FSC 4920 Aircraft Maintenance and Repair Shop Specialized Equipment: 4920-01-331-4214, 4920-01-331-5034, 4920-01-331-9092

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NSNMFG SKUItem NameDetailsManufacturer (CAGE)RFQ
4920-01-331-4214
4920013314214
2427923-2Simulator Three LruRaytheon Company (96214)

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4920-01-331-4591
4920013314591
LMT-539-4971Fixture, Aircraft MaintenanceGE Aviation Systems LLC (35351)

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4920-01-331-4838
4920013314838
K410A18007Adapter kit, TestSpecial Features: C/O gearbox adapter plate, P/N D21397; adapter tube, P/N B17578; adapter tube, P/N 17579; charge pressure fitting, P/N 434918; test cable assemblies, P/N C16042 and C17390; power cable, P/N B16701; spline adapter plug, P/N B20891; hose, P/N B15328; hose, P/N B15330; hose, P/N B15332; associate equipment listed in serd no. 42600, test stand, generator
Functional Description: Used to provide the electrical connections between the slave generator, P/N 977J330, and the, test stand control console
End Item Identification: F-16C/D constant speed drive
Avtron Aerospace Inc. (01014)

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4920-01-331-4867
4920013314867
506T738-03Adapter Assembly, Interface DevicSpecial Features: Brass; 3.250 in. L, 1.000 dia
Functional Description: Used to isolate primary passabe duringpreassy flow test
End Item Identification: F108-GE-100 engine
CFM International Inc. (58828)

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4920-01-331-5034
4920013315034
2353256-1Support, Aircraft, MaRaytheon Company (96214)

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4920-01-331-5436
4920013315436
717751363-219Target AlignmentEnd Item Identification: Lantirn mobility shelter test station
Reference Data and Literature: Martin marietta drawing 717751363
FSC Application Data: Target wheel assembly
Lockheed Martin Corporation (04939)

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4920-01-331-5437
4920013315437
717751363-199Target OpticalEnd Item Identification: Lantirn mobility shelter test station
Reference Data and Literature: Martin marietta drawing no. 717751363
FSC Application Data: Target wheel assembly
Lockheed Martin Corporation (04939)

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4920-01-331-5606
4920013315606
1128SAV49400-3Test Station, Electrical-ElectronNorthrop Grumman Systems Corporation (26512)

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4920-01-331-6230
4920013316230
MX-11443/ALM-206B
150-033987-001
Adapter, TestFunctional Description: Used at depot lvl in testing of the converter input/output circuit card assembly
End Item Identification: AN/ALR-56 se; AN/ALM-246
Reference Data and Literature: Northrup serd no. I51 AGAVGF-15 internal countermeasures system
Joint Electronics Type Designation (80058)
Northrop Grumman Systems Corporation (26916)

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4920-01-331-6237
4920013316237
68D040319-1001
68D040319-1003
Case, Test setSpecial Features: Weight: empty 525 lbs and 915 lbs full
End Item Identification: F-15 acft tacical intermediate support system
Width: 48.000 inches nominal
Boeing Company,, The (76301)

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4920-01-331-6900
4920013316900
T425483
3C3006P03
Fixture, Aircraft MaintenanceEnd Item Identification: Pacer special
Eaton Aerospace LLC (62983)
General Electric Company (07482)

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4920-01-331-6901
4920013316901
PWA70408Fixture, Engine Maintenance, AircrFunctional Description: Lused to pressure test the fan inlet case PS2 pressure tube and outer fitting subassembly and full tube assembly after braze assembly in case; test with air at 50-55 psig; is used with PWA21875 pressure regulator
End Item Identification: F100-PW-220 engine
Reference Data and Literature: Serd no. 6313; T.O. 2J-F100-94
United Technologies Corporation (77445)

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4920-01-331-7476
4920013317476
10046059-102Test Program setEnd Item Identification: F-15A/B/C/D/E acft age
Supplementary Features: Company name-test package, analog modules
Honeywell International Inc. (94580)

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4920-01-331-7877
4920013317877
299-1022-001Adapter set, TestEnd Item Identification: B-1B OSE13C68C
Technology Development Corp. (58570)

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4920-01-331-7944
4920013317944
42277-728Fixture, Aircraft MaintenanceEnd Item Identification: H-60 helicopter
Reference Data and Literature: T.M. 55-1680-320-23 & P
Triumph Gear Systems Inc. (82402)
Goodrich Corporation (00462)

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4920-01-331-7945
4920013317945
328500TF1-1001Fixture, Aircraft MaintenanceSpecial Features: Size is approximately 3 feet long by 3 feet wide by 2 feet high; weighsapproximately 200 pounds; material is steel and aluminum
Functional Description: The fixture holds the integrated flight control module firmly in place while simulating the aircraft response using a dedicated actuator during bench tests and post maintenance tests; this fixture holds the integrated flight control module and then the integrated flight control module is connected to the electrical test console and the hydraulic test stand
End Item Identification: C-17 aircraft
Parker-Hannifin Corporation (82106)

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4920-01-331-7946
4920013317946
T-449041Fixture, Aircraft MaintenanceSpecial Features: Item is considered a non-complex item per MIL-STD-490; data will meet the requirement of a type B3 specification
Functional Description: The fixture provides a means to postion the ac motor pump for repair
End Item Identification: Ac motor pumps, 693640, on the C-17A acft
Eaton Aerospace LLC (62983)

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4920-01-331-8448
4920013318448
GS21692-1Fixture, Engine Maintenance, AircrSpecial Features: 4.440 in. O.D.; 3.440 in. I.D.
Functional Description: Used to support the impeller during shimming process
End Item Identification: F100-PW-229 turbofan engine
Hamilton Sundstrand Corporation (73030)

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4920-01-331-8449
4920013318449
GS21690-1Support, Bearing HousingFunctional Description: Used to support the bearing housing during assembly/disassembly
End Item Identification: F100-PW-229 turbofan engine
Reference Data and Literature: Pratt whitney serd no. 5718
Hamilton Sundstrand Corporation (73030)

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4920-01-331-9092
4920013319092
2455343-1Test set Sub BaseRaytheon Company (96214)

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