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also manually select other vertical modes (pitch, flight level change, vertical speed, altitude hold)
and modify airspeed/Mach references while VNAV is active. These actions will suspend FMS
control, but do not prevent subsequent mode activation by the FMS.
NOTE
The altitude preselector overrides any VNAV commands, except
FMS glide path (GP) mode.
In the event the FMS vertical flight plan is not valid when VNAV is selected, a yellow VNAV
annunciation appears in the vertical armed field of the FMA.
VNAV mode is cleared by:
• Pushing the VNAV button,
• Capturing an ILS glideslope,
• Changing the NAV SOURCE on the coupled side, or
• Pushing the TOGA button.
For additional information on VNAV, refer to the Collins FMS–6000 Flight Management System
Pilot’s Guide.
AUTOMATIC FLIGHT CONTROL SYSTEM
Description
Vol. 2 04−10−42
REV 74, Nov 07/08
CL−604 Operating Manual
PSP 604−6
FLIGHT DIRECTORS (CONT'D)
Turbulence (TURB) Mode
When turbulence mode is active, the FCC reduces autopilot gains for turbulent flight conditions.
This prevents the FCC from instantaneously responding to pitch and roll changes brought about
by flight through turbulent air.
Turbulence mode is available when the autopilot is engaged and can be selected by pressing
the TURB button on the FCP. The green status indicator lights on each side of the TURB button
illuminate when turbulence mode is selected. There is no indication of TURB mode selection on
the PFDs.
TURB mode is cleared by any one of following:
• Pushing the TURB button again,
• On-side LOC capture, or
• Autopilot disengagement.
Turbulence Mode Button
Figure 04−10−37
NOTE
The maximum IAS or MACH for turbulent air penetration is 280 KIAS
or 0.75 MACH.
AUTOMATIC FLIGHT CONTROL SYSTEM
Description
Vol. 2 04−10−43
REV 74, Nov 07/08
CL−604 Operating Manual
PSP 604−6
CONTROLS AND INDICATORS
General
The flight control panel (FCP) provides the majority of controls for flight director and autopilot
operation. The reversionary/inhibit panel allows selection between AFCS 1 and 2. Both the pilot’s
and copilot’s control wheel incorporates pushbuttons for autopilot disconnect and flight director
synchronization.
The PFD flight mode annunciator (FMA) provides an indication of autopilot and flight director
status. The EICAS primary and status pages provide the system warning, caution and status
messages, respectively.
Reversionary/Inhibit Panel
Reversionary/Inhibit Panel
Figure 04−10−38
AUTOMATIC FLIGHT CONTROL SYSTEM
Description
Vol. 2 04−10−44
REV 74, Nov 07/08
CL−604 Operating Manual
PSP 604−6
CONTROLS AND INDICATORS (CONT'D)
Flight Control Panel (FCP) – Autopilot/Flight Director Modes
Flight Control Panel (FCP) − Autopilot/Flight Director Modes
Figure 04−10−39
AUTOMATIC FLIGHT CONTROL SYSTEM
Description
Vol. 2 04−10−45
REV 74, Nov 07/08
CL−604 Operating Manual
PSP 604−6
CONTROLS AND INDICATORS (CONT'D)
Flight Control Panel (FCP) – Lateral Modes
Flight Control Panel (FCP) − Flight Director Lateral Modes
Figure 04−10−40
AUTOMATIC FLIGHT CONTROL SYSTEM
Description
Vol. 2 04−10−46
REV 74, Nov 07/08
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PSP 604−6
CONTROLS AND INDICATORS (CONT'D)
Flight Control Panel (FCP) – Vertical Modes
Flight Control Panel (FCP) − Flight Director Vertical Modes
Figure 04−10−41
AUTOMATIC FLIGHT CONTROL SYSTEM
Description
Vol. 2 04−10−47
REV 74, Nov 07/08
CL−604 Operating Manual
PSP 604−6
CONTROLS AND INDICATORS (CONT'D)
AFCS Cockpit Switches
Cockpit Switches − Autopilot/Flight Director Function
Figure 04−10−42
AUTOMATIC FLIGHT CONTROL SYSTEM
Description
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PSP 604−6
CONTROLS AND INDICATORS (CONT'D)
PFD Annunciations
The following figure and table provide a summary of FCC-related annunciations which may be
presented on the PFD.
PFD Annunciations
Figure 04−10−43
AUTOMATIC FLIGHT CONTROL SYSTEM
Description
Vol. 2 04−10−49
REV 74, Nov 07/08
CL−604 Operating Manual
PSP 604−6
CONTROLS AND INDICATORS (CONT'D)
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