Engine failure caused by crankshaft counterweight detachment in Piper PA 31

Casualties unknown • letiště Krakow Balice, Polsko, CZ

A Piper PA 31-350 experienced a sudden left engine failure during an aerial photography mission near Krakow, Poland, due to a mechanical failure within the engine.

What happened

On July 7, 2012, at 10:10 UTC, a Piper PA 31-350, registration OK-EKV, was conducting aerial photography near Krakow, Poland. During the climb phase of the flight, the crew experienced a sudden, heavy impact originating from the left engine, which was immediately followed by a loss of power and engine shutdown.

The pilot promptly implemented single-engine emergency procedures. Given the aircraft's proximity to Krakow Balice Airport (EPKK), the pilot elected to return to the departure airfield. The aircraft landed safely at EPKK without any damage to the airframe or injuries to the two-member crew.

The investigation

The ÚZPLN investigation focused on a technical examination of the left Lycoming TIO 540J2BD engine. Upon inspection of the engine cowling, investigators discovered significant structural damage to the upper engine casing.

Detailed disassembly of the engine revealed that a segment of the crankshaft counterweight (p/n LW-19210) had become detached. The investigation found that a circular washer (p/n 71907) within the weight's retaining pin hole had failed and broken into several pieces, which were recovered from the oil sump. This failure allowed the retaining pin to shift axially, damaging the retaining ring and allowing the counterweight segment to loosen. The loose component then struck the engine casing, the connecting rod of the sixth cylinder, and the camshaft, causing the camshaft to deform and disengage from the gears.

Findings

  • The primary cause of the engine failure was the detachment of a crankshaft counterweight segment.
  • The failure originated from the structural failure of a circular washer, likely due to material fatigue.
  • The loss of the washer allowed the retaining pin to move, leading to the subsequent destruction of the engine casing and internal rotating components.
  • Standard maintenance procedures do not include a specific inspection of this internal component, meaning the defect could not have been detected without a complete engine teardown.
  • The aircraft was maintained in accordance with all applicable regulations, and the pilot was fully qualified and competent.

Probable cause

The engine failure was caused by the detachment of a crankshaft counterweight segment, resulting from the fatigue-induced failure of a circular washer within the engine assembly.

Frequently asked questions

What happened in the 2012-07-07 Piper PA 31-350 accident near letiště Krakow Balice, Polsko, CZ?

A Piper PA 31-350 experienced a sudden left engine failure during an aerial photography mission near Krakow, Poland, due to a mechanical failure within the engine.

What aircraft was involved and where did it happen?

The accident on 2012-07-07 involved a Piper PA 31-350, registration OK-EKV, at letiště Krakow Balice, Polsko, CZ.

What was the probable cause of the accident?

The engine failure was caused by the detachment of a crankshaft counterweight segment, resulting from the fatigue-induced failure of a circular washer within the engine assembly.

Investigation report by the Czech Air Accidents Investigation Institute (UZPLN). Original record: https://uzpln.gov.cz/incident/309. This page is a structured re-presentation; facts and quotes are in the Ustav pro odborne zjistovani pricin leteckych nehod (UZPLN), Czech Republic.

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