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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 - 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:
2 - 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.
3 - 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?
4 - 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:
5 - 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:
6 - 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.
7 - 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?
8 - 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:
9 - 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?
10 - 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?
11 - 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
12 - 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?
13 - 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:
14 - 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:
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15 - 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?
16 - The ILS frequency and identifier for RWY 26R are:
question 033-11064A.webp
17 - 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?
18 - 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:
19 - 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?
20 - When a pilot fills in an ATC flight plan, he must indicate the wake turbulence category. This category is a function of which mass?
21 - 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:
22 - 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:
23 - 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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24 - Excluding RVSM an appropriate flight level for IFR flight in accordance with semi-circular height rules on a magnetic course of 200° is:
25 - 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:
26 - 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:
27 - The purpose of the decision point procedure is:
28 - 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:
29 - 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?
30 - The maximum wind velocity (°/kt) shown in the vicinity of MUNICH (48°N 012°E) is:
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31 - 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
32 - 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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33 - In the ATC flight plan Item 15, a cruising speed of 470 knots will be entered as:
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34 - 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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35 - 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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36 - 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)
question fig451.webp
37 - From which of the following would you expect to find facilitation information regarding customs and health formalities?
38 - 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?
39 - General Student Pilot Route Manual - VFR Chart ED-4 Flying 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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40 - In an ATC flight plan, Item 15 (route), a cruising pressure altitude of 32000 feet would be entered as:
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41 - What is the temperature deviation (°C) from ISA over 50° N 010°E?
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42 - 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 course line in order to stay 1000 ft clear of obstacles.
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43 - 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:
44 - The final reserve fuel for aeroplanes with turbine engines is
45 - 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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46 - 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
47 - 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:
48 - 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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49 - 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?
50 - 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)
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51 - The required time for final reserve fuel for turbojet aeroplane 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 - VFR flights shall not be flown over the congested areas of cities at a height less than
54 - 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.
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55 - 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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56 - Which of the following statements regarding filing a ATC flight plan is correct?
57 - 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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58 - 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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59 - 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:
60 - 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:
question fp34.webp
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 - 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'
question 451.webp
63 - 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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64 - 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?
65 - 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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66 - What lowest cloud conditions (oktas/ft) are forecast for JOHANNESBURG/JAN SMUTS at 0300 UTC?
question 033-12329A.webp
67 - Refer to the General Student Pilot Route Manual - VFR Chart ED-4. Give the frequency of ZURICH VOLMET.
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68 - 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:
69 - 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 distance.
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70 - 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?
71 - 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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72 - Refer to the General Student Pilot Route Manual - VFR Chart ED-4. Give the frequency of STUTTGART ATIS.
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73 - Refer to Performance Manual 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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74 - 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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75 - 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?
76 - 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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77 - 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:
78 - Refer to Performance Manual MRJT1 Page 19 Figure 4.5.1 En-route Climb 280/0.74 Given: brake release mass 57500 kg temperature ISA -10°C headwind component 16 kt initial FL 280 Find: still-air distance (NAM) and ground distance (NGM) for the climb
question 451.webp
79 - What is the mean temperature deviation (°C) from the ISA over 50°N 010°W?
question 033-11190A.webp
80 - 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?
81 - 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
82 - 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
83 - 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.
question fp6.webp
84 - A commercial air transport aeroplane with reciprocating engines, the final reserve should be:
85 - 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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86 - 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
87 - 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?
88 - 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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89 - 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:
90 - 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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91 - 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
92 - 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:
question fp20.webp
93 - 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?
94 - 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
95 - 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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96 - A 'current flight plan' is a:
97 - 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:
98 - In the ATS flight plan, for a non-scheduled flight which of the following letters should be entered in item 8 (type of flight):
99 - 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?
100 - 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
101 - 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.
102 - The maximum permissible take-off mass of an aircraft for the L wake turbulence category on an ATC flight plan is:
103 - 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:
104 - 'Integrated range' curves or tables are presented in the Aeroplane Operations Manuals. Their purpose is
105 - 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)
106 - 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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107 - 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?
108 - 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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109 - 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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110 - 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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111 - In the vicinity of SHANNON (52° N 009°W) the tropopause is at about FL
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112 - For an ATC flight plan filed before the flight, the indicated time of departure is:
113 - 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?
114 - When completing an ATC flight plan, an elapsed time (Item 16) of 1 hour 55 minutes should be entered as:
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115 - If your destination airport has no ICAO indicator, in the appropriate box of your ATC flight plan, you write:
116 - 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?
117 - 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
118 - 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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119 - Which navigation aid is located in position 48°55'N, 009°20'E?
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120 - 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)?
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