Airframe Structural Components: 12B2935-13, 12B2973-11, 12B3055-7
MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
---|---|---|---|---|---|
12B2935-13 12B293513 | 1560-00-436-7985 | Door, Access, Aircraft | Material: Aluminum alloy 2024 Securing Device Type: Hinge FSC Application Data: Fuselage sections, airframe | Lockheed Martin Corporation (81755) | |
12B2937-1 12B29371 | 1560-00-762-8425 | Door, Access, Aircraft | Material: Aluminum alloy A356.0 Material Document and Classification: QQ-A-596 fed spec single material response Securing Device Type: Flush catch and hinge | Lockheed Martin Corporation (81755) | |
12B2937-3 12B29373 | 1560-00-762-8425 | Door, Access, Aircraft | Material: Aluminum alloy A356.0 Material Document and Classification: QQ-A-596 fed spec single material response Securing Device Type: Flush catch and hinge | Lockheed Martin Corporation (81755) | |
12B2964-10 12B296410 | 1560-00-360-1536 | Beam, Upper Fairing | General Characteristics Item Description: Aluminum alloy, 2024-T6, QQ-A-250-5 | Lockheed Martin Corporation (81755) | |
12B2964-9 12B29649 | 1560-00-360-1537 | Beam, Upper Fairing | General Characteristics Item Description: Aluminum alloy, 2024-T6, QQ-A-250-5 | Lockheed Martin Corporation (81755) | |
12B2968-3 12B29683 | 1560-00-137-4004 | Support, Structural Component, Aircraft | III End Item Identification: Acft model F-111 Special Features: C/O ar rivets P/N C089-6, ar rivets P/N C086-6, beam P/N 12B2968-9, stiffener P/N 12B2968-7; beam matl aluminum alloy QQ-A-250/5-T62, 32.0 in. lg, 6.0 in. W, 0.071 in. thk; stiffener matl aluminum alloy QQ-A-250/-5-T62, 22.0IN. lg, 2.0 in. W, 0.100 in. thk | Lockheed Martin Corporation (81755) | |
12B2968-4 12B29684 | 1560-00-242-1818 | Support, Structural Component, Air | Aircraft Mission Design Series: F-111 | Lockheed Martin Corporation (81755) | |
12B2969-1 12B29691 | 1560-00-409-2702 | Support, Fairing | General Characteristics Item Description: Aluminum alloy casting AMS-4260, 3.19 in. lg 1.060 in. W, 0.230 in. thk | Lockheed Martin Corporation (81755) | |
12B2969-3 12B29693 | 1560-00-184-5844 | Support, Structural Component, Aircraft | Aircraft Mission Design Series: F-111 Overall Length: 3.190 inches nominal Overall Width: 1.060 inches nominal | Lockheed Martin Corporation (81755) | |
12B2970-1 12B29701 | 1560-00-237-9562 | Support, Structural Component, Air | Aircraft Mission Design Series: F-111 Overall Length: 3.360 inches nominal Overall Width: 1.000 inches nominal | Lockheed Martin Corporation (81755) | |
12B2971-1 12B29711 | 1560-00-190-4274 | Support, Structural Component, Air | Aircraft Mission Design Series: F-111 Overall Length: 4.000 inches nominal Overall Width: 1.260 inches nominal | Lockheed Martin Corporation (81755) | |
12B2972-801 12B2972801 | 1560-00-405-3166 | Bracket Assembly, Fairing Support | III End Item Identification: Acft model F-111 General Characteristics Item Description: Make foam casting P/N 12B2972-7, cres steel per AMS-5355 17-4PH, also requirers liner P/N 12B2972-21 and adhesive 12B2972-23 per FMS-1097 | Lockheed Martin Corporation (81755) | |
12B2973-11 12B297311 | 1560-00-236-7378 | Bracket, Structural Component, Air | Lockheed Martin Corporation (81755) | ||
12B2973-7 12B29737 | 1560-00-236-7385 | Bracket, Structural Component, Air | Aircraft Mission Design Series: F-111 Aircraft Location: Upper glove support bracket | Lockheed Martin Corporation (81755) | |
12B2973-8 12B29738 | 1560-00-137-4005 | Bracket, Upper Glove Support | III End Item Identification: Acft model F111 General Characteristics Item Description: 1.700 in. lg | Lockheed Martin Corporation (81755) | |
12B3012-9 12B30129 | 1560-00-997-7562 | Spacer, Cover, Antenna | General Characteristics Item Description: Aluminum alloy, QQ-A-250/5, 0.090 in. thk | Lockheed Martin Corporation (81755) | |
12B3041-801 12B3041801 | 1560-00-997-3750 | Door, Access, Aircraft | Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-250/5 fed spec single material response Securing Device Type: Flush catch and hinge | Lockheed Martin Corporation (81755) | |
12B3045-801 12B3045801 | 1560-00-411-7259 | Skin, Aircraft | Material: Aluminum alloy 2024 Aircraft Location: Wing, airframe Material Document and Classification: QQ-A-250/5-T81 fed spec single material response | Lockheed Martin Corporation (81755) | |
12B3048-9 12B30489 | 1560-00-188-5344 | Support, Structural Component, Air | Aircraft Mission Design Series: F-111 Overall Length: 7.340 inches nominal Overall Width: 6.970 inches nominal | Lockheed Martin Corporation (81755) | |
12B3055-7 12B30557 | 1560-00-411-7259 | Skin, Aircraft | Material: Aluminum alloy 2024 Aircraft Location: Wing, airframe Material Document and Classification: QQ-A-250/5-T81 fed spec single material response | Lockheed Martin Corporation (81755) |