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Performance - ATPL - Airline Transport Pilot license
Performance - ATPL - Airline Transport Pilot license
Test 10 domande Performance, tempo libero
Cambia Materia
Nuovo Test!
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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