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Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
ENGINE INDICATION AND CREW ALERTING SYSTEM (CONT'D)
The following table defines the conditions for a takeoff configuration warning annunciation. The
warning is automatically removed when the configuration error is corrected.
Takeoff Configuration Warnings
CONDITION VOICE WARNING EICAS MESSAGE
AUTOPILOT ENGAGED “CONFIG AUTOPILOT” CONFIG AP
FLAPS NOT SET FOR TAKEOFF “CONFIG FLAPS” CONFIG FLAPS
ALL SPOILERS NOT IN TAKEOFF
POSITION
“CONFIG SPOILERS” CONFIG SPOILERS
HORIZONTAL STAB NOT IN TAKEOFF
RANGE
“CONFIG TRIM” CONFIG STAB
PARKING BRAKE SET “CONFIG BRAKES” PARKING BRAKE
Inhibited EICAS Caution Messages
During the takeoff and landing phases of flight, the DCUs inhibit the display of certain EICAS
messages that may be distracting to the flight crew. Generally, these are messages that do not
require immediate crew action during takeoff and landing.
Message Inhibit – Takeoff
During takeoff, the DCUs inhibit caution messages that are not considered critical. The takeoff
phase, for the purpose of caution message inhibiting, occurs when the following conditions are
set:
• Aircraft is on the ground;
• Both engines are operating above 79% N1; and
• Aircraft airspeed has transitioned from below 80 knots to above 80 knots.
The DCUs remove the takeoff inhibit conditions, permitting the display of any caution message,
when one of the following conditions are set:
• Aircraft has climbed above 400 feet of radio altitude;
• Both engines are operating below 79% N1; or
• 30 seconds since takeoff inhibit conditions were set.
Not all caution messages are inhibited during takeoff. Some messages relate to systems or
conditions that may require pilot attention during takeoff. See the following table for a list of
caution messages that will not be inhibited.
AURAL/VISUAL WARNING SYSTEM
Description
Vol. 2 03−10−23
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
ENGINE INDICATION AND CREW ALERTING SYSTEM (CONT'D)
Caution Messages Remaining Available During Takeoff
System Message
Power Plant APR CMD SET
APR INOP
L (R) REV UNLOCKED
Fuel L (R) FUEL LO PRESS
Flight Controls ELEVATOR SPLIT
GND SPLRS DEPLOY
Landing Gear A/SKID INBD (OUTBD)
INBD (OUTBD) BRAKE PRESS
Instruments EFIS COMP MON
L PITOT TUBE HEAT
Message Inhibit – Landing
• During the approach to landing, the DCUs inhibit the display of certain caution
messages that are not considered critical. The landing phase, for the purpose of
caution message inhibiting, occurs when the following conditions are set:
• Aircraft is in the air;
• Any landing gear is down and locked; and
• Aircraft altitude has transitioned from >200 ft to <200 ft radio altitude.
The DCUs remove the landing inhibit conditions, permitting the display of any caution
message, when one of the following conditions are set:
• Radio altitude returns to above 200 feet radio altitude;
• 30 seconds after aircraft has transitioned from air to ground (WOW); or
• 90 seconds since landing inhibit conditions were set.
Not all caution messages are inhibited during landing. Some messages relate to systems or
conditions that may require pilot attention during landing. See the following table for a list of
EICAS caution messages that will not be inhibited.
AURAL/VISUAL WARNING SYSTEM
Description
Vol. 2 03−10−24
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
ENGINE INDICATION AND CREW ALERTING SYSTEM (CONT'D)
Caution Messages Remaining Available During Landing
System Message
Power Plant APR INOP
APR CMD SET
L (R) REV UNLOCKED
L (R) REV UNSAFE
Fuel L (R) FUEL LO PRESS
FUEL IMBALANCE
Hydraulics HYD 3 LO PRESS
Flight Controls ELEVATOR SPLIT
FLAPS FAIL
FLT SPLRS
FLT SPLRS DEPLOY
GND SPLRS
GND SPLRS DEPLOY
GND SPLRS NOT ARMED
STAB TRIM
Fire Protection APU BTL LO
ENG BTL 1 (2) LO
Landing Gear A/SKID INBD (OUTBD)
INBD (OUTBD) BRAKE PRESS
STEERING INOP
WOW INPUT (OUTPUT)
PROX SYS
Autopilot AP PITCH TRIM
AP TRIM IS LWD (RWD) (ND) (NU)
Instruments EFIS COMP MON
L PITOT TUBE HEAT
Aural Alerts
EICAS aural alerts are initiated by the DCU, processed by the audio integrating system, and
played through the flight deck speakers. There are two categories of aural alerts: aural tones and
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庞巴迪挑战者605机组操作手册 CL605-AURAL_and_VISUAL_WARNING_S(7)
