Originally Posted by
HazelNuts39
How does airspeed affect the 'calculated maximum alpha', isn't alpha-max equal to 17.5 degrees?
Not sure - but AoA is a function of airspeed and pitch attitude, no?
I don't understand how an airplane can maintain a constant pitch attitude in essentially level flight while it decelerates from 140 kts to 112 kts,
To the best of my recollection, the pitch attitude was not constant.