FSC 1560 Airframe Structural Components: 1560-01-152-4414, 1560-01-152-4416, 1560-01-152-4434
| NSN | MFG SKU | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 1560-01-152-4414 1560011524414 | 35-10716-7 | Plate, Structural, Aircraft | Aircraft Mission Design Series: B-52 Material: Aluminum alloy 2024 Aircraft Location: Nose cowl longeron | The Boeing Company (81205) | |
| 1560-01-152-4415 1560011524415 | 35-10716-8 | Plate, Structural, Aircraft | Aircraft Mission Design Series: B-52 Material: Aluminum alloy 2024 Aircraft Location: Nose cowl longeron | The Boeing Company (81205) | |
| 1560-01-152-4416 1560011524416 | 35-10716-801 | Plate, Structural, Aircraft | Aircraft Mission Design Series: B-52 Material: Aluminum alloy 2024 Aircraft Location: Nose cowl longeron | The Boeing Company (81205) | |
| 1560-01-152-4417 1560011524417 | 35-10716-802 | Plate, Structural, Aircraft | Aircraft Mission Design Series: B-52 Material: Aluminum alloy 2024 Aircraft Location: Nose cowl longeron | The Boeing Company (81205) | |
| 1560-01-152-4418 1560011524418 | 35-10701-172 | Plate, Structural, Aircraft | Aircraft Mission Design Series: B-52 Material: Aluminum alloy 5052 Aircraft Location: Scupper, upper door, upper cowl panel assembly | The Boeing Company (81205) | |
| 1560-01-152-4419 1560011524419 | 35-10701-179 | Plate, Structural, Aircraft | Aircraft Mission Design Series: B-52 Special Features: Finish F-8.05; opposite pn -180 Material: Steel comp 301 | The Boeing Company (81205) | |
| 1560-01-152-4420 1560011524420 | 35-10701-181 | Plate, Structural, Aircraft | Aircraft Mission Design Series: B-52 Special Features: Ht tr 180, 000-200, 000 psi; finish F-8.05; opposite pn -182 Material: Steel corrosion resisting | The Boeing Company (81205) | |
| 1560-01-152-4421 1560011524421 | 35-10701-182 | Plate, Structural, Aircraft | Aircraft Mission Design Series: B-52 Special Features: Ht tr 180, 000-200, 000 psi; finish F-8.05; oppossite pn -181 Material: Steel corrosion resisting | The Boeing Company (81205) | |
| 1560-01-152-4422 1560011524422 | 35-10701-188 | Plate, Structural, Aircraft | Aircraft Mission Design Series: B-52 Special Features: Ht tr 180, 000-200, 000 psi; finish F-8.05 Material: Steel corrosion resisting | The Boeing Company (81205) | |
| 1560-01-152-4424 1560011524424 | 39-10785-4 | Plate, Structural, Aircraft | Aircraft Mission Design Series: B-52 Material: Aluminum alloy 2024 Aircraft Location: Doubler isc engine wrap cowl | The Boeing Company (81205) | |
| 1560-01-152-4425 1560011524425 | 39-10785-801 | Plate, Structural, Aircraft | Aircraft Mission Design Series: B-52 Material: Aluminum alloy 2024 Aircraft Location: Doubler misc engine wrap cowl | The Boeing Company (81205) | |
| 1560-01-152-4426 1560011524426 | 35-8226-204 | Plate, Structural, Aircraft | Aircraft Mission Design Series: B-52 Special Features: Doubler, fininsh F-10.10 Material: Titanium | The Boeing Company (81205) | |
| 1560-01-152-4427 1560011524427 | 35-8226-211 | Plate, Structural, Aircraft | Aircraft Mission Design Series: B-52 Special Features: Doulber; finish F-10.10 Material: Titanium | The Boeing Company (81205) | |
| 1560-01-152-4428 1560011524428 | 35-10704-53 | Support, Structural Component, Air | Aircraft Mission Design Series: B-52 Special Features: Used as intercostal aft, on panel-engine wrap cowl, lower Material: Aluminum alloy 2024 | The Boeing Company (81205) | |
| 1560-01-152-4429 1560011524429 | 25-2779-19 | Support, Structural Component, Air | Aircraft Mission Design Series: B-52 Special Features: Opp 25-2779-20;USED as retainer on tip assembly, fairing Material: Aluminum alloy 2024 | The Boeing Company (81205) | |
| 1560-01-152-4430 1560011524430 | 25-2779-20 | Support, Structural Component, Air | Aircraft Mission Design Series: B-52 Special Features: Opp 25-2779-19;USED as retainer on tip assembly, fairing Material: Aluminum alloy 2024 | The Boeing Company (81205) | |
| 1560-01-152-4431 1560011524431 | 25-2779-21 | Support, Structural Component, Air | Aircraft Mission Design Series: B-52 Special Features: Opp 25-2779-22;USED as retainer-outboard on tip assembly, fairing Material: Aluminum alloy 2024 | The Boeing Company (81205) | |
| 1560-01-152-4432 1560011524432 | 25-2779-22 | Support, Structural Component, Air | Aircraft Mission Design Series: B-52 Special Features: Opp 25-2779-21;USED as retainer-outboard on tip assembly, fairing Material: Aluminum alloy 2024 | The Boeing Company (81205) | |
| 1560-01-152-4433 1560011524433 | 25-2780-10 | Support, Structural Component, Air | Aircraft Mission Design Series: B-52 Material: Aluminum alloy 7075 Aircraft Location: Fuselage, gap cover | The Boeing Company (81205) | |
| 1560-01-152-4434 1560011524434 | 25-2780-11 | Support, Structural Component, Air | Aircraft Mission Design Series: B-52 Material: Aluminum alloy 7075 Aircraft Location: Fuselage gap cover | The Boeing Company (81205) |