Pilot’s Guide for the Cirrus SR2x with Cirrus Perspective by Garmin
190-00820-11 Rev. A
664
ADDITIONAL FEATURES
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
8.17 ABNORMAL OPERATION
SVT TROUBLESHOOTING
SVT is intended to be used with traditional attitude, heading, obstacle, terrain, and traffic inputs. SVT is
disabled when valid attitude or heading data is not available for the display. In case of invalid SVT data, the
PFD display reverts to the standard blue-over-brown attitude display.
SVT becomes disabled without the following data resources:
• Attitude data
• Heading data
• GPS position data
• 9 Arc-second Terrain data
• Obstacle data
• TAWS-B function is not available, in test mode, or failed
• The position of the aircraft exceeds the range of the terrain database.
REVERSIONARY MODE
SVT can be displayed on the Multifunction Display (MFD) in Reversionary Mode. If it is enabled when switching
to Reversionary Mode, SVT will take up to 30 seconds to be displayed. The standard, non-SVT PFD display will
be shown in the interim.
Figure 8-140 SVT Reversionary Mode
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