What was found
RIGHT RUDDER PEDAL DEFLECTED FORWARD APPROXIMATELY 2 INCHES THEN BACK TO NEUTRAL. *S/D* REMOVED AND REPLACED THE FOLLOWING: YAW DAMPER COUPLER, MAIN RUDDER PCU & STANDBY RUDDER PCU. MEGGERED WIRES FROM YAW DAMPER COUPLER TO P5-3 PANEL, AND TO RUDDER PCU. PERFORMED GROUND FUNCTIONAL TEST OF AUTOPILOT SYSTEM. CHECKED YAW DAMPER CONNECTOR FOR CORROSION AND FLUID CONTAMINATION AND ALL PIN TENSIONS. REMOVED FLIGHT RECORDER AND SENT TO NTSB.