Airframe Structural Components: 12L215-7, 12L248-9, 12L267-1
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 12L215-7 12L2157 | 1560-00-184-5848 | Filler, Door Hinge Stop | General Characteristics Item Description: Glass laminate, FMS1024, mfr 81755, 3.000 in. lg, 2.420 in. W, 0.355 in. thk | Lockheed Martin Corporation (81755) | |
| 12L217-3 12L2173 | 1560-00-995-9574 | Fitting, Structural Component, Air | Aircraft Mission Design Series: F-111 Aircraft Location: Hinge release fitting Overall Length: 6.390 inches nominal | Lockheed Martin Corporation (81755) | |
| 12L219-3 12L2193 | 1560-00-958-4445 | Support, Structural Component, Air | Aircraft Mission Design Series: F-111 | Lockheed Martin Corporation (81755) | |
| 12L232-1 12L2321 | 1560-00-480-9502 | Bracket Assembly, Pivot | General Characteristics Item Description: 3.100 in. O/a lg, 2.125 in. O/a W, 1.200 in. O/a H | Lockheed Martin Corporation (81755) | |
| 12L242-9 12L2429 | 1560-00-958-0854 | Link, Valve Drive, Door | III End Item Identification: Acft model F111 General Characteristics Item Description: Steel cres 17-4PH per ams 5355, used on door main landing gear | Lockheed Martin Corporation (81755) | |
| 12L243-1 12L2431 | 1560-00-958-4446 | Support, Structural Component, Air | Aircraft Mission Design Series: F-111 | Lockheed Martin Corporation (81755) | |
| 12L244-1 12L2441 | 1560-00-958-4447 | Support, Structural Component, Aircraft | III End Item Identification: Aircraft model F111 Special Features: Aluminum alloy, AMS4260, 2.570 in.lg, 1.620 in. W, 2 holes 0.375 in. dia, 4 holes 0.245 in. dia | Lockheed Martin Corporation (81755) | |
| 12L244-801 12L244801 | 1560-00-247-1684 | Support, Structural Component, Air | Aircraft Mission Design Series: F-111 | Lockheed Martin Corporation (81755) | |
| 12L246-1 12L2461 | 1560-00-958-4448 | Bell Crank | Special Features: First arm end radius: 0.310 in. nominal; second arm end radius: 0.310 in. nominal; first arm thickness: 0.620 in. nominal; second arm thickness: 0.620 in. nominal; first arm slot depth: 0.690 in. nominal; first arm slot width: 0.130 in. nominal; second arm horizontal slot width: 0.130 in. nominal Material: Aluminum alloy Features Provided: Fulcrum bore and lubrication fitting accommodation | Lockheed Martin Corporation (81755) | |
| 12L246-3 12L2463 | 1560-00-102-5473 | Bell Crank | Material: Aluminum alloy Bore Diameter: 0.375 inches nominal Bore Length: 0.970 inches nominal | Lockheed Martin Corporation (81755) | |
| 12L248-9 12L2489 | 1560-00-920-2309 | Guide, Roller Mlg Uplock | III End Item Identification: Aircraft model F-111 General Characteristics Item Description: Steel, ams 5355 | Lockheed Martin Corporation (81755) | |
| 12L259-9 12L2599 | 1560-00-928-7662 | Arm, Switch Actuating | General Characteristics Item Description: Aluminum alloy, AMS4260, 2.300 in. lg, 1.490 in. W, 0.360 in. H, mtghole 0.506 in. min, 0.516 in. max dia | Lockheed Martin Corporation (81755) | |
| 12L262-11 12L26211 | 1560-00-767-8594 | Retainer, Nose Gear Uplock | General Characteristics Item Description: Bronze maganese, QQ-B-726, 2.350 in. lg, 1.000 in. W, 0.800 in. dia hole thru 1 end | Lockheed Martin Corporation (81755) | |
| 12L262-9 12L2629 | 1560-00-767-8594 | Retainer, Nose Gear Uplock | General Characteristics Item Description: Bronze maganese, QQ-B-726, 2.350 in. lg, 1.000 in. W, 0.800 in. dia hole thru 1 end | Lockheed Martin Corporation (81755) | |
| 12L265-1 12L2651 | 1560-01-012-5283 | Bracket Assembly, Door, Nose Landi | III End Item Identification: Aircraft model F111 General Characteristics Item Description: Aluminum alloy, MIL-A-21180, A356, T6 | Lockheed Martin Corporation (81755) | |
| 12L265-803 12L265803 | 1560-01-012-5283 | Bracket Assembly, Door, Nose Landi | III End Item Identification: Aircraft model F111 General Characteristics Item Description: Aluminum alloy, MIL-A-21180, A356, T6 | Lockheed Martin Corporation (81755) | |
| 12L265-805 12L265805 | 1560-01-012-5766 | Bracket Assembly, Door, Nose Landing Gear | III End Item Identification: Aircraft model F111 General Characteristics Item Description: Aluminum alloy, MIL-A-21180, A356, T6 | Lockheed Martin Corporation (81755) | |
| 12L266-13 12L26613 | 1560-00-131-9113 | Bracket, Door, Nose Landing | General Characteristics Item Description: Aluminum alloy, AMS4218 alloy A356 temper T6, 5.265 in. O/a lg, 2.417 in. O/a W, 2.100 in. O/a H | Lockheed Martin Corporation (81755) | |
| 12L266-17 12L26617 | 1560-00-131-9113 | Bracket, Door, Nose Landing | General Characteristics Item Description: Aluminum alloy, AMS4218 alloy A356 temper T6, 5.265 in. O/a lg, 2.417 in. O/a W, 2.100 in. O/a H | Lockheed Martin Corporation (81755) | |
| 12L267-1 12L2671 | 1560-00-723-3594 | Bracket Assembly, Actuating | General Characteristics Item Description: Aluminum alloy, QQ-A-367, 3.730 in. O/a lg, 2.820 in. O/a W | Lockheed Martin Corporation (81755) |