Please can I clarify this to my own satisfaction. Airbus person.
My understanding is that this 'gotcha' of inreasing thrust after a V1 cut is only applicable to a derate take off (Boeing) as opposed to a flex thrust (assumed temp) take off (Airbus) - a generality I know. Am I correct?
My concern is operating to increased/improved V2 on a wet r/w when close in obstacle limited as has been debated before on this forum.
Regards
mcdhu