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As the throttles are advanced beyond 65º in the flight range, there is a distinctive "torque bump"
when the TD system transitions to the temperature controlling mode, where TIT becomes a
function of throttle position.
If wind gusts are called, increase rotate, takeoff, approach, threshold, and touchdown speeds by
the full gust increment up to a maximum of 10 knots.
Since the C-130 does not have rudder pedal nose wheel steering, coordination is required during
both left and right seat takeoffs to assure that one pilot is controlling the yoke at all times during
the takeoff roll: