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Performance and flight planning - PPL(A) English - Private Pilot License (Aircraft)
Performance and flight planning - PPL(A) English - Private Pilot License (Aircraft)
Test 10 domande Performance and flight planning, tempo libero
Cambia Materia
Nuovo Test!
1 - The speed Vy is defined as...
Best speed of climb.
Best angle of climb.
Best distance of climb.
Best distance of climb.
2 - The center of gravity has to be located...
Between the front and the rear C.G. limit.
Behind the rear C.G. limit.
In front of the front C.G. limit
Right of the lateral C. G. limit.
3 - What is the required fuel to climb from FL 65 to FL 95 under the following conditions? Aircraft mass: 3000 lb. OAT in FL 65: -5° C OAT in FL 95: -15° C See annex (PFP-023) (1,00 P.) Siehe Anlage 14
1 GAL
2 GAL
6 GAL
3 GAL
4 - The result of a front C.G. position is: 1. Increase in stability. 2. Increase in fuel consumption. 3. Increase in stall speed. 4. Increase in range.
2. 4
1, 2
1, 2, 3
2, 3, 4
5 - For a take-off from runway 22 and a reported wind of 250°/10 kt, the longitudinal wind component equals...
9 kt tailwind
5 kt tailwind.
9 kt headwind.
9 kt headwind.
6 - It is possible that the surface wind speed at an airport is reduced due to friction. When a surface area with a minor tailwind condition is left during the initial climb, the pilot might expect...
An increase in airspeed and rate of climb due to decreasing tailwind
A deacrease in airspeed and climb performance due to decreasing tailwind
An increase in airspeed and rate of climb due to increasing tailwind.
A decrease in airspeed and rate of climb due to increasing tailwind.
7 - (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
8 - 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.
9 - 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
10 - The EOBT (estimated off-block time) is specified in the ATS flight plan as...
Coordinated Universal Time (UTC)
Standard Time (ST)
Local Mean Time (LMT).
Central European Time (CET).
Invia il test per la correzione
Cambia Materia
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