No big problem here, I roughly altered the thrust value which was stated as "rough" because I don't have an insight on the drag components on this bird (and those would be the ones to look at for a "fine" solution").

No big deal, talking about a fun product here but if CS goes for some changes in 1.1, I suggest to leave the thrust value were it is and go for some more drag to avoid those 500 knots climb phases.

Another one could be the rollout phase of the automated flight were the commanded heading is established fairly late because the (in my eyes) too soon reduction of the roll rate.