Airframe Structural Components: 12T404-131, 12T404-83, 12T404-99
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 12T404-131 12T404131 | 1560-01-265-5144 | Rib, Airfoil | Aircraft Mission Design Series: F-111A/E/F/D/FB/EF Material: Aluminum alloy 2024 Aircraft Location: Leading edge, rudder | Lockheed Martin Corporation (81755) | |
| 12T404-133 12T404133 | 1560-01-265-5145 | Rib, Airfoil | Aircraft Mission Design Series: F-111A/E/F/D/EF/FB Material: Aluminum alloy 2024 Aircraft Location: Leading edge, rudder | Lockheed Martin Corporation (81755) | |
| 12T404-135 12T404135 | 1560-00-241-9017 | Skin, Aircraft | III End Item Identification: F-111 Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-250/5-T6 fed spec single material response | Lockheed Martin Corporation (81755) | |
| 12T404-25 12T40425 | 1560-00-869-2545 | Skin, Aircraft | III End Item Identification: F-111 Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-250/5-T6 fed spec single material response | Lockheed Martin Corporation (81755) | |
| 12T404-33 12T40433 | 1560-00-869-2546 | Skin, Aircraft | III End Item Identification: F-111 Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-250/5-T6 fed spec single material response | Lockheed Martin Corporation (81755) | |
| 12T404-35 12T40435 | 1560-00-241-9017 | Skin, Aircraft | III End Item Identification: F-111 Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-250/5-T6 fed spec single material response | Lockheed Martin Corporation (81755) | |
| 12T404-67 12T40467 | 1560-01-301-8280 | Plate, Structural, Aircraft | Aircraft Mission Design Series: F-111A/FB/D/E/F/EF Aircraft Location: Plate, leading edge, rudder | Bombardier Inc. Canadair (88308) Lockheed Martin Corporation (81755) | |
| 12T404-7 12T4047 | 1560-00-997-7722 | Skin, Aircraft | III End Item Identification: F-111 Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-250/5-T6 fed spec single material response | Lockheed Martin Corporation (81755) | |
| 12T404-71 12T40471 | 1560-01-301-8282 | Plate, Structural, Aircraft | Aircraft Mission Design Series: F-111A/FB/D/E/F/EF Aircraft Location: Plate, leading edge, rudder | Bombardier Inc. Canadair (88308) Lockheed Martin Corporation (81755) | |
| 12T404-73 12T40473 | 1560-01-301-8283 | Plate, Structural, Aircraft | Aircraft Mission Design Series: F-111A/FB/D/E/F/E/EF aircraft Aircraft Location: Plate, leading edge, rudder | Bombardier Inc. Canadair (88308) Lockheed Martin Corporation (81755) | |
| 12T404-77 12T40477 | 1560-01-301-8284 | Plate, Structural, Aircraft | Aircraft Mission Design Series: F-111A/FB/D/E/F/EF Aircraft Location: Plate, leading edge, rudder | Bombardier Inc. Canadair (88308) Lockheed Martin Corporation (81755) | |
| 12T404-79 12T40479 | 1560-01-301-8285 | Plate, Structural, Aircraft | Aircraft Mission Design Series: F-111A/FB/D/E/F/EF Aircraft Location: Plate, leading edge, rudder | Aero Metal Forms Inc. (3T761) Airborne Technologies Inc. (58730) Bombardier Inc. Canadair (88308) Kent Associates Inc. (8R034) Lockheed Martin Corporation (81755) Southwest Machine & Manufacturing (33927) | |
| 12T404-8 12T4048 | 1560-00-869-2548 | Skin, Aircraft | III End Item Identification: F-111 Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-250/5-T6 fed spec single material response | Lockheed Martin Corporation (81755) | |
| 12T404-83 12T40483 | 1560-01-301-8287 | Plate, Structural, Aircraft | Aircraft Mission Design Series: F-111A/FB/D/E/F/EF Aircraft Location: Plate, leading edge, rudder | Bombardier Inc. Canadair (88308) Lockheed Martin Corporation (81755) | |
| 12T404-85 12T40485 | 1560-01-300-3410 | Plate, Structural, Aircraft | Aircraft Mission Design Series: F-111A/FB/D/E/F/EF Aircraft Location: Plate, leading edge, rudder | Bombardier Inc. Canadair (88308) Lockheed Martin Corporation (81755) | |
| 12T404-87 12T40487 | 1560-01-301-8288 | Plate, Structural, Aircraft | Aircraft Mission Design Series: F-111A/FB/D/E/F/EF Aircraft Location: Plate, leading edge, rudder | Bombardier Inc. Canadair (88308) Lockheed Martin Corporation (81755) | |
| 12T404-91 12T40491 | 1560-01-301-8289 | Plate, Structural, Aircraft | Aircraft Mission Design Series: F-111A/FB/D/E/F/EF Aircraft Location: Plate, leading edge, rudder | Bombardier Inc. Canadair (88308) Lockheed Martin Corporation (81755) | |
| 12T404-93 12T40493 | 1560-00-869-2549 | Cover, Access | Lockheed Martin Corporation (81755) | ||
| 12T404-97 12T40497 | 1560-00-869-2551 | Cover, Access | Lockheed Martin Corporation (81755) | ||
| 12T404-99 12T40499 | 1560-00-787-8937 | Cover, Access, Aircraft | Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-250/5 fed spec single material response Securing Device Type: Threaded fastener | Lockheed Martin Corporation (81755) |