Propeller strike during demonstration flight at Buochs

Casualties unknown • Buochs Flugplatz (LSZC), NW, CH

A Pilatus Turbo-Porter experienced a nose-over during landing at Buochs, resulting in the destruction of the engine and propeller.

What happened

On June 10, 1969, a Pilatus Turbo-Porter HB-FDP, operated by Pilatus Flugzeugwerke AG, was conducting a demonstration flight at Buochs airfield. The flight included the pilot and a passenger, a journalist attending the flight to write a report for a French aviation magazine.

During the approach to runway 07, the pilot executed an exceptionally steep and short final approach. The aircraft initially touched down on its main landing gear approximately 100 meters past the threshold. Following this initial contact, the aircraft briefly lifted again before performing a three-point landing. During the landing sequence, the pilot engaged the reverse thrust. Immediately after the second touchdown in the three-point position, the tail of the aircraft lifted, causing the propeller to strike the ground.

The investigation

The investigation examined the aircraft's recent modifications and the pilot's handling of the landing. The HB-FDP had recently been equipped with a new Hartzell wide-chord propeller, which provided enhanced performance and stronger reverse thrust capabilities. Additionally, the aircraft had been upgraded with Goodyear dual-piston brakes, which offered significantly more braking power than the previous single-piston version.

Investigators reviewed the pilot's qualifications and flight experience. While the pilot was fully licensed and experienced in the aircraft type, this was his first flight operating with the new propeller configuration and the upgraded braking system. The investigation also confirmed that the aircraft's weight and balance were within limits and that the pilot had correctly configured the flaps and trim for a light load.

Findings

  • The two occupants remained uninjured during the event.
  • The engine and propeller sustained total destruction due to the ground strike.
  • The primary cause of the accident was careless landing technique, specifically the pilot's failure to account for the increased effectiveness of the new braking system and the altered handling characteristics of the new propeller.

Probable cause

The accident was caused by improper landing technique, as the pilot did not adequately adjust for the significantly increased braking performance and the stronger reverse thrust provided by the newly installed equipment.

Frequently asked questions

What happened in the 1969-06-10 PILATUS FLUGZEUGWERKE AG PC-6/B1-H2 accident near Buochs Flugplatz (LSZC), NW, CH?

A Pilatus Turbo-Porter experienced a nose-over during landing at Buochs, resulting in the destruction of the engine and propeller.

What aircraft was involved and where did it happen?

The accident on 1969-06-10 involved a PILATUS FLUGZEUGWERKE AG PC-6/B1-H2, registration HB-FDP, at Buochs Flugplatz (LSZC), NW, CH.

What was the probable cause of the accident?

The accident was caused by improper landing technique, as the pilot did not adequately adjust for the significantly increased braking performance and the stronger reverse thrust provided by the newly installed equipment.

Investigation report by the Swiss Transportation Safety Investigation Board (STSB / SUST). Original record: https://www.sust.admin.ch/inhalte/AV-berichte/513.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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