Airframe Structural Components: 3P22502-139, 3P22502-225, 3P22502-249
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 3P22502-139 3P22502139 | 1560-01-260-2950 | Plate, Structural, Aircraft | III End Item Identification: C-141 Material: Aluminum alloy 2024 Aircraft Location: Doubler U/P nozzle assembly-exhaust, secondary | Lockheed Martin Corporation (98897) | |
| 3P22502-141 3P22502141 | 1560-01-294-5101 | Support, Structural Component, Air | Aircraft Mission Design Series: C-141 Special Features: Opposite -142; NHA:3P22542;MATL: 301/302 annealed Aircraft Location: Secondary exhaust nozzle assy | Lockheed Martin Corporation (98897) | |
| 3P22502-142 3P22502142 | 1560-01-294-5100 | Support, Structural Component, Air | Aircraft Mission Design Series: C-141 Special Features: Opposite -141; NHA:3P22542;MATL: 301/302 annealed Aircraft Location: Secondary exhaust nozzle assy | Lockheed Martin Corporation (98897) | |
| 3P22502-169 3P22502169 | 1560-01-327-4731 | Skin, Aircraft | Aircraft Mission Design Series: C-141 Material: Titanium alloy Aircraft Location: Exhaust nozzle, secondary | Lockheed Martin Corporation (98897) | |
| 3P22502-173 3P22502173 | 1560-01-279-0122 | Skin, Aircraft | III End Item Identification: C-141 | Lockheed Martin Corporation (98897) | |
| 3P22502-181 3P22502181 | 1560-01-297-6587 | Skin, Aircraft | III End Item Identification: C-141 Special Features: Cond T3 clad Material: Aluminum alloy 2024 | Lockheed Martin Corporation (98897) | |
| 3P22502-183 3P22502183 | 1560-01-294-5099 | Support, Structural Component, Air | Aircraft Mission Design Series: C-141 Special Features: Opposite -184; NHA:3P22542;MATL: 301/302 annealed Aircraft Location: Secondary exhaust nozzle assy | Lockheed Martin Corporation (98897) | |
| 3P22502-184 3P22502184 | 1560-01-294-5098 | Support, Structural Component, Air | Aircraft Mission Design Series: C-141 Special Features: Opposite -183; NHA:3P22542;MATL: 301/302 annealed Aircraft Location: Secondary exhaust nozzle assy | Lockheed Martin Corporation (98897) | |
| 3P22502-191 3P22502191 | 1560-01-297-6538 | Plate, Structural, Aircraft | III End Item Identification: C-141 Material: Titanium Aircraft Location: Pan P/O exhaust nozzle, secondary | Lockheed Martin Corporation (98897) | |
| 3P22502-199 3P22502199 | 1560-01-267-7676 | Support, Structural Component, Air | Aircraft Mission Design Series: C-141 | Lockheed Martin Corporation (98897) | |
| 3P22502-203 3P22502203 | 1560-01-267-7675 | Support, Structural Component, Air | Aircraft Mission Design Series: C-141 | Lockheed Martin Corporation (98897) | |
| 3P22502-211 3P22502211 | 1560-01-297-6555 | Support, Structural Component, Air | Aircraft Mission Design Series: C-141 Special Features: Temper T6 Material: Aluminum alloy 2024 | Lockheed Martin Corporation (98897) | |
| 3P22502-225 3P22502225 | 1560-01-268-4619 | Plate, Structural, Aircraft | III End Item Identification: C-141 Material: Titanium alloy Aircraft Location: End cap, P/O -091 nozzle assy-exhaust, secondary | Lockheed Martin Corporation (98897) | |
| 3P22502-226 3P22502226 | 1560-01-268-4621 | Plate, Structural, Aircraft | III End Item Identification: C-141 Material: Titanium alloy Aircraft Location: End cap, -091 nozzle assy-exhaust secondary | Lockheed Martin Corporation (98897) | |
| 3P22502-227 3P22502227 | 1560-01-268-2809 | Plate, Structural, Aircraft | III End Item Identification: C-141 Material: Titanium alloy Aircraft Location: -091 nozzel assy-exhaust, secondaru, end cap | Lockheed Martin Corporation (98897) | |
| 3P22502-229 3P22502229 | 1560-01-260-5408 | Former, Aircraft | III End Item Identification: C-141 | Lockheed Martin Corporation (98897) | |
| 3P22502-235 3P22502235 | 1560-01-268-4629 | Support, Structural Component, Air | Aircraft Mission Design Series: C-141 Overall Length: 3.000 inches nominal Overall Width: 2.000 inches nominal | Lockheed Martin Corporation (98897) | |
| 3P22502-236 3P22502236 | 1560-01-268-2813 | Support, Structural Component, Air | Aircraft Mission Design Series: C-141 Overall Length: 3.000 inches nominal Overall Width: 2.000 inches nominal | Lockheed Martin Corporation (98897) | |
| 3P22502-241 3P22502241 | 1560-01-268-2807 | Plate, Structural, Aircraft | III End Item Identification: C-141 Special Features: Channel Material: Aluminum alloy 2024 | Lockheed Martin Corporation (98897) | |
| 3P22502-249 3P22502249 | 1560-01-268-8486 | Plate, Structural, Aircraft | III End Item Identification: C-141 Material: Titanium Aircraft Location: Channel, nozzle assembly, exhaust secondary | Lockheed Martin Corporation (98897) |