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CONTROL SWITCHES AND FUNCTION
Switches located on the ANTI-ICE panel control windshield and window heat. The L WSHLD/WINDOW switch controls the left windshield and left window. The R WSHLD/WINDOW switch controls the right windshield and right window.
Overheat protection circuits for each windshield or window remove power from the affected surface during an overheat condition. Selecting the L (R) WSHLD/WINDOW off de-energizes the applicable windshield and window and resets the temperature controller.
Volume 2 Flight Crew Operating Manual May 06/2005 CSP 100-6 REV 2
14-01-08 CONTROLS AND INDICATIONS
DESCRIPTION
The ANTI-ICE control panel located on the center pedestal is used to operate the anti-ice systems.
Anti-ice system operation and fault presentation is provided on the ANTI-ICE synoptic display. The ANTI-ICE synoptic display monitors the pneumatically-operated anti-icing and ice detection systems.
ANTI-ICE CONTROL PANEL
CFO1401002_001
May 06/2005 Flight Crew Operating Manual Volume 2 REV 2 CSP 100-6
14-01-09
ICE AND RAIN PROTECTION
CONTROLS AND INDICATIONS (Cont) ANTI-ICE SYNOPTIC PAGE
The ANTI-ICE synoptic page is used to monitor the pneumatically operated anti-icing and ice detection systems.
Volume 2 Flight Crew Operating Manual May 06/2005 CSP 100-6 REV 2
14-01-10 EICAS MESSAGES
The ice and rain protection system messages are shown on the EICAS. In the table below, the ice and rain protection system messages are listed. A brief explanation of each message is provided.
MESSAGE INHIBITS MEANING AURAL WARNING
WING ANTI-ICE LEAK A leak has been detected along the wing anti-ice ducting
L (R) WING OVERHEAT A wing anti-ice overheat condition exists in the indicated wing
L (R) ENG ANTI-ICE FAIL TO Bleed air pressure to the respective nacelle is too low for effective anti-icing, or the electrically heated T2 heater has failed when the respective L or R ENG switch is ON
ICE DETECTED TO/LAND Ice has been detected, and both the engine and wing anti-ice systems are not selected on
ICE DETECTOR FAIL TO/LAND Both ice detectors have failed
L (R) PITOT HEAT FAIL TO/LAND The respective pitot mast or base heater has failed
L (R) PROBE HEAT OFF TO/LAND Probe heat is off
STBY PITOT HEAT FAIL TO/LAND The standby pitot heater has failed
STBY STAT HEAT FAIL TO/LAND The respective standby static heater has failed
L (R) WING A/I LOW TEMP TO/LAND Indicates that the respective wing has an anti-ice low temperature condition
L (R) WING ANTI-ICE FAIL TO/LAND The respective anti-ice system has failed
WINDOW 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 condensa-tion (fog) on the window
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