Garmin Software Version 0534.15 Betriebsanweisung Seite 78

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Seitenansicht 77
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
190-00567-04 Rev. A
62
Abnormal Operation
Flight
InstrumentsEIS
Nav/Com/
XPDR/AudioAFCSGPS Nav
Flight
PlanningProcedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
AlertsAppendixIndex
UNUSUAL ATTITUDES
The PFD ‘declutters’ when the aircraft enters an unusual attitude. Only the primary
functions are displayed in these situations.
The following information is removed from the PFD (and corresponding softkeys
are disabled) when the aircraft experiences unusual attitudes:
• TrafcAnnunciations
• AFCSAnnunciations
• FlightdirectorCom-
mand Bars
• InsetMap
• Temperatures
• DMEInformation
Window
• WindData
• SelectedHeadingBox
• SelectedCourseBox
• TransponderStatus
Box
• SystemTime
• PFDSetupMenu
• Windowsdisplayedin
the lower right corner
of the PFD:
Timer/References
Nearest Airports
Flight Plan
Messages
Procedures
ADF/DME Tuning
• BarometricMinimum
Descent Altitude Box
• Glideslope,Glide-
path, and Vertical
Deviation Indicators
• AltimeterBarometric
Setting
• SelectedAltitude
• VNV Target Altitude
Extreme Pitch Indication
DEAD RECKONING
While in Enroute or Oceanic phase of flight, if the G1000 detects an invalid GPS
solution or is unable to calculate a GPS position, the system automatically reverts to
Dead Reckoning (DR) Mode. In DR Mode, the G1000 uses its last-known position
combined with continuously updated airspeed and heading data (when available) to
calculate and display the aircraft’s current estimated position.
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