Airframe Structural Components: 6-23408-10, 6-23436-5, 6-23442-1
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 6-23408-10 62340810 | 1560-00-148-1874 | Rib, Airfoil | III End Item Identification: F-5 | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 6-23413-1 6234131 | 1560-01-199-0326 | Cover, Access, Aircraft | Special Features: Cover, electrical connector-pylon, wg sta 114.50;C/O: -3 PLATE(1), PAD(1), LATCH-NUT(2), anchor BLOCK(2), shim PLATE(2), SCREW(2), RIVET(4); End Item Identification: F-5A aircraft | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 6-23415-7 6234157 | 1560-00-983-5025 | Rib, Airfoil | Aircraft Mission Design Series: F5A and F5B Special Features: Material to comply with MIL-S-5626; part of rib installation, wing part number 6-23414-1 Material: Steel | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 6-23415-8 6234158 | 1560-00-983-5024 | Rib, Airfoil | Aircraft Mission Design Series: F5A and F5B Special Features: Material to comply to MIL-S-5626; part of rib installation, wing part number 6-23414-2 Material: Steel | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 6-23418-1 6234181 | 1560-00-932-2037 | Bracket, Electrical | General Characteristics Item Description: Aluminum alloy QQ-A-250/13 | Aeromax Industries Inc. (40581) Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 6-23421-7 6234217 | 1560-00-150-8323 | Spar, Aircraft | Material: Aluminum Overall Length: 58.210 inches nominal Overall Width: 5.200 inches nominal | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 6-23423-9 6234239 | 1560-00-148-4065 | Spar, Aircraft | Aircraft Mission Design Series: F-5 Aircraft Location: Center wing section Material Document and Classification: MP-335 T73 mfr ref single material response | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 6-23425-5 6234255 | 1560-00-150-8324 | Spar, Aircraft | Material: Aluminum Overall Length: 54.700 inches nominal Overall Width: 4.565 inches nominal | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 6-23432-7 6234327 | 1560-00-162-6955 | Spar, Aircraft | Material: Aluminum alloy Material Document and Classification: QQ-A-277 fed spec single material response Overall Length: 19.000 inches nominal | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 6-23432-8 6234328 | 1560-00-162-6956 | Spar, Aircraft | Material: Aluminum alloy Material Document and Classification: QQ-A-277 fed spec single material response Overall Length: 19.000 inches nominal | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 6-23434-5 6234345 | 1560-00-150-8328 | Spar, Aircraft | Aircraft Mission Design Series: F-5 Special Features: Manufactuer suggested name - SPAR-21%, W.O.P., W.s. 85.00 to 114.50 Material: Aluminum alloy 7075 | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 6-23434-6 6234346 | 1560-00-150-8331 | Spar, Aircraft | Material: Aluminum alloy Aircraft Location: WING | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 6-23436-5 6234365 | 1560-00-150-8333 | Spar, Aircraft | Material: Aluminum alloy Material Document and Classification: QQ-A-200/11 fed spec single material response Overall Length: 18.600 inches nominal | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 6-23436-6 6234366 | 1560-00-150-8334 | Spar, Aircraft | Material: Aluminum alloy Material Document and Classification: QQ-A-200/11 fed spec single material response Overall Length: 18.600 inches nominal | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 6-23438-5 6234385 | 1560-00-153-9288 | Spar, Aircraft | Material: Aluminum alloy Overall Length: 25.350 inches nominal Overall Width: 2.750 inches nominal | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 6-23438-6 6234386 | 1560-00-153-9289 | Spar, Aircraft | Material: Aluminum alloy Overall Length: 25.350 inches nominal Overall Width: 2.750 inches nominal | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 6-23440-5 6234405 | 1560-00-150-8335 | Spar, Aircraft | Material: Aluminum alloy Material Document and Classification: QQ-A-200/11 fed spec single material response Overall Length: 18.400 inches nominal | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 6-23441-1 6234411 | 1560-00-148-4068 | Spar, Aircraft | Aircraft Mission Design Series: F-5 Special Features: Forging Material: Aluminum alloy 7075 | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 6-23441-2 6234412 | 1560-00-148-4069 | Spar, Aircraft | Aircraft Mission Design Series: F-5 Material: Aluminum alloy 7075 Aircraft Station Number: Ws 29.677 to 53.000 | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 6-23442-1 6234421 | 1560-01-515-4371 | Spar, Aircraft | Aircraft Mission Design Series: F-5 Aircraft Location: Outer wing Aircraft Station Number: W.s. 48.5 to W.s. 142.6 | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) |