NSN 1680-01-510-3510
Yaw Ratio Adjuster Assembly
Datasheet
-
Product description
Yaw Ratio Adjuster Assembly NSN 1680-01-510-3510.
-
MPN or Model
123CM11232-511
-
Schedule B
8803.30.0060 (Other parts of airplanes or helicopters for use in military aircraft (excludes propellers, rotors, undercarriages, and parts thereof))
More from these suppliers
- 1680-00-004-2857 MPN A51M20030-1Flap Stop Arm Assembly
- 5935-00-009-8021 MPN GC800FD36-47SWElectrical Plug Connector
- 1560-00-037-1493 MPN 89458-22Stack Weld Assembly
- 5940-00-114-1305 MPN GT805P8-4Lug Terminal
- 1560-00-151-4166 MPN 121W10003-623Wing Panel Assembly
- 5305-00-157-5572 MPN GB511M3-7Socket Head Cap Screw
- 1560-00-169-7886 MPN 123BM10556-3Escape Hatch Fuselage Fitting
- 5306-00-182-9249 MPN 128PM10219-11Shoulder Bolt
Yaw Ratio Adjuster Assembly
Assemblies, cables, and pedals, engaged by the pilot or co-pilot to adjust controls which govern the yaw of the aircraft.
Pricing and Availability
Get a quote for 1680-01-510-3510 yaw ratio adjuster assemblyManufacturer Part Numbers and Alternates
| MPN manufacturer part number | Registrant or Supplier |
|---|---|
| 123CM11232-511 | Northrop Grumman Systems Corporation |
| 123CM11232-511 | Northrop Grumman Systems Corporation |
| 123CM11232-511 | Northrop Grumman Systems Corporation |
Stock Check
Availability of this NSN has not been updated recently. Submit
the pricing and availbility form above to receive an up to date quote.
