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Exam simulation Flight Planning and Monitoring - ATPL - Airline Transport Pilot license

Exam simulation ATPL Flight Planning and Monitoring 120 questions on 120 minutes

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1 - Refer to the General Student Pilot Route Manual - VFR Chart ED-4: Flying from SAULGAU airport (48°02'N, 009°31'E) to ALTENSTADT airport (47°50'N, 010°53'E). Find magnetic course and the distance.
question fp16.webp
2 - Refer to the General Student Pilot Route Manual - VFR Chart ED-4. Which navigation aid is located in position 48°23'N, 008°39'E?
question fp14.webp
3 - What is the temperature deviation (°C) from ISA over 50° N 010°E?
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4 - According to ICAO rules for the ATC flight plan (Item 9), the wake turbulence category 'H' (Heavy) indicates an aircraft with a maximum certificated take-off mass of:
5 - During climb to cruising level, the zero-wind time is 36 min and the zero-wind distance travelled is 157 NM. What distance will be travelled with an average tailwind component of 60 kt?
6 - When completing Item 9 of the ATC flight plan, if there is no appropriate aircraft designator, the following should be entered:
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7 - Which navigation aid is located in position 48°55'N, 009°20'E?
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8 - Item 9 of the ATC flight plan includes 'NUMBER AND TYPE OF AIRCRAFT'. In this case 'NUMBER' means:
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9 - Given: Distance from departure to destination 1860 NM GS Out 360 kt GS Home 400 kt. What is the time of the PET from the departure point?
10 - Find: Air distance in Nautical Air Miles (NAM) for this leg and fuel consumption. Given: Flight time from top of climb at FL 280 to the enroute point is 48 minutes. Cruise procedure is long range cruise. Temperature is ISA -5°C. The take-off mass is 56000 kg and climb fuel 1100 kg.
question 033-508.webp
11 - Refer to Performance Manual MRJT1 Figures 4.5.2 and 4.5.3.4 Given: Distance C - D: 540 NM Cruise 300 KIAS at FL 210 Temperature Deviation from ISA: +20°C Headwind component: 50 kt Gross mass at C: 60 000 kg. The fuel required from C to D is:
question fp53.webp
12 - Given: Distance from departure to destination: 210 NM Endurance: 3,5 h True Track: 310 W/V: 270/30 TAS: 120 kt What is the distance of the PSR from the departure point?
13 - When completing an ATC flight plan for a European destination, clock times are to be expressed in:
14 - In an ATC flight plan, Item 15 (route), a cruising pressure altitude of 32000 feet would be entered as:
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15 - From which of the following would you expect to find facilitation information regarding customs and health formalities?
16 - Refer to the General Student Pilot Route Manual - VFR Chart ED-4. Flying VFR from VILLINGEN (48°03.5'N, 008°27.0'E) to FREUDENSTADT (48°28.0'N, 008°24.0'E) determine the magnetic course.
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17 - Given: Maximum allowable take-off mass 64.400 kg; maximum landing mass 56.200 kg; maximum zero fuel mass 53.000 kg; dry operating mass 35.500 kg; estimated load 14.500 kg; estimated trip fuel 4.900 kg; minimum take-off fuel 7.400 kg. Find: maximum additional load
18 - In an ATC flight plan Item 15 (route), in terms of latitude and longitude, a significant point at 41°35' north 4°15' east should be entered as:
19 - Given: Dry operating mass (DOM)= 33510 kg Traffic Load= 7600 kg. Trip fuel (TF)= 2040 kg Final reserve fuel= 983 kg Alternate fuel= 1100 kg. Contingency fuel= 5% of trip fuel. Which of the listed estimated masses is correct?
20 - In the ATC flight plan Item 15 (Cruising speed), when not expressed as a Mach number, cruising speed is expressed as:
21 - What is the worst hazard, if any, that could be associated with the type of feature at 38°N 015°E?
question 033-11181A.webp
22 - Given: Distance from departure to destination 2800 NM True track 140 W/V 140/100 TAS 500 kt What is the distance and time of the PET from the departure point?
23 - The planned departure time from the parking area is 1815 UTC. The estimated take-off time is 1825 UTC. The flight plan must be filed with ATC at the latest at:
24 - Given: Distance from departure to destination: 210 NM Endurance: 2,5 h True Track: 035 W/V: 250/20 TAS: 105 kt. What is the distance of the PSR from the departure point?
25 - Refer to Performance Manual MRJT1 Page 21 Figure 4.5.1 En-route Climb 280/0.74 (continued) Find: Time, Fuel, Still-Air Distance and TAS for an enroute climb 280/.74 to FL 350. Given: Brake release mass 64000 kg, ISA +10°C, airport elevation 3000'
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26 - The ILS frequency and identifier for RWY 26R are:
question 033-11064A.webp
27 - A descent is planned from 7500 ft AMSL so as to arrive at 1000 ft AMSL 6 NM from a VORTAC. With a GS of 156 kt and a rate of descent of 800 ft/min. The distance from the VORTAC when descent is started is:
28 - Find the time to the Point of Safe Return (PSR). Given: Maximum useable fuel 15000 kg, Minimum reserve fuel 3500 kg, TAS out 425 kt, Head wind component out 30 kt, TAS return 430 kt, Tailwind component return 20 kt, Average fuel flow 2150 kg/h
29 - Given: Distance from departure to destination 340 NM True track 320 W/V 160/40 TAS 110 kt What is the distance of the PET from the departure point?
30 - Refer to Performance Manual MRJT1 Figure 4.5.4 (Descent) A descent is planned at.74/250KIAS from 35000 ft to 5000 ft. How much fuel will be consumed during this descent?
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31 - Given: Distance from departure to destination: 330 NM Endurance: 5 h True Track: 170 W/V: 140/25 TAS: 125 kt. What is the distance of the PSR from the departure point?
32 - The fuel burn of an aircraft turbine engine is 220 l/h with a fuel density of 0,80. If the density is 0,75, the fuel burn will be:
33 - Excluding RVSM an appropriate flight level for IFR flight in accordance with semi-circular height rules on a magnetic course of 200° is:
34 - Find the SHORT DISTANCE CRUISE ALTITUDE for the twin jet aeroplane. Given: Brake release mass=45000 kg, Temperature=ISA + 20°C, Trip distance=50 Nautical Air Miles (NAM)
question fig4.2.webp
35 - Minimum planned take-off fuel is 160 kg (30% total reserve fuel is included). Assume the groundspeed on this trip is constant. When the aircraft has done half the distance the remaining fuel is 70 kg. Is diversion to a nearby alternate necessary?
36 - Refer to Performance Manual MRJT1 Page 75 Figure 4.7.2 Area of Operation - Diversion Distance One Engine Inoperative Using the above table, in ISA conditions and at a speed of M.70/280KIAS, in an elapsed time of 90 minutes an aircraft with mass at point of diversion 48000 kg could divert a distance of:
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37 - The navigation plan reads: Trip fuel: 100 kg Flight time: 1h35min Taxi fuel: 3 kg Block fuel: 181 kg The endurance on the ICAO flight plan should read:
38 - The maximum permissible take-off mass of an aircraft for the L wake turbulence category on an ATC flight plan is:
39 - An aircraft has a maximum certificated take-off mass of 137000 kg but is operating at take-off mass 135000 kg. In Item 9 of the ATC flight plan its wake turbulence category is:
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40 - Which of the following statements is (are) correct with regard to computer flight plans 1. The computer takes account of bad weather on the route and adds extra fuel. 2. The computer calculates alternate fuel sufficient for a missed approach, climb, cruise, descent and approach and landing at the destination alternate.
41 - For a planned flight the calculated fuel is as follows: Flight time: 3h06min The reserve fuel, at any time, should not be less than 30% of the remaining trip fuel. Taxi fuel: 8 kg Block fuel: 118 kg How much fuel should remain after 2 hours flight time?
42 - Given: Distance from departure to destination: 400 NM Endurance: 2,5 h TAS: 115 kt Ground Speed Out: 130 kt Ground Speed Home: 105 kt What is the distance of the PSR from the departure point?
43 - True Air speed: 170 kt. Wind in the area: 270°/40 kt. According to the attached the navigation log, an aircraft performs a turn overhead BULEN to re-route to ARD via TGJ. The given wind conditions remaining constant. The fuel consumption during the turn is 20 litres. The total fuel consumption at position overhead ARD will be:
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44 - When a pilot fills in an ATC flight plan, he must indicate the wake turbulence category. This category is a function of which mass?
45 - Which of the following statements regarding filing a ATC flight plan is correct?
46 - In the ATC flight plan item 15, it is necessary to enter any point at which a change of cruising speed takes place. For this purpose a 'change of speed' is defined as:
47 - In the ATC flight plan Item 10 (equipment), the letter to indicate the carriage of a serviceable transponder - mode A (4 digits-4096 codes) and mode C, is:
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48 - A minimum sector altitude (MSA) is defined in relation to a radio navigation facility. Unless a different distance is specified, this altitude is valid within:
49 - Find the OPTIMUM ALTITUDE for the twin jet aeroplane. Given: Cruise mass=50000 kg,.78 Mach
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50 - In the ATC flight plan Item 15, a cruising speed of 470 knots will be entered as:
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51 - 'Integrated range' curves or tables are presented in the Aeroplane Operations Manuals. Their purpose is
52 - In the ATC flight plan item 15, when entering a route for which standard departure (SID) and standard arrival (STAR) procedures exist:
53 - In the ATC flight plan Item 15, for a flight along a designated route, where the departure aerodrome is not on or connected to that route:
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54 - Which of the following statements is (are) correct with regard to the advantages of computer flight plans? 1. The computer can file the ATC flight plan. 2. Wind data used by the computer is always more up-to-date than that available to the pilot.
55 - A repetitive flight plan (RPL) is filed for a scheduled flight: Paris-Orly to Angouleme, Paris Orly as alternate. Following heavy snow falls, Angouleme airport will be closed at the expected time of arrival. The airline decides before departure to plan a re-routing of that flight to Limoges.
56 - Given: Distance from departure to destination 150 NM True track 142 W/V 200/15 TAS 132 kt What is the distance of the PET from the departure point?
57 - Refer to Performance Manual SEP1 Figure 2.1 Time, Fuel and Distance to Climb. Given: take-off mass 3 500 lb, departure aerodrome pressure altitude 2 500 ft, OAT +10°C, first cruising level FL 140, OAT -5°C. Find the time, fuel and still-air distance to climb.
question fp52.webp
58 - Given: Distance from departure to destination 140 NM GS Out 90 kt GS Home 80 kt What is the distance of the PET from the departure point?
59 - Refer to the Student Pilot Route Manual, Paris Charles-de-Gaulle (Plate 20-2): The route distance from CHIEVRES (CIV) to BOURSONNE (BSN) is:
question 033-11043A.webp
60 - On a given path, it is possible to choose between four flight levels (FL), each associated with a mandatory flight Mach Number (M). The flight conditions, static air temperature (SAT) and headwind component (HWC) are given below: FL 370 - M = 0.80 Ts = -60°C HWC = -15 kt. FL 330 - M = 0.78 Ts = -60°C HWC= - 5 kt. FL 290 - M = 0.80 Ts = -55°C HWC = -15 kt. FL 270 - M = 0.76 Ts = -43°C HWC = 0. The flight level allowing the highest ground speed is:
61 - Refer to General Student Pilot Route Manual: In the ATC flight plan Item 10, 'standard equipment' is considered to be:
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62 - An aircraft is flying at Mach 0.84 at FL 330. The static air temperature is -48°C and the headwind component 52 kt. At 1338 UTC the controller requests the pilot to cross the meridian of 030W at 1500 UTC. Given the distance to go is 570 NM, the reduced Mach No. should be:
63 - Planning an IFR-flight from Paris to London (Heathrow). Name the identifier and frequency of the initial approach fix (IAF) of the BIG 2A arrival route.
question 033-3301A.webp
64 - An aeroplane has the following masses: ESTLWT= 50.000 kg; Trip fuel= 4.300 kg; Contingency fuel= 215 kg; Alternate fuel (final reserve included)= 2.100 kg Taxi= 500 kg; Block fuel= 7.115 kg; Before departure the captain orders to make the block fuel 9.000 kg. The trip fuel in the operational flight plan should read:
65 - Refer to the General Student Pilot Route Manual - VFR Chart ED-4. An aeroplane is flying VFR and approaching position TANGO VORTAC (48°37'N, 009°16'E) at FL 055 and magnetic course 090°, distance from VORTAC TANGO 20 NM. What is the frequency of the TANGO VORTAC.
question fp1.webp
66 - See Flight planning Manual SEP 1 Figure 2.3 Table 2.3.1. Using the Power Setting Table, for the single engine aeroplane, determine the cruise TAS and fuel flow (lbs/hr) with full throttle and cruise lean mixture in the following conditions. Given: OAT: 3°C; Pressure altitude: 6000 ft; Power: Full throttle / 21,0 in/Hg./ 2100 RPM
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67 - Given: Distance from departure to destination: 3750 NM Endurance: 9,5 h True Track: 360 W/V: 360/50 TAS: 480 kt What is the distance of the PSR from the departure point?
68 - For an ATC flight plan filed before the flight, the indicated time of departure is:
69 - After flying for 16 min at 100 kt TAS with a 20 kt tail wind component, you have to return to the airfield of departure. You will arrive after:
70 - An aircraft flies at a TAS of 380 kt. It flies from A to B and back to distance AB = 480 NM. When going from A to B, it experiences a headwind component = 60 kt. The wind remains constant. The duration of the flight will be:
71 - What mean temperature (°C) is likely on a course of 360° (T) from 40°N to 50°N at 040°E?
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72 - Refer to the General Student Pilot Route Manual - VFR Chart ED-4. Give the name and frequency of the Flight Information Service for an aeroplane in position (47°59'N, 010°14'E) at 5000'.
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73 - Refer to Performance Manual MRJT1 Figure 4.7.2 (One Engine Inop): An aircraft on an extended range operation is required never to be more than 120 minutes from an alternate, based on 1 engine inoperative LRC conditions in ISA. Using the above table and a given mass of 40000 kg at the most critical point, the maximum air distance to the relevant alternate is:
question img472.webp
74 - Which is the heaviest type of precipitation, if any, forecast for BORDEAUX/MERIGNAC at 1000 UTC?
question 033-12335A.webp
75 - Refer to Performance Manual MRJT1 Figure 4.4 Given: twin jet aeroplane, Estimated mass on arrival at the alternate 50000 kg, Estimated mass on arrival at the destination 52525 kg, Alternate elevation MSL, Destination elevation 1500 ft Find: Final reserve fuel and corresponding time
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76 - The maximum wind velocity (°/kt) shown in the vicinity of MUNICH (48°N 012°E) is:
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77 - VFR flights shall not be flown over the congested areas of cities at a height less than
78 - Given: Distance from departure to destination 338 NM True track 045 W/V 225/35 TAS 120 kt What is the distance and time of the PET from the departure point? What is the distance and time of the PET from the departure point?
79 - Refer to the Student Pilot Route Manual - 5 AT (HI) The initial great circle course from position A (80°00'N 170°00'E) to position B (75°00'N 011°E) is 177° (G). The final grid course at position B will be:
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80 - For a planned flight the calculated fuel is as follows: Flight time: 2h42min The reserve fuel, at any time, should not be less than 30% of the remaining trip fuel. Taxi fuel: 9 kg Block fuel: 136 kg How much fuel should remain after 2 hours flight time?
81 - See TRM (VFR), Aberdeen (Dyce) Information Page (19-6). What is the designated departure route when using Runway 23 in bad weather and/or low visibility?
82 - You are flying a constant compass heading of 252°. Variation is 22°E, deviation is 3°W and your INS is showing a drift of 9° right. True track is?
83 - Given: Distance from departure to destination: 2000 NM Endurance: 5 h TAS: 500 kt Ground Speed Out: 480 kt Ground Speed Home: 520 kt. What is the distance of the PSR from the departure point?
84 - Refer to the General Student Pilot Route Manual - VFR Chart ED-4 Flying VFR from PEITING (47°48.0'N, 010°55.5'E) to IMMENSTADT (47°33.5'N, 010°13.0'E) determine the magnetic course.
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85 - Refer to Student Pilot Route Manual Amsterdam, Schiphol (Plate 10- 3): Which of the following statements is correct for ANDIK departures from runway 19L?
question 033-11048A.webp
86 - What is the mean temperature deviation (°C) from the ISA over 50°N 010°W?
question 033-11190A.webp
87 - Given: FL 330 long range cruise OAT -63°C gross mass 50 500 kg. Find: true airspeed (TAS)
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88 - Refer to the Student Pilot Route Manual - PARIS CDG Plate 20-3: Planning an IFR-flight from Paris (Charles de Gaulle) RWY 27 to London. Given: Distance from PARIS Charles-de-Gaulle to top of climb 50 NM Determine the distance from the top of climb (TOC) to ABB 116.6.
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89 - Refer to Performance Manual MRJT1 Page 13 Figure 4.3.3C Simplified Flight Planning - Trip Distances Given: ground distance to destination aerodrome 1600 NM headwind component 50 kt FL 330 cruise 0.78 Mach ISA +20 °C estimated landing weight 55000 kg. Find: simplified flight planning to determine estimated trip fuel and trip time.
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90 - Given: Dry operating mass (DOM)= 33510 kg Traffic Load= 7600 kg. Final reserve fuel= 983 kg Alternate fuel= 1100 kg Contingency fuel 102 kg. The estimated landing mass at alternate should be:
91 - An aircraft plans to depart London at 1000 UTC and arrive at Munich (EDDM) at 1215 UTC. In the ATC flight plan Item 16 (destination/EET) should be entered with:
92 - The required time for final reserve fuel for turbojet aeroplane is:
93 - Given: Distance from departure to destination: 180 NM Endurance: 2 h TAS: 120 kt Ground Speed Out: 135 kt Ground Speed Home: 105 kt. What is the distance and time of the PSR from the departure point?
94 - In the cruise at FL 155 at 260 kt TAS, the pilot plans for a 500 feet/min descent in order to fly overhead MAN VOR at 2000 feet (QNH 1030). TAS will remain constant during descent, wind is negligible, temperature is standard. The pilot must start the descent at a distance from MAN of:
95 - An aircraft, following a 215° true track at variation 3°W, must fly over a 10 600 ft obstacle with a minimum obstacle clearance of 1 500 ft. Knowing the QNH received from an airport close by, which is almost at sea-level, is 1035 and the temperature is ISA -15°C, the minimum flight level will be:
96 - Given: maximum allowable take-off mass 64400 kg maximum landing mass 56200 kg maximum zero fuel mass 53000 kg dry operating mass 35500 kg estimated load 14500 kg estimated trip fuel 4900 kg minimum take-off fuel 7400 kg Find the maximum allowable take-off fuel:
97 - The following fuel consumption figures are given for a jet aeroplane: -standard taxi fuel: 600 kg. -average cruise consumption: 10000 kg/h. -holding fuel consumption at 1500 ft above alternate airfield elevation: 8000 kg/h. -flight time from departure to destination: 6 hours -fuel for diversion to alternate: 10200 kg. The minimum ramp fuel load is:
98 - The true course is 042°. The variation in the area is 6° W and the wind is calm. The deviation card is reproduced in the annex. In order to follow this course, the pilot must fly a compass heading of:
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99 - An aircraft is in cruising flight at FL 095, GS 155 kt. The pilot intends to descend at 500 fpm to arrive overhead the MAN VOR at 2000' (QNH 1030 hPa). The TAS remains constant in the descent, wind is negligible, temperature standard. At which distance from MAN should the pilot commence the descent?
100 - Given: Distance from departure to destination 95 NM True track 105 W/V 060/15 TAS 140 kt What is the distance of the PET from the departure point?
101 - In the vicinity of SHANNON (52° N 009°W) the tropopause is at about FL
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102 - Refer to the Student Pilot Route Manual - E HI 2. An aircraft has to fly on airways from SVEDA (56°10'N 012°34'E) to SKARA (58°23'N 013°15'E). Which of the following is the correct route?
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103 - When completing an ATC flight plan for a flight commencing under IFR but possibly changing to VFR, the letters entered in Item 8 (FLIGHT RULES) would be:
104 - See Flight Planning Manual SEP 1 Figure 2.5. Given: FL 75, Lean mixture, Full throttle, 2300 RPM. Take-off fuel: 444 lbs, Take-off from MSL. Find: Endurance in hours and minutes.
question fp31.webp
105 - Given the following: D = flight distance X = distance to Point of Equal Time GSo = groundspeed out GSr = groundspeed return. The correct formula to find distance to Point of Equal Time is:
106 - What lowest cloud conditions (oktas/ft) are forecast for JOHANNESBURG/JAN SMUTS at 0300 UTC?
question 033-12329A.webp
107 - Refer to Figure 4.7.3 Given: Diversion distance 720 NM Tail wind component 25 kt. Mass at point of diversion 55000 kg Temperature ISA Diversion fuel available 4250 kg. What is the minimum pressure altitude at which the above conditions may be met?
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108 - In the ATC flight plan Item 19, if the number of passengers to be carried is not known when the plan is ready for filing:
109 - Given: Distance from departure to destination: 950 NM Endurance: 3,5 h TAS: 360 kt Ground Speed Out: 320 kt Ground Speed Home: 400 kt. What is the distance and time of the PSR from the departure point?
110 - Refer to the General Student Pilot Route Manual ED-4: Flying VFR from PEITING (47°48.0'N, 010°55.5'E) to IMMENSTADT (47°33.5'N, 010°13.0'E). Determine the minimum altitude within a corridor 5 NM left and 5 NM right of the course line in order to stay 1000 ft clear of obstacles.
question fp7.webp
111 - During a flight the fuel indicators show that the remaining amount of fuel is 100 lbs after 38 minutes. The total amount of fuel at departure was 160 lbs. For the alternate fuel, 30 lbs is necessary. The planned fuel for taxi is 13 lbs. Final reserve fuel is estimated at 50 lbs. If the fuel flow remains the same, how many minutes can be flown to the destination with the remaining fuel?
112 - The Trip Fuel for a jet aeroplane to fly from the departure aerodrome to the destination aerodrome is 5 350 kg. Fuel consumption in holding mode is 6 000 kg/h. The quantity of fuel which is needed to carry out one go-around and land on the alternate airfield is 4 380 kg. The destination aerodrome has a single runway. What is the minimum quantity of fuel which should be on board at take-off?
113 - Refer to 5AT(HI): On airway PTS P from Vigra (62°33'N 006°02'E), the initial great circle grid course is:
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114 - When filling in an ATC flight plan before departure, the time information which should be entered in item 13: 'Time' is:
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115 - Given: True course (TC) 017°, W/V 340°/30 kt, True air speed (TAS) 420 kt Find: Wind correction angle (WCA) and ground speed (GS)
116 - In the ATS flight plan, for a non-scheduled flight which of the following letters should be entered in item 8 (type of flight):
117 - The still-air distance in the climb is 189 Nautical Air Miles (NAM) and time 30 minutes. What ground distance would be covered in a 30 kt head wind?
118 - A sector distance is 450 NM long. The TAS is 460 kt. The wind component is 50 kt tailwind. What is the still-air distance?
119 - Following in-flight depressurisation, a turbine powered aeroplane is forced to divert to an en-route alternate airfield. If actual flight conditions are as forecast, the minimum quantity of fuel remaining on arrival at the airfield will be:
120 - The fuel burn off is 200 kg/h with a relative fuel density of 0.8. If the relative density is 0.75, the fuel burn will be:
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