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onside approach mode or localizer capture), or can also be cleared by pressing the 1/2 BANK
button again.
Automatic Half Bank
Half bank is automatically selected if either flight director is selected and the airplane climbs
through a transition altitude of 31,600 feet MSL, or if the airplane is above this altitude when
the flight director is turned on. Half bank mode automatically clears when the airplane
descends below 31,600 feet MSL. Manual operation of half bank mode overrides the FCC
automatic transitions to or from half bank mode.
AUTOMATIC FLIGHT CONTROL SYSTEM
Description
Vol. 2 04−10−18
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
FLIGHT DIRECTORS (CONT'D)
Half Bank Mode
Figure 04−10−17
NAV Mode
Pushing the NAV button on the FCP alternately selects and clears the navigation mode, and
causes the flight director to generate lateral commands to capture and track the active
navigation source (VOR, LOC, FMS).
The displayed navigation source will determine which navigation submode will be in operation.
NAV Source Selection
The navigation source may be selected using the PRESET NAV box or the PFD menu.
• PRESET NAV box: Select desired preset NAV source by rotating the data knob on the
DCP, then push the NAV SRC swap button.
• PFD menu: Press MENU button on the DCP, and use the menu ADV/DATA knob to
select the desired NAV source.
LOC or VOR navigation source is determined by the ground station frequency set in the radio
tuning window.
All NAV mode annunciations appear in the lateral field of the FMA: armed modes in white, and
active/captured modes in green. Captures that are inhibited due to invalid data are
annunciated on the PFDs as a red horizontal line through the mode annunciation.
AUTOMATIC FLIGHT CONTROL SYSTEM
Description
Vol. 2 04−10−19
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
FLIGHT DIRECTORS (CONT'D)
Display Control Panel
Figure 04−10−18
Navigation Source Selection Display
Figure 04−10−19
AUTOMATIC FLIGHT CONTROL SYSTEM
Description
Vol. 2 04−10−20
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
FLIGHT DIRECTORS (CONT'D)
VOR Navigation Mode
In the VOR navigation mode, the flight director generates lateral steering commands to capture
and track the selected VOR radial (inbound or outbound), using the course displayed on the
active navigation source.
When the NAV button is pressed and the active navigation source is VOR1 or VOR2, the VOR
navigation mode is armed. The armed lateral mode field on both PFDs shows a white VOR1
(or VOR2) annunciation. When the VOR mode is captured, the armed annunciations are
removed, and a green VOR1 (or VOR2) annunciation is displayed in the active lateral mode
field on the PFDs.
The CRS1 and CRS2 knobs, located on the FCP, provide the means to select the desired
course on the left and right PFD HSI respectively. Pressing the PUSH DIRECT knob within the
CRS knob synchronizes the corresponding course display, and provides a “direct-to” VOR
course.
VOR navigation mode is designed to permit tracking over station, and allow for course
changes while tracking. When over a VOR station, the system can accept and follow a course
change of up to 90°. Dead reckoning operation (based on memorized heading) is provided
during VOR station passage. A white DR annunciation appears next to the active VOR mode
annunciation during dead reckoning operation.
When captured, VOR navigation mode is cleared automatically by selection of another lateral
mode, by changing the active NAV source, or by loss of the VOR signal. VOR navigation mode
can also be cleared by pressing the NAV button again.
AUTOMATIC FLIGHT CONTROL SYSTEM
Description
Vol. 2 04−10−21
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
FLIGHT DIRECTORS (CONT'D)
VOR Navigation Mode
Figure 04−10−20
Localizer Navigation Mode
In localizer navigation mode, the flight director provides lateral steering commands to capture
and track the front course localizer from the active navigation source.
Whenever LOC navigation mode arms, a white LOC1 (or LOC2) annunciation is displayed in
the armed lateral mode field on both PFDs. When the LOC mode is captured, the armed
annunciation is removed, and a green LOC1 (or LOC2) is displayed in the active lateral mode
field on both PFDs.
AUTOMATIC FLIGHT CONTROL SYSTEM
Description
Vol. 2 04−10−22
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庞巴迪挑战者605机组操作手册 CL605-AUTOMATIC_FLIGHT_CONTROL_S(8)
