Regardless of the question of whether GA should have been called earlier, it'd be great if I could get some clarification on another point that seems to be unconfirmed in this thread.
As I understood it, the Airbus FBW system when in Normal Mode will do its best to keep the wings as level as possible when the sidestick is centred. Does this extend to automatically correcting the roll effect of a reasonably hard rudder deflection or not?
Thanks in advance!