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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
Manufacturer: Tempest Aero Group®
Weight: 0.333000 kg
Manufacturer: McFarlane Aviation, Inc
Weight: 0.272155 kg