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A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
ICE AND RAIN PROTECTION
GENERAL - DESCRIPTION
A318/A319/A320/A321 FLEET DSC-30-10-10 P 1/4
FCOM 19 AUG 10
GENERAL
Applicable to: ALL
The ice and rain protection system allows unrestricted operation of the aircraft in icing conditions and
heavy rain.
ANTI-ICING
Applicable to: ALL
Either hot air or electrical heating protects critical areas of the aircraft as follows.
HOT AIR
‐ three outboard leading-edge slats of each wing.
‐ engine air intakes.
ELECTRICAL HEATING
‐ flight compartment windows.
‐ sensors, pitot probes and static ports.
‐ waste-water drain mast.
RAIN REMOVAL
Applicable to:
,
,
MSN,,,,
Wipers and when necessary, fluid rain repellent, remove rain from the front windshield panels.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
ICE AND RAIN PROTECTION
GENERAL - DESCRIPTION
A318/A319/A320/A321 FLEET DSC-30-10-10 P 2/4
FCOM 19 AUG 10
RAIN REMOVAL
Applicable to:
Wipers remove rain from the front windshield panels.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
ICE AND RAIN PROTECTION
GENERAL - DESCRIPTION
A318/A319/A320/A321 FLEET DSC-30-10-10 P 3/4
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
ICE AND RAIN PROTECTION
GENERAL - DESCRIPTION
Intentionally left blank
A318/A319/A320/A321 FLEET DSC-30-10-10 P 4/4
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
ICE AND RAIN PROTECTION
WING ANTI-ICE - DESCRIPTION
A318/A319/A320/A321 FLEET DSC-30-20-10 P 1/4
FCOM 19 AUG 10
DESCRIPTION
Applicable to:
, ,
MSN
In flight, hot air from the pneumatic system heats the three outboard slats (3-4-5) of each wing.
Air is supplied through one valve in each wing.
The WING pushbutton on the ANTI ICE panel controls the valves.
When the aircraft is on ground, the flight crew can initiate a 30-second test sequence by turning the
system ON.
If the system detects a leak during normal operation, the affected side’s wing anti-ice valve
automatically closes (Refer to DSC-36-10-50 LEAK DETECTION).
When wing anti-ice is selected, the N1 limit is automatically reduced, and the idle N1 is automatically
increased.
If the electrical power supply fails, the valves close.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
ICE AND RAIN PROTECTION
WING ANTI-ICE - DESCRIPTION
A318/A319/A320/A321 FLEET DSC-30-20-10 P 2/4
FCOM 19 AUG 10
DESCRIPTION
Applicable to: MSN
4566,,,
In flight, hot air from the pneumatic system heats the three outboard slats (3-4-5) of each wing.
Air is supplied through one valve in each wing.
The WING pushbutton on the ANTI ICE panel controls the valves.
When the aircraft is on ground, the flight crew can initiate a 30-second test sequence by turning the
system ON.
If the system detects a leak during normal operation, the affected side’s wing anti-ice valve
automatically closes (Refer to DSC-36-10-50 LEAK DETECTION).
When wing anti-ice is selected, the EPR limit is automatically reduced, and the idle EPR is
automatically increased.
If the electrical power supply fails, the valves close.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
ICE AND RAIN PROTECTION
WING ANTI-ICE - DESCRIPTION
A318/A319/A320/A321 FLEET DSC-30-20-10 P 3/4
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
ICE AND RAIN PROTECTION
WING ANTI-ICE - DESCRIPTION
Intentionally left blank
A318/A319/A320/A321 FLEET DSC-30-20-10 P 4/4
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
ICE AND RAIN PROTECTION
WING ANTI-ICE - CONTROLS AND INDICATORS
A318/A319/A320/A321 FLEET DSC-30-20-20 P 1/2
FCOM 19 AUG 10
OVERHEAD PANEL
Applicable to: ALL
(1) WING ANTI ICE pb sw
This switch controls the wing anti ice system on the left and right sides simultaneously.
ON : It lights up blue.
WING A. ICE appears on the ECAM MEMO page.
Wing anti ice control valves open if a pneumatic supply is available.
On the ground the wing anti-icing control valves open for 30 s only (test sequence).
Off : ON light goes off.
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A320机组操作手册FLIGHT CREW OPERATING MANUAL 3(74)
