Airframe Structural Components: 5-86389-194, 5-86528-54, 5-86871-14
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 5-86389-194 586389194 | 1560-01-616-8346 | Stiffener, Aircraft | The Boeing Company (82918) | ||
| 5-86389-195 586389195 | 1560-01-617-4768 | Stiffener, Aircraft | The Boeing Company (82918) | ||
| 5-86510-3002 5865103002 | 1560-01-613-4124 | Panel, Structural, Aircraft | The Boeing Company (81205) | ||
| 5-86528-108 586528108 | 1560-01-593-9516 | Bracket, Structural Component, Air | Aircraft Mission Design Series: KC-135 Special Features: Make from alter BAC1506-974;HEAT treat T6;FINISH F-2.30 Material: Aluminum alloy 7075 | The Boeing Company (82918) | |
| 5-86528-29 58652829 | 1560-01-593-9496 | Bracket, Structural Component, Air | Aircraft Mission Design Series: KC-135 Special Features: Heat treat T6;FINISH F-2.30;MAKE from BAC1506-575 Material: Aluminum alloy 7075 | The Boeing Company (82918) | |
| 5-86528-49 58652849 | 1560-01-593-9501 | Stiffener, Aircraft | Aircraft Mission Design Series: KC-135 Special Features: Make from AND10133-0701;HEAT treat T6;FINISH F-2.30 Material: Aluminum alloy 7075 | The Boeing Company (82918) | |
| 5-86528-54 58652854 | 1560-01-593-9507 | Bracket, Structural Component, Air | Aircraft Mission Design Series: KC-135 Special Features: Make alter BAC1506-575;HEAT treat T6;FINISH F-2.30 Material: Aluminum alloy 7075 | The Boeing Company (82918) | |
| 5-86528-55 58652855 | 1560-01-593-9512 | Bracket, Structural Component, Air | Aircraft Mission Design Series: KC-135 Special Features: Make from alter BAC1506-575;HEAT treat T6;FINISH F-2.30 Material: Aluminum alloy 7075 | The Boeing Company (82918) | |
| 5-86531 586531 | 1560-01-603-2676 | Support, Structural Component, Air | END Item Identification: 5935011189183 Special Features: Heat treet to max 200.000. Material: Steel comp 4120 | The Boeing Company (82918) | |
| 5-86543-12 58654312 | 1560-01-595-9977 | Stiffener, Aircraft | The Boeing Company (81205) | ||
| 5-86543-18 58654318 | 1560-01-601-8665 | Stiffener, Aircraft | END Item Identification: 5935011189183 | The Boeing Company (81205) | |
| 5-86543-2 5865432 | 1560-01-603-2802 | Support, Structural Component, Air | END Item Identification: 5935011189183 Special Features: Sta 420, upper cargo door Aircraft Location: Upper cargo door | The Boeing Company (81205) | |
| 5-86543-22 58654322 | 1560-01-602-7942 | Stiffener, Aircraft | END Item Identification: 5935011189183 | The Boeing Company (81205) | |
| 5-86543-25 58654325 | 1560-01-602-7967 | Stiffener, Aircraft | END Item Identification: 5935011189183 | The Boeing Company (81205) | |
| 5-86543-8 5865438 | 1560-01-593-4067 | Frame, Aircraft | The Boeing Company (81205) | ||
| 5-86547 586547 | 1560-01-593-7566 | Frame, Aircraft | Aircraft Mission Design Series: KC-135 Special Features: 0 temp;finish F-2.30 Material: Aluminum alloy 7075 | The Boeing Company (82918) | |
| 5-86574 586574 | 1560-01-593-7551 | Frame, Aircraft | Aircraft Mission Design Series: KC-135 Special Features: Heat treat T6;FINISH F-2.30 Material: Aluminum alloy 7075 | The Boeing Company (82918) | |
| 5-86868-17 58686817 | 1560-01-613-7339 | Skin, Aircraft | END Item Identification: KC-135 aircraft Aircraft Mission Design Series: KC-135 Special Features: Skin panel installation | The Boeing Company (81205) | |
| 5-86869-67 58686967 | 1560-01-617-1341 | Skin, Aircraft | END Item Identification: B52 Part Name Assigned BY Controlling Agency: Skin, panel instl upper body | The Boeing Company (81205) | |
| 5-86871-14 58687114 | 1560-01-614-1388 | Stringer, Aircraft | The Boeing Company (82918) |