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

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

1 - The angle of descent is defined as... The ratio between the change in height and the horizontal distance travelled within the same time, expressed in percent [%] The angle between a horizontal plane and the actual flight path, expressed in degrees [°]. The ratio between the change in height and the horizontal distance distance travelled within the same time, expressed in degrees [°]. The angle between a horizontal plane and the actual flight path, expressed in percent [%].

2 - 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

3 - During an unaccelerated flight... Drag equals lift and thrust equals gravity. Thrust equals the sum of drag and gravity. Thrust equals lift and drag equals gravity. Thrust equals drag and lift equals gravity.

4 - Considering the following fuel data, how much trip fuel is required? Fuel for start-up and taxi: 5 L Fuel for take-off and climb: 12 L Fuel for cruise flight: 25 L Fuel for descent, approach and landing: 7 L Fuel for taxi and parking: 3 L Fuel to alternate: 13 L Final reserve fuel: 10 L 75 L 52 L 49 L 44 L

5 - 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

6 - The term "maximum elevation figure" (MEF) is defined as... The highest elevation within an area covering 30 minutes of latitude and 30 minutes of longitude. The highest elevation within an area covering 30 minutes of latitude and 30 minutes of longitude plus a safety margin, rounded to the next higher 100 ft. The highest elevation within an area covering 30 minutes of latitude and 30 minutes of longitude plus a safety margin of 1000 ft (305 m), rounded to the next higher 100 ft The highest elevation within an area covering 1 degree of latitude and 1 degree of longitude plus a safety margin, rounded to the next lower 100 ft.

7 - For the purpose of a flight preparation, the pilot calculates a total take-off mass of 750 kg and a total moment of 625 mmkg. Which cross marks the center of gravity (CG)? See annex (PFP-003) (1,00 P.) Siehe Anlage 3

4 2 1 3

8 - Which is the maximum rate of climb for the aircraft at 6500 ft pressure altitude and an OAT of 0° C? See annex (PFP-011) (1,00 P.) Siehe Anlage 11

480 ft / min 400 ft / min 520 ft / min 800 ft / min

9 - For the purpose of a flight preparation the pilot calculates a total take-off mass of 775 kg and a total moment of 700 mmkg. Which cross marks the center of gravity (CG)? See annex (PFP-005) (1,00 P.) Siehe Anlage 5

3 2 4 1

10 - 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.

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