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 term "center of gravity" is defined as... The heaviest point on an aeroplane. Half the distance between the neutral point and the datum line. Another designation for the neutral point The point at which the total mass of the aeroplane is considered to act.

2 - What is the fuel flow and the true airspeed for cruise flight with 60 % power in flight level 85 at an OAT of -25° C? See annex (PFP-014) (1,00 P.) Siehe Anlage 13

Fuel flow: 17 l. TAS: 81 kt. Fuel flow: 17.5 l. TAS: 83 kt Fuel flow: 20 l. TAS: 89 kt. Fuel flow: 18.5 l. TAS: 85 kt.

3 - Calculated take-off mass = 1082 kg, calculated CG = 0.254 m, fuel burn = 55 l on station 0.40 m. Where is the CG situated after the landing? 24.6 cm 25.2 cm 25.4 cm 24.8 cm

4 - The speed VFE is defined as... Stalling or minimum steady flight speed with the flaps retracted. Stalling or minimum steady flight speed with the flaps retracted. Stalling or minimum steady flight speed with the flaps extended. Maximum landing gear extended speed

5 - Loads must be adequately secured in order to... Carry extra fuel Allow steep turns Avoid any centre of gravity (C.G.) movements Prevent excessive 'g'-loading during the landing flare

6 - The EOBT (estimated off-block time) is specified in the ATS flight plan as... Coordinated Universal Time (UTC) Standard Time (ST) Local Mean Time (LMT). Central European Time (CET).

7 - The position of the center of gravity equals... See figure (PFP-052e) (1,00 P.) Siehe Anlage 1 147.5 in. 145.7 in. 142 in. 137.5 in

8 - What is the take-off distance at 705 kg take-off mass, OAT 20° C, QNH 1013 hPa at an elevation of 3500 ft with 5 kt tailwind? See annex (PFP-009) (1,00 P.) Siehe Anlage 9

720 m 880 m 790 m 820 m

9 - (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

10 - What mass equals 102 litres of Avgas 100LL? 142 lbs 74 lbs 142 kg 74 kg

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