Quote:
What could the autoflight have done to get this aircraft to so obviously be nibbling at aerodynamic STALL?
How's an a/c "nibbling at stall" supposed to do that 3000 ft climb?
Just before!
In NORMAL law
αsw = 23° (fixed value for all flight phases) In ALT & DIRECT Law
αsw = function of M and S/F config. S/F is not applicable, in this flight phase
αsw = function of M only.
αsw---- MACH
10.8°-- <= 0.28
9.9°--- <= 0.35
7.6°--- <= 0.53
5.2°--- <= 0.75
3.8°--- <= 0.866
-Inhibited M >0.866
-Inhibited on GND (if not in test)