1. (For this question use annex 033-11215A)
A turbojet aeroplane is flying using the following data:
. optimum flight level, Mach 0.80, mass of 190 000 kg
. temperature: ISA
. tailwind component: 100 kt
The fuel mileage and the fuel consumption per hour are:

2. 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:

3. (For this question use annex 033-9735A,
AERONAUTICAL CHART ICAO 1:500 000 STUTTGART
(NO 47/6) or Route Manual VFR+GPS chart ED-6)
Flying VFR from VILLINGEN (48°03.5'N, 008°27.0'E) to
FREUDENSTADT (48°28.0'N, 008°24.0'E) determine the
distance.

4. (For this question use annex 033-9712A and 033-9712 B
or Route Manual STAR 10-2 and Instrument approach
chart 11-4 ILS/DME Rwy 27R for London (Heathrow))
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.

5. For a planned flight the calculated fuel is as follows:

Flight time: 2h42min
The reserve fuel, at any time, should not be less than
30% of the remaining trip fuel.
Taxi fuel: 9 kg
Block fuel: 136 kg
How much fuel should remain after 2 hours flight time?

6. For a flight plan filed before the flight, the indicated time
of departure is:

7. (For this question use annex 033- 10992A or Route
Manual chart E(HI)4 CAA-Edition)
Of the following, the preferred airways routing from
CLACTON CLN 114.55 (51°51'N 001°09'E) to DINARD DIN
114.3 (48°35'N 002°05'W) above FL245 is:

8. In a flight plan when the destination aerodrome is A and
the alternate aerodrome is B, the final reserve fuel for a
turbojet engine aeroplane corresponds to:

9. (For this question use annex 033- 10995A or Route
Manual chart E(LO)5)
The magnetic course/distance from ELBE LBE 115.1
(53°39'N 009°36'E) to LUNUD (54°50'N 009°19'E) on
airway H12 is:

10. (For this question use annexes 033-12302A and 033-
12302B or Flight Planning Manual MRJT 1 Figure 4.5.2
and 4.5.3.1)
Given : Distance C - D : 3200 NM
Long Range Cruise at FL 340
Temperature Deviation from ISA : +12°C
Tailwind component : 50 kt
Gross mass at C : 55 000 kg
The fuel required from C - D is :

11. (For this question use annex 033- 11034A or Route
Manual chart E(HI)5 CAA-Edition)
An appropriate flight level for flight on airway UR24 from
NANTES NTS 117.2 (47°09'N 001°37'W) to CAEN CAN
115.4 (49°10'N 000°27'W) is:

12. (For this question use annex 033-9733A or Flight
Planning Manual SEP1 Figure 2.2 Table 2.2.3)
A flight has to be made with the single engine sample
aeroplane. For the fuel calculation allow 10 lbs fuel for
start up and taxi, 3 minutes and 1 gallon of additional
fuel to allow for the climb, 10 minutes and no fuel
correction for the descent.
Planned flight time (overhead to overhead) is 02 hours
and 37 minutes.
Reserve fuel 30% of the trip fuel.
Power setting is 23 in.HG (or full throttle), 2300 RPM,
20°C lean.
Flight level is 50 and the OAT -5°C.
The minimum block fuel is:

13. (For this question use annex 033- 11005A or Route
Manual chart E(LO)1 )
The radio navigation aid at TOPCLIFFE (54°12'N
001°22'W) is a:

14. In the ATS flight plan, for a non-scheduled flight which
of the following letters schould be entered in Item 8
(Type of Flight) :

15. (For this question use annexes 033-11223A, 033-11223B
and 033-11223C)
Given:
. Take-off mass: 150 000 kg
. Planned cruise at FL 350
. Long range MACH
. Standard Atmosphere (ISA)
. CG: 37 %
Covering an air distance of 2 000 NM, your trip fuel from
take-off to landing will be:

16. An aircraft, following a 215° true track, 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:

17. (For this question use annex 033-9572A or Flight
Planning Manual MRJT 1 Figure 4.5.3.1)
Find: Air distance in Nautical Air Miles (NAM) for this leg
and fuel consumption
Given: 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.

18. Unless otherwise shown on charts for standard
instrument departure the routes are given with:

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. The final reserve fuel for aeroplanes with turbine
engines is

21. (For this question use annex 033-3313A or Route Manual
chart E(HI)4 CAA-Edition)
An aeroplane has to fly from Abbeville (50°08.1'N
001°51.3'E) to Biggin (51°19.8'N 000°00.2'E). What is the
distance of this leg ?

22. (For this question use annexes 033-12307A and 033-
12307B or Flight Planning Manual MRJT 1 Figure 4.5.2
and 4.5.3.3)
Given : Distance B - C : 1200 NM
Cruise Mach 0.78 at FL300
Temperature Deviation from ISA : -14°C
Tailwind component : 40 kt
Gross mass at B : 50 200 kg
The fuel required from B - C is :

23. 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?

24. (For this question use annex 033- 11067A or Route
Manual chart MUNICH NDB DME Rwy 26L approach (16-
3))
The frequency and identifier of the NDB for the
published approachs are:

25. (For this question use annex 033-12377A or Route
Manual chart NAP)
The distance (NM) from C (62°N020°W) to B (58°N004°E)
is

26. (For this question use annex 033-9734A,
AERONAUTICAL CHART ICAO 1:500 000 STUTTGART
(NO 47/6) or Route Manual VFR+GPS chart ED-6)
Flying 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.

27. 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 ATS flight plan its wake turbulence
category is :

28. (For this question use annex 033- 11032A or Route
Manual chart E(LO)5)
An appropriate flight level for flight on airway G9 from
SUBI SUI 116.7 (52°23'N 014°35'E) to CZEMPIN CZE
114.5 (52°08'N 016°44'E) is:

29. In an ATS 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 :

30. An appropriate flight level for IFR flight in accordance
with semi-circular height rules on a magnetic course of
200° is:

31. In the ATS flight plan item 15, when entering a route for
which standard departure (SID) and standard arrival
(STAR) procedures exist :

32. Minimum planned take-off fuel is 160 kg (30% total
reserve fuel is included). Assume the groundspeed on
this trip is constant. When the aeroplane has done half
the distance the remaining fuel is 70 kg. Is diversion to a
nearby alternate necessary?

33. (For this question use annex 033-11193A)
What is the mean temperature deviation (°C) from the
ISA over 50°N 010°W ?

34. When an ATS flight plan has been submitted for a
controlled flight, the flight plan should be amended or
cancelled in the event of the off-block time being
delayed by :

35. When an ATS flight plan has been submitted for a
controlled flight, the flight plan should be amended or
cancelled in the event of the off-block time being
delayed by :

36. (For this question use annex 033-12371A or Route
Manual chart NAP)
The initial true course from C (62°N020°W) to B
(58°N004°E) is

37. (For this question use annex 033- 11066A or Route
Manual chart ZURICH ILS Rwy 16 (11-2))
The lowest published authorised RVR for an ILS
approach glide slope out, all other aids serviceable,
aeroplane category A is:

38. (For this question use annex 033-4622A or Flight
Planning Manual MEP 1 Figure 3.3)
A flight has to be made with a multi engine piston
aeroplane (MEP 1). 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 from overhead to overhead is 1h47min.
Powersetting is 45%, 2600 RPM. Calculated reserve fuel
is 30% of the trip fuel. FL 100. Temperature -5°C. Find
the minimum block fuel.

39. (For this question use annex 033-11238A)
The flight crew of a turbojet aeroplane prepares a flight
using the following data:
- Flight level FL 370 at "Long Range" (LR) cruise regime
- (Prescribed) mass at brake release: 204 500 kg
- Flight leg ground distance: 2 000 NM
- Temperatures: ISA
- Headwind component: 70 kt
- "Total anti-ice" set on "ON" for the entire flight
- no requested climb and descent correction of the fuel
consumption
The fuel required from take-off to landing is:

40. For a repetitive flight plan (RPL) to be used, flights must
take place on a regular basis on at least :

41. Given :
Distance A to B 3060 NM
Mean groundspeed 'out' 440 kt
Mean groundspeed 'back' 540 kt
Safe Endurance 10 hours
The time to the Point of Safe Return (PSR) is:

42. Given :
Distance A to B 3060 NM
Mean groundspeed 'out' 440 kt
Mean groundspeed 'back' 540 kt
Safe Endurance 10 hours
The time to the Point of Safe Return (PSR) is:

43. (For this question use annex 033-12305A or Flight
Planning Manual MRJT 1 Figure 4.5.1)
Given : Brake release mass : 62 000 kg
Temperature : ISA + 15°C
The fuel required for a climb from Sea Level to FL330 is :

44. (For this question use annex 033-11190A)
The wind direction and velocity (°/kt) at 50°N 040°E is:

45. (For this question use annex 033-12326A )
Which describes the maximum intensity of turbulence, if
any, forecast for FL260 over TOULOUSE (44°N001°E) ?

46. (For this question use annex 033-3321A or Flight
Planning Manual MRJT 1 Figure 4.3.1.B)
Given : estimated zero fuel mass 50 t; estimated landing
mass at alternate 52 t; final reserve fuel 2 t; alternate fuel
1 t; flight to destination, distance 720 NM, true course
(TC) 030, W/V 340/30; cruise: long range FL 330, outside
air temperature -30 ° C.
Find : estimated trip fuel and time

47. (For this question use annex 033-12367A or Flight
Planning Manual MRJT 1 Figure 4.5.4)
A descent is planned at .74/250KIAS from 35000ft to
5000ft. How much fuel will be consumed during this
descent?

48. (For this question use annex 033-12336A )
What maximum surface windspeed (kt) is forecast for
BORDEAUX/MERIGNAC at 1600 UTC ?

49. (For this question use annex 033-9574A or Flight
Planning Manual MRJT 1 Figure 4.5.1)
Given: Brake release mass 57500 kg, Temperature ISA -
10°C, Headwind component 16 kt, Initial FL 280
Find: Still air distance (NAM) and ground distance (NM)
for the enroute climb 280/.74

50. On a VFR flight plan, the total estimated time is:

51. An executive pilot is to carry out a flight to a French
aerodrome, spend the night there and return the next
day. Where will he find the information concerning
parking and landing fees ?

52. In the ATS flight plan Item 19, if the number of
passengers to be carried is not known when the plan is
ready for filing :

53. (For this question use annex 033-12328A )
Over LONDON (51°N000°E/W), the lowest FL listed which
is unaffected by CAT is:

54. (For this question use annex 033-11189A)
The wind velocity over ITALY is

55. (For this question use annex 033- 11044A or Route
Manual SID chart for LONDON HEATHROW (10-3))
Which of the following is a correct Minimum Safe
Altitude (MSA) for the Airport?

56. (For this question use annex 033- 11065A or Route
Manual chart PARIS CHARLES DE GAULLE ILS Rwy 10
(21-8))
The ILS localizer course is :

57. (For this question use annex 033-9558A)
Finish the ENDURANCE/FUEL CALCULATION and
determine ATC ENDURANCE for a twin jet aeroplane,
with the help of the table provided. Contingency is 5% of
the planned trip fuel and fuel flow for extra fuel is 2400
kg/h.

58. You must fly IFR on an airway orientated 135° magnetic
with a MSA at 7 800 ft. Knowing the QNH is 1 025 hPa
and the temperature is ISA + 10°, the minimum flight
level you must fly at is:

59. (For this question use annex 033-3311A or Flight
Planning Manual MRJT 1 Figure 4.5.3.1)
Given :FL 330; long range cruise; OAT -63°C; gross
mass 50 500 kg.
Find: true airspeed (TAS)

60. (For this question use annexes 033-9494A and 033-
9694B or Flight Planning Manual MRJT 1 Figure 4.5.3.1
and Figure 4.3.1B)
Given: twin jet aeroplane, Zero fuel mass 50000 kg,
Landing mass at alternate 52000 kg, Final reserve fuel
2000 kg, Alternate fuel 1000 kg, Flight to destination:
Distance 720 NM, True course 030°, W/V 340°/30 kt, Long
range cruise, FL 330, Outside air temperature -30°C
Find: Estimated trip fuel and time with simplified flight
planning

61. (For this question use annex 033-12333A )
Which best describes the weather, if any, at
LYON/SATOLAS at 1330 UTC ?

62. (For this question use annex 033-11259A and 033-
11259B)
The flight crew of a turbojet aeroplane prepares a flight
using the following data:
- Flight leg air distance: 2 700 NM
- Flight level FL 310, true airspeed: 470 kt
- Tailwind component at this level: 35 kt
- Initially planned take-off mass (without extra fuel on
board): 180 000 kg
- Fuel price: 0.28 Euro/l at departure; 0.26 Euro/l at
destination
To maximize savings, the commander chooses to carry
extra fuel in addition to that which is necessary.
The optimum quantity of fuel which should be carried in
addition to the prescribed quantity is:

63. (For this question use annex 033-3909A or Route Manual
chart E(HI)4 CAA-Edition)
Planning a IFR flight from Paris Charles de Gaulle (N49
00.9 E002 36.9) to London Heathrow
(N51 29.2 W000 27.9).
Determine the preplanning distance by calculating the
direct distance plus 10%.
The preplanning distance is:

64. (For this question use annex 033-12341A or Flight
Planning Manual MRJT 1 Figure 4.3.1C)
For a flight of 1900 ground nautical miles the following
apply :
Head wind component 10 kt
Temperature ISA -5°C
Trip fuel available 15000 kg
Landing mass 50000kg
What is the minimum cruise level (pressure altitude)
which may be planned ?

65. (For this question use annex 033-11197A)
Which affects the visibility forecast for 0000 UTC at
LAHORE (OPLA) ?

66. In the appropriate box of a flight plan, for endurance,
one must indicate the time corresponding to:

67. On an ATC flight plan, to indicate that you will overfly
the way-point TANGO at 350 kts at flight level 280, you
write:

68. (For this question use annex 033- 11004A or Route
Manual chart E(HI)5 CAA-Edition)
The magnetic course/distance from LIMOGES LMG
114.5 (45°49'N 001°02'E) to CLERMONT FERRAND CMF
117.5 (45°47'N 003°11'E) on airway UG22 is:

69. (For this question use annex 033- 11031A or Route
Manual chart E(HI)4 CAA-Edition)
An appropriate flight level for flight on airway UG1 from
ERLANGEN ERL 114.9 (49°39°'N 011°09'E) to
FRANKFURT FFM 114.2 (50°03'N 008°38'E) is :

70. (For this question use annex 033-12319A)
The approximate mean wind component (kt) along true
course 180° from 50°N to 40°N at 005° W is

71. (For this question use annex 033-9728A,
AERONAUTICAL CHART ICAO 1:500 000 STUTTGART
(NO 47/6) or Route Manual VFR+GPS chart ED-6)
Which navigation aid is located in position 48°55'N,
009°20'E ?

72. During an IFR flight in a Beech Bonanza 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?

73. 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:

74. (For this question use annex 033-12277A)
In the event that SELCAL, is prescribed by an
appropriate authority, in which section of the ATS flight
plan will the SELCAL code be entered ?

75. An aircraft is in cruising flight at FL 095, IAS 155kt. The
pilot intends to descend at 500 ft/min to arrive overhead
the MAN VOR at 2 000 FT (QNH 1 030hPa). The TAS
remains constant in the descent, wind is negligeable,
temperature standard. At which distance from MAN
should the pilot commence the descent?

76. (For this question use annex 033-12353A or Route
Manual chart 5 AT(HI))
On airway PTS P from Vigra (62°334N 006°02'E), the
initial great circle grid course is :

77. Find the distance to the POINT OF SAFE RETURN (PSR).
Given: maximum useable fuel 15000 kg, minimum
reserve fuel 3500 kg, Outbound: TAS 425 kt, head wind
component 30 kt, fuel flow 2150 kg/h, Return: TAS 430
kt, tailwind component 20 kt, fuel flow 2150 kg/h

78. (For this question use annex 033-11195A)
What lowest cloud conditions (oktas/ft) are forecast for
1900 UTC at HAMBURG (EDDH) ?

79. Which of the following statements is (are) correct with
regard to computer flight plans
1. 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.

80. (For this question use annex 033-3324A or Flight
Planning Manual MRJT 1 Figure 4.4)
Given: dry operating mass 35 500 kg; estimated load 12
000 kg, contingency approach and landing fuel 2 500 kg;
elevation at departure aerodrome 500 ft; elevation at
alternate aerodrome 30 ft.
Find: final reserve fuel for a jet aeroplane (holding) and
give the elevation which is relevant.

81. (For this question use annex 033-9719A,
AERONAUTICAL CHART ICAO 1:500 000 STUTTGART
(NO 47/6) or Route Manual VFR+GPS chart ED-6)
An 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.
Name the frequency of the TANGO VORTAC

82. (For this question use annex 033-9730A,
AERONAUTICAL CHART ICAO 1:500 000 STUTTGART
(NO 47/6) or Route Manual VFR+GPS chart ED-6)
Which navigation aid is located in position 48°30'N,
007°34'E?

83. (For this question use annex 033-12327A )
The maximum wind velocity (°/kt) immediately north of
TUNIS (36°N010°E) is

84. (For this question use annex 033-11194A)
The wind direction and velocity (°/kt) at 40°N 040°E is

85. In the ATS 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 :

86. (For this question use annex 033-12352A or Flight
Planning Manual MRJT 1 Figure 4.3.1C)
For a flight of 2400 ground nautical miles the following
apply :
Tail wind component 25 kt
Temperature ISA -10°C
Cruise altitude 31000ft
Landing mass 52000kg
The (a) trip fuel and (b) trip time respectively are :

87. (For this question use annexes 033-3308A or Flight
Planning Manual MRJT 1 Figure 4.5.1)
Given : brake release mass 57 500 kg
temperature ISA -10°C; head wind component 16 kt
initial FL 280
Find: still air distance (NAM) and ground distance (NM)
for the climb

88. (For this question use annex 033-9723A,
AERONAUTICAL CHART ICAO 1:500 000 STUTTGART
(NO 47/6) or Route Manual VFR+GPS chart ED-6)
Flying from ERBACH airport (48°21'N, 009°55'E) to
POLTRINGEN airport (48°33'N, 008°57'E). Find magnetic
course and the distance.

89. (For this question use annex 033-12313A or Flight
Planning Manual MRJT 1 Figure 4.3.6)
Given : Distance to Alternate : 400 NM
Landing mass at Alternate : 50 000kg
Headwind component : 25 kt
The alternate fuel required is :

90. (For this question use annex 033-9691A or Flight
Planning Manual MRJT 1 Figure 4.5.3.1)
Given: twin jet aeroplane, FL 330, Long range cruise,
Outside air temperature -63°C, Gross mass 50500 kg
Find: True air speed (TAS)

91. (For this question use annex 033-12354A or Route
Manual chart NAP)
On a direct great circle course from Shannon (52°43' N
008°53'W) to Gander (48°54'N054°32'W), the
(a) average true course, and
(b) distance, are :

92. 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:

93. According to the chart the minimum obstruction
clearance altitude (MOCA) is 8500 ft. The meteorological
data gives an outside air temperature of -20°C at FL 85.
The QNH, given by a met. station at an elevation of
4000ft, is 1003 hPa.
What is the minimum pressure altitude which should be
flown according to the given MOCA?

94. An aeroplane is flying from an airport to another.
In cruise, the calibrated airspeed is I50 kt, true airspeed
180 kt, average groundspeed 210 kt, the speed box on
the filed flight plan shall be filled as follows:

95. Planning a flight from Paris (Charles de Gaulle) to
London (Heathrow) for a twin - jet aeroplane.
Preplanning:
Maximum Take-off Mass: 62 800 kg
Maximum Zero Fuel Mass: 51 250 kg
Maximum Landing Mass: 54 900 kg
Maximum Taxi Mass: 63 050 kg
Assume the following preplanning results:
Trip fuel: 1 800 kg
Alternate fuel: 1 400 kg
Holding fuel (final reserve): 1 225 kg
Dry Operating Mass: 34 000 kg
Traffic Load: 13 000 kg
Catering: 750 kg
Baggage: 3 500 kg
Find the Take-off Mass (TOM):

96. (For this question use annex 033-12349A or Flight
Planning Manual MRJT 1 Figure 4.3.1C)
For a flight of 2400 ground nautical miles the following
apply :
Temperature ISA -10°C
Cruise altitude 29000ft
Landing mass 45000kg
Trip fuel available 16000kg
What is the maximum headwind component which may
be accepted ?

97. (For this question use annex 033-12355A or Route
Manual chart 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 :

98. (For this question use annex 033-11209A and 033-
11209B)
Assuming a departure/destination fuel price ratio of
0.91, the commander decides to optimize fuel tankering
by using the following data:
. Cruise flight level: FL 350
. Air distance to be covered: 2 500 NM
. Planned take-off mass: 200 000 kg (with the minimum
prescribed fuel quantity of 38 000 kg that includes a trip
fuel of 29 000 kg)
. Maximum landing mass: 180 000 kg
. Maximum take-off mass: 205 000 kg
. Maximum tank capacity: 40 000 kg
The additional fuel quantity will be:

99. A METAR reads : SA1430 35002KY 7000 SKC 21/03
QI024 =
Which of the following information is contained in this
METAR ?

100. (For this question use annex 033-11188A)
The maximum wind velocity (°/kt) shown in the vicinity
of MUNICH (48°N 012°E) is :

101. (For this question use annex 033- 11012A or Route
Manual chart E(LO)1)
The radio navigation aid at BELFAST CITY (54°37'N
005°53'W) is :

102. (For this question use annex 033-11210A and 033-
11210B)
Assuming a departure/destination fuel price ratio of
0.92, the commander decides to optimize fuel tankering
by using the following data:
. Cruise flight level: FL 350
. Air distance to be covered: 1 830 NM
. Planned take-off mass: 190 000 kg (with a minimum
prescribed fuel quantity of 30 000 kg that includes a trip
fuel of 22 000 kg)
. Maximum landing mass: 180 000 kg
. Maximum take-off mass: 205 000 kg
. Maximum tank capacity: 40 000 kg
The additional fuel quantity will be:

103. (For this question use annex 033-12332A)
The surface wind velocity (°/kt) at PARIS/CHARLES-DEGAULLE
at 1330 UTC was

104. (For this question use annex 033-9543A or Flight
Planning Manual MRJT 1 Figure 4.4)
The final reserve fuel taken from the HOLDING
PLANNING table for the twin jet aeroplane is based on
the following parameters:

105. (For this question use annex 033-11261A)
Prior to an IFR flight, when filling in the ICAO flight plan,
the time information which should be entered in box 13:
"Time" is:

106. (For this question use annex 033-3306A or Flight
Planning Manual MRJT 1 Figure 4.5.3.1)
Given: flight time from top of climb to the enroute point
in FL280 is 48 min. Cruise procedure is long range
cruise (LRC).
Temp. ISA -5° C
Take-off mass 56 000 kg
Climb fuel 1 100 kg
Find: distance in nautical air miles (NAM) for this leg and
fuel consumption:

107. (For this question use annex 033-12375A or Route
Manual chart NAP)
The initial magnetic course from A (64°N006°E) to C
(62°N020°W) is

108. (For this question use annex 033-9550A or Flight
Planning Manual MRJT 1 Figure 4.2.2)
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)

109. On a given path, it is possible to chose 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 kt
FL 270 - M = 0.76 Ts = -43°C HWC = 0
The flight level allowing the highest ground speed is:

110. (For this question use annex 033-9706A or Flight
Planning Manual MRJT 1 Figure 4.5.4 )
Planning an IFR-flight from Paris to London for the twin
jet aeroplane.
Given: Estimated Landing Mass 49700 kg, FL 280, W/V
280°/40 kt, Average True Course 320°, Procedure for
descent .74 M/250 KIAS
Determine the fuel consumption from the top of descent
to London (elevation 80 ft).

111. (For this question use annex 033-12276A)
In the ATS flight plan Item 15, for a flight along a
designated route, where the departure aerodrome is not
on or connected to that route :

112. (For this question use annex 033-11213A and 033-
11213B)
Assuming the following data:
. Ground distance to be covered: 2 500 NM
. Cruise flight level: FL 350
. Cruising speed: Mach 0.82 (true airspeed: 470 kt)
. Tailwind component: 40 kt
. Planned destination landing mass: 150 000 kg
. Temperature: ISA
. CG: 37%
. Total anti-ice: OFF
. Air conditioning: normal
Fuel consumption for such a flight is:

113. (For this question use annex 033-9571A or Flight
Planning Manual MRJT 1 Figure 4.5.3.1)
Find: Final fuel consumption for this leg
Given: Long range cruise, Temperature -63°C, FL 330,
Initial gross mass enroute 54100 kg, Leg flight time 29
min

114. (For this question use annex 033-11202A)
Which of the following flight levels, if any, is forecast to
be clear of significant cloud, icing and CAT along the
marked route from SHANNON (53°N 10°W) to BERLIN
(53°N 13°E) ?

115. (For this question use annex 033-12340A or Flight
Planning Manual MRJT 1 Figure 4.3.5)
For a flight of 2800 ground nautical miles the following
apply :
Head wind component 20 kt
Temperature ISA + 15°C
Brake release mass 64700 kg
The (a) trip fuel, and (b) trip time respectively are :

116. (For this question use annex 033-12373A or Route
Manual chart NAP)
The average magnetic course from A (64°N006°E) to C
(62°N020°W) is

117. (For this question use annex 033-11216A)
A turbojet aeroplane is flying using the following data:
. flight level FL 250, Long Range (LR) cruise, mass of
150 000 kg
. temperature: ISA
. head wind component: 100 kt
. remaining flight time: 1 h 40 min
The ground distance that can be covered during the
cruise flight is:

118. The navigation plan reads:
Trip fuel: 136 kg
Flight time: 2h45min
Calculated reserve fuel: 30% of trip fuel
Fuel in tank is minimum (no extra fuel on board)
Taxi fuel: 3 kg
The endurance on the ICAO flight plan should read:

119. (For this question use annexes 033-9707A, 033-9707B or
Route Manual chart E(HI)4 CAA-Edition, Instrument
approach chart ILS DME Rwy 27R)
Planning an IFR-flight from Paris to London (Heathrow)
via initial approach fix (IAF) Biggin VOR .
Given: distance from top of descent (TOD) to Rwy 27R is
76 NM
Determine the distance from ABB 116.6 to TOD.

120. (For this question use annex 033- 10997A or Route
Manual chart E(LO)2)
The magnetic course/distance from CAMBRAI CMB
112.6 (50°14'N 003°09'E) to TALUN (49°33'N 003°25'E) on
airway B3 is:

121. In the ATS flight plan Item 13, in a flight plan submitted
before departure, the departure time entered is the :

122. 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?

123. (For this question use annex 033-9576A or Route
Manual chart E(HI)5 CAA-Edition)
Given: Leg Moulins(N46 24.4 E003 38.0)/Dijon(N47 16.3
E005 05.9).
Find: Route designator and total distance

124. When a pilot fills in a flight plan, he must indicate the
wake turbulence category. This category is a function of
which mass?

125. 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:

126. (For this question use annexes 033-3911A and 033-
3911B) or (Route Manual chart E(HI)4 CAA-Edition and
Flight planning manual Figure 4.3.6)
Planning a flight from Paris Charles de Gaulle (N49 00.9
E002 36.9) to London Heathrow (N51 29.2 W000 27.9) for
a twin - jet aeroplane. The alternate airport is
Manchester (N53 21.4 W002 15.7)
Preplanning:
The wind from London to Manchester is 250°/30 kt
The distance from London to Manchester is 160 NM.
Assume the Estimated Landing Mass at alternate is
about 50 000 kg.
Find the alternate fuel and the according time.

127. (For this question use annex 033-3907A or Route Manual
chart STAR LONDON Heathrow (10-2))
Planning a IFR flight from Paris (Charles de Gaulle) to
London (Heathrow).
Find the elevation of the destination aerodrome

128. (For this question use annex.033-12342A or Flight
Planning Manual MRJT 1 Figure 4.3.5)
Given the following :
Head wind component 50 kt
Temperature ISA + 10°C
Brake release mass 65000kg
Trip fuel available 18000kg
What is the maximum possible trip distance ?

129. (For this question use annex 031-11229A )
For a turbojet aeroplane flying with a mass of 190 000
kg, at Mach 0.82, and knowing that the temperature at
flight level FL 370 is - 35° C, the optimum flight altitude
calculated using the annex is:

130. (For this question use annex 033-12338A )
Which best describes the weather, if any, forecast for
JOHANNESBURG/JAN SMUTS at 0400 UTC?

131. (For this question use annex 033-12312A or Flight
Planning Manual MRJT 1 Figure 4.3.6)
Given: Distance to Alternate 450 NM
Landing mass at Alternate : 45 000 kg
Tailwind component : 50 kt
The Alternate fuel required is :

132. (For this question use annex 033- 11046A or Route
Manual SID charts for ZURICH (10-3))
Which is the correct ALBIX departure via AARAU for
runway 16?

133. 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 kg
Find: Maximum additional load

134. ((For this question use annex 033-9727A,
AERONAUTICAL CHART ICAO 1:500 000 STUTTGART
(NO 47/6) or Route Manual VFR+GPS chart ED-6)
Give the frequency of ZÜRICH VOLMET

135. (For this question use annex 033- 11030A or Route
Manual chart E(HI)4 CAA-Edition)
An appropriate flight level for flight on airway UR1 from
ORTAC (50°00'N 002°00'W) to MIDHURST MID 114.0
(51°03'N 000°37'W) is:

136. "Integrated range" curves or tables are presented in the
Aeroplane Operations Manuals. Their purpose is

137. (For this question use annex 033-9703A or Route Manual
SID chart 20-3 for PARIS Charles-de-Gaulle)
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.

138. (For this question use annex 033-3910A or Flight
Planning Manual MRJT 1 Figure 4.4)
Planning a flight from Paris Charles de Gaulle to London
Heathrow for a twin - jet aeroplane.
Preplanning:
Dry Operating Mass (DOM): 34 000 kg
Traffic Load: 13 000 kg
The holding is planned at 1 500 ft above alternate
elevation. The alternate elevation is 256 ft. The holding
is planned for 30 minutes with no reductions.
Determine the Estimated Landing Mass at alternate
Manchester.

139. (For this question use annex 033-9732A or Flight
Planning Manual SEP1 Figure 2.2 Table 2.2.2)
A flight has to be made with the single engine sample
aeroplane. For the fuel calculation allow 10 lbs fuel for
start up and taxi, 3 minutes and 1 gallon of additional
fuel to allow for the climb, 10 minutes and no fuel
correction for the descent.
Planned flight time (overhead to overhead) is 03 hours
and 12 minutes.
Reserve fuel 30% of the trip fuel.
Power setting is 25 in.HG (or full throttle), 2100 RPM,
20°C lean.
Flight level is 70 and the OAT 11°C.
The minimum block fuel is:

140. (For this question use annex 033-11211A and 033-
11211B )
Assuming the following data:
. Ground distance to be covered: 2 000 NM
. Cruise flight level: FL 330
. Cruising speed: Mach 0.82 (true airspeed: 470 kt)
. Head wind component: 30 kt
. Planned destination landing mass: 160 000 kg
. Temperature: ISA
. CG: 37%
. Total anti-ice: ON
. Pack flow: HI
Time needed to carry out such a flight is:

141. (For this question use annex 033- 11062A or Route
Manual chart LONDON HEATHROW ILS DME Rwy 09R
(11-1))
The Minimum Descent Altitude (MDA) for an ILS glide
slope out, is:

142. (For this question use annex 033-11182A)
The surface weather system over England (53°N 002°W)
is

143. (For this question use annex 033-10991A or Route
Manual chart E(HI)5 CAA-Edition)
Of the following, the preferred airways routing from
AMBOISE AMB 113.7 (47°26'N 001°04'E) to AGEN AGN
(43°53°'N 000°52'E) above FL200 is:

144. Given:
Dry operating mass (DOM)= 33000 kg
Load= 8110 kg
Final reserve fuel= 983 kg
Alternate fuel= 1100 kg
Contingency fuel 102 kg
The estimated landing mass at alternate should be :

145. (For this question use annex 033-9564A or Flight
Planning Manual MRJT 1 Figure 4.5.1)
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 ft

146. (For this question use annex 033-12374A or Route
Manual chart NAP)
The average true course from A (64°N006°E) to C
(62°N020°W) is

147. Given the following:
D = flight distance
X = distance to Point of Equal Time
GSo = groundspeed out
GSr = groundspeed return
The correct formula to find distance to Point of Equal
Time is :

148. Given :
Distance X to Y 2700 NM
Mach Number 0.75
Temperature -45°C
Mean wind component 'on' 10 kt tailwind
Mean wind compontent 'back' 35 kt tailwind
The distance from X to the point of equal time (PET)
between X and Y is :

149. From which of the following would you expect to find
the dates and times when temporary danger areas are
active

150. (For this question use annexes 033-3912A and 033-
3912B or Route Manual chart E(HI)4 CAA-Edition and
Flight planning manual Figure 4.3.2A)
Planning a flight from Paris Charles de Gaulle (N49 00.9
E002 36.9) to London Heathrow
(N51 29.2 W000 27.9) for a twin - jet aeroplane.
Preplanning:
Powersetting: Mach= 0.74
Planned flight level FL 280
The Landing Mass in the fuel graph is 50 000 kg
The trip distance used for calculation is 200 NM
The wind from Paris to London is 280°/40 kt
Find the estimated trip fuel.

151. (For this question use annex 033-12310A or Flight
Planning Manual MRJT 1 Figure 4.4)
- HOLDING PLANNING
The fuel required for 30 minutes holding, in a racetrack
pattern, at PA 1500 ft, mean gross mass 45 000 kg, is :

152. In an ATS 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 :

153. On a flight plan you are required to indicate in the box
marked "speed" the planned speed for the first part of
the cruise or for the entire cruise.
This speed is:

154. (For this question use annex 033- 11010A or Route
Manual chart E(HI)4 CAA-Edition)
The radio navigation aid at CHIOGGIA (45°04'N 012°17'E)
is a:

155. (For this question use annex 033-9704A or Flight
Planning Manual MRJT 1 Figure 4.5.4 )
Planning an IFR-flight from Paris to London for the twin
jet aeroplane.
Given: Estimated Landing Mass 49700 kg, FL 280, W/V
280°/40 kt, Average True Course 320°, Procedure for
descent .74 M/250 KIAS
Determine the distance from the top of descent to
London (elevation 80 ft).

156. (For this question use annex 033-11214A)
Assuming the following data:
. Ground distance to be covered: 2 600 NM
. Cruise flight level: FL 370
. Cruising speed: Mach 0.82 (true airspeed: 470 kt)
. Wind: zero wind during flight
. Planned destination landing mass: 140 000 kg
. Temperature: ISA + 15° C
. CG: 37 %
. Total anti-ice: ON
. Air conditioning: normal
Fuel consumption for such a flight is:

157. When an ATS 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 :

158. (For this question use annex 033- 11023A or Route
Manual chart E(HI)5 CAA-Edition)
The minimum enroute altitude available on airway
UR160 from NICE NIZ 112.4 (43°46'N 007°15'E) to
BASTIA BTA 116.2 (42°32'N 009°29'E) is:

159. (For this question use annex 033-9575A or Flight
Planning Manual MRJT 1 Figure 4.5.1)
Given: Brake release mass 57500 kg, Temperature ISA -
10°C, Average headwind component 16 kt, Initial FL 280
Find: Climb fuel for enroute climb 280/.74

160. (For this question use annex 033-11241A)
The flight crew of a turbojet aeroplane prepares a flight
using the following data:
- Flight level FL 370 at "Long Range" (LR) cruise regime
- Mass at brake release: 212 800 kg
- Flight leg ground distance: 2 500 NM
- Temperatures: ISA
- CG: 37%
- Headwind component: 30 kt
- "Total anti-ice" set on "ON" for the entire flight
- No requested climb and descent correction of the fuel
consumption
The fuel consumption (from take-off to landing) is:

161. (For this question use annexes 033-11074A, 033-11074B,
033-11074C and 033-11074D)
Planning a MACH 0,82 cruise at FL 390, the estimated
landing mass is 160 000 kg.
The ground distance is 2 800 NM and the mean wind is
equal to zero. ISA conditions.
Fuel consumption will be:

162. (For this question use annex 033-9709A or SID chart
Paris Charles de Gaulle 20-3 )
Planning an IFR-flight from Paris Charles de Gaulle to
London. SID is ABB 8A.
Assume Variation 3° W, TAS 430kts, W/V 280/40 and
distance to top of climb 50NM
Determine the magnetic course, ground speed and wind
correction angle from top of climb to ABB 116.6.

163. When completing an ATS flight plan, an elapsed time
(Item 16) of 1 hour 55 minutes should be entered as :

164. (For this question use annex 033- 11063A or Route
Manual chart PARIS CHARLES DE GAULLE ILS Rwy 27
(21-2))
The crossing altitude and descent instruction for a
propeller aircraft at COULOMMIERS (CLM) are :

165. (For this question use annex 033-11185A)
Which best describes the significant cloud, if any,
forecast for the area southwest of BODO (67°N 014°E)

166. How many feet you have to climb to reach FL 75?
Given: FL 75; departure aerodrome elevation 1500 ft;
QNH = 1023 hPa; temperature = ISA; 1 hPa = 30 ft

167. (For this question use annex 033-12348A or Flight
Planning Manual MRJT 1 Figure 4.3.5)
The following apply:
Temperature ISA +15°C
Brake release mass 62000kg
Trip time 5hr 20 min
What is the trip fuel ?

168. (For this question use annexes 033-9554A and 033-
9554B or Flight Planning Manual MRJT 1 Paragraph 2.1
and Figure 4.2.1)
Find the FUEL MILEAGE PENALTY for the twin jet
aeroplane with regard to the given FLIGHT LEVEL .
Given: Long range cruise, Cruise mass=53000 kg, FL 310

169. (For this question use annex 033 11702 A)
The measured course 042° T.
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:

170. (For this question use annex 033-12311A or Flight
Planning Manual MRJT 1 Figure 4.4)
- HOLDING PLANNING)
The fuel required for 45 minutes holding, in a racetrack
pattern,
at PA 5000 ft, mean gross mass 47 000 kg, is :

171. It is possible, in flight, to:
1 - file an IFR flight plan
2 - modify an active IFR or VFR flight plan
3 - cancel an active VFR flight plan
4 - close an active VFR flight plan
Which of the following combinations contains all of the
correct statements?

172. (For this question use annex 033-4616A or Flight
Planning Manual MRJT 1 Figure 4.3.6)
In order to get alternate fuel and time, the twin -jet
aeroplane operations manual graph shall be entered
with:

173. (For this question use annex 033-11191A)
The wind direction and velocity (°/kt) at 60°N 015°W is

174. Given:
Dry operating mass (DOM)= 33510 kg
Load= 7600 kg
Final reserve fuel= 983 kg
Alternate fuel= 1100 kg
Contingency fuel 102 kg
The estimated landing mass at alternate should be :

175. (For this question use annexes 033-12303A and 033-
12303B or Flight Planning Manual MRJT 1 Figure 4.5.2
and 4.5.3.1))
Given : Distance C - D : 680NM
Long Range Cruise at FL340
Temperature Deviation from ISA : 0° C
Headwind component : 60 kt
Gross mass at C : 44 700 kg
The fuel required from C - D is :

176. When completing an ATS flight plan for a flight
commencing under IFR but possibly changing to VFR,
the letters entered in Item 8 (FLIGHT RULES) would be :

177. (For this question use annex 033-3323A or Flight
Planning Manual MRJT 1 Figure 4.3.3C)
Given: ground distance to destination aerodrome 1 600
NM; headwind component 50 kt; FL 330; cruise 0.78
Mach; ISA + 20 ° C; estimated landing weight 55000 kg .
Find: simplified flight planning to determine estimated
trip fuel and trip time.

178. (For this question use annex 033-11212A and 033-
11212B)
Assuming the following data:
. Ground distance to be covered: 1 500 NM
. Cruise flight level: FL 310
. Cruising speed: Mach 0.82 (true airspeed: 470 kt)
. Head wind component: 40 kt
. Planned destination landing mass: 140 000 kg
. Temperature: ISA + 15° C
. CG: 37 %
. Total anti-ice: ON
. Pack flow: HI
Fuel consumption for such a flight is:

179. (For this question use annex 033-12345A or Flight
Planning Manual MRJT 1 Figure 4.3.5)
Given a trip time of about 9 hours, within the limits of
the data given, a temperature decrease of 30°C will
affect the trip time by approximately :

180. (For this question use annex 033-12347A or Flight
Planning Manual MRJT 1 Figure 4.3.5)
For a flight of 3500 ground nautical miles, the following
apply :
Tail wind component 50 kt
Temperature ISA +10°C
Brake release mass 65000kg
The (a) trip fuel and (b) trip time respectively are :

181. (For this question use annex 033-11254A, 033-11254B,
033-11254C and 033-11254D)
Knowing that:
. Mass at brake release: 190 000 kg
. Selected cruise speed: 0.82 Mach
. Flight leg distance: 1 500 NM
. Cruise level: optimum
. Air conditioning: standard
. Anti-icing: OFF
. Temperature: ISA
. CG: 37%
Assuming zero wind, the planned landing mass at
destination will be:

182. The cruising speed to write in the appropriate box of a
flight plan is:

183. (For this question use annex 033-12314A )
The W/V (°/kt) at 50°N015°W is:

184. (For this question use annex 033-9562A or Flight
Planning Manual MRJT 1 Figure 4.5.3.1)
The aeroplane gross mass at top of climb is 61500 kg.
The distance to be flown is 385 NM at FL 350 and OAT -
54.3 °C. The wind component is 40 kt tailwind.Using long
range cruise procedure what fuel is required?

185. (For this question use annex 033- 10998A or Route
Manual chart E(LO)1)
The magnetic course/distance from WALLASEY WAL
114.1 (53°23N 003°28'W° to LIFFY (53°29'N 005°30'W) on
airway B1 is:

186. (For this question use annex 033-9578A or Flight
Planning Manual MRJT 1 Figure 4.5.3.1)
Given: Long range cruise, OAT -45°C at FL 350, Gross
mass at the beginning of the leg 40000 kg, Gross mass
at the end of the leg 39000 kg
Find: True air speed (TAS) and cruise distance (NAM)
for a twin jet aeroplane

187. (For this question use annex 033- 11061A or Route
Manual chart AMSTERDAM JAA MINIMUMS (10-9X)
The Radio Altimeter minimum altitude for a CAT 2 ILS
DME approach to Rwy 01L is :

188. (For this question use annex 033-9557A or Flight
Planning Manual MRJT 1 Figure 4.5.3.2)
Find the FUEL FLOW for the twin jet aeroplane with
regard to the following data.
Given: MACH .74 cruise, Flight level 310, Gross mass
50000 kg, ISA conditions

189. 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
- payload : 400 kg
- maximum take-off mass : 4200 kg
- maximum landing mass : 3700 kg

190. An appropriate flight level for IFR flight in accordance
with semi-circular height rules on a course of 180° (M) is:

191. (For this question use annex 033-12322A )
Which describes the intensity of icing, if any, at FL 150
in the vicinity of TOULOUSE (44° N 01°E) ?

192. A "current flight plan" is a :

193. A jet aeroplane is to fly from A to B. The minimum final
reserve fuel must allow for :

194. (For this question use annex 033-12364A or Flight
Planning Manual MRJT 1 Figure 4.7.2)
For the purpose of planning an extended range flight it
is required that with a start of diversion mass of 55000kg
a diversion of 600 nautical miles should be achieved in
90 minutes. Using the above table, the only listed cruise
technique to meet that requirement is :

195. (For this question use annex 033-9736A,
AERONAUTICAL CHART ICAO 1:500 000 STUTTGART
(NO 47/6) or Route Manual VFR+GPS chart ED-6)
Flying 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 5NM left and 5 NM
right of the courseline in order to stay 1000 ft clear of
obstacles.

196. (For this question use annex 033-12316A )
The W/V (°/kt) at 40°N 020°W is

197. An operator (turbojet engine) shall ensure that
calculation up of usable fuel for a flight for which no
destination alternate is required includes, taxi fuel, trip
fuel, contingency fuel and fuel to fly for:

198. (For this question use annex 033-11228A)
For a long distance flight at FL 390, "Long Range"
regime, divided into four flight legs with the following
characteristics:
- segment AB - Ground distance: 2 000 NM. head wind
component: 50 kt
- segment BC - Ground distance: 1 000 NM. head wind
component: 30 kt
- segment CD - Ground distance: 500 NM. tail wind
component: 100 kt
- segment DE - Ground distance: 1 000 NM. head wind
component: 70 kt
The air distance of the entire flight is approximately:

199. On a ATC flight plan, to indicate that you will overfly the
way-point ROMEO at 120 kt at flight level 085, you will
write :

200. (For this question use annex 033-12368A or Route
Manual chart NAP)
The average magnetic course from C (62°N020°W) to B
(58°N004°E) is

201. When calculating the fuel required to carry out a given
flight, one must take into account :

1 - the wind
2 - foreseeable airborne delays
3 - other weather forecasts
4 - any foreseeable conditions which may delay landing
The combination which provides the correct statement
is :

202. (For this question use annex 033-12356A or Route
Manual chart 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 :

203. 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 2 000 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:

204. (For this question use annex 033- 10990A or Route
Manual chart E(HI)5 CAA-Edition)
Of the following, the preferred airways routing from
MARTIGUES MTG 117.3 (43°23'N 005°05'E) to ST PREX
SPR 113.9 (46°28'N 006°27'E) above FL245 is :

205. (For this question use annex 033-12320A )
Which best describes the significant cloud forecast for
the area east of Tunis (36°N010°E) ?

206. (For this question use annexes 033-12306A and 033-
12306B or Flight Planning Manual MRJT 1 Figure 4.5.2
and 4.5.3.3)
Given : Distance B - C :
Cruise Mach 0.78 at FL300
Temperature : - 52°C
Headwind component : 50 kt
Gross mass at B : 64 500 kg
The fuel required from B - C is :

207. (For this question use annex 033-3906A or Route Manual
chart SID PARIS Charles-De-Gaulle (20-3))
Planning a IFR flight from Paris (Charles de Gaulle) to
London (Heathrow).
Find the elevation of the departure aerodrome

208. (For this question use annex 033-3908A or Route Manual
chart E(HI)4 CAA-Edition)
Planning a IFR flight from Paris Charles de Gaulle (N49
00.9 E002 36.9) to London Heathrow
(N51 29.2 W000 27.9).
Find the average true course from Paris to London.

209. An airway is marked 3500T 2100 a. This indicates that:

210. (For this question use annex 033-9695A or Flight
Planning Manual MRJT 1 Figure 4.3.3C)
Given: Twin jet aeroplane, Ground distance to
destination aerodrome is 1600 NM, Headwind
component 50 kt, FL 330, Cruise .78 Mach, ISA Deviation
+20°C and Landing mass 55000 kg
Find: Fuel required and trip time with simplified flight
planning

211. For flight planning purposes the landing mass at
alternate is taken as:

212. You have a flight plan IFR from Amsterdam to London.
In the flight plan it is noted that you will deviate from the
ATS route passing the FIR boundary
Amsterdam/London. The airway clearance reads:
Cleared to London via flight planned route.
Which of the following statements is correct?

213. Which of the following statements is (are) correct with
regard to the operation of flight planning computers ?
1. The computer can file the ATC flight plan.
2. In the event of inflight re-routing the computer
produces a new plan.

214. A public transport aeroplane with reciprocating
engines,is flying from PARlS to LYON. The final reserve
corresponds to:

215. (For this question use annex 033-3327A or Flight
Planning Manual MEP 1 Figure 3.2)
A flight is to be made in a multi engine piston aeroplane
(MEP1). The cruising level will be 11000ft. The outside
air temperature at FL is -15 ° C. The usable fuel is 123
US gallons. The power is set to economic cruise. Find
the range in NM with 45 min reserve fuel at 45 % power.

216. (For this question use annex 033-11271A)
The flight crew of a turbojet aeroplane prepares a flight
using the following data:
. Take-off mass: 210 500 kg
. Flight leg ground distance: 2 500 NM
. Flight level FL 330; "Long Range" flight regime
. Tailwind component at this level: 70 kt
. Total anti-ice set on "ON"
. Fixed taxi fuel: 500 kg; final reserve: 2 400 kg
. Ignore alternate fuel.
The effects of climb and descent are not corrected for
consumption.
The quantity of fuel that must be loaded at the parking
area is:

217. 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:

218. (For this question use annex 033- 11060A or Route
Manual chart MADRID BARAJAS ILS DME Rwy 33 (11-1))
The minimum glide slope interception altitude for a full
ILS is:

219. (For this question use annex 033-11196A)
What minimum visibility (m) is forecast for 0600 UTC at
LONDON LHR (EGLL) ?

220. (For this question use annex 033-9739A,
AERONAUTICAL CHART ICAO 1:500 000 STUTTGART
(NO 47/6) or Route Manual VFR+GPS chart ED-6)
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 5NM left and 5 NM
right of the courseline in order to stay 1000 ft clear of
obstacles.

221. (For this question use annex 033-12369A or Route
Manual chart NAP)
The average true course from C (62°N020°W) to B
(58°N004°E) is

222. (For this question use annex 033-12365A or Flight
Planning Manual MRJT 1 Figure 4.7.2)
Using 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 :

223. (For this question use annex 033-4623A or Flight
Planning Manual MEP 1 Figure 3.3)
A flight has to be made with a multi engine piston
aeroplane (MEP 1). 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.
Powersetting is 65%, 2500 RPM. Calculated reserve fuel
is 30% of the trip fuel. FL 120. Temperature 1°C. Find the
minimum block fuel.

224. (For this question use annex 033-11240A and 033-
11240B)
The flight crew of a turbojet aeroplane prepares a flight
using the following data:
- Flight leg distance: 3 500 NM
- Flight level FL 310, true airspeed: 450 kt
- Headwind component at this level: 55 kt
- Initially planned take-off mass (without extra fuel on
board): 180 000 kg
- Fuel price: 0.27 $/l at destination
The commander may carry on board 8 000 kg more fuel
than that which is necessary.
For this fuel transport operation to be cost effective, the
maximum fuel price at departure must be:

225. Given:maximum allowable take-off mass 64 400 kg
maximum landing mass 56 200 kg
maximum zero fuel mass 53 000 kg
dry operating mass 35 500 kg
estimated load 14 500 kg
estimated trip fuel 4 900kg
minimum take-off fuel 7 400 kg
Find the maximum allowable take-off fuel:

226. (For this question use annexes 033-11226A and 033-
11226B)
In standard atmosphere, assuming a mass of 197 000 kg,
in order to fly at FL 370 and to be at the optimum
altitude, your Mach number should be:

227. The maximum permissible take-off mass of an aircraft
for the L wake turbulence category on a flight plan is: