Airframe Structural Components: 23-4159, 2347191-2, 23499-2
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 23-4159 234159 | 1560-00-627-1627 | Retainer, nut, Forward Hinge-Tip P | III End Item Identification: Acft model B-52 General Characteristics Item Description: C/O nut plate P/N K1000-428, radius filler P/N 23-4159-1 | The Boeing Company (81205,82918) | |
| 2341982-4-1 234198241 | 1560-01-571-7792 | Duct Assembly, Bleed Air | Aircraft Mission Design Series: F-16 III Part Name Assigned BY Controlling Agency: Air duct assembly | Honeywell International Inc. (70210) | |
| 2342609 | 1560-00-024-3284 | Ring Assembly, Window | III End Item Identification: Aircraft model C-118A | Boeing Company, The (18355,88277) | |
| 23-4281-1 2342811 | 1560-00-670-3672 | Pivot Assembly, Adapter | General Characteristics Item Description: Steel, MIL-S-6050 and MIL-S-6758, 0.860 in. lg, W/pin | The Boeing Company (81205,82918) | |
| 23-43005 2343005 | 1560-00-125-1952 | Support, Engine Cont | Boeing Company, The (43999) | ||
| 234-4030 2344030 | 1560-01-524-5386 | Latch Assembly, Aircraft | III End Item Identification: Transport aircraft, boeing 707, air refueling pod, sargent fletcher inc | Sargent Fletcher Inc. (72429) | |
| 2344584 | 1560-00-046-1858 | Fairing, Aircraft | Aircraft Mission Design Series: C-118/D6 Special Features: C/O 2 cres type 347 sheet | Boeing Company, The (18355,88277) | |
| 2344M0004-03 2344M000403 | 1560-01-557-8176 | Support, Structural Component, Air | Aircraft Mission Design Series: C-130 Material: Aluminum alloy 6061 Aircraft Location: Copilots side panel AQ-36 lpcr | MTC Technologies Inc. (0YCM5) | |
| 2344M0007-01 2344M000701 | 1560-01-557-8181 | Panel, Structural, Aircraft | Aircraft Mission Design Series: C-130 Material: Aluminum alloy 6061 Aircraft Location: AQ-36 lpcr | MTC Technologies Inc. (0YCM5) | |
| 2344M0007-10 2344M000710 | 1560-01-558-3170 | Panel, Structural, Aircraft | Aircraft Mission Design Series: C-130 Material: Aluminum alloy 6061 Material Document and Classification: AMS-QQ-250/AA std mil std single material response | MTC Technologies Inc. (0YCM5) | |
| 23-45002-2 23450022 | 1560-00-123-7746 | Pedal Assembly, Engi | Boeing Company, The (43999) | ||
| 234-5013 2345013 | 1560-01-530-7385 | Canopy Assembly | III End Item Identification: Tornado aircraft Special Features: Next higher assembly buddy-buddy refueling pod | Sargent Fletcher Inc. (72429) | |
| 2345-808 2345808 | 1560-01-151-2427 | Former, Aircraft | Aircraft Mission Design Series: B-52 aircraft Material: Titanium Aircraft Location: Inbd strut stiffener fillet fairing instl | The Boeing Company (81205) | |
| 23-4598 234598 | 1560-00-778-9410 | Plug, Adjustment Access | General Characteristics Item Description: Aluminum alloy, QQ-A-250/5, 0.50 in. dia, 0.016 in. thk | Airborne Industries Inc. (66860) CCF Enterprises Inc. (08QQ4) The Boeing Company (81205,82918) | |
| 2347191-2 23471912 | 1560-00-696-9754 | Fitting, Structural Component, Air | Aircraft Mission Design Series: C-47 | Boeing Company, The (18355,88277) | |
| 2348193 | 1560-00-303-7121 | Brace, Carburetor Preheat Pulley | General Characteristics Item Description: Steel, MIL-T-6736, 0.438 in. od, 0.035 in. wall thk, 0.277 in. min, 0.283 max dia hole 1 end, 0.312 in. min, 0.316 max dia hole opposite end | Boeing Company, The (18355,88277) | |
| 23498-1 234981 | 1560-00-252-8604 | Armor Panel | Saint-Gobain Abrasives Inc. (44197) | ||
| 23498-3 234983 | 1560-00-252-8604 | Armor Panel | Saint-Gobain Abrasives Inc. (44197) | ||
| 23499-1 234991 | 1560-00-252-8606 | Armor Panel | Saint-Gobain Abrasives Inc. (44197) | ||
| 23499-2 234992 | 1560-00-252-8609 | Armor Panel | Saint-Gobain Abrasives Inc. (44197) | ||
| 23499-2 234992 | 1560-01-256-7959 | Armor, Supplemental, Small Arms-Fr | Saint-Gobain Abrasives Inc. (44197) |