The pilot reported that, while on approach to landing, the airplane was hard to control, so he elected to troubleshoot the control issue in the air and initiated a go-around. The airplane lifted off the runway and began a climb, but rapidly rolled to the right, then left and impacted terrain. The pilot further described that the right rudder pedal was not functioning properly prior to the flight during taxi and that he had difficulty maintaining directional control during the approach. In addition, the pilot stated he lost directional control due to a rudder anomaly during a flight in the airplane that occurred several weeks prior.

A Federal Aviation Administrator inspector examined the airplane after the accident and confirmed that the airplane's wings had been substantially damaged during the accident. A postaccident examination of the rudder control system revealed no evidence of a pre accident mechanical failure or malfunction that would have precluded normal operation.