Garmin CIRRUS PERSPECTIVE TOUCH+ - COMPARATOR ANNUNCIATIONS

Cockpit Reference Guide for the Cirrus SR2x with Perspective Touch+ by Garmin
190-02954-01 Rev. A 197
Annunciations & Alerts
Flight
Instruments EIS
Nav/Com/
XPDR/Audio
Flight
Management
Hazard
Avoidance AFCS
Additional
Features Annun/Alerts Appendix Index
Flight
Instruments EAS
Audio and
CNS
Flight
Management
Hazard
Avoidance AFCS
Additional
Features
Abnormal
Operation Annun/Alerts Appendix Index
Crew Profile Import/
Export Results
Description
‘Overwrite existing profile?’ Displayed if the profile name matches the name of existing
profile.
‘Profile name invalid. Enter a
different profile name.’
Displayed if the profile name is invalid.
‘All available crew profiles in
use. Delete a profile before
importing another.’
Displayed if the maximum number for crew profiles has been
reached.
‘Crew profile import failed.’ Displayed if the importing operation fails for any other reason.
‘Crew profile import
succeeded.’
Displayed if the importing operation succeeds.
‘Overwrite existing file?’ Displayed if the filename matches the name of an existing file
on the SD card.
‘Crew profile export failed.’ Displayed if the export operation fails.
‘Crew profile export
succeeded.’
Displayed if the export operation succeeds.
Crew Profile Import/Export Messages
COMPARATOR ANNUNCIATIONS
The Comparator monitors critical values generated by redundant sensors. If differences in
the sensors exceed a specified amount, a comparator annunciation is displayed in black text
on a amber background. If one or both of the sensed values are unavailable, the comparator
annunciation is black text on a white background. The following is a list of the possible an-
nunciations:
Comparator
Annunciation
Condition
A LT
Difference in altitude sensors is > 200 ft.
IAS
If both airspeed sensors detect < 35 knots, this is inhibited.
If either airspeed sensor detects > 35 knots, and the difference in sensors is ≥ 10
knots.
If either airspeed sensor detects > 80 knots, and the difference in sensors is ≥ 7
knots.
HDG
Difference in heading sensors is > 6 degrees.
PIT
Difference in pitch sensors is > 5 degrees.