Unintended Braking Leads to Runway Excursion in Beechcraft C90GTi

Casualties unknown • Les Eplatures aérodrome LSGC, NE, CH

A Hawker Beechcraft C90GTi crashed into an instrument approach structure after the pilot initiated a late rejected takeoff following insufficient acceleration.

What happened

On January 15, 2010, a Hawker Beechcraft C90GTi, registration HB-GPL, was attempting a takeoff from runway 24 at Les Eplatures Airport (LSGC) in Switzerland. During the takeoff roll, the pilot observed that the aircraft's airspeed failed to increase, peaking at 88 knots before dropping to 85 knots.

In response to the lack of acceleration, the pilot decided to abort the takeoff and apply the brakes. However, the decision to terminate the takeoff was made too late. The aircraft overran the end of the runway and collided violently with an instrument approach system structure located immediately beyond the runway threshold. The impact caused significant damage to the aircraft, which was destroyed, and heavily damaged the concrete block supporting the approach equipment. One occupant sustained serious injuries, while the other was slightly injured.

The investigation

The investigation examined the aircraft's performance, the pilot's experience, and the mechanical state of the braking system. Investigators found no mechanical defects in the aircraft's braking system. Instead, evidence suggested that the pilot's foot had slipped at the beginning of the takeoff roll, causing a significant leftward deviation. This slip likely resulted in unintended braking during the acceleration phase.

Furthermore, the investigation reviewed the takeoff configuration. The pilot had selected a "flaps up" configuration, which required a higher takeoff speed of 93 knots. The investigation noted that using a different flap setting, such as flaps approach, would have lowered the required takeoff speed and potentially reduced the downward force on the wheels, mitigating the effect of any accidental braking.

Findings

  • The primary cause of the accident was a collision with an obstacle following a late rejected takeoff procedure.
  • The insufficient acceleration was almost certainly caused by the pilot unintentionally applying the brakes during the takeoff roll.
  • The pilot had limited experience with this specific aircraft model.
  • The takeoff configuration (flaps up) was inappropriate for the circumstances.
  • The pilot's multi-engine training had been conducted on a different aircraft type, leading to incomplete familiarization, particularly regarding operations on short runways.

Probable cause

The accident was caused by a collision with an obstacle following a late aborted takeoff, which resulted from insufficient acceleration due to the pilot's unintended application of the brakes during the takeoff roll.

Frequently asked questions

What happened in the 2010-01-15 HAWKER BEECHCRAFT CORPORATION C90GTi accident near Les Eplatures aérodrome LSGC, NE, CH?

A Hawker Beechcraft C90GTi crashed into an instrument approach structure after the pilot initiated a late rejected takeoff following insufficient acceleration.

What aircraft was involved and where did it happen?

The accident on 2010-01-15 involved a HAWKER BEECHCRAFT CORPORATION C90GTi, registration HB-GPL, at Les Eplatures aérodrome LSGC, NE, CH.

What was the probable cause of the accident?

The accident was caused by a collision with an obstacle following a late aborted takeoff, which resulted from insufficient acceleration due to the pilot's unintended application of the brakes during the takeoff roll.

Investigation report by the Swiss Transportation Safety Investigation Board (STSB / SUST). Original record: https://www.sust.admin.ch/inhalte/AV-berichte/2097.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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