Accident Narrative
The right engine lost power during the initial climb after lift-off. A witness reported hearing a noise and observing flames emanating from the right engine cowling as the airplane climbed. After climbing approximately 200 feet, the airplane entered a turn, descended through a small grove of trees, crashed in a pasture, and burned. The pilot, the sole occupant, was killed.
Weight and Balance
At the time of takeoff, the airplane's gross weight was approximately 11,050 lbs, and its center of gravity (CG) was behind the aft limit. The maximum certified weight limit for the airplane was 9,700 lbs. The pilot was aware of the gross weight problem before departure.
Engine Examination
An examination revealed that the left engine propeller was in the feathered position at impact, while the right propeller was not feathered. Inspection of the right engine disclosed that the number 3 cylinder intake valve had failed due to fatigue.
Probable Cause
The official probable cause of the accident was the pilot's improper emergency procedure by shutting down the wrong engine, which resulted in a forced landing. Factors related to the accident were the failure of the number three intake valve in the right engine due to fatigue, and the presence of trees in the emergency landing area.