Pilot's Guide

Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT/GTi 190-00663-02 Rev. B 519
ADDITIONAL FEATURES
Once engaged, ESP
™
force will be applied between 30° and 75°,asillustratedinFigure8-81.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°.
Figure 8-81 ESP Roll Operating Range When Engaged
(Force Increases as Roll Increases & Decreases as Roll Decreases)
0º
10º
10º
20º
20º
30º
30º
45º
45º
60º
60º
75º
75º
90º
90º
ESP
™
is automatically disengaged if the aircraft reaches the autopilot roll engagement attitude limit of 75°
(Figure8-82).
Figure 8-82 Roll Attitude Autopilot Engagement Limit (ESP Engaged)
ESP Upper Disengage Limit (75°)
Aircraft Roll Attitude = 74°
PITCH ENGAGEMENT
ESP
™
engages at 17° nose-up and 15° nose-down. Once ESP
™
is engaged, it will apply increasing opposing
force between 17° and 20° nose-up and between 15°and18°nose-down,asindicatedinFigure8-83.Maximum
opposing force is applied between 20° and 50°nose-upandbetween18° and 50° nose-down. ESP
™
disengages
when 50° is exceeded in a nose-up or nose-down attitude.