So the trims all are there to relieve load on flying the aircraft. One would think that if the load is so great he would have reach down and put in the opposite load on the ruddef trim. This would relieve the load on his leg.
lets face some facts here and now. Learn from this so it dont happens to yourself.
he has **** up pure and simple.
A small error in not setting the trim has taken them all out. Over thinking whats going on rather than fly it out and then get on top has caused this accident.
There is no yaw control from the aircraft because it is doing it all right as in both engines were making power.
As for the CVR it all came about in this class of aircraft because of anotherB200 accident in FNQ when a flight between miners cause an aft CofG causeing a complete loss of control of the aircraft. That cause the cao to fit Cvr,s. The have no data inputs only voice mic and inputs from tghe audio pannel.
Mmm 2000rpm and not 1746 rpm well ill be !