Performance - ATPL - Airline Transport Pilot license

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

1 - The speed V2 is defined for jet aeroplane as: Take-off decision speed Lift off speed Critical engine failure speed Take-off climb speed or speed at 35'

2 - Which take-off speed is affected by the presence or absence of stopway and / or clearway? V1 VMCA VMCG V2

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

4 - Refer to CAP698 Section 3 - MEP1 Figure 3.1 Normal Procedure Given:OAT -15 °CPressure Altitude: 4000' RWY 12RWind· 080/12 KTTake-off Mass: 4000 lbs Runway Surface: tarred and dryWhat is the minimum runway length? No stopway or clearway is available.

1250 ft 1750 ft 1950 ft 1550 ft

5 - The tangent from the origin to the power required against true airspeed curve, for a jet aeroplane, determines the speed for: Maximum endurance Critical angle of attack Maximum specific range Minimum power

6 - Which of the following is true according to regulations for turbo propeller powered aeroplanes not performing a steep approach? Maximum Landing Distance at destination is 0,95 x LDA (Landing Distance Available). Maximum use of clearway is 1,5 x runway. Maximum Landing Distance at the destination aerodrome and at any alternate aerodrome is 0,7 x LDA (Landing Distance Available). Maximum Take-off Run is 0,5 x runway.

7 - Other factors remaining constant, how does increasing altitude affect Vx and Vy in terms of TAS? Both will remain the same Both will decrease Both will increase Vx will decrease and Vy will increase

8 - In the event of engine failure below V1, the first action to be taken by the pilot in order to decelerate the aeroplane is to: Apply wheel brakes Reverse engine thrust Deploy airbrakes or spoilers Reduce the engine thrust

9 - Any acceleration in climb, with a constant power setting: Improves the rate of climb if the airspeed is below VY Improves the climb gradient if the airspeed is below VX Decreases rate of climb and increases angle of climb Decreases the rate of climb and the angle of climb

10 - The use of reduced take-off thrust is permitted, only if: The actual take-off mass (TOM) including a margin is greater than the performance limited TOM The take-off distance available is lower than the take-off distance required one engine out at V1 The actual take-off mass (TOM) is greater than the climb limited TOM The actual take-off mass (TOM) is lower than the field length limited TOM

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