Garmin G500 Manuel - Page 24

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Garmin G500 Manuel

Section 3. EMERGENCY PROCEDURES

3.1

Emergency Procedures

3.1.1 PFD 1 Failure
PFD 1 failure is indicated by the loss of displayed information on the PFD,
including blank, frozen, or unresponsive display.
1.
Use standby flight instruments for attitude, airspeed, altitude, and
heading reference.
2.
Refer directly to navigation source for navigation information (such as
GPS).
If autopilot is engaged:
3.
Verify autopilot mode and cross check against standby flight and
navigation data.
3.1.2 AHRS Failure
Attitude and Heading Reference System (AHRS) failure is indicated by removal
of the sky/ground presentation, a red X, and a yellow "ATTITUDE FAIL" on the
PFD. Rate-of-turn information (heading trend vector) will not be available. A
heading failure will also occur as described in Section 3.2.1.
1.
Use Standby Attitude Indicator.
2.
Seek VFR conditions or land as soon as practical.
AFMS, GARMIN G500 PFD/MFD SYSTEM
FAA APPROVED
190-01102-01 Rev. 9
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