CL60, Almaty Kazakstan, 2007

CL60, Almaty Kazakstan, 2007

Summary

On 26 December 2007, the crew of a Bombardier Challenger 604 which had received a 2-stage ground de/anti icing treatment lost roll control as the aircraft got airborne from a snow-covered runway at Almaty in freezing mist and light snow conditions and it crashed within the airport perimeter before continuing through the perimeter fence and catching fire. The Investigation concluded that the loss of control was probably caused by contamination of the wing leading edge with frozen deposits during the take off roll as a result of the crew's decision not to select wing anti-ice on contrary to applicable procedures.

Description

On 26 December 2007, a Bombardier CL 604 Challenger (D-ARWE) being operated by the German Company JetConnection BusinessFlight on a private charter flight from Almaty to Macau took off at night into icing conditions from a 4398 metres long runway which was covered by dry snow and roll control was lost just after beginning rotation. The aircraft wing tip impacted the runway surface and the aircraft subsequently crashed through the perimeter fence, the fuselage broke into three pieces and a fire started. The co pilot was killed and the other three occupants -two crew members and one passenger - sustained serious injuries.

Investigation

An Investigation was conducted by the Interstate Aviation Committee with assistance from the accident investigation agencies of the State of the Operator and the State of the Manufacturer. Flight Data Recorder (FDR) and Cockpit Voice Recorder (CVR) data were recovered.

The co-pilot had been assigned PF duties. It was established that ground de/anti icing with Type II fluid had been completed in accordance with normal procedures and that the aircraft commander had decided that Wing Anti Ice (WAI) should only be selected ‘on’ after take off. However, the Aircraft Flight Manual (AFM) stipulates that in the conditions prevailing for the take off, the wing anti-ice (WAI) system must be ‘on’ but that when Type II, III or IV anti-icing fluids have been applied, the WAI must only be selected ‘on’ just prior to thrust increase for takeoff.

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