Garmin G1000 Pilot’s Guide for the Diamond DA42NG
190-00962-02 Rev. A558
ADDITIONAL FEATURES
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICESINDEX
Once engaged, ESP
™
force will be applied between 30° and 75°,asillustratedinFigure8-100.Theforce
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
™
willdisengageat30°.
Figure 8-100 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°
(Figure8-101).
Figure 8-101 Roll Attitude Autopilot Engagement Limit (ESP Engaged)
ESP Upper Disengage Limit (75°)
Aircraft Roll Attitude = 74°
PITCH ENGAGEMENT
ESP
™
engages at 15°nose-upand18° nose-down. Once ESP
™
is engaged, it will apply increasing opposing
force between 15° and 20° nose-up and between 18° and 23° nose-down, as indicated in Figure 8-102.
Maximumopposingforceisappliedbetween20° and 50° nose-up and between 23° and 50° nose-down. ESP
™
disengages when 50° is exceeded in a nose-up or nose-down attitude.
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