Test 120 exam questions on Flight Planning and Monitoring for ATPL

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

-55 -10 +10 +2

2 - 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

3 - 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.

4 - 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

5 - The ILS frequency and identifier for RWY 26R are: 108.7 IMSW 108.3 IMNW 108.7 IMNW 108.3 IMSW[see Annex]

6 - The W/V (°/kt) at 60° N015° W is

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

7 - 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?

SVD UH40 PAPER UA9 BAK UB44 SKA SVD UH40 PAPER UA9 BAK UR156 SKA UR1 HIL UV30 BTD UH42 SKA SVD UB45 LAV UR156 SKA

8 - 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. 12 400 kg, 04h 12 min 11 400 kg, 04h 12 min 11 400 kg, 03h 55 min 12 400 kg, 03h 55 min[see Annex]

9 - 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

10 - 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.

11 - VFR flights shall not be flown over the congested areas of cities at a height less than 500 ft above the highest obstacle. 2000 ft above the highest obstacle within a radius of 600 ft from the aircraft. The highest obstacle. 1000 ft above the highest obstacle within a radius of 600 m from the aircraft.

12 - 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. 33.0 US gallons/hour 30.3 US gallons/hour 21.3 US gallons/hour 37.9 US gallons/hour

13 - What is the the worst hazard, if any, that could be associated with the type of feature at 38°N 015°E ? Reduced visibility Severe attenuation in the HF R/T band There is no hazard Engine flame out and windscreen damage[see Annex]

14 - 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)

15 - 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:

172° (G) 194° (G) 353° (G) 177° (G)

16 - 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. 345 NAM 1994 kg 349 NAM 2000 kg The take-off mass is 56000 kg and climb fuel 1100 kg. 345 NAM 1994 kg 349 NAM2000 kg 345 NAM2006 kg 345 NAM 2000 kg[see Annex]

17 - 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 ? 26000ft 16000ft 14500ft 20000ft[see Annex]

18 - '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.

19 - If your destination airport has no ICAO indicator, in the appropriate box of your ATC flight plan, you write: ZZZZ XXXX AAAA ////

20 - 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

21 - 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: FL290 FL270 FL370 FL330

22 - 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.

05 hours 12 minutes 05 hours 23 minutes 04 hours 42 minutes 05 hours 20 minutes

23 - 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]

24 - 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

25 - 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

26 - 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

27 - 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

28 - 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]

29 - 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

30 - 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

31 - 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

32 - 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

33 - 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: EDDM0215 EDDM2H15 In the ATC flight plan Item 16 (destination/EET) should be entered with: EDDM0215 EDDM2H15 EDDM AT 0215 EDDM1415

34 - 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

35 - 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

36 - An aeroplane has the following masses: ESTLWT= 50 000 kgTrip fuel= 4 300 kg Contingency fuel= 215 kgAlternate fuel (final reserve included)= 2 100kg Taxi= 500 kgBlock fuel= 7 115 kgBefore departure the captain orders to make the block fuel 9 000 kg. The trip fuel in the operational flight plan should read: 6 185 kg. 9 000 kg. 4 300 kg. 6 400 kg.

37 - Refer to CAP697 Section 4 - MRJT1 Page 17 Figure 4.4 Holding Fuel Flow - Flaps RetractedThe final reserve fuel taken from the HOLDING PLANNING table for the twin jet aeroplane is based on the following parameters: Pressure altitude, aeroplane mass and flaps up with maximum range speed Pressure altitude, aeroplane mass and flaps down with maximum range speed Pressure altitude, aeroplane mass and flaps down with minimum drag airspeed Pressure altitude, aeroplane mass and flaps up with minimum drag airspeed[see Annex]

38 - 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.

46 NM 58 NM 32 NM 36 NM

39 - 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]

40 - 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? 48 NM 38 NM 41 NM 45 NM

41 - 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

42 - 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°

43 - 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

44 - 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:

FL50 FL80 FL170 FL60

45 - 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

46 - 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? 203 NM 174 NM 193 NM 188 NM

47 - In the ATS flight plan, for a non-scheduled flight which of the following letters should be entered in item 8 (type of flight): N/S G N X

48 - 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

49 - 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

50 - 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

51 - 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

52 - Find the OPTIMUM ALTITUDE for the twin jet aeroplane. Given: Cruise mass=50000 kg, .78 MACH 36700 ft 36200 ft Maximum operating altitude 35500 ft[see Annex]

53 - 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]

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 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

56 - 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

57 - 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

58 - 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

59 - 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]

60 - 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

61 - 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

62 - The final reserve fuel for aeroplanes with turbine engines is Fuel to fly for 30 minutes at holding speed at 1500 ft (450 m) above aerodrome elevation in standard conditions. Fuel to fly for 60 minutes at holding speed at 1500 ft (450 m) above aerodrome elevation in standard conditions. Fuel to fly for 45 minutes at holding speed at 1000 ft (300 m) above aerodrome elevation in standard conditions. Fuel to fly for 45 minutes at holding speed at 1500 ft (450 m) above aerodrome elevation in standard conditions.

63 - Refer to the General Student Pilot Route Manual - VFR Chart ED-4 Give the frequency of ZURICH VOLMET.

127.20 kHz 127.20 MHz 118.10 MHz 128.525 MHz

64 - 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]

65 - 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.

66 - 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.

67 - 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]

68 - 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

69 - 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

70 - 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 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: 810 NM 794 NM 875 NM 735 NM[see Annex]

71 - 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

72 - 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

73 - 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

74 - 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? 194 NM 150 NM 303 NM 30 NM

75 - 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

76 - 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

77 - 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

78 - 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]

79 - 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? West sector 2300 ft within 25 NM East sector 2100 ft within 50 NM West sector 2100 ft within 25 NM East sector 2300 ft within 50 NM[see Annex]

80 - 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'

81 - 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)

82 - 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

83 - 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.

84 - 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

85 - 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

86 - 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

87 - 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

88 - 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

89 - 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) 3 min 11 min 15 min 12 min[see Annex]

90 - 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

91 - 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

92 - 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

93 - 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]

94 - 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? Distance: 218 NM Time: 85 min Distance: 169 NM Time: 85 min Distance: 120 NM Time: 46 min Distance: 185 NM Time: 72 min

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

96 - 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 700 kg 1000 kg 500 kg 800 kg

97 - 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 2 h 59 min 3 h 43 min 2 h 43 min 2 h 51 min

98 - 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

99 - 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

100 - When completing an ATC flight plan, an elapsed time (Item 1 6) of 1 hour 55 minutes should be entered as:

0155 0115 115M 1H55

101 - 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]

102 - 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

103 - Refer to the General Student Pilot Route Manual - VFR Chart ED-4Flying VFR from PEITING (47°48.0'N, 010°55.5'E) to IMMENSTADT (47°33.5'N, 010°13.0'E)determine the magnetic course.

257° 063° 077° 243°

104 - 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: 20 NM 25 NM 10 NM 15 NM

105 - Given:Distance from departure to destination: 400 NM Endurance: 2,5 hTAS: 115 ktGround Speed Out: 130 kt Ground Speed Home: 105 ktWhat is the distance of the PSR from the departure point? 73 NM 179 NM 255 NM 145 NM

106 - 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

107 - 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: 42093 kg. 42195 kg. 42312 kg. 42210 kg.

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

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

109 - 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

110 - 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°

111 - 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.

112 - For an ATC flight plan filed before the flight, the indicated time of departure is: The time at which the flight plan is filed. The estimated off-block time The time overhead the first reporting point after take-off. The time of take-off.

113 - 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?

NDB VOR/DME TACAN VOR

114 - 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

115 - 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.

116 - 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)

117 - 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

118 - 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'

119 - 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: 76100 kg 80500 kg 77800 kg 79200 kg

120 - 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°

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

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