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Home > Exam Tests > Performance and flight planning - PPL(A) - Private Pilot License

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 - Given the following data for a VFR flight: Trip fuel = 70 US gallons Contingency fuel = 5% of trip fuel Alternate and final reserve fuel = 20 US gallons Usable fuel at take-off = 95 US gallons After half of the distance you read that you have consumed 40 US gallons. Assume that fuel flow remains unchanged. Which statement is correct? Upon landing 15.0 US gallons will remain in addition to alternate and final reserve fuel. Upon landing 5.0 US gallons will remain in addition to alternate and final reserve fuel Upon landing, a total of 40.0 US gallons will remain. The remaining fuel is insufficient for a landing at destination with alternate and final reserve fuel remaining.

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

question 70-48-49-50.jpg

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

3 - The VFR semicircular rules are based on the... True course (TC). Magnetic heading (MH) Magnetic course (MC). True heading (TH).

4 - Baggage and cargo must be properly stowed and fastened, otherwise a shift of the cargo may cause... Continuous attitudes which can be corrected by the pilot using the flight controls. Structural damage, angle of attack stability, velocity stability Uncontrollable attitudes, structural damage, risk of injuries. Calculable instability if the C.G. is shifting by less than 10 %.

5 - The term "steady flight" is defined as... Flight with a steady power setting without changing course Climb or descent with a constant climb or descent rate in calm weather conditions. Unaccelerated flight. The four forces thrust, drag, lift, and weight are in equilibrium. Flight in smooth air without turbulence and a perfectly trimmed aircraft.

6 - Wie beeinflusst die Lufttemperatur die Leistung eines Kolbenmotors? Geringere Temperatur entspricht höherer Luftdichte, dies führt zu geringerer Motorleistung Höhere Temperatur entspricht geringerer Luftdichte, dies führt zu geringerer Motorleistung Höhere Temperatur entspricht höherer Luftdichte, dies führt zu höherer Motorleistung Geringere Temperatur entspricht geringerer Luftdichte, dies führt zu höherer Motorleistung

7 - The term "balance arm" in the context of a mass and balance calculation defines the... Distance from the datum to the center of gravity of a mass. Distance of a mass from the center of gravity. Point on the longitudinal axis of an aeroplane or its extension from which the centers of gravity of all masses are referenced. Point through which the force of gravity is said to act on a mass.

8 - What is the take-off distance at 750 kg take-off mass, standard (ISA) conditions at an elevation of 4000 ft with 5 kt tailwind? See annex (PFP-009) (1,00 P.) Siehe Anlage 9

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900 m 320 m 630 m 480 m

9 - Given the following data for a VFR flight: Take-off fuel: 180 kg including reserve fuel, which is 30% of take off fuel. After half of the distance the remaining fuel is 100 kg. Assume that cruise conditions will remain unchanged. Determine the remaining fuel at the destination: 80 kg 40 kg 10 kg 20 kg

10 - 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

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90 kt 120 kt 110 kt 100 kt

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