Main Gearbox Failure Leads to Helicopter Crash in Norway

Casualties unknown • Gausdal / Lillehamer, PL

A Hughes Helicopters Inc. 369D experienced a catastrophic loss of rotor power during a landing approach in Follebu, Norway, resulting in substantial aircraft damage but no injuries.

What happened

On 1 August 2019, a Hughes Helicopters Inc. 369D helicopter, registration SE-JVJ, was conducting power line inspections for an electricity grid company in Follebu, Norway. Approximately 52 minutes into the flight, the commander detected abnormal vibrations in the aircraft. As the flight continued, the vibrations intensified and were accompanied by a loud metallic sound.

In an attempt to inspect the cause of the disturbance, the commander decided to abort the mission and locate a landing site. While hovering at an altitude of approximately 2 to 3 meters over a grassy field, a loud bang occurred, and the aircraft suffered a sudden loss of power to the rotor system. The helicopter rotated sharply, the right skid collapsed upon impact, and the main rotor blades struck the ground. The crew members were uninjured, though the aircraft sustained severe damage.

The investigation

The Norwegian Safety Investigation Authority (NSIA) examined the wreckage and performed metallurgical analyses on the components. The investigation focused on the mechanical failure of the main gearbox and the maintenance history of the aircraft. Investigators scrutinized the continuing airworthiness management of the operator, First European Aviation Company Sp. z.o.o, and reviewed the maintenance logs and documentation regarding the gearbox's service life.

Findings

  • The primary cause of the loss of rotor power was a fracture in the main gearbox input pinion due to fatigue.
  • Metallurgical examination revealed that the fracture had likely been developing for several years.
  • An oil leak related to the developing fracture had been improperly addressed using two wine corks as plugs, which effectively concealed the leak and prevented necessary troubleshooting.
  • The main gearbox had exceeded its required overhaul interval by 749 hours due to errors in the operator's maintenance program and inaccurate tracking of operating hours.
  • The operator's continuing airworthiness management and maintenance documentation were found to be inadequate, specifically regarding the ability to trace vital maintenance history for safety-critical components.

Probable cause

The accident was caused by the fatigue failure of the main gearbox input pinion, a condition that likely could have been detected had the gearbox overhaul been performed according to the required intervals and had the improper use of wine corks not masked an underlying oil leak.

Frequently asked questions

What happened in the 2019-08-01 Hughes 369D accident near Gausdal / Lillehamer, PL?

A Hughes Helicopters Inc. 369D experienced a catastrophic loss of rotor power during a landing approach in Follebu, Norway, resulting in substantial aircraft damage but no injuries.

What aircraft was involved and where did it happen?

The accident on 2019-08-01 involved a Hughes 369D, registration SE-JVJ, at Gausdal / Lillehamer, PL.

What was the probable cause of the accident?

The accident was caused by the fatigue failure of the main gearbox input pinion, a condition that likely could have been detected had the gearbox overhaul been performed according to the required intervals and had the improper use of wine corks not masked an underlying oil leak.

Investigation report by the Polish State Commission on Aircraft Accidents Investigation (PKBWL). Original record: https://pkbwl.gov.pl/raporty/2019-3241/. This page is a structured re-presentation; facts and quotes are in the Panstwowa Komisja Badania Wypadkow Lotniczych (PKBWL), Poland.

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