Airframe Structural Components: 12C771-3, 12C789-1, 12C818-801
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 12C771-3 12C7713 | 1560-00-962-8860 | Support, Structural Component, Air | Special Features: Aluminum alloy, 2024-T851, QQ-A-225-6 | Lockheed Martin Corporation (81755) | |
| 12C772-3 12C7723 | 1560-00-887-2454 | Support, Structural Component, Air | III End Item Identification: Aircraft model F111 Special Features: Aluminum alloy, QQ-A-225/6, 3.968 in. lg, 2.000 in. W, 1.705 in. H, 2 holes 0.375 in. dia, 5 holes 0.284 in. dia | Lockheed Martin Corporation (81755) | |
| 12C774-1 12C7741 | 1560-00-531-8925 | Support, Structural Component, Air | III End Item Identification: Aircraft model F111 Special Features: Aluminum alloy, QQ-A-200/3 | Lockheed Martin Corporation (81755) | |
| 12C775-3 12C7753 | 1560-00-520-3845 | Support, Structural Component, Air | III End Item Identification: Aircraft model F111 Special Features: Aluminum alloy, QQ-A-200/3, 2.312 in. lg, 1.718 in. W, 2.000 in. H, 2 holes 0.500 in. dia, 4 holes 0.132 in. dia | Lockheed Martin Corporation (81755) | |
| 12C782-1 12C7821 | 1560-00-088-8288 | Stop, Pitch Channel | General Characteristics Item Description: Aluminum alloy, QQ-A-225/6, alloy 2024-T4 III FSC Application Data: Fuselage, airframe | Lockheed Martin Corporation (81755) | |
| 12C787-1 12C7871 | 1560-00-088-2244 | Idler Assembly, Fuselage | III End Item Identification: Aircraft model F111 | Lockheed Martin Corporation (81755) | |
| 12C788-1 12C7881 | 1560-00-088-2245 | Link Assembly, Bellcrank | General Characteristics Item Description: Titanium alloy, MIL-T-9047, 4.750 in. lg, roller bearing pressed in 4 places | Lockheed Martin Corporation (81755) | |
| 12C789-1 12C7891 | 1560-00-104-0606 | Stop, Mixer Input, Roll Channel | III End Item Identification: Aircraft model F111 General Characteristics Item Description: Aluminum alloy, AMS4260 | Lockheed Martin Corporation (81755) | |
| 12C78C-3 12C78C3 | 1560-00-104-0606 | Stop, Mixer Input, Roll Channel | III End Item Identification: Aircraft model F111 General Characteristics Item Description: Aluminum alloy, AMS4260 | Lockheed Martin Corporation (81755) | |
| 12C801-805 12C801805 | 1560-00-924-6532 | Lever, Rudder Idler | General Characteristics Item Description: Titanium alloy, AMS4928, 5.375 in. lg, 1.000 in. W | Lockheed Martin Corporation (81755) | |
| 12C801-807 12C801807 | 1560-00-924-6532 | Lever, Rudder Idler | General Characteristics Item Description: Titanium alloy, AMS4928, 5.375 in. lg, 1.000 in. W | Lockheed Martin Corporation (81755) | |
| 12C802-1 12C8021 | 1560-00-962-8864 | Bracket, Structural Component, Air | Aircraft Mission Design Series: F-111 Aircraft Location: Rudder idler bracket Material Document and Classification: QQ-A-225 fed spec single material response | Lockheed Martin Corporation (81755) | |
| 12C809-707 12C809707 | 1560-00-105-5134 | Bracket, Structural Component, Air | Aircraft Mission Design Series: F-111 Aircraft Location: Horizontal tail bracket Material Document and Classification: QQ-A-367 fed spec single material response | Lockheed Martin Corporation (81755) | |
| 12C811-1 12C8111 | 1560-00-104-8241 | Bracket, Structural Component, Air | Aircraft Mission Design Series: F-111 Aircraft Location: Equipment bay bracket | Lockheed Martin Corporation (81755) | |
| 12C811-3 12C8113 | 1560-00-104-8241 | Bracket, Structural Component, Air | Aircraft Mission Design Series: F-111 Aircraft Location: Equipment bay bracket | Lockheed Martin Corporation (81755) | |
| 12C815-5 12C8155 | 1560-00-972-1316 | Lever, Crossover, Rudder | General Characteristics Item Description: Titanium alloy, AMS4928, 12.750 in. lg, fork on both ends, roller bearing pressed in 4.946 in. from end 2 places | Lockheed Martin Corporation (81755) | |
| 12C815-803 12C815803 | 1560-00-455-8326 | Lever, Crossover, Rudder | General Characteristics Item Description: Titanium alloy, AMS4928, 12.750 in. lg, fork on both ends, roller bearing pressed in 4.946 in. from end 2 places | Lockheed Martin Corporation (81755) | |
| 12C816-3 12C8163 | 1560-00-688-8073 | Bracket, Aft Rudder Stop | General Characteristics Item Description: Steel AMS-53355, 3.690 in. W, 2.398 in. H | Lockheed Martin Corporation (81755) | |
| 12C818-1 12C8181 | 1560-00-067-3646 | No Item Name Available | III End Item Identification: Aircraft model F111 | Lockheed Martin Corporation (81755) | |
| 12C818-801 12C818801 | 1560-01-204-7466 | Idler Assembly | III End Item Identification: Acft model F-111 General Characteristics Item Description: C/O modified idler assy P/N 12C818-1, tube P/N 12C818-7, tube P/N 12C818-9 and attaching hardware III Functional Description: Used on cross rudder | Lockheed Martin Corporation (81755) |