Miscellaneous Aircraft Accessories and Components: 16VM003002-4, 16VM003004-2, 16VP108-11
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 16VM003002-4 16VM0030024 | 1680-01-230-1280 | Actuator, Electro-Mechanical, Rota | Lockheed Martin Corporation (81755) | ||
| 16VM003002-5 16VM0030025 | 1680-01-230-1279 | Actuator, Mechanical, Aircraft | Special Features: Overall length 13.551; overall width 7.280; used on F-16C/D acft Design Type: Rotary | Lockheed Martin Corporation (81755) | |
| 16VM003002-6 16VM0030026 | 1680-01-276-8711 | Actuator, Electro-Mechanical, Rota | III Supplementary Features: F-16C/D aircraft; tail effectivity 5C 0358 0477 | Lockheed Martin Corporation (81755) | |
| 16VM003004-1 16VM0030041 | 1680-01-045-1018 | Gearbox Assembly, Aircraft | Material: Aluminum alloy Aircraft Mission Design Series: F-16 Aircraft Location: Leading edge flap system | Lockheed Martin Corporation (81755) | |
| 16VM003004-2 16VM0030042 | 1680-01-355-0721 | Gearbox Assembly, Aircraft | Side for Which Designed: Both sides Aircraft Location: Leading edge flap system Aircraft Mission Design Series: F-16 | Lockheed Martin Corporation (81755) | |
| 16VM003004-3 16VM0030043 | 1680-01-355-0721 | Gearbox Assembly, Aircraft | Side for Which Designed: Both sides Aircraft Location: Leading edge flap system Aircraft Mission Design Series: F-16 | Lockheed Martin Corporation (81755) | |
| 16VM003006-2 16VM0030062 | 1680-01-126-0296 | Brake, Asymmetry | III End Item Identification: F-16 aircraft General Characteristics Item Description: On leading edge drive system | Lockheed Martin Corporation (81755) | |
| 16VM003006-4 16VM0030064 | 1680-01-168-9396 | Actuator, Electro-Mechanical, line | Special Features: F-16A/B;ACACTUATION system outline flap;clockwise shaft rotation produces SW1, SW2, SW3 switch sequence;tail effectivity 61 0001 9999 FSC Application Data: Aircraft accessory equipment | Lockheed Martin Corporation (81755) | |
| 16VM005001-1 16VM0050011 | 1680-01-450-6899 | Gearbox Assembly, Aircraft | Criticality Code Justification: FEAT Part Name Assigned BY Controlling Agency: Manufacturers suggested name - rotary actuator gearbox, leading edge drive system Aircraft Station Number: Wing leading edge | Lockheed Martin Corporation (81755) | |
| 16VM005001-2 16VM0050012 | 1680-01-264-9872 | Gearbox Assembly, Aircraft | III End Item Identification: F-16C/D aircraft Reference Number Differentiating Characteristics: As differnetiated by repairable parts | Lockheed Martin Corporation (81755) | |
| 16VM005001-2 16VM0050012 | 1680-01-450-6900 | Gearbox Assembly, Aircraft | Criticality Code Justification: CZEK Part Name Assigned BY Controlling Agency: Manufacturers suggested name - rotary actuator gearbox, leading edge drive system Aircraft Station Number: Wing leading edge | Lockheed Martin Corporation (81755) | |
| 16VM005001-3 16VM0050013 | 1680-01-264-9870 | Gearbox Assembly, Aircraft | Aircraft Mission Design Series: F-16C/D | Lockheed Martin Corporation (81755) | |
| 16VM005001-4 16VM0050014 | 1680-01-343-1467 | Gearbox Assembly, Aircraft | III End Item Identification: F-16 aircraft Aircraft Location: Leading edge drive system | Lockheed Martin Corporation (81755) | |
| 16VM005-1 16VM0051 | 1680-01-254-0471 | Actuator, Electro-Mechanical, Rota | END Item Identification: F-16 aircraft Special Features: Consists of rotary actuator, P/N 183200-1; tiebar wing side, P/N 183217-1; tiebar wing side, P/N 183204-1; tiebar flap side, P/N 183203-1 FSC Application Data: Leading edge flap, P/N 16M005-1 | Lockheed Martin Corporation (81755) | |
| 16VM005-2 16VM0052 | 1680-01-254-0470 | Actuator, Electro-Mechanical, Rota | III End Item Identification: F-16 aircraft Special Features: Consists of rotary actuator, P/N 183220-1; tiebar wing side, P/N 183218-1; tiebar wing side, P/N 183212-1; tiebar flap side, P/N 183203-3 III Fsc Application Data: Leading edge flap, P/N 16M005-2 | Lockheed Martin Corporation (81755) | |
| 16VP003-1 16VP0031 | 1680-01-057-3391 | Receptacle Assembly, Flight Refue | End Item Identification: Acft aerial refueling system, F-16 General Characteristics Item Description: Support 29, support assy 3, retainer 2, fitting 2, housing assy 1, light assy 2, door assy 24, wall 2, switch 2, receptacle 1, actuator 1, rod assy 1, link assy 4, coupling 2 | Lockheed Martin Corporation (81755) | |
| 16VP003-3 16VP0033 | 1680-01-057-3391 | Receptacle Assembly, Flight Refue | End Item Identification: Acft aerial refueling system, F-16 General Characteristics Item Description: Support 29, support assy 3, retainer 2, fitting 2, housing assy 1, light assy 2, door assy 24, wall 2, switch 2, receptacle 1, actuator 1, rod assy 1, link assy 4, coupling 2 | Lockheed Martin Corporation (81755) | |
| 16VP003-4 16VP0034 | 1680-01-432-7271 | Receptacle Assembly, Flight Refue | End Item Identification: F-16 aircraft Special Features: Drawing name - receptacle, aerialrefuel | Lockheed Martin Corporation (81755) | |
| 16VP020-2 16VP0202 | 1680-01-054-4794 | Reservoir, Halon | III End Item Identification: Fire extinguishing system, F-16 General Characteristics Item Description: Container 1, electric heater assy 110.0-124.0 vac, 380.0 hz to 420.0 hz, 400.0 watts, pressure relief valve 600.0 psig, pressure switch | Lockheed Martin Corporation (81755) | |
| 16VP108-10 16VP10810 | 1680-01-051-0820 | Control Assembly, Engine | III End Item Identification: Acft model F-16 General Characteristics Item Description: 287.000 in. lg, rod end 2, end rod 1, swivel disconnect 1, anchor sleeve 1, pressure seal sleeve 1, bearing 1, firewall seal 1, pull wire fitting 1, flexible casing 3 | Lockheed Martin Corporation (81755) | |
| 16VP108-11 16VP10811 | 1680-01-052-0801 | Control Assembly, Quadrant | Special Features: 220.000 in. lg. End Item Identification: Acft engine control model F-16 (Non-Core Data) Fsc Application Data: Throttle quadrant assy | Lockheed Martin Corporation (81755) |