ACTUATOR,RUDDER TRIM (P/N 8408) - As Removed
P/N: 8408
Category: Servos & Trim Systems
This product requires a custom quote. Please contact our sales team for pricing information or submit an RFQ (Request for Quote).
Available Inventory
| Condition | Stock |
|---|---|
| As Removed | 2 Available |
Product Description
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.
Frequently Asked Questions
What is the ACTUATOR,RUDDER TRIM (P/N 8408)?
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.
What conditions is the 8408 available in?
The 8408 is currently available in the following conditions: As Removed. Each condition reflects the part's maintenance history and certification status per FAA standards.
How do I get pricing for the 8408?
The 8408 requires a custom quote. Submit a Request for Quote (RFQ) through our website or call our sales team at (904) 998-9101 for immediate pricing assistance.
Do you offer expedited shipping for the 8408?
Yes, we offer same-day processing on in-stock items and provide 24/7 AOG (Aircraft on Ground) support for urgent needs. Standard, expedited, and overnight shipping options are available.
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