Airframe Structural Components: 12W8101-51, 12W8150-12, 12W8203M1-12
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 12W8101-51 12W810151 | 1560-01-181-4226 | Rub Strip | III End Item Identification: Acft model F-111BR General Characteristics Item Description: Material per P5153-2-4, 10.000 in. lg III Functional Description: Used on trailing edge no. 3 | Lockheed Martin Corporation (81755) | |
| 12W8130-25 12W813025 | 1560-01-123-7338 | Rub Strip | III End Item Identification: Acft model F111 General Characteristics Item Description: Material per P5153-2-4, 74.000 in. lg | Lockheed Martin Corporation (81755) | |
| 12W8130-5 12W81305 | 1560-00-460-9305 | Spoiler Assembly, Outboard | III End Item Identification: Aircraft model F111 | Lockheed Martin Corporation (81755) | |
| 12W8130-5 12W81305 | 1560-01-244-1327 | Spoiler, Wing, Aircraft | Aircraft Mission Design Series: F-111A/FB/EF/C/D/E/F | Lockheed Martin Corporation (81755) | |
| 12W8130-801 12W8130801 | 1560-00-473-1647 | Spoiler, Wing, Aircraft | Aircraft Mission Design Series: F-111 | Lockheed Martin Corporation (81755) | |
| 12W8130-802 12W8130802 | 1560-00-451-9977 | Spoiler, Wing, Aircraft | Aircraft Mission Design Series: F-111 | Lockheed Martin Corporation (81755) | |
| 12W8131-36 12W813136 | 1560-01-165-3579 | Core Assembly, Spoiler, Outboard | III End Item Identification: Acft model F-111 | Lockheed Martin Corporation (81755) | |
| 12W8132-11 12W813211 | 1560-01-110-6523 | Skin, Aircraft | III End Item Identification: F-111 | Lockheed Martin Corporation (81755) | |
| 12W8132-12 12W813212 | 1560-01-111-2064 | Skin, Aircraft | III End Item Identification: F-111 | Lockheed Martin Corporation (81755) | |
| 12W8133-10 12W813310 | 1560-01-112-9389 | Spar, Aircraft | Aircraft Mission Design Series: F-111 Material: Aluminum alloy Material Document and Classification: QQ-A-250/4 T62 fed spec single material response | Lockheed Martin Corporation (81755) | |
| 12W8150-12 12W815012 | 1560-01-120-2321 | Skin, Aircraft | III End Item Identification: F-111 Material: Aluminum alloy 2024 Overall Length: 16.000 inches nominal | Lockheed Martin Corporation (81755) | |
| 12W8150-8 12W81508 | 1560-01-120-7904 | Skin, Aircraft | III End Item Identification: F-111 Material: Aluminum alloy 2024 Overall Length: 15.000 inches nominal | Lockheed Martin Corporation (81755) | |
| 12W8151-10 12W815110 | 1560-01-241-8922 | Trailing Edge, Aircraft | Aircraft Mission Design Series: F-111 Special Features: C/O rub strip P/N 12W8151-28, stiffener P/N 12W8042-10, skin P/N 12W8150-10 and attaching hardware Aircraft Location: Trailing edge installation no. 3 | Lockheed Martin Corporation (81755) | |
| 12W8151-7 12W81517 | 1560-01-115-2788 | Trailing Edge, Aircraft | Aircraft Mission Design Series: F-111 Special Features: C/O stiffener P/N 12W8042-7, skin P/N 12W8150-7, 4 ea. rub strip and attaching hardware Aircraft Station Number: Span station 250.765 | Lockheed Martin Corporation (81755) | |
| 12W8151-8 12W81518 | 1560-01-116-9486 | Trailing Edge, Aircraft | Aircraft Mission Design Series: F-111 Special Features: C/O skin P/N 12W8150-8, stiffener P/N 12W8042-8, 4 ea. rub strip and attaching hardware | Lockheed Martin Corporation (81755) | |
| 12W8151-9 12W81519 | 1560-01-145-9646 | Trailing Edge, Aircraft | Aircraft Mission Design Series: F-111 Special Features: C/O rub strip P/N 12W8151-13, rub strip P/N 12W8151-15, rub strip P/N 12W8151-17, rub strip P/N 12W8151-17, rub strip P/N 12W8151-27, stiffener P/N 12W8042-9, skin P/N 12W8150-9, 3 ea. nut P/NC068-02-2, 8 ea. nut P/N C2949-02, as required rivet P/N C088-4 and rivet MS20426AD3 | Lockheed Martin Corporation (81755) | |
| 12W8188-3 12W81883 | 1560-00-088-2247 | Seal, Track | III End Item Identification: Aircraft model F111 General Characteristics Item Description: 6.100 in. O/a lg, 0.900 in. O/a W, 0.070 in. O/a H | Lockheed Martin Corporation (81755) | |
| 12W8203-71 12W820371 | 1560-00-252-0686 | Plate, Rib, Track | III End Item Identification: Aircraft model F-111 General Characteristics Item Description: Steel, 0.125 in. thk | Lockheed Martin Corporation (81755) | |
| 12W8203-72 12W820372 | 1560-00-252-0692 | Plate, RIB, Track | III End Item Identification: Aircraft model F-111 General Characteristics Item Description: Steel, 0.125 in. thk | Lockheed Martin Corporation (81755) | |
| 12W8203M1-11 12W8203M111 | 1560-00-264-1114 | Stop, Splice, Flap Track NO.1 | General Characteristics Item Description: Aluminum alloy, QQ-A-250/4, alloy 2024, T851, stock size, 5.500 in. lg, 4.500IN. W, 2.000 in. H | Lockheed Martin Corporation (81755) | |
| 12W8203M1-12 12W8203M112 | 1560-00-264-1117 | Stop, Splice, Flap Track NO.1 | General Characteristics Item Description: Aluminum alloy, QQ-A-250/4, alloy 2024, T851, stock size, 5.500 in. lg, 4.500IN. W, 2.000 in. H | Lockheed Martin Corporation (81755) |