Airframe Structural Components: 26-1911-802, 26-1921-506, 26-1925-1
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 26-1911-802 261911802 | 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 (81205) | |
| 26-1912-501 261912501 | 1560-01-151-6655 | Support, Structural Component, Air | III End Item Identification: Acft model B52 Special Features: Al clad 2024-0 per QQ-A-250/5, 0.071 in.thk, 1.800 in.W, 10.000 in.lg, left hand, used on tail fairing, station 245.30 | The Boeing Company (81205) | |
| 26-1912-502 261912502 | 1560-01-152-1602 | Support, Structural Component, Air | III End Item Identification: Acft model B52 Special Features: Al clad 2024-0 per QQ-A-250/5, 0.071 in.thk, 1.800 in.W, 10.000 in.lg, right hand, used on tail fairing station 245.30 | The Boeing Company (81205) | |
| 26-1912-503 261912503 | 1560-01-152-1603 | Support, Structural Component, Air | III End Item Identification: Acft model B52 Special Features: Al clad 2024-0 per QQ-A-250/5, 0.071 in.thk, 2.100 in.W, 10.500 in.lg, left hand, used on tail fairing station 245.30 | The Boeing Company (81205) | |
| 26-1912-504 261912504 | 1560-01-152-1604 | Support, Structural Component, Air | III End Item Identification: Acft model B52 Special Features: Al clad 2024-0 per qq-a 250/5, 0.071 in.thk, 2.100 in.W, 10.500 in.lg, right hand, used on tail fairing station 245.30 | The Boeing Company (81205) | |
| 26-1914-1 2619141 | 1560-01-152-9690 | Support, Structural Component, Air | III End Item Identification: Acft model B52 Special Features: Al clad 2024-0 per QQ-A-362, 0.063 in.thk, 1.600 in.W, 5.800 in.lg, used on tail fairing, l.H., inboard strut, at sta 280.65 | The Boeing Company (81205) | |
| 26-1918-501 261918501 | 1560-01-092-4476 | Support Angle | III End Item Identification: Acft B52 General Characteristics Item Description: Tail fairing installation, lefthand, inboard strut, sta. 262.65 | The Boeing Company (82918) | |
| 26-1918-502 261918502 | 1560-01-092-4474 | Support Angle | III End Item Identification: Acft B52 General Characteristics Item Description: Lefthand, inboard strut. sta. 271.65 | The Boeing Company (82918) | |
| 26-1918-801 261918801 | 1560-01-092-4476 | Support Angle | III End Item Identification: Acft B52 General Characteristics Item Description: Tail fairing installation, lefthand, inboard strut, sta. 262.65 | The Boeing Company (82918) | |
| 26-1918-802 261918802 | 1560-01-092-4474 | Support Angle | III End Item Identification: Acft B52 General Characteristics Item Description: Lefthand, inboard strut. sta. 271.65 | The Boeing Company (82918) | |
| 26-1919 261919 | 1560-01-092-4475 | Attach Angle | III End Item Identification: Acft B52 General Characteristics Item Description: Tail fairing installation, lefthand, inboard strut. sta. 236.25 | The Boeing Company (82918) | |
| 26-1921-505 261921505 | 1560-01-092-8293 | Support Angle | III End Item Identification: Acft B52 General Characteristics Item Description: Lefthand, inboard strut, sta. 271.65 | The Boeing Company (82918) | |
| 26-1921-506 261921506 | 1560-01-092-4473 | Support Angle | III End Item Identification: Acft B52 General Characteristics Item Description: Lefthand, inboard strut. sta. 271.65 | The Boeing Company (82918) | |
| 26-1921-801 261921801 | 1560-01-092-8293 | Support Angle | III End Item Identification: Acft B52 General Characteristics Item Description: Lefthand, inboard strut, sta. 271.65 | The Boeing Company (82918) | |
| 26-1921-802 261921802 | 1560-01-092-4473 | Support Angle | III End Item Identification: Acft B52 General Characteristics Item Description: Lefthand, inboard strut. sta. 271.65 | The Boeing Company (82918) | |
| 26-1922-1 2619221 | 1560-01-155-6878 | Plate, Structural, Aircraft | III End Item Identification: B-52 acft Special Features: Matl al alloy, QQ-A-287, 7075-0; matl size 0.063 by 2.100 by 3.600 in. lg; opposite to P/N 26-1922-2; used as stiffener angle frame station 85.27, nose cowl | The Boeing Company (82918) | |
| 26-1922-2 2619222 | 1560-01-155-6879 | Plate, Structural, Aircraft | III End Item Identification: B-52 acft Special Features: Matl al alloy, QQ-A-287, 7075-0; matl size 0.063 by 2.100 by 3.600 in. lg; opposite to P/N 26-1922-1; used as stiffener angle on frame station 85.27, nose cowl | The Boeing Company (82918) | |
| 26-1922-3 2619223 | 1560-01-155-6880 | Plate, Structural, Aircraft | III End Item Identification: B-52 acft Special Features: Matl al alloy, QQ-A-287, 7075-0; matl size 0.063 by 2.100 by 4.100 in. lg; opposite to P/N 26-1922-4; used as stiffener angle on frame station 85.27, nose cowl | The Boeing Company (82918) | |
| 26-1922-4 2619224 | 1560-01-155-6881 | Plate, Structural, Aircraft | III End Item Identification: B-52 acft Special Features: Matl al alloy, QQ-A-287, 7075-0; matl size 0.063 by 2.100 by 4.100 in. lg; opposite to P/N 26-1922-3; used as stiffener angle on frame station 85.27, nose cowl | The Boeing Company (82918) | |
| 26-1925-1 2619251 | 1560-01-152-1575 | Plate, Structural, Aircraft | Aircraft Mission Design Series: B-52 Material: Aluminum alloy 2024 Aircraft Location: No. 4 rib, inboard and outboard sstrut | The Boeing Company (81205) |