Garmin da42-l360 User Manual

Page of 102
Garmin G1000 Cockpit Reference Guide for the DA42-L360
190-01062-01 Rev. A
51
Abnormal Operation
Flight
Instruments
EIS
Nav/Com/
XPDR/Audio
AFCS
GPS Nav
Flight
Planning
Pr
ocedur
es
Hazar
d
Avoidance
Additional
Featur
es
Abnormal
Oper
ation
Annun/
Alerts
Appendix
Index
AbnOrmAl OperAtiOn
reversiOnArY mODe
Should a system detected failure occur in either display, the G1000 automatically 
enters  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 pressing the 
DISPLAY 
BACKUP
 Button on the audio panel.
 
NOTE: The Diamond DA42-L360 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.
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