No fatalities

23 Dec 2019: ZENITH CH 750 — Xenia, OH

Xenia, OH, United States

On 23 Dec 2019, a ZENITH CH 750 was involved in an aviation accident near Xenia, OH. No fatalities were reported. Investigators recorded the probable cause as: The pilot’s failure to maintain airplane control during landing, which resulted in the right tire contacting the runway first followed by the left wing. This summary draws on records from NTSB; 12 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 1778583330Data APIEditorial standards

During the first flight of an experimental amateur-built airplane, the pilot reported a landing accident where the left wing dropped after right tire contact, shearing the left tire and axle, causing a skid and substantial damage.

Accident Details

The pilot of an experimental amateur-built airplane was conducting the aircraft's first flight. The accident occurred during landing at the airport. According to the pilot, he was lined up with the runway centerline with an airspeed of 60 mph and engine tachometer reading 1,600 rpm when he felt the right tire contact the runway. He reported that "in an instant the left wing came down and the left tire and axle [were] sheared off. The left wing contacted the runway and the plane skidded about 40 feet and came to a full stop."

Pilot Actions and Environment

The pilot stated that he used a higher landing airspeed because other builders of that airplane told him he needed to land with speed "so as not get near the stall speed as this aircraft does have leading edge slats and this equates to a high lift wing." He reported that the wind was calm at the accident airport, the altimeter setting was 30.12 inches, and the temperature was 55°F. A nearby airport 8 miles north recorded wind from 200° at 12 knots.

Aircraft Damage

Postaccident examination of the airplane revealed that the left wing tip was bent up, the nose landing gear "U" channel was bent 90°, and the skin around the left wing strut and landing gear attachment points was buckled. No preimpact anomalies with the airplane were reported.

Contributing factors

Performance/control parameters — Not attained/maintainedPilot