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Quiz

2. Performance

Jose Antonio Vazquez 22 Fragen

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Fragen in diesem Quiz (22)

  1. 187) The danger associated with low speed and/or high speed buffet
    1. Alimits the maneuvering load factor at high altitudes.
    2. Bcan be reduced by increasing the load factor.
    3. Cexists only above MMO.
    4. Dhas to be considered at take-off and landing.
  2. 276) Given a jet aircraft. Which order of increasing speeds in the performance diagram is correct?
    1. AVs, Maximum range speed, Vx
    2. BMaximum endurance speed, Maximum range speed, Vx
    3. CVs, Vx, Maximum range speed
    4. DMaximum endurance speed, Long range speed, Maximum range speed
  3. 377) If the climb speed schedule is changed from 280/.74 to 290/.74 the new crossover altitude is
    1. Aunchanged.
    2. Bonly affected by the aeroplane gross mass.
    3. Clower.
    4. Dhigher.
  4. 478) Reduced take-off thrust should normally not be used when:
    1. Ait is dark.
    2. Bthe runway is wet.
    3. Cobstacles are present close to the end of the runway.
    4. Dthe runway is contaminated.
  5. 579) Which data can be extracted from the Buffet Onset Boundary Chart?
    1. AThe value of the Mach number at which low speed and shockstall occur at various weights and altitudes.
    2. BThe values of the Mach number at which low speed and Mach buffet occur at various masses and altitudes.
    3. CThe value of maximum operating Mach number (MMO) at various masses and power settings.
    4. DThe value of the critical Mach number at various masses and altitudes.
  6. 680) With zero wind, the angle of attack for maximum range for an aeroplane with turbojet engines is:
    1. Aequal to that of maximum lift to drag ratio.
    2. Bequal to that maximum endurance.
    3. Cequal to that corresponding to zero induced drag.
    4. Dlower than that of maximum lift to drag ratio.
  7. 781) The speed V2 is defined for jet aeroplane as
    1. Atake-off climb speed or speed at 35 ft.
    2. Blift off speed.
    3. Ctake-off decision speed.
    4. Dcritical engine failure speed.
  8. 882) An increase in atmospheric pressure has, among other things, the following consequences on take-off performance:
    1. Aa reduced take-off distance and degraded initial climb performance
    2. Ba reduced take-off distance and improved initial climb performance
    3. Can increases take-off distance and degraded initial climb performance
    4. Dan increased take-off distance and improved initial climb performance
  9. 983) The induced drag of an aeroplane at constant gross weight and altitude is highest at
    1. AVSO (stalling speed in landing configuration)
    2. BVS1 (stalling speed in clean configuration)
    3. CVMO (maximum operating limit speed)
    4. DVA (design manoeuvring speed)
  10. 1084) On a twin engined piston aircraft with variable pitch propellers, for a given mass and altitude, the minimum drag speed is 125 kt and the holding speed (minimum fuel burn per hour) is 95 kt.

    The best rate of climb speed will be obtained for a speed:
    1. Ainferior to 95 kts
    2. Bis between 95 and 125 kt
    3. Cequal to 125 kt
    4. Dequal to 95 kt

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Tema 1 Performances Quiz am 2. Performance, erstellt von Jose Antonio Vazquez am 01/11/2018.
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