Incident Overview
During the final approach for a third touch-and-go landing in a STOL modified airplane, the pilot observed that the airspeed was 40 knots. The pilot applied partial power, and after recognizing that the airspeed did not increase, added slightly more power. The airplane then veered to the left and pitched up; the pilot corrected with right rudder and aileron.
Sequence of Events
The airplane continued in a nose-high attitude. The pilot reported attempting to correct the pitch by applying forward pressure on the control column, but was unable to lower the nose. Subsequently, the pilot heard the stall warning horn and applied full power, full right rudder, and aileron. Despite these inputs, the airplane continued to the left and collided with trees. The airplane came to rest upright with the right wing separated.
Pilot and Inspection Findings
The pilot stated that there was no engine failure or malfunction during the event. An FAA airworthiness inspector examined the flight controls and found no evidence of binding or failure for roll, pitch, or yaw control systems.