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Cursor Control Panel
Figure 03−10−4
Reversionary Control Panel
The multipurpose reversionary control panel, located on the center pedestal, includes several
rotary selectors and switch/lights. The functions are as follows:
• TUNE INHIBIT PUSH switch/lights – used to inhibit the tuning functions of a CDU or
MFD (see Chapter 6, Communications)
• L(R) DISPLAYS selector – used to control the reversionary functions of the left (right)
PFD and MFD
• EICAS selector – used to control the location of the displayed EICAS information
• ADC selector – used to define the source of air data information (see Chapter 11, Flight
Instruments)
• AFCS SEL selector – used to define source of autoflight commands (see Chapter 4,
Automatic Flight Control System)
AURAL/VISUAL WARNING SYSTEM
Description
Vol. 2 03−10−6
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
ENGINE INDICATION AND CREW ALERTING SYSTEM (CONT'D)
Reversionary Control Panel
Figure 03−10−5
Master Warning/Caution Switch/lights
The MASTER WARNING/CAUTION switch/lights are installed on the left and right glareshield
panels.
The red master warning lights are associated with red warning messages. The amber master
caution lights are associated with amber caution messages.
Pressing either left or right switch/light will extinguish the flashing red or amber light.
AURAL/VISUAL WARNING SYSTEM
Description
Vol. 2 03−10−7
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
ENGINE INDICATION AND CREW ALERTING SYSTEM (CONT'D)
MASTER WARNING/CAUTION Switch/Lights
Figure 03−10−6
Audio Warning Panel
The AUDIO WARNING panel, located on the copilot side console, includes two switch/lights
(DCU 1 (2)), used to disable and silence EICAS aural warnings.
AUDIO WARNING Panel
Figure 03−10−7
Miscellaneous Test Panel
The miscellaneous test panel, located on the center pedestal, includes control switches for
testing the EICAS aural warning and flight deck panel lamp functions. The AURAL WARN TEST
switch is used to test the audio outputs of the DCUs, while the LAMP TEST switch is used to
check operation of panel switch/lights.
AURAL/VISUAL WARNING SYSTEM
Description
Vol. 2 03−10−8
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
ENGINE INDICATION AND CREW ALERTING SYSTEM (CONT'D)
Miscellaneous Test Panel
Figure 03−10−8
EICAS Presentation
Engine indicating and crew alerting (EICAS) information can be presented on one or more displays
and display windows. The following titled pages are available:
• EICAS page (full format);
• EICAS page (compressed);
• Synoptic pages; and
• SUMMARY page.
EICAS Page - Full Format
The EICAS page, in full format, is available for display on the upper window of the MFDs, and is
the main page showing engine and system parameters and crew alerting messages. It can be
shown on either the left or right MFD, when the display is operating in a split window
configuration.
Normally, only one MFD is configured to display the EICAS page. The EICAS selector switch,
located on the reversionary control panel, includes selectable L MFD and R MFD positions.
Normally, the switch is selected to the L MFD position, which locks the EICAS page on the left
MFD, preventing any other format selection on the upper window.
The EICAS page, when displayed in full format, is divided into three vertical columns with radio
tuning functions shown in a horizontal block above. EICAS information is presented as follows:
• Left column: engine parameters and related indications;
• Center column: system data such as trim, APU, spoiler position, etc; and
• Right column: crew alerting messages.
Engine indications are presented in circular gauge format and as digital readouts, and include:
• N1 speed gauge;
• N1 takeoff thrust setting;
• Interturbine temperature (ITT) gauge;
• N2 speed guage;
• Fuel flow;
AURAL/VISUAL WARNING SYSTEM
Description
Vol. 2 03−10−9
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
ENGINE INDICATION AND CREW ALERTING SYSTEM (CONT'D)
• Oil pressure;
• Oil temperature;
• Fan vibration; and
• Fuel quantity (individual tank and total)
Additional information is presented, as required, in the form of annunciations shown in the
center of the three circular gauges (N1, ITT, N2). This information includes thrust reverser status,
　
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