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 - What is the true airspeed (TAS) [kt] and fuel consumption [l/h] for cruise flight with 70 % 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

110 kt. 23.9 l/h. 100 kt. 19.3 l/h. 95 kt. 19.6 l/h. 105 kt. 21.5 l/h

2 - (For this question, please use annex PFP-061) According ICAO, what symbol indicates a group of unlighted obstacles? (2,00 P.) Siehe Anlage 22

C B A D

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

4 - The red marking at the end of the yellow arc (5) indicates which airspeed? See figure (PFP-008) (1,00 P.) Siehe Anlage 8

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

5 - Given the following data: Take-Off fuel = 200 lbs Alternate fuel = 40 lbs Final reserve fuel = 30 lbs After 25 minutes the remaining fuel is 120 lbs. Assuming that fuel flow will remain unchanged, the remaining time to the destination should not exceed: 37.5 min 20.0 min 15.6 min 59.4 min

6 - The distance between the center of gravity and the datum is called... Span width. Balance arm. Lever Torque

7 - (For this question, please use annex PFP-063) According ICAO, what symbol indicates a general spot elevation? (2,00 P.) Siehe Anlage 24

B C A D

8 - (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

9 - 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.

10 - During a flight with a flight plan submitted, landing is conducted at an airfield other than the destination stated in the filed flight plan. Who has to be contacted by the pilot immediately? Local office for aereal supervision The flight manager on duty Aeronatical Information Service (AIS). The police department.

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