Garmin Software Version 1983.00 User's Guide Page 90

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Garmin G1000 Cockpit Reference Guide for the Piper PA-44-180 Seminole
190-01462-01 Rev. A
72
Additional Features
Flight
InstrumentsEIS
Nav/Com/
XPDR/AudioAFCSGPS Nav
Flight
PlanningProcedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
AlertsAppendixIndex
The pilot can interrupt ESP by pressing and holding either the Control Wheel Steering
(CWS) or Autopilot Disconnect (AP/YD DISC TRIM INTRPT) switch. Upon releasing
the CWS or AP/YD DISC TRIM INTRPT switch, ESP force will again be applied,
provided aircraft attitude and/or airspeed are within their respective engagement limits.
ESP can also be overridden by overpowering the servo’s mechanical torque limit.
ESP is automatically enabled on system power up.
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.
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.
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.
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°
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