Airframe Structural Components: 24-1617-3, 24-1724-3, 24-1724-4
MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
---|---|---|---|---|---|
24-1617-3 2416173 | 1560-01-544-5889 | Panel, Structural, Aircraft | The Boeing Company (81205) | ||
24-1617-6 2416176 | 1560-01-552-2880 | Panel, Structural, Aircraft | Aircraft Mission Design Series: B-52 stratotanker Special Features: Matl al aly 2024 ;dim are stock matl Material: Aluminum alloy 2024 | The Boeing Company (81205) | |
24-1618-2 2416182 | 1560-00-614-6963 | Trailing Edge, Aircraft | Aircraft Mission Design Series: B-52 | The Boeing Company (82918) | |
24-1619-1 2416191 | 1560-00-610-7226 | Tip Assy, Frangible, | The Boeing Company (82918) | ||
24-1619-510 241619510 | 1560-00-610-7226 | Tip Assy, Frangible, | Aero Engineering & Manufacturing (17772) Ceco Inc. (32916) Duncan Models (6U345) Kaman Aerostructures- Wichita Inc. (96145) LAM TEX Composites Inc. (5N928) Sonfarrel Inc. (09036) The Boeing Company (81205,82918) Wilson Products Inc. (58060) | ||
24-1662 241662 | 1560-00-793-1497 | Power box Assembly, Main and Inte | General Characteristics Item Description: Plastic | The Boeing Company (81205,82918) | |
24-1662-512 241662512 | 1560-00-978-0203 | Box Assembly, External Power | III End Item Identification: B-52 aircraft General Characteristics Item Description: Bns main and interphone | The Boeing Company (82918) | |
24-1673-13 24167313 | 1560-01-099-9724 | Rail, Ladder | III End Item Identification: Acft B52 General Characteristics Item Description: Main entry door. 27.700 in. lg, 10.000 in. W, 0.050 in. thk. 2024-T3 clad sht QQ-A-362 T3 temp, heat treat T4 | The Boeing Company (81205,82918) | |
24-1673-14 24167314 | 1560-01-099-9725 | Rail, Ladder | III End Item Identification: Acft B52 General Characteristics Item Description: Main entry door. 27.700 in. lg, 10.000 in. W, 0.050 in. thk. 2024-T3 clad sht QQ-A-362 T3 temp, heat treat T4 | The Boeing Company (82918) | |
24170-10-500 2417010500 | 1560-01-470-6244 | Retainer Assy | Aeroquip Corp. (066F0) Eaton Corporation (00624) | ||
24-1705-2 2417052 | 1560-01-551-5638 | Bracket, Structural Component, Air | The Boeing Company (81205) | ||
24-1706-2 2417062 | 1560-01-551-5623 | Bracket, Structural Component, Air | The Boeing Company (81205) | ||
24-1707-2 2417072 | 1560-01-551-5611 | Bracket, Structural Component, Air | The Boeing Company (81205) | ||
24-1710-1 2417101 | 1560-01-551-5601 | Bracket, Structural Component, Air | The Boeing Company (81205) | ||
24-1712-2 2417122 | 1560-01-551-5629 | Bracket, Structural Component, Air | The Boeing Company (81205) | ||
24-1714-1 2417141 | 1560-01-551-5608 | Bracket, Structural Component, Air | The Boeing Company (81205) | ||
24-1716-1 2417161 | 1560-01-551-1337 | Support, Structural Component, Air | Aircraft Mission Design Series: B-52 Material: Aluminum alloy 2024 Aircraft Location: Hinge instl rudder | The Boeing Company (81205) | |
241718 | 1560-01-299-1996 | Cover, Access | Material: Aluminum alloy 6061 END Item Identification: Acommon armament/fire control Material Document AND Classification: Ams 4027, alloy 6061-T6 assn std single material response | The Marquardt Company (86845) | |
24-1724-3 2417243 | 1560-01-549-9193 | Support, Structural Component, Air | Boeing Company, The (4PF93) The Boeing Company (81205) | ||
24-1724-4 2417244 | 1560-01-552-1265 | Support, Structural Component, Air | Aircraft Mission Design Series: B-52 Special Features: Matl al aly 7075 T6 temp; U/O 57-6468 and on; dim are stock matl Material: Aluminum alloy 7075 | The Boeing Company (81205) |