Accident Sequence
The accident occurred during an attempted go-around from runway 21. On final approach, the pilot had configured the airplane with full flaps and full nose-up trim. The initial touchdown resulted in a bounce, prompting the pilot to initiate a go-around. Full power was added, but the flaps were not retracted and the trim setting was not changed.
At approximately 10 feet above ground level, the left wing stalled. The airplane subsequently collided with the ground and came to rest inverted, facing a 030-degree heading.
Pilot's Operating Handbook Guidance
The Pilot's Operating Handbook (POH) for the airplane specifies that during a go-around, the pilot should add full power, retract the flaps to 20 degrees, and achieve an airspeed of 55 knots. In this instance, the flaps remained at the full setting and the trim remained at full nose-up, which differed from the recommended procedure.
Post-Accident Observations
The airplane was found inverted on the ground. No further details about the aircraft condition or occupant status were provided in the source.