Originally Posted by CONF iture
Don't forget that this procedure is new from December 2010 and therefore was not in force at the time of AF447.
You are correct on that one. The old procedure called for the pilots to power himself out of the stall with minimal altitude loss. Nose down and power reduction were only to be used in a Note, if method one did not work.
So in this pilot's mind, both Unreliable Airspeed Drill and and Stall Recovery procedures would require power.
UAS would need nose up 5 degrees with CLB power while the stall recovery would require to maintain approximate pitch and TO/GA.