Annunciations & Alerts
GFC 700 AFCS ALERTS
Condition
Annunciation Description
Pitch Failure
Roll Failure
Pitch Trim Axis
Control Failure
Yaw Damper
Failure
System Failure
Automatic
Descent Mode
Elevator Mistrim
Up
Elevator Mistrim
Down
Aileron Mistrim
Left
Aileron Mistrim
Right
Rudder Mistrim
Left
Rudder Mistrim
Right
Preflight Test
124
Cirrus Perspective
Pitch axis control failure.
Roll axis control failure.
If annunciated when AP is engaged, a failure has occurred in
the pitch trim system.
YD control failure (SR22 only).
AP and MET are unavailable. FD may still be available.
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.
A condition has developed causing the pitch servo to
provide a sustained force in the nose up direction.
A condition has developed causing the pitch servo to
provide a sustained force in the nose down direction.
A condition has developed causing the roll servo to provide
a sustained left force.
A condition has developed causing the roll servo to provide
a sustained right force.
A condition has developed causing the yaw servo to
provide a sustained force (SR22 only).
A condition has developed causing the yaw servo to provide a
sustained force (SR22 only).
Performing preflight system test.
Preflight system test has failed.
™
by Garmin – Cockpit Reference Guide for the SR20/SR22/SR22T
190-00821-09 Rev. A