FSC 4920 Aircraft Maintenance and Repair Shop Specialized Equipment: 4920-01-310-0101, 4920-01-310-0514, 4920-01-310-2488
| NSN | MFG SKU | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 4920-01-310-0101 4920013100101 | 16A11857-1 | Fixture, Aircraft Maintenance | Special Features: Matl: alum alloy; 17.7 lbs. Functional Description: Used to repair the cover, engine access-lower left hand; used on the F-16C/D acft Nominal Overall Length: 56.000 inches | Lockheed Martin Corporation (81755) | |
| 4920-01-310-0104 4920013100104 | 16A13198-1 | Fixture, Aircraft Maintenance | Special Features: C/o:aluminum alloy panels, stiffeners, forged hinges and actuator arm riveted TOGETHER;PINS;BOLTS;DIM:67.000 IN.LG;30.000 IN.W;8.000 in.h; Functional Description: Used to repair a damaged left hand main landing gear door; used on the F-16 acft | Lockheed Martin Corporation (81755) | |
| 4920-01-310-0105 4920013100105 | 298251-1 | Fixture, Aircraft Maintenance | Special Features: Matl: stainless steel; 3.0 lbs Functional Description: Used to hold the nozzle assembly while torquing atomizer and bending tabs of the key washers against hex flats of atomizer; used on the C-17 acft Nominal Overall Height: 2.000 inches | Honeywell International Inc. (99193) | |
| 4920-01-310-0107 4920013100107 | 16A11858-1 | Fixture, Aircraft Maintenance | Special Features: Matl: alum alloy; 14.7 lbs Functional Description: The fixture assemblt is used to repair the cover, engine access right hand lower on the F-16C/D acft Nominal Overall Length: 56.000 inches | Lockheed Martin Corporation (81755) | |
| 4920-01-310-0108 4920013100108 | 6414803-1 | Fixture, Aircraft Maintenance | End Item Identification: F-15 ais support equipment | Honeywell Intl Inc. (55974) | |
| 4920-01-310-0109 4920013100109 | 685-0562-001 | Fixture, Aircraft Maintenance | Special Features: Plate, protection;post;contact assy;cover, tuning;cable, coaxial;bumper, rubber;block, clamp;pin, guide;connector;plate;cover;chassis;chassis, electrica; Functional Description: Used to check current sense | Rockwell Collins Inc. (13499) | |
| 4920-01-310-0258 4920013100258 | 68D040198-1001 | Adapter, Test | Functional Description: Used to provide programming functions required during off station maintenance of the pilots grip assy controller line replacable unit End Item Identification: F-15E acft Reference Data and Literature: Serd no. 3958 | Boeing Company,, The (76301) | |
| 4920-01-310-0259 4920013100259 | 16A14289L1-1 | Adapter, Test | Functional Description: Provide the required electrical and mechanical interface between the unit under test (uut) and the test equipment; used on the F-16A/B/C/D acft Test Item Connection Method: Connector | Lockheed Martin Corporation (81755) | |
| 4920-01-310-0503 4920013100503 | 7085-H | Clamp Assembly, Special | End Item Identification: Acft F-18 | Columbus Jack Corporation (00994) AGE Logistics Corporation (02708) | |
| 4920-01-310-0504 4920013100504 | T7-708718-4 | Jig Assembly | End Item Identification: Acft F-18 | AGE Logistics Corporation (02708) Columbus Jack Corporation (00994) | |
| 4920-01-310-0514 4920013100514 | E10-09699-1 | Guide Block, Inspect | End Item Identification: Aircraft model A-7 | Naval Aviation Depot (96547) | |
| 4920-01-310-0528 4920013100528 | 5SE00841-1 TYPE11-LD#38 | Trap, Oil | General Characteristics Item Description: L2.750 in. O/a diameter; 7.250 in. lg; opr. range M40.0 to P250.0 f; discharge oil from gas under a differential pressure of 1 at a rate of 10 lb per hour; tamper-proof construction; pressure range: up to 150 psi | Armstrong International Inc. (03933) Naval Air Warfare Center Aircraft (80020, 28638) | |
| 4920-01-310-0530 4920013100530 | 795-0237-001 | Cable-Test | End Item Identification: Tacmo III | Rockwell Collins Inc. (13499) | |
| 4920-01-310-0787 4920013100787 | 16A11860-1 | Fixture, Aircraft Maintenance | Special Features: Alum alloy skin W/riveted alum alloy stiffeners; contains provisions for installation of a nav light and two antennas; 22.000 in. by 44.000 in.; 12.8 lbs. nominal Functional Description: Used at depot level of maintenance to repair the ammunition drum cover assembly End Item Identification: F-16C acft age | Lockheed Martin Corporation (81755) | |
| 4920-01-310-0788 4920013100788 | 3C3737G01 | Fixture, Aircraft Maintenance | Special Features: C/O assy; support; cam shaft 3; cams 3; misc hdwr; 150.0 lbs. nominal; matl: carbon steel; finish: black oxide Functional Description: Used to position/restrain seal during machining out old honeycomb/edm new honeycomb to finish dim End Item Identification: B-1B acft age. | General Electric Co. (66464) | |
| 4920-01-310-0789 4920013100789 | 3C3524G02 | Fixture, Aircraft Maintenance | Special Features: 22.000 in. by 32.000 in. by 9.000 in.; 30.0 lbs. nominal; C/O welded assy/nylon liner bushing. the mild steel welded assy C/O nylon 135 deg segment of a 37.250 in. od by 34.340 in. id by 0.380 in. thk ring; a 180 deg split/hinged bushing that is 5.250 in. od BY4.750 in. id by 2.750 in. L, and a set of 3 L shaped legs that connect bushing W/ring segment; legs are spaced 59.0 deg apart radially Functional Description: Used to support lpt rotor assy/maintain radial/axial relationship of stage 2 nozzle/turbine frame to lpt rotor shaft End Item Identification: B-1B acft age. | General Electric Co. (66464) | |
| 4920-01-310-0790 4920013100790 | 3031606-1 MX-11394/AAM-84 | Adapter, Test | Special Features: Appx 30 lbs Functional Description: Holds the elevation resolver assy/contains mating gearing, gear rotation mechanism, and interface cable from fixture to servo subassy test set End Item Identification: Infrared detecting set | Raytheon Company (96214) Joint Electronics Type Designation (80058) | |
| 4920-01-310-0859 4920013100859 | 17G130505-1 | Adapter, Test | Special Features: Mtbr for the wheel speed transducer, wuc 13JGJ, is 1137 hrs; test adapter used in conjunction with: test set, indicator-generator, tachometer; test cable-wheel speed transducer and breakout adapter; breakout adapter; decade resistor and capacitor; oscilloscope Functional Description: Used to attach the wheel speed transducer to the tachometer test set End Item Identification: C-17 acft age | Boeing Company, The (88277) | |
| 4920-01-310-2478 4920013102478 | DAA7127P002-101 C025005-001 | Test Program set | Northrop Grumman Systems Corporation (1W025) | ||
| 4920-01-310-2488 4920013102488 | 17G110114-1 | Fixture, Aircraft Maintenance | Special Features: Matl: steel; finish: 16473 gray paint; 20.0 lbs. nominal Functional Description: Jthe fixture holds the "c" balance assembly and provide a means of winding the springs and setting the torsion to a spscified value; used on the troop door counterbalance spring tensioner; used on the C-17 acft Nominal Overall Height: 12.000 inches | Boeing Company, The (88277) |