Pilot Test ZonePPL(A) exam questions — Flight Performance & Planning
A bank of 54 PPL(A) ULC exam questions for Flight Performance & Planning. Check the correct answers; full EASA/ICAO explanations are available in the app.
All topics: Flight Performance & Planning →
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- Barometric error occurs when
- Temperature error occurs when
- Component weight 55 kg, arm = 2.3 m. The moment [kgm]
- The international standard atmosphere (International Standard Atmosphere) defines the following conditions at the sea level: temperature / pressure / density / temperature gradient
- The center of gravity can be defined as
- The center of gravity can be defined as
- Weighing of the aircraft (SP): readout on the scales under the front gear - 155 kg, readout - the sum on the main 320 kg. Distance SP front - front gear 0.8 m, front SP - main 2.4 m. What is the distance between the front SP and the center of gravity
- Weighing of the aircraft: the readout on the scales under the front gear 205 kg, the readout - the sum of the main 420 kg. Front gear arm - 0.9m front, main 2.6 m. What is the distance between the front CG - the center of gravity
- Formula fo the moment
- The pressure altitude of the airport on a particular day can be determined
- "The influence of the earth" allows
- "The influence of the earth " is a phenomenon consisting in
- For the hydroplaning phenomenon (dynamic) to take place during the run / roll of the airplane the following factors are necessary
- What is VX
- What is VY
- Does high humidity contribute to decrease in the aircraft performance
- For each combination of the altitude of the flight and aircraft weight, in the scale of minimum to maximum speed there is
- High density altitude (in relation to low density altitude) means
- How will high ambient temperature influence the aircraft take-off run (at a given airport) in comparison with the case when the ambient temperature is low
- How will the plane take-off from an airport located in the mountains influence the lengh of the take-off run in comparison with the take-off in the same temperature, aircraft weigh and wind conditions and with the setting of the flaps from the airport at 0 m above the sea level
- How will the use of higher flap setting (than usual) influence the length of the take-off run
- How will increase of the weigh of the aircraft influence the lengh of the take-off run
- What shall be the effects of changes in ambient temperature on the performance of the aircraft if all other parameters remain unchanged
- What shall be the effects of changes in ambient temperature on the performance of the aircraft if all other parameters remain unchanged
- If the center of gravity is near the extreme front position
- If the centre of gravity is maximum forward position the aircraft among others shall
- The direction of the airstrip 040°, wind 270/18 kt (ATIS). What are the components of the wind
- The direction of the airstrip 150°, wind 220/22 kt (ATIS). What are the components of the wind
- The direction of the airstrip 200°, wind 080 thirteenths kt (ATIS). What are the components of the wind
- The direction of the airstrip 220°, wind 160/26 kt (ATIS). What are the components of the wind
