Garmin G300 Pilot’s Guide
190-00921-00 Rev. E
Appendix E
255
System
Overview
Flight
Instruments
EIS
COM
Interface
GPS
Navigation
Flight
Planning
Hazar
d
Avoidance
Additional
Featur
es
Integr
ated
Autopilot
Annun/Alerts
Appendix
Index
REVERSIONARY MODE
In the event of a display failure, the G300 System automatically switches
to reversionary (backup) mode. In reversionary mode, all flight information is
presented on the remaining display in the same format as the split-screen system.
If a display failure occurs with the GDU 375, the
WX
and
XM
Pages will no
longer be available since the XM receiver resides in the GDU 375.
G300 Reversionary Mode (Failed PFD)
SYNTHETIC VISION TROUBLESHOOTING
Synthetic Vision is intended to be used with traditional attitude, heading,
obstacle, and terrain inputs (in most areas). Synthetic Vision is disabled
when valid attitude or heading data is not available for the display. In case
of invalid Synthetic Vision data, the PFD display reverts to the standard
blue-over-brown attitude display.
Synthetic Vision becomes disabled without the following data resources:
• Attitude data
• Heading data
• GPS position data
• Terrain data
• The position of the aircraft exceeds the range of the terrain database
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