Airframe Structural Components: 114S4606-2, 114S4622-11, 114S4836-1
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 114S4606-2 114S46062 | 1560-00-831-0940 | Cover, Access | Material: Aluminum alloy 2024 Material Document AND Classification: QQ-A-250/5, T3 fed spec single material response Surface Treatment: Anodize | The Boeing Company (77272) | |
| 114S4607-2 114S46072 | 1560-00-827-0742 | Cover, Access | Material: Aluminum alloy 2024 Material Document AND Classification: QQ-A-250/5, T3 fed spec single material response Surface Treatment: Anodize | The Boeing Company (77272) | |
| 114S4621-115 114S4621115 | 1560-01-462-1628 | Support, Structural Component, Air | Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-362, T4 fed spec single material response Overall Length: 13.500 inches nominal | The Boeing Company (77272) | |
| 114S4621-118 114S4621118 | 1560-00-950-2433 | Support Assembly, BL | The Boeing Company (77272) | ||
| 114S4622-11 114S462211 | 1560-01-380-3394 | Support, Structural Component, Air | The Boeing Company (77272) | ||
| 114S4801-1 114S48011 | 1560-00-906-6762 | Fitting Attachment, | The Boeing Company (77272,81205) | ||
| 114S4802-1 114S48021 | 1560-00-918-2679 | Support Assembly, Aft Platform | General Characteristics Item Description: Magnesium alloy, QQ-M-40, comp ZK60A, temp T5 or comp AZ80A-F | The Boeing Company (77272,81205) | |
| 114S4802-3 114S48023 | 1560-00-918-2678 | Support, Structural Component, Air | Special Features: Magnesium alloy QQ-M-40 | The Boeing Company (77272,81205) | |
| 114S4802-5 114S48025 | 1560-00-916-2605 | Support, Structural Component, Air | Special Features: Magnesium alloy QQ-M-40 | The Boeing Company (77272) | |
| 114S4802-7 114S48027 | 1560-00-916-2604 | Support, Structural Component, Air | Special Features: C/osupport 114S4802-15, magnesium alloy QQ-M-40, support 114S4802-25, magnesium alloy QQ-M-31 | The Boeing Company (77272) | |
| 114S4802-9 114S48029 | 1560-01-459-2742 | Support, Structural Component, Air | Aircraft Mission Design Series: CH47D Material: Aluminum Aircraft Location: Aft pylon | The Boeing Company (77272) | |
| 114S4811-5 114S48115 | 1560-00-828-3320 | Fitting, Trunnion Ac | The Boeing Company (77272) | ||
| 114S4823-1 114S48231 | 1560-00-133-6975 | Support Assy, Bell Crank | General Characteristics Item Description: Aluminum alloy, 7075, T6; QQ-A-277, T6; 5.480 in. nom O/a lg | The Boeing Company (77272) | |
| 114S4824-1 114S48241 | 1560-00-949-8255 | Support, Structural Component, Air | Special Features: Aluminum alloy QQ-A-200/11 7075-T6, 9.440 in. lg | The Boeing Company (77272) | |
| 114S4827-7 114S48277 | 1560-01-380-3771 | Support, Structural Component, Air | The Boeing Company (77272) | ||
| 114S4828-12 114S482812 | 1560-01-500-7091 | Truss Assembly, Aircraft | III End Item Identification: CH-47 Special Features: Next higher assembly nsn 1560-00-071-7766 and part number 114S4828-2 III Part Name Assigned BY Controlling Agency: Truss assembly support | The Boeing Company (77272) | |
| 114S4828-2 114S48282 | 1560-00-071-7766 | Truss Assy, Support, | The Boeing Company (77272) | ||
| 114S4832-3 114S48323 | 1560-00-106-2378 | Support, Aft Thrust | The Boeing Company (77272) | ||
| 114S4832-4 114S48324 | 1560-01-380-3855 | Support, Structural Component, Air | The Boeing Company (77272) | ||
| 114S4836-1 114S48361 | 1560-01-449-6256 | Support, Structural Component, Air | Special Features: Used on the chinook helicopter | The Boeing Company (77272) |