Garmin G300 Pilot’s Guide
190-00921-00 Rev. E
195
Integrated Autopilot
System
Overview
Flight
Instruments
EIS
COM
Interface
GPS
Navigation
Flight
Planning
Hazar
d
Avoidance
Additional
Featur
es
Integr
ated
Autopilot
Annun/Alerts
Appendix
Index
DISENGAGING THE INTEGRATED AUTOPILOT
The Integrated Autopilot is manually disengaged by pressing the autopilot
disconnect button on the control stick or yoke. Manual disengagement is indicated
by a five-second flashing yellow ‘AP’ annunciation and an aural alert.
Automatic disengagement is indicated by a flashing red ‘AP’ annunciation and
an aural alert. The flashing indication continues until acknowledged by pressing
the
ENT
Key. Automatic disengagement occurs due to:
•
System failure
•
Invalid sensor data
•
Inability to compute default autopilot modes
CONTROL WHEEL STEERING (CWS)
Control Wheel Steering allows the aircraft to be hand-flown without disengaging
the Integrated Autopilot. Press and hold the external autopilot unit’s CWS Button
to temporarily disengage the pitch and roll servos from the flight control surfaces
and hand-fly the aircraft. The G300 autopilot control is synchronized to the
aircraft attitude during Control Wheel Steering. The green ‘AP’ annunciation is
temporarily replaced by a white ‘CW’ for the duration of Control Wheel Steering
maneuvers.
In most scenarios, releasing the CWS Button reengages the Integrated Autopilot
with a new reference. Refer to Sections 9.2 (Vertical Modes) and 9.3 (Lateral
Modes) for Control Wheel Steering behavior in each mode.
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