Garmin Software Version 0734.54 Podręcznik Użytkownika Strona 117

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Cockpit Reference Guide for the Prodigy
®
Flight Deck 100
190-00685-04 Rev. A 101
Abnormal Operation
Flight
Instruments EAS
Nav/Com/
XPDR/Audio AFCS GPS Nav
Flight
Planning Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts Appendix Index
inverse video (white text on red background) (B).
If an asymmetrical pitch trim
condition exists, the pointers turn yellow and the readout is displayed with a
Red “X”
(C).
Rudder
Mistrim
Aileron
Mistrim
A - Mistrim
C - Asymmetrical
Pitch Trim
Condition
B - Pitch Trim
Outside Takeoff
Configuration
REVERSIONARY MODE
If the system detects a failure in PFD1 or MFD, reversionary mode is entered
automatically. Reversionary mode must be entered manually in the case of
PFD2 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.
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.
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