12 January 2022

Helicopter crash highlights inadequacies of upper torso restraints

Start the conversation
Overlay image of helicopter crash site with notes

Wreckage of VH-HUE, which crashed on 17 April, 2018, looking upstream towards the drill site, showing the nose of the helicopter and pilot’s seat. Photo: Australian Transport Safety Bureau.

A helicopter crash in the NSW Snowy Mountains has highlighted the inadequacies of standard restraints in aerial firefighting and long-line lifting, with an Australian Transport Safety Bureau (ATSB) investigation finding they are likely not fit-for-purpose.

On 17 April, 2018, the pilot of a Garlick Helicopters UH-1H ‘Huey’ helicopter was conducting long-line lifting operations near Talbingo, in the Snowy Mountains, to assist drilling works for the Snowy 2.0 project.

After 11 uneventful lifting runs between a drill site and a laydown area, the pilot was climbing clear of trees near the drill site, waiting for the next load to be ready.

As the helicopter started to climb, the pilot heard a loud mechanical “screaming” noise and started planning for a forced landing. Witnesses also reported seeing smoke, and some advised they heard a “bang” at about the same time.

READ ALSO ANU scientists create first rocket powered by… mothballs

Almost immediately, the pilot also heard an audible alarm, then experienced noticeable yaw and engine power loss.

Unable to determine if ground crew would be clear of the helicopter at the drill site clearing, the pilot opted instead to conduct the forced landing in the nearby Yarrangobilly riverbed to the southwest.

The helicopter subsequently hit trees and the riverbed, and was destroyed. Ground personnel from the drill site immediately responded to the accident, extinguishing a small fire in the engine bay and removing the pilot from the wreckage.

The pilot was wearing a lapbelt and a helmet, but was not wearing the fitted upper torso restraint. He suffered serious head injuries.

Overlay image of helicopter crash site with notes

The forced landing flightpath showing the drill site and helicopter wreckage. Photo: Australian Transport Safety Bureau.

“It was virtually certain that this lack of upper torso restraint use resulted in the pilot sustaining serious head injuries when the aircraft collided with the riverbed,” said ATSB director of transport safety, Dr Stuart Godley.

In Australia, vertical reference flying – when a pilot looks down as well as out to position the helicopter – mainly comprises aerial firefighting, and to a lesser extent, lifting operations.

During the ATSB investigation, it was identified that a notable proportion of pilots conducting vertical reference flying operations are likely not routinely wearing upper torso restraints.

“In the majority of helicopters used for vertical reference flying, the pilot often needs to be able to lean out to look below the helicopter to observe the line and load,” said Dr Godley.

“Standard upper torso restraints are likely not fit-for-purpose for these operations. This means, in the event of an accident, the restraints cannot provide the important defence to reduce the severity of injuries.

“Engineering innovations for these restraints could reduce the risk associated with this problem, which is particularly relevant in Australia during bushfire season when the frequency of vertical reference flying is elevated.”

During the examination of the wreckage at the site, the ATSB identified cracking and material loss visible in the exhaust diffuser area.

READ ALSO Narooma Mountain Bike Hub’s new contractor revealed in plan to create 100km trail network

The helicopter’s engine was sent to the manufacturer’s facilities in the US, where it underwent a teardown examination.

“This examination revealed extensive fatigue cracking in the exhaust diffuser inner struts, which supports the rear of the power turbine assembly,” said Dr Godley.

“When these fatigue cracks led the engine exhaust diffuser inner struts to fracture, this resulted in a complete loss of engine power.”

It was determined this high-cycle metal fatigue had not been detected for at least 34 daily, and two phased maintenance inspections prior to the accident.

Although the helicopter’s engine failed close to the cleared drilling area, the pilot did not have assurance that ground support personnel could vacate the drill site in an emergency.

The ATSB found that the documented risk assessment for the helicopter’s lifting operations at the drill site operations did not consider the hazard of an emergency landing.

“This increased the risk that ground personnel were not clear of the load pick-up area in the event an emergency landing was required,” said Dr Godley.

“In this accident, this lack of assurance led the pilot to conduct the forced landing to a less suitable location, increasing the severity of impact forces during the subsequent collision with terrain.”

Start the conversation

Daily Digest

Do you like to know what’s happening around your region? Every day the About Regional team packages up our most popular stories and sends them straight to your inbox for free. Sign-up now for trusted local news that will never be behind a paywall.

By submitting your email address you are agreeing to Region Group's terms and conditions and privacy policy.