Airframe Structural Components: 5-88792-3125, 5-88795-27, 5-88795-54
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 5-88792-3125 5887923125 | 1560-01-159-6749 | Panel, Structural, Aircraft | III End Item Identification: C/KC-135 aircraft Aircraft Mission Design Series: C/KC-135 Special Features: Opposite P/N -3126 | The Boeing Company (82918) | |
| 5-88792-3126 5887923126 | 1560-01-159-6750 | Panel, Structural, Aircraft | III End Item Identification: C/KC-135 Aircraft Location: Side, no. 4 nacelle Side FOR Which Designed: Left side | The Boeing Company (82918) | |
| 5-88792-32 58879232 | 1560-00-340-9312 | Cover, Access, Aircraft | Securing Device Type: Threaded fastener Mounting Opening Shape Style: 1 unthreaded hole Hole Diameter: 0.218 inches minimum and 0.229 inches maximum | The Boeing Company (81205) | |
| 5-88792-43 58879243 | 1560-00-897-8104 | Former, Aircraft | The Boeing Company (81205) | ||
| 5-88792-44 58879244 | 1560-00-005-1822 | Angle, Wing Attachment | The Boeing Company (17765,82918) | ||
| 5-88792-5 5887925 | 1560-00-340-9313 | Panel, Structural, Aircraft | III End Item Identification: KC-135 stratolifter aircraft Aircraft Mission Design Series: KC-135 Material: Aluminum alloy | The Boeing Company (81205) | |
| 5-88792-6 5887926 | 1560-00-346-9611 | Panel, Structural, Aircraft | III End Item Identification: KC-135 stratolifter aircraft Aircraft Mission Design Series: KC-135 Material: Aluminum alloy | The Boeing Company (81205) | |
| 5-88792-7 5887927 | 1560-00-340-9314 | Panel, Structural, Aircraft | III End Item Identification: KC-135 stratolifter aircraft Aircraft Mission Design Series: KC-135 Material: Aluminum alloy | The Boeing Company (81205) | |
| 5-88792-8 5887928 | 1560-00-340-9315 | Panel, Structural, Aircraft | III End Item Identification: KC-135 stratolifter aircraft Aircraft Mission Design Series: KC-135 Material: Aluminum alloy | The Boeing Company (81205) | |
| 5-88794-530 588794530 | 1560-00-767-2799 | Header Assembly, Control | III End Item Identification: Aircraft model C135 | The Boeing Company (81205) | |
| 5-88795-17 58879517 | 1560-00-992-8184 | Former, Aircraft | Aircraft Mission Design Series: KC-135 | The Boeing Company (81205) | |
| 5-88795-27 58879527 | 1560-00-525-7845 | Fairing, Aircraft | Aircraft Mission Design Series: KC-135 | The Boeing Company (81205) | |
| 5-88795-28 58879528 | 1560-00-525-7846 | Fairing, Aircraft | Aircraft Mission Design Series: KC-135 | The Boeing Company (81205) | |
| 5-88795-31 58879531 | 1560-01-122-9961 | Frame, Aircraft | The Boeing Company (81205) | ||
| 5-88795-4 5887954 | 1560-00-723-2186 | Former, Aircraft | Aircraft Mission Design Series: KC-135 | The Boeing Company (81205,82918) | |
| 5-88795-49 58879549 | 1560-01-120-1961 | Cowling | III End Item Identification: KC-135 Special Features: Annealed Material: Titanium | The Boeing Company (81205) | |
| 5-88795-5 5887955 | 1560-01-114-9479 | Skin, Aircraft | III End Item Identification: C-135 and KC-135 airplane. Aircraft Mission Design Series: C-135 and KC-135 Special Features: Finish F-12.10 | The Boeing Company (81205) | |
| 5-88795-50 58879550 | 1560-01-120-1962 | Cowling | III End Item Identification: KC-135 Special Features: Annealed Material: Titanium | The Boeing Company (81205) | |
| 5-88795-53 58879553 | 1560-01-114-9429 | Channel, Mid Fairing | III End Item Identification: Acft C135 General Characteristics Item Description: Engine nacelle strut. 4.700 in. lg, 3.400 in. W, 0.050 in. thk. 4130 annealed or normalized sht. AN-QQ-S-685, heat treat 150, 000 to 170, 000 psi, finish F1.20 | The Boeing Company (81205) | |
| 5-88795-54 58879554 | 1560-01-115-3165 | Channel, Mid Fairing | III End Item Identification: Acft C135 General Characteristics Item Description: Engine nacelle strut. 4.700 in. lg, 3.400 in. W, 0.050 in. thk. 4130 annealed or normalized sht. AN-QQ-S-685, heat treat 150, 000 to 170, 000 psi, finish F1.20 | The Boeing Company (81205) |