What happened
Following a recent annual inspection, the pilot intended to return the aircraft to their home base. After obtaining clearance from air traffic control, the pilot initiated takeoff. During the takeoff roll, the aircraft reached a maximum groundspeed of 81 knots at a distance of approximately 2,075 feet along the 4,097-foot runway.
Once the aircraft became airborne, it began drifting toward the right. The pilot then contacted air traffic control to communicate an urgent requirement to return to the airport. Although the controller provided clearance to land, no subsequent communications were received from the aircraft. Flight track data indicated that the aircraft slowed down while turning back toward the left, with the speed continuing to drop throughout the remainder of the flight path. The final recorded groundspeed was 45 knots, which, when accounting for a 15-knot headwind, resulted in an airspeed of 60 knots.
Findings
Post-accident investigations of the engine and airframe showed no signs of mechanical failure or malfunction that would have prevented standard operation. Evidence from the engine suggested it was producing power at the moment of impact, though the specific power level was unknown.
Data regarding the aircraft's stall speed, wind conditions, and flight track confirmed that the aircraft encountered an aerodynamic stall prior to hitting the ground near the end of the runway. Because the impact occurred before the aircraft reached the airport perimeter, the pilot likely lacked the necessary altitude to perform a forced landing in the empty field located beyond the departure end of the runway. While the pilot's decision to return to the airport was documented, the specific reason for the urgent return could not be established due to the extent of the damage and the post-impact fire.