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Exam simulation Performance ATPL - Airline Transport Pilot license

Exam simulation ATPL Performance 120 questions on 120 minutes

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1 - Considering VR, which statement is correct?
2 - Other factors remaining constant, how does increasing altitude affect Vx and Vy in terms of TAS?
3 - Density altitude is the:
4 - Which statement with respect to the step climb is correct?
5 - To minimize the risk of hydroplaning during landing the pilot should:
6 - Which of the following factors determines the maximum flight altitude in the 'Buffet Onset Boundary' graph?
7 - If the aircraft mass, in a horizontal unaccelerated flight, decreases:
8 - The stopway is an area which allows an increase only in the:
9 - The net flight path gradient after take-off compared to the actual climb gradient is:
10 - ETOPS flight is a twin engine jet aeroplane flight conducted over a route, where no suitable airport is within an area of:
11 - A 'Balanced Field Length' is said to exist where:
12 - Which of the following statements, concerning the obstacle limited take-off mass for performance class A aeroplane, is correct?
13 - A four jet-engine aeroplane (mass = 150 000 kg) is established on climb with all engines operating. The lift-to-drag ratio is 14. Each engine has a thrust of 75 000 Newton. The gradient of climb is: (given: g = 10 m/s²)
14 - Maximum Tyre Speed can limit the Lift-off Speed. Which kind of speed can be directly used to determine this limitation?
15 - Long range cruise is selected as
16 - An aircraft has two certified landing flaps positions, 25° and 35°. If a pilot chooses 35° instead of 25°, the aircraft will have:
17 - Which of the following will decrease V1?
18 - Reduced take-off thrust should normally not be used when:
19 - Which is the correct sequence of speeds during take-off?
20 - According to PART-CAT, which one of the following statements concerning the landing distance for a turbojet aeroplane is correct?
21 - A headwind will:
22 - During certification flight testing on a four engine turbojet aeroplane the actual take-off distances measured are: -3050 m with failure of the critical engine recognised at V1; -2555 m with all engines operating and all other things being equal. The take-off distance adopted for the certification file is:
23 - Which statement is correct for a descent without engine thrust at maximum lift to drag ratio speed?
24 - The danger associated with low speed and/or high speed buffet
25 - The take-off safety speed V2 for two-engine or three-engine turbo propeller powered aeroplanes may not be less than:
26 - The approach climb requirement has been established so that the aeroplane will achieve:
27 - The optimum long-range cruise altitude for a turbojet aeroplane:
28 - What is the effect of tailwind on the time to climb to a given altitude?
29 - Which of the following statements is correct?
30 - Which of the following statements is applicable to the acceleration height at the beginning of the 3rd climb segment?
31 - The 'climb gradient' is defined as the ratio of:
32 - Following a take-off determined by the 50' (15 m) screen height, a light twin climbs on a 10% over-the-ground climb gradient. It will clear a 900 m high obstacle in relation to the runway (horizontally), situated at 10000 m from the 50' clearing point with an obstacle clearance of:
33 - The speed V2 is:
34 - Why are 'step climbs' used on long distance flights?
35 - Consider the graphic representation of the power required versus true air speed (TAS), for a piston engine aeroplane with a given mass. When drawing the tangent from the origin, the point of contact (A) determines the speed of:
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36 - The take-off distance available is:
37 - The speed for maximum lift/drag ratio will result in:
38 - V1 has to be:
39 - The speed V2 is defined for jet aeroplane as:
40 - Two identical turbojet aeroplanes (whose specific fuel consumption is assumed to be constant) are in a holding pattern at the same altitude. The mass of the first one is 95000 kg and its hourly fuel consumption is equal to 3100 kg/h. Since the mass of the second one is 105000 kg, its hourly fuel consumption is:
41 - Which of the following statements with regard to the actual acceleration height at the beginning of the 3rd climb segment is correct?
42 - An aircraft has two certified landing flaps positions, 25° and 35°. If a pilot chooses 25° instead of 35°, the aircraft will have:
43 - What will be the influence on the aeroplane performance if aerodrome pressure altitude is increased?
44 - When compared to still air conditions, a constant headwind component:
45 - The drift down procedure specifies requirements concerning the:
46 - Which combination of circumstances or conditions would most likely lead to a tyre speed limited take-off?
47 - Other factors remaining constant and not limiting, how does increasing pressure altitude affect allowable take-off mass?
48 - Which take-off speed is affected by the presence or absence of stopway and / or clearway?
49 - The pilot of a single engine aircraft has established the climb performance. The carriage of an additional passenger will cause the climb performance to be:
50 - The result of a higher flap setting up to the optimum at take-off is:
51 - Refer to CAP698 Section 3 - MEP1 Figure 3.1 Normal Procedure Given: OAT 24 °C; Pressure Altitude: 3000'; RWY 12L; Wind 080/12 KT; Take-off Mass: 3800 lbs. Other conditions as associated in the header of the graph. What is the take-off distance over a 50 ft obstacle?
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52 - If the climb speed schedule is changed from 280/.74 to 290/.74 the new crossover altitude will be:
53 - During climb to the cruising level, a headwind component:
54 - Refer to CAP698 Section 3 - MEP1 Figure 3.1 Normal Procedure Given: OAT 24 °C; Pressure Altitude: 3000 ft; RWY 30R; Wind 060/04 KT; Take-off Mass: 3800 lbs. Other conditions as associated in the header of the graph. What is the Ground Roll Distance under the conditions given?
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55 - In case of an engine failure which is recognized at or above V1:
56 - Which of the following combinations basically has an effect on the angle of descent in a glide? (Ignore compressibility effects.)
57 - On a dry runway the accelerate-stop distance is increased:
58 - The landing reference speed VREF has, in accordance with CS-25, the following margins above reference stall speed in landing configuration:
59 - How does the best angle of climb and best rate of climb vary with increasing altitude for an aeroplane with a normal aspirated piston engine?
60 - During a descent at constant Mach number, the margin to low speed buffet will:
61 - Which statement about reduced thrust is correct?
62 - The maximum operating altitude for a certain aeroplane with a pressurised cabin
63 - In which of the following distances can the length of a stopway be included?
64 - What is the influence of the mass on maximum rate of climb (ROC) speed if all other parameters remain constant?
65 - The best rate of climb at a constant gross mass:
66 - What is the most important aspect of the 'backside of the power curve'?
67 - The maximum indicated air speed of a piston engine aeroplane without turbo charger, in level flight, is reached:
68 - The long range cruise speed is in relation to the speed for maximum range cruise.
69 - In accordance to CS-25 which of the following listed speeds are used for determination of V2min:
70 - The landing field length required for jet aeroplanes at the alternate (wet condition) is the demonstrated landing distance plus
71 - If a flight is performed with a higher 'Cost Index' at a given mass which of the following will occur?
72 - What is the effect of a headwind component, compared to still air, on the maximum range speed (IAS) and the speed for maximum climb angle respectively?
73 - On a reciprocating engine aeroplane, to maintain a given angle of attack, configuration and altitude at higher gross mass:
74 - What will be the effect on an aeroplane's performance if aerodrome pressure altitude is decreased?
75 - The climb limited take-off mass can be increased by:
76 - If the take-off mass of an aeroplane is tyre speed limited, downhill slope would:
77 - The length of a clearway may be included in:
78 - During the flight preparation the climb limited take-off mass (TOM) is found to be much greater than the field length limited TOM using 5° flap. In what way can the performance limited TOM be increased? There are no limiting obstacles.
79 - In relation to the net take-off flight path, the required 35 ft vertical distance to clear all obstacles is:
80 - A higher outside air temperature (OAT):
81 - In a given configuration the endurance of a piston engine aeroplane only depends on:
82 - The landing field length required for turbojet aeroplanes at the destination (wet condition) is the demonstrated landing distance plus:
83 - The thrust of a jet engine at constant RPM
84 - Which statement regarding V1 is correct?
85 - If there is a tailwind, the climb limited TOM will:
86 - The lowest point of the thrust required curve of a jet aeroplane is the point for:
87 - Which of the following is true according to regulations for turbo propeller powered aeroplanes not performing a steep approach?
88 - The take-off mass of an aeroplane is restricted by the climb limit. What would be the effect on this limit of an increase in the headwind component?
89 - According to CS-25 the landing reference speed VREF may not be less than:
90 - Regarding take-off, the take-off decision speed V1?
91 - The approach climb requirement has been established to ensure:
92 - Two identical turbojet aeroplanes (whose specific fuel consumptions are considered to be equal) are at holding speed at the same altitude. The mass of the first aircraft is 130000 kg and its hourly fuel consumption is 4300 kg/h. The mass of the second aircraft is 115000 kg and its hourly fuel consumption is:
93 - In straight horizontal steady flight, at speeds below that for minimum drag:
94 - A jet aeroplane is climbing at a constant IAS and maximum climb thrust, how will the climb angle / the pitch angle change?
95 - Which statement is correct?
96 - Can the length of a stopway be added to the runway length to determine the take-off distance available?
97 - The determination of the maximum mass on brake release, of a certified turbojet aeroplane with 5°, 15° and 25° flap angles on take-off, leads to the following values: Flap angle: 5° 15° 25°; Runway limitation (kg): 66000 69500 71500; 2nd segment climb limitation: 72200 69000 61800; Wind correction: Headwind: +120 kg / KT Tailwind: -360 kg / KT; Given that the tailwind component is equal to 5 KT, the maximum mass on brake release and corresponding flap angle will be:
98 - On a long distance flight the gross mass decreases continuously as a consequence of the fuel consumption. The result is:
99 - Long range cruise is a flight procedure which gives:
100 - When determining the maximum landing mass of a turbojet powered aeroplane during the planning phase what factor must be used on the landing distance available (dry runway)
101 - On a reciprocating engine aeroplane, with increasing altitude at constant gross mass, angle of attack and configuration the power required:
102 - The maximum speed in horizontal flight occurs when:
103 - Which of the alternatives represents the correct relationship?
104 - A twin engine aeroplane in cruise flight with one engine inoperative has to fly over high ground. In order to maintain the highest possible altitude the pilot should choose:
105 - In case of an engine failure recognized below V1:
106 - An aeroplane carries out a descent from FL 410 to FL 270 at cruise Mach number, and from FL 270 to FL 100 at the IAS reached at FL 270. How does the angle of descent change in the first and in the second part of the descent? Assume idle thrust and clean configuration and ignore compressibility effects.
107 - At a constant Mach number the thrust and the fuel flow of a jet engine
108 - Which of the following three speeds of a jet aeroplane are basically identical? The speeds for:
109 - Below the optimum cruise altitude:
110 - The point at which a tangent out of the origin touches the power required curve
111 - Take-off performance data, for the ambient conditions, show the following limitations with flap 10° selected: - runway limit: 5270 kg - obstacle limit: 4630 kg. Estimated take-off mass is 5000 kg. Considering a take-off with flaps at:
112 - The speed V1 is defined as:
113 - A headwind component increasing with altitude, as compared to zero wind condition, (assuming IAS is constant):
114 - With regard to the drift down performance of the twin jet aeroplane, why does the curve representing 35000 kg gross mass in the chart for drift down net profiles start at approximately 4 minutes at FL370?
115 - The tangent from the origin to the power required against true airspeed curve, for a jet aeroplane, determines the speed for:
116 - In the event of engine failure below V1, the first action to be taken by the pilot in order to decelerate the aeroplane is to:
117 - With a true airspeed of 194 KT and a vertical speed of 1000 fpm, the climb gradient is about:
118 - Which data can be extracted from the Buffet Onset Boundary Chart?
119 - With regard to the drift down performance of the twin jet aeroplane, what is meant by 'equivalent gross weight at engine failure'?
120 - Which statement related to a take-off from a wet runway is correct?
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