Engine failure caused by intake valve breakage in Robinson R44

Casualties unknown • GLP Staldenhorn, BE, CH

A Robinson R44 experienced a significant loss of engine power following an intake valve failure during a mountain flight training session in Switzerland.

What happened

On May 25, 2018, a Robinson R44 II, registration HB-ZJW, was conducting a mountain flight training mission (MOU) departing from Sion Airport. The crew, consisting of an instructor and a student pilot, intended to perform several landings at various mountain locations, including the Staldenhorn site in the Canton of Bern.

After completing several landings at altitudes below 2,000 meters, the helicopter landed at the Staldenhorn landing site. Shortly after touchdown, while the engine was at reduced power, the crew heard a sharp noise. This was immediately followed by an increase in manifold pressure, a drop in engine RPM, and smoke emerging from the engine compartment. The engine subsequently ceased operation. Following the incident, engine oil was observed leaking from the aircraft, and the helicopter was deemed unserviceable.

The investigation

The investigation focused on the Lycoming IO-540-AE1A5 engine, which had 804 hours since its last overhaul. The engine was transported to a specialized center for a comprehensive teardown, and specific components were sent to a laboratory for macroscopic analysis.

Upon disassembly, investigators identified that the intake valve of cylinder number one had broken. The valve head had fractured into three separate pieces, and the stem had become detached from the head. \n## Findings

  • The primary cause of the engine power loss was the rupture of the intake valve in cylinder number one.
  • Detailed examination suggested that the engine may have been subject to engine detonation, although the specific origin of these detonations could not be determined.
  • These detonation events likely led to the premature wear of the intake valve in cylinder number one.
  • While cylinder number five was noted as the hottest cylinder, cylinder number one benefited from better ambient air convection cooling; however, the structural failure of the valve led to the engine failure.

Probable cause

The engine failure was caused by the breakage of the intake valve in cylinder number one, resulting from premature wear potentially induced by engine detonation.

Frequently asked questions

What happened in the 2018-05-25 ROBINSON HELICOPTER COMPANY R44 II accident near GLP Staldenhorn, BE, CH?

A Robinson R44 experienced a significant loss of engine power following an intake valve failure during a mountain flight training session in Switzerland.

What aircraft was involved and where did it happen?

The accident on 2018-05-25 involved a ROBINSON HELICOPTER COMPANY R44 II, registration HB-ZJW, at GLP Staldenhorn, BE, CH.

What was the probable cause of the accident?

The engine failure was caused by the breakage of the intake valve in cylinder number one, resulting from premature wear potentially induced by engine detonation.

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