Airframe Structural Components: 17P2A3955-513, 17P2A5005-3, 17P2A5010-77
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 17P2A3955-513 17P2A3955513 | 1560-01-547-6541 | Fairing, Aircraft | Boeing Company, The (88277) | ||
| 17P2A3955-514 17P2A3955514 | 1560-01-468-6515 | Fairing, Aircraft | Aircraft Mission Design Series: C-17A Special Features: Manufactuer suggested name - fairings, outbd mlg door hinges, lhs, rhs;nha 17P2A3997 Material: Plastic aramid and plastic epoxy | Boeing Company, The (88277) | |
| 17P2A3965-501 17P2A3965501 | 1560-01-444-2942 | Support, Structural Component, Air | Aircraft Mission Design Series: C-17A Special Features: Requested name - arm assembly, fwd outbd door stop-mlg sta 933.000; nha 17P2A3998 Material: Aluminum alloy | Boeing Company, The (88277) | |
| 17P2A3965-502 17P2A3965502 | 1560-01-443-4090 | Support, Structural Component, Air | Aircraft Mission Design Series: C-17A Special Features: Requested name - arm assembly, fwd outbd door stop-mlg sta 933.000; nha 17P2A3998;17A001-034 Material: Aluminum alloy | Boeing Company, The (88277) | |
| 17P2A3967-1 17P2A39671 | 1560-01-485-5652 | Fitting, Structural Component, Air | Boeing Company, The (88277) | ||
| 17P2A3971-1 17P2A39711 | 1560-01-541-3177 | Hinge, Aircraft | Aircraft Mission Design Series: C-17A Special Features: Effectivity 17A164-184; nha 17P2A3901; C/O 1 fitting (material aluminum flatique qualified 7050-T7451); 2 bushing Aircraft Location: Mlg door, inbd fwd | Boeing Company, The (88277) | |
| 17P2A3971-501 17P2A3971501 | 1560-01-541-2460 | Hinge, Door, Aircraft | Aircraft Mission Design Series: C-17A Special Features: Hinge assy, plate alum al 7075-T745;DIM are stock matl Material: Aluminum alloy 7075 | Boeing Company, The (88277) | |
| 17P2A3971-503 17P2A3971503 | 1560-01-541-2461 | Hinge, Door, Aircraft | Aircraft Mission Design Series: C-17A Special Features: Plate alum al 7075-T7451;DIM are stock matl Material: Aluminum alloy 7075 | Boeing Company, The (88277) | |
| 17P2A3971-505 17P2A3971505 | 1560-01-541-2463 | Hinge, Door, Aircraft | Aircraft Mission Design Series: C-17A Special Features: Matl plate alum al 7075-T7451;DIM are stock matl Material: Aluminum alloy 7075 | Boeing Company, The (88277) | |
| 17P2A3971-507 17P2A3971507 | 1560-01-541-8040 | Hinge, Door, Aircraft | III End Item Identification: C-17A Aircraft Mission Design Series: C-17A Special Features: Opposite -503; effectivity 17A164-17A999; nha 17P2A3901; C/O 1 (-15 fitting, 3.5 X 5 X 9.5 gr lgwise, DMS2459 plate fatique qualified T7451 AL7050;DIM. are stock matl | Boeing Company, The (88277) | |
| 17P2A3971-509 17P2A3971509 | 1560-01-541-7472 | Hinge, Door, Aircraft | III End Item Identification: C-17A Aircraft Mission Design Series: C-17A Special Features: C/O 1(BUSHING m/F 54928911-8A038), 1 fitting 3.5 X 5 X 7 gr lgwise; heattreat T7451 alum plate, fatique qualified; DMS2459; dim. are stock matl | Boeing Company, The (88277) | |
| 17P2A3971-511 17P2A3971511 | 1560-01-541-4083 | Hinge, Door, Aircraft | Aircraft Mission Design Series: C-17 Special Features: M/O AL2050 Material: Aluminum alloy | Boeing Company, The (88277) | |
| 17P2A3971-513 17P2A3971513 | 1560-01-541-4084 | Hinge, Door, Aircraft | Aircraft Mission Design Series: C-17 Special Features: M/O AL2050 Material: Aluminum alloy | Boeing Company, The (88277) | |
| 17P2A5003-3 17P2A50033 | 1560-01-432-2895 | Panel, Structural, Aircraft | Aircraft Mission Design Series: C-17A Special Features: Panel instl, mlg pod - rh, Y=487.000 - Y=511.500 Material: Plastic epoxy and plastic polyamide | Boeing Company, The (88277) | |
| 17P2A5004-3 17P2A50043 | 1560-01-432-2891 | Panel, Structural, Aircraft | Aircraft Mission Design Series: C-17A Special Features: Panel instl - mlg pod, rh, Y=683.500 to Y=808.500 Material: Plastic epoxy and plastic polyamide | Boeing Company, The (88277) | |
| 17P2A5005-3 17P2A50053 | 1560-01-432-2890 | Panel, Structural, Aircraft | Aircraft Mission Design Series: C-17A Special Features: Panel instl, mlg pod - rh, Y=511.500 - Y=585.000 Material: Plastic epoxy and plastic polyamide | Boeing Company, The (88277) | |
| 17P2A5006-80 17P2A500680 | 1560-01-416-8800 | Panel, Structural, Aircraft | Aircraft Mission Design Series: C-17A Special Features: Panel instl, mlg pod, Y=1001.500 to Y=1066.875 Material: Plastic polyamide and plastic aramid | Boeing Company, The (88277) | |
| 17P2A5008-109 17P2A5008109 | 1560-01-455-7290 | Panel, Structural, Aircraft | Boeing Company, The (88277) | ||
| 17P2A5008-3 17P2A50083 | 1560-01-453-7662 | Plate, Structural, Aircraft | Boeing Company, The (88277) | ||
| 17P2A5010-77 17P2A501077 | 1560-01-432-2897 | Panel, Structural, Aircraft | Aircraft Mission Design Series: C-17A Special Features: Panel instl - mlg pod, rh, Y=696.000 - Y=808.500 Material: Plastic epoxy and plastic polyamide | Boeing Company, The (88277) |