Casualties unknown

1964-05-31: DE HAVILLAND AIRCRAFT COMPANY LIMITED DH 82 A (HB-UBH) — Courtelary Aérodrome (LSZJ), BE, CH

Courtelary Aérodrome (LSZJ), BE, CH

On May 31, 1964, a DE HAVILLAND AIRCRAFT COMPANY LIMITED DH 82 A (registration HB-UBH) was involved in an aviation accident near Courtelary Aérodrome (LSZJ), BE, CH. Investigators recorded the probable cause as: The accident was caused by a sudden wind shift that pushed the aircraft off course, combined with the pilot's delayed decision to release the glider, leading to a collision with a parked aircraft. This summary draws on records from the Swiss Transportation Safety Investigation Board (STSB / SUST).

Sourcesthe Swiss Transportation Safety Investigation Board (STSB / SUST)Primary reportUpdated 1785034239Data APIEditorial standards

A De Havilland Tiger Moth towing a glider collided with a parked aircraft after a sudden wind change during takeoff at Courtelary.

What happened

On May 31, 1964, a De Havilland DH-82 Tiger Moth, registration HB-UBH, was performing a glider tow operation at the Courtelary aerodrome. The flight was intended to tow a Mucha HB-614 glider. During the takeoff roll, approximately 100 meters after applying full power, the aircraft encountered a sudden and powerful lateral gust from the south. This wind shift pushed the aircraft toward a nearby hangar.

In an attempt to maintain the runway centerline, the pilot banked the aircraft to the left, which caused the left wing to approach the ground. To mitigate the developing crisis, the pilot released the glider and attempted to continue the takeoff. However, the aircraft's path intersected with an L-Spatz 55 glider parked at the edge of the field. The Tiger Moth's landing gear struck the stationary glider, causing the pilot to lose control. The aircraft tilted sharply to the left and performed a heavy landing in an adjacent wheat field.

The investigation

The investigation examined the meteorological conditions at the time of the accident, noting that while the day began clearly, storm activity was approaching. The wind had recently shifted from a northerly breeze to a westerly direction. Investigators also reviewed the pilot's actions during the critical moments of the takeoff roll and the mechanical state of the aircraft.

Findings

  • A sudden change in wind direction caused the towing aircraft to be pushed off its intended course.
  • The pilot failed to maintain the aircraft's alignment with the runway following the gust.
  • The pilot delayed the release of the glider for too long, failing to realize the collision course with the parked aircraft in time.
  • The collision with the stationary glider resulted in a loss of control and the subsequent heavy landing.

There were no injuries to the pilot or any other persons during the event.

Probable cause

The accident was caused by a sudden wind shift that pushed the aircraft off course, combined with the pilot's delayed decision to release the glider, leading to a collision with a parked aircraft.

Investigation report by the Swiss Transportation Safety Investigation Board (STSB / SUST). Original record: https://www.sust.admin.ch/inhalte/AV-berichte/186.pdf. This page is a structured re-presentation; facts and quotes are in the Swiss Transportation Safety Investigation Board (STSB), Switzerland.