Uncontrolled descent following propeller pitch control failure

No fatalities • Vigo Park, United States of America • Flight

An aircraft experienced a rapid descent and subsequent terrain impact after the propeller entered beta mode following severe turbulence.

What happened

While operating in the cruise phase of flight, the aircraft encountered severe clear air turbulence characterized by three rapid, heavy jolts. During this period of instability, the pilot moved the throttle to the flight idle position, at which point an audible pop was heard. As the pilot attempted to increase power to compensate for decreasing airspeed, the throttle became stuck in the flight idle position, causing the propeller to enter the beta range.

Following this mechanical failure, the aircraft entered a steep, near-vertical dive with a descent rate exceeding 10,000 feet per minute. The pilot, who was wearing a sport parachute during the flight, initiated an emergency evacuation and successfully deployed the parachute. The aircraft subsequently struck the ground.

Findings

Post-accident inspections of the engine, propeller, and airframe revealed no mechanical defects or anomalies that would account for the incident. Investigators were unable to identify the specific reason why the propeller lost pitch control and transitioned into beta mode.

Probable cause

The cause of the propeller transitioning into beta mode and the subsequent loss of pitch control remains undetermined.

Frequently asked questions

What happened in the 2003-08-28 Pilatus PC-6 (Porter & Turbo Porter) accident near Vigo Park, United States of America?

An aircraft experienced a rapid descent and subsequent terrain impact after the propeller entered beta mode following severe turbulence.

Were there any fatalities in the 2003-08-28 Pilatus PC-6 (Porter & Turbo Porter) accident?

No fatalities were recorded in this accident.

What aircraft was involved and where did it happen?

The accident on 2003-08-28 involved a Pilatus PC-6 (Porter & Turbo Porter), registration N394R, operated by Tom Bishop, at Vigo Park, United States of America.

What was the probable cause of the accident?

The cause of the propeller transitioning into beta mode and the subsequent loss of pitch control remains undetermined.

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