Vmca2 vs Vmco during missed approach
G'day all
I'll sum up the scenario before I ask my question.
At work we were discussing 2 engine out procedures on a particular aircraft and what the computers TOLD calculations are and FD guidance given during a missed approach. Basically the aircraft in question, upon hitting the TOGA button, will continue to descend the aircraft whilst accelerating towards Vmco. In the end this amounts to a large amount of height loss at a critical stage of an approach (assuming at DH or MAPT).
My question is, clearly the aircraft is at or above Vmca2 during the approach, so is there any reason why the aircraft can't apply max power, and as it accelerates away from Vmca2, raise the nose to a level attitude so the amount of height loss significantly decreases and then begin a slight ROC until it reaches Vmco? (long sentance).
There is clearly a reason why it doesn't do this and it is not due to the aircraft being limited in power (it has it in spades). So i'm stuck trying to figure out if there is any technical/aerodynamical/legal requirement that i'm missing.
Any thoughts?
Cheers,
Spaceman