Originally Posted by
SteinarN
Anyway, what my calculations was suggesting is that without MCAS the stick force is not only increasing as it should, when going from say 10 to 14 degrees AOA, but that the stick force needs to be relaxed towards zero force and the stick position needs to be brought to near neutral position when going from say 10 to 14 degrees AOA.
Not sure whether I got it correctlyn but if the stick force goes to zero and the yoke has to be brought to neutral when approaching say 14 degrees AOA, then the aircraft can't be qualified as stable.
If so the public will never be willing to board the airplane again.