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ATPL(A) 062 Radio Navigation > 062.05 AERA NAVIGATION SYSTEMS AND RNAV OR FMS > Flashcards

062.05 AERA NAVIGATION SYSTEMS AND RNAV OR FMS Flashcards

1
Q

On an EFIS display, the recommended colour code for selected data and values is (white/green/amber/red/magenta).

A

On an EFIS display, the recommended colour code for selected data and values is (green)​.

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2
Q

On an EFIS display, the recommended colour code for cautions and abnormal sources is (white/green/amber/red/magenta).

A

On an EFIS display, the recommended colour code for cautions and abnormal sources is (amber)​.

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3
Q

One of the main functions of the FMS is to construct a (three/four)​-dimensional aircraft trajectory.

A

One of the main functions of the FMS is to construct a (four)-dimensional aircraft trajectory.

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4
Q

A simple VOR/DME - RNAV system uses waypoint (phantom station), valid VOR/DME signal and desired (course/heading)​ as input data.

A

A simple VOR/DME - RNAV system uses waypoint (phantom station), valid VOR/DME signal and desired (course) as input data.

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5
Q

Cross track distance (XTK-distance) in an Area Navigation System is the distance between (actual/air)​ position and the great circle track between active waypoints.

A

Cross track distance (XTK-distance) in an Area Navigation System is the distance between (actual) position and the great circle track between active waypoints.

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6
Q

Full-scale deviation on RNAV mode 2-dot HSI/CDI indications in approach mode is (…)​ NM.

A

Full-scale deviation on RNAV mode 2-dot HSI/CDI indications in approach mode is (1) NM.

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7
Q

A fix obtained by “rho-rho” navigation is based on information from two (VORs/NDBs/DMEs)​.

A

A fix obtained by “rho-rho” navigation is based on information from two (DMEs).

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8
Q

On an EFIS display, the recommended colour code for an aircraft symbol is (white/green/amber/red/magenta).

A

On an EFIS display, the recommended colour code for an aircraft symbol is (white)​.

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9
Q

Basic RNAV (B-RNAV) requires a track-keeping accuracy of +/- (…) NM for 95% of the flight time.

A

Basic RNAV (B-RNAV) requires a track-keeping accuracy of +/- (5.0) NM for 95% of the flight time.

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10
Q

On an EFIS display, the recommended colour code for active route is (white/green/amber/red/magenta).

A

On an EFIS display, the recommended colour code for active route is (magenta)​.

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11
Q

A phantom station gives (slant/cross track/ground) ​range.

A

A phantom station gives (ground) range.

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12
Q

On an EFIS display, the recommended colour code for armed AFCS mode is (white/green/amber/red/magenta).

A

On an EFIS display, the recommended colour code for armed AFCS mode is (white)​.

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13
Q

Precision RNAV (P-RNAV) requires a track-keeping accuracy of +/- (…) NM for 95% of the flight time.

A

Precision RNAV (P-RNAV) requires a track-keeping accuracy of +/- (1.0) NM for 95% of the flight time.

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14
Q

Full-scale deviation on RNAV mode 5-dot HSI/CDI indications in approach mode is (…)​ NM.

A

Full-scale deviation on RNAV mode 5-dot HSI/CDI indications in approach mode is (1.25) NM.

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15
Q

On an EFIS display, the recommended colour code for engaged modes is (white/green/amber/red/magenta).

A

On an EFIS display, the recommended colour code for engaged modes is (green)​.

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16
Q

Created waypoint can be entered into the scratch pad of the B737-400 FMS in the formats:

  • Place Bearing/Distance
  • Place (Bearing/Bearing / Distance/Distance)
  • (Across/Along)-Track Displacement
  • Latitude and Longitude
A

Created waypoint can be entered into the scratch pad of the B737-400 FMS in the formats:

  • Place Bearing/Distance
  • Place (Bearing/Bearing)
  • (Along)-Track Displacement
  • Latitude and Longitude
17
Q

Aircraft equipped to operate to RNP 1 and better should be able to (correct by the exact value/compute an estimate)​ of its position error.

A

Aircraft equipped to operate to RNP 1 and better should be able to (compute an estimate) of its position error.

18
Q

On an EFIS display, the recommended colour code for turbulence is (white/green/amber/red/magenta).

A

On an EFIS display, the recommended colour code for turbulence is (magenta)​.

19
Q

The navigational function of the horizontal situation indicator (HSI) in relation to area navigation systems is the indication of the (track angle error/wind component/cross track distance)​.

A

The navigational function of the horizontal situation indicator (HSI) in relation to area navigation systems is the indication of the (cross track distance).

20
Q

The purpose of the FMS is to provide (manual/continuous automatic)navigation guidance as well as(manual/continuous automatic) performance management.

A

The purpose of the FMS is to provide (continuous automatic)navigation guidance as well as(continuous automatic) performance management.

21
Q

Full-scale deviation on RNAV mode 2-dot HSI/CDI indications in en-route mode is (…)​ NM.

A

Full-scale deviation on RNAV mode 2-dot HSI/CDI indications in en-route mode is (4) NM.

22
Q

On an EFIS display, the recommended colour code for warnings, flight envelope and system limits is (white/green/amber/red/magenta).

A

On an EFIS display, the recommended colour code for warnings, flight envelope and system limits is (red)​.

23
Q

Area Navigation (RNAV) is a method of navigation which permits aircraft operation on any desired flight path (outside of/within) the coverage of station-referenced navigation aids or within the limits of the capability of self-contained aids, or a combination of these.

A

Area Navigation (RNAV) is a method of navigation which permits aircraft operation on any desired flight path (within) the coverage of station-referenced navigation aids or within the limits of the capability of self-contained aids, or a combination of these.

24
Q

Full-scale deviation on RNAV mode 5-dot HSI/CDI indications in en-route mode is (…)​ NM.

A

Full-scale deviation on RNAV mode 5-dot HSI/CDI indications in en-route mode is (5) NM.

25
Q

On an EFIS display, the recommended colour code for current data and values is (white/green/amber/red/magenta).

A

On an EFIS display, the recommended colour code for current data and values is (white)​.

26
Q

State which of the following frequency bands is used by the Loran C navigation system:

  • 1750 - 1950 kHz
  • 10.2 - 13.6 kHz
  • 90 - 110 kHz
  • 978 - 1213 MHz
A

State which of the following frequency bands is used by the Loran C navigation system:

  • 1750 - 1950 kHz
  • 10.2 - 13.6 kHz
  • 90 - 110 kHz
  • 978 - 1213 MHz

ATPL(A) 062 Radio Navigation (6 decks)

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