Garmin Software Version 0720.05 Guia do Utilizador Página 71

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Garmin G1000 Cockpit Reference Guide for the Piper PA-46 Meridian
190-00764-01 Rev. A
55
Abnormal Operation
Flight
Instruments EICAS
Nav/Com/
XPDR/Audio AFCS GPS Nav
Flight
Planning Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts Appendix Index
ABNORMAL OPERATION
REVERSIONARY MODE
If the system detects an MFD failure, reversionary mode is entered automatically.
Reversionary mode must be entered manually in the case of a PFD failure. In reversionary
mode, critical flight instrumentation is combined with engine instrumentation on the
remaining display.
Manual activation of reversionary display mode is accomplished by pressing the
DISPLAY BACKUP Button on the appropriate audio panel.
• PFD1 – By pressing the DISPLAY BACKUP Button on the left audio panel.
MFD – By pressing the DISPLAY BACKUP Button on the left or the right
audio panel.
PFD2 – By pressing the DISPLAY BACKUP Button on the right audio
panel.
NOTE: The Piper PA-46 Meridian Pilot’s Operating Handbook (POH) always
takes precedence over the information found in this section.
ABNORMAL COM OPERATION
When a COM tuning failure is detected by the system, the emergency frequency
(121.500 MHz) is automatically loaded into the active frequency field of the COM
radio for which the tuning failure was detected. In the event of a failure of both PFDs,
the emergency frequency (121.500 MHz) automatically becomes the active frequency
on both COM radios.
HAZARD DISPLAYS WITH LOSS OF GPS POSITION
If GPS position is lost, or becomes invalid, selected hazards being displayed on the
Navigation Map Page are removed until GPS position is again established.
Loss of Hazard Functions with Loss of GPS
Position
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