In-flight structural failure of Piper PA-30 near Eclose

Casualties unknown • Eclose, CH

A Piper PA-30 disintegrated in mid-air near Eclose, France, after the pilot encountered deteriorating weather conditions and lost control of the aircraft.

What happened

On December 20, 1980, a Piper PA-30, registration HB-LAC, departed from Saint-Rambert d'Albon for a private VFR flight toward Annemasse. During the flight, the pilot encountered worsening weather characterized by low cloud ceilings, rain, and snow showers. Upon encountering these conditions, the pilot performed a 180-degree turn near the A 43 motorway junction. During or immediately after this maneuver, the aircraft entered instrument meteorological conditions (IMC). Witnesses observed the aircraft emerging from the clouds in pieces, with parts of the engine, wing, and tail separating and falling over a distance of nearly 2 km. The aircraft entered a spin and crashed, resulting in the death of the pilot.

The investigation

Investigators examined the wreckage distributed across the terrain, noting that eight major components were recovered. Technical analysis of the debris revealed that the outer portion of the left wing had failed due to upward bending and torsion, and the horizontal stabilizers had broken due to excessive downward aerodynamic loads. Radar data from Lyon-Satolas helped reconstruct the flight path, showing the aircraft did not fly over the intended VOR station and had its transponder turned off. The investigation also reviewed the pilot's training records, which indicated a lack of proficiency in instrument flight. Engines and propellers were inspected, but no mechanical failures or fuel issues were identified as the cause of the engine's behavior.

Findings

  • The pilot entered IMC conditions while not qualified for instrument flight.
  • The aircraft's structural failure was caused by extreme aerodynamic loads during uncontrolled maneuvers.
  • The horizontal stabilizers broke due to an excessive nose-down force, likely resulting from an uncontrolled pitch or an inverted flight position.
  • The left wing failure was caused by violent rolling forces at high speed.
  • The pilot's lack of recent instrument training contributed to the loss of control during the weather transition.

Probable cause

The loss of control in instrument meteorological conditions by a pilot not qualified for such flight, leading to extreme aerodynamic loads that caused the aircraft to disintegrating in mid-air.

Frequently asked questions

What happened in the 1980-12-20 PIPER AIRCRAFT CORPORATION PA-30 accident near Eclose, CH?

A Piper PA-30 disintegrated in mid-air near Eclose, France, after the pilot encountered deteriorating weather conditions and lost control of the aircraft.

What aircraft was involved and where did it happen?

The accident on 1980-12-20 involved a PIPER AIRCRAFT CORPORATION PA-30, registration HB-LAC, at Eclose, CH.

What was the probable cause of the accident?

The loss of control in instrument meteorological conditions by a pilot not qualified for such flight, leading to extreme aerodynamic loads that caused the aircraft to disintegrating in mid-air.

Investigation report by the Swiss Transportation Safety Investigation Board (STSB / SUST). Original record: https://www.sust.admin.ch/inhalte/AV-berichte/999.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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