Aircraft Maintenance and Repair Shop Specialized Equipment: 16A46159-1, 16A7400-13, 16A74008-3
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 16A46159-1 16A461591 | 4920-01-124-4801 | Adapter set, Aircraft Maintenance | End Item Identification: F-16 age. Special Features: C/O adapter W/flange to the pylon air disconnect, pressure gage, adapter to flowmeter assy; used to measure and regulate air pressure Reference Data and Literature: To 1F-16A-4-4 | BAE Systems Information And (94117) Lockheed Martin Corporation (81755) | |
| 16A46159-77 16A4615977 | 4920-01-447-8858 | Shaft, Adapter Assy | End Item Identification: F16 aircraft, fuel system ground equipment | Lockheed Martin Corporation (81755) | |
| 16A46177-1 16A461771 | 4920-01-141-0970 | Plug kit, Sense Port | End Item Identification: F-16 acft Special Features: To name: plug kit, sense ports, internal and external fuel tank Reference Data and Literature: To 1F-16A-4-4 | BAE Systems Information And (94117) Lockheed Martin Corporation (81755) | |
| 16A46184L1-1 16A46184L11 | 4920-01-138-2342 | Adapter Assembly, Interface Devic | Functional Description: Used to accomplish the leakage tests on the centrifugal power driven dual inlet fuel booster pump during overhaul End Item Identification: F-16 acft age. Supplementary Features: Company item name-adapter assembly, check valve pump, fuel boost | Lockheed Martin Corporation (81755) | |
| 16A46185L1-1 16A46185L11 | 4920-01-140-5855 | Adapter, Test | End Item Identification: F-16 acft Special Features: To name: adapter assy, pressure, nitrogen service unit, aerial refueling receptacle; C/O a hose with provisi ons at each end to adapt to GN2 cart and pressure switch Reference Data and Literature: To 1F-16A-4-4 | BAE Systems Information And (94117) Lockheed Martin Corporation (81755) | |
| 16A46186L1-1 16A46186L11 | 4920-01-228-5279 | Fixture, Aircraft Maintenance | Lockheed Martin Corporation (81755) | ||
| 16A46198-1 16A461981 | 4920-01-147-8335 | Maintenance kit, Aircraft | Special Features: C/O 3 transparent panels to observe fuel components during test; fitting for a pressure gage or pressure source is provided End Item Identification: F-16A/B acft age Reference Data and Literature: To 1F-16A-4-4 | Lockheed Martin Corporation (81755) | |
| 16A46198L1-1 16A46198L11 | 4920-01-147-8335 | Maintenance kit, Aircraft | Special Features: C/O 3 transparent panels to observe fuel components during test; fitting for a pressure gage or pressure source is provided End Item Identification: F-16A/B acft age Reference Data and Literature: To 1F-16A-4-4 | Lockheed Martin Corporation (81755) | |
| 16A46207L1-1 16A46207L11 | 4920-01-325-2406 | Adapter, Test, Fuel Systems Compon | Functional Description: Will perform in flow/shut-off functional tests of the external fuel transfer shut-off valve; will verify fuel shut-off capability after overhaul and include the application of test fluid to 150 gpm at the valve inlet port; this item will adapt the part number 60814 coil valve to the test tank inlet adapter and must provide sufficient clearance between valve with control port adapter hose installed and top of test tank; the control port on valve supplies pressure to an internal poppet, controlling fuel flow, using control port adapter, or equivalent, for test tank internal bulkhead connection End Item Identification: F-16 a/B/C/D General Characteristics Item Description: A fabric bag shall be required for retention of loose parts; a rigid end item container shall also be required; consist of a four hole flanged adapter; split clamp | Lockheed Martin Corporation (81755) | |
| 16A46219L1-1 16A46219L11 | 4920-01-313-7439 | Fixture, Aircraft Maintenance | Special Features: C/O valve block; 3 adapters; matl: alum; 15.0 lbs. nominal Functional Description: Used to check leakage in the external fuel tank vent and pressurization valve; used on the F-16A/B/C/D acft Nominal Overall Length: 12.000 inches | Lockheed Martin Corporation (81755) | |
| 16A46227-1 16A462271 | 4920-01-375-8734 | Maintenance kit, Aircraft | Special Features: C/O five (5) aircraft covers modified with fuel resistant transparent panels installed to allow simultaneous observation of fuel component operation in both wings having been modified with ecp 1637/4014 retrofit & the fuel vent box; 1 panel for vent box; 2 panels for refueling/xfer float valve; 2 panels for ext. tank xfer S.O.V.; each panel will have a fitting for a pressure gage or pressure source; will include necessary gaskets, nuts & caps; a bag for retention of fasteners will be attached to each panel by a lanyard Functional Description: To physically observe the operation of various fuel components of the aircraft (F-16) End Item Identification: F-16A/B/C/D, pre-block 40 | BAE Systems Information And (94117) Lockheed Martin Corporation (81755) | |
| 16A46229-1 16A462291 | 4920-01-375-1473 | Maintenance kit, Aircraft | End Item Identification: F-16C/D, block 40 and on Functional Classification: FF-2.2 Special Features: Panel kit consists of 5 acft covers modified W/fuel resistant transparent panels installed to allow simultaneous observation of fuel component operation in both wings and the fuel vent box; each panel will have a fitting for pressure gage or pressure souuce; the kit will also include the necessary gaskets, nuts and caps | BAE Systems Information And (94117) Lockheed Martin Corporation (81755) | |
| 16A46230-1 16A462301 | 4920-01-376-0351 | Panel, Interface Device | Special Features: Measures approximately 12" X 18" X 1" and is attached to the airframe by 1/4" structural bolts; a fabric container will be required for surface protection & retention of loose parts End Item Identification: F-16/A/B/C/D End Item Name: Test station | BAE Systems Information And (94117) Lockheed Martin Corporation (81755) | |
| 16A47065001G001 | 4920-01-500-9505 | Adapter kit, Test | Modine Manufacturing Company Inc. (3FQN6) Modine Mfg Co. (41197) | ||
| 16A55001-1 16A550011 | 4920-01-055-4831 | Clamp Assembly, Bonding, Strain Ga | Functional Description: Used to apply 30-40 psi pressure throughout a heat range of room temperature to 325 degrees End Item Identification: F-16 a/B acft/age. General Characteristics Item Description: Aluminum | BAE Systems Information And (94117) Lockheed Martin Corporation (81755) | |
| 16A55002-1 16A550021 | 4920-01-065-4876 | Clamp Assembly, Bonding-Mechanica | End Item Identification: F-16 a/B age. Overall Length: 10.000 inches nominal Overall Height: 4.000 inches nominal | Lockheed Martin Corporation (81755) | |
| 16A7400-13 16A740013 | 4920-01-546-2808 | Fixture Assy | End Item Identification: F-16 aircraft Part Name Assigned BY Controlling Agency: FOOT FSC Application Data: Fixture assy, check E-O/T-F pod mount | Lockheed Martin Corporation (81755) | |
| 16A7400-59 16A740059 | 4920-01-546-2806 | Fixture Assy | End Item Identification: F-16 aircraft Part Name Assigned BY Controlling Agency: FOOT FSC Application Data: Fixture assy, check E-O/T-F pod mount | Lockheed Martin Corporation (81755) | |
| 16A74008-1 16A740081 | 4920-01-087-2202 | Fixture, Aircraft Maintenance | Special Features: Matl: aluminum End Item Identification: F-16A acft age. Nominal Overall Height: 12.000 inches | Lockheed Martin Corporation (81755) | |
| 16A74008-3 16A740083 | 4920-01-143-3823 | Fixture, Aircraft Maintenance | End Item Identification: F-16A/B/C/D | Lockheed Martin Corporation (81755) |