Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
190-00600-02 Rev. A
49
Abnormal operation
Flight
Instruments
EICAS
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
If the system detects a failure in PFD1, reversionary mode is entered
automatically. Reversionary mode must be entered manually in the case of
PFD2 or MFD failure.
. In reversionary mode, critical flight instrumentation is
combined with engine instrumentation on the remaining display.
Manual activation of reversionary display mode is accomplished by pressing the
DISPLAY BACKUP
Button on the appropriate audio panel.
•
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 Cessna Citation Mustang Airplane Flight Manual (AFM) 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. 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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