1 - 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)
2 - 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:
3 - 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 magnetic course.
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4 - 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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5 - 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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6 - 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:
7 - 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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8 - In the ATC flight plan Item 19, emergency and survival equipment carried on the flight should be indicated by:
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9 - The required time for final reserve fuel for turbojet aeroplane is:
10 - Refer to the General Student Pilot Route Manual - VFR Chart ED-4 Give the frequency of ZURICH VOLMET.
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11 - On an ATC flight plan, an aircraft indicated as 'H' for 'Heavy'
12 - 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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13 - 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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14 - Excluding RVSM an appropriate flight level for IFR flight in accordance with semi-circular height rules on a magnetic course of 200° is:
15 - 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?
16 - 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:
17 - 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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18 - 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 ?
19 - 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
20 - 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?
21 - 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?
22 - 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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23 - A public transport aeroplane with reciprocating engines, the final reserve should be:
24 - In an ATC flight plan, Item 15 (route), a cruising pressure altitude of 32000 feet would be entered as:
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25 - 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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26 - 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 ?
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 - 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?
29 - 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:
30 - 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.
31 - 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:
32 - 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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33 - When completing an ATC flight plan for a European destination, clock times are to be expressed in:
34 - 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 ?
35 - 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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36 - Given: true course (TC) 017 W/V 340/30 TAS 420 kt Find: wind correction angle (WCA) and ground speed (GS)
37 - 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:
38 - 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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39 - 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.
40 - 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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41 - 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:
42 - 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?
43 - 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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44 - For an ATC flight plan filed before the flight, the indicated time of departure is:
45 - 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?
46 - 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?
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 - 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
49 - From which of the following would you expect to find facilitation information regarding customs and health formalities ?
50 - 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)
51 - 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
52 - 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:
53 - 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?
54 - 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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55 - 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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56 - If your destination airport has no ICAO indicator, in the appropriate box of your ATC flight plan, you write:
57 - 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?
58 - 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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59 - How many feet you have to climb to reach FL 75?Given: FL 75 departure aerodrome elevation 1500'QNH = 1023 hPatemperature = ISA1 hPa = 30'
60 - 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?
61 - Refer to JAR Student Pilot Route Manual, Paris, Charles-de-Gaulle (Plate 20- 2): The route distance from CHIEVRES (CIV) to BOURSONNE (BSN) is:
62 - Which of the following statements regarding filing a ATC flight plan is correct?
63 - 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
64 - The maximum wind velocity (°/kt) shown in the vicinity of MUNICH (48°N 012°E) is:
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65 - 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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66 - 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?
67 - Refer to the General Student Pilot Route Manual - VFR Chart ED-4 Give the frequency of STUTTGART ATIS.
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68 - 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:
69 - 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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70 - 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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71 - 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.
72 - VFR flights shall not be flown over the congested areas of cities at a height less than
73 - 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.
74 - 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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75 - 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
76 - 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:
77 - The W/V (°/kt) at 60° N015° W is
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78 - In the ATS flight plan, for a non-scheduled flight which of the following letters should be entered in item 8 (type of flight):
79 - 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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80 - 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:
81 - An aircraft flies at a TAS of 380 kt. It flies from A to B and back to
82 - 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?
83 - The purpose of the decision point procedure is:
84 - 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?
85 - The maximum permissible take-off mass of an aircraft for the L wake turbulence category on an ATC flight plan is:
86 - The ILS frequency and identifier for RWY 26R are:
87 - What is the mean temperature deviation (°C) from the ISA over 50°N 010°W ?
88 - 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:
89 - What is the temperature deviation (°C) from ISA over 50° N 010°E ?
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90 - 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:
91 - 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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92 - 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:
93 - 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?
94 - 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:
95 - In the ATC flight plan Item 15, a cruising speed of 470 knots will be entered as:
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96 - Find the OPTIMUM ALTITUDE for the twin jet aeroplane. Given: Cruise mass=50000 kg, .78 MACH
97 - 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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98 - Given: FL 330 long range cruiseOAT -63°Cgross mass 50 500 kg. Find: true airspeed (TAS)
99 - In the ATC flight plan Item 15 (Cruising speed), when not expressed as a Mach number, cruising speed is expressed as:
100 - 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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101 - 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
102 - 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:
103 - 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
104 - 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:
105 - Which navigation aid is located in position 48°55'N, 009°20'E ?
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106 - 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.
107 - 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:
108 - 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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109 - In the ATC flight plan item 15, when entering a route for which standard departure (SID) and standard arrival (STAR) procedures exist:
110 - 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?
111 - 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'
112 - 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?
113 - 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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114 - 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?
115 - 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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116 - In the ATC flight plan item 7, for a radio equipped aircraft, the identifier must always:
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117 - 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:
118 - 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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119 - 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?
120 - A 'current flight plan' is a: