No fatalities

Beech 200 F-GMPO accident at Montpellier aerodrome

Conséquences et dommages, FR

On January 7, 2011, a Beech 200 was involved in an aviation accident near Conséquences et dommages, FR. No fatalities were reported. Investigators recorded the probable cause as: The accident resulted from a confusion between the ENG AUTO IGNITION and IGNITION AND ENGINE START switches, not detected by the crew despite the amber MASTER CAUTION light; non-application of the DUAL GENERATOR FAILURE procedure, made very difficult by… This summary draws on records from the French Bureau d'Enquêtes et d'Analyses (BEA); 8 related events involving the same aircraft type or operator are linked below.

Sourcesthe French Bureau d'Enquêtes et d'Analyses (BEA)Primary reportUpdated 2026-10-18Data APIEditorial standards

On 7 January 2011, a Beech 200 (F-GMPO) suffered a total electrical failure in initial climb after a likely switch confusion. The crew made an emergency landing at Montpellier, where the main landing gear collapsed.

Accident overview and flight sequence On Friday 7 January 2011 at 08:13 local time, a Beech 200 registered F-GMPO, operated by a company, departed runway 13L at Montpellier aerodrome for an IFR flight to Albert Bray with two passengers. During initial climb, the pilot flying, seated in the left seat, found the left attitude indicator unusable. The captain, in the right seat, took control and continued using the right attitude indicator. The pilot flying then noticed the amber generator warning lights illuminated and attempted, without success, to reset the generators. The captain decided to interrupt the flight and asked the pilot flying to extend the landing gear. During the normal gear-extension sequence, the aircraft experienced a total electrical failure. Cockpit illumination was very low, making instrument indications difficult to read. The captain asked the pilot flying to illuminate the instruments with an electric torch. The captain briefly saw the threshold of runway 31R. The pilot flying suggested a go-around because of a doubt about gear lock. During a low circuit, the pilot flying continued the manual gear-extension procedure. As the precautionary landing became imminent, the pilot flying interrupted the manual extension, still uncertain whether the gear was locked because sufficient resistance had not been felt. Given the weather and instrument-reading difficulties, the captain decided to land. During landing roll, the main landing gear slowly collapsed, the fuselage contacted the ground, and the aircraft stopped on the runway. The aircraft was heavily damaged.

Probable cause

The accident resulted from a confusion between the ENG AUTO IGNITION and IGNITION AND ENGINE START switches, not detected by the crew despite the amber MASTER CAUTION light; non-application of the DUAL GENERATOR FAILURE procedure, made very difficult by environmental conditions; and incomplete application of the emergency landing-gear extension procedure in a phase of flight allowing little time to complete it. The similarity and proximity of the switches were a contributory factor.

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Frequently asked questions

What happened in the 7 Jan 2011 Beech 200 accident near Conséquences et dommages, FR?

On 7 January 2011, a Beech 200 (F-GMPO) suffered a total electrical failure in initial climb after a likely switch confusion. The crew made an emergency landing at Montpellier, where the main landing gear collapsed.

Were there any fatalities in the 7 Jan 2011 Beech 200 accident?

No fatalities were recorded in this accident.

What aircraft was involved and where did it happen?

The accident on 7 Jan 2011 involved a Beech 200, at Conséquences et dommages, FR.

What was the probable cause of the accident?

The accident resulted from a confusion between the ENG AUTO IGNITION and IGNITION AND ENGINE START switches, not detected by the crew despite the amber MASTER CAUTION light; non-application of the DUAL GENERATOR FAILURE procedure, made very difficult by environmental conditions; and incomplete application of the…