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┃ A~7-~'M" A321 ┃ GENERAL ┃SEQ 001 ┃REV 28 ┃
┃ FLIGHT CREW OPERATING MANUAL ┃ ┃ ┃ ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━━━━━━━┻━━━━┻━━━━┛
The ice and rain protection system allows unrestricted operation of the aircraft in icing
conditions and heavy rain.
ANTI-ICING
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
Wipers and when necessary, fluid rain repellent, remove rain from the front windshield
panels.
WINDOW
HEATING
PROBE HEATING
(FOR LOCATION REFER TO 1-34-10)
N MAST
CCM ALL
┏━━━━━━━━━━━━━━━━┳━━━━━━━━━━━━┳━━━━━━━━━━━┓
┃I -~ A318 ┃ICE AND RAIN PROTECTION ┃1.30.20 P 1 ┃
┃ .-,,.8, ,, ~L,~ A319 ┃ ┃ ┃
┃ ┃ ┣━━━━━┳━━━━━┫
┃ Lli,~ A320 ┃ ┃SEQ 010 I ┃I REV 34 ┃
┃ A~7-~'M" A321 ┃ WING ANTI ICE ┃ ┃ ┃
┃ FLIGHT CREW OPERATING MANUAL ┃ ┃ ┃ ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━━━━━━━┻━━━━━┻━━━━━┛
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 (see 1.36.10).
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.
CCM ALL
┏━━━━━━━━━━━━━━━━┳━━━━━━━━━━━━━━━┳━━━━━━━━━━━┓
┃ ┃ ┃1.30.20 P 2 ┃
┃ ┃ ┣━━━━━┳━━━━━┫
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本文链接地址：
AIRBUS A320 Flight Crew Operating Manual3(166)
