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4). 1. Instruments Response to Attitude or Power Changes. A factor influencing crosscheck technique is the characteristic manner in which instruments respond to changes of attitude or power. The control instruments provide direct and immediate indications of attitude or power changes. 2. Lag on Performance Instruments. Changes in the indications on the performance instruments will lag slightly behind changes of attitude or power. This lag is due to inertia of the aircraft and the operating principles and mechanisms of the performance instruments.

Power-Off Descent (Autorotation). If an emergency exists that requires the execution of an autorotation, enter smoothly by lowering the collective and closely cross-checking the control and performance instruments. Pay particular attention to keeping the helicopter in coordinated flight. Using the techniques described for constant airspeed descents will aid in flying the autorotation. Turns during autorotation are accomplished by using the same techniques as outlined in descending turns. If required, determine the angle of bank required by considering the time and altitude available to accomplish the turn.

2). Pitch changes are made by cyclic inputs to change the "pitch attitude" of the miniature aircraft or fuselage dot definite amounts in relation to the horizon. These changes are referred to as bar widths or fractions thereof, or degrees depending upon the type of attitude indicator. A bar width is approximately 2 degrees on most attitude indicators. The amount of deviation from the desired performance will determine the magnitude of the correction. 2. Bank Control. Bank changes are made by cyclic inputs to change the "bank attitude" or bank pointers definite amounts in relation to the bank scale.

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