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display.
Pressing either MASTER WARNING/CAUTION switch/light:
• Extinguishes the flashing MASTER CAUTION switch/lights;
• Silences the single warning chime; and
• Resets the CAS system to allow the annunciation of additional caution messages.
AURAL/VISUAL WARNING SYSTEM
Description
Vol. 2 03−10−19
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
ENGINE INDICATION AND CREW ALERTING SYSTEM (CONT'D)
Caution Messages
Figure 03−10−18
Advisory Messages
Green advisory messages are next in order of priority, and are shown below the caution
messages. Advisory messages are used to advise of:
• Aircraft configuration for a particular phase of flight;
• Successful system test;
• Confirmation of shut-off valve (SOV) closure; and/or
• Receipt of SELCAL communications.
Depending on the message, a corresponding panel switch/light may also be shown in green.
Additional indications can also be displayed on the EICAS page or related synoptic page.
Status Messages
White status messages appear directly below any advisory messages that may be present.
Status messages are used to:
• Provide status of a specific system that has been manually or automatically activated;
and/or
• Identify a low-priority system failure.
Depending on the message, a corresponding panel switch/light may also be shown in white.
Additional indications can also be displayed on a related synoptic page or EFIS display.
AURAL/VISUAL WARNING SYSTEM
Description
Vol. 2 03−10−20
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
ENGINE INDICATION AND CREW ALERTING SYSTEM (CONT'D)
Advisory/Status Messages
Figure 03−10−19
CAS Message Pagination
It is possible to have more than one page of CAS messages. The CAS message block includes
sufficient space to display 25 messages when the full EICAS page is located on the upper
window of the MFD. This is reduced to 11 messages when EICAS is shown in the compressed
format. A boxed page number is shown at the bottom of the CAS message list when more than
one page of messages exist. The CAS button, located on the cursor control panel, is used to
view the next page of messages. Continued selection of the CAS button moves the display
forward, or returns the display to the first page of messages.
Crew Alerting Message Pagination
Figure 03−10−20
AURAL/VISUAL WARNING SYSTEM
Description
Vol. 2 03−10−21
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
ENGINE INDICATION AND CREW ALERTING SYSTEM (CONT'D)
CAS Message De-Clutter
The CAS button can also be used to de-clutter the EICAS message stack, should a large
number of messages be shown. When selected, the CAS message stack is removed from view
and replaced with a white MSGS icon, indicating that CAS messages are being hidden. Warning
messages, however, cannot be hidden and always remain in view.
The CAS message stack can be viewed by reselecting the CAS button. On ground, the
de-cluttering function can only be carried out when both engines are running. In the air, the
function can be carried out at any time, regardless of engine operation. The decluttering function
does not cause any new messages to be hidden. Rather, new messages are displayed on initial
occurrence as normal.
Should the CAS function of both DCUs fail, a red X is displayed across the full CAS message
block.
Crew Alerting Message De-Clutter
Figure 03−10−21
EICAS Comparator Monitoring
All of the EICAS warning and caution messages and accompanying aural alerts, issued by one
DCU, are compared with the results of the other DCU. An EICAS status message of CAS
MISCOMP is displayed, should the two DCUs disagree for a particular message or aural alert.
Each DCU continually cross-checks engine data processed by the other DCU. A caution
message of EICAS COMP INOP is displayed, should either DCU circuitry lose this ability to
cross check engine data.
Takeoff Configuration Warning
Certain warning messages are triggered by the DCUs, should a takeoff be commenced when
the aircraft is not in the proper takeoff configuration. The takeoff configuration warning function
is armed on the ground when both thrust levers of both engines are advanced above 70% N1.
The takeoff configuration warning condition is accompanied by a voice warning, EICAS takeoff
configuration warning message and flashing MASTER WARNING/CAUTION switch/lights.
AURAL/VISUAL WARNING SYSTEM
Description
Vol. 2 03−10−22
　
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