For engines
installed below the wing, applying maximum thrust can
create a strong nose up pitching moment, if speed is low.
For aircraft with engines mounted above the wings, thrust
application creates a helpful pitch down tendency.
From the EASA discussion doc link posted by BEagle ! Citation has engines mounted above the wings.
Nose down pitch control-Apply
Nose down pitch trim-As needed
• Reduce the angle of attack
• Some altitude loss may be
necessary
Again from the new recommendations but note the referance to some altitude loss may be necessary? Firstly how much is some? and how much reduction in AOA.
Having read the new recommendations I will write to the Examiners in question for an update on their recommendations regarding the document.
MadJock
Take your points regarding stabilised approach but consider wind shear?
multiple lapses in both flight monitoring and also flying
.
Isnt that the case in ANY inadvertant stall on a stabilised approach or infact any point of flight?
Pace