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M11c13
23問 • 4ヶ月前
  • ユーザ名非公開
  • 通報

    問題一覧

  • 1

    An air-ground sensing is required by many systems on a large aircraft and is performed by

    a simple microswitch or proximity sensor located usually on one or both main landing gear.

  • 2

    Brake Compensating Rods

    prevent the rear wheels on a main wheel bogie system, lifting during braking.

  • 3

    The colour of a thermal relief fuse plug indicates the

    temperature at which it will operate.

  • 4

    A tyre has a designation code of 17.5 x 5.75 – 8. The tyre width is

    5.75 inches.

  • 5

    A tyre specification 32 x 10.75-14. The 10.75 refers to

    section width.

  • 6

    A red line painted on a tyre and wheel is intended to indicate

    tyre creep

  • 7

    The drag strut in the main landing gear is fitted to absorb

    braking and take-off acceleration loads.

  • 8

    Wheel Track is the

    distance between the far left and far right wheels.

  • 9

    The centring cams on a nose landing gear are to

    enable the landing gear to be retracted into the wheel well safely.

  • 10

    On a radial tyre, the carcass plies are laid

    at 90 degrees to the centreline or direction of rotation of the tyre.

  • 11

    A brake belt is sometimes used on

    the nose landing gear only.

  • 12

    Twin-contact tread tyres are sometimes fitted to the nose wheel to assist in

    preventing nose wheel shimmy

  • 13

    Tyers should always be stored indoors in a

    dark room

  • 14

    If higher than normal braking energized are experienced during above than normal landing speed rejected take off, the tire must

    be removed and return to an approved repair station for inspection.

  • 15

    The function of the oil in a shock absorber is to

    damp the rebound.

  • 16

    Vents holes are found on

    tubed and tubeless tyres.

  • 17

    On large aircraft, braked wheel assemblies are normally inflated with

    Nitrogen and not more than 5% of air.

  • 18

    Spongy brakes are usually a result of

    air in the system

  • 19

    Aquaplaning can be reduced by

    an anti-skid device.

  • 20

    The purpose of the flutter plate in a shock absorber is to

    permit free flow of oil during compression and restriction of oil during extension.

  • 21

    Squat switch also known as

    weight on wheels switch

  • 22

    is fitted to maintain correct nose-wheel alignment.

    A torque link

  • 23

    A yellow fuse plug melts at temperature of

    199 C

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    問題一覧

  • 1

    An air-ground sensing is required by many systems on a large aircraft and is performed by

    a simple microswitch or proximity sensor located usually on one or both main landing gear.

  • 2

    Brake Compensating Rods

    prevent the rear wheels on a main wheel bogie system, lifting during braking.

  • 3

    The colour of a thermal relief fuse plug indicates the

    temperature at which it will operate.

  • 4

    A tyre has a designation code of 17.5 x 5.75 – 8. The tyre width is

    5.75 inches.

  • 5

    A tyre specification 32 x 10.75-14. The 10.75 refers to

    section width.

  • 6

    A red line painted on a tyre and wheel is intended to indicate

    tyre creep

  • 7

    The drag strut in the main landing gear is fitted to absorb

    braking and take-off acceleration loads.

  • 8

    Wheel Track is the

    distance between the far left and far right wheels.

  • 9

    The centring cams on a nose landing gear are to

    enable the landing gear to be retracted into the wheel well safely.

  • 10

    On a radial tyre, the carcass plies are laid

    at 90 degrees to the centreline or direction of rotation of the tyre.

  • 11

    A brake belt is sometimes used on

    the nose landing gear only.

  • 12

    Twin-contact tread tyres are sometimes fitted to the nose wheel to assist in

    preventing nose wheel shimmy

  • 13

    Tyers should always be stored indoors in a

    dark room

  • 14

    If higher than normal braking energized are experienced during above than normal landing speed rejected take off, the tire must

    be removed and return to an approved repair station for inspection.

  • 15

    The function of the oil in a shock absorber is to

    damp the rebound.

  • 16

    Vents holes are found on

    tubed and tubeless tyres.

  • 17

    On large aircraft, braked wheel assemblies are normally inflated with

    Nitrogen and not more than 5% of air.

  • 18

    Spongy brakes are usually a result of

    air in the system

  • 19

    Aquaplaning can be reduced by

    an anti-skid device.

  • 20

    The purpose of the flutter plate in a shock absorber is to

    permit free flow of oil during compression and restriction of oil during extension.

  • 21

    Squat switch also known as

    weight on wheels switch

  • 22

    is fitted to maintain correct nose-wheel alignment.

    A torque link

  • 23

    A yellow fuse plug melts at temperature of

    199 C