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Home > Training for exam quizzes ATPL, PPL(A), PPL(H), BPL Hot Air, BPL Gas, SPL - Sailplane, EASA Drone, FAA Drone > Performance - ATPL - Airline Transport Pilot license

Quiz Performance - ATPL - Airline Transport Pilot license

Test 10 Questions ATPL - Airline Transport Pilot license - Performance, no time limit

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1 - Regarding the obstacle limited take-off mass, which of the following statements is correct? Wind speed plays no role when calculating this particular mass A take-off in the direction of an obstacle is also permitted in tail wind condition The maximum bank angle which can be used is 10° The obstacle limited mass can never be lower than the climb limited take-off mass

2 - 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

3 - 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.

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1250 ft 1750 ft 1950 ft 1550 ft

4 - The optimum long-range cruise altitude for a turbojet aeroplane: Is always equal to the powerplant ceiling Is independent of the aeroplane mass Increases when the aeroplane mass decreases Is only dependent on the outside air temperature

5 - 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

6 - Consider the graphic representation of the power required versus true air speed (TAS), for a piston engine aeroplane with a given mass. When drawing the tangent from the origin, the point of contact (A) determines the speed of:

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Maximum specific range Critical angle of attack Maximum thrust Maximum endurance

7 - What is the minimum field length required for the worst wind situation, landing a twin jet aeroplane with the anti-skid inoperative?Elevation: 2000 ftQNH: 1013 hPaLanding mass: 50 000 kgFlaps: as required for minimum landing distance Runway condition: dryWind:Maximum allowable tailwind: 15 kt Maximum allowable headwind: 50 kt 2600 m. 3100 m. 2900 m. 2700 m.[see Annex]

8 - If the take-off mass of an aeroplane is tyre speed limited, downhill slope would: Have no effect on the maximum mass for take-off Increase the required take-off distance Increase the maximum mass for take-off Decrease the maximum mass for take-off

9 - Why are 'step climbs' used on long distance flights ? To fly as close as possible to the optimum altitude as aeroplane mass reduces. To respect ATC flight level constraints. Step climbs do not have any special purpose for jet aeroplanes They are used for piston engine aeroplanes only.

10 - 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

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