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Home > Training for exam quizzes ATPL, PPL(A), PPL(H), BPL Hot Air, BPL Gas, SPL - Sailplane, EASA Drone, FAA Drone > Performance - ATPL - Airline Transport Pilot license

Quiz Performance - ATPL - Airline Transport Pilot license

Test 10 Questions ATPL - Airline Transport Pilot license - Performance, no time limit

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1 - Which of the following factors determines the maximum flight altitude in the 'Buffet Onset Boundary' graph? Service ceiling Theoretical ceiling Economy Aerodynamics

2 - 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.

3 - In a given configuration the endurance of a piston engine aeroplane only depends on: Altitude, speed, mass and fuel on board. Speed, mass and fuel on board. Speed and mass. Altitude, speed and mass.

4 - What is the result of a large take off flap setting compared to a small take off flap setting on required Take-off Distance (TOD) and the field length limited Take-off Mass (TOM)? Increased TOD required and decreased field length limited TOM Decreased TOD required and increased field length limited TOM Decreased TOD required and decreased field length limited TOM Increased TOD required and increased field length limited TOM

5 - The take-off distance available is: The runway length plus half of the clearway The runway length minus stopway The total runway length, without clearway even if this one exists The length of the take-off run available plus the length of the clearway available

6 - During climb to the cruising level, a headwind component: Increases the climb time Increases the amount of fuel for the climb Decreases the climb time Decreases the ground distance flown during that climb

7 - Below the optimum cruise altitude: The IAS for long range cruise increases continuously with decreasing altitude The TAS for long range cruise increases continuously with decreasing altitude The Mach number for long range cruise decreases continuously with decreasing altitude The Mach number for long range cruise increases continuously with decreasing altitude

8 - A four jet-engine aeroplane (mass = 150 000 kg) is established on climb with all engines operating. The lift-to-drag ratio is 14.Each engine has a thrust of 75 000 Newton. The gradient of climb is: (given: g= 10 m/s 2) 27%. 1.286%. 7.86%. 12.86%.

9 - If there is a tail wind, the climb limited TOM will: Not be affected Increase in the flaps extended case Decrease Increase

10 - Other factors remaining constant and not limiting, how does increasing pressure altitude affect allowable take-off mass? Allowable take-off mass increases There is no effect on allowable take-off mass Allowable take-off mass decreases Allowable take-off mass remains uninfluenced up to 5000' pressure altitude

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