1 - Which is the heaviest type of precipitation, if any, forecast for BORDEAUX/MERIGNAC at 1000 UTC ?
2 - 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 - The ILS frequency and identifier for RWY 26R are:
4 - VFR flights shall not be flown over the congested areas of cities at a height less than
5 - What lowest cloud conditions (oktas/ft) are forecast for JOHANNESBURG/JAN SMUTS at 0300 UTC?
6 - 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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7 - 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?
8 - 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'
9 - 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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10 - 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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11 - 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:
12 - The lowest cloud conditions (oktas/ft) at BORDEAUX/MERIGNAC at 1330 UTC were
13 - 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:
14 - 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:
15 - 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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16 - 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:
17 - When completing an ATC flight plan for a European destination, clock times are to be expressed in:
18 - In the ATC flight plan Item 15, a cruising speed of 470 knots will be entered as:
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19 - 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)
20 - 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:
21 - 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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22 - 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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23 - 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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24 - 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:
25 - 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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26 - 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)
27 - Refer to the General Student Pilot Route Manual - VFR Chart ED-4 Give the frequency of ZURICH VOLMET.
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28 - Given: true course (TC) 017 W/V 340/30 TAS 420 kt Find: wind correction angle (WCA) and ground speed (GS)
29 - 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'
30 - Item 9 of the ATC flight plan includes 'NUMBER AND TYPE OF AIRCRAFT'. In this case 'NUMBER' means:
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31 - If your destination airport has no ICAO indicator, in the appropriate box of your ATC flight plan, you write:
32 - 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?
33 - Refer to Student Pilot Route Manual Amsterdam, Schipol (Plate 10- 3):Which of the following statements is correct for ANDIK departures from runway 19L?
34 - 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:
35 - 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'.
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36 - 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:
37 - Which of the following statements regarding filing a ATC flight plan is correct?
38 - 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 ?
39 - 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?
40 - In the ATC flight plan item 7, for a radio equipped aircraft, the identifier must always:
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41 - 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.
42 - 'Integrated range' curves or tables are presented in the Aeroplane Operations Manuals. Their purpose is
43 - In the ATC flight plan Item 19, emergency and survival equipment carried on the flight should be indicated by:
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44 - 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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45 - Given: true course (TC) 017 W/V 340/30TAS 420 kt Find: wind correction angle (WCA) and ground speed (GS)
46 - 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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47 - 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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48 - 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.
49 - 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?
50 - 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?
51 - When a pilot fills in an ATC flight plan, he must indicate the wake turbulence category. This category is a function of which mass?
52 - Refer to General Student Pilot Route Manual:In the ATC flight plan Item 10, 'standard equipment' is considered to be:
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53 - 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:
54 - What is the temperature deviation (°C) from ISA over 50° N 010°E ?
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55 - 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?
56 - 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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57 - 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:
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58 - Refer to the General Student Pilot Route Manual - VFR Chart ED-4 Give the frequency of STUTTGART ATIS.
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59 - 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:
60 - 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?
61 - For an ATC flight plan filed before the flight, the indicated time of departure is:
62 - 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)?
63 - 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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64 - 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?
65 - 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?
66 - 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:
67 - 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.
68 - 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:
69 - 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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70 - 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:
71 - 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:
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72 - 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
73 - 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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74 - 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?
75 - 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?
76 - Find the OPTIMUM ALTITUDE for the twin jet aeroplane. Given: Cruise mass=50000 kg, .78 MACH
77 - 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
78 - 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:
79 - 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?
80 - 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?
81 - 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:
82 - In the ATC flight plan item 15, when entering a route for which standard departure (SID) and standard arrival (STAR) procedures exist:
83 - 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?
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:
85 - 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?
86 - 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:
87 - 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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88 - 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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89 - 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 ?
90 - 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:
91 - What is the the worst hazard, if any, that could be associated with the type of feature at 38°N 015°E ?
92 - 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.
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:
94 - 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?
95 - 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)
96 - 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?
97 - 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?
98 - 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:
99 - 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?
100 - 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?
101 - 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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102 - 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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103 - 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?
104 - 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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105 - 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:
106 - 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:
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107 - 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?
108 - 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:
109 - The purpose of the decision point procedure is:
110 - The maximum wind velocity (°/kt) shown in the vicinity of MUNICH (48°N 012°E) is:
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111 - 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:
112 - 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?
113 - How many feet you have to climb to reach FL 75?Given: FL 75 departure aerodrome elevation 1500'QNH = 1023 hPatemperature = ISA1 hPa = 30'
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 - 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?
116 - 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:
117 - 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?
118 - 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
119 - In the vicinity of SHANNON (52° N009°W) the tropopause is at about FL
120 - 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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