Airframe Structural Components: 6-62493-10, 66-2583, 66-2687-3
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 6-62493-10 66249310 | 1560-00-673-0015 | Cylinder Assembly | The Boeing Company (81205) | ||
| 6-62493-5 6624935 | 1560-00-673-0015 | Cylinder Assembly | The Boeing Company (82918) | ||
| 6-62493-503 662493503 | 1560-00-673-0015 | Cylinder Assembly | The Boeing Company (81205,82918) | ||
| 6-62493-8 6624938 | 1560-00-673-0015 | Cylinder Assembly | The Boeing Company (81205) | ||
| 66-2500-1 6625001 | 1560-01-018-4070 | Retainer | The Boeing Company (81205) | ||
| 66-25039 6625039 | 1560-00-419-8411 | Block, Rotary Latch | III End Item Identification: Acft model KC-135 III Functional Description: Used on nacelle access door rotary latch anchor block | The Boeing Company (81205,82918) | |
| 66-25040-1 66250401 | 1560-00-419-8412 | Plate, Shim | The Boeing Company (81205,82918) | ||
| 66-25040-3 66250403 | 1560-00-419-8414 | Plate, Structural, Aircraft | III End Item Identification: Acft model KC-135 Special Features: Used on 69-11161, -2 and -3 (Non-Core Data) Supplementary Features: Used on nacelle access door rotary latch shim plate | The Boeing Company (81205) | |
| 66-25040-4 66250404 | 1560-00-419-8415 | Plate, Structural, Aircraft | III End Item Identification: Acft model B-52 | The Boeing Company (81205) | |
| 6-62513-1 6625131 | 1560-00-916-6960 | Cover, Access | Material: Aluminum alloy 7075 Material Document AND Classification: QQ-A-250/12 fed spec single material response Hole Diameter: 0.193 inches nominal | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 66-2515 662515 | 1560-01-027-6761 | Plate, Structural, Aircraft | Aircraft Mission Design Series: E-3A | The Boeing Company (81205) | |
| 66-2574 662574 | 1560-01-019-8149 | Tab Shaft | The Boeing Company (81205) | ||
| 66-2575 662575 | 1560-01-019-8150 | Terminal, TAB Shaft | The Boeing Company (81205) | ||
| 66-2583 662583 | 1560-01-322-7096 | Plate, Structural, Aircraft | Aircraft Mission Design Series: C-135 Material: Aluminum alloy 2024 Aircraft Location: Rudder to body | The Boeing Company (81205) | |
| 66-2655 662655 | 1560-01-033-9216 | Rod Assembly | III End Item Identification: E-3A acft | The Boeing Company (81205) | |
| 66-2658 662658 | 1560-01-029-0905 | Roller, Shaft | III End Item Identification: E-3A acft | The Boeing Company (81205) | |
| 66-2659-1 6626591 | 1560-01-196-6032 | Plate, Structural, Aircraft | III End Item Identification: Acft model C-18A Special Features: Nha 50-7983-1 (Non-Core Data) Supplementary Features: Used as aft galley door hinge cover | The Boeing Company (17765,81205) | |
| 66-2677 662677 | 1560-01-344-0352 | Crank, Torque Tube | III End Item Identification: Acft E-3A General Characteristics Item Description: Make from 4130 steel bar per MIL-S-6758; 2.300 in lg, 2.000 in wd, 1.200 in thk; used on aft entry door | The Boeing Company (81205) | |
| 66-2687-2 6626872 | 1560-01-027-6760 | Retainer Bearing | III End Item Identification: Acft model E-3A | The Boeing Company (81205) | |
| 66-2687-3 6626873 | 1560-01-020-5096 | Plate, Structural, Aircraft | The Boeing Company (17765,81205) |