A320 Crossover Angle of attack
I have recently watched a video about the 737 where at medium angle of attacks (flaps 5 speed Vref+40) a complete deflection of the rudder will generate a more powerful roll moment than the ailerons can. This comes from the 737-300 PCU issues you may have heard about. Note this is an all engine operating case.
I am wondering if this exists on the 320 family as well ( assume it is a factor, but the flight control computers will prevent this in normal law) and if this can become an issue in Alternate / Direct law, and roughly what angle of attack this is.
If anyone has some good documents of the test flight results of the A320 family, there are some more things I'd like to know, for example the Mach no where control services can reverse.
Thanks in advance