Airframe Structural Components: 22393A, 2240579, 22423
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 22393A | 1560-00-875-6527 | Bracket Assembly, Mo | Donallco Inc. (56705) Ontic Engineering & Manufacturing (45934) | ||
| 2239971 | 1560-00-122-8493 | Flange Assembly, Fuel | III End Item Identification: Aircraft model C54 | Boeing Company, The (18355,88277) | |
| 223F145 | 1560-01-379-4717 | Fitting, Structural Component, Air | III End Item Identification: Chinook Special Features: Adapter, mounting | General Dynamics Armament And (05606) | |
| 224 | 1560-00-386-8236 | Manifold, E, Haust, Ai | Hanlon and Wilson Co. (73056) | ||
| 224-0301-501 2240301501 | 1560-01-553-3939 | Duct Assembly, Bleed Air | Aircraft Mission Design Series: C5 mod | Rohr Inc. (51563) | |
| 2240579 | 1560-00-185-1148 | Fitting, Structural Component, Air | Aircraft Mission Design Series: C-54 Special Features: U/a: seat tie down fitting assy; make from steel | Boeing Company, The (18355,88277) | |
| 22405A | 1560-00-875-6528 | Support Assembly, Shaft End | General Characteristics Item Description: 1.998 in. min 2.000 in. flange dia., 1.529 in. min 1.531 in. max body dia, 4 mtg holes, 0.898 in. min 0.902 in. max O/a H | Donallco Inc. (56705) Ontic Engineering & Manufacturing (45934) | |
| 22409 | 1560-00-507-3610 | Cable Assy, Main J b | Test Data Document: 77646-22409 drawing (this is the basic governing drawing, such as a contractor drawing, original equipment manufacturer drawing, etc.; excludes any specification, standard or other document that may be referenced in a basic governing drawing) | Northrop Grumman Corporation (77646) | |
| 22410 | 1560-00-397-7779 | Magnet Assembly, Par | Test Data Document: 77646-22410 drawing (this is the basic governing drawing, such as a contractor drawing, original equipment manufacturer drawing, etc.; excludes any specification, standard or other document that may be referenced in a basic governing drawing) | Northrop Grumman Corporation (77646) | |
| 22412 | 1560-00-532-9363 | Post Assy, Tail | Piper Aircraft Inc. (77294) | ||
| 2-24131-2 2241312 | 1560-01-072-2706 | Leading Edge, Aircraft | III End Item Identification: T-38 Special Features: Improved leading edge Side FOR Which Designed: Right side | Northrop Grumman Systems Corporation (76823) | |
| 2-24131-501 224131501 | 1560-00-819-1679 | Leading Edge, Aircraft | Material: Aluminum alloy | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 2-24131-502 224131502 | 1560-01-072-2706 | Leading Edge, Aircraft | III End Item Identification: T-38 Special Features: Improved leading edge Side FOR Which Designed: Right side | Northrop Grumman Systems Corporation (76823) | |
| 2-24131-603 224131603 | 1560-00-779-6877 | Cover, Access, Aircraft | Material: Aluminum alloy 7075 Material Document and Classification: QQ-A-250/13, T6 fed spec single material response Securing Device Type: Turnlock fastener | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 2-24131-605 224131605 | 1560-00-779-6879 | Cover, Access, Aircraft | Material: Aluminum alloy 7075 Material Document and Classification: QQ-A-250/13, T6 fed spec single material response Securing Device Type: Turnlock fastener | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 2-24131-606 224131606 | 1560-00-779-6880 | Cover, Access, Aircraft | Material: Aluminum alloy 7075 Material Document and Classification: QQ-A-250/13, T6 fed spec single material response Securing Device Type: Turnlock fastener | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 2-24132-2 2241322 | 1560-01-072-2706 | Leading Edge, Aircraft | III End Item Identification: T-38 Special Features: Improved leading edge Side FOR Which Designed: Right side | Northrop Grumman Systems Corporation (76823) | |
| 2-24137-601 224137601 | 1560-00-777-4441 | Strap Assembly, Wing Tip Splice | III End Item Identification: Aircraft model T38 | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 2-24137-602 224137602 | 1560-00-777-4442 | Strap Assembly, Wing Tip Splice | III End Item Identification: Aircraft model T38 | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 22423 | 1560-00-754-5027 | Housing, Rotary Linear Control | III End Item Identification: Model F104 acft | Triumph Controls LLC (78710) |