Casualties unknown

1998 Robin DR 400-140B Accident at Ecuvillens Aerodrome (HB-KDB)

Ecuvillens Aérodrome (LSGE), FR, CH

On October 16, 1998, an AVIONS PIERRE ROBIN S.A. ROBIN DR 400/140 B (registration HB-KDB) was involved in an aviation accident near Ecuvillens Aérodrome (LSGE), FR, CH. Investigators recorded the probable cause as: Loss of control during deceleration after landing, likely induced by erroneous rudder input. This summary draws on records from the Swiss Transportation Safety Investigation Board (STSB / SUST).

Sourcesthe Swiss Transportation Safety Investigation Board (STSB / SUST)Primary reportUpdated 2026-09-13Data APIEditorial standards

On October 16, 1998, a privately owned Robin DR 400-140B (HB-KDB) departed the runway during landing at Ecuvillens. The student pilot lost control after touchdown, likely due to erroneous rudder input, resulting in a rollover and minor injuries.

Incident Overview

On October 16, 1998, at 14:06 local time (UTC+2), a privately owned Robin DR 400-140B with registration HB-KDB was involved in an accident at the Ecuvillens aerodrome in Switzerland. The aircraft was operated by a student pilot holding a valid license for single-engine airplanes. The flight originated from Sion and followed a planned route to Ecuvillens. During the final approach, the pilot executed a stabilized landing on runway 28.

Sequence of Events

Witnesses described the touchdown as a precise three-point landing with wings level, though at an apparently high speed. Immediately after contact with the ground, the aircraft began to turn slowly to the right without apparent corrective action from the pilot. The plane left the paved runway, crossed the grass safety area, and entered a freshly plowed field. As the trajectory curved left, the nose gear dug into the soil, causing the right wing to strike the ground. The aircraft subsequently rolled over, resting on its nose wheel and propeller.

Investigation Findings

The investigation determined that the pilot was in good health and the aircraft was airworthy, with weight and balance within limits. Technical inspections of the braking system revealed no defects or maintenance issues. Skid marks indicated that the left main wheel skidded due to centrifugal force generated by the right turn, confirming that the wheel rotation was not obstructed.

Probable Cause Analysis

The accident was attributed to a loss of control during the deceleration phase after landing. The probable cause was identified as an erroneous action on the rudder pedals. The pilot later acknowledged a tendency to press the right pedal when the aircraft deviated to the right, particularly under stress or divided attention. This realization led the student to discontinue their flight training.

Investigation report by the Swiss Transportation Safety Investigation Board (STSB / SUST). Original record: https://www.sust.admin.ch/inhalte/AV-berichte/1720.pdf. This page is a structured re-presentation; facts and quotes are in the Swiss Transportation Safety Investigation Board (STSB), Switzerland.