Modern flight training has moved to stall recognition and recovery because if the airplane doesn't stall it can't spin. If it does stall and proper stall recovery techniques will ensure yaw is prevented and again a spin can't occur.
Sanctimonious claptrap!
Stupid 3 times? No. Just stupid once.
It is exceeding the critical angle of attack that stalls the aerofoil, or part of it. That can happen at any speed.
Attempting a manoeuvre that stalls part of a wing causes an upset that may develop into a spin if incorrect control inputs are then applied or maintained.
Your proposed logic does not cover the full range of the flight envelope because after the pilot has tried "unstall" and "correct yaw" they have nothing else left in the tool box.