Airframe Structural Components: 261344, 263001-3, 264A369-14
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 261344 | 1560-01-608-4927 | Plate, Structural, Aircraft | END Item Identification: CH-53E-ACCUMULATOR | Commanding Officer (96916) Valcor Engineering Corp. (96487) | |
| 2-6165-21 2616521 | 1560-01-602-7894 | Stiffener, Aircraft | Aircraft Mission Design Series: B-52G/H Special Features: Opposite -22;MAKE from BAC1506;HEAT treat T6;FINISH F-2.30 Aircraft Location: Hinge bomb door rib instl | The Boeing Company (82918) | |
| 2-6165-22 2616522 | 1560-01-602-7898 | Stiffener, Aircraft | Aircraft Mission Design Series: B-52G/H Special Features: Opposite -21;MAKE from BAC1506;HEAT treat T6;FINISH F-2.30 Aircraft Location: Hinge bomb door rib instl | The Boeing Company (82918) | |
| 2-6179 26179 | 1560-01-592-8779 | Trailing Edge, Aircraft | Part Name Assigned BY Controlling Agency: Trailing edge strip | The Boeing Company (81205) | |
| 2-6191-1 261911 | 1560-01-605-7130 | Rib, Rudder | The Boeing Company (81205) | ||
| 26-2353 262353 | 1560-01-614-9004 | Support, Structural Component, Air | The Boeing Company (81205) | ||
| 26-2353-2 2623532 | 1560-01-614-7670 | Fitting, Structural Component, Air | The Boeing Company (81205) | ||
| 2623CC-44SCL-488-26 2623CC44SCL48826 | 1560-01-601-1472 | Angle Positioning | END Item Identification: Aircraft | Hamilton Sundstrand Corporation (99167) | |
| 263001-3 2630013 | 1560-01-594-5038 | Fitting, Structural Component, Air | Aircraft Location: Base frame assembly | The Boeing Company (81205) | |
| 26-3157-3 2631573 | 1560-01-606-8442 | Bracket, Structural Component, Air | END Item Identification: B-52 Aircraft Mission Design Series: B-52 aircraft Special Features: Angle clip, side beam entry door | The Boeing Company (81205) | |
| 26-3157-8 2631578 | 1560-01-606-3037 | Support, Structural Component, Air | The Boeing Company (81205) | ||
| 26-3161-2 2631612 | 1560-01-606-6771 | Support, Structural Component, Air | The Boeing Company (81205) | ||
| 26-3163-1 2631631 | 1560-01-606-6770 | Fitting, Structural Component, Air | The Boeing Company (81205) | ||
| 26-3207-501 263207501 | 1560-01-605-2563 | Fitting, Structural Component, Air | The Boeing Company (81205) | ||
| 2633-100-01 PC NO. 304-2 263310001PCNO3042 | 1560-01-480-8174 | Valve, Check, Aircraf | Electric Boat Corporation (96169) | ||
| 26-3634 263634 | 1560-01-606-1846 | Stiffener, Aircraft | The Boeing Company (81205) | ||
| 2642-1 26421 | 1560-00-075-6702 | Cushion, Nacelle | END Item Identification: Aircraft model CH53A General Characteristics Item Description: Rubber and cork composition, ams 3251, general purpose, medium, 22.000 in. lg, 1.000 in. W | Transdigm Inc. (83930) | |
| 26-4305-1 2643051 | 1560-01-616-3195 | Fitting, Structural Component, Air | END Item Identification: B52 aircraft Material: Aluminum alloy 2024 Material Document AND Classification: QQA267 T4 fed std 1ST material response | The Boeing Company (82918) | |
| 26-4305-2 2643052 | 1560-01-616-3199 | Fitting, Structural Component, Air | END Item Identification: B-52 aircraft Material: Aluminum alloy 2024 Material Document AND Classification: QQ-A267 T4 fed std 1ST material response | The Boeing Company (82918) | |
| 264A369-14 264A36914 | 1560-01-524-8327 | Fairing, Aircraft | Aircraft Mission Design Series: C-130 Special Features: Made with aluminum astro strike and masterbond EP76M adhesive epoxy Material: Aluminum alloy and glass fiber and plastic epoxy | Lockheed Martin Corporation (03640) |