How did AIRBUS avoid the installation of a Shaker/Pusher?
This is why I made the comment I did regarding the aircraft being considered "un-stallable".
It was considered that the aircraft would prevent itself from stalling. The small detail omitted is that it only does this in Normal Law. Combined with the STALL audio warning (problem: it is silenced when the airspeed drops below 60 kts), this was considered sufficient protection.