Originally Posted by
IFMU
Are they planning to use the extra power? If so they may want strain gauge data on the tail rotor in flight at higher gross weights.
Thats a great question, which raises another question
that I haven’t seen addressed anywhere: how much more power can the current UH-60M drivetrain handle? And then there are airframe limits so can the power be used with an increased useful load?
Fltmech