Airframe Structural Components: 17P2G1198-501, 17P2N1044-49, 17P2N3001-511
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 17P2G1198-501 17P2G1198501 | 1560-01-479-7806 | Support, Structural Component, Air | Aircraft Mission Design Series: C-17 Special Features: Consists of (1) -5 plate and 5 nut plates. manufacturers suggested name is plate, structural, rail cover, ads Material: Steel corrosion resisting | Boeing Company, The (88277) | |
| 17P2G1329-525 17P2G1329525 | 1560-01-446-5563 | Cover, Access, Aircraft | Boeing Company, The (88277) | ||
| 17P2G3051-1 17P2G30511 | 1560-01-539-0851 | Support, Structural Component, Air | III End Item Identification: C-17A Aircraft Mission Design Series: C-17A Special Features: Release latch, roller converyor | Boeing Company, The (88277) | |
| 17P2G3501-1 17P2G35011 | 1560-01-391-6450 | Support, Structural Component, Air | Boeing Company, The (88277) | ||
| 17P2G3501-2 17P2G35012 | 1560-01-384-0118 | Support, Structural Component, Air | Boeing Company, The (88277) | ||
| 17P2G3502-1 17P2G35021 | 1560-01-383-9879 | Support, Structural Component, Air | Boeing Company, The (88277) | ||
| 17P2G3503 | 1560-01-466-1538 | Support, Structural Component, Air | III End Item Identification: E/I C-17A aircraft Special Features: Effective length 35.220 inches nominal; body thickness 1.000 inch nominal Material: Aluminum alloy | Boeing Company, The (88277) | |
| 17P2G3503-1 17P2G35031 | 1560-01-466-1538 | Support, Structural Component, Air | III End Item Identification: E/I C-17A aircraft Special Features: Effective length 35.220 inches nominal; body thickness 1.000 inch nominal Material: Aluminum alloy | Boeing Company, The (88277) | |
| 17P2G3503-501 17P2G3503501 | 1560-01-384-0088 | Support, Structural Component, Air | Boeing Company, The (88277) | ||
| 17P2G3532-1 17P2G35321 | 1560-01-393-1734 | Support, Structural Component, Air | III End Item Identification: C-17 globemaster aircraft Aircraft Mission Design Series: C-17 Special Features: Base ,support arm, retainer-ctr-aft fuselage; molded polyetherimide plastic with ten percent glass fiber, black;stock size 0.060X2.50X6.20 | Boeing Company, The (88277) | |
| 17P2G5203-10 17P2G520310 | 1560-01-456-1766 | Support, Tubing, Aircraft | Boeing Company, The (88277) | ||
| 17P2G5203-9 17P2G52039 | 1560-01-456-1767 | Support, Tubing, Aircraft | Boeing Company, The (88277) | ||
| 17P2G5536-2 17P2G55362 | 1560-01-477-6951 | Bracket, Structural Component, Air | Boeing Company, The (88277) | ||
| 17P2N1035-501 17P2N1035501 | 1560-01-530-7871 | Duct Assembly, Bleed Air | Aircraft Mission Design Series: C-17A aircraft Special Features: C/O 1 duct, 2 doubler, 2 duct half, 2 gusset, 3 flange, 6 bushing Material: Titanium alloy | Boeing Company, The (88277) | |
| 17P2N1044-49 17P2N104449 | 1560-01-541-1437 | Bracket, Structural Component, Air | Aircraft Mission Design Series: C-17A Material: Titanium Aircraft Location: Duct assy air cond heating tee gnd conn | Boeing Company, The (88277) | |
| 17P2N1102-1 17P2N11021 | 1560-01-543-8298 | Duct Assembly, Bleed Air | Aircraft Mission Design Series: C-17A Special Features: Max operating temp 450 degrees F Material: Titanium alloy | Boeing Company, The (88277) | |
| 17P2N1103-1 17P2N11031 | 1560-01-544-3211 | Duct Assembly, Bleed Air | Boeing Company, The (88277) | ||
| 17P2N1104-1 17P2N11041 | 1560-01-543-6923 | Duct Assembly, Bleed Air | Aircraft Mission Design Series: C-17 Material: Titanium alloy Aircraft Location: Tee-obiggs | Boeing Company, The (88277) | |
| 17P2N3001-507 17P2N3001507 | 1560-01-445-8070 | Scoop, Aircraft | Boeing Company, The (88277) | ||
| 17P2N3001-511 17P2N3001511 | 1560-01-442-8390 | Scoop, Aircraft | Aircraft Mission Design Series: C-17A Special Features: Inlet assembly, scoop-ram air;nha 17N2N0257;17A033-999 | Boeing Company, The (88277) |