Gfc 700 Afcs Alerts - Garmin Cirrus Perspective SR20 Cockpit Reference Manual

Garmin integrated avionics system reference guide
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gFC 700 aFCs alerts

Condition
Annunciation Description
Pitch Failure
Roll Failure
Pitch Trim Axis
Control Failure
Yaw Damper
Failure
System Failure
Elevator Mistrim
Up
Elevator Mistrim
Down
Aileron Mistrim
Left
Aileron Mistrim
Right
Rudder Mistrim
Left
Rudder Mistrim
Right
Preflight Test
190-00821-03 Rev. A
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.
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. Upon completion of the
test, the aural alert will be heard.
Preflight system test has failed.
®
by Garmin – Cockpit Reference Guide for the SR20/SR22
annunciations & alerts
73

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