I am trying to figure out single engine configuration of Bell helicopter if one engine is to shut down. The helicopter was flying in following conditions :-
Weight - 10606 pounds
Altitude - 7000 feet pressure altitude
Temperature - 34 degree Celsius
Air Speed - 70 KIAS
According to the OEI performance graph of 11000 weight category given in Rotorcraft Flight Manual the Bell helicopter will get a rate of descend of 370 feet per minute.
My query is that if pilot is flying the helicopter in weight confi