Garmin G500 Manual - Página 40
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4.6.9 GAD 43 Operation
The GAD 43 Adapter provides attitude, heading, and barometric correction
information from the G500 System to the autopilot. The GAD 43 can also be
configured to provide synchro heading output to other systems and its attitude
output can be used for RADAR stabilization. The GAD 43 has the ability to
disconnect the autopilot if an error in the GAD 43 output or GRS 77 is detected.
This disconnect mechanism must be tested prior to each flight in the following
manner:
1.
Upon G500 startup, an AP TEST soft key will be available on the G500
PFD side of the G500 display.
2.
Engage the AP while on the ground.
3.
Press the AP TEST soft key and verify that the autopilot disconnects.
Do not use the autopilot if the AP TEST key fails to disengage the autopilot
Pressing and holding the AP TEST key for longer than 1 second will
prevent the test from running and the AP TEST key will remain displayed.
4.6.10 Dual G500 Autopilot Interface
If the installation has dual G500 PFD/MFD systems installed, control of
navigation course, heading, or altitude data affecting the autopilot from the co-
pilot side can only be made if the systems are synchronized with each other.
Refer to the Garmin G500 Cockpit Reference Guide for additional information.
Section 5. PERFORMANCE
No change.
Section 6. WEIGHT AND BALANCE
See current weight and balance data.
Section 7. SYSTEM DESCRIPTIONS
See Garmin G500 PFD/MFD System Cockpit Reference Guide
P/N 190-01102-03 for basic operational aspects of the system. For a complete
detailed explanation of all the G500's capabilities see the G500 Pilot's Guide
P/N 190-01102-02.
AFMS, GARMIN G500 PFD/MFD SYSTEM
FAA APPROVED
CAUTION
normally.
NOTE
190-01102-01 Rev. 9
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