Hi, i-2021, this is a very interesting case indeed! since fcom doesnt delve into this straight, its a good scenario to think..according to me FMA is:
MAN VS-XXX NAV
TOGA ALT
[LVR CLB]
you can compare to the case to mode reversion when you select a lower altitude when the aircraft climbs,or vice versa.
I may be wrong, but the FCOM + FCTM is not clear about this scenario.
I cant find the reference , where it says SRS remains engaged after GA acceleration altitude like in the takeoff scenario.
Last edited by EIU_EEC; 3rd Feb 2013 at 12:32.