Airframe Structural Components: 12L301-13, 12L344-4, 12L385-1
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 12L301-13 12L30113 | 1560-00-927-6636 | Bracket, Structural Component, Air | Aircraft Mission Design Series: F-111 Aircraft Location: Fairing support bracket Overall Length: 2.000 inches nominal | Lockheed Martin Corporation (81755) | |
| 12L301-14 12L30114 | 1560-00-927-6637 | Bracket, Structural Component, Air | Aircraft Mission Design Series: F-111 Aircraft Location: Fairing support bracket Overall Length: 2.000 inches nominal | Lockheed Martin Corporation (81755) | |
| 12L302-10 12L30210 | 1560-00-927-6639 | Brace, Fixed, Fairing | III End Item Identification: Aircraft model F111 General Characteristics Item Description: Aluminum alloy, QQ-A-601 | Lockheed Martin Corporation (81755) | |
| 12L302-9 12L3029 | 1560-00-927-6638 | Brace, Fixed, Fairing | III End Item Identification: Aircraft model F111 General Characteristics Item Description: Aluminum alloy, QQ-A-601 | Lockheed Martin Corporation (81755) | |
| 12L325-7 12L3257 | 1560-00-841-6575 | Spool, Valve Mechanism | General Characteristics Item Description: Steel, QQ-S-763, class 440C III FSC Application Data: Fuselage, airframe | Lockheed Martin Corporation (81755) | |
| 12L327-9 12L3279 | 1560-00-929-2243 | Link, Switch Contact | III End Item Identification: Aircraft model F111 General Characteristics Item Description: Steel, AMS5355, 2.030 in. O/a lg, 0.380 in. O/a W, 0.380 in. O/a H, two holes in line one end 0.250 in. min, 0.255 in. max dia, one hole other end 0.250 in. min, 0.255 in. max dia | Lockheed Martin Corporation (81755) | |
| 12L328-9 12L3289 | 1560-00-929-2244 | Link, Switch Mechanism | III End Item Identification: Aircraft model F111 General Characteristics Item Description: Steel, AMS5355, 2.510 in. O/a lg, 1.270 in. O/a W, 0.150 in. O/a thk | Lockheed Martin Corporation (81755) | |
| 12L339-7 12L3397 | 1560-00-243-7932 | Retainer, Spring rod | General Characteristics Item Description: Aluminum alloy, QQ-A-200/3, 1.250 in. dia, 0.460 in. min, 0.465 in. max id, 0.180 in. thk | Lockheed Martin Corporation (81755) | |
| 12L344-1 12L3441 | 1560-00-825-6629 | Beam, Support, Door, Main Landing g | General Characteristics Item Description: Aluminum alloy QQ-A-367, W/bushings | Lockheed Martin Corporation (81755) | |
| 12L344-3 12L3443 | 1560-00-438-9987 | Beam, Support, Door, Main Landing g | General Characteristics Item Description: Aluminum alloy QQ-A-367, W/bushing | Lockheed Martin Corporation (81755) | |
| 12L344-4 12L3444 | 1560-00-438-9991 | Beam, Support, Door, Main Landing g | General Characteristics Item Description: Aluminum alloy QQ-A-367, W/bushing | Lockheed Martin Corporation (81755) | |
| 12L347-1 12L3471 | 1560-00-074-3769 | Bracket, Structural Component, Air | Aircraft Mission Design Series: F-111 Aircraft Location: Main landing gear door bracket | Lockheed Martin Corporation (81755) | |
| 12L347-2 12L3472 | 1560-00-074-3777 | Bracket, Structural Component, Air | Aircraft Mission Design Series: F-111 Aircraft Location: Main landing gear door bracket | Lockheed Martin Corporation (81755) | |
| 12L354-21 12L35421 | 1560-00-481-4862 | Cam, Control, Door Postion | III End Item Identification: Acft model F-111 General Characteristics Item Description: Make from rough casting P/N 12L354-19, steel alloy per AMS-5355 17-4PH, 0.504 in. dia center hole, 1.150 in. oa W | Lockheed Martin Corporation (81755) | |
| 12L355-1 12L3551 | 1560-00-105-1719 | Link Assembly, Uplock, Main Landin | III End Item Identification: Acft model F111 General Characteristics Item Description: Aluminum alloy, 7075-T6, QQ-A-367, 6.450 in lg | Lockheed Martin Corporation (81755) | |
| 12L362-1 12L3621 | 1560-00-105-1721 | Beam, Uplock, Main Landing Gear | General Characteristics Item Description: Aluminum alloy QQ-A-367, 13.710 in. O/a lg, 3.875 in. O/a W, W/bushing | Lockheed Martin Corporation (81755) | |
| 12L362-3 12L3623 | 1560-00-105-1721 | Beam, Uplock, Main Landing Gear | General Characteristics Item Description: Aluminum alloy QQ-A-367, 13.710 in. O/a lg, 3.875 in. O/a W, W/bushing | Lockheed Martin Corporation (81755) | |
| 12L365-3 12L3653 | 1560-00-195-9517 | Hook Assembly, Uplock, Main Landin | General Characteristics Item Description: Steel, stock size, 8.000 in. lg, 8.000 in. W, 1.250 in. thk III FSC Application Data: Fuselage, airframe | Lockheed Martin Corporation (81755) | |
| 12L383-1 12L3831 | 1560-01-011-0393 | Support, Structural Component, Aircraft | III End Item Identification: Aircrat model F111 Special Features: Steel, MIL-S-8844, stock size, 5.000IN. lg, 2.400 in. W, 1.750 in. thk. | Lockheed Martin Corporation (81755) | |
| 12L385-1 12L3851 | 1560-01-011-0318 | Link Assembly, Support, Aft Door, m | III End Item Identification: Aircraft model F111 General Characteristics Item Description: Steel, MIL-S-8844, stock size, 10.100 in. lg, 1.500 in. dia | Lockheed Martin Corporation (81755) |