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also be indicated by the formation of condensation
(fog) on the window
WING ANTI-ICE FAULT TO/LAND
Both outboard wing leading-edge sensors have
failed
WING A/ICE LOOP
FAIL TO
Both detection loops failed. This is only checked
during power up self-test
L (R) WING A/I PRESS
HI TO/LAND
High pressure has been sensed in the wing antiice
system
REV 4
ICE AND RAIN PROTECTION
Volume 2 Flight Crew Operating Manual Sep 14/2005
14-01-12 CSP 100-6 REV 4
EICAS MESSAGES (Cont)
MESSAGE INHIBITS MEANING
AURAL
WARNING
L (R) WSHLD HEAT
FAIL TO/LAND
The respective window heat has failed, and the
temperature is too low or too high. a failure may
also be indicated by the formation of ice or condensation
(fog) on the windshield
L (R) AOA CASE HEAT
FAIL TO/LAND
The respective angle-of-attack case heater has
failed
L (R) ENG A/ICE FAIL
ON TO/LAND
The respective engine nacelle anti-ice has failed
ON. If the T2 probe heater has failed on, an
amber “T2” icon will be displayed on the anti-ice
synoptic. If engine anti-ice bleed air has failed
on, a green flow line will be displayed downstream
of the failed anti-ice valve on the synoptic
ICE DETECTED TO/LAND
Ice has been detected and the engine and wing
anti-ice systems are selected on
ICE DETECTOR FAULT TO/LAND
One ice detector has failed; the other should
continue to operate normally
L (R) PROBE HT CTRL
FAIL TO/LAND
The respective probe heat controller has failed.
The probe heat will fail ON
TAT HEAT FAIL TO/LAND
The total air temperature probe heater has
failed
WING SOURCE
XBLEED TO/LAND Wing crossbleed valve is open
WING ANTI-ICE FAULT TO/LAND
One channel has failed on the outboard wing
leading-edge sensor. The wing anti-ice should
work normally
L (R) ENGINE ANTI-ICE
ON
The respective (or both) ENG ANTI-ICE
switch(es) is/are ON
ENGINE ANTI-ICE ON The respective (or both) ENG ANTI-ICE
switch(es) is/are ON
PROBE HEAT TEST OK The pilot initiated probe heat test has passed.
WING ANTI-ICE ON The WING ANTI-ICE switch is selected ON
WING/ENG ANTI-ICE
ON
The wing and both engine anti-ice systems are
ON
WING SOURCE
XBLEED
Either FROM L or FROM R has been selected
on the ANTI-ICE WING SOURCE switch
ICE AND RAIN PROTECTION
Sep 13/2004 Flight Crew Operating Manual Volume 2
REV 1 CSP 100-6 14-01-13
EICAS MESSAGES (Cont)
MESSAGE INHIBITS MEANING
AURAL
WARNING
L (R) AOA CASE HEAT
FAIL TO/LAND
The respective angle-of-attack case heater has
failed
L (R) ENG A/ICE FAIL
ON TO/LAND
The respective engine nacelle anti-ice has failed
ON. If the T2 probe heater has failed on, an
amber “T2” icon will be displayed on the anti-ice
synoptic. If engine anti-ice bleed air has failed
on, a green flow line will be displayed downstream
of the failed anti-ice valve on the synoptic
ICE DETECTED TO/LAND
Ice has been detected and the engine and wing
anti-ice systems are selected on
ICE DETECTOR FAULT TO/LAND
One ice detector has failed; the other should
continue to operate normally
L (R) PROBE HT CTRL
FAIL TO/LAND
The respective probe heat controller has failed.
The probe heat will fail ON
TAT HEAT FAIL TO/LAND
The total air temperature probe heater has
failed
WING SOURCE
XBLEED Wing xbleed valve open
WING ANTI-ICE FAULT TO/LAND
One channel has failed on the outboard wing
leading-edge sensor. The wing anti-ice should
work normally
L (R) ENGINE ANTI-ICE
ON
The respective (or both) ENG ANTI-ICE
switch(es) is/are ON
ENGINE ANTI-ICE ON The respective (or both) ENG ANTI-ICE
switch(es) is/are ON
PROBE HEAT TEST OK The pilot initiated probe heat test has passed.
WING ANTI-ICE ON The WING ANTI-ICE switch is selected ON
WING/ENG ANTI-ICE
ON
The wing and both engine anti-ice systems are
ON
WING SOURCE
XBLEED
Either FROM L or FROM R has been selected
on the ANTI-ICE WING SOURCE switch

　
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