Airframe Structural Components: 26-1689-3, 26-1907-1, 26-1911-801
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 26-1689-3 2616893 | 1560-01-152-9657 | Plate, Structural, Aircraft | Aircraft Mission Design Series: B-52 Special Features: Do not use cadmium plated tools on this item; optional spec bms 7-7E Material: Titanium | The Boeing Company (81205) | |
| 26-1689-4 2616894 | 1560-01-152-9658 | Plate, Structural, Aircraft | Aircraft Mission Design Series: B-52 Special Features: Do not use cadmium plated tools on this item; optional spec bms 7-7E Material: Titanium | The Boeing Company (81205) | |
| 2619 | 1560-00-589-4298 | Collar, Pylon Hinge Lock | General Characteristics Item Description: Aluminum alloy QQ-A-225/6 | Sams Machine and Tool Shop Inc. (16418) | |
| 26-1900-501 261900501 | 1560-01-152-8479 | Support, Structural Component, Air | III End Item Identification: Acft model B52 Special Features: Al clad 2024-0 per QQ-A-250/5, 0.063 in.thk, 1.400 in.W, 6.600 in.lg, left hand, used on outboard strut tail fairing | The Boeing Company (81205) | |
| 26-1904-1 2619041 | 1560-01-158-7374 | Plate, Structural, Aircraft | III End Item Identification: Acft model B52 Special Features: Comm pure titanium, 0.020 in.thk, 5.300 in.W, 8.800 in.lg, used on firewall nose cowl, left hand | The Boeing Company (82918) | |
| 26-1904-2 2619042 | 1560-01-158-7375 | Plate, Structural, Aircraft | III End Item Identification: Acft model B52 Special Features: Comm pure titanium per ams 4901, annealed, 0.020 in.thk, 5.300 in.W, 8.800 in.lg, used on firewall nose cowl, rh | The Boeing Company (82918) | |
| 26-1906-801 261906801 | 1560-01-158-7377 | Plate, Structural, Aircraft | III End Item Identification: Acft model B52 Special Features: Steel cres 302 annealed per MIL-S-5059, 0.064 in.thk, 6.100 in.W, 9.000 in.lg, used on nose cowl frame station 85.25 | The Boeing Company (82918) | |
| 26-1906-804 261906804 | 1560-01-158-7379 | Plate, Structural, Aircraft | III End Item Identification: Acft model B52 Special Features: Cres steel 302 annealed per MIL-S-5059, 0.072 in.thk, 0.900 in.W, 3.000 in.lg, used on nose cowl frame station 85.25 | The Boeing Company (82918) | |
| 26-1907 261907 | 1560-01-159-7812 | Bracket, Structural Component, Air | Aircraft Mission Design Series: B-52 Special Features: C/O bracket, rivet Material: Aluminum alloy 2024 | The Boeing Company (81205) | |
| 26-1907-1 2619071 | 1560-01-160-3119 | Support, Structural Component, Air | Aircraft Mission Design Series: B-52 | The Boeing Company (81205) | |
| 26-1909-1 2619091 | 1560-01-152-9659 | Plate, Structural, Aircraft | III End Item Identification: Acft model B52 Special Features: Do not use cadmium plated tools on this item, commercially pure titanium per 4900 annealed, 0.025 in.thk, 1.800 in.W, 10.800 in.lg, used on tail fairing at station 236.25, left hand | The Boeing Company (81205) | |
| 26-1909-2 2619092 | 1560-01-152-9660 | Plate, Structural, Aircraft | III End Item Identification: Acft model B52 Special Features: Do not use cadmium plated tools on this item, commercially pure titanium per ams 4900 annealed, 0.025 in.thk, 1.800 in.W, 10.800 in.lg, used on tail fairing at sta 236.25, right hand | The Boeing Company (81205) | |
| 26-1909-3 2619093 | 1560-01-152-9661 | Plate, Structural, Aircraft | III End Item Identification: Acft model B52 Special Features: Do not use cadmium plated tools on this item, cp titanium per ams 4900 annealed, 0.025 in.thk, 2.000 in.W, 15.200 in.lg, left hand, used on tail fairing at station 236.25 | The Boeing Company (81205) | |
| 26-1909-4 2619094 | 1560-01-152-9662 | Plate, Structural, Aircraft | III End Item Identification: Acft model B52 Special Features: Do not use cadmium plated tools on this item, cp titanium per ams 4900 annealed, 0.025 in.thk, 2.000 in.W, 15.200 in.lg, right hand, used on tail fairing at station 236.25 | The Boeing Company (81205) | |
| 26-1909-5 2619095 | 1560-01-152-9663 | Plate, Structural, Aircraft | III End Item Identification: Acft model B52 Special Features: Do not use cadmium plated tools on this item, cp titanium per ams 4900 annealed, 0.028 in.thk, 1.200 in.W, 3.000 in.lg, used on tail fairing, at station 236.25, left hand | The Boeing Company (81205) | |
| 26-1909-6 2619096 | 1560-01-152-9664 | Plate, Structural, Aircraft | III End Item Identification: Acft model B52 Special Features: Do not use cadmium plated tools on this item, cp titanium per ams 4900 annealed, 0.028 in.thk, 1.200 in.W, 3.000 in.lg, right hand, used on tail fairing at station 236.25 | The Boeing Company (81205) | |
| 26-1910-801 261910801 | 1560-01-151-6632 | Plate, Structural, Aircraft | III End Item Identification: Acft model B52 Special Features: Do not use cadmium plated tools on this item, 0.025 in.thk, 1.500 in.W, 10.100 in.lg, used on tail fairing, left hand, inboard strut | The Boeing Company (81205) | |
| 26-1911-503 261911503 | 1560-01-092-4477 | Frame, Tail Fairing | III End Item Identification: Acft B52 General Characteristics Item Description: Lefthand, inboard strut, sta. 262.65 | The Boeing Company (82918) | |
| 26-1911-504 261911504 | 1560-01-091-8765 | Frame, Tail Fairing | III End Item Identification: Acft B52 General Characteristics Item Description: Sta. 262.65, lefthand inboard strut. 15.500 in. lg, 3.000 in. W, 0.063 in. th. clad 2024-0 QQ-A-362 0 temper, heat treat T4, finish F-2.10 | The Boeing Company (82918) | |
| 26-1911-801 261911801 | 1560-01-092-4477 | Frame, Tail Fairing | III End Item Identification: Acft B52 General Characteristics Item Description: Lefthand, inboard strut, sta. 262.65 | The Boeing Company (82918) |