Garmin G500 Manuale - Pagina 34

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Garmin G500 Manuale
4.6

Autopilot Operations with the G500 System

The G500 PFD/MFD System offers various integration capabilities dependent
mainly upon the type of autopilot installed in a particular aircraft.
The G500 installation in this aircraft provides the following autopilot integration
capabilities:
 This installation does not interface with the autopilot (basic wing
leveling autopilot or no autopilot is installed in the aircraft).
 Course / NAV Selection coupling to the autopilot.
 Heading Bug coupling capability to the autopilot.
 Roll Steering emulated via heading mode.
 Roll Steering capable autopilot.
 Altitude Pre-Selector integrated with the autopilot.
 Vertical speed bug integrated with the autopilot.
 Flight Director display driven from external autopilot or FD computer.
 Flight Director is not available with Synthetic Vision enabled.
 A GAD 43 Adapter is installed in this aircraft
 GAD 43 provides attitude to the autopilot
 GAD 43 provides yaw rate to the yaw damper
 GAD 43 provides baro correction to the altitude preselector
 GDU 620 provides attitude / air data to autopilot
4.6.1 Attitude and Rate Based Autopilots
Attitude-based autopilots may be driven by the standby gyro, a remote mounted
gyro, the GDU 620, or the GAD 43 adapter. If the GDU 620 or GAD 43 is
providing attitude to the autopilot, it will be indicated in section 4.6 above.
Otherwise, if the attitude-based autopilot is receiving attitude from the standby
or a remote gyro, the autopilot attitude input is independent of the attitude
displayed on the PFD.
Rate-based autopilots are driven by a turn coordinator gyro which may be
mounted in the instrument panel or remotely mounted. The autopilot rate input
is independent of the G500 system.
The pilot must understand the autopilot system inputs to detect faults and
capabilities with inoperative equipment. Refer to the autopilot flight manual for
operational information.
AFMS, GARMIN G500 PFD/MFD SYSTEM
FAA APPROVED
190-01102-01 Rev. 9
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