Event Description
The pilot of a tailwheel-equipped airplane reported that during the takeoff roll on Runway 28, winds were from 260 degrees at 10 knots. At about 60 miles per hour, he began to raise the tail for a wheel takeoff. At that point, the airplane started to veer to the left. The pilot attempted to correct the deviation by applying right rudder and right brake, but the airplane continued left, departed the runway, and ground looped on top of a hill.
Damage and Inspection
The accident resulted in substantial damage to the aft fuselage and empennage. Examination of the runway revealed skid marks; the right side skid mark was more pronounced than the left. Investigators found no evidence of any malfunction in the flight controls or brake system.
Pilot Report
The pilot reported the wind conditions and his actions during the takeoff. He stated that he was performing a wheel takeoff, a technique commonly used in tailwheel airplanes to raise the tail early for better visibility and control. The airplane began to veer left as he brought the tail up, and his corrective inputs were insufficient to prevent the excursion.
Findings
The investigation did not identify any mechanical anomalies that could have contributed to the loss of directional control. The more pronounced right skid mark suggests asymmetric braking or rudder application, but the exact sequence of events was not specified beyond the pilot's account.