Airframe Structural Components: 12W9454-1, 12W9464-9, 12W949-1
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 12W9454-1 12W94541 | 1560-00-360-1534 | Stop, Translating Flap Track | General Characteristics Item Description: Copper alloy, QQ-C-390, 2.480 in. lg, 0.191 in. min, 0.196 in. max dia hole thru 1 place | Lockheed Martin Corporation (81755) | |
| 12W9454-15 12W945415 | 1560-01-141-3006 | Stop, Forward, Translating Track | III End Item Identification: Acft model F-111 General Characteristics Item Description: Al-bronze per QQ-B-671, located flap number 5 | Lockheed Martin Corporation (81755) | |
| 12W9454-16 12W945416 | 1560-01-141-3003 | Stop, Forward, Translating Track | Lockheed Martin Corporation (81755) | ||
| 12W9454-3 12W94543 | 1560-00-360-1534 | Stop, Translating Flap Track | General Characteristics Item Description: Copper alloy, QQ-C-390, 2.480 in. lg, 0.191 in. min, 0.196 in. max dia hole thru 1 place | Lockheed Martin Corporation (81755) | |
| 12W9454-5 12W94545 | 1560-00-360-1534 | Stop, Translating Flap Track | General Characteristics Item Description: Copper alloy, QQ-C-390, 2.480 in. lg, 0.191 in. min, 0.196 in. max dia hole thru 1 place | Lockheed Martin Corporation (81755) | |
| 12W9454-801 12W9454801 | 1560-00-360-1534 | Stop, Translating Flap Track | General Characteristics Item Description: Copper alloy, QQ-C-390, 2.480 in. lg, 0.191 in. min, 0.196 in. max dia hole thru 1 place | Lockheed Martin Corporation (81755) | |
| 12W9454-802 12W9454802 | 1560-00-360-1535 | Stop, Translating Flap Track | General Characteristics Item Description: Copper alloy, QQ-C-390, 2.480 in. lg, 0.191 in. min, 0.196 in. max dia hole thru 1 place | Lockheed Martin Corporation (81755) | |
| 12W9456-11 12W945611 | 1560-00-131-8881 | Plate, Guide, Track | General Characteristics Item Description: Aluminum bronze, QQ-C-450, 0.180 in. thk 1 side, 0.270 in. thk oppositeside, serrations 0.500 in. W on 1 side, 0.830 in. O/a W, 1.570 in. lg, 2HOLES drilled thru 0.312 in. min. 0.320 max dia, 0.750 in.apart in LINE0.530 in. from side beginning 0.410 in. from end | Lockheed Martin Corporation (81755) | |
| 12W9459-9 12W94599 | 1560-00-934-1071 | Plate, Structural, Aircraft | Aircraft Mission Design Series: F-111 Special Features: U/a:plate, guide, track NO.3;MATL: alum bronze;c/o: 2 holes drilled thru 0.191IN min, 0.199IN max dia, in line 0.380IN from end Material Document and Classification: QQ-C-450 fed spec single material response | Lockheed Martin Corporation (81755) | |
| 12W946-11 12W94611 | 1560-00-575-9164 | Cover, Access, Aircraft | Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-250/4, T81 fed spec single material response Securing Device Type: Threaded fastener | Lockheed Martin Corporation (81755) | |
| 12W9462-9 12W94629 | 1560-00-131-8894 | Guide, Upper Flap Track | General Characteristics Item Description: Aluminum bronze alloy, QQ-C-390, 1.410 in. lg, 0.760 in. W, 0.234 in. min, 0.242 in. max dia hole thru 2 places | Lockheed Martin Corporation (81755) | |
| 12W9463-9 12W94639 | 1560-00-130-9708 | Guide, Flap Track | General Characteristics Item Description: 1.420 in. lg, 0.880 in. W, 0.140 in. thk, 2 mtgholes 0.191 in. min, 0.199 in. max dia couterbored 0.410 in. dia 0.040 deep | Lockheed Martin Corporation (81755) | |
| 12W9464-9 12W94649 | 1560-00-131-8896 | Guide, Lower Flap Track | General Characteristics Item Description: Aluminum bronze alloy, QQ-C-390, 1.420 in. lg, 1.010 in. W, 0.191 in. min, 0.199 in. max dia hole thru 2 places | Lockheed Martin Corporation (81755) | |
| 12W9469-11 12W946911 | 1560-00-927-6266 | Support, Structural Component, Air | III End Item Identification: Acft model F111 Special Features: Steel, ams 5355, 17-4PH, 41.800 in. lg, 10.000 in. W, 1 hole 0.312 in. dia, 2 holes 0.191 in. min, 0.196 in. max dia, 1 hole 0.437 in. dia | Lockheed Martin Corporation (81755) | |
| 12W9469-12 12W946912 | 1560-00-927-6273 | Support, Structural Component, Aircraft | III End Item Identification: Acft model F111 Special Features: Steel, ams 5355, 17-4PH, 41.800 in. lg, 10.000 in. W, 1 hole 0.312 in. dia, 2 holes 0.191 in. min, 0.196 in. max dia, 1 hole 0.437 in. dia | Lockheed Martin Corporation (81755) | |
| 12W9470-11 12W947011 | 1560-00-927-6281 | Support, Structural Component, Air | III End Item Identification: Acft model F111 Special Features: Steel, ams 5355, 17-4PH, 4.180 in. lg, 1.000 in. W, 2 holes 0.312 in. dia, 2 holes 0.191 in. min, 0.196 in. max dia, 1 hole 0.437 in. dia | Lockheed Martin Corporation (81755) | |
| 12W9470-12 12W947012 | 1560-00-927-6287 | Support, Structural Component, Air | III End Item Identification: Acft model F111 Special Features: Steel, ams 5355, 17-4PH, 4.180 in. lg, 1.000 in. W, 2 holes 0.312 in. dia, 2 holes 0.191 in. min, 0.196 in. max dia, 1 hole 0.437 in. dia | Lockheed Martin Corporation (81755) | |
| 12W948-3 12W9483 | 1560-00-970-6001 | Cover, Access | Material: Aluminum alloy 2024 Material Document AND Classification: QQ-A-250/4, T81 fed spec single material response Hole Diameter: 0.257 inches minimum and 0.262 inches maximum | Lockheed Martin Corporation (81755) | |
| 12W948-4 12W9484 | 1560-00-970-6002 | Cover, Access | Lockheed Martin Corporation (81755) | ||
| 12W949-1 12W9491 | 1560-00-980-8892 | Cover, Access | Lockheed Martin Corporation (81755) |