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
674
APPENDIX A
Annunciation Window Text
Alerts Window Text
Audio Alert
SLCT MAG
The system notifies the pilot to set the Nav Angle
units on the Avioncs Settings Screen to Magnetic.
Double Chime
SLCT NON-MAG
The system notifies the pilot to set the Nav Angle
units on the Avioncs Settings Screen to True.
Double Chime
START ENGAGED
Starter is engaged.
Double Chime
Optional / * Not applicable to all models /
TKS NH (optional) /
TKS FIKI (optional) /
1
In air only /
†
Garmin AFCS required
Table A-2 Caution Alerts
NOTE:
The ice protection system (optional) must be operated in accordance with the approved flight
manual limitations. This option is only available on SR22 and SR22T models.
Annunciation Window Text
Alerts Window Text
Audio Alert
ALTITUDE SEL
Climbing away from selected altitude.
None
ALTITUDE SEL
Descending away from selected altitude.
None
AOA FAIL
Dynamic stall speed band is not available.
None
ARE YOU ALERT?
†
Are you alert?
None
COURSE SEL
Current track will not intercept selected course.
None
FUEL IMBALANCE
Fuel quantity imbalance has been detected.
None
HIGH MP FF*
Avoid fuel flow 18 to 30 GPH and MP above 26”.
None
L FUEL QTY
Check left fuel tank level.
None
OXYGEN LEFT ON
Oxygen system is left on after shutdown.
Double Chime
OXYGEN QTY
Oxygen quantity is low.
None
PUMP BACKUP
Anti-ice backup pump mode has been selected (TKS).
None
R FUEL QTY
Check right fuel tank level.
None
Optional / * Not applicable to all models /
TKS FIKI (optional)/
†
Garmin AFCS required
Table A-3 Advisory Alerts
Comparator Window Text
Condition
ALT MISCOMP
Difference in altitude sensors is > 200 ft.
IAS MISCOMP
If both airspeed sensors detect < 35 knots, this is inhibited.
If either airspeed sensor detects > 35 knots, and the difference in sensors is > 10 kts.
If either airspeed sensor detects > 80 knots, and the difference in sensors is > 7 kts.
HDG MISCOMP
Difference in heading sensors is > 6 degrees.
PIT MISCOMP
Difference in pitch sensors is > 5 degrees.
ROL MISCOMP
Difference in roll sensors is > 6 degrees.
ALT NO COMP
No data from one or both altitude sensors.
IAS NO COMP
No data from one or both airspeed sensors.
HDG NO COMP
No data from one or both heading sensors.
PIT NO COMP
No data from one or both pitch sensors.
ROL NO COMP
No data from one or both roll sensors.
Table A-4 Comparator Alerts (Dual AHRS and/or Dual Air Data Computer installations only)