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AGK PREP EXAM 9

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AGK PREP EXAM 9

Frage 1 von 50

1

401 From what is true altitude derived?

Wähle eine der folgenden:

  • O Pressure altitude.

  • O Density altitude.

  • O Critical altitude.

  • O Mach number compensated for true temperature.

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Frage 2 von 50

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402 What is QNH?

Wähle eine der folgenden:

  • O Sea level pressure.

  • O Measured ambient pressure at the airfield elevation.

  • O Q-code for hellicopters.

  • O Sea level pressure in ISA conditions .

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Frage 3 von 50

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403 What is QNH?

Wähle eine der folgenden:

  • O The pressure to be set on the altimeter subscale, to obtain an indication of ambient sea level pressure.

  • O The pressure to be set on the altimeter subscale to obtain an indication of zero on the runway.

  • O The pressure to be set on the altimeter subscale to obtain a reading of the pressure altitude of the runway.

  • O The pressure to be set on the altimeter subscale to obtain density altitude when on the runway.

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Frage 4 von 50

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404 The pressure altitude of the field can be found by?

Wähle eine der folgenden:

  • O Setting QNH on the altimeter subscale.

  • O Setting QFE on the altimeter subscale.

  • O Setting 1013 hPa on the altimeter subscale.

  • O Setting QUJ on the altimeter subscale.

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Frage 5 von 50

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405 A barometric altimeter is consisted of?

Wähle eine der folgenden:

  • O An aneroid capsule sensing static pressure.

  • O An aneroid capsule sensing pitot and dynamic pressure.

  • O A differential capsule sensing pitot static pressure compensated for temperature.

  • O A bellows type sensing temperature and static pressure.

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Frage 6 von 50

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406 (Fig.13) If QNH is 998 hPa, what is the pressure altitude at an elevation of 18000 ft?

Wähle eine der folgenden:

  • O 18450 ft.

  • O 20000 ft.

  • O 17550 ft.

  • O 18000 ft.

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Frage 7 von 50

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407 (Fig.13) If pressure altitude is 13600 ft, at an elevation of 12000 ft, what is QNH?

Wähle eine der folgenden:

  • O 960 hPa.

  • O 976 hPa.

  • O 1000 hPa.

  • O 1024 hPa.

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Frage 8 von 50

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408 (Fig.13) If field elevation is 4700 ft amsl and QNH is 903 hPa, what is the pressure altitude?

Wähle eine der folgenden:

  • O 8000 ft.

  • O 5600 ft.

  • O 4700 ft.

  • O 3800 ft.

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Frage 9 von 50

1

409 If QNH changes from 1015 hPa to 1030 hPa will?

Wähle eine der folgenden:

  • O Increase QNH.

  • O Increase field elevation.

  • O Not affect QNH.

  • O Decrease QNH.

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Frage 10 von 50

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410 As pressure altitude increases?

Wähle eine der folgenden:

  • O Temperature decreases then remains constant.

  • O Temperature is unaffected.

  • O Temperature increases rapidly.

  • O Temperature increases then remains constant.

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Frage 11 von 50

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411 Pressure altitude is?

Wähle eine der folgenden:

  • O The altimeter indication when 1013.25 hPa is set on the sub-scale.

  • O The lowest pressure observed in the centre of a dipression.

  • O The altimeter indication when QFE is set on the sub-scale.

  • O The altimeter indication when QNH is set on the subscale.

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Frage 12 von 50

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412 If QNH changes from 1009 hPa to 1018 hPa this will?

Wähle eine der folgenden:

  • O Not affect field elevation.

  • O Increase field elevation.

  • O Decrease field elevation.

  • O Decrease QFE.

  • O Pressure altitude corrected for temperature.

  • O True altitude corrected for density.

  • O Cabin altitude corrected for density.

  • O Temperature altitude corrected for pressure.

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Frage 13 von 50

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414 (Fig.7) How will altimeter reading be affected if the static vent pipe becomes blocked?

Wähle eine der folgenden:

  • O Readings will freeze.

  • O Reads absolute zero.

  • O Read higher than true.

  • O Read lower than true.

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Frage 14 von 50

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415 (Fig.7) If icing, debris or insects would cause pressure disturbances at the static source,
the effect will be?

Wähle eine der folgenden:

  • O Increased position error.

  • O Instrument damage.

  • O Increased instrument error.

  • O Decreased altitude indication.

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Frage 15 von 50

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416 (Fig7.) If an aircraft flying at constant height over a level surface, meets a hotter-than ISA- air mass, the altimeter will?

Wähle eine der folgenden:

  • O Indicate lower than true.

  • O Indicate higher than true.

  • O Indicate false readings.

  • O Indicate the same.

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Frage 16 von 50

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417 (Fig.7) In a barometric altimeter…………. is fed into the capsule and .............. is fed into the
case?

Wähle eine der folgenden:

  • O Vacuum static pressure.

  • O Static pressure dynamic pressure.

  • O Dynamic pressure vacuum.

  • O Ram air static pressure.

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Frage 17 von 50

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418 (Fig.7) If the static pressure source in an un-pressurised aircraft became blocked the
altimeter would...........but might be rectified by..........?

Wähle eine der folgenden:

  • O Freeze break the altimeter glass.

  • O Read zero break the altimeter glass.

  • O Read zero open the windows.

  • O Freeze descending to lower altitudes.

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Frage 18 von 50

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419 (Fig.7) Barometric altimeter readings can become erratic during landing because?

Wähle eine der folgenden:

  • O Static pressure is changed by ground effect.

  • O Static ports can become blocked by debris,

  • O Due to increased angle of attack.

  • O Static ports become shielded by other parts of the aircraft at high angles of attack.

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Frage 19 von 50

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420 (Fig.7) What type of pressure sensor is employed in a barometric altimeter?

Wähle eine der folgenden:

  • O Aneroid capsule.

  • O Mercury type.

  • O Synthetic or metallic bellows.

  • O Bourdon helical tube.

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Frage 20 von 50

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421 (Fig.7) If the pressure feed line to a barometric altimeter becomes detached from the back of the instrument in flight the instrument will?

Wähle eine der folgenden:

  • O Read cabin altitude.

  • O Freeze

  • O Over read.

  • O Under read.

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Frage 21 von 50

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422 (Fig.8) If the pitot pipe becomes partly blocked?

Wähle eine der folgenden:

  • O The VSI will not be actually affected.

  • O The VSI indication will be too low when climbing.

  • O The VSI will be too low when descending.

  • O The VSI will have low respond time when descending and too high when climbing.

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Frage 22 von 50

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423 (Fig.8) If the static pipe becomes partly blocked?

Wähle eine der folgenden:

  • O The VSI indication will be too low when climbing or descending.

  • O The VSI indication will be too high when entering a thermal.

  • O The VSI indication will be too high when coring a thermal.

  • O The VSI indication will be unaffected in turbulence.

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Frage 23 von 50

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424 (Fig.6) The correct action to be taken when the static vent blocks on an unpressurised
light aircraft is to?

Wähle eine der folgenden:

  • O Use the standby static source.

  • O Break the VSI glass.

  • O Use altimeter for vertical speed indications.

  • O Open a window to equalise pressures.

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Frage 24 von 50

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425 (Fig.8) A VSI?

Wähle eine der folgenden:

  • O Measures the difference between the pressure inside and outside a capsule.

  • O Measures the accelerations difference and converts to vertical speed indications.

  • O Measures the difference between total pressure and static pressure.

  • O Measures only dynamic pressure.

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Frage 25 von 50

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426 (Fig.8) A VSI indicates increasing rate of descent (ROD), by?

Wähle eine der folgenden:

  • O VSI needle moving downwards.

  • O VSI needle moving upwards, then downwards.

  • O VSI needle stationary and the warning light is blinking.

  • O The VSI indicates only vertical speeds, not accelerations.

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Frage 26 von 50

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427 (Fig.8) As an aircraft moves close to the ground during a landing the VSI might?

Wähle eine der folgenden:

  • O Become inaccurate due to ground effect.

  • O Become inaccurate due to turbulence.

  • O Stick due to loss of pitot pressure reference.

  • O Become inaccurate due to aircraft attitude decelerations.

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Frage 27 von 50

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428 (Fig.8) If the static pipe becomes partly blocked?

Wähle eine der folgenden:

  • O The VSI indication will be too low when descending.

  • O The VSI indication will be too high when descending.

  • O The VSI indication will be too high when accelerating at constant altitude.

  • O The VSI indication will have erratic indications during level flight.

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Frage 28 von 50

1

429 (Fig.8) If the pitot pipe becomes partly blocked?

Wähle eine der folgenden:

  • O The VSI will be unaffected.

  • O The VSI will over read when climbing or descending.

  • O The VSI will over under read at all times.

  • O The VSI will read zero since vacuum does not respond properly.

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Frage 29 von 50

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430 (Fig.4) If the pitot source and drain become blocked by ice when in cruise flight, how will the ASI respond when descending?

Wähle eine der folgenden:

  • O It will under read.

  • O It will over read due to accelerations.

  • O It will read zero in all flight conditions.

  • O It will freeze or remain fixed at the reading at which it became blocked.

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Frage 30 von 50

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431 (Fig.4) In an ASI system, what does the pitot probe sense?

Wähle eine der folgenden:

  • O Total pressure.

  • O Differential pressure.

  • O Static pressure.

  • O Ambient pressure.

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Frage 31 von 50

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432 (Fig.2) What are indicated by the lower and upper ends of the white arc on an ASI?

Wähle eine der folgenden:

  • O Vso and Vfe

  • O Vfe and Vfo.

  • O Vs and Vfe.

  • O Vno and Vne.

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Frage 32 von 50

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433 What exactly speed, is VNO?

Wähle eine der folgenden:

  • O That which may only be exceeded with caution and only in still air.

  • O That which may never be exceeded.

  • O That which may be exceeded only in emergencies.

  • O The maximum at which fully control deflection is possible without overstressing the aircraft structure.

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Frage 33 von 50

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434 (Fig.5) What will be the effect if the drain hole and pitot tapping in a pitot probe are
blocked, whilst the static source remains open?

Wähle eine der folgenden:

  • O The ASI will respond to changes in cabin or just pressure altitude only.

  • O The ASI will not respond at all.

  • O The ASI will under read at all speeds normally since alternate static source exist.

  • O The ASI will over read when accelerating, decelerating, climbing or descending.

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Frage 34 von 50

1

435 (Fig.2) What do the upper and lower limits of the yellow arc on an ASI represent?

Wähle eine der folgenden:

  • O VNO and VNE.

  • O VFE and UFO.

  • O VM0 and VNE.

  • O VN0 and VMO.

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Frage 35 von 50

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436 VFE is the?

Wähle eine der folgenden:

  • O Maximum speed at which the aircraft is permitted to fly with its flaps
    extended.

  • O Maximum speed at which the flaps can be extended or retracted.

  • O The minimum speed for flaps up flight retracted.

  • O The maximum speed with 10° flaps extend.

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Frage 36 von 50

1

437 RAS is?

Wähle eine der folgenden:

  • O IAS corrected for position error and instrument error.

  • O GS corrected for position error and compressibility error.

  • O TAS corrected for instrument error and ram effect.

  • O IAS corrected for density error and position error.

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Frage 37 von 50

1

438 (Fig.4) If the pitot pipe becomes partly blocked?

Wähle eine der folgenden:

  • O The IAS reading will be too low when descending and too high when climbing.

  • O The IAS reading will be erratic when climbing.

  • O The IAS reading will be freezed.

  • O The IAS reading will be too low at all times.

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Frage 38 von 50

1

439 (Fig.4) If the pitot pipe becomes partly blocked?

Wähle eine der folgenden:

  • O The IAS will be too low when accelerating.

  • O The IAS will be unaffected.

  • O The IAS will be too low when decelerating.

  • O The IAS will be too low at all faces of flght.

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Frage 39 von 50

1

440 (Fig.11) If the static pipe becomes partly blocked?

Wähle eine der folgenden:

  • O The IAS and ROC will be too low when climbing.

  • O The IAS and ROC will be too low when descending.

  • O The IAS and ROC will be too low at all faces of flght.

  • O The IAS will be be unaffected.

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Frage 40 von 50

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441 The pitot source in an ASI system provides?

Wähle eine der folgenden:

  • O Total pressure.

  • O Dynamic pressure.

  • O Kinetic energy and inertia.

  • O Kinetic pressure.

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Frage 41 von 50

1

442 (Fig.2) The yellow arc on an ASI indicates?

Wähle eine der folgenden:

  • O VNo at lower end and VNe at upper end.

  • O Vne at lower end and Vmo at upper end.

  • O Vle at lower end and Vfe at upper end.

  • O Vmd at lower end and Vmp at upper end.

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Frage 42 von 50

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443 RAS is IAS corrected for?

Wähle eine der folgenden:

  • O Position error.

  • O Instrument error.

  • O Compressibility error.

  • O Density error.

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Frage 43 von 50

1

444 (Fig.2) What does the white arc on an ASI indicate?

Wähle eine der folgenden:

  • O Vso at the lower end and Vfe at the upper end.

  • O Vso at the lower end and Vmd at the upper end.

  • O Vsi at the lower end and Vfe at the upper end.

  • O Vsi at the lower end and Vmd at the upper end.

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Frage 44 von 50

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445 (Fig.2) Where on an ASI is VFE indicated?

Wähle eine der folgenden:

  • O The upper end of the white arc.

  • O The lower end of the yellow arc.

  • O The blue arc limit.

  • O The upper red dead line.

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Frage 45 von 50

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446 (Fig.2) Where on an ASI is VNO indicated?

Wähle eine der folgenden:

  • O Upper end of green mark and lower end of yellow arc.

  • O Lower end of green arc and upper end of white arc.

  • O Upper end of white arc and lower end of green arc.

  • O Upper end of red arc and lower end of yellow arc.

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Frage 46 von 50

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447 VNEis?

Wähle eine der folgenden:

  • O The speed that must never be exceeded.

  • O The maximum speed for normal operations.

  • O The maximum speed with flaps extended.

  • O The maximum speed flying in turbulence.

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Frage 47 von 50

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448 What is VFE?

Wähle eine der folgenden:

  • O The maximum speed for flight with the flaps extended.

  • O The maximum speed for extending or retracting flaps, applied only to B class aeroplanes as categorized by JAR's.

  • O The maximum permissible speed for the whole flight envelope.

  • O The minimum speed for extending or retracting the flaps.

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Frage 48 von 50

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449 (Fig.2) What does the green arc on an ASI indicate?

Wähle eine der folgenden:

  • O Vsi at the lower end and Vno at the upper end.

  • O Vx at the lower end and Vy at the upper end.

  • O Vfe at the lower end and Vfo at the upper end.

  • O Vsi at the lower end and Mmd at the upper end.

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Frage 49 von 50

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450 VN0 is the maximum…………………………………?

Wähle eine der folgenden:

  • O Maximum cruise speed in the entire flight envelope.

  • O Maximum operating speed at operating ceiling.

  • O Maximum emergency speed at absolute ceiling.

  • O Maximum permissible speed during spiral dive.

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Frage 50 von 50

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451 (Fig.2) Vne is.......................and is indicated by the.......................on an ASI?

Wähle eine der folgenden:

  • O never exceed speed / red radial line at the upper end of the yellow arc.

  • O never entry spin speed / upper end of white arc.

  • O maximum flat spin speed / lower end of green arc.

  • O normal endurance speed / green radial at the upper end of the green arc.

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