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A320 GEN FAM
100問 • 2ヶ月前
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    問題一覧

  • 1

    Equipment and furnishings are installed in different compartments, except:

    Avionics Compartment

  • 2

    What type of seats does the cabin attendant have?

    Folding Seats

  • 3

    This panel is mounted on the side of the cabin which includes the window contour, inner window panels and sun visors.

    Upper Side Wall Panel

  • 4

    This panel extends from the firat to the last seat row on the left and right side of the cabin and are different sizes arranged to fit the cabin layout.

    OVERHEAD STOWAGE PANEL

  • 5

    If the escape slide of the passenger door does not inflate automatically, the red manual inflation handle is located ____ and can be used for manual inflation.

    RH SIDE OF THE GIRT BAR

  • 6

    How many assist handles are there in the passenger door to enhance safety during door operations?

    3

  • 7

    For the A320, the emergency exit escape slide containers are installed in _____

    WING ROOT FAIRING

  • 8

    It displays different pages related to the different systems connected to the CIDS.

    FLIGHT ATTENDANT PANEL

  • 9

    The magnetic level indicator are used to calculate the______

    TANK FUEL QUANTITIES

  • 10

    Which of the following is not true about the fuel level sensing control units?

    INSTALLED IN THE AIRCRAFT BELLY FAIRINGS

  • 11

    Which of the following is not part of the safety precautions during fueling and defueling of the aircraft

    TESTING OF HF SYSTEMS

  • 12

    Is a requirement to preserve a critical ignition source prevention feature of the fuel system design that is necessary to prevent the occurrence of an unsafe condition.

    CDCCL

  • 13

    It memorizes and centralizes all information concerning aircraft system failures.

    CFDIU

  • 14

    System report/test function is available___

    ON GROUND ONLY

  • 15

    Summarizes and displays the list of ECAM warning and fault messages that occurred during the last flight.

    POST FLIGHT REPORT

  • 16

    It replaces 3 conventional standby instruments.

    ISIS

  • 17

    Testing of probes must not exceed____

    60 SECONDS

  • 18

    Which of the following oxygen system uses high pressure cylinder with continuous flow type mask and smoking hoods.

    PORTABLE OXYGEN SYSTEM

  • 19

    The cockpit crew oxygen system has a high-pressure oxygen cylinder that can be isolated for maintenance by____

    ON/OFF VALVE

  • 20

    The flight crew can receive maximum oxygen during an emergency by means of_____

    EMERGENCY ROTATING KNOB

  • 21

    Where are the locations of portable oxygen bottles?

    COCKPIT AND CABIN

  • 22

    What shuts off the supply oxygen to the crew mask?

    CREW SUPPLY P/B

  • 23

    What pushbutton indicates if there is a fault in the oxygen system?

    TMR RESET P/B

  • 24

    The source of oxygen for the cabin oxygen system?

    CHEMICAL OXYGEN GENERATOR

  • 25

    It is used to isolate water supply to the galley or lavatories.

    MANUAL SHUT OFF VALVE

  • 26

    Potable water system is mainly pressurized by______

    BLEED AIR SYSTEM

  • 27

    On the A320, where is the potable water service panel located?

    Rear lower fuselage, LH side

  • 28

    How many drain servicing panels does the A320 have?

    2

  • 29

    Where is the potable water tank located on the A320?

    Lower RH fuselage behind the forward cargo compartment

  • 30

    What prevents constant cabin depressurization in the toilet system?

    Air stop valves

  • 31

    On the ground and in flight below 16,000 ft, what creates suction for the toilet system?

    Vacuum generator

  • 32

    Above 16,000 ft, what is used for suction in the toilet system?

    Differential pressure

  • 33

    Which component controls, monitors, and indicates toilet system operation and faults?

    Vacuum System Controller Function (VSCF)

  • 34

    Where are water and waste indications displayed?

    Flight Attendant Panel (FAP)

  • 35

    The potable water system on the A320 can be serviced:

    With or without electrical power

  • 36

    What system receives vacuum toilet system failure data from the VSCF?

    Centralized Fault Display System (CFDS)

  • 37

    Which unit monitors the toilet flush operation and sends fault signals to the VSCF?

    Flash Control Unit (FCU)

  • 38

    How many independent hydraulic systems does the aircraft have?

    3

  • 39

    Each hydraulic system supplies power at what pressure?

    3000 PSI

  • 40

    Which hydraulic systems are pressurized by Engine Driven Pumps (EDP)?

    Green and Yellow

  • 41

    The yellow hydraulic system can also be pressurized by:

    Electric pump

  • 42

    The yellow system’s electric pump is mainly used for:

    Cargo door operation and ground maintenance

  • 43

    What can be used if no electrical power is available to operate the cargo doors?

    Hand pump in yellow system

  • 44

    What is the function of the Power Transfer Unit (PTU)?

    Transfers hydraulic power without fluid transfer

  • 45

    The blue hydraulic system is pressurized by:

    Electric pump

  • 46

    The PTU is located in the:

    Main landing gear bay

  • 47

    The blue reservoir is located:

    Aft of MLG bay, LH side

  • 48

    Where is the green reservoir located?

    Inside main landing gear bay

  • 49

    The yellow reservoir is located:

    Inside yellow hydraulic bay

  • 50

    What does the visual indicator on the top of the door display?

    LOCKED or UNLOCKED

  • 51

    The visual indicator on the slide arming lever shows:

    Whether the slide is ARMED or DISARMED

  • 52

    The Fuel Level Sensing Control Units (FLSCUs) are located:

    In the avionics compartment

  • 53

    What component ensures the monitoring and control of automatic refueling?

    FQIC

  • 54

    Where is the Fuel Quantity Indication Computer (FQIC) located?

    In the avionics compartment

  • 55

    How many fuel pumps are installed on the A318/A319/A320?

    6

  • 56

    How many fuel pumps are installed on the A321?

    4

  • 57

    How are the A318/A319/A320 fuel pumps distributed?

    Two each for left, center, and right tanks

  • 58

    Each lavatory has how many smoke detectors?

    1

  • 59

    The lavatory smoke detectors are monitored by the:

    Smoke Detection Function (SDF) in CIDS

  • 60

    Lavatory smoke warnings are sent to:

    The FWC (flight crew) and CIDS (cabin crew)

  • 61

    The cargo smoke detectors are monitored by the:

    Smoke Detection Function (SDF) in CIDS

  • 62

    Each cargo compartment cavity holds how many smoke detectors?

    2

  • 63

    The avionics smoke detector is installed in:

    The extraction duct

  • 64

    The avionics smoke detector is monitored by the:

    Avionics Equipment Ventilation Controller (AEVC)

  • 65

    An AVIONICS SMOKE warning appears on:

    Two overhead panels

  • 66

    FDU 1 monitors:

    Engine 1

  • 67

    What does the Fire Detection Unit (FDU) send to the Flight Warning Computer (FWC)?

    Fire and fault signals

  • 68

    The AGENT P/B switches for engine fire extinguishing are located on the:

    Overhead FIRE panel

  • 69

    The APU is installed in which part of the aircraft?

    Unpressurized tail cone

  • 70

    What type of engine is the APU?

    Single-shaft gas turbine

  • 71

    The APU provides bleed air for:

    Engine starting and air conditioning

  • 72

    The Load Control Valve (LCV) provides:

    Pneumatic power to start air conditioning

  • 73

    The Bleed Control Valve (BCV) provides:

    Pneumatic power for starting and air conditioning

  • 74

    The Surge Control Valve protects the load compressor from:

    Insufficient airflow

  • 75

    The ECB is physically located in:

    The aft cargo compartment, right-hand side

  • 76

    The maximum altitude for APU bleed air operation for the Honeywell model is:

    25,500 ft

  • 77

    The APIC APU model provides bleed air up to:

    20,000 ft

  • 78

    The CFM56-5B engine is classified as what type of engine?

    Dual-rotor, variable stator, high bypass ratio turbofan

  • 79

    The engine is attached to the aircraft pylon using:

    Two mounts (forward and aft)

  • 80

    The annular combustion chamber is located between:

    The HP compressor and HP turbine

  • 81

    How many fuel nozzles are installed in the combustion chamber?

    20

  • 82

    How many igniter plugs are used in the combustion chamber?

    2

  • 83

    Which of the following components are driven by the gearbox?

    Fuel pumps, oil pumps, hydraulic pump, IDG, and FADEC alternator

  • 84

    The FADEC provides:

    Full engine control for steady and transient operation

  • 85

    On which side of the engine are the fuel and oil systems located?

    Left-hand side (LH)

  • 86

    The right-hand side (RH) of the engine mainly contains:

    Computers and control units

  • 87

    Each engine is controlled by which electronic component?

    Engine Control Unit (ECU)

  • 88

    Where is the ECU located?

    On the engine fan case, right-hand side

  • 89

    The autothrust can be disconnected using:

    Two Instinctive disconnect pushbuttons

  • 90

    The Engine Vibration Monitoring Unit (EVMU):

    Collects and displays engine vibration data on ECAM

  • 91

    Storage and preservation procedures are required if the engine is not operated for:

    More than 30 days

  • 92

    Power for FADEC operation is supplied by:

    Dual-output FADEC alternator

  • 93

    The vibration information gathered by the EVMU is also available through:

    CFDS

  • 94

    Which of the following is not a source of HP air?

    Ram Air System

  • 95

    The pneumatic system operates pneumatically and is monitored by how many Bleed Monitoring Computers (BMC)?

    2

  • 96

    Each BMC corresponds to:

    One Engine Bleed System

  • 97

    What is the function of the Pressure Regulating Valve (PRV)?

    To pneumatically regulate airflow and act as a protective shutoff valve

  • 98

    How many display units make up the EIS?

    6

  • 99

    What does ECAM stand for?

    Electronic Centralized Aircraft Monitoring

  • 100

    What does EFIS stand for?

    Electronic Flight Information System

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    問題一覧

  • 1

    Equipment and furnishings are installed in different compartments, except:

    Avionics Compartment

  • 2

    What type of seats does the cabin attendant have?

    Folding Seats

  • 3

    This panel is mounted on the side of the cabin which includes the window contour, inner window panels and sun visors.

    Upper Side Wall Panel

  • 4

    This panel extends from the firat to the last seat row on the left and right side of the cabin and are different sizes arranged to fit the cabin layout.

    OVERHEAD STOWAGE PANEL

  • 5

    If the escape slide of the passenger door does not inflate automatically, the red manual inflation handle is located ____ and can be used for manual inflation.

    RH SIDE OF THE GIRT BAR

  • 6

    How many assist handles are there in the passenger door to enhance safety during door operations?

    3

  • 7

    For the A320, the emergency exit escape slide containers are installed in _____

    WING ROOT FAIRING

  • 8

    It displays different pages related to the different systems connected to the CIDS.

    FLIGHT ATTENDANT PANEL

  • 9

    The magnetic level indicator are used to calculate the______

    TANK FUEL QUANTITIES

  • 10

    Which of the following is not true about the fuel level sensing control units?

    INSTALLED IN THE AIRCRAFT BELLY FAIRINGS

  • 11

    Which of the following is not part of the safety precautions during fueling and defueling of the aircraft

    TESTING OF HF SYSTEMS

  • 12

    Is a requirement to preserve a critical ignition source prevention feature of the fuel system design that is necessary to prevent the occurrence of an unsafe condition.

    CDCCL

  • 13

    It memorizes and centralizes all information concerning aircraft system failures.

    CFDIU

  • 14

    System report/test function is available___

    ON GROUND ONLY

  • 15

    Summarizes and displays the list of ECAM warning and fault messages that occurred during the last flight.

    POST FLIGHT REPORT

  • 16

    It replaces 3 conventional standby instruments.

    ISIS

  • 17

    Testing of probes must not exceed____

    60 SECONDS

  • 18

    Which of the following oxygen system uses high pressure cylinder with continuous flow type mask and smoking hoods.

    PORTABLE OXYGEN SYSTEM

  • 19

    The cockpit crew oxygen system has a high-pressure oxygen cylinder that can be isolated for maintenance by____

    ON/OFF VALVE

  • 20

    The flight crew can receive maximum oxygen during an emergency by means of_____

    EMERGENCY ROTATING KNOB

  • 21

    Where are the locations of portable oxygen bottles?

    COCKPIT AND CABIN

  • 22

    What shuts off the supply oxygen to the crew mask?

    CREW SUPPLY P/B

  • 23

    What pushbutton indicates if there is a fault in the oxygen system?

    TMR RESET P/B

  • 24

    The source of oxygen for the cabin oxygen system?

    CHEMICAL OXYGEN GENERATOR

  • 25

    It is used to isolate water supply to the galley or lavatories.

    MANUAL SHUT OFF VALVE

  • 26

    Potable water system is mainly pressurized by______

    BLEED AIR SYSTEM

  • 27

    On the A320, where is the potable water service panel located?

    Rear lower fuselage, LH side

  • 28

    How many drain servicing panels does the A320 have?

    2

  • 29

    Where is the potable water tank located on the A320?

    Lower RH fuselage behind the forward cargo compartment

  • 30

    What prevents constant cabin depressurization in the toilet system?

    Air stop valves

  • 31

    On the ground and in flight below 16,000 ft, what creates suction for the toilet system?

    Vacuum generator

  • 32

    Above 16,000 ft, what is used for suction in the toilet system?

    Differential pressure

  • 33

    Which component controls, monitors, and indicates toilet system operation and faults?

    Vacuum System Controller Function (VSCF)

  • 34

    Where are water and waste indications displayed?

    Flight Attendant Panel (FAP)

  • 35

    The potable water system on the A320 can be serviced:

    With or without electrical power

  • 36

    What system receives vacuum toilet system failure data from the VSCF?

    Centralized Fault Display System (CFDS)

  • 37

    Which unit monitors the toilet flush operation and sends fault signals to the VSCF?

    Flash Control Unit (FCU)

  • 38

    How many independent hydraulic systems does the aircraft have?

    3

  • 39

    Each hydraulic system supplies power at what pressure?

    3000 PSI

  • 40

    Which hydraulic systems are pressurized by Engine Driven Pumps (EDP)?

    Green and Yellow

  • 41

    The yellow hydraulic system can also be pressurized by:

    Electric pump

  • 42

    The yellow system’s electric pump is mainly used for:

    Cargo door operation and ground maintenance

  • 43

    What can be used if no electrical power is available to operate the cargo doors?

    Hand pump in yellow system

  • 44

    What is the function of the Power Transfer Unit (PTU)?

    Transfers hydraulic power without fluid transfer

  • 45

    The blue hydraulic system is pressurized by:

    Electric pump

  • 46

    The PTU is located in the:

    Main landing gear bay

  • 47

    The blue reservoir is located:

    Aft of MLG bay, LH side

  • 48

    Where is the green reservoir located?

    Inside main landing gear bay

  • 49

    The yellow reservoir is located:

    Inside yellow hydraulic bay

  • 50

    What does the visual indicator on the top of the door display?

    LOCKED or UNLOCKED

  • 51

    The visual indicator on the slide arming lever shows:

    Whether the slide is ARMED or DISARMED

  • 52

    The Fuel Level Sensing Control Units (FLSCUs) are located:

    In the avionics compartment

  • 53

    What component ensures the monitoring and control of automatic refueling?

    FQIC

  • 54

    Where is the Fuel Quantity Indication Computer (FQIC) located?

    In the avionics compartment

  • 55

    How many fuel pumps are installed on the A318/A319/A320?

    6

  • 56

    How many fuel pumps are installed on the A321?

    4

  • 57

    How are the A318/A319/A320 fuel pumps distributed?

    Two each for left, center, and right tanks

  • 58

    Each lavatory has how many smoke detectors?

    1

  • 59

    The lavatory smoke detectors are monitored by the:

    Smoke Detection Function (SDF) in CIDS

  • 60

    Lavatory smoke warnings are sent to:

    The FWC (flight crew) and CIDS (cabin crew)

  • 61

    The cargo smoke detectors are monitored by the:

    Smoke Detection Function (SDF) in CIDS

  • 62

    Each cargo compartment cavity holds how many smoke detectors?

    2

  • 63

    The avionics smoke detector is installed in:

    The extraction duct

  • 64

    The avionics smoke detector is monitored by the:

    Avionics Equipment Ventilation Controller (AEVC)

  • 65

    An AVIONICS SMOKE warning appears on:

    Two overhead panels

  • 66

    FDU 1 monitors:

    Engine 1

  • 67

    What does the Fire Detection Unit (FDU) send to the Flight Warning Computer (FWC)?

    Fire and fault signals

  • 68

    The AGENT P/B switches for engine fire extinguishing are located on the:

    Overhead FIRE panel

  • 69

    The APU is installed in which part of the aircraft?

    Unpressurized tail cone

  • 70

    What type of engine is the APU?

    Single-shaft gas turbine

  • 71

    The APU provides bleed air for:

    Engine starting and air conditioning

  • 72

    The Load Control Valve (LCV) provides:

    Pneumatic power to start air conditioning

  • 73

    The Bleed Control Valve (BCV) provides:

    Pneumatic power for starting and air conditioning

  • 74

    The Surge Control Valve protects the load compressor from:

    Insufficient airflow

  • 75

    The ECB is physically located in:

    The aft cargo compartment, right-hand side

  • 76

    The maximum altitude for APU bleed air operation for the Honeywell model is:

    25,500 ft

  • 77

    The APIC APU model provides bleed air up to:

    20,000 ft

  • 78

    The CFM56-5B engine is classified as what type of engine?

    Dual-rotor, variable stator, high bypass ratio turbofan

  • 79

    The engine is attached to the aircraft pylon using:

    Two mounts (forward and aft)

  • 80

    The annular combustion chamber is located between:

    The HP compressor and HP turbine

  • 81

    How many fuel nozzles are installed in the combustion chamber?

    20

  • 82

    How many igniter plugs are used in the combustion chamber?

    2

  • 83

    Which of the following components are driven by the gearbox?

    Fuel pumps, oil pumps, hydraulic pump, IDG, and FADEC alternator

  • 84

    The FADEC provides:

    Full engine control for steady and transient operation

  • 85

    On which side of the engine are the fuel and oil systems located?

    Left-hand side (LH)

  • 86

    The right-hand side (RH) of the engine mainly contains:

    Computers and control units

  • 87

    Each engine is controlled by which electronic component?

    Engine Control Unit (ECU)

  • 88

    Where is the ECU located?

    On the engine fan case, right-hand side

  • 89

    The autothrust can be disconnected using:

    Two Instinctive disconnect pushbuttons

  • 90

    The Engine Vibration Monitoring Unit (EVMU):

    Collects and displays engine vibration data on ECAM

  • 91

    Storage and preservation procedures are required if the engine is not operated for:

    More than 30 days

  • 92

    Power for FADEC operation is supplied by:

    Dual-output FADEC alternator

  • 93

    The vibration information gathered by the EVMU is also available through:

    CFDS

  • 94

    Which of the following is not a source of HP air?

    Ram Air System

  • 95

    The pneumatic system operates pneumatically and is monitored by how many Bleed Monitoring Computers (BMC)?

    2

  • 96

    Each BMC corresponds to:

    One Engine Bleed System

  • 97

    What is the function of the Pressure Regulating Valve (PRV)?

    To pneumatically regulate airflow and act as a protective shutoff valve

  • 98

    How many display units make up the EIS?

    6

  • 99

    What does ECAM stand for?

    Electronic Centralized Aircraft Monitoring

  • 100

    What does EFIS stand for?

    Electronic Flight Information System