Airframe Structural Components: 2-31407-20, 23-1600-801, 23-1605
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 2-31407-20 23140720 | 1560-00-718-0872 | Dorsal, Vertical Stabilizer | III End Item Identification: Aircraft model T38 General Characteristics Item Description: Aluminum alloy | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 2-31407-509 231407509 | 1560-01-342-7111 | Panel, Structural, Aircraft | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | ||
| 2-31411-11 23141111 | 1560-01-321-0046 | Support, Structural Component, Air | Aircraft Mission Design Series: T-38 Material: Aluminum alloy 7075 Aircraft Location: Vertical stabilizer | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 2-31411-7 2314117 | 1560-01-321-0046 | Support, Structural Component, Air | Aircraft Mission Design Series: T-38 Material: Aluminum alloy 7075 Aircraft Location: Vertical stabilizer | Northrop Grumman Systems Corporation (76823) | |
| 2-31413-501 231413501 | 1560-01-094-2379 | Spar, Aircraft | Aircraft Mission Design Series: T-38 Material: Aluminum alloy 7075 Material Document and Classification: QQ-A-250 fed spec single material response | Aeromax Industries Inc. (40581) Cell Wireless Corporation (0F2Y3) Eltee Tool & DIE Co. (7U740) Maven Engineering Corporation (65273) Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 2-31418-11 23141811 | 1560-01-341-8270 | Rib, Airfoil | III End Item Identification: Used on cf 116 F5 freedom fighter material sheet alclad .050X4.100X11.90, QQ-R-250/13 | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 2-31429-3 2314293 | 1560-00-969-4639 | Tip, Aircraft | Material: Aluminum alloy 7075 or aluminum alloy 5052 Material Document and Classification: QQ-A-250/13 fed spec 1ST material response or QQ-A-250/8 fed spec 2ND material response | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 2-31435-501 231435501 | 1560-00-101-9298 | Angle, Fuselage | General Characteristics Item Description: Aluminum alloy | Airborne Technologies Inc. (58730) Derco Aerospace Inc. (8X044) Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 2-31435-502 231435502 | 1560-00-101-9299 | Angle, Fuselage | General Characteristics Item Description: Aluminum alloy | Derco Aerospace Inc. (8X044) Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 2-31435-503 231435503 | 1560-01-010-9211 | Support, Structural Component, Air | III End Item Identification: Aircraft model F5E Special Features: Left side mtg | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 2-31435-504 231435504 | 1560-01-011-6421 | Support, Structural Component, Air | III End Item Identification: Aircraft model F5E Special Features: Right side mtg | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 2-31440-3 2314403 | 1560-01-341-2556 | Clip, Special | III End Item Identification: Aircraft CF116 | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 2-31440-4 2314404 | 1560-01-342-8100 | Clip Special | III End Item Identification: CF116 General Characteristics Item Description: 3.200 in. lg; aluminum 7075-T6 QQ-A-277, 45 deg corner | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 23147-100 23147100 | 1560-00-740-7091 | Bellows Assembly | General Characteristics Item Description: Steel | Hamilton Sundstrand Corporation (55820) Solar Turbines Incorporated (66195) Triumph Fabrications - SAN Diego (10234) | |
| 23-1532 231532 | 1560-01-147-7247 | Support, Structural Component, Air | Aircraft Mission Design Series: B-52 | The Boeing Company (81205) | |
| 23-1600 231600 | 1560-00-604-6309 | Ball, Hanger Beam, Engine Mount | III End Item Identification: Aircraft model B-52 General Characteristics Item Description: CRES | The Boeing Company (82918) | |
| 23-1600-801 231600801 | 1560-00-772-6151 | Ball, Hanger Beam, Engine Mount | III End Item Identification: Aircraft model B-52 General Characteristics Item Description: CRES | The Boeing Company (81205,82918) | |
| 23-1603 231603 | 1560-01-092-4487 | Attach Channel | III End Item Identification: Acft B52 General Characteristics Item Description: Tail fairing installation, lefthand, inboard strut, sta. 262 | The Boeing Company (81205,82918) | |
| 23-1603-1 2316031 | 1560-01-092-8277 | Attach Channel, Forward | III End Item Identification: Acft B52 General Characteristics Item Description: Tail fairing installation. 2.800 in. lg, 2.200 in. W, 0.063 in. th. 2024-0 clad QQ-A-362 0 temper, heat treat T4, finish F-2.10 | The Boeing Company (82918) | |
| 23-1605 231605 | 1560-01-148-0545 | Support, Structural Component, Air | III End Item Identification: B-52 acft Special Features: Matl al alloy, QQ-A-364, 2024-0; matl size 0.063 by 1.000 by 1.600 in. lg; used as attachment angle on tail fairing lh inboard strut | The Boeing Company (81205) |