Accident Sequence
The pilot of a tailwheel-equipped airplane reported that during takeoff with a "heavy load" from a 2,600 ft private runway, the airplane lifted off normally. However, due to a shifting wind and high density altitude, the airplane aerodynamically stalled and impacted a field at the end of the runway. The airplane nosed over and was consumed by a postimpact fire.
Pilot Report
The pilot stated that there were no preaccident mechanical failures or malfunctions with the airplane that would have precluded normal operation. The pilot reported that the gross weight of the airplane at the time of the accident was 9,350 pounds, while the manufacturer's maximum gross takeoff weight was 9,400 pounds.
Weather Information
The automated weather observation station, located 6 miles north of the accident, reported that about 37 minutes before the accident, the wind was from 190° at 10 knots, visibility 10 statute miles, scattered clouds at 5,000 ft, temperature 90°F, dew point 70°F, and altimeter setting 30.04 inches of mercury. About 22 minutes after the accident, the wind was from 040° at 6 knots. The calculated density altitude was 2,189 ft. The airplane was departing on runway 12.
Aircraft Damage
The airplane sustained substantial damage to the fuselage. The postimpact fire consumed the aircraft.