Loss of control leads to motor glider crash at Granges airport

Casualties unknown • Grenchen Flugplatz (LSZG), SO, CH

A pilot lost control of a Ventus-2cM motor glider during final approach, resulting in the destruction of the aircraft after a failed engine retraction attempt.

What happened

On May 3, 2003, a Ventus-2cM motor glider, registration HB-2098, crashed just before the threshold of runway 25 at Granges regional airport. The pilot was undergoing training to transition from standard gliders to self-launching motor gliders. During the flight, the pilot attempted to retract the engine but encountered difficulties because the propeller had not properly aligned.

While attempting to manage the partially extended engine, the pilot entered the final approach phase. During the turn to final, the aircraft's nose pitched up sharply, creating a dangerous flight attitude that risked an aerodynamic stall. The aircraft subsequently struck the ground on an asphalt cycle path before sliding into a nearby field. The impact resulted in the destruction of the aircraft, though there were no fatalities.

The investigation

Investigators examined the cockpit configuration and the pilot's training history. It was established that the pilot had recently completed training on a DG-505MB glider and was now transitioning to his own single-seat Ventus-2cM. The investigation focused on why the engine retraction failed and why the pilot lost control during the landing sequence.

Technical inspections revealed a mechanical issue with the camber flap lever, which could slip from its set position when the engine was running. Furthermore, the investigation looked into the cockpit ergonomics, noting that the control layout in the Ventus-2cM differed significantly from the pilot's previous training aircraft.

Probable cause

The primary cause of the accident was the pilot losing control of the aircraft during final approach. This was exacerbated by **a non-standardized cockpit control layout** that likely caused the pilot to confuse the camber flap lever with the landing gear lever, combined with insufficient flight experience for the specific aircraft type.

Frequently asked questions

What happened in the 2003-05-03 SCHEMPP-HIRTH FLUGZEUGBAU GMBH VENTUS-2cM accident near Grenchen Flugplatz (LSZG), SO, CH?

A pilot lost control of a Ventus-2cM motor glider during final approach, resulting in the destruction of the aircraft after a failed engine retraction attempt.

What aircraft was involved and where did it happen?

The accident on 2003-05-03 involved a SCHEMPP-HIRTH FLUGZEUGBAU GMBH VENTUS-2cM, registration HB-2298, at Grenchen Flugplatz (LSZG), SO, CH.

What was the probable cause of the accident?

The primary cause of the accident was the pilot losing control of the aircraft during final approach. This was exacerbated by **a non-standardized cockpit control layout** that likely caused the pilot to confuse the camber flap lever with the landing gear lever, combined with insufficient flight experience for the…

Investigation report by the Swiss Transportation Safety Investigation Board (STSB / SUST). Original record: https://www.sust.admin.ch/inhalte/AV-berichte/1856_f.pdf. This page is a structured re-presentation; facts and quotes are in the Swiss Transportation Safety Investigation Board (STSB), Switzerland.

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