Honeywell KFC 150 Pilot's Manual page 15

Vertical Trim
Glideslope (GS)
I
Trim Failure
Warning
I
Flight
/
Director (FD)
/
Altitude
Hold (ALT)
Self-Test Autopilot
Engage
I '
(AP ENG)
(APR) (ILS,
VOR or RNAV)
/
.
.---ing
Back
Select (HDG)
/
Navigation
(NAV)
(VO R/RN AV)
Course (BC)
Electric
Trim Switch
Autopilbt
Disconnect/
Trim Interrupt
I
Ei:ISteeri(ng
(CWS)
Mode Flight DirectorlAutopilot Action
Attitude Reference Power on and no modes selected. FCI displays
aircraft attitude and
PNI
displays aircraft heading.
Command V-bar is biased
out
of view. Aircraft
engine@) must be running for pressure or vacuum
to be applied to FCI attitude gyro.
Flight Director (FD) V-bar will appear and command wings level
and pitch attitude of the aircraft at the time of
mode selection.
Autopilot Engage (AP
ENG)
Aircraft control surfaces (ailerons and elevators)
smoothly respond to all selected Flight Director
mode commands with automatic pitch trim.
Engages Yaw Damper
if
present.
14