P/N: 4012373-812
Category: Autopilot Systems
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 4012373-812 is a linear electromechanical actuator for aircraft yaw damper systems. This unit converts electrical control commands into precise rudder movements to counteract Dutch roll and maintain lateral stability. Installed in the stability augmentation system's rudder servo loop, it interfaces directly with flight-control electronics.
The actuator provides synchronized yaw damping during cruise and approach phases. Installation and rigging must follow the applicable Aircraft Maintenance Manual and approved procedures. Cross-referenced to 600-92601-5 for Bombardier Challenger 601 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 4012373-812 is a linear electromechanical actuator for aircraft yaw damper systems. This unit converts electrical control commands into precise rudder movements to counteract Dutch roll and maintain lateral stability.
Avionics compatibility depends on your aircraft model and existing installation. The ACTUATOR, LINEAR YAW DAMPER is available in: As Removed. We recommend checking your aircraft's wiring diagrams and STC documentation, or contact our avionics team for compatibility assistance.
Availability of an FAA 8130-3 tag depends on the part condition. Overhauled and repaired units typically include 8130-3 documentation. As-removed units may include a removal tag with trace history. Contact us for specific documentation on the condition you need.
We can arrange bench testing through our network of FAA-certified repair stations. Call (904) 998-9101 for testing availability and turnaround times, or submit an RFQ with your specific requirements.