Airframe Structural Components: 12W9407-18, 12W943-803, 12W945-3
MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
---|---|---|---|---|---|
12W9407-18 12W940718 | 1560-00-106-9148 | Lever, Actuation, Vane | General Characteristics Item Description: Cres 17-4PH, ams 5355, 0.439 in. id, 0.312 in. lg pivot hole 1ST end, 0.220 in. thk arm, angled clevis 2ND end, 0.500 in. od, 0.440 in. lg, 0.302 in. min, 0.317 in. max id intermediate boss lug, 2.500 in. C to C W 1ST end hole | Lockheed Martin Corporation (81755) | |
12W9408-13 12W940813 | 1560-00-754-7561 | Lever, Actuation, Van | Lockheed Martin Corporation (81755) | ||
12W9408-14 12W940814 | 1560-00-754-7562 | Lever, Actuation, Vane | General Characteristics Item Description: Cres 17-4PH, ams 5355, 0.439 in. id pivot hole on 0.182 in. lg, 0.560 in. od hub 1ST end, 0.220 in. thk arm, angled clevis 2ND end, 0.420 in. lg, 0.500 in. od, 0.302 in. min, 0.317 in. max id lug 0.312 in. from base of clevis | Lockheed Martin Corporation (81755) | |
12W9409-21 12W940921 | 1560-00-131-8976 | Lever, Actuation, Vane | III End Item Identification: Aircraft model F111 | Lockheed Martin Corporation (81755) | |
12W9411-13 12W941113 | 1560-00-125-0572 | Lever, Actuation, Vane | III End Item Identification: Aircraft model F111 | Lockheed Martin Corporation (81755) | |
12W9411-15 12W941115 | 1560-00-125-0572 | Lever, Actuation, Vane | III End Item Identification: Aircraft model F111 | Lockheed Martin Corporation (81755) | |
12W9414-15 12W941415 | 1560-00-131-0097 | Bracket, Structural Component, Aircraft | Lockheed Martin Corporation (81755) | ||
12W9414-16 12W941416 | 1560-00-131-0098 | Bracket, Structural Component, Aircraft | Lockheed Martin Corporation (81755) | ||
12W941-5 12W9415 | 1560-00-997-3581 | Cover, Access | Lockheed Martin Corporation (81755) | ||
12W9418-13 12W941813 | 1560-00-927-6242 | Support, Structural Component, Air | III End Item Identification: Acft model F111 Special Features: Steel, ams 5355, 17-4PH, 2.920 in. lg, 0.920 in. W, 0.720 in. H, 2 holes 0.312 in. dia, 1 hole 0.437 in. dia | Lockheed Martin Corporation (81755) | |
12W9418-15 12W941815 | 1560-00-888-9856 | Support, Structural Component, Air | III End Item Identification: Acft model F111 Special Features: Steel, ams 5355, 17-4PH, 2.920 in. lg, 0.920 in. W, 0.720 in. H, 2 holes 0.312 in. dia, 1 hole 0.437 in. dia | Lockheed Martin Corporation (81755) | |
12W9423-9 12W94239 | 1560-00-865-5127 | Spacer, Flap Track Carriage | General Characteristics Item Description: Aluminum alloy, QQ-A-250/4, 4.020 in. lg, 0.890 in. W, 0.196 in. min, 0.204 in. max dia hole thru 4 places | Lockheed Martin Corporation (81755) | |
12W942-801 12W942801 | 1560-00-079-4786 | Cover Assembly, Pylon | III End Item Identification: Aircraft model no. F-111 | Lockheed Martin Corporation (81755) | |
12W943-23 12W94323 | 1560-00-369-6691 | Stiffener, Aircraft | Lockheed Martin Corporation (81755) | ||
12W943-24 12W94324 | 1560-00-369-6712 | Stiffener, Aircraft | Lockheed Martin Corporation (81755) | ||
12W9434-10 12W943410 | 1560-01-212-4041 | Support, Structural Component, Air | Lockheed Martin Corporation (81755) | ||
12W943-803 12W943803 | 1560-00-190-4279 | Cover, Access, Aircraft | Securing Device Type: Threaded fastener FSC Application Data: Wing, airframe Features Provided: Observation facility | Lockheed Martin Corporation (81755) | |
12W944-3 12W9443 | 1560-00-980-8874 | Cover, Access | Material: Aluminum alloy 2024 Material Document AND Classification: QQ-A-250/4, T851 fed spec single material response Length: 9.090 inches nominal | Lockheed Martin Corporation (81755) | |
12W9443-9 12W94439 | 1560-00-252-0699 | Guide, Translating Track | General Characteristics Item Description: Aluminum bronze alloy | Lockheed Martin Corporation (81755) | |
12W945-3 12W9453 | 1560-00-837-4916 | Cover, Access | Lockheed Martin Corporation (81755) |