Primary finding
Probable cause
A loss of directional control due to a weld joint failure of the left rudder pedal.
Investigator assessment
Analysis narrative
The pilot reported that during the landing roll on the asphalt runway, the left rudder pedal separated and he was unable to maintain directional control. Subsequently, the airplane ground-looped and exited the right side of the runway. The fuselage and left wing were structurally damaged. The left rudder pedal was separated at its weld point. No further anomalies were noted with the flight control systems.
Source record
Factual narrative
The pilot reported that during the landing roll on the asphalt runway, the left rudder pedal separated and he was unable to maintain directional control. Subsequently, the airplane ground looped and exited the right side of the runway. The fuselage and left wing were structurally damaged. The left rudder pedal was separated at its weld point. No further anomalies were noted with the flight control systems.