暗記メーカー

暗記メーカー

​
ログイン
M17c3
20問 • 15日前
  • ユーザ名非公開
    • 通報

    問題一覧

  • 1

    When the pilot select propeller to Beta range the propeller will

    operates between maximum reverse pitch and flight idle pitch.

  • 2

    In Beta range, propeller pitch is directly controlled by

    power lever.

  • 3

    in order to un feather the propeller

    a separate source of oil under pressure that supplied to the propeller hub

  • 4

    If the pilot set the propeller to beta range when the power lever is advanced engine throttle (increase fuel flow)

    propeller blade angle will increase.

  • 5

    Constant Speed propeller speed

    remains constant whilst running stationary and facing into head wind.

  • 6

    If force applied to the top of speeder spring (increasing RPM),

    blade angle moves to fine pitch.

  • 7

    Constant Speed Propeller for take-off is

    set to low pitch (fine) and high RPM position

  • 8

    A propeller control Unit is supplied with oil from the

    Engine oil system

  • 9

    Propeller is fitted with a counterweight at the blade root which is used to make it move toward fine-pitch

    the oil pressure

  • 10

    If the propeller governor flyweights overcome the speeder spring the propeller

    is over speeding

  • 11

    A constant speed Propeller provides maximum efficiency

    by Adjusting blade angle for most condition encountered during flight.

  • 12

    The constant speed control unit is also called

    a governor

  • 13

    Propeller over speed governor is a backup for propeller governor and is mounted on reduction gear box

    it has its own flyweight and pilot valve

  • 14

    When the compressive force on a speeder spring is reduced the propeller blade will

    coarsen

  • 15

    On an over speed condition, the blades are Turned

    to coarse pitch

  • 16

    If a force is a applied to the speeder spring what will happen

    blade angle finer

  • 17

    Many types of constant speed propeller

    use governor

  • 18

    Constant speed propeller system

    permits the pilot to select propeller and engine speed

  • 19

    Governor oil pump and the flyweight assembly are driven by

    geared to the engine

  • 20

    The rotational speed of the flyweight assembly varies

    directly with engine speed and control the position of the pilot valve

    • M17c6

    M17c6

    ユーザ名非公開 · 19問 · 15日前

    M17c6

    M17c6

    19問 • 15日前
    ユーザ名非公開

    M17c4

    M17c4

    ユーザ名非公開 · 7問 · 15日前

    M17c4

    M17c4

    7問 • 15日前
    ユーザ名非公開

    M17c2

    M17c2

    ユーザ名非公開 · 26問 · 15日前

    M17c2

    M17c2

    26問 • 15日前
    ユーザ名非公開

    M17c1

    M17c1

    ユーザ名非公開 · 21問 · 15日前

    M17c1

    M17c1

    21問 • 15日前
    ユーザ名非公開

    BASICS AERODYNAMICS

    BASICS AERODYNAMICS

    Nicole · 51問 · 1ヶ月前

    BASICS AERODYNAMICS

    BASICS AERODYNAMICS

    51問 • 1ヶ月前
    Nicole

    CRM Y FISIOLOGÍA DE VUELO SKYVIP

    CRM Y FISIOLOGÍA DE VUELO SKYVIP

    ユーザ名非公開 · 50問 · 2ヶ月前

    CRM Y FISIOLOGÍA DE VUELO SKYVIP

    CRM Y FISIOLOGÍA DE VUELO SKYVIP

    50問 • 2ヶ月前
    ユーザ名非公開

    A320 GEN FAM

    A320 GEN FAM

    ユーザ名非公開 · 100問 · 2ヶ月前

    A320 GEN FAM

    A320 GEN FAM

    100問 • 2ヶ月前
    ユーザ名非公開

    M15c16

    M15c16

    مقطع من الاغاني عراقيه قصيره · 14問 · 2ヶ月前

    M15c16

    M15c16

    14問 • 2ヶ月前
    مقطع من الاغاني عراقيه قصيره

    M7c17

    M7c17

    ユーザ名非公開 · 14問 · 2ヶ月前

    M7c17

    M7c17

    14問 • 2ヶ月前
    ユーザ名非公開

    9 Fuel System

    9 Fuel System

    Via · 49問 · 4ヶ月前

    9 Fuel System

    9 Fuel System

    49問 • 4ヶ月前
    Via

    Ivan 2

    Ivan 2

    Via · 40問 · 4ヶ月前

    Ivan 2

    Ivan 2

    40問 • 4ヶ月前
    Via

    Aircraft Familiarization

    Aircraft Familiarization

    Benjie · 156問 · 6ヶ月前

    Aircraft Familiarization

    Aircraft Familiarization

    156問 • 6ヶ月前
    Benjie

    Class 2 Principal Airports

    Class 2 Principal Airports

    Saint Thomas Aquinas! · 23問 · 1年前

    Class 2 Principal Airports

    Class 2 Principal Airports

    23問 • 1年前
    Saint Thomas Aquinas!

    CLASSIFICATION of AIRPORTS CAAP and ATO

    CLASSIFICATION of AIRPORTS CAAP and ATO

    Saint Thomas Aquinas! · 33問 · 1年前

    CLASSIFICATION of AIRPORTS CAAP and ATO

    CLASSIFICATION of AIRPORTS CAAP and ATO

    33問 • 1年前
    Saint Thomas Aquinas!

    ALL Carrier Codes (Airline Codes)

    ALL Carrier Codes (Airline Codes)

    Saint Thomas Aquinas! · 95問 · 1年前

    ALL Carrier Codes (Airline Codes)

    ALL Carrier Codes (Airline Codes)

    95問 • 1年前
    Saint Thomas Aquinas!

    test 2

    test 2

    ユーザ名非公開 · 35問 · 1年前

    test 2

    test 2

    35問 • 1年前
    ユーザ名非公開

    ATE MULTIPLE Choice

    ATE MULTIPLE Choice

    Miles T. · 79問 · 1年前

    ATE MULTIPLE Choice

    ATE MULTIPLE Choice

    79問 • 1年前
    Miles T.

    HYDRAULIC AND PNUEMATIC POWER SYSTEM

    HYDRAULIC AND PNUEMATIC POWER SYSTEM

    Jude Sibolinao · 83問 · 1年前

    HYDRAULIC AND PNUEMATIC POWER SYSTEM

    HYDRAULIC AND PNUEMATIC POWER SYSTEM

    83問 • 1年前
    Jude Sibolinao

    Airline Terminologies

    Airline Terminologies

    Saint Thomas Aquinas! · 100問 · 1年前

    Airline Terminologies

    Airline Terminologies

    100問 • 1年前
    Saint Thomas Aquinas!

    JAI

    JAI

    ユーザ名非公開 · 20問 · 1年前

    JAI

    JAI

    20問 • 1年前
    ユーザ名非公開

    問題一覧

  • 1

    When the pilot select propeller to Beta range the propeller will

    operates between maximum reverse pitch and flight idle pitch.

  • 2

    In Beta range, propeller pitch is directly controlled by

    power lever.

  • 3

    in order to un feather the propeller

    a separate source of oil under pressure that supplied to the propeller hub

  • 4

    If the pilot set the propeller to beta range when the power lever is advanced engine throttle (increase fuel flow)

    propeller blade angle will increase.

  • 5

    Constant Speed propeller speed

    remains constant whilst running stationary and facing into head wind.

  • 6

    If force applied to the top of speeder spring (increasing RPM),

    blade angle moves to fine pitch.

  • 7

    Constant Speed Propeller for take-off is

    set to low pitch (fine) and high RPM position

  • 8

    A propeller control Unit is supplied with oil from the

    Engine oil system

  • 9

    Propeller is fitted with a counterweight at the blade root which is used to make it move toward fine-pitch

    the oil pressure

  • 10

    If the propeller governor flyweights overcome the speeder spring the propeller

    is over speeding

  • 11

    A constant speed Propeller provides maximum efficiency

    by Adjusting blade angle for most condition encountered during flight.

  • 12

    The constant speed control unit is also called

    a governor

  • 13

    Propeller over speed governor is a backup for propeller governor and is mounted on reduction gear box

    it has its own flyweight and pilot valve

  • 14

    When the compressive force on a speeder spring is reduced the propeller blade will

    coarsen

  • 15

    On an over speed condition, the blades are Turned

    to coarse pitch

  • 16

    If a force is a applied to the speeder spring what will happen

    blade angle finer

  • 17

    Many types of constant speed propeller

    use governor

  • 18

    Constant speed propeller system

    permits the pilot to select propeller and engine speed

  • 19

    Governor oil pump and the flyweight assembly are driven by

    geared to the engine

  • 20

    The rotational speed of the flyweight assembly varies

    directly with engine speed and control the position of the pilot valve