A320 Engine Failure After V1
In the FCTM there is a Note which states as follows:
" If the decision has been taken to delay the acceleration, the flight crew must not delay the engine out maximum acceleration altitude. ( The engine out maximum acceleration altitude corresponds to the maximum altitude that can be achieved with one engine out and the other engine operating at takeoff thrust for a maximum of 10 minutes).
My query is this: Isn't the time limit 0f 10 minutes only for TOGA thrust? Why is it mentioned as "takeoff' thrust as it will then include Flex thrust also?
Last edited by Boyington; 2nd Jun 2018 at 15:25.