P/N: 8408
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 | 2 Available |
The 8408 is an electromechanical rudder trim actuator for aircraft vertical tail control systems. It positions the rudder trim tab to reduce yaw forces and decrease pilot pedal input requirements during flight. Mounted in the tail linkage, the actuator converts electrical or manual trim commands into rotary or jackscrew motion that drives the tab to the commanded deflection.
Installation follows the Aircraft Maintenance Manual with verification against the Illustrated Parts Catalog for airframe compatibility. Proper rigging ensures trim tab movement remains synchronized with control inputs.
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 8408 is an electromechanical rudder trim actuator for aircraft vertical tail control systems. It positions the rudder trim tab to reduce yaw forces and decrease pilot pedal input requirements during flight.
The ACTUATOR,RUDDER TRIM 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 ACTUATOR,RUDDER TRIM. 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 8408.