Airframe Structural Components: 2-23240-1, 2-23258-1, 2-23277-2
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 2-23240-1 2232401 | 1560-00-139-0851 | Spar, Aircraft | Aircraft Mission Design Series: T-38 Material: Aluminum alloy 7075 Material Thickness: 47.720 inches nominal | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 2-23244-13 22324413 | 1560-00-153-9306 | Spar, Aircraft | Material: Aluminum alloy Material Document and Classification: QQ-A-277 fed spec single material response Overall Length: 39.200 inches nominal | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 2-23244-14 22324414 | 1560-00-153-9307 | Spar, Aircraft | Material: Aluminum alloy Material Document and Classification: QQ-A-277 fed spec single material response Overall Length: 39.200 inches nominal | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 2-23248-3 2232483 | 1560-00-139-0842 | Spar, Wing | III End Item Identification: Aircraft model T-38 | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 2-23248-6 2232486 | 1560-01-503-1899 | Spar, Aircraft | Material: Aluminum Overall Length: 40.000 inches nominal | Holts B A R Precision Machine Inc. (1BCC8) | |
| 2-23250-5 2232505 | 1560-01-515-6625 | Spar, Wing | III End Item Identification: F5 aircraft | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 2-23254-1 2232541 | 1560-00-137-3791 | Spar, Aircraft | Aircraft Mission Design Series: T-38 Material: Aluminum alloy 7075 | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 2-23258-1 2232581 | 1560-00-137-3785 | Spar, Aircraft | Aircraft Mission Design Series: T-38 Material: Aluminum alloy 7075 Aircraft Station Number: Sta 64.800 to 101.000 | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 2-23260-1 2232601 | 1560-00-137-3775 | Spar, Aircraft | Aircraft Mission Design Series: T-38 Material: Aluminum alloy 7075 Material Document and Classification: QQ-A-200/11 T6 fed spec single material response | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 2-23260-2 2232602 | 1560-00-137-3776 | Spar, Aircraft | Aircraft Mission Design Series: T-38 Material: Aluminum alloy 7075 Material Document and Classification: QQ-A-200/11 T6 fed spec single material response | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 2-23262-1 2232621 | 1560-00-137-3787 | Spar, Aircraft | Aircraft Mission Design Series: T-38 Material: Aluminum alloy 7075 Material Document and Classification: QQ-A-200/11 T6 fed spec single material response | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 2-23262-2 2232622 | 1560-00-137-3774 | Spar, Aircraft | Aircraft Mission Design Series: T-38 Material: Aluminum alloy 7075 Material Document and Classification: QQ-A-200/11 T6 fed spec single material response | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 2-23264-3 2232643 | 1560-00-137-3777 | Spar, Aircraft | Aircraft Mission Design Series: T-38 Material: Aluminum alloy 7075 Material Document and Classification: QQ-A-299/11 T6 fed spec single material response | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 2-23264-4 2232644 | 1560-00-137-3778 | Spar, Aircraft | Aircraft Mission Design Series: T-38 Material: Aluminum alloy 7075 Material Document and Classification: QQ-A-200/11 T6 fed spec single material response | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 2-23271-11 22327111 | 1560-00-137-3789 | Spar, Aircraft | Aircraft Mission Design Series: T-38 Material: Aluminum alloy 7075 Material Document and Classification: QQ-A-200/11 T6 fed spec single material response | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 2-23271-12 22327112 | 1560-00-137-3790 | Spar, Aircraft | Aircraft Mission Design Series: T-38 Material: Aluminum alloy 7075 Material Document and Classification: QQ-Q-200/11 T6 fed spec single material response | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 2-23271-9 2232719 | 1560-00-909-8340 | Spar, Aircraft | Material: Aluminum alloy 7075 Material Document and Classification: QQ-A-277 T6 fed spec single material response | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 2-23276-1 2232761 | 1560-00-767-9566 | Bracket, Attaching | III End Item Identification: Aircraft model T38 General Characteristics Item Description: Steel, 17-4PH cres | Alamo Aircraft Supply Inc. (55345) JO-Bar Manufacturing Corp. (15077) Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 2-23277-1 2232771 | 1560-00-709-3702 | Flap Hinge, Aileron | General Characteristics Item Description: Aluminum alloy Criticality Code Justification: TEXT | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 2-23277-2 2232772 | 1560-00-709-7218 | Flap Hinge, Aileron | General Characteristics Item Description: Aluminum alloy | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) |