曝光台 注意防骗
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capture is the same as NAV mode; B/C1 (or B/C2) shows in white in the armed lateral mode
field on both PFDs. When armed, the FCC operates in a heading select submode until capture
of the localizer occurs.
If the back course approach is selected from the FMS, the localizer frequency is tuned
automatically and the course display is set to the appropriate inbound course. With back course
mode armed, the active navigation source will automatically change from FMS to LOC
(automatic NAV to NAV transfer) at localizer capture.
After capture, the FCC generates commands to track the reciprocal of the selected course. The
front course track must be set in order to have valid B/C guidance. Capture of the back course is
indicated by a green B/C1 or B/C2 in the active field of the FMA. Glideslope is inhibited when
B/C mode is active.
Back course mode is cleared by selecting another lateral mode, or by changing the active side
navigation source or frequency.
AUTOMATIC FLIGHT CONTROL SYSTEM
Description
Vol. 2 04−10−29
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
FLIGHT DIRECTORS (CONT'D)
Back Course Mode
Figure 04−10−25
AUTOMATIC FLIGHT CONTROL SYSTEM
Description
Vol. 2 04−10−30
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
FLIGHT DIRECTORS (CONT'D)
Lateral Takeoff
On the ground, pushing either TOGA (takeoff/go-around) button, mounted on the thrust levers,
selects takeoff mode and clears all other lateral modes. Lateral and vertical takeoff mode
selections are coincident. When takeoff mode is active, a green TO appears in the active lateral
field of the FMA. During takeoff mode, the flight directors operate in dual independent mode.
NOTE
The autopilot will disengage whenever a TOGA button is pressed on
the ground or in-flight. The autopilot visual and aural disengage
warnings may be canceled by pushing either TOGA button again, or
by pushing any AP/SP DISC switch.
With takeoff mode selected, the heading reference is continuously set to the current aircraft
heading while maneuvering on the ground. After lift-off (weight off wheels), the takeoff mode
generates a heading hold command, with a five-degree bank limit, using the heading which
existed at the moment of lift-off. These heading references are independent of the HDG bug.
Takeoff lateral mode is cleared by selecting another lateral mode.
Lateral Takeoff Mode
Figure 04−10−26
AUTOMATIC FLIGHT CONTROL SYSTEM
Description
Vol. 2 04−10−31
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
FLIGHT DIRECTORS (CONT'D)
Lateral Go-Around Mode
In the air, pushing either TOGA (takeoff/go-around) button, mounted on the thrust levers, selects
the go−around mode and clears all other lateral modes. Lateral and vertical go−around mode
(GA) selections are coincident. When go−around mode is active, a green GA appears in the
active lateral field of the FMA. During go-around mode, the flight directors operate in dual
independent mode.
NOTE
The autopilot will disengage whenever a TOGA button is pressed on
the ground or in-flight. The autopilot visual and aural disengage
warnings may be canceled by pushing either TOGA button again, or
by pushing any AP/SP DISC switch.
The lateral component of go-around mode (GA) generates commands to maintain the heading
that existed at the moment of GA mode activation. Go-around mode generates a heading hold
command with a five-degree bank limit. This heading reference is independent of the HDG bug.
Go-around mode is cleared by selecting another lateral mode.
Lateral Go-Around Mode
Figure 04−10−27
Flight Director Vertical Modes
There are nine vertical flight director modes (bold letters refer to the flight control panel button
selections):
• Pitch
• Altitude preselect
• Altitude hold (ALT)
• Vertical speed (VS)
• Flight level change (FLC)
• Takeoff
AUTOMATIC FLIGHT CONTROL SYSTEM
Description
Vol. 2 04−10−32
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
FLIGHT DIRECTORS (CONT'D)
• Go-around
• Glideslope
• FMS vertical navigation (VNAV)
Vertical modes are armed or activated by the FCP push-buttons, a pitch wheel on the flight control
panel, or by TOGA switches on the thrust levers. In general, disabling the active vertical mode is
accomplished by reselecting the active FCP push-button, or by selecting another vertical mode.
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