Airframe Structural Components: 24-1565-7, 24-1606-1005, 24-1616-3
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 24-1565-7 2415657 | 1560-01-475-0267 | Beam, Aircraft | Air Force United States Department (98748) | ||
| 24-1565-8 2415658 | 1560-01-544-3431 | Support, Structural Component, Air | Aircraft Mission Design Series: B-52G Special Features: Dim. are stock material Material: Aluminum alloy 7075 | The Boeing Company (81205) | |
| 24-1602-1001 2416021001 | 1560-01-549-9188 | Beam, Aircraft | The Boeing Company (81205) | ||
| 24-1602-1003 2416021003 | 1560-01-550-2481 | Beam, Aircraft | Boeing Company, The (4PF93) The Boeing Company (81205) | ||
| 24-1602-2 2416022 | 1560-01-518-9025 | Support, Structural Component, Air | Aircraft Mission Design Series: B-52 Material: Aluminum alloy 2024 Aircraft Location: Pan installation-wheel well door | The Boeing Company (81205) | |
| 24-1602-3 2416023 | 1560-01-542-3602 | Support, Structural Component, Air | Aircraft Mission Design Series: B-52 Material: Aluminum alloy 2024 Aircraft Location: Wheel well door | The Boeing Company (81205) | |
| 24-1603-4 2416034 | 1560-01-527-9922 | Support, Structural Component, Air | Aircraft Mission Design Series: B-52 III Part Name Assigned BY Controlling Agency: Chord lwr | The Boeing Company (82918) | |
| 24-1603-5 2416035 | 1560-01-527-9934 | Support, Structural Component, Air | Aircraft Mission Design Series: B-52 III Part Name Assigned BY Controlling Agency: Chord upper | The Boeing Company (82918) | |
| 24-1604-2 2416042 | 1560-01-549-7855 | Web, Structural Component, Aircraf | Aircraft Mission Design Series: B-52 Special Features: Dim are stock material; m/f: clad 7075 sht, 0 temp, ht T6, fin: F-2.115 Material: Aluminum alloy 7075 | The Boeing Company (81205) | |
| 24-1604-3 2416043 | 1560-01-549-8216 | Support, Structural Component, Air | The Boeing Company (81205) | ||
| 24-1604-4 2416044 | 1560-01-550-1358 | Support, Structural Component, Air | III End Item Identification: Rib installation-wheel well door Aircraft Mission Design Series: B-52G Special Features: Dim are stock material; heat: T6; finish: F-2.115; U/O pn 24-1604, rib installation | The Boeing Company (81205) | |
| 24-1605-1002 2416051002 | 1560-01-544-5199 | Plate, Structural, Aircraft | The Boeing Company (81205) | ||
| 24-1605-4 2416054 | 1560-01-549-6131 | Web, Structural Component, Aircraf | The Boeing Company (81205) | ||
| 24-1606-1003 2416061003 | 1560-01-544-5194 | Plate, Structural, Aircraft | The Boeing Company (81205) | ||
| 24-1606-1005 2416061005 | 1560-01-549-3250 | Plate, Structural, Aircraft | The Boeing Company (81205) | ||
| 24-1607-4 2416074 | 1560-01-552-1256 | Support, Structural Component, Air | Aircraft Mission Design Series: B-52 Special Features: Matl al aly 7075 T6 sht;u/O 57-6468 and on; dim are stock matl Material: Aluminum alloy 7075 | The Boeing Company (81205) | |
| 24-1611-1 2416111 | 1560-00-610-7302 | Tip, Aircraft | Aircraft Mission Design Series: B-52 Special Features: C/O 2 splice plate, 1 fwd skin, 1 nose skin, 1 fin tfp assy | The Boeing Company (82918) | |
| 24-1614-2 2416142 | 1560-01-549-6331 | Support, Structural Component, Air | The Boeing Company (81205) | ||
| 24-1614-3 2416143 | 1560-01-549-3522 | Support, Structural Component, Air | Aircraft Mission Design Series: B-52 stratofortress Special Features: Matl al aly 7075 QQ-A-287 temp 0, dim are stock matl Material: Aluminum alloy 7075 | The Boeing Company (81205) | |
| 24-1616-3 2416163 | 1560-01-550-2211 | Support, Structural Component, Air | The Boeing Company (81205) |