Airframe Structural Components: 12W8910-816, 12W8989-7, 12W8991-11
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 12W8910-816 12W8910816 | 1560-00-083-0790 | Flap, Wing Landing | Aircraft Mission Design Series: F-111 Aircraft Location: Auxiliary flap assembly | Lockheed Martin Corporation (81755) | |
| 12W8910-819 12W8910819 | 1560-00-083-0787 | Flap, Wing Landing | Aircraft Mission Design Series: F-111 Aircraft Location: Auxiliary flap assembly | Lockheed Martin Corporation (81755) | |
| 12W8910-820 12W8910820 | 1560-00-083-0790 | Flap, Wing Landing | Aircraft Mission Design Series: F-111 Aircraft Location: Auxiliary flap assembly | Lockheed Martin Corporation (81755) | |
| 12W8914-1 12W89141 | 1560-00-767-8174 | Stop, Flap Track | General Characteristics Item Description: Aluminum alloy, QQ-A-250/4, alloy 2024-T851 III FSC Application Data: Wing, airframe | Lockheed Martin Corporation (81755) | |
| 12W8950-1 12W89501 | 1560-00-967-4370 | Filler, Auxiliary Flap | III End Item Identification: Aircraft model F111 General Characteristics Item Description: Plastic sponge, dacron fabric covered | Lockheed Martin Corporation (81755) | |
| 12W8950-2 12W89502 | 1560-00-967-4371 | Filler, Auxiliary Flap | III End Item Identification: Aircraft model F111 General Characteristics Item Description: Plastic sponge, dacron fabric covered | Lockheed Martin Corporation (81755) | |
| 12W8962-819 12W8962819 | 1560-00-460-1503 | Track Assembly, Outboard | III End Item Identification: Acft model F-111 General Characteristics Item Description: Aluminum alloy plate per FMS-10102024-T851, 38.0 in. stock lg, 11.0 in.stock W, 3.375 in. stock thk, make FR0M track P/N 12W8962-45, rub strip P/N 12W8962-33, coating P/N 12W8962-15 PERFMS-1027, use on auxilary flap | Lockheed Martin Corporation (81755) | |
| 12W8962-820 12W8962820 | 1560-00-460-1504 | Track Assembly, Outboard | III End Item Identification: Acft model F-111 General Characteristics Item Description: Aluminum alloy plate per FMS-10102024-T851, 38.0 in. stock lg, 11.0 in.stock W, 3.375 in. stock thk, make from track P/N 12W8962-46, rub strip P/N 12W8962-33, coating P/N 12W8962-15 PERFMS-1027, use on auxilary flap | Lockheed Martin Corporation (81755) | |
| 12W8963-7 12W89637 | 1560-01-046-9978 | Bracket, Structural Component, Air | Aircraft Mission Design Series: F-111 | Lockheed Martin Corporation (81755) | |
| 12W8963-8 12W89638 | 1560-01-036-3230 | Bracket, Structural Component, Air | Aircraft Mission Design Series: F-111 Material: Aluminum alloy 2024 Overall Length: 39.000 inches nominal | Lockheed Martin Corporation (81755) | |
| 12W8981-8 12W89818 | 1560-00-970-6004 | Stop, Auxiliary Flap | General Characteristics Item Description: 2.670 in. lg, 1.320 in. W, 0.600 in. H, 2 holes 0.250 in. min, 0.255IN. max dia on 1.150 in. C to C along lgth III FSC Application Data: Flap, wing, airframe | Lockheed Martin Corporation (81755) | |
| 12W8983-5 12W89835 | 1560-00-438-4574 | Support, Structural Component, Air | III End Item Identification: Acft model F111 Special Features: Aluminum, 2 holes 0.250 in. min, 0.256 in. max dia | Lockheed Martin Corporation (81755) | |
| 12W8983-6 12W89836 | 1560-00-438-4575 | Support, Structural Component, Air | III End Item Identification: Acft model F111 Special Features: Aluminum, 2 holes 0.250 in. min, 0.256 in. max dia | Lockheed Martin Corporation (81755) | |
| 12W8983-801 12W8983801 | 1560-00-438-4570 | Support, Structural Component, Air | III End Item Identification: Acft model F111 Special Features: Aluminum, 2 holes 0.250 in. min, 0.256 in. max dia | Lockheed Martin Corporation (81755) | |
| 12W8983-802 12W8983802 | 1560-00-438-4576 | Support, Structural Component, Air | III End Item Identification: Acft MODELF111 Special Features: Aluminum, 2 holes 0.250 in. min, 0.256 in. max dia | Lockheed Martin Corporation (81755) | |
| 12W8986-7 12W89867 | 1560-01-167-7779 | Cover, Access | Material: Aluminum alloy FSC Application Data: Used on acft model F-111 | Lockheed Martin Corporation (81755) | |
| 12W8989-7 12W89897 | 1560-00-929-2321 | Plate, Bushing Lock | General Characteristics Item Description: Aluminum alloy 2024-T851, QQ-A-250/4, 1.260 in. lg, 1.040 in. W, 0.200 in. thk, serrated bushing hole per NAS541-48-38 on 0.520 in. radius, 1 ea locking edge slot | Lockheed Martin Corporation (81755) | |
| 12W8990-10 12W899010 | 1560-00-975-4584 | Support, Structural Component, Air | III End Item Identification: Aircraft model F111 Special Features: Aluminum alloy, QQ-A-250/4, 1.530 in. lg, 0.840 in. W, 2 holes 0.195 in. dia, 1 hole 0.080 in. dia | Lockheed Martin Corporation (81755) | |
| 12W8990-9 12W89909 | 1560-00-975-4578 | Support, Structural Component, Air | III End Item Identification: Aircraft model F111 Special Features: Aluminum alloy, QQ-A-250/4, 1.530 in. lg, 0.840 in. W, 2 holes 0.195 in. dia, 1 hole 0.080 in. dia | Lockheed Martin Corporation (81755) | |
| 12W8991-11 12W899111 | 1560-00-463-9130 | Guide, Carriage, Auxiliary Flap | General Characteristics Item Description: 1.530 in. lg, 0.815 in. min, 0.865 in. max W, 0.250 in. min, 0.255 in. max dia hole thru 1 place | Lockheed Martin Corporation (81755) |