P/N: 418-00884-001
Category: Valves & Actuators
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.
Hydraulic component compatibility depends on the aircraft system design. Common aviation hydraulic fluids include MIL-PRF-5606 (mineral-based), MIL-PRF-83282 (synthetic), and Skydrol (phosphate ester). Verify the YAW TRIM ACTUATOR against your aircraft maintenance manual for fluid compatibility.
Overhauled and repaired hydraulic components are pressure-tested per manufacturer specifications and include 8130-3 documentation. The YAW TRIM ACTUATOR is available in: Serviceable. Contact us for test documentation on your selected condition.
In-stock hydraulic components ship same business day before 3 PM EST. We provide 24/7 AOG support at (904) 998-9101 for urgent hydraulic system needs. RFQ submissions are typically quoted within 24 hours.