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• A triple chime
• Flashing master warning lights
• Red light on the faulted control switch, or a red indication on EFIS, EICAS, or a synoptic
page
Warning messages, in addition to the above indication, can also generate one or both of the
following:
• Aural warning tone
• Voice message
Pressing either master warning switch/light:
• Silences the aural alerts
• Stops the master warning lights from flashing
• Resets the switch/light to allow it to indicate another fault
AURAL/VISUAL WARNING SYSTEM
Description
Vol. 2 03−10−11
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
CONTROLS AND INDICATORS (CONT'D)
Caution Messages
Caution messages are second in order of importance. Caution messages are presented in
amber on the primary page and appear directly below any warning messages that may be
displayed. It is possible to have more than one page of caution messages. The CAS pushbutton
on the ECP allows the pilot to page forward and backward to view the entire list of caution
messages. During flight or on the ground when both engines are stabilized at idle, caution
message(s) can be removed from view or recalled to the screen by pressing the CAS key on the
ECP. A white MSGS icon will appear, advising the crew that the caution message(s) are out of
view. Pressing the CAS button a second time will cause the caution message(s) to reappear.
DCU generation of a new caution message will remove the MSGS icon and the new message
will be displayed on the top of the caution message stack.
Caution messages require prompt action and are always accompanied by:
• A single chime
• Flashing master caution lights
• Amber light on the faulted control switch, or an amber indication on EFIS, EICAS, or a
synoptic page
Pressing either master caution switch/light:
• Stops the flashing of the master caution lights
• Resets the master caution switch/light to allow it to annunciate another fault
Advisory Messages
Green advisory messages are presented at the top of the status page. Advisory messages
cannot be removed from view until the cause is deselected or deactivated. Advisory messages
are used to advise of:
• Aircraft configuration for a particular phase of flight
• Successful system test
• Confirmation of SOV closure
• SELCAL
Status Messages
White status message are presented on the status page and appear directly below any advisory
messages that may be present. Status message(s) can be removed from view or recalled to the
screen by pressing the STAT key on the ECP. A white MSGS icon will appear, advising the crew
that the status message(s) are out of view. Pressing the STAT button a second time will allow
the status message(s) to reappear. DCU generation of a new status message will remove the
MSGS icon and the new message will be displayed on the top of the status message stack.
Status messages are used to inform of:
• Status of a specific system that has been manually or automatically
activated/deactivated
• Low-priority system failures
AURAL/VISUAL WARNING SYSTEM
Description
Vol. 2 03−10−12
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
CONTROLS AND INDICATORS (CONT'D)
Takeoff Configuration Warning
The takeoff configuration warnings (TOC) are armed on the ground when both engines accelerate
as a result of thrust levers being advanced above 70% N1. A voice warning, an EICAS warning
message and flashing red Master Warning annunciators are provided for any of the following
conditions:
Takeoff Configuration Warnings
CONDITION VOICE WARNING EICAS MESSAGE MASTER WARNING
AUTOPILOT ENGAGED “CONFIG AUTOPILOT” CONFIG AP FLASHES
FLAPS NOT SET FOR
TAKEOFF
“CONFIG FLAPS” CONFIG FLAPS FLASHES
ALL SPOILERS NOT IN
TAKEOFF POSITION
“CONFIG SPOILERS” CONFIG SPOILERS FLASHES
HORIZONTAL STAB NOT
IN T/O RANGE
“CONFIG TRIM” CONFIG STAB FLASHES
PARKING BRAKE SET “CONFIG BRAKES” PARKING BRAKE FLASHES
All TOC warnings are cancelled when the configuration error is corrected.
Inhibited EICAS Caution Messages
During takeoff and landing, the DCU inhibits distracting EICAS caution messages. The logic
inhibits messages during takeoff when the left and right engine N1 are greater or equal to 79% and
above 80 kts with weight-on-wheels. On landing, the messages are inhibited when radio altitude is
less than 400 feet above ground level (AGL) with landing gear extended.
The inhibited logic is removed when:
　
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