On 19 December 2010, a Raytheon 390 inbound to Samedan from Zagreb made a daylight approach to runway 21 at destination in marginal VMC which involved a steep and unstable descent from which a landing was not possible. The subsequent go around was followed by entry to a visual right hand circuit which was contrary to local procedures due to terrain constraints. Overbanking in the turn towards final approach was followed by a stall and loss of control which led to ground impact which, with the post crash fire, destroyed the aeroplane and fatally injured both occupants.
Description
On 19 December 2010, a Raytheon (Hawker Beechcraft) 390 being operated by German Air Taxi operator Windrose Air Jetcharter on a positioning flight from Zagreb to Samedan with just the two pilots on board cancelled Instrument Flight Rules (IFR) and made a daylight approach to runway 21 at destination in marginal Visual Meteorological Conditions (VMC) which involved a steep and evidently unstable descent from which a landing was not possible. The subsequent go around was followed by entry to a visual right hand circuit which was contrary to local procedures due to terrain constraints. Controlled flight was exited during an overbanked turn towards final approach and in the subsequent ground impact and fire, the aeroplane was destroyed and both occupants were fatally injured.
Investigation
An Investigation was carried out by the Aviation Division of the Swiss AIB. The Investigation was heavily dependent on the successful downloading of the NVM from the Terrain Avoidance and Warning System (TAWS) equipment since no Flight Data Recorder (FDR) was fitted (or required to be fitted) and the search for the 2 hour CVR was unsuccessful.
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