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Home > Training for exam quizzes ATPL, PPL(A), PPL(H), BPL Hot Air, BPL Gas, SPL - Sailplane, EASA Drone, FAA Drone > Performance and flight planning - PPL(A) - Private Pilot License

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

Test 10 Questions PPL(A) - Private Pilot License - Performance and flight planning, no time limit

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1 - The empty weight and the corresponding center of gravity (CG) of an aircraft are initially determined... By weighing Through data provided by the aircraft manufacturer. By calculation. For one aircraft of a type only, since all aircraft of the same type have the same mass and CG position.

2 - The balance arm is the horizontal distance between... The front C.G. limit and the datum line The C.G. of a mass and the rear C.G. limit The C.G. of a mass and the datum line The front C.G. limit and the rear C.G. limit

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 - What range can be achieved at the following conditions? Outside air temperature: 6° C Pressure Altitude: 6000 ft Power: 65 % See annex (PFP-013) (1,00 P.) Siehe Anlage 12

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457 NM 503 NM 444 NM 482 NM

5 - 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

6 - What must be considered for cross-border flights? Transmission of hazard reports Regular location messages Approved exceptions Requires flight plans

7 - The speed Vy is defined as... Best speed of climb. Best angle of climb. Best distance of climb. Best distance of climb.

8 - Exceeding the maximum allowed aircraft mass is... Not permissible and essentially dangerous Only relevant if the excess is more than 10 % Compensated by the pilot's control inputs Exceptionally permissible to avoid delays.

9 - 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

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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.

10 - 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

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