ログイン

Instruments, Engines and Systems

Instruments, Engines and Systems
42問 • 2年前
  • Angelo Ortiz
  • 通報

    問題一覧

  • 1

    Which statement is true about magnetic deviation of a compass? Deviation

    varies for different headings of the same aircraft

  • 2

    Maximum structural cruising speed is the maximum speed at which an airplane can be operated during

    normal operations

  • 3

    Why should flight speeds above VNE be avoided?

    Design limit load factors may be exceeded, if gusts are encountered

  • 4

    Which airspeed would a pilot be unable to identify by the color coding of an airspeed indicator?

    The maneuvering speed

  • 5

    Calibrated airspeed is best described as indicated airspeed corrected for

    installation and instrument error

  • 6

    True airspeed is best described as calibrated airspeed corrected for

    altitude and nonstandard temperature

  • 7

    What is an advantage of an electric turn coordinator if the airplane has a vacuum system for other gyroscopic instruments?

    It is a backup in case of vacuum system failure

  • 8

    What is an operational difference between the turn coordinator and the turn-and-slip indicator? The turn coordinator

    indicates roll rate, rate of turn, and coordination; the turn-and-slip indicator indicates rate of turn and coordination

  • 9

    Fouling of spark plugs is more apt to occur if the aircraft

    gains altitude with no mixture adjustment

  • 10

    What will occur if no leaning is made with the mixture control as the flight altitude increases?

    The density of air entering the carburetor decreases and the amount of fuel remains constant

  • 11

    Unless adjusted, the fuel/air mixture becomes richer with an increase in altitude because the amount of fuel

    remains constant while the density of air decreases

  • 12

    The basic purpose of adjusting the fuel/air mixture control at altitude is to

    decrease the fuel flow to compensate for decreased air density

  • 13

    At high altitudes, an excessively rich mixture will cause the

    fouling of spark plugs

  • 14

    The pilot controls the air/fuel ratio with the

    mixture control

  • 15

    Fuel/air ratio is the ratio between the

    weight of fuel and weight of air entering the cylinder

  • 16

    The best power mixture is that fuel/air ratio at which

    the most power can be obtained for any given throttle setting

  • 17

    The mixture control can be adjusted, which

    prevents the fuel/air combination from becoming too rich at higher altitudes

  • 18

    What effect, if any, would a change in ambient temperature or air density have on gas turbine engine performance?

    As temperature increases, thrust decreases

  • 19

    Which statement is true concerning the effect of the application of carburetor heat?

    It enriches the fuel/air mixture

  • 20

    Applying carburetor heat will

    enrich the fuel/air mixture

  • 21

    Leaving the carburetor heat on during takeoff

    will increase the ground roll

  • 22

    Detonation occurs in a reciprocating aircraft engine when

    the unburned fuel/air charge in the cylinders is subjected to instantaneous combustion

  • 23

    Detonation can be caused by

    using a lower grade of fuel than recommended

  • 24

    The uncontrolled firing of the fuel/air charge in advance of normal spark ignition is known as

    pre-ignition

  • 25

    Detonation may occur at high-power settings when

    the fuel mixture ignites instantaneously instead of burning progressively and evenly

  • 26

    Before shutdown, while at idle, the ignition key is momentarily turned OFF. The engine continues to run with no interruption; this

    should not normally happen. Indicates a magneto not grounding in OFF position

  • 27

    A way to detect a broken magneto primary grounding lead is to

    idle the engine and momentarily turn the ignition off

  • 28

    The most probable reason an engine continues to run after the ignition switch has been turned off is

    a broken magneto ground wire

  • 29

    A detuning of engine crankshaft counterweights is a source of overstress that may be caused by

    rapid opening and closing of the throttle

  • 30

    If the ground wire between the magneto and the ignition switch becomes disconnected, the engine

    could accidently start if the propeller is moved with fuel in the cylinder

  • 31

    For internal cooling, reciprocating aircraft engines are especially dependent on

    the circulation of lubricating oil

  • 32

    An abnormally high engine oil temperature indication may be caused by

    the oil level being too low

  • 33

    Frequent inspections should be made of aircraft exhaust manifold-type heating systems to minimize the possibility of

    exhaust gases leaking into the cockpit

  • 34

    Propeller efficiency is the

    ratio of thrust horsepower to brake horsepower

  • 35

    The reason for variations in geometric pitch (twisting) along a propeller blade is that it

    permits a relatively constant angle of attack along its length when in cruising flight

  • 36

    A fixed-pitch propeller is designed for best efficiency only at a given combination of

    airspeed and RPM

  • 37

    Which statement best describes the operating principle of a constant-speed propeller?

    The propeller control regulates the engine RPM and in turn the propeller RPM

  • 38

    To develop maximum power and thrust, a constant-speed propeller should be set to a blade angle that will produce a

    small angle of attack and high RPM

  • 39

    For takeoff, the blade angle of a controllable-pitch propeller should be set at a

    small angle of attack and high RPM

  • 40

    To establish a climb after takeoff in an aircraft equipped with a constant-speed propeller, the output of the engine is reduced to climb power by decreasing manifold pressure and

    decreasing RPM by increasing propeller blade angle

  • 41

    In aircraft equipped with constant-speed propellers and normally-aspirated engines, which procedure should be used to avoid placing undue stress on the engine components? When power is being

    increased, increase the RPM before increasing the manifold pressure

  • 42

    A propeller rotating clockwise as seen from the rear, creates a spiraling slipstream that tends to rotate the airplane to the

    left around the vertical axis, and to the right around the longitudinal axis

  • B777 - Part 8

    B777 - Part 8

    Angelo Ortiz · 50問 · 3年前

    B777 - Part 8

    B777 - Part 8

    50問 • 3年前
    Angelo Ortiz

    B777 - Part 3

    B777 - Part 3

    Angelo Ortiz · 50問 · 3年前

    B777 - Part 3

    B777 - Part 3

    50問 • 3年前
    Angelo Ortiz

    B777 - Part 6

    B777 - Part 6

    Angelo Ortiz · 50問 · 3年前

    B777 - Part 6

    B777 - Part 6

    50問 • 3年前
    Angelo Ortiz

    B777 - Part 4

    B777 - Part 4

    Angelo Ortiz · 50問 · 3年前

    B777 - Part 4

    B777 - Part 4

    50問 • 3年前
    Angelo Ortiz

    B777 - Part 1

    B777 - Part 1

    Angelo Ortiz · 50問 · 3年前

    B777 - Part 1

    B777 - Part 1

    50問 • 3年前
    Angelo Ortiz

    B777 - Part 7

    B777 - Part 7

    Angelo Ortiz · 50問 · 3年前

    B777 - Part 7

    B777 - Part 7

    50問 • 3年前
    Angelo Ortiz

    B777 - Part 9

    B777 - Part 9

    Angelo Ortiz · 28問 · 3年前

    B777 - Part 9

    B777 - Part 9

    28問 • 3年前
    Angelo Ortiz

    B777 - Part 2

    B777 - Part 2

    Angelo Ortiz · 50問 · 3年前

    B777 - Part 2

    B777 - Part 2

    50問 • 3年前
    Angelo Ortiz

    B777 - Part 5

    B777 - Part 5

    Angelo Ortiz · 50問 · 3年前

    B777 - Part 5

    B777 - Part 5

    50問 • 3年前
    Angelo Ortiz

    AIA - VUL

    AIA - VUL

    Angelo Ortiz · 100問 · 2年前

    AIA - VUL

    AIA - VUL

    100問 • 2年前
    Angelo Ortiz

    Underwriting

    Underwriting

    Angelo Ortiz · 66問 · 2年前

    Underwriting

    Underwriting

    66問 • 2年前
    Angelo Ortiz

    Airplanes and Aerodynamics

    Airplanes and Aerodynamics

    Angelo Ortiz · 49問 · 2年前

    Airplanes and Aerodynamics

    Airplanes and Aerodynamics

    49問 • 2年前
    Angelo Ortiz

    Airplane Instruments, Engines and Systems

    Airplane Instruments, Engines and Systems

    Angelo Ortiz · 77問 · 2年前

    Airplane Instruments, Engines and Systems

    Airplane Instruments, Engines and Systems

    77問 • 2年前
    Angelo Ortiz

    Airport, ATC and Airspace

    Airport, ATC and Airspace

    Angelo Ortiz · 88問 · 2年前

    Airport, ATC and Airspace

    Airport, ATC and Airspace

    88問 • 2年前
    Angelo Ortiz

    Federal Aviation Regulations - Part 1

    Federal Aviation Regulations - Part 1

    Angelo Ortiz · 100問 · 2年前

    Federal Aviation Regulations - Part 1

    Federal Aviation Regulations - Part 1

    100問 • 2年前
    Angelo Ortiz

    Federal Aviation Regulations - Part 2

    Federal Aviation Regulations - Part 2

    Angelo Ortiz · 89問 · 2年前

    Federal Aviation Regulations - Part 2

    Federal Aviation Regulations - Part 2

    89問 • 2年前
    Angelo Ortiz

    Airplane Weight and Balance

    Airplane Weight and Balance

    Angelo Ortiz · 10問 · 2年前

    Airplane Weight and Balance

    Airplane Weight and Balance

    10問 • 2年前
    Angelo Ortiz

    Medical Factors and Decision Making

    Medical Factors and Decision Making

    Angelo Ortiz · 25問 · 2年前

    Medical Factors and Decision Making

    Medical Factors and Decision Making

    25問 • 2年前
    Angelo Ortiz

    Weather and Services

    Weather and Services

    Angelo Ortiz · 87問 · 2年前

    Weather and Services

    Weather and Services

    87問 • 2年前
    Angelo Ortiz

    Navigation

    Navigation

    Angelo Ortiz · 30問 · 2年前

    Navigation

    Navigation

    30問 • 2年前
    Angelo Ortiz

    Airplanes and Aerodynamics

    Airplanes and Aerodynamics

    Angelo Ortiz · 51問 · 2年前

    Airplanes and Aerodynamics

    Airplanes and Aerodynamics

    51問 • 2年前
    Angelo Ortiz

    Airports, ATC and Airspaces

    Airports, ATC and Airspaces

    Angelo Ortiz · 39問 · 2年前

    Airports, ATC and Airspaces

    Airports, ATC and Airspaces

    39問 • 2年前
    Angelo Ortiz

    Federal Aviation Regulations - Part 1

    Federal Aviation Regulations - Part 1

    Angelo Ortiz · 100問 · 2年前

    Federal Aviation Regulations - Part 1

    Federal Aviation Regulations - Part 1

    100問 • 2年前
    Angelo Ortiz

    Federal Aviation Regulations

    Federal Aviation Regulations

    Angelo Ortiz · 26問 · 2年前

    Federal Aviation Regulations

    Federal Aviation Regulations

    26問 • 2年前
    Angelo Ortiz

    Performance and Weight and Balance

    Performance and Weight and Balance

    Angelo Ortiz · 9問 · 2年前

    Performance and Weight and Balance

    Performance and Weight and Balance

    9問 • 2年前
    Angelo Ortiz

    Medical and ADM

    Medical and ADM

    Angelo Ortiz · 32問 · 2年前

    Medical and ADM

    Medical and ADM

    32問 • 2年前
    Angelo Ortiz

    Weather

    Weather

    Angelo Ortiz · 91問 · 2年前

    Weather

    Weather

    91問 • 2年前
    Angelo Ortiz

    Weather Services

    Weather Services

    Angelo Ortiz · 46問 · 2年前

    Weather Services

    Weather Services

    46問 • 2年前
    Angelo Ortiz

    Navigation

    Navigation

    Angelo Ortiz · 43問 · 2年前

    Navigation

    Navigation

    43問 • 2年前
    Angelo Ortiz

    Flight Operations

    Flight Operations

    Angelo Ortiz · 23問 · 2年前

    Flight Operations

    Flight Operations

    23問 • 2年前
    Angelo Ortiz

    Instruments

    Instruments

    Angelo Ortiz · 64問 · 2年前

    Instruments

    Instruments

    64問 • 2年前
    Angelo Ortiz

    Instrument Flying and Aerodynamics

    Instrument Flying and Aerodynamics

    Angelo Ortiz · 58問 · 2年前

    Instrument Flying and Aerodynamics

    Instrument Flying and Aerodynamics

    58問 • 2年前
    Angelo Ortiz

    Navigation Systems

    Navigation Systems

    Angelo Ortiz · 35問 · 2年前

    Navigation Systems

    Navigation Systems

    35問 • 2年前
    Angelo Ortiz

    Regulations

    Regulations

    Angelo Ortiz · 86問 · 2年前

    Regulations

    Regulations

    86問 • 2年前
    Angelo Ortiz

    Airports, ATC and Airspace

    Airports, ATC and Airspace

    Angelo Ortiz · 100問 · 2年前

    Airports, ATC and Airspace

    Airports, ATC and Airspace

    100問 • 2年前
    Angelo Ortiz

    Holding and Instrument Approaches

    Holding and Instrument Approaches

    Angelo Ortiz · 100問 · 2年前

    Holding and Instrument Approaches

    Holding and Instrument Approaches

    100問 • 2年前
    Angelo Ortiz

    Aeromedical

    Aeromedical

    Angelo Ortiz · 18問 · 2年前

    Aeromedical

    Aeromedical

    18問 • 2年前
    Angelo Ortiz

    Weather

    Weather

    Angelo Ortiz · 85問 · 2年前

    Weather

    Weather

    85問 • 2年前
    Angelo Ortiz

    Weather Services

    Weather Services

    Angelo Ortiz · 41問 · 2年前

    Weather Services

    Weather Services

    41問 • 2年前
    Angelo Ortiz

    IFR

    IFR

    Angelo Ortiz · 30問 · 2年前

    IFR

    IFR

    30問 • 2年前
    Angelo Ortiz

    NTSB

    NTSB

    Angelo Ortiz · 46問 · 2年前

    NTSB

    NTSB

    46問 • 2年前
    Angelo Ortiz

    Regulations and Hazardous Materials

    Regulations and Hazardous Materials

    Angelo Ortiz · 71問 · 2年前

    Regulations and Hazardous Materials

    Regulations and Hazardous Materials

    71問 • 2年前
    Angelo Ortiz

    General Knowledge

    General Knowledge

    Angelo Ortiz · 10問 · 1年前

    General Knowledge

    General Knowledge

    10問 • 1年前
    Angelo Ortiz

    Safety

    Safety

    Angelo Ortiz · 16問 · 1年前

    Safety

    Safety

    16問 • 1年前
    Angelo Ortiz

    Indicating/Recording Systems

    Indicating/Recording Systems

    Angelo Ortiz · 30問 · 1年前

    Indicating/Recording Systems

    Indicating/Recording Systems

    30問 • 1年前
    Angelo Ortiz

    Electrical

    Electrical

    Angelo Ortiz · 44問 · 1年前

    Electrical

    Electrical

    44問 • 1年前
    Angelo Ortiz

    Pneumatic

    Pneumatic

    Angelo Ortiz · 18問 · 1年前

    Pneumatic

    Pneumatic

    18問 • 1年前
    Angelo Ortiz

    Air Conditioning/Pressurization/Ventilation

    Air Conditioning/Pressurization/Ventilation

    Angelo Ortiz · 65問 · 1年前

    Air Conditioning/Pressurization/Ventilation

    Air Conditioning/Pressurization/Ventilation

    65問 • 1年前
    Angelo Ortiz

    Navigation/Auto Flight

    Navigation/Auto Flight

    Angelo Ortiz · 99問 · 1年前

    Navigation/Auto Flight

    Navigation/Auto Flight

    99問 • 1年前
    Angelo Ortiz

    Hydraulics

    Hydraulics

    Angelo Ortiz · 67問 · 1年前

    Hydraulics

    Hydraulics

    67問 • 1年前
    Angelo Ortiz

    Landing Gear

    Landing Gear

    Angelo Ortiz · 60問 · 1年前

    Landing Gear

    Landing Gear

    60問 • 1年前
    Angelo Ortiz

    Power Plant (CFM 56)

    Power Plant (CFM 56)

    Angelo Ortiz · 59問 · 1年前

    Power Plant (CFM 56)

    Power Plant (CFM 56)

    59問 • 1年前
    Angelo Ortiz

    Flight Control

    Flight Control

    Angelo Ortiz · 51問 · 1年前

    Flight Control

    Flight Control

    51問 • 1年前
    Angelo Ortiz

    Fuel

    Fuel

    Angelo Ortiz · 59問 · 1年前

    Fuel

    Fuel

    59問 • 1年前
    Angelo Ortiz

    APU

    APU

    Angelo Ortiz · 24問 · 1年前

    APU

    APU

    24問 • 1年前
    Angelo Ortiz

    Power Plant (IAE 2500)

    Power Plant (IAE 2500)

    Angelo Ortiz · 6回閲覧 · 29問 · 1年前

    Power Plant (IAE 2500)

    Power Plant (IAE 2500)

    6回閲覧 • 29問 • 1年前
    Angelo Ortiz

    Fire Protection

    Fire Protection

    Angelo Ortiz · 36問 · 1年前

    Fire Protection

    Fire Protection

    36問 • 1年前
    Angelo Ortiz

    Ice and Rain Protection

    Ice and Rain Protection

    Angelo Ortiz · 31問 · 1年前

    Ice and Rain Protection

    Ice and Rain Protection

    31問 • 1年前
    Angelo Ortiz

    Communications

    Communications

    Angelo Ortiz · 38問 · 1年前

    Communications

    Communications

    38問 • 1年前
    Angelo Ortiz

    Oxygen and Emergency Equipment

    Oxygen and Emergency Equipment

    Angelo Ortiz · 12問 · 1年前

    Oxygen and Emergency Equipment

    Oxygen and Emergency Equipment

    12問 • 1年前
    Angelo Ortiz

    Practice Exam 1

    Practice Exam 1

    Angelo Ortiz · 55問 · 1年前

    Practice Exam 1

    Practice Exam 1

    55問 • 1年前
    Angelo Ortiz

    Practice Exam 2

    Practice Exam 2

    Angelo Ortiz · 52問 · 1年前

    Practice Exam 2

    Practice Exam 2

    52問 • 1年前
    Angelo Ortiz

    AIRCONDITIONING - PRESSURIZATION

    AIRCONDITIONING - PRESSURIZATION

    Angelo Ortiz · 59問 · 1年前

    AIRCONDITIONING - PRESSURIZATION

    AIRCONDITIONING - PRESSURIZATION

    59問 • 1年前
    Angelo Ortiz

    AUXILIARY POWER UNIT

    AUXILIARY POWER UNIT

    Angelo Ortiz · 21問 · 1年前

    AUXILIARY POWER UNIT

    AUXILIARY POWER UNIT

    21問 • 1年前
    Angelo Ortiz

    COMMUNICATIONS

    COMMUNICATIONS

    Angelo Ortiz · 32問 · 1年前

    COMMUNICATIONS

    COMMUNICATIONS

    32問 • 1年前
    Angelo Ortiz

    ELECTRICAL SYSTEM

    ELECTRICAL SYSTEM

    Angelo Ortiz · 39問 · 1年前

    ELECTRICAL SYSTEM

    ELECTRICAL SYSTEM

    39問 • 1年前
    Angelo Ortiz

    INDICATING/RECORDING SYSTEMS

    INDICATING/RECORDING SYSTEMS

    Angelo Ortiz · 21問 · 1年前

    INDICATING/RECORDING SYSTEMS

    INDICATING/RECORDING SYSTEMS

    21問 • 1年前
    Angelo Ortiz

    FIRE PROTECTION

    FIRE PROTECTION

    Angelo Ortiz · 17問 · 1年前

    FIRE PROTECTION

    FIRE PROTECTION

    17問 • 1年前
    Angelo Ortiz

    FLIGHT CONTROLS

    FLIGHT CONTROLS

    Angelo Ortiz · 43問 · 1年前

    FLIGHT CONTROLS

    FLIGHT CONTROLS

    43問 • 1年前
    Angelo Ortiz

    FMGS NAVIGATION

    FMGS NAVIGATION

    Angelo Ortiz · 76問 · 1年前

    FMGS NAVIGATION

    FMGS NAVIGATION

    76問 • 1年前
    Angelo Ortiz

    FUEL SYSTEM

    FUEL SYSTEM

    Angelo Ortiz · 48問 · 1年前

    FUEL SYSTEM

    FUEL SYSTEM

    48問 • 1年前
    Angelo Ortiz

    HYDRAULIC SYSTEM

    HYDRAULIC SYSTEM

    Angelo Ortiz · 62問 · 1年前

    HYDRAULIC SYSTEM

    HYDRAULIC SYSTEM

    62問 • 1年前
    Angelo Ortiz

    ICE AND RAIN

    ICE AND RAIN

    Angelo Ortiz · 30問 · 1年前

    ICE AND RAIN

    ICE AND RAIN

    30問 • 1年前
    Angelo Ortiz

    LANDING GEAR

    LANDING GEAR

    Angelo Ortiz · 49問 · 1年前

    LANDING GEAR

    LANDING GEAR

    49問 • 1年前
    Angelo Ortiz

    OXYGEN-EMERGENCY EQUIPMENT

    OXYGEN-EMERGENCY EQUIPMENT

    Angelo Ortiz · 9問 · 1年前

    OXYGEN-EMERGENCY EQUIPMENT

    OXYGEN-EMERGENCY EQUIPMENT

    9問 • 1年前
    Angelo Ortiz

    PNEUMATIC SYSTEM

    PNEUMATIC SYSTEM

    Angelo Ortiz · 13問 · 1年前

    PNEUMATIC SYSTEM

    PNEUMATIC SYSTEM

    13問 • 1年前
    Angelo Ortiz

    POWERPLANT

    POWERPLANT

    Angelo Ortiz · 49問 · 1年前

    POWERPLANT

    POWERPLANT

    49問 • 1年前
    Angelo Ortiz

    SAFETY

    SAFETY

    Angelo Ortiz · 13問 · 1年前

    SAFETY

    SAFETY

    13問 • 1年前
    Angelo Ortiz

    SMOKE

    SMOKE

    Angelo Ortiz · 12問 · 1年前

    SMOKE

    SMOKE

    12問 • 1年前
    Angelo Ortiz

    A320 - Limitations

    A320 - Limitations

    Angelo Ortiz · 62問 · 1年前

    A320 - Limitations

    A320 - Limitations

    62問 • 1年前
    Angelo Ortiz

    問題一覧

  • 1

    Which statement is true about magnetic deviation of a compass? Deviation

    varies for different headings of the same aircraft

  • 2

    Maximum structural cruising speed is the maximum speed at which an airplane can be operated during

    normal operations

  • 3

    Why should flight speeds above VNE be avoided?

    Design limit load factors may be exceeded, if gusts are encountered

  • 4

    Which airspeed would a pilot be unable to identify by the color coding of an airspeed indicator?

    The maneuvering speed

  • 5

    Calibrated airspeed is best described as indicated airspeed corrected for

    installation and instrument error

  • 6

    True airspeed is best described as calibrated airspeed corrected for

    altitude and nonstandard temperature

  • 7

    What is an advantage of an electric turn coordinator if the airplane has a vacuum system for other gyroscopic instruments?

    It is a backup in case of vacuum system failure

  • 8

    What is an operational difference between the turn coordinator and the turn-and-slip indicator? The turn coordinator

    indicates roll rate, rate of turn, and coordination; the turn-and-slip indicator indicates rate of turn and coordination

  • 9

    Fouling of spark plugs is more apt to occur if the aircraft

    gains altitude with no mixture adjustment

  • 10

    What will occur if no leaning is made with the mixture control as the flight altitude increases?

    The density of air entering the carburetor decreases and the amount of fuel remains constant

  • 11

    Unless adjusted, the fuel/air mixture becomes richer with an increase in altitude because the amount of fuel

    remains constant while the density of air decreases

  • 12

    The basic purpose of adjusting the fuel/air mixture control at altitude is to

    decrease the fuel flow to compensate for decreased air density

  • 13

    At high altitudes, an excessively rich mixture will cause the

    fouling of spark plugs

  • 14

    The pilot controls the air/fuel ratio with the

    mixture control

  • 15

    Fuel/air ratio is the ratio between the

    weight of fuel and weight of air entering the cylinder

  • 16

    The best power mixture is that fuel/air ratio at which

    the most power can be obtained for any given throttle setting

  • 17

    The mixture control can be adjusted, which

    prevents the fuel/air combination from becoming too rich at higher altitudes

  • 18

    What effect, if any, would a change in ambient temperature or air density have on gas turbine engine performance?

    As temperature increases, thrust decreases

  • 19

    Which statement is true concerning the effect of the application of carburetor heat?

    It enriches the fuel/air mixture

  • 20

    Applying carburetor heat will

    enrich the fuel/air mixture

  • 21

    Leaving the carburetor heat on during takeoff

    will increase the ground roll

  • 22

    Detonation occurs in a reciprocating aircraft engine when

    the unburned fuel/air charge in the cylinders is subjected to instantaneous combustion

  • 23

    Detonation can be caused by

    using a lower grade of fuel than recommended

  • 24

    The uncontrolled firing of the fuel/air charge in advance of normal spark ignition is known as

    pre-ignition

  • 25

    Detonation may occur at high-power settings when

    the fuel mixture ignites instantaneously instead of burning progressively and evenly

  • 26

    Before shutdown, while at idle, the ignition key is momentarily turned OFF. The engine continues to run with no interruption; this

    should not normally happen. Indicates a magneto not grounding in OFF position

  • 27

    A way to detect a broken magneto primary grounding lead is to

    idle the engine and momentarily turn the ignition off

  • 28

    The most probable reason an engine continues to run after the ignition switch has been turned off is

    a broken magneto ground wire

  • 29

    A detuning of engine crankshaft counterweights is a source of overstress that may be caused by

    rapid opening and closing of the throttle

  • 30

    If the ground wire between the magneto and the ignition switch becomes disconnected, the engine

    could accidently start if the propeller is moved with fuel in the cylinder

  • 31

    For internal cooling, reciprocating aircraft engines are especially dependent on

    the circulation of lubricating oil

  • 32

    An abnormally high engine oil temperature indication may be caused by

    the oil level being too low

  • 33

    Frequent inspections should be made of aircraft exhaust manifold-type heating systems to minimize the possibility of

    exhaust gases leaking into the cockpit

  • 34

    Propeller efficiency is the

    ratio of thrust horsepower to brake horsepower

  • 35

    The reason for variations in geometric pitch (twisting) along a propeller blade is that it

    permits a relatively constant angle of attack along its length when in cruising flight

  • 36

    A fixed-pitch propeller is designed for best efficiency only at a given combination of

    airspeed and RPM

  • 37

    Which statement best describes the operating principle of a constant-speed propeller?

    The propeller control regulates the engine RPM and in turn the propeller RPM

  • 38

    To develop maximum power and thrust, a constant-speed propeller should be set to a blade angle that will produce a

    small angle of attack and high RPM

  • 39

    For takeoff, the blade angle of a controllable-pitch propeller should be set at a

    small angle of attack and high RPM

  • 40

    To establish a climb after takeoff in an aircraft equipped with a constant-speed propeller, the output of the engine is reduced to climb power by decreasing manifold pressure and

    decreasing RPM by increasing propeller blade angle

  • 41

    In aircraft equipped with constant-speed propellers and normally-aspirated engines, which procedure should be used to avoid placing undue stress on the engine components? When power is being

    increased, increase the RPM before increasing the manifold pressure

  • 42

    A propeller rotating clockwise as seen from the rear, creates a spiraling slipstream that tends to rotate the airplane to the

    left around the vertical axis, and to the right around the longitudinal axis