Automatic Pilot Mechanisms and Airborne Gyro Components: 16VC003-6, 171082-901, 1715426
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 16VC003-6 16VC0036 | 6615-01-084-4988 | Computer, Flight Control | III End Item Identification: F-16A/B acft General Characteristics Item Description: 20.32 in. O/a lg; 10.26 in. w; 8.10 in. H | Lockheed Martin Corporation (81755) | |
| 16VC003-8 16VC0038 | 6615-01-356-6851 | Computer, Flight Control | III End Item Identification: F16A/B block 15 acft III Reference Data and Literature: T.O.5A7-3-38-4 | Lockheed Martin Corporation (81755) | |
| 16VC003-9 16VC0039 | 6615-01-141-2981 | Computer, Flight | III End Item Identification: F-16 C/D acft General Characteristics Item Description: 20.320 in. lg; 10.260 in. w; 8.100 in. H | Lockheed Martin Corporation (81755) | |
| 16VC006-2 16VC0062 | 6615-01-071-4513 | Gyroscope, Rate | Overall Length: 4.220 inches minimum and 4.720 inches maximum Overall Height: 1.040 inches nominal Overall Width: 1.040 inches nominal | CS Industries (41820) Lockheed Martin Corporation (81755) | |
| 16VC010-1 16VC0101 | 6615-01-041-5661 | Force Sensor Assembly | III End Item Identification: F-16 acft | Lockheed Martin Corporation (81755) | |
| 16VC010-7 16VC0107 | 6615-01-439-3035 | Sensor Assy, Force | III End Item Identification: F-16 acft | Lockheed Martin Corporation (81755) | |
| 16VC026-12 16VC02612 | 6615-01-448-6152 | Controller, Flight, Automatic Pilo | III End Item Identification: F-16 aircraft Power Source: External Maximum Overall Length: 20.280 inches | Lockheed Martin Corporation (81755) | |
| 16VC026-9 16VC0269 | 6615-01-351-7337 | Computer, Flight Control | III End Item Identification: F16 General Characteristics Item Description: O/a dim. 20.28 in. l. max, 10.93 in. W. max, 8, 78 in. H. max;functional description:converts information from flight controller to move the flight control surfaces | Lockheed Martin Corporation (81755) | |
| 16VE017005 | 6615-01-049-0201 | Gyroscope, Rate | III End Item Identification: F-16 acft Overall Length: 9.560 inches nominal Overall Width: 6.680 inches nominal | Lockheed Martin Corporation (81755) | |
| 16VE017005-5 16VE0170055 | 6615-01-078-4943 | Gyroscope, Rate | III End Item Identification: F-16 acft Special Features: Critical application Overall Length: 9.560 inches nominal | Lockheed Martin Corporation (81755) | |
| 16VZ001-55 16VZ00155 | 6615-00-137-6038 | Gyroscope, Rate | Overall Length: 5.195 inches nominal Overall Height: 2.872 inches nominal Overall Width: 2.890 inches nominal | Lockheed Martin Corporation (81755) | |
| 170034 | 6615-00-487-7641 | Retainer-Adj Retain | Lockheed Martin Corporation (56232) | ||
| 170596 | 6615-00-031-9826 | Element Asy | Lockheed Martin Corporation (56232) | ||
| 1706C1 | 6615-00-602-0050 | Servocylinder | Overall Width: 3.500 inches nominal Overall Height: 4.500 inches nominal Integral Valve Operation Method: Electric | Moog Inc. (94697) | |
| 1706C2 | 6615-00-625-7215 | Servocylinder | Overall Width: 3.500 inches nominal Overall Height: 4.500 inches nominal Integral Valve Operation Method: Electric | Moog Inc. (94697) | |
| 1708D | 6615-00-695-1972 | Servocylinder | Overall Width: 4.060 inches nominal Overall Height: 4.440 inches nominal Integral Valve Operation Method: Hydraulic | Moog Inc. (94697) | |
| 1708E | 6615-00-603-7984 | Servocylinder | Overall Width: 4.060 inches nominal Overall Height: 4.440 inches nominal Integral Valve Operation Method: Hydraulic | Moog Inc. (94697) | |
| 171082-901 171082901 | 6615-00-981-5687 | Spring Cushion | Solartron Electronics Inc. (65092) | ||
| 171450-01 17145001 | 6615-01-303-7957 | Accelerometer, Electrical, Linear | III Fsc Application Data: Pacer special | GE Aviation Systems LLC (35351) | |
| 1715426 | 6615-00-075-8572 | Nut, Anchor | General Characteristics Item Description: O/a dim. 0.969 in. l; 0.391 in. w; 0.219 in. h; cadmium plated steel; red nylon insert | Lockheed Martin Corporation (56232) |