Airframe Structural Components: 12M4914-7, 12M4975-7, 12M5536-13
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 12M4914-7 12M49147 | 1560-00-907-7305 | Seal, POD, Secondary Controls | III End Item Identification: Aircraft model F111 General Characteristics Item Description: Rubber, MIL-R-5847 class III grade 50 | Lockheed Martin Corporation (81755) | |
| 12M4914-9 12M49149 | 1560-00-907-7306 | Seal, Pod, Secondary Controls | III End Item Identification: Aircraft model F111 General Characteristics Item Description: Rubber, MIL-R-5847 class III grade 50 | Lockheed Martin Corporation (81755) | |
| 12M4933-3 12M49333 | 1560-00-855-2936 | Support, Mid Fuel Controls | III End Item Identification: Aircraft model F111 General Characteristics Item Description: Aluminum alloy, comp 2024 cond T4 | Lockheed Martin Corporation (81755) | |
| 12M4971-7 12M49717 | 1560-00-420-8500 | Support, Structural Component, Aircraft | III End Item Identification: Acft MODELF-111 Special Features: 3.360 in. min, 3.400 in. max lg O/a, 0.380 in. W, 0.562 in. H, roundedends, 5 rounded notches for tube rests, 0.390 in. W typical | Lockheed Martin Corporation (81755) | |
| 12M4972-7 12M49727 | 1560-00-244-6457 | Clamp, Controls, Lower Fuselage | III End Item Identification: Aircraft model F111 General Characteristics Item Description: Plastic | Lockheed Martin Corporation (81755) | |
| 12M4975-11 12M497511 | 1560-01-017-2695 | Support, Controls | III End Item Identification: Aircraft model F111 | Lockheed Martin Corporation (81755) | |
| 12M4975-13 12M497513 | 1560-00-152-3987 | Support, Controls, Fairleads | General Characteristics Item Description: Plastic, polycarbonate, general dynamics, fort worth, spec. control P5091 III FSC Application Data: Fuselage, airframe | Lockheed Martin Corporation (81755) | |
| 12M4975-7 12M49757 | 1560-00-130-9914 | Support, Structural Component, Air | Aircraft Mission Design Series: F-111 Overall Length: 3.780 inches nominal Overall Width: 0.380 inches nominal | Lockheed Martin Corporation (81755) | |
| 12M5041-17 12M504117 | 1560-01-048-1952 | Boot, Control | III End Item Identification: Aircraft model F-111 | Lockheed Martin Corporation (81755) | |
| 12M5041-7 12M50417 | 1560-01-048-1952 | Boot, Control | III End Item Identification: Aircraft model F-111 | Lockheed Martin Corporation (81755) | |
| 12M5042-11 12M504211 | 1560-00-314-3113 | Retainer, Boot, Brake Control Syst | III End Item Identification: Aircraft model F111 | Lockheed Martin Corporation (81755) | |
| 12M5102-7 12M51027 | 1560-01-182-7153 | Plate, Structural, Aircraft | Aircraft Mission Design Series: F-111BA Special Features: Used as spacer Aircraft Location: Nose wheel steering linkage | Lockheed Martin Corporation (81755) | |
| 12M5130-7 12M51307 | 1560-00-928-3047 | Housing, Torque Tube | Lockheed Martin Corporation (81755) | ||
| 12M5137-9 12M51379 | 1560-00-929-2318 | Bracket, Structural Component, Air | Aircraft Mission Design Series: F-111 Aircraft Location: Nose wheel universal bracket Material Document and Classification: QQ-A-601 fed spec single material response | Lockheed Martin Corporation (81755) | |
| 12M5141-1 12M51411 | 1560-00-927-6644 | Housing Assembly, Upper | General Characteristics Item Description: QQ-A-367 | Lockheed Martin Corporation (81755) | |
| 12M5144-1 12M51441 | 1560-00-929-2323 | Shaft, Universal | III End Item Identification: Acft model F-111 General Characteristics Item Description: Used on nose wheel steering assembly | Lockheed Martin Corporation (81755) | |
| 12M5412-803 12M5412803 | 1560-00-469-7194 | Bracket Assembly, Barrier Hook | III End Item Identification: Acft model F-111 General Characteristics Item Description: 2024 aluminum alloy QQ-A-250/4-T4, assembly requires fairlead P/N 12M5419-9, ar rivets P/N MS20470AD3, 1.930OA lg, hole 0.750 in. min 0.755 in. max dia for hook, 2 holes 0.196 in. min 0.204 in. max dia | Lockheed Martin Corporation (81755) | |
| 12M5474-1 12M54741 | 1560-00-463-9167 | Carrier Assembly, Barrier | General Characteristics Item Description: Aluminum alloy, AMS4260 | Lockheed Martin Corporation (81755) | |
| 12M5475-1 12M54751 | 1560-00-464-3667 | Bracket, Hook Control | General Characteristics Item Description: Aluminum alloy, 2024, T3, QQ-A-250-5, 7.12 in. lg | Lockheed Martin Corporation (81755) | |
| 12M5536-13 12M553613 | 1560-00-841-6614 | Guide Assembly, Wing Sweep | III End Item Identification: Aircraft model F-111 General Characteristics Item Description: Aluminum alloy, QQ-A-250-4, temper T4 | Lockheed Martin Corporation (81755) |