Garmin Software Version 0764.02 Guide de l'utilisateur Page 87

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Cirrus Perspective
by Garmin – Cockpit Reference Guide for the SR20/SR22
190-00821-02 Rev. A 71
Annunciations & Alerts
Flight
Instruments EIS
Nav/Com/
XPDR/Audio AFCS GPS Nav
Flight
Planning Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts Appendix Index
AFCS ALERTS
Condition Annunciation Description
Pitch Failure Pitch axis control failure.
Roll Failure Roll axis control failure.
Pitch Trim Axis
Control Failure
If annunciated when AP is engaged, a failure has occurred in
the pitch trim system.
Yaw Damper
Failure
YD control failure (SR22/SR22T only).
System Failure AP and MET are unavailable. FD may still be available.
Elevator Mistrim
Up
A condition has developed causing the pitch servo to
provide a sustained force in the nose up direction.
Elevator Mistrim
Down
A condition has developed causing the pitch servo to
provide a sustained force in the nose down direction.
Aileron Mistrim
Left
A condition has developed causing the roll servo to provide
a sustained left force.
Aileron Mistrim
Right
A condition has developed causing the roll servo to provide
a sustained right force.
Rudder Mistrim
Left
A condition has developed causing the yaw servo to
provide a sustained force (SR22/SR22T only).
Rudder Mistrim
Right
A condition has developed causing the yaw servo to provide a
sustained force (SR22/SR22T only).
Preflight Test Performing preflight system test. Upon completion of the
test, the aural alert will be heard.
Preflight system test has failed.
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