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Other factors

High gross weight and density altitude.


Increase in these means decrease in power Margin of max vs. Required to hover



Low indicated airspeed.


Below ETL, tail rotor required to produce nearly all directional control. Loss of thrust will cause right yaw.



Power droop. - rapid power application may cause transient power droop. Decrease in rotor RPM will cause corresponding t r thrust reduction. Additional left pedal required.


Lte defined

The occurrence of an uncommanded and Rapid right you're right which does not subside of its own accord and which, if not quickly reacted to can result in the loss of aircraft control. Thrust variations can usually be corrected with immediate additional left pedal. Correct And Timely pilot response.

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