Runway excursion following engine component failure and braking issues

No fatalities • Chinchilla Airport, Queensland

An aircraft veered off a narrow runway after an engine ECU failure and unexpected braking limitations led to a loss of directional control.

What happened

During a flight, the crew experienced an Electronic Control Unit (ECU) failure on the right engine. Following established operator procedures, the crew decided to proceed with the planned flight, noting that the pilot flying was experienced in managing such limitations. The crew was aware that the failure meant reverse thrust would be unavailable on the right engine, but they had developed a plan to manage this.

Upon arrival, the aircraft landed on a wet runway with a tailwind. The landing roll was longer than anticipated, which decreased the remaining runway available for stopping. During the rollout, the outer right tyre locked up, triggering the anti-skid system to release brake pressure on both outboard wheels. This left only the inboard wheels providing braking force, significantly reducing deceleration effectiveness.

As the crew focused on the urgent task of stopping the aircraft before the runway end, they missed a standard cockpit call that would have prompted the captain to use the tiller for directional control. Consequently, the aircraft drifted laterally. Due to the narrowness of the runway, the left landing gear eventually left the sealed surface. The crew did not realize a runway excursion had occurred until a post-landing inspection revealed mud on the tyres.

The investigation

The investigation examined the effectiveness of the operator's procedures regarding ECU failures. It was found that the procedures used to decide whether to continue the flight did not prompt the crew to consider other environmental variables, such as the impact of a wet runway, a tailwind, or the increased risk of asymmetric deceleration on a narrow runway.

Additionally, the investigation reviewed regulatory compliance regarding in-flight performance calculations. While regulations require crews to calculate landing performance based on current reports, the investigation noted that the guidance material regarding the transition from dry to wet runway conditions was not sufficiently clear. This ambiguity meant the requirement to discontinue an approach when a runway surface is unexpectedly wet was not explicitly understood.

Probable cause

The aircraft veered off the runway due to a combination of reduced braking effectiveness caused by an anti-skid activation and the crew's failure to transition to tiller steering, all occurring while managing the asymmetric thrust from an engine ECU failure.

Frequently asked questions

What happened in the 2022-05-23 De Havilland Canada/De Havilland Aircraft of Canada DHC-8-102 accident near Chinchilla Airport, Queensland?

An aircraft veered off a narrow runway after an engine ECU failure and unexpected braking limitations led to a loss of directional control.

Were there any fatalities in the 2022-05-23 De Havilland Canada/De Havilland Aircraft of Canada DHC-8-102 accident?

No fatalities were recorded in this accident.

What aircraft was involved and where did it happen?

The accident on 2022-05-23 involved a De Havilland Canada/De Havilland Aircraft of Canada DHC-8-102, registration VH-QQB, operated by SKYTRANS PTY LTD, at Chinchilla Airport, Queensland.

What was the probable cause of the accident?

The aircraft veered off the runway due to a combination of reduced braking effectiveness caused by an anti-skid activation and the crew's failure to transition to tiller steering, all occurring while managing the asymmetric thrust from an engine ECU failure.

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