Engine failure caused by cooling fan disintegration leads to emergency landing in Switzerland

Casualties unknown • Wichtrach, BE, CH

A training flight in a Cabri G2 ended in an emergency autorotation after a cooling fan failure caused engine power loss and smoke.

What happened

On July 13, 2013, a Cabri G2 helicopter, registration HB-ZLJ, was conducting a training flight near Neuhaus, Switzerland. The flight, involving a flight instructor and a student, initially proceeded without issue through the Bernese Oberland. However, during a series of landing exercises, the crew heard a loud bang followed by a distinct smell. The instructor performed an immediate landing to inspect the engine compartment.

During the inspection, a mechanic joined the crew and identified a loose strobe light component and some singed material on the air filter. After a brief test flight to return to the student, the crew experienced a recurrence of the smell, followed by visible grey smoke emerging from the engine cowling. As the pilot attempted a precautionary landing, a rattling noise and heavy vibrations occurred, leading to a total engine failure. The pilot successfully executed an autorotation, landing in a grain field after striking a fence line. The occupants escaped the aircraft without injury, though the helicopter sustained heavy damage.

The investigation

SUST examined the engine compartment and the components of the cooling system. The investigation focused on the sequence of events following the initial mechanical noise and the subsequent smoke. Investigators analyzed the physical state of the cooling fan and the material properties of its components to determine why the engine failed during the second flight segment.

Findings

  • The primary cause of the engine failure was the disintegration of the cooling system fan.
  • The fan's front disc failed due to material fatigue.
  • The design of the cooling fan was inadequate for the operational stresses encountered.
  • The front disc exhibited insufficient lateral stiffness and material inconsistencies, including brittleness and a wall thickness that was up to 25% below specifications in certain areas.

Safety action

Following the investigation, safety recommendations were issued to the European Union Aviation Safety Agency (EASA) to ensure the manufacturer, Hélicoptères Guimbal, implemented a fleet-wide inspection program and took necessary measures to prevent future fan disintegrations.

Probable cause

The engine failure was caused by the structural failure of the cooling fan's front disc due to material fatigue, inadequate design stiffness, and manufacturing defects in the material thickness and composition.

Frequently asked questions

What happened in the 2013-07-13 HÉLICOPTÈRES GUIMBAL CABRI G2 accident near Wichtrach, BE, CH?

A training flight in a Cabri G2 ended in an emergency autorotation after a cooling fan failure caused engine power loss and smoke.

What aircraft was involved and where did it happen?

The accident on 2013-07-13 involved a HÉLICOPTÈRES GUIMBAL CABRI G2, registration HB-ZLJ, at Wichtrach, BE, CH.

What was the probable cause of the accident?

The engine failure was caused by the structural failure of the cooling fan's front disc due to material fatigue, inadequate design stiffness, and manufacturing defects in the material thickness and composition.

Investigation report by the Swiss Transportation Safety Investigation Board (STSB / SUST). Original record: https://www.sust.admin.ch/inhalte/AV-berichte/2267_d.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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