Airframe Structural Components: 225-48000-96, 225-5, 2-26101-1
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 225-48000-96 2254800096 | 1560-00-079-0940 | Tank, Fuel, Aircraft | Verco Industries (52764) | ||
| 225-48000-97 2254800097 | 1560-00-079-0939 | Tank, Fuel, Aircraft | Verco Industries (52764) | ||
| 225-48002 22548002 | 1560-00-587-9230 | Tube Assembly, Fuel Tank | III End Item Identification: Acft model A1E | Pastushin Aviation Co. (81032) | |
| 22549 | 1560-00-950-5938 | Housing, Rotary Linear Control | III End Item Identification: Model F104 acft | Triumph Controls LLC (78710) | |
| 225-5 2255 | 1560-00-694-4605 | Core, Heater Exhaust | General Characteristics Item Description: Cres type 321 | Hanlon and Wilson Co. (73056) | |
| 22564-34 2256434 | 1560-00-703-9642 | Clamp Assembly, Collector | General Characteristics Item Description: Steel | Lawrence Aviation Industries (13805) | |
| 2-26000-1 2260001 | 1560-01-515-6626 | Flap, Wing Landing | III End Item Identification: F5 aircraft | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 2-26000-2 2260002 | 1560-01-515-6627 | Flap, Wing Landing | III End Item Identification: F5 aircraft | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 226017 | 1560-00-198-7811 | Beam, Aircraft | Aircraft Mission Design Series: T-33 Special Features: U/a: beam assy, rudder walking; MATL:0.250IN min, 0.267IN max dia hole thru side 2 places, roller bearing staked in thru side 3 places | Lockheed Martin Corporation (98897) | |
| 226061 | 1560-00-124-2302 | Rod End Assembly, Pe | Lockheed Martin Corporation (98897) | ||
| 2-26100-4 2261004 | 1560-01-515-6628 | Strip Flap | Special Features: Used on T38 aircraft | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 2-26100-501 226100501 | 1560-00-868-2156 | Flap, Wing Landing | III End Item Identification: Aircraft model no. T-38 | Northrop Grumman Systems Corporation (76823) | |
| 2-26100-502 226100502 | 1560-00-868-2157 | Flap, Wing Landing | III End Item Identification: Aircraft model no. T-38 | Northrop Grumman Systems Corporation (76823) | |
| 2-26100-503 226100503 | 1560-00-868-2156 | Flap, Wing Landing | III End Item Identification: Aircraft model no. T-38 | Northrop Grumman Systems Corporation (76823) | |
| 2-26100-504 226100504 | 1560-00-868-2157 | Flap, Wing Landing | III End Item Identification: Aircraft model no. T-38 | Northrop Grumman Systems Corporation (76823) | |
| 2-26100-505 226100505 | 1560-00-868-2156 | Flap, Wing Landing | III End Item Identification: Aircraft model no. T-38 | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 2-26100-506 226100506 | 1560-00-868-2157 | Flap, Wing Landing | III End Item Identification: Aircraft model no. T-38 | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 2-26100-601 226100601 | 1560-00-868-2156 | Flap, Wing Landing | III End Item Identification: Aircraft model no. T-38 | Northrop Grumman Systems Corporation (76823) | |
| 2-26100-602 226100602 | 1560-00-868-2157 | Flap, Wing Landing | III End Item Identification: Aircraft model no. T-38 | Northrop Grumman Systems Corporation (76823) | |
| 2-26101-1 2261011 | 1560-00-908-1795 | Support, Structural Component, Air | Material: Aluminum alloy Material Document and Classification: QQ-A-250/13 T6 fed spec single material response or QQ-A-250/5 T0 fed spec single material response | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) |