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CESSNA 400B IFCS
(TYPE IF-550A)
PILOT'S OPERATING HANDBOOK
SUPPLEMENT
4
1.
CONTROL UNIT - Provides the autopilot ON-OFF switch
and
the primary
_
manual
controls
for operating the autopilot.
2.
PITCH
CONTROL - Controls pitch attitude of
airplane.
When rotated toward
UP,
airplane
will pitch up. When rotated toward DWN,
airplane
will pitch
down.
Pitch
attitude
depends
on
displacement
of the control from
level flight
position.
3.
TURN
CONTROL KNOB (TURN) - When turned, airplane will bank right
(R)
or
left (L). When
turned, disconnects
heading (HDG) or navigation (NAV)
modes
selected on Mode
Selector.
4.
LATERAL TRIM CONTROL
(TRIM)
- When TURN knob is centered,
(with
no
,,-,
lateral modes
engaged
and
the
airplane
manually trimmed for
existing
flight
conditions),
the TRIM
control
is used
to trim
for
a
wings level
attitude
.
5.
AUTOPILOT ON-OFF
SWITCH
(AP/
ON) - Controls primary power to autopilot.
AP annunciator on
Mode Selector will illuminate
green
when autopilot is
engaged.
6.
ACCESSORY UNIT - Provides
the
pilot with
an automatic
autopilot disconnect
-
-
warning
light and
an autopilot
disconnect self-test
operation for
use prior
to
flight.
Figure
1.
Cessna 400B IFCS (Type IF-550A) (Sheet 2 of 6)
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