FSC 1560 Airframe Structural Components: 1560-01-273-4315, 1560-01-273-4327, 1560-01-273-4350
| NSN | MFG SKU | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 1560-01-273-4315 1560012734315 | 64-1070-1 | Plate, Structural, Aircraft | III End Item Identification: Acft model KC-135 Special Features: 7075-0 sheet per QQ-A-250/12; heat treat T6; finish F-2.133 and srf 12.205 interior; 23.90 in lg, 11.20 in wd, 0.080 in thk; nha 65-2516 (Non-Core Data) Supplementary Features: Used on inboard nacelle strut froont spar installation | The Boeing Company (82918) | |
| 1560-01-273-4317 1560012734317 | 64-1070-9 | Plate, Structural, Aircraft | III End Item Identification: Acft model KC-135 Special Features: 2024-0 sheet per QQ-A-250/4; heat treat T4; finish SRF2.30; 7.50 in lg, 3.00 in wd, 0.071 in thk;nha 65-2516 (Non-Core Data) Supplementary Features: Used on inboard nacelle strut front spar installation | The Boeing Company (82918) | |
| 1560-01-273-4319 1560012734319 | 64-1070-17 | Support, Structural Component, Air | III End Item Identification: Acft model KC-135 Special Features: 2024-0 sheet per QQ-A-250/4; heat treat T4; finish SRF-2.30; 77.9 in lg, 5.50 in wd, 0.160 in thk;nha 65-2516 III Supplementary Features: Functional description:used on inboard nacelle strut front spar installation | The Boeing Company (82918) | |
| 1560-01-273-4321 1560012734321 | 64-1070-30 | Support, Structural Component, Air | III End Item Identification: Acft model KC-135 Special Features: 2024-0 sheet per QQ-A-250/4; heat treat T4; finish SRF-2.30; 77.9 in lg, 5.50 in wd, 0.160 in thk; nha 65-2516; opposite -31 III Supplementary Features: Functional description:used on inboard nacelle strut front spar installation | The Boeing Company (82918) | |
| 1560-01-273-4322 1560012734322 | 64-1072-3811 64-1072-3813 | Support, Structural Component, Air | III End Item Identification: Acft model KC-135 Special Features: Steel sheet annealed 4130 per AN-QQ-S-685 or 8630 AN-S-12; heat treat 150, 000-170, 000 psi;finish F-1.20; 116.0 in lg, 7.5 in wd, 0.125 in thk; nha 65-2516 III Supplementary Features: Functional description:used on inboard strut lower spar instl | The Boeing Company (81205, 82918) | |
| 1560-01-273-4323 1560012734323 | 64-1072-3131 | Support, Structural Component, Air | III End Item Identification: Acft model KC-135 Special Features: Steel sheet annealed 4130 per AN-QQ-S-685 or 8630 AN-S-12;HEAT treat 150, 000-170, 000 psi;finish F-1.20; 116.0 in lg, 7.5 in wd, 0.125 in thk; nha 65-2516 III Supplementary Features: Functional description:used on inboard strut lower spar instl | The Boeing Company (17765, 82918) | |
| 1560-01-273-4324 1560012734324 | 64-1072-3132 | Support, Structural Component, Air | III End Item Identification: Acft model KC-135 Special Features: Steel sheet annealed 4130 per AN-QQ-S-685 or 8630 AN-S-12;FINISH F-1.20;HEAT treat 150, 000-170, 000 psi; 116.0 in lg, 7.5 in wd, 0.125 in thk; nha 65-2516 III Supplementary Features: Functional description:used on inboard strut lower spar instl | The Boeing Company (82918, 17765) | |
| 1560-01-273-4325 1560012734325 | 64-1064-3023 | Support, Structural Component, Air | III End Item Identification: KC-135 aircraft Special Features: Size .112X19X21;PART of bulkhead instl-fwd engine mount, inboard nac STA136 III Supplementary Features: Functional description:chord | The Boeing Company (82918) | |
| 1560-01-273-4326 1560012734326 | 65-2542-3040 | Support, Structural Component, Air | III End Item Identification: KC-135 aircraft Special Features: Matl 7075-0 extrusion per QQ-A-277;PART of closure rib installation-inbd nacelle strut | The Boeing Company (82918) | |
| 1560-01-273-4327 1560012734327 | 65-2542-3041 | Support, Structural Component, Air | III End Item Identification: KC-135 aircraft Special Features: Matl 7075-0 extrusion per QQ-A-277;PART of closure rib installation-inbd nacelle strut | The Boeing Company (82918) | |
| 1560-01-273-4328 1560012734328 | 64-1070-31 | Support, Structural Component, Air | III End Item Identification: Acft model KC-135 Special Features: 2024-0 sheet per QQ-A-250/4; heat treat T4; finish SRF-2.30; 77.9 in lg, 5.50 in wd, 0.160 in thk; opposite -30; nha 65-2516 III Supplementary Features: Functional description:used on inboard nacelle strut front spar installation | The Boeing Company (82918) | |
| 1560-01-273-4329 1560012734329 | 35-35736-1 | Strut, Aircraft | Aircraft Mission Design Series: KC-135 Aircraft Location: Outbd eng spare strut | The Boeing Company (82918) | |
| 1560-01-273-4330 1560012734330 | 65-2542-3015 | Support, Structural Component, Air | Aircraft Mission Design Series: KC-135 Material: Aluminum alloy 7075 Aircraft Location: Closure rib instl/inbd nacelle strut | The Boeing Company (82918, 17765) | |
| 1560-01-273-4331 1560012734331 | 65-2542-3016 | Support, Structural Component, Air | Aircraft Mission Design Series: KC-135 Material: Aluminum alloy 7075 Aircraft Location: Closure rib instl/inbd nacelle strut | The Boeing Company (17765, 82918) | |
| 1560-01-273-4333 1560012734333 | 65-2542-3002 | Support, Structural Component, Air | III End Item Identification: KC-135 aircraft Special Features: Matl 7075-0 extrusion per QQ-A-277;PART of closure rib installation-inbd nacelle strut | The Boeing Company (82918) | |
| 1560-01-273-4335 1560012734335 | 5-86022-5 | Support, Structural Component, Air | III End Item Identification: Acft model KC-135 Special Features: Clad 2024-0 sht per QQ-A-250/5, 0 temper; heat treat T4; finish F2.130; 20.0 in lg, 9.0 in wd, 0.040 in thk; nha 5-86024; located sta 1640-1676 III Supplementary Features: Functional description:used on tail cone skin installation | The Boeing Company (81205) | |
| 1560-01-273-4347 1560012734347 | 64-1072-3005 | Former, Aircraft | Aircraft Mission Design Series: KC-135 Special Features: Opposite -3006; finish F-8.05; nha 65-2516 Material: Steel comp 301 | The Boeing Company (82918, 17765) | |
| 1560-01-273-4348 1560012734348 | 64-1072-3006 | Former, Aircraft | Aircraft Mission Design Series: KC-135 Special Features: Finish F-8.05; opposite -3005; nha 65-2516 Material: Steel comp 301 | The Boeing Company (82918) | |
| 1560-01-273-4349 1560012734349 | 64-1072-3017 | Former, Aircraft | Aircraft Mission Design Series: KC-135 Special Features: Opposite -3018; nha 65-2516 Material: Steel comp 301 | The Boeing Company (82918) | |
| 1560-01-273-4350 1560012734350 | 64-1072-3018 | Former, Aircraft | Aircraft Mission Design Series: KC-135 Special Features: Finish F-8.05; opposite -3017; nha 65-2516 Material: Steel comp 301 | The Boeing Company (82918) |