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Bob 1
40問 • 4ヶ月前
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    問題一覧

  • 1

    Where is the external power receptacle located?

    In front of the nose landing gear

  • 2

    Where are the Localizer and Glideslope antennas located?

    Behind the nose radome

  • 3

    How many persons can be seated in the Cockpit?

    4, one pilot, one co-pilot and two observers

  • 4

    With the aircraft on the ground, engines shutdown and no faults, which page is displayed on the lower ECAM DU (SD)?

    DOOR

  • 5

    When does the STATUS page appear automatically?

    Once the crew has cleared all the pages corresponding to the current failure, or when the slats are extended (if failure still exists)

  • 6

    What computer generates RED warnings?

    FWC

  • 7

    The ECAM display uses a colour code that indicates the importance of the failure or the indication. What colour indicates crew should be aware but need not take immediate action?

    Amber

  • 8

    What Permanent data is displayed on the lower section of the SD?

    Temperature, G LOAD, UTC and GW

  • 9

    Why are some Circuit Breakers (C/Bs) green instead of black?

    They are monitored and will show up on the ECAM approx. 1 minute after being triggered

  • 10

    Can the generators be connected in parallel?

    No

  • 11

    What's the purpose of the TR's?

    To Transform and Rectify A/C power to D/C power

  • 12

    What source normally provides power to the AC ESS BUS?

    AC BUS 1

  • 13

    If AP 2 is engaged, which FMGC is master and controls the A/THR?

    No. 2

  • 14

    How is a temporary Flight Plan indicated on the ND?

    A dotted yellow line

  • 15

    How many legs can a flight plan contain?

    200

  • 16

    What unit is used for short-term interface?

    FCU

  • 17

    What color indicates a secondary flight plan in PLAN mode?

    White

  • 18

    How long must the RESET p/o on the ISIS be pressed to reset the attitude indication?

    For at least 2 seconds

  • 19

    Below what height do the FWC's generate height announcements?

    2500 feet

  • 20

    How many GPS receivers are connected to the IR part of the ADIRUs?

    Two independent receivers

  • 21

    If ALL / Nis selected on the ATC/TCAS panel, what is the altitude range of intruders that are displayed?

    2700 feet above and 2700 feet below the aircraft

  • 22

    With the Predictive Windshear (PWS) switch in AUTO, below what height is data displayed on the ND?

    1500 feet RA

  • 23

    What causes amber XX in the BLEED indication on APU SD page?

    ADIRS 1 or 2 are not available or selected OFF, or the data from the ECB are invalid or not transmitted

  • 24

    Which fuel feed line supplies the APU?

    The Left fuel feed line supplies the APU

  • 25

    What is the ECB in the APU system?

    The Electronic Control Box (ECB) is a full-authority digital electronic controller

  • 26

    What controls and monitors the Pneumatic system ?

    Two Bleed Monitoring Computers

  • 27

    The air bleed system supplies the aircraft with high pressure air, and uses it for:

    Air conditioning, Engine Starting, Water System Pressurisation, Wing anti-icing and Hydraulic reservoir pressurisation

  • 28

    What happens when the pressure and temperature are not sufficient to supply the corresponding engine bleed valve?

    The HP valve opens and the IP stage remains in the same configuration

  • 29

    In which part of the air conditioning pack is the hot air expanded?

    In the turbine

  • 30

    When does the hot air valve close automatically?

    When a duct overheat or absence of pneumatic pressure exists

  • 31

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

    18-30 deg C

  • 32

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

    Close automatically

  • 33

    When will the RAT deploy automatically?

    If AC BUS 1 and AC BUS 2 are both lost

  • 34

    What is the normal operating hydraulic pressure?

    3000 PSI (2500 PSI when powered by the RAT)

  • 35

    Can the PTU operate and pressurize the Green system without an engine running?

    Yes, by selecting the YELLOW ELEC pump to ON, PTU switch to AUTO and differential pressure >500 PSI

  • 36

    When does the Blue electrical pump operate automatically?

    If AC power is available and in flight, or on the ground, if one engine is running

  • 37

    Side Stick control orders are sent to which flight control computer?

    ELAC and SEC

  • 38

    In normal law, what happens if the pilot holds full lateral side stick deflection?

    The bank angle goes to 67° and no further

  • 39

    Is mechanical control of the THS always available?

    Yes, if either the green or yellow hydraulic systems are functioning

  • 40

    What is true regarding the flight controls on an Airbus 320?

    They are all electrically controlled and hydraulically activated

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    問題一覧

  • 1

    Where is the external power receptacle located?

    In front of the nose landing gear

  • 2

    Where are the Localizer and Glideslope antennas located?

    Behind the nose radome

  • 3

    How many persons can be seated in the Cockpit?

    4, one pilot, one co-pilot and two observers

  • 4

    With the aircraft on the ground, engines shutdown and no faults, which page is displayed on the lower ECAM DU (SD)?

    DOOR

  • 5

    When does the STATUS page appear automatically?

    Once the crew has cleared all the pages corresponding to the current failure, or when the slats are extended (if failure still exists)

  • 6

    What computer generates RED warnings?

    FWC

  • 7

    The ECAM display uses a colour code that indicates the importance of the failure or the indication. What colour indicates crew should be aware but need not take immediate action?

    Amber

  • 8

    What Permanent data is displayed on the lower section of the SD?

    Temperature, G LOAD, UTC and GW

  • 9

    Why are some Circuit Breakers (C/Bs) green instead of black?

    They are monitored and will show up on the ECAM approx. 1 minute after being triggered

  • 10

    Can the generators be connected in parallel?

    No

  • 11

    What's the purpose of the TR's?

    To Transform and Rectify A/C power to D/C power

  • 12

    What source normally provides power to the AC ESS BUS?

    AC BUS 1

  • 13

    If AP 2 is engaged, which FMGC is master and controls the A/THR?

    No. 2

  • 14

    How is a temporary Flight Plan indicated on the ND?

    A dotted yellow line

  • 15

    How many legs can a flight plan contain?

    200

  • 16

    What unit is used for short-term interface?

    FCU

  • 17

    What color indicates a secondary flight plan in PLAN mode?

    White

  • 18

    How long must the RESET p/o on the ISIS be pressed to reset the attitude indication?

    For at least 2 seconds

  • 19

    Below what height do the FWC's generate height announcements?

    2500 feet

  • 20

    How many GPS receivers are connected to the IR part of the ADIRUs?

    Two independent receivers

  • 21

    If ALL / Nis selected on the ATC/TCAS panel, what is the altitude range of intruders that are displayed?

    2700 feet above and 2700 feet below the aircraft

  • 22

    With the Predictive Windshear (PWS) switch in AUTO, below what height is data displayed on the ND?

    1500 feet RA

  • 23

    What causes amber XX in the BLEED indication on APU SD page?

    ADIRS 1 or 2 are not available or selected OFF, or the data from the ECB are invalid or not transmitted

  • 24

    Which fuel feed line supplies the APU?

    The Left fuel feed line supplies the APU

  • 25

    What is the ECB in the APU system?

    The Electronic Control Box (ECB) is a full-authority digital electronic controller

  • 26

    What controls and monitors the Pneumatic system ?

    Two Bleed Monitoring Computers

  • 27

    The air bleed system supplies the aircraft with high pressure air, and uses it for:

    Air conditioning, Engine Starting, Water System Pressurisation, Wing anti-icing and Hydraulic reservoir pressurisation

  • 28

    What happens when the pressure and temperature are not sufficient to supply the corresponding engine bleed valve?

    The HP valve opens and the IP stage remains in the same configuration

  • 29

    In which part of the air conditioning pack is the hot air expanded?

    In the turbine

  • 30

    When does the hot air valve close automatically?

    When a duct overheat or absence of pneumatic pressure exists

  • 31

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

    18-30 deg C

  • 32

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

    Close automatically

  • 33

    When will the RAT deploy automatically?

    If AC BUS 1 and AC BUS 2 are both lost

  • 34

    What is the normal operating hydraulic pressure?

    3000 PSI (2500 PSI when powered by the RAT)

  • 35

    Can the PTU operate and pressurize the Green system without an engine running?

    Yes, by selecting the YELLOW ELEC pump to ON, PTU switch to AUTO and differential pressure >500 PSI

  • 36

    When does the Blue electrical pump operate automatically?

    If AC power is available and in flight, or on the ground, if one engine is running

  • 37

    Side Stick control orders are sent to which flight control computer?

    ELAC and SEC

  • 38

    In normal law, what happens if the pilot holds full lateral side stick deflection?

    The bank angle goes to 67° and no further

  • 39

    Is mechanical control of the THS always available?

    Yes, if either the green or yellow hydraulic systems are functioning

  • 40

    What is true regarding the flight controls on an Airbus 320?

    They are all electrically controlled and hydraulically activated