Engine failure leads to ditching of Piper PA-46 near Ibiza

Casualties unknown • Ibiza (Illes Balears), ES

A private Piper PA-46 350P experienced a total engine failure during flight, resulting in a controlled ditching in the Mediterranean Sea.

What happened

On April 30, 2007, a private PIPER PA-46 350P, registration EC-IQX, departed from Cuatro Vientos Airport (LECU) bound for Palma de Mallorca. The flight was carrying a pilot and three passengers. During the descent to 13,000 feet, the pilot attempted to increase power but received no response from the engine. The pilot observed that both engine torque and Interstage Turbine Temperature (ITT) had dropped to zero, indicating the turbine had stopped.

Despite several attempts to troubleshoot the issue by switching fuel tanks, using the emergency pump, and performing an in-flight restart procedure similar to a ground start, the engine failed to restart. The pilot declared an emergency at 17:17:01, citing a loss of fuel supply, and subsequently diverted the aircraft toward Ibiza. After losing communication with air traffic control, the pilot performed a controlled ditching approximately 15 NM north of Ibiza at 17:33:00. The aircraft struck the water with its tail, causing significant impact. All four occupants survived the impact, though the aircraft eventually sank after approximately 40 minutes.

Probable cause

The engine flameout was likely caused by an interruption in the fuel flow to the engine, leading to a simultaneous drop in torque and ITT.

Frequently asked questions

What happened in the 2007-04-30 Piper PA-46 Malibu accident near Ibiza (Illes Balears), ES?

A private Piper PA-46 350P experienced a total engine failure during flight, resulting in a controlled ditching in the Mediterranean Sea.

What aircraft was involved and where did it happen?

The accident on 2007-04-30 involved a Piper PA-46 Malibu, registration EC-IQX, at Ibiza (Illes Balears), ES.

What was the probable cause of the accident?

The engine flameout was likely caused by an interruption in the fuel flow to the engine, leading to a simultaneous drop in torque and ITT.

Investigation report by the Spanish Civil Aviation Accident and Incident Investigation Commission (CIAIAC). Original record: https://www.transportes.gob.es/recursos_mfom/2007_018_a_0.pdf. This page is a structured re-presentation; facts and quotes are in the Comision de Investigacion de Accidentes e Incidentes de Aviacion Civil (CIAIAC), Spain - Ministerio de Transportes y Movilidad Sostenible.

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