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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 anti-ice system
Sep 14/2005 Flight Crew Operating Manual Volume 2 REV 4 CSP 100-6
14-01-11 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 con-densation (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 down-stream of the failed anti-ice valve on the synop-tic
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
Volume 2 Flight Crew Operating Manual Sep 14/2005 CSP 100-6 REV 4
14-01-12 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 down-stream of the failed anti-ice valve on the synop-tic
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