Amateur-built KR-2 accident near Richfield, Utah, June 23, 2010

The NTSB's narrative final · quoted from the NTSB record

The pilot reported that he had recently purchased the airplane and, before flying it, he had a resident mechanic perform a condition inspection on the airplane, which was signed off on the day of the accident. The pilot stated that he did several long static engine runs on the ground and then planned to perform several high-speed taxi runs. During the second high-speed taxi, with a tailwind, the airplane became airborne. This was the first time the pilot had flown the airplane and he decided to continue the takeoff to stay in the traffic pattern and return for landing. The pilot reported that when he had climbed to about 250 feet, the engine began to lose power and the airplane began to descend. He turned back towards the runway's midpoint to land and the right wing suddenly dropped and impacted the airport's perimeter fence. The airplane came to rest inverted with its engine broken off and under the fuselage. The left wing was broken at the wing root, but not separated from the fuselage. Postaccident examination of the engine by a Federal Aviation Administration inspector and the resident mechanic found that the slide-type carburetor contained a gummy residue and did not operate freely. Additionally, the spark plugs appeared to have excessive carbon buildup. During the examination of the airplane, other than the condition of the carburetor and spark plugs, no preimpact mechanical anomalies were found.

The complete narrative as the NTSB published it. The NTSB's docket holds the report as a PDF and any photographs, statements and other documents from the investigation.