No fatalities

19 Jul 2019: Cessna 210 5(205) (N8260Z) — Dallesport, OR

Dallesport, OR, United States

On 19 Jul 2019, a Cessna 210 5(205) Undesignat (registration N8260Z) was involved in an aviation accident near Dallesport, OR. No fatalities were reported. Investigators recorded the probable cause as: The pilot’s improper pitch control during the aborted takeoff, which resulted in a bounced landing and landing gear collapse. 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

On July 19, 2019, a Cessna 210-5 (N8260Z) was destroyed during takeoff near Dallesport, Oregon. The private pilot was not injured. Loss of airspeed indication led to an aborted takeoff, porpoising, nose gear collapse, and subsequent fire.

Accident Details

On July 19, 2019, at 0700 Pacific daylight time, a Cessna 210-5 (205), registration N8260Z, was destroyed in an accident near Dallesport, Oregon. The private pilot, the sole occupant, was not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

Pilot Account

According to the pilot, he arrived at the airport, checked the weather, and performed a preflight inspection and engine run-up with no anomalies noted. During the takeoff roll, he observed no airspeed indication and reduced engine power to abort the takeoff. He stated that he lightly pulled back on the yoke, felt the airplane lift off the runway, and then released the yoke. The airplane porpoised “3 possibly 4” times, “with each getting larger,” until the nose landing gear collapsed. The airplane slid down the runway and came to rest on the runway surface. As the pilot exited the airplane, he noticed flames near the door. The airplane was subsequently consumed by fire.

Investigation Findings

Postcrash fire damage precluded examination of the pitot-static system or airspeed indicator. The reason for the lack of airspeed indication during the takeoff roll could not be determined.

Contributing factors

Pitch control — Not attained/maintainedPilot