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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-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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2 - In the vicinity of SHANNON (52° N009°W) the tropopause is at about FL
3 - 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:
4 - 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?
5 - 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.
6 - When completing an ATC flight plan, an elapsed time (Item 1 6) of 1 hour 55 minutes should be entered as:
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7 - 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:
8 - The ILS frequency and identifier for RWY 26R are:
9 - 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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10 - 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?
11 - 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?
12 - 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.
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 - 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:
15 - 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:
16 - 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:
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' clear of obstacles.
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18 - 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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19 - A public transport aeroplane with reciprocating engines, the final reserve should be:
20 - An aircraft flies at a TAS of 380 kt. It flies from A to B and back to
21 - Refer to JAR Student Pilot Route Manual, Paris, Charles-de-Gaulle (Plate 20- 2): The route distance from CHIEVRES (CIV) to BOURSONNE (BSN) is:
22 - 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
23 - What is the temperature deviation (°C) from ISA over 50° N 010°E ?
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24 - From which of the following would you expect to find facilitation information regarding customs and health formalities ?
25 - The required time for final reserve fuel for turbojet aeroplane is:
26 - For an ATC flight plan filed before the flight, the indicated time of departure is:
27 - 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?
28 - 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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29 - 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?
30 - 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:
31 - When a pilot fills in an ATC flight plan, he must indicate the wake turbulence category. This category is a function of which mass?
32 - 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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33 - 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?
34 - Refer to CAP697 Section 4 - MRJT1 Page 2 Figure 4.1 / 4.2 and Page 41 Figure 4.5.3.2Given: Estimated take-off mass 57000 kg, Ground distance 150 NM, Temperature ISA -10°C, Cruise at 0.74 MachFind: Cruise altitude and expected true air speed
35 - 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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36 - 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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37 - 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)
38 - 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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39 - 'Integrated range' curves or tables are presented in the Aeroplane Operations Manuals. Their purpose is
40 - A 'current flight plan' is a:
41 - 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?
42 - 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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43 - In an ATC flight plan, Item 15 (route), a cruising pressure altitude of 32000 feet would be entered as:
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44 - 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:
45 - 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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46 - In the ATC flight plan item 15, when entering a route for which standard departure (SID) and standard arrival (STAR) procedures exist:
47 - 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:
48 - In the ATC flight plan Item 15, a cruising speed of 470 knots will be entered as:
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49 - For a planned flight the calculated fuel is as follows: Flight time: 2h42minThe reserve fuel, at any time, should not be less than 30% of the remaining trip fuel. Taxi fuel: 9 kgBlock fuel: 136 kgHow much fuel should remain after 2 hours flight time?
50 - Refer to Student Pilot Route Manual Amsterdam, Schipol (Plate 10- 3):Which of the following statements is correct for ANDIK departures from runway 19L?
51 - 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?
52 - 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:
53 - 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:
54 - In the ATC flight plan item 7, for a radio equipped aircraft, the identifier must always:
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55 - Refer to the General Student Pilot Route Manual - VFR Chart ED-4 Give the frequency of ZURICH VOLMET.
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56 - Refer to General Student Pilot Route Manual:In the ATC flight plan Item 10, 'standard equipment' is considered to be:
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57 - The W/V (°/kt) at 60° N015° W is
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58 - In the ATC flight plan Item 19, emergency and survival equipment carried on the flight should be indicated by:
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59 - 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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60 - 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:
61 - 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:
62 - 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?
63 - 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)?
64 - 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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65 - 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?
66 - 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 ?
67 - 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 KTFL 330cruise 0.78 MachISA +20 ° Cestimated landing weight 55000 kg.Find: simplified flight planning to determine estimated trip fuel and trip time.
68 - 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:
69 - Which navigation aid is located in position 48°55'N, 009°20'E ?
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70 - Refer to CAP697 Section 4 - MRJT1 Page 75 Figure 4.7.2 Area of Operation - Diversion Distance One Engine InoperativeUsing 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:
71 - 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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72 - 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 ?
73 - When completing an ATC flight plan for a European destination, clock times are to be expressed in:
74 - What lowest cloud conditions (oktas/ft) are forecast for JOHANNESBURG/JAN SMUTS at 0300 UTC?
75 - 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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76 - 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:
77 - 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?
78 - 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:
79 - Given: FL 330 long range cruiseOAT -63°Cgross mass 50 500 kg. Find: true airspeed (TAS)
80 - The final reserve fuel for aeroplanes with turbine engines is
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 - The purpose of the decision point procedure is:
83 - 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:
84 - Refer to CAP697 MRJT1 Figure 4.5.4 (Descent)A descent is planned at .74/250KIAS from 35000ft to 5000ft. How much fuel will be consumed during this descent?
85 - 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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86 - 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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87 - The maximum permissible take-off mass of an aircraft for the L wake turbulence category on an ATC flight plan is:
88 - The maximum wind velocity (°/kt) shown in the vicinity of MUNICH (48°N 012°E) is:
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89 - In the ATS flight plan, for a non-scheduled flight which of the following letters should be entered in item 8 (type of flight):
90 - Given:Distance from departure to destination: 2000 NM Endurance: 5 hTAS: 500 ktGround Speed Out: 480 kt Ground Speed Home: 520 ktWhat is the distance of the PSR from the departure point?
91 - 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'
92 - Given: Maximum allowable take-off mass 64 400 kg maximum landing mass 56200 kgmaximum zero fuel mass 53 000 kgdry operating mass 35 500 kgestimated load 14 500 kg estimated trip fuel 4 900 kgminimum take-off fuel 7 400 kg.Find: maximum additional load
93 - 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:
94 - 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?
95 - 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?
96 - 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:
97 - Given: maximum allowable take-off mass 64400 kg maximum landing mass 56200 kgmaximum zero fuel mass 53000 kg dry operating mass 35500 kg estimated load 14500 kg estimated trip fuel 4900kg minimum take-off fuel 7400 kgFind the maximum allowable take-off fuel:
98 - Which is the heaviest type of precipitation, if any, forecast for BORDEAUX/MERIGNAC at 1000 UTC ?
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 - 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.
101 - 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 conditionsGiven:OAT: 3°CPressure altitude: 6000 ftPower: Full throttle / 21,0 in/Hg./ 2100 RPM
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102 - 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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103 - 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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104 - 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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105 - 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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106 - The navigation plan reads: Trip fuel: 100 kgFlight time: 1h35min Taxi fuel: 3 kgBlock fuel: 181 kgThe endurance on the ICAO flight plan should read:
107 - 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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108 - Given: true course (TC) 017 W/V 340/30 TAS 420 kt Find: wind correction angle (WCA) and ground speed (GS)
109 - 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:
110 - On an ATC flight plan, an aircraft indicated as 'H' for 'Heavy'
111 - 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:
112 - 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?
113 - If your destination airport has no ICAO indicator, in the appropriate box of your ATC flight plan, you write:
114 - Refer to Student Pilot Route Manual London, Heathrow (Plate 10- 3):Which of the following is a correct Minimum Safe Altitude (MSA) for the Airport?
115 - The lowest cloud conditions (oktas/ft) at BORDEAUX/MERIGNAC at 1330 UTC were
116 - 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?
117 - 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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118 - 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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119 - Given: true course (TC) 017 W/V 340/30TAS 420 kt Find: wind correction angle (WCA) and ground speed (GS)
120 - 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?
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