Garmin DA40F GPS Receiver User Manual


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Garmin G1000 Pilot’s Guide for the Diamond DA40/40F
190-00592-06 Rev A474
ADDITIONAL FEATURES
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICESINDEX
8.9 ABNORMAL OPERATION
SVS TROUBLESHOOTING
SVS is intended to be used with traditional attitude, heading, obstacle, terrain, and traffic inputs. SVS is
disabled when valid attitude or heading data is not available for the display. In case of invalid SVS data, the PFD
display reverts to the standard blue-over-brown attitude display.
SVS becomes disabled without the following data resources:
•Attitudedata
•Headingdata
•GPSpositiondata
•9Arc-secondTerraindata
•Obstacledata
•TAWSfunctionisnotavailable,intestmode,orfailed
•Thepositionoftheaircraftexceedstherangeoftheterraindatabase.
REVERSIONARY MODE
SVS can be displayed on the Multifunction Display (MFD) in Reversionary Mode. If it is enabled when switching
to Reversionary Mode, SVS will take up to 30 seconds to be displayed. The standard, non-SVS PFD display will
be shown in the interim.
Figure 8-81 SVS Reversionary Mode
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