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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:
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
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
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.
Invia il test per la correzione
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