No fatalities

Go-Around Ends in Collision with Trees After Power Loss Following Balloon on Approach (N91081)

Grand Canyon-National Park, United States of AmericaLanding (descent or approach)

On April 13, 1990, a Cessna 207 Skywagon/Stationair (registration N91081) operated by Windrock Aviation was involved in an aviation accident near Grand Canyon-National Park, United States of America during landing or approach. No fatalities were reported. Investigators recorded the probable cause as: Improper adjustment of the turbocharger absolute pressure controller, and improper manipulation of the power plant controls by the pilot during the go-around. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 2026-06-11Data APIEditorial standards

An aircraft on approach to runway 21 ballooned to 70 ft agl, initiated a go-around, then lost power and crashed into trees about half a mile from the departure end of the runway. The turbocharger controller was set too low, and the pilot had insufficient experience with turbocharged engines.

Accident Sequence

Witnesses reported that the aircraft was about to touch down on runway 21 after a normal approach when it encountered variable wind conditions and ballooned to approximately 70 feet above ground level. The pilot then initiated a go-around. Shortly thereafter, witnesses observed a puff of smoke emanating from the aircraft. The pilot transmitted that the flight was 'going down'. The aircraft subsequently collided with trees on wooded terrain about half a mile from the departure end of the runway.

Post-Accident Examination

Examination of the wreckage revealed a lack of power signatures on the propeller. Evidence of sooting was found on the spark plugs, indicating a rich mixture. Testing of the turbo-controller showed that it had been adjusted to a low setting; the turbo would only produce a maximum air flow equal to high cruise power. The engine manufacturer reported that this situation could produce an over-rich mixture, particularly if the throttle and/or mixture controls were improperly manipulated.

Pilot Background

The pilot was reported to lack experience in aircraft with turbocharged engines and was not trained in accordance with the company training program.

Probable Cause and Factors

The probable cause of the accident was improper adjustment of the turbocharger absolute pressure controller, and improper manipulation of the power plant controls by the pilot during the go-around. Factors related to the accident were the failure of company management to properly train the pilot in accordance with the approved company training program, and the pilot's lack of experience in turbocharged engine operations.