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Performance and flight planning - PPL(A) English - Private Pilot License (Aircraft)

Test 10 domande Performance and flight planning, tempo libero

1 - The term "maximum elevation figure" (MEF) is defined as... The highest elevation within an area covering 30 minutes of latitude and 30 minutes of longitude. The highest elevation within an area covering 30 minutes of latitude and 30 minutes of longitude plus a safety margin, rounded to the next higher 100 ft. The highest elevation within an area covering 30 minutes of latitude and 30 minutes of longitude plus a safety margin of 1000 ft (305 m), rounded to the next higher 100 ft The highest elevation within an area covering 1 degree of latitude and 1 degree of longitude plus a safety margin, rounded to the next lower 100 ft.

2 - For the purpose of a flight preparation, the pilot calculates a total take-off mass of 750 kg and a total moment of 625 mmkg. Which cross marks the center of gravity (CG)? See annex (PFP-003) (1,00 P.) Siehe Anlage 3

4 2 1 3

3 - The upper limit of LO R 16 equals... See annex (PFP-056) (1,00 P.) Siehe Anlage 15

FL150. 1 500 m MSL. 1 500 ft MSL. 1.500 ft GND.

4 - The position of the center of gravity (including fuel) equals... See figure(PFP-053e) (1,00 P.) Siehe Anlage 2

37.1 cm 0.401 m 37.3 cm 0.403 m.

5 - What is the true airspeed (TAS) [kt] and fuel consumption [l/h] for cruise flight with 60 % power in flight level 60 under the following conditions? Temperature: ISA - 20° C QNH: 980 hPa See annex (PFP-012) (2,00 P.) Siehe Anlage 10

96 kt. 19.1 l/h. 95 kt. 19.6 l/h. 110 kt. 25.1 l/h. 95,75 kt. 19.8 l/h.

6 - The end of the green arc (4) indicates which airspeed? See figure (PFP-008) (1,00 P.) Siehe Anlage 8

VNO: Maximum speed for normal operations VNE: Never-exceed spee VFE: Maximum flap extended speed VS1: Stall speed with flaps up

7 - At which airspeed do you climb to flight level (FL) 75 after a departure from an airfield which is located at a pressure altitude of 3000 ft with an initial mass of 3000 lbs? OAT at airfield: 25° C OAT in FL 75: 0° C See annex (PFP-023) (1,00 P.) Siehe Anlage 14

90 kt 120 kt 110 kt 100 kt

8 - What happens to the true airspeed at a constant indicated airspeed during a climb? It decreases It increases It remains constant below 5000 ft It remains constant above 5000 ft

9 - Given the following conditions, the take-off distance equals... Outside air temperature: -20° C Pressure Altitude: 5000 ft Aeroplane mass: 750 kg Headwind: 10 kt

450 m. 380 m 410 m 310 m.

10 - The angle of descent is defined as... The ratio between the change in height and the horizontal distance travelled within the same time, expressed in percent [%] The angle between a horizontal plane and the actual flight path, expressed in degrees [°]. The ratio between the change in height and the horizontal distance distance travelled within the same time, expressed in degrees [°]. The angle between a horizontal plane and the actual flight path, expressed in percent [%].

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