Casualties unknown

2010-08-26: PIPER AIRCRAFT CORPORATION PA-32R-300 (HB-PRE) — Saanen, BE, CH

Saanen, BE, CH

On August 26, 2010, a PIPER AIRCRAFT CORPORATION PA-32R-300 (registration HB-PRE) was involved in an aviation accident near Saanen, BE, CH. Investigators recorded the probable cause as: The accident was due to a collision with terrain shortly after takeoff because the aircraft could not gain sufficient altitude due to significantly reduced engine performance caused by corrosion and wear damage to the camshaft and tappet bodies. This summary draws on records from the Swiss Transportation Safety Investigation Board (STSB / SUST).

Sourcesthe Swiss Transportation Safety Investigation Board (STSB / SUST)Primary reportUpdated 1785639345Data APIEditorial standards

On 26 August 2010, a Piper PA-32R-300 aircraft, registration HB-PRE, collided with terrain shortly after takeoff from Oey, Switzerland. The accident was caused by reduced engine performance due to corrosion and wear on the camshaft and tappet bodies.

Flight History

On 26 August 2010, a Piper PA-32R-300 aircraft, registration HB-PRE, departed from Oey in the municipality of Saanen/BE, Switzerland. Shortly after takeoff, the aircraft collided with terrain. The report does not specify the number of occupants or their injuries.

Engine Examination

Post-accident examination of the engine revealed corrosion and wear damage to the camshaft and tappet bodies. This damage led to a marked reduction in engine power, preventing the aircraft from gaining sufficient altitude after takeoff. The manufacturer had issued Service Letter L180B addressing known corrosion issues, but these recommendations were not incorporated into the engine maintenance program.

Cause and Contributing Factors

The accident was caused by the aircraft's inability to gain sufficient altitude due to significantly reduced engine performance resulting from corrosion and wear on the camshaft and tappet bodies. Contributing factors included the continuation of the takeoff despite reduced engine power, failure to follow the manufacturer's recommendations regarding known corrosion problems, and failure to integrate those recommendations into the engine maintenance program.

Probable cause

The accident was due to a collision with terrain shortly after takeoff because the aircraft could not gain sufficient altitude due to significantly reduced engine performance caused by corrosion and wear damage to the camshaft and tappet bodies. Contributing factors were the continuation of takeoff despite reduced engine power, failure to follow manufacturer's recommendations regarding known corrosion issues, and failure to integrate those recommendations into the engine maintenance program.

Investigation report by the Swiss Transportation Safety Investigation Board (STSB / SUST). Original record: https://www.sust.admin.ch/inhalte/AV-berichte/2160_e.pdf. This page is a structured re-presentation; facts and quotes are in the Swiss Transportation Safety Investigation Board (STSB), Switzerland.