Performance - ATPL - Airline Transport Pilot license

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

1 - With zero wind, the angle of attack for maximum range for an aeroplane with turbojet engines is: Lower than the angle of attack corresponding to maximum endurance Equal to the angle of attack corresponding to maximum lift to drag ratio Equal to the angle of attack corresponding to zero induced drag Equal to the angle of attack corresponding to maximum endurance

2 - When determining the maximum landing mass of an turbojet powered aeroplane during the planning phase what factor must be used on the landing distance available (dry runway) 115/100 1.67 0.60 60/115

3 - Considering VR, which statement is correct? VR is the lowest climb speed after engine failure In case of engine failure below VR the take-off should be aborted VR is the speed at which rotation should be initiated VR is the lowest speed for directional control in case of engine failure

4 - Maximum Tyre Speed can limit the Lift-off Speed.Which kind of speed can be directly used to determine this limitation? Groundspeed EAS TAS IAS

5 - At reference or see Performance Manual MRJT 1 Figure 4.28.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

3100 m. 2900 m. 2700 m. 2600 m.

6 - According to PART-CAT, for turbo-prop aeroplanes, the required runway length at a destination airport is: Less then that required at an alternate airport. More than that required at an alternate airport. The same as that required at an alternate airport. 60% greater than that required at an alternate airport

7 - In case of an engine failure which is recognized at or above V1: A height of 50 ft must be reached within the take-off distance The take-off must be rejected if the speed is still below VLOF The take-off should be rejected if the speed is still below VR The take-off must be continued

8 - The determination of the maximum mass on brake release, of a certified turbojet aeroplane with 5°, 15° and 25° flap angles on take-off, leads to the following values:Flap angle: 5° 15° 25°Runway limitation (kg): 66000 69500 715002nd segment climb limitation: 72200 69000 61800Wind correction:Headwind: +120 kg / KT Tailwind: -360 kg / KTGiven that the tailwind component is equal to 5 KT, the maximum mass on brake release and corresponding flap angle will be: 69000 kg / 15 deg 67700 kg / 15 deg 69700 kg / 25 deg 72200 kg / 5 deg

9 - A 'Balanced Field Length' is said to exist where: The clearway does not equal the stopway The accelerate stop distance is equal to the all engine take-off distance The accelerate stop distance is equal to the take-off distance available The one engine out take-off distance is equal to the all engine take-off distance

10 - 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

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