"At 15.22:51 (6 seconds after initiating Go Around) engine power reached 83% N1. By 15.23:11 pitch angle increased to more than 25 degrees, and the first "push" movement of the yoke was registered. At that moment airplane was at 2000', climbing 4000'/min. During next 5 seconds pitch decreased from 25 degrees to nearly normal horizontal flight condition and continued to decrease. Plane stopped climbing at 2300'. G-force = 0,5g. At 15.23:16 the second "push" movement of the yoke was registered. As a result of it, pitch changed to -20 degrees, speed to -5000'/min, G-force =0g, speed 140 kt, increasing 10kt/s. At 15.23:21 the third "push" movement of the yoke was registered. As a result of it, G-force changed to -0.9g, pitch angle to -60 degrees. At 15.23:28 airplane collided with the ground close to runway with an airspeed 245kt and pitch angle -75 degrees."
17.11.2013, Tatarstan 363, Kazan.