Pilot's Guide

Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT/GTi 190-00663-02 Rev. B 525
ADDITIONAL FEATURES
8.10 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 8-87 SVS Reversionary Mode