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Air Conditioning/Pressurization/Ventilation
65問 • 1年前
  • Angelo Ortiz
  • 通報

    問題一覧

  • 1

    Hot air FAULT light illuminates on the air conditioning panel:

    The hot air press reg. valve closes and the trim air valves close

  • 2

    In case of Air Conditioning System Controller dual lane failure:

    The related Pack is lost, and the hot air pressure regulating valve and associated trim air valves closes

  • 3

    During normal flight the Avionics Ventilation System controls the temperature of the cooling air by:

    Passing air through a skin heat exchanger

  • 4

    The RAM AIR switch should be used:

    Only when delta P is less than 1 psi

  • 5

    Air Conditioning System Controller, one lane failure will result in:

    The second lane takes over

  • 6

    Air Conditioning System Controller, both lanes fail:

    Pack is lost

  • 7

    Each Pack consists of heat exchangers, compressor and turbine. The purpose of the turbine is to:

    Drives the compressor, cooling air fan and also expands and cools the air.

  • 8

    The Mixer Unit connects to cabin fans, LP ground connector, emergency ram air inlet, Pack 1 and 2. The statement is:

    True

  • 9

    Hot air pressure regulating valve failed in open position:

    No effect

  • 10

    With bleed air supplied from the APU (APU bleed valve open), the pack flow is automatically selected:

    High

  • 11

    Each trim air valve optimizes the temperature by:

    Adding hot air

  • 12

    The hot air pressure regulating valves:

    Regulate the pressure of hot air tapped upstream of the packs

  • 13

    The pack flow control valve is:

    Pneumatically operated and electrically controlled

  • 14

    The temperature selectors are located in:

    Both (The cockpit) and (the cabin (FAP)) are correct

  • 15

    Pack flow may be selected from:

    The cockpit

  • 16

    When the cooling demand can’t be satisfied due to low bleed air pressure:

    The minimum idle is increased automatically

  • 17

    What is the maximum normal cabin alt:

    8,000 feet

  • 18

    What is the maximum negative differential pressure for the cabin:

    -1 psi

  • 19

    Is it recommended to use Packs and LP Ground Unit simultaneously during long stops on a hot airfield?

    No

  • 20

    Trim air valves are controlled by:

    The air conditioning system controller

  • 21

    The mixer unit is connected to:

    Packs, cabin air, emergency ram air inlet and LP ground connector

  • 22

    Once set to "ON" the air conditioning packs operate:

    Automatically and independently of each other

  • 23

    When the RAM AIR pushbutton is ON, the ram air valve will open:

    If ΔP < 1 psi and the DITCHING pushbutton is in normal position

  • 24

    Hot-Air Pressure-Regulating Valve is controlled by the:

    Air Conditioning System Controller 1

  • 25

    Conditioned air is normally distributed to:

    Cockpit, forward and aft cabins

  • 26

    The cabin zone temperature sensors are ventilated by the air extracted by the lavatory and galleys fans:

    True

  • 27

    Temperature regulation is automatic and is controlled by:

    Air conditioning system controllers

  • 28

    The Hot-Air Pressure-Regulating Valve closes automatically when;

    Both (Both lanes of the Air Conditioning System Controller 1 fails) and (Both lanes of the Air Conditioning System Controller 2 fails) are correct

  • 29

    The Hot-Air Pressure-Regulating Valve closes automatically when:

    Cockpit trim air valve or cabin trim air valves fail

  • 30

    When the pack flow control selector is positioned to HI, air flow is:

    120% of normal

  • 31

    When using APU bleed to supply the Packs, with the Pack Flow Selector at LO, the Pack air flow is:

    120% of normal

  • 32

    The pack flow control valve closes automatically in case of:

    Pack overheating, engine starting, or operation of the fire or ditching pushbutton pressed

  • 33

    Trim air valve failure

    The optimized temperature regulation of the corresponding zone is lost

  • 34

    There are how many trim air valves?

    3 - one for the cockpit and two for the cabin

  • 35

    During landing run, ram air inlet flaps open when the speed is less than:

    70 knots ( after a 20 sec delay)

  • 36

    When APU is supplying the packs, they send a demand signal to increase airflow when a zone temperature can’t be satisfied:

    To the APU ECB

  • 37

    When the ditching switch is selected ON, it sends a closure signal to:

    Both (Outflow valve) and (Ram air inlet, ventilation extract valves and the pack flow control valves) are correct

  • 38

    In flight, with pressure controller 1 in use, if it fails:

    Transfers automatically to controller 2

  • 39

    In normal operation, pressurization is:

    Fully automatic

  • 40

    The outflow valve is powered by:

    One of three electric motors

  • 41

    During ground operation, the outflow valve is:

    Fully open

  • 42

    To see the position of the outflow valve, it is necessary to call ECAM:

    PRESS Page

  • 43

    Two identical, independent, pressurization controllers are used for system control:

    One controller active, one in standby

  • 44

    Which controller generates excess cabin altitude and pressure outputs for ECAM indication in manual mode:

    N°1

  • 45

    When Ram Air pb is set to ON, the outflow valve will open 50% when delta P is:

    < 1 psi

  • 46

    The purpose of the safety valves is to avoid:

    Both (Excessive positive pressure differential) and (excessive negative pressure differential) are correct

  • 47

    The safety valves are operated:

    Pneumatically

  • 48

    When landing elevation is set to AUTO, the landing elevation is sent to the controller from:

    FMGC

  • 49

    When Mode SEL is set to MANUAL, the outflow valve is controlled by signals sent via controller 1 or 2:

    False

  • 50

    On ECAM CAB PRESS page, the outflow valve indicator changes to amber if:

    The valve opens more than 95% during flight

  • 51

    On ECAM CAB PRESS page, the safety valve indication changes to amber if:

    Either valve is not closed

  • 52

    On ECAM CAB PRESS page the cabin altitude indicator changes to red when the cabin altitude is:

    > 9, 550 feet

  • 53

    Following a SYS 1 fault:

    System 2 takes over automatically without crew action

  • 54

    Cabin pressurization starts at:

    Take-off

  • 55

    The pressure safety valves open at:

    8.6 psi above ambient pressure

  • 56

    In automatic mode, cabin pressurization is optimized by using information from:

    FMGS landing field elev, dest. QNH and static pressure information

  • 57

    During normal flight and with skin temp. below 35 °C, the avionics ventilation system controls the temperature of the cooling air by:

    Passing air through a skin heat exchanger

  • 58

    When the RAM AIR pushbutton is set to ON, the emergency ram air inlet valve will open:

    When ∆P < 1 psi and ditching is not selected

  • 59

    The Residual Pressure Control Unit (RPCU) automatically depressurized the aircraft in case of abnormal residual pressure, it automatically opens the outflow valve when:

    The OFV is not fully open + both CPCs fail + a/c on ground + all engines shutdown

  • 60

    When the RAM AIR pb is set to ON the outflow valve:

    Opens about 50% only when ΔP is less than 1 psi

  • 61

    With the BLOWER and EXTRACT pushbuttons in OVRD, the avionics bay ventilation gets air from the:

    Air conditioning inlet valve

  • 62

    In the air conditioning system, is temperature regulation of the temperature, is ensured by?

    A zone controller and two pack controllers, or two Air Conditioning System Controllers (ACSC)

  • 63

    The Pressurization system is normally controlled in what way?

    Fully automatic

  • 64

    In what range can the temperature be regulated with the zone temperature selectors on the overhead panel?

    18-30 deg C

  • 65

    How are the Pack Flow Control valves controlled during engine start?

    Close automatically

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    問題一覧

  • 1

    Hot air FAULT light illuminates on the air conditioning panel:

    The hot air press reg. valve closes and the trim air valves close

  • 2

    In case of Air Conditioning System Controller dual lane failure:

    The related Pack is lost, and the hot air pressure regulating valve and associated trim air valves closes

  • 3

    During normal flight the Avionics Ventilation System controls the temperature of the cooling air by:

    Passing air through a skin heat exchanger

  • 4

    The RAM AIR switch should be used:

    Only when delta P is less than 1 psi

  • 5

    Air Conditioning System Controller, one lane failure will result in:

    The second lane takes over

  • 6

    Air Conditioning System Controller, both lanes fail:

    Pack is lost

  • 7

    Each Pack consists of heat exchangers, compressor and turbine. The purpose of the turbine is to:

    Drives the compressor, cooling air fan and also expands and cools the air.

  • 8

    The Mixer Unit connects to cabin fans, LP ground connector, emergency ram air inlet, Pack 1 and 2. The statement is:

    True

  • 9

    Hot air pressure regulating valve failed in open position:

    No effect

  • 10

    With bleed air supplied from the APU (APU bleed valve open), the pack flow is automatically selected:

    High

  • 11

    Each trim air valve optimizes the temperature by:

    Adding hot air

  • 12

    The hot air pressure regulating valves:

    Regulate the pressure of hot air tapped upstream of the packs

  • 13

    The pack flow control valve is:

    Pneumatically operated and electrically controlled

  • 14

    The temperature selectors are located in:

    Both (The cockpit) and (the cabin (FAP)) are correct

  • 15

    Pack flow may be selected from:

    The cockpit

  • 16

    When the cooling demand can’t be satisfied due to low bleed air pressure:

    The minimum idle is increased automatically

  • 17

    What is the maximum normal cabin alt:

    8,000 feet

  • 18

    What is the maximum negative differential pressure for the cabin:

    -1 psi

  • 19

    Is it recommended to use Packs and LP Ground Unit simultaneously during long stops on a hot airfield?

    No

  • 20

    Trim air valves are controlled by:

    The air conditioning system controller

  • 21

    The mixer unit is connected to:

    Packs, cabin air, emergency ram air inlet and LP ground connector

  • 22

    Once set to "ON" the air conditioning packs operate:

    Automatically and independently of each other

  • 23

    When the RAM AIR pushbutton is ON, the ram air valve will open:

    If ΔP < 1 psi and the DITCHING pushbutton is in normal position

  • 24

    Hot-Air Pressure-Regulating Valve is controlled by the:

    Air Conditioning System Controller 1

  • 25

    Conditioned air is normally distributed to:

    Cockpit, forward and aft cabins

  • 26

    The cabin zone temperature sensors are ventilated by the air extracted by the lavatory and galleys fans:

    True

  • 27

    Temperature regulation is automatic and is controlled by:

    Air conditioning system controllers

  • 28

    The Hot-Air Pressure-Regulating Valve closes automatically when;

    Both (Both lanes of the Air Conditioning System Controller 1 fails) and (Both lanes of the Air Conditioning System Controller 2 fails) are correct

  • 29

    The Hot-Air Pressure-Regulating Valve closes automatically when:

    Cockpit trim air valve or cabin trim air valves fail

  • 30

    When the pack flow control selector is positioned to HI, air flow is:

    120% of normal

  • 31

    When using APU bleed to supply the Packs, with the Pack Flow Selector at LO, the Pack air flow is:

    120% of normal

  • 32

    The pack flow control valve closes automatically in case of:

    Pack overheating, engine starting, or operation of the fire or ditching pushbutton pressed

  • 33

    Trim air valve failure

    The optimized temperature regulation of the corresponding zone is lost

  • 34

    There are how many trim air valves?

    3 - one for the cockpit and two for the cabin

  • 35

    During landing run, ram air inlet flaps open when the speed is less than:

    70 knots ( after a 20 sec delay)

  • 36

    When APU is supplying the packs, they send a demand signal to increase airflow when a zone temperature can’t be satisfied:

    To the APU ECB

  • 37

    When the ditching switch is selected ON, it sends a closure signal to:

    Both (Outflow valve) and (Ram air inlet, ventilation extract valves and the pack flow control valves) are correct

  • 38

    In flight, with pressure controller 1 in use, if it fails:

    Transfers automatically to controller 2

  • 39

    In normal operation, pressurization is:

    Fully automatic

  • 40

    The outflow valve is powered by:

    One of three electric motors

  • 41

    During ground operation, the outflow valve is:

    Fully open

  • 42

    To see the position of the outflow valve, it is necessary to call ECAM:

    PRESS Page

  • 43

    Two identical, independent, pressurization controllers are used for system control:

    One controller active, one in standby

  • 44

    Which controller generates excess cabin altitude and pressure outputs for ECAM indication in manual mode:

    N°1

  • 45

    When Ram Air pb is set to ON, the outflow valve will open 50% when delta P is:

    < 1 psi

  • 46

    The purpose of the safety valves is to avoid:

    Both (Excessive positive pressure differential) and (excessive negative pressure differential) are correct

  • 47

    The safety valves are operated:

    Pneumatically

  • 48

    When landing elevation is set to AUTO, the landing elevation is sent to the controller from:

    FMGC

  • 49

    When Mode SEL is set to MANUAL, the outflow valve is controlled by signals sent via controller 1 or 2:

    False

  • 50

    On ECAM CAB PRESS page, the outflow valve indicator changes to amber if:

    The valve opens more than 95% during flight

  • 51

    On ECAM CAB PRESS page, the safety valve indication changes to amber if:

    Either valve is not closed

  • 52

    On ECAM CAB PRESS page the cabin altitude indicator changes to red when the cabin altitude is:

    > 9, 550 feet

  • 53

    Following a SYS 1 fault:

    System 2 takes over automatically without crew action

  • 54

    Cabin pressurization starts at:

    Take-off

  • 55

    The pressure safety valves open at:

    8.6 psi above ambient pressure

  • 56

    In automatic mode, cabin pressurization is optimized by using information from:

    FMGS landing field elev, dest. QNH and static pressure information

  • 57

    During normal flight and with skin temp. below 35 °C, the avionics ventilation system controls the temperature of the cooling air by:

    Passing air through a skin heat exchanger

  • 58

    When the RAM AIR pushbutton is set to ON, the emergency ram air inlet valve will open:

    When ∆P < 1 psi and ditching is not selected

  • 59

    The Residual Pressure Control Unit (RPCU) automatically depressurized the aircraft in case of abnormal residual pressure, it automatically opens the outflow valve when:

    The OFV is not fully open + both CPCs fail + a/c on ground + all engines shutdown

  • 60

    When the RAM AIR pb is set to ON the outflow valve:

    Opens about 50% only when ΔP is less than 1 psi

  • 61

    With the BLOWER and EXTRACT pushbuttons in OVRD, the avionics bay ventilation gets air from the:

    Air conditioning inlet valve

  • 62

    In the air conditioning system, is temperature regulation of the temperature, is ensured by?

    A zone controller and two pack controllers, or two Air Conditioning System Controllers (ACSC)

  • 63

    The Pressurization system is normally controlled in what way?

    Fully automatic

  • 64

    In what range can the temperature be regulated with the zone temperature selectors on the overhead panel?

    18-30 deg C

  • 65

    How are the Pack Flow Control valves controlled during engine start?

    Close automatically