The aircraft would be just fine if it did not [b=left]need[/b] to comply a "feel" requirement that would almost never be experienced by all crews ever.=left
To follow your argument to its natural conclusion, you appear to be advocating removal of the FAR 25/ CS 25 requirements for stick force gradient. The aircraft was clearly not fine before installation of MCAS or the FAA test pilots would simply have accepted it as presented. If inadequate stick force gradient in any part of the envelope - however likely the encounter - is OK for the MAX, does that make it OK for every aircraft?