Airframe Structural Components: 12C263-801, 12C272-9, 12C345-3
MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
---|---|---|---|---|---|
12C263-801 12C263801 | 1560-00-442-8790 | Support, Structural Component, Air | Aircraft Mission Design Series: F-111 Aircraft Location: Pedal support assembly Overall Length: 4.425 inches nominal | Lockheed Martin Corporation (81755) | |
12C263-802 12C263802 | 1560-00-997-7620 | Support, Structural Component, Air | Aircraft Mission Design Series: F-111 Aircraft Location: Pedal support assembly Overall Length: 4.425 inches nominal | Lockheed Martin Corporation (81755) | |
12C270-9 12C2709 | 1560-00-929-2233 | Shaft, Hanger Pivot | III End Item Identification: Aircraft model F111 General Characteristics Item Description: Steel, 6.940 in. O/a lg, 0.7509 in. min, 0.7514 in. max O/a od, thread both ends 0.500-20 UNF3A per MIL-S-7742 | Lockheed Martin Corporation (81755) | |
12C272-11 12C27211 | 1560-00-975-5489 | Gasket, Support Assemblies Rudder | III End Item Identification: Aircraft model F111 | Lockheed Martin Corporation (81755) | |
12C272-7 12C2727 | 1560-00-967-4249 | Gasket, Rudder Support | III End Item Identification: Aircraft model F111 | Lockheed Martin Corporation (81755) | |
12C272-9 12C2729 | 1560-00-967-4251 | Gasket, Rudder Support | III End Item Identification: Aircraft model F111 | Lockheed Martin Corporation (81755) | |
12C299-19 12C29919 | 1560-00-086-0202 | Shaft, Disconnect-Rudder | General Characteristics Item Description: Aluminum alloy QQ-A-200/11, 7.900 in. lg | Lockheed Martin Corporation (81755) | |
12C300-835 12C300835 | 1560-00-088-2242 | Rudder, Aircraft | Aircraft Mission Design Series: F-111A | Lockheed Martin Corporation (81755) | |
12C312-5 12C3125 | 1560-00-828-5875 | Support Assembly, Rudder | III End Item Identification: Aircraft model F111 General Characteristics Item Description: Steel, AMS5355, 13.410 in. O/a lg, 4.740 in. O/a W, 3.540 in. O/a H | Lockheed Martin Corporation (81755) | |
12C313-1 12C3131 | 1560-00-828-5876 | Support Assembly, Elevator | III End Item Identification: Aircraft model F111 General Characteristics Item Description: Steel, FMS1086, 18.680 in. O/a lg, 14.700 in. O/a W, 5.000 in. O/a H | Lockheed Martin Corporation (81755) | |
12C315-3 12C3153 | 1560-00-078-6496 | Support, Structural Component, Air | Aircraft Mission Design Series: F-111 | Lockheed Martin Corporation (81755) | |
12C317-8 12C3178 | 1560-00-929-2286 | Guard, cable, Tension | III End Item Identification: Aircraft model F-111 General Characteristics Item Description: Aluminum alloy, QQ-A-250-4, temper T6 | Lockheed Martin Corporation (81755) | |
12C318-9 12C3189 | 1560-00-929-2287 | Guard, cable, Tension | III End Item Identification: Aircraft model F-111 General Characteristics Item Description: Aluminum alloy, ams 4260, temper T6 | Lockheed Martin Corporation (81755) | |
12C322-3 12C3223 | 1560-00-929-2288 | Bracket, Structural Component, Air | Aircraft Mission Design Series: F-111 Aircraft Location: Bellcrank bracket | Lockheed Martin Corporation (81755) | |
12C327-1 12C3271 | 1560-00-929-2289 | Support, Structural Component, Aircraft | Aircraft Mission Design Series: F-111 Aircraft Location: Pulley support assembly | Lockheed Martin Corporation (81755) | |
12C330-3 12C3303 | 1560-00-929-2290 | Support, Structural Component, Aircraft | Aircraft Mission Design Series: F-111 Aircraft Location: Pulley support assembly | Lockheed Martin Corporation (81755) | |
12C337-1 12C3371 | 1560-00-949-0335 | Coupling Assembly, Disconnect | III End Item Identification: Acft model F111 General Characteristics Item Description: 1.170 in.O/a width, 3.500 in.O/a length, C/O coupling assy 1 ea P/N 12C337-9, wedge 2 ea P/N 12C336-7, washer 2 ea P/N AN960C10, washer 2 ea P/N AN960C10L, bolt 2 ea P/N C630-3-8, used on primary control | Lockheed Martin Corporation (81755) | |
12C337-3 12C3373 | 1560-00-949-0335 | Coupling Assembly, Disconnect | III End Item Identification: Acft model F111 General Characteristics Item Description: 1.170 in.O/a width, 3.500 in.O/a length, C/O coupling assy 1 ea P/N 12C337-9, wedge 2 ea P/N 12C336-7, washer 2 ea P/N AN960C10, washer 2 ea P/N AN960C10L, bolt 2 ea P/N C630-3-8, used on primary control | Lockheed Martin Corporation (81755) | |
12C342-1 12C3421 | 1560-00-929-2314 | Bracket, Structural Component, Air | Aircraft Mission Design Series: F-111 Material Document and Classification: QQ-A-601 fed spec single material response | Lockheed Martin Corporation (81755) | |
12C345-3 12C3453 | 1560-00-961-0789 | Switch Assembly, Rudder Feel | General Characteristics Item Description: Components include switch, connector, mounting bracket, bearing and clamp | Lockheed Martin Corporation (81755) |