Airframe Structural Components: 17P2B1230-601, 17P2B1236-2, 17P2D1045-1
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 17P2B1230-601 17P2B1230601 | 1560-01-473-3986 | Door, Access, Aircraft | Special Features: Manufacturer suggested name - escutcheon, cargo compartment, sidewall;nha 17P2B1202 Material: Plastic epoxy Material Document and Classification: DMS2297 mfr ref single material response | Boeing Company, The (88277) | |
| 17P2B1230-65 17P2B123065 | 1560-01-473-3984 | Door, Access, Aircraft | Special Features: Manufacturer suggested name - escutcheon, cargo compartment, sidewall;nha 17P2B4139, 17P2B4149, 17P2B4150, 17P2B4151, 17P2B4152, 17P2B4154, 17P2B4155, 17P2B4156, 17P2B4159, & 17P2B4160 Material: Plastic epoxy Material Document and Classification: DMS2297 mfr ref single material response | Boeing Company, The (88277) | |
| 17P2B1236-1 17P2B12361 | 1560-01-480-8118 | Panel, Structural, Aircraft | Aircraft Mission Design Series: C-17 Special Features: Manufacturers suggested name-liner, troop door;core is grade b with density of 1.8 pcf Material: Glass fiber and plastic polyimide | Boeing Company, The (88277) | |
| 17P2B1236-2 17P2B12362 | 1560-01-480-8119 | Panel, Structural, Aircraft | Aircraft Mission Design Series: C-17 Special Features: Manufacturers suggested name-liner, troop door;core is grade b with density of 1.8 pcf Material: Glass fiber and plastic polyimide | Boeing Company, The (88277) | |
| 17P2B1262-727 17P2B1262727 | 1560-01-453-5910 | Bracket, Structural Component, Air | Boeing Company, The (88277) | ||
| 17P2B4159-501 17P2B4159501 | 1560-01-442-1975 | Panel, Structural, Aircraft | Special Features: Panel structural | Boeing Company, The (88277) | |
| 17P2C1376-503 17P2C1376503 | 1560-01-528-9890 | Support, Structural Component, Air | Aircraft Mission Design Series: C-17A Special Features: Matl bar steel 4340, ams 6414, heattreat to 160000-180000 psi per dps 5.00AMS 2759 may be used subject to the restrictions of note AAZ1; dim are stock matl Material: Steel comp 4340 | Boeing Company, The (88277) | |
| 17P2C7835-1 17P2C78351 | 1560-01-518-0005 | Bracket, Mounting | Boeing Company, The (88277) | ||
| 17P2C7835-501 17P2C7835501 | 1560-01-532-0541 | Bracket, Mounting | Boeing Company, The (88277) | ||
| 17P2C7835-502 17P2C7835502 | 1560-01-534-5752 | Bracket, Mounting | Material: Aluminum alloy 7050 END Item Identification: C-17 globemaster iii Special Features: Matl plate al 7050-T7651, dms 2233TEMPER T7651;DIM are stock matl;nha 17P2C7801 | Boeing Company, The (88277) | |
| 17P2C7841-501 17P2C7841501 | 1560-01-531-5910 | Support, Structural Component, Air | Aircraft Mission Design Series: C-17A Special Features: The -502 opposite Aircraft Location: Plate assy-uplock mechanism, stabilizer strut | Boeing Company, The (88277) | |
| 17P2C7841-502 17P2C7841502 | 1560-01-531-5914 | Support, Structural Component, Air | Aircraft Mission Design Series: C-17A Special Features: The -501 opposite Aircraft Location: Plate assy uplock mechanism, stabilizer strut | Boeing Company, The (88277) | |
| 17P2C7844-1 17P2C78441 | 1560-01-531-5068 | Latch Assembly, Aircraft | Aircraft Mission Design Series: C-17 Aircraft Location: Hook assy, uplock mechanism, stabilizer strut III Part Name Assigned BY Controlling Agency: HOOK | Boeing Company, The (88277) | |
| 17P2C7844-501 17P2C7844501 | 1560-01-541-0952 | Latch Assembly, Aircraft | Aircraft Mission Design Series: C-17 Aircraft Location: Hook assembly, uplock mechanism, stabilizer strut | Boeing Company, The (88277) | |
| 17P2C7848-501 17P2C7848501 | 1560-01-531-2015 | Guide, Roller | III End Item Identification: C-17 acft Special Features: Matl per AMS5862 Material: Steel corrosion resisting | Boeing Company, The (88277) | |
| 17P2C7851-1 17P2C78511 | 1560-01-525-7413 | Bracket, Structural Component, Air | Aircraft Mission Design Series: C-17A Special Features: Dim are stock matl; heat treat T7651; opposite -2 Material: Aluminum alloy 7050 | Boeing Company, The (88277) | |
| 17P2C7851-2 17P2C78512 | 1560-01-525-5168 | Bracket, Structural Component, Air | Aircraft Mission Design Series: C-17A Special Features: Dim are stock matl;matl al 7050-T7651 Material: Aluminum alloy 7050 | Boeing Company, The (88277) | |
| 17P2C7853-1 17P2C78531 | 1560-01-542-4233 | Bracket, Structural Component, Air | Aircraft Mission Design Series: C-17A Special Features: Matl al plate 7050/DMS 2233 T7651DIM are stock matl Material: Aluminum alloy 7050 | Boeing Company, The (88277) | |
| 17P2C7857-1 17P2C78571 | 1560-01-542-3836 | Bracket, Structural Component, Air | Aircraft Mission Design Series: C-17A Special Features: Matl al plate 7050-T7651, dms 2233TEMPER T7651;DIM are stock matl Material: Aluminum alloy 7050 | Boeing Company, The (88277) | |
| 17P2D1045-1 17P2D10451 | 1560-01-361-4043 | Tube Assembly, Metal | END Item Identification: C-17 aircraft Part Name Assigned BY Controlling Agency: Fuel line, fabricated, airframe | Boeing Company, The (88277) |