Airframe Structural Components: 12S1702-3, 12S1710-21, 12S1714-9
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 12S1702-3 12S17023 | 1560-01-097-3874 | Door, Aircraft | Aircraft Mission Design Series: Acft model F111 Aircraft Station Number: Fs 385.0 to 460.55 Side FOR Which Designed: Left side | Lockheed Martin Corporation (81755) | |
| 12S1702-4 12S17024 | 1560-01-096-3322 | Door, Aircraft | Aircraft Mission Design Series: Acft model F-111F Aircraft Location: Pave tack weapons bay Side FOR Which Designed: Right side | Lockheed Martin Corporation (81755) | |
| 12S1702-77 12S170277 | 1560-01-108-8642 | Retainer | III End Item Identification: Acft model F111 General Characteristics Item Description: Aluminum alloy per QQ-A-250/5, 49.000 in. lg, 6.000 in. W, 0.032 in. thk | Lockheed Martin Corporation (81755) | |
| 12S1705-11 12S170511 | 1560-01-105-8313 | Support, Structural Component, Air | III End Item Identification: Acft model F-111F Special Features: Al alloy 2024-T851 per FMS-1010-T851, 3.000 in.thk, 13.000 in.W, 32.000 in.lg, used on fwd pave tack pod | Lockheed Martin Corporation (81755) | |
| 12S1706-9 12S17069 | 1560-01-105-8314 | Support, Structural Component, Air | III End Item Identification: Acft model F-111F Special Features: Al alloy 2024-T851 per FMS-1010-T851, 3.000 in.thk, 11.000 in.W, 37.656 in.lg, used on aft pave tack pod | Lockheed Martin Corporation (81755) | |
| 12S1708-7 12S17087 | 1560-01-080-0246 | Torque Tube, Pave, Tack Cradle | III End Item Identification: Pave tack ECP3278; F111F acft General Characteristics Item Description: Cres, AMS5629; passivated FINISH;15.350 in. lg; 1ST end 3.500 in. od; 2.870 in. id; 6.350 in. dia flange 0.2IN. W located 0.500 in. from 1ST end; 10 mtg holes 0.438 in. min 0.443 in. max dia evenly spaced on 5.000 in. boltcircle dia; 2ND end 3.250 in. dia; 2.875-12 unj class 3B thd 0.880 in. DEEP;55 external involute splines; 16/32 pitch fillet root side class 2 fit 4.760IN. lg; 3.500 in. dia located 2.230 in. from 2ND end | Lockheed Martin Corporation (81755) | |
| 12S1710-13 12S171013 | 1560-01-092-8300 | Fitting, Structural Component, Air | Aircraft Mission Design Series: F-111 Overall Length: 5.750 inches nominal Overall Width: 2.500 inches nominal | Lockheed Martin Corporation (81755) | |
| 12S1710-15 12S171015 | 1560-01-092-8301 | Fitting, Structural Component, Air | Aircraft Mission Design Series: F-111 Overall Length: 5.420 inches nominal Overall Width: 2.500 inches nominal | Lockheed Martin Corporation (81755) | |
| 12S1710-19 12S171019 | 1560-01-111-2042 | Support, Structural Component, Air | III End Item Identification: Acft model F111 Special Features: Material per FMS-0131, 6.000 in. lg, 3.000 in. W, 1.750 in. thk, used on pave tack cradle | Lockheed Martin Corporation (81755) | |
| 12S1710-21 12S171021 | 1560-01-111-2041 | Support, Structural Component, Air | III End Item Identification: Acft model F111 Special Features: Material per FMS-0131, 6.000 in. lg, 3.000 in. W, 1.75 in. thk, used on pave tack cradle | Lockheed Martin Corporation (81755) | |
| 12S1710-23 12S171023 | 1560-01-111-2042 | Support, Structural Component, Air | III End Item Identification: Acft model F111 Special Features: Material per FMS-0131, 6.000 in. lg, 3.000 in. W, 1.750 in. thk, used on pave tack cradle | Lockheed Martin Corporation (81755) | |
| 12S1714-1 12S17141 | 1560-01-097-0540 | Skin, Aircraft | Aircraft Mission Design Series: F-111F Aircraft Location: Inner pave tack cradle | Lockheed Martin Corporation (81755) | |
| 12S1714-11 12S171411 | 1560-01-109-1566 | Plate, Structural, Aircraft | Aircraft Mission Design Series: F-111 Material: Aluminum alloy Material Document and Classification: QQ-A-250/5 fed spec single material response | Lockheed Martin Corporation (81755) | |
| 12S1714-13 12S171413 | 1560-01-109-1567 | Plate, Structural, Aircraft | Aircraft Mission Design Series: F-111 Material: Aluminum alloy Material Document and Classification: QQ-A-250/5 fed spec single material response | Lockheed Martin Corporation (81755) | |
| 12S1714-21 12S171421 | 1560-01-108-8736 | Former, Aircraft | III End Item Identification: F-111 Material: Aluminum alloy Material Document and Classification: QQ-A-250/5 fed spec single material response | Lockheed Martin Corporation (81755) | |
| 12S1714-43 12S171443 | 1560-01-109-1569 | Plate, Structural, Aircraft | Aircraft Mission Design Series: F-111 Material: Aluminum alloy Material Document and Classification: QQ-A-250/5 fed spec single material response | Lockheed Martin Corporation (81755) | |
| 12S1714-45 12S171445 | 1560-01-109-3275 | Plate, Structural, Aircraft | Aircraft Mission Design Series: F-111 Material: Aluminum alloy Material Document and Classification: QQ-A-250/5 fed spec single material response | Lockheed Martin Corporation (81755) | |
| 12S1714-7 12S17147 | 1560-01-109-1576 | Skin, Aircraft | III End Item Identification: F-111 Material: Aluminum alloy Material Document and Classification: QQ-A-250/5 fed spec single material response | Lockheed Martin Corporation (81755) | |
| 12S1714-8 12S17148 | 1560-01-109-1577 | Skin, Aircraft | III End Item Identification: F-111 Material: Aluminum alloy Material Document and Classification: QQ-A-250/5 fed spec single material response | Lockheed Martin Corporation (81755) | |
| 12S1714-9 12S17149 | 1560-01-109-1565 | Plate, Structural, Aircraft | Aircraft Mission Design Series: F-111 Material: Aluminum alloy Material Document and Classification: QQ-A-250/5 fed spec single material response | Lockheed Martin Corporation (81755) |