Garmin Software Version 0321.19 Manual de usuario Pagina 62

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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT
GARMIN G1000 INTEGRATED AVIONICS SYSTEM
DIAMOND MODEL DA 40
DIAMOND MODEL DA 40 F
190-00492-10 Rev 5 Diamond DA 40 / DA 40F
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The GFC 700 autopilot contains an electric pitch trim system which is used by
the autopilot for automatic pitch trim during autopilot operation and by the pilot
for manual electric pitch trim when the autopilot is not engaged. The manual
electric pitch trim system is operated by a split switch on the left control stick.
The GFC 700 autopilot and manual electric trim (MET) will not operate until
the system has satisfactorily completed a preflight test. The preflight test begins
automatically with initial power application to the autopilot (AVIONIC
MASTER Switch is set to the ON position).
The following conditions will cause the autopilot to automatically disconnect:
Electrical power failure
Internal autopilot system failure
AHRS malfunction
Loss of Air Data Computer information
The GFC 700 may be manually disconnected by any of the following means:
Depressing the red AP DISC button on either control stick
Moving the left (outboard) side of the manual electric trim switch on the
left control stick
Pushing the AP button on the autopilot mode controller when the autopilot
is engaged
Depressing the GA button on the left side of the throttle
Pulling the AFCS circuit breaker
Turning off the AVIONIC MASTER switch
Turning off the airplane Master (ALT/BAT) switch
In addition, the CWS (control wheel steering) switch on the pilot’s control stick
will disconnect the autopilot servos from the airplane flight controls as long as
the CWS switch is depressed.
Power to the GFC 700 autopilot and electric trim system is supplied through the
AVIONIC MASTER switch and the AFCS circuit breaker. The AVIONIC
MASTER switch can be used as an additional means to disable the autopilot and
electric trim system.
The red AP DISC switch on the either control stick will interrupt power to the
manual electric trim for as long as the switch is depressed.
Loss of instruments or components of the G1000 system will affect the GFC
700 AFCS as follows:
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