FSC 4920 Aircraft Maintenance and Repair Shop Specialized Equipment: 4920-01-335-5837, 4920-01-335-8527, 4920-01-335-9705
| NSN | MFG SKU | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 4920-01-335-5837 4920013355837 | A05G0576-1 | Test set, Stores Management Subsy | Functional Description: Used in weapons release shop to perform electrical continuity and fault isolation tests End Item Identification: LAU-114, LAU-106 missle launchers; ADU-407 launched adapter; SUU-59, SUU-60 pylons; MAU-12 bomb racks Reference Data and Literature: Serd no. 8655S | Boeing Company, The (0PXV4) McDonnell Douglas Corp. (12464) | |
| 4920-01-335-5838 4920013355838 | A05G0575-1 | Test set, Preload Armament Circui | Special Features: Provides on a single station basis, the capability to perform preload electrical and stray voltage checks End Item Identification: In support of the F-15 acft Reference Data and Literature: Serd no. 8656S | McDonnell Douglas Corp. (12464) | |
| 4920-01-335-5852 4920013355852 | 16A24498L1-1 | Flushing kit | End Item Identification: F-16A/B/C/D acft age. Reference Data and Literature: Serd no. 24498 General Characteristics Item Description: Used to purge and flush hydrazine from components of the turbine power test system (from the H-70 supply line between the epu fuel tank disconnect and the three way fuel valve); includes a pressurized water reservior, a holding tank, a pressure regulator, and supply hoses and return lines with fittings | Lockheed Martin Corporation (81755) | |
| 4920-01-335-6029 4920013356029 | 3C3782G02 | Fixture, Aircraft Maintenance | Special Features: 10.000 in. by 12.000 in. by 3.000 in.; 18 lbs; C/O a bracket and separate coupling adapter of steel construction; bracket has two dowel pins that fit thru two bolt holes on front frame aft circular mtg flange; bracket aft mount C/O a steel bar W/hole for securing to an engine bracket; coupling adapter C/O a socket extension welded to a swivel adapter and welded to a drive plate W/three bolt holes that atch the adapter to the pto coupling shaft Functional Description: Is attached to an engine bracket and an adapter for the pto coupling shaft for motoring the core engine End Item Identification: F110-GE-129 engine | General Electric Co. (66464) | |
| 4920-01-335-6078 4920013356078 | 16U81M01L1-1 | Adapter, Test | Special Features: C/O 4 relays; 2 circuit breakers;misc resistors and diode End Item Identification: F-16C/D acft age Reference Data and Literature: Serd no. 81M01 | Lockheed Martin Corporation (81755) | |
| 4920-01-335-6137 4920013356137 | PDL1037B | Calibrator, Computer | Lockheed Martin Corporation (98897) | ||
| 4920-01-335-6750 4920013356750 | L9481111101 | Fixture, Aircraft Maintenance | Functional Description: 1THIS fixture calibrates the torque shaft strain gage and torque display indicator; it locks the torque shaft at the load pump end so 400-3600 in-lbs in either direction may be applied; the torque must be held for one minute with no variation End Item Identification: B-1B aircraft Reference Data and Literature: Serd number 99C42C | Dayton T. Brown Inc. (96362) | |
| 4920-01-335-6751 4920013356751 | 2211380-001 | Fixture, Aircraft Maintenance | Functional Description: This holding fixture is used on the 4920012369377 (test station, electrical-electronic equipment); holds a drawer for circuit cards End Item Identification: F-16 C/D Reference Data and Literature: Serd 90747 | BAE Systems National Security (12436) | |
| 4920-01-335-6814 4920013356814 | 4E4818-02-0028 | Panel, Patching, Programming | End Item Identification: Engine F100 (gse)test equipment | Hamilton Sundstrand Corporation (73030) | |
| 4920-01-335-6852 4920013356852 | 3C3966G05 | Test Stand, Aircraft Engine | Special Features: C/O two sections ea 14 ft lg, 7 ft D, 7 ft h; incl forklift channels; must be installed in a non-hazardous area; one section contains all elec components and motors for stand operation; also contains oil and pneumatic systems for testing of the components; 480 VAC/30/60 HZ/4 wire Reference Data and Literature: Operation and maintenance instruction 33D4-6-688-1; aft control and cits processor test stand; serd 1889 Test Type for Which Designed: Lube accessories | General Electric Co. (66464) | |
| 4920-01-335-7567 4920013357567 | 220-10104-103 | Test set, Power Control | End Item Identification: Sram ii ests | The Boeing Company (81205) | |
| 4920-01-335-8232 4920013358232 | 16A11840-1 | Repair kit, Aircraft, Maintenance | Special Features: A fabric end item container will be reqd for storagte/retention of pins, bushings, handles, etc Functional Description: Required to locate/drill the fairing seal fastener holes in wing box assy to match the fastener holes in 16W380/16W382 fairing seals End Item Identification: Lh/rh wing box assy | Lockheed Martin Corporation (81755) | |
| 4920-01-335-8396 4920013358396 | PWA70491 | Fixture, Engine Maintenance, Aircr | Special Features: C/O a machined cylinder atch to a steel base; a pre-masked 1ST, 2ND or 3RD stage compressor blade will be inserted into cylinder Functional Description: Used to shotpeen repaired areas of the root and platform area of the 1ST, 2ND and 3RD stg compressor rotor blades End Item Identification: F100-PW-229 engine | United Technologies Corporation (77445) | |
| 4920-01-335-8397 4920013358397 | 17G450264-1 | Fixture, Aircraft Maintenance | Special Features: Consist of a base and screw mechanism; the screw mechanism has a weight scale, 0-60 lbs, and a linear scale, 3 inch long in .2 inch inclement; the base can be shifted from side to side Functional Description: Fixture is used to mount the dual brake control valve assembly and to control the lever position during an acceptance test; also used to measure lever position and the applied force; the item it supports is P/N 70758; this item is made of aluminum and steel End Item Identification: C-17 aircraft | Boeing Company, The (88277) | |
| 4920-01-335-8398 4920013358398 | 16A11850-1 | Fixture, Aircraft Maintenance | Special Features: A rigie end item container will be reqd for protection of fixture and retenetion of pins Functional Description: Nused to install the nas 1724 bolt, tapered shank, shear type, 100 deg head, that is used to attach the 183204-1, 183212-1, 183217-1 and 183281-1, tie bar wing side, lef rotary actuator W/installed on 16W1030 wing box assy End Item Identification: F-16C/D acft age. | Lockheed Martin Corporation (81755) | |
| 4920-01-335-8515 4920013358515 | AN/ALM-262 12937742 | Test set, Countermeasures Dispens | Functional Description: Performs a system output performance verification test on AN/ALE-40/45 cmds. test set evaluates emds's dispense firing pulses at breech plate assy output to ensure they meet min/max characteristics End Item Identification: Countermeasures test set Reference Data and Literature: DD-61 DRW-90-01; U.S. army dwg P/N 12937742 | Joint Electronics Type Designation (80058) U S Army Armament Research (19200) | |
| 4920-01-335-8527 4920013358527 | 235A527-1 235A527 | Adapter, Test | Functional Description: Provides fault detection, fault isolation and repair verification of airspeed mach number indicator mechanism assy End Item Identification: B-1B acft age. Reference Data and Literature: Serd 51D51C; to 35-1-271-1 | Honeywell Intl Inc. (55972) | |
| 4920-01-335-9330 4920013359330 | 856A4004G02 | Fixture, Aircraft Maintenance | Special Features: C/O plenum; pressure probes; clamps Functional Description: Used to hold the hpt blades during repair End Item Identification: F101-GE-102/110-GE-100 engine | CFM International Inc. (58828) | |
| 4920-01-335-9380 4920013359380 | 25-1083-00 | Maintenance kit, Aircraft | End Item Identification: AH-64A | Task Research Inc. (61272) | |
| 4920-01-335-9705 4920013359705 | 20000810035-001 | Rigging kit, Aircraft Maintenance | Special Features: C/O lru tray assy, lru hoist adapter, hand winch W/cable routing bracketry; entire rigging kit is removable from plane when not in use Functional Description: Used to remove/replace lru's of cm receiver, transmitter, tranceiver, signal controller, and transmission line switch End Item Identification: AC-130U gunship age | Boeing Company, The (43999) |