
Garmin G1000 Cockpit Reference Guide for the Diamond DA62
190-01896-00 Rev. A
84
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ELECTRONIC STABILITY AND PROTECTION (GARMIN ESP
™
) (OPTIONAL)
NOTE: Refer to the Airplane Flight Manual to determine approval of Garmin
ESP functionality.
The pilot can interrupt ESP by pressing and holding the Autopilot Disconnect (AP
DISC) switch. Upon releasing the or AP DISC switch, ESP force will again be applied,
provided aircraft roll attitude is within engagement limits. ESP can also be overridden
by overpowering the servo’s mechanical torque limit.
ESP can be enabled or disabled on the AUX-SYSTEM SETUP 2 Page on the MFD.
To enable or disable ESP:
1) Turn the large
FMS
Knob to select the AUX Page Group.
2) Turn the small
FMS
Knob to select the System Setup Page.
3) If necessary, select the
SETUP 2
Softkey to display the AUX-SYSTEM SETUP 2
Page. If the AUX-SYSTEM SETUP 2 is already displayed, proceed to step 4.
4) Press the
FMS
Knob to activate the cursor.
5) Turn the large
FMS
Knob to place the cursor in the STABILITY & PROTECTION
field.
6) Turn the small
FMS
Knob to select ‘ENABLE’ or ‘DISABLE’.
7) Press the
FMS
Knob to remove the cursor.
ESP is automatically enabled on system power up.
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°.
Pitch Engagement
ESP engages at 16° nose-up and 22° nose-down. Once ESP is engaged, it will apply
increasing opposing force between 16° and 20° nose-up and between 22° and 25° nose-
down. Maximum opposing force is applied between 20° and 50° nose-up and between
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