P/N: 418-00884-001
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).
| Condition | Stock |
|---|---|
| Serviceable | 1 Available |
The 418-00884-001 is an electromechanical yaw trim actuator that biases rudder trim to reduce pilot pedal forces during flight. This actuator integrates with the rudder trim system and autopilot/yaw damper interface, working in conjunction with trim tabs or feel units to enhance directional control. Installation and rigging must follow the aircraft maintenance manual or FAA AC 43.13-1B guidance.
Commonly found in general aviation and business aircraft equipped with active yaw control systems.
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 418-00884-001 is an electromechanical yaw trim actuator that biases rudder trim to reduce pilot pedal forces during flight. This actuator integrates with the rudder trim system and autopilot/yaw damper interface, working in conjunction with trim tabs or feel units to enhance directional control.
The 418-00884-001 is currently available in the following conditions: Serviceable. Each condition reflects the part's maintenance history and certification status per FAA standards.
The 418-00884-001 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.
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.