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    PNEUMATIC SYSTEM

    AIR

    P 1

    MAY 98

    001

    1.03.20

    20.1 DESCRIPTION (See schematic p 7/8)

    Compressed air is bled from the engine compressors at the LP or HP stages.The pneumatic system consists of all the systems designed to supply air to thevarious aircraft systems, zones or engines, with associated control, monitoring andindicating components. It supplies under pressure air for air conditioning,pressurization and ice protection system. A protection against overheat due to possible leakage around the hot air ducts isprovided.

    AIR BLEED- Air conditioning and pressurizationThe system is designed to :S select the compressor stage from which air is bled, depending on the pressure

    and/or temperature existing at these stages.S regulate air pressure in order to avoid excessive pressuresAir is generally bled from the low compressor stage (LP). At low engine speed whenpressure from LP stage is insufficient, air source is automatically switched to thehigh compressor stage HP. (This may occur on ground and during descent at F.I.).Transfer of air is achieved by means of a pneumatically operated and electrically

    controlled b tterfl al e (HP al e) hich remains closed in absence of electrical

    AA

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    PNEUMATIC SYSTEM

    AIR

    P 2

    NOV 99

    100

    1.03.20

    CROSSFEED

    The crossfeed valve installed on the crossfeed duct is designed to connect LH and RHair lbeed systems.- On the ground, it is always open except when both engines are running and

    propeller brake is disengaged.- In flight, the crossfeed valve is normally closed. This is a spring loaded closed,

    solenoid controlled, pneumatic shut off valve. The valve is closed with solenoiddeenergized.

    LEAK DETECTION SYSTEM

    A continuous monitoring system is installed in order to detect overheat due to ductleakage and to protect the structure and components in the vicinity of hot air ducts :- Wing leading edge and wing to fuselage fairing,- Upper and lower fuselage floor,- Air conditioning pack area.

    In order to ensure rapid leak sensing, a Kevlar envelope is installed around the majorpart of the high temperature ducts to collect and direct leaking air to the sensingelements.The sensing system includes two single loop detection assemblies, one for the RH

    d f th LH i d t t

    AA

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    PNEUMATIC SYSTEM

    AIR

    P 3

    NOV 99

    100

    1.03.20

    20.2 CONTROLS

    AIR BLEED PANEL

    TOFA010320003100AA

    AA

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    PNEUMATIC SYSTEM

    AIR

    P 5

    NOV 99

    100

    1.03.20

    MFC LOGIC

    See chapter 1.01

    SYSTEM MONITORING

    The following conditions are monitored by visual and aural alerts :

    - Bleed valve position in disagree with command.D See BLEED VALVE FAULT procedure in chapter 2.05.08

    - Overheat in bleed duct (T ductu 274C/525F).D See BLEED OVHT procedure in chapter 2.05.08

    - Bleed air leak (Loopu 153C/307F).D See BLEED LEAK procedure in chapter 2.05.08

    AA

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    ATR 42 Model : 500

    PNEUMATIC SYSTEM

    AIR

    P 7/8

    NOV 99

    001

    1.03.20

    20.5 SCHEMATIC

    AA

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    ATR 42 Model : 500

    PNEUMATIC SYSTEM

    AIR

    P 7/8

    NOV 99

    400

    1.03.20

    20.5 SCHEMATIC

    AA

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    AIR CONDITIONING

    AIR

    P 2

    NOV 99

    090

    1.03.30

    AIR VENTILATION

    Conditioned air is blown into the cabin by outlet ramps located under the hot racksthrough two electrical isolating valves (CAB VENT).

    It is then evacuated through guides along the cabin side walls at floor level. A part ofit is recirculated by the fans, the other part being evacuated overboard through theoutflow valves installed in the rear under floor.

    The toilet is ventilated by differential pressure through a vent line.

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    AIR CONDITIONING

    AIR

    P 2

    NOV 99

    090

    1.03.30

    AIR VENTILATION

    Conditioned air is blown into the cabin by outlet ramps located under the hot racksthrough two electrical isolating valves (CAB VENT).

    It is then evacuated through guides along the cabin side walls at floor level. A part ofit is recirculated by the fans, the other part being evacuated overboard through theoutflow valves installed in the rear under floor.

    The toilet is ventilated by differential pressure through a vent line.

    AA

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    AIR CONDITIONING

    AIR

    P 10

    NOV 99

    090

    1.03.30

    30.3 ELECTRICAL SUPPLY/MFC LOGIC/SYSTEM MONITORING

    ELECTRICAL SUPPLY

    EQUIPMENTDC BUS SUPPLY

    (C/B)

    LH SIDEPack valve DC ESS BUS

    (on lateral panel PACK VALVE)

    Recirculation fan DC UTIL BUS 1

    (on lateral panel PWR SUPPLY CTL)Pack and recirculation fan alert DC ESS BUS

    (on lateral panel PACK and RECIRC FANCAUTION)

    FLT COMPTautomatic temperature control

    DC ESS BUS(on lateral panel AUTO)

    FLT COMPT Manualtemperature control

    DC ESS BUS(on lateral panel MAN)

    RH SIDE

    AA

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    AIR CONDITIONING

    AIR

    P 10

    NOV 99

    410

    1.03.30

    30.3 ELECTRICAL SUPPLY/MFC LOGIC/SYSTEM MONITORING

    ELECTRICAL SUPPLY

    EQUIPMENTDC BUS SUPPLY

    (C/B)

    LH SIDEGround cooling fan DC BUS 1

    (on lateral panel GND COOLING FAN CTL)

    Pack valve DC ESS BUS

    (on lateral panel PACK VALVE)Recirculation fan DC UTIL BUS 1

    (on lateral panel PWR SUPPLY CTL)

    Pack and recirculationfan alert

    DC ESS BUS(on lateral panel PACK and RECIRC FAN

    CAUTION)

    FLT COMPTautomatic temperaturecontrol

    DC ESS BUS(on lateral panel AUTO)

    AA

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    R Mod : 4273 ATR 42 Model : 500

    AIR CONDITIONING

    AIR

    P 15/16

    NOV 99

    090

    1.03.30

    AA

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    Mod : 4273 ATR 42 Model : 400

    AIR CONDITIONING

    AIR

    P 15/16

    NOV 99

    410

    1.03.30

    AA

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