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CSP 700−5000−6
Volume 2
14−10−18
ICE AND RAIN EICAS MESSAGES
L−R WINDOW HEAT FAIL
Indicates that the
respective window heater
temperature controller has
failed.
ICE
Indicates that ice has been
detected and one or the other
system is OFF.
WING A/ICE OVHT
Indicates that an overtemperature
has been detected in the wing
antiice
system.
L−R WING A/ICE FAIL
Indicates that the wing antiice
valve is not in the selected
position.
PITOT 1−2−3 HT FAIL
Indicates that the respective
pitot heater has failed.
WING A/ICE LEAK
Indicates that a bleed leak has been
detected in the wing antiice
system.
STBY PITOT HEAT FAIL
Indicates that the standby pitot
heater has failed.
ICE DETECTOR FAIL
Indicates the loss of both
ice detectors.
L−R COWL A/ICE FAIL
Indicates that the cowl antiice
valve is not in the selected
position.
L−R WSHLD HEAT FAIL
Indicates that the respective
windshield heater temperature
controller has failed.
L−R AOA HEAT FAIL
Indicates that respective
AOA has failed.
WING A/ICE LO HEAT
Indicates that there is insufficient
heat in the wing leading edge duct.
GF1410_029a
R AOA HEAT FAIL
ICE DETECTOR FAIL
L AOA HEAT FAIL
ICE
L WINDOW HEAT FAIL
L COWL A/ICE FAIL
R COWL A/ICE FAIL
R WING A/ICE FAIL
R WINDOW HEAT FAIL
L WING A/ICE FAIL
L WSHLD HEAT FAIL
R WSHLD HEAT FAIL
PITOT 1 HT FAIL
WING A/ICE OVHT
PITOT 2 HT FAIL
PITOT 3 HT FAIL
STBY PITOT HT FAIL
WING A/ICE LEAK
WING A/ICE LO HEAT
ICE AND RAIN PROTECTION
Rev 3, Apr 25, 2005 Flight Crew Operating Manual
CSP 700−5000−6
Volume 2
14−10−19
ICE AND RAIN EICAS MESSAGES (CONT'D)
ICE DETECTOR FAULT
Indicates that there is a loss of
one ice detector.
L−R PROBE MON FAIL
Indicates that the heater status
of the probes and associated
systems is not verified.
TAT HT 1−2−3 FAIL
Indicates that the respective
TAT heater has failed.
WING A/ICE FAULT
Indicates loss of redundancy
on wing antiice
system.
ICE
Indicates that cowl or wing antiicing
has
been detected with antiice
systems ON.
WING A/ICE SENSOR
Indicates loss of both outboard
wing antiice
temperature
sensors.
L−R COWL A/ICE FAULT
Indicates that there is a loss of
the affected cowl antiice.
YD HEAT 1−2 FAIL
Indicates that the respective
yaw damper heater has failed.
GF1410_030a
R PROBE MON FAIL
L PROBE MON FAIL
TAT HT 3 FAIL
TAT HT 1 FAIL
TAT HT 2 FAIL
WING A/ICE FAULT
WING A/ICE SENSOR
R COWL A/ICE FAULT
TAT 3 FAIL
TAT 1 FAIL
TAT 2 FAIL
ICE DETECTOR FAULT
L COWL A/ICE FAULT
ICE
YD HEAT 1 FAIL
YD HEAT 2 FAIL
TAT 1−2−3 FAIL
Indicates that the respective
TAT has failed.
ICE AND RAIN PROTECTION
Flight Crew Operating Manual Rev 3, Apr 25, 2005
CSP 700−5000−6
Volume 2
14−10−20
ICE AND RAIN EICAS MESSAGES (CONT'D)
L−R COWL A/ICE ON
Indicates that the respective cowl
antiice
has been selected ON.
L−R WSHLD HEAT OFF
Indicates that the respective
temperature controller
selector is selected to
OFF/RESET.
WING XBLEED FROM L − R
Indicates that wing antiice
is
being supplied from the
selected side.
WING A/ICE AUTO
Indicates that wing antiice
has been selected to AUTO.
WING A/ICE ON
Indicates that wing antiice
has been selected ON.
L−R COWL A/ICE AUTO
Indicates that the
respective cowl antiice
has been selected to AUTO.
GF1410_031
L COWL A/ICE AUTO
R COWL A/ICE AUTO
L COWL A/ICE ON
R COWL A/ICE ON
L WSHLD HEAT OFF
R WSHLD HEAT OFF
WING A/ICE AUTO
WING A/ICE ON
WING XBLEED FROM L
WING XBLEED FROM R
ICE AND RAIN PROTECTION
Rev 3, Apr 25, 2005 Flight Crew Operating Manual
CSP 700−5000−6
Volume 2
14−10−21
ICE AND RAIN PROTECTION
Flight Crew Operating Manual Rev 3, Apr 25, 2005
CSP 700−5000−6
Volume 2
14−10−22
THIS PAGE INTENTIONALLY LEFT BLANK
CB - ICE SYSTEM
GF1420_001
STAT SYS BUS PREV CNTL TEST
PAGE
　
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