Airframe Structural Components: 9-55649-2005, 9-55650-2001, 9-55673-3
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 9-55649-2005 9556492005 | 1560-01-530-7802 | Support, Structural Component, Air | The Boeing Company (81205) | ||
| 9-55649-2006 9556492006 | 1560-01-530-7803 | Support, Structural Component, Air | The Boeing Company (81205) | ||
| 9-55649-2008 9556492008 | 1560-01-530-7805 | Support, Structural Component, Air | The Boeing Company (81205) | ||
| 9-55649-2010 9556492010 | 1560-01-583-8392 | Support, Structural Component, Air | Special Features: Used on an airborne warning and control system | The Boeing Company (81205) | |
| 9-55649-2011 9556492011 | 1560-01-530-7804 | Support, Structural Component, Air | The Boeing Company (81205) | ||
| 9-55649-3 9556493 | 1560-00-912-1396 | Support, Structural Component, Air | III End Item Identification: Acft model C-135 Special Features: Used on flap track, rear spar wing station 546.30 to 700.50 | The Boeing Company (81205) | |
| 9-55649-4 9556494 | 1560-01-134-6371 | Support, Structural Component, Air | III End Item Identification: Acft model C135 Special Features: Used as rear spar flap track support | The Boeing Company (81205) | |
| 9-55650-2001 9556502001 | 1560-01-524-9292 | Support, Structural Component, Air | The Boeing Company (81205) | ||
| 9-55663 955663 | 1560-01-418-9489 | Fitting, Structural Component, Air | Aircraft Mission Design Series: C-135 Special Features: Used as a stiffener tie fitting; make from -1 forging Material: Aluminum alloy 7075 | The Boeing Company (81205) | |
| 9-55664-1 9556641 | 1560-01-428-2656 | Fitting, Structural Component, Air | III End Item Identification: E-3A aircraft Aircraft Mission Design Series: E-3A Material: Aluminum alloy 7075 | The Boeing Company (81205) | |
| 9-55664-2 9556642 | 1560-01-428-2653 | Fitting, Structural Component, Air | III End Item Identification: E-3A aircraft Aircraft Mission Design Series: E-3A Material: Aluminum alloy 7075 | The Boeing Company (81205) | |
| 9-55665 955665 | 1560-01-394-4335 | Stiffener, Aircraft | Aircraft Mission Design Series: C-135 Special Features: Make from -1 forging Material: Aluminum alloy 7075 | The Boeing Company (81205) | |
| 9-55666 955666 | 1560-01-394-3436 | Stiffener, Aircraft | Aircraft Mission Design Series: KC-135 Special Features: Nha 5-86872;FINISH 2.30 Material: Aluminum alloy 7075 | The Boeing Company (81205) | |
| 9-55667 955667 | 1560-01-396-0344 | Fitting, Structural Component, Air | Aircraft Mission Design Series: KC-135 Special Features: Finish F-2.30;NHA 5-87831 and 5-87835 Material: Aluminum alloy 7075 | The Boeing Company (81205) | |
| 9-55668 955668 | 1560-01-394-3447 | Stiffener, Aircraft | Aircraft Mission Design Series: KC-135 Special Features: Finish F-2.30; nha 5-87831 and 5-87832 Material: Aluminum alloy 7075 | The Boeing Company (81205) | |
| 9-55668-2 9556682 | 1560-01-394-3450 | Stiffener, Aircraft | Aircraft Mission Design Series: KC-135 Special Features: Nha 5-87831 and 5-87832; finish F-2.30 Material: Aluminum alloy 7075 | The Boeing Company (81205) | |
| 9-55669 955669 | 1560-01-394-3437 | Stiffener, Aircraft | Aircraft Mission Design Series: KC-135 Special Features: Finish SRF-2.30;NHA 5-87831 Material: Aluminum alloy 7075 | The Boeing Company (81205) | |
| 95567-1 955671 | 1560-00-172-2334 | Loop Assembly, cable | Northrop Grumman Corporation (77646) | ||
| 9-55673 955673 | 1560-01-492-6541 | Plate, Structural, Aircraft | The Boeing Company (81205) | ||
| 9-55673-3 9556733 | 1560-01-520-5596 | Channel, Aircraft | Aircraft Mission Design Series: C-135 Special Features: Dim is stock material Material: Aluminum alloy 7075 | The Boeing Company (81205) |