and we suffer an engine failure then we raise the acceleration altitude to MSA
We maintain that configuration until the missed approach altitude is reached where we level off and clean up to hold or enroute speeds
That gets us out of the configuration change/gradient problem. However, given that thrust for GA generally is the same as/similar to TO, do we give any concern to time limits at GA thrust ?
Also if a turn is required we must allow for 0.9%.
Good (although a tad higher than I might have expected) but how do we account for turn radius/terrain ?