Garmin Non_Airframe Specific User's Guide download pdf (Page 28)

18 G600 Cockpit Reference Guide

190-00601-03 Rev F

PRIMARY FLIGHT DISPLAY (PFD)

PRIMARY FLIGHT DISPLAY

Autopilot (AP)

The G600 is able to interface to certain autopilot systems to provide the

functions described in this section. Please refer to your particular Airplane Flight

Manual and autopilot documentation for speciﬁ c information and operating

instructions.

GAD 43 Attitude

If the GAD 43 Adapter is providing attitude to the autopilot, test the disconnect

mechanism prior to each ﬂ ight in the following manner:

1) Allow all avionics to complete power up and begin normal operation.

2) Engage the autopilot while on the ground.

3) Press and release the AP TEST soft key and verify that the autopilot

disconnects normally.

NOTE: If the AP TEST soft key is held for longer than one second, the test

will not run.

CAUTION: Do not use the autopilot if the AP TEST key fails to disconnect

the autopilot.

Autopilot Disconnect

When the GDU 620 attitude monitors have detected an AHRS malfunction,

or the inability to actively monitor the AHRS, a “Check Attitude” annunciation

will be displayed on the PFD and the autopilot will automatically disconnect.

NOTE: Only appears with the installation of an optional GAD 43

Adapter.

Check Attitude Annunciation

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Garmin Non_Airframe Specific User's Guide Page 28