go around flap retraction SOPs
Could any line pilots of heavy aircraft (Boeing / Airbus etc) please help with the following question?
What criteria is used to retract flap in a go-around, both normal ops and assymetric? For example, is flap selection based on airspeed, AoA, rate of climb, or some combination of the above?
This is to help me better instruct my budding airline pilot students in their C172's...
Cheers,. .O8