Airframe Structural Components: 12C350-1, 12C360-15, 12C450-1
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 12C350-1 12C3501 | 1560-00-907-7398 | No Item Name Available | III End Item Identification: Aircraft model F111 General Characteristics Item Description: 21.630 in. O/a lg, 3.360 in. O/a W, 1.710 in. O/a H | Lockheed Martin Corporation (81755) | |
| 12C350-2 12C3502 | 1560-00-425-8095 | Frame Assembly, Rudder | III End Item Identification: Aircraft model F111 General Characteristics Item Description: 21.630 in. O/a lg, 3.360 in. O/a W, 1.710 in. O/a H | Lockheed Martin Corporation (81755) | |
| 12C350-2 12C3502 | 1560-00-907-7414 | No Item Name Available | III End Item Identification: Aircraft model F111 General Characteristics Item Description: 21.630 in. O/a lg, 3.360 in. O/a W, 1.710 in. O/a H | Lockheed Martin Corporation (81755) | |
| 12C350-3 12C3503 | 1560-00-425-8094 | Frame Assembly, Rudder | III End Item Identification: Aircraft model F111 General Characteristics Item Description: 21.630 in. O/a lg, 3.360 in. O/a W, 1.710 in. O/a H | Lockheed Martin Corporation (81755) | |
| 12C350-4 12C3504 | 1560-00-425-8095 | Frame Assembly, Rudder | III End Item Identification: Aircraft model F111 General Characteristics Item Description: 21.630 in. O/a lg, 3.360 in. O/a W, 1.710 in. O/a H | Lockheed Martin Corporation (81755) | |
| 12C356-1 12C3561 | 1560-00-929-2291 | Support, Structural Component, Air | Aircraft Mission Design Series: F-111 | Lockheed Martin Corporation (81755) | |
| 12C357-3 12C3573 | 1560-00-081-2577 | Tie Assembly, Frame, Rudder Feel | General Characteristics Item Description: Aluminum alloy, 7075-T73, QQ-A-367, applicable to F111 acft | Lockheed Martin Corporation (81755) | |
| 12C358-1 12C3581 | 1560-00-929-2292 | Support, Structural Component, Air | Aircraft Mission Design Series: F-111 | Lockheed Martin Corporation (81755) | |
| 12C360-10 12C36010 | 1560-00-929-2293 | Support, cable Guard | III End Item Identification: Aircraft model F-111 General Characteristics Item Description: 1.600 in. W, 1.500 in. H | Lockheed Martin Corporation (81755) | |
| 12C360-13 12C36013 | 1560-00-405-1116 | Support, Structural Component, Air | Aircraft Mission Design Series: F-4 Special Features: U/a: cable guard support Overall Width: 1.600 inches nominal | Lockheed Martin Corporation (81755) | |
| 12C360-15 12C36015 | 1560-00-405-1116 | Support, Structural Component, Air | Aircraft Mission Design Series: F-4 Special Features: U/a: cable guard support Overall Width: 1.600 inches nominal | Lockheed Martin Corporation (81755) | |
| 12C361-9 12C3619 | 1560-00-929-2295 | Clevis, Actuator, Variable Feel | III End Item Identification: Aircraft model F111 | Lockheed Martin Corporation (81755) | |
| 12C363-801 12C363801 | 1560-00-079-4878 | Feel Input, Bellcrank Assembly | III End Item Identification: Acft model F111 General Characteristics Item Description: C/O bellcrank 1 ea P/N 12C363-15, bushing 1 ea P/N 12C653-21, bearing 1 ea P/N C525KP4, sealant as required P/N P5026-2-2 | Lockheed Martin Corporation (81755) | |
| 12C365-11 12C36511 | 1560-00-929-9896 | Shaft, Geared, Tension | General Characteristics Item Description: Steel | Lockheed Martin Corporation (81755) | |
| 12C383-5 12C3835 | 1560-00-442-8818 | Link, Variable Feel, Rudder | III End Item Identification: Aircraft model F111 | Lockheed Martin Corporation (81755) | |
| 12C384-1 12C3841 | 1560-00-997-3634 | Support, Structural Component, Aircraft | Aircraft Mission Design Series: F-111 Overall Length: 2.500 inches nominal Overall Width: 1.434 inches nominal | Lockheed Martin Corporation (81755) | |
| 12C403-1 12C4031 | 1560-00-498-5217 | Strip, Rub, Controls | III End Item Identification: Aircraft model F111 General Characteristics Item Description: Aluminum alloy, QQ-A-250/11 comp 6061 cond T6, 1.600 in. O/a lg, 1.360 in. O/a W, 0.280 in. O/a thk | Lockheed Martin Corporation (81755) | |
| 12C407-5 12C4075 | 1560-00-114-2957 | Support, Structural Component, Air | Aircraft Mission Design Series: F-111 | Lockheed Martin Corporation (81755) | |
| 12C416-1 12C4161 | 1560-00-929-2297 | Bracket, Structural Component, Air | Aircraft Mission Design Series: F-111 Material Document and Classification: QQ-A-367 fed spec single material response | Lockheed Martin Corporation (81755) | |
| 12C418-3 12C4183 | 1560-00-088-2249 | Bracket, Structural Component, Air | Aircraft Mission Design Series: F-111 Aircraft Location: Pulley support bracket | Lockheed Martin Corporation (81755) | |
| 12C450-1 12C4501 | 1560-00-455-8310 | Lever, Aileron | III End Item Identification: Aircraft model F111 General Characteristics Item Description: Titanium alloy, MIL-T-9047 | Lockheed Martin Corporation (81755) |