Airframe Structural Components: 35-8226-242, 35-8226-249, 35-8226-49
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 35-8226-242 358226242 | 1560-01-150-2128 | Former, Aircraft | Aircraft Mission Design Series: B-52 Special Features: Opposite -241;USED on -516, -522, and -545;TEMPERED to T3; finish F-2.115; stiffener Material: Aluminum alloy 2024 | The Boeing Company (81205) | |
| 35-8226-244 358226244 | 1560-01-150-2067 | Frame, Aircraft | Aircraft Mission Design Series: B-52 Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-362 fed spec single material response | The Boeing Company (81205) | |
| 35-8226-246 358226246 | 1560-01-150-2068 | Block | III End Item Identification: B-52 aircraft General Characteristics Item Description: Stock SIZE-.4 X .6 X 1.2 inches;material-laminated thermo setting sheet asbestos, phenolic resin MIL-P-8059 grade aa form sheet III Functional Description: Block-spacer | The Boeing Company (81205) | |
| 35-8226-249 358226249 | 1560-01-150-2069 | Block | III End Item Identification: B-52 aircraft General Characteristics Item Description: Stock SIZE-.5 X .7 X 1.0 INCHES;FINISH-F-6.1;MATERIAL-LAMINATED thermo setting sheet asbestos, phenolic resin MIL-P-8059 grade aa form sheet III Functional Description: Block-spacer | The Boeing Company (81205) | |
| 35-8226-250 358226250 | 1560-01-150-2456 | Block | III End Item Identification: B-52 aircraft General Characteristics Item Description: Opposite -249;STOCK SIZE-.5 X .7 X 3.0 INCHES;FINISH-F-6.;MATERIAL-LAMINATED thermo setting sheet asbestos, phenolic resin per MIL-D-8059 grade aa form sheet III Functional Description: Block-spacer | The Boeing Company (81205) | |
| 35-8226-251 358226251 | 1560-01-150-2535 | Former, Aircraft | Aircraft Mission Design Series: B-52 Special Features: Finish F-2.115; heat treated to T4; stiffener Material: Aluminum alloy 2024 | The Boeing Company (81205) | |
| 35-8226-252 358226252 | 1560-01-150-2536 | Former, Aircraft | Aircraft Mission Design Series: B-52 Special Features: Finish F-2.115; heat treated to T4; stiffener Material: Aluminum alloy 2024 | The Boeing Company (81205) | |
| 35-8226-253 358226253 | 1560-01-150-2537 | Former, Aircraft | Aircraft Mission Design Series: B-52 Special Features: Stiffener; opposite -254; finish F-2.115 Material: Aluminum alloy 2024 | The Boeing Company (81205) | |
| 35-8226-254 358226254 | 1560-01-150-2538 | Former, Aircraft | Aircraft Mission Design Series: B-52 Special Features: Stiffener; opposite -253; finish F-2.115 Material: Aluminum alloy 2024 | The Boeing Company (81205) | |
| 35-8226-255 358226255 | 1560-01-150-2553 | Longeron | Aircraft Mission Design Series: B-52 Special Features: Opposite pn -256; inboard; finish F-10.10 Material: Titanium | The Boeing Company (81205) | |
| 35-8226-256 358226256 | 1560-01-150-2554 | Longeron | Aircraft Mission Design Series: B-52 Special Features: Opposite pn -255; finish F-10.10; inboard Material: Titanium | The Boeing Company (81205) | |
| 35-8226-257 358226257 | 1560-01-150-2501 | Support, Structural Component, Air | Aircraft Mission Design Series: B-52 Special Features: Used on -516, -522 and -545;FINISH F-2.115;T3 tempered Material: Aluminum alloy 2024 | The Boeing Company (81205) | |
| 35-8226-258 358226258 | 1560-01-150-2502 | Support, Structural Component, Air | Aircraft Mission Design Series: B-52 Special Features: Opposite -257;USED on -516, -522 and -545;FINISH F-2.115;TEMPER T3 Material: Aluminum alloy 2024 | The Boeing Company (81205) | |
| 35-8226-260 358226260 | 1560-01-150-5184 | Support, Structural Component, Air | Overall Length: 6.500 inches nominal Overall Width: 4.200 inches nominal Material Thickness: 0.050 inches nominal | The Boeing Company (81205) | |
| 35-8226-261 358226261 | 1560-01-150-5190 | Former, Aircraft | Aircraft Mission Design Series: B-52 Special Features: Channel; finish F-2.115; used on -516, -522 & -545; heat treated to T4; clad Material: Aluminum alloy 2024 | The Boeing Company (81205) | |
| 35-8226-4 3582264 | 1560-01-150-5170 | Plate, Structural, Aircraft | Aircraft Mission Design Series: B-52 Special Features: Used on- -516, -522 and -545;FINISH F-10.10; web Material: Titanium | The Boeing Company (81205) | |
| 35-8226-44 35822644 | 1560-00-862-6207 | Door, Access, Aircraft | End Item Identification: Aircraft model B52 | The Boeing Company (81205,82918) | |
| 35-8226-47 35822647 | 1560-00-773-3953 | Fairing, Aircraft | Aircraft Mission Design Series: B-52 | The Boeing Company (81205,82918) | |
| 35-8226-48 35822648 | 1560-00-773-3954 | Fairing, Aircraft | Aircraft Mission Design Series: B-52 | The Boeing Company (81205,82918) | |
| 35-8226-49 35822649 | 1560-01-150-2539 | Former, Aircraft | Aircraft Mission Design Series: B-52 Special Features: Angle frame;opposite -50; finish F-2.115; heat treated to T6 Material: Aluminum alloy 2024 | The Boeing Company (81205) |