Accident Sequence
The pilot aborted the first takeoff after perceiving an engine problem. Six minutes later, a second takeoff was initiated. During the climb, the aircraft reached an altitude of 50 feet before drifting to the right, rolling right, and impacting the ground in the infield.
Wind Conditions
At the time of the accident, the airport experienced strong, gusty winds with speeds varying from 15 to 30 knots. Wind direction varied between southwest and northwest. These winds exceeded the aircraft's demonstrated crosswind limitation.
Power and Propeller Settings
Post-crash examination revealed that both engines and propellers had no operational defects and were producing power at impact. The propeller condition levers were found in the taxi position. The power levers were set asymmetrically: the left engine was near flight idle, while the right engine was at the takeoff position.
Pilot Restraint Use
No evidence was found that the pilot was using the seat belt or shoulder harness during the flight.
Operational Context
The aircraft was a complex type operated by a single pilot.