ATP 03 Gerard 2020

40 Questions | Attempts: 48
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ATP 03 Gerard 2020 - Quiz

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Questions and Answers
  • 1. 
    Why is VMCG determine with the nose wheel steering disconnected
    • A. 

      Because nose wheel staring has no affected on the value of VMCG

    • B. 

      Because the value of VMCG must also be applicable on wet and / or slippery rwys

    • C. 

      Because the nose wheel steering could become inoperative after ab engine has failed

    • D. 

      Because it must be possible to abort the take of even after the nose wheel has already been lifted off the ground

  • 2. 
    When spoilers are used as speed break
    • A. 

      CL max of the polar curve is not affected 

    • B. 

      They do not affected wheel braking action during landing 

    • C. 

      At same angle of attack CL remains unaffected

    • D. 

      At same angle of attack ,CD is increased and CL is decreased

  • 3. 
    How does VMCG change with increasing field elevation and temperature
    • A. 

      Increases , because al a lower density a larger IAS is necessary to generate the required rudder force

    • B. 

      Increases, because VMCG is related to V1 and VR and those speeds increase if the density decreases

    • C. 

      Decreases, because the engine thrust decreases 

    • D. 

      Decreases , because VMCG is expressed in IAS and the IAS decreases with TAS constant and decreasing density,

  • 4. 
    The flight Mach number is 0.8 and the TAS is 400 Kts. the speed of sound is
    • A. 

      500 Kts

    • B. 

      320 Kts

    • C. 

      480 Kts

    • D. 

      600 Kts 

  • 5. 
    The bank angle in a rate-one turn depends on 
    • A. 

      TAS

    • B. 

      Weight

    • C. 

      Load factor

    • D. 

      Wind

  • 6. 
    The stall speed increases , when (all other factors of importance being constant
    • A. 

      Spoilers are selected from OUT to IN

    • B. 

      Pulling up from a dive 

    • C. 

      Weight decreases

    • D. 

      Minor altitude changes occur e.g 0--10.000 ft

  • 7. 
    After T.O the slats (when installed ) are always retracted later than Flaps  , why 
    • A. 

      Because FLAPS EXTENDED gives a large decrease in stall speed with relatively less drag

    • B. 

      Because SLATS EXTENDED give a large decrease in stall speed with relatively less drag

    • C. 

      Because SLATS EXTENDED provides a better view from the cockpit than FLAPS EXTENDED

    • D. 

      Because VMCA with SLATS EXTENDED is more favorable compared to the FLAPS EXTENDED situation

  • 8. 
    A higher altitudes , the stall speed (IAS)
    • A. 

      Increases

    • B. 

      Decreases

    • C. 

      Remain the same 

    • D. 

      Decreases until tropopause

  • 9. 
    The stall speed 
    • A. 

      Does not depend on weight

    • B. 

      Increases with the length of the wingspan

    • C. 

      Increases with an increased weight

    • D. 

      Decreases with an increased weight

  • 10. 
    The following factors increase stall speed
    • A. 

      A lower weight deceasing bank angle , a smaller flap setting

    • B. 

      An increase in load factor , a forward c.g shift , decrease in thrust

    • C. 

      A higher weight selecting a higher flap setting , a forward cog shift.

    • D. 

      Increasing bank angle , increasing thrust , slat extension

  • 11. 
    A jet aeroplane is rolled into a turn , while maintaining airspeed and holding altitude .In such a case , the Pilot has to
    • A. 

      Increase angle of attack and keep thrust unchanged

    • B. 

      Increase thrust and angle of attack

    • C. 

      Increase thrust and keep angle of attack unchanged 

    • D. 

      Increase thrust and decrease angle of attack

  • 12. 
    The center of gravity moving after will
    • A. 

      Increase the elevator up effectiveness

    • B. 

      Decrease the elevator up effectiveness

    • C. 

      Not affected the elevator up or down effectiveness

    • D. 

      Increase or decrease the elevator up effectiveness , depending on wing location.

  • 13. 
    Mcritic is the free stream Mach Number at wich 
    • A. 

      Shock stall occurs.

    • B. 

      The critical angle of attack is reached 

    • C. 

      Somewhere about the airframe Mach 1 is reached locally

    • D. 

      Mach buffet occurs

  • 14. 
    When comparing a rectangular wing and swept back wing of the same wing area and loading , the swept back wing has the advantage of 
    • A. 

      Winglets

    • B. 

      Swept wings

    • C. 

      Straight wings

    • D. 

      Wing dihedral

  • 15. 
    One disadvantage of the swept back wing is its stalling characteristics . At the stall 
    • A. 

      Increased longitudinal stability

    • B. 

      Lower stalling speed

    • C. 

      Higher critical mach

    • D. 

      Greater strength 

  • 16. 
    What wing shape or wing characteristics is the least sensitive to turbulence 
    • A. 

      Winglets

    • B. 

      Swept wings

    • C. 

      Straight wings

    • D. 

      Wing diedral

  • 17. 
    One disadvantage of the swept back wing is its stalling characteristics At the stall
    • A. 

      Wing root stall will occur first , wich produces a rolling moment

    • B. 

      Tip stall will occur first wich produces a nose down moment 

    • C. 

      Leading edge stall will occur first , wich produces a nose down moment 

    • D. 

      Tip stall will occur first wich produces a pitch --up moment

  • 18. 
    Floating due to ground effect during an approach to land will occur
    • A. 

      When a higher than normal angle of attack is used 

    • B. 

      At a speed approaching the stall 

    • C. 

      When the height is less than halve of the length of the wing span above the surface

    • D. 

      When the height is less than twice the length of the wing span above the surface 

  • 19. 
    What will happen in group effect 
    • A. 

      A significant increase in thrust required

    • B. 

      The induced angle of attack and induced drag decreased 

    • C. 

      The wing downwash on the tail surface increases

    • D. 

      An increase in strength in the win tip vortices

  • 20. 
    If an airplane flies in the ground effect
    • A. 

      The lift is increased and the drag is decreased

    • B. 

      The effective angle of attack is decreased

    • C. 

      The induced angle of attack is increased 

    • D. 

      Drag and lift are reduced

  • 21. 
    Ground effect has the following influence on the landing distance
    • A. 

      Decreases 

    • B. 

      Does not change 

    • C. 

      Increases only if the landing flaps are fully extended

    • D. 

      Increases

  • 22. 
    The centre of gravity moving aft will
    • A. 

      Increase the elevator up effectiveness  

    • B. 

      Decrease the elevator up effectiveness

    • C. 

      Not affect the elevator up or down effectiveness

    • D. 

      Increase or decrease the elevator up effectiveness depend on wing location  

  • 23. 
    Which moments or motions interact in a dutch roll
    • A. 

      Pitching and adverse yaw

    • B. 

      Rolling and Yawing

    • C. 

      Pitching and yawing

    • D. 

      Pitching and rolling

  • 24. 
    Rotation about the lateral axis is called
    • A. 

      Yawing

    • B. 

      Slipping

    • C. 

      Pitching 

    • D. 

      Rolling

  • 25. 
    The maximum validity of a SNOWTAM is 
    • A. 

      3 hours

    • B. 

      24 hours

    • C. 

      12 hours

    • D. 

      6 hours

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