The timing of applying full rudder is critical. If instigated too soon it results in a
wingover. If instigated too late the plane will fall into a
sideslip or else enter a
tailslide which most aircraft are restricted from doing. Performing the pivot requires sufficient airflow over the rudder. In planes with a suitably-positioned propeller, the
propwash may provide this. Otherwise, rudder must be applied sooner while the plane still has forward airspeed. This maneuver demands there be no rolling at all but when airflow is minimal ailerons become ineffective. So as soon as the yaw is established reduce throttle to prevent the aircraft from
rolling due to engine
torque. Do not open the throttle again until the dive when sufficient airspeed has been gained for aileron control. Reduced throttle will also prevent
gyroscopic precession from pitching the nose up. Higher lift from the faster moving outside right wing will roll the airplane to the left. To maintain attitude in addition to left rudder, holding forward right stick necessary throughout the pivot. Depending on the direction of the turn, the opposite may apply. ==SAR reversal==