Airframe Structural Components: 6-83850-2, 683L117-101, 6-84016-1
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 6-83850-2 6838502 | 1560-00-332-2694 | Support, Structural Component, Air | III End Item Identification: Aircraft model C135K Special Features: Aluminum alloy, QQ-A-200/3 comp 2024 cond T4, 3.050 in. O/a lg, 2.520 in. O/a W | The Boeing Company (81205) | |
| 6-83856-1 6838561 | 1560-01-551-9271 | Channel, Aircraft | Aircraft Mission Design Series: KC-135 Special Features: Dim. are stock material Material: Aluminum alloy 7075 | The Boeing Company (82918) | |
| 6-83879 683879 | 1560-01-527-2290 | Plate, Structural, Aircraft | Aircraft Mission Design Series: C-135 Special Features: Matl AL2024-T3;DIM are stock matl Material: Aluminum alloy 2024 | The Boeing Company (82918) | |
| 6-83879-1 6838791 | 1560-01-530-1160 | Plate, Structural, Aircraft | III End Item Identification: KC-135 stratotanker Aircraft Mission Design Series: KC-135 Special Features: Matl 2024-T3 sheet QQ-A-355 T3 temper;dim are stock matl | The Boeing Company (82918) | |
| 6-83879-2 6838792 | 1560-01-527-3962 | Plate, Structural, Aircraft | Aircraft Mission Design Series: C-135 Special Features: Heat treat T3; sht; dim are stocksize Material: Aluminum alloy 2024 | The Boeing Company (82918) | |
| 6-83879-3 6838793 | 1560-01-511-9293 | Plate, Structural, Aircraft | The Boeing Company (82918) | ||
| 6-83879-4 6838794 | 1560-01-509-8630 | Tab, Trim, Aircraft | III End Item Identification: C-135 aircraft Aircraft Location: Elevator Material Thickness: 0.095 inches minimum and 0.100 inches maximum | The Boeing Company (82918) | |
| 6-83887 683887 | 1560-01-552-3999 | Channel, Aircraft | The Boeing Company (82918) | ||
| 68393-1 683931 | 1560-01-371-1575 | Support, Structural Component, Air | III End Item Identification: HC-130 hercules airplane Aircraft Mission Design Series: HC-130H Aircraft Location: Aft cargo door | Hammond Cliff Trucking Inc. (77723) | |
| 683L117-101 683L117101 | 1560-00-871-5602 | Link, Nlg Steer | Lockheed Martin Corporation (98897) | ||
| 6-84003-61 68400361 | 1560-00-069-8025 | Cover, Access, Aircraft | Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-250/5, T3 fed spec single material response End Item Identification: F-5 aircraft | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 6-84004-3 6840043 | 1560-00-069-8027 | Cover, Access | END Item Identification: F-5 A/B aircraft Hole Diameter: 0.381 inches minimum and 0.387 inches maximum Securing Device Type: Turnlock fastener | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 6-84008-1 6840081 | 1560-00-069-8023 | Support, Structural Component, Air | III End Item Identification: F-5A aircraft Material: Aluminum alloy Material Document and Classification: MIL-A-21180 mil spec single material response | Northrop Grumman Systems Corporation (76823) | |
| 6-84008-1C 6840081C | 1560-00-069-8023 | Support, Structural Component, Air | III End Item Identification: F-5A aircraft Material: Aluminum alloy Material Document and Classification: MIL-A-21180 mil spec single material response | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 6-84014-4 6840144 | 1560-00-069-8031 | Panel Assy, Fuselage | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | ||
| 6-84014-53 68401453 | 1560-00-912-5731 | Panel Assembly, Pylon Rack Access | III End Item Identification: Aircraft model F5 General Characteristics Item Description: Aluminum alloy, QQ-A-250/13 | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 6-84014-59 68401459 | 1560-00-957-8218 | Panel, Structural, Aircraft | Aircraft Mission Design Series: F-5 Material Document and Classification: QQ-A-250 fed spec single material response | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 6-84014-601 684014601 | 1560-00-069-8029 | Panel Assy, Fuselage | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | ||
| 6840153 | 1560-00-343-8022 | Fitting, Structural Component, Air | III End Item Identification: T-56 aircraft engine Special Features: Bracket is flat, contains 3 mounting holes and 1 leg extending at an angle from the base, leg contains 1 hole | Allison Transmission Inc. (73342) General Motors Corp. (24617) Rolls-Royce Corporation (63005) | |
| 6840153 | 1560-01-503-6245 | Fitting, Structural Component, Air | III End Item Identification: Engine, aircraft, T56-A-7/15 (C-130B/E/H/N/P) III Part Name Assigned BY Controlling Agency: Fitting, red. gear P/s strut lh | Rolls-Royce Corporation (63005) | |
| 6-84016-1 6840161 | 1560-00-997-0689 | Guide, Pin | General Characteristics Item Description: Aluminum alloy, QQ-A-225-6 | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) |