FSC 4920 Aircraft Maintenance and Repair Shop Specialized Equipment: 4920-01-020-8639, 4920-01-020-9965, 4920-01-021-0520

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NSNMFG SKUItem NameDetailsManufacturer (CAGE)RFQ
4920-01-020-8639
4920010208639
PWA52881Fixture, Engine Maintenance, AircrSpecial Features: Company item name-base
Functional Description: Used to install combustion chamber on base during various weld operations
End Item Identification: F100-PW-100/200 engine
United Technologies Corporation (77445)

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4920-01-020-8640
4920010208640
PWA52893Fixture, Engine Maintenance, AircrFunctional Description: Used to position combustion chamber on fixture W/aft end down
End Item Identification: F100-PW-100/200/220 aircraft engine
Reference Data and Literature: Serd no. 2545; T.O. 2J-F100-94
United Technologies Corporation (77445)

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4920-01-020-8641
4920010208641
PWA52895Fixture, Engine Maintenance, AircrSpecial Features: Circular configuration
Functional Description: Used to install combustion chamber in fixture and machine weld brackets assy to combustion chamber after the tack welding operation
Reference Data and Literature: T.O. 2J-F100-94
United Technologies Corporation (77445)

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4920-01-020-8765
4920010208765
204-91710
204-91710-1
Adapter, TestTest Item Connection Method: Electric cable assy
FSC Application Data: Test set, electronic systems, specialy designed, acft
Functional Classification: AA-12.11
The Boeing Company (81205)

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4920-01-020-8766
4920010208766
204-91924-1Adapter, TestSpecial Features: Contains a breakout box with test jacks and an interface cable and connector for mating with the unit under test
Functional Description: Used for breaking out signals at the test connector of the series yaw damper coupler, part of the E-3A aircraft automatic flight control system
End Item Identification: E-3A aircraft
The Boeing Company (81205)

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4920-01-020-8767
4920010208767
204-91925-1Adapter, TestSpecial Features: Contains a breakout box with test jacks and an interface cable and connector for mating with the unit under test
Functional Description: Used for breaking out signals at the test connector of the parallel yaw damper coupler, part of the E-3A aircraft automatic flight control system
End Item Identification: E-3A aircraft
The Boeing Company (81205)

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4920-01-020-9952
4920010209952
PWA37246Fixture, Aircraft MaintenanceSpecial Features: Matl: steel
Nominal Overall Height: 5.000 inches
Nominal Overall Diameter: 16.000 inches
United Technologies Corporation (77445)

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4920-01-020-9955
4920010209955
FAB12-35S6Gage, Strain, Test setGeneral Characteristics Item Description: Phenolic-glass
Vishay BLH Inc. (03089)

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4920-01-020-9964
4920010209964
204-90095-1Adapter, TestSpecial Features: Contains a 28VDC power cable, a cable for mating with relay assembly test connector, and a four-section connector for mating with connector on back of relay assembly
Functional Description: Used to fault isolate relay assembly RE1101/A
End Item Identification: E-3A aircraft
The Boeing Company (81205)

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4920-01-020-9965
4920010209965
90018Test set, IndicatorFunctional Description: For laboratory calibration on and acceptance testing of kratos (CAPTIN/5) series transmitter/indicator sys
Reference Data and Literature: T.O. 33D2-6-229-1
Test Type for Which Designed: Operational
Rogerson Kratos (34830)

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4920-01-020-9966
4920010209966
204-91957-1Adapter, cable BreakoutEnd Item Identification: E-3A awacs acft age
The Boeing Company (81205)

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4920-01-020-9970
4920010209970
21C5469G01Adapter Assembly, Interface DevicSpecial Features: To name: shaft assembly, pivot engine; 27 lbs
End Item Identification: TF34-GE-100A engine
Reference Data and Literature: To 2J-TF34-4
General Electric Company (07482)

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4920-01-020-9972
4920010209972
21C5460G03Stand, Maintenance, Aircraft EnginSpecial Features: To name: stand, buildup; 5 ft lg, 5 ft W, 2 ft H
End Item Identification: TF34-GE-100A engine
Reference Data and Literature: To 2J-TF34-4
General Electric Company (07482)

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4920-01-020-9978
4920010209978
PWA53361A
PWA53361
Fixture, Engine Maintenance, AircrSpecial Features: Company item name-adapter
Functional Description: Used on no. 5 bearing seal plate retaining nut
End Item Identification: F100-PW-100/200/220/220E/229 aircraft engine
United Technologies Corporation (77445)

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4920-01-020-9979
4920010209979
103-2041-7Arm, Transducer InstallationEnd Item Identification: 4920005089135
Atec Inc. (09552)

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4920-01-021-0102
4920010210102
PWA53655Drift, Pulley Assembly Bearing ReSpecial Features: Company item name-drift, pulley assembly bearing removal
End Item Identification: F100-PW-100/200/220/220E/229 aircraft engine
Reference Data and Literature: Serd no. 2958; T.O. 2J-F100-94; 33D4-6-573-1
United Technologies Corporation (77445)

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4920-01-021-0103
4920010210103
PWA53716Adapter Assembly, Interface DevicFunctional Description: Used as a tube-pressure test adapter
End Item Identification: F100-PW-100/200/220 engine
Reference Data and Literature: Serd no. 2961
United Technologies Corporation (77445)

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4920-01-021-0105
4920010210105
PWA53516Fixture, Engine Maintenance, AircrSpecial Features: Drawing name setter, gage; used to set gages PWA16246 and PWA17113 which are used to check the 7TH stage compressor stator replacement vane angle after vane has been tackwelded in position
Functional Description: Used during aircraft engine component repair/maintenance
End Item Identification: F100-PW-100/200/220 engine
United Technologies Corporation (77445)

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4920-01-021-0434
4920010210434
D7300Test Stand, Hydraulic System CompSpecial Features: Welded steel; trailer mounted mobile testing unit for acft hydraulic systems; pneumatic pressure: 3 cfm at 150 psi; hydraulic pressure 0-30 gmp at 3000 psi
Reference Data and Literature: T.O. 33A2-2-27-21
Functional Classification: GG-5.3
Hannon Company, The (06455)

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4920-01-021-0520
4920010210520
803AS500-1Control cab AssemblNaval Air Systems Command (30003)
Wilson Machine Co. Inc. (22392)

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