Accident Overview
A single-pilot operation in a complex aircraft ended in a fatal accident during a second takeoff attempt. The first takeoff was aborted due to a perceived engine problem. Six minutes later, the aircraft began its second takeoff, climbed to about 50 feet, then drifted to the right, rolled right, and impacted the infield. The pilot, sole occupant, was killed.
Sequence of Events
After aborting the first takeoff for a perceived engine issue, the pilot initiated a second takeoff. The aircraft reached an altitude of approximately 50 feet before deviating to the right. It subsequently rolled right and struck the ground. The wreckage examination revealed that the prop condition levers were in the taxi position. The power levers were set with the left engine near flight idle and the right engine at takeoff power.
Weather Conditions
At the time of the accident, strong, gusty winds prevailed at the airport. Wind speeds varied from 15 to 30 knots, with direction shifting between southwest and northwest. These conditions exceeded the aircraft's demonstrated crosswind limitation. The accident occurred during dark night conditions.
Post-Crash Investigation
A thorough investigation of both engines and propellers found no operational defects; both were producing power at impact. There was no evidence that the pilot was using the seat belt or shoulder harness. The pilot's failure to use these restraints is noted in the official findings.
Probable Cause
Official findings categorized the accident into two occurrences: loss of control in flight and in-flight collision with terrain. Contributing factors included weather conditions (gusts and crosswind), the pilot's failure to maintain compensation for wind conditions, excessive workload (task overload), dark night, improper directional control, improper procedures/directives, and failure to use seat belt and shoulder harness.