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Garmin G1000 Cockpit Reference Guide for the Piper PA32
SECTION 11 – ABNORMAL
OPERATION
11-1
SECTION 11: ABNORMAL
OPERATION
11.1 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. Minimal navigation capability is available on the
Reversionary Mode display.
Normal PFD Display
MFD in Reversionary Mode
Normal MFD Display
Figure 11-1 G1000 Reversionary Mode: Failed PFD
11.2 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 dual display failure, the emergency frequency (121.500
MHz) automatically becomes the active frequency to the
pilot through the pilot headset.
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