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Flight in super-cooled large droplet icing (SLD) conditions may, but not necessarily be indicated by ice accretion on
side windows. Temperature controllers, one for each windshield and window, monitor the electrical resistance of the temperature
sensors that are embedded in the glass. The temperature controllers cycle power on and off to maintain a predetermined
glass surface temperature.
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.
CFO14001002_007
SIDE WINDOW
SENSING
ELEMENTS
BUS
BARS
SENSING
ELEMENTS
BUS
BARS
SIDE WINDOW
SENSING
ELEMENTS
ICE AND RAIN PROTECTION
May 06/2005 Flight Crew Operating Manual Volume 2
REV 2 CSP 100-6 14-01-09
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
ANTI-ICE
L
ON
R
ON
L
OFF
R
OFF
ENG
WSHLD/WINDOW
ON OFF OFF
L R
WING PROBES
L R
FROM
NORM
FROM
WING
SOURCE
ICE AND RAIN PROTECTION
Volume 2 Flight Crew Operating Manual May 06/2005
14-01-10 CSP 100-6 REV 2
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.
CFO0305002_009
CAS
CKLST SKIP
FRMT TFC ENTER
ELEC FLT HYD
L R
ECS FUEL
TR/WX SUMRY
COM1 NAV1 ATC1/TCAS ADF1 HF1 COM3 COM2
118.000 108.00 7777 1799.5 118.000 118.000
118.000 108.00 STBY 190.0 2.0000 118.000 118.000
ABV
TX 2.0000 AM
DN
UP
CAB ALT
CAB RATE
APU RPM
APU EGT
FUEL QTY LBS
TOTAL
N2
OIL PRESS
OIL TEMP
FF PPH
I T T
N1 NU
ND
STAB AIL
TRIM
LWD RWD
RUD
FLAPS GEAR
SPOILERS
7300
1000
0
61.0
600
84.7
46
115
7300
300
250
12000
6000 6000
93.0
84.7
46
115
7300
ST
A
RT
ST
A
RT
600
IGN IGN
85.0 MCT
MACH
HOLD
VIB VIB
FIRE
85.0 MCT
REV
L R
6.6
MSGS
60
PSI
45
PSI
ANTI-ICE
A/ICE
MFD CONTROL
AUTO PLAN
SHLDR SIDE
REV 2
ICE AND RAIN PROTECTION
Sep 14/2005 Flight Crew Operating Manual Volume 2
REV 4 CSP 100-6 14-01-11
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 antiice
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 antiice
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
　
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