Airframe Structural Components: 5-96283-21, 5-96283-22, 5-96284-14
MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
---|---|---|---|---|---|
5-96283-21 59628321 | 1560-01-535-7890 | Skin, Aircraft | The Boeing Company (81205) | ||
5-96283-22 59628322 | 1560-01-538-0013 | Skin, Aircraft | The Boeing Company (82918) | ||
5-96283-23 59628323 | 1560-01-535-7896 | Skin, Aircraft | The Boeing Company (81205) | ||
5-96283-24 59628324 | 1560-01-537-9665 | Skin, Aircraft | The Boeing Company (82918) | ||
5-96283-25 59628325 | 1560-01-535-6928 | Support, Structural Component, Air | The Boeing Company (81205) | ||
5-96283-26 59628326 | 1560-01-535-8890 | Former, Aircraft | Aircraft Mission Design Series: KC-135 acft Special Features: Heat treat T3; same as -821 except for hole pattern Material: Aluminum alloy 2024 | The Boeing Company (81205) | |
5-96283-805 596283805 | 1560-01-536-1582 | Skin, Aircraft | Aircraft Mission Design Series: C-135 acft Special Features: Heat treat T3 Material: Aluminum alloy 2024 | The Boeing Company (81205) | |
5-96283-806 596283806 | 1560-01-537-9968 | Skin, Aircraft | The Boeing Company (82918) | ||
5-96283-809 596283809 | 1560-01-528-2845 | Skin, Aircraft | Aircraft Mission Design Series: C-135 Special Features: Dim are stock matl;matl al 2024-T3 sheet, QQ-A-362 T3 temper Material: Aluminum alloy 2024 | The Boeing Company (82918) | |
5-96283-810 596283810 | 1560-01-528-3027 | Skin, Aircraft | Aircraft Mission Design Series: C-135 aircraft Special Features: Heat treat T3 temper; opposite -809; sheet clad; used on -2 and -28; dimensions are stock matl. Material: Aluminum alloy 2024 | The Boeing Company (82918) | |
5-96283-813 596283813 | 1560-01-528-3254 | Skin, Aircraft | Aircraft Mission Design Series: C-135 aircraft Special Features: Heat treat T3 temper; opposite -814; clad sheet; used on -1 & -27; dimensions are stock matl. Material: Aluminum alloy 2024 | The Boeing Company (82918) | |
5-96283-814 596283814 | 1560-01-531-3326 | Skin, Aircraft | The Boeing Company (82918) | ||
5-96283-817 596283817 | 1560-01-528-3946 | Skin, Aircraft | The Boeing Company (82918) | ||
5-96283-818 596283818 | 1560-01-528-3549 | Skin, Aircraft | The Boeing Company (82918) | ||
5-96283-821 596283821 | 1560-00-899-6430 | Former, Aircraft | III End Item Identification: C-135 Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-362 T3 fed spec single material response | The Boeing Company (81205) | |
5-96283-9 5962839 | 1560-01-535-9432 | Skin, Aircraft | Aircraft Mission Design Series: C-135 Special Features: Matl al aly 2024-T3, QQ-A-362 T3 temp; -10 opp; -9 same as -807;DIM are stock matl Material: Aluminum alloy 2024 | The Boeing Company (81205) | |
5-96284-11 59628411 | 1560-01-535-8855 | Web, Structural Component, Aircraf | Aircraft Mission Design Series: C-135 Special Features: Matl al aly 2024-0 clad sheet, QQ-A-362 0 temp;dim are stock matl Material: Aluminum alloy 2024 | The Boeing Company (81205) | |
5-96284-12 59628412 | 1560-01-546-6260 | Web, Structural Component, Aircraf | The Boeing Company (82918) | ||
5-96284-13 59628413 | 1560-01-535-8777 | Support, Structural Component, Air | Aircraft Mission Design Series: C-135 Special Features: Matl al aly 2024-T3, qq-a- 362 T3 temp;dim are stock matl Material: Aluminum alloy 2024 | The Boeing Company (81205) | |
5-96284-14 59628414 | 1560-01-546-6262 | Plate, Structural, Aircraft | The Boeing Company (82918) |