Performance - ATPL - Airline Transport Pilot license

Test 10 domande ATPL - Airline Transport Pilot license - Performance, tempo libero

1 - Considering TAS for maximum range and maximum endurance, other factors remaining constant: Both will stay constant regardless of altitude Both will decrease with increasing altitude TAS for maximum range will increase with increased altitude while TAS for maximum endurance will decrease with increased altitude Both will increase with increasing altitude

2 - With regard to the drift down performance of the twin jet aeroplane, why does the curve representing 35000 kg gross mass in the chart for drift down net profiles start at approximately 4 minutes at FL370? Due to higher TAS at this mass it takes more time to develop the optimal rate of descent, because of the inertia involved Because at this mass the engines slow down at a slower rate after failure, there is still some thrust left during four minutes All the curves start at the same point, which is situated outside the chart Because at this mass it takes approximately 4 minutes to decelerate to the optimum speed for drift down at the original cruising level[see Annex]

3 - On a reciprocating engine aeroplane, to maintain a given angle of attack, configuration and altitude at higher gross mass: The airspeed will be decreased and the drag increased The airspeed and the drag will be increased The airspeed will be increased but the drag does not change The lift / drag ratio must be increased

4 - To minimize the risk of hydroplaning during landing the pilot should: Use maximum reverse thrust, and should start braking below the hydroplaning speed. Use normal landing-, braking- and reverse technique. Make a 'positive' landing and apply maximum reverse thrust and brakes as quickly as possible. Postpone the landing until the risk of hydroplaning no longer exists.

5 - Considering a rate of climb diagram (ROC versus TAS) for an aeroplane. Which of the diagrams shows the correct curves for 'flaps down' compared to 'clean' configuration?

B C A D

6 - The drift down procedure specifies requirements concerning the: Engine power at the altitude at which engine failure occurs. Climb gradient during the descent to the net level-off altitude. Obstacle clearance after engine failure. Weight during landing at the alternate.

7 - With an true airspeed of 194 KT and a vertical speed of 1000 fpm, the climb gradient is about: 5° 3% 8% 3°

8 - 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

9 - Which statement concerning the inclusion of a clearway in take-off calculation is correct? The field length limited take-off mass will increase V1 remains constant V1 is increased The usable length of the clearway is not limited

10 - For a jet aeroplane, the maximum climb angle is achieved at a speed corresponding to: 1.2 Vs The maximum CL/CD2 ratio 1.1 Vs The maximum CL/CD ratio

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