As a new airbus driver I am wondering...
How the heck the stall warning sounded?
In the findings in the report:
"The triggering of the first stall warning in normal law, at an angle of attack
close to the theoretical angle of attack triggering the warning in landing
configuration, indicates that angle of attack sensor 3 was working at that
moment."
When you have 2 identical but false AOA values, the 3rd ADR is rejected by the voting principle even if correct, and now we have a stall warning from this probe?
My concern is that it sounded in normal law