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FUEL SYSTEM
  • Angelo Ortiz

  • 問題数 48 • 7/31/2024

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    問題一覧

  • 1

    APU fuel is supplied by:

    Either one

  • 2

    Amber FAULT light illuminates on MODE SEL pushbutton when:

    Center tank has more than 250 kg and any wing tank has less than 5,000 kg

  • 3

    Amber FAULT light illuminates on tank pump pb when:

    The delivery fuel pressure drops

  • 4

    Are the engines still supplied in case of fuel filter CLOG:

    Yes, fuel bypassing the fuel filter (bypass valve)

  • 5

    At which fuel quantity is the low level "LO LVL" warning triggered on the ECAM?

    Below 750 kg (1650 lb)

  • 6

    During take off, center tank fuel is:

    Not supplied while slats are extended

  • 7

    FOB ( Fuel on Board) half-boxed amber on EW/D means:

    The quantity shown is not fully usable

  • 8

    For what purpose is fuel used by electrical systems?

    To cool the IDG oil

  • 9

    How can you check that fuel quantity (FQI) is in degraded mode?

    FQ indication is dashed amber across the two last digits on the upper ECAM and ECAM fuel page must be called to check which tank is affected

  • 10

    How many cells in each wing tank?

    Two

  • 11

    How many channels is/are used in the Fuel Quantity Indications System?

    2

  • 12

    How many pumps are there in each fuel tank?

    Two fuel pumps in each wing tank

  • 13

    If open, when will the transfer valves close again?

    Transfer valves close automatically at the next refueling operation

  • 14

    In case of single engine operation:

    Cross feed valve must be kept open

  • 15

    In normal operation the cross feed valve is:

    Closed for the take off

  • 16

    In normal operation, each engine is supplied by:

    Two wing tank pumps and one center tank pump

  • 17

    Is the gravity feeding from center tank possible:

    No

  • 18

    On the crossfeed pb, what is the meaning of the "ON" white light?

    The valve opens

  • 19

    Suction valves are:

    Normally closed by pumps pressure

  • 20

    The LP valves are controlled to off position by:

    Engine master switches and fire pushbuttons

  • 21

    The engine low pressure (LP) valve is closed by:

    Engine fire pb or the engine MASTER SW

  • 22

    The fuel return valve is controlled by:

    FADEC

  • 23

    The maximum fuel imbalance is (Take Off & Landing) at heavier tank full:

    1,500 kg

  • 24

    The maximum refueling pressure is:

    50 psi (3.5 bars)

  • 25

    The normal tank filling order is:

    Wing tanks then center tank

  • 26

    What are the minimum fuel quantity for the take off and maximum fuel quantity imbalance (heavier tank full) for take off or landing?

    1500 kg - 1500 kg

  • 27

    What does the FAULT light illuminated amber in the wing tank pb indicate?

    Delivery pressure drops

  • 28

    What does the MODE SEL pb control:

    Center tank pumps only

  • 29

    What happens to the IDG cooling fuel when the outer cells are full:

    Fuel overflows into the inner cell through a spill pipe

  • 30

    What happens to the IDG cooling fuel when the wing tank is full:

    The system select CTR TK pumps off. WING TK pumps feed approx. 500 kg, then CTR TK pumps run again

  • 31

    What is the maximum total fuel capacity?

    19,004 kg

  • 32

    What is the purpose of the capacitance probes?

    Both are correct

  • 33

    What is the purpose of the pressure relief sequence valves?

    When all pumps are running, center pumps will deliver fuel preferentially

  • 34

    What is the refueling time at nominal pressure (approx):

    Either (20 mins for all tanks) or (17 mins for wing tanks)

  • 35

    When passing FL 200 gravity feeding occurs, what is the maximum flight level:

    150 (FL 100 if jet B)

  • 36

    When the center tank is empty (MODE SEL at AUTO), center tank pumps:

    Stop automatically 5 min. after LO level is reached in center tank

  • 37

    When the wing tank pb is set OFF, the FAULT light is:

    Inhibited

  • 38

    Where are the transfer valves located?

    On each sealed rib of each wing tank

  • 39

    Where can you check the fuel quantity of each tank?

    On ECAM lower display FUEL page only

  • 40

    Where is the fuel remaining in the surge tank scavenged?

    Outer cell

  • 41

    Where is the vent surge tank located?

    Outboard of each wing tank

  • 42

    Where is the vent surge tank located?

    In the outer section of each wing

  • 43

    Which type of motor controls the fuel cross feed valve?

    Double

  • 44

    Why has a 2% additional space been provided in each fuel tank?

    For fuel expansion without spillage into the vent surge tank

  • 45

    With all fuel pumps switches ON, are wing tank pumps running while center tank is supplying?

    Yes, wing tank pumps are always running

  • 46

    With fuel in all tanks, in flight, fuel is used:

    From the center tank, then from the inner cells to predetermined level, then outer cell fuel combines with inner cell fuel

  • 47

    With slats extended, the center tank pumps run on ground:

    Yes, after engine start for 2 mins.

  • 48

    FOB (Fuel on Board) half-boxed amber on ECAM FUEL page means:

    Both transfer valves fail to open when inner cell is at low level