Introduction
A pilot reported experiencing an engine power loss during the initial climb after takeoff at approximately 200 feet above ground level. In response, the pilot attempted a forced landing by applying full left rudder and forward stick to maintain airspeed. The pilot stated that he had no further recollection of the accident sequence.
Witness Observations
A witness reported observing the airplane during its climb out. The airspeed was described as slow. The airplane was then observed to make a steep left turn, estimated at 45 degrees or more, while between 200 and 250 feet in altitude. Following the turn, the nose of the airplane pitched downward, and the airplane subsequently collided with terrain.
Pilot Report
The pilot's account indicated that the engine lost power at a critical phase of flight, prompting an immediate forced landing maneuver. The pilot's inputs of full left rudder and forward stick were aimed at maintaining airspeed during the descent. The pilot did not recall any events after initiating these control inputs.
Post-Accident Examination
An examination of the flight control system and engine assembly was conducted following the accident. The examination revealed no evidence of a pre-crash mechanical failure or malfunction in either system.