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40問 • 1年前
  • ユーザ名非公開
  • 通報

    問題一覧

  • 1

    The primary condition(s) that allow(s) microorganisms to grow in the fuel in aircraft fuel tank is (are)

    The presence of water

  • 2

    Boost pumps in a fuel system

    Provide positive flow of fuel to the engine pump.

  • 3

     It is desirable that fuel lines have a gentle slope upward or downward and not have sharp curves or sharp rises and/or falls in order to

    Prevent vapor lock

  • 4

    Kerosene is used as turbine engine fuel because

    Kerosene has more heat per gallon and lubricates fuel system components

  • 5

    Where physical separation of the fuel lines from electrical wiring or conduit is impracticable, locate the fuel line

    Below the wiring and clamp the line securely to the airframe structure

  • 6

    What are the principal advantages of the duplex fuel nozzle used in many turbine engines?

    Provides better atomization and uniform flow pattern

  • 7

    What is the final authority for the details of carburetor overhaul?

    The manufacturer’s recommendations

  • 8

    Which of the following turbine fuel filters has the greatest filtering action of any present day filter type?

    Micron filter

  • 9

    When an electric primer is used, fuel pressure is built up by the

    Booster pump

  • 10

    (Refer to Figure 7) What is the purpose of the fuel transfer ejectors?

    To assist in the transfer of fuel from the main tank to the boost pump sump

  • 11

     Fuel pressure produced by the engine-driven fuel pump is adjusted by the

    Relief valve adjusting screw

  • 12

     It is necessary to control acceleration and deceleration rates in turbine engines in order to

    Prevent blowout or die-out

  • 13

    Fuel boost pumps are operated

    To provide a positive flow of fuel to the engine

  • 14

    Maximum power is normally considered to be developed in a reciprocating engine with a fuel/air mixture ratio of approximately

    12:1

  • 15

    Fuel crossfeed systems are used in aircraft to

    Maintain aircraft stability

  • 16

     The fuel pump relief valve directs excess fuel to the

    Inlet side of the fuel pump

  • 17

    What causes the fuel divider valve to open in a turbine engine duplex fuel nozzle?

    Fuel pressure

  • 18

    The fuel systems of aircraft certificated in the standard classification must include which of the following?

    A positive means of shutting off the fuel to all engines

  • 19

    If an engine equipped with a float-type carburetor backfires or misses when the throttle is advanced, a likely cause is that the

    Accelerating pump is not operating properly

  • 20

     What is a characteristics of a centrifugal-type fuel boost pump?

    It separates air and vapor from the fuel

  • 21

    A fuel strainer or filter must be located between the

    Tank outlet and the fuel metering device

  • 22

    The purpose of the diaphragm in most vane-type fuel pumps is to

    Compensate fuel pressures to altitude changes

  • 23

    Fuel pump relief valves designed to compensate for atmospheric pressure variations are known as

    Balanced-type relief valves

  • 24

    How often should float carburetors be overhauled?

    At engine overhaul

  • 25

    What precaution should be taken when putting thread lubricant on a tapered pipe plug in a carburetor float bowl?

    Engage the first thread of the plug, then put a small amount of lubricant on the second thread and screw the plug in

  • 26

    During what period does the fuel pump bypass valve open and remain open?

    When the boost pump pressure is greater then fuel pump pressure

  • 27

    Fuel lines are kept away from sources of heat, and sharp bends and steep rises are avoided to reduce the possibility of

    Vapor lock

  • 28

    Where is the engine fuel shutoff valve usually located?

    Aft of the firewall

  • 29

    What is the purpose of an engine-driven fuel pump bypass valve?

    To prevent a damaged or inoperative pump from blocking the fuel flow of another pump in series with it

  • 30

    Which type of pump is commonly used as a fuel pump on reciprocating engines?

    Vane

  • 31

    What is the purpose of the flow divider in a turbine engine duplex fuel nozzle?

    Creates the primary and secondary fuel supplies

  • 32

    Excessively rich or lean idle mixtures result in

    Incomplete combustion

  • 33

    Boost pumps in a fuel system

    Provide a positive flow of fuel to the engine pump

  • 34

    A pilot reports that the fuel pressure fluctuates and exceeds the upper limits whenever the throttle is advanced. The most likely cause of the trouble is

    A sticking fuel pump relief valve

  • 35

     A rotary-vane pump is best described as a

    Positive-displacement pump

  • 36

    Which of the following statements concerning a centrifugal-type fuel boost pump located in a fuel supply tank is NOT true?

    The centrifugal-type pump is classified as a positive displacement pump

  • 37

    Where should the main fuel strainer be located in the aircraft fuel system?

    At the lowest point in the fuel system

  • 38

    The Federal Aviation Regulations require the fuel flow rate for gravity systems (main and reserve) to be

    150 percent of the takeoff fuel consumption of the engine

  • 39

    Most large aircraft reciprocating engines are equipped with which of the following types of engine-driven fuel pumps?

    Rotary-vane-type fuel pump

  • 40

    Which statement is true regarding proper throttle rigging of an airplane?

    The throttle stop on the carburetor must be contacted before the stop in the cockpit

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    ユーザ名非公開 · 36問 · 1年前

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    FUEL METERING SYSTEM

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    ユーザ名非公開 · 95問 · 1年前

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    95問 • 1年前
    ユーザ名非公開

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    ユーザ名非公開 · 39問 · 1年前

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    ユーザ名非公開 · 100問 · 1年前

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    ユーザ名非公開 · 32問 · 1年前

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    ユーザ名非公開 · 39問 · 1年前

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    39問 • 1年前
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    問題一覧

  • 1

    The primary condition(s) that allow(s) microorganisms to grow in the fuel in aircraft fuel tank is (are)

    The presence of water

  • 2

    Boost pumps in a fuel system

    Provide positive flow of fuel to the engine pump.

  • 3

     It is desirable that fuel lines have a gentle slope upward or downward and not have sharp curves or sharp rises and/or falls in order to

    Prevent vapor lock

  • 4

    Kerosene is used as turbine engine fuel because

    Kerosene has more heat per gallon and lubricates fuel system components

  • 5

    Where physical separation of the fuel lines from electrical wiring or conduit is impracticable, locate the fuel line

    Below the wiring and clamp the line securely to the airframe structure

  • 6

    What are the principal advantages of the duplex fuel nozzle used in many turbine engines?

    Provides better atomization and uniform flow pattern

  • 7

    What is the final authority for the details of carburetor overhaul?

    The manufacturer’s recommendations

  • 8

    Which of the following turbine fuel filters has the greatest filtering action of any present day filter type?

    Micron filter

  • 9

    When an electric primer is used, fuel pressure is built up by the

    Booster pump

  • 10

    (Refer to Figure 7) What is the purpose of the fuel transfer ejectors?

    To assist in the transfer of fuel from the main tank to the boost pump sump

  • 11

     Fuel pressure produced by the engine-driven fuel pump is adjusted by the

    Relief valve adjusting screw

  • 12

     It is necessary to control acceleration and deceleration rates in turbine engines in order to

    Prevent blowout or die-out

  • 13

    Fuel boost pumps are operated

    To provide a positive flow of fuel to the engine

  • 14

    Maximum power is normally considered to be developed in a reciprocating engine with a fuel/air mixture ratio of approximately

    12:1

  • 15

    Fuel crossfeed systems are used in aircraft to

    Maintain aircraft stability

  • 16

     The fuel pump relief valve directs excess fuel to the

    Inlet side of the fuel pump

  • 17

    What causes the fuel divider valve to open in a turbine engine duplex fuel nozzle?

    Fuel pressure

  • 18

    The fuel systems of aircraft certificated in the standard classification must include which of the following?

    A positive means of shutting off the fuel to all engines

  • 19

    If an engine equipped with a float-type carburetor backfires or misses when the throttle is advanced, a likely cause is that the

    Accelerating pump is not operating properly

  • 20

     What is a characteristics of a centrifugal-type fuel boost pump?

    It separates air and vapor from the fuel

  • 21

    A fuel strainer or filter must be located between the

    Tank outlet and the fuel metering device

  • 22

    The purpose of the diaphragm in most vane-type fuel pumps is to

    Compensate fuel pressures to altitude changes

  • 23

    Fuel pump relief valves designed to compensate for atmospheric pressure variations are known as

    Balanced-type relief valves

  • 24

    How often should float carburetors be overhauled?

    At engine overhaul

  • 25

    What precaution should be taken when putting thread lubricant on a tapered pipe plug in a carburetor float bowl?

    Engage the first thread of the plug, then put a small amount of lubricant on the second thread and screw the plug in

  • 26

    During what period does the fuel pump bypass valve open and remain open?

    When the boost pump pressure is greater then fuel pump pressure

  • 27

    Fuel lines are kept away from sources of heat, and sharp bends and steep rises are avoided to reduce the possibility of

    Vapor lock

  • 28

    Where is the engine fuel shutoff valve usually located?

    Aft of the firewall

  • 29

    What is the purpose of an engine-driven fuel pump bypass valve?

    To prevent a damaged or inoperative pump from blocking the fuel flow of another pump in series with it

  • 30

    Which type of pump is commonly used as a fuel pump on reciprocating engines?

    Vane

  • 31

    What is the purpose of the flow divider in a turbine engine duplex fuel nozzle?

    Creates the primary and secondary fuel supplies

  • 32

    Excessively rich or lean idle mixtures result in

    Incomplete combustion

  • 33

    Boost pumps in a fuel system

    Provide a positive flow of fuel to the engine pump

  • 34

    A pilot reports that the fuel pressure fluctuates and exceeds the upper limits whenever the throttle is advanced. The most likely cause of the trouble is

    A sticking fuel pump relief valve

  • 35

     A rotary-vane pump is best described as a

    Positive-displacement pump

  • 36

    Which of the following statements concerning a centrifugal-type fuel boost pump located in a fuel supply tank is NOT true?

    The centrifugal-type pump is classified as a positive displacement pump

  • 37

    Where should the main fuel strainer be located in the aircraft fuel system?

    At the lowest point in the fuel system

  • 38

    The Federal Aviation Regulations require the fuel flow rate for gravity systems (main and reserve) to be

    150 percent of the takeoff fuel consumption of the engine

  • 39

    Most large aircraft reciprocating engines are equipped with which of the following types of engine-driven fuel pumps?

    Rotary-vane-type fuel pump

  • 40

    Which statement is true regarding proper throttle rigging of an airplane?

    The throttle stop on the carburetor must be contacted before the stop in the cockpit