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Miko 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

    What cargo compartment can handle containers if the aircraft has that option?

    Both FWD and AFT cargo compartments

  • 3

    Where is the VHF 1 antenna located?

    On top of the fuselage

  • 4

    How many Flight Phases are there?

    10

  • 5

    In normal operation, what displays are receiving information from DMC 1?

    PFD 1, ND 1, E/WD and SD

  • 6

    In which flight phases are "T.O. INHIBIT" displayed on EW/D?

    3, 4 and 5

  • 7

    Regarding Warning/Caution classification, what level is most critical?

    Level 3

  • 8

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

    DOOR

  • 9

    Can the generators be connected in parallel?

    No

  • 10

    What source normally provides power to the AC ESS BUS?

    AC BUS 1

  • 11

    In normal configuration, what sources can supply power to the AC system when the aircraft is on ground?

    GEN 1, GEN 2, External Power and APU GEN

  • 12

    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

  • 13

    Which of the following units are part of the Flight Management System (FMGS)?

    Two Flight Management Guidance Computers (FMGC) and Two Multipurpose Control and Display Units (MCDU) and One Flight Control Unit (FCU) and Two Flight Augmentation Computers (FAC)

  • 14

    What color indicates a secondary flight plan in PLAN mode?

    White

  • 15

    In SRS mode, what speed does the aircraft maintain with 2 engines operative and with 1 engine operative?

    V2+10 knots / Highest of V2 or current speed (maximum V2+15 knots)

  • 16

    What unit is used for short-term interface?

    FCU

  • 17

    What is the normal mode for the FMGCs?

    Dual mode

  • 18

    How long must the RESET p/b 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

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

    1500 feet RA

  • 21

    If ALL / N is 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

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

    Two independent receivers

  • 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

    What does the message LOW OIL LEVEL means?

    Advisory message regarding APU oil level when aircraft is on the ground and APU not running

  • 25

    When will the electrical starter engage?

    The starter engages if the MASTER SWITCH and START p/b are on and the air inlet flap is fully open

  • 26

    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

  • 27

    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

  • 28

    When does the APU bleed valve open?

    When N > 95%

  • 29

    In the Air Conditioning system, temperature regulation of the temperature, is ensured by...?

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

  • 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 many air condition zones do we have on an Airbus A320?

    3, cockpit, FWD and AFT zone

  • 33

    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 diferential pressure >500 PSI

  • 34

    When will the RAT deploy automatically?

    If AC BUS 1 and AC BUS 2 are both lost

  • 35

    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

  • 36

    What is the purpose of the priority valves?

    Priority valves cut off hydraulic power to heavy load users if hydraulic pressure in a system gets low

  • 37

    Which Flight Control Computer normally operates the ailerons?

    ELAC 1

  • 38

    Is mechanical control of the THS always available?

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

  • 39

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

    The bank angle goes to 67° and no further

  • 40

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

    ELAC and SEC

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    問題一覧

  • 1

    Where is the external power receptacle located?

    In front of the nose landing gear

  • 2

    What cargo compartment can handle containers if the aircraft has that option?

    Both FWD and AFT cargo compartments

  • 3

    Where is the VHF 1 antenna located?

    On top of the fuselage

  • 4

    How many Flight Phases are there?

    10

  • 5

    In normal operation, what displays are receiving information from DMC 1?

    PFD 1, ND 1, E/WD and SD

  • 6

    In which flight phases are "T.O. INHIBIT" displayed on EW/D?

    3, 4 and 5

  • 7

    Regarding Warning/Caution classification, what level is most critical?

    Level 3

  • 8

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

    DOOR

  • 9

    Can the generators be connected in parallel?

    No

  • 10

    What source normally provides power to the AC ESS BUS?

    AC BUS 1

  • 11

    In normal configuration, what sources can supply power to the AC system when the aircraft is on ground?

    GEN 1, GEN 2, External Power and APU GEN

  • 12

    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

  • 13

    Which of the following units are part of the Flight Management System (FMGS)?

    Two Flight Management Guidance Computers (FMGC) and Two Multipurpose Control and Display Units (MCDU) and One Flight Control Unit (FCU) and Two Flight Augmentation Computers (FAC)

  • 14

    What color indicates a secondary flight plan in PLAN mode?

    White

  • 15

    In SRS mode, what speed does the aircraft maintain with 2 engines operative and with 1 engine operative?

    V2+10 knots / Highest of V2 or current speed (maximum V2+15 knots)

  • 16

    What unit is used for short-term interface?

    FCU

  • 17

    What is the normal mode for the FMGCs?

    Dual mode

  • 18

    How long must the RESET p/b 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

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

    1500 feet RA

  • 21

    If ALL / N is 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

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

    Two independent receivers

  • 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

    What does the message LOW OIL LEVEL means?

    Advisory message regarding APU oil level when aircraft is on the ground and APU not running

  • 25

    When will the electrical starter engage?

    The starter engages if the MASTER SWITCH and START p/b are on and the air inlet flap is fully open

  • 26

    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

  • 27

    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

  • 28

    When does the APU bleed valve open?

    When N > 95%

  • 29

    In the Air Conditioning system, temperature regulation of the temperature, is ensured by...?

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

  • 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 many air condition zones do we have on an Airbus A320?

    3, cockpit, FWD and AFT zone

  • 33

    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 diferential pressure >500 PSI

  • 34

    When will the RAT deploy automatically?

    If AC BUS 1 and AC BUS 2 are both lost

  • 35

    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

  • 36

    What is the purpose of the priority valves?

    Priority valves cut off hydraulic power to heavy load users if hydraulic pressure in a system gets low

  • 37

    Which Flight Control Computer normally operates the ailerons?

    ELAC 1

  • 38

    Is mechanical control of the THS always available?

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

  • 39

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

    The bank angle goes to 67° and no further

  • 40

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

    ELAC and SEC