On Nov 19th 2013 the MAK reported that first read outs of the flight data recorder revealed that the crew did not follow the standard approach profile, went around due to considering the approach as unstable (attitude not within stable approach parameters), the engine thrust levers were moved to TOGA and the autopilot disconnected, the aircraft was under manual control for the remainder of the flight. While the engines accelerated to near takeoff thrust, the flaps were reduced from 30 to 15 degrees, the gear was retracted and the aircraft pitched up to about 25 degrees nose up, the indicated airspeed began to decay. Only after the airspeed had decreased from about 150 KIAS to 125 KIAS the crew began to issue control inputs to counter the nose up, the climb was stopped while the nose was lowered by control inputs. The aircraft reached a maximum height of 700 meters (2300 feet and began to rapidly descend until the aircraft impacted ground at a nose down attitude of 75 degrees at a speed of 450 kph (242 knots) about 20 seconds after reaching the maximum height of 700 meters. The engines were operating nominally until impact, the flight data recorders did not reveal any system malfunction. The cockpit voice recorder was not found inside its container, the assembly is missing and a search is under way.
