Originally Posted by OG
If you read Chris Scotts posting 1107 you will see that the discussion related to the 60kt validity limit not the maximum angle the vane could read so your remarks aren't really relevant to Chris's point.
And I question that 60kt validity limit.
Why CAS measurements should invalidate AoA values and shut down the stall warning ?
That aircraft was in an airflow of 100kt, ample airflow for the AoA probes to positively confirm the stall.
Just when the captain enters the flight deck, the stall warning quits. For him if stall there was, it is not anymore. His mental perception of the situation is send on erroneous tracks.
As Uplinker mentioned in his experiment, when you start thinking in one direction, it is hard to turn back.