Originally Posted by Dozy
Therefore, if the pitch attitude is limited by AoA protection and the pitch-up moment from the increase in thrust is expected to exceed that attitude, then the systems will be correct in counteracting that tendency through the elevators.
If thrust alone is able to pitch up the airplane, why the system should waste such a potential when 2.5 deg are still to be grabbed ?
Can you prove that the extra 2.5 degrees of pitch would have avoided the crash?
No and I have no desire to, but I certainly can prove that preventing the aircraft from getting the available 2.5 deg of AoA made the crash inevitable.
We don't know what the CONF setting was for either.
What about you read the Habsheim report ... ?
You're getting some signs of confusion now. Maybe time to take a rest.