Garmin G500 Pilot's Manual page 28

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Attitude and heading information is displayed on the PFD when the AHRS

receives appropriate combinations of information from the external sensor

Magnetometer

* GSU 75 only.

Loss of GPS, magnetometer, or air data inputs is communicated to the pilot by

message advisory alerts. Refer to section 6 for specific AHRS alert information.

Any failure of the internal AHRS inertial sensors results in loss of attitude and

heading information. This is indicated by red "X" flags over the corresponding

flight instruments.

Unavailable No Air/

No Mag Available*/

Table 1-2 AHRS Operation

Figure 1-6 AHRS Operation

Garmin G500/G600 Pilot's Guide

AHRS Outputs

Unavailable Unavailable

Unavailable Unavailable

Attitude/Heading

190-00601-02 Rev. J