Garmin Beechcraft 200 Series, Cockpit Reference Manual

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Garmin G1000 NXi Cockpit Reference Guide for the Beechcraft 200/B200 Series 190-02040-01 Rev. B 171
Flight
Instruments
EIS
Nav/Com/
XPDR/Audio
Flight
Management
Hazar
d
Avoidance
AFCS
Additional
Featur
es
Abnormal
Oper
ation
Annun/Alerts
Appendix
Index
Abnormal Operation
ABNORMAL OPERATION
REVERSIONARY MODE
NOTE:
The system alerts the pilot when backup paths are utilized by the LRUs.
Refer to the Appendices for further information regarding system-specific
alerts.
In the event of a display failure, the system can be manually switched to reversionary
(backup) mode (all remaining displays enter reversionary mode). In reversionary mode,
all important flight information is presented on the remaining display(s) in the same
format as in normal operating mode.
When a display fails, the system automatically switches to reversionary (backup) mode
as follows:
•
PFD1 failure
– MFD and PFD2 remain in normal mode.
•
MFD failure
– PFD1 automatically switches to reversionary mode.
•
PFD2 failure
– MFD and PFD1 remain in normal mode.
Reversionary mode can be activated manually by pressing the dedicated
DISPLAY
BACKUP
button at the bottom of the audio panel. Pressing this button again deactivates
reversionary mode.
Each display can be configured to operate in reversionary mode, as follows:
•
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.
COM TUNING FAILURE
In case of a COM system tuning failure, the emergency frequency (121.500 MHz) is
automatically tuned in the radio in which the tuning failure occurred.
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