Airframe Structural Components: 35-10703-527, 35-10703-532, 35-10703-812
MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
---|---|---|---|---|---|
35-10703-527 3510703527 | 1560-01-124-4885 | Stringer, Aircraft | Aircraft Mission Design Series: B-52 Material: Aluminum alloy 7075 Material Document and Classification: QQ-A-287 fed spec single material response | The Boeing Company (81205) | |
35-10703-528 3510703528 | 1560-01-124-4886 | Stringer, Aircraft | Aircraft Mission Design Series: B-52 Material: Aluminum alloy 7075 Aircraft Location: Upr engine cowl | Allfab Aerospace Corporation (30819) Clark Manufacturing Inc. (22585) Tect Aerospace Inc. (34336) The Boeing Company (81205) | |
35-10703-529 3510703529 | 1560-01-152-6470 | Channel, Aircraft | Aircraft Mission Design Series: B-52 Special Features: U/a: frame channel; opp -530; matl: clad sht; 0 temper Material: Aluminum alloy 2024 | The Boeing Company (81205) | |
35-10703-530 3510703530 | 1560-01-152-6471 | Channel, Aircraft | Aircraft Mission Design Series: B-52 Special Features: U/a: frame channel; opp -529; matl:clad sht; 0 temper Material: Aluminum alloy 2024 | The Boeing Company (81205) | |
35-10703-531 3510703531 | 1560-01-152-6472 | Channel, Aircraft | Aircraft Mission Design Series: B-52 Special Features: U/a: frame channel; matl: clad sht; 0 temper; opposite -532 Material: Aluminum alloy 2024 | The Boeing Company (81205) | |
35-10703-532 3510703532 | 1560-01-152-6473 | Channel, Aircraft | Aircraft Mission Design Series: B-52 Special Features: U/a:frame channel; matl: clad sht, 0 temper; opposite -531 Material: Aluminum alloy 2024 | The Boeing Company (81205) | |
35-10703-533 3510703533 | 1560-01-152-6591 | Stringer, Aircraft | Aircraft Mission Design Series: B-52 Special Features: Matl; clad alum sht, 0 temper; opposite -534 Material: Aluminum alloy 7075 | The Boeing Company (81205) | |
35-10703-534 3510703534 | 1560-01-152-6592 | Stringer, Aircraft | Aircraft Mission Design Series: B-52 Special Features: Matl: clad sht; 0 temper; opposite -533 Material: Aluminum alloy 7075 | The Boeing Company (81205) | |
35-10703-535 3510703535 | 1560-01-152-6593 | Stringer, Aircraft | Aircraft Mission Design Series: B-52 Special Features: Matl: clad sht; 0 temper; opposite -536 Material: Aluminum alloy 7075 | The Boeing Company (81205) | |
35-10703-536 3510703536 | 1560-01-152-6594 | Stringer, Aircraft | Aircraft Mission Design Series: B-52 Special Features: Matl: clad sht; 0 temper; opposite -535 Material: Aluminum alloy 7075 | The Boeing Company (81205) | |
35-10703-537 3510703537 | 1560-01-152-6595 | Stringer, Aircraft | Aircraft Mission Design Series: B-52 Special Features: U/a: stringer-hat section; matl: clad sht, 0 temper; opposite -538 Material: Aluminum alloy 7075 | The Boeing Company (81205) | |
35-10703-538 3510703538 | 1560-01-152-6596 | Stringer, Aircraft | Aircraft Mission Design Series: B-52 Special Features: U/a: stringer-hat section; matl: clad sht; 0 temp; opposite -537 Material: Aluminum alloy 7075 | The Boeing Company (81205) | |
35-10703-801 3510703801 | 1560-01-152-6474 | Support, Structural Component, Air | Aircraft Mission Design Series: B-52 | The Boeing Company (81205) | |
35-10703-802 3510703802 | 1560-01-152-6475 | Support, Structural Component, Air | Aircraft Mission Design Series: B-52 | The Boeing Company (81205) | |
35-10703-805 3510703805 | 1560-01-145-0229 | Skin, Aircraft | III End Item Identification: Acft model B-52 Special Features: Magnesium alloy sheet AZ31B-H24 per QQ-M-44, condition H24; 70.200 in. lg, 39.000 in. W, 0.050 in. thk; opposite P/N 35-10703-806 | The Boeing Company (81205) | |
35-10703-806 3510703806 | 1560-01-145-0230 | Skin, Aircraft | III End Item Identification: Acft model B-52 Special Features: Magnesium alloy sheet, AZ31B-H24 per QQ-M-44, condition H24; 70.200 in. lg, 39.000 in. W, 0.050 in thk; opposite P/N 35-10703-805 | The Boeing Company (81205) | |
35-10703-807 3510703807 | 1560-01-152-6366 | Former, Aircraft | Aircraft Mission Design Series: B-52 Special Features: Opp 35-10703-1;0 temper;heat treat T4;FINISH F-2.115 Material: Aluminum alloy 2024 | The Boeing Company (81205) | |
35-10703-808 3510703808 | 1560-01-152-6367 | Former, Aircraft | Aircraft Mission Design Series: B-52 Special Features: Opp 35-10703-2;0 temper;heat treat T4;FINISH F-2.115 Material: Aluminum alloy 2024 | The Boeing Company (81205) | |
35-10703-811 3510703811 | 1560-01-152-6368 | Plate, Structural, Aircraft | Aircraft Mission Design Series: B-52 Special Features: Finish F-2.115, heat treat T4 Material: Aluminum alloy 2024 | The Boeing Company (81205) | |
35-10703-812 3510703812 | 1560-01-152-6369 | Plate, Structural, Aircraft | Aircraft Mission Design Series: B-52 Special Features: Finish F-2.115; heat treat T4 Material: Aluminum alloy 2024 | The Boeing Company (81205) |