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Performance - ATPL - Airline Transport Pilot license

Test 10 domande Performance, tempo libero

1 - At a given mass, the reference stall speed of a twin engine turboprop aircraft is 100 KT in the landing configuration. The minimum speed a pilot must maintain in short final is: 115 KT 125 KT 123 KT 120 KT

2 - During the flight preparation the climb limited take-off mass (TOM) is found to be much greater than the field length limited TOM using 5° flap. In what way can the performance limited TOM be increased? There are no limiting obstacles. By selecting a higher V2 By selecting a lower V2 By selecting a higher flap setting By selecting a lower flap setting

3 - 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

4 - If other factors are unchanged, the fuel mileage (nautical miles per kg) is: Independent from the centre of gravity position Lower with an aft centre of gravity position Lower with a forward centre of gravity position Higher with a forward centre of gravity position

5 - The speed V1 is defined as: Take-off climb speed Speed for best angle of climb Take-off decision speed Engine failure speed

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

7 - A constant headwind: Increases the angle of descent Increases the rate of descent Increases the angle of the descent flight path Increases the descent distance over ground

8 - A climb gradient required is 3.3%. For an aircraft maintaining 100 KT true airspeed, no wind, this climb gradient corresponds to a rate of climb of approximately: 3 300 fpm 330 fpm 33.0 m/s 3.30 m/s

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 - The danger associated with low speed and/or high speed buffet Can be reduced by increasing the load factor. Limits the manoeuvring load factor at high altitudes. Has to be considered at take-off and landing. Exists only above MMO.

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