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Performance - ATPL - Airline Transport Pilot license

Test 10 domande Performance, tempo libero

1 - What will be the influence on the aeroplane performance if aerodrome pressure altitude is increased? It will increase the take-off distance available It will decrease the take-off distance It will decrease the take-off run It will increase the take-off distance

2 - Which of the following statements is correct? The performance limited take-off mass is independent of the wind component The accelerate stop distance required is independent of the runway condition The climb limited take-off mass is independent of the wind component The take-off distance with one engine out is independent of the wind component

3 - How does the best angle of climb and best rate of climb vary with increasing altitude for an aeroplane with a normal aspirated piston engine? Both increase Best angle of climb increases while best rate of climb decreases Both decrease Best angle of climb decreases while best rate of climb increases

4 - The length of a clearway may be included in: The take-off distance available The distance to reach V1 The take-off run available The accelerate-stop distance available

5 - The take-off mass of an aeroplane is restricted by the climb limit. What would be the effect on this limit of an increase in the headwind component? The climb limited take-off mass would increase The effect would vary depending upon the height of any obstacle within the net take-off flight path The climb limited take-off mass would decrease None

6 - The following parameters affect the take off ground run: 1 decreasing take off mass2 increasing take off mass 3 increasing density4 decreasing density5 increasing flap setting 6 decreasing flap setting7 increasing pressure altitude 8 decreasing pressure altitudeWhich parameters will decrease the take off ground run? 2, 4, 5 and 7 1, 4, 6 and 8 2, 3, 6 and 7 1, 3, 5 and 8

7 - Which statement is correct for a descent without engine thrust at maximum lift to drag ratio speed? The higher the gross mass the lower is the speed for descent. The higher the average temperature (OAT) the lower is the speed for descent. The higher the gross mass the greater is the speed for descent. The mass of an aeroplane does not have any effect on the speed for descent.

8 - On a dry runway the accelerate stop distance is increased: By headwind By uphill slope By a lower take-off mass because the aeroplane accelerates faster to V1 By low outside air temperature

9 - Which of the following factors leads to the maximum flight time of a glide? High mass Low mass Tailwind Headwind

10 - What is the equation for the climb gradient expressed in percentage during unaccelerated flight (applicable to small angles only)? Climb Gradient = ((Thrust - Drag) / Weight) x 100 Climb Gradient = (Lift / Weight) x 100 Climb Gradient = ((Thrust - Mass) / Lift) x 100 Climb Gradient = ((Thrust + Drag) / Lift) x 100

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