RHM38E[F] Rev NR Date 08/29/13 Parts List No RHM38E[F]PP Rev NR Date 08/29/13 or later FAA approved revisions

Models:

GO-300-A, B, C, D, E, F, IO-240-A, B, IOF-240-B, IO-346-A, IO-360-A, AB, B, BB, C, CB, D, DB, E, EB, F, FB, G, GB, H, HB, JB, KB, LB, MB, RB, SB, L/TSIO-360-A, AB, B, BB, C, CB, D, DB, E, EB, F, FB, G, GB, H, HB, JB, KB, LB, MB, RB, SB, E-165, E-185, O-470-2, 4, 11, 13, 13A, 15, B, G, H, M, N, P, IO-470-C, G, J, K, R, P, T) Lycoming Engines (O-320-H, O-360-A, C, E, F, J, IO-360-A, B, C, D, E, F, J, L, M, N, LO-360-A, E, LIO-360-A, AEIO-360-A, GO-435-C, GO-480-B, D, F, O-540-A, B, E, F, G, H, J, IO-540-A, B, C, D, E, G, K, J, L, N, L, T, V, W, AB, AE, AF, AEIO-540-L, IO-720-A, B, C, D

ReplacedPartNumber:

Lycoming Engines 66GC15SFNN

ApprovalBasis:

Identicality Per 14 CFR 21.303 DWG No 4372 Rev E Date 01/17/05 or later FAA approved revisions

Models:

AEIO-360-A1E6, IO-360-A3B6

ReplacedPartNumber:

Continental Motors 629978 Lycoming Engines 1182-W3 Champion RHM40E[F]

ApprovalBasis:

Identicality Per 14 CFR 21.303 DWG No RHM40E[G] Rev NR Date 08/29/13 Parts List No RHM40E[G]PP Rev NR Date 08/29/13 or later FAA approved revisions

Models:

A-40, A-50, A-65, A-75, A-80, C-75, C-85, C-90, O-200-A, B, C, D, X, C-115, C-125, C-145, O-300-A, B, C, D, GO-300-A, B, C, D, E, F, IO-346-A, E-165, E-185, E-225, O-470-2, 4, 11, 13, 13A, 15, A, B, E, G, H, J, K, L, M, N, R, S, P, IO-470-C, G, J, K, R, P, T) Lycoming Engines (O-320-H, O-360-A, C, E, F, J, IO-360-B, E, F, L, M, N, LO-360-A, E, GO-435-C, GO-480-B, D, F, O-540-A, B, E, F, G, H, J, IO-540-C, D, J, N, T, V, W

ReplacedPartNumber:

Lycoming Engines 67U20638 67U20639

ApprovalBasis:

Identicality per 14 CFR 21.303 DWG No 503099 - ( ) Rev B Date 04/08/09 or later FAA approved revisions

Models:

O-540-A4E5

ReplacedPartNumber:

Continental Motors 646629 Lycoming Engines 1182-J7 Champion REM38S[B]

ApprovalBasis:

Identicality Per 14 CFR 21.303 DWG No REM38S[C] Rev NR Date 10/02/13 Parts List No REM38S[C]PP Rev NR Date 10/02/13 or later FAA approved revisions

Models:

A-65, A-75, C-75, C-85, C-90, O-200-A, B, C, D, X, C-115, C-125, C-145, O-300-A, B, C, D, GO-300-A, B, C, D, E, F, IO-346-A, IO-360-A, AB, B, BB, C, CB, D, DB, E, EB, F, FB, G, GB, H, HB, JB, KB, LB, MB, RB, SB, L/TSIO-360-A, AB, B, BB, C, CB, D, DB, E, EB, F, FB, G, GB, H, HB, JB, KB, LB, MB, RB, SB, E-165, E-185, E-225, O-470-2, 4, 11, 13, 13A, 15, A, B, E, G, H, J, K, L, M, N, R, S, P, IO-470-C, G, J, K, R, P, T) Lycoming Engines (O-235-C, E, F, G, H, J, K, L, M, N, P, O-290, O-320-A, B, C, D, E, H, IO-320-A, B, C, D, E, F, LIO-320-B, AEIO-320-A, D, E, O-360-A, B, C, D, F, J, IO-360-A, B, C, D, E, F, J, L, M, N, HO-360-A, B, C, LO-360-A, HIO-360-A, B, C, D, G, LIO-360-C, M, LHIO-360-C, AIO-360-A, B, AEIO-360-A, B, H, VO-360-A, B, GO-435-C, VO-435-A, GO-480-B, D, F, GSO-480-A, B, IGSO-480, O-540-A, B, E, F, G, H, J, IO-540-A, B, C, D, E, G, J, K, L, N, T, V, AB, AE, AEIO-540-D, L

ReplacedPartNumber:

Lycoming Engines 66LC45SDNN

ApprovalBasis:

Identicality Per 14 CFR 21.303 DWG No 6355 Rev D Date 01/18/05 or later FAA approved revisions

Models:

O-540-E4B5

ReplacedPartNumber:

Continental Motors 627643 Lycoming Engines 1182-B3 Champion REM40E[E]

ApprovalBasis:

Identicality Per 14 CFR 21.303 DWG No REM40E[F] Rev NR Date 07/12/13 Parts List No REM40E[F]PP Rev NR Date 07/11/13 or later FAA approved revisions

Models:

A-40, A-50, A-65, A-75, A-80, C-75, C-85, C-90, O-200-A, B, C, D, X, C-115, C-125, C-145, O-300-A, B, C, D, GO-300-A, B, C, D, E, F, IO-346-A, E-165, E-185, E-225, O-470-2, 4, 11, 13, 13A, 15, A, B, E, G, H, J, K, L, M, N, R, S, P, IO-470-C, G, J, K, R, P, T) Lycoming Engines (O-235-C, E, H, K, L, M, N, P, O-290, O-320-A, B, C, D, E, H, IO-320-A, B, C, D, E, F, LIO-320-B, AEIO-320-A, D, E, O-360-A, B, C, D, F, J, IO-360-B, E, F, L, M, N, HO-360-A, B, C, LO-360-A, HIO-360-A, B, G, LIO-360-M, AEIO-360-B, H, VO-360-A, B, GO-435-C, VO-435-A, GO-480-B, D, F, GSO-480-A, B, IGSO-480, O-540-A, B, E, F, G, H, J, IO-540-C, D, J, N, T, V, W, AEIO-540-D

ReplacedPartNumber:

Lycoming Engines 66LR37SCNN

ApprovalBasis:

Identicality Per 14 CFR 21.303 DWG No 6393 Rev E Date 01/18/05 or later FAA approved revisions

Models:

AEIO-540-D4B5, AEIO-540-D4D5, AEIO-540-L1B5, AEIO-580-B1A, IO-540-AC1A5, IO-540-K1A5, IO-540-K1B5, IO-540-K1E5, IO-540-K1G5, IO-540-K1H5, IO-540-K1K5, IO-540-L1C5, IO-540-M1C5, IO-580-B1A, O-540-B2B5, O-540-B2C5, O-540-E4B5, O-540-E4C5, O-540-G1A5, O-540-G2A5, TIO-540-AJ1A, TIO-540-W2A

ReplacedPartNumber:

Lycoming Engines 66GP-0RANN

ApprovalBasis:

Identicality Per 14 CFR 21.303 DWG No 4302 Rev E Date 01/17/05 or later FAA approved revisions

Models:

LO-360-A1H6, LIO-360-M1A

ReplacedPartNumber:

Lycoming Engines 67P20413 67P20412

ApprovalBasis:

Identicality per 14 CFR 21.303 DWG No 503099 - ( ) Rev B Date 04/08/09 or later FAA approved revisions

Models:

AEIO-390-A, IO-360-M1A, IO-360-N1A, IO-390-A, IO-390-C

ReplacedPartNumber:

International Aero Engines P/N 740-2001-515

ApprovalBasis:

Tests and Computations per 14 CFR 21.303, Dwg No. 740-2001-515KT, Rev. NC, Dated 4/27/2017, or later FAA approved revisions.

Models:

IAE) (V2500-A1) (IAE) c/o IAE Airworthiness (V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, V2533-A5

ReplacedPartNumber:

International Aero Engines P/N 2A3383

ApprovalBasis:

Tests and Computations per 14 CFR 21.303, Dwg No. M2A3383, Rev. B, Dated 18-SEP-2017, or later FAA approved revisions.

Models:

IAE) (V2500-A1, V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, V2525-D5, V2528-D5, V2533-A5

ReplacedPartNumber:

Part Name Pompe a carburant Part Number 340-402-109-0, 340-402-110-0, 340-402-111-0(*) (*) Only P/N 828300-11 / 340-402-111-0 is eligible to all engine models

ApprovalBasis:

Licensing agreement Per 14 CFR 21.303, between Eaton Industrial Corp. and CFM International S.A. Safran Aircraft Engine Type Certificate EASA EASA.E.004 FAA E00055EN E00056EN Certified Design CAD-MODA10627 (Change in design) Approved 18-May-2017 by AAS 28677 or later FAA-approved revision.

Models:

CFM56-7B, forty-nine engine models (49) (*) -7B20, -7B20/2, -7B20/3, -7B20E, -7B22, -7B22/2, -7B22/3, -7B22/B1, -7B22/3B1, -7B22E, -7B22E/B1, -7B24, -7B24/2, -7B24/3, -7B24/B1, -7B24/3B1, -7B24E, -7B24E/B1, -7B26, -7B26/2, -7B26/3, -7B26/3F, -7B26/B1, -7B26/3B1, -7B26/B2, -7B26/3B2, -7B26/3B2F, -7B26E, -7B26E/F, -7B26E/B1, -7B26E/B2, -7B26E/B2F, -7B27, -7B27/2, -7B27/3, 7B27/3F, 7B27/B1, -7B27/3B1, -7B27/3B1F, -7B27/B3, -7B27/3B3, -7B27A, -7B27A/3, -7B27E, -7B27E/F, -7B27E/B1, -7B27E/B1F, -7B27E/B3, -7B27AE

ReplacedPartNumber:

Lycoming Engines LW-10025

ApprovalBasis:

Test & Computations per 14 CFR 21.303 DWG No 8002437 Rev A Date 04/17/2016, or later FAA-approved revisions

Models:

TIO-541-E1A4, TIO-541-E1B4, TIO-541-E1C4, TIO-541-E1D4

ReplacedPartNumber:

International Aero Engines AG CH31964-1

ApprovalBasis:

Identicality Per 14 CFR 21.303, licensing agreement between Champion Aerospace LLC and International Aero Engines Letter Dated 04/13/17 Dwg. No CH31964-1 Rev A and Parts List Rev NR Dated 10/06/16

Models:

V2500-A1, V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, V2533-A5, V2525-D5, V2528-D5, V2531-E5

ReplacedPartNumber:

Dynamic Air Engineering 2793-102-2

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No. M4401-F Rev - Date January 27, 2016 or later FAA approved revisions

Models:

340A (SAAB/SF340A), SAAB 340B

ReplacedPartNumber:

International Aero Engines P/N 2A2351

ApprovalBasis:

Tests and Computations per 14 CFR 21.303, Dwg No. 2A2351JA, Rev. A, Dated 2016/07/21, or later FAA approved revisions.

Models:

V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, V2533-A5, V2525-D5, V2528-D5

ReplacedPartNumber:

Woodward Aircraft Engine Systems P/N 1391-326

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No P01312 Rev - Date 08/17/2015 or later FAA-approved revisions

Models:

A319-131, A319-132, A319-133, A320-231, A320-232, A320-233, A321-131, A321-232, A321-231) International Aero Engines (V2522-A5, V2524-A5, V2527-A5, V2530-A5, V2533-A5, V2525-D5, V2528-D5

ReplacedPartNumber:

Woodward Aircraft Engine Systems P/N 1391-180

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No P01307 Rev - Date 08/17/2015 or later FAA-approved revisions

Models:

A319-131, A319-132, A319-133, A320-231, A320-232, A320-233, A321-131, A321-232, A321-231) International Aero Engines (V2522-A5, V2524-A5, V2527-A5, V2530-A5, V2533-A5, V2525-D5, V2528-D5

ReplacedPartNumber:

Woodward Aircraft Engine Systems P/N 1391-246

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No P01309 Rev - Date 08/17/2015 or later FAA-approved revisions

Models:

A319-131, A319-132, A319-133, A320-231, A320-232, A320-233, A321-131, A321-232, A321-231) International Aero Engines (V2522-A5, V2524-A5, V2527-A5, V2530-A5, V2533-A5, V2525-D5, V2528-D5

ReplacedPartNumber:

Woodward Aircraft Engine Systems P/N 1391-578

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No P01314 Rev - Date 08/17/2015 or later FAA-approved revisions

Models:

A319-131, A319-132, A319-133, A320-231, A320-232, A320-233, A321-131, A321-232, A321-231) International Aero Engines (V2522-A5, V2524-A5, V2527-A5, V2530-A5, V2533-A5, V2525-D5, V2528-D5

ReplacedPartNumber:

Woodward Aircraft Engine Systems P/N 1355-092

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No P01299 Rev - Date 08/27/2015 or later FAA-approved revisions

Models:

A319-131, A319-132, A319-133, A320-231, A320-232, A320-233, A321-131, A321-232, A321-231) International Aero Engines (V2522-A5, V2524-A5, V2527-A5, V2530-A5, V2533-A5, V2525-D5, V2528-D5

ReplacedPartNumber:

Woodward Aircraft Engine Systems P/N 1355-290

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No P01302 Rev - Date 08/27/2015 or later FAA-approved revisions

Models:

A319-131, A319-132, A319-133, A320-231, A320-232, A320-233, A321-131, A321-232, A321-231) International Aero Engines (V2522-A5, V2524-A5, V2527-A5, V2530-A5, V2533-A5, V2525-D5, V2528-D5

ReplacedPartNumber:

Woodward Aircraft Engine Systems P/N 1355-282

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No P01301 Rev - Date 08/27/2015 or later FAA-approved revisions

Models:

A319-131, A319-132, A319-133, A320-231, A320-232, A320-233, A321-131, A321-232, A321-231) International Aero Engines (V2522-A5, V2524-A5, V2527-A5, V2530-A5, V2533-A5, V2525-D5, V2528-D5

ReplacedPartNumber:

Woodward Aircraft Engine Systems P/N 1391-202

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No P01308 Rev - Date 08/17/2015 or later FAA-approved revisions

Models:

A319-131, A319-132, A319-133, A320-231, A320-232, A320-233, A321-131, A321-232, A321-231) International Aero Engines (V2522-A5, V2524-A5, V2527-A5, V2530-A5, V2533-A5, V2525-D5, V2528-D5

ReplacedPartNumber:

Woodward Aircraft Engine Systems P/N 1391-332

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No P01313 Rev - Date 08/17/2015 or later FAA-approved revisions

Models:

A319-131, A319-132, A319-133, A320-231, A320-232, A320-233, A321-131, A321-232, A321-231) International Aero Engines (V2522-A5, V2524-A5, V2527-A5, V2530-A5, V2533-A5, V2525-D5, V2528-D5

ReplacedPartNumber:

Woodward Aircraft Engine Systems P/N 1391-164

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No P01305 Rev - Date 08/17/2015 or later FAA-approved revisions

Models:

A319-131, A319-132, A319-133, A320-231, A320-232, A320-233, A321-131, A321-232, A321-231) International Aero Engines (V2522-A5, V2524-A5, V2527-A5, V2530-A5, V2533-A5, V2525-D5, V2528-D5

ReplacedPartNumber:

Woodward Aircraft Engine Systems P/N 1391-290

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No P01310 Rev - Date 08/17/2015 or later FAA-approved revisions

Models:

A319-131, A319-132, A319-133, A320-231, A320-232, A320-233, A321-131, A321-232, A321-231) International Aero Engines (V2522-A5, V2524-A5, V2527-A5, V2530-A5, V2533-A5, V2525-D5, V2528-D5

ReplacedPartNumber:

Woodward Aircraft Engine Systems P/N 1391-296

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No P01311 Rev - Date 08/17/2015 or later FAA-approved revisions

Models:

A319-131, A319-132, A319-133, A320-231, A320-232, A320-233, A321-131, A321-232, A321-231) International Aero Engines (V2522-A5, V2524-A5, V2527-A5, V2530-A5, V2533-A5, V2525-D5, V2528-D5

ReplacedPartNumber:

Woodward Aircraft Engine Systems P/N 1391-166

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No P01306 Rev - Date 08/17/2015 or later FAA-approved revisions

Models:

A319-131, A319-132, A319-133, A320-231, A320-232, A320-233, A321-131, A321-232, A321-231) International Aero Engines (V2522-A5, V2524-A5, V2527-A5, V2530-A5, V2533-A5, V2525-D5, V2528-D5

ReplacedPartNumber:

Woodward Aircraft Engine Systems P/N 1355-270

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No P01300 Rev - Date 08/27/2015 or later FAA-approved revisions

Models:

A319-131, A319-132, A319-133, A320-231, A320-232, A320-233, A321-131, A321-232, A321-231) International Aero Engines (V2522-A5, V2524-A5, V2527-A5, V2530-A5, V2533-A5, V2525-D5, V2528-D5

ReplacedPartNumber:

Woodward Aircraft Engine Systems P/N 1382-228

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No P01304 Rev A Date 10/29/2015 or later FAA-approved revisions

Models:

A319-131, A319-132, A319-133, A320-231, A320-232, A320-233, A321-131, A321-232, A321-231) International Aero Engines (V2522-A5, V2524-A5, V2527-A5, V2530-A5, V2533-A5, V2525-D5, V2528-D5

ReplacedPartNumber:

International Aero Engines, LLC P/N 5323065

ApprovalBasis:

Identicality per 14 CFR Sec. 21.303 (c), licensing agreement between International Aero Engines, LLC and Lear Romec Division Crane Co. Dwg. No. 5323065 Rev. (none) Date 30 September, 2014 or later FAA-approved revisions.

Models:

International Aero Engines, LLC Series Engines, PW1133G-JM, PW1133GA-JM, PW1130G-JM, PW1127G-JM, PW1127GA-JM, PW1124G1-JM, PW1124G-JM, PW1122G-JM, PW1127G1-JM

ReplacedPartNumber:

International Aero Engines, LLC P/N 5314333

ApprovalBasis:

Identicality per 14 CFR Sec. 21.303 (c), licensing agreement between International Aero Engines, LLC and Lear Romec Division Crane Co. Dwg. No. 5314333 Rev. (none) Date 19 September, 2013 or later FAA-approved revisions.

Models:

International Aero Engines, LLC Series Engines, PW1133G-JM, PW1133GA-JM, PW1130G-JM, PW1127G-JM, PW1127GA-JM, PW1124G1-JM, PW1124G-JM, PW1122G-JM, PW1127G1-JM

ReplacedPartNumber:

International Aero Engines P/N 2A1226

ApprovalBasis:

Tests and Computations per 14 CFR 21.303, Dwg No. DEC47-003, Rev. - , Dated 6/11/04, or later FAA approved revisions.

Models:

V2500-A1, V2522-A5, V2524-A5, V2525-D5, V2527-A5, V2527E-A5, V2528-D5, V2530-A5, V2533-A5

ReplacedPartNumber:

International Aero Engines P/N 2A1226

ApprovalBasis:

Tests and Computations per 14 CFR 21.303, Dwg No. DEC47-003, Rev. - , Dated 6/11/04, or later FAA approved revisions.

Models:

V2500-A1, V2522-A5, V2524-A5, V2525-D5, V2527-A5, V2527E-A5, V2528-D5, V2530-A5, V2533-A5

ReplacedPartNumber:

International Aero Engines P/N 3A1819

ApprovalBasis:

Tests and Computations per 14 CFR 21.303, Dwg No. 3A1819DEC, Rev. - , Dated 10/23/14, or later FAA approved revisions.

Models:

V2500-A1, V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, V2533-A5, V2525-D5, V2528-D5

ReplacedPartNumber:

International Aero Engines P/N 2A3125-01

ApprovalBasis:

Tests and Computations per 14 CFR 21.303, Dwg No. DEC2A3125-01, Rev. H, Dated 5/5/11, or later FAA approved revisions.

Models:

V2500-A1, V2527-A5, V2530-A5, V2533-A5

ReplacedPartNumber:

International Aero Engines P/N 3A1800

ApprovalBasis:

Tests and Computations per 14 CFR 21.303, Dwg No. 3A1800DEC, Rev. A, Date 3/7/12, or later FAA approved revisions.

Models:

V2500-A1, V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, V2533-A5, V2525-D5, V2528-D5

ReplacedPartNumber:

International Aero Engines P/N 3A1822

ApprovalBasis:

Tests and Computations per 14 CFR 21.303, Dwg No. 3A1822DEC, Rev. - , Dated 10/23/14, or later FAA approved revisions.

Models:

V2500-A1, V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, V2533-A5, V2525-D5, V2528-D5

ReplacedPartNumber:

Intl. Aero Engines P/N 2A1212

ApprovalBasis:

Tests and Computations per 14 CFR 21.303, Dwg No. 2A1212DEC, Rev. B, Dated 8/29/14, or later FAA approved revisions.

Models:

V2500-A1, V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, V2533-A5, V2525-D5, V2528-D5

ReplacedPartNumber:

International Aero Engines P/N 3A1802

ApprovalBasis:

Tests and Computations per 14 CFR 21.303, Dwg No. 3A1802DEC, Rev. A, Date 3/7/12, or later FAA approved revisions.

Models:

V2500-A1, V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, V2533-A5, V2525-D5, V2528-D5

ReplacedPartNumber:

Intl. Aero Engines P/N 2A1211

ApprovalBasis:

Tests and Computations per 14 CFR 21.303, Dwg No. 2A1211DEC, Rev. B, Dated 8/29/14, or later FAA approved revisions.

Models:

V2500-A1, V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, V2533-A5, V2525-D5, V2528-D5

ReplacedPartNumber:

International Aero Engines P/N 3A1821

ApprovalBasis:

Tests and Computations per 14 CFR 21.303, Dwg No. 3A1821DEC, Rev. - , Dated 10/23/14, or later FAA approved revisions.

Models:

V2500-A1, V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, V2533-A5, V2525-D5, V2528-D5

ReplacedPartNumber:

International Aero Engines P/N 3A1801

ApprovalBasis:

Tests and Computations per 14 CFR 21.303, Dwg No. 3A1801DEC, Rev. A, Date 3/7/12, or later FAA approved revisions.

Models:

V2500-A1, V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, V2533-A5, V2525-D5, V2528-D5

ReplacedPartNumber:

Kelly Aerospace/ Hartzell Engine Technologies ALV 9510, ALV-9510L ALV-9401, ALV-9401L TCM Crittenden 642056, 646842, 646491, 649304 Textron Lycoming LW-18873

ApprovalBasis:

Test an Computation Per 14 CFR 21.303 Dwg. No. ALV-9610 Rev. C Dated. 7/23/08 or Later FAA approved revisions

Models:

IO-520-B , BA, BB, C, CB, M, MB, TSIO-520-B, BB, BE, D, DB, E, EB, J, JB, K, KB, L, LB, N, NB, U, UB, VB, WB, GTSIO-520-C, D, F, G, H, K, L, M, N, R, IO-520-A, B, C, G, N, P, R, TSIO-550-A, B, C, E, TSIOL-550-A, B, C) Beech (E55, E55A, 58, 58A) Textron Lycoming (TIGO-541-C1A, D1A, D1B, E1A, G1AD

ReplacedPartNumber:

Bendix 10-720642

ApprovalBasis:

Identicality per 14 CFR 21.303 Dwg No. 201 Rev B Dated 3/7/78 or later FAA Approved revisions

Models:

Series A-50, A-65, A-75, A-80, C-75, C-85, C-90, C-125, C-145, E-165, E-185, O200, E-225, O-300, IO-360, LTISO-360. TSIO-360, GIO-470 IO-470, O-470, TSIO-470, GTSIO-520, IO-520, LTSIO-520, TSIO-520, IO-550, TSIOL-550.) Textron Lycoming (O-235, O-290, AEIO-320, AIO-320, IO-320, LIO-320, O-320, O-340, AIO-360, AEIO-360, HIO-360, HO-360, IO-360, IVO-360, O-360, VO-360, TO-360, LTO-360, LO-360, LIO-360, GO-435, TVO-435, VO-435, O-435, GSO-480, GO-480, IGO-480, IGSO-480, O-480, IO-540 AEIO-540, LTIO-540, IGO-540, O-540, IGSO-540, VO-540, TIO-540, TIVO-540, IVO-540, VO-540, TIGO-541, TIO-541) Franklin (BIO-720. IO-720) Ward Aero Engine Applications (6A4150, 6A4165. 6A4178, 6A4200, 4A-235-B, 6A-335-A, B. 6AS-335-A, B. 6V-335-A, 6VS-335-A, B. 6A-350-C.

ReplacedPartNumber:

Modification Part (All Type Certificated Engines with an ignition lead stamped FAA Approved.)

ApprovalBasis:

Test and Computations per 21.303 Dwg No. 100, Rev E Dated 12/2/82 or later FAA approved revisions

Models:

Series TCM A-50, A-65, A-75, A-80, C-75, C-85, C-90, C-125, C-145, E-165, E-185, O200, E-225, O-300, IO-360, LTISO-360. TSIO-360, GIO-470 IO-470, O-470, TSIO-470, GTSIO-520, IO-520, LTSIO-520, TSIO-520, IO-550, TSIOL-550. Series Lycoming O-235, O-290, AEIO-320, AIO-320, IO-320, LIO-320, O-320, O-340, AIO-360, AEIO-360, HIO-360, HO-360, IO-360, IVO-360, O-360, VO-360, TO-360, LTO-360, LO-360, LIO-360, GO-435, TVO-435, VO-435, O-435, GSO-480, GO-480, IGO-480, IGSO-480, O-480, IO-540, IGO-540, O-540, VO-540, AEIO-540, VO-540, LTIO-540, TIO-540, IGSO-540, IVO-540, TIVO-540, TIO-541, TIGO-541, IO-720 BIO-720. Series Franklin 6A4150, 6A4165. 6A4178, 6A4200, 4A-235-B, 6A-335-A, B. 6AS-335-A, B. 6V-335-A, 6VS-335-A, B. 6A-350-C.

ReplacedPartNumber:

Modification Part (All Type Certificated Engines with an ignition lead stamped FAA Approved.)

ApprovalBasis:

Test and Computations per 21.303 Dwg No A9-4, Rev none, Dated 6/20/78 or later FAA approved revisions

Models:

TCM Series A-50, A-65, A-75, A-80, C-75, C-85, C-90, C-125, C-145, E-165, E-185, O200, E-225, O-300, IO-360, TSIO-360, LTISO-360. GIO-470, O-470, IO-470, TSIO-470, GTSIO-520, IO-520, LTSIO-520, TSIO-520, IO-550, TSIOL-550. LYC Series O-235, O-290, AEIO-320, IO-320, AIO-320, LIO-320, O-320, O-340, AIO-360, AEIO-360, HIO-360, HO-360, IO-360, IVO-360, VO-360, TO-360, LTO-360, O-360, LO-360, LIO-360, GO-435, TVO-435, VO-435, O-435, GSO-480, GO-480, IGO-480, IGSO-480, O-480, IO-540, AEIO-540, LTIO-540, IGO-540, O-540, IGSO-540, VO-540, TIO-540, TIVO-540, IVO-540, VO-540, TIGO-541, TIO-541, BIO-720. IO-720 Franklin Series 6A4150, 6A4165. 6A4178, 6A4200, 4A-235-B, 6A-335-A, B. 6AS-335-A, B. 6V-335-A, 6VS-335-A, B. 6A-350-C.

ReplacedPartNumber:

Modification Part (All Type Certificated Engines with an ignition lead stamped FAA Approved.)

ApprovalBasis:

Test and Computations per 21.303 Dwg No. 103, Rev B Dated 3/7/78 or later FAA approved revisions

Models:

Series TCM A-50, A-65, A-75, A-80, C-75, C-85, C-90, C-125, C-145, E-165, E-185, O200, E-225, O-300, IO-360, LTISO-360. TSIO-360, GIO-470 IO-470, O-470, TSIO-470, GTSIO-520, IO-520, LTSIO-520, TSIO-520, IO-550, TSIOL-550. Series Lycoming O-235, O-290, AEIO-320, AIO-320, IO-320, LIO-320, O-320, O-340, AIO-360, AEIO-360, HIO-360, HO-360, IO-360, IVO-360, O-360, VO-360, TO-360, LTO-360, LO-360, LIO-360, GO-435, TVO-435, VO-435, O-435, GSO-480, GO-480, IGO-480, IGSO-480, O-480, IO-540 AEIO-540, LTIO-540, IGO-540, O-540, IGSO-540, VO-540, TIO-540, TIVO-540, IVO-540, VO-540, TIGO-541, TIO-541, BIO-720. IO-720 Series Franklin 6A4150, 6A4165. 6A4178, 6A4200, 4A-235-B, 6A-335-A, B. 6AS-335-A, B. 6V-335-A, 6VS-335-A, B. 6A-350-C.

ReplacedPartNumber:

Bendix 10-720642 Ward Aero 200-[ ]

ApprovalBasis:

Identicality per 14 CFR 21.303 Dwg No. 200 Rev E Dated 12/2/82 or later FAA Approved revisions

Models:

Series A-50, A-65, A-75, A-80, C-75, C-85, C-90, C-125, C-145, E-165, E-185, O200, E-225, O-300, IO-360, LTISO-360. TSIO-360, GIO-470 IO-470, O-470, TSIO-470, GTSIO-520, IO-520, LTSIO-520, TSIO-520, IO-550, TSIOL-550.) Textron Lycoming (O-235, O-290, AEIO-320, AIO-320, IO-320, LIO-320, O-320, O-340, AIO-360, AEIO-360, HIO-360, HO-360, IO-360, IVO-360, O-360, VO-360, TO-360, LTO-360, LO-360, LIO-360, GO-435, TVO-435, VO-435, O-435, GSO-480, GO-480, IGO-480, IGSO-480, O-480, IO-540 AEIO-540, LTIO-540, IGO-540, O-540, IGSO-540, VO-540, TIO-540, TIVO-540, IVO-540, VO-540, TIGO-541, TIO-541) Franklin (BIO-720. IO-720) Ward Aero Engine Applications (6A4150, 6A4165. 6A4178, 6A4200, 4A-235-B, 6A-335-A, B. 6AS-335-A, B. 6V-335-A, 6VS-335-A, B. 6A-350-C.

ReplacedPartNumber:

Bendix 10-720643 (If used for Bendix P/N 10-163048 with S20, S200, S1200, D2000, D3000 series magneto.)

ApprovalBasis:

Identicality per 14 CFR 21.303 Dwg No. 102 Rev B Dated 3/7/78 or later FAA Approved revisions

Models:

Series A-50, A-65, A-75, A-80, C-75, C-85, C-90, C-125, C-145, E-165, E-185, O200, E-225, O-300, IO-360, LTISO-360. TSIO-360, GIO-470 IO-470, O-470, TSIO-470, GTSIO-520, IO-520, LTSIO-520, TSIO-520, IO-550, TSIOL-550.) Textron Lycoming (O-235, O-290, AEIO-320, AIO-320, IO-320, LIO-320, O-320, O-340, AIO-360, AEIO-360, HIO-360, HO-360, IO-360, IVO-360, O-360, VO-360, TO-360, LTO-360, LO-360, LIO-360, GO-435, TVO-435, VO-435, O-435, GSO-480, GO-480, IGO-480, IGSO-480, O-480, IO-540 AEIO-540, LTIO-540, IGO-540, O-540, IGSO-540, VO-540, TIO-540, TIVO-540, IVO-540, VO-540, TIGO-541, TIO-541) Franklin (BIO-720. IO-720) Ward Aero Engine Applications (6A4150, 6A4165. 6A4178, 6A4200, 4A-235-B, 6A-335-A, B. 6AS-335-A, B. 6V-335-A, 6VS-335-A, B. 6A-350-C.

ReplacedPartNumber:

Bendix 10-720643

ApprovalBasis:

Identicality per 14 CFR 21.303 Dwg No. 104 Rev B Dated 3/7/78 or later FAA Approved revisions

Models:

Series A-50, A-65, A-75, A-80, C-75, C-85, C-90, C-125, C-145, E-165, E-185, O200, E-225, O-300, IO-360, LTISO-360. TSIO-360, GIO-470 IO-470, O-470, TSIO-470, GTSIO-520, IO-520, LTSIO-520, TSIO-520, IO-550, TSIOL-550.) Textron Lycoming (O-235, O-290, AEIO-320, AIO-320, IO-320, LIO-320, O-320, O-340, AIO-360, AEIO-360, HIO-360, HO-360, IO-360, IVO-360, O-360, VO-360, TO-360, LTO-360, LO-360, LIO-360, GO-435, TVO-435, VO-435, O-435, GSO-480, GO-480, IGO-480, IGSO-480, O-480, IO-540 AEIO-540, LTIO-540, IGO-540, O-540, IGSO-540, VO-540, TIO-540, TIVO-540, IVO-540, VO-540, TIGO-541, TIO-541) Franklin (BIO-720. IO-720) Ward Aero Engine Applications same as above (6A4150, 6A4165. 6A4178, 6A4200, 4A-235-B, 6A-335-A, B. 6AS-335-A, B. 6V-335-A, 6VS-335-A, B. 6A-350-C.

ReplacedPartNumber:

Modification Part (All Type Certificated Engines with an ignition lead stamped FAA Approved.)

ApprovalBasis:

Test and Computations per 21.303 Dwg No. 102, Rev B Dated 3/7/78 or later FAA approved revisions

Models:

Series TCM A-50, A-65, A-75, A-80, C-75, C-85, C-90, C-125, C-145, E-165, E-185, O200, E-225, O-300, IO-360, LTISO-360. TSIO-360, GIO-470 IO-470, O-470, TSIO-470, GTSIO-520, IO-520, LTSIO-520, TSIO-520, IO-550, TSIOL-550. Series Lycoming O-235, O-290, AEIO-320, AIO-320, IO-320, LIO-320, O-320, O-340, AIO-360, AEIO-360, HIO-360, HO-360, IO-360, IVO-360, O-360, VO-360, TO-360, LTO-360, LO-360, LIO-360, GO-435, TVO-435, VO-435, O-435, GSO-480, GO-480, IGO-480, IGSO-480, O-480, IO-540 AEIO-540, LTIO-540, IGO-540, O-540, IGSO-540, VO-540, TIO-540, TIVO-540, IVO-540, VO-540, TIGO-541, TIO-541, IO-720 BIO-720. Series Franklin 6A4150, 6A4165. 6A4178, 6A4200, 4A-235-B, 6A-335-A, B. 6AS-335-A, B. 6V-335-A, 6VS-335-A, B. 6A-350-C.

ReplacedPartNumber:

Bendix 10-720641 & 10-720643

ApprovalBasis:

Identicality per 14 CFR 21.303 Dwg No. 100 Rev E Dated 12/2/82 or later FAA Approved revisions

Models:

Series A-50, A-65, A-75, A-80, C-75, C-85, C-90, C-125, C-145, E-165, E-185, O200, E-225, O-300, IO-360, LTISO-360. TSIO-360, GIO-470 IO-470, O-470, TSIO-470, GTSIO-520, IO-520, LTSIO-520, TSIO-520, IO-550, TSIOL-550.) Textron Lycoming (O-235, O-290, AEIO-320, AIO-320, IO-320, LIO-320, O-320, O-340, AIO-360, AEIO-360, HIO-360, HO-360, IO-360, IVO-360, O-360, VO-360, TO-360, LTO-360, LO-360, LIO-360, GO-435, TVO-435, VO-435, O-435, GSO-480, GO-480, IGO-480, IGSO-480, O-480, IO-540 AEIO-540, LTIO-540, IGO-540, O-540, IGSO-540, VO-540, TIO-540, TIVO-540, IVO-540, VO-540, TIGO-541, TIO-541) Franklin (BIO-720. IO-720) Ward Aero Engine Applications (6A4150, 6A4165. 6A4178, 6A4200, 4A-235-B, 6A-335-A, B. 6AS-335-A, B. 6V-335-A, 6VS-335-A, B. 6A-350-C.

ReplacedPartNumber:

Modification. Part (All Type Certificated Engines with an ignition lead stamped FAA Approved.)

ApprovalBasis:

Test and Computations per 21.303 Dwg No Q-2 Rev none Dated 6/20/78 or later FAA approved revisions

Models:

Series TCM A-50, A-65, A-75, A-80, C-75, C-85, C-90, C-125, C-145, E-165, E-185, O200, E-225, O-300, IO-360, LTISO-360. TSIO-360, GIO-470 IO-470, O-470, TSIO-470, GTSIO-520, IO-520, LTSIO-520, TSIO-520, IO-550, TSIOL-550. Series Lycoming O-235, O-290, AEIO-320, AIO-320, IO-320, LIO-320, O-320, O-340, AIO-360, AEIO-360, HIO-360, HO-360, IO-360, IVO-360, O-360, VO-360, TO-360, LTO-360, LO-360, LIO-360, GO-435, TVO-435, VO-435, O-435, GSO-480, GO-480, IGO-480, IGSO-480, O-480, IO-540 AEIO-540, LTIO-540, IGO-540, O-540, IGSO-540, VO-540, TIO-540, TIVO-540, IVO-540, VO-540, TIGO-541, TIO-541, BIO-720. IO-720 Series Franklin 6A4150, 6A4165. 6A4178, 6A4200, 4A-235-B, 6A-335-A, B. 6AS-335-A, B. 6V-335-A, 6VS-335-A, B. 6A-350-C.

ReplacedPartNumber:

Bendix 10-720643

ApprovalBasis:

Identicality per 14 CFR 21.303 Dwg No. 103 Rev B Dated 3/7/78 or later FAA Approved revisions

Models:

Series A-50, A-65, A-75, A-80, C-75, C-85, C-90, C-125, C-145, E-165, E-185, O200, E-225, O-300, IO-360, LTISO-360. TSIO-360, GIO-470 IO-470, O-470, TSIO-470, GTSIO-520, IO-520, LTSIO-520, TSIO-520, IO-550, TSIOL-550.) Textron Lycoming (O-235, O-290, AEIO-320, AIO-320, IO-320, LIO-320, O-320, O-340, AIO-360, AEIO-360, HIO-360, HO-360, IO-360, IVO-360, O-360, VO-360, TO-360, LTO-360, LO-360, LIO-360, GO-435, TVO-435, VO-435, O-435, GSO-480, GO-480, IGO-480, IGSO-480, O-480, IO-540 AEIO-540, LTIO-540, IGO-540, O-540, IGSO-540, VO-540, TIO-540, TIVO-540, IVO-540, VO-540, TIGO-541, TIO-541) Franklin (BIO-720. IO-720) Ward Aero Engine Applications (6A4150, 6A4165. 6A4178, 6A4200, 4A-235-B, 6A-335-A, B. 6AS-335-A, B. 6V-335-A, 6VS-335-A, B. 6A-350-C.

ReplacedPartNumber:

Elsinore Engineering, Inc. Smoke Detector P/N 100-0649-01

ApprovalBasis:

STC ST00511LA and Licensing Agreement between Securaplane Technologies LLC and Hollingsead International Inc. dated 11/24/98

Models:

737-300

ReplacedPartNumber:

Elsinore Engineering, Inc. Identification Plug P/N 100-1026-01

ApprovalBasis:

STC ST00511LA and Licensing Agreement between Securaplane Technologies LLC and Hollingsead International Inc. dated 11/24/98.

Models:

737-300

ReplacedPartNumber:

Elsinore Engineering, Inc. Identification Plug P/N 100-1026-02

ApprovalBasis:

STC ST00388LA-D and Licensing Agreement between Securaplane Technologies LLC and Hollingsead International, Inc. dated 9/28/98

Models:

737-300

ReplacedPartNumber:

Elsinore Engineering, Inc. Configuration Module P/N 100-1024-01

ApprovalBasis:

STC ST00511LA and Licensing Agreement between Securaplane Technologies, LLC and Hollingsead International, Inc. dated 11/24/98

Models:

737-300

ReplacedPartNumber:

Elsinore Engineering, Inc. Smoke Detector P/N 100-0649-01

ApprovalBasis:

STC ST00511LA and Licensing agreement between Securaplane Technologies, LLC and Hollingsead International, Inc. dated 9/28/98

Models:

737-300

ReplacedPartNumber:

Elsinore Engineering, Inc. Identification Plug P/N 100-1026-01

ApprovalBasis:

STC ST00388LA and Licensing Agreement between Securaplane Technologies LLC and Hollingsead International Inc. dated 9/28/98

Models:

737-300

ReplacedPartNumber:

Elsinore Engineering, Inc. Control Display Unit P/N 100-0120-01

ApprovalBasis:

STC ST00511LA and Licensing Agreement between Securaplane Technologies, LLC and Hollingsead International, Inc. dated 11/24/98

Models:

737-300

ReplacedPartNumber:

Elsinore Engineering, Inc. Suppressant Control Unit P/N 100-1019-01

ApprovalBasis:

STC ST00511LA and Licensing Agreement between Securaplane Technologies, LLC and Hollingsead International, Inc. dated 11/24/98

Models:

737-300

ReplacedPartNumber:

Elsinore Engineering, Inc. Central Control Unit P/N 100-0127-01

ApprovalBasis:

STC ST00511LA and Licensing Agreement between Securaplane Technologies LLC and Hollingsead International, Inc. dated 11/24/98

Models:

737-300

ReplacedPartNumber:

Elsinore Engineering, Inc. Identification Plug P/N 100-1026-02

ApprovalBasis:

STC ST00511LA and Licensing Agreement between Securaplane Technologies LLC and Hollingsead International, Inc. dated 11/24/98

Models:

737-300

ReplacedPartNumber:

International Aero Engines LLC p/n 5314333

ApprovalBasis:

Identicality per 14 CFR Sec. 21.303 (c), licensing agreement between Crane Lear Romec and International Aero Engine LLC Dwg. No. 5314333 Rev. No Revision Date 9/19/2013 or later FAA Approved Revision.

Models:

International Aero Engines, LLC PW1133G-JM Series Engine(s)

ReplacedPartNumber:

International Aero Engines LLC p/n 5323065

ApprovalBasis:

Identicality per 14 CFR Sec. 21.303 (c), licensing agreement between Crane Lear Romec and International Aero Engine LLC Dwg. No. 5323065 Rev. No Revision Date 9/19/2013 or later FAA Approved Revision.

Models:

International Aero Engines, LLC PW1133G-JM Series Engine(s)

ReplacedPartNumber:

Dynamic Air Engineering 420A20

ApprovalBasis:

Test and Computation per 14 CFR, 21.303, DWG No. TR-420A20 Rev - Date January 21, 2015 Or later FAA approved revisions

Models:

65-90, 200) British Aerospace (Jetstream 3101

ReplacedPartNumber:

International Aero Engines P/N 6B1137

ApprovalBasis:

Tests and Computations per 14 CFR 21.303, Dwg No. JA6B1137, Rev. B, Dated 2014/01/14, or later FAA approved revisions.

Models:

V2500-A1, V2522-A5, V2524-A5, V2527-A5, V2533-A5, V2527E-A5, V2527M-A5, V2530-A5, V2525-D5, V2528-D5

ReplacedPartNumber:

International Aero Engines P/N 3A1819

ApprovalBasis:

Tests and Computations per 14 CFR 21.303, Dwg No. 3A1819DEC, Rev. - , Dated 10/23/14, or later FAA approved revisions.

Models:

V2500-A1, V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, V2533-A5, V2525-D5, V2528-D5

ReplacedPartNumber:

International Aero Engines P/N 3A1822

ApprovalBasis:

Tests and Computations per 14 CFR 21.303, Dwg No. 3A1822DEC, Rev. - , Dated 10/23/14, or later FAA approved revisions.

Models:

V2500-A1, V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, V2533-A5, V2525-D5, V2528-D5

ReplacedPartNumber:

International Aero Engines P/N 6B1336

ApprovalBasis:

Tests and Computations per 14 CFR 21.303, Dwg No. JA6B133-01, Rev. - , Dated 2013/06/28, or later FAA approved revisions.

Models:

V2522-A5, V2524-A5, V2527-A5, V2533-A5, V2527E-A5, V2527M-A5, V2530-A5, V2525-D5, V2528-D5

ReplacedPartNumber:

International Aero Engines P/N 3A1821

ApprovalBasis:

Tests and Computations per 14 CFR 21.303, Dwg No. 3A1821DEC, Rev. - , Dated 10/23/14, or later FAA approved revisions.

Models:

V2500-A1, V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, V2533-A5, V2525-D5, V2528-D5

ReplacedPartNumber:

International Aero Engines P/N 6B1334

ApprovalBasis:

Tests and Computations per 14 CFR 21.303, Dwg No. JA6B133-01, Rev. - , Dated 2013/06/28, or later FAA approved revisions.

Models:

V2522-A5, V2524-A5, V2527-A5, V2533-A5, V2527E-A5, V2527M-A5, V2530-A5, V2525-D5, V2528-D5

ReplacedPartNumber:

International Aero Engines P/N 6B1333

ApprovalBasis:

Tests and Computations per 14 CFR 21.303, Dwg No. JA6B133-01, Rev. - , Dated 2013/06/28, or later FAA approved revisions.

Models:

V2522-A5, V2524-A5, V2527-A5, V2533-A5, V2527E-A5, V2527M-A5, V2530-A5, V2525-D5, V2528-D5

ReplacedPartNumber:

International Aero Engines P/N 2A2256

ApprovalBasis:

Tests and Computations per 14 CFR 21.303, Dwg No. M2A2256, Rev. N/C, Dated 2013/07/23, or later FAA approved revisions.

Models:

V2500-A1, V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, V2533-A5, V2525-D5, V2528-D5

ReplacedPartNumber:

Clinton Engines Corp. 12030 Eaton Corp. R15287

ApprovalBasis:

Test and Computation per 14 CFR, 21.303, DWG No. TR-R15287, Rev - Date February 14, 2013 Or later FAA approved revisions

Models:

65-A80, 65-90, 65-A90, B90, C90, C90A, C90GT, E90, F90, C99, 100, A100, B100, A200 (C-12C), A200(UC-12B), B200C(UC-12F), A200CT(C-12D), A200CT(C-12F), B200C(UC-12M), B200C(C-12F), B200, B200T, B200C, B200CT, 300, 300LW, B300, B300C

ReplacedPartNumber:

974710-1 Used on engine P/N 2704506-1, 2704506-2

ApprovalBasis:

Test and Computation per 14 CFR 21.303 DWG No 3-684-700 Rev None Date 03/02/2009 or later FAA-approved revisions

Models:

MD-90-30) Airbus (A319 Model -111, A319 Model -112, A319 Model -113, A319 Model -114, A319 Model -115, A319 Model -131, A319 Model -132, A319 Model -133, A320 Model -111, A320 Model -211, A320 Model -212, A320 Model -214, A320 Model -231, A320 Model -232, A320 Model -233, A321 Model -111, A321 Model -112, A321 Model -131, A321 Model -211, A321 Model -231, A321 Model -21, A321 Model -213, A321 Model -232) Airbus (A319 Model -111, A319 Model -112, A319 Model -113, A319 Model -114, A319 Model -115, A319 Model -131, A319 Model -132, A319 Model -133, A320 Model -111, A320 Model -211, A320 Model -212, A320 Model -214, A320 Model -231, A320 Model -232, A320 Model -233, A321 Model -111, A321 Model -112, A321 Model -131, A321 Model -211, A321 Model -231, A321 Model -212, A321 Model -213, A321 Model -232

ReplacedPartNumber:

974710-1 Used on engine P/N 2704482-2, 2704482-3

ApprovalBasis:

Test and Computation per 14 CFR 21.303 DWG No 3-684-700 Rev None Date 03/02/2009 or later FAA-approved revisions

Models:

MD-90-30

ReplacedPartNumber:

Clinton Engines Corp. 12030, Eaton Corp. R15287

ApprovalBasis:

Test and Computation per 14 CFR 21.303, DWG. No. TR-R15287, Rev. - Date February 14, 2013 Or later FAA approved revisions

Models:

65-A80, 65-90, 65-A90, B90, C90, C90A, C90GT, E90, F90, C99, 100, A100, B100, A200 (C-12C), A200(UC-12B) B200C(UC-12F), A200CT(C-12D), A200CT(C-12F), B200C(UC-12M), B200C(C-12F), B200, B200T, B200C, B200CT, 300, 300LW, B300, B300C

ReplacedPartNumber:

Clinton Engines Corp. 12030, Eaton Corp. R15287

ApprovalBasis:

Test and Computation per 14 CFR 21.303, DWG. No. TR-R15287, Rev. - Date February 14, 2013 Or later FAA approved revisions

Models:

65-A80, 65-90, 65-A90, B90, C90, C90A, C90GT, E90, F90, C99, 100, A100, B100, A200 (C-12C), A200(UC-12B) B200C(UC-12F), A200CT(C-12D), A200CT(C-12F), B200C(UC-12M), B200C(C-12F), B200, B200T, B200C, B200CT, 300, 300LW, B300, B300C

ReplacedPartNumber:

Clinton Engines Corp. 12030, Eaton Corp. R15287

ApprovalBasis:

Test and Computation per 14 CFR 21.303, DWG. No. TR-R15287, Rev. - Date February 14, 2013 Or later FAA approved revisions

Models:

65-A80, 65-90, 65-A90, B90, C90, C90A, C90GT, E90, F90, C99, 100, A100, B100, A200 (C-12C), A200(UC-12B), B200C(UC-12F), A200CT(C-12D), A200CT(C-12F), B200C(UC-12M), B200C(C-12F), B200, B200T, B200C, B200CT, 300, 300LW, B300, B300C

ReplacedPartNumber:

Honeywell P/N 515203-1 Installed in NHA Motor - Engine Starter

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No. P01190 Rev. A Date 01/30/2014 or later FAA-approved revisions

Models:

A300, Model B4-603, A300, Model B4-605R, A300, Model B4-620, A310, Model 204, A310, Model 222, A310, Model 304, A310, Model 322, A310, Model 324, A310, Model 325) Boeing (757-200 Series, 767-200 Series, 767-300 Series, 767-400ER Series

ReplacedPartNumber:

Honeywell P/N 515203-2 Installed in NHA Motor - Engine Starter

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No. P01191 Rev. A Date 01/30/2014 or later FAA-approved revisions

Models:

A300, Model B4-603, A300, Model B4-605R, A300, Model B4-620, A310, Model 204, A310, Model 222, A310, Model 304, A310, Model 322, A310, Model 324, A310, Model 325) Boeing (757-200 Series, 767-200 Series, 767-300 Series, 767-400ER Series

ReplacedPartNumber:

Intl. Aero Engines P/N 2A1212

ApprovalBasis:

Tests and Computations per 14 CFR 21.303, Dwg No. 2A1212DEC, Rev. A, Dated 09/18/12, or later FAA approved revisions.

Models:

V2525-D5, V2528-D5

ReplacedPartNumber:

Intl. Aero Engines P/N 2A1211

ApprovalBasis:

Tests and Computations per 14 CFR 21.303, Dwg No. 2A1211DEC, Rev. - , Dated 12/22/11, or later FAA approved revisions.

Models:

V2525-D5, V2528-D5

ReplacedPartNumber:

Woodward Governor P/N 1039-754 installed in Main Engine Control P/Ns

ApprovalBasis:

Test and Computations per 14 CFR 21.303 DWG No. P01172 Rev. NC Date 06/18/2013 or later FAA approved revisions

Models:

737-300 Series, 737-400 Series, 737-500 Series

ReplacedPartNumber:

International Aero Engines P/N 14155-00

ApprovalBasis:

Tests and Computations per 14 CFR 21.303, Dwg No. JA14155-00, Rev. - , Dated 2013/03/27, or later FAA approved revisions.

Models:

V2525-D5, V2528-D5) Boeing (MD-90-30