Garmin G1000 Reference Manual page 102

Additional Features
Roll Engagement
Roll Limit Indicators are displayed on the roll scale at 45° right and left, indicating
where ESP will engage. As roll attitude exceeds 45°, ESP will engage and the on-
side Roll Limit Indicator will move to 30°. The Roll Limit Indicator is now showing
where ESP will disengage as roll attitude decreases to within the desirable roll attitude
range.
Once engaged, ESP force will be applied between 30° and 75°. The force increases
as roll attitude increases and decreases as roll attitude decreases. The applied force
is intended to encourage pilot input that returns the airplane to a more normal roll
attitude. As roll attitude decreases, ESP will disengage at 30°.
ESP is automatically disengaged if the aircraft reaches the autopilot roll engagement
attitude limit of 75°.
Pitch Engagement
ESP engages at 20° nose-up and 17° nose-down. Once ESP is engaged, it will apply
opposing force between 15° and 50° nose-up and between 12° and 50° nose-down.
Maximum opposing force is applied between 25° and 50° nose-up and between 22°
and 50° nose-down.
The opposing force increases or decreases depending on the pitch angle and the
direction of pitch travel. This force is intended to encourage movement in the pitch
axis in the direction of the normal pitch attitude range for the aircraft.
There are no indications marking the pitch ESP engage and disengage limits in
these nose-up/nose-down conditions.
High Airspeed Protection
Exceeding Vmo or Mmo will result in ESP applying force to raise the nose of
the aircraft. When the high airspeed condition is remedied, ESP force is no longer
applied.
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Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
190-01344-00 Rev. B