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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 - 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:
2 - Refer to the Student Pilot Route Manual - VFR Chart ED-4Flying 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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3 - 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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4 - 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)
5 - Given the following: D = flight distanceX = distance to Point of Equal Time GSo = groundspeed outGSr = groundspeed return The correct formula to find distance to Point of Equal Time is:
6 - Refer to the Student Pilot Route Manual: E LO 2An 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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7 - Refer to Figure 4.7.3 Given:Diversion distance 720NM Tail wind component 25ktMass at point of diversion 55000kg Temperature ISADiversion fuel available 4250kgWhat is the minimum pressure altitude at which the above conditions may be met ?
8 - In the ATC flight plan Item 15 (Cruising speed), when not expressed as a Mach number, cruising speed is expressed as:
9 - 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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10 - In an ATC flight plan, Item 15 (route), a cruising pressure altitude of 32000 feet would be entered as:
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11 - A public transport aeroplane with reciprocating engines, the final reserve should be:
12 - Refer to the Student Pilot Route Manual - North Atlantic Plotting Chart.On a direct great circle course from Shannon (5243N 00853W) to Gander (4854N 05432W), the(a) average true course, and(b) distance, are:
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13 - Given:Distance from departure to destination: 330 NM Endurance: 5 hTrue Track:170 W/V: 140/25TAS: 125 kt What is the distance of the PSR from the departure point?
14 - 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°CFind the time, fuel and still air distance to climb.
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15 - Refer to the Jeppesen General Student Pilot Route Manual - VFR Chart ED-4Flying 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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16 - Refer to the General Student Pilot Route Manual - VFR Chart ED-4 Give the frequency of STUTTGART ATIS.
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17 - Find: Air distance in Nautical Air Miles (NAM) for this leg and fuel consumptionGiven: 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.
18 - Refer to JAR Student Pilot Route Manual, Paris, Charles-de-Gaulle (Plate 20- 2): The route distance from CHIEVRES (CIV) to BOURSONNE (BSN) is:
19 - 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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20 - 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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21 - 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)
22 - Given:Distance from departure to destination 2800 NM True track 140W/V 140/100TAS 500 k What is the distance and time of the PET from the departure point?
23 - In the ATC flight plan Item 15, a cruising speed of 470 knots will be entered as:
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24 - Given: Maximum allowable take-off mass 64400 kg, Maximum landing mass 56200 kg, Maximum zero fuel mass 53000 kg, Dry operating mass 35500 kg, Traffic load 14500 kg, Trip fuel 4900 kg, Take-off fuel 7400 kgFind: Maximum additional load
25 - 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 IS
26 - 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.
27 - If your destination airport has no ICAO indicator, in the appropriate box of your ATC flight plan, you write:
28 - Given:Distance from departure to destination: 950 NM Endurance: 3,5 hTAS: 360 ktGround Speed Out: 320 kt Ground Speed Home: 400 ktWhat is the distance and time of the PSR from the departure point?
29 - Given:Distance from departure to destination: 180 NM Endurance: 2 hTAS: 120 ktGround Speed Out: 135 kt Ground Speed Home: 105 ktWhat is the distance and time of the PSR from the departure point?
30 - See Flight Planning Manual MRJT 1 Figure 4.5.2 and 4.5.3.4 Given:Distance B - C: 350 NM Cruise 300 KIAS at FL 210 Temperature: - 40°C Tailwind component:70 kt Gross mass at B: 53 200 kgThe fuel required from B - C is:
31 - For a planned flight the calculated fuel is as follows: Flight time: 3h06minThe reserve fuel, at any time, should not be less than 30% of the remaining trip fuel. Taxi fuel: 8 kgBlock fuel: 118 kgHow much fuel should remain after 2 hours flight time?
32 - The planned flight is over a distance of 440 NMBased on the wind charts at altitude the following components are found: FL50: -30kt FL100: -50kt FL180: -70ktThe 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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33 - 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:
34 - Following in-flight depressurisation, a turbine powered aeroplane is forced to divert to anen-route alternate airfield. If actual flight conditions are as forecast, the minimum quantity of fuel remaining on arrival at the airfield will be:
35 - Refer to Student Pilot Route Manual Amsterdam, Schipol (Plate 10- 3):Which of the following statements is correct for ANDIK departures from runway 19L?
36 - An aeroplane has the following masses: ESTLWT= 50 000 kgTrip fuel= 4 300 kg Contingency fuel= 215 kgAlternate fuel (final reserve included)= 2 100kg Taxi= 500 kgBlock fuel= 7 115 kgBefore departure the captain orders to make the block fuel 9 000 kg. The trip fuel in the operational flight plan should read:
37 - Refer to CAP 697 Section 4 MRJT1 Figure 4.4Given: 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 ftFind: Final reserve fuel and corresponding time
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38 - Refer to CAP697 Section 4 - MRJT1 Page 17 Figure 4.4 Holding Fuel Flow - Flaps RetractedThe final reserve fuel taken from the HOLDING PLANNING table for the twin jet aeroplane is based on the following parameters:
39 - What is the the worst hazard, if any, that could be associated with the type of feature at 38°N 015°E ?
40 - In the ATC flight plan item 15, when entering a route for which standard departure (SID) and standard arrival (STAR) procedures exist:
41 - In the ATC flight plan item 7, for a radio equipped aircraft, the identifier must always:
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42 - Given:Dry operating mass (DOM)= 33510 kg Traffic Load= 7600 kgFinal reserve fuel= 983 kg Alternate fuel= 1100 kg Contingency fuel 102 kgThe estimated landing mass at alternate should be:
43 - Which navigation aid is located in position 48°55'N, 009°20'E ?
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44 - Given: FL 330 long range cruiseOAT -63°Cgross mass 50 500 kg. Find: true airspeed (TAS)
45 - Given:Dry operating mass (DOM)= 33000 kg Traffic Load= 8110 kgFinal reserve fuel= 983 kg Alternate fuel= 1100 kg Contingency fuel 102 kgThe estimated landing mass at alternate should be:
46 - VFR flights shall not be flown over the congested areas of cities at a height less than
47 - 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)
48 - Refer to CAP697 Section 4 - 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'
49 - Given:Distance from departure to destination 1860 NM GS Out 360 KTGS Home 400 KTWhat is the time of the PET from the departure point?
50 - In an ATC flight plan Item 15, in order to define a position as a bearing and distance from a VOR, the group of figures should consist of:
51 - Item 9 of the ATC flight plan includes 'NUMBER AND TYPE OF AIRCRAFT'. In this case 'NUMBER' means:
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52 - 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.
53 - 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)?
54 - You are to determine the maximum fuel load which can be carried in the following conditions: - dry operating mass : 2800 kg- trip fuel : 300 kg- traffic load : 400 kg- maximum take-off mass : 4200 kg- maximum landing mass : 3700 kg
55 - The W/V (°/kt) at 60° N015° W is
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56 - For turbojet engine driven aeroplane, given: Taxi fuel 600 kgFuel flow for cruise 10000 kg/h Fuel flow for holding 8000 kg/h Alternate fuel 10200 kgPlanned flight time to destination 6 h Forecast visibility at destination 2000 m The minimum ramp fuel required is:
57 - 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?
58 - In the vicinity of SHANNON (52° N009°W) the tropopause is at about FL
59 - 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:
60 - 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:
61 - 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?
62 - 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.
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63 - 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 ktFL 270 - M = 0.76 Ts = -43°C HWC = 0 The flight level allowing the highest ground speed is:
64 - Refer to the General Student Pilot Route Manual - VFR Chart ED-4Flying 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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65 - Refer to the General Student Pilot Route Manual - VFR Chart ED-4 Give the frequency of ZURICH VOLMET.
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66 - 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:
67 - Given:Distance from departure to destination 95 NM True track 105W/V 060/15TAS 140 kt What is the distance of the PET from the departure point?
68 - The maximum wind velocity (°/kt) shown in the vicinity of MUNICH (48°N 012°E) is:
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69 - 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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70 - What is the temperature deviation (°C) from ISA over 50° N 010°E ?
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71 - In the ATC flight plan Item 19, emergency and survival equipment carried on the flight should be indicated by:
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72 - Given:Distance from departure to destination: 3750 NM Endurance: 9,5 hTrue Track: 360 W/V: 360/50TAS: 480 kt What is the distance of the PSR from the departure point?
73 - 'Integrated range' curves or tables are presented in the Aeroplane Operations Manuals. Their purpose is
74 - 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
75 - General Student Pilot Route Manual - VFR Chart ED-4Flying from Position SIGMARINGEN (48°05'N, 009°13'E) to BIBERACH airport (48°07'N, 009°46'E). Find magnetic course and the distance.
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76 - An aircraft flies at a TAS of 380 kt. It flies from A to B and back to
77 - Given:Distance from departure to destination 150 NM True track 142W/V 200/15TAS 132 kt What is the distance of the PET from the departure point?
78 - Refer to the Student Pilot Route Manual - E HI 2An 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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79 - Refer to CAP697 Section 4 - MRJT1 Figures 4.5.2 and 4.5.3.4 Given: Distance C - D: 540 NMCruise 300 KIAS at FL 210 Temperature Deviation from ISA: +20°C Headwind component: 50 ktGross mass at C: 60 000 kgThe fuel required from C to D is:
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80 - Given:Dry operating mass (DOM)= 33510 kg Traffic Load= 7600 kgTrip fuel (TF)= 2040 kg Final reserve fuel= 983 kg Alternate fuel= 1100 kgContingency fuel= 5% of trip fuelWhich of the listed estimated masses is correct?
81 - Given:Distance from departure to destination 1950 NM GS Out 400 ktGS Home 300 kt What is the time of the PET from the departure point?
82 - 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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83 - From which of the following would you expect to find facilitation information regarding customs and health formalities ?
84 - Refer to the Jeppesen General Student Pilot Route Manual - VFR Chart ED-4An 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.
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85 - Given:Distance from departure to destination: 210 NM Endurance: 2,5 hTrue Track: 035 W/V: 250/20TAS: 105 kt What is the distance of the PSR from the departure point?
86 - 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 ?
87 - True Air speed: 170 ktWind 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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88 - 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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89 - The final reserve fuel for aeroplanes with turbine engines is
90 - 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:
91 - 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 kts and a rate of descent of 800 ft/min. The distance from the VORTAC when descent is started is:
92 - 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?
93 - 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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94 - 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?
95 - The required time for final reserve fuel for turbojet aeroplane is:
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 - Refer to the Student Pilot Route Manual - VFR Chart ED-4Flying 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' clear of obstacles.
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98 - Given:X = Distance A to point of equal time (PET) between A and B E = EnduranceD = Distance A to B O = Groundspeed 'on'H = Groundspeed 'back'The formula for calculating the distance X to point of equal time (PET) is:
99 - Given:Distance from departure to destination 338 NM True track 045W/V 225/35TAS 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?
100 - The planned departure time from the parking area is 1815 UTC The estimated take-off time is 1825 UTCThe flight plan must be filed with ATC at the latest at:
101 - 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:
102 - 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' clear of obstacles.
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103 - Refer to the General Student Pilot Route Manual - VFR Chart ED-4Flying 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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104 - The ILS frequency and identifier for RWY 26R are:
105 - 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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106 - Find the OPTIMUM ALTITUDE for the twin jet aeroplane. Given: Cruise mass=50000 kg, .78 MACH
107 - Refer to 5AT(HI):On airway PTS P from Vigra (62°334N 006°02'E), the initial great circle grid course is:
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108 - Given:Distance from departure to destination 2800 NM True track 140W/V 140/100TAS 500 kt What is the distance and time of the PET from the departure point?
109 - Refer to CAP697 Section 4 - MRJT1 Page 19 Figure 4.5.1 En-route Climb 280/0.74 Given: brake release mass 57500 kgtemperature ISA -10°C head wind component 16 KT initial FL 280Find: still air distance (NAM) and ground distance (NGM) for the climb
110 - When completing an ATC flight plan for a European destination, clock times are to be expressed in:
111 - Which of the following statements regarding filing a ATC flight plan is correct?
112 - A 'current flight plan' is a:
113 - 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 ?
114 - Which of the following statements is (are) correct with regard to computer flight plans1. 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.
115 - How many feet you have to climb to reach FL 75?Given: FL 75 departure aerodrome elevation 1500'QNH = 1023 hPatemperature = ISA1 hPa = 30'
116 - The following fuel consumption figures are given for a jet aeroplane:-standard taxi fuel: 600 kg.-average cruise consumption: 10 000 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: 10 200 kg. The minimum ramp fuel load is:
117 - 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?
118 - Given:Distance from departure to destination 140 NM GS Out 90 ktGS Home 80 kt What is the distance of the PET from the departure point?
119 - 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?
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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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