Performance - ATPL - Airline Transport Pilot license

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

1 - Which statement, in relation to the climb limited takeoff mass of a jet aeroplane, is correct? The climb limited takeoff mass is determined at the speed for best rate of climb The climb limited takeoff mass decreases with increasing OAT On high elevation airports equipped with long runways the aeroplane will always be climb limited 50% of a head wind is taken into account when determining the climb limited takeoff mass

2 - What is the effect of tail wind on the time to climb to a given altitude? The time to climb increases The time to climb decreases The time to climb does not change The effect on the time to climb will depend on the helicopter type

3 - The drift down requirements are based on: The obstacle clearance during a descent to the new cruising altitude if an engine has failed The landing mass limit at the alternate The maximum flight path gradient during the descent The actual engine thrust output at the altitude of engine failure

4 - In relation to the net take-off flight path, the required 35 ft vertical distance to clear all obstacles is: Based on pressure altitudes The minimum vertical distance between the lowest part of the aeroplane and all obstacles within the obstacle domain The height at which power is reduced to maximum climb thrust The height by which acceleration and flap retraction should be completed

5 - The one engine out take-off run is the distance between the brake release point and: The lift-off point The point where V2 is reached The middle of the segment between VLOF point and 35 ft point The point half way between V1 and V2

6 - As long as an aeroplane is in a positive climb: VX may be greater or less than VY depending on altitude VX is always below VY VY is always above VMO VX is always above VY

7 - In which of the following distances can the length of a stopway be included? In the one-engine failure case, take-off distance In the accelerate stop distance available In the take-off run available In the all-engine take-off distance

8 - Complete the following statement regarding the take-off performance of an aeroplane in performance class Following an engine failure at (i) ........... and allowing for a reactiontime of (ii) ........... a correctly loaded aircraft must be capable of decelerating to a halt withinthe (iii) ......... (i) V2 (ii) 3 seconds (iii) Take-off distance available (i) V1 (ii) 2 seconds (iii) Accelerate - stop distance available (i) V1 (ii) 2 seconds (iii) Take-off distance available (i) V1 (ii) 1 second (iii) Accelerate - stop distance available

9 - Which of the following combinations adversely affects take-off and initial climb performance? High temperature and high relative humidity Low temperature and low relative humidity High temperature and low relative humidity Low temperature and high relative humidity

10 - During take-off the third segment begins: When landing gear is fully retracted When acceleration to flap retraction speed is started When flap retraction is completed When acceleration starts from VLOF to V2

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