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ATPL Nav Revision 8
18問 • 11ヶ月前
  • Will Erwin
  • 通報

    問題一覧

  • 1

    The error associated with the NDB/ADF is

    quadrantal error

  • 2

    An NDB station radiates a signal which is

    Omni directional

  • 3

    An NDB signal is received by and ADF in an inbound aircraft equipped with a fixed card ADF. The navigation information is presented as ?

    a relative bearing to the station

  • 4

    In a vertical axis gyro at the South Pole -

    drift and topple due to the earth rate rotation will be zero

  • 5

    In a horizontal axis gyro at the South Pole -

    drift will be maximum and topple will be zero

  • 6

    On a lamberts conformal conic projection, a straight line is drawn from 35’S 139’E to the destination at 38’S 145’E The rhumb line track for the same trip would be ?

    left of the straight line track

  • 7

    On a lamberts conformal conic projection a straight line is drawn from 35”S 139”E to the destination at 28”S 139”E The rhumb line track for the same trip would be ?

    on the straight line track

  • 8

    On a polar stereographic chart, meridians appear as ?

    straight lines

  • 9

    When flying at an altitude of 4500ft on local QNH with a temp of ISA+10, your true altitude is approximately?

    4680

  • 10

    In an Inertial Navigation System , compensation for the earth rate rotation must be applied -

    according to a specific latitude

  • 11

    In an inertial navigation system , compensation for transport rate must be applied

    according to the aircraft’s speed over the ground

  • 12

    In an inertial navigation system, the platform on which the accelerometers mounted must be aligned with -

    true north

  • 13

    Coastal refraction is an error which results in -

    NDB signals bending toward the coast when approaching an inland station from overwater at an acute angle to the coast

  • 14

    As an aircraft approaches an enroute DME station, when overflying, the DME ground speed readout will -

    reduce at an increasing rate to zero overhead, the increase at a decreasing rate back to the correct value after station passage

  • 15

    If an aircraft pitot becomes blocked while in cruise at a constant flight level and then starts to climb, the airspeed indicator will ?

    over read

  • 16

    A Doppler VOR installation has the advantage of reducing errors associated with -

    obstructions in the vicinity of the site

  • 17

    The purpose of the annunciator in a gyrostabilised remote indicating compass is to indicate?

    that the magnetic detector unit and gyro are correctly aligned and synchronised

  • 18

    A horizontally polarised radio signal is best received by

    horizontal antenna

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    問題一覧

  • 1

    The error associated with the NDB/ADF is

    quadrantal error

  • 2

    An NDB station radiates a signal which is

    Omni directional

  • 3

    An NDB signal is received by and ADF in an inbound aircraft equipped with a fixed card ADF. The navigation information is presented as ?

    a relative bearing to the station

  • 4

    In a vertical axis gyro at the South Pole -

    drift and topple due to the earth rate rotation will be zero

  • 5

    In a horizontal axis gyro at the South Pole -

    drift will be maximum and topple will be zero

  • 6

    On a lamberts conformal conic projection, a straight line is drawn from 35’S 139’E to the destination at 38’S 145’E The rhumb line track for the same trip would be ?

    left of the straight line track

  • 7

    On a lamberts conformal conic projection a straight line is drawn from 35”S 139”E to the destination at 28”S 139”E The rhumb line track for the same trip would be ?

    on the straight line track

  • 8

    On a polar stereographic chart, meridians appear as ?

    straight lines

  • 9

    When flying at an altitude of 4500ft on local QNH with a temp of ISA+10, your true altitude is approximately?

    4680

  • 10

    In an Inertial Navigation System , compensation for the earth rate rotation must be applied -

    according to a specific latitude

  • 11

    In an inertial navigation system , compensation for transport rate must be applied

    according to the aircraft’s speed over the ground

  • 12

    In an inertial navigation system, the platform on which the accelerometers mounted must be aligned with -

    true north

  • 13

    Coastal refraction is an error which results in -

    NDB signals bending toward the coast when approaching an inland station from overwater at an acute angle to the coast

  • 14

    As an aircraft approaches an enroute DME station, when overflying, the DME ground speed readout will -

    reduce at an increasing rate to zero overhead, the increase at a decreasing rate back to the correct value after station passage

  • 15

    If an aircraft pitot becomes blocked while in cruise at a constant flight level and then starts to climb, the airspeed indicator will ?

    over read

  • 16

    A Doppler VOR installation has the advantage of reducing errors associated with -

    obstructions in the vicinity of the site

  • 17

    The purpose of the annunciator in a gyrostabilised remote indicating compass is to indicate?

    that the magnetic detector unit and gyro are correctly aligned and synchronised

  • 18

    A horizontally polarised radio signal is best received by

    horizontal antenna