Originally Posted by
Rananim
FCC controls both STS and AP stab trim and it gets CAS,AoA,IVSI from ADIRU as well as engine N1 from DEU and flap position from FSEU.
In the NG the Elevator Feel System has its own pitots to determine airspeed and might be sensing very different data than the ADIRU. If the same is true on the MAX, could it be an additional source of confusion that the pilots might experience a combination of trim behaviour and yoke forces that they would not normally encounter?