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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 - 'Integrated range' curves or tables are presented in the Aeroplane Operations Manuals. Their purpose is
2 - VFR flights shall not be flown over the congested areas of cities at a height less than
3 - In the ATC flight plan Item 15, a cruising speed of 470 knots will be entered as:
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4 - What is the worst hazard, if any, that could be associated with the type of feature at 38°N 015°E ?
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5 - 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:
6 - Planning an IFR-flight from Paris (Charles de Gaulle) to London (Heathrow) for the twin jet aeroplane. Given: Estimated Take-off Mass (TOM) 52000 kg, Airport elevation 387 ft, FL 280, W/V 280°/40 kt, ISA Deviation -10°C, Average True Course 340° Find: Time to the top of climb (TOC)
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7 - How many feet you have to climb to reach FL 75? Given: FL 75 departure aerodrome elevation 1500' QNH = 1023 hPa temperature = ISA 1 hPa = 30'
8 - Given: Dry operating mass (DOM)= 33000 kg Traffic Load= 8110 kg. Final reserve fuel= 983 kg Alternate fuel= 1100 kg Contingency fuel 102 kg. The estimated landing mass at alternate should be:
9 - 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?
10 - 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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11 - 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:
12 - Refer to the 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 minimum altitude within a corridor 5 NM left and 5 NM right of the courseline in order to stay 1000 ft clear of obstacles.
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13 - Refer to the General Student Pilot Route Manual - VFR Chart ED-4. Which navigation aid is located in position 48°30'N, 007°34'E?
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14 - Refer to JAR Student Pilot Route Manual, Paris, Charles-de-Gaulle (Plate 20-2): The route distance from CHIEVRES (CIV) to BOURSONNE (BSN) is:
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15 - 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:
16 - 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?
17 - 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 courseline in order to stay 1000 ft clear of obstacles.
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18 - 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?
19 - In the ATS flight plan, for a non-scheduled flight which of the following letters should be entered in item 8 (type of flight):
20 - Refer to the General Student Pilot Route Manual - VFR Chart ED-4. Give the frequency of STUTTGART ATIS.
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21 - When a pilot fills in an ATC flight plan, he must indicate the wake turbulence category. This category is a function of which mass?
22 - 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
23 - 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:
24 - What is the mean temperature deviation (°C) from the ISA over 50°N 010°W ?
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25 - 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.
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26 - Refer to CAP697 Section 4 - 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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27 - 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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28 - The fuel plan gives a trip fuel of 65 US gallons. The alternate fuel, final reserve included, is 17 US gallons. Contingency fuel is 5% of the trip fuel. The usable fuel at departure is 93 US gallons. At a certain moment the fuel consumed according to the fuel gauges is 40 US gallons and the distance flown is half of the total distance. Assume that fuel consumption doesn't change. Which statement is right ?
29 - 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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30 - 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.
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31 - Refer to the Student Pilot Route Manual - 5 AT (HI) The initial great circle true course from Keflavik (64°00'N 022°36' W) to Vigra (62°33'N 006°02'E) measures 084°. On a polar enroute chart where the grid is aligned with the 000° meridian the initial grid course will be:
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32 - A flight has to be made with a multi engine piston aeroplane (MEP 1 Fig. 3. 3). For the fuel calculations take 5 US gallons for the taxi, and an additional 13 minutes at cruise condition to account for climb and descent. Calculated time overhead to overhead is 2h37min. Power setting is 65%, 2500 RPM. Calculated reserve fuel is 30% of the trip fuel. FL 120. Temperature 1°C. Find the minimum block fuel.
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33 - What lowest cloud conditions (oktas/ft) are forecast for JOHANNESBURG/JAN SMUTS at 0300 UTC?
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34 - 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:
35 - The final reserve fuel for aeroplanes with turbine engines is
36 - 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:
37 - Refer to the Student Pilot Route Manual: E LO 2 An appropriate flight level for flight on airway B3 from CHATILLON CTL 117.6 (49°08'N 003°35'E) to CAMBRAI CMB 112.6 (50°14'N 003°09'E) is:
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38 - How many hours in advance of EOBT should a ATC flight plan be filed in the case of flights into areas subject to air traffic flow management (ATFM)?
39 - 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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40 - The ILS frequency and identifier for RWY 26R are:
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41 - A public transport aeroplane with reciprocating engines, the final reserve should be:
42 - 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?
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 - Item 9 of the ATC flight plan includes 'NUMBER AND TYPE OF AIRCRAFT'. In this case 'NUMBER' means:
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45 - 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.
46 - 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 ?
47 - Given: FL 330 long range cruise OAT -63°C gross mass 50 500 kg. Find: true airspeed (TAS)
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48 - Refer to the General Student Pilot Route Manual - VFR Chart ED-4. Give the frequency of ZURICH VOLMET.
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49 - 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 distance.
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50 - When an ATC flight plan is submitted for a flight outside designated ATS routes, points included in Item 15 (route) should not normally be at intervals of more than:
51 - Refer to CAP697 Section 4 - MRJT1 Page 19 Figure 4.5.1 En-route Climb 280/0.74 Given: brake release mass 57500 kg temperature ISA -10°C head wind component 16 kt initial FL 280 Find: still air distance (NAM) and ground distance (NGM) for the climb
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52 - Refer to Student Pilot Route Manual Amsterdam, Schipol (Plate 10- 3): Which of the following statements is correct for ANDIK departures from runway 19L?
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53 - Flight planning chart for an aircraft states, that the time to reach the cruising level at a given gross mass is 36 min and the distance travelled is 157 NM (zero-wind). What will be the distance travelled with an average tailwind component of 60 kt?
54 - The required time for final reserve fuel for turbojet aeroplane is:
55 - In the ATC flight plan item 7, for a radio equipped aircraft, the identifier must always:
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56 - 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?
57 - 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:
58 - 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:
59 - 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?
60 - If your destination airport has no ICAO indicator, in the appropriate box of your ATC flight plan, you write:
61 - 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:
62 - 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
63 - 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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64 - For the purposes of Item 9 (Wake turbulence category) of the ATC flight plan, an aircraft with a maximum certificated take-off mass of 62000 kg is:
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65 - 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:
66 - Prior to an IFR flight, when filling in the ATC flight plan, the time information which should be entered in box 16: 'Total estimated time' is the time elapsed from:
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67 - 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?
68 - The planned flight is over a distance of 440 NM. Based on the wind charts at altitude the following components are found: FL50: -30kt, FL100: -50kt, FL180: -70kt. The Operations Manual in appendix details the aircraft's performances. Which of the following flight levels (FL) gives the best range performance:
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69 - 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?
70 - 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:
71 - Refer to CAP697 Section 4 - 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:
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72 - 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?
73 - The lowest cloud conditions (oktas/ft) at BORDEAUX/MERIGNAC at 1330 UTC were
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74 - 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?
75 - 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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76 - 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:
77 - 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.
78 - Refer to CAP697 Section 4 - MRJT1 Page 17 Figure 4.4 Holding Fuel Flow - Flaps Retracted The final reserve fuel taken from the HOLDING PLANNING table for the twin jet aeroplane is based on the following parameters:
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79 - 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)
80 - 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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81 - The W/V (°/kt) at 60° N 015° W is
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82 - 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:
83 - 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:
84 - 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:
85 - Refer to CAP697 Section 4 - 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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86 - 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?
87 - 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?
88 - 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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89 - 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:
90 - 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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91 - 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?
92 - Refer to the Jeppesen 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 distance.
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93 - On an instrument approach chart, a minimum sector altitude (MSA) is defined in relation to a radio navigation facility. Without any particular specification on distance, this altitude is valid to:
94 - Find the OPTIMUM ALTITUDE for the twin jet aeroplane. Given: Cruise mass=50000 kg, .78 Mach
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95 - In the ATC flight plan item 15, when entering a route for which standard departure (SID) and standard arrival (STAR) procedures exist:
96 - Excluding RVSM an appropriate flight level for IFR flight in accordance with semi-circular height rules on a magnetic course of 200° is:
97 - In the vicinity of SHANNON (52° N 009°W) the tropopause is at about FL
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98 - In the ATC flight plan Item 19, emergency and survival equipment carried on the flight should be indicated by:
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99 - 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:
100 - Given: Distance from departure to destination 1950 NM GS Out 400 kt GS Home 300 kt What is the time of the PET from the departure point?
101 - 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?
102 - The maximum permissible take-off mass of an aircraft for the L wake turbulence category on an ATC flight plan is:
103 - Refer to the Student Pilot Route Manual - VFR Chart ED-4 Flying from ERBACH airport (48°21'N, 009°55'E) to POLTRINGEN airport (48°33'N, 008°57'E). Find magnetic course and the distance.
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104 - Refer to CAP697 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:
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105 - Given: X = Distance A to point of equal time (PET) between A and B E = Endurance D = Distance A to B O = Groundspeed 'on' H = Groundspeed 'back'. The formula for calculating the distance X to point of equal time (PET) is:
106 - During a VFR flight at a navigational checkpoint the remaining usable fuel in tanks is 60 US gallons. The reserve fuel is 12 US gallons. According to the flight plan the remaining flight time is 1h35min. Calculate the highest acceptable rate of consumption possible for the rest of the trip.
107 - 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?
108 - What is the temperature deviation (°C) from ISA over 50° N 010°E ?
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109 - The maximum wind velocity (°/kt) shown in the vicinity of MUNICH (48°N 012°E) is:
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110 - When completing an ATC flight plan, an elapsed time (Item 16) of 1 hour 55 minutes should be entered as:
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111 - A 'current flight plan' is a:
112 - For an ATC flight plan filed before the flight, the indicated time of departure is:
113 - 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:
114 - 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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115 - Refer to CAP 697 Section 2 SEP1 Page 3 Figure 2.1 Time, Fuel and Distance to Climb. Given: Take-off mass 3500 lbs, departure aerodrome pressure altitude 2500 ft, OAT +10°C, First cruising level: FL 140, OAT -5°C Find the time, fuel and still air distance to climb.
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116 - Refer to CAP 697 Section 4 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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117 - See TRM, De Kooy Area chart (19- 1) What is the minimum altitude it is permissible to fly over the "Quiet Zone" in the vicinity of DE KOOY?
118 - 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?
119 - 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?
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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