190-00820-11 Rev. A
Pilot’s Guide for the Cirrus SR2x with Cirrus Perspective by Garmin
SY
STEM
O
VER
VIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO P
ANEL
& CNS
FLIGHT
MANA
GEMENT
HAZARD
AV
OID
ANCE
AFCS
ADDITIONAL
FEA
TURES
APPENDICES
INDEX
691
APPENDIX A
GARMIN AFCS ALERTS
The following annunciations (listed in order of increasing priority) can appear on the PFD between the
Airspeed and Attitude indicators. Only one annunciation may occur at a time, and messages are prioritized by
criticality.
Figure A-7 Garmin AFCS Status Annunciation
AFCS Status Annunciation
Alert Condition
Annunciation
Description
Rudder Mistrim Right
Yaw servo providing sustained force in the indicated direction
Rudder Mistrim Left
Aileron Mistrim Right
Roll servo providing sustained force in the indicated direction
Aileron Mistrim Left
Elevator Mistrim Down
Pitch servo providing sustained force in the indicated direction
Elevator Mistrim Up
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.
Pitch Trim Failure
If AP engaged, take control of the aircraft and disengage AP
If AP disengaged, move
MET
switch to unstick
Yaw Damper Failure
YD control failure
Roll Failure
Roll axis control failure; AP inoperative
Pitch Failure
Pitch axis control failure
System Failure
AP and MET are unavailable; FD may still be available
Preflight Test
Displayed during the preflight system test. Do not press the
AP DISC
Switch
during servo power-up and preflight system tests as this may cause the preflight
system test to fail or never to start (if servos fail their power-up tests). Power must
be cycled to the servos to remedy the situation.
Preflight system test failed; aural alert sounds at failure
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