Originally Posted by
ASH26E
I wonder what the FAA and EASA will make of the recent Lion Air 737 Max event resulting from the failure of a single AoA sensor in the light of 25.901(c)
I think that is already known. They consider that if the actions for a stab trim runaway had been taken there would have been no problem, just switch off the stab trim with the switches provided
for just that purpose. Therefore, more than a single failure was required,