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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 conversion factor from kilogram [kg] into pounds [lb] is... Kg x 2 = lb. Kg x 2.205 = lb. Kg / 2.205 = lb. Kg x 0.454 = lb

2 - The term "moment" with regard to a mass and balance calculation is referred to as... Sum of a mass and a balance arm. Quotient of a mass and a balance arm. Difference of a mass and a balance arm Product of a mass and a balance arm.

3 - How does aircraft flap configuration influence the take-off performance? A higher flap setting decreases ground roll and increases lift-off speed and climb performance A higher flap setting decreases ground roll and lift-off speed and increases climb performance A higher flap setting increases ground roll, lift-off speed, and climb performance A higher flap setting decreases ground roll and lift-off speed, but also climb performance

4 - The term "datum" with regard to a mass and balance calculation defines... The point on the lateral axis of an aeroplane or its extension from which the centers of gravity of all masses are referenced. The point on the vertical axis of an aeroplane or its extension from which the centers of gravity of all masses are referenced. The point on the longitudinal axis of an aeroplane or its extension from which the centers of gravity of all masses are referenced. The distance from the reference plane to the center of gravity of an aircraft.

5 - During a VFR flight the remaining usable fuel at a checkpoint is 80 USG. Reserve fuel is 20 USG, remaining flight time according to flight plan is 2h 20min. What is the highest acceptable fuel flow (FF) for the rest of the trip? FF = 8.6 USG/h FF = 42.9 USG/h FF = 25.7 USG/h FF = 34.3 USG/h

6 - Given the following conditions, the TAS equals... Outside air temperature: 10° C Pressure altitude: 6000 ft Power: 65 % See annex (PFP-014) (1,00 P.) Siehe Anlage 13

96 kt. 92 kt 88 kt. 100 kt.

7 - Which is the most recently determined empty mass and the associated center of gravity (CG) arm from the aircraft documentation? See annex (PFP-006) (1,00 P.) Siehe Anlage 6

5 kg; 1.3 m 4 kg; 1.1 m 498 kg; 280.59 m 512 kg; 285.39 m

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

9 - 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

10 - (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

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