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庞巴迪挑战者605公务机机组操作手册 CL605-AUTOMATIC_FLIGHT_CONTROL_SYSTEM(21)

时间:2011-10-27 00:46来源:蓝天飞行翻译 作者:公务机
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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.
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.

 


NOTE
The maximum IAS or MACH for turbulent air penetration is 280 KIAS or
0.75 MACH.


 AUTOMATIC FLIGHT CONTROL SYSTEM Description  Vol. 2  04.10.45 
Oct 05/06 


Turbulence Mode Button
Figure 04.10.37

 

 AUTOMATIC FLIGHT CONTROL SYSTEM Description  Vol. 2  04.10.46 
Oct 05/06 

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 push-buttons 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  04.10.47 
Oct 05/06 


Flight Control Panel (FCP) . Autopilot/Flight Director Modes
Figure 04.10.39

 

 AUTOMATIC FLIGHT CONTROL SYSTEM Description  Vol. 2  04.10.48 
Oct 05/06 


Flight Control Panel (FCP) . Flight Director Lateral Modes
Figure 04.10.40

 

 AUTOMATIC FLIGHT CONTROL SYSTEM Description  Vol. 2  04.10.49 
Oct 05/06 
 
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