Airframe Structural Components: 962378-105, 9-62402-1, 9-62430-1
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 962378-105 962378105 | 1560-01-025-8370 | Clampblock | General Characteristics Item Description: Phenolic cotton fabric, 3.220 in. min, 3.233 in. max dia 2 holes | Lockheed Martin Corporation (98897) | |
| 962379-101 962379101 | 1560-01-071-9227 | Clampblock, Brake H | Lockheed Martin Corporation (98897) | ||
| 962379-103 962379103 | 1560-01-071-9228 | Clampblock, Brake H | Lockheed Martin Corporation (98897) | ||
| 9-62401-2003 9624012003 | 1560-01-183-0091 | Support, Structural Component, Air | Aircraft Mission Design Series: E-3A Special Features: Make from 9-61956-3 | The Boeing Company (81205) | |
| 9-62401-2004 9624012004 | 1560-01-545-7070 | Support, Structural Component, Air | The Boeing Company (82918) | ||
| 9-62401-4 9624014 | 1560-01-545-7055 | Support, Structural Component, Air | The Boeing Company (82918) | ||
| 9-62401-5 9624015 | 1560-01-564-3392 | Support, Structural Component, Air | The Boeing Company (82918) | ||
| 9-62401-6 9624016 | 1560-01-564-3338 | Support, Structural Component, Air | The Boeing Company (82918) | ||
| 9-62402-1 9624021 | 1560-01-144-0731 | Stop, Throttle | III End Item Identification: Acft model C-135 General Characteristics Item Description: Steel sheet 4130 per AN-QQ-S-685; used on control stand | The Boeing Company (81205) | |
| 9-62402-11 96240211 | 1560-01-144-0731 | Stop, Throttle | III End Item Identification: Acft model C-135 General Characteristics Item Description: Steel sheet 4130 per AN-QQ-S-685; used on control stand | The Boeing Company (81205) | |
| 9-62418 962418 | 1560-01-394-3440 | Stiffener, Aircraft | Aircraft Mission Design Series: KC-135 Special Features: Finish F-2.30; nha 5-87824 and 5-87825 Material: Aluminum alloy 7075 | The Boeing Company (17765,81205) | |
| 9-62419 962419 | 1560-01-396-0343 | Fitting, Structural Component, Air | Aircraft Mission Design Series: KC-135 Special Features: Finish F-2.30; nha 5-87824 and 5-87825 Material: Aluminum alloy 7075 | The Boeing Company (81205) | |
| 9-62421 962421 | 1560-01-394-5232 | Stiffener, Aircraft | Aircraft Mission Design Series: KC-135 Special Features: Finish F-2.30 Material: Aluminum alloy 7075 | The Boeing Company (81205) | |
| 9-62425 962425 | 1560-01-394-3438 | Stiffener, Aircraft | Aircraft Mission Design Series: KC-135 Special Features: Finish F-2.30 Material: Aluminum alloy 7075 | The Boeing Company (81205) | |
| 9-62426-1 9624261 | 1560-01-394-3441 | Stiffener, Aircraft | Aircraft Mission Design Series: KC-135 Special Features: Finish F-2.115; nha 5-87828 Material: Aluminum alloy 7075 | The Boeing Company (81205) | |
| 9-62426-2 9624262 | 1560-01-394-3445 | Stiffener, Aircraft | Aircraft Mission Design Series: KC-135 Special Features: Finish F-2.115; nha 5-87828 Material: Aluminum alloy 7075 | The Boeing Company (81205) | |
| 9-62426-4 9624264 | 1560-01-394-3442 | Stiffener, Aircraft | Aircraft Mission Design Series: KC-135 Special Features: Nha 5-87828;FINISH F-2.115 Material: Aluminum alloy 7075 | The Boeing Company (81205) | |
| 9-62427 962427 | 1560-01-394-3439 | Stiffener, Aircraft | Aircraft Mission Design Series: KC-135 Special Features: Finish F-2.30; nha 5-87828 and 5-58529 Material: Aluminum alloy 7075 | The Boeing Company (81205) | |
| 9-62428 962428 | 1560-01-394-5236 | Fitting, Structural Component, Air | Aircraft Mission Design Series: C-135 Special Features: Make from -1 forging; per adcn W2:MATL 7075-T73511 extr; U/a:stiffener tie fitting Material: Aluminum alloy 7075 | The Boeing Company (81205) | |
| 9-62430-1 9624301 | 1560-01-034-6340 | Fitting, Structural Component, Air | Aircraft Mission Design Series: E-3A | The Boeing Company (81205) |