Airframe Structural Components: 17P2A3307-551, 17P2A3307-554, 17P2A3310-2
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 17P2A3307-551 17P2A3307551 | 1560-01-456-1285 | Plate, Structural, Aircraft | Boeing Company, The (88277) | ||
| 17P2A3307-552 17P2A3307552 | 1560-01-455-5166 | Plate, Structural, Aircraft | Boeing Company, The (88277) | ||
| 17P2A3307-553 17P2A3307553 | 1560-01-455-5492 | Plate, Structural, Aircraft | Boeing Company, The (88277) | ||
| 17P2A3307-554 17P2A3307554 | 1560-01-455-5161 | Plate, Structural, Aircraft | Boeing Company, The (88277) | ||
| 17P2A3307-555 17P2A3307555 | 1560-01-455-5489 | Plate, Structural, Aircraft | Boeing Company, The (88277) | ||
| 17P2A3307-556 17P2A3307556 | 1560-01-455-5160 | Plate, Structural, Aircraft | Boeing Company, The (88277) | ||
| 17P2A3307-557 17P2A3307557 | 1560-01-455-5191 | Plate, Structural, Aircraft | Boeing Company, The (88277) | ||
| 17P2A3307-558 17P2A3307558 | 1560-01-455-5158 | Plate, Structural, Aircraft | Boeing Company, The (88277) | ||
| 17P2A3307-559 17P2A3307559 | 1560-01-455-5187 | Plate, Structural, Aircraft | Boeing Company, The (88277) | ||
| 17P2A3307-560 17P2A3307560 | 1560-01-455-5156 | Plate, Structural, Aircraft | Boeing Company, The (88277) | ||
| 17P2A3307-561 17P2A3307561 | 1560-01-455-5152 | Plate, Structural, Aircraft | Boeing Company, The (88277) | ||
| 17P2A3307-562 17P2A3307562 | 1560-01-467-4141 | Plate, Structural, Aircraft | III End Item Identification: C-17 acft/panel deflector troop door | Boeing Company, The (88277) | |
| 17P2A3307-563 17P2A3307563 | 1560-01-502-9752 | Panel, Structural, Aircraft | Aircraft Mission Design Series: C17-A aircraft Special Features: C/O 1 panel P/N 17P2A3307-16; material - part molded polylauryl-lactam (nylon 12); 3 plates P/N 17P2A3307-27, stock size .040 3 X 3 sheet, alclad 2024-T351, rivet (MS20426AD3) (alt), nut P/N 3D0038-3 | Boeing Company, The (88277) | |
| 17P2A3307-564 17P2A3307564 | 1560-01-503-1470 | Panel, Structural, Aircraft | Aircraft Mission Design Series: C-17A Special Features: C/O 1 panel, P/N 17P2A3307-16, 3 plates P/N 17P2A3307-27, stock size .040X3X3 sheet, (alcald T351), 9 shim, m/F -33 (al 2024-T351), rivet (MS20426AD3) (alt), nut P/N 3D0038-3 (matl.part, molded polylauryl-lactam) (NYLON-12) Material: Plastic and aluminum alloy 2024 | Boeing Company, The (88277) | |
| 17P2A3307-565 17P2A3307565 | 1560-01-503-0046 | Panel, Structural, Aircraft | Aircraft Mission Design Series: C-17A Special Features: C/O 1 panel, P/N 17P2A3307-15, (stocsize .100X9.27), matl.part, molded POLYLAURYL-LACTAM(NYLON-12); 3 plates, P/N 17P2A3307-27, .040X3X3, material sheet, ALCLAD2024-T3; 3 plate assy, P/N 17P2A3307-31; 9 shims, P/N 17P2A3307-33, .312X1X1, plate, AL2024-T351; rivets, P/N MS20426AD3(ALT) and 3D0276AD3(AR); effectivity 17A085-17A999; nha 17P2A3300-531 Material: Plastic and aluminum alloy 2024 | Boeing Company, The (88277) | |
| 17P2A3307-566 17P2A3307566 | 1560-01-503-0045 | Panel, Structural, Aircraft | Aircraft Mission Design Series: C-17A Special Features: C/O 1 panel, P/N 17P2A3307-16, stocksize .100X9X27, matl. part, molded polylauryl-lactam(nylon 12), 3 plates, P/N 17PA3307-27, .040X3X3, sheet, ALCLAD2024-T3; 3 plate assy., P/N 17P2A3307-31; 9 shims, P/N 17P2A3307-33, .312X1X1, plate, AL2024-T351; rivets, P/N MS20426AD3(ALT) & 3D0276AD3(AR); nha 17P2A3300-532;EFFECTIVITY 17A085-17A999 Material: Plastic and aluminum alloy 2024 | Boeing Company, The (88277) | |
| 17P2A3308-502 17P2A3308502 | 1560-01-368-1291 | Fitting, Structural Component, Air | Boeing Company, The (88277) | ||
| 17P2A3309-501 17P2A3309501 | 1560-01-382-9570 | Fitting, Structural Component, Air | Boeing Company, The (88277) | ||
| 17P2A3309-502 17P2A3309502 | 1560-01-368-1292 | Fitting, Structural Component, Air | III End Item Identification: C-17 | Boeing Company, The (88277) | |
| 17P2A3310-2 17P2A33102 | 1560-01-392-9853 | Fitting, Structural Component, Air | Boeing Company, The (88277) |