Propeller damage during ground excursion at Bern-Belpmoos

Casualties unknown • Bern Flughafen (LSZB), BE, CH

A Beagle E 3 aircraft experienced a sudden directional swing during landing rollout, resulting in propeller tip contact with the runway surface.

What happened

On July 19, 1963, a Beagle E 3 (registration G-ASCC) was conducting pattern work at Bern-Belpmoos airfield for the purpose of pilot type conversion. The flight, involving two experienced pilots, consisted of several landing attempts. During the initial landings, the aircraft demonstrated a consistent tendency to veer toward the left, requiring the pilot to apply right-side braking to maintain the centerline.

Following a successful fourth landing at approximately 09:1s, the pilot signaled to continue the pattern. However, while the second pilot was adjusting the flap settings, the aircraft began to swing left again. The pilot attempted to correct this by applying the right brakes. During this corrective maneuver, the aircraft suddenly swerved approximately 90 degrees to the right. This abrupt movement caused the tailwheel to lift off the ground, leading the propeller tips to strike the runway surface.

There were no injuries to the occupants during the event.

The investigation

Investigators examined the mechanical condition of the aircraft and the runway environment. The weather at the time of the incident was clear, cloudless, and calm with no wind and 10 km visibility. The accident occurred on the paved runway at the airfield.

Technical inspection of the braking system revealed an imbalance in wheel rotation. When rotated manually, the right wheel spun freely for several revolutions, whereas the left wheel moved only a fraction of a turn. This indicated that the left wheel had significantly higher resistance or drag than the right.

Findings

  • The primary cause of the sudden rightward swerve was excessive braking applied during the attempt to correct the initial leftward drift.
  • The aircraft exhibited a natural tendency to wander or swing during the landing rollout, likely due to the characteristics of the unsteered tailwheel.
  • A disparity in braking resistance existed between the wheels, as the left wheel exhibited much higher drag than the right wheel, contributing to the initial leftward deviation.

Probable cause

The sudden 90-degree swerve and subsequent propeller strike were caused by the pilot applying excessive braking force to correct a leftward veer, compounded by an imbalance in wheel braking resistance.

Frequently asked questions

What happened in the 1963-07-18 BEAGLE AIRCRAFT LTD. E3 M11 accident near Bern Flughafen (LSZB), BE, CH?

A Beagle E 3 aircraft experienced a sudden directional swing during landing rollout, resulting in propeller tip contact with the runway surface.

What aircraft was involved and where did it happen?

The accident on 1963-07-18 involved a BEAGLE AIRCRAFT LTD. E3 M11, registration G-ASCC, at Bern Flughafen (LSZB), BE, CH.

What was the probable cause of the accident?

The sudden 90-degree swerve and subsequent propeller strike were caused by the pilot applying excessive braking force to correct a leftward veer, compounded by an imbalance in wheel braking resistance.

Investigation report by the Swiss Transportation Safety Investigation Board (STSB / SUST). Original record: https://www.sust.admin.ch/inhalte/AV-berichte/121.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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