Electronic Stability And Protection (Esp ) (Optional) - Garmin CIRRUS PERSPECTIVE SR22T Reference Manual

Additional Features
As the aircraft reaches 12,500 feet the system sets the AFCS to Altitude Hold
mode. The AFCS will also remain in Automatic Descent Mode as indicated by 'EDM'
continuing to be displayed as an AFCS Status Annunciation as well as the continuing
presence of the repeating chime. At this point, the AFCS must be disconnected to
cancel Automatic Descent Mode.
ELECTRONIC STABILITY AND PROTECTION (ESP
The pilot can interrupt ESP
(AP DISC) switch. Upon releasing the AP DISC switch, ESP
applied, provided aircraft roll attitude is within engagement limits. ESP
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
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
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
ESP is automatically disengaged if the aircraft reaches the autopilot roll engagement
™
attitude limit of 75°.
106
Cirrus Perspective
by pressing and holding the Autopilot Disconnect
™
:
™
force will be applied between 30° and 75°. The force increases
™
™
™ by Garmin – Cockpit Reference Guide for the SR20/SR22/SR22T
) (OPTIONAL)
™
™ will engage and the on-side
will disengage at 30°.
force will again be
™
can also be
™
190-00821-09 Rev. A