Cockpit Reference Guide

Garmin G1000 Pilot’s Guide for the Piper PA-46 Meridian 190-00763-02 Rev. A 515
ADDITIONAL FEATURES
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EICAS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES INDEX
8.8 ABNORMAL OPERATION
SVS TROUBLESHOOTING
SVSisintendedtobeusedwithtraditionalattitude,heading,obstacle,terrain,andtrafc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 8-80 SVS Reversionary Mode