
Garmin G1000 Cockpit Reference Guide for the Quest KODIAK 100
190-00645-05 Rev. A 61
Abnormal Operation
Flight
Instruments EIS
Nav/Com/
XPDR/Audio GPS Nav
Flight
Planning Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation Annun/Alerts Appendix Index
ABNORMAL OPERATION
REVERSIONARY MODE
In reversionary mode, critical flight instrumentation is combined with engine
instrumentation on the remaining display.
Reversionary display mode can be manually activated by the pilot.
• 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 Quest KODIAK 100 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
(121.500MHz) is automaticallyloadedinto theactivefrequencyeld oftheCOM
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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