SWITCH YAW (P/N 97564-7502) - As Removed

The 97564-7502 is an electromechanical yaw switch for aircraft flight and autopilot panels. This metal-contact panel-mounted switch commands the yaw damper or rudder trim circuit during flight operations. Installation requires routing wiring per the aircraft maintenance manual and AC 43.13-1B guidance, with torque specifications matched to panel hardware.

Verify proper operation using the aircraft wiring diagram before returning to service. Commonly found in general aviation and business aircraft cockpits where yaw control engagement is pilot-initiated.

What is the SWITCH YAW (P/N 97564-7502)?

The 97564-7502 is an electromechanical yaw switch for aircraft flight and autopilot panels. This metal-contact panel-mounted switch commands the yaw damper or rudder trim circuit during flight operations.

Is the 97564-7502 compatible with my aircraft's avionics suite?

Avionics compatibility depends on your aircraft model and existing installation. The SWITCH YAW is available in: As Removed. We recommend checking your aircraft's wiring diagrams and STC documentation, or contact our avionics team for compatibility assistance.

Does the 97564-7502 come with an 8130-3 airworthiness tag?

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.

Do you offer bench testing for the 97564-7502?

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.