Airframe Structural Components: 3F31220-102, 3F31224-102, 3F31275-103
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 3F31220-102 3F31220102 | 1560-01-014-1866 | Fitting, Structural Component, Air | Aircraft Mission Design Series: C-141 | Lockheed Martin Corporation (98897) | |
| 3F31221-101 3F31221101 | 1560-01-410-3447 | Fitting, Structural Component, Air | Aircraft Mission Design Series: C-141 Material: Aluminum alloy 7075 Aircraft Location: Splice fitting-stringer NO.74 | Lockheed Martin Corporation (98897) | |
| 3F31221-102 3F31221102 | 1560-01-410-3451 | Fitting, Structural Component, Air | Aircraft Mission Design Series: C-141 Material: Aluminum alloy 7075 Aircraft Location: Splice fitting-stringer NO.74 | Lockheed Martin Corporation (98897) | |
| 3F31222-101 3F31222101 | 1560-01-429-3486 | Fitting, Structural Component, Air | Aircraft Mission Design Series: C-141 Material: Aluminum alloy 7075 Aircraft Location: Splice-forward, stringer NO.50 | Lockheed Martin Corporation (98897) | |
| 3F31222-102 3F31222102 | 1560-01-429-4499 | Fitting, Structural Component, Air | Aircraft Mission Design Series: C-141 Special Features: Made from 3F31207-992 FORGING;ECO82C0001 deviation indicates manufacture from 7075-T6 bar stock in lieu of forging;p/N 3F3122-101 opposite configuration;fitting, 998 kit Material: Aluminum alloy 7075 | Lockheed Martin Corporation (98897) | |
| 3F31224-101 3F31224101 | 1560-01-429-3490 | Fitting, Structural Component, Air | Aircraft Mission Design Series: C141 Material: Aluminum alloy 7075 Aircraft Location: Splice-stringer no. 52 | Lockheed Martin Corporation (98897) | |
| 3F31224-102 3F31224102 | 1560-01-429-6327 | Fitting, Structural Component, Air | Aircraft Mission Design Series: C-141 Material: Aluminum alloy 7075 Aircraft Location: Splice-stringer NO.52 | Lockheed Martin Corporation (98897) | |
| 3F31234-101 3F31234101 | 1560-00-941-6726 | Stop, Conveyor Lock | General Characteristics Item Description: Aluminum alloy, 2024-T351, QQ-A-250/4, 4.660 in. l, 0.900 in. W, 0.600IN. thk, two mounting holes, 0.249 in. min, 0.255 in. max dia | Lockheed Martin Corporation (98897) | |
| 3F31234-103 3F31234103 | 1560-00-941-6726 | Stop, Conveyor Lock | General Characteristics Item Description: Aluminum alloy, 2024-T351, QQ-A-250/4, 4.660 in. l, 0.900 in. W, 0.600IN. thk, two mounting holes, 0.249 in. min, 0.255 in. max dia | Lockheed Martin Corporation (98897) | |
| 3F31243-107 3F31243107 | 1560-00-482-5712 | Lock Assembly, Roller Conveyor | General Characteristics Item Description: 5.350 in. lg, 0.193 in. min, 0.199 in. max dia hole thru base 4 places | Lockheed Martin Corporation (98897) | |
| 3F31247-101 3F31247101 | 1560-00-069-7894 | Adapter, Antenna | General Characteristics Item Description: Aluminum alloy, 10.200 in. dia, 0.290 in. O/a thk, 30 mtg holes 0.156IN. dia | KAL Nelson Aviation Inc. (1F754) Lockheed Martin Corporation (98897) Specialty Engineering Co. (60607) | |
| 3F31264-101 3F31264101 | 1560-00-868-5269 | Support, Structural Component, Air | III End Item Identification: Acft model C141 Special Features: Magnesium per QQ-M-55 COMPOSITIONAZ91C temper T6 | Lockheed Martin Corporation (98897) | |
| 3F31265-101 3F31265101 | 1560-00-907-1881 | Support, Structural Component, Air | III End Item Identification: Aircraft model C141 Special Features: Magnesium, QQ-M-56, comp AZ91C, cond T6, 8.590 in. lg, 5.000 in. W | Lockheed Martin Corporation (98897) | |
| 3F31265-102 3F31265102 | 1560-00-868-5271 | Support, Structural Component, Air | III End Item Identification: Aircraft model C141 Special Features: Magnesium, QQ-M-56, comp AZ91C, cond T6, 8.590 in., 5.000 in. W | Lockheed Martin Corporation (98897) | |
| 3F31265-104 3F31265104 | 1560-00-868-5273 | Support, Structural Component, Air | III End Item Identification: Aircraft model C141 Special Features: Magnesium, QQ-M-56, comp AZ91C, cond T6, 8.590 in. lg, 5.000 in. W | Lockheed Martin Corporation (98897) | |
| 3F31268-103 3F31268103 | 1560-01-423-4306 | Fitting, Structural Component, Air | Aircraft Mission Design Series: C-141 Material: Aluminum alloy 7075 Aircraft Location: Splice fitting-outboard longeron | Lockheed Martin Corporation (98897) | |
| 3F31274-101 3F31274101 | 1560-00-432-5671 | Bracket, Lower Bulkhead | III End Item Identification: Aircraft model C141 | Lockheed Martin Corporation (98897) | |
| 3F31274-101 3F31274101 | 1560-00-432-5698 | Bracket, Lower Bulkhead | III End Item Identification: Aircraft model C141 | Aero Components Inc. (59213) | |
| 3F31274-102 3F31274102 | 1560-00-432-5698 | Bracket, Lower Bulkhead | III End Item Identification: Aircraft model C141 | Advanced Metal Products Inc. (1HT92) Lockheed Martin Corporation (98897) | |
| 3F31274-104 3F31274104 | 1560-00-502-5413 | Fitting, Lower Bulkhead | General Characteristics Item Description: Aluminum alloy, QQ-A-367, composition 7075, temper T6, anodized | Lockheed Martin Corporation (98897) | |
| 3F31275-103 3F31275103 | 1560-01-429-4506 | Fitting, Structural Component, Air | Aircraft Mission Design Series: C-141 Special Features: Fitting, 998 kit;made from P/N 3F31275-991 forging Material: Aluminum alloy 7075 | Lockheed Martin Corporation (98897) |