I think that Capt Glenn is the only one that understood my point.
I agree with you CApt GLenn, as so far you climbed with 2 engines, so of course your gradient is much higher than the one of single engine. But do you know of how much higher? What would be the convergency from the 2 engines gradient to the single engine gradient?
At the engine failure "time" you were in a situation in which you are in CLMB Thrust ,and still in the second segment
Of course you would put max thrust but during a second you were in clmb thrust in the second segment of take off path
From a legal point of view is it okay? Not talking about aircraft capability.