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data system and the inertial reference system (IRS).
FLIGHT INSTRUMENTS
Description
Vol. 2 11−10−1
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
GENERAL (CONT'D)
Integrated Flight Instruments
Figure 11−10−1
FLIGHT INSTRUMENTS
Description
Vol. 2 11−10−2
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
PRIMARY FLIGHT DISPLAY (PFD)
Description
The two primary flight displays (PFDs) provide the pilots with the information necessary for the
safe operation of the aircraft. They are integrated displays of attitude, air data, and navigation
information. The PFD is divided into the following main areas:
• Attitude ADI;
• Airspeed/Mach;
• AOA;
• Altitude;
• Vertical speed;
• Flight mode annunciator (FMA) for the AFCS;
• Lateral deviation indicator; and
• Navigation display.
FLIGHT INSTRUMENTS
Description
Vol. 2 11−10−3
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
PRIMARY FLIGHT DISPLAY (PFD) (CONT'D)
Primary Flight Display
Figure 11−10−2
FLIGHT INSTRUMENTS
Description
Vol. 2 11−10−4
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
MULTIFUNCTION DISPLAY (MFD)
Description
The two multifunction displays (MFDs) can be operated in three basic configurations: split window,
chart window and STAT window. The most common configuration for normal operation is the split
window, which consists of four distinct windows:
• Radio tuning window;
• Upper window;
• Lower window; and
• Lower window overlay.
During normal operation, the upper window of the left MFD displays the EICAS page, including
engine indications, full time system indications, and CAS messages. The upper window of the right
MFD displays the SUMMARY page, or the electronic checklist. For maintenance actions, the
upper window of the right MFD can also display maintenance diagnostic system information. The
lower window of both the left and right MFDs can display synoptic pages or navigation information.
Overlays such as TCAS traffic, terrain, weather and lightning can be presented on PPOS
navigation format. The MFDs are controlled using the cursor control panel (CCP).
L and R MFDs − Split Window Configuration
Figure 11−10−3
FLIGHT INSTRUMENTS
Description
Vol. 2 11−10−5
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
EFIS CONTROL PANELS
Description
Information related to speed, altitude, barometric setting, navaid source, navigation display formats
and system reversion (adaptive flight display AFD, ADC, IRS) is inserted through controls on the
following control panels:
• Display control panel (DCP);
• Cursor control panel (CCP);
• Flight control panel (FCP);
• BARO knob (glareshield); and
• Reversionary panel.
Display Control Panel (DCP)
The display control panels (DCPs), located on the center pedestal, are the primary pilot interface
to select the information presented on the PFDs. The left DCP controls the selectable information
displayed on the left PFD. The right DCP controls the selectable information displayed on the right
PFD.
Display Control Panel (DCP)
Figure 11−10−4
Each DCP provides control for the following:
NAV SRC (Navigation Source) Pushbutton
This pushbutton interchanges the active and preset navigation sources.
MENU Pushbutton
This pushbutton selects the PFD MENU. The items on the PFD MENU are changed using the
selection box method. The menu list automatically times out after 20 secs of inactivity.
ESC (Escape) Pushbutton
This pushbutton steps one level out of a selected menu.
FLIGHT INSTRUMENTS
Description
Vol. 2 11−10−6
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
EFIS CONTROL PANELS (CONT'D)
MENU ADV/DATA/PUSH SELECT Knob
This is a double stack knob that consists of the following:
• MENU ADV (outer knob) – Provides control to move the focus indicator* within the
menu.
• DATA (inner knob) – Provides control to change the selection in the focus indicator*.
• PUSH SELECT (center knob) – Makes DATA knob entries active, or changes the
status of the item in the selection box.
* The focus indicator is the symbol (cyan box) indicating which control is currently highlighted.
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庞巴迪挑战者605机组操作手册 CL605-FLIGHT_INSTRUMENTS(3)
