Airframe Structural Components: 12W952-12, 12W9560-3, 12W9563-29
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 12W952-12 12W95212 | 1560-00-369-6694 | Fairing, Aircraft | III End Item Identification: F-100 | Lockheed Martin Corporation (81755) | |
| 12W952-9 12W9529 | 1560-00-369-6696 | Fairing, Aircraft | III End Item Identification: F-111 | Lockheed Martin Corporation (81755) | |
| 12W953-7 12W9537 | 1560-00-369-6697 | Fairing, Aircraft | III End Item Identification: F-111 | Lockheed Martin Corporation (81755) | |
| 12W953-8 12W9538 | 1560-00-369-6698 | Fairing, Aircraft | III End Item Identification: F-111 | Lockheed Martin Corporation (81755) | |
| 12W9540-10 12W954010 | 1560-00-842-3253 | CAM, Airflow Deflector | General Characteristics Item Description: Steel MIL-S-5000, 3.00 in. lg, 0.95 in. W, 0.69 in. H | Lockheed Martin Corporation (81755) | |
| 12W9540-9 12W95409 | 1560-00-227-9129 | Cam, Airflow Deflector | General Characteristics Item Description: Steel MIL-S-5000, 3.00 in. lg, 0.95 in. W, 0.69 in. H | Lockheed Martin Corporation (81755) | |
| 12W9541-10 12W954110 | 1560-00-199-5404 | Cam, Airflow Deflector | III End Item Identification: Acft model F-111 General Characteristics Item Description: Cres steel 17-4PH per AMS-5355, make from casting P/N 12W9541-8, irregular shape, used for NO.3 deflection | Lockheed Martin Corporation (81755) | |
| 12W9541-11 12W954111 | 1560-00-199-5403 | Cam, Airflow Deflector | General Characteristics Item Description: Steel MIL-S-5000, 3.00 in. lg, 0.71 in. H | Lockheed Martin Corporation (81755) | |
| 12W9541-12 12W954112 | 1560-00-199-5404 | Cam, Airflow Deflector | III End Item Identification: Acft model F-111 General Characteristics Item Description: Cres steel 17-4PH per AMS-5355, make from casting P/N 12W9541-8, irregular shape, used for NO.3 deflection | Lockheed Martin Corporation (81755) | |
| 12W9541-9 12W95419 | 1560-00-199-5403 | Cam, Airflow Deflector | General Characteristics Item Description: Steel MIL-S-5000, 3.00 in. lg, 0.71 in. H | Lockheed Martin Corporation (81755) | |
| 12W9542-10 12W954210 | 1560-00-369-6764 | Cam, Airflow Deflector | General Characteristics Item Description: Steel MIL-S-5000, 3.22 in. lg, 0.92 in. H | Lockheed Martin Corporation (81755) | |
| 12W9542-11 12W954211 | 1560-00-369-6767 | Cam, Airflow Deflector | General Characteristics Item Description: Steel MIL-S-5000, 3.22 in. lg, 0.92 in. H, two oblong mounting holes | Lockheed Martin Corporation (81755) | |
| 12W9542-12 12W954212 | 1560-00-369-6764 | Cam, Airflow Deflector | General Characteristics Item Description: Steel MIL-S-5000, 3.22 in. lg, 0.92 in. H | Lockheed Martin Corporation (81755) | |
| 12W9542-9 12W95429 | 1560-00-369-6767 | Cam, Airflow Deflector | General Characteristics Item Description: Steel MIL-S-5000, 3.22 in. lg, 0.92 in. H, two oblong mounting holes | Lockheed Martin Corporation (81755) | |
| 12W9550-12 12W955012 | 1560-01-186-2897 | Former, Aircraft | III End Item Identification: Acft model F-111 | Lockheed Martin Corporation (81755) | |
| 12W9550-9 12W95509 | 1560-01-245-4959 | Former, Aircraft | Aircraft Mission Design Series: F-11A/FB/D/E/C/EF Material: Aluminum alloy 2024 Aircraft Location: Frame-airflow deflector, no. 1 | Lockheed Martin Corporation (81755) | |
| 12W9560-1 12W95601 | 1560-00-476-4349 | Stop, Flap Track No. 2 | General Characteristics Item Description: Aluminum alloy, QQ-A-250/4, alloy 2024, T851, stock size, 2.000 in. lg, 2.000 in. W, 0.500 in. thk III FSC Application Data: Flap, wing, airframe | Lockheed Martin Corporation (81755) | |
| 12W9560-2 12W95602 | 1560-00-104-9764 | Stop, Flap Track NO.2 | General Characteristics Item Description: Aluminum alloy, QQ-A-268, alloy 2024, T851, stock size, 2.000 in. lg, 1.000 in. W, 0.500 in. thk III FSC Application Data: Flap, wing, airframe | Lockheed Martin Corporation (81755) | |
| 12W9560-3 12W95603 | 1560-00-476-4349 | Stop, Flap Track No. 2 | General Characteristics Item Description: Aluminum alloy, QQ-A-250/4, alloy 2024, T851, stock size, 2.000 in. lg, 2.000 in. W, 0.500 in. thk III FSC Application Data: Flap, wing, airframe | Lockheed Martin Corporation (81755) | |
| 12W9563-29 12W956329 | 1560-01-136-9327 | Trailing Edge, Aircraft | Aircraft Mission Design Series: F-111 Overall Length: 56.080 inches nominal Overall Width: 0.250 inches nominal | Lockheed Martin Corporation (81755) |