No fatalities

2003-08-28: Pilatus PC-6 (Porter & Turbo Porter) (N394R) — Tom Bishop — Vigo Park, United States of America

Vigo Park, United States of AmericaFlight

On August 28, 2003, a Pilatus PC-6 (Porter & Turbo Porter) (registration N394R) operated by Tom Bishop was involved in an aviation accident near Vigo Park, United States of America in flight. No fatalities were reported. Investigators recorded the probable cause as: The loss of propeller pitch control for undetermined reasons. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781200865Data APIEditorial standards

A pilot with 33,000 hours reported extreme clear air turbulence and a loud pop before losing propeller pitch control. The airplane descended at over 10,000 fpm in a near-vertical attitude. The pilot evacuated and deployed his parachute. The aircraft impacted terrain. No mechanical anomalies were found; cause of control loss undetermined.

Incident Overview

During a cruise flight, a pilot with 33,000 hours of flight experience reported encountering "extreme clear air turbulence followed by three jolts in rapid succession." According to the pilot's statement, he heard a loud pop as he moved the throttle to the flight idle position. As airspeed decreased, the pilot attempted to increase power but found that the throttle would not move from the flight idle position. Simultaneously, the propeller entered the BETA range.

Aircraft Behavior

The airplane pitched downward as the pilot continued efforts to push the throttle lever forward. During this event, the aircraft established a rate of descent exceeding 10,000 feet per minute at a near-vertical attitude. The pilot subsequently initiated an evacuation of the airplane and deployed his sport parachute, which he was wearing during the flight. The airplane then impacted terrain.

Post-Accident Inspection

A post-accident examination of the airframe, propeller, and engine revealed no mechanical anomalies that could have caused the accident. The reason for the loss of propeller pitch control could not be determined.

Probable Cause

The official probable cause is the loss of propeller pitch control for undetermined reasons.