Airframe Structural Components: 39-10786-3, 39-10797-1, 39-10798
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 39-10786-3 39107863 | 1560-01-151-8470 | Support, Structural Component, Air | Aircraft Mission Design Series: B-52 Special Features: Used on temperature regulator, inboard strut Material: Aluminum alloy 2024 | The Boeing Company (81205) | |
| 39-10789-1 39107891 | 1560-00-796-0773 | Support, Structural Component, Air | III End Item Identification: Aircraft model B52 Special Features: Aluminum alloy, QQ-A-596 comp 356 cond T51, 1.500 in. O/a lg, 1.480 in. O/a W, 1.260 in. O/a H | The Boeing Company (81205,82918) | |
| 39-10789-2 39107892 | 1560-00-796-0774 | Support, Structural Component, Air | III End Item Identification: Aircraft model B52 Special Features: Aluminum alloy, QQ-A-596 comp 356 cond T51, 1.500 in. O/a lg, 1.480 in. O/a W, 1.260 in. O/a H | The Boeing Company (81205,82918) | |
| 39-10790-806 3910790806 | 1560-01-153-2141 | Former, Aircraft | Aircraft Mission Design Series: B-52 Special Features: Decarb per ams 6350 Material: Steel comp 4130 | The Boeing Company (81205) | |
| 39-10790-807 3910790807 | 1560-01-152-7312 | Intercostal, Aircraft | Aircraft Mission Design Series: B-52 Special Features: Used on trailing edge fairing, inboard nacelle;steel sheet, annealed decard per AMS6350 Material: Steel comp 4130 | The Boeing Company (81205) | |
| 39-10790-808 3910790808 | 1560-01-152-7313 | Intercostal, Aircraft | Aircraft Mission Design Series: B-52 Special Features: Used on trailing edge fairing, inboard nacelle;steel sheet, annealed decard per AMS6350 Material: Steel comp 4130 | The Boeing Company (81205) | |
| 39-10790-809 3910790809 | 1560-01-152-7314 | Intercostal, Aircraft | Aircraft Mission Design Series: B-52 Special Features: Used on trailing edge fairing, inborad nacelle;steel sheet, annealed decard per ams 6350 Material: Steel comp 4130 | The Boeing Company (81205) | |
| 39-10790-810 3910790810 | 1560-01-152-7315 | Intercostal, Aircraft | Aircraft Mission Design Series: B-52 Special Features: Used on trailing edge fairing, inboard nacelle;steel sheet, annealed decarb per AMS6350 Material: Steel comp 4130 | The Boeing Company (81205) | |
| 39-10790-811 3910790811 | 1560-01-152-7316 | Intercostal, Aircraft | Aircraft Mission Design Series: B-52 Special Features: Used on trailing edge fairing, inboard nacelle;steel sheet, annealed decard per AMS6350 Material: Steel comp 4130 | The Boeing Company (81205) | |
| 39-10791-1 39107911 | 1560-01-152-6427 | Plate, Structural, Aircraft | III End Item Identification: B-52 Special Features: Laminated thermo-setting sheet, asbestos, phenolic resin Material Document and Classification: MIL-P-8059, grade aa mil spec single material response | The Boeing Company (81205) | |
| 39-10791-2 39107912 | 1560-01-152-6429 | Plate, Structural, Aircraft | III End Item Identification: B-52 Special Features: Laminated thermo-setting sheet, asbestos, phenolic resin Aircraft Location: Nose cowl | The Boeing Company (81205) | |
| 39-10794-2 39107942 | 1560-01-487-6576 | Support, Structural Component, Air | Air Force United States Department (98748) | ||
| 39-10795 3910795 | 1560-01-152-6378 | Stay Assembly | III End Item Identification: Acft model B-52 General Characteristics Item Description: Located BL-CL-5-8 opt to BL55 CL085 III Functional Description: Used on engine wrap cowl | The Boeing Company (81205) | |
| 39-10795-1 39107951 | 1560-00-787-9663 | Stay Assembly, Engine Wrap Cowl | General Characteristics Item Description: Aluminum alloy tube, 2024-T3, WW-T-700/3, 0.620 in. od, 0.028 in. wall thkns, bearing, rod end on one end, connector, rod end on opposite end, 24.250 in. C to C lg | The Boeing Company (81205,82918) | |
| 39-10795-2 39107952 | 1560-00-787-9664 | Stay Assembly, Engine Wrap Cowl | General Characteristics Item Description: Aluminum alloy tube, 2024-T3, WW-T-700/3, 0.620 in. od, 0.028 in. wall thkns, bearing, rod end on one end, connector, rod end on opposite end, 22.650 in. C to C lg | The Boeing Company (81205,82918) | |
| 39-10795-5 39107955 | 1560-01-162-6521 | Support, Structural Component, Air | Aircraft Mission Design Series: B-52 Material: Aluminum alloy 2024 Aircraft Location: Insert tube on stay assy engine wrap cowl | The Boeing Company (81205) | |
| 39-10797 3910797 | 1560-00-777-9249 | Plate, Duct Support, | General Characteristics Item Description: Aluminum alloy, 2024-T3, QQ-A-250/5, triangular shape, 2.200 in. l, 2.150 in. W, 0.125 in. thk, one hole 0.250 in. min, 0.254 in. max dia, three pilot holes for 3/16 rivets, applicable to B52 acft | Industrial Gasket Inc. (14890) Tect Aerospace Inc. (34336) The Boeing Company (81205,82918) | |
| 39-10797-1 39107971 | 1560-00-777-9250 | Plate, Duct Support, | General Characteristics Item Description: Aluminum alloy, 2024-T3, QQ-A-250/5, triangular shape, 2.850 in. l, 1.950 in. W, 0.125 in. thk, one hole 0.250 in. min, 0.254 in. max dia, three pilot holes for 3/16 rivets, applicable to B52 acft | The Boeing Company (81205,82918) | |
| 39-10797-2 39107972 | 1560-01-072-5365 | Plate, Structural, Aircraft | Aircraft Mission Design Series: B-52 Special Features: T3 temper;finish F2.115 Material: Aluminum alloy 2024 | The Boeing Company (81205) | |
| 39-10798 3910798 | 1560-00-787-9730 | Fitting, Cowl Support rod | III End Item Identification: Aircraft model B52 General Characteristics Item Description: Aluminum alloy, QQ-A-596 comp 356 cond T51, 1.800 in. O/a lg, 1.740 in. O/a W, 0.700 in. O/a H, 4 mtg holes 0.189 in. min, 0.199 in. max dia, one thru hole 0.189 in. min, 0.199 in. max dia | The Boeing Company (81205,82918) |