Airframe Structural Components: 2327007-1, 23-3105, 2332584
MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
---|---|---|---|---|---|
2327007-1 23270071 | 1560-01-284-0213 | Fairing, Aircraft | Aircraft Mission Design Series: BQM-34A Special Features: C/O 1 shell; 1 laminate, cloth and resin as required III FSC Application Data: Used on rudder actuator fairing; nha 232T002 | Northrop Grumman Corporation (78022) | |
2327030 | 1560-00-396-7666 | Pulley Assembly, Fluid Shutoff Va | III End Item Identification: Aircraft model C47 | Boeing Company, The (18355,88277) | |
2327030-1 23270301 | 1560-00-396-7667 | Pulley Assembly, Fluid Shutoff Ba | III End Item Identification: Aircraft model C47 | Boeing Company, The (18355,88277) | |
2327031 | 1560-00-386-5674 | Bracket, Airframe | III End Item Identification: Aircraft model C-47A General Characteristics Item Description: Aluminum alloy, composition 3, QQ-A-601 | Boeing Company, The (18355,88277) | |
2327031-1 23270311 | 1560-00-396-7668 | Bracket, Airframe | III End Item Identification: Aircraft model C-47A General Characteristics Item Description: Aluminum alloy, composition 3, QQ-A-601 | Boeing Company, The (18355,88277) | |
23-2762 232762 | 1560-00-604-6310 | Guard, Switch, Main Fuel Tank | III End Item Identification: Aircraft model B52 | The Boeing Company (82918) | |
23-2777-1 2327771 | 1560-01-128-7236 | Free link, Control | III End Item Identification: Acft model B52G General Characteristics Item Description: Al alloy 2024-T4 per QQ-A-355, 0.300 in.thk, 1.000 in.W, 1.200 in.lg | The Boeing Company (81205) | |
23-2962 232962 | 1560-00-607-2173 | Shaft, Overspeed Bra | The Boeing Company (82918) | ||
23-2964 232964 | 1560-00-607-2174 | Plug, Coupling Shaft | General Characteristics Item Description: Plastic, L-P-410, 0.750 in. O/a dia | The Boeing Company (82918) | |
232S001-1 232S0011 | 1560-01-284-8804 | Rudder, Aircraft | Aircraft Mission Design Series: BQM-34A Material: Aluminum alloy 2024 | Northrop Grumman Corporation (78022) | |
232T003-11 232T00311 | 1560-01-310-2035 | Stabilizer, Horizontal | Aircraft Mission Design Series: BQM-34A Special Features: Empennage Side FOR Which Designed: Both sides | Northrop Grumman Corporation (78022) | |
232T003-13 232T00313 | 1560-01-310-2035 | Stabilizer, Horizontal | Aircraft Mission Design Series: BQM-34A Special Features: Empennage Side FOR Which Designed: Both sides | Northrop Grumman Corporation (78022) | |
232T003-9 232T0039 | 1560-01-310-2035 | Stabilizer, Horizontal | Aircraft Mission Design Series: BQM-34A Special Features: Empennage Side FOR Which Designed: Both sides | Northrop Grumman Corporation (78022) | |
232T004-5 232T0045 | 1560-01-285-5827 | Stabilizer, Vertical | Aircraft Mission Design Series: BQM-34A Special Features: Nha 232T002 and 232T102 Aircraft Location: Vertical stablizer | Northrop Grumman Corporation (78022) | |
232T007-1 232T0071 | 1560-01-478-0828 | Fairing, Aircraft | Aircraft Mission Design Series: BQM-34 Special Features: M/f: glass fabric type viii and polyester resin gr a cl 0 Material: Plastic polyester and glass fiber | Northrop Grumman Corporation (78022) | |
233 | 1560-00-335-9697 | Detector, Position l | Echols S T Inc. (13803) | ||
23-3061 233061 | 1560-00-723-2156 | Snap, Slide Thermal | General Characteristics Item Description: Nylon MIL-P-17091 type I | The Boeing Company (81205,82918) | |
23-3105 233105 | 1560-00-614-6959 | Plug, Outboard Screw | General Characteristics Item Description: Plastic, L-P-410, 0.87 in. O/a dia, 0.43 in. lg | The Boeing Company (82918) | |
233149 | 1560-00-037-1712 | Fitting, Structural Component, Air | Overall Length: 1.125 inches nominal | Lockheed Martin Corporation (98897) | |
2332584 | 1560-00-396-7933 | Bracket, Structural Component, Air | Aircraft Mission Design Series: C-118 Special Features: U/a:antidrag ring attach bracket matl: U-shape, 1.534IN id wd; 0.266IN thick; 0.620IN. min, 0.631IN. max dia hole in line, 1.250IN from base on ctr line, 2.125IN lg | Boeing Company, The (18355,88277) |