Garmin Cirrus Perspective SR22T, Reference Manual

Page: 142 / 192

Cirrus Perspective ™ by Garmin – Cockpit Reference Guide for the SR20/SR22/SR22T
190-00821-09 Rev. A
124
Annunciations & Alerts
Flight
Instruments
EIS
Nav/Com/
XPDR/Audio
AFCS
GPS Nav
Flight
Planning
Pr
ocedur
es
Hazar
d
Avoidance
Additional
Featur
es
Abnormal Oper
ation
Annun/
Alerts
Appendix
Index
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.