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Cirrus Perspective
by Garmin – Cockpit Reference Guide for the SR20/SR22/SR22T
190-00821-08 Rev. A
118
Annunciations & Alerts
Flight
InstrumentsEIS
Nav/Com/
XPDR/AudioAFCSGPS Nav
Flight
PlanningProcedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
AlertsAppendixIndex
GFC 700 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 only).
System Failure AP and MET are unavailable. FD may still be available.
Automatic
Descent Mode
Displayed when the AFCS enters Automatic Descent
Mode as a result of the Hypoxia Recognition System
detecting pilot incapacitation. When this mode is active, a
continuous repeating chime is heard.
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 only).
Rudder Mistrim
Right
A condition has developed causing the yaw servo to provide a
sustained force (SR22 only).
Preflight Test Performing preflight system test.
Preflight system test has failed.
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