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each cabin zone temperature that is selected from the cockpit, with a limited authority of ± 2.5 °C. ( ±
4.5 °F).
Low-pressure air is supplied to the mixing unit by a ground connection.
ARCHITECTURE
Applicable to:
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
AIR CONDITIONING / PRESSURIZATION / VENTILATION
AIR CONDITIONING - GENERAL
A318/A319/A320/A321 FLEET DSC-21-10-10 P 3/4
FCOM 19 AUG 10
ARCHITECTURE
Applicable to:
MSN,
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
AIR CONDITIONING / PRESSURIZATION / VENTILATION
AIR CONDITIONING - GENERAL
A318/A319/A320/A321 FLEET DSC-21-10-10 P 4/4
FCOM 19 AUG 10
ARCHITECTURE
Applicable to: ,
, MSN,,
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
AIR CONDITIONING / PRESSURIZATION / VENTILATION
AIR CONDITIONING - MAIN COMPONENTS
A318/A319/A320/A321 FLEET DSC-21-10-20 P 1/12
FCOM 19 AUG 10
AIR CONDITIONING PACK
Applicable to:
The two packs operate automatically and independently of each other. Pack operation is controlled
by pack controller signals.
Warm pre-conditioned bleed air enters the cooling path via the pack flow control valve, and is ducted
to the primary heat exchanger.
Then, the cooled bleed air enters the compressor section of the air-cycle machine and is compressed
to a higher pressure and temperature.
It is cooled again in the main heat exchanger and enters the turbine section, where it expands and, in
expanding, generates power to drive the compressor and cooling air fan.
The removal of energy during this process reduces air temperature, resulting in very low air
temperature at turbine discharge.
L3A water separator system dries the air before it enters the turbine section.
AIR CONDITIONING PACK
Applicable to:
,
,
MSN,,,,
The two packs operate automatically and independently of each other. Pack operation is controlled
by air conditioning system controller signals.
Warm pre-conditioned bleed air enters the cooling path via the pack flow control valve, and is ducted
to the primary heat exchanger.
Then, the cooled bleed air enters the compressor section of the air-cycle machine and is compressed
to a higher pressure and temperature.
It is cooled again in the main heat exchanger and enters the turbine section, where it expands and, in
expanding, generates power to drive the compressor and cooling air fan.
The removal of energy during this process reduces air temperature, resulting in very low air
temperature at turbine discharge.
L3A water separator system dries the air before it enters the turbine section.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
AIR CONDITIONING / PRESSURIZATION / VENTILATION
AIR CONDITIONING - MAIN COMPONENTS
A318/A319/A320/A321 FLEET DSC-21-10-20 P 2/12
FCOM 19 AUG 10
PACK SCHEMATIC (SIMPLIFIED)
Applicable to:
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
AIR CONDITIONING / PRESSURIZATION / VENTILATION
AIR CONDITIONING - MAIN COMPONENTS
A318/A319/A320/A321 FLEET DSC-21-10-20 P 3/12
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
AIR CONDITIONING / PRESSURIZATION / VENTILATION
AIR CONDITIONING - MAIN COMPONENTS
A318/A319/A320/A321 FLEET DSC-21-10-20 P 4/12
FCOM 19 AUG 10
PACK SCHEMATIC (SIMPLIFIED)
Applicable to:
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
AIR CONDITIONING / PRESSURIZATION / VENTILATION
AIR CONDITIONING - MAIN COMPONENTS
A318/A319/A320/A321 FLEET DSC-21-10-20 P 5/12
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
AIR CONDITIONING / PRESSURIZATION / VENTILATION
AIR CONDITIONING - MAIN COMPONENTS
A318/A319/A320/A321 FLEET DSC-21-10-20 P 6/12
FCOM 19 AUG 10
PACK SCHEMATIC (SIMPLIFIED)
Applicable to:
MSN,
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
AIR CONDITIONING / PRESSURIZATION / VENTILATION
AIR CONDITIONING - MAIN COMPONENTS
A318/A319/A320/A321 FLEET DSC-21-10-20 P 7/12
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
AIR CONDITIONING / PRESSURIZATION / VENTILATION
AIR CONDITIONING - MAIN COMPONENTS
A318/A319/A320/A321 FLEET DSC-21-10-20 P 8/12
FCOM 19 AUG 10
PACK SCHEMATIC (SIMPLIFIED)
Applicable to: ,
, MSN,,
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
　
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