Domande esame ATPL per Performance

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Test 10 domande Performance, tempo libero

1 - Which statement regarding V1 is correct? V1 must not exceed VMCG V1 must not exceed VR The V1 correction for up-slope is negative When determining the V1, reverse thrust is only allowed to be taken into account on the remaining symmetric engines

2 - Any acceleration in climb, with a constant power setting: Improves the rate of climb if the airspeed is below VY Improves the climb gradient if the airspeed is below VX Decreases rate of climb and increases angle of climb Decreases the rate of climb and the angle of climb

3 - The optimum altitude: Decreases as mass decreases Increases as mass decreases and is the altitude at which the specific range reaches its maximum Is the altitude up to which cabin pressure of 8 000 ft can be maintained Is the altitude at which the specific range reaches its minimum

4 - Can the length of a stopway be added to the runway length to determine the takeoff distance available? Yes, but the stopway must be able to carry the weight of the aeroplane No, unless its centreline is on the extended centreline of the runway Yes, but the stopway must have the same width as the runway No

5 - A higher outside air temperature (OAT): Increases the climb limited take-off mass Increases the field length limited take-off mass Decreases the take-off distance Decreases the brake energy limited take-off mass

6 - Which statement with respect to the step climb is correct? Executing a desired step climb at high altitude can be limited by buffet onset at g-loads greater than 1 A step climb is executed in principle when, just after levelling off, the 1.3g altitude is reached A step climb is executed because ATC desires a higher altitude A step climb must be executed immediately after the aeroplane has exceeded the optimum altitude

7 - The approach climb requirement has been established to ensure: Minimum climb gradient in case of a go-around with one engine inoperative. Manoeuvrability during approach with full flaps and gear down, all engines operating. Manoeuvrability in case of landing with one engine inoperative. Obstacle clearance in the approach area.

8 - The maximum indicated air speed of a piston engine aeroplane without turbo charger, in level flight, is reached: At the optimum cruise altitude At the lowest possible altitude At the practical ceiling At the service ceiling

9 - The maximum speed in horizontal flight occurs when: The maximum thrust is equal to the total drag The thrust does not increase further with increasing speed The thrust is equal to minimum drag The thrust is equal to the maximum drag

10 - Which of the following are to be taken into account for the runway in use for take-off? Airport elevation, runway slope, standard temperature, pressure altitude and wind components Airport elevation, runway slope, standard temperature, standard pressure and wind components Airport elevation, runway slope, outside air temperature, standard pressure and wind components Airport elevation, runway slope, outside air temperature, pressure altitude and wind components

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