Airframe Structural Components: 134B10302-1, 134BM30021-1, 134BP10034-421
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 134B10302-1 134B103021 | 1560-01-237-8063 | Handle Assembly, Upp | Northrop Grumman Systems Corporation (26512) | ||
| 134B10316-27 134B1031627 | 1560-00-860-7409 | SEAL | Northrop Grumman Systems Corporation (26512) | ||
| 134B10381-11 134B1038111 | 1560-00-967-7682 | Plate, Support, Lever | General Characteristics Item Description: 1.375 in. od, 0.499 in. min 0.506 in. max aperature dia, 0.095 in. thk, 3 bolt holes 0.127 in. min 0.133 in. max dia unequally spaced on a 1.000 in. bolt circle dia | Northrop Grumman Systems Corporation (26512) | |
| 134B10400-29 134B1040029 | 1560-00-860-7407 | SEAL | Northrop Grumman Systems Corporation (26512) | ||
| 134B10551-5 134B105515 | 1560-00-963-5789 | Skin, Aircraft | III End Item Identification: Aircraft, model OV-1B Aircraft Mission Design Series: OV-1B Material: Aluminum alloy | Northrop Grumman Systems Corporation (26512,61174) | |
| 134B20180-406 134B20180406 | 1560-00-864-3427 | Door Assembly, Right | Northrop Grumman Systems Corporation (26512) | ||
| 134B75047-3 134B750473 | 1560-00-774-8640 | Door, Access, Aircraft | Northrop Grumman Systems Corporation (26512) | ||
| 134B80146-1 134B801461 | 1560-00-404-6021 | Fairing Assembly, Fuselage | General Characteristics Item Description: Consist of a fairing assy, a bond assy, seals and assorted hardware | Northrop Grumman Systems Corporation (26512) | |
| 134BM10093-10 134BM1009310 | 1560-01-225-0427 | Fitting | Northrop Grumman Systems Corporation (26512) | ||
| 134BM10126-81 134BM1012681 | 1560-00-235-1985 | Fitting Assy, Landing | General Characteristics Item Description: Aluminum alloy | Northrop Grumman Systems Corporation (26512) | |
| 134BM10163-2 134BM101632 | 1560-00-133-4139 | Sector, Latch, Door R | General Characteristics Item Description: Steel MIL-S-5000 comp 4340; arc shape 9.000 in. od, subtends an arc of 56.0 degrees; 10 holes; arc has internal teeth | Northrop Grumman Systems Corporation (26512) | |
| 134BM10220-6 134BM102206 | 1560-00-152-3724 | Fitting Assembly, Fuselage | General Characteristics Item Description: Aluminum alloy, QQ-A-225/9, 2 holes, 0.126 in. min, 0.133 in. max dia, spaced 0.500 in. C to C, with press fit bearing | Northrop Grumman Systems Corporation (26512) | |
| 134BM30021-1 134BM300211 | 1560-00-682-2341 | Cover Plate, Antenna | Northrop Grumman Systems Corporation (26512) | ||
| 134BM80000-3 134BM800003 | 1560-00-404-6019 | Fitting Assembly, Fuselage | General Characteristics Item Description: Consists of 1 al alloy, QQ-A-367, 7075-T3 fitting, 1 receptacle, 5 bushings, 2 rivets | Northrop Grumman Systems Corporation (26512) | |
| 134BM80062-1 134BM800621 | 1560-00-181-4831 | Fitting Assembly, Fuselage | General Characteristics Item Description: Fitting, aluminum alloy, QQ-A-225/9; bushings, nutplate, nut, washers and rivets | Northrop Grumman Systems Corporation (26512) | |
| 134BP10000-602 134BP10000602 | 1560-00-130-6023 | Windshield Panel, Aircraft | III End Item Identification: Aircraft, OV-1B Aircraft Mission Design Series: OV-1B | Northrop Grumman Systems Corporation (26512) | |
| 134BP10002-3 134BP100023 | 1560-00-770-6013 | Glass Assembly, Wind | Northrop Grumman Systems Corporation (26512) | ||
| 134BP10002-4 134BP100024 | 1560-01-306-8293 | Window Panel, Aircraft | III End Item Identification: OV-1 series aircraft Aircraft Mission Design Series: OV-1 Material: Glass | Northrop Grumman Systems Corporation (26512) | |
| 134BP10002-6 134BP100026 | 1560-01-306-8293 | Window Panel, Aircraft | III End Item Identification: OV-1 series aircraft Aircraft Mission Design Series: OV-1 Material: Glass | Northrop Grumman Systems Corporation (26512) | |
| 134BP10034-421 134BP10034421 | 1560-00-866-6023 | Panel Assembly, Came | Northrop Grumman Systems Corporation (26512) |