Accident Overview
During the initial climb after takeoff, at approximately 200 feet above ground level, the aircraft's engine stopped producing power. The pilot performed a forced landing in an open field. Upon touchdown, the aircraft nosed over.
Post-Accident Examination
An FAA inspector examined the wreckage. The magneto switch was found in the BOTH position. The mixture control was positioned near idle cutoff, and the carburetor heat control was fully forward in the cold position. The mixture control was located adjacent to the carburetor heat control.
Technical Details
No further details regarding the aircraft type, registration, operator, or other specifics were reported in the source. The circumstances of the engine failure beyond the control positions were not provided.