A320
Good post and I assume by disconnecting 2 ADR's that put you in ALT2 Law as per AF447? Its concerning that the system allows full up trim on the THS to be achieved in a short time followed by a stall whilst then not allowing trim to unwind in time to enable a recovery.
I wonder how many manual turns of the trim wheel would be necessary to initiate a recovery and if the automations can be improved to assist in stall recovery?