rrr
If we can satisfy the required OEI climb gradient, and we suffer an engine failure then we raise the acceleration altitude to MSA or 1st published stop Altitude or level acceleration Alt (when published).
How well would that method work in the example procedure provided by aterpster?
MDA =
4580
First published altitude =
13,000
Would the company have us going all the way from 4580 to 13,000 in an approach climb configuration?
MSA =
15,500
And as JT noted, we probably shouldn't omit to take into account the time limit at GA thrust...
