FSC 1560 Airframe Structural Components: 1560-00-962-3680, 1560-00-962-6518, 1560-00-962-6522
| NSN | MFG SKU | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 1560-00-962-3680 1560009623680 | 784105-1 | Cover Assy | Lockheed Martin Corporation (98897) | ||
| 1560-00-962-3713 1560009623713 | 797146-1 | Panel, Structural, Aircraft | Aircraft Mission Design Series: F-104G | Lockheed Martin Corporation (98897) | |
| 1560-00-962-3714 1560009623714 | 797147-1 | Panel Assy Plastic | Lockheed Martin Corporation (98897) | ||
| 1560-00-962-3715 1560009623715 | 652294-30 12-21928-30 | Insulation Blanket | Hitco Carbon Composites Inc. (78741) Lockheed Martin Corporation (98897) | ||
| 1560-00-962-5845 1560009625845 | 3F42292-101 | Fitting, Latch, Ramp | General Characteristics Item Description: Cres, 4.660 in. lg, 4.624 in. W, 0.500 in. thk | Lockheed Martin Corporation (98897) | |
| 1560-00-962-6310 1560009626310 | 79F1300079-17 | Trough Assembly | Northrop Grumman Systems Corporation (26512) | ||
| 1560-00-962-6509 1560009626509 | 64-8328-232 | Skin, Aircraft | The Boeing Company (81205) | ||
| 1560-00-962-6510 1560009626510 | 64-8328-233 | Skin, Aircraft | The Boeing Company (81205) | ||
| 1560-00-962-6511 1560009626511 | 64-8328-235 | Duct Assembly, Air Conditioning-H | III End Item Identification: C-135 aircraft Aircraft Mission Design Series: C-135 Material: Aluminum alloy | The Boeing Company (81205) | |
| 1560-00-962-6512 1560009626512 | 64-8328-258 | Skin, Aircraft | The Boeing Company (81205) | ||
| 1560-00-962-6513 1560009626513 | 64-8327-23 | Skin, Aircraft | III End Item Identification: Acft model KC-135 Aircraft Mission Design Series: KC-135 | The Boeing Company (81205) | |
| 1560-00-962-6514 1560009626514 | 64-8327-25 | Skin, Aircraft | III End Item Identification: Acft model KC-135 Aircraft Mission Design Series: KC-135 | The Boeing Company (81205) | |
| 1560-00-962-6515 1560009626515 | 64-8327-27 | Skin, Aircraft | III End Item Identification: Acft model KC-135 Aircraft Mission Design Series: KC-135 | The Boeing Company (81205) | |
| 1560-00-962-6516 1560009626516 | 64-8327-291 | Skin, Aircraft | III End Item Identification: KC-135 | The Boeing Company (81205) | |
| 1560-00-962-6517 1560009626517 | 64-8327-400 64-8327-30 | Longeron | III End Item Identification: Aircraft, model C-135 Material: Titanium Material Document and Classification: MIL-T-9046, class 6 mil spec single material response | The Boeing Company (81205) | |
| 1560-00-962-6518 1560009626518 | 64-8327-21 64-8327-1100 | Skin, Aircraft | Aircraft Mission Design Series: KC-135 Material: Aluminum alloy 2024 Aircraft Location: Cowl panel assembly | The Boeing Company (81205, 82918) | |
| 1560-00-962-6519 1560009626519 | 64-8327-24 | Skin, Aircraft | III End Item Identification: KC-135 statotanker Aircraft Mission Design Series: KC-135 tanker Material: Aluminum alloy 2024 | The Boeing Company (81205) | |
| 1560-00-962-6520 1560009626520 | 64-8327-26 | Skin, Aircraft | III End Item Identification: Aircraft, model KC-135 Aircraft Mission Design Series: KC-135 Material: Steel comp 302 | The Boeing Company (81205) | |
| 1560-00-962-6521 1560009626521 | 64-8327-28 | Skin, Aircraft | III End Item Identification: Aircraft, model KC-135 Aircraft Mission Design Series: KC-135 Material: Steel comp 302 | The Boeing Company (81205) | |
| 1560-00-962-6522 1560009626522 | 64-8327-292 | Plate, Structural, Aircraft | III End Item Identification: Acft model C/KC-135 Special Features: Al alloy clad sheet 2024-0 per QQ-A-362, 0 temper, heat treated to condition T4; 95.000 in. lg, 5.200 in. W, 0.063 in. thk; used as doubler-splice on cowl panel assembly of engine nacelle | The Boeing Company (81205) |