Airframe Structural Components: 12M3578-9, 12M403-9, 12M4047-801
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 12M3578-9 12M35789 | 1560-00-104-0608 | Cap, Torque Limiter | General Characteristics Item Description: Aluminum alloy, AMS4260 | Lockheed Martin Corporation (81755) | |
| 12M3582-7 12M35827 | 1560-00-104-0607 | CAP, Torque Limiter | General Characteristics Item Description: Aluminum alloy, QQ-A-225-6, 1.446 in. lg | Lockheed Martin Corporation (81755) | |
| 12M3583-7 12M35837 | 1560-00-079-4972 | Driver, Torque Limiter | III End Item Identification: Aircraft model F111 General Characteristics Item Description: Aluminum alloy, QQ-A-225/6 comp 2024 cond T351, 0.7154 in. min, 0.7159 in. max O/a dia, 3.050 in. O/a lg | Lockheed Martin Corporation (81755) | |
| 12M3583-9 12M35839 | 1560-00-106-5117 | Driver, Torque Limiter | III End Item Identification: Aircraft model F111 General Characteristics Item Description: Aluminum alloy, QQ-A-225/6 comp 2024 cond T351, 0.7154 in. min, 0.7159 in. max O/a dia, 2.514 in. O/a lg | Lockheed Martin Corporation (81755) | |
| 12M3587-7 12M35877 | 1560-00-079-4975 | Spring, Torque Limiter | General Characteristics Item Description: 3.530 in. min, 3.540 in. max lg, 0.7159 in.min, 0.7164 in. max id, 0.9445 in. min, 0.9450 max od, 0.125 in. min, 0.126IN. max dia pin hole on each end | Lockheed Martin Corporation (81755) | |
| 12M3592-2 12M35922 | 1560-00-319-0965 | Crank Assembly, Actuator, Glove dr | Lockheed Martin Corporation (81755) | ||
| 12M3592-4 12M35924 | 1560-00-319-0965 | Crank Assembly, Actuator, Glove dr | Lockheed Martin Corporation (81755) | ||
| 12M3594-9 12M35949 | 1560-00-406-8568 | Support, Shaft | III End Item Identification: Aircraft model no. F-111 | Lockheed Martin Corporation (81755) | |
| 12M3612-805 12M3612805 | 1560-00-406-5981 | Guide, Flexible Shaft | III End Item Identification: Aircraft model F-111 General Characteristics Item Description: Aluminum alloy, QQ-A-250-5, temper T4 | Lockheed Martin Corporation (81755) | |
| 12M3612-806 12M3612806 | 1560-00-406-5982 | Guide, Flexible Shaft | III End Item Identification: Aircraft model F-111 General Characteristics Item Description: Aluminum alloy, QQ-A-250-5, temper T4 | Lockheed Martin Corporation (81755) | |
| 12M3621-12 12M362112 | 1560-00-421-5535 | Support, Structural Component, Air | III End Item Identification: Aircraft model F111 Special Features: Aluminum alloy, QQ-A-200/3, 3.750 in. lg, 2.660 in. W, 1.610 in. H | Lockheed Martin Corporation (81755) | |
| 12M3654-809 12M3654809 | 1560-00-774-2852 | CAM Assembly, Position Mechanism | General Characteristics Item Description: Consists of 1 cam, P/N 12M3655-25, 1 stop, P/N 12M3657-7, 1 screw, P/N 12M3656-11, 2 screws, P/N NAS1101-02-4, 2 nuts, P/N MS21042L02, 1 washer, P/N AN960-4, 2 washers, P/N NAS620-2 III FSC Application Data: Fuselage, airframe | Lockheed Martin Corporation (81755) | |
| 12M3657-7 12M36577 | 1560-00-081-2598 | Lock, cam Mechanism | III End Item Identification: Aircraft model F111 General Characteristics Item Description: Steel, MIL-S-9747 alloy 1095 cond a, 0.875 in. O/a lg, 0.008 in. thk, two holes 0.093 in. min, 0.098 in. max dia | Lockheed Martin Corporation (81755) | |
| 12M3660-5 12M36605 | 1560-00-195-7589 | Cover, Access, Aircraft | Material: Aluminum alloy 5052 Material Document and Classification: QQ-A-250/8 fed spec single material response Cross-Sectional Shape Style: 5 oblong recess | Lockheed Martin Corporation (81755) | |
| 12M3665-9 12M36659 | 1560-00-869-4693 | Retainer, Worm Shaft, Position Mec | III End Item Identification: Aircraft model F111 General Characteristics Item Description: Aluminum alloy, QQ-A-225/6, 1.120 in. lg, 1.760 in. W flange end, 2 mounting holes 0.196 in dia, other end threaded 3/4-16UNF-2B | Lockheed Martin Corporation (81755) | |
| 12M402-17 12M40217 | 1560-00-480-9266 | Bracket, Lanyard, Weapons bay | III End Item Identification: Acft model F-111 General Characteristics Item Description: 1.875 in. oa lg, 1.750 in. oa H, 1.750 in. oa W, T-bar stock, 4 holes thru top 0.261 in. min 0.269 in. max dia, hole 0.812 in. dia on center | Lockheed Martin Corporation (81755) | |
| 12M403-7 12M4037 | 1560-00-894-4901 | Retainer, Lanyard Tube | III End Item Identification: Aircraft model F111 General Characteristics Item Description: 3.290 in. lg, 0.120 in. min, 0.125 in. max dia hole 1 in line 2 places | Lockheed Martin Corporation (81755) | |
| 12M403-9 12M4039 | 1560-00-894-4903 | Retainer, Lanyard Tube | General Characteristics Item Description: 1.180 in. lg, 0.076 in. min, 0.091 in. max W slot 0.430 in. deep 1 end, 0.120 in. min, 0.125 in. max dia hole 1 in line 2 places | Lockheed Martin Corporation (81755) | |
| 12M4047-5 12M40475 | 1560-00-081-2537 | Bracket Assembly, Interconnect | III End Item Identification: Aircraft model F111 | Lockheed Martin Corporation (81755) | |
| 12M4047-801 12M4047801 | 1560-00-081-2539 | Bracket Assembly, Interconnect | III End Item Identification: Aircraft model F111 | Lockheed Martin Corporation (81755) |