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Performance - ATPL - Airline Transport Pilot Licence

Test 10 domande Performance, tempo libero

1 - 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

2 - The landing field length required for jet aeroplanes at the alternate (wet condition) is the demonstrated landing distance plus 92% 67% 70% 43%

3 - Which of the following statements with regard to the actual acceleration height at the beginning of the 3rd climb segment is correct? A lower height than 400 ft is allowed in special circumstances e.g. noise abatement The minimum value according to regulations is 1000' The minimum value according to regulations is 400' There is no legal minimum value, because this will be determined from case to case during the calculation of the net flight path

4 - Which statement is correct? The performance limited take-off mass is the highest of: field length limited take-off mass climb limited take-off mass obstacle limited take-off mass The climb limited take-off mass will increase if the headwind component increases The climb limited take-off mass depends on pressure altitude and outer air temperature The climb limited take-off mass increases when a larger take-off flap setting is used

5 - With regard to the drift down performance of the twin jet aeroplane, what is meant by 'equivalent gross weight at engine failure'? The increment represents fuel used before engine failure The equivalent gross weight at engine failure is the actual gross weight corrected for OAT higher than ISA +10°C The increment accounts for the higher fuel flow at higher temperatures This gross weight accounts for the lower Mach number at higher temperatures[see Annex]

6 - The length of a clearway may be included in: The take-off distance available The distance to reach V1 The take-off run available The accelerate-stop distance available

7 - What happens to the drag of a jet aeroplane if, during the initial climb after take off, constant IAS is maintained?(Assume a constant mass) The drag decreases The drag increases considerably The drag increases initially and decreases thereafter The drag remains almost constant

8 - The speed V2 is: The lowest airspeed required to retract flaps without stall problems That speed at which the PIC should decide to continue or not the take-off in the case of an engine failure The lowest safety airspeed at which the aeroplane is under control with aerodynamic surfaces in the case of an engine failure The take-off safety speed

9 - The speed for maximum lift/drag ratio will result in: The maximum endurance for a propeller driven aeroplane The maximum range for a jet aeroplane The maximum angle of climb for a propeller driven aeroplane The maximum range for a propeller driven aeroplane

10 - On a dry runway the accelerate stop distance is increased: By headwind By uphill slope By a lower take-off mass because the aeroplane accelerates faster to V1 By low outside air temperature

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