Test 120 exam questions on Flight Planning and Monitoring for ATPL

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1 - 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:

The letters 'DCT' should be entered, followed by the point of joining the ATS route It is not necessary to indicate the point of joining that route as it will be obvious to the ATS unit. The words 'as cleared' should be entered It is necessary only to give the first reporting point on that route

2 - What mean temperature (°C) is likely on a course of 360° (T) from 40°N to 50°N at 040°E ?

-46 -47 -50 -49

3 - An aircraft flies at a TAS of 380 kt. It flies from A to B and back to Distance AB = 480 NM. When going from A to B, it experiences a headwind component = 60 kt. The wind remains constant.The duration of the flight will be: 3h 00 min 2h 10 min 2h 35 min 2h 32 min

4 - How many feet you have to climb to reach FL 75?Given: FL 75 departure aerodrome elevation 1500'QNH = 1023 hPatemperature = ISA1 hPa = 30' 6000' 6300' 7800' 5700'

5 - 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) WCA -2°, GS 396 kt WCA +2°, GS 416 kt WCA -2°, GS 426 kt WCA +2°, GS 396 kt

6 - When completing an ATC flight plan for a European destination, clock times are to be expressed in: Local mean time Local standard time UTC Central European Time

7 - On an ATC flight plan, an aircraft indicated as 'H' for 'Heavy' Is of the highest wake turbulence category Requires a runway length of at least 2 000m at maximum certified take-off mass Has a certified take-off mass greater than or equal to 140 000 kg Has a certified landing mass greater than or equal to 136 000 kg

8 - 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: 10 min 40 sec 20 min 16 min 24 min

9 - 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: VOR ident, true bearing and distance in kilometres VOR ident, magnetic bearing and distance in kilometres VOR ident, magnetic bearing and distance in nautical miles Full name of VOR, true bearing and distance in kilometres

10 - 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? 12 minutes. 4 minutes. 44 minutes. 63 minutes.

11 - 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 ? 242° 224° 262° 280°

12 - When filling in an ATC flight plan before departure, the time information which should be entered in item 13: 'Time' is:

Planned take-off time. Estimated off-block time. The time of flight plan filing. Planned engine start time.

13 - In an ATC flight plan, Item 15 (route), a cruising pressure altitude of 32000 feet would be entered as:

S3200 FL320 32000 F320

14 - 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? 66 NM 124 NM 70 NM 74 NM

15 - When a pilot fills in an ATC flight plan, he must indicate the wake turbulence category. This category is a function of which mass? Estimated take-off mass Maximum certified landing mass Maximum certified take-off mass Actual take-off mass

16 - 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: Laid down by the operator, with the quantity being specified in the operating manual At least equivalent to the quantity required to fly to another aerodrome in the event that weather conditions so require At least equivalent to 45 minutes flying time At least equivalent to 30 minutes flying time

17 - 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? 39 kg trip fuel and 12 kg reserve fuel. 30 kg trip fuel and 9 kg reserve fuel. 39 kg trip fuel and no reserve fuel. 27 kg trip fuel and 12 kg reserve fuel.

18 - 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: 213 kg/h 188 kg/h 200 kg/h 267 kg/h

19 - 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? 13 000 kg 13 230 kg 11 730 kg 14 730 kg

20 - 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:

040° 058° 044° 052°

21 - What is the temperature deviation (°C) from ISA over 50° N 010°E ?

-55 -10 +10 +2

22 - 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.

Magnetic course 093°, distance 42 KM Magnetic course 084°, distance 22 NM Magnetic course 086°, distance 32 NM Magnetic course 267°, distance 22 NM

23 - 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 3 000 kg 5 600 kg 7 000 kg 4 000 kg

24 - Which is the heaviest type of precipitation, if any, forecast for BORDEAUX/MERIGNAC at 1000 UTC ? Rain showers Light rain Nil Heavy rain associated with thunderstorms[see Annex]

25 - 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)? 1:00 hour. 3:00 hours. 2 hours. 0:30 hours.

26 - The lowest cloud conditions (oktas/ft) at BORDEAUX/MERIGNAC at 1330 UTC were 1 to 4 at 3000 3 to 4 at 2000 1 to 2 at 3000 3 to 4 at 800[see Annex]

27 - 'Integrated range' curves or tables are presented in the Aeroplane Operations Manuals. Their purpose is To determine the flight time for a certain leg under consideration of temperature deviations. To determine the fuel consumption for a certain still air distance considering the decreasing fuel flow with decreasing mass. To determine the optimum speed considering the fuel cost as well as the time related cost of the aeroplane. To determine the still air distance for a wind components varying with altitude.

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? Distance: 622 NM Time: 117 min Distance: 328 NM Time: 62 min Distance: 311 NM Time: 52 min Distance: 528 NM Time: 79 min

29 - Item 9 of the ATC flight plan includes 'NUMBER AND TYPE OF AIRCRAFT'. In this case 'NUMBER' means:

The registration number of the aircraft The number of aircraft which will separately be using a repetitive flight plan (RPL) The number of aircraft flying in a group The ICAO type designator number as set out in ICAO Doc 8643

30 - 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? 414 Nautical Air Miles (NAM) 499 Nautical Air Miles (NAM) 511 Nautical Air Miles (NAM) 406 Nautical Air Miles (NAM)

31 - 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.

5500' 6600' 6900' 5300'

32 - The maximum permissible take-off mass of an aircraft for the L wake turbulence category on an ATC flight plan is: 2 700 kg 7 000 kg 10 000 kg 5 700 kg

33 - 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:

Heavy 'H' Light 'L' Medium 'M' Unclassified 'U'

34 - 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? H3 H6 H5 H1

35 - 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: 20 km per hour or 0.1 Mach or more 10 % TAS or 0.05 Mach or more 20 knots or 0.05 Mach or more 5% TAS or 0.01 Mach or more

36 - 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. Statement 2 only Neither statement Statement 1 only Both statements

37 - 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: 79 800 kg 74 800 kg 77 200 kg 77 800 kg

38 - 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:

FL 100 FL 180 Either FL 050 or FL 100 FL 050

39 - 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' 20 min, 1750 kg, 117 Nautical Air Miles (NAM), 288 KT 26 min, 2050 kg, 157 Nautical Air Miles (NAM), 399 KT 25 min, 1875 kg, 148 Nautical Air Miles (NAM), 391 KT 26 min, 1975 kg, 157 Nautical Air Miles (NAM), 399 KT[see Annex]

40 - Refer to the General Student Pilot Route Manual - VFR Chart ED-4 Give the frequency of STUTTGART ATIS.

119.05 MHZ 135.775 MHz 116.12 kHz 126.12 MHz

41 - 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.

4300 ft 1500 ft FL045 3300 ft

42 - When completing Item 9 of the ATC flight plan, if there is no appropriate aircraft designator, the following should be entered:

The most descriptive abbreviation 'XXXX' followed by an entry in Item 18 'NONE' 'ZZZZ' followed by an entry in Item 18

43 - 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.

112.50 MHz 109.20 MHz 112.50 MHz 109.20 MHz 422 kHz 118.80 MHz

44 - 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? 79 NM 134 NM 75 NM 71 NM

45 - Refer to General Student Pilot Route Manual:In the ATC flight plan Item 10, 'standard equipment' is considered to be:

VHF RTF, ADF, VOR and transponder VHF RTF, ADF, VOR and ILS VHF RTF, VOR, INS and transponder VHF RTF, VOR, ILS and transponder

46 - 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

136 kt and 56,9 lbs/hr 134 kt and 55,7 lbs/hr 125 kt and 55,7 lbs/hr 131 kt and 56,9 lbs/hr

47 - 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? 1248 NM 752 NM 624 NM 1040 NM

48 - 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? 13 000 kg 13 230 kg 11 730 kg 14 730 kg

49 - What is the mean temperature deviation (°C) from the ISA over 50°N 010°W ? +9 +2 +13 -2[see Annex]

50 - 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.

24.5 NM 31 NM 36.5 NM 33 NM

51 - Minimum planned take-off fuel is 160 kg (30% total reserve fuel is included). Assume the groundspeed on this trip is constant. When the aircraft has done half the distance the remaining fuel is 70 kg. Is diversion to a nearby alternate necessary? Diversion to a nearby alternate is not necessary, because it is allowed to calculate without reserve fuel. Diversion to a nearby alternate is not necessary, because the reserve fuel has not been used completely. Diversion to a nearby alternate is necessary, unless the captain decides to continue on his own responsibility. Diversion to a nearby alternate is necessary, because the remaining fuel is not sufficient.

52 - 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:

4242 kg 3350 kg 3680 kg 4620 kg

53 - 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:

1 182 litres 1 545 litres 1 600 litres 1 326 litres

54 - From which of the following would you expect to find facilitation information regarding customs and health formalities ? NAV/RAD charts ATCC AIP NOTAM

55 - 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: 563 NM 603 NM 584 NM 608 NM[see Annex]

56 - What lowest cloud conditions (oktas/ft) are forecast for JOHANNESBURG/JAN SMUTS at 0300 UTC? 5 to 7 at 400 3 to 4 at 400 5 to 7 at 800 3 to 4 at 800[see Annex]

57 - 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: 235 l/h 176 l/h 220 l/h 206 l/h

58 - 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? 33 kg trip fuel and 10 kg reserve fuel. 25 kg trip fuel and 8 kg reserve fuel. 33 kg trip fuel and no reserve fuel. 23 kg trip fuel and 10 kg reserve fuel.

59 - 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: 0.76 0.78 Given the distance to go is 570 NM, the reduced MACH No. should be: 0.76 0.78 0.72 0.80

60 - 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:

A) 281° (b) 2730 NM A) 244° (b) 1520 NM A) 262° (b) 1720 NM A) 281° (b) 1877 NM

61 - 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 7000 kg 4000 kg 5600 kg 3000 kg

62 - 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 thatflight to Limoges. The RPL must be cancelled for that day and a specific flight plan has to be filed. The pilot-in-command must advise ATC of his intention to divert to Limoges at least 15 minutes before the planned time of arrival. It is not possible to plan another destination and the flight has to be simply cancelled that day (scheduled flight and not chartered). The airline's 'Operations ' Department has to transmit a change in the RPL at the ATC office, at least half an hour before the planned time of departure.

63 - A 'current flight plan' is a: Filed flight plan. Flight plan with the correct time of departure. Filed flight plan with amendments and clearance included. Flight plan in the course of which radio communication should be practised between aeroplane and AT

64 - 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.

24 min, 7.7 GAL, 47 NAM 16.5 min, 4.9 GAL, 34.5 NAM 23.5 min, 7.1 GAL, 48.5 NAM 23 min, 7.7 GAL, 50 NAM

65 - 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: 1725 UTC 1745 UTC 1715 UTC 1755 UTC

66 - Which of the following statements regarding filing a ATC flight plan is correct? In case of ATFM (Air Traffic Flow Management) the flight plan should be filed at least three hours in advance of the EOBT. A flying college can file repetitive flight plan for VFR flights. A flight plan should be filed when a national FIR boundary will be crossed. Any flight plan should be filed at least 10 minutes before departure.

67 - 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) 7500 ft 12500 ft 10000 ft 11000 ft[see Annex]

68 - Refer to JAR Student Pilot Route Manual, Paris, Charles-de-Gaulle (Plate 20- 2): The route distance from CHIEVRES (CIV) to BOURSONNE (BSN) is: 83 NM 96 NM 73 NM 88 NM[see Annex]

69 - Refer to 5AT(HI):On airway PTS P from Vigra (62°334N 006°02'E), the initial great circle grid course is:

344 350 347 353

70 - In the ATC flight plan item 15, when entering a route for which standard departure (SID) and standard arrival (STAR) procedures exist: SIDs should be entered but not STARs Both should be entered in the ATC plan where appropriate Neither SID nor STAR should be entered STARS should be entered but not SIDs

71 - 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.

91 US gallons 118 US gallons Find the minimum block fuel. 91 US gallons 118 US gallons 76 US gallons 86 US gallons

72 - 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: An estimate may be entered but that number may not subsequently be exceeded The plan should be filed with the relevant box blank The plan may not be filed until the information is available 'TBN' (to be notified) may be entered in the relevant box

73 - 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: 140 150 130 120

74 - 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:

Medium 'M' Heavy/medium 'H/M' Medium plus 'M+' Heavy 'H'

75 - Refer to the General Student Pilot Route Manual - VFR Chart ED-4Give the name and frequency of the Flight Information Service for an aeroplane in position (47°59'N, 010°14'E) at 5000'.

MUNCHEN INFORMATION 126.95 MHz MEMMINGEN INFORMATION 122.1 MHz FRANKFURT INFORMATION 128.95 MHz MUNCHEN INFORMATION 120.65 MHz

76 - 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? 64 NM 88 NM 172 NM 127 NM

77 - 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:

B A C P

78 - 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: 41110 kg. 42195 kg. 42312 kg. 42210 kg.

79 - In the ATC flight plan Item 15, a cruising speed of 470 knots will be entered as:

N0470 N470 0470K KN470

80 - 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: 2h 49min 2h 52min 2h 04min 1h 35min

81 - The maximum wind velocity (°/kt) shown in the vicinity of MUNICH (48°N 012°E) is:

300/100 300/140 290/110 300/160

82 - 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? 223 min 167 min 125 min 29 min

83 - 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? 2070 NM 2255 NM 1495 NM 1128 NM

84 - 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: X = (D/2) x GSo / (GSo + GSr) X = D x GSo / (GSo + GSr) X = (D/2) + GSr / (GSo + GSr) X = D x GSr / (GSo + GSr)

85 - Given:Distance from departure to destination 340 NM True track 320W/V 160/40 TAS 110 ktWhat is the distance of the PET from the departure point? 228 NM 112 NM 219 NM 121 NM

86 - 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: 4135N00415E N4135 E00415 N04135E0415 41°35' N 04° 15'E

87 - 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? Distance: 1400 NM Time: 168 min Distance: 1120 NM Time: 112 min Distance: 1120 NM Time: 134 min Distance: 1680 NM Time: 252 min

88 - 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.

257° 063° 077° 243°

89 - 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 24000', 445 KT 25000', 435 KT 33900', 420 KT 33500', 430 KT[see Annex]

90 - 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: G N/S X Y

91 - 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?

VOR VORTAC VOR/DME NDB

92 - The W/V (°/kt) at 60° N015° W is

320/60 300/70 115/60 300/60

93 - 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? Estimated take-off mass= 45233 kg. Estimated landing mass at destination= 43193 kg. Estimated landing mass at destination= 43295 kg. Estimated take-off mass= 43295 kg.

94 - In the ATC flight plan item 7, for a radio equipped aircraft, the identifier must always:

Include the aircraft registration marking Include the operating agency designator Be the RTF callsign to be used Include an indication of the aircraft type

95 - A public transport aeroplane with reciprocating engines, the final reserve should be: Fuel to fly for 2 hours Fuel to fly for 1 hour at holding speed Fuel to fly for 45 minutes Fuel to fly for 30 minutes at holding speed

96 - 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: X = D x H / (O + H) X = D x O x H / (O + H) X = E x H / (O + H) X = D x O / (O + H)

97 - Given: true course (TC) 017 W/V 340/30 TAS 420 kt Find: wind correction angle (WCA) and ground speed (GS) WCA +2° GS 396 kt WCA -2° GS 426 kt WCA -2° GS 396 kt WCA +2° GS 416 kt

98 - 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: 15,0 NM 27,1 NM 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: 15,0 NM 27,1 NM 30,2 NM 11,7 NM

99 - 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? Distance: 1400 NM Time: 168 min Distance: 1120 NM Time: 112 min Distance: 1120 NM Time: 134 min Distance: 1680 NM Time: 252 min

100 - 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: 6 185 kg. 9 000 kg. 4 300 kg. 6 400 kg.

101 - 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: 110 NM 140 NM 130 NM 120 NM

102 - 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: 20 minutes flying time or 150 km 15 minutes flying time or 100 km 30 minutes flying time or 370 km 1 hour flying time or 500 km

103 - Refer to Student Pilot Route Manual Amsterdam, Schipol (Plate 10- 3):Which of the following statements is correct for ANDIK departures from runway 19L? Contact SCHIPOL DEPARTURE 119.05 passing 2000 ft and report altitude Maximum IAS 250kt turning left at SPL 3.1 DME The distance to ANDIK is 25 NM Cross ANDIK below FL60[see Annex]

104 - 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? 3000ft 3500ft 32800ft 1500ft

105 - 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.

Magnetic course 285°, distance 41 NM Magnetic course 289°, distance 76 KM Magnetic course 287°, distance 60 NM Magnetic course 108°, distance 41 NM

106 - Given:Distance from departure to destination: 210 NM Endurance: 3,5 hTrue Track: 310 W/V: 270/30TAS: 120 kt What is the distance of the PSR from the departure point? 200 NM 10 NM 100 NM 125 NM

107 - 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? 132 min 147 min 163 min 22 min

108 - In the ATC flight plan Item 19, emergency and survival equipment carried on the flight should be indicated by:

Placing a tick in the relevant box Circling the relevant box Listing the items carried on the 'REMARKS' line Crossing out the box relevant to any equipment not carried

109 - 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.

176° 355° 185° 004°

110 - 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.

Magnetic course 282°, distance 112 KM Magnetic course 092°, distance 82 NM Magnetic course 091°, distance 54 NM Magnetic course 078°, distance 82 NM

111 - 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. Both statements Statement 2 only Neither statement Statement 1 only

112 - Given: FL 330 long range cruiseOAT -63°Cgross mass 50 500 kg. Find: true airspeed (TAS) 433 kt 420 kt 418 kt 431 kt[see Annex]

113 - 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? 150kg 140kg 278kg 290kg[see Annex]

114 - 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: 14400 kg 11400 kg 8600 kg 11100 kg

115 - 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.

24 NM 41 km 28 NM 46 NM

116 - 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? Distance: 79 NM Time: 45 min Distance: 118 NM Time: 53 min Distance: 62 NM Time: 28 min Distance: 59 NM Time: 30 min

117 - The required time for final reserve fuel for turbojet aeroplane is: 45 min. 60 min. 30 min. Variable with wind velocity.

118 - 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:

080° 096° 106° 066°

119 - Given: true course (TC) 017 W/V 340/30TAS 420 kt Find: wind correction angle (WCA) and ground speed (GS) WCA +2° GS 396 kt WCA -2° GS 426 kt WCA -2° GS 396 kt WCA +2° GS 416 kt

120 - 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? 128 NM 193 NM 228 NM 157 NM

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Exam simulation Flight Planning and Monitoring ATPL - Airline Transport Pilot license

Exam simulation atpl 120 questions on 120 minutes