This sounds like spectacularly bad design that manages to extract negative value from having two sensors. What is the logic behind this?
There is no good reason for only listening to one sensor.
There is a sort of good reason for having a split between pilot/copilot side: the instruments are redundant (both physically and electrically), so in the event of malfunction you can failover to the other side.
It just seems to be that this is some terrible engineering done on Boeing's end of not fully understanding the critical situation here.
Generally two failures: 1. a lack of redundancy in a mission critical sensor 2. a blind trust on MCAS's priority over pilots
There is redundancy in the sensors, but the sensors are not being used in a redundant manner. There are whispers that the 767 fuel tanker (KC-46/KC-767) has a system similar to MCAS that will look at both alpha vanes for disagreement, which is a bit damning to say the least.
a blind trust on MCAS's priority over pilots
The entire purpose of MCAS is to engage only when the pilot is flying to prevent the pilot from doing something dangerous. Previous generations of 737 had the same problem but the MAX is more delicate and compounds it with nacelles that generate lift.
Plus the bug with the resets on the limiter.