Hi dozywannabe,
Good to read you back again and I agree with your post.
Additionally from the present A320 FCTM:
"The so-called "abnormal attitude" law is :
• Pitch alternate with load factor protection (without autotrim)
• Lateral direct law with yaw alternate
These laws trigger, when extreme values are reached:
• Pitch (50 ° up, 30 ° down)
• Bank (125 °)
• AOA (30 °, -10 °)
• Speed (440 kt, 60 kt)
• Mach (0.96, 0.1).
It is very unlikely that the aircraft will reach these attitudes, because fly-by-wire provides protection to ensure rapid reaction far in advance. This will minimize the effect and potential for such aerodynamic upsets.
The effectiveness of fly-by-wire architecture, and the existence of control laws, eliminate the need for upset recovery maneuvers to be trained on protected Airbus aircraft."
I think the last paragraph may have to be changed.