P/N: 105-630000-83
Category: Flight Controls
This product requires a custom quote. Please contact our sales team for pricing information or submit an RFQ (Request for Quote).
| Condition | Stock |
|---|---|
| As Removed | 1 Available |
The 105-630000-83 is a rudder tab assembly for aircraft yaw trim control. This trailing-edge mounted component reduces rudder pedal forces during flight by providing aerodynamic trim assistance. The assembly interfaces with the rudder via standard AN/MS hardware and connects to the yaw trim system per aircraft drawings.
Installation requires rigging to aircraft specifications and verification against the Illustrated Parts Catalog. Used in the empennage for in-flight or ground-adjustable trim adjustment on general aviation aircraft.
Please note: Product descriptions are provided for informational purposes. Always refer to your aircraft's Illustrated Parts Catalog (IPC) to verify part compatibility and specifications.
The 105-630000-83 is a rudder tab assembly for aircraft yaw trim control. This trailing-edge mounted component reduces rudder pedal forces during flight by providing aerodynamic trim assistance.
The TAB ASSEM-RUDDER may be available as an OEM (Original Equipment Manufacturer) or PMA (Parts Manufacturer Approval) part depending on condition and source. Both carry FAA certification for airworthiness. Currently available in: As Removed. Contact us for sourcing details.
Installation hardware requirements vary by application. Check your aircraft's Structural Repair Manual (SRM) or Illustrated Parts Catalog (IPC) for the complete installation kit requirements for the TAB ASSEM-RUDDER. We stock related hardware and can help identify companion parts.
Yes, we ship airframe components worldwide. International orders typically arrive within 3-14 business days depending on destination. Export documentation and customs forms are included. Contact us for international shipping quotes on the 105-630000-83.