Airframe Structural Components: 12B13960-14, 12B13960-9, 12B2017-9
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 12B13960-14 12B1396014 | 1560-01-247-4331 | Former, Aircraft | Aircraft Mission Design Series: F-111 Material: Steel comp 321 Aircraft Location: Center body | Lockheed Martin Corporation (81755) | |
| 12B13960-7 12B139607 | 1560-01-247-4338 | Former, Aircraft | Aircraft Mission Design Series: F-111 Material: Steel comp 321 Aircraft Location: Center body | Lockheed Martin Corporation (81755) | |
| 12B13960-8 12B139608 | 1560-01-247-4337 | Former, Aircraft | Aircraft Mission Design Series: F-111 Material: Steel comp 321 Aircraft Location: Center body | Lockheed Martin Corporation (81755) | |
| 12B13960-9 12B139609 | 1560-01-247-4336 | Former, Aircraft | Aircraft Mission Design Series: F-111 Material: Steel comp 321 Aircraft Location: Center body | Lockheed Martin Corporation (81755) | |
| 12B13964-1 12B139641 | 1560-00-125-0616 | Retainer, Door Seal | Lockheed Martin Corporation (81755) | ||
| 12B13965-1 12B139651 | 1560-00-125-0628 | Retainer, Door Seal | General Characteristics Item Description: Aluminum alloy 2024-T6, QQ-A-250/4, 0.040 in. matl thk, integral stiffener | Lockheed Martin Corporation (81755) | |
| 12B1735-17 12B173517 | 1560-01-231-6343 | Plate, Structural, Aircraft | Lockheed Martin Corporation (81755) | ||
| 12B179-1 12B1791 | 1560-00-410-0954 | Pad, Support, Structural | General Characteristics Item Description: Cres, 17-4PH, 2.500 in. lg, 0.990 in. min, 1.020 in. max W, 0.125 in. thk base, 0.315 in. H, 0.495 in. min, 0.510 in. max od boss W/insert | Lockheed Martin Corporation (81755) | |
| 12B183-1 12B1831 | 1560-00-186-0343 | Support, Structural Component, Air | Aircraft Mission Design Series: F-111 Aircraft Location: Inbd vertical load support Aircraft Station Number: Sta 370.00 | Lockheed Martin Corporation (81755) | |
| 12B1893 | 1560-01-087-8964 | Pin Overwing, Longeron | III End Item Identification: F-111 acft General Characteristics Item Description: Fs 449, 3.600 in. lg | Lockheed Martin Corporation (81755) | |
| 12B1893-7 12B18937 | 1560-01-087-8964 | Pin Overwing, Longeron | III End Item Identification: F-111 acft General Characteristics Item Description: Fs 449, 3.600 in. lg | Bazile Machining Co. (2U262) Lockheed Martin Corporation (81755) Master Research & Manufacturing Inc. (9U245) Streetman Precision Inc. (5Y249) | |
| 12B1897-5 12B18975 | 1560-01-373-2731 | Fitting, Structural Component, Air | Aircraft Mission Design Series: F-111 Special Features: Longeron, splice assembly Material: Steel | Lockheed Martin Corporation (81755) | |
| 12B1899-1 12B18991 | 1560-00-887-2447 | Pad Assembly, Hinged | General Characteristics Item Description: Aluminum alloy support, QQ-A-250/5-T62, O/a dim. 0.080 by 3.00 by 7.00IN. | Lockheed Martin Corporation (81755) | |
| 12B1899-2 12B18992 | 1560-00-887-2450 | Pad Assembly, Hinged | General Characteristics Item Description: Aluminum alloy support, QQ-A-250/5-T62, O/a dim. 0.080 by 3.00 by 7.00IN. | Lockheed Martin Corporation (81755) | |
| 12B2011-45 12B201145 | 1560-00-342-2121 | Bulkhead, Aircraft | Aircraft Mission Design Series: F-111 Material: Aluminum alloy 2024 Aircraft Location: Fuselage canted bulkhead | Lockheed Martin Corporation (81755) | |
| 12B2014-801 12B2014801 | 1560-01-315-0429 | ROD Assembly, Radome Lock | III End Item Identification: F-111A, F-111D, F-111E, F-111F, EF-111A, FB-111A General Characteristics Item Description: 1.25 in. dia, 28.70 in. LG;2024-T3 WW-T-700/3-T3;TO. 1F-F111A-4-1-49;USED to hold radome in open position | Lockheed Martin Corporation (81755) | |
| 12B2014-803 12B2014803 | 1560-00-118-0910 | ROD Assembly, Radome Lock | General Characteristics Item Description: Aluminum alloy, WW-T-700/3 | Lockheed Martin Corporation (81755) | |
| 12B2014-805 12B2014805 | 1560-01-315-0429 | ROD Assembly, Radome Lock | III End Item Identification: F-111A, F-111D, F-111E, F-111F, EF-111A, FB-111A General Characteristics Item Description: 1.25 in. dia, 28.70 in. LG;2024-T3 WW-T-700/3-T3;TO. 1F-F111A-4-1-49;USED to hold radome in open position | Lockheed Martin Corporation (81755) | |
| 12B2017-13 12B201713 | 1560-00-127-4159 | Support, Structural Component, Air | Aircraft Mission Design Series: F-111 | Lockheed Martin Corporation (81755) | |
| 12B2017-9 12B20179 | 1560-00-837-5054 | Support, Radome Lock | General Characteristics Item Description: Aluminum alloy, QQ-A-225-6 | Lockheed Martin Corporation (81755) |