Structural failure and terrain impact in Bulman region

Casualties unknown • 237 km east-north-east of Katherine, Northern Territory

An aircraft experienced a right wing separation following exposure to severe thunderstorm activity and turbulence in the Bulman region.

What happened

While operating in the Bulman region, the aircraft encountered intense convective activity stemming from a rapidly developing thunderstorm. This weather system subjected the aircraft to significant turbulence and a marked reduction in visibility. During this period of severe weather, the aircraft experienced excessive structural loading, which resulted in the in-flight separation of the right wing from the fuselage. Following this structural failure, the aircraft collided with the terrain.

The investigation

Investigators examined the circumstances surrounding the encounter with the thunderstorm. The analysis focused on the interaction between the atmospheric conditions and the aircraft's flight parameters. The investigation looked into how the combination of environmental turbulence, the aircraft's airspeed relative to its manoeuvring speed, and specific control inputs contributed to the structural failure of the airframe.

Probable cause

The aircraft likely suffered structural failure due to excessive loading caused by a combination of thunderstorm-induced turbulence, airspeed exceeding manoeuvring limits, and specific control inputs.

Frequently asked questions

What happened in the 2022-12-24 Cessna Aircraft Company 210N accident near 237 km east-north-east of Katherine, Northern Territory?

An aircraft experienced a right wing separation following exposure to severe thunderstorm activity and turbulence in the Bulman region.

What aircraft was involved and where did it happen?

The accident on 2022-12-24 involved a Cessna Aircraft Company 210N, registration VH-TFT, operated by KATHERINE AVIATION PTY LTD, at 237 km east-north-east of Katherine, Northern Territory.

What was the probable cause of the accident?

The aircraft likely suffered structural failure due to excessive loading caused by a combination of thunderstorm-induced turbulence, airspeed exceeding manoeuvring limits, and specific control inputs.

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