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

Test 10 domande PPL(A) English - Private Pilot License (Aircraft) - Performance and flight planning, tempo libero

1 - The upper limit of LO R 4 equals... See annex (PFP-030) (1,00 P.) Siehe Anlage 16

4.500 ft AGL 4.500 ft MSL. 1.500 ft MSL. 1.500 ft AGL

2 - (For this questions use attachment or CAP697 SEP1 Fig. 2.2 Table 2.2.3) For planning a VFR flight, the following data are given: Flight time with planning "overhead-overhead" = 2h 43min Pressure Altitude = 6.500 ft Temperature = ISA-20 Power setting = 2300 RPM Taxi Fuel = 2 USG Additional time for climb = 7 min, Additional time for approach and landing = 10 min The reserve fuel has to be 30% of trip fuel. Determine the minimum block fuel: (2,00 P.) Siehe Anlage 21

47.3 USG 50.4 USG 43.8 USG 39.2 USG

3 - The center of gravity has to be located... Between the front and the rear C.G. limit. Behind the rear C.G. limit. In front of the front C.G. limit Right of the lateral C. G. limit.

4 - 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.

5 - (For this questions, use attachment or CAP697 SEP1 Fig. 2.2 Table 2.2.3) Planning a flight from EDWF (Leer Papenburg) to EDWH (Oldenburg Hatten), the following conditions apply: Cruise level = FL 75 Temperature = ISA Cruise weight = 3400 lbs Power setting = 23.0 in. HG @ 2300 RPM Determine True Airspeed (TAS) and Fuel Flow (FF): (2,00 P.) Siehe Anlage 21

TAS = 145 kt FF = 71.1 GPH TAS = 160 kt FF = 12.3 GPH TAS = 160 kt FF = 11.9 GPH TAS = 145 kt FF = 11.9 GPH

6 - When preparing to carry out the weighing procedure on an aircraft, which of the following is required? Drain all engine tank oil Remove service equipment Drain all useable fuel Remove the batteries

7 - (For this questions use attachment or CAP697 SEP1 Fig. 2.2 Table 2.2.3) For planning a VFR flight, the following data are given: Flight time with planning "overhead-overhead" = 2h 42min Pressure Altitude = 7.500 ft Temperature = ISA Power setting = 2300 RPM Taxi Fuel = 2 USG Additional time for climb = 8 min, Additional time for approach and landing = 10 min The reserve fuel has to be 30% of trip fuel. Determine the minimum block fuel: (2,00 P.) Siehe Anlage 21

51.8 USG 37.7 USG 46.4 USG 48.4 USG

8 - 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.

9 - Up to which altitude is an overflight prohibited according to the NOTAM? See figure (PFP-024) (1,00 P.) Siehe Anlage 18

Height 9500 ft Altitude 9500 ft MSL Altitude 9500 m MSL Flight Level 95

10 - The total weight of an aeroplane is acting vertically through the... Stagnation point. Neutral point. Center of pressure. Center of gravity.

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