No fatalities

2002-05-13: Socata TBM-700 (N700AR) — European Aeronautics Defense & Space Company - EADS — Moulins, France

Moulins, FranceLanding (descent or approach)

On May 13, 2002, a Socata TBM-700 (registration N700AR) operated by European Aeronautics Defense & Space Company - EADS was involved in an aviation accident near Moulins, France during landing or approach. No fatalities were reported. Investigators recorded the probable cause as: The approach was completed with the engine at reduced power. It was not possible to determine if the engine was running at 'full reduced power' or at a minimum of 10% of torque as recommended by the manufacturer. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 8 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781201859Data APIEditorial standards

A single-engine aircraft on an aerial photography flight struck its left wing tip on the runway during landing, slid 95 meters, caught fire, and was destroyed. Both occupants escaped uninjured.

Incident

A single-engine aircraft was completing an aerial photography flight from Clermont-Ferrand, carrying one pilot and one passenger. On final approach to Moulins-Montbeugny Airport runway 08, at a speed of 85 knots, the pilot estimated that the nose-up attitude of the aircraft was excessive and increased engine power. The aircraft then rolled to the left, causing the left wing tip to strike the runway surface. Out of control, the aircraft impacted the ground, lost its undercarriage, and slid for 95 metres before coming to rest, bursting into flames. Both occupants escaped uninjured. The fire brigade arrived 15 minutes later. The aircraft was destroyed by fire.

Probable Cause

The official investigation reported that the approach was completed with the engine at reduced power. It was not possible to determine if the engine was running at 'full reduced power' or at a minimum of 10% of torque as recommended by the manufacturer. During an approach completed with an engine at 'full reduced power', full power can be obtained only after a period of five seconds.