Incident Description
A pilot conducted three low-altitude passes near his son's home. According to reports, the third pass was made at an altitude of approximately 40 to 50 feet above ground level (AGL). Following this pass, a witness observed the pilot initiate an abrupt pull-up, climbing at an angle of about 45 degrees.
After climbing an additional 40 to 50 feet, the aircraft entered an aerodynamic stall and subsequently impacted the ground. The sequence of events suggests that the maneuver exceeded the aircraft's performance capabilities at low altitude.
Witness Account
The witness reported that the engine cut out at the highest point above the ground during the climb. However, this observation was not corroborated by the subsequent examination.
Examination Findings
A post-accident examination of the wreckage found no evidence of a power loss or mechanical malfunction. The aircraft's fuel system was partially filled with automotive gasoline, which was noted but not identified as a cause of the accident. No other anomalies were detected.
No further details regarding the aircraft type, registration, or occupant status were provided in the source material.