A little further..
I was thinking about the effect of laoding Gs on the aircraft with increased AoA and then 2destroying the airflow over the wing by puting the stick sideway to turn the roll.
If i might, this would get the "inside" wing to loose its lift quiet dramatically with the change of its curvature (aileron up) when the need is for more camber to make sure dynamic the G-load isn't passed over?
Depending on tha mount of Gs this could cause adynamic stall on one wing only and the result is a spin methink.
At very high AoA i would personnaly try the rudder to get the wings around, depending on the qualities of the airframe it works on some aircrafts and looks safer.