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

Question 1

What happens to the true airspeed at a constant indicated airspeed during a climb?

Accepted Answer

It increases

Answer

It decreases

Answer

It remains constant below 5000 ft

Answer

It remains constant above 5000 ft

Question 2

The result of a rear C.G. position is...

Accepted Answer

A decrease of stability.

Answer

An increased fuel consumption.

Answer

A decrease of range.

Answer

An increased stall speed.

Question 3

Given the following conditions, the fuel consumption equals... Pressure altitude: 2000 ft Temperature: 31° C RPM: 2400 See annex (PFP-012) (1,00 P.) Siehe Anlage 10

Accepted Answer

19.5 l/h.

Answer

19.1 l/h.

Answer

21.7 l/h

Answer

22.8 l/h

Question 4

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

Accepted Answer

4

Answer

3

Answer

2

Answer

1

Question 5

Wie beeinflusst die Lufttemperatur die Leistung eines Kolbenmotors?

Accepted Answer

Höhere Temperatur entspricht geringerer Luftdichte, dies führt zu geringerer Motorleistung

Answer

Geringere Temperatur entspricht höherer Luftdichte, dies führt zu geringerer Motorleistung

Answer

Höhere Temperatur entspricht höherer Luftdichte, dies führt zu höherer Motorleistung

Answer

Geringere Temperatur entspricht geringerer Luftdichte, dies führt zu höherer Motorleistung

Question 6

The speed VFE is defined as...

Accepted Answer

Stalling or minimum steady flight speed with the flaps retracted.

Answer

Stalling or minimum steady flight speed with the flaps extended.

Answer

Maximum landing gear extended speed

Question 7

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

Accepted Answer

95 kt. 19.6 l/h.

Answer

96 kt. 19.1 l/h.

Answer

110 kt. 25.1 l/h.

Answer

95,75 kt. 19.8 l/h.

Question 8

What is the purpose of "interception lines" in visual navigation?

Accepted Answer

They are used as easily recognizable guidance upon a possible loss of orientation

Answer

To visualize the range limitation from the departure aerodrome

Answer

They help to continue the flight when flight visibility drops below VFR minima

Answer

To mark the next available en-route airport during the flight

Question 9

For a take-off from runway 22 and a reported wind of 250°/10 kt, the longitudinal wind component equals...

Accepted Answer

9 kt headwind.

Answer

9 kt tailwind

Answer

5 kt tailwind.

Question 10

The upper limit of LO R 4 equals... See annex (PFP-030) (1,00 P.) Siehe Anlage 16

Accepted Answer

4.500 ft MSL.

Answer

4.500 ft AGL

Answer

1.500 ft MSL.

Answer

1.500 ft AGL

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