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M17c6
19問 • 15日前
  • ユーザ名非公開
  • 通報

    問題一覧

  • 1

    If a 2 blade prop is placed a knife edge and ends up horizontal blade

    at 3 and 9 o’clock it horizontally balance.

  • 2

    We can adjusted the blade track on the wooden or fixed pitch metal propeller by

    fitting shims to the propeller shaft hub.

  • 3

    Cropping of propeller blade tips is permitted up to max of

    1 inch (25mm) on all blades.

  • 4

    If slight tip or trailing edge in a wooden propeller damaged

    it repaired by sanding to new profile, both blades must be similarly shaped.

  • 5

    All composite propellers repair (minor & major) should be accomplished

    in approved composite propeller repair facility only.

  • 6

    The suitable inspection method for crack in the aluminum alloy propeller is

    dye penetrant inspection.

  • 7

    If Propeller over-speeding between

    100%-110% NO maintenance action required.

  • 8

    If Propeller over-speeding between 115%-130% required maintenance action

    remove propeller for inspection.

  • 9

    Aerodynamic correction factor ACF

    corrects the unequal thrust.

  • 10

    After a lightning strike to metal propeller the propeller heat element

    should be checked for continuity and insulation.

  • 11

    Bent, twist, crack, or severe surface damage the propeller must

    be return to manufacturer or approved repair facility.

  • 12

    The instruments that monitor the performance of a turbo prop engine are

    Tachometer, Torque meter, Fuel flow meter and EGT indicator.

  • 13

    Inspection of taper contact between crank shaft and propeller hub is determined by

    bearing blue colour transfer.

  • 14

    Propeller blade angle at full feather

    is 86 ±5

  • 15

    A body capable of rotating about a fixed point is said to be in a static balance when

    its center of gravity lies on axis of rotation

  • 16

    After installation a propeller the engine must be ground run to check propeller operation so the

    aircraft should be facing into wind

  • 17

    When the propeller blade angle and fuel flow for any given power setting are governed automatically during flight

    this is know as alpha range

  • 18

    Propeller static balance check should be

    in horizontal and vertical planes

  • 19

    The propeller track should be checked

    every annual inspection And 100hrs inspection and time vibration isa problem .

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    問題一覧

  • 1

    If a 2 blade prop is placed a knife edge and ends up horizontal blade

    at 3 and 9 o’clock it horizontally balance.

  • 2

    We can adjusted the blade track on the wooden or fixed pitch metal propeller by

    fitting shims to the propeller shaft hub.

  • 3

    Cropping of propeller blade tips is permitted up to max of

    1 inch (25mm) on all blades.

  • 4

    If slight tip or trailing edge in a wooden propeller damaged

    it repaired by sanding to new profile, both blades must be similarly shaped.

  • 5

    All composite propellers repair (minor & major) should be accomplished

    in approved composite propeller repair facility only.

  • 6

    The suitable inspection method for crack in the aluminum alloy propeller is

    dye penetrant inspection.

  • 7

    If Propeller over-speeding between

    100%-110% NO maintenance action required.

  • 8

    If Propeller over-speeding between 115%-130% required maintenance action

    remove propeller for inspection.

  • 9

    Aerodynamic correction factor ACF

    corrects the unequal thrust.

  • 10

    After a lightning strike to metal propeller the propeller heat element

    should be checked for continuity and insulation.

  • 11

    Bent, twist, crack, or severe surface damage the propeller must

    be return to manufacturer or approved repair facility.

  • 12

    The instruments that monitor the performance of a turbo prop engine are

    Tachometer, Torque meter, Fuel flow meter and EGT indicator.

  • 13

    Inspection of taper contact between crank shaft and propeller hub is determined by

    bearing blue colour transfer.

  • 14

    Propeller blade angle at full feather

    is 86 ±5

  • 15

    A body capable of rotating about a fixed point is said to be in a static balance when

    its center of gravity lies on axis of rotation

  • 16

    After installation a propeller the engine must be ground run to check propeller operation so the

    aircraft should be facing into wind

  • 17

    When the propeller blade angle and fuel flow for any given power setting are governed automatically during flight

    this is know as alpha range

  • 18

    Propeller static balance check should be

    in horizontal and vertical planes

  • 19

    The propeller track should be checked

    every annual inspection And 100hrs inspection and time vibration isa problem .