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Practice Exam 2
  • Angelo Ortiz

  • 問題数 52 • 7/18/2024

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    問題一覧

  • 1

    Which hydraulic system is used for gear retraction/extension?

    Green

  • 2

    Does the alternate brake system have anti skid protection?

    Yes, if the A/SKID & N/W STRG switch is ON

  • 3

    Which computer controls the landing gear indicator panel lights?

    Landing Gear Control Interface Unit (LGCIU) 1 only

  • 4

    What would be the consequence if the pilots’ respective handwheels were turned in the same direction but at different rates?

    Orders are added algebraically

  • 5

    What is the maximum deflection of the nose wheel if controlled by the rudder pedals?

    6 deg

  • 6

    What could cause the center tank indication to become boxed amber

    Both center tank pumps are failed, or are switched OFF

  • 7

    When is the LO LVL warning displayed on the ECAM?

    When the fuel quantity in one wing tank goes below 750 kg

  • 8

    Will the center pumps, if commanded ON, operate if slats are extended?

    Yes, if CTR TK MODE SEL is set to MAN

  • 9

    When will fuel automatically transfer from the outer to the inner wing tanks?

    When any inner tank fuel reaches 750 kg

  • 10

    What is the purpose of the fuel recirculation system?

    Ensures the IDG cooling

  • 11

    What source supplies hot air for engine anti ice?

    An independent air bleed from the high pressure compressor protects each engine nacelle from ice

  • 12

    Regarding window heat, how many power levels do we have?

    Low on ground and normal in flight for the windshield; one level for windows

  • 13

    How many Probe Heat Computers (PHCs) are installed on an A320?

    3

  • 14

    Is it possible to select wing anti ice on ground?

    Yes, the wing anti icing control valves open for 30 sec only (test sequence)

  • 15

    Regarding the Manual engine start procedure on ground, which statement is true:

    The FADEC monitors the engine during a manual start and aborts the start on the ground, if the start EGT limit is exceeded before reaching 50% N2

  • 16

    Regarding Full Authority Digital Engine Control (FADEC), which statement is true?

    Each FADEC has 2 channels, one of which is active and the other is on standby

  • 17

    Some of the fuel flowing out of the Hydromechanical Unit (HMU) cools the oil systems of the IDG and:

    Then returns to the tank or fuel pump unit

  • 18

    During manual engine start on the ground:

    Both igniters are cut off when N2 reaches approximately 50%

  • 19

    What is the minimum oil quantity for aircraft dispatch?

    Oil quantity must be at or above 9.5 qt + estimated consumption (max average estimated consumption ~ 0.5 qt/h)

  • 20

    Single engine, what is the maximum time limit in TOGA power?

    10 min

  • 21

    On the overhead maintenance panel, what is the function of the TMR reset p/b?

    The maintenance crew uses this p/b to reset the control circuit, after the system has operated

  • 22

    HI ALT SET memo ID displayed on the ECAM indicates what?

    It indicates that the crew set the HI ALT LANDING p/b to ON and in this case the masks drop if the cabin pressure exceeds 16,000 feet

  • 23

    When the masks in the cabin are released, the passenger address system automatically broadcasts pre-recorded instructions for their use

    True

  • 24

    Can an engine fire be detected if one loop is faulty

    Yes

  • 25

    How many smoke detectors, in total, are installed in the FWD and AFT cargo compartment?

    6

  • 26

    When the pilot pushes the ENG 1 (or 2) fire p/b, what will be the effect?

    Silences the aural fire warning, arms the fire extinguisher squibs, closes the low pressure fuel valve, closes the hydraulic fire shut off valve, closes the engine bleed valve, closes the pack flow control valve, cuts off the FADEC power supply and deactivates the IDG

  • 27

    If the system detects an APU fire while the aircraft is on the ground, what happens?

    The system shuts down the APU automatically and discharges extinguishing agent

  • 28

    The engines and the APU each have a fire and overheat detection system consisting of:

    Two identical gas detection loops (A and B) mounted in parallel and a Fire Detection Unit (FDU)

  • 29

    If the frequency is tuned on the RMP, how is it activated?

    By pushing the transfer key

  • 30

    Which panel is used to select a VHF transceiver?

    Audio Control Panel (ACP)

  • 31

    When is the Cockpit Voice Recorder (CVR) automatically energized?

    On the ground when one engine is operating

  • 32

    What interphone system is used for the ground mechanic jack on the external power panel?

    Flight crew interphone

  • 33

    How many passenger doors are fitted on an A320?

    4

  • 34

    What is true regarding the cockpit sliding windows?

    Each escape rope is long enough to reach the ground from any window

  • 35

    What color on the S/D DOOR page indicates that a slide is armed?

    White

  • 36

    With the EMER EXIT LT selector at ARM, when does the emergency escape path marking system come on?

    When normal aircraft electrical power fails, or when DC SHED ESS BUS is lost

  • 37

    How do you adjust the brightness of the Flight Control Unit (FCU) displays?

    Using the rotary switch located beneath the FCU

  • 38

    The NAV&LOGO switch has two positions, 1 and 2. What is the difference between the two positions?

    Position 1 turns on the logo lights and the first set of nav lights, position 2 turn on the logo lights and the second set of nav lights

  • 39

    Where will you find the water and waste control panel?

    On the forward attendant control panel

  • 40

    On the ground and below 16,000 feet, how is the necessary differential pressure produced to force waste from the toilet bowls into the storage tank?

    A vacuum generator produces the necessary pressure differential

  • 41

    How many turns and in which direction, must the flight crew crank the EMERGENCY EXTENSION handle to extend the landing gear by gravity?

    3 turns clockwise

  • 42

    At which speed does the landing gear safety valve close?

    260 knots

  • 43

    How many engine fuel pumps are installed on an Airbus 320?

    6

  • 44

    Which surfaces are protected with hot air?

    Three outboard leading-edge slats of each wing and engine air intakes

  • 45

    If the ENG 1 or ENG 2 master switch are set to off, which fuel shut off valves are affected?

    The LP and HP fuel valves

  • 46

    Which engine parameters are displayed on the E/WD?

    N1, N2. EGT and F.F.

  • 47

    How many cargo fire extinguisher bottles are installed?

    1 bottle that can discharge in either compartment

  • 48

    What happens if the captains RMP is unserviceable?

    The remaining RMP controls all the transceivers

  • 49

    What is the purpose of the red “CABIN PRESSURE” light installed on the passenger doors?

    Flashes when one or both engines are stopped, the slides are disarmed and the cabin differential pressure is more than 2.5 Hpa

  • 50

    Which hydraulic system provides pressure for operation of the FWD and AFT cargo doors?

    Yellow

  • 51

    How is the NO SMOKING sign controlled when the switch is in AUTO position?

    NO SMOKING light will illuminate when either the landing gear is extended, or flaps/slats are extended (position 1, 2, 3 or FULL)

  • 52

    What is the capacity of the waste tank?

    170 l