Airframe Structural Components: 17P8D9305-581, 17P8D9351-1, 17P8N1055-501
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 17P8D9305-581 17P8D9305581 | 1560-01-533-9876 | Fireseal, Aircraft | III End Item Identification: C-17A Aircraft Mission Design Series: C-17A aircraft Special Features: Nha 17P8D9329; effectivity 17A041-17A999; dim. are stocksize | Boeing Company, The (88277) | |
| 17P8D9305-583 17P8D9305583 | 1560-01-484-0707 | Fireseal, Aircraft | Aircraft Mission Design Series: C-17 Special Features: Dimensions are stock size Material: Steel corrosion resisting | Boeing Company, The (88277) | |
| 17P8D9305-585 17P8D9305585 | 1560-01-484-0708 | Fireseal, Aircraft | Aircraft Mission Design Series: C-17 Special Features: Dimensions are stock size Material: Steel corrosion resisting | Boeing Company, The (88277) | |
| 17P8D9332-503 17P8D9332503 | 1560-01-483-4677 | Fairing, Aircraft | Boeing Company, The (88277) | ||
| 17P8D9332-504 17P8D9332504 | 1560-01-483-3598 | Fairing, Aircraft | Boeing Company, The (88277) | ||
| 17P8D9332-505 17P8D9332505 | 1560-01-479-1989 | Fairing, Aircraft | Aircraft Mission Design Series: C-17 Special Features: Material is molding compound, nylon 6, 10 percent glass filled, heat stabilized Material: Plastic polyamide | Boeing Company, The (88277) | |
| 17P8D9332-506 17P8D9332506 | 1560-01-479-1988 | Fairing, Aircraft | Aircraft Mission Design Series: C-17 Special Features: Material is molding compound, nylon 6, 10 percent glass filled, heat stabilized Material: Plastic polyamide | Boeing Company, The (88277) | |
| 17P8D9335-1 17P8D93351 | 1560-01-449-0735 | Door, Access, Aircraft | Boeing Company, The (88277) | ||
| 17P8D9335-501 17P8D9335501 | 1560-01-446-9452 | Door, Access, Aircraft | Special Features: Door assembly latch access End Item Identification: C-17 | Boeing Company, The (88277) | |
| 17P8D9342-1 17P8D93421 | 1560-01-486-1325 | Fairing, Aircraft | Aircraft Mission Design Series: C-17 Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-250/4 temp 3 fed spec single material response | Boeing Company, The (88277) | |
| 17P8D9342-2 17P8D93422 | 1560-01-486-1327 | Fairing, Aircraft | Aircraft Mission Design Series: C-17 Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-250/4 temp 3 fed spec single material response | Boeing Company, The (88277) | |
| 17P8D9351-1 17P8D93511 | 1560-01-481-9287 | Support, Structural Component, Air | Aircraft Mission Design Series: C-17 Material: Steel corrosion resisting Aircraft Location: Thrust reverser translating sleeve | Boeing Company, The (88277) | |
| 17P8D9355-1 17P8D93551 | 1560-01-509-5955 | Support, Structural Component, Air | Aircraft Mission Design Series: C-17A aircraft Special Features: Make from 17P8D9355-3; investment casting, cres 15-5PH 180 ksi uts; nhap/N 17P8D9243; C/O 1 casting Material: Steel corrosion resisting | Boeing Company, The (88277) | |
| 17P8D9355-2 17P8D93552 | 1560-01-509-2693 | Support, Structural Component, Air | Aircraft Mission Design Series: C-17A Special Features: Make from 17P8D9355-4; investment casting; cres 15-5 ph, 180 ksi uts; nha 17P8D9243; C/O 1 casting; effectivity 17A041-058 Material: Steel corrosion resisting | Boeing Company, The (88277) | |
| 17P8D9355-501 17P8D9355501 | 1560-01-509-2691 | Support, Structural Component, Air | Aircraft Mission Design Series: C-17A Special Features: Plate, annealed; dim. are stocksize; nha 17P8D9243; effectivity 17A063-184; lh; dms 1592 Material: Titanium | Boeing Company, The (88277) | |
| 17P8D9355-502 17P8D9355502 | 1560-01-509-2694 | Support, Structural Component, Air | Aircraft Mission Design Series: C-17A Special Features: Hna 17P8D9243;EFFECTIVITY 17A063-184; rh; dms 1592;DIMENSIONS are stocksize Material: Titanium | Boeing Company, The (88277) | |
| 17P8D9501-1 17P8D95011 | 1560-01-444-2917 | Fairing, Aircraft | Aircraft Mission Design Series: C-17A Special Features: Requested name tailcone assembly-core thrust reverser;nha 17N8D0836 | Boeing Company, The (88277) | |
| 17P8D9619-1 17P8D96191 | 1560-01-507-1927 | Fairing, Aircraft | Aircraft Mission Design Series: C-17A airlifter Special Features: Effectivity from 17A055 thru 100;NHA 17P8D8618; molding epoxy; interchgwith and replaces for spares 17P8D8619-1 and -501 Material: Glass fiber | Boeing Company, The (88277) | |
| 17P8N1024-501 17P8N1024501 | 1560-01-476-1029 | Bracket, Structural Component, Air | Boeing Company, The (88277) | ||
| 17P8N1055-501 17P8N1055501 | 1560-01-359-3135 | Support, Structural Component, Air | Aircraft Mission Design Series: C-17 Special Features: Rod assembly, duct support, pneumatic system Material: Steel corrosion resisting | Boeing Company, The (88277) |