Honeywell KFC 150 Pilot's Manual page 16

Flight control system
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Mode
Flight Director/Autopilot Action
Heading (HDG)
Select desired heading on PNI, then select
HDG mode. The V-bar will command the
necessary bank to turn to and maintain the
selected heading.
Navigate (NAV)
(VOR/RNAV)
The V-bar will command the bank necessary
to turn to and maintain a V O R or RNAV course
selected by the pilot.
The V-bar will command the bank and pitch
necessary to capture and track localizer and
glideslope for ILS approaches, or to capture and
track the appropriate course for V O R or RNAV.
The V-bar will command the bank necessary
to capture and track a reverse localizer course.
Glideslope is locked out.
Approach (APR)
(ILS, VOR or RNAV)
Back Course (BC)
Altitude Hold (ALT)
The V-bar will command the pitch attitude
necessary to maintain the engaged altitude
Test Button
Depressing the test button initiates a test of the
KFC
150
circuitry, including operation of various
modes and of the trim. The test must be
performed after power is applied and before the
autopilot can be engaged, but the flight director
can be used without the test being performed.
Vertical Trim
This rocker switch allows you to make small
corrections in selected altitude while in altitude
hold, or adjust pitch attitude at a rate of
approximately
.9
degrees per second when not
in altitude hold.
Control Wheel
Steering
(CWS)
This button mounted on the control wheel allows
you to maneuver the aircraft in pitch and roll
without disengaging the autopilot. After the CWS
button is released, the autopilot resumes control
of the aircraft.

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