Originally Posted by
Latestormer
If a normal G/A scares a Capt to the point he quietly pushes the control column thinking 15° pitch is just too much, I'd pay tickets to watch his previous checkrides and carefully listen to what it's like flying with him.
I doubt that's the case here. The flight parameters show the pitch was stabilised at just under 15° during the initial go-around and stayed there for several seconds. The FO then started moving the control column aft. The Capt almost immediately opposed the rearward movement, presumably with sufficient force to desynchronise the control columns. At that point, the control column on the FO's side kept moving aft, while the control column on the Capt's side moved forward. The net result was an increase in the pitch attitude to 24°.
The question is: Having established the go-around attitude, why did the FO then start trying to raise the nose further?