Airframe Structural Components: 5-88447-1, 5-88480-3144, 5-88480-69
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 5-88447-1 5884471 | 1560-01-126-4294 | Former, Aircraft | Aircraft Mission Design Series: KC-135 Material: Aluminum alloy 7075 Material Document and Classification: QQ-A-287 fed spec single material response | The Boeing Company (81205) | |
| 5-88447-4 5884474 | 1560-01-125-9491 | Former, Aircraft | Aircraft Mission Design Series: KC-135 Material: Aluminum alloy 7075 Material Document and Classification: QQ-A-287 fed spec single material response | The Boeing Company (81205) | |
| 5-88451 588451 | 1560-01-467-1532 | Fuel Filler cap | Special Features: One-inch thick, wing station 295.3 Material: Aluminum Overall Length: 21.500 inches nominal | The Boeing Company (81205) | |
| 5-88452 588452 | 1560-01-466-9511 | Fuel Filler cap | Special Features: 1" thick;wing sta 295.3 Material: Aluminum Overall Length: 21.500 inches nominal | The Boeing Company (81205) | |
| 5-88453 588453 | 1560-01-466-9237 | Adapter | III End Item Identification: KC-135 | The Boeing Company (81205) | |
| 5-88467 588467 | 1560-00-992-8186 | Cover, Access | Material: Aluminum alloy 6061 Securing Device Type: Threaded fastener FSC Application Data: Tank fuel, aircraft | The Boeing Company (81205) | |
| 5-88468 588468 | 1560-00-331-4844 | Cover, Access, Aircraft | The Boeing Company (81205) | ||
| 5-88471-11 58847111 | 1560-00-570-3674 | Duct Assembly, Spar Door | III End Item Identification: Aircraft model C-135 General Characteristics Item Description: Cres, MIL-T-8606 | The Boeing Company (81205) | |
| 5-88471-9 5884719 | 1560-00-570-3674 | Duct Assembly, Spar Door | III End Item Identification: Aircraft model C-135 General Characteristics Item Description: Cres, MIL-T-8606 | The Boeing Company (81205) | |
| 5-88478-3004 5884783004 | 1560-01-035-0547 | Crank Assembly, Door | III End Item Identification: E-3A awacs acft General Characteristics Item Description: Magnesium alloy casting QQM56 comp AZ91 cond hta | The Boeing Company (81205) | |
| 5-88479-10 58847910 | 1560-01-395-6755 | Spar, Aircraft | Aircraft Mission Design Series: C-135 Special Features: Opp -9; matl per bac 1560-985;T6 temper; fin: F-2.22 & F-2.30 shown on drwg; do not allow primer on surfaces calling for F-2.22; U/a a spar chord Material: Aluminum alloy 7178 | The Boeing Company (81205) | |
| 5-88479-7 5884797 | 1560-01-395-5346 | Spar, Aircraft | Aircraft Mission Design Series: KC-135 Special Features: Opposite -8; BAC1506-986; finish F-2.22 and F-2.30; heat treat T6 Material: Aluminum alloy 7178 | The Boeing Company (81205) | |
| 5-88479-8 5884798 | 1560-01-395-5345 | Spar, Aircraft | Aircraft Mission Design Series: KC-135 Special Features: BAC1506-986; finish F.2.22 and F-2.30; opposite -7 Material: Aluminum alloy 7178 | The Boeing Company (81205) | |
| 5-88479-9 5884799 | 1560-01-395-5347 | Spar, Aircraft | Aircraft Mission Design Series: C-135 Special Features: Opp -010; matl per bac 1506-985; T6 temper; fin: F-2.22 & F-2.30 shown shown on drawing & allow no primer on surfaces calling for F-2.22 Material: Aluminum alloy 7178 | The Boeing Company (81205) | |
| 5-88480-3144 5884803144 | 1560-01-583-8454 | Spar, Aircraft | Special Features: Used on an airborne warning and control system Material: Aluminum alloy 7178 Aircraft Location: Rear outboard wing | The Boeing Company (81205) | |
| 5-88480-5 5884805 | 1560-01-570-4459 | Web, Structural Component, Aircraf | The Boeing Company (82918) | ||
| 5-88480-65 58848065 | 1560-01-397-1370 | Spar, Aircraft | Aircraft Mission Design Series: KC-135 Special Features: C/O 1 rear spar assy, 1 filler, 2SCREW, 4 bolt; opposite -66 Aircraft Location: Outbd wing rear lower spar installation | The Boeing Company (81205) | |
| 5-88480-66 58848066 | 1560-01-397-1373 | Spar, Aircraft | Aircraft Mission Design Series: KC-135 Special Features: C/O 1 rear spar assy, 1 filler, 2SCREW, 4 bolt; opposite -65; heat treat T6 Aircraft Location: Outbd wing rear spar installation | The Boeing Company (81205) | |
| 5-88480-68 58848068 | 1560-01-397-1373 | Spar, Aircraft | Aircraft Mission Design Series: KC-135 Special Features: C/O 1 rear spar assy, 1 filler, 2SCREW, 4 bolt; opposite -65; heat treat T6 Aircraft Location: Outbd wing rear spar installation | The Boeing Company (81205) | |
| 5-88480-69 58848069 | 1560-01-397-1369 | Spar, Aircraft | Aircraft Mission Design Series: KC-135 Special Features: Opposite -070; heat treat T6 Aircraft Location: Outbd wing rear upper spar installation | The Boeing Company (81205) |