Casualties unknown

2024-07-20: Airbus Helicopters AS 350 BA, s/n 1671 (ZK-HJM) — Amuri Helicopters Limited — Paringa River 43° 38.7´ south 169° 26.0´ east, NZ

Paringa River 43° 38.7´ south 169° 26.0´ east, NZ

On July 20, 2024, an Airbus Helicopters AS 350 BA, s/n 1671 (registration ZK-HJM) operated by Amuri Helicopters Limited was involved in an aviation accident near Paringa River 43° 38.7´ south 169° 26.0´ east, NZ. Investigators recorded the probable cause as: The left and right main rotor hydraulic servo actuators were swapped during maintenance. It is virtually certain that the bolt securing the lower end of the left-hand servo became detached during flight. This summary draws on records from the New Zealand Transport Accident Investigation Commission (TAIC).

Sourcesthe New Zealand Transport Accident Investigation Commission (TAIC)Primary reportUpdated 1785093374Data APIEditorial standards

On 20 July 2024, an Airbus Helicopters AS350 BA (ZK-HJM) crashed during a precautionary landing after a bolt securing the left main rotor servo detached, leading to a control issue. Both occupants suffered minor injuries.

Accident Sequence

On 20 July 2024 at 1347, an Airbus Helicopters AS 350 BA helicopter, registered ZK-HJM, departed from Queenstown Aerodrome for a non-revenue repositioning flight to Franz Josef. The helicopter was operated by Amuri Helicopters Limited and had recently undergone maintenance by Salus Aviation (AW) Limited. On board were two people: a pilot and a passenger, who was also the operator's chief pilot.

After approximately 52 minutes of flight, the pilot felt a jolt and noticed the main rotor blade tips were no longer following the same path. About seven minutes later, during a descent for a precautionary landing near the Paringa River mouth, the cyclic control became significantly harder to push in one direction. Despite this, the helicopter remained controllable.

As the helicopter descended to land at about 10 to 20 feet above the ground, it experienced an unintentional roll to the left and collided with terrain. The helicopter came to rest on its left side, facing about 180 degrees from its original direction of travel.

The helicopter's emergency locator transmitter activated automatically, alerting the Rescue Coordination Centre, which dispatched a rescue helicopter. Both occupants were transported to hospital with minor injuries. The helicopter suffered significant damage.

Maintenance Issues

Prior to the accident flight, during a maintenance check that included a 150-hour airframe and 300-hour engine check, the left and right main rotor hydraulic servo actuators were swapped over at the operator's request to balance wear. The duplicate safety inspection, required to verify critical maintenance tasks, was certified as complete by trained personnel.

However, it is virtually certain that the bolt securing the lower end of the left-hand servo became detached during flight, leading to a change in control characteristics. It is very likely that the engineers performing the duplicate safety inspection were distracted and did not adequately verify the swap. Additionally, it is likely that the engineer who certified the second part of the inspection was experiencing cumulative fatigue, which contributed to the error.

After the accident, the missing bolt was found on the helicopter's transmission deck, but the nut was not located.

Aftermath

The pilot and passenger inspected the helicopter post-accident and discovered the missing bolt at the lower attachment point of the left servo. The rescue helicopter arrived about 1600 and transported the occupants to Grey Hospital in Greymouth with minor injuries.

Probable cause

The left and right main rotor hydraulic servo actuators were swapped during maintenance. It is virtually certain that the bolt securing the lower end of the left-hand servo became detached during flight. It is very likely that the engineers were distracted and did not adequately verify the swap. It is likely that the engineer who certified the second part of the duplicate safety inspection was experiencing cumulative fatigue that contributed to the error.

Investigation report by the New Zealand Transport Accident Investigation Commission (TAIC). Original record: https://taic.org.nz/inquiry/ao-2024-005. This page is a structured re-presentation; facts and quotes are in the Transport Accident Investigation Commission (TAIC), New Zealand.