AFMS N°D01 FOR GARMIN GFC700 AUTOPILOT INSTALLATION AND
RNAV/RNP NAVIGATION ELIGIBILITY
AUTOPILOT DESCRIPTION
AUTOPILOT DESCRIPTION 12
P2010 aircraft is equipped, as an optional equipment, with an integrated 2-axis au-
topilot suite manufactured by Garmin and identified as GFC 700. This autopilot
suite was designed as an option for the G1000 integrated flight deck. The autopi-
lot is controlled via dedicated keys grouped in a control panel located on the
MFD. The installed MFD display is different with respect to standard P2010 con-
figuration since it is GDU 1044.
The autopilot suite installed on P2010 is based on the following configuration:
1 Roll servo
1 Pitch servo
1 Pitch Trim servo
Neither yaw axis nor rudder trim tab control is provided.
The autopilot is connected to electric system through the below listed circuit
breakers connected to the avionics bus:
1) A/P (5A)
2) PITCH TRIM (3A)
The installed servos are 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 P2010 and
its interconnections with the autopilot servos:
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