Cessna TURBO CENTURION T210M 1978 Pilot Operating Handbook page 325

PILOT'S OPERATING HANDBOOK
SUPPLEMENT
CESSNA 200A AUTOPILOT
(TYPE AF-295B)
SUPPLEMENT
CESSNA NAVOMATIC
200A AUTOPILOT
(Type AF-295B)
SECTION 1
GENERAL
The Cessna 200A Navomatic is an all electric, single-axis (aileron
control) autopilot system that provides added lateral and directional
~ stability. Components are a computer-amplifier, a turn coordinator, an
' aileron actuator, and a course deviation indicator(s) incorporating a
localizer reversed (BC) indicator light
Roll and yaw motions of the airplane are sensed by the turn coordina-
tor gyro. The computer-amplifier electronically computes the necessary
~ , correction and signals the actuator to move the ailerons to maintain the
airplane in the commanded lateral attitude.
The 200A Navomatic will also capture and track
a
VOR or localizer
course using signals from a VHF navigation receiver.
The operating controls for the Cessna 200A N avomatic are located on
the front panel of the computer-amplifier, shown in Figure
1.
The primary
function pushbuttons (DIR HOLD, NAV CAPT, and NAV TRK), are
inter locked so that only one function can be selected at a time. The HI SENS
and BACK ORS pushbuttons are not interlocked so that either or both of
these functions can be selected at any time.
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