Edited (because a human being tragically died what I consider to be an unnecessary death and i have no desire to call out anyone or embbarras.)
From the final report: airplane collided with terrain... pilot was fatally injured... airplane was destroyed by impact forces and post impact fire... operating it under the provisions of Title 14 Code of Federal Regulations Part 91. Visual flight rules conditions existed near the accident site at the time of the accident...
The pilot was conducting the first flight... since purchasing it... the pilot aborted the takeoff for unknown reasons. The pilot taxied the airplane back to the end of the runway and then took off again.
Witnesses described the airplane pitching up while banking during the takeoff. One witness stated that he could see the top of the wings, as if the airplane was straight up and down, before it turned to the southeast. Several witnesses reported hearing "good" engine sounds. Other witnesses, who saw the airplane just before the impact, reported that it was in a steep nose-down, left descending spiral. Two witnesses reported seeing the airplane spiral one and a half to three times before it descended below the trees, followed by a plume of black smoke.
data indicated that the airplane departed... The climb then continued to 1,050 agl, at which point the airplane entered a descent and was then lost on radar.
The pilot held a private pilot certificate with a single-engine land rating, which was issued (28 years, 11 months, and 20 days before the crash)... According to (the pilot's logbook his) total time was 312.1 hours, of which the pilot recorded 4.8 hours with a flight instructor (obtaining a tail wheel endorsement between 66 and 45 days before the crash)...at which time the pilot completed a flight review...
The pilot's logbook contained entries from (his first lesson), between (18 and 12 years before the crash) the pilot recorded 10.2 hours of flight experience. There were no entries between (then and the 4.8 hours with an instructor noted above). The pilot did not log any flight time in a (type of aircraft he crashed) airplane... the logbook did contain a tailwheel endorsement. The pilot's most recent Federal Aviation Administration (FAA) medical certificate was issued on (6 months and 3 days before the crash).
The flight instructor, who had flown with the pilot (and endorsed his log book)... stated that they had discussed whether to have an experienced pilot conduct the first flight in the pilot's airplane after purchase. The flight instructor stated that the pilot replied that he was going to conduct the first flight...
On (5 months, 3 days before the accident, and 2 months 3 days before starting with the CFI to obtain his tailwheel endorsement), the pilot ground looped the airplane, which resulted in landing gear damage, while taxiing...
The wreckage path from the initial impact point to the main wreckage was on a magnetic heading of 30°... The right wing was found wrapped around a pole about 210 ft from the initial impact. Further along the wreckage path were the fuel tanks, the engine, portions of t he cockpit/fuselage, the empennage, and the propeller hub. The wreckage from the right wing to the end of the wreckage path was mostly destroyed by fire. Pieces of the splintered composite propeller blade, plexiglass, and wood were scattered along the entire wreckage path.
The fuselage and cockpit area were destroyed by fire. The main landing gear assembly was separated from the fuselage. The bottom of the right wing was destroyed from the wing root to the aileron attachment point. The fabric on the top of the wing was scorched and melted in the wing root area. The inboard section of the flap was separated from the wing, and the outboard section remained attached. The aileron remained intact and attached to the wing. The control cables were pulled out from the wing and remained attached to the cockpit control column.
The left wing was destroyed by fire. The left aileron was separated from the wing. The aileron control cable was found near the burned wing, and it remained attached to the cockpit control column.
The fuel tanks were separated from the wings and burned. The fuel tank caps were not in place; however, melted material was visible around the base of the filler neck. Material was visible inside the left fuel tank, and it appeared to be portions of the melted fuel cap. The position of the cockpit fuel selector could not be determined due to impact and fire damage.
The rudder cables remained attached to the bottom of the rudder and tailwheel. Cable continuity from the cockpit area to the forward and aft seat right rudder pedals was established. The forward and aft seat left rudder pedals were not found. However, the left cable was intact, and it contained the turnbuckles and rudder pedal attachment hardware.
The engine was burned, and its right side was impact-damaged. The right valve cover was impact-damaged and was separated from the engine. Two of the valve lifters on the right side were separated from the engine. The left valve cover was in place, and the valves and springs were intact. The oil pan was removed from the engine, and the inside of the engine was intact and contained oil. The propeller was separated from the engine. The ring gear was smashed rearward against the engine case.
One of the propeller's composite blades remained mostly intact and attached to the hub. The butt end of the other two blades remained attached to the hub. The propeller spinner was separated from the hub. The spinner was flattened and exhibited a small amount of torsional bending.
conducted an autopsy of the pilot. The pilot's death was attributed to "multiple blunt force injuries due to an airplane crash."
The FAA's Bioaeronautical Research Sciences Laboratory, Oklahoma City, Oklahoma, performed toxicology testing on specimens from the pilot. The testing was negative for carbon monoxide, cyanide, ethanol, and drugs.
