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bank angle limit in HDG,
VOR, or NAV modes.
Heading (HDG )
Button
Used to move the heading
bug on PFD.
Push Synchronize (PUSH
SYNC) Button
When pushed, causes
heading bug to synchronize
to airplane heading.
Approach (APP) Switch
Used to arm the lateral
guidance for localizer or VOR
approach capture. When
localizer capture, vertical
guidance is armed for
glideslope
capture.
Course 1 (CRS 1)
Button
Used to move the
course pointer on
selected PFD.
Push Direct (PUSH
DCT) Button
When pushed,
causes course
pointer to
indicate deviation
course to tuned
VOR.
Back Course (BC)
Switch
Used to select approach
mode guidance for capture
and tracking of back course
data.
NOTE
Annunciator, (on all flight
director mode switches),
illuminates when selected
mode is armed or active.
Annunciator
Light
GF0410_003
FLC
SPD
PUSH CHG
CRS 1 FMS MAN
PUSH DCT
HDG
PUSH SYNC
DN
UP
ALT CRS 2
PUSH DCT
SPD
PUSH CHG
CRS 1 FMS MAN
PUSH DCT
HDG
PUSH SYNC
AUTOMATIC FLIGHT CONTROL SYSTEM
Flight Crew Operating Manual REV 41, Jul 08, 2004
CSP 700−6
Volume 2
04−10−2
GUIDANCE PANEL (CONT'D)
GF0410_004
Coupled (CPL)
AP and YD Pointers
Illuminates to indicate which AP FGC
or YD is engaged. Whichever AP or
YD pointer was active on the last
landing becomes the standby FGC on
next power−up.
Speed/Pitch Wheel
Used to change vertical
reference value being used
by vertical speed (VS)
mode. Functional only when
AP engaged, or flight
director active.
DN − Rotate the wheel
forward to select pitch down
and speed increase.
UP − Rotate the wheel
backwards to select pitch
up and speed decrease.
Vertical Speed (VS)
Switch
Used to hold a vertical
speed. When pushed, the
vertical speed reference is
synchronized to current
vertical speed , displayed
on PFD. Use speed/pitch
wheel to change vertical
value.
Vertical Navigation
(VNAV) Switch
Used to select the vertical
navigation mode, tracking
vertical flight profile from
selected FMS.
Altitude (ALT)
Switch
Used to maintain
indicated altitude at
time of selection.
Altitude (ALT)
Preselect Button
Used to preselect
altitude, displayed
on PFD.
Course 2 (CRS 2)
Button
Used to move the course
pointer on selected PFD.
Push Direct (PUSH DCT)
Button
When pushed, causes
course pointer to indicate
deviation course to tuned
VOR.
Switch (lateral and vertical
flight guidance)
Used to couple either pilot’s
or copilot’s PFD and
associated ADC data to
FGC1 and FGC2.
Autopilot (AP)
Switch
Used to engage and disengage
autopilot. When autopilot
engaged, the yaw damper is
engaged simultaneously.
Disengaging the autopilot does not
disengage the yaw damper.
Yaw Damper (YD)
Switch
Used to engage and
disengage the yaw
damper. Disengaging the
yaw damper, disengages
the autopilot.
Flight Director (FD)
Switch
Used to remove flight
director command bars
from the PFD not selected
by the flight director.
CPL Pointer
Illuminates to indicate whether
the associated AP is coupled
to FGC1 or to FGC2. Both
pointers will illuminate during
an ILS approach.
AP
YD
CPL
SPD
PUSH CHG
CRS 1 FMS MAN
PUSH DCT
HDG
PUSH SYNC
DN
UP
ALT CRS 2
PUSH DCT
DN
UP
ALT CRS 2
PUSH DCT
AUTOMATIC FLIGHT CONTROL SYSTEM
REV 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 2
04−10−3
AUTOPILOT SYSTEM
GF0410_005
CONTROL WHEEL
GUIDANCE PANEL
CONTROL SURFACE POSITION
AILERON RUDDER ELEVATOR
TRIM SYSTEM
TRIM SWITCHES TOUCH CONTROL
AP DISC STEERING (TCS)
BUTTON
TOGA
BUTTONS
AUTOMATIC FLIGHT CONTROL SYSTEM
Flight Crew Operating Manual REV 41, Jul 08, 2004
CSP 700−6
Volume 2
04−10−4
AUTOPILOT
The autopilot (AP) system automatically controls the airplane in pitch and roll attitude via servo
control of ailerons, elevator and aircraft trim system. The two autopilot computer channels operate in
　
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