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FAULT lt : Comes on in amber, with an ECAM caution, if the position of the anti-ice valve
disagrees with the ENG pushbutton selection.
Note: The amber FAULT light comes on briefly, while the valve transits.
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
ICE AND RAIN PROTECTION
ENGINE ANTI-ICE - WARNINGS AND CAUTIONS
A330/A340 FLEET DSC-30-30-30 P 1/2
FCOM 19 AUG 10
WARNINGS AND CAUTIONS
Applicable to:
E/WD: FAILURE TITLE
conditions
AURAL
WARNING
MASTER
LIGHT
SD PAGE
CALLED
LOCAL
WARNING
FLT PHASE
INHIB
ENG 1(2)(3)(4) VALVE CLOSED
valve disagree
ENG 1(2)(3)(4) VALVE OPEN
valve disagree
SINGLE
CHIME
MASTER
CAUT NL
ENG
affected
ANTI ICE
FAULT
It
3. 4. 5
7. 8
MEMO DISPLAY
“ENG A.ICE” appears in green, if one ENG ANTI ICE pushbutton is ON, or if the nacelle anti-ice
valves are opened.
If the ice detection system is installed on the aircraft, “ICE NOT DET” appears in green if ice is no
longer detected after 130 s.
WARNINGS AND CAUTIONS
Applicable to: ,
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
ICE AND RAIN PROTECTION
ENGINE ANTI-ICE - WARNINGS AND CAUTIONS
A330/A340 FLEET DSC-30-30-30 P 2/2
FCOM 19 AUG 10
E/WD: FAILURE TITLE
conditions
AURAL
WARNING
MASTER
LIGHT
SD PAGE
CALLED
LOCAL
WARNING
FLT PHASE
INHIB
ENG 1(2) VALVE CLOSED
valve disagree
ENG 1(2) VALVE OPEN
valve disagree
SINGLE
CHIME
MASTER
CAUT NL
ENG
affected
ANTI ICE
FAULT
It
4. 5
7. 8
MEMO DISPLAY
“ENG A.ICE” appears in green, if one ENG ANTI ICE pushbutton is ON, or if the nacelle anti-ice
valve’s electrical power is lost.
ICE NOT DET appears in green, if ice is no longer detected after 130 seconds.
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
ICE AND RAIN PROTECTION
ENGINE ANTI-ICE - ELECTRICAL SUPPLY
A330/A340 FLEET DSC-30-30-40 P 1/2
FCOM 19 AUG 10
BUS EQUIPMENT LIST
Applicable to:
NORM EMER ELEC
AC DC DC BAT AC ESS DC ESS HOT
ENG ENG 1 and ENG 3 DC2
ANTI ICE
CLOSURE ENG 2 and ENG 4 DC1
BUS EQUIPMENT LIST
Applicable to: ,
NORM EMER ELEC
AC DC DC BAT AC ESS DC ESS HOT
ENG ENG 1 DC1
ANTI ICE
CLOSURE ENG 2 DC2
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
ICE AND RAIN PROTECTION
ENGINE ANTI-ICE - ELECTRICAL SUPPLY
Intentionally left blank
A330/A340 FLEET DSC-30-30-40 P 2/2
FCOM 19 AUG 10
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
ICE AND RAIN PROTECTION
WINDOW HEAT - DESCRIPTION
A330/A340 FLEET DSC-30-40-10 P 1/2
FCOM 19 AUG 10
DESCRIPTION
Applicable to:
The aircraft uses electrical heating for anti icing each windshield and demisting the cockpit side
windows.
Two independent Window Heat Computers (WHC), one on each side, automatically regulate the
system and protect it against overheating and indicate faults.
Window heating comes on :
automatically when engine ‐ 2 or 3 is running, or in flight
‐ manually when the flight crew switches ON the PROBE/WINDOW HEAT pushbutton switch.
The windshield heating operates at low power on the ground and at normal power in flight.
Only one heating level exists for the windows.
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
ICE AND RAIN PROTECTION
WINDOW HEAT - DESCRIPTION
A330/A340 FLEET DSC-30-40-10 P 2/2
FCOM 19 AUG 10
DESCRIPTION
Applicable to: ,
The aircraft uses electrical heating for anti icing each windshield and demisting the cockpit side
windows.
Two independent Window Heat Computers (WHC), one on each side, automatically regulate the
system and protect it against overheating and indicate faults.
Window heating comes on :
automatically when at least one ‐ engine is running, or in flight
‐ manually when the flight crew switches ON the PROBE/WINDOW HEAT pushbutton switch.
The windshield heating operates at low power on the ground and at normal power in flight.
Only one heating level exists for the windows.
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
ICE AND RAIN PROTECTION
WINDOW HEAT - CONTROLS AND INDICATORS
A330/A340 FLEET DSC-30-40-20 P 1/2
FCOM 19 AUG 10
OVERHEAD PANEL
Applicable to: ALL
(Refer to DSC-36-20 OVERHEAD PANEL)
　
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