Emergency landing for Pilatus PC-24 following flight control failure

Casualties unknown • Kelowna, British Columbia, CA

A privately operated Pilatus PC-24 was forced to declare an emergency and land in Kelowna, British Columbia, after experiencing a flight control malfunction during flight.

What happened

On 03 November 2023, a Pilatus PC-24, operated by Mark Anthony Group Inc., was en route from Vancouver International Airport to Kelowna Airport. While climbing toward its cruising altitude, the crew identified a malfunction within the aircraft's flight controls. In response to the issue, the crew contacted NAV CANADA’s Vancouver Control Centre to declare an emergency and requested that aircraft rescue and firefighting services be positioned at Kelowna Airport for their arrival.

The aircraft subsequently completed its flight and landed at the destination without further incident.

The investigation

Following the landing, maintenance personnel performed an initial inspection of the aircraft, which is registered as C-XXXX (Note: Source did not provide specific registration, only operator). The inspection revealed that the rudder mass balance weight arm had suffered a break, a failure that restricted the full range of motion for the rudder. Additionally, investigators found that the control rods for the rudder trim tab had disconnected from the rudder trim actuator.

Probable cause

The mechanical failure of the rudder mass balance weight arm and the subsequent separation of the rudder trim tab control rods from the actuator caused a flight control malfunction.

Frequently asked questions

What happened in the 2023-11-03 Pilatus PC-24, C-FMHR accident near Kelowna, British Columbia, CA?

A privately operated Pilatus PC-24 was forced to declare an emergency and land in Kelowna, British Columbia, after experiencing a flight control malfunction during flight.

What aircraft was involved and where did it happen?

The accident on 2023-11-03 involved a Pilatus PC-24, C-FMHR, operated by Mark Anthony Group Inc., at Kelowna, British Columbia, CA.

What was the probable cause of the accident?

The mechanical failure of the rudder mass balance weight arm and the subsequent separation of the rudder trim tab control rods from the actuator caused a flight control malfunction.

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