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EXA 1

EXA 1
32問 • 2年前
  • Juan Sebastian Ruiz Diaz
    • 通報

    問題一覧

  • 1

    Where are the class 1 shown?

    They are shown on the ECAM E/WD

  • 2

    Select the correct statemen about alert levels:

    Level 2 alert generates a single chime and a master caution light

  • 3

    What is a type 3 system characteristic?

    They are interfaced with the CFDIU by discrete only

  • 4

    Where are the flight phases generated?

    In the FWC

  • 5

    The EIS (Electronic Instrument System) presents data for:

    EFIS and ECAM

  • 6

    In case of a display unit failure…

    "INVALID DISPLAY UNIT” is displayed on the relevant screen

  • 7

    The Post Flight Report includes:

    The Last Leg Report and the Last Leg ECAM Report

  • 8

    When is started the flight mode for type 2 BITE?

    The flight mode is started in flight phase 5b

  • 9

    The TEST/RESET only option is available in this BITE system…

    BITE Type 3

  • 10

    What is the meaning of the STS indication in the Engine and Warning display?

    The status page is not empty

  • 11

    In case of TR 1 failure…

    The TR Essential operates

  • 12

    When are activated automatically the RAT and Emergency Generator?

    In case of AC BUS 1 and AC BUS 2 dual failure or loss of power

  • 13

    Is it possible to start the APU during RAT deploy?

    No, it is not possible

  • 14

    In case of TR1 failure, which one of these units will provides power to the DC BAT BUS in flight?

    The TR N° 2 will supply the DC BAT BUS

  • 15

    In normal condition which component send power to the DC ESS BUS?

    The DC BAT BUS

  • 16

    Which component controls the Main Battery Charge?

    BCL1 and BCL2

  • 17

    When is activated the static inverter?

    When the airplane is powered by batteries only, (Emergency Condition)

  • 18

    Is it possible to feed the AC BUS 1 from both AC main generators at the same time?

    No, it is not possible, just one generator can supply any AC BUS

  • 19

    When are the runway turnoff lights electrically powered?

    When the nose landing gear down locked and the switch is ON

  • 20

    The purpose of the Emergency Lighting System is…

    To provide the illumination in case of emergency condition for a few minutes

  • 21

    What is the “lights out philosophy” meaning?

    Lights out means that there is no failure active in those local warnings

  • 22

    How many frames are added in the A321, in relation to A320?

    13 frames

  • 23

    What is the local warning light color that points out a “Deactivated” system?

    A white color

  • 24

    What is the main purpose of the System Data Acquisition Concentrator?

    To concentrate data to be used by others computers

  • 25

    What is the panel used to select system pages?

    ECAM control panel

  • 26

    What color are the monitored circuit breakers?

    They are green

  • 27

    Where is located the solid-state flight data recorder?

    It is located in the aircraft tail, close to the cockpit voice recorder.

  • 28

    Which one of the following display units shows the Pitch/Roll data?

    The PFD DU

  • 29

    Class 2 failure means:

    A fault that does not affect the flight but should be repair in a short time.

  • 30

    The Airbus “Fly By Wire” philosophy is related to:

    It is related to flight controls surfaces controlled by computers.

  • 31

    Where is station zero located?

    It is located 100 inches before aircraft nose.

  • 32

    The standard electrical power frequency for the A320 family stands to:

    400 Hz

    • 問題一覧

  • 1

    Where are the class 1 shown?

    They are shown on the ECAM E/WD

  • 2

    Select the correct statemen about alert levels:

    Level 2 alert generates a single chime and a master caution light

  • 3

    What is a type 3 system characteristic?

    They are interfaced with the CFDIU by discrete only

  • 4

    Where are the flight phases generated?

    In the FWC

  • 5

    The EIS (Electronic Instrument System) presents data for:

    EFIS and ECAM

  • 6

    In case of a display unit failure…

    "INVALID DISPLAY UNIT” is displayed on the relevant screen

  • 7

    The Post Flight Report includes:

    The Last Leg Report and the Last Leg ECAM Report

  • 8

    When is started the flight mode for type 2 BITE?

    The flight mode is started in flight phase 5b

  • 9

    The TEST/RESET only option is available in this BITE system…

    BITE Type 3

  • 10

    What is the meaning of the STS indication in the Engine and Warning display?

    The status page is not empty

  • 11

    In case of TR 1 failure…

    The TR Essential operates

  • 12

    When are activated automatically the RAT and Emergency Generator?

    In case of AC BUS 1 and AC BUS 2 dual failure or loss of power

  • 13

    Is it possible to start the APU during RAT deploy?

    No, it is not possible

  • 14

    In case of TR1 failure, which one of these units will provides power to the DC BAT BUS in flight?

    The TR N° 2 will supply the DC BAT BUS

  • 15

    In normal condition which component send power to the DC ESS BUS?

    The DC BAT BUS

  • 16

    Which component controls the Main Battery Charge?

    BCL1 and BCL2

  • 17

    When is activated the static inverter?

    When the airplane is powered by batteries only, (Emergency Condition)

  • 18

    Is it possible to feed the AC BUS 1 from both AC main generators at the same time?

    No, it is not possible, just one generator can supply any AC BUS

  • 19

    When are the runway turnoff lights electrically powered?

    When the nose landing gear down locked and the switch is ON

  • 20

    The purpose of the Emergency Lighting System is…

    To provide the illumination in case of emergency condition for a few minutes

  • 21

    What is the “lights out philosophy” meaning?

    Lights out means that there is no failure active in those local warnings

  • 22

    How many frames are added in the A321, in relation to A320?

    13 frames

  • 23

    What is the local warning light color that points out a “Deactivated” system?

    A white color

  • 24

    What is the main purpose of the System Data Acquisition Concentrator?

    To concentrate data to be used by others computers

  • 25

    What is the panel used to select system pages?

    ECAM control panel

  • 26

    What color are the monitored circuit breakers?

    They are green

  • 27

    Where is located the solid-state flight data recorder?

    It is located in the aircraft tail, close to the cockpit voice recorder.

  • 28

    Which one of the following display units shows the Pitch/Roll data?

    The PFD DU

  • 29

    Class 2 failure means:

    A fault that does not affect the flight but should be repair in a short time.

  • 30

    The Airbus “Fly By Wire” philosophy is related to:

    It is related to flight controls surfaces controlled by computers.

  • 31

    Where is station zero located?

    It is located 100 inches before aircraft nose.

  • 32

    The standard electrical power frequency for the A320 family stands to:

    400 Hz