Airframe Structural Components: 114S6505-14, 114S6552-5, 114S6601-49
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 114S6505-14 114S650514 | 1560-00-427-1724 | Support, Structural Component, Air | Material: Aluminum alloy Material Document and Classification: QQ-A-250/5 fed spec single material response and MIL-H-6088 mil spec single material response Material Thickness: 0.050 inches nominal | The Boeing Company (77272) | |
| 114S6505-15 114S650515 | 1560-01-453-0928 | Former, Aircraft | III End Item Identification: CH-47D chinook helicopter | The Boeing Company (77272) | |
| 114S6505-16 114S650516 | 1560-01-464-5065 | Former, Aircraft | III End Item Identification: Used on boeing CH47-D helicopter Material: Aluminum alloy Side FOR Which Designed: Right side | The Boeing Company (77272) | |
| 114S6505-5 114S65055 | 1560-00-115-4974 | Strake, Beam Installation | General Characteristics Item Description: Aluminum alloy QQ-A-250/5 2024 to | The Boeing Company (77272) | |
| 114S6505-6 114S65056 | 1560-00-115-4976 | Strake, Beam Installation | General Characteristics Item Description: Aluminum alloy QQ-A-250/5 2024 to | The Boeing Company (77272) | |
| 114S6505-7 114S65057 | 1560-00-115-4975 | Strake, Beam Installation | General Characteristics Item Description: Aluminum alloy QQ-A-250/5 2024 to | The Boeing Company (77272) | |
| 114S6505-8 114S65058 | 1560-00-115-4973 | Strake, Beam Installation | General Characteristics Item Description: Aluminum alloy QQ-A-250/5 2024 to | The Boeing Company (77272) | |
| 114S6551-7 114S65517 | 1560-00-802-8122 | Panel Assembly, Floo | III End Item Identification: CH-47 chinook airframe unit | The Boeing Company (77272,81205) | |
| 114S6552-27 114S655227 | 1560-00-253-1732 | Floor, Aircraft | III End Item Identification: CH-47 helicopter, cargo tr | The Boeing Company (77272) | |
| 114S6552-28 114S655228 | 1560-00-251-8751 | Floor, Aircraft | III End Item Identification: CH-47 series aircraft | The Boeing Company (77272) | |
| 114S6552-31 114S655231 | 1560-01-344-2730 | Floor Assembly | III End Item Identification: Chinook | The Boeing Company (77272) | |
| 114S6552-5 114S65525 | 1560-01-451-5490 | Ramp Assembly, Aircraft | III End Item Identification: Chinook helicopter Aircraft Mission Design Series: CH-47D Aircraft Location: Ramp floor | The Boeing Company (77272) | |
| 114S6554-1 114S65541 | 1560-01-510-3947 | Ramp Assembly, Aircraft | III End Item Identification: 1520-01-088-3669: T.M.1520-240-23P | The Boeing Company (77272) | |
| 114S6554-13 114S655413 | 1560-00-802-8130 | Skid Rail, Ramp Edge | The Boeing Company (77272,81205) | ||
| 114S6554-15 114S655415 | 1560-00-802-8062 | Strip, Chafe, Cargo R | The Boeing Company (77272,81205) | ||
| 114S6554-17 114S655417 | 1560-00-802-8063 | Strip, Chafe, Cargo Ramp | III End Item Identification: Acft model CH47A, b, C | The Boeing Company (77272,81205) | |
| 114S6554-19 114S655419 | 1560-00-802-8064 | Strip, Chafe, Cargo R | The Boeing Company (77272,81205) | ||
| 114S6554-21 114S655421 | 1560-00-802-8067 | Strip, Chafe, Cargo R | The Boeing Company (77272,81205) | ||
| 114S6554-5 114S65545 | 1560-00-802-8068 | Edge Assembly, Ramp | General Characteristics Item Description: Magnesium alloy, QQ-M-31 | The Boeing Company (77272,81205) | |
| 114S6601-49 114S660149 | 1560-01-231-1757 | Support Assy, Track | The Boeing Company (77272) |