Structural failure leads to fatal Piper Cherokee crash near Châtelat

Casualties unknown • Biel-Kappelen Flugplatz (LSZP), BE, CH

A Piper PA-28R-200 disintegrated in mid-air over the Jura region after encountering severe weather and structural overload.

What happened

On the afternoon of May 20, 1977, a Piper PA-28R-200 Cherokee Arrow II, registration HB-OQM, departed from the Bienne-Kappelen airfield for a planned one-hour local flight. The aircraft was carrying the pilot and three passengers. At the time, the region was experiencing unstable weather, with heavy cloud cover and developing thunderstorms along the Jura mountains.

Around 16:15, a witness observed the aircraft climbing through a gap in the clouds near Tavannes, surrounded by significant vertical cloud development. Shortly thereafter, at approximately 16:25, witnesses near Châtelat reported seeing the aircraft emerge from the clouds performing erratic maneuvers. During this period, observers noted that a portion of the wing was already missing. The aircraft then underwent a sudden mid-air disintegration, with the main wreckage falling into a forest near Monible and a large wing fragment landing over a kilometer away in a field.

All four occupants of the aircraft perished in the accident, and the aircraft was destroyed.

The investigation

The investigation focused on the structural integrity of the aircraft and the pilot's performance. Technical examination of the wreckage revealed that the left wing failed at station 118 due to the buckling of the upper spar cap. This failure was caused by a high positive load factor applied during flight. Laboratory analysis confirmed that the wing materials and construction met all required specifications and that no pre-existing fatigue or corrosion contributed to the break.

Medical examinations of the pilot revealed a blood alcohol concentration of 0.9‰, while the passengers showed varying levels of alcohol, including one at 1.0‰. The investigation also looked into the pilot's flight capabilities, noting he was qualified for visual flight rules (VFR) but not for instrument flight rules (IFR).

Findings

  • The pilot continued a VFR flight into unfavorable meteorological conditions involving thunderstorms.
  • The aircraft was subjected to structural loads exceeding the design limits, leading to the separation of the left wing.
  • The pilot's decision-making and ability to manage the flight were impaired by alcohol consumption.

Probable cause

The accident was caused by the decision to continue visual flight through deteriorating weather and thunderstorms, which led to structural failure due to excessive load factors, compounded by the pilot's impaired judgment resulting from alcohol use.

Frequently asked questions

What happened in the 1977-05-20 PIPER AIRCRAFT CORPORATION PA-28R-200 accident near Biel-Kappelen Flugplatz (LSZP), BE, CH?

A Piper PA-28R-200 disintegrated in mid-air over the Jura region after encountering severe weather and structural overload.

What aircraft was involved and where did it happen?

The accident on 1977-05-20 involved a PIPER AIRCRAFT CORPORATION PA-28R-200, registration HB-OQM, at Biel-Kappelen Flugplatz (LSZP), BE, CH.

What was the probable cause of the accident?

The accident was caused by the decision to continue visual flight through deteriorating weather and thunderstorms, which led to structural failure due to excessive load factors, compounded by the pilot's impaired judgment resulting from alcohol use.

Investigation report by the Swiss Transportation Safety Investigation Board (STSB / SUST). Original record: https://www.sust.admin.ch/inhalte/AV-berichte/900.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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