Airframe Structural Components: 233T5221-11, 234P5001-1, 234P5001-16
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 233T5221-11 233T522111 | 1560-01-687-4130 | Plate, Structural, Aircraft | The Boeing Company (81205) | ||
| 233T5221-12 233T522112 | 1560-01-687-1115 | Plate, Structural, Aircraft | The Boeing Company (81205) | ||
| 233T5227-41 233T522741 | 1560-01-687-0788 | Panel, Structural, Aircraft | The Boeing Company (81205) | ||
| 233T5227-42 233T522742 | 1560-01-687-0790 | Panel, Structural, Aircraft | The Boeing Company (81205) | ||
| 233T5227-43 233T522743 | 1560-01-687-0792 | Panel, Structural, Aircraft | The Boeing Company (81205) | ||
| 233T5227-44 233T522744 | 1560-01-687-3459 | Panel, Structural, Aircraft | The Boeing Company (81205) | ||
| 233W6301-12B 233W630112B | 1560-01-687-0566 | Panel, Structural, Aircraft | The Boeing Company (81205) | ||
| 233W6301-13B 233W630113B | 1560-01-686-9341 | Panel, Structural, Aircraft | The Boeing Company (81205) | ||
| 233W6301-14B 233W630114B | 1560-01-686-9342 | Panel, Structural, Aircraft | The Boeing Company (81205) | ||
| 2344788 | 1560-01-689-0987 | Fitting, Structural Component, Air | End Item Identification: U-2 aircraft Part Name Assigned BY Controlling Agency: Fitting-ejection seat 21B | Lockheed Martin Corporation (0L1E5) | |
| 234N0003-6 234N00036 | 1560-01-689-5764 | Absorber Assembly | End Item Identification: CH47 chinook helicopter Part Name Assigned BY Controlling Agency: Absorber assembly, vibration | The Boeing Company (77272) | |
| 234N1011-1 234N10111 | 1560-01-675-4763 | Fitting, Structural Component, Air | End Item Identification: CH-47D helicopter Part Name Assigned BY Controlling Agency: Fitting Special Features: Used for isolation assy, independent fuel | The Boeing Company (77272) | |
| 234N3002-2 234N30022 | 1560-01-692-6981 | Insert Assembly | The Boeing Company (77272) | ||
| 234P4116-6 234P41166 | 1560-01-679-7534 | Cover, Access, Aircraft | Width: 3.10 inches nominal Length: 3.10 inches nominal Body Thickness: 0.50 inches maximum | The Boeing Company (77272) | |
| 234P5001-1 234P50011 | 1560-01-686-0306 | Parts kit, Fuselage | The Boeing Company (77272) | ||
| 234P5001-10 234P500110 | 1560-01-677-2792 | Panel, Structural, Aircraft | The Boeing Company (77272) | ||
| 234P5001-11 234P500111 | 1560-01-677-2583 | Panel, Structural, Aircraft | The Boeing Company (77272) | ||
| 234P5001-12 234P500112 | 1560-01-682-2114 | Panel, Structural, Aircraft | The Boeing Company (77272) | ||
| 234P5001-13 234P500113 | 1560-01-682-2111 | Panel, Structural, Aircraft | The Boeing Company (77272) | ||
| 234P5001-16 234P500116 | 1560-01-682-2104 | Panel, Structural, Aircraft | The Boeing Company (77272) |