No fatalities

2012-05-25: Cessna 208B Grand Caravan (D-FAAF) — Skydive Flyzone — Lézignan-Corbières, France

Lézignan-Corbières, FranceLanding (descent or approach)

On May 25, 2012, a Cessna 208B Grand Caravan (registration D-FAAF) operated by Skydive Flyzone was involved in an aviation accident near Lézignan-Corbières, France during landing or approach. No fatalities were reported. Investigators recorded the probable cause as: The investigation was unable to determine the cause of the turbine failure on final approach. Sufficient fuel (about 500 pounds) was still present in the tanks and all analysis of the engine, fuel supply control system and the fuel pump did not reveal any… This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781194830Data APIEditorial standards

A single-engine aircraft with a pilot and skydivers experienced an engine stoppage on final approach, resulting in an emergency landing in a vineyard. The pilot was uninjured; the aircraft was damaged beyond repair.

Incident Overview

A single-engine aircraft departed Lézignan-Corbières Airport at 1650 hours local time with a pilot and several skydivers on board. The flight proceeded uneventfully as the aircraft climbed to an altitude of 10,500 feet, where all skydivers exited the aircraft. Following the jump, the pilot reduced altitude to return to the departure airport.

Flight Sequence

On final approach to runway 08, at a height of 700 feet and a speed of 90 knots, the pilot slightly increased engine power to maintain the glide, then reduced power again. At that moment, the engine stopped and the propeller auto-feathered. The aircraft became unable to reach the runway, prompting the pilot to attempt an emergency landing.

Emergency Landing

The pilot executed an emergency landing in a vineyard located approximately 800 meters short of runway 08, to the right of its extended centerline. The pilot sustained no injuries, but the aircraft was damaged beyond repair as a result of the landing.

Investigation

The investigation was unable to determine the cause of the turbine failure on final approach. Sufficient fuel, about 500 pounds, remained in the tanks at the time of the incident. Analysis of the engine, fuel supply control system, and fuel pump did not reveal any anomalies.

Probable cause

The investigation was unable to determine the cause of the turbine failure on final approach. Sufficient fuel (about 500 pounds) was still present in the tanks and all analysis of the engine, fuel supply control system and the fuel pump did not reveal any anomalies.