Is there an airspeed input component to MCAS ?
http://www.b737.org.uk/mcas.htm this mentions “at airspeed approaching stall”
I wondered because we know there was likely an UAS situation for ET, so potentially a pitot hardware issue.
If AoA was all that MCAS received , then we’d be looking at possible alpha vane failure as well, therefore we’d have hardware issues with two separate components.
So - could a blocked pitot be another single point of failure? And the AoA was fine?....