Airframe Structural Components: 12B9680-3, 12C103-805, 12C103-811
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 12B9680-3 12B96803 | 1560-00-941-1258 | Torque Tube, Door | General Characteristics Item Description: 5.467 in. lg, 0.750 in. tube dia, 1.937 in. W end flanges, 4 mtg HOLES0.129 in. min, 0.133 in. max dia | Lockheed Martin Corporation (81755) | |
| 12B9696-1 12B96961 | 1560-00-758-1094 | Plate, Structural, Aircraft | Aircraft Mission Design Series: F-111 | Lockheed Martin Corporation (81755) | |
| 12B9697-10 12B969710 | 1560-00-928-7683 | Bushing, Ventral Fairing | Lockheed Martin Corporation (81755) | ||
| 12B9697-9 12B96979 | 1560-00-928-7684 | Bushing, Ventral Fairing | General Characteristics Item Description: Aluminum alloy 2024, QQ-A-200/3, 0.718 in. greater od, beveled surface, 0.358 in. min, 0.365 in. max id bore | Lockheed Martin Corporation (81755) | |
| 12B9718-7 12B97187 | 1560-00-929-2357 | Retainer, Trunnion Lug | III End Item Identification: Aircraft model F111 General Characteristics Item Description: 3.437 in. od, tap 3.000-16 UNF3B in. thd, 0.625 in. thk | Lockheed Martin Corporation (81755) | |
| 12B9722-1 12B97221 | 1560-00-928-7685 | Bushing Assembly, Clamp | General Characteristics Item Description: Aluminum alloy 2024-T851, QQ-A-250/4, 1.200 in. lg, 0.750 in. W, 0.055 in. min, 0.065 in. max plate thk, 0.375 in. bushing od, 0.152 in. min, 0.157 in. max bushing protrusion | Lockheed Martin Corporation (81755) | |
| 12B9722-803 12B9722803 | 1560-00-400-9410 | Bushing Assembly, Clamp up | III End Item Identification: Acft model F111 General Characteristics Item Description: C/O bushing 1 ea P/N 12B9722-13, nut plate 1 ea P/N NAS697A3, rivet as required P/N C088-3 | Lockheed Martin Corporation (81755) | |
| 12B9722-9 12B97229 | 1560-00-119-2863 | Bushing Assembly, Clamp | General Characteristics Item Description: Aluminum alloy 2024-T851, QQ-A-250/4, 1.200 in. lg, 0.750 in. W, 0.055 in. min, 0.065 in. max plate thk, 0.375 in. bushing od, 0.076 in. min, 0.081 in. max bushing protrusion | Lockheed Martin Corporation (81755) | |
| 12B9738-7 12B97387 | 1560-00-928-7686 | Pin, Taper Coupling | General Characteristics Item Description: Steel, MIL-S-5000, 2.148 in. lg, 0.876 in. id | Lockheed Martin Corporation (81755) | |
| 12B9740-7 12B97407 | 1560-00-929-2256 | Pin, Coupling, Fuselage | General Characteristics Item Description: Steel, MIL-S-5000, stock size 1.375 dia by 2.000 in. | Master Spline Tool and Gage Co. (12150) | |
| 12B9747-1 12B97471 | 1560-00-997-3691 | Cover, Access | Lockheed Martin Corporation (81755) | ||
| 12B9747-11 12B974711 | 1560-00-825-6556 | Cover, Access | Material: Aluminum alloy 2024 Material Document AND Classification: QQ-A-250/4 fed spec single material response Hole Diameter: 0.127 inches minimum and 0.133 inches maximum | Lockheed Martin Corporation (81755) | |
| 12B9764-7 12B97647 | 1560-00-929-2310 | PIN, Connection, Fuselage | General Characteristics Item Description: Steel, FMS-1012, stock size 0.750 dia by 2.000 in. | Lockheed Martin Corporation (81755) | |
| 12B9819-7 12B98197 | 1560-01-293-5501 | Plate, Structural, Aircraft | Aircraft Mission Design Series: F-111 Aircraft Location: Stiffener hook | Lockheed Martin Corporation (81755) | |
| 12BB11086-526 12BB11086526 | 1560-01-366-0864 | Track Assembly, Fuselage, Forward | III End Item Identification: Aircraft, hawkeye E-2C General Characteristics Item Description: 4130 steel, 0.050 in. thk, 3.000 in. W, 23.000 in. lg; R-H side | Northrop Grumman Systems Corporation (26512,61174) | |
| 12C102-3 12C1023 | 1560-00-102-0067 | Support Assembly, Elevator | III End Item Identification: Aircraft model F111 | Lockheed Martin Corporation (81755) | |
| 12C102-5 12C1025 | 1560-00-102-0067 | Support Assembly, Elevator | III End Item Identification: Aircraft model F111 | Lockheed Martin Corporation (81755) | |
| 12C103-805 12C103805 | 1560-00-450-2594 | Support, Structural Component, Aircraft | III End Item Identification: Aircraft model F111 Special Features: Aluminum alloy, QQ-A-367 | Lockheed Martin Corporation (81755) | |
| 12C103-809 12C103809 | 1560-00-102-0070 | Support, Structural Component, Aircraft | III End Item Identification: Aircraft model F111 Special Features: Aluminum alloy, QQ-A-367; | Lockheed Martin Corporation (81755) | |
| 12C103-809 12C103809 | 1560-00-450-2594 | Support, Structural Component, Aircraft | III End Item Identification: Aircraft model F111 Special Features: Aluminum alloy, QQ-A-367 | Lockheed Martin Corporation (81755) | |
| 12C103-811 12C103811 | 1560-00-450-2594 | Support, Structural Component, Aircraft | III End Item Identification: Aircraft model F111 Special Features: Aluminum alloy, QQ-A-367 | Lockheed Martin Corporation (81755) |