AFMS
N"D07
FOR
GARMIN
GFC700
AUTOPILOT
AND
VARIABLE
PITCH
PROPELLER
EQUIPPED
AEROPLANES
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12.
AUTOPILOT
DESCRIPTION
P20 I 0 aircraft
is
equipped. as an optional equipment, with an inlcgrnlcd 2-axis aulopilot
suite manufaclnrcd by Garmin and identified as GFC 700. This autopilol suite was de-
signed as an option for lhc G
IOOO
integrated flight deck. The aulopilol
is
controlled via
dedicated keys grouped
in
a control panel located on the MFD.
The aulupilol suite installed on P2010
is
based on the following configuration:
I Roll servo
I Pitch servo
I Pilch Trim servo
Neither yaw axis nor rudder lrim tab control
is
provided.
The autopilot
is
connected lo clcclric system through the below listed circuit breakers
connected lo the avionics bus:
I) A/I' (5A)
2) PITCI I
TRIM
(3A)
The installed servos arc capstan type and are composed
of
two main components:
A servo motor
A servo capstan including the servo clutch
The following block diagram describes the avionic system installed on P20
JO
and its in-
terconnections with the autopilot servos:
Section
1 -
General
AUTOPILOT
DESCRIPTION
Ed.
2,
Rev.I
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