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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 - V1 has to be:
2 - A climb gradient required is 3.3%. For an aircraft maintaining 100 KT true airspeed, no wind, this climb gradient corresponds to a rate of climb of approximately:
3 - Which take-off speed is affected by the presence or absence of stopway and / or clearway?
4 - If the take-off mass of an aeroplane is brake energy limited a higher uphill slope would:
5 - Long range cruise is selected as
6 - The speed V2 is:
7 - Maximum Tyre Speed can limit the Lift-off Speed.Which kind of speed can be directly used to determine this limitation?
8 - What is the result of a large take off flap setting compared to a small take off flap setting on required Take-off Distance (TOD) and the field length limited Take-off Mass (TOM)?
9 - 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?
10 - The maximum indicated air speed of a piston engine aeroplane without turbo charger, in level flight, is reached:
11 - The take-off distance available is:
12 - The centre of gravity near, but still within, the aft limit:
13 - With all engines out, a pilot wants to fly for maximum time. Therefore he has to fly the speed corresponding to:
14 - In accordance to CS 25 which of the following listed speeds are used for determination of V2min:
15 - Below the optimum cruise altitude:
16 - If the take-off mass of an aeroplane is tyre speed limited, downhill slope would:
17 - During certification test flights for a turbojet aeroplane, the actual measured take-off runs from brake release to a point equidistant between the point at which VLOF is reached and the point at which the aeroplane is 35' above the take-off surface are:- 1747 m, all engines operating- 1950 m, with the critical engine failure recognized at V1, the other factors remaining unchanged.Considering both possibilities to determine the take-off run (TOR). What is the correct distance?
18 - Which of the following statements with regard to the actual acceleration height at the beginning of the 3rd climb segment is correct?
19 - Other factors remaining constant, how does increasing altitude affect Vx and Vy in terms of TAS?
20 - What is the influence of the mass on maximum rate of climb (ROC) speed if all other parameters remain constant?
21 - 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?
22 - If the thrust available exceeds the thrust required for level flight
23 - Any acceleration in climb, with a constant power setting:
24 - Which of the following combinations adversely affects take-off and initial climb performance?
25 - Can the length of a stopway be added to the runway length to determine the takeoff distance available?
26 - The landing field length required for jet aeroplanes at the alternate (wet condition) is the demonstrated landing distance plus
27 - When determining the maximum landing mass of an turbojet powered aeroplane during the planning phase what factor must be used on the landing distance available (dry runway)
28 - The speed V1 is defined as:
29 - Considering VR, which statement is correct?
30 - When compared to still air conditions, a constant headwind component:
31 - Which statement regarding V1 is correct?
32 - Which of the following sets of factors will increase the climb-limited TOM (every factor considered independently)?
33 - According to CS 25 the landing reference speed VREF may not be less than:
34 - In straight horizontal steady flight, at speeds below that for minimum drag:
35 - The length of a clearway may be included in:
36 - The maximum operating altitude for a certain aeroplane with a pressurised cabin
37 - The force exactly opposing and balance lift in a glide descent is:
38 - Which combination of circumstances or conditions would most likely lead to a tyre speed limited take-off?
39 - The optimum altitude:
40 - During a glide at constant Mach number, the pitch angle of the aeroplane will:
41 - Which of the following provides maximum obstacle clearance during climb?
42 - 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.
43 - 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:
44 - The maximum rate of climb that can be maintained at the absolute ceiling is:
45 - With regard to the graph for the light twin aeroplane, will the accelerate and stop distance be achieved in a take-off where the brakes are released before take-off power is set?
46 - Density altitude is the:
47 - 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:
48 - The take-off safety speed V2 for two-engine or three-engine turbo propeller powered aeroplanes may not be less than:
49 - Regarding the obstacle limited take-off mass, which of the following statements is correct?
50 - What will be the effect on an aeroplane's performance if aerodrome pressure altitude is decreased?
51 - Which of the following statements is applicable to the acceleration height at the beginning of the 3rd climb segment?
52 - Which data can be extracted from the Buffet Onset Boundary Chart?
53 - Which statement about reduced thrust is correct?
54 - Which statement is correct for a descent without engine thrust at maximum lift to drag ratio speed?
55 - A higher pressure altitude at ISA temperature:
56 - With regard to an unaccelerated horizontal flight, which of the following statements is correct?(no compressibility effects)
57 - According to PART-CAT, for turbo-prop aeroplanes, the required runway length at a destination airport is:
58 - A higher outside air temperature (OAT):
59 - VX is:
60 - A 'Balanced Field Length' is said to exist where:
61 - Is there any difference between the vertical speed versus forward speed curves for two identical aeroplanes having different masses ? (assume zero thrust and wind)
62 - The minimum climb gradient required on the 2nd flight path segment after the take-off of a jet aeroplane is defined by the following parameters:1 Gear up2 Gear down3 Wing flaps retracted4 Wing flaps in take-off position 5 N engines at the take-off thrust6 (N- 1) engines at the take-off thrust7 Speed over the path equal to V2 + 10 kt 8 Speed over the path equal to 1.3 VS9 Speed over the path equal to V210 At a height of 35 ft above the runway The correct statements are:
63 - The optimum long-range cruise altitude for a turbojet aeroplane:
64 - Uphill slope:
65 - The approach climb requirement has been established so that the aeroplane will achieve:
66 - An aircraft has two certified landing flaps positions, 25° and 35°. If a pilot chooses 35° instead of 25°, the aircraft will have:
67 - Field length is balanced when:
68 - Refer to CAP698 Section 3 - MEP1 Figure 3.1 Normal Procedure Given:OAT 24 °CPressure Altitude: 3000 ft RWY 30RWind· 060/04 KTTake-off Mass: 3800 lbsOther conditions as associated in the header of the graph. What is the Ground Roll Distance under the conditions given?
question perf3.webp
69 - Why are 'step climbs' used on long distance flights ?
70 - 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?
71 - At reference or use or Performance Manual MEP 1 Figure 3.2 Given:OAT: 25°CPressure Altitude: 3000 ft RWY: 24LWind: 310°/20ktsTake off Mass: 4400 lbs Heavy Duty Brakes installed.Other conditions as associated in the header of the graph.What is the Accelerate and Stop Distance under the conditions given?
72 - Which of the following are to be taken into account for the runway in use for take-off?
73 - With zero wind, the angle of attack for maximum range for an aeroplane with turbojet engines is:
74 - A jet aeroplane is climbing at a constant IAS and maximum climb thrust, how will the climb angle / the pitch angle change?
75 - If a flight is performed with a higher 'Cost Index' at a given mass which of the following will occur?
76 - The landing reference speed VREF has, in accordance with CS 25, the following margins above reference stall speed in landing configuration:
77 - The angle of climb with flaps extended, compared to that with flaps retracted, will normally be:
78 - On a dry runway the accelerate stop distance is increased:
79 - The net flight path gradient after take-off compared to the actual climb gradient is:
80 - Refer to CAP698 Section 3 - MEP1 Figure 3.1 Normal Procedure Given:OAT -15 °CPressure Altitude: 4000' RWY 12RWind· 080/12 KTTake-off Mass: 4000 lbs Runway Surface: tarred and dryWhat is the minimum runway length? No stopway or clearway is available.
question perf2.webp
81 - The tangent from the origin to the power required against true airspeed curve, for a jet aeroplane, determines the speed for:
82 - Which of the following will decrease V1?
83 - During climb to the cruising level, a headwind component:
84 - Density Altitude:
85 - Which of the following factors leads to the maximum flight time of a glide?
86 - An increase in atmospheric pressure has, among other things, the following consequences on take-off performance:
87 - The maximum mass for landing could be limited by
88 - The take-off runway performance requirements for transport category aeroplanes are based upon:
89 - A constant headwind:
90 - The long range cruise speed is in relation to the speed for maximum range cruise.
91 - 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/s 2)
92 - At a given mass, the reference stall speed of a twin engine turboprop aircraft is 100 KT in the landing configuration. The minimum speed a pilot must maintain in short final is:
93 - If the aircraft mass, in a horizontal unaccelerated flight, decreases:
94 - For a jet aeroplane, the maximum climb angle is achieved at a speed corresponding to:
95 - At a constant Mach number the thrust and the fuel flow of a jet engine
96 - Which of the following answers is true?
97 - The point at which a tangent out of the origin touches the power required curve
98 - A runway is contaminated by a 0.5 cm layer of wet snow. The take-off is nevertheless authorized by a light-twin's flight manual.The take-off distance in relation to a dry runway will be:
99 - If the climb speed schedule is changed from 280/.74 to 290/.74 the new crossover altitude will be:
100 - The climb gradient of an aircraft after take-off is 6% in standard atmosphere, no wind, at 0' pressure altitude.Using the following corrections:'± 0.2 % / 1000' field elevation''± 0.1 % / °C from standard temperature' '- 1 % with wing anti-ice''- 0.5% with engine anti-ice'The climb gradient after take-off from an airport situated at 1000', 17°C
101 - At reference or use Performance Manual MEP 1 Figure 3.2 Given:OAT: -10°CPressure Altitude: 4000' RWY: 30LWind: 180°/10 KTTake off Mass: 4600 lbs Heavy Duty Brakes installedOther conditions as associated in the header of the graph.What is the Accelerate and Stop Distance under the conditions given?
question perf8.webp
102 - The 'maximum tyre speed' limits:
103 - In which of the following distances can the length of a stopway be included?
104 - Which statement is correct?
105 - A jet aeroplane is climbing with constant IAS. Which operational speed limit is most likely to be reached?
106 - What is the equation for the climb gradient expressed in percentage during unaccelerated flight (applicable to small angles only)?
107 - With regard to the drift down performance of the twin jet aeroplane, what is meant by 'equivalent gross weight at engine failure'?
108 - If there is a tail wind, the climb limited TOM will:
109 - In relation to the net take-off flight path, the required 35 ft vertical distance to clear all obstacles is:
110 - The lowest point of the thrust required curve of a jet aeroplane is the point for:
111 - Which of the following factors determines the maximum flight altitude in the 'Buffet Onset Boundary' graph?
112 - After engine failure the aeroplane is unable to maintain its cruising altitude. What is the procedure which should be followed?
113 - Which statement with respect to the step climb is correct?
114 - According to PART-CAT, which one of the following statements concerning the landing distance for a turbojet aeroplane is correct?
115 - If other factors are unchanged, the fuel mileage (nautical miles per kg) is:
116 - The maximum speed in horizontal flight occurs when:
117 - Regarding take-off, the take-off decision speed V1:
118 - The drift down procedure specifies requirements concerning the:
119 - The approach climb requirement has been established to ensure:
120 - A head wind will:
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