190-00592-00 Rev. A
Garmin G1000 Pilot’s Guide for the Diamond DA40
1-12
SYSTEM OVERVIEW
REVERSIONARY MODE
Should a failure occur in either display, the G1000
automatically enters reversionary mode. In reversionary
mode, all important flight information is shown on the
remaining display. Figure 1-7 shows an example of G1000
reversionary mode where the PFD has failed.
If a display fails, the appropriate GIA 63-GDU 1040
Ethernet interface is cut off. Thus, the IAU can no longer
communicate with the remaining display (refer to Figure
1-1), and the NAV and COM functions provided to the
failed display by the IAU are flagged as invalid on the
remaining display. The system reverts to backup paths for
the AHRS, ADC, Engine/Airframe Unit, and transponder,
as required. The change to backup paths is completely
automated for all LRUs and no pilot action is required.
Figure 1-7 G1000 Reversionary Mode (Failed PFD)
NOTE:
The system alerts the pilot when backup
paths are utilized by the LRUs. Refer to the
Annunciations and Alerts section for further
information regarding these and other system
alerts.
If the system fails to detect a display problem,
reversionary mode may be manually activated by pressing
the Audio Panel’s red
DISPLAY BACKUP
button.
Pressing this button again deactivates reversionary mode.
Содержание G1000 Series
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