Originally Posted by
FCeng84
737MAX elevator feel system pressure is a function of stabilizer position, impact pressure, and AOA. The AOA dependency provides increased feel stiffness when AOA is near stall AOA. This has been added to provide one of the characteristics associated with stall identification "nose down pitch that cannot be readily arrested".
Thanks, same question as sp, also, does that not describe MCAS also, or is this in addition to MCAS?