FSC 1680 Miscellaneous Aircraft Accessories and Components: 1680-01-053-9338, 1680-01-053-9340, 1680-01-054-4787
| NSN | MFG SKU | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 1680-01-053-9338 1680010539338 | 4011-5 | Guide, Roller | III End Item Identification: Acft F-16A/B General Characteristics Item Description: Cres 17-4PH, AMS5643, 1.000 in. dia, 0.785 in. lg, 1 hole through center 0.470 in. dia | Parker-Hannifin Corporation (59211, 3H889) XAR Industries Inc. (50105) | |
| 1680-01-053-9339 1680010539339 | 4011-7 | Collar | III End Item Identification: Acft F-16A/B | XAR Industries Inc. (50105) | |
| 1680-01-053-9340 1680010539340 | 4011-8 | Plate, Scuff | III End Item Identification: Acft F-16A/B General Characteristics Item Description: Cres 304, MIL-S-5059, 4.100 in. lg, 2.380 in. W, 0.062 in. thk, 0.187 in. dia holes 5 places | XAR Industries Inc. (50105) | |
| 1680-01-054-0065 1680010540065 | H16DW702-03 | Wiring Harness, Branched | III End Item Identification: F-16A/B aircraft, tail effectivity 0007 0008 Special Features: Fuel tank at station 286 to 373; used on 16D1535-803 | Lockheed Martin Corporation (81755) | |
| 1680-01-054-0330 1680010540330 | 80-0368-3 209-075-325-71 | Panel, Fault-Function Indicator, a | Special Features: 7.200 in. lg, 2.166 in. H, 5.840 in. W Reference Number Differentiating Characteristics: As differentiated by source control dwg no. 209-075-325-71 | Grimes Aerospace Company (72914) Bell Helicopter Textron Inc. (97499) | |
| 1680-01-054-1341 1680010541341 | H16DW802-21 H16DW802-20 | Wiring Harness, Branched | III End Item Identification: Acft model F-16 Special Features: Located in right wing | Lockheed Martin Corporation (81755) | |
| 1680-01-054-1342 1680010541342 | H16DW804-20 | Wiring Harness, Branched | III End Item Identification: Acft model F-16 Special Features: Located from right wing disc to station 6 disc | Lockheed Martin Corporation (81755) | |
| 1680-01-054-1344 1680010541344 | H16DW806-20 | Wiring Harness, Branched | III End Item Identification: Acft model F-16 Special Features: Located from right wing disc to station 7 disc. | Lockheed Martin Corporation (81755) | |
| 1680-01-054-1735 1680010541735 | A288851 | Rod End, Controls | III End Item Identification: TAV-8A aircraft | BAE Systems PLC (K1987) British Aerospace Military (K0289) | |
| 1680-01-054-1777 1680010541777 | D2921-17 673032-127 | Actuator, Electro-Mechanical, Rota | Reference Number Differentiating Characteristics: As differentiated by the source control dwg no. Body Length: 4.200 inches nominal Body Height: 2.950 inches nominal | Eaton Corporation (17472) Ontic Engineering & Manufacturing (45934) Lockheed Martin Corporation (98897) | |
| 1680-01-054-2720 1680010542720 | 77227-5 | Track, Horizontal, Seat | III End Item Identification: Acft seat assy, KC-135 | MAG Aerospace Industries Inc. DBA (92824) | |
| 1680-01-054-2721 1680010542721 | 800040-3 800040 | Cover Assembly, Aircraft Seatback | III End Item Identification: Acft seat assy, KC-135 | MAG Aerospace Industries Inc. DBA (92824) Weber Industries Inc. (29067) MAG Aerospace Industries Inc. (29780) | |
| 1680-01-054-2722 1680010542722 | 810381-7 | Guide, Carriage Assembly | III End Item Identification: Acft seat assy, C-5A | MAG Aerospace Industries Inc. DBA (92824) | |
| 1680-01-054-2723 1680010542723 | 0113462-01 | Bracket, Initiator Clamp | III End Item Identification: Acft ejection seat, F-4 | Pacific Scientific Company (45402) | |
| 1680-01-054-2734 1680010542734 | 1211180-124 | SEAT | Arkwin Industries Inc. (98391) | ||
| 1680-01-054-2735 1680010542735 | 2045616-2 | Shaft, Planet Gear | General Characteristics Item Description: Steel 4330M, 0.669 in. dia, 0.905 in. lg, 0.470 in. dia hole through center, 1 offset in either end 0.110 in. deep | Honeywell International Inc. (70210) | |
| 1680-01-054-2736 1680010542736 | 2046106-1 | Shaft, Splined | General Characteristics Item Description: Steel MIL-S-5000, COMP4340, 2.265 in. lg, 1.005 in. dia, 0.635 in. dia hole through center, 0.751 in. dia hole in one end 0.960 in. deep, 1 hole through both walls on large end 0.315 in. dia, splined end 0.973 in. major dia, 15 teeth, 30.0 deg pressure angle | Honeywell International Inc. (70210) | |
| 1680-01-054-2749 1680010542749 | 1011-87-1 | Piston Assembly, Latch Cylinder | III End Item Identification: Acft model F-16A/B General Characteristics Item Description: Stem 1, piston head 1, piston rod 1, spring 1, packing retainer 1, packing, preformed 1 | Parker-Hannifin Corporation (59211, 3H889) XAR Industries Inc. (50105) | |
| 1680-01-054-2801 1680010542801 | H16DW068-01 | Wiring Harness, Branched | III End Item Identification: Acft model F-16 Special Features: Used on aft engine fuel backup control | Lockheed Martin Corporation (81755) | |
| 1680-01-054-4787 1680010544787 | BLS4LA125S | Pin, Ball Lock | III End Item Identification: Acft ejection seat, T-37 acft | Avibank MFG. Inc. (84256) |