Airframe Structural Components: 12C819-1, 12C819-3, 12E1046-817
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 12C819-1 12C8191 | 1560-00-964-2985 | Bracket, Structural Component, Air | Aircraft Mission Design Series: F-111 Aircraft Location: Crossover bracket assembly Overall Length: 2.530 inches nominal | Lockheed Martin Corporation (81755) | |
| 12C819-3 12C8193 | 1560-00-964-3006 | Bracket, Structural Component, Air | Aircraft Mission Design Series: F-111 Aircraft Location: Crossover bracket assembly Overall Length: 2.530 inches nominal | Lockheed Martin Corporation (81755) | |
| 12C852-1 12C8521 | 1560-00-929-6968 | Bracket, Structural Component, Air | Aircraft Mission Design Series: F-111 Aircraft Location: Horizontal bracket assembly Overall Length: 2.780 inches nominal | Lockheed Martin Corporation (81755) | |
| 12C854-5 12C8545 | 1560-00-081-8139 | Bracket Assebmly, Crossover | General Characteristics Item Description: CRES | Lockheed Martin Corporation (81755) | |
| 12C854-6 12C8546 | 1560-00-885-1420 | Bracket Assembly, Cross Over | General Characteristics Item Description: CRES | Lockheed Martin Corporation (81755) | |
| 12C858-701 12C858701 | 1560-00-928-7660 | Bracket, Structural Component, Air | Aircraft Mission Design Series: F-111 Aircraft Location: Horizontal bracket assembly Overall Length: 3.750 inches nominal | Lockheed Martin Corporation (81755) | |
| 12C858-702 12C858702 | 1560-00-928-7661 | Bracket, Structural Component, Aircraft | Aircraft Mission Design Series: F-111 Aircraft Location: Horizontal bracket assembly Overall Length: 3.750 inches nominal | Lockheed Martin Corporation (81755) | |
| 12C858-705 12C858705 | 1560-01-257-5359 | Support, Structural Component, Aircraft | III End Item Identification: Acft model F-111 III Supplementary Features: Functional description:used on bracket assembly-structure feed back, horizontal tail | Lockheed Martin Corporation (81755) | |
| 12C858-706 12C858706 | 1560-01-257-5360 | Support, Structural Component, Air | III End Item Identification: Acft model F-111 III Supplementary Features: Functional description:used on bracket assembly-structure feed back, horizontal tail | Lockheed Martin Corporation (81755) | |
| 12C867-5 12C8675 | 1560-00-443-3510 | Lever Assembly, Feedback Multiplier | General Characteristics Item Description: Titanium alloy, AMS4928, 7.632 in. lg hole to hole center | Lockheed Martin Corporation (81755) | |
| 12C867-801 12C867801 | 1560-00-443-3510 | Lever Assembly, Feedback Multiplier | General Characteristics Item Description: Titanium alloy, AMS4928, 7.632 in. lg hole to hole center | Lockheed Martin Corporation (81755) | |
| 12C910-1 12C9101 | 1560-00-772-0782 | Bracket, Rudder | III End Item Identification: Aircraft model F111 | Lockheed Martin Corporation (81755) | |
| 12C912-1 12C9121 | 1560-00-105-1714 | Lever, Rudder Input Control | General Characteristics Item Description: Titanium alloy, MIL-T-9047, 0.625 in. dia hole 1 in line 2 places first end, 0.374 in. dia hole 1 in line 2 places second end | Lockheed Martin Corporation (81755) | |
| 12C980-1 12C9801 | 1560-00-825-6363 | Tube Assembly, Fixed Flight Control | III End Item Identification: Acft model F111 General Characteristics Item Description: C/O tube 1 ea P/N 12C963-47, bearing 2 ea P/N C3116-4H8A, rivet 4 ea P/N NAS1198-4-14 | Lockheed Martin Corporation (81755) | |
| 12C991-1 12C9911 | 1560-01-079-5644 | Link, Connector | III End Item Identification: Acft model F-111 General Characteristics Item Description: Cres steel 17-4PH, tubular body, 8.625 in. oa lg, 1.250 in. oa W, 0.750IN. oa thk | Lockheed Martin Corporation (81755) | |
| 12E066-13 12E06613 | 1560-00-901-8637 | Hook, Mounting, Inertial unit | General Characteristics Item Description: Cres, AMS5355 | Lockheed Martin Corporation (81755) | |
| 12E071-7 12E0717 | 1560-00-929-2315 | CUP, Boresighting, Inertial Reference Unit | III End Item Identification: Aircraft model F111 General Characteristics Item Description: Aluminum alloy, QQ-A-225/6, 2.150 in. lg, 2.150 in. W, 0.560 in. H | Lockheed Martin Corporation (81755) | |
| 12E102-7 12E1027 | 1560-00-929-2316 | Support, Structural Component, Air | Aircraft Mission Design Series: F-111 Special Features: U/a:support, flight computer | Lockheed Martin Corporation (81755) | |
| 12E1046-351 12E1046351 | 1560-01-105-8312 | Support, Structural Component, Air | III End Item Identification: Acft model F-111F Special Features: C/O bracket 1 ea P/N 12E1046-147, washer 12 ea, screw 4 ea, nut 4 ea, rivet as required | Lockheed Martin Corporation (81755) | |
| 12E1046-817 12E1046817 | 1560-01-057-7009 | Bracket Assembly, Wiring Support | III End Item Identification: Acft model F-16 General Characteristics Item Description: C/O bracket P/N 12E858-643, 3 screws P/N AN520DD10R10, 3 washers P/N AN960-10L, 3 washers P/N AN960D10L, 3 nuts P/N NAS697A3, 3WASHER P/N MS35337-81, ar rivets P/N MS20426AD3 | Lockheed Martin Corporation (81755) |