Airframe Structural Components: 17P2A5155-4, 17P2A5270-501, 17P2A5510-508
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 17P2A5155-4 17P2A51554 | 1560-01-454-8457 | Panel, Structural, Aircraft | Aircraft Mission Design Series: C-17A Special Features: Manufacturer suggested name - panel assembly, fuselage, aircraft, Y=1137.5 - Y=1160.5;NHA 17P2A5155-2 Aircraft Location: Center fuselage | Boeing Company, The (88277) | |
| 17P2A5156-3 17P2A51563 | 1560-01-467-9423 | Panel, Structural, Aircraft | Aircraft Mission Design Series: C-17A Special Features: Manufacturer suggested name - panel, structural, aircraft-instl, Y=1160.500-1166.350;NHA 17P2A5156-1 & -501 Material: Plastic epoxy | Boeing Company, The (88277) | |
| 17P2A5156-4 17P2A51564 | 1560-01-455-7284 | Panel, Structural, Aircraft | Boeing Company, The (88277) | ||
| 17P2A5204-1 17P2A52041 | 1560-01-500-3399 | Panel, Structural, Aircraft | Boeing Company, The (88277) | ||
| 17P2A5204-2 17P2A52042 | 1560-01-518-9434 | Panel, Structural, Aircraft | Aircraft Mission Design Series: C-17A Special Features: Nha 7P2A5618-514; effectivity from 17A103-184; plate, heat treat T7451 Material: Aluminum alloy 7075 | Boeing Company, The (88277) | |
| 17P2A5204-501 17P2A5204501 | 1560-01-518-9435 | Panel, Structural, Aircraft | Boeing Company, The (88277) | ||
| 17P2A5204-502 17P2A5204502 | 1560-01-518-9436 | Panel, Structural, Aircraft | Aircraft Mission Design Series: C-17A Special Features: Nha 17P2A5618-516; dms 2233; same as -2 except;dimensions are stocksize;plate, heat treat T7451 Material: Aluminum alloy 7075 | Boeing Company, The (88277) | |
| 17P2A5270-501 17P2A5270501 | 1560-01-487-0194 | Frame, Aircraft | Boeing Company, The (88277) | ||
| 17P2A5270-502 17P2A5270502 | 1560-01-479-3518 | Frame, Aircraft | Boeing Company, The (88277) | ||
| 17P2A5326-143 17P2A5326143 | 1560-01-413-2250 | Plate, Structural, Aircraft | Boeing Company, The (88277) | ||
| 17P2A5326-73 17P2A532673 | 1560-01-413-2247 | Plate, Structural, Aircraft | Boeing Company, The (88277) | ||
| 17P2A5326-99 17P2A532699 | 1560-01-413-2249 | Plate, Structural, Aircraft | Boeing Company, The (88277) | ||
| 17P2A5360-101 17P2A5360101 | 1560-01-411-3554 | Cover, Access | Boeing Company, The (88277) | ||
| 17P2A5379-1 17P2A53791 | 1560-01-486-8691 | Support, Structural Component, Air | Boeing Company, The (88277) | ||
| 17P2A5452-101 17P2A5452101 | 1560-01-468-6263 | Plate, Structural, Aircraft | Aircraft Mission Design Series: C-17 acft Material: Aluminum alloy 7075 Overall Length: 48.000 inches nominal | Boeing Company, The (88277) | |
| 17P2A5452-111 17P2A5452111 | 1560-01-469-3080 | Plate, Structural, Aircraft | III End Item Identification: C-17A, acft Aircraft Mission Design Series: C17A, acft Material: Aluminum alloy 7075 | Boeing Company, The (88277) | |
| 17P2A5510-1 17P2A55101 | 1560-01-411-6599 | Support, Structural Component, Air | Boeing Company, The (88277) | ||
| 17P2A5510-503 17P2A5510503 | 1560-01-411-6600 | Support, Structural Component, Air | III End Item Identification: Aircraft C-17A Aircraft Mission Design Series: C-17A Material: Aluminum alloy | Boeing Company, The (88277) | |
| 17P2A5510-505 17P2A5510505 | 1560-01-414-3401 | Support, Structural Component, Air | Boeing Company, The (88277) | ||
| 17P2A5510-508 17P2A5510508 | 1560-01-414-3402 | Support, Structural Component, Aircraft | Boeing Company, The (88277) |