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automatic performance reserve operation, hot start annunciation and core vibration
annunciations.
Systems represented by graphical display and/or digital readout on the center column include:
• Horizontal stabilizer trim;
• Aileron trim;
• Rudder trim;
• Landing gear position;
• Flap position;
• Spoiler position;
• Pressurization data (cabin altitude, rate of climb/descent, differential pressure);
• Cabin temperature;
• Crew oxygen bottle pressure; and
• Auxiliary power unit EGT and RPM.
EICAS Page
Figure 03−10−9
AURAL/VISUAL WARNING SYSTEM
Description
Vol. 2 03−10−10
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
ENGINE INDICATION AND CREW ALERTING SYSTEM (CONT'D)
EICAS Page - Compressed Format
The EICAS page, in compressed format, is used when the crew needs to place EICAS, flight
and navigation data on a single display, i.e, in the event of a single or multiple display failure.
In reversionary operation, a subset of the EICAS information is made available in the
compressed display mode. This operation is enabled by using the L (R) DISPLAYS and EICAS
selectors on the reversionary control panel.
When the compressed format is enabled, the EICAS information is automatically reconfigured to
fit in the available display space as follows:
• Radio tuning data and functions are removed from the top of the display;
• Only N1 remains available as a circular gauge – all other engine data is shown as a
numerical readout only;
• Pressurization data, cabin temperature and crew oxygen bottle pressure are removed
from the system data column – all other system data remain in view. Includes trim, gear,
flap, spoiler position and APU RPM and EGT;
• Total fuel quantity remains in view, but individual tank quantity is removed; and
• Crew alerting messages remain available on the right side of the display.
EICAS Page − Compressed
Figure 03−10−10
EICAS Synoptic Pages
Synoptic pages are available as a page overlay, and are normally viewed on the lower window
of a MFD. Each EICAS synoptic page allows the crew to view a dynamic representation of the:
• AC electrical system;
• DC electrical system;
• Hydraulic system; and
• Flight control system.
Synoptic pages are selectable on the lower window of the MFD by buttons on the cursor control
panels (CCP). The buttons are labelled according to the system being represented: AC ELEC,
DC ELEC, HYD, FLT.
AURAL/VISUAL WARNING SYSTEM
Description
Vol. 2 03−10−11
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
ENGINE INDICATION AND CREW ALERTING SYSTEM (CONT'D)
Synoptic pages can also be shown on the upper window of an MFD that is not configured as an
EICAS page. This feature can only be selected from the upper window main menu of the MFD,
which is not available when the EICAS page is locked on the MFD. Locking the EICAS page on
a particular MFD is a function of the EICAS selector on the reversionary control panel.
The synoptic pages include digital readouts, colored flow lines, component outlines and system
messages. Specific colors are used to depict normal, precautionary and maximum system limits
as follows:
• Indicator is green; normal range;
• Indicator turns amber; precautionary range; and
• Indicator turns red; limits exceeded.
Specific colors are used to depict the flow lines as follows:
• Black, indicates no flow;
• Amber, indicates below normal values;
• Green, indicates normal value; and
• Red, indicates exceeding normal values.
When a synoptic page is being shown, a tab, located in the right corner of the synoptic page,
identifies which navigation format is being displayed. Selection of the quick access button for the
synoptic page being displayed causes the page to be removed and replaced with the previously
selected format (as identified by the tab).
AURAL/VISUAL WARNING SYSTEM
Description
Vol. 2 03−10−12
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
ENGINE INDICATION AND CREW ALERTING SYSTEM (CONT'D)
Synoptic Page Selection (1 of 3)
Figure 03−10−11
AURAL/VISUAL WARNING SYSTEM
Description
Vol. 2 03−10−13
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
ENGINE INDICATION AND CREW ALERTING SYSTEM (CONT'D)
Synoptic Pages (2 of 3)
Figure 03−10−12
　
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