Accident Sequence
During final approach to runway 26, a crosswind shifted to a tailwind. The pilot reported that the aircraft was configured with full flaps and carburetor heat when the touchdown was made, despite the airspeed being 14 knots. After landing, the pilot determined that insufficient runway length remained and initiated a go-around by applying full throttle. However, the flaps and carburetor heat were not repositioned for the go-around attempt.
Engine Response
Following the application of full throttle, the engine did not respond for a period of 3 to 5 seconds. The pilot subsequently closed the throttle. The aircraft then skidded off the runway and came to rest in the overrun area.
Post-Accident Findings
Engine tests were conducted after the event. These tests confirmed that the engine exhibited an average hesitation of 4 seconds before reaching full throttle response. The source did not specify any other findings or causal factors.