As the crew were proceeding with another manual approach, they decided to go around again at a height of 220 meters (4 km before the runway) and initiated climb setting the engine to takeoff thrust. At a height of 900 m there was a simultaneous control column nose down input and stabilizer 5-degree nose down deflection, resulting in abrupt descent with negative vertical acceleration of -1g. The following crew actions to recover did not allow to avoid an impact with the ground. The impact occurred with a speed of over 600 km/h over 50 degrees nose down.
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