Pilot’s Guide for the Cirrus SR2x with Cirrus Perspective by Garmin
190-00820-11 Rev. A
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
670
APPENDIX A
•
Audio Alerting System:
The system issues audio alert tones when specific system conditions are met. See
the Alert Level Definitions Section for more information. The annunciation tone may be tested from the AUX
- System Status Page.
Testing the system annunciation tone:
1)
Use the
FMS
Knob to select the AUX - System Status Page.
2)
Select the
ANN TEST
Softkey.
Or
:
a)
Press the
MENU
Key.
b)
Highlight ‘Enable Annunciator Test Mode’ and press the
ENT
Key.
Figure A-2 Annunciation Tone Testing
(AUX-System Status Page)
Press to Test Annunciation Tone
•
Comparator Window (Dual AHRS and/or Dual Air Data Computer installations only):
Critical
values generated by redundant sensors are monitored by comparators. If differences in the sensors exceed a
specified amount, the Comparator Window appears in the upper right corner of the PFD and the discrepancy
is annunciated in the Comparator Window as a ‘MISCOMP’ (miscompare). If one or both of the sensed values
are unavailable, it will be annunciated as a ‘NO COMP’ (no compare).
Figure A-3 Comparator Window
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