----------------------------------------------------------------------------------------------------------------------------------------------------------------001.
A “current flight plan” is a ;
a)
filed flight plan with amendments and clearance included.
b)
flight plan in the course of which radio communication should be practised between aeroplane and ATC.
c)
filed flight plan.
d)
flight plan with the correct time of departure.
Answer ;
a)
filed flight plan with amendments and clearance included.
----------------------------------------------------------------------------------------------------------------------------------------------------------------002.
( For this question use annex 033-12367A or Flight Planning Manual MRJT 1 Figure 4.5.4 )
Annex 033-12367A
A descent is planned at .74/250 KIAS from 35000 ft to 5000 ft. How much fuel will be consumed during this descent ?
a)
150 kg
b)
278 kg
c)
290 kg
d)
140 kg
Answer ;
a)
150 kg
----------------------------------------------------------------------------------------------------------------------------------------------------------------003.
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 ;
a)
11.7 NM
b)
15.0 NM
c)
30.2 NM
d)
27.1 NM
Answer ;
d)
27.1 NM
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
1
Flight Planning & Monitoring
004.
( For this question use annex 033-4623A or Flight Planning Manual MEP 1 Figure 3.3 )
Annex 033-4623A
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
1h 47min. Power setting is 45% , 2600 RPM. Calculated reserve fuel is 30% of the trip fuel. FL 100. Temperature -5°C.
Find the minimum block fuel ;
a)
470 US gallons.
b)
37 US gallons.
c)
47 US gallons.
d)
60 US gallons.
Answer ;
c)
47 US gallons.
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
2
Flight Planning & Monitoring
005.
( For this question use annex 033-4623A or Flight Planning Manual MEP 1 Figure 3.3 )
Annex 033-4623A
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
2 h 37 min. 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 ;
a)
91 US gallons.
b)
76 US gallons.
c)
86 US gallons.
d)
118 US gallons.
Answer ;
a)
91 US gallons.
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
3
Flight Planning & Monitoring
006.
( For this question use annex 033-9733A or Flight Planning Manual SEP1 Figure 2.2 Table 2.2.3 )
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 ;
a)
265 lbs
b)
250 lbs
c)
208 lbs
d)
270 lbs
Answer ;
a)
265 lbs
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
4
Flight Planning & Monitoring
007.
( For this question use annex 033-9732A or Flight Planning Manual SEP1 Figure 2.2 Table 2.2.2 )
Annex 033-9732A
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 ;
a)
252 lbs
b)
283 lbs
c)
268 lbs
d)
215 lbs
Answer ;
b)
283 lbs
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
5
Flight Planning & Monitoring
008.
( For this question use Flight Planning Manual SEP1 Figure 2.2 Table 2.2.3 )
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 6 lbs 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 Standard Day ( ISA ). The minimum block fuel is ;
a)
256 lbs
b)
260 lbs
c)
276 lbs
d)
281 lbs
Answer ;
c)
276 lbs
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
6
Flight Planning & Monitoring
009.
( For this question use Flight Planning Manual SEP1 Figure 2.2 Table 2.2.3 )
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 10 lbs 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 23 in.HG ( or full throttle )
, 2300 RPM , 20°C lean. Flight level is 70 and OAT is ISA + 20ºC. The minimum block fuel is ;
a)
289 lbs
b)
325 lbs
c)
306 lbs
d)
349 lbs
Answer ;
b)
325 lbs
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
7
Flight Planning & Monitoring
010.
( For this question use annex 033-3301A or Flight Planning Manual MEP1 Figure 3.1 )
Annex 033-3301A
A flight is to be made from one airport ( elevation 3000 ft ) to another in a multi engine piston aeroplane ( MEP1 ). The
cruising level will be FL 110. The temperature at FL 110 is ISA -10° C. The temperature at the departure aerodrome is -1° C.
Calculate the fuel to climb with mixture rich ;
a)
12 US gallon
b)
9 US gallon
c)
3 US gallon
d)
6 US gallon
Answer ;
d)
6 US gallon
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
8
Flight Planning & Monitoring
011.
( For this question use annex 033-3327A or Flight Planning Manual MEP 1 Figure 3.2 )
Annex 033-3327A
A flight is to be made in a multi engine piston aeroplane ( MEP1 ). The cruising level will be 11000 ft. 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 ;
a)
852 NM
b)
602 NM
c)
610 NM
d)
752 NM
Answer ;
d)
752 NM
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
9
Flight Planning & Monitoring
012.
( For this question use annex 033-3302A or Flight Planning Manual MEP1 Figure 3.6 )
Annex 033-3302A
A flight is to be made to an airport , pressure altitude 3000 ft , in a multi engine piston aeroplane ( MEP1 ). The forecast OAT
for the airport is -1° C. The cruising level will be FL 110 , where OAT is -10° C. Calculate the still air descent distance for ;
145 KIAS , Rate of descent 1000 ft/min , Gears and flaps up ;
a)
36 NM
b)
20 NM
c)
29 NM
d)
25 NM
Answer ;
b)
20 NM
----------------------------------------------------------------------------------------------------------------------------------------------------------------013.
A jet aeroplane has a cruising fuel consumption of 4060 kg/h , and 3690 kg/h during holding. If the destination is an isolated
airfield , the aeroplane must carry , in addition to contingency reserves , additional fuel of ;
a)
3500 kg.
b)
1845 kg.
c)
8120 kg.
d)
7380 kg.
Answer ;
c)
8120 kg.
----------------------------------------------------------------------------------------------------------------------------------------------------------------014.
A jet aeroplane is to fly from A to B. The minimum final reserve fuel must allow for ;
a)
15 minutes hold at 1500 ft above destination aerodrome elevation.
b)
30 minutes hold at 1500 ft above mean sea level.
c)
30 minutes hold at 1500 ft above destination aerodrome elevation , when no alternate is required.
d)
20 minutes hold over alternate airfield.
Answer ;
c)
30 minutes hold at 1500 ft above destination aerodrome elevation , when no alternate is required.
----------------------------------------------------------------------------------------------------------------------------------------------------------------015.
A METAR reads : SA1430 35002KT 7000 SKC 21/03 QI024 =
Which of the following information is contained in this METAR ?
a)
runway in use
b)
period of validity
c)
temperature/dewpoint
d)
day/month
Answer ;
c)
temperature/dewpoint
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
10
Flight Planning & Monitoring
016.
A public transport aeroplane with reciprocating engines , the final reserve should be ;
a)
fuel to fly for 1 hour at holding speed
b)
fuel to fly for 30 minutes at holding speed
c)
fuel to fly for 2 hours
d)
fuel to fly for 45 minutes
Answer ;
d)
fuel to fly for 45 minutes
----------------------------------------------------------------------------------------------------------------------------------------------------------------017.
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
rerouting of that flight to Limoges.
a)
The pilot-in-command must advise ATC of his intention to divert to Limoges at least 15 minutes before the
planned time of arrival.
b)
The RPL must be cancelled for that day and a specific flight plan has to be filed.
c)
The airline’s “Operations” Department has to transmit a change in the RPL at the ATC office , at least half an
hour before the planned time of departure.
d)
It is not possible to plan another destination and the flight has to be simply cancelled that day ( scheduled
flight and not chartered ).
Answer ;
b)
The RPL must be cancelled for that day and a specific flight plan has to be filed.
----------------------------------------------------------------------------------------------------------------------------------------------------------------018.
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 ?
a)
499 Nautical Air Miles ( NAM )
b)
511 Nautical Air Miles ( NAM )
c)
406 Nautical Air Miles ( NAM )
d)
414 Nautical Air Miles ( NAM )
Answer ;
c)
406 Nautical Air Miles ( NAM )
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
11
Flight Planning & Monitoring
019.
( For this question use annex 033-11270A )
Annex 033-11270A
A turbojet aeroplane flies using the following data ;
flight level : FL 330
flight regime “Long Range”( LR )
mass 156 500 kg
tailwind component at this level : 40 kt
With a remaining flight time of 1 h 10 min the ground distance that can be covered by the aeroplane at cruising speed is ;
a)
539 NM
b)
518 NM
c)
471 NM
d)
493 NM
Answer ;
a)
539 NM
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
12
Flight Planning & Monitoring
020.
( For this question use annex 033-11215A )
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 ;
a)
71 NM/1000 kg , 5330 kg/h
b)
105 NM/1000 kg , 6515 kg/h
c)
86 NM/1000 kg , 6515 kg/h
d)
105 NM/1000 kg , 5330 kg/h
Answer ;
d)
105 NM/1000 kg , 5330 kg/h
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
13
Flight Planning & Monitoring
021.
( For this question use annex 033-11216A )
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 ;
a)
445 NM
b)
612 NM
c)
2031 NM
d)
841 NM
Answer ;
a)
445 NM
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
14
Flight Planning & Monitoring
022.
( For this question use annex 033-11207A and 033-11207B )
Annex 033-11207A , 033-11207B
A turbojet aeroplane is prepared for a 1300 NM flight at FL 350 , with a true airspeed of 460 kt and a head wind of 160 kt.
The take-off runway limitation is 174 000 kg , the planned departure mass is 160 000 kg. The departure fuel price is equal to 0.92
times the arrival fuel price ( fuel price ratio = 0.92 ). In order for the airline to optimize its savings , the additional fuel quantity that
must be loaded on board is ;
a)
30 000 kg
b)
14 000 kg
c)
42 000 kg
d)
12 000 kg
Answer ;
b)
14 000 kg
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
15
Flight Planning & Monitoring
023.
( For this question use annex 033-11208A )
Annex 033-11208A
A turbojet aeroplane , weighing 200 000 kg , initiates its cruise at the optimum level at M 0.84 ( ISA , CG = 37% , Total Anti
Ice ON ). A head wind of 30 kt is experienced and , after a distance of 500 NM , severe icing is encountered and this requires an
immediate descent. The aeroplane mass at start of descent is ;
a)
193 000 kg
b)
193 800 kg
c)
192 500 kg
d)
193 400 kg
Answer ;
c)
192 500 kg
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
16
Flight Planning & Monitoring
024.
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 ?
a)
8800 ft.
b)
12800 ft.
c)
8200 ft.
d)
8500 ft.
Answer ;
a)
8800 ft.
----------------------------------------------------------------------------------------------------------------------------------------------------------------025.
( For this question use annex 033- 11040A or Route Manual STAR charts for ZURICH (10-2,10-2A,10-2B) )
Aeroplane arriving via route BLM 2Z only , should follow the following route to EKRON int ;
a)
BLM R111 to GOLKE int then TRA R-247 inbound to EKRON int
b)
HOC R067 via GOLKE to EKRON int
c)
WIL R018 outbound to EKRON int
d)
TRA R247 outbound to EKRON int
Answer ;
a)
BLM R111 to GOLKE int then TRA R-247 inbound to EKRON int
----------------------------------------------------------------------------------------------------------------------------------------------------------------026.
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 ;
a)
20 min
b)
24 min
c)
16 min
d)
10 min 40 sec
Answer ;
b)
24 min
----------------------------------------------------------------------------------------------------------------------------------------------------------------027.
An aeroplane has the following masses ;
ESTLWT : 50 000 kg
Trip fuel : 4 300 kg
Contingency fuel : 215 kg
Alternate fuel ( final reserve included ) : 2 100kg
Taxi : 500 kg
Block fuel : 7 115 kg
Before departure the captain orders to make the block fuel 9 000 kg. The trip fuel in the operational flight plan should read ;
a)
6 185 kg.
b)
6 400 kg.
c)
4 300 kg.
d)
9 000 kg.
Answer ;
c)
4 300 kg.
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
17
Flight Planning & Monitoring
028.
( For this question use annex 033-3312A or Route Manual chart E(HI)4 CAA-Edition )
Annex 033-3312A
An aeroplane has to fly from Abbeville ( 50°08.1'N 001°51.3'E ) to Biggin ( 51°19.8'N 00°00.2'E ). At Biggin you can
find : 141°. This is ;
a)
The average true course of the great circle from Biggin to Abbeville.
b)
Te radial , referenced to true north , of Biggin to fly inbound.
c)
The magnetic course from Biggin to Abbeville.
d)
The magnetic course to fly inbound to Biggin.
Answer ;
c)
The magnetic course from Biggin to Abbeville.
----------------------------------------------------------------------------------------------------------------------------------------------------------------029.
( For this question use annex 033-3312A or Route Manual chart E(HI)4 CAA-Edition )
Annex 033-3312A
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 ?
a)
b)
c)
d)
100 NM
38 NM
62 NM
64 NM
Answer ;
a)
100 NM
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
18
Flight Planning & Monitoring
030.
( For this question use annex 033-3312A or Route Manual chart E(HI)4 CAA-Edition )
Annex 033-3312A
An aeroplane has to fly from Abbeville ( 50°08.1'N 001°51.3'E ) to Biggin ( 51°19.8'N 00°00.2'E ). What is the first FL
above FL295 that can be flown on an IFR flight plan ?
a)
FL 310
b)
FL 300
c)
FL 320
d)
FL 330
Answer ;
b)
FL 300
----------------------------------------------------------------------------------------------------------------------------------------------------------------031.
( For this question use annex 033-3313A or Route Manual chart E(HI)4 CAA-Edition )
Annex 033-3313A
An aeroplane has to fly from Salzburg ( 48°00.2'N 012°53.6'E ) to Klagenfurt ( 46°37.5'N 014°33.8'E ). Which statement is
correct ?
a)
b)
c)
d)
The airway UB5 can be used for flight to/from Klagenfurt and Salzburg.
The airway UB5 cannot be used , there is one way traffic to the north.
The airway UB5 is closed for southboud traffic above FL200.
The airway UB5 is closed in this direction except during the weekends.
Answer ;
a)
The airway UB5 can be used for flight to/from Klagenfurt and Salzburg.
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
19
Flight Planning & Monitoring
032.
( 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 )
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 ;
a)
422 kHz
b)
118.60 MHz
c)
112.50 MHz
d)
118.80 MHz
Answer ;
c)
112.50 MHz
----------------------------------------------------------------------------------------------------------------------------------------------------------------033.
An aeroplane is on an IFR flight. The flight is to be changed from IFR to VFR. Is it possible ?
a)
No , only ATC can order you to do this.
b)
Yes , but only with permission from ATC.
c)
Yes , the pilot in command must inform ATC using the phrase “cancelling my IFR flight”.
d)
No , you have to remain IFR in accordance to the filed flight plan.
Answer ;
c)
Yes , the pilot in command must inform ATC using the phrase “cancelling my IFR flight”.
----------------------------------------------------------------------------------------------------------------------------------------------------------------034.
An aircraft flies at a TAS of 380 kt. It flies from A to B and back to A. Distance AB = 480 NM. When going from A to B , it
experiences a headwind component = 60 kt. The wind remains constant. The duration of the flight will be:
a)
2 h 35 min
b)
3 h 00 min
c)
2 h 10 min
d)
2 h 32 min
Answer ;
a)
2 h 35 min
----------------------------------------------------------------------------------------------------------------------------------------------------------------035.
An aircraft , following a 215° true track , must fly over a 10600 ft obstacle with a minimum obstacle clearance of 1500 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 , what is
the minimum FL the aircraft should fly at allowing for the temperature variation ?
a)
120
b)
130
c)
140
d)
150
Answer ;
c)
140
----------------------------------------------------------------------------------------------------------------------------------------------------------------036.
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 ;
a)
heavy “H”.
b)
medium “M”.
c)
heavy/medium “H/M”.
d)
medium plus “M+”.
Answer ;
a)
heavy “H”.
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
20
Flight Planning & Monitoring
037.
( For this question use Route Manual chart E(HI)2 )
An aircraft has to fly from Aalborg ( 57º06'N 010º00'E ) to Bottna ( 57º45'N 013º48'E ) on airway UR46. What is the track
distance for this flight ?
a)
130 NM
b)
260 NM
c)
60 NM
d)
70 NM
Answer ;
a)
130 NM
----------------------------------------------------------------------------------------------------------------------------------------------------------------038.
( For this question use annex 033-3312A or Route Manual chart E(HI)4 CAA-Edition )
Annex 033-3312A
An aircraft has to fly from Abbeville ( 50°08.1'N 001°51.3'E ) to Biggin ( 51°19.8'N 00°00.2'E ). At Biggin you can find :
141°. This is ;
a)
The magnetic course to fly inbound to Biggin.
b)
The magnetic course from Biggin to Abbeville.
c)
The radial , referenced to true north , of Biggin to fly inbound.
d)
The average true course of the great circle from Biggin to Abbeville.
Answer ;
b)
The magnetic course from Biggin to Abbeville.
----------------------------------------------------------------------------------------------------------------------------------------------------------------039.
( For this question use annex 033-3312A or Route Manual chart E(HI)4 CAA-Edition )
Annex 033-3312A
An aircraft 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 ?
a)
b)
c)
d)
64NM
38 NM
62NM
100 NM
Answer ;
d)
100 NM
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
21
Flight Planning & Monitoring
040.
( For this question use Route Manual chart E(HI)2 )
An aircraft has to fly from ALMA ( 55º25'N 013º34'E ) to BACKA ( 57º33'N 011º59'E ) on airways UB45 UH40 and UA9.
What is the total track distance for this flight ?
a)
105 NM
b)
143 NM
c)
119 NM
d)
146 NM
Answer ;
b)
143 NM
----------------------------------------------------------------------------------------------------------------------------------------------------------------041.
( For this question use Route Manual chart E(HI)2 )
An aircraft has to fly from ALMA ( 55º25'N 013º34'E ) to PETER ( 56º50'N 013º35'E ). Excluding RVSM , what is the
lowest Flight Level above FL400 that can be flown on an IFR flight Plan ?
a)
FL 420
b)
FL 440
c)
FL 410
d)
FL 430
Answer ;
d)
FL 430
----------------------------------------------------------------------------------------------------------------------------------------------------------------042.
( For this question use Route Manual chart E(HI)2 )
An aircraft has to fly from ALMA ( 55º25'N 013º34'E ) to SHILLING (57º33'N 014º00'E). What is the distance between
these two points ?
a)
60 NM
b)
86 NM
c)
131NM
d)
45 NM
Answer ;
c)
131NM
----------------------------------------------------------------------------------------------------------------------------------------------------------------043.
( For this question use Route Manual chart E(HI)1 )
An aircraft has to fly from beacon BEN ( 57º29'N 007º22'W ) to beacon ADN ( 57º19'N 002º16'W ). What is the average
True course for this route ?
a)
093º
b)
101º
c)
281º
d)
109º
Answer ;
a)
093º
----------------------------------------------------------------------------------------------------------------------------------------------------------------044.
( For this question use Route Manual chart E(HI)1 )
An aircraft has to fly from Glasgow ( 55º52'N 004º27'W ) to Benbecula ( 57º29'N 007º22'W ) , cruising at 320 kt TAS.
Assuming a headwind of 40 kt and cruise fuel consumption of 2300 kg/h , what is the forecast fuel used for this flight ?
a)
978 kg
b)
1117 kg
c)
869 kg
d)
2300 kg
Answer ;
b)
1117 kg
----------------------------------------------------------------------------------------------------------------------------------------------------------------045.
( For this question use Route Manual chart E(HI)1 )
An aircraft has to fly from GOW (55º52'N 004º27'W ) to INS ( 57º33'N 004º03'W ) routing via FINDO ( 56º22'N
003º28'W ). For Flight Planning purposes , what is the track distance for this flight ?
a)
102 NM
b)
73 NM
c)
441NM
d)
117 NM
Answer ;
d)
117 NM
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
22
Flight Planning & Monitoring
046.
( For this question use Route Manual chart E(HI)2 )
An aircraft has to fly from ODIN ( 55º35'N 010º39'E ) to LANDVETTER ( 57º39'N 012º17'E ). What is the magnetic course
on this route ?
a)
156º
b)
052º
c)
204º
d)
024º
Answer ;
d)
024º
----------------------------------------------------------------------------------------------------------------------------------------------------------------047.
( For this question use Annex 033-3313A or Route Manual chart E(HI)4 CAA-Edition )
Annex 033-3313A
An aircraft has to fly from Salzburg ( 48°00.2'N 012°53.6'E ) to Klagenfurt ( 46°37.5'N 014°33.8'E ). At Salzburg there is
stated on the chart D 113.8 SBG. That means ;
a)
VOR/DME SBG will be deleted in the future and cannot be used for navigation.
b)
VOR/DME with identification SBG frequency 113.8 MHz can be used.
c)
Only the DME with identification SBG can be used , for which frequency 113.8 MHz should be tuned , VOR
is not available.
d)
ILS/DME 113.8 MHz of Salzburg airport can be used for navigation.
Answer ;
b)
VOR/DME with identification SBG frequency 113.8 MHz can be used.
----------------------------------------------------------------------------------------------------------------------------------------------------------------048.
( For this question use annex 033-3313A or Route Manual chart E(HI)4 CAA-Edition )
Annex 033-3313A
An aircraft has to fly from Salzburg ( 48°00.2'N 012°53.6'E ) to Klagenfurt ( 46°37.5'N 014°33.8'E ). Which statement is
correct ?
a)
b)
c)
The figure 13.4 means that the minimum sector altitude ( MSA ) is 13400 ft.
The figure 13.4 means that the minimum enroute altitude ( MEA ) is 13400 ft.
The figure 108 means that the minimum obstacle clearance altitude ( MOCA ) on this route is 10800 ft above
MSL.
The figure 13.4 means that the minimum grid safe altitude in this sector is 13400 ft above MSL.
d)
Answer ;
d)
The figure 13.4 means that the minimum grid safe altitude in this sector is 13400 ft above MSL.
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
23
Flight Planning & Monitoring
049.
( For this question use Annex 033-3313A or Route Manual chart E(HI)4 CAA-Edition )
Annex 033-3313A
An aircraft has to fly from Salzburg ( 48°00.2'N 012°53.6'E ) to Klagenfurt ( 46°37.5'N 014°33.8'E ). Which statement is
correct ?
a)
b)
c)
d)
The airway UB5 cannot be used , there is one way traffic to the north.
The airway UB5 is closed in this direction except during the weekends.
The airway UB5 is closed for southbound traffic above FL 200.
The airway UB5 can be used for flights to/from Klagenfurt and Salzburg.
Answer ;
d)
The airway UB5 can be used for flights to/from Klagenfurt and Salzburg.
----------------------------------------------------------------------------------------------------------------------------------------------------------------050.
( For this question use Annex 033-3313A or Route Manual chart E(HI)4 CAA-Edition )
Annex 033-3313A
An aircraft has to fly from Salzburg ( 48°00.2'N 012°53.6'E ) to Klagenfurt ( 46°37.5'N 014°33.8'E ). Which statement is
correct ?
a)
b)
c)
d)
The airway UB5 can be used for flights to/from Klagenfurt and Salzburg.
The airway UB5 cannot be used , there is one way traffic to the north.
The airway UB5 is closed in this direction except during the weekends.
The airway UB5 is closed for southbound traffic above FL200.
Answer ;
a)
The airway UB5 can be used for flights to/from Klagenfurt and Salzburg.
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
24
Flight Planning & Monitoring
051.
( For this question use Route Manual chart E(HI)2 )
An aircraft has to fly from SHILLING ( 57º33'N 014º00'E ) to ALMA ( 55º25'N 013º34'E ). What is the minimum grid safe
altitude for this route ?
a)
2900 ft
b)
2700 ft
c)
2500 ft
d)
3200 ft
Answer ;
d)
3200 ft
----------------------------------------------------------------------------------------------------------------------------------------------------------------052.
( For this question use Route Manual chart E(HI)1 )
An aircraft has to fly from TALLA ( 55º30'N 003º21'W ) to FINDO ( 56º22'N 003º28'W ). Excluding RVSM , what is the
first flight Level above FL400 that can be flown on this leg on an IFR flight Plan ?
a)
FL410
b)
FL400
c)
FL430
d)
FL420
Answer ;
c)
FL430
----------------------------------------------------------------------------------------------------------------------------------------------------------------053.
( For this question use Route Manual chart E(HI)1 )
An aircraft has to fly from the airport at Aberdeen ( 57º19'N 002º16'W ) to the airport at Benbecula ( 57º29'N 007º22'W ).
Given ;
Time to climb 11 min
Time to descend is 15 min
TOC is at 3W
TOD is at 6W
TAS 210 kts ( still air )
Find the total journey time ?
a)
47 min
b)
28 min
c)
16 min
d)
54 min
Answer ;
d)
54 min
----------------------------------------------------------------------------------------------------------------------------------------------------------------054.
( For this question use Route Manual chart E(HI)2 )
An aircraft has to fly from the beacon TNO ( 55º46'N 011º26'E ) on a direct route to the beacon HAR ( 57º50'N 012º42'E ).
What is the magnetic track and distance for this flight ?
a)
007º / 131 NM
b)
029º / 69 NM
c)
013º / 117 NM
d)
018º / 129 NM
Answer ;
d)
018º / 129 NM
----------------------------------------------------------------------------------------------------------------------------------------------------------------055.
( For this question use Route Manual chart E(HI)1 )
An aircraft has to fly from TIREE ( 56º29'N 006º53'W ) direct to ABERDEEN ( 57º19'N 002º16'W ). What is the minimum
grid safe altitude for this route ?
a)
4400 ft
b)
5700 ft
c)
3600 ft
d)
5600 ft
Answer ;
b)
5700 ft
----------------------------------------------------------------------------------------------------------------------------------------------------------------056.
( For this question use Route Manual chart E(HI)2 )
An aircraft has to fly on airways from ODIN ( 55º35'N 010º39'E ) to BOTTNA ( 57º45'N 013º48'E ). Which of the following
is an acceptable route for this flight ?
a)
ODN UR156 LAV D17 CINDY UR46 BTD
b)
ODN UR12/UN872 HIL UV30 BTD
c)
ODN UR12 PER UG5 SHG UH42 BTD
d)
ODN UR156 SKA UH42 BTD
Answer ;
d)
ODN UR156 SKA UH42 BTD
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
25
Flight Planning & Monitoring
057.
( For this question use Route Manual chart E(HI)2 )
An aircraft has to fly on airways from SKARA ( 58º23'N 013º15'E ) to SVEDA ( 56º10'N 012º34'E ). Once airborne , if
approved , which of the following is an acceptable route for this flight ?
a)
SKA UH42 BTD UV30 HIL UR1 SVD
b)
SKA UB44 BAK UA9 PAPER UH40 SVD
c)
SKA UR156 LAV UB45 SVD
d)
SKA DCT SVD
Answer ;
a)
SKA UH42 BTD UV30 HIL UR1 SVD
----------------------------------------------------------------------------------------------------------------------------------------------------------------058.
( For this question use Route Manual chart E(HI)2 )
An aircraft has to fly on airways from SVEDA (56º10'N 012º34'E) to SKARA (58º23'N 013º15'E). Which of the following is
the correct route ?
a)
SVD UH40 PAPER UA9 BAK UR156 SKA
b)
SVD UH40 PAPER UA9 BAK UB44 SKA
c)
SVD UB45 LAV UR156 SKA
d)
UR1 HIL UV30 BTD UH42 SKA
Answer ;
b)
SVD UH40 PAPER UA9 BAK UB44 SKA
----------------------------------------------------------------------------------------------------------------------------------------------------------------059.
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 ;
a)
0.80
b)
0.78
c)
0.72
d)
0.76
Answer ;
a)
0.80
----------------------------------------------------------------------------------------------------------------------------------------------------------------060.
( For this question use Route Manual chart E(HI)2 )
An aircraft is flying from BACKA ( 57°33'N 011°59'E) to BOTTNA ( 57°45'N 013°48'E ) on airway UR46. Which of the
following would be a useful cross-reference to check the aircraft’s position at CINDY ?
a)
BAK078 / BTD258
b)
BTD D60
c)
HAR161 / LAV092
d)
LAV D17
Answer ;
c)
HAR161 / LAV092
----------------------------------------------------------------------------------------------------------------------------------------------------------------061.
( For this question use Route Manual chart E(HI)1 )
An aircraft is flying Northbound on the direct route from DEAN CROSS that passes through position 57°00.0'N 003°10.0'W.
Excluding RVSM , what is the first flight Level above FL410 that can be used on an IFR flight Plan ?
a)
FL420
b)
FL430
c)
FL440
d)
FL450
Answer ;
d)
FL450
----------------------------------------------------------------------------------------------------------------------------------------------------------------062.
( For this question use Route Manual chart E(HI)1 )
An aircraft is flying towards GOW ( 55º52'N 004º27W ) on airway UN615 prior to an arrival in the London FIR. According
to the information on the chart , what is the most relevant frequency to receive the broadcast weather for London FIR ( North ) ?
a)
133.67
b)
126.60
c)
115.4
d)
129.22
Answer ;
b)
126.60
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
26
Flight Planning & Monitoring
063.
An aircraft is in cruising flight at FL 095 , GS 155kt. The pilot intends to descend at 500 ft/min to arrive overhead the MAN
VOR at 2000 FT ( QNH 1030hPa ). The TAS remains constant in the descent , wind is negligible , temperature standard. At which
distance from MAN should the pilot commence the descent ?
a)
38 NM
b)
48 NM
c)
45 NM
d)
41 NM
Answer ;
d)
41 NM
----------------------------------------------------------------------------------------------------------------------------------------------------------------064.
An aircraft is on an IFR flight. The flight is to be changed from IFR to VFR. Is it possible ?
a)
No , you have to remain IFR in accordance to the filed flight plan.
b)
No , only ATC can order you to do this.
c)
Yes , but only with permission from ATC.
d)
Yes , the pilot in command must inform ATC using the phrase “cancelling my IFR flight”.
Answer ;
d)
Yes , the pilot in command must inform ATC using the phrase “cancelling my IFR flight”.
----------------------------------------------------------------------------------------------------------------------------------------------------------------065.
( For this question use annex 033-12364A or Flight Planning Manual MRJT 1 Figure 4.7.2 )
Annex 033-12364A
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 ISA.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 ;
a)
735 NM
b)
810 NM
c)
794 NM
d)
875 NM
Answer ;
a)
735 NM
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
27
Flight Planning & Monitoring
066.
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 ;
a)
EDDM0215
b)
EDDM2H15
c)
EDDM1415
d)
EDDM AT 0215
Answer ;
a)
EDDM0215
----------------------------------------------------------------------------------------------------------------------------------------------------------------067.
An airway is marked 3500T 2100a. This indicates that ;
a)
the minimum enroute altitude ( MEA ) is 3500 ft.
b)
the minimum obstruction clearance altitude ( MOCA ) is 3500 ft.
c)
the airway base is 3500 ft MSL.
d)
the airway is a low level link route 2100 ft - 3500 ft MSL.
Answer ;
b)
the minimum obstruction clearance altitude ( MOCA ) is 3500 ft.
----------------------------------------------------------------------------------------------------------------------------------------------------------------068.
An airway is marked 5000 2900a. The notation 5000 is the ;
a)
base of the airway ( AGL )
b)
minimum enroute altitude ( MEA )
c)
maximum authorised altitude ( MAA )
d)
minimum holding altitude ( MHA )
Answer ;
b)
minimum enroute altitude ( MEA )
----------------------------------------------------------------------------------------------------------------------------------------------------------------069.
An airway is marked FL 80 1500a. This indicates that ;
a)
the airway base is 1500 ft MSL.
b)
1500 ft MSL is the minimum radio reception altitude ( MRA ).
c)
the minimum enroute altitude ( MEA ) is FL 80.
d)
the airways extends from 1500 ft MSL to FL 80.
Answer ;
c)
the minimum enroute altitude ( MEA ) is FL 80.
----------------------------------------------------------------------------------------------------------------------------------------------------------------070.
( For this question use annex 033- 11031A or Route Manual chart E(HI)4 CAA-Edition )
An appropriate flight level for flight in RVSM airspace 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 ;
a)
FL310
b)
FL330
c)
FL300
d)
FL290
Answer ;
c)
FL300
----------------------------------------------------------------------------------------------------------------------------------------------------------------071.
( For this question use Route Manual chart E(LO)1 )
An appropriate flight level for flight on airway A2 from TALLA 113.8 TLA ( 55°30'N 003°21'W ) to DEAN CROSS 115.2
DCS ( 54°43'N 003°20'W ) is ;
a)
FL100
b)
FL50
c)
FL80
d)
FL90
Answer ;
d)
FL90
----------------------------------------------------------------------------------------------------------------------------------------------------------------072.
( For this question use annex 033- 11035A or Route Manual chart E(LO)2 )
An 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 ;
a)
FL80
b)
FL60
c)
FL170
d)
FL50
Answer ;
c)
FL170
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
28
Flight Planning & Monitoring
073.
( 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 ;
a)
FL70
b)
FL60
c)
FL80
d)
FL50
Answer ;
a)
FL70
----------------------------------------------------------------------------------------------------------------------------------------------------------------074.
( For this question use annex 033- 11037A or Route Manual chart E(LO)6 )
An appropriate flight level for flight on airway R10 from MONTMEDY MMD 109.4 ( 49°24'N 005°08'E ) to CHATILLON
CTL 117.6 ( 49°08'N 003°35'E ) is ;
a)
FL60
b)
FL40
c)
FL70
d)
FL50
Answer ;
a)
FL60
----------------------------------------------------------------------------------------------------------------------------------------------------------------075.
( For this question use annex 033- 11033A or Route Manual chart E(HI)5 CAA-Edition )
An appropriate flight level for flight on airway UG5 in RVSM airspace from MENDENASBINALS MEN 115.3 ( 44°36'N
003°10'E ) to GAILLAC GAI 115.8 ( 43°57'N 001°50'E ) is ;
a)
FL280
b)
FL300
c)
FL320
d)
FL290
Answer ;
d)
FL290
----------------------------------------------------------------------------------------------------------------------------------------------------------------076.
( For this question use annex 033- 11030A or Route Manual chart E(HI)4 CAA-Edition )
Route Manual chart E(HI)4
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 ;
a)
FL260
b)
FL230
c)
FL250
d)
FL240
Answer ;
c)
FL250
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
29
Flight Planning & Monitoring
077.
( 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 ;
a)
FL270
b)
FL290
c)
FL300
d)
FL310
Answer ;
c)
FL300
----------------------------------------------------------------------------------------------------------------------------------------------------------------078.
( For this question use annex 033- 11036A or Route Manual chart E(LO)6 )
An appropriate flight level for flight on airway W37 from CHEB OKG 115.7 ( 50°04'N 012°24'E ) to RODING RDG 114.7
( 49°02'N 012°32'E ) is ;
a)
FL80
b)
FL70
c)
FL40
d)
FL50
Answer ;
a)
FL80
----------------------------------------------------------------------------------------------------------------------------------------------------------------079.
An appropriate flight level for IFR flight in accordance with semi-circular height rules on a course of 180° ( M ) is ;
a)
FL95
b)
FL90
c)
FL105
d)
FL100
Answer ;
d)
FL100
----------------------------------------------------------------------------------------------------------------------------------------------------------------080.
An IFR flight is planned outside airways on a course of 235° magnetic. The minimum safe altitude is 7800 ft. Knowing the
QNH is 995 hPa , the temperature is ISA , the minimum flight level you must fly is ;
a)
90
b)
80
c)
85
d)
100
Answer ;
d)
100
----------------------------------------------------------------------------------------------------------------------------------------------------------------081.
An operator shall ensure that calculation of usable fuel for an IFR-flight with a turbojet aeroplane for which no destination
alternate is required includes , taxi fuel , trip fuel , contingency fuel and fuel to fly for ;
a)
45 minutes plus 15% of the flight time planned to be spent at cruising level or two hours whichever is less.
b)
45 minutes at holding speed at 450 m above aerodrome elevation in standard conditions.
c)
45 minutes at holding speed at 450 m above MSL in standard conditions.
d)
2 hours at normal cruise consumption.
Answer ;
b)
45 minutes at holding speed at 450 m above aerodrome elevation in standard conditions.
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
30
Flight Planning & Monitoring
082.
( For this question use annex 033-11207A and 033-11207B )
Annex 033-11207A , 033-11207B
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 ;
a)
0 kg
b)
2 000 kg
c)
3 000 kg
d)
4 000 kg
Answer ;
a)
0 kg
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
31
Flight Planning & Monitoring
083.
( For this question use annex 033-11207A and 033-11207B )
Annex 033-11207A , 033-11207B
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 ;
a)
10 000 kg
b)
12 000 kg
c)
20 000 kg
d)
15 000 kg
Answer ;
a)
10 000 kg
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
32
Flight Planning & Monitoring
084.
( For this question use annex 033-11211A and 033-11211B )
Annex 033-11211A , 033-11211B
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 ;
a)
21 700 kg
b)
23 500 kg
c)
19 900 kg
d)
21 500 kg
Answer ;
b)
23 500 kg
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
33
Flight Planning & Monitoring
085.
( For this question use annex 033-11211A and 033-11211B )
Annex 033-11211A , 033-11211B
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 ;
a)
28 300 kg
b)
27 800 kg
c)
29 200 kg
d)
27 000 kg
Answer ;
b)
27 800 kg
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
34
Flight Planning & Monitoring
086.
( For this question use annex 033-11214A and 033-11214B )
Annex 033-11211A , 033-11211B
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 ;
a)
29 100 kg
b)
29 400kg
c)
31 500 kg
d)
27 400 kg
Answer ;
c)
31 500 kg
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
35
Flight Planning & Monitoring
087.
( For this question use annex 033-11211A and 033-11211B )
Annex 033-11211A , 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 ;
a)
5 h 02 min
b)
4 h 10 min
c)
4 h 26 min
d)
4 h 43 min
Answer ;
d)
4 h 43 min
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
36
Flight Planning & Monitoring
088.
Determine the Take-off Mass for the following single engine aeroplane ;
Given ;
Standard Empty Mass 1764 lbs
Optional Equipment 35 lbs
Pilot + Front seat passenger 300 lbs
Cargo Mass 350 lbs
Ramp Fuel = Block Fuel 60 Gal.
Trip Fuel 35 Gal.
Fuel density 6 lbs/Gal.
Start up and Taxy Fuel 10 lbs
a)
2809 lbs
b)
2659 lbs
c)
2764 lbs
d)
2799 lbs
Answer ;
d)
2799 lbs
----------------------------------------------------------------------------------------------------------------------------------------------------------------089.
During a flight at night a position has to be reported to ATC. The aeroplane is at a distance of 750 NM from the ground
station and at flight level 350. The frequency to be used is ;
a)
123.9 MHz.
b)
17286 kHz.
c)
11336 kHz.
d)
5649 kHz.
Answer ;
d)
5649 kHz.
----------------------------------------------------------------------------------------------------------------------------------------------------------------090.
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 ?
a)
12 minutes.
b)
4 minutes.
c)
44 minutes.
d)
63 minutes.
Answer ;
a)
12 minutes.
----------------------------------------------------------------------------------------------------------------------------------------------------------------091.
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 1 h 35 min. Calculate the highest acceptable rate of consumption
possible for the rest of the trip ;
a)
21.3 US gallons/hour
b)
30.3 US gallons/hour
c)
37.9 US gallons/hour
d)
33.0 US gallons/hour
Answer ;
b)
30.3 US gallons/hour
----------------------------------------------------------------------------------------------------------------------------------------------------------------092.
During an IFR flight in a Beech Bonanza the fuel indicators show that the remaining amount of fuel is 100 lbs after 38
minutes. Fuel at take off is 160l bs. 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 ?
a)
44 minutes.
b)
63 minutes.
c)
12 minutes.
d)
4 minutes.
Answer ;
c)
12 minutes.
----------------------------------------------------------------------------------------------------------------------------------------------------------------093.
During an IFR flight TAS and time appear to deviate from the data in the ATC flight plan. The minimum deviations , that
should be reported to ATC in order to conform to PANS-RAC , are ;
a)
TAS 5 kt and time 5 minutes.
b)
TAS 5% and time 3 minutes.
c)
TAS 3% and time 3 minutes.
d)
TAS 10 kt and time 2 minutes.
Answer ;
b)
TAS 5% and time 3 minutes.
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
37
Flight Planning & Monitoring
094.
Excluding RVSM an appropriate flight level for IFR flight in accordance with semicircular height rules on a course of
180° ( M ) is ;
a)
FL100
b)
FL90
c)
FL95
d)
FL105
Answer ;
a)
FL100
----------------------------------------------------------------------------------------------------------------------------------------------------------------095.
Excluding RVSM an appropriate flight level for IFR flight in accordance with semicircular height rules on a magnetic course
of 200° is ;
a)
FL290
b)
FL310
c)
FL300
d)
FL320
Answer ;
b)
FL310
----------------------------------------------------------------------------------------------------------------------------------------------------------------096.
( For this question use annex 033-9572A or Flight Planning Manual MRJT 1 Figure 4.5.3.1 )
Annex 033-9572A
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.
a)
345 NAM , 1994 kg
b)
345 NAM , 2000 kg
c)
349 NAM , 2000 kg
d)
345 NAM , 2006 kg
Answer ;
a)
345 NAM , 1994 kg
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
38
Flight Planning & Monitoring
097.
( For this question use annex 033-9571A or Flight Planning Manual MRJT 1 Figure 4.5.3.1 )
Annex 033-9571A
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
a)
1107 kg
b)
1100 kg
c)
1000 kg
d)
1093 kg
Answer ;
d)
1093 kg
----------------------------------------------------------------------------------------------------------------------------------------------------------------098.
Find the distance from waypoint 3 ( WP 3 ) to the critical point ;
Given ;
distance from WP 3 to WP 4 : 750 NM
TAS out 430 kt
TAS return 425 kt
tailwind component out 30 kt
head wind component return 40 kt
a)
408 NM
b)
375 NM
c)
403 NM
d)
342 NM
Answer ;
d)
342 NM
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
39
Flight Planning & Monitoring
099.
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
a)
1125 NM
b)
1143 NM
c)
1463 NM
d)
1491 NM
Answer ;
a)
1125 NM
----------------------------------------------------------------------------------------------------------------------------------------------------------------100.
( For this question use annex 033-9557A or Flight Planning Manual MRJT 1 Figure 4.5.3.2 )
Annex 033-9557A
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
a)
2300 kg/h
b)
2994 kg/h
c)
1497 kg/h
d)
1150 kg/h
Answer ;
a)
2300 kg/h
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
40
Flight Planning & Monitoring
101.
4.2.1 )
( For this question use annexes 033-9554A and 033-9554B or Flight Planning Manual MRJT 1 Paragraph 2.1 and Figure
Annex 033-9554A
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
a)
0%
b)
4%
c)
10 %
d)
1%
Answer ;
b)
4%
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
41
Flight Planning & Monitoring
102.
( For this question use annex 033-9553A or Flight Planning Manual MRJT 1 Figure 4.2.1 )
Annex 033-9550A
Find the OPTIMUM ALTITUDE for the twin jet aeroplane.
Given ;
Cruise mass = 50000 kg
.78 MACH
a)
36200 ft
b)
36700 ft
c)
maximum operating altitude
d)
35500 ft
Answer ;
d)
35500 ft
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
42
Flight Planning & Monitoring
103.
( For this question use annex 033-9550A or Flight Planning Manual MRJT 1 Figure 4.2.1 )
Annex 033-9550A
Find the OPTIMUM ALTITUDE for the twin jet aeroplane ;
Given ;
Cruise mass : 54000 kg
Long range cruise or .74 MACH
a)
33800 ft
b)
maximum operating altitude
c)
34500 ft
d)
35300 ft
Answer ;
c)
34500 ft
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
43
Flight Planning & Monitoring
104.
( For this question use annex 033-9550A or Flight Planning Manual MRJT 1 Figure 4.2.2 )
Annex 033-9550A
Find the SHORT DISTANCE CRUISE ALTITUDE for the twin jet aeroplane ;
Given ;
Brake release mass : 40000 kg
Temperature : ISA + 20°C
Trip distance : 150 Nautical Air Miles ( NAM )
a)
27500 ft
b)
30000 ft
c)
21000 ft
d)
25000 ft
Answer ;
b)
30000 ft
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
44
Flight Planning & Monitoring
105.
( For this question use annex 033-9550A or Flight Planning Manual MRJT 1 Figure 4.2.2 )
Annex 033-9550A
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 )
a)
12500 ft
b)
11000 ft
c)
7500 ft
d)
10000 ft
Answer ;
d)
10000 ft
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
45
Flight Planning & Monitoring
106.
( For this question use annex 033-9556A or Flight Planning Manual MRJT 1 Figure 4.14 )
Annex 033-9556A
Find the SPECIFIC RANGE for the twin jet aeroplane flying below the optimum altitude ( range loss = 6% ) and using the
following data ;
Given ;
MACH .74 CRUISE
Flight level : 310
Gross mass : 50000 kg
ISA conditions
a)
2994 NAM/1000 kg
b)
2807 NAM/1000 kg
c)
176 NAM/1000 kg
d)
187 NAM/1000 kg
Answer ;
c)
176 NAM/1000 kg
----------------------------------------------------------------------------------------------------------------------------------------------------------------107.
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
a)
2 h 59 min
b)
2 h 43 min
c)
2 h 51 min
d)
3 h 43 min
Answer ;
c)
2 h 51 min
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
46
Flight Planning & Monitoring
108.
( For this question use annex 033-9564A or Flight Planning Manual MRJT 1 Figure 4.5.1 )
Annex 033-9564A
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
a)
25 min , 1875 kg , 148 Nautical Air Miles ( NAM ) , 391 kt
b)
26 min , 1975 kg , 157 Nautical Air Miles ( NAM ) , 399 kt
c)
20 min , 1750 kg , 117 Nautical Air Miles ( NAM ) , 288 kt
d)
26 min , 2050 kg , 157 Nautical Air Miles ( NAM ) , 399 kt
Answer ;
b)
26 min , 1975 kg , 157 Nautical Air Miles ( NAM ) , 399 kt
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
47
Flight Planning & Monitoring
109.
( For this question use annex 033-9558A )
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 ;
a)
ATC ENDURANCE : 03:37
b)
ATC ENDURANCE : 03:52
c)
ATC ENDURANCE : 04:07
d)
ATC ENDURANCE : 04:12
Answer ;
c)
ATC ENDURANCE : 04:07
----------------------------------------------------------------------------------------------------------------------------------------------------------------110.
Flight planning chart for an aeroplane , states that the time to reach FL 190 at a given gross mass is 22 minutes and the
distance travelled is 66 NM ( no wind ). What will be the distance travelled with a average head wind component of 35 kt ?
a)
61 NM
b)
79 NM
c)
53 NM
d)
85 NM
Answer ;
c)
53 NM
----------------------------------------------------------------------------------------------------------------------------------------------------------------111.
Flight planning chart for an aircraft states that the time to reach the cruising level at a given gross mass is 36 minutes and the
distance travelled is 157 NM ( zero-wind ).What will be the distance travelled with an average tailwind component of 60 kt ?
a)
228 NM
b)
128 NM
c)
193 NM
d)
157 NM
Answer ;
c)
193 NM
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
48
Flight Planning & Monitoring
112.
( For this question use Route Manual VFR+GPS chart ED-6 )
Route Manual VFR+GPS chart ED-6
Flying from EDPJ LAICHINGEN airport ( 48°30'N , 009°38'E ) to EDSZ ROTTWEIL ZEPFENHAN ( 48°12'N , 008°44'E )
. Find magnetic course and the distance ;
a)
Magnetic course 063º , distance 41 NM
b)
Magnetic course 243º , distance 62 NM
c)
Magnetic course 243º , distance 41 NM
d)
Magnetic course 063º , distance 62 NM
Answer ;
c)
Magnetic course 243º , distance 41 NM
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
49
Flight Planning & Monitoring
113.
( For this question use Route Manual VFR+GPS chart ED-6 )
Route Manual VFR+GPS chart ED-6
Flying from EDPJ LAICHINGEN airport ( 48°30'N , 009°38'E ) to EDTM MENGEN airport ( 48°03'N , 009°22'E ). Find
magnetic course and the distance ;
a)
Magnetic course 202º , distance 44 NM
b)
Magnetic course 202º , distance 28 NM
c)
Magnetic course 022º , distance 44 NM
d)
Magnetic course 022º , distance 28 NM
Answer ;
b)
Magnetic course 202º , distance 28 NM
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
50
Flight Planning & Monitoring
114.
( For this question use Route Manual VFR+GPS chart ED-6 )
Route Manual VFR+GPS chart ED-6
Flying from EDSZ ROTTWEIL ZEPFENHAN ( 48°12'N , 008°44'E ) to EDPJ LAICHINGEN airport ( 48°30'N , 009°38'E )
. Determine the highest obstacle within a corridor 5 NM left and 5 NM right of the courseline ;
a)
3612 ft
b)
2852 ft
c)
3760 ft
d)
3278 ft
Answer ;
c)
3760 ft
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
51
Flight Planning & Monitoring
115.
( For this question use Route Manual VFR+GPS chart ED-6 )
Route Manual VFR+GPS chart ED-6
Flying from EDSZ ROTTWEIL ZEPFENHAN ( 48°12'N , 008°44'E ) to EDPJ LAICHINGEN airport ( 48°30'N , 009°38'E )
. Find magnetic course and the distance ;
a)
Magnetic course 243° , distance 41 NM
b)
Magnetic course 063° , distance 41 NM
c)
Magnetic course 243° , distance 62 NM
d)
Magnetic course 063° , distance 62 NM
Answer ;
b)
Magnetic course 063° , distance 41 NM
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
52
Flight Planning & Monitoring
116.
( For this question use Route Manual VFR+GPS chart ED-6 )
Route Manual VFR+GPS chart ED-6
Flying from EDSZ ROTTWEIL ZEPFENHAN ( 48°12'N , 008°44'E ) to EDTM MENGEN airport ( 48°03'N , 009°22'E ).
Determine the highest obstacle within a corridor 5 NM left and 5 NM right of the courseline ;
a)
3760 ft
b)
2920 ft
c)
3331 ft
d)
2605 ft
Answer ;
a)
3760 ft
----------------------------------------------------------------------------------------------------------------------------------------------------------------117.
( For this question use Route Manual VFR+GPS chart ED-6 )
Route Manual VFR+GPS chart ED-6
Flying from EDSZ ROTTWEIL ZEPFENHAN ( 48°12'N , 008°44'E ) to EDTM MENGEN airport ( 48°03'N , 009°22'E ).
Find magnetic course and the distance ;
a)
Magnetic course 288° , distance 27 NM
b)
Magnetic course 108° , distance 40 NM
c)
Magnetic course 288° , distance 40 NM
d)
Magnetic course 108° , distance 27 NM
Answer ;
d)
Magnetic course 108° , distance 27 NM
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
53
Flight Planning & Monitoring
118.
( For this question use Route Manual VFR+GPS chart ED-6 )
Route Manual VFR+GPS chart ED-6
Flying from EDTM MENGEN airport ( 48°03'N , 009°22'E ) to EDPJ LAICHINGEN airport ( 48°30'N , 009°38'E ).
Determine the highest obstacle within a corridor 5 NM left and 5 NM right of the courseline ;
a)
2507 ft
b)
2120 ft
c)
2838 ft
d)
2870 ft
Answer ;
d)
2870 ft
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
54
Flight Planning & Monitoring
119.
( For this question use Route Manual VFR+GPS chart ED-6 )
Route Manual VFR+GPS chart ED-6
Flying from EDTM MENGEN airport ( 48°03'N , 009°22'E ) to EDPJ LAICHINGEN airport ( 48°30'N , 009°38'E ). Find
magnetic course and the distance ;
a)
Magnetic course 022° , distance 28 NM
b)
Magnetic course 202° , distance 28 NM
c)
Magnetic course 202° , distance 44 NM
d)
Magnetic course 022° , distance 44 NM
Answer ;
a)
Magnetic course 022° , distance 28 NM
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
55
Flight Planning & Monitoring
120.
( For this question use Route Manual VFR+GPS chart ED-6 )
Route Manual VFR+GPS chart ED-6
Flying from EDTM MENGEN airport ( 48°03'N , 009°22'E ) to EDSZ ROTTWEIL ZEPFENHAN ( 48°12'N, 008°44'E ).
Find magnetic course and the distance ;
a)
Magnetic course 288° , distance 40 NM
b)
Magnetic course 108° , distance 27 NM
c)
Magnetic course 288° , distance 27 NM
d)
Magnetic course 108° , distance 40 NM
Answer ;
c)
Magnetic course 288° , distance 27 NM
----------------------------------------------------------------------------------------------------------------------------------------------------------------121.
( 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 )
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 ;
a)
Magnetic course 287° , distance 60 NM
b)
Magnetic course 252° , distance 41 NM
c)
Magnetic course 287° , distance 41 NM
d)
Magnetic course 108° , distance 60 NM
Answer ;
c)
Magnetic course 287° , distance 41 NM
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
56
Flight Planning & Monitoring
122.
( 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 )
Route Manual VFR+GPS chart ED-6
Flying from Position SIGMARINGEN ( 48°05'N , 009°13'E ) to BIBERACH airport ( 48°07'N , 009°46'E ). Find magnetic
course and the distance ;
a)
Magnetic course 086° , distance 32 NM
b)
Magnetic course 267° , distance 22 NM
c)
Magnetic course 093° , distance 41 NM
d)
Magnetic course 086° , distance 22 NM
Answer ;
d)
Magnetic course 086° , distance 22 NM
----------------------------------------------------------------------------------------------------------------------------------------------------------------123.
( For this question use annex 033-9722A , AERONAUTICAL CHART ICAO 1:500 000 STUTTGART (NO 47/6) or Route
Manual VFR+GPS chart ED-6 )
Route Manual VFR+GPS chart ED-6
Flying from SAULGAU airport ( 48°02'N , 009°31'E ) to ALTENSTADT airport ( 47°50'N , 010°53'E ). Find magnetic
course and the distance ;
a)
Magnetic course 102° , distance 56 NM
b)
Magnetic course 282° , distance 56 NM
c)
Magnetic course 078° , distance 82 NM
d)
Magnetic course 102° , distance 82 NM
Answer ;
a)
Magnetic course 102° , distance 56 NM
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
57
Flight Planning & Monitoring
124.
( For this question use annex 033-9738A, 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 distance ;
a)
36 NM
b)
58 NM
c)
32 NM
d)
46 NM
Answer ;
c)
32 NM
----------------------------------------------------------------------------------------------------------------------------------------------------------------125.
( For this question use annex 033-9737A , 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 magnetic
course ;
a)
243°
b)
063°
c)
257°
d)
077°
Answer ;
a)
243°
----------------------------------------------------------------------------------------------------------------------------------------------------------------126.
( 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 5 NM left and 5 NM right of the courseline in order to stay 1000 ft clear of obstacles ;
a)
6900 ft
b)
6600 ft
c)
5500 ft
d)
5300 ft
Answer ;
a)
6900 ft
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
58
Flight Planning & Monitoring
127.
( 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 )
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 ;
a)
28 NM
b)
24 km
c)
46 NM
d)
24 NM
Answer ;
d)
24 NM
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
59
Flight Planning & Monitoring
128.
( 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 )
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.
a)
176°
b)
004°
c)
356°
d)
185°
Answer ;
c)
356°
----------------------------------------------------------------------------------------------------------------------------------------------------------------129.
( 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 5 NM left and 5 NM right of the courseline in order to stay 1000 ft clear of obstacles ;
a)
1500 ft
b)
4200 ft
c)
2900 ft
d)
3900 ft
Answer ;
d)
3900 ft
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
60
Flight Planning & Monitoring
130.
Following in-flight depressurisation , a turbine powered aeroplane is forced to divert to an en-route alternate airfield. If
actual
flight conditions are as forecast , the minimum quantity of fuel remaining on arrival at the airfield will be ;
a)
at least equivalent to 30 minutes flying time.
b)
at least equivalent to the quantity required to fly to another aerodrome in the event that weather conditions so
require.
c)
laid down by the operator , with the quantity being specified in the operating manual.
d)
at least equivalent to 45 minutes flying time.
Answer ;
a)
at least equivalent to 30 minutes flying time.
----------------------------------------------------------------------------------------------------------------------------------------------------------------131.
( For this question use annex 033-12341A or Flight Planning Manual MRJT 1 Figure 4.3.1C )
Annex 033-12341A
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 50000 kg
What is the minimum cruise level ( pressure altitude ) which may be planned ?
a)
10000 ft
b)
14000 ft
c)
17000 ft
d)
22000 ft
Answer ;
c)
17000 ft
Ateş Murat Üstünbıçak , ATPL
61
Flight Planning & Monitoring
----------------------------------------------------------------------------------------------------------------------------------------------------------------132.
( For this question use annex 033-12344A or Flight Planning Manual MRJT 1 Figure 4.3.1C )
Annex 033-12344A
For a flight of 2000 ground nautical miles , cruising at 30000 ft , within the limits of the data given , a headwind component
of 25 kt will affect the trip time by approximately ;
a)
-3.6%
b)
+2.3%
c)
+7.6%
d)
+5.3%
Answer ;
c)
+7.6%
Ateş Murat Üstünbıçak , ATPL
62
Flight Planning & Monitoring
----------------------------------------------------------------------------------------------------------------------------------------------------------------133.
( For this question use annex 033-12351A or Flight Planning Manual MRJT 1 Figure 4.3.5 )
Annex 033-12351A
For a flight of 2400 ground nautical miles the following apply ;
Tail wind 25 kt
Temperature ISA - 10°C
Brake release mass 66000 kg
The (a) trip fuel and (b) trip time respectively are ;
a)
(a) 14000 kg , (b) 5 hr 35 min
b)
(a) 15000 kg , (b) 6 hr 00 min
c)
(a) 15800 kg , (b) 6 hr 20 min
d)
(a) 14600 kg , (b) 5 hr 45 min
Answer ;
a)
(a) 14000 kg , (b) 5 hr 35 min
Ateş Murat Üstünbıçak , ATPL
63
Flight Planning & Monitoring
----------------------------------------------------------------------------------------------------------------------------------------------------------------134.
( For this question use annex 033-12349A or Flight Planning Manual MRJT 1 Figure 4.3.1C )
Annex 033-12349A
For a flight of 2400 ground nautical miles the following apply ;
Tail wind component 25 kt
Temperature ISA -10°C
Cruise altitude 31000 ft
Landing mass 52000 kg
The (a) trip fuel and (b) trip time respectively are ;
a)
(a) 12000 kg , (b) 5 hr 15 min
b)
(a) 13600 kg , (b) 6 hr 30 min
c)
(a) 14200 kg , (b) 5 hr 30 min
d)
(a) 16200 kg , (b) 5 hr 45 min
Answer ;
c)
(a) 14200 kg , (b) 5 hr 30 min
Ateş Murat Üstünbıçak , ATPL
64
Flight Planning & Monitoring
----------------------------------------------------------------------------------------------------------------------------------------------------------------135.
( For this question use annex 033-12349A or Flight Planning Manual MRJT 1 Figure 4.3.1C )
Annex 033-12349A
For a flight of 2400 ground nautical miles the following apply ;
Temperature ISA -10°C
Cruise altitude 29000 ft
Landing mass 45000 kg
Trip fuel available 16000 kg
What is the maximum headwind component which may be accepted ?
a)
35 kt
b)
0
c)
70 kt
d)
15 kt
Answer ;
a)
35 kt
Ateş Murat Üstünbıçak , ATPL
65
Flight Planning & Monitoring
----------------------------------------------------------------------------------------------------------------------------------------------------------------136.
( For this question use annex 033-12339A or Flight Planning Manual MRJT 1 Figure 4.3.1C )
Annex 033-12339A
For a flight of 2800 ground nautical miles the following apply ;
Head wind component 15 kt
Temperature ISA + 15°C
Cruise altitude 35000 ft
Landing mass 50000 kg
The (a) trip fuel and (b) trip time respectively are ;
a)
(a) 20000 kg , (b) 7 hr 00 min
b)
(a) 16200 kg , (b) 6 hr 20 min
c)
(a) 17600 kg , (b) 6 hr 50 min
d)
(a) 17000 kg , (b) 6 hr 10 min
Answer ;
c)
(a) 17600 kg , (b) 6 hr 50 min
Ateş Murat Üstünbıçak , ATPL
66
Flight Planning & Monitoring
----------------------------------------------------------------------------------------------------------------------------------------------------------------137.
( For this question use annex 033-12340A or Flight Planning Manual MRJT 1 Figure 4.3.5 )
Annex 033-12340A
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 ;
a)
(a) 15800 kg , (b) 6 hr 15 min
b)
(a) 17000 kg , (b) 6 hr 45 min
c)
(a) 16200 kg , (b) 6 hr 20 min
d)
(a) 18400 kg , (b) 7 hr 00 min
Answer ;
b)
(a) 17000 kg , (b) 6 hr 45 min
Ateş Murat Üstünbıçak , ATPL
67
Flight Planning & Monitoring
----------------------------------------------------------------------------------------------------------------------------------------------------------------138.
( For the question use annex 033-12346A or Flight Planning Manual MRJT 1 Figure 4.3.1C )
Annex 033-12346A
For a flight of 2800 ground nautical miles the following apply ;
Tail wind component 45 kt
Temperature ISA - 10°C
Cruise altitude 29000 ft
Landing mass 55000 kg
The (a) trip fuel (b) trip time respectively are ;
a)
(a) 16000 kg , (b) 6 hr 25 min
b)
(a) 17100 kg , (b) 6 hr 07 min
c)
(a) 20000 kg , (b) 6 hr 40 min
d)
(a) 18000 kg , (b) 5 hr 50 min
Answer ;
b)
(a) 17100 kg , (b) 6 hr 07 min
Ateş Murat Üstünbıçak , ATPL
68
Flight Planning & Monitoring
----------------------------------------------------------------------------------------------------------------------------------------------------------------139.
( For this question use annex 033-12347A or Flight Planning Manual MRJT 1 Figure 4.3.5 )
Annex 033-12347A
For a flight of 3500 ground nautical miles the following apply ;
Tail wind component 50 kt
Temperature ISA +10°C
Brake release mass 65000 kg
The (a) trip fuel and (b) trip time respectively are ;
a)
(a) 21800 kg , (b) 9 hr 25 min
b)
(a) 18100 kg , (b) 7 hr 20 min
c)
(a) 15800 kg , (b) 6 hr 00 min
d)
(a) 19000 kg , (b) 7 hr 45min
Answer ;
b)
(a) 18100 kg , (b) 7 hr 20 min
Ateş Murat Üstünbıçak , ATPL
69
Flight Planning & Monitoring
----------------------------------------------------------------------------------------------------------------------------------------------------------------140.
( For this question use Annex 031-11228A )
Annex 033-11228A
For a long distance flight at FL 370 , “Long Range” regime , divided into four flight legs with the following specifications ;
- segment AB - Ground distance : 2 000 NM. headwind component : 50 kt
- segment BC - Ground distance : 1 000 NM. headwind component : 30 kt
- segment CD - Ground distance : 500 NM. tailwind component : 70 kt
- segment DE - Ground distance : 1 000 NM. headwind component : 20 kt
The total air distance is approximately ;
a)
4 580 NM
b)
4 940 NM
c)
4 800 NM
d)
4 820 NM
Answer ;
c)
4 800 NM
Ateş Murat Üstünbıçak , ATPL
70
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----------------------------------------------------------------------------------------------------------------------------------------------------------------141.
( For this question use Annex 033-11228A )
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 ;
a)
5 040 NM
b)
5 120 NM
c)
4 900 NM
d)
4 630 NM
Answer ;
c)
4 900 NM
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142.
For a planned flight the calculated fuel is as follows ;
Flight time : 3 h 06 min
The reserve fuel , at any time , should not be less than 30% of the remaining trip fuel.
Taxi fuel : 8 kg
Block fuel : 118 kg
How much fuel should remain after 2 hours flight time ?
a)
39 kg trip fuel and 12 kg reserve fuel.
b)
30 kg trip fuel and 9 kg reserve fuel.
c)
27 kg trip fuel and 12 kg reserve fuel.
d)
39 kg trip fuel and no reserve fuel.
Answer ;
b)
30 kg trip fuel and 9 kg reserve fuel.
----------------------------------------------------------------------------------------------------------------------------------------------------------------143.
For a planned flight the calculated fuel is as follows ;
Flight time : 2 h 42 min
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 ?
a)
25 kg trip fuel and 8 kg reserve fuel.
b)
33 kg trip fuel and no reserve fuel.
c)
33 kg trip fuel and 10 kg reserve fuel.
d)
23 kg trip fuel and 10 kg reserve fuel.
Answer ;
a)
25 kg trip fuel and 8 kg reserve fuel.
----------------------------------------------------------------------------------------------------------------------------------------------------------------144.
For a repetitive ATC flight plan ( RPL ) to be used , flights must take place on a regular basis on at least ;
a)
30 occasions.
b)
50 occasions.
c)
20 occasions.
d)
10 occasions.
Answer ;
d)
10 occasions.
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
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145.
( For this question use annex 031-11229A )
Annex 033-11229A
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 ;
a)
37400 ft
b)
38600 ft
c)
34600 ft
d)
37800 ft
Answer ;
a)
37400 ft
----------------------------------------------------------------------------------------------------------------------------------------------------------------146.
For an ATC flight plan filed before the flight , the indicated time of departure is ;
a)
the time at which the flight plan is filed.
b)
the time overhead the first reporting point after take-off.
c)
the estimated off-block time.
d)
the time of take-off.
Answer ;
c)
the estimated off-block time.
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-----------------------------------------------------------------------------------------------------------------------------------------------------------------
147.
For flight planning purposes the landing mass at alternate is taken as ;
a)
Zero Fuel Mass plus Final Reserve Fuel and Alternate Fuel.
b)
Zero Fuel Mass plus Final Reserve Fuel and Contingency Fuel.
c)
Landing Mass at destination plus Alternate Fuel.
d)
Zero Fuel Mass plus Final Reserve Fuel.
Answer ;
b)
Zero Fuel Mass plus Final Reserve Fuel and Contingency Fuel.
----------------------------------------------------------------------------------------------------------------------------------------------------------------148.
( For this question use annex 033- 11045A or Route Manual STAR chart for MADRID BARAJAS (10-2A,B) )
Annex 033-11045A
For runway 33 arrivals from the east and south , the Initial Approach Fix ( IAF ) inbound from airway UR10 is ;
a)
CJN
b)
MOTIL
c)
CENTA
d)
VTB
Answer ;
d)
VTB
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
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Flight Planning & Monitoring
149.
( For this question use annex 033-12364A or Flight Planning Manual MRJT 1 Figure 4.7.2 )
Annex 033-12364A
For the purpose of planning an extended range flight it is required that with a start of diversion mass of 55000 kg 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 ;
a)
LRC
b)
M/KIAS .74/290
c)
M/KIAS .74/330
d)
M/KIAS .70/280
Answer ;
c)
M/KIAS .74/330
---------------------------------------------------------------------------------------------------------------------------------------------------------------150.
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 ;
a)
unclassified “U”
b)
heavy “H”
c)
light “L”
d)
medium “M”
Answer ;
d)
medium “M”
----------------------------------------------------------------------------------------------------------------------------------------------------------------151.
For turbojet engine driven aeroplane , given ;
Taxi fuel 600 kg
Fuel flow for cruise 10 000 kg/h
Fuel flow for holding 8 000 kg/h
Alternate fuel 10 200 kg
Planned flight time to destination 6 h
Forecast visibility at destination 2000 m
The minimum ramp fuel required is ;
a)
77 800 kg
b)
76 100 kg
c)
79 200 kg
d)
80 500 kg
Answer ;
a)
77 800 kg
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152.
From the options given below select those flights which require ATC flight plan notification ;
1.
Any Public Transport flight.
2.
Any IFR flight
3.
Any flight which is to be carried out in regions which are designated to ease the provision of the
Alerting Service or the operations of Search and Rescue.
4.
Any cross-border flights
5.
Any flight which involves overflying water
a)
1,5
b)
2,4
c)
3,4,5
d)
1,2,3
Answer ;
b)
2,4
----------------------------------------------------------------------------------------------------------------------------------------------------------------153.
From which of the following would you expect to find details of the Search and Rescue organisation and procedures
( SAR ) ?
a)
NOTAM
b)
AIP
c)
SIGMET
d)
ATCC broadcasts
Answer ;
b)
AIP
----------------------------------------------------------------------------------------------------------------------------------------------------------------154.
From which of the following would you expect to find facilitation information regarding customs and health formalities ?
a)
NAV/RAD charts
b)
AIP
c)
ATCC
d)
NOTAM
Answer ;
b)
AIP
----------------------------------------------------------------------------------------------------------------------------------------------------------------155.
From which of the following would you expect to find information regarding known short unserviceability of VOR , TACAN
, and NDB ?
a)
ATCC broadcasts
b)
AIP
c)
SIGMET
d)
NOTAM
Answer ;
d)
NOTAM
----------------------------------------------------------------------------------------------------------------------------------------------------------------156.
From which of the following would you expect to find the dates and times when temporary danger areas are active ?
a)
SIGMET
b)
NOTAM and AIP
c)
RAD/NAV charts
d)
Only AIP
Answer ;
b)
NOTAM and AIP
----------------------------------------------------------------------------------------------------------------------------------------------------------------157.
( For this question use annex 033-9721A , AERONAUTICAL CHART ICAO 1:500 000 STUTTGART (NO 47/6) or Route
Manual VFR+GPS chart ED-6 )
Give the frequency of STUTTGART ATIS ;
a)
112.250 MHz
b)
135.775 MHz
c)
126.125 MHz
d)
126.125 kHz
Answer ;
c)
126.125 MHz
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
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158.
( For this question use annex 033-9721A , AERONAUTICAL CHART ICAO 1:500 000 STUTTGART (NO 47/6) or Route
Manual VFR+GPS chart ED-6 )
Give the frequency of ZÜRICH VOLMET ;
a)
127.20 MHz
b)
127.20 kHz
c)
128.525 MHz
d)
118.10 MHz
Answer ;
a)
127.20 MHz
----------------------------------------------------------------------------------------------------------------------------------------------------------------159.
( For this question use annex 033-9721A , AERONAUTICAL CHART ICAO 1:500 000 STUTTGART (NO 47/6) or Route
Manual VFR+GPS chart ED-6 )
Give the name and frequency of the Flight Information Service for an aeroplane in position ( 47°59'N , 010°14'E ) ;
a)
FRANKFURT INFORMATION 128.95 MHz
b)
MEMMINGEN INFORMATION 122.1 MHz
c)
MÜNCHEN INFORMATION 126.95 MHz
d)
MÜNCHEN INFORMATION 120.65 MHz
Answer ;
c)
MÜNCHEN INFORMATION 126.95 MHz
----------------------------------------------------------------------------------------------------------------------------------------------------------------160.
( For this question use annex 033-9716A or Flight Planning Manual SEP 1 Figure 2.4 )
Annex 033-9716A
Given ;
Aeroplane mass at start-up 3663 lbs
Aviation gasoline ( density 6 lbs/gal )-fuel load 74 gal
Take-off altitude sea level
Headwind 40 kt
Cruising altitude 8000 ft
Power setting full throttle 2300 RPM 20°C lean of peak EGT
Calculate the ground range ;
a)
633 NM
b)
547.5 NM
c)
730 NM
d)
844 NM
Answer ;
a)
633 NM
Ateş Murat Üstünbıçak , ATPL
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----------------------------------------------------------------------------------------------------------------------------------------------------------------161.
( 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 ;
a)
19 660 kg
b)
20 260 kg
c)
22 360 kg
d)
21 760 kg
Answer ;
c)
22 360 kg
----------------------------------------------------------------------------------------------------------------------------------------------------------------162.
( For this question use annex 033-3309A or Flight Planning Manual MRJT 1 Figure 4.5.1 )
Annex 033-3307A
Given ;
mass at brake release 57 500 kg
temperature ISA -10°C
average head wind component 16 kt
initial cruise FL 280
Find : Climb fuel ;
a)
1040 kg
b)
1238 kg
c)
1387 kg
d)
1138 kg
Answer ;
d)
1138 kg
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----------------------------------------------------------------------------------------------------------------------------------------------------------------163.
( For this question use annex 033-3307A or Flight Planning Manual MRJT 1 Figure 4.5.1 )
Annex 033-3307A
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 ;
a)
1040 kg
b)
1238 kg
c)
1138 kg
d)
1387 kg
Answer ;
c)
1138 kg
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----------------------------------------------------------------------------------------------------------------------------------------------------------------164.
( For this question use annex 033-3307A or Flight Planning Manual MRJT 1 Figure 4.5.1 )
Annex 033-3307A
Given ;
estimated take-off mass 57 500 kg
initial cruise FL 280
average temperature during climb ISA -10°C;
average head wind component 18 kt
Find : Climb time ;
a)
15 min
b)
13 min
c)
11 min
d)
14 min
Answer ;
b)
13 min
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----------------------------------------------------------------------------------------------------------------------------------------------------------------165.
( For this question use annex 033-3307A or Flight Planning Manual MRJT 1 Figure 4.5.1 )
Annex 033-3307A
Given ;
Brake release mass 57500 kg
Initial FL 280
Average temperature during climb ISA -10°C
Average head wind component 18 kt
Find : Climb time for enroute climb 280/.74 ;
a)
11 min
b)
13 min
c)
15 min
d)
14 min
Answer ;
b)
13 min
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----------------------------------------------------------------------------------------------------------------------------------------------------------------166.
( For this question use annexes 033-3320A , 033-3320B and 033-3320C or Flight Planning Manual MRJT 1 Figures 4.2.1 ,
4.2.2 and 4.5.3.2 )
Annexes 033-3320A , 033-3320B , 033-3320C
Given ;
Estimated take-off mass 57000 kg
Ground distance 150 NM
Temperature ISA -10°C
Cruise at .74 Mach
Find : Cruise altitude and expected true air speed ;
a)
33900 ft , 420 kt
b)
24000 ft , 445 kt
c)
33500 ft , 430 kt
d)
25000 ft , 435 kt
Answer ;
d)
25000 ft , 435 kt
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Flight Planning & Monitoring
----------------------------------------------------------------------------------------------------------------------------------------------------------------167.
( For this question use annexes 033-3320A , 033-3320B and 033-3320C or Flight Planning Manual MRJT 1 Figures 4.2.1 ,
4.2.2 and 4.5.3.2 )
Annexes 033-3320A , 033-3320B , 033-3320C
Given ;
Estimated take-off mass 57 000 kg
Still air distance 150 NAM
Outside air temperature ( OAT ) ISA -10K
Cruise at 0.74 Mach.
Find : Cruise altitude and expected true airspeed ;
a)
22 000 ft , 451 kt
b)
25 000 ft , 435 kt
c)
25 000 ft , 445 kt
d)
22 000 ft , 441 kt
Answer ;
b)
25 000 ft , 435 kt
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168.
( For this question use annex 033-3306A or Flight Planning Manual MRJT 1 Figure 4.5.3.1 )
Annex 033-3306A
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 : 1100 kg
Find : Distance in nautical air miles ( NAM ) for this leg and fuel consumption ;
a)
437 NAM ,2100 kg
b)
345 NAM ,2000 kg
c)
350 NAM ,2000 kg
d)
345 NAM ,2100 kg
Answer ;
b)
345 NAM ;,2000 kg
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
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169.
( For this question use annex 033-4735A or Flight Planning Manual SEP 1 Figure 2.5 )
Annex 033-4735A
Given ;
FL 75
Lean mixture
Full throttle
2300 RPM
Take-off fuel : 444 lbs
Take-off from MSL
Find : Endurance in hours and minutes ;
a)
05:20
b)
05:12
c)
04:42
d)
05:23
Answer ;
b)
05:12
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
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170.
( For this question use annex 033-3321A or Flight Planning Manual MRJT 1 Figure 4.3.1.B )
Annex 033-3321A
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 ;
a)
4 750 kg , 02: 00
b)
4 800 kg , 01: 45
c)
4 600 kg , 02: 05
d)
4 400 kg , 02: 05
Answer ;
b)
25 000 ft , 435 kt
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171.
( For this question use annexes 033-9694A and 033-9694B or Flight Planning Manual MRJT 1 Figure 4.5.3.1 and Figure
4.3.1B )
Annexes 033-9694A , 033-9694B
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 ;
a)
4400 kg , 02 h 05 min
b)
4800 kg , 01 h 51 min
c)
4750 kg , 02 h 00 min
d)
4600 kg , 02 h 05 min
Answer ;
b)
4800 kg , 01 h 51 min
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
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172.
( For this question use annex 033-9697A or Flight Planning Manual MRJT 1 Figure 4.4 )
Annex 033-9697A
Given ;
Twin jet aeroplane
Estimated mass on arrival at the alternate 50000 kg
Elevation at destination aerodrome 3500 ft
Elevation at alternate aerodrome 30 ft
Find : Final reserve fuel ;
a)
1150 kg
b)
1180 kg
c)
2300 kg
d)
2360 kg
Answer ;
b)
1180 kg
----------------------------------------------------------------------------------------------------------------------------------------------------------------173.
( For this question use annex 033-9697A or Flight Planning Manual MRJT 1 Figure 4.4 )
Annex 033-9697A
Given ;
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 ft
Find : Final reserve fuel and corresponding time ;
a)
1180 kg , 45 min
b)
1180 kg , 30 min
c)
2360 kg , 30 min
d)
2360 kg , 01 h 00 min
Answer ;
b)
1180 kg , 30 min
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
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174.
( For this question use annex 033-9697A or Flight Planning Manual MRJT 1 Figure 4.4 )
Annex 033-9697A
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 ;
a)
2 360 kg , destination elevation
b)
1 180 kg , alternate elevation
c)
1 180 kg , destination elevation
d)
2 360 kg , alternate elevation
Answer ;
b)
1 180 kg , alternate elevation
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
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175.
( For this question use annex 033-3322A or Flight Planning Manual MRJT 1 Figure 4.3.6 )
Annex 033-3322A
Given ;
Estimated dry operation mass 35 500 kg
Estimated load 14 500 kg
Final reserve fuel 1200 kg
Distance to alternate 95 NM
Average true track 219°
Head wind component 10 kt
Find : Fuel and time to alternate ;
a)
800 kg , 24 min
b)
1 100 kg , 44 min
c)
1 100 kg , 25 min
d)
800 kg , 40 min
Answer ;
c)
1 100 kg , 25 min
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
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176.
( For this question use annex 033-3305A or Flight Planning Manual MRJT 1 Figure 4.5.3.1 )
Annex 033-3305A
Given ;
long range cruise : temp. -63° C at FL 330
initial gross mass enroute : 54 100 kg
leg flight time : 29 min
Find : Fuel consumption for this leg ;
a)
1 200 kg
b)
1 680 kg
c)
1 100 kg
d)
1 000 kg
Answer ;
c)
1 100 kg
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
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Flight Planning & Monitoring
177.
( For this question use annex 033-4736A or Flight Planning Manual SEP 1 Table 2.2.3 )
Annex 033-4736A
Given ;
FL 70
OAT -19°C
Lean mixture
2300 RPM
Find : Fuel flow in gallons per hour ( GPH ) and TAS ;
a)
12.35 GPH , TAS : 151 kt
b)
73.90 GPH , TAS : 159 kt
c)
11.95 GPH , TAS : 160 kt
d)
12.35 GPH , TAS : 159 kt
Answer ;
d)
12.35 GPH , TAS : 159 kt
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
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Flight Planning & Monitoring
178.
( For this question use annex 033-4736A or Flight Planning Manual SEP 1 Table 2.2.3 )
Annex 033-4736A
Given ;
FL 75
OAT +10°C
Lean mixture
2300 RPM
Find : Fuel flow in gallons per hour ( GPH ) and TAS ;
a)
68.5 GPH , TAS : 160 kt
b)
11.6 GPH , TAS : 143 kt
c)
11.6 GPH , TAS : 160 kt
d)
71.1 GPH , TAS : 143 kt
Answer ;
c)
11.6 GPH , TAS : 160 kt
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
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179.
( For this question use annex 033-9696A or Flight Planning Manual MRJT 1 Figure 4.3.6 )
Given ;
Annex 033-9696A
Twin jet aeroplane
Dry operating mass 35500 kg
Traffic load 14500 kg
Final reserve fuel 1200 kg
Distance to alternate 95 NM
Tailwind component 10 kt
Find : Fuel required and trip time to alternate with simplified flight planning ( ALTERNATE PLANNING ) ;
a)
1000 kg , 24 min
b)
800 kg , 0.4 hr
c)
1000 kg , 40 min
d)
800 kg , 24 min
Answer ;
a)
1000 kg , 24 min
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
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Flight Planning & Monitoring
180.
( For this question use annex 033-9695A or Flight Planning Manual MRJT 1 Figure 4.3.3C )
Annex 033-9695A
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 ;
a)
11600 kg , 04 h 15 min
b)
12000 kg , 03 h 51 min
c)
11400 kg , 04 h 12 min
d)
12400 kg , 04 h 00 min
Answer ;
d)
12400 kg , 04 h 00 min
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
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Flight Planning & Monitoring
181.
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 ;
a)
7000 kg
b)
3000 kg
c)
5600 kg
d)
4000 kg
Answer ;
b)
3000 kg
----------------------------------------------------------------------------------------------------------------------------------------------------------------182.
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
Minimum Take-off Fuel 7400 kg
Find : Maximum allowable take-off fuel ;
a)
14400 kg
b)
11400 kg
c)
8600 kg
d)
11100 kg
Answer ;
d)
11100 kg
----------------------------------------------------------------------------------------------------------------------------------------------------------------183.
( For this question use annex 033-9576A or Route Manual chart E(HI)5 CAA-Edition )
Given ;
Leg Moulins ( N46 42.4 E003 38.0 ) / Dijon ( N47 16.3 E005 05.9 ).
Find : Route designator and total distance ;
a)
UG 21 , 26 NM
b)
UG 21 , 69 NM
c)
Direct route , 69 NM
d)
D , 44 NM
Answer ;
c)
Direct route , 69 NM
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
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184.
( For this question use annex 033-3323A or Flight Planning Manual MRJT 1 Figure 4.3.3C )
Annex 033-3323A
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 ;
a)
12 400 kg , 04 h 12 min
b)
12 400 kg , 03 h 55 min
c)
11 400 kg , 04 h 12 min
d)
11 400 kg , 03 h 55 min
Answer ;
b)
12 400 kg , 03 h 55 min
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
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Flight Planning & Monitoring
185.
( For this question use annexes 033-3307A or Flight Planning Manual MRJT 1 Figure 4.5.1 )
Annex 033-3307A
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 ;
a)
67 NAM , 71 NM
b)
62 NAM , 59 NM
c)
71 NAM , 67 NM
d)
59 NAM , 62 NM
Answer ;
b)
62 NAM , 59 NM
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----------------------------------------------------------------------------------------------------------------------------------------------------------------186.
( For this question use annex 033-3307A or Flight Planning Manual MRJT 1 Figure 4.5.1 )
Annex 033-3307A
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 ;
a)
59 NAM , 62 NM
b)
62 NAM , 59 NM
c)
62 NAM , 71 NM
d)
71 NAM , 67 NM
Answer ;
b)
62 NAM , 59 NM
Ateş Murat Üstünbıçak , ATPL
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Flight Planning & Monitoring
----------------------------------------------------------------------------------------------------------------------------------------------------------------187.
( For this question use annex 033-4737A or Flight Planning Manual SEP 1 Figure 2.1 )
Annex 033-4737A
Given ;
FL 75
OAT +5°C
During climb average head wind component 20 kt
Take-off from MSL with the initial mass of 3 650 lbs.
Find : Still air distance ( NAM ) and ground distance ( NM ) using the graph “time , fuel , distance to climb” ;
a)
16 NAM. , 18 NM.
b)
14 NAM. , 18 NM.
c)
18 NAM. , 13 NM.
d)
18 NAM. , 15 NM.
Answer ;
d)
18 NAM. , 15 NM.
----------------------------------------------------------------------------------------------------------------------------------------------------------------188.
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 ;
a)
14 400 kg
b)
8 600 kg
c)
11 400 kg
d)
11 100 kg
Answer ;
d)
11 100 kg
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----------------------------------------------------------------------------------------------------------------------------------------------------------------189.
Given ;
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
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 ) ;
a)
51.515 kg
b)
55.765 kg
c)
52.265 kg
d)
51.425 kg
Answer ;
a)
51.515 kg
----------------------------------------------------------------------------------------------------------------------------------------------------------------190.
( For this question use annex 033-9715A or Flight Planning Manual SEP 1 Figure 2.1 )
Annex 033-9715A
Given ;
Take-off mass 3500 lbs
Departure aerodrome pressure altitude 2500 ft
OAT +10°C
First cruising level : FL 140 , OAT -5°C
Find the time , fuel and still air distance to climb ;
a)
22 min , 6.7 GAL , 45 NAM
b)
23 min , 7.7 GAL , 50 NAM
c)
24 min , 7.7 GAL , 47 NAM
d)
16.5 min , 4.9 GAL , 34.5 NAM
Answer ;
a)
22 min , 6.7 GAL , 45 NAM
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191.
( For this question use annex 033-4737A or Flight Planning Manual SEP 1 Figure 2.1)
Annex 033-4737A
Given ;
FL 75
OAT +5°C
During climb average head wind component 20 kt
Take-off from MSL with the initial mass of 3650 lbs.
Find : Time and fuel to climb ;
a)
9 min. , 2.7 USG
b)
7 min. , 2.6 USG
c)
9 min. , 3.3 USG
d)
10 min , 3.6 USG
Answer ;
c)
9 min. , 3.3 USG
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192.
( For this question use annex 033-3305A or Flight Planning Manual MRJT 1 Figure 4.5.3.1 )
Annex 033-3305A
Given ;
FL 330
Long range cruise
OAT -63°C
Gross mass 50 500 kg
Find : True airspeed ( TAS )
a)
431 kt
b)
420 kt
c)
418 kt
d)
433 kt
Answer ;
b)
420 kt
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193.
( For this question use annex 033-9691A or Flight Planning Manual MRJT 1 Figure 4.5.3.1 )
Annex 033-9691A
Given ;
Twin jet aeroplane
FL 330
Long range cruise
Outside air temperature -63°C
Gross mass 50500 kg
Find : True air speed ( TAS ) ;
a)
431 kt
b)
418 kt
c)
433 kt
d)
420 kt
Answer ;
d)
420 kt
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
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194.
( For this question use annex 033-9578A or Flight Planning Manual MRJT 1 Figure 4.5.3.1 )
Annex 033-9578A
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 ;
a)
TAS 423 kt , 227 NAM
b)
TAS 433 kt , 227 NAM
c)
TAS 433 kt , 1163 NAM
d)
TAS 423 kt , 936 NAM
Answer ;
b)
TAS 433 kt , 227 NAM
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195.
( For this question use annex 033-3318A or Flight Planning Manual MRJT 1 Figure 4.5.3.1 )
Annex 033-3318A
Given ;
long range cruise
outside air temperature ( OAT ) -45 ° C in FL 350
mass at the beginning of the leg 40 000 kg
mass at the end of the leg 39 000 kg.
Find : True airspeed ( TAS ) at the end of the leg and the distance ( NAM ) ;
a)
TAS 431 kt , 1163 NAM
b)
TAS 423 kt , 227 NAM
c)
TAS 431 kt , 227 NAM
d)
TAS 423 kt , 936 NAM
Answer ;
c)
TAS 431 kt , 227 NAM
----------------------------------------------------------------------------------------------------------------------------------------------------------------196.
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 ) ;
a)
WCA +2° , GS 396 kt
b)
WCA -2° , GS 426 kt
c)
WCA +2° , GS 416 kt
d)
WCA -2° , GS 396 kt
Answer ;
d)
WCA -2° , GS 396 kt
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Flight Planning & Monitoring
197.
( For this question use Image 13 )
Image 13
Given ;
Planned and actual data as shown in the Flight Log excerpt. Actual Ground Speed ( GS ) on the leg BETA to GAMMA will
be 100 KT. If all other flight parameters remain unchanged , what fuel remaining should be expected at waypoint GAMMA ?
a)
2600 kg
b)
2770 kg
c)
2820 kg
d)
2684 kg
Answer ;
a)
2600 kg
----------------------------------------------------------------------------------------------------------------------------------------------------------------198.
( For this question use Image 43 )
Image 43
Given ;
Planned and actual data as shown in the Flight Log excerpt. Actual Ground Speed ( GS ) on the leg BETA to GAMMA will
be 100 KT. If all other flight parameters remain unchanged , what fuel remaining should be expected at waypoint GAMMA ?
a)
3109 kg
b)
3390 kg
c)
3080 kg
d)
2950 kg
Answer ;
d)
2950 kg
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----------------------------------------------------------------------------------------------------------------------------------------------------------------199.
( For this question use Image 44 )
Image 44
Given ;
Planned and actual data as shown in the Flight Log excerpt. Actual Ground Speed ( GS ) on the leg BETA to GAMMA will
be 105 KT. If all other flight parameters remain unchanged , what fuel remaining should be expected at waypoint GAMMA ?
a)
3430 kg
b)
3480 kg
c)
3260 kg
d)
3318 kg
Answer ;
c)
3260 kg
----------------------------------------------------------------------------------------------------------------------------------------------------------------200.
( For this question use Image 40 )
Image 40
Given ;
Planned and actual data as shown in the Flight Log excerpt. Actual Ground Speed ( GS ) on the leg BETA to GAMMA will
be 110 KT. If all other flight parameters remain unchanged , what fuel remaining should be expected at waypoint GAMMA ?
a)
2160 kg
b)
2000 kg
c)
2310 kg
d)
2062 kg
Answer ;
b)
2000 kg
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
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201.
( For this question use Image 42 )
Image 42
Given ;
Planned and actual data as shown in the Flight Log excerpt. Actual Ground Speed ( GS ) on the leg BETA to GAMMA will
be 110 KT. If all other flight parameters remain unchanged , what fuel remaining should be expected at waypoint GAMMA ?
a)
2900 kg
b)
2625 kg
c)
2820 kg
d)
2723 kg
Answer ;
b)
2625 kg
----------------------------------------------------------------------------------------------------------------------------------------------------------------202.
( For this question use Image 41 )
Image 41
Given ;
Planned and actual data as shown in the Flight Log excerpt. Actual Ground Speed ( GS ) on the leg BETA to GAMMA will
be 115 KT. If all other flight parameters remain unchanged , what fuel remaining should be expected at waypoint GAMMA ?
a)
2400 kg
b)
2230 kg
c)
2530 kg
d)
2274 kg
Answer ;
b)
2230 kg
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
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Flight Planning & Monitoring
203.
( For this question use Image 8 )
Image 8
Given ;
Planned and actual data as shown in the Flight Log excerpt. Arriving overhead GAMMA you are cleared for direct routing to
MIKE. The flight time for direct flight GAMMA to MIKE will be 1 hr 06 mins , assuming other flight data remains constant , what
fuel will be expected on arrival overhead MIKE?
a)
1036 kg
b)
1706 kg
c)
2644 kg
d)
1720 kg
Answer ;
b)
1706 kg
----------------------------------------------------------------------------------------------------------------------------------------------------------------204.
( For this question use Image 6 )
Image 6
Given ;
Planned and actual data as shown in the Flight Log excerpt. Arriving overhead GAMMA you are cleared for direct routing to
MIKE. The flight time for direct flight GAMMA to MIKE will be 1 hr 08 mins , assuming other flight data remains constant , what
fuel will be expected on arrival overhead MIKE ?
a)
582 kg
b)
1250 kg
c)
2338 kg
d)
1272 kg
Answer ;
d)
1272 kg
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
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Flight Planning & Monitoring
205.
( For this question use Image 3 )
Image 3
Given ;
Planned and actual data as shown in the Flight Log excerpt. Arriving overhead GAMMA you are cleared for direct routing to
MIKE. The flight time for direct flight GAMMA to MIKE will be 1 hr 10 mins , assuming other flight data remains constant , what
fuel will be expected on arrival overhead MIKE ?
a)
1510 kg
b)
380 kg
c)
2910 kg
d)
1300 kg
Answer ;
d)
1300 kg
----------------------------------------------------------------------------------------------------------------------------------------------------------------206.
( For this question use Image 4 )
Image 4
Given ;
Planned and actual data as shown in the Flight Log excerpt. Arriving overhead GAMMA you are cleared for direct routing to
MIKE. The flight time for direct flight GAMMA to MIKE will be 40 minutes , assuming other flight data remains constant , what fuel
will be expected on arrival overhead MIKE ?
a)
1852 kg
b)
1268 kg
c)
2652 kg
d)
1900 kg
Answer ;
d)
1900 kg
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
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Flight Planning & Monitoring
207.
( For this question use Image 9 )
Image 9
Given ;
Planned and actual data as shown in the Flight Log excerpt. Arriving overhead GAMMA you are cleared for direct routing to
MIKE. The flight time for direct flight GAMMA to MIKE will be 42 minutes , assuming other flight data remains constant , what fuel
will be expected on arrival overhead MIKE ?
a)
1475 kg
b)
2245 kg
c)
1195 kg
d)
670 kg
Answer ;
a)
1475 kg
----------------------------------------------------------------------------------------------------------------------------------------------------------------208.
( For this question use Image 7 )
Image 7
Given ;
Planned and actual data as shown in the Flight Log excerpt. Arriving overhead GAMMA you are cleared for direct routing to
MIKE. The flight time for direct flight GAMMA to MIKE will be 45 minutes , assuming other flight data remains constant , what fuel
will be expected on arrival overhead MIKE ?
a)
1384 kg
b)
252 kg
c)
1002 kg
d)
2082 kg
Answer ;
a)
1384 kg
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
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209.
( For this question use Image 5 )
Image 5
Given ;
Planned and actual data as shown in the Flight Log excerpt. Arriving overhead GAMMA you are cleared for direct routing to
MIKE. The flight time for direct flight GAMMA to MIKE will be 57 minutes , assuming other flight data remains constant , what fuel
will be expected on arrival overhead MIKE ?
a)
2305 kg
b)
1720 kg
c)
1450 kg
d)
790 kg
Answer ;
b)
1720 kg
----------------------------------------------------------------------------------------------------------------------------------------------------------------210.
( For this question use Image 45 )
Image 45
Given ;
Planned and actual data as shown in the Flight Log excerpt. Provided that flight conditions on the leg GAMMA to DELTA
remain unchanged and fuel consumption remains unchanged , what fuel remaining should be expected at waypoint DELTA ?
a)
4220 kg
b)
4430 kg
c)
3800 kg
d)
4340 kg
Answer ;
a)
4220 kg
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
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Flight Planning & Monitoring
211.
( For this question use Image 46 )
Image 46
Given ;
Planned and actual data as shown in the Flight Log excerpt. Provided that flight conditions on the leg GAMMA to DELTA
remain unchanged and fuel consumption remains unchanged , what fuel remaining should be expected at waypoint DELTA ?
a)
4440 kg
b)
4510 kg
c)
4690 kg
d)
4160 kg
Answer ;
c)
4690 kg
----------------------------------------------------------------------------------------------------------------------------------------------------------------212.
( For this question use Image 47 )
Image 47
Given ;
Planned and actual data as shown in the Flight Log excerpt. Provided that flight conditions on the leg GAMMA to DELTA
remain unchanged and fuel consumption remains unchanged , what fuel remaining should be expected at waypoint DELTA ?
a)
4140 kg
b)
4740 kg
c)
4640 kg
d)
4550 kg
Answer ;
d)
4550 kg
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
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Flight Planning & Monitoring
213.
( For this question use Image 48 )
Image 48
Given ;
Planned and actual data as shown in the Flight Log excerpt. Provided that flight conditions on the leg GAMMA to DELTA
remain unchanged and fuel consumption remains unchanged , what fuel remaining should be expected at waypoint DELTA ?
a)
4250 kg
b)
4745 kg
c)
4475 kg
d)
4635 kg
Answer ;
c)
4475 kg
----------------------------------------------------------------------------------------------------------------------------------------------------------------214.
( For this question use Image 49 )
Image 49
Given ;
Planned and actual data as shown in the Flight Log excerpt. Provided that flight conditions on the leg GAMMA to DELTA
remain unchanged and fuel consumption remains unchanged , what fuel remaining should be expected at waypoint DELTA ?
a)
4850 kg
b)
4640 kg
c)
4790 kg
d)
4550 kg
Answer ;
b)
4640 kg
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
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Flight Planning & Monitoring
215.
( For this question use Image 50 )
Image 50
Given ;
Planned and actual data as shown in the Flight Log excerpt. Provided that flight conditions on the leg GAMMA to DELTA
remain unchanged and fuel consumption remains unchanged , what fuel remaining should be expected at waypoint DELTA ?
a)
5090 kg
b)
5010 kg
c)
4940 kg
d)
4690 kg
Answer ;
c)
4940 kg
----------------------------------------------------------------------------------------------------------------------------------------------------------------216.
( For this question use Image 55 )
Image 55
Given ;
Planning data as shown in the Flight Log excerpt ( Fuel Planning Section ). After a balked landing at the destination airport ,
you have to divert to the alternate airport with the gear extended. The re-calculated flight time to the alternate airport with the gear
extended. The re-calculated flight time to the alternate due to the reduced speed is 1 h 50 min and the fuel flow will be 840 kg/h. Final
Reserve Fuel remains unchanged. What will be the estimated landing mass at the alternate airport ?
a)
6530 kg
b)
5530 kg
c)
7390 kg
d)
5890 kg
Answer ;
d)
5890 kg
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----------------------------------------------------------------------------------------------------------------------------------------------------------------217.
( For this question use Image 54 )
Image 54
Given ;
Planning data as shown in the Flight Log excerpt ( Fuel Planning Section ). After a balked landing at the destination airport ,
you have to divert to the alternate airport with the gear extended. The re-calculated flight time to the alternate due to the reduced
speed is 1 h 10 min and the fuel flow will be 600 kg/h. Final Reserve Fuel remains unchanged. What will be the estimated landing
mass at the alternate airport ?
a)
5849 kg
b)
6157 kg
c)
6689 kg
d)
5457 kg
Answer ;
a)
5849 kg
----------------------------------------------------------------------------------------------------------------------------------------------------------------218.
( For this question use Image 12 )
Image 12
Given ;
Planning data as shown in the Flight Log excerpt ( Fuel Planning Section ). After a balked landing at the destination airport ,
you have to divert to the alternate airport with the gear extended. The re-calculated flight time to the alternate due to the reduced
speed is 1 h 10 min and the fuel flow will be 900 kg/h. Final Reserve Fuel remains unchanged. What will be the estimated landing
mass at the alternate airport ?
a)
5987 kg
b)
7427 kg
c)
5510 kg
d)
6470 kg
Answer ;
a)
5987 kg
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----------------------------------------------------------------------------------------------------------------------------------------------------------------219.
( For this question use Image 52 )
Image 52
Given ;
Planning data as shown in the Flight Log excerpt ( Fuel Planning Section ). After a balked landing at the destination airport ,
you have to divert to the alternate airport with the gear extended. The re-calculated flight time to the alternate due to the reduced
speed is 1 h 20 min and the fuel flow will be 720 kg/h. Final Reserve Fuel remains unchanged. What will be the estimated landing
mass at the alternate airport ?
a)
5874 kg
b)
7074 kg
c)
6170 kg
d)
5290 kg
Answer ;
a)
5874 kg
----------------------------------------------------------------------------------------------------------------------------------------------------------------220.
( For this question use Image 53 )
Image 53
Given ;
Planning data as shown in the Flight Log excerpt ( Fuel Planning Section ). After a balked landing at the destination airport ,
you have to divert to the alternate airport with the gear extended. The re-calculated flight time to the alternate due to the reduced
speed is 1 h 20 min and the fuel flow will be 720 kg/h. Final Reserve Fuel remains unchanged. What will be the estimated landing
mass at the alternate airport ?
a)
5669 kg
b)
6175 kg
c)
5320 kg
d)
6749 kg
Answer ;
a)
5669 kg
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----------------------------------------------------------------------------------------------------------------------------------------------------------------221.
( For this question use Image 51 )
Image 51
Given ;
Planning data as shown in the Flight Log excerpt ( Fuel Planning Section ). After a balked landing at the destination airport ,
you have to divert to the alternate airport with the gear extended. The re-calculated flight time to the alternate due to the reduced
speed is 1 h 30 min and the fuel flow will be 600 kg/h. Final Reserve Fuel remains unchanged. What will be the estimated landing
mass at the alternate airport ?
a)
7672 kg
b)
5177 kg
c)
5642 kg
d)
6017 kg
Answer ;
c)
5642 kg
----------------------------------------------------------------------------------------------------------------------------------------------------------------222.
( For this question use Image 10 )
Image 10
Given ;
Planning data as shown in the Flight Log excerpt ( Fuel Planning Section ). After a balked landing at the destination airport ,
you have to divert to the alternate airport with the gear extended. The re-calculated flight time to the alternate due to the reduced
speed is 2 h 20 min and the fuel flow will be 780 kg/h. Final Reserve Fuel remains unchanged. What will be the estimated landing
mass at the alternate airport ?
a)
6070 kg
b)
5080 kg
c)
5440 kg
d)
7240 kg
Answer ;
c)
5440 kg
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----------------------------------------------------------------------------------------------------------------------------------------------------------------223.
( For this question use Flight Planning Manual MRJT 1 Figure 4.7.3 )
Flight Planning Manual MRJT 1 Figure 4.7.3
Given ;
Diversion fuel available 8500 kg
Diversion cruise altitude 10000 ft
Mass at point of diversion 62500 kg
Head wind component 50 kt
Temperature ISA -5°C
The (a) maximum diversion distance , and (b) elapsed time alternate , are approximately ;
a)
(a) 860 NM , (b) 3 h 20 min
b)
(a) 1000 NM , (b) 3 h 40 min
c)
(a) 760 NM , (b) 4 h 30 min
d)
(a) 1130 NM , (b) 3 h 30 min
Answer ;
a)
(a) 860 NM , (b) 3 h 20 min
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224.
( For this question use annex 033-12312A or Flight Planning Manual MRJT 1 Figure 4.3.6 )
Annex 033-12312A
Given ;
Distance to Alternate : 400 NM
Landing mass at Alternate : 50 000 kg
Headwind component : 25 kt
The Alternate fuel required is ;
a)
2800 kg
b)
2550 kg
c)
2900 kg
d)
2650 kg
Answer ;
a)
2800 kg
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225.
( For this question use annex 033-12312A or Flight Planning Manual MRJT 1 Figure 4.3.6 )
Given ;
Annex 033-12312A
Distance to Alternate 450 NM
Landing mass at Alternate : 45 000 kg
Tailwind component : 50 kt
The Alternate fuel required is ;
a)
3050 kg
b)
2750 kg
c)
2900 kg
d)
2500 kg
Answer ;
d)
2500 kg
----------------------------------------------------------------------------------------------------------------------------------------------------------------226.
Given ;
Distance X to Y 2700 NM
Mach Number 0.75
Temperature -45°C
Mean wind component “on” 10 kt tailwind
Mean wind component “back” 35 kt tailwind
The distance from X to the point of equal time ( PET ) between X and Y is ;
a)
1350 NM
b)
1386 NM
c)
1425 NM
d)
1313 NM
Answer ;
b)
1386 NM
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----------------------------------------------------------------------------------------------------------------------------------------------------------------227.
Given ;
Distance A to B 2050 NM
Mean groundspeed “on” 440 kt
Mean groundspeed “back” 540 kt
The distance to the point of equal time ( PET ) between A and B is ;
a)
920 NM
b)
1025 NM
c)
1130 NM
d)
1153 NM
Answer ;
c)
1130 NM
----------------------------------------------------------------------------------------------------------------------------------------------------------------228.
( For this question use Flight Planning Manual MRJT 1 Figure 4.7.3 )
Flight Planning Manual MRJT 1 Figure 4.7.3
Given ;
Diversion distance 650 NM
Diversion pressure altitude 16 000 ft
Mass at point of diversion 57 000 kg
Head wind component 20 kt
Temperature ISA + 15°C
The diversion (a) fuel required and (b) time are approximately ;
a)
(a) 6200 kg , (b) 2 h 10 min
b)
(a) 4400 kg , (b) 1 h 35 min
c)
(a) 4800 kg , (b) 2 h 03 min
d)
(a) 3900 kg , (b) 1 h 45 min
Answer ;
c)
(a) 4800 kg , (b) 2 h 03 min
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229.
Given:
Dry operating mass ( DOM ) : 33510 kg
Traffic Load : 7600 kg
Final reserve fuel : 983 kg
Alternate fuel : 1100 kg
Contingency fuel : 102 kg
The estimated landing mass at alternate should be ;
a)
42312 kg.
b)
42210 kg.
c)
42093 kg.
d)
42195 kg.
Answer ;
d)
42195 kg.
----------------------------------------------------------------------------------------------------------------------------------------------------------------230.
Given ;
Dry operating mass ( DOM ) : 33000 kg
Traffic Load : 8110 kg
Final reserve fuel : 983 kg
Alternate fuel : 1100 kg
Contingency fuel : 102 kg
The estimated landing mass at alternate should be ;
a)
41110 kg.
b)
42210 kg.
c)
42195 kg.
d)
42312 kg.
Answer ;
c)
42195 kg.
----------------------------------------------------------------------------------------------------------------------------------------------------------------231.
Given ;
X = Distance A to point of equal time ( PET ) between A and B
E = Endurance
D = Distance A to B
O = Groundspeed “on”
H = Groundspeed “back”
The formula for calculating the distance X to point of equal time ( PET ) is ;
a)
X=DxH/(O+H)
b)
X=ExH/(O+H)
c)
X=DxO/(O+H)
d)
X=DxOxH/(O+H)
Answer ;
a)
X=DxH/(O+H)
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232.
( For this question use annex 033-12305A or Flight Planning Manual MRJT 1 Figure 4.5.1 )
Annex 033-12305A
Given ;
Brake release mass : 62 000 kg
Temperature : ISA + 15°C
The fuel required for a climb from Sea Level to FL330 is ;
a)
1700 kg
b)
1750 kg
c)
1800 kg
d)
1650 kg
Answer ;
a)
1700 kg
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233.
( 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 )
Annexes 033-12306A , 033-12306B
Given ;
Cruise Mach 0.78 at FL300
Distance B - C : 800 NM
Temperature : - 55°C
Headwind component : 50 kt
Gross mass at B : 64 500 kg
The fuel required from B - C is ;
a)
6090 kg
b)
4975 kg
c)
6125 kg
d)
4945 kg
Answer ;
a)
6090 kg
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234.
( For this question use annexes 033-12308A and 033-12308B or Flight Planning Manual MRJT 1 Figure 4.5.2 and 4.5.3.4 )
Annexes 033-12308A , 033-12308B
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 kg
The fuel required from B - C is ;
a)
1940 kg
b)
2800 kg
c)
2670 kg
d)
1810 kg
Answer ;
a)
1940 kg
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235.
( 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 )
Annexes 033-12307A , 033-12307B
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 ;
a)
5850 kg
b)
6150 kg
c)
7050 kg
d)
7300 kg
Answer ;
b)
6150 kg
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236.
( 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 )
Annexes 033-12302A , 033-12302B
Given ;
Distance C - D : 680 NM
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 ;
a)
3100 kg
b)
3400 kg
c)
3700 kg
d)
4000 kg
Answer ;
c)
3700 kg
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Ateş Murat Üstünbıçak , ATPL
129
Flight Planning & Monitoring
237.
( 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 )
Annexes 033-12302A , 033-12302B
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 ;
a)
14 500 kg
b)
17 500 kg
c)
17 800 kg
d)
14 200 kg
Answer ;
a)
14 500 kg
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
130
Flight Planning & Monitoring
238.
( For this question use annexes 033-12308A and 033-12308B or Flight Planning Manual MRJT 1 Figure 4.5.2 and 4.5.3.4 )
Annexes 033-12308A , 033-12308B
Given ;
Distance C - D : 540 NM
Cruise 300 KIAS at FL 210
Temperature Deviation from ISA : +20°C
Headwind component : 50 kt
Gross mass at C : 60 000 kg
The fuel required from C to D is ;
a)
3350 kg
b)
3680 kg
c)
4200 kg
d)
4620 kg
Answer ;
c)
4200 kg
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
131
Flight Planning & Monitoring
239.
( For this question use annex 033-12304A or Flight Planning Manual MRJT 1 Figure 4.5.1 )
Annex 033-12304A
Given ;
Brake release mass : 58 000 kg
Temperature : ISA + 15
The fuel required to climb from an aerodrome at elevation 4000 ft to FL300 is ;
a)
1450 kg
b)
1250 kg
c)
1350 kg
d)
1400 kg
Answer ;
b)
1250 kg
Ateş Murat Üstünbıçak , ATPL
132
Flight Planning & Monitoring
----------------------------------------------------------------------------------------------------------------------------------------------------------------240.
Given ;
Fuel density : 0.78 kg/l
Dry operating mass : 33500 kg
Traffic load : 10 600 kg
Maximum allowable take-off mass : 66200 kg
Taxi fuel : 200 kg
Tank capacity : 22 500 Litres
The maximum possible take-off fuel is ;
a)
17 350 kg
b)
21 900 kg
c)
17 550 kg
d)
22 100 kg
Answer ;
a)
17 350 kg
----------------------------------------------------------------------------------------------------------------------------------------------------------------241.
( For this question use Flight Planning Manual MRJT 1 Figure 4.7.3 )
Flight Planning Manual MRJT 1 Figure 4.7.3
Given ;
Distance to alternate 950 NM
Head wind component 20 kt
Mass at point of diversion 50000 kg
Diversion fuel available 5800 kg
The minimum pressure altitude at which the above conditions may be met is ;
a)
22000 ft
b)
18000 ft
c)
20000 ft
d)
26000 ft
Answer ;
a)
22000 ft
Ateş Murat Üstünbıçak , ATPL
133
Flight Planning & Monitoring
----------------------------------------------------------------------------------------------------------------------------------------------------------------242.
Given ;
FL 370
M = 0.74
OAT = -47°C
The TAS is ;
a)
415 kt
b)
434 kt
c)
428 kt
d)
424 kt
Answer ;
b)
434 kt
----------------------------------------------------------------------------------------------------------------------------------------------------------------243.
Given ;
Course A to B 088° ( T )
Distance 1250 NM
Mean TAS 330 kt
Mean W/V 340°/60 kt
The time from A to the PET between A and B is ;
a)
2 hours 02 minutes
b)
1 hour 54 minutes
c)
1 hour 39 minutes
d)
1 hour 43 minutes
Answer ;
d)
1 hour 43 minutes
----------------------------------------------------------------------------------------------------------------------------------------------------------------244.
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 ;
a)
5 hours 20 minutes
b)
3 hours 55 minutes
c)
5 hours 45 minutes
d)
5 hours 31 minutes
Answer ;
d)
5 hours 31 minutes
----------------------------------------------------------------------------------------------------------------------------------------------------------------245.
Given ;
Distance from departure to destination 270 NM
True track 030
W/V 120/35
TAS 125 kt
What is the distance and time of the PET from the departure point ?
a)
Distance : 141 NM Time : 68 min
b)
Distance : 141 NM Time : 65 min
c)
Distance : 130 NM Time : 68 min
d)
Distance : 135 NM Time : 68 min
Answer ;
d)
Distance : 135 NM Time : 68 min
----------------------------------------------------------------------------------------------------------------------------------------------------------------246.
Given ;
Distance from departure to destination 338 NM
True track 045
W/V 225/35
TAS 120 kt
What is the distance and time of the PET from the departure point ?
a)
Distance : 185 NM Time : 72 min
b)
Distance : 120 NM Time : 46 min
c)
Distance : 218 NM Time : 85 min
d)
Distance : 169 NM Time : 85 min
Answer ;
b)
Distance : 120 NM Time : 46 min
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
134
Flight Planning & Monitoring
247.
Given ;
Distance from departure to destination 350 NM
True track 320
W/V 350/30
TAS 130 kt
What is the distance and time of the PET from the departure point ?
a)
Distance : 210 NM Time : 122 min
b)
Distance : 139 NM Time : 54 min
c)
Distance : 139 NM Time : 81 min
d)
Distance : 123 NM Time : 74 min
Answer ;
a)
Distance : 210 NM Time : 122 min
----------------------------------------------------------------------------------------------------------------------------------------------------------------248.
Given ;
Distance from departure to destination 500 NM
True track 090
W/V 090/20
TAS 150 kt
What is the distance and time of the PET from the departure point ?
a)
Distance : 250 NM Time : 88 min
b)
Distance : 283 NM Time : 131 min
c)
Distance : 382 NM Time : 176min
d)
Distance : 217 NM Time : 100 min
Answer ;
b)
Distance : 283 NM Time : 131 min
----------------------------------------------------------------------------------------------------------------------------------------------------------------249.
Given ;
Distance from departure to destination 875 NM
True track 240
W/V 060/50
TAS 500 kt
What is the distance and time of the PET from the departure point ?
a)
Distance : 716 NM Time : 78 min
b)
Distance : 481 NM Time : 64 min
c)
Distance : 394 NM Time : 43 min
d)
Distance : 438 NM Time : 53 min
Answer ;
c)
Distance : 394 NM Time : 43 min
----------------------------------------------------------------------------------------------------------------------------------------------------------------250.
Given ;
Distance from departure to destination 1100 NM
True track 280
W/V 100/80
TAS 440 kt
What is the distance and time of the PET from the departure point ?
a)
Distance : 450 NM Time : 52 min
b)
Distance : 650 NM Time : 75 min
c)
Distance : 550 NM Time : 75 min
d)
Distance : 650 NM Time : 108 min
Answer ;
a)
Distance : 450 NM Time : 52 min
----------------------------------------------------------------------------------------------------------------------------------------------------------------251.
Given ;
Distance from departure to destination 2200 NM
True track 150
W/V 330/50
TAS 460 kt
What is the distance and time of the PET from the departure point ?
a)
Distance : 980 NM Time : 144 min
b)
Distance : 1100 NM Time : 179 min
c)
Distance : 1120 NM Time : 179 min
d)
Distance : 980 NM Time : 115 min
Answer ;
d)
Distance : 980 NM Time : 115 min
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
135
Flight Planning & Monitoring
252.
Given ;
Distance from departure to destination 2800 NM
True track 140
W/V 140/100
TAS 500 kt
What is the distance and time of the PET from the departure point ?
a)
Distance : 1120 NM Time : 134 min
b)
Distance : 1400 NM Time : 168 min
c)
Distance : 1680 NM Time : 252 min
d)
Distance : 1120 NM Time : 112 min
Answer ;
c)
Distance : 1680 NM Time : 252 min
----------------------------------------------------------------------------------------------------------------------------------------------------------------253.
Given ;
Distance from departure to destination : 150 NM
Safe Endurance : 3.2 h
TAS : 90 kt
Ground Speed Out : 100 kt
Ground Speed Home : 80 kt
What is the distance and time of the PSR from the departure point ?
a)
Distance : 71 NM Time : 47 min
b)
Distance : 8 NM Time : 5 min
c)
Distance : 67 NM Time : 50 min
d)
Distance : 142 NM Time : 85 min
Answer ;
d)
Distance : 142 NM Time : 85 min
----------------------------------------------------------------------------------------------------------------------------------------------------------------254.
Given ;
Distance from departure to destination : 180 NM
Endurance : 2 h
TAS : 120 kt
Ground Speed Out : 135 kt
Ground Speed Home : 105 kt
What is the distance and time of the PSR from the departure point ?
a)
Distance : 79 NM Time : 45 min
b)
Distance : 118 NM Time : 53 min
c)
Distance : 59 NM Time : 30 min
d)
Distance : 62 NM Time : 28 min
Answer ;
b)
Distance : 118 NM Time : 53 min
----------------------------------------------------------------------------------------------------------------------------------------------------------------255.
Given ;
Distance from departure to destination : 240 NM
Safe Endurance : 3.5 h
TAS : 125 kt
Ground Speed Out : 110 kt
Ground Speed Home : 140 kt
What is the distance and time of the PSR from the departure point ?
a)
Distance : 108 NM Time : 52 min
b)
Distance : 134 NM Time : 58 min
c)
Distance : 216 NM Time : 118 min
d)
Distance : 24 NM Time : 13 min
Answer ;
c)
Distance : 216 NM Time : 118 min
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
136
Flight Planning & Monitoring
256.
Given ;
Distance from departure to destination : 500 NM
Safe Endurance : 4 h
TAS : 140 kt
Ground Speed Out : 150 kt
Ground Speed Home : 130 kt
What is the distance and time of the PSR from the departure point ?
a)
Distance : 232 NM Time : 107 min
b)
Distance : 221 NM Time : 89 min
c)
Distance : 279 NM Time : 111 min
d)
Distance : 139 NM Time : 60 min
Answer ;
c)
Distance : 279 NM Time : 111 min
----------------------------------------------------------------------------------------------------------------------------------------------------------------257.
Given ;
Distance from departure to destination : 950 NM
Safe Endurance : 3.5 h
TAS : 360 kt
Ground Speed Out : 320 kt
Ground Speed Home : 400 kt
What is the distance and time of the PSR from the departure point ?
a)
Distance : 311 NM Time : 52 min
b)
Distance : 622 NM Time : 117 min
c)
Distance : 328 NM Time : 62 min
d)
Distance : 528 NM Time : 79 min
Answer ;
b)
Distance : 622 NM Time : 117 min
----------------------------------------------------------------------------------------------------------------------------------------------------------------258.
Given ;
Distance from departure to destination 95 NM
True track 105
W/V 060/15
TAS 140 kt
What is the distance of the PET from the departure point ?
a)
51 NM
b)
47.5 NM
c)
82 NM
d)
44 NM
Answer ;
a)
51 NM
----------------------------------------------------------------------------------------------------------------------------------------------------------------259.
Given ;
Distance from departure to destination 140 NM
GS Out 90 kt
GS Home 80 kt
What is the distance of the PET from the departure point ?
a)
124 NM
b)
66 NM
c)
70 NM
d)
74 NM
Answer ;
b)
66 NM
----------------------------------------------------------------------------------------------------------------------------------------------------------------260.
Given ;
Distance from departure to destination 150 NM
True track 142
W/V 200/15
TAS 132 kt
What is the distance of the PET from the departure point ?
a)
79 NM
b)
134 NM
c)
75 NM
d)
71 NM
Answer ;
a)
79 NM
Ateş Murat Üstünbıçak , ATPL
137
Flight Planning & Monitoring
----------------------------------------------------------------------------------------------------------------------------------------------------------------261.
Given ;
Distance from departure to destination 150 NM
True track 020
W/V 180/30
TAS 130 kt
What is the distance of the PET from the departure point ?
a)
91 NM
b)
59 NM
c)
75 NM
d)
65 NM
Answer ;
b)
59 NM
----------------------------------------------------------------------------------------------------------------------------------------------------------------262.
Given ;
Distance from departure to destination 165 NM
True track 055
W/V 360/20
TAS 105 kt
What is the distance of the PET from the departure point ?
a)
73 NM
b)
83 NM
c)
92 NM
d)
132 NM
Answer ;
c)
92 NM
----------------------------------------------------------------------------------------------------------------------------------------------------------------263.
Given ;
Distance from departure to destination 180 NM
True track 310
W/V 010/20
TAS 115 kt
What is the distance of the PET from the departure point ?
a)
92 NM
b)
82 NM
c)
90 NM
d)
98 NM
Answer ;
d)
98 NM
----------------------------------------------------------------------------------------------------------------------------------------------------------------264.
Given ;
Distance from departure to destination 220 NM
True track 175
W/V 220/10
TAS 135 kt
What is the distance of the PET from the departure point ?
a)
103 NM
b)
136 NM
c)
116 NM
d)
110 NM
Answer ;
c)
116 NM
----------------------------------------------------------------------------------------------------------------------------------------------------------------265.
Given ;
Distance from departure to destination 250 NM
GS Out 130 kt
GS Home 100 kt
What is the distance of the PET from the departure point ?
a)
192 NM
b)
109 NM
c)
141 NM
d)
125 NM
Answer ;
b)
109 NM
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
138
Flight Planning & Monitoring
266.
Given ;
Distance from departure to destination 256 NM
GS Out 160 kt
GS Home 110 kt
What is the distance of the PET from the departure point ?
a)
176 NM
b)
104 NM
c)
128 NM
d)
152 NM
Answer ;
b)
104 NM
----------------------------------------------------------------------------------------------------------------------------------------------------------------267.
Given ;
Distance from departure to destination 285 NM
True track 348
W/V 280/25
TAS 128 kt
What is the distance of the PET from the departure point ?
a)
153 NM
b)
123 NM
c)
131 NM
d)
143 NM
Answer ;
a)
153 NM
----------------------------------------------------------------------------------------------------------------------------------------------------------------268.
Given ;
Distance from departure to destination 315 NM
True track 343
W/V 015/15
TAS 100 kt
What is the distance of the PET from the departure point ?
a)
176 NM
b)
148 NM
c)
139 NM
d)
167 NM
Answer ;
a)
176 NM
----------------------------------------------------------------------------------------------------------------------------------------------------------------269.
Given ;
Distance from departure to destination 340 NM
True track 320
W/V 160/40
TAS 110 kt
What is the distance of the PET from the departure point ?
a)
219 NM
b)
121 NM
c)
228 NM
d)
112 NM
Answer ;
d)
112 NM
----------------------------------------------------------------------------------------------------------------------------------------------------------------270.
Given ;
Distance from departure to destination 340 NM
GS Out 150 kt
GS Home 120 kt
What is the distance of the PET from the departure point ?
a)
189 NM
b)
151 NM
c)
170 NM
d)
272 NM
Answer ;
b)
151 NM
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
139
Flight Planning & Monitoring
271.
Given ;
Distance from departure to destination 435 NM
GS Out 110 kt
GS Home 130 kt
What is the distance of the PET from the departure point ?
a)
199 NM
b)
236 NM
c)
218 NM
d)
368 NM
Answer ;
b)
236 NM
----------------------------------------------------------------------------------------------------------------------------------------------------------------272.
Given ;
Distance from departure to destination 470 NM
True track 237
W/V 300/25
TAS 125 kt
What is the distance of the PET from the departure point ?
a)
235 NM
b)
214 NM
c)
256 NM
d)
205 NM
Answer ;
c)
256 NM
----------------------------------------------------------------------------------------------------------------------------------------------------------------273.
Given ;
Distance from departure to destination 500 NM
GS Out 95 kt
GS Home 125 kt
What is the distance of the PET from the departure point ?
a)
216 NM
b)
380 NM
c)
284 NM
d)
250 NM
Answer ;
c)
284 NM
----------------------------------------------------------------------------------------------------------------------------------------------------------------274.
Given ;
Distance from departure to destination : 150 NM
Safe Endurance : 2.4 h
True Track : 250
W/V : 280/15
TAS : 120 kt
What is the distance of the PSR from the departure point ?
a)
98 NM
b)
83 NM
c)
142 NM
d)
71 NM
Answer ;
c)
142 NM
----------------------------------------------------------------------------------------------------------------------------------------------------------------275.
Given ;
Distance from departure to destination : 180 NM
Safe Endurance : 2.8 h
True Track : 065
W/V : 245/25
TAS : 100 kt
What is the distance of the PSR from the departure point ?
a)
49 NM
b)
68 NM
c)
66 NM
d)
131 NM
Answer ;
d)
131 NM
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
140
Flight Planning & Monitoring
276.
Given ;
Distance from departure to destination : 190 NM
Safe Endurance : 2.4 h
True Track : 120
W/V : 030/40
TAS : 130 kt
What is the distance of the PSR from the departure point ?
a)
44 NM
b)
73 NM
c)
148 NM
d)
95 NM
Answer ;
c)
148 NM
---------------------------------------------------------------------------------------------------------------------------------------------------------------277.
Given ;
Distance from departure to destination : 200 NM
Safe Endurance : 3 h
TAS : 130 kt
Ground Speed Out : 150 kt
Ground Speed Home : 110 kt
What is the distance of the PSR from the departure point ?
a)
85 NM
b)
95 NM
c)
190 NM
d)
10 NM
Answer ;
c)
190 NM
----------------------------------------------------------------------------------------------------------------------------------------------------------------278.
Given ;
Distance from departure to destination : 210 NM
Safe Endurance : 2.5 h
True Track : 035
W/V : 250/20
TAS : 105 kt
What is the distance of the PSR from the departure point ?
a)
172 NM
b)
64 NM
c)
88 NM
d)
127 NM
Answer ;
d)
127 NM
----------------------------------------------------------------------------------------------------------------------------------------------------------------279.
Given ;
Distance from departure to destination : 210 NM
Safe Endurance : 3.5 h
True Track : 310
W/V : 270/30
TAS : 120 kt
What is the distance of the PSR from the departure point ?
a)
10 NM
b)
200 NM
c)
125 NM
d)
100 NM
Answer ;
b)
200 NM
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
141
Flight Planning & Monitoring
280.
Given ;
Distance from departure to destination : 215 NM
Safe Endurance : 3.3 h
True Track : 005
W/V : 290/15
TAS : 125 kt
What is the distance of the PSR from the departure point ?
a)
112 NM
b)
103 NM
c)
205 NM
d)
9 NM
Answer ;
c)
205 NM
----------------------------------------------------------------------------------------------------------------------------------------------------------------281.
Given ;
Distance from departure to destination : 260 NM
Safe Endurance : 4.1 h
True Track :150
W/V : 100/30
TAS : 110 kt
What is the distance of the PSR from the departure point ?
a)
107 NM
b)
47 NM
c)
213 NM
d)
154 NM
Answer ;
c)
213 NM
----------------------------------------------------------------------------------------------------------------------------------------------------------------282.
Given ;
Distance from departure to destination : 300 NM
Safe Endurance : 4 h
TAS : 110 kt
Ground Speed Out : 120 kt
Ground Speed Home : 100 kt
What is the distance of the PSR from the departure point ?
a)
136 NM
b)
109 NM
c)
218 NM
d)
82 NM
Answer ;
c)
218 NM
----------------------------------------------------------------------------------------------------------------------------------------------------------------283.
Given ;
Distance from departure to destination : 320 NM
Safe Endurance : 4.3 h
True Track : 120
W/V : 180/40
TAS : 130 kt
What is the distance of the PSR from the departure point ?
a)
185 NM
b)
262 NM
c)
131NM
d)
59 NM
Answer ;
b)
262 NM
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
142
Flight Planning & Monitoring
284.
Given ;
Distance from departure to destination : 330 NM
Safe Endurance : 5 h
True Track : 170
W/V : 140/25
TAS : 125 kt
What is the distance of the PSR from the departure point ?
a)
30 NM
b)
194 NM
c)
303 NM
d)
150 NM
Answer ;
c)
303 NM
----------------------------------------------------------------------------------------------------------------------------------------------------------------285.
Given ;
Distance from departure to destination : 360 NM
Safe Endurance : 4.5 h
True Track : 345
W/V : 260/30
TAS : 140 kt
What is the distance of the PSR from the departure point ?
a)
308 NM
b)
52NM
c)
154 NM
d)
185 NM
Answer ;
a)
308 NM
----------------------------------------------------------------------------------------------------------------------------------------------------------------286.
Given ;
Distance from departure to destination : 400 NM
Safe Endurance : 2.5 h
TAS : 115 kt
Ground Speed Out : 130 kt
Ground Speed Home : 105 kt
What is the distance of the PSR from the departure point ?
a)
255 NM
b)
179 NM
c)
145 NM
d)
73 NM
Answer ;
c)
145 NM
----------------------------------------------------------------------------------------------------------------------------------------------------------------287.
Given ;
Distance from departure to destination : 410 NM
Safe Endurance : 3.6 h
True Track : 055
W/V : 180/35
TAS : 120 kt
What is the distance of the PSR from the departure point ?
a)
102 NM
b)
169 NM
c)
203 NM
d)
207 NM
Answer ;
c)
203 NM
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
143
Flight Planning & Monitoring
288.
Given ;
Distance from departure to destination : 480 NM
Safe Endurance : 5 h
True Track : 315
W/V : 100/20
TAS : 115 kt
What is the distance of the PSR from the departure point ?
a)
205 NM
b)
199 NM
c)
141 NM
d)
280 NM
Answer ;
d)
280 NM
----------------------------------------------------------------------------------------------------------------------------------------------------------------289.
Given ;
Distance from departure to destination : 550 NM
Endurance : 3.6 h
True Track : 200
W/V : 220/15
TAS : 130 kt
What is the distance of the PSR from the departure point ?
a)
319 NM
b)
116 NM
c)
231 NM
d)
305 NM
Answer ;
c)
231 NM
----------------------------------------------------------------------------------------------------------------------------------------------------------------290.
Given ;
Distance from departure to destination : 1000 NM
Safe Endurance : 4 h
TAS : 500 kt
Ground Speed Out : 550 kt
Ground Speed Home : 450 kt
What is the distance of the PSR from the departure point ?
a)
450 NM
b)
990 NM
c)
10 NM
d)
495 NM
Answer ;
b)
990 NM
----------------------------------------------------------------------------------------------------------------------------------------------------------------291.
Given ;
Distance from departure to destination : 2000 NM
Endurance : 5 h
TAS : 500 kt
Ground Speed Out : 480 kt
Ground Speed Home : 520 kt
What is the distance of the PSR from the departure point ?
a)
752 NM
b)
624 NM
c)
1040 NM
d)
1248 NM
Answer ;
d)
1248 NM
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
144
Flight Planning & Monitoring
292.
Given ;
Distance from departure to destination : 3750 NM
Safe Endurance : 9.5 h
True Track : 360
W/V : 360/50
TAS : 480 kt
What is the distance of the PSR from the departure point ?
a)
2070 NM
b)
1128 NM
c)
2255 NM
d)
1495 NM
Answer ;
c)
2255 NM
----------------------------------------------------------------------------------------------------------------------------------------------------------------293.
Given ;
Distance from departure to destination : 4630 NM
Safe Endurance : 12.4 h
True Track : 240
W/V : 060/80
TAS : 530 kt
What is the distance of the PSR from the departure point ?
a)
1419 NM
b)
3211 NM
c)
6106 NM
d)
1966 NM
Answer ;
b)
3211 NM
----------------------------------------------------------------------------------------------------------------------------------------------------------------294.
Given ;
Distance from departure to destination : 5000 NM
Safe Endurance : 10 h
TAS : 450 kt
Ground Speed Out : 500 kt
Ground Speed Home : 400 kt
What is the distance of the PSR from the departure point ?
a)
2500 NM
b)
1111 NM
c)
2778 NM
d)
2222 NM
Answer ;
d)
2222 NM
----------------------------------------------------------------------------------------------------------------------------------------------------------------295.
Given ;
Distance from departure to destination : 6340 NM
Safe Endurance : 15 h
True Track : 090
W/V : 270/100
TAS : 520 kt
What is the distance of the PSR from the departure point ?
a)
1878 NM
b)
3756 NM
c)
2584 NM
d)
2560 NM
Answer ;
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
145
Flight Planning & Monitoring
296.
( For this question use Flight Planning Manual MRJT 1 Figure 4.7.3 )
Flight Planning Manual MRJT 1 Figure 4.7.3
Given ;
Diversion distance 720 NM
Tail wind component 25 kt
Mass at point of diversion 55000 kg
Temperature ISA
Diversion fuel available 4250 kg
What is the minimum pressure altitude at which the above conditions may be met ?
a)
14500 ft
b)
20000 ft
c)
25000 ft
d)
16000 ft
Answer ;
c)
25000 ft
Ateş Murat Üstünbıçak , ATPL
146
Flight Planning & Monitoring
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
297.
Given ;
Distance from departure to destination 950 NM
GS Out 275 kt
GS Home 225 kt
What is the time of the PET from the departure point ?
a)
39 min
b)
139 min
c)
93 min
d)
114 min
Answer ;
c)
93 min
----------------------------------------------------------------------------------------------------------------------------------------------------------------298.
Given ;
Distance from departure to destination 1345 NM
GS Out 480 kt
GS Home 360 kt
What is the time of the PET from the departure point ?
a)
128 min
b)
50 min
c)
72 min
d)
96 min
Answer ;
c)
72 min
----------------------------------------------------------------------------------------------------------------------------------------------------------------299.
Given ;
Distance from departure to destination 1860 NM
GS Out 360 kt
GS Home 400 kt
What is the time of the PET from the departure point ?
a)
132 min
b)
22 min
c)
147 min
d)
163 min
Answer ;
d)
163 min
----------------------------------------------------------------------------------------------------------------------------------------------------------------300.
Given ;
Distance from departure to destination 1950 NM
GS Out 400 kt
GS Home 300 kt
What is the time of the PET from the departure point ?
a)
125 min
b)
223 min
c)
167 min
d)
29 min
Answer ;
a)
125 min
----------------------------------------------------------------------------------------------------------------------------------------------------------------301.
Given ;
Distance from departure to destination 2380 NM
GS Out 420 kt
GS Home 520 kt
What is the time of the PET from the departure point ?
a)
19 min
b)
188 min
c)
152 min
d)
123 min
Answer ;
b)
188 min
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
147
Flight Planning & Monitoring
302.
Given ;
Distance from departure to destination 2500 NM
GS Out 540 kt
GS Home 470 kt
What is the time of the PET from the departure point ?
a)
129 min
b)
171 min
c)
149 min
d)
28 min
Answer ;
a)
129 min
----------------------------------------------------------------------------------------------------------------------------------------------------------------303.
Given ;
Distance from departure to destination : 1500 NM
Safe Endurance : 4.5 h
TAS : 450 kt
Ground Speed Out : 480 kt
Ground Speed Home : 410 kt
What is the time of the PSR from the departure point ?
a)
101 min
b)
124 min
c)
63 min
d)
66 min
Answer ;
b)
124 min
----------------------------------------------------------------------------------------------------------------------------------------------------------------304.
Given ;
Distance from departure to destination : 2450 NM
Safe Endurance : 7.5 h
TAS : 410 kt
Ground Speed Out : 360 kt
Ground Speed Home : 460 kt
What is the time of the PSR from the departure point ?
a)
111 min
b)
252 min
c)
156 min
d)
198 min
Answer ;
b)
252 min
----------------------------------------------------------------------------------------------------------------------------------------------------------------305.
Given ;
Distance from departure to destination : 3000 NM
Safe Endurance : 8 h
TAS : 520 kt
Ground Speed Out : 600 kt
Ground Speed Home : 440 kt
What is the time of the PSR from the departure point ?
a)
277 min
b)
117 min
c)
203 min
d)
173 min
Answer ;
c)
203 min
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
148
Flight Planning & Monitoring
306.
Given ;
Dry operating mass ( DOM ) : 33510 kg
Traffic Load : 7600 kg
Trip fuel ( TF ) : 2040 kg
Final reserve fuel : 983 kg
Alternate fuel : 1100 kg
Contingency fuel : 5% of trip fuel
Which of the listed estimated masses is correct ?
a)
Estimated take-off mass = 45233 kg.
b)
Estimated landing mass at destination = 43193 kg.
c)
Estimated landing mass at destination = 43295 kg.
d)
Estimated take-off mass = 43295 kg.
Answer ;
c)
Estimated landing mass at destination = 43295 kg.
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
149
Flight Planning & Monitoring
307.
( For this question use annexes 033-11224A , 033-11224B and 033-11224C )
Annexes 033-11224A , 033-11224B , 033-11224C
Given ;
Take-off mass : 150 000 kg
Planned cruise at FL 350
Long range MACH
Standard Atmosphere ( ISA )
CG : 37 %
You have to cover an air distance of 2 000 NM. Your flight time will be ;
a)
298 minutes
b)
304 minutes
c)
359 minutes
d)
288 minutes
Answer ;
b)
304 minutes
Ateş Murat Üstünbıçak , ATPL
150
Flight Planning & Monitoring
----------------------------------------------------------------------------------------------------------------------------------------------------------------308.
( For this question use Annex 033-12345A or Flight Planning Manual MRJT 1 Figure 4.3.5 )
Annex 033-12345A
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 ;
a)
+3%
b)
+ 7%
c)
-4%
d)
-10%
Answer ;
b)
+ 7%
Ateş Murat Üstünbıçak , ATPL
151
Flight Planning & Monitoring
----------------------------------------------------------------------------------------------------------------------------------------------------------------309.
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 ;
a)
X = D x GSr / ( GSo + GSr )
b)
X = ( D/2 ) x GSo / ( GSo + GSr )
c)
X = ( D/2 ) + GSr / ( GSo + GSr )
d)
X = D x GSo / ( GSo + GSr )
Answer ;
a)
X = D x GSr / ( GSo + GSr )
----------------------------------------------------------------------------------------------------------------------------------------------------------------310.
( For this question use annex.033-12342A or Flight Planning Manual MRJT 1 Figure 4.3.5 )
Annex 033-12342A
Given the following ;
Head wind component 50 kt
Temperature ISA + 10°C
Brake release mass 65000 kg
Trip fuel available 18000 kg
What is the maximum possible trip distance ?
a)
3480 NM
b)
2740 NM
c)
2540 NM
d)
3100 NM
Answer ;
b)
2740 NM
Ateş Murat Üstünbıçak , ATPL
152
Flight Planning & Monitoring
----------------------------------------------------------------------------------------------------------------------------------------------------------------311.
( For this question use annex 033-12310A or Flight Planning Manual MRJT 1 Figure 4.4 )
Annex 033-12310A
HOLDING PLANNING ;
The fuel required for 30 minutes holding , in a racetrack pattern , at PA 1500 ft , mean gross mass 45 000 kg , is ;
a)
1310 kg
b)
1090 kg
c)
1010 kg
d)
2180 kg
Answer ;
b)
1090 kg
----------------------------------------------------------------------------------------------------------------------------------------------------------------312.
( For this question use annex 033-12310A or Flight Planning Manual MRJT 1 Figure 4.4 )
Annex 033-12310A
HOLDING PLANNING ;
The fuel required for 45 minutes holding , in a racetrack pattern , at PA 5000 ft , mean gross mass 47 000 kg , is ;
a)
1090 kg
b)
1635 kg
c)
1125 kg
d)
1690 kg
Answer ;
b)
1635 kg
----------------------------------------------------------------------------------------------------------------------------------------------------------------313.
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
a)
6300 ft.
b)
6600 ft.
c)
7800 ft.
d)
6000 ft.
Answer ;
a)
6300 ft.
----------------------------------------------------------------------------------------------------------------------------------------------------------------314.
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 ) ?
a)
1:00 hour.
b)
3:00 hours.
c)
0:30 hours.
d)
2 hours.
Answer ;
b)
3:00 hours.
Ateş Murat Üstünbıçak , ATPL
153
Flight Planning & Monitoring
----------------------------------------------------------------------------------------------------------------------------------------------------------------315.
If a pilot lands at an aerodrome other than the destination aerodrome specified in the flight plan , he must ensure that the ATS
unit at the destination aerodrome is informed within a certain number of minutes of his planned ETA at destination. This number of
minutes is ;
a)
10
b)
30
c)
15
d)
45
Answer ;
b)
30
----------------------------------------------------------------------------------------------------------------------------------------------------------------316.
If CAS is 190 kts , Altitude 9000 ft. Temp. ISA -10°C , True Course ( TC ) 350° , W/V 320/40 , distance from departure to
destination is 350 NM , endurance 3 hours , and actual time of departure is 1105 UTC. The distance from departure to Point of Equal
Time ( PET ) is ;
a)
167 NM
b)
203 NM
c)
183 NM
d)
147 NM
Answer ;
b)
203 NM
----------------------------------------------------------------------------------------------------------------------------------------------------------------317.
If CAS is 190 kts , Altitude 9000 ft. Temp. ISA -10°C , True Course ( TC ) 350° , W/V 320/40 , distance from departure to
destination is 350 NM , endurance 3 hours , and actual time of departure is 1105 UTC. The Point of Equal Time ( PET ) is reached at ;
a)
1203 UTC
b)
1221 UTC
c)
1233 UTC
d)
1213 UTC
Answer ;
d)
1213 UTC
----------------------------------------------------------------------------------------------------------------------------------------------------------------318.
( For this question use TRM , Barcelona Area chart (10-1V) )
If routeing along the Barcelona VFR corridors from Reus REP to SAN CELONI , what is the maximum altitude available
without changing ?
a)
3000 ft
b)
2000 ft
c)
3500 ft
d)
4500 ft
Answer ;
b)
2000 ft
----------------------------------------------------------------------------------------------------------------------------------------------------------------319.
If your destination airport has no ICAO indicator , in the appropriate box of your ATC flight plan , you write ;
a)
XXXX
b)
ZZZZ
c)
AAAA
d)
////
Answer ;
b)
ZZZZ
----------------------------------------------------------------------------------------------------------------------------------------------------------------320.
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 ;
a)
30 minutes holding 1.500 feet above aerodrome B
b)
30 minutes holding 2.000 feet above aerodrome B
c)
15 minutes holding 2.000 feet above aerodrome A
d)
30 minutes holding 1.500 feet above aerodrome A
Answer ;
a)
30 minutes holding 1.500 feet above aerodrome B
----------------------------------------------------------------------------------------------------------------------------------------------------------------321.
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 ;
a)
full name of VOR , true bearing and distance in kilometres.
b)
VOR ident , magnetic bearing and distance in kilometres.
c)
VOR ident , magnetic bearing and distance in nautical miles.
d)
VOR ident , true bearing and distance in kilometres.
Answer ;
c)
VOR ident , magnetic bearing and distance in nautical miles.
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
154
Flight Planning & Monitoring
322.
In an ATC flight plan Item 15 ( route ) , a cruising pressure altitude of 32000 feet would be entered as ;
a)
S3200
b)
FL320
c)
F320
d)
32000
Answer ;
c)
F320
----------------------------------------------------------------------------------------------------------------------------------------------------------------323.
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 ;
a)
41°35' N 04° 15'E
b)
4135N00415E
c)
N4135 E00415
d)
N04135E0415
Answer ;
b)
4135N00415E
----------------------------------------------------------------------------------------------------------------------------------------------------------------324.
( For this question use annex 033-4616A or Flight Planning Manual MRJT 1 Figure 4.3.6 )
Annex 033-4616A
In order to find ALTERNATE FUEL and TIME TO ALTERNATE , the AEROPLANE OPERATING MANUAL shall be
entered with ;
a)
distance in nautical miles ( NM ) , wind component , zero fuel mass.
b)
distance in nautical air miles ( NAM ) , wind component , landing mass at alternate.
c)
distance in nautical miles ( NM ) , wind component , dry operating mass plus holding fuel.
d)
distance in nautical miles ( NM ) , wind component , landing mass at alternate.
Answer ;
d)
distance in nautical miles ( NM ) , wind component , landing mass at alternate.
Ateş Murat Üstünbıçak , ATPL
155
Flight Planning & Monitoring
----------------------------------------------------------------------------------------------------------------------------------------------------------------325.
( For this question use annex 033-11702 A )
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 ;
a)
052°
b)
044°
c)
040°
d)
058°
Answer ;
a)
052°
----------------------------------------------------------------------------------------------------------------------------------------------------------------326.
( For this question use annex 033-4616A or Flight Planning Manual MRJT 1 Figure 4.3.6 )
Annex 033-4616A
In order to get alternate fuel and time , the twin-jet aeroplane operations manual graph shall be entered with ;
a)
Flight time , wind component , landing mass at alternate.
b)
Still air distance , wind component , zero fuel mass.
c)
Distance ( NM ) , wind component , zero fuel mass.
d)
Distance ( NM ) , wind component , landing mass at alternate.
Answer ;
d)
Distance ( NM ) , wind component , landing mass at alternate.
Ateş Murat Üstünbıçak , ATPL
156
Flight Planning & Monitoring
----------------------------------------------------------------------------------------------------------------------------------------------------------------327.
( For this question use annexes 033-11226A and 033-11226B )
Annexes 033-11226A , 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 ;
a)
0.80
b)
0.84
c)
the same as for LRC (Long Range Cruise)
d)
0.82
Answer ;
d)
0.82
----------------------------------------------------------------------------------------------------------------------------------------------------------------328.
In the appropriate box of an ATC flight plan , for endurance , one must indicate the time corresponding to ;
a)
the required fuel for the flight plus the alternate and 45 minutes.
b)
the total usable fuel on board.
c)
the total usable fuel on board minus reserve fuel.
d)
the required fuel for the flight.
Answer ;
b)
the total usable fuel on board.
----------------------------------------------------------------------------------------------------------------------------------------------------------------329.
In the appropriate box of an ATC flight plan form , concerning equipment , the letter to be used to indicate that the aircraft is
equipped with a mode A 4096 codes transponder with altitude reporting capability is ;
a)
S
b)
C
c)
A
d)
P
Answer ;
b)
C
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
157
Flight Planning & Monitoring
330.
In the appropriate box of an ATC flight plan form , corresponding to the estimated time of departure , the time indicated is
that at which the aircraft intends to ;
a)
go off blocks.
b)
pass the departure beacon.
c)
start-up.
d)
take-off.
Answer ;
a)
go off blocks.
----------------------------------------------------------------------------------------------------------------------------------------------------------------331.
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 ;
a)
P
b)
C
c)
B
d)
A
Answer ;
b)
C
----------------------------------------------------------------------------------------------------------------------------------------------------------------332.
In the ATC flight plan Item 10 , “standard equipment” is considered to be ;
a)
VHF RTF , ADF , VOR and ILS
b)
VHF RTF , ADF , VOR and transponder
c)
VHF RTF , VOR , INS and transponder
d)
VHF RTF , VOR , ILS and transponder
Answer ;
a)
VHF RTF , ADF , VOR and ILS
----------------------------------------------------------------------------------------------------------------------------------------------------------------333.
In the ATC flight plan Item 13 , in a flight plan submitted before departure , the departure time entered is the ;
a)
estimated time over the first point en route.
b)
estimated take-off time.
c)
estimated off-block time.
d)
allocated slot time.
Answer ;
c)
estimated off-block time.
----------------------------------------------------------------------------------------------------------------------------------------------------------------334.
In the ATC flight plan Item 15 , a cruising speed of 470 knots will be entered as ;
a)
KN470
b)
N0470
c)
0470K
d)
N470
Answer ;
b)
N0470
----------------------------------------------------------------------------------------------------------------------------------------------------------------335.
In the ATC flight plan Item 15 ( Cruising speed ) , when not expressed as a Mach number , cruising speed is expressed as ;
a)
CAS
b)
Groundspeed
c)
TAS
d)
IAS
Answer ;
c)
TAS
----------------------------------------------------------------------------------------------------------------------------------------------------------------336.
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 ;
a)
it is not necessary to indicate the point of joining that route as it will be obvious to the
ATS unit.
b)
the letters “DCT” should be entered , followed by the point of joining the ATS route
c)
the words “as cleared” should be entered
d)
it is necessary only to give the first reporting point on that route
Answer ;
b)
the letters “DCT” should be entered , followed by the point of joining the ATS route
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
158
Flight Planning & Monitoring
337.
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 ;
a)
10 % TAS or 0.05 Mach or more.
b)
20 km per hour or 0.1 Mach or more.
c)
5% TAS or 0.01 Mach or more.
d)
20 knots or 0.05 Mach or more.
Answer ;
c)
5% TAS or 0.01 Mach or more.
----------------------------------------------------------------------------------------------------------------------------------------------------------------338.
In the ATC flight plan item 15 , when entering a route for which standard departure ( SID ) and standard arrival ( STAR )
procedures exist ;
a)
neither SID nor STAR should be entered.
b)
both should be entered in the ATC plan where appropriate.
c)
SIDs should be entered but not STARs.
d)
STARS should be entered but not SIDs.
Answer ;
b)
both should be entered in the ATC plan where appropriate.
----------------------------------------------------------------------------------------------------------------------------------------------------------------339.
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 ;
a)
“TBN” ( to be notified ) may be entered in the relevant box.
b)
the plan may not be filed until the information is available.
c)
an estimate may be entered but that number may not subsequently be exceeded.
d)
the plan should be filed with the relevant box blank.
Answer ;
a)
“TBN” ( to be notified ) may be entered in the relevant box.
----------------------------------------------------------------------------------------------------------------------------------------------------------------340.
In the ATS flight plan , for a non-scheduled flight which of the following letters should be entered in Item 8 ( Type of
Flight ) ;
a)
G
b)
X
c)
N
d)
N/S
Answer ;
c)
N
----------------------------------------------------------------------------------------------------------------------------------------------------------------341.
In the ATS flight plan item 7 , for a radio equipped aircraft , the identifier must always ;
a)
be the RTF callsign to be used
b)
include an indication of the aircraft type
c)
include the aircraft registration marking
d)
include the operating agency designator
Answer ;
a)
be the RTF callsign to be used
----------------------------------------------------------------------------------------------------------------------------------------------------------------342.
In the ATS flight plan Item 19 , emergency and survival equipment carried on the flight should be indicated by ;
a)
placing a tick in the relevant box
b)
crossing out the box relevant to any equipment not carried
c)
listing the items carried on the “REMARKS” line
d)
circling the relevant box
Answer ;
b)
crossing out the box relevant to any equipment not carried
----------------------------------------------------------------------------------------------------------------------------------------------------------------343.
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 ;
a)
130 NM
b)
110 NM
c)
120 NM
d)
140 NM
Answer ;
c)
120 NM
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
159
Flight Planning & Monitoring
344.
In the event that SELCAL , is prescribed by an appropriate authority , in which section of the ATC flight plan will the
SELCAL code be entered ?
a)
OTHER INFORMATION
b)
ROUTE
c)
EQUIPMENT
d)
AIRCRAFT IDENTIFICATION
Answer ;
a)
OTHER INFORMATION
----------------------------------------------------------------------------------------------------------------------------------------------------------------345.
( For this question use annex 033-11183A )
Annex 033-11181A
In the vicinity of PARIS ( 49°N 003°E ) the tropopause is at about ;
a)
FL400
b)
FL350
c)
FL340
d)
FL380
Answer ;
d)
FL380
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
160
Flight Planning & Monitoring
346.
( For this question use annex 033-12320A )
Annex 033-12320A
In the vicinity of SHANNON ( 52° N 009°W ) the tropopause is at about FL ;
a)
300
b)
360
c)
350
d)
270
Answer ;
b)
360
----------------------------------------------------------------------------------------------------------------------------------------------------------------347.
“Integrated range” curves or tables are presented in the Aeroplane Operations Manuals.Their purpose is ;
a)
to determine the fuel consumption for a certain still air distance considering the decreasing fuel flow with
decreasing mass.
b)
to determine the optimum speed considering the fuel cost as well as the time related cost of the aeroplane.
c)
to determine the still air distance for a wind components varying with altitude.
d)
to determine the flight time for a certain leg under consideration of temperature deviations.
Answer ;
a)
to determine the fuel consumption for a certain still air distance considering the decreasing fuel flow with
decreasing mass.
----------------------------------------------------------------------------------------------------------------------------------------------------------------348.
It is possible , in flight , to ;
1.
file an ATC flight plan
2.
modify an active ATC flight plan
3.
cancel an active ATC flight plan
4.
close an active ATC flight plan
Which of the following combinations contains all of the correct statements ?
a)
1,2,3,4
b)
2,3,4
c)
1,2,4
d)
1,2,3
Answer ;
a)
1,2,3,4
Ateş Murat Üstünbıçak , ATPL
161
Flight Planning & Monitoring
----------------------------------------------------------------------------------------------------------------------------------------------------------------349.
Item 9 of the ATC flight plan includes “NUMBER AND TYPE OF AIRCRAFT”. In this case “NUMBER” means ;
a)
the number of aircraft flying in a group
b)
the registration number of the aircraft
c)
the number of aircraft which will separately be using a repetitive flight plan ( RPL )
d)
the ICAO type designator number as set out in ICAO Doc 8643
Answer ;
a)
the number of aircraft flying in a group
----------------------------------------------------------------------------------------------------------------------------------------------------------------350.
( For this question use annex 033-11253A , 033-11253B , 033-11253C and 033-11253D )
Annex 033-11253A , 033-11253B , 033-11253C , 033-11253D
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 flight time from take-off to landing needed to complete this flight will be ;
a)
203 minutes
b)
198 minutes
c)
209 minutes
d)
192 minutes
Answer ;
c)
209 minutes
Ateş Murat Üstünbıçak , ATPL
162
Flight Planning & Monitoring
----------------------------------------------------------------------------------------------------------------------------------------------------------------351.
( For this question use annex 033-11252A , 033-11252B and 033-11252C )
Annex 033-11252A , 033-11252B , 033-11252C
Knowing that ;
Mass at brake release : 210 000 kg
Selected cruise speed : 0.82 Mach
Air distance : 3 000 NM
Cruise level : optimum
Air conditioning : standard
Anti-icing : OFF
Temperature : ISA
CG : 37%
Assuming zero wind , the planned flight time from take-off to landing needed to complete this flight will be ;
a)
394 minutes
b)
400 minutes
c)
389 minutes
d)
383 minutes
Answer ;
b)
400 minutes
Ateş Murat Üstünbıçak , ATPL
163
Flight Planning & Monitoring
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
352.
( For this question use annex 033-11253A , 033-11253B , 033-11253C and 033-11253D )
Annex 033-11253A , 033-11253B , 033-11253C , 033-11253D
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 ;
a)
170 200 kg
b)
169 200 kg
c)
171 200 kg
d)
174 800 kg
Answer ;
c)
171 200 kg
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
164
Flight Planning & Monitoring
353.
( For this question use annex 033-11252A , 033-11252B , and 033-11252C )
Annex 033-11252A , 033-11252B , 033-11252C
Knowing that ;
Mass at brake release : 210 000 kg
Selected cruise speed : 0.82 Mach
Flight leg distance : 3 000 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 ;
a)
172 300 kg
b)
170 400 kg
c)
171 300 kg
d)
176 100 kg
Answer ;
a)
172 300 kg
Ateş Murat Üstünbıçak , ATPL
165
Flight Planning & Monitoring
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
354.
Mark the correct statement ;
If a decision point procedure is applied for flight planning ;
a)
the trip fuel to the destination aerodrome is to be calculated via the suitable enroute alternate.
b)
the trip fuel to the destination aerodrome is to be calculated via the decision point.
c)
the fuel calculation is based on a contingency fuel from departure aerodrome to the decision point.
d)
a destination alternate is not required.
Answer ;
b)
the trip fuel to the destination aerodrome is to be calculated via the decision point.
----------------------------------------------------------------------------------------------------------------------------------------------------------------355.
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 ?
a)
Diversion to a nearby alternate is not necessary , because it is allowed to calculate without reserve fuel.
b)
Diversion to a nearby alternate is necessary , because the remaining fuel is not sufficient.
c)
Diversion to a nearby alternate is necessary , unless the captain decides to continue on his own responsibility.
d)
Diversion to a nearby alternate is not necessary , because the reserve fuel has not been used completely.
Answer ;
b)
Diversion to a nearby alternate is necessary , because the remaining fuel is not sufficient.
----------------------------------------------------------------------------------------------------------------------------------------------------------------356.
( 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 ;
a)
UH40 FOUCO UH20 PERIC UA34
b)
UB19 CGC UA25
c)
UB19 POI UB195
d)
UA34
Answer ;
d)
UA34
----------------------------------------------------------------------------------------------------------------------------------------------------------------357.
( 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 ;
a)
UR12 MID UA47 DPE UA475 SOKMU UH111
b)
UR12 MID UR8 SAM UB11 BARLU UW115
c)
UB29 LAM UR1 MID UA34 LILAN UR9
d)
UB29 LAM UR1 ORTAC UR14
Answer ;
d)
UB29 LAM UR1 ORTAC UR14
----------------------------------------------------------------------------------------------------------------------------------------------------------------358.
( For this question use annex 033-10989A or Route Manual chart E(HI)4 CAA-Edition )
Of the following , the preferred airways routing from FRANKFURT FFM 114.2 ( 50°03'N 008°38'E ) to KOKSY ( 51°06'N
002°39'E ) above FL245 , on a Wednesday is ;
a)
UG1
b)
UR10 NTM UB6 BUB ATS
c)
UB69 DINKI UB6 BUB ATS
d)
UG108 SPI UG1
Answer ;
b)
UR10 NTM UB6 BUB ATS
----------------------------------------------------------------------------------------------------------------------------------------------------------------359.
( 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 ;
a)
UB284 VILAR UB28
b)
UA6 LSA UG52
c)
UB28
d)
UB282 DGN UB46
Answer ;
d)
UB282 DGN UB46
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
166
Flight Planning & Monitoring
360.
( For this question use Route Manual chart NAP )
On a direct great circle course from REYKJAVIK ( 64°10' N 022°00'W ) to AMSTERDAM ( 52°32'N 004°50'E ) , the (a)
average true course , and (b) distance , are ;
a)
(a) 118º , (b) 1095 NM
b)
(a) 311º , (b) 1824 NM
c)
(a) 140º , (b) 1824 NM
d)
(a) 131º , (b) 1095 NM
Answer ;
d)
(a) 131º , (b) 1095 NM
----------------------------------------------------------------------------------------------------------------------------------------------------------------361.
( For this question use Route Manual chart NAP )
On a direct great circle course from Shannon ( 52°43' N 008°53'W ) to Gander ( 48°54' N 054°32'W ) , the (a) average true
course , and (b) distance , are ;
a)
(a) 281º , (b) 1877 NM
b)
(a) 281º , (b) 2730 NM
c)
(a) 244º , (b) 1520 NM
d)
(a) 262º , (b) 1720 NM
Answer ;
d)
(a) 262º , (b) 1720 NM
----------------------------------------------------------------------------------------------------------------------------------------------------------------362.
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 ;
a)
FL330
b)
FL270
c)
FL290
d)
FL370
Answer ;
b)
FL270
----------------------------------------------------------------------------------------------------------------------------------------------------------------363.
On a VFR ATC flight plan , the total estimated time is ;
a)
the estimated time from take-off to overhead the destination airport , plus 15 minutes.
b)
the estimated time from take-off to landing at the alternate airport.
c)
the estimated time required from take-off to arrive over the destination airport.
d)
the estimated time from engine start to landing at the destination airport.
Answer ;
c)
the estimated time required from take-off to arrive over the destination airport.
----------------------------------------------------------------------------------------------------------------------------------------------------------------364.
( 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 ;
a)
344
b)
353
c)
350
d)
347
Answer ;
a)
344
----------------------------------------------------------------------------------------------------------------------------------------------------------------365.
On an ATC flight plan , an aircraft indicated as “H” for “Heavy” ;
a)
is of the highest wake turbulence category.
b)
has a certified landing mass greater than or equal to 136 000 kg.
c)
has a certified take-off mass greater than or equal to 140 000 kg.
d)
requires a runway length of at least 2 000m at maximum certified take-off mass.
Answer ;
a)
is of the highest wake turbulence category.
----------------------------------------------------------------------------------------------------------------------------------------------------------------366.
On an ATC flight plan , the letter “Y” is used to indicate that the flight is carried out under the following flight rules ;
a)
IFR
b)
VFR followed by IFR
c)
VFR
d)
IFR followed by VFR
Answer ;
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d)
IFR followed by VFR
----------------------------------------------------------------------------------------------------------------------------------------------------------------367.
On an ATC flight plan , to indicate that you will overfly the waypoint ROMEO at 120 kt at flight level 085 , you will write ;
a)
ROMEO/FL085N0120
b)
ROMEO/K0120FL085
c)
ROMEO/F085N0120
d)
ROMEO/N0120F085
Answer ;
d)
ROMEO/N0120F085
----------------------------------------------------------------------------------------------------------------------------------------------------------------368.
On an ATC flight plan , to indicate that you will overfly the way-point TANGO at 350 kts at flight level 280 , you write ;
a)
TANGO/N0350F280
b)
TANGO/T350F280
c)
TANGO/K0350FL280
d)
TANGO/FL280N0350
Answer ;
a)
TANGO/N0350F280
----------------------------------------------------------------------------------------------------------------------------------------------------------------369.
On an ATC 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 ;
a)
The estimated ground speed.
b)
The indicated airspeed.
c)
The equivalent airspeed.
d)
The true airspeed.
Answer ;
d)
The true airspeed.
----------------------------------------------------------------------------------------------------------------------------------------------------------------370.
On an IFR navigation chart , in a 1° quadrant of longitude and latitude , appears the following information “80”. This means
that within this quadrant ;
a)
the minimum safe altitude is 8000 ft
b)
the minimum flight level is FL 80
c)
the altitude of the highest obstacle is 8000 ft
d)
the floor of the airway is at 8000 ft
Answer ;
a)
the minimum safe altitude is 8000 ft
----------------------------------------------------------------------------------------------------------------------------------------------------------------371.
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 ;
a)
15 NM
b)
25 NM
c)
10 NM
d)
20 NM
Answer ;
b)
25 NM
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372.
( For this question use annex 033-12328A )
Annex 033-12320A
Over LONDON ( 51°N 000°E/W ) , the lowest FL listed which is unaffected by CAT is ;
a)
270
b)
230
c)
360
d)
310
Answer ;
b)
230
----------------------------------------------------------------------------------------------------------------------------------------------------------------373.
( For this question use Image 14 )
Image 14
Planned and actual data as shown in the Flight Log excerpt. Actual Ground Speed ( GS ) on the leg BETA to GAMMA will
be 105 KT. If all other flight parameters remain unchanged , what fuel remaining should be expected at waypoint GAMMA ?
a)
3250 kg
b)
3430 kg
c)
3318 kg
d)
3480 kg
Answer ;
a)
3250 kg
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-----------------------------------------------------------------------------------------------------------------------------------------------------------------
374.
( For this question use Image 11 )
Image 11
Planned and actual data as shown in the Flight Log excerpt. Actual Ground Speed ( GS ) on the leg BETA to GAMMA will
be 110 KT. If all other flight parameters remain unchanged , what fuel remaining should be expected at waypoint GAMMA ?
a)
2625 kg
b)
2900 kg
c)
2820 kg
d)
2723 kg
Answer ;
a)
2625 kg
----------------------------------------------------------------------------------------------------------------------------------------------------------------375.
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 ) ;
a)
55 765 kg.
b)
52 265 kg.
c)
51 425 kg.
d)
51 515 kg.
Answer ;
d)
51 515 kg.
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
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376.
( For this question use annex 033-3910A or Flight Planning Manual MRJT 1 Figure 4.4 )
Annex 033-3910A
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 ;
a)
2 250 kg.
b)
48 125 kg.
c)
49 250 kg.
d)
48 675 kg.
Answer ;
b)
48 125 kg.
----------------------------------------------------------------------------------------------------------------------------------------------------------------377.
( 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 ;
Power setting : 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 ;
a)
1 550 kg.
b)
1 740 kg.
c)
1 900 kg.
d)
1 450 kg.
Answer ;
b)
1 740 kg.
----------------------------------------------------------------------------------------------------------------------------------------------------------------378.
( 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 ;
a)
1 300 kg and 28 minutes.
b)
1 200 kg and 26 minutes.
c)
1 450 kg and 32 minutes.
d)
1 600 kg and 36 minutes.
Answer ;
c)
1 450 kg and 32 minutes.
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-----------------------------------------------------------------------------------------------------------------------------------------------------------------
379.
( For this question use annexes 033-11073A , 033-11073B , 033-11073C and 033-11073D )
Annex 033-11073A
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Annex 033-11073C
Annex 033-11073D
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 tailwind is 100 kt , ISA conditions. Fuel consumption will be ;
a)
26 950 kg
b)
22 860 kg
c)
30 117 kg
d)
24 900 kg
Answer ;
a)
26 950 kg
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
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380.
( For this question use annexes 033-11073A , 033-11073B , 033-11073C and 033-11073D )
Annex 033-11073A
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Annex 033-11073C
Annex 033-11073D
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 ;
a)
30 117 kg
b)
27 577 kg
c)
30 371 kg
d)
32 657 kg
Answer ;
d)
32 657 kg
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
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381.
( For this question use annex 033-9703A or Route Manual SID chart 20-3 for PARIS Charles-de-Gaulle )
Annex 033-9703A
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 ;
a)
31 NM
b)
24.5 NM
c)
33 NM
d)
36.5 NM
Answer ;
b)
24.5 NM
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
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382.
( For this question use annex 033-9703A or Route Manual chart SID PARIS Charles-De-Gaulle (20-3) )
Annex 033-9703A
Planning an IFR flight from Paris ( Charles de Gaulle ) to London ( Heathrow ). Find the elevation of the departure
aerodrome ;
a)
217 ft.
b)
2 ft.
c)
268 ft.
d)
387 ft.
Answer ;
d)
387 ft.
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
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383.
( For this question use annex 033-9710B or Route Manual chart STAR LONDON Heathrow (10-2) )
Annex 033-9710B
Planning an IFR flight from Paris ( Charles de Gaulle ) to London ( Heathrow ). Find the elevation of the destination
aerodrome ;
a)
100 ft.
b)
80 ft.
c)
77 ft.
d)
177 ft.
Answer ;
b)
80 ft.
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
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384.
( For this question use annex 033-9700A or Flight Planning Manual MRJT 1 Figure 4.5.1 )
Annex 033-9700A
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 ) ;
a)
15 min
b)
3 min
c)
12 min
d)
11 min
Answer ;
d)
11 min
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-----------------------------------------------------------------------------------------------------------------------------------------------------------------
385.
( For this question use annex 033-3908A or Route Manual chart E(HI)4 CAA-Edition )
Planning an 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 ;
a)
343°.
b)
322°.
c)
330°.
d)
142°.
Answer ;
b)
80 ft.
----------------------------------------------------------------------------------------------------------------------------------------------------------------386.
( For this question use annex 033-3909A or Route Manual chart E(HI)4 CAA-Edition )
Planning an 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 ;
a)
188 NM.
b)
207 NM.
c)
218 NM.
d)
308 NM.
Answer ;
b)
207 NM.
----------------------------------------------------------------------------------------------------------------------------------------------------------------387.
( 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 50 NM. Determine the magnetic course , ground speed and wind correction angle from top of
climb to ABB 116.6 ;
a)
MC 349° , GS 414 kt , WCA -5°
b)
MC 169° , GS 450 kt , WCA +4°
c)
MC 169° , GS 414 kt , WCA +5°
d)
MC 349° , GS 414 kt , WCA +5°
Answer ;
a)
MC 349° , GS 414 kt , WCA -5°
----------------------------------------------------------------------------------------------------------------------------------------------------------------388.
( For this question use annex 033-9702A or Route Manual SID chart 20-3 for PARIS Charles-de-Gaulle )
Planning an IFR-flight from Paris to London. Determine the distance of the departure route ABB 8A ;
a)
83 NM
b)
72.5 NM
c)
56 NM
d)
74.5 NM
Answer ;
d)
74.5 NM
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389.
( For this question use annex 033-9704A or Flight Planning Manual MRJT 1 Figure 4.5.4 )
Annex 033-9704A
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 ) ;
a)
97 NM
b)
87 NM
c)
76 NM
d)
65 NM
Answer ;
c)
76 NM
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
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390.
( For this question use annex 033-9706A or Flight Planning Manual MRJT 1 Figure 4.5.4 )
Annex 033-9706A
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 ) ;
a)
320 kg
b)
263 kg
c)
210 kg
d)
273 kg
Answer ;
d)
273 kg
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
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391.
( For this question use annex 033-9708A or Flight Planning Manual MRJT 1 Figure 4.5.3.2 )
Annex 033-9708A
Planning an IFR-flight from Paris to London for the twin jet aeroplane.
Given ;
Gross mass 50000 kg
FL 280
ISA Deviation -10°C
Cruise procedure Mach 0.74
Determine the TAS ;
a)
427 kt
b)
430 kt
c)
440 kt
d)
417 kt
Answer ;
b)
430 kt
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
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392.
( For this question use annex 033-9705A or Flight Planning Manual MRJT 1 Figure 4.5.4 )
Annex 033-9705A
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 time from the top of descent to London ( elevation 80 ft ) ;
a)
17 min
b)
10 min
c)
8 min
d)
19 min
Answer ;
d)
19 min
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
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393.
( For this question use annex 033-9700A or Flight Planning Manual MRJT 1 Figure 4.5.1 )
Annex 033-9700A
Planning an IFR-flight from Paris to London 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 : Fuel to the top of climb ( TOC ) ;
a)
1500 lbs
b)
1100 kg
c)
1000 lbs
d)
1000 kg
Answer ;
d)
1000 kg
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
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394.
4.5.1 )
( For this question use annex 033-9699A and 033-9699B or Flight Planning Manual MRJT 1 Paragraph 5.1 and Figure
Annex 033-9699A , 033-9699B
Planning an IFR-flight from Paris to London for a 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 : Ground distance to the top of climb ( TOC ) ;
a)
53 NM
b)
56 NM
c)
47 NM
d)
50 NM
Answer ;
d)
50 NM
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----------------------------------------------------------------------------------------------------------------------------------------------------------------395.
( For this question use annexes 033-3908A , 033-9710B and 033-9710C or Route Manual chart E(HI)4 CAA-Edition , 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 ).
Assume ;
STAR is BIG 2A
Variation 5° W
En-route TAS 430 kts
W/V 280/40
Descent distance 76NM
Determine the magnetic course , ground speed and wind correction angle from ABB 116.6 ( N50 08.1 E001 51.3 ) to top of
descent ;
a)
MC 141° , GS 396 kt , WCA -3°
b)
MC 141° , GS 396 kt , WCA +3°
c)
MC 319° , GS 396 kt , WCA -3°
d)
MC 321° , GS 396 kt , WCA -3°
Answer ;
d)
MC 321° , GS 396 kt , WCA -3°
----------------------------------------------------------------------------------------------------------------------------------------------------------------396.
( 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) )
Annex 033-3301A
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 ;
a)
BIG 115.1 kHz
b)
EPM 316 kHz
c)
OCK 115.3 MHz
d)
BIG 115.1 MHz
Answer ;
d)
BIG 115.1 MHz
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-----------------------------------------------------------------------------------------------------------------------------------------------------------------
397.
( For this question use annex 033-11262A )
Annex 033-11262A
Prior to an IFR flight , when filling in the ICAO flight plan , the time information which should be entered in box 13 :
“Time” is ;
a)
planned take-off time.
b)
the time of flight plan filing.
c)
estimated off-block time.
d)
planned engine start time.
Answer ;
c)
estimated off-block time.
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
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398.
( For this question use annex 033-11262A )
Annex 033-11262A
Prior to an IFR flight , when filling in the ICAO flight plan , the time information which should be entered in box 16 : “Total
estimated time” is the time elapsed from ;
a)
take-off until reaching the IAF ( Initial Approach Fix ) of the destination aerodrome.
b)
take-off until landing.
c)
taxi-out prior to take-off until taxiing completion after landing.
d)
taxiing until the IAF ( Initial Approach Fix ) of the destination aerodrome.
Answer ;
a)
take-off until reaching the IAF ( Initial Approach Fix ) of the destination aerodrome.
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
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399.
( For this question use annex 033-9562A or Flight Planning Manual MRJT 1 Figure 4.5.3.1 )
Annex 033-9562A
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 ?
a)
2050 kg
b)
2250 kg
c)
2350 kg
d)
2150 kg
Answer ;
d)
2150 kg
----------------------------------------------------------------------------------------------------------------------------------------------------------------400.
( For this question use annex 033- 11016A or Route Manual chart E(LO)5 )
The airway intersection at RONNEBY ( 56°18'N 015°16'E ) is marked by ;
a)
a TACAN callsign RON
b)
a fan marker callsign LP
c)
an NDB callisign N
d)
an NDB callsign LF
Answer ;
c)
an NDB callisign N
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
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401.
( For this question use annex 033-12319A )
Annex 033-12314A
The approximate mean wind component ( kt ) along true course 180° from 50°N to 40°N at 005° W is ;
a)
tail wind 55 kt
b)
tail wind 70 kt
c)
tail wind 40 kt
d)
headwind 55 kt
Answer ;
a)
tail wind 55 kt
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
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402.
( For this question use annex 033-11192A )
Annex 033-11190A
The approximate mean wind component ( kt ) at Mach 0.78 along true course 270° at 50°N from 000° to 010°W is ;
a)
40 kt headwind component
b)
35 kt tailwind component
c)
25 kt tailwind component
d)
55 kt headwind component
Answer ;
a)
40 kt headwind component
----------------------------------------------------------------------------------------------------------------------------------------------------------------403.
( For this question use annex 033-12373A or Route Manual chart NAP )
The average magnetic course from A ( 64°N 006°E ) to C ( 62°N 020°W ) is ;
a)
279°
b)
271°
c)
247°
d)
259°
Answer ;
b)
271°
----------------------------------------------------------------------------------------------------------------------------------------------------------------404.
( For this question use annex 033-12368A or Route Manual chart NAP )
The average magnetic course from C ( 62°N 020°W ) to B ( 58°N 004°E ) is ;
a)
119°
b)
118°
c)
099°
d)
109°
Answer ;
a)
119°
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
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405.
( For this question use annex 033-12374A or Route Manual chart NAP )
The average true course from A ( 64°N 006°E ) to C ( 62°N 020°W ) is ;
a)
079°
b)
271°
c)
247°
d)
259°
Answer ;
d)
259°
----------------------------------------------------------------------------------------------------------------------------------------------------------------406.
( For this question use annex 033-12369A or Route Manual chart NAP )
The average true course from C ( 62°N 020°W ) to B ( 58°N 004°E ) is ;
a)
109°
b)
119°
c)
120°
d)
099°
Answer ;
a)
109°
----------------------------------------------------------------------------------------------------------------------------------------------------------------407.
( For this question use TRM , Athinai (Hellinikon) Approach chart (29-1) )
The callsign and frequency to use to obtain start up clearance is ;
a)
Approach 119.10
b)
Tower 118.10
c)
Ground 121.70
d)
ATIS 123.40
Answer ;
c)
Ground 121.70
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408.
( For this question use annex 033- 11049A or Route Manual STAR charts for MUNICH (10-2A,B) )
Annex 033-11049A
The correct arrival route and Initial Approach Fix ( IAF ) for an arrival from the west via TANGO for runway 08 L/R is ;
a)
NDG 1T , IAF ROKIL
b)
DKB 1T , IAF ROKIL
c)
AALEN 1T , IAF ROKIL
d)
AALEN 1T , IAF MBG
Answer ;
c)
AALEN 1T , IAF ROKIL
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----------------------------------------------------------------------------------------------------------------------------------------------------------------409.
( For this question use annex 033- 11063A or Route Manual chart PARIS CHARLES DE GAULLE ILS Rwy 27 (21-2) )
Annex 033-11063A
The crossing altitude and descent instruction for a propeller aircraft at COULOMMIERS ( CLM ) are ;
a)
Cross at FL70 descend to 4000 ft
b)
Cross at FL60 and maintain
c)
Cross at FL60 descend to 4000 ft
d)
Cross at FL80 descend to FL70
Answer ;
c)
Cross at FL60 descend to 4000 ft
Ateş Murat Üstünbıçak , ATPL
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Flight Planning & Monitoring
----------------------------------------------------------------------------------------------------------------------------------------------------------------410.
The cruising speed to write in the appropriate box of an ATC flight plan is ;
a)
calibrated air speed.
b)
true air speed.
c)
ground speed.
d)
indicated air speed.
Answer ;
b)
true air speed.
----------------------------------------------------------------------------------------------------------------------------------------------------------------411.
( For this question use annex 033- 11058A or Route Manual chart LONDON HEATHROW ILS DME Rwy 09L (11-2) )
Annex 033-11058A
The Decision Altitude ( DA ) for a ILS straight-in landing is ;
a)
400 ft
b)
200 ft
c)
480 ft
d)
280 ft
Answer ;
d)
280 ft
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
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Flight Planning & Monitoring
412.
( For this question use Route Manual chart E(HI)1 )
The direct distance from TIREE 117.7 TIR ( 56°30'N 006°53'W ) to INVERNESS 109.2 INS ( 57°32'N 004°03'W ) is ;
a)
204 NM
b)
112 NM
c)
192 NM
d)
360 km
Answer ;
a)
204 NM
----------------------------------------------------------------------------------------------------------------------------------------------------------------413.
( For this question use annex 033-12372A or Route Manual chart NAP )
The distance ( NM ) from A ( 64°N 006°E ) to C ( 62°N 020°W ) is ;
a)
720
b)
690
c)
1590
d)
1440
Answer ;
a)
720
----------------------------------------------------------------------------------------------------------------------------------------------------------------414.
( For this question use Annex 033-12377A or Route Manual chart NAP )
The distance ( NM ) from C ( 62°N 020°W ) to B ( 58°N 004°E ) is ;
a)
760
b)
775
c)
725
d)
700
Answer ;
a)
760
----------------------------------------------------------------------------------------------------------------------------------------------------------------415.
( For this question use Route Manual chart E(LO)1 )
The distance on airway B4 from POLE HILL 112.1 POL to SHAPP ( 54°30'N 002°38'W ) is ;
a)
30 NM
b)
51 NM
c)
31 NM
d)
49 NM
Answer ;
d)
49 NM
----------------------------------------------------------------------------------------------------------------------------------------------------------------416.
( For this question use TRM (VFR) , Aberdeen Information Page (19-3) )
The East Apron and Eastern Twy have restricted access. The maximum permitted wingspan ;
a)
is 20 ft.
b)
is the same as a Beech 200.
c)
does not apply to helicopters.
d)
is 20 m.
Answer ;
d)
is 20 m.
----------------------------------------------------------------------------------------------------------------------------------------------------------------417.
The final reserve fuel for aeroplanes with turbine engines is ;
a)
fuel to fly for 45 minutes at holding speed at 1000 ft ( 300 m ) above aerodrome elevation in standard
conditions.
b)
fuel to fly for 30 minutes at holding speed at 1500 ft ( 450 m ) above aerodrome elevation in standard
conditions.
c)
fuel to fly for 45 minutes at holding speed at 1500 ft ( 450 m ) above aerodrome elevation in standard
conditions.
d)
fuel to fly for 60 minutes at holding speed at 1500 ft ( 450 m ) above aerodrome elevation in standard
conditions.
Answer ;
b)
fuel to fly for 30 minutes at holding speed at 1500 ft ( 450 m ) above aerodrome elevation in standard
conditions.
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
197
Flight Planning & Monitoring
418.
( For this question use annex 033-9543A or Flight Planning Manual MRJT 1 Figure 4.4 )
Annex 033-9543A
The final reserve fuel taken from the HOLDING PLANNING table for the twin jet aeroplane is based on the following
parameters ;
a)
pressure altitude , aeroplane mass and flaps up with minimum drag airspeed.
b)
pressure altitude , aeroplane mass and flaps down with maximum range speed.
c)
pressure altitude , aeroplane mass and flaps up with maximum range speed.
d)
pressure altitude , aeroplane mass and flaps down with minimum drag airspeed.
Answer ;
a)
pressure altitude , aeroplane mass and flaps up with minimum drag airspeed.
----------------------------------------------------------------------------------------------------------------------------------------------------------------419.
( For this question use Route Manual chart E(HI)4 CAA-Edition )
The first ( lowest ) available 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 ;
a)
FL320
b)
FL300
c)
FL290
d)
FL310
Answer ;
b)
FL300
----------------------------------------------------------------------------------------------------------------------------------------------------------------420.
( For this question use Route Manual chart E(HI)4 CAA-Edition )
The first ( lowest ) available flight level for flight on airway UG5 from MENDE-NASBINALS MEN 115.3 ( 44°36'N
003°10'E ) to GAILLAC GAI 115.8 ( 43°57'N 001°50'E ) is ;
a)
FL290
b)
FL300
c)
FL280
d)
FL310
Answer ;
a)
FL290
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
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Flight Planning & Monitoring
421.
( For this question use annex 033-11239A and 031-11239B )
Annexes 033-11239A , 031-11239B
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 : 0.30 $/l at departure
The commander may carry a fuel quantity of 8 000 kg in addition to that which is necessary. For this fuel transport operation
to be cost effective, the maximum fuel price at arrival must be ;
a)
0.28 $/l
b)
0.27 $/l
c)
0.26 $/l
d)
0.33 $/l
Answer ;
b)
0.27 $/l
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
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Flight Planning & Monitoring
422.
( For this question use annex 033-11239A and 031-11239B )
Annexes 033-11239A , 031-11239B
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 ;
a)
0.28 $/l
b)
0.30 $/l
c)
0.29 $/l
d)
0.24 $/l
Answer ;
b)
0.30 $/l
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
200
Flight Planning & Monitoring
423.
( For this question use annex 033-11241A )
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 ;
a)
34 430 kg
b)
30 440 kg
c)
32 480 kg
d)
28 720 kg
Answer ;
a)
34 430 kg
Ateş Murat Üstünbıçak , ATPL
201
Flight Planning & Monitoring
----------------------------------------------------------------------------------------------------------------------------------------------------------------424.
( For this question use annexes 033-11204A , 033-11204B and 033-11204C )
The flight crew of a turbojet aeroplane prepares a flight using the
following data ;
Flight leg ground distance : 4 000 NM
Flight level FL 370 : “Long range” flight regime
Effective wind at this level : head wind of 50 kt
Temperature : ISA
Centre of gravity ( CG ) : 37 %
Pack flow : LOW ( LO )
Anti ice : OFF
Reference landing mass : 140 000 kg
Taxi fuel : 500 kg
Annexes 033-11204A , 033-11204B , 033-11204C
Final reserve fuel : 2 400 kg
The fuel quantity which must be loaded on board the aircraft is ;
a)
51 860 kg
b)
41 950 kg
c)
52 060 kg
d)
46 340 kg
Answer ;
a)
51 860 kg
Ateş Murat Üstünbıçak , ATPL
202
Flight Planning & Monitoring
----------------------------------------------------------------------------------------------------------------------------------------------------------------425.
( For this question use annex 033-11238A )
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 ;
a)
27 770 kg
b)
22 160 kg
c)
20 900 kg
d)
29 440 kg
Answer ;
d)
29 440 kg
Ateş Murat Üstünbıçak , ATPL
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Flight Planning & Monitoring
----------------------------------------------------------------------------------------------------------------------------------------------------------------426.
( For this question use annex 033-11272A )
Annex 033-11272A
The flight crew of a turbojet aeroplane prepares a flight using the following data ;
Take-off mass : 168 500 kg
Flight leg ground distance : 2 000 NM
Flight level FL 370 , “Long Range” flight regime
Tailwind component at this level : 30 kt
Total anti-ice set on “ON”
Fixed taxi fuel : 500 kg , final reserve : 2 000 kg
Ignore alternate fuel.
The effects of climb and descent are not corrected for consumption.
The prescribed quantity of trip fuel for the flight leg is ;
a)
23 000 kg
b)
23 300 kg
c)
20 500 kg
d)
22 500 kg
Answer ;
c)
20 500 kg
Ateş Murat Üstünbıçak , ATPL
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Flight Planning & Monitoring
----------------------------------------------------------------------------------------------------------------------------------------------------------------427.
( For this question use annex 033-11271A )
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 ;
a)
30 200 kg
b)
39 750 kg
c)
31 840 kg
d)
31 340 kg
Answer ;
c)
31 840 kg
Ateş Murat Üstünbıçak , ATPL
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Flight Planning & Monitoring
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
428.
( For this question use annex 033-11245A and 033-11245B )
Annex 033-11245A , 033-11245B
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 ;
a)
The fuel transport operation is not recommended in this case.
b)
6 000 kg.
c)
10 000 kg.
d)
4 000 kg.
Answer ;
a)
The fuel transport operation is not recommended in this case.
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
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Flight Planning & Monitoring
429.
( For this question use annex 033-11245A and 033-11245B )
Annex 033-11245A , 033-11245B
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 ) : 195 000 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 ;
a)
5 000 kg.
b)
10 000 kg.
c)
8 000 kg.
d)
The fuel transport operation is not recommended in this case.
Answer ;
d)
The fuel transport operation is not recommended in this case.
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
207
Flight Planning & Monitoring
430.
( For this question use Annex 033-11245A and 033-11245B )
Annex 033-11245A , 033-11245B
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 : 0.30 Euro/l at departure , 0.27 Euro/l at destination
To maximize savings , the commander chooses to carry extra fuel in addition to that which is necessary. Using the appended
annex , the optimum quantity of fuel which should be carried in addition to the prescribed quantity is ;
a)
The fuel transport operation is not recommended in this case.
b)
22 000 kg.
c)
15 000 kg.
d)
8 000 kg.
Answer ;
a)
The fuel transport operation is not recommended in this case.
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
208
Flight Planning & Monitoring
431.
( For this question use Annex 033-11245A and 033-11245B )
Annex 033-11245A , 033-11245B
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 : 5 kt
Initially planned take-off mass ( without extra fuel on board ) : 180 000 kg
Fuel price : 0.35 US Dollars/l at departure , 0.315 US Dollars/l at destination
To maximize savings , the commander chooses to carry extra fuel in addition to that which is necessary. Using the appended
annex , the optimum quantity of fuel which should be carried in addition to the prescribed quantity is ;
a)
The fuel transport operation is not recommended in this case.
b)
22 000 kg.
c)
15 000 kg.
d)
8 000 kg.
Answer ;
a)
The fuel transport operation is not recommended in this case.
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
209
Flight Planning & Monitoring
432.
( For this question use annex 033-11245A and 033-11245B )
Annex 033-11245A , 033-11245B
The flight crew of a turbojet aeroplane prepares a flight using the following data ;
Flight leg distance : 4 000 NM
Flight level FL 310 , true airspeed : 450 kt
Headwind component at this level : 50 kt
Initially planned take-off mass ( without extra fuel on board ) : 170 000 kg
Fuel price : 0.27 Euro/l at departure , 0.30 Euro/l at destination
To maximize savings , the commander chooses to carry extra fuel in addition to that which is necessary. Using the appended
annex , the optimum quantity of fuel which should be carried in addition to the prescribed quantity is ;
a)
18 000 kg.
b)
8 000 kg.
c)
The fuel transport operation is not recommended in this case.
d)
32 000 kg.
Answer ;
b)
8 000 kg.
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
210
Flight Planning & Monitoring
433.
( For this question use annex 033-11245A and 033-11245B )
Annex 033-11245A , 033-11245B
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 : 0.30 Euro/l at departure , 0.27 Euro/l at destination
To maximize savings , the commander decides to carry extra fuel in addition to that which is necessary. Using the appended
annex , the optimum quantity of fuel which should be carried in addition to the prescribed quantity is ;
a)
15 000 kg
b)
22 000 kg
c)
The fuel transport operation is not recommended in this case.
d)
8 000 kg
Answer ;
c)
The fuel transport operation is not recommended in this case.
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
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Flight Planning & Monitoring
434.
( For this question use annex 033-12350A or Flight Planning Manual MRJT 1 Figure 4.3.5 )
The following apply ;
Annex 033-12350A
Tail wind component 10 kt
Temperature ISA +10°C
Brake release mass 63000 kg
Trip fuel available 20000 kg
What is the maximum possible trip distance ?
a)
3740 NM
b)
3250 NM
c)
3500 NM
d)
3640 NM
Answer ;
a)
3740 NM
Ateş Murat Üstünbıçak , ATPL
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Flight Planning & Monitoring
----------------------------------------------------------------------------------------------------------------------------------------------------------------435.
( For this question use annex 033-12348A or Flight Planning Manual MRJT 1 Figure 4.3.5 )
Annex 033-12348A
The following apply ;
Temperature ISA +15°C
Brake release mass 62000 kg
Trip time 5 hr 20 min
What is the trip fuel ?
a)
13800 kg
b)
13000 kg
c)
13200 kg
d)
13500 kg
Answer ;
d)
13500 kg
Ateş Murat Üstünbıçak , ATPL
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Flight Planning & Monitoring
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
436.
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 ;
a)
79 800 kg.
b)
77 200 kg.
c)
74 800 kg.
d)
77 800 kg.
Answer ;
d)
77 800 kg.
----------------------------------------------------------------------------------------------------------------------------------------------------------------437.
( For this question use annex 033-12330A )
Annex 033-12330A
The forecast period covered by the PARIS/CHARLES-DE-GAULLE TAFs totals ( hours ) ;
a)
27
b)
20
c)
18
d)
9
Answer ;
a)
27
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
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Flight Planning & Monitoring
438.
( For this question use annex 033- 11067A or Route Manual chart MUNICH NDB DME Rwy 26L approach (16-3) )
Annex 033-11067A
The frequency and identifier of the NDB for the published approaches are ;
a)
112.3 MUN
b)
400 MSW
c)
338 MNW
d)
108.6 DMS
Answer ;
b)
400 MSW
Ateş Murat Üstünbıçak , ATPL
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Flight Planning & Monitoring
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
439.
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:
a)
206 l/h
b)
176 l/h
c)
220 l/h
d)
235 l/h
Answer ;
d)
235 l/h
----------------------------------------------------------------------------------------------------------------------------------------------------------------440.
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 ;
a)
188 kg/h
b)
267 kg/h
c)
213 kg/h
d)
200 kg/h
Answer ;
d)
200 kg/h
----------------------------------------------------------------------------------------------------------------------------------------------------------------441.
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 ?
a)
The remaining fuel is not sufficient to reach the destination with reserves intact.
b)
At departure the reserve fuel was 28 US gallons.
c)
At destination the required reserves remain intact.
d)
At the destination there will still be 30 US gallons in the tanks.
Answer ;
a)
The remaining fuel is not sufficient to reach the destination with reserves intact.
----------------------------------------------------------------------------------------------------------------------------------------------------------------442.
( For this question use Route Manual chart E(HI)2 )
The identifier of the radio navigation aid at ( 56°06'N 012°15'E ) is ;
a)
NORA
b)
NOA
c)
SVD04
d)
WX
Answer ;
b)
NOA
----------------------------------------------------------------------------------------------------------------------------------------------------------------443.
( For this question use Route Manual chart E(HI)2 )
The identifier of the radio navigation aid at ( 56°07'N 012°58'E ) is ;
a)
AOR
b)
SVD03
c)
SVD
d)
ASTOR
Answer ;
a)
AOR
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
216
Flight Planning & Monitoring
444.
( For this question use annex 033- 11064A or Route Manual chart MUNICH ILS Rwy 26R (11-4) )
Annex 033-11064A
The ILS frequency and identifier are ;
a)
108.3 IMNW
b)
108.7 IMSW
c)
108.3 IMSW
d)
108.7 IMNW
Answer ;
d)
108.7 IMNW
Ateş Murat Üstünbıçak , ATPL
217
Flight Planning & Monitoring
----------------------------------------------------------------------------------------------------------------------------------------------------------------445.
( For this question use annex 033- 11065A or Route Manual chart PARIS CHARLES DE GAULLE ILS Rwy 10 (21-8) )
Annex 033-11065A
The ILS localizer course is ;
a)
088°
b)
118°
c)
268°
d)
100°
Answer ;
a)
088°
Ateş Murat Üstünbıçak , ATPL
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Flight Planning & Monitoring
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
446.
( 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 ;
a)
172° ( G )
b)
353° ( G )
c)
177° ( G )
d)
194° ( G )
Answer ;
c)
177° ( G )
----------------------------------------------------------------------------------------------------------------------------------------------------------------447.
( 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 ;
a)
106°
b)
080°
c)
066°
d)
096°
Answer ;
a)
106°
----------------------------------------------------------------------------------------------------------------------------------------------------------------448.
( For this question use annex 033- 10996A or Route Manual chart E(LO)5 )
The initial magnetic course/distance from EELDE EEL 112.4 ( 53°10'N 006°40'E ) to WELGO ( 54°18'N 007°25'E ) on
airway A7 is ;
a)
023°/ 47 NM
b)
023°/ 157 NM
c)
024°/ 20 NM
d)
024°/ 73 NM
Answer ;
d)
024°/ 73 NM
----------------------------------------------------------------------------------------------------------------------------------------------------------------449.
( For this question use annex 033-12375A or Route Manual chart NAP )
The initial magnetic course from A ( 64°N 006°E ) to C ( 62°N 020°W ) is ;
a)
275°
b)
267°
c)
262°
d)
271°
Answer ;
a)
275°
----------------------------------------------------------------------------------------------------------------------------------------------------------------450.
( For this question use annex 033-12370A or Route Manual chart NAP )
The initial magnetic course from C ( 62°N 020°W ) to B ( 58°N 004°E ) is ;
a)
113°
b)
080°
c)
098°
d)
116°
Answer ;
d)
116°
----------------------------------------------------------------------------------------------------------------------------------------------------------------451.
( For this question use Route Manual chart E(HI)1 )
The initial magnetic course from INVERNESS 109.2 INS ( 57°32'N0 04°03'W ) direct to TIREE 117.7 TIR ( 56°30'N
006°53'W ) is ;
a)
230°
b)
218°
c)
244°
d)
237°
Answer ;
c)
244°
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
219
Flight Planning & Monitoring
452.
( For this question use Route Manual chart E(HI)1 )
The initial magnetic course from TIREE 117.7 TIR ( 56°30'N 006°53'W ) direct to INVERNESS 109.2 INS ( 57°32'N
004°03'W ) is ;
a)
236º
b)
064º
c)
048º
d)
056º
Answer ;
b)
064º
----------------------------------------------------------------------------------------------------------------------------------------------------------------453.
( For this question use Route Manual chart E(HI)1 )
The initial magnetic course from TIREE 117.7 TIR ( 56°30'N 006°53'W ) direct to STORNOWAY 115.1 STN ( 58°12'N
006°11'W ) is ;
a)
192º
b)
019º
c)
003º
d)
011º
Answer ;
b)
019º
----------------------------------------------------------------------------------------------------------------------------------------------------------------454.
( For this question use annex 033-12376A or Route Manual chart NAP )
The initial true course from A ( 64°N 006°E ) to C ( 62°N 020°W ) is ;
a)
271°
b)
246°
c)
275°
d)
267°
Answer ;
a)
271°
----------------------------------------------------------------------------------------------------------------------------------------------------------------455.
( For this question use annex 033-12371A or Route Manual chart NAP )
The initial true course from C ( 62°N 020°W ) to B ( 58°N 004°E ) is ;
a)
278°
b)
116°
c)
098°
d)
080°
Answer ;
c)
098°
----------------------------------------------------------------------------------------------------------------------------------------------------------------456.
( For this question use Route Manual chart E(HI)1 )
The initial true course from INVERNESS 109.2 INS ( 57°32'N 004°03'W ) direct to TIREE 117.7 TIR ( 56°30'N 006°53'W )
is ;
a)
218°
b)
230°
c)
244°
d)
237°
Answer ;
d)
237°
----------------------------------------------------------------------------------------------------------------------------------------------------------------457.
( For this question use Route Manual chart E(HI)1 )
The initial true course from TIREE 117.7 TIR ( 56°30'N 006°53'W ) direct to INVERNESS 109.2 INS ( 57°32'N 004°03'W )
is ;
a)
054°
b)
048°
c)
236°
d)
062°
Answer ;
a)
054°
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
220
Flight Planning & Monitoring
458.
( For this question use Route Manual chart E(HI)1 )
The initial true course from TIREE 117.7 TIR ( 56°30'N 006°53'W ) direct to STORNOWAY 115.1 STN ( 58°12'N 006°11'W
) is ;
a)
b)
c)
d)
019°
003°
011°
192°
Answer ;
c)
011°
----------------------------------------------------------------------------------------------------------------------------------------------------------------459.
( For this question use annex 033-12331A )
Annex 033-12331A
The lowest cloud conditions ( oktas/ft ) at BORDEAUX/MERIGNAC at 1330 UTC were ;
a)
1 to 2 at 3000
b)
3 to 4 at 2000
c)
3 to 4 at 800
d)
1 to 4 at 3000
Answer ;
a)
1 to 2 at 3000
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
221
Flight Planning & Monitoring
460.
( For this question use annex 033- 11066A or Route Manual chart ZURICH ILS Rwy 16 (11-2) )
Annex 033-11066A
The lowest published authorised RVR for an ILS approach glide slope out , all other aids serviceable , aircraft category A is ;
a)
720m
b)
800m
c)
1500m
d)
600m
Answer ;
a)
720m
Ateş Murat Üstünbıçak , ATPL
222
Flight Planning & Monitoring
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
461.
( 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 ;
a)
b)
c)
d)
349° / 26 NM
169° / 68 NM
169° / 42 NM
349° / 42 NM
Answer ;
c)
169° / 42 NM
----------------------------------------------------------------------------------------------------------------------------------------------------------------462.
( For this question use Route Manual chart E(LO)1 )
The magnetic course/distance from DEAN CROSS 115.2 DCS ( 54°43'N 003°20'W° ) to POLE HILL 112.1 POL ( 53°45'N
002°06'W ) on airway A2 is ;
a)
149º / 73 NM
b)
155º / 73 NM
c)
329º / 53 NM
d)
143º / 53 NM
Answer ;
a)
149º / 73 NM
----------------------------------------------------------------------------------------------------------------------------------------------------------------463.
( For this question use annex 033- 10993A or Route Manual chart E(HI)4 CAA-Edition )
The magnetic course/distance from DINKELSBUHL DKB 117.8 ( 49°09'N 010°14'E ) to ERLANGEN ERL 114.9
( 49°39'N 011°09'E ) on airway UR11 is ;
a)
050° / 47 NM
b)
230° / 97NM
c)
052° / 97 NM
d)
133° / 85 NM
Answer ;
a)
050° / 47 NM
----------------------------------------------------------------------------------------------------------------------------------------------------------------464.
( For this question use annex 033- 11003A or Route Manual chart E(HI)5 CAA-Edition )
The magnetic course/distance from ELBA ELB 114.7 ( 42°44'N 010°24'E ) to SPEZI ( 43°49'N 009°34'E ) on airway UA35
is ;
a)
332° / 76 NM
b)
332° / 118 NM
c)
322° / 60 NM
d)
152° / 42 NM
Answer ;
a)
332° / 76 NM
----------------------------------------------------------------------------------------------------------------------------------------------------------------465.
( 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 ;
a)
352° / 72 NM
b)
339° / 80 NM
c)
339° / 125 NM
d)
352° / 96 NM
Answer ;
a)
352° / 72 NM
----------------------------------------------------------------------------------------------------------------------------------------------------------------466.
( For this question use annex 033- 10994A or Route Manual chart E(LO)6 )
The magnetic course/distance from GROSTENQUIN GTQ 111.25 ( 49°00'N 006°43'E ) to LINNA ( 49°41'N 006°15'E ) on
airway R7 is ;
a)
157° / 58 NM
b)
337° / 46 NM
c)
337° / 58 NM
d)
337° / 31 NM
Answer ;
b)
337° / 46 NM
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
223
Flight Planning & Monitoring
467.
( 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 ;
a)
046° / 70 NM
b)
113° / 142 NM
c)
067° / 122 NM
d)
094° / 90 NM
Answer ;
d)
094° / 90 NM
----------------------------------------------------------------------------------------------------------------------------------------------------------------468.
( For this question use Route Manual chart E(LO)1 )
The magnetic course/distance from POLE HILL 112.1 POL ( 53°44'N 002°06'W) to TALLA 113.8 TLA ( 55°30'N
003°21'W ) on airway B4 is ;
a)
343º / 114 NM
b)
337º / 114 NM
c)
157º / 106 NM
d)
163º / 106 NM
Answer ;
a)
343º / 114 NM
----------------------------------------------------------------------------------------------------------------------------------------------------------------469.
( For this question use annex 033- 11002A or Route Manual chart E(HI)4 CAA-Edition )
The magnetic course/distance from SALZBURG SBG 113.8 ( 48°00'N 012°54'E ) to STAUB ( 48°44'N 012°38'E ) on
airway UB5 is ;
a)
346° / 43 NM
b)
166° / 64 NM
c)
346° / 45 NM
d)
346° / 64 NM
Answer ;
c)
346° / 45 NM
----------------------------------------------------------------------------------------------------------------------------------------------------------------470.
( For this question use annex 033- 11001A or Route Manual chart E(HI)4 CAA-Edition )
The magnetic course/distance from ST PREX SPR 113.9 ( 46°28'N 006°27'E ) to FRIBOURG FRI 115.1 ( 46°47'N
007°14'E ) on airway UG60 is ;
a)
048° / 46 NM
b)
041° / 78 NM
c)
061° / 28 NM
d)
061° / 37 NM
Answer ;
d)
061° / 37 NM
----------------------------------------------------------------------------------------------------------------------------------------------------------------471.
( For this question use Route Manual chart E(LO)1 )
The magnetic course/distance from TALLA 113.8 TLA ( 55°30'N 003°21'W ) to DEAN CROSS 115.2 DCS ( 54°43'N
003°20'W ) on airway A2 is ;
a)
185° / 18 NM
b)
005° / 18 NM
c)
185° / 47 NM
d)
005° / 47 NM
Answer ;
c)
185° / 47 NM
----------------------------------------------------------------------------------------------------------------------------------------------------------------472.
( For this question use annex 033- 11000A or Route Manual chart E(HI)4 CAA-Edition )
The magnetic course/distance from TANGO TGO 112.5 ( 48°37'N 009°16'E ) to DINKELSBUHL DKB 117.8 ( 49°09'N
010°14E ) on airway UR11 is ;
a)
132° / 43 NM
b)
105° / 105 NM
c)
052° / 50 NM
d)
007° / 60 NM
Answer ;
c)
052° / 50 NM
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
224
Flight Planning & Monitoring
473.
( For this question use annex 033- 10999A or Route Manual chart E(HI)4 CAA-Edition )
The magnetic course/distance from TRENT TNT 115.7 ( 53°03'N 001°40'W ) to WALLASEY WAL 114.1 ( 53°23'N
003°08W ) on airway VR3 is ;
a)
117° / 71 NM
b)
297° / 57 NM
c)
297° / 70 NM
d)
117° / 57 NM
Answer ;
b)
297° / 57 NM
----------------------------------------------------------------------------------------------------------------------------------------------------------------474.
( 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 ;
a)
279° / 85 NM
b)
279° / 114 NM
c)
311° / 85 NM
d)
311° / 114 NM
Answer ;
a)
279° / 85 NM
----------------------------------------------------------------------------------------------------------------------------------------------------------------475.
( For this question use Route Manual chart E(LO)1 )
The magnetic course from DEAN CROSS 115.2 DCS ( 54°43'N 003°20'W° ) to NEWCASTLE 114.25 NEW ( 55°02'N
001°41'W ) on airway W911D is ;
a)
083º
b)
263º
c)
077º
d)
257º
Answer ;
c)
077º
----------------------------------------------------------------------------------------------------------------------------------------------------------------476.
( For this question use TRM , Barcelona Area chart (10-1V) )
The maximum altitude that may be used to transit the whole VFR corridor from REUS to SAN CELONI is ;
a)
2000 ft
b)
4500 ft
c)
3000 ft
d)
3500 ft
Answer ;
a)
2000 ft
----------------------------------------------------------------------------------------------------------------------------------------------------------------477.
The maximum permissible take-off mass of an aircraft for the L wake turbulence category on an ATC flight plan is ;
a)
2 700 kg
b)
7 000 kg
c)
5 700 kg
d)
10 000 kg
Answer ;
b)
7 000 kg
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
225
Flight Planning & Monitoring
478.
( For this question use annex 033-12320A )
Annex 033-12320A
The maximum wind velocity ( °/ kt ) immediately north of TUNIS ( 36°N 010°E ) is ;
a)
250/85
b)
280/110
c)
180/105
d)
190/95
Answer ;
d)
190/95
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
226
Flight Planning & Monitoring
479.
( For this question use annex 033-11181A )
Annex 033-11181A
The maximum wind velocity ( °/
kt ) shown in the vicinity of MUNICH ( 48°N 012°E ) is ;
a)
300/100
b)
300/160
c)
300/140
d)
290/110
Answer ;
c)
300/140
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
227
Flight Planning & Monitoring
480.
( For this question use annex 033- 11062A or Route Manual chart LONDON HEATHROW ILS DME Rwy 09R (11-1) )
Annex 033-11062A
The Minimum Descent Altitude ( MDA ) for an ILS glide slope out , is ;
a)
480 ft
b)
405 ft
c)
275 ft
d)
200 ft
Answer ;
a)
480 ft
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
228
Flight Planning & Monitoring
481.
( 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 ;
a)
FL260
b)
FL210
c)
FL250
d)
FL200
Answer ;
c)
FL250
----------------------------------------------------------------------------------------------------------------------------------------------------------------482.
( For this question use Route Manual chart E(LO)1 )
The minimum enroute altitude ( MEA ) that can be maintained continuously on advisory route W911D from NEWCASTLE
114.25 NEW ( 55°02'N 001°24'W ) to DEAN CROSS 115.2 DCS ( 54°43'N 003°20'W ) is ;
a)
4700 ft
b)
FL150
c)
4520 ft
d)
FL50
Answer ;
d)
FL50
----------------------------------------------------------------------------------------------------------------------------------------------------------------483.
( For this question use Route Manual chart E(LO)1 )
The minimum enroute altitude ( MEA ) that can be maintained continuously on airway B226 from TALLA 113.8 TLA
( 55°30 N003°21'W ) to reporting point ANGUS ( 56°42'N003°03'W ) is ;
a)
5000 ft
b)
FL80
c)
FL70
d)
5500 ft
Answer ;
c)
FL70
----------------------------------------------------------------------------------------------------------------------------------------------------------------484.
( For this question use annex 033- 11027A or Route Manual chart E(LO)2 )
The minimum enroute altitude ( MEA ) that can be maintained continuously on airway G4 from JERSEY JSY 112.2
( 49°13'N 002°03'W ) to LIZAD ( 49°35'N 004°20'W ) is ;
a)
2800 ft MSL
b)
1000 ft MSL
c)
FL60
d)
FL140
Answer ;
d)
FL140
----------------------------------------------------------------------------------------------------------------------------------------------------------------485.
( For this question use Route Manual chart E(LO)1 )
The minimum enroute altitude ( MEA ) that can be maintained continuously on airway L602 from TALLA 113.8 TLA
( 55°30N 003°21'W ) to NEWCASTLE 114.25 NEW ( 55°02'N001°24'W ) is ;
a)
FL200
b)
3900 ft
c)
3100 ft
d)
FL100
Answer ;
a)
FL200
----------------------------------------------------------------------------------------------------------------------------------------------------------------486.
( For this question use Route Manual chart E(LO)5 )
The minimum enroute altitude that can be maintained continuously on airway B65/H65 from DOXON ( 55°27'N 018°10'E )
to RONNE ROE 112.0 ( 55°04'N 014°46'E ) is ;
a)
1000 ft
b)
FL60
c)
FL100
d)
2500 ft
Answer ;
c)
FL100
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
229
Flight Planning & Monitoring
487.
( For this question use annex 033- 11025A or Route Manual chart E(LO)1 )
The minimum enroute altitude that can be maintained continuously on airway G1 from STRUMBLE STU 113.1 ( 52°00'N
005°02'W ) to BRECON BCN 117.45 ( 51°43'N 003°16'W ) is ;
a)
4100ft MSL
b)
FL80
c)
FL110
d)
2900 ft MSL
Answer ;
c)
FL110
----------------------------------------------------------------------------------------------------------------------------------------------------------------488.
( For this question use annex 033-11029A or Route Manual chart E(LO)5 )
The minimum enroute altitude that can be maintained continuously on airway G24 from KOLJA ( 56° 00'N 016°49'E ) to
RONNE ROE 112.0 ( 55°04'N 014°46'E ) is ;
a)
FL100
b)
1000ft
c)
2500 ft
d)
FL60
Answer ;
a)
FL100
----------------------------------------------------------------------------------------------------------------------------------------------------------------489.
( For this question use annex 033- 11024A or Route Manual chart E(HI)4 CAA-Edition )
The minimum enroute altitude that can be maintained continuously on airway UA34 from WALLASEY WAL 114.1
( 53°23'N 003°08'W ) to MIDHURST MID 114.0 ( 51°03'N 000°37'W ) is ;
a)
FL290
b)
FL250
c)
FL330
d)
FL245
Answer ;
a)
FL290
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
230
Flight Planning & Monitoring
490.
( For this question use annex 033- 11060A or Route Manual chart MADRID BARAJAS ILS DME Rwy 33 (11-1) )
Annex 033-11060A
The minimum glide slope interception altitude for a full ILS is ;
a)
3500 ft
b)
4000 ft
c)
2067 ft
d)
1567 ft
Answer ;
b)
4000 ft
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
231
Flight Planning & Monitoring
491.
( For this question use annex 033- 11042A or Route Manual STAR chart for LONDON HEATHROW (10-2D) )
Annex 033-11042A
The minimum holding altitude ( MHA ) and maximum holding speed ( IAS ) at MHA at OCKHAM OCK 115.3 are ;
a)
9000ft and 250kt
b)
7000ft and 250kt
c)
7000 ft and 220kt
d)
9000ft and 220kt
Answer ;
c)
7000 ft and 220kt
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
232
Flight Planning & Monitoring
492.
( For this question use annex 033- 11059A or Route Manual chart AMSTERDAM SCHIPHOL ILS DME Rwy 22 (11-6) )
Annex 033-11059A
The Missed Approach procedure is to climb to an altitude of (i) .................... on a track of (ii) .....................
a)
(i) 3000 ft , (ii) 160°
b)
(i) 200 ft , (ii) 223°
c)
(i) 3000 ft , (ii) 223°
d)
(i) 2000 ft , (ii) 160°
Answer ;
d)
(i) 2000 ft , (ii) 160°
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
233
Flight Planning & Monitoring
493.
The navigation plan reads ;
Trip fuel : 100 kg
Flight time : 1 h 35 min
Taxi fuel : 3 kg
Block fuel : 181 kg
The endurance on the ICAO flight plan should read ;
a)
2 h 04 min
b)
1 h 35 min
c)
2 h 49 min
d)
2 h 52 min
Answer ;
c)
2 h 49 min
----------------------------------------------------------------------------------------------------------------------------------------------------------------494.
The navigation plan reads ;
Trip fuel : 136 kg
Flight time : 2 h 45 min
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 ;
a)
3 h 38 min
b)
3 h 34 min
c)
2 h 49 min
d)
2 h 45 min
Answer ;
b)
3 h 34 min
----------------------------------------------------------------------------------------------------------------------------------------------------------------495.
( For this question use annex 033- 11015A or Route Manual chart E(LO)5 )
The NDB at DENKO ( 52°49'N 015°50'E ) can be identified on ;
a)
Channel 440 , BFO off
b)
Frequency 440 kHz , BFO off
c)
Frequency 440 kHz , BFO on
d)
Channel 440 , BFO on
Answer ;
c)
Frequency 440 kHz , BFO on
----------------------------------------------------------------------------------------------------------------------------------------------------------------496.
The planned departure time from the parking area is 1815 UTC. The estimated take-off time is 1825 UTC. The flight plan
must be filed with ATC at the latest at ;
a)
1755 UTC
b)
1725 UTC
c)
1715 UTC
d)
1745 UTC
Answer ;
c)
1715 UTC
----------------------------------------------------------------------------------------------------------------------------------------------------------------497.
( For this question use annex 033-11717A )
Annex 033-11717A
The planned flight is over a distance of 440 NM. Based on the wind charts at altitude the following components are found ;
FL50 : -30 kt , FL100 : -50 kt , FL180 : -70 kt
The Operations Manual in appendix details the aircraft’s performances. Which of the following flight levels ( FL ) gives the
best range performance ;
a)
Either FL 050 or FL 100
b)
FL 180
c)
FL 050
d)
FL 100
Answer ;
b)
FL 180
Ateş Murat Üstünbıçak , ATPL
234
Flight Planning & Monitoring
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
498.
The purpose of the decision point procedure is ;
a)
to increase the safety of the flight.
b)
to reduce the landing weight and thus reduce the structural stress on the aircraft.
c)
to reduce the minimum required fuel and therefore be able to increase the traffic load.
d)
to increase the amount of extra fuel.
Answer ;
c)
to reduce the minimum required fuel and therefore be able to increase the traffic load.
----------------------------------------------------------------------------------------------------------------------------------------------------------------499.
The quantity of fuel which is calculated to be necessary for a jet aeroplane to fly IFR from departure aerodrome to the
destination aerodrome is 5352 kg. Fuel consumption in holding mode is 6000 kg/h. Alternate fuel is 4380 kg. Contingency should be
5% of trip fuel. What is the minimum required quantity of fuel which should be on board at take-off ?
a)
13370 kg.
b)
14500 kg.
c)
13000 kg.
d)
13220 kg.
Answer ;
c)
13000 kg.
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
235
Flight Planning & Monitoring
500.
( For this question use annex 033- 11061A or Route Manual chart AMSTERDAM JAA MINIMUMS (10-x) )
Annex 033-11061A
The Radio Altimeter minimum altitude for a CAT 2 ILS DME approach to Rwy 01L is ;
a)
300 ft
b)
100 ft
c)
188 ft
d)
88 ft
Answer ;
b)
100 ft
Ateş Murat Üstünbıçak , ATPL
236
Flight Planning & Monitoring
----------------------------------------------------------------------------------------------------------------------------------------------------------------501.
( For this question use Route Manual chart E(HI)2 )
The radio navigation aid at ( 57°45'N 013°48'E ) is a ;
a)
VOR , frequency 355 MHz.
b)
VOR , frequency 355 kHz
c)
NDB , frequency 355 MHz.
d)
NDB , frequency 355 kHz.
Answer ;
d)
NDB , frequency 355 kHz.
----------------------------------------------------------------------------------------------------------------------------------------------------------------502.
( 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 ;
a)
an NDB , frequency 420 kHz , NOT continuous operation
b)
an NDB , frequency 420 kHz , continuous operation
c)
a fan marker , frequency 420 kHz
d)
a TACAN , channel 420
Answer ;
a)
an NDB , frequency 420 kHz , NOT continuous operation
----------------------------------------------------------------------------------------------------------------------------------------------------------------503.
( 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 ;
a)
VOR , frequency 114.1 MHz , and TACAN frequency 408 MHz
b)
VOR , frequency 114.1 MHz , and TACAN channel 408
c)
VOR/DME only , frequency 114.1 MHz
d)
VOR/DME , frequency 114.1 MHz , and NDB frequency 408 kHz
Answer ;
d)
VOR/DME , frequency 114.1 MHz , and NDB frequency 408 kHz
----------------------------------------------------------------------------------------------------------------------------------------------------------------504.
( For this question use Route Manual chart E(LO)1 )
The radio navigation aid at LEEDS BRADFORD ( 53°52'N 001°39'W ) is ;
a)
an NDB , frequency 402.5 kHz , NOT continuous operation
b)
a TACAN , channel 402.5
c)
a fan marker , frequency 402.5 kHz
d)
an NDB , frequency 402.5 kHz , continuous operation
Answer ;
a)
an NDB , frequency 402.5 kHz , NOT continuous operation
----------------------------------------------------------------------------------------------------------------------------------------------------------------505.
( For this question use Annex 033- 11013A or Route Manual chart E(LO)1 )
The radio navigation aid at SHANNON ( 52°43'N 008°53'W ) is ;
a)
an NDB , frequency 352 kHz
b)
a VOR only , frequency 113.3 MHz
c)
a TACAN , frequency 113.3 kHz
d)
a VOR/DME , frequency 113.3 MHz
Answer ;
d)
a VOR/DME , frequency 113.3 MHz
----------------------------------------------------------------------------------------------------------------------------------------------------------------506.
( For this question use Route Manual chart E(LO)1 )
The radio navigation aid at ST ABBS ( 55°55'N 002°12'W ) is ;
a)
a TACAN , channel 112.5
b)
a VORDME , frequency 112.5 MHz
c)
an NDB , frequency 112.5 MHz
d)
a VOR only , frequency 112.5 MHz
Answer ;
b)
a VORDME , frequency 112.5 MHz
----------------------------------------------------------------------------------------------------------------------------------------------------------------507.
( For this question use annex 033- 11007A or Route Manual chart E(HI)4 CAA-Edition )
The radio navigation aid at ST DIZIER ( 48°38N 004°53'E ) is a ;
a)
VOR , frequency 114.0 MHz , and TACAN channel 87
b)
TACAN , channel 87 , frequency 114.0 MHz
c)
TACAN , channel 114.0
d)
TACAN , channel 87 , and NDB frequency 114.0 kHz
Answer ;
b)
TACAN , channel 87 , frequency 114.0 MHz
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
237
Flight Planning & Monitoring
508.
( For this question use annex 033- 11008A or Route Manual chart E(HI)4 CAA-Edition )
The radio navigation aid at TOPCLIFFE ( 54°12'N 001°22'W ) is a ;
a)
VORTAC , frequency 113.7 MHz , and an NDB frequency 92 kHz.
b)
TACAN only , channel 84 , ( frequency 113.7 MHz )
c)
TACAN , channel 84 , and a VOR frequency 113.7 MHz only.
d)
TACAN , channel 84 , and an NDB frequency 92 kHz only.
Answer ;
b)
TACAN only , channel 84 , ( frequency 113.7 MHz )
----------------------------------------------------------------------------------------------------------------------------------------------------------------509.
( For this question use annex 033- 11008A or Route Manual chart E(HI)4 CAA-Edition )
The radio navigation aid at ZURICH ( 47°36'N 008°49'E ) is ;
a)
a VOR only , frequency 115.0 MHz
b)
an NDB only , frequency 115.0 kHz
c)
a TACAN , frequency 115.0 MHz
d)
a VOR/DME , frequency 115.0MHz
Answer ;
a)
a VOR only , frequency 115.0 MHz
----------------------------------------------------------------------------------------------------------------------------------------------------------------510.
( For this question use annex 033- 11011A or Route Manual chart E(HI)4 CAA-Edition )
The radio navigation aid on airway UG4 at LUXEUIL ( 47°41'N 006°18'E ) is a ;
a)
VOR/DME only , identifier LUL
b)
VOR only , identifier LUL
c)
VOR , identifier LUL , frequency paired with TACAN identifier LXI
d)
VOR/DME and NDB , identifier LXI
Answer ;
b)
VOR only , identifier LUL
----------------------------------------------------------------------------------------------------------------------------------------------------------------511.
( For this question use annex 033- 11006A or Route Manual chart E(HI)4 CAA-Edition )
The radio navigation aid serving STRASBOURG ( 48°30'N 007°34'E ) is a ;
a)
VOR only , frequency 115.6 MHz
b)
DME only , channel 115.6
c)
VOR/TACAN , frequency 115.6 MHz
d)
TACAN only , frequency 115.6 MHz
Answer ;
c)
VOR/TACAN , frequency 115.6 MHz
----------------------------------------------------------------------------------------------------------------------------------------------------------------512.
( For this question use annex 033- 11009A or Route Manual chart E(HI)4 CAA-Edition )
The radio navigation aid STAD ( 51°45'N 004°15'E ) is ;
a)
a VOR/DME , on channel 386
b)
a TACAN , on channel 386
c)
a VOR , frequency 386 MHz
d)
an NDB , frequency 386 kHz
Answer ;
d)
an NDB , frequency 386 kHz
----------------------------------------------------------------------------------------------------------------------------------------------------------------513.
( For this question use Route Manual chart E(HI)2 )
The radio navigation aid(s) at ( 55°26'N 011°38'E ) is/are ;
a)
VORDME , frequency 128.75 MHz.
b)
NDB , frequency 112.8 kHz.
c)
VORDME , frequency 112.8 MHz.
d)
VORDME , frequency 128.15 MHz.
Answer ;
c)
VORDME , frequency 112.8 MHz.
----------------------------------------------------------------------------------------------------------------------------------------------------------------514.
( For this question use Route Manual chart E(HI)2 )
The radio navigation aid(s) at ( 55°59'N 014°06'E ) is/are ;
a)
VORDME , frequency 116.9 MHz.
b)
NDB , frequency 116.9 kHz.
c)
NDB , frequency 363 kHz.
d)
VOR , frequency 363 kHz.
Answer ;
c)
NDB , frequency 363 kHz.
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
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Flight Planning & Monitoring
515.
( For this question use Route Manual chart E(HI)2 )
The radio navigation aid(s) at ( 56°09'N 013°14'E ) is/are ;
a)
VORDME , frequency 116.9 MHz.
b)
VOR , frequency 116.2 MHz.
c)
VOR , frequency 116.9 MHz.
d)
VORDME , frequency 116.2 MHz.
Answer ;
c)
VOR , frequency 116.9 MHz.
----------------------------------------------------------------------------------------------------------------------------------------------------------------516.
( For this question use Route Manual chart E(HI)2 )
The radio navigation aid(s) at ( 56°17'N 010°47'E ) is/are ;
a)
VOR , frequency 374 MHz.
b)
VORDME , frequency 374 kHz.
c)
NDB, frequency 374 kHz , for Temporary Use ( TU ).
d)
NDB , frequency 374 kHz.
Answer ;
d)
NDB , frequency 374 kHz.
----------------------------------------------------------------------------------------------------------------------------------------------------------------517.
( For this question use Route Manual chart E(HI)1 )
The radio navigation aid(s) at ( 57°32'N 004°03'W ) is/are ;
a)
VORDME , frequency 109.2 MHz.
b)
VORDME , frequency 109.2 kHz.
c)
VOR , frequency 109.2 MHz , no DME available.
d)
VOR , frequency 109.2 MHz , for INS update only.
Answer ;
a)
VORDME , frequency 109.2 MHz.
----------------------------------------------------------------------------------------------------------------------------------------------------------------518.
The required time for final reserve fuel for turbojet aeroplane is ;
a)
Variable with wind velocity.
b)
60 min.
c)
45 min.
d)
30 min.
Answer ;
d)
30 min.
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
239
Flight Planning & Monitoring
519.
( For this question use annex 033- 11043A or Route Manual STAR charts for PARIS CHARLES DE GAULLE (20-2) )
Annex 033-11043A
The route distance from CHIEVRES ( CIV ) to BOURSONNE ( BSN ) is ;
a)
88 NM
b)
83 NM
c)
73 NM
d)
96 NM
Answer ;
d)
96 NM
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
240
Flight Planning & Monitoring
520.
( For this question use annex 033- 11047A or Route Manual SID chart for AMSTERDAM SCHIPHOL (10-3B) )
Annex 033-11047A
The route distance from runway 27 to ARNEM is ;
a)
35 NM
b)
59 NM
c)
52 NM
d)
67 NM
Answer ;
d)
67 NM
Ateş Murat Üstünbıçak , ATPL
241
Flight Planning & Monitoring
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
521.
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 ?
a)
193 NM
b)
174 NM
c)
188 NM
d)
203 NM
Answer ;
b)
174 NM
----------------------------------------------------------------------------------------------------------------------------------------------------------------522.
( For this question use annex 033-12320A )
Annex 033-12320A
The surface system over VIENNA ( 48°N 016°E ) is a ;
a)
cold front moving west
b)
cold front moving east
c)
warm front moving north
d)
stationary occluded front
Answer ;
b)
cold front moving east
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
242
Flight Planning & Monitoring
523.
( For this question use annex 033-11181A )
Annex 033-11181A
The surface weather system over England ( 53°N 002°W ) is ;
a)
a cold front moving east
b)
a warm front moving southeast
c)
an occluded front moving east
d)
a depression moving north
Answer ;
c)
an occluded front moving east
----------------------------------------------------------------------------------------------------------------------------------------------------------------524.
( For this question use annex 033-12332A )
Annex 033-12332A
The surface wind velocity ( °/ kt ) at PARIS/CHARLES-DE-GAULLE at 1330 UTC was ;
a)
180/12
b)
300/05
c)
270/04
d)
270/08
Answer ;
c)
270/04
Ateş Murat Üstünbıçak , ATPL
243
Flight Planning & Monitoring
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
525.
( For this question use annex 033-11704A )
True Air speed : 170 kt
Wind 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 ;
a)
1 326 litres
b)
1 182 litres
c)
1 600 litres
d)
1 545 litres
Answer ;
d)
1 545 litres
----------------------------------------------------------------------------------------------------------------------------------------------------------------526.
The Trip Fuel for a jet aeroplane to fly from the departure aerodrome to the destination aerodrome is 5350 kg. Fuel
consumption in holding mode is 6000 kg/h. The quantity of fuel which is needed to carry out one go-around and land on the alternate
airfield is 4380 kg. The destination aerodrome has a single runway. What is the minimum quantity of fuel which should be on board at
take-off ?
a)
13 000 kg
b)
13 230 kg
c)
14 730 kg
d)
11 730 kg
Answer ;
b)
13 230 kg
----------------------------------------------------------------------------------------------------------------------------------------------------------------527.
( For this question refer to Image 1 )
Image 1
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 ;
a)
052º
b)
040º
c)
044º
d)
058º
Answer ;
a)
052º
----------------------------------------------------------------------------------------------------------------------------------------------------------------528.
( For this question use annex 033- 11014A or Route Manual chart E(LO)5 )
The VOR and TACAN on airway G9 at OSNABRUCK ( 52°12'N 008°17'E ) are ;
a)
frequency paired , and have different identifiers
b)
NOT frequency paired , and have different identifiers
c)
NOT frequency paired , and have the same identifier
d)
frequency paired , and have the same identifier
Answer ;
b)
NOT frequency paired , and have different identifiers
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
244
Flight Planning & Monitoring
529.
( For this question use annex 033-11190A )
Annex 033-11190A
The wind direction and velocity ( °/ kt ) at 40°N 040°E is ;
a)
300/75
b)
330/85
c)
330/75
d)
150/75
Answer ;
c)
330/75
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
245
Flight Planning & Monitoring
530.
( For this question use annex 033-11190A )
Annex 033-11190A
The wind direction and velocity ( °/ kt ) at 50°N 040°E is ;
a)
200/70
b)
020/70
c)
020/80
d)
350/70
Answer ;
b)
020/70
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
246
Flight Planning & Monitoring
531.
( For this question use annex 033-11190A )
Annex 033-11190A
The wind direction and velocity ( °/ kt ) at 60°N 015°W is ;
a)
290/155
b)
290/185
c)
110/155
d)
320/155
Answer ;
a)
290/155
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
247
Flight Planning & Monitoring
532.
( For this question use annex 033-11189A )
Annex 033-11181A
The wind velocity over ITALY is ;
a)
110 kt at FL380 maximum velocity not shown on chart
b)
a maximum of 110 kt at FL380
c)
130 kt at FL380 maximum velocity not shown on chart
d)
a maximum of 160 kt at FL 380
Answer ;
b)
a maximum of 110 kt at FL380
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
248
Flight Planning & Monitoring
533.
( For this question use annex 033-12314A )
Annex 033-12314A
The W/V ( °/ kt ) at 40°N 020°W is ;
a)
155/40
b)
334/40
c)
135/40
d)
310/40
Answer ;
d)
310/40
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
249
Flight Planning & Monitoring
534.
( For this question use annex 033-12314A )
Annex 033-12314A
The W/V ( °/ kt ) at 50°N015°W is ;
a)
310/85
b)
310/75
c)
290/75
d)
100/75
Answer ;
c)
290/75
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
250
Flight Planning & Monitoring
535.
( For this question use annex 033-12314A )
Annex 033-12314A
The W/V ( °/ kt ) at 60° N015° W is ;
a)
300/60
b)
115/60
c)
320/60
d)
300/70
Answer ;
a)
300/60
----------------------------------------------------------------------------------------------------------------------------------------------------------------536.
( For this question refer to Image 2 )
Image 2
True Air speed :170 kt , Wind 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 ;
a)
1 600 litres
b)
1 182 litres
c)
1 545 litres
d)
1 326 litres
Answer ;
c)
1 545 litres
Ateş Murat Üstünbıçak , ATPL
251
Flight Planning & Monitoring
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
537.
Unless otherwise shown on charts for standard instrument departure the routes are given with ;
a)
true headings
b)
magnetic course
c)
magnetic headings
d)
true course
Answer ;
b)
magnetic course
----------------------------------------------------------------------------------------------------------------------------------------------------------------538.
( For this question use annex 033-12364A or Flight Planning Manual MRJT 1 Figure 4.7.2 )
Annex 033-12364A
Using the above table , in ISA conditions and at a speed of M.70/280 KIAS , in an elapsed time of 90 minutes an aircraft
with mass at point of diversion 48000 kg could divert a distance of ;
a)
584 NM
b)
603 NM
c)
608 NM
d)
563 NM
Answer ;
a)
584 NM
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
252
Flight Planning & Monitoring
539.
( For this question use Flight Planning Manual SEP 1 Figure 2.3 Table 2.3.1 )
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 conditions ;
Given ;
OAT : 3°C
Pressure altitude : 6000 ft
Power : Full throttle / 21.0 in/Hg / 2100 RPM
a)
136 kt and 56.9 lbs/hr
b)
131 kt and 56.9 lbs/hr
c)
125 kt and 55.7 lbs/hr
d)
134 kt and 55.7 lbs/hr
Answer ;
d)
134 kt and 55.7 lbs/hr
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
253
Flight Planning & Monitoring
540.
( For this question use Flight Planning Manual SEP 1 Figure 2.2 Table 2.2.3 )
Flight Planning Manual SEP 1 Figure 2.2 Table 2.2.3
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 conditions ;
Given ;
OAT : 13°C
Pressure altitude : 8000 ft
RPM : 2300
a)
160 kt and 71.1 lbs/hr
b)
160 kt and 69.3 lbs/hr
c)
159 kt and 71.7 lbs/hr
d)
158 kt and 74.4 lbs/hr
Answer ;
b)
160 kt and 69.3 lbs/hr
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
254
Flight Planning & Monitoring
541.
( For this question use Flight Planning Manual SEP 1 Figure 2.2 Table 2.2.3 )
Flight Planning Manual SEP 1 Figure 2.2 Table 2.2.3
Using the Power Setting Table , for the single engine aeroplane , determine the manifold pressure and fuel flow ( lbs/hr ) with
full throttle and cruise lean mixture in the following conditions ;
Given ;
OAT : 13°C
Pressure altitude : 8000 ft
RPM : 2300
a)
22.4 in.Hg and 69.3 lbs/hr
b)
22.4 in.Hg and 71.1 lbs/hr
c)
22.4 in.Hg and 73.8 lbs/hr
d)
23.0 in.Hg and 69.0 lbs/hr
Answer ;
a)
22.4 in.Hg and 69.3 lbs/hr
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
255
Flight Planning & Monitoring
542.
( For this question use Flight Planning Manual SEP 1 Figure 2.4 Table 2.4 )
Flight Planning Manual SEP 1 Figure 2.4 Table 2.4
Using the Range Profile Diagramm , for the single engine aeroplane , determine the range, with 45 minutes reserve , in the
following conditions ;
Given ;
O.A.T. : ISA +16°C
Pressure altitude : 4000 ft
Power : Full throttle / 25.0 in/Hg / 2100 RPM
a)
865 NM
b)
739 NM
c)
911 NM
d)
851 NM
Answer ;
a)
865 NM
----------------------------------------------------------------------------------------------------------------------------------------------------------------543.
VFR flights shall not be flown over the congested areas of cities at a height less than ;
a)
1000 ft above the highest obstacle within a radius of 600 m from the aircraft.
b)
the highest obstacle.
c)
2000 ft above the highest obstacle within a radius of 600 ft from the aircraft.
d)
500 ft above the highest obstacle.
Answer ;
a)
1000 ft above the highest obstacle within a radius of 600 m from the aircraft.
----------------------------------------------------------------------------------------------------------------------------------------------------------------544.
( For this question use Route Manual chart E(LO)1 )
What are the applicable GRID MORAs for a flight from DEAN CROSS 115.2 DCS ( 54°43'N 003°20'W ) to TALLA 113.8
TLA ( 55°30'N 003°21'W ) on airway A2 ?
a)
45 and 39
b)
45 and 40
c)
42 and 40
d)
42 and 39
Answer ;
b)
45 and 40
Ateş Murat Üstünbıçak , ATPL
256
Flight Planning & Monitoring
----------------------------------------------------------------------------------------------------------------------------------------------------------------545.
( For this question use TRM (VFR) , Aberdeen (Dyce) Information Page (19-6) )
What are the designated departure routes when using (i) Rwy 34 and (ii) Rwy 05 ?
a)
(i) H1 , (ii) H3
b)
(i) H6 , (ii) H2
c)
(i) H5 , (ii) H1
d)
(i) H2 , (ii) H4
Answer ;
d)
(i) H2 , (ii) H4
----------------------------------------------------------------------------------------------------------------------------------------------------------------546.
( For this question use TRM , Esbjerg Aerodrome chart (19-2) )
What are the dimensions of runway 08/36 at Esbjerg ?
a)
8530 ft x 45 ft
b)
8530 m x 45 m
c)
2600 ft x 148 ft
d)
2600 m x 45 m
Answer ;
d)
2600 m x 45 m
----------------------------------------------------------------------------------------------------------------------------------------------------------------547.
( For this question use Route Manual chart E(LO)1 )
What are the magnetic course and distance when flying on airway B4 from the reporting point SHAPP ( 54°30'N 002°38W )
to the reporting point ESKDO ( 55°18'N 003°12'W ) ?
a)
163º / 39 NM
b)
343º / 52 NM
c)
343º / 114 NM
d)
163º / 52 NM
Answer ;
b)
343º / 52 NM
----------------------------------------------------------------------------------------------------------------------------------------------------------------548.
( For this question use TRM (VFR) , Aberdeen (Dyce) Area chart (19-5) )
What ATIS frequency(ies) is/are available when on the ground ?
a)
114.30 or 121.85
b)
121.85 only
c)
121.70 or 121.85
d)
121.70 only
Answer ;
a)
114.30 or 121.85
----------------------------------------------------------------------------------------------------------------------------------------------------------------549.
( For this question use Route Manual VFR+GPS chart ED-6 )
What is elevation of LSZH ZURICH KLOTHEN airport ( 47°28'N , 008°33'E ) ?
a)
1572 ft
b)
1416 ft
c)
1000 m
d)
1421 ft
Answer ;
b)
1416 ft
----------------------------------------------------------------------------------------------------------------------------------------------------------------550.
( For this question use TRM , De Kooy Area chart (19-1) )
What is (i) the frequency and (ii) QDM of the ILS at De Kooy Aerodrome ?
a)
(i) 123.30 , (ii) 220ºT
b)
(i) 123.30 , (ii) 220ºM
c)
(i) 109.70 , (ii) 216ºM
d)
(i) 109.70 , (ii) 214ºT
Answer ;
c)
(i) 109.70 , (ii) 216ºM
----------------------------------------------------------------------------------------------------------------------------------------------------------------551.
( For this question use TRM (VFR) , Aberdeen (Dyce) Area chart (19-5) )
What is the ATIS frequency that may not be used when in flight ?
a)
121.70
b)
114.30
c)
121.85
d)
118.10
Answer ;
c)
121.85
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
257
Flight Planning & Monitoring
552.
( For this question use Route Manual chart E(HI)1 )
What is the average magnetic course from ABERDEEN ( 57º19'N 002º16'W ) to TIREE ( 56º30'N 006º53'W ) ?
a)
247º
b)
260º
c)
253º
d)
267º
Answer ;
b)
260º
----------------------------------------------------------------------------------------------------------------------------------------------------------------553.
( For this question use TRM (VFR) , Aberdeen (Dyce) Area chart (10-1V) )
What is the correct frequency to contact Scottish Information when overhead reporting point “BANCHORY” to the
southwest of Aberdeen Airport ?
a)
126.25
b)
135.17
c)
134.10
d)
119.87
Answer ;
d)
119.87
----------------------------------------------------------------------------------------------------------------------------------------------------------------554.
( For this question use TRM , Esbjerg Area chart (19-1) )
What is the course and distance from Locator HP to the threshold of Runway 08 ?
a)
080º (T) / 4.2 Km
b)
080º (M) / 4.2 NM
c)
080º (M) / 4.2 Km
d)
080º (T) / 4.2 NM
Answer ;
b)
080º (M) / 4.2 NM
----------------------------------------------------------------------------------------------------------------------------------------------------------------555.
( For this question use TRM (VFR) , Aberdeen (Dyce) Information Page (19-6) )
What is the designated departure route when using Runway 23 in bad weather and/or low visibility ?
a)
H1
b)
H3
c)
H5
d)
H6
Answer ;
d)
H6
----------------------------------------------------------------------------------------------------------------------------------------------------------------556.
( For this question use annex 033-11198A )
What is the earliest time ( UTC ) , if any, that thunderstorms are forecast for DOHA ( OTBD ) ?
a)
0800
b)
Nil forecast
c)
1000
d)
0600
Answer ;
c)
1000
----------------------------------------------------------------------------------------------------------------------------------------------------------------557.
( For this question use annex 033-12334A )
Annex 033-12334A
What is the earliest time ( UTC ) , if any , that thunderstorms are forecast for TUNIS/CARTHAGE ?
a)
nil
b)
1800
c)
0800
d)
1300
Answer ;
b)
1800
Ateş Murat Üstünbıçak , ATPL
258
Flight Planning & Monitoring
----------------------------------------------------------------------------------------------------------------------------------------------------------------558.
( For this question use TRM (VFR) , Aberdeen (Dyce) Area chart (10-1V) )
What is the elevation of the highest ground within the boundary of Aberdeen Control Zone ?
a)
2025 ft
b)
2105 ft
c)
1245 ft
d)
1733 ft
Answer ;
d)
1733 ft
----------------------------------------------------------------------------------------------------------------------------------------------------------------559.
( For this question use TRM (VFR) , Aberdeen (Dyce) Area chart (10-1V) )
What is the elevation of the highest obstacle within the boundary of Aberdeen Control Area ?
a)
2025 ft
b)
2105 ft
c)
1245 ft
d)
1733 ft
Answer ;
b)
2105 ft
----------------------------------------------------------------------------------------------------------------------------------------------------------------560.
( For this question use TRM , Athinai (Hellinikon) Approach chart (29-1) )
What is the frequency and ident of the DVOR/DME shown at the northern end of Hellinikon airfield ?
a)
294 HN
b)
357 KVR
c)
114.40 ATH
d)
275 HK
Answer ;
c)
114.40 ATH
----------------------------------------------------------------------------------------------------------------------------------------------------------------561.
( For this question use TRM , VFR directory for Greece (7-3) )
What is the local time ( LT ) in Greece in (i) Winter and (ii) Summer ?
a)
(i) LT + 2 Hours = UTC , (ii) LT + 3 Hours = UTC
b)
(i) LT – 3 Hours = UTC , (ii) LT – 2 Hours = UTC
c)
(i) LT = UTC – 2 Hours , (ii) LT = UTC – 3 Hours
d)
(i) LT = UTC + 2 Hours , (ii) LT = UTC + 3 Hours
Answer ;
d)
(i) LT = UTC + 2 Hours , (ii) LT = UTC + 3 Hours
----------------------------------------------------------------------------------------------------------------------------------------------------------------562.
( For this question use TRM , VFR directory for Netherlands (7-3) )
What is the local time ( LT ) in the Netherlands in (i) Winter and (ii) Summer ?
a)
(i) LT = UTC – 1 Hour , (ii) LT = UTC – 2 Hours
b)
(i) LT = UTC + 2 Hours , (ii) LT = UTC + 1 Hour
c)
(i) LT – 1 Hour = UTC , (ii) LT – 2 Hours = UTC
d)
(i) LT – 2 Hours = UTC , (ii) LT – 1 Hour = UTC
Answer ;
c)
(i) LT – 1 Hour = UTC , (ii) LT – 2 Hours = UTC
----------------------------------------------------------------------------------------------------------------------------------------------------------------563.
( For this question use Route Manual chart E(LO)1 )
What is the Maximum Authorised Altitude ( MAA ) on airway W911D from DEAN CROSS 115.2 DCS ( 54°43'N
003°20'W° ) to NEWCASTLE 114.25 NEW ( 55°02'N 001°41'W ) ?
a)
FL50
b)
FL150
c)
4200 ft
d)
4700 ft
Answer ;
b)
FL150
----------------------------------------------------------------------------------------------------------------------------------------------------------------564.
( For this question use TRM , Athinai (Hellinikon) Area chart (29-1) )
What is the maximum permitted altitude if routeing inbound from “Abeam Patroklos” to Hellinikon ?
a)
1.500 ft
b)
300 ft
c)
322 ft
d)
4.000 ft
Answer ;
b)
300 ft
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
259
Flight Planning & Monitoring
565.
( For this question use annex 033-11190A )
Annex 033-11190A
What is the mean temperature deviation ( °C ) from the ISA over 50°N 010°W ?
a)
-2
b)
+9
c)
+2
d)
+13
Answer ;
a)
-2
----------------------------------------------------------------------------------------------------------------------------------------------------------------566.
( For this question use Route Manual chart E(HI)2 )
What is the meaning of the chart information for the beacon(s) at position 55º59'N 014º06'E ?
a)
Doppler VOR , ident SUP and NDB , ident OE
b)
NDB , ident OE and VOR , ident VEY
c)
NDB only , ident OE
d)
VOR only , ident VEY
Answer ;
c)
NDB only , ident OE
----------------------------------------------------------------------------------------------------------------------------------------------------------------567.
( For this question use Route Manual chart E(HI)2 )
What is the meaning of the chart information for the navaid(s) LANDVETTER (57º39'N 012º17'E ) ?
a)
Doppler VOR only with identification LAV available on frequency 114.6 MHz.
b)
VORDME and NDB with identification LAV available on frequency 114.6 MHz.
c)
DME only with identification LAV available on frequency 114.6 MHz.
d)
VORDME with identification LAV available on frequency 114.6 MHz.
Answer ;
d)
VORDME with identification LAV available on frequency 114.6 MHz.
Ateş Murat Üstünbıçak , ATPL
260
Flight Planning & Monitoring
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
568.
( For this question use 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 ?
a)
3.500 ft
b)
1.500 ft
c)
3.000 ft
d)
32.800 ft
Answer ;
b)
1.500 ft
----------------------------------------------------------------------------------------------------------------------------------------------------------------569.
( For this question use Route Manual chart E(LO)1 )
What is the Minimum Enroute Altitude ( MEA ) on airway W911D from DEAN CROSS 115.2 DCS ( 54°43'N 003°20'W° )
to NEWCASTLE 114.25 NEW ( 55°02'N 001°41'W ) ?
a)
FL150
b)
4700 ft
c)
FL50
d)
4200 ft
Answer ;
c)
FL50
----------------------------------------------------------------------------------------------------------------------------------------------------------------570.
( For this question use TRM (VFR) , Aberdeen (Dyce) Information Page (19-6) )
What is the minimum flight visibility required when landing at Aberdeen ( Dyce ) Airport other than when using Route H6 ?
a)
4 Km
b)
3 Km
c)
2 Km
d)
5 Km
Answer ;
c)
2 Km
----------------------------------------------------------------------------------------------------------------------------------------------------------------571.
( For this question use TRM , Athinai (Hellinikon) Landing Chart (29-2) )
What is the position of the Aerodrome Reference Point ?
a)
37°53.2'N 23°43.3'E
b)
37°53.8'N 23°43.7'E
c)
37°54.8'N 23°44.7'E
d)
37°54.2'N 23°44.3'E
Answer ;
b)
37°53.8'N 23°43.7'E
----------------------------------------------------------------------------------------------------------------------------------------------------------------572.
( For this question use TRM , Esbjerg Aerodrome chart (19-2) )
What is the position of the Aerodrome Reference Point at Esbjerg ?
a)
55°32.4'N 008°34.9'W
b)
55°32.4'N 008°34.9'E
c)
55°31.6'N 008°33.1'W
d)
55°31.6'N 008°33.1'E
Answer ;
d)
55°31.6'N 008°33.1'E
----------------------------------------------------------------------------------------------------------------------------------------------------------------573.
( For this question use or TRM , Sabadell Area chart (19-1) )
What is the published frequency for Barcelona ATIS ?
a)
118.65
b)
124.70
c)
116.10
d)
119.10
Answer ;
a)
118.65
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
261
Flight Planning & Monitoring
574.
( For this question use annex 033-12314A )
Annex 033-12314A
What is the temperature deviation ( °C ) from ISA over 50° N 010°E ?
a)
-10
b)
+2
c)
-55
d)
+10
Answer ;
a)
-10
----------------------------------------------------------------------------------------------------------------------------------------------------------------575.
( For this question use TRM , Athinai (Hellinikon) Approach chart (29-1) )
What is the total distance when following the VFR routeing from “Abeam Patroklos” to Hellinikon ?
a)
14 NM
b)
16 NM
c)
19 NM
d)
19 km
Answer ;
c)
19 NM
----------------------------------------------------------------------------------------------------------------------------------------------------------------576.
( For this question use TRM , Esbjerg Area chart (19-1) )
What is the track and distance shown on the chart from VOR/DME SKR to overhead Esbjerg ?
a)
308º (M) / 29 NM
b)
308º (M) / 29 Km
c)
308º (T) / 29 NM
d)
308º (T) / 29 Km
Answer ;
a)
308º (M) / 29 NM
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
262
Flight Planning & Monitoring
577.
( For this question use TRM , Athinai (Hellinikon) Approach chart (29-1) )
Athinai ( Hellinikon ) Approach chart ( 29-1 )
What is the variation shown on the chart ?
a)
5ºE
b)
3ºE
c)
3ºW
d)
5ºW
Answer ;
b)
3ºE
Ateş Murat Üstünbıçak , ATPL
263
Flight Planning & Monitoring
----------------------------------------------------------------------------------------------------------------------------------------------------------------578.
( For this question use annex 033-11195A )
Annex 033-11195A
What lowest cloud conditions ( oktas/ft ) are forecast for 1900 UTC at HAMBURG ( EDDH ) ?
a)
3 to 4 at 500
b)
5 to 7 at 1200
c)
5 to 7 at 500
d)
5 to 7 at 2000
Answer ;
c)
5 to 7 at 500
----------------------------------------------------------------------------------------------------------------------------------------------------------------579.
( For this question use annex 033-12329A )
Annex 033-12329A
What lowest cloud conditions ( oktas/ft ) are forecast for JOHANNESBURG/JAN SMUTS at 0300 UTC ?
a)
3 to 4 at 800
b)
3 to 4 at 400
c)
5 to 7 at 800
d)
5 to 7 at 400
Answer ;
d)
5 to 7 at 400
----------------------------------------------------------------------------------------------------------------------------------------------------------------580.
( For this question use annex 033-12336A )
Annex 033-12336A
What maximum surface windspeed ( kt ) is forecast for BORDEAUX/MERIGNAC at 1600 UTC ?
a)
30
b)
5
c)
25
d)
10
Answer ;
a)
30
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
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Flight Planning & Monitoring
581.
( For this question use annex 033-12314A )
Annex 033-12314A
What mean temperature ( °C ) is likely on a true course of 270° from 025° E to 010°E at 45°N ?
a)
-50
b)
-54
c)
-52
d)
-48
Answer ;
a)
-50
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
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Flight Planning & Monitoring
582.
( For this question use annex 033-11190A )
Annex 033-11190A
What mean temperature ( °C ) is likely on a course of 360° ( T ) from 40°N to 50°N at 040°E ?
a)
-47
b)
-46
c)
-49
d)
-50
Answer ;
a)
-47
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
266
Flight Planning & Monitoring
583.
( For this question use Route Manual VFR+GPS chart ED-6 )
Route Manual VFR+GPS chart ED-6
What minimum grid area altitude is applicable for EDPJ LAICHINGEN airport ( 48°30'N , 009°38'E ) ?
a)
43
b)
46
c)
402 m
d)
2434 ft
Answer ;
a)
43
----------------------------------------------------------------------------------------------------------------------------------------------------------------584.
( For this question use Route Manual VFR+GPS chart ED-6 )
Route Manual VFR+GPS chart ED-6
What minimum grid area altitude is applicable for EDTM MENGEN airport ( 48°03'N , 009°22'E ) ?
a)
46
b)
1120 m
c)
43
d)
1819 ft
Answer ;
a)
46
Ateş Murat Üstünbıçak , ATPL
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Flight Planning & Monitoring
----------------------------------------------------------------------------------------------------------------------------------------------------------------585.
( For this question use annex 033-12332A )
Annex 033-12332A
What minimum visibility is forecast for PARIS/CHARLES-DE-GAULLE at 2100 UTC ?
a)
8000 m
b)
6000 m
c)
10 km
d)
2000 m
Answer ;
b)
6000 m
----------------------------------------------------------------------------------------------------------------------------------------------------------------586.
( For this question use annex 033-11196A )
Annex 033-11196A
What minimum visibility ( m ) is forecast for 0600 UTC at LONDON LHR ( EGLL ) ?
a)
1500
b)
10000
c)
5000
d)
2200
Answer ;
a)
1500
----------------------------------------------------------------------------------------------------------------------------------------------------------------587.
( Use Route Manual chart E(HI)1 )
What navigation aid(s) is/are available to civil aircraft at the military airfield of Kinloss ( 57º40'N 003º32'W ) ?
a)
The bearing element only of TACAN on VOR frequency 109.8 MHz.
b)
The range element only of TACAN on DME frequency 109.8 MHz.
c)
VOR and DME on frequency 109.8.
d)
TACAN range and bearing on Channel 35.
Answer ;
b)
The range element only of TACAN on DME frequency 109.8 MHz.
----------------------------------------------------------------------------------------------------------------------------------------------------------------588.
When a pilot fills in an ATC flight plan , he must indicate the wake turbulence category. This category is a function of which
mass ?
a)
Maximum certified landing mass
b)
Actual take-off mass
c)
Estimated take-off mass
d)
Maximum certified take-off mass
Answer ;
d)
Maximum certified take-off mass
----------------------------------------------------------------------------------------------------------------------------------------------------------------589.
When an ATC 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 ;
a)
90 minutes or more.
b)
30 minutes or more.
c)
60 minutes or more.
d)
45 minutes or more.
Answer ;
b)
30 minutes or more.
Ateş Murat Üstünbıçak , ATPL
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Flight Planning & Monitoring
----------------------------------------------------------------------------------------------------------------------------------------------------------------590.
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 ;
a)
15 minutes flying time or 100 km.
b)
1 hour flying time or 500 km.
c)
30 minutes flying time or 370 km.
d)
20 minutes flying time or 150 km.
Answer ;
c)
30 minutes flying time or 370 km.
----------------------------------------------------------------------------------------------------------------------------------------------------------------591.
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 ;
a)
1 , 2 , 3 , 4.
b)
1 , 2 , 3.
c)
1 , 3.
d)
2 , 4.
Answer ;
a)
1 , 2 , 3 , 4.
----------------------------------------------------------------------------------------------------------------------------------------------------------------592.
When completing an ATC flight plan , an elapsed time ( Item 16 ) of 1 hour 55 minutes should be entered as ;
a)
0115
b)
1H55
c)
115M
d)
0155
Answer ;
d)
0155
----------------------------------------------------------------------------------------------------------------------------------------------------------------593.
When completing an ATC flight plan for a European destination , clock times are to be expressed in ;
a)
Local mean time
b)
Local standard time
c)
Central European Time
d)
UTC
Answer ;
d)
UTC
----------------------------------------------------------------------------------------------------------------------------------------------------------------594.
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 ;
a)
X
b)
G
c)
N/S
d)
Y
Answer ;
d)
Y
----------------------------------------------------------------------------------------------------------------------------------------------------------------595.
When completing Item 9 of the ATC flight plan , if there is no appropriate aircraft designator , the following should be
entered ;
a)
the most descriptive abbreviation
b)
“XXXX” followed by an entry in Item 18
c)
“NONE”
d)
“ZZZZ” followed by an entry in Item 18
Answer ;
d)
“ZZZZ” followed by an entry in Item 18
----------------------------------------------------------------------------------------------------------------------------------------------------------------596.
When filling in an ATC flight plan before departure , the time information which should be entered in item 13 : “Time” is ;
a)
planned take-off time.
b)
the time of flight plan filing.
c)
planned engine start time.
d)
estimated off-block time.
Answer ;
d)
estimated off-block time.
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
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Flight Planning & Monitoring
597.
When using decision point procedure , you reduce the ;
a)
reserve fuel from 10% down to 5%.
b)
holding fuel by 30%.
c)
contingency fuel by adding contingency only from the burnoff between decision point and destination.
d)
contingency fuel by adding contingency only from the burnoff between the decision airport and destination.
Answer ;
c)
contingency fuel by adding contingency only from the burnoff between decision point and destination.
----------------------------------------------------------------------------------------------------------------------------------------------------------------598.
( For this question use annex 033-11181A )
Annex 033-11181A
Which best describes the maximum intensity of CAT , if any , forecast for FL330 over BENGHAZI ( 32°N 020°E ) ?
a)
Light
b)
Nil
c)
Severe
d)
Moderate
Answer ;
b)
Nil
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
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Flight Planning & Monitoring
599.
( For this question use annex 033-11181A )
Annex 033-11181A
Which best describes the maximum intensity of icing , if any , at FL150 in the vicinity of BUCHAREST ( 45°N 026°E ) ?
a)
Severe
b)
Nil
c)
Moderate
d)
Light
Answer ;
c)
Moderate
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
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Flight Planning & Monitoring
600.
( For this question use annex.033-12320A )
Annex 033-12320A
Which best describes the maximum intensity of icing , if any , at FL160 in the vicinity of BERLIN ( 53° N 013°E ) ?
a)
severe
b)
nil
c)
moderate
d)
light
Answer ;
c)
moderate
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
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Flight Planning & Monitoring
601.
( For this question use annex 033-12320A )
Annex 033-12320A
Which best describes the significant cloud forecast for the area east of Tunis ( 36°N 010°E ) ?
a)
5 to 7 oktas CU and AC base FL100 tops FL180
b)
3 to 4 oktas CU and AC base FL100 tops FL160
c)
3 to 4 oktas CU and AC base below FL100 tops FL180
d)
5 to 7 oktas CU and AC base below FL100 tops FL180
Answer ;
d)
5 to 7 oktas CU and AC base below FL100 tops FL180
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
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Flight Planning & Monitoring
602.
( For this question use annex 033-12320A )
Annex 033-12320A
Which best describes the significant cloud forecast over TOULOUSE ( 44°N001°E ) ?
a)
broken AC/CU base below FL100 tops FL150 , embedded isolated CB base below FL100 tops FL270
b)
5 to 7 oktas CU and AC base below FL100 tops to FL270
c)
isolated CB embedded in layer cloud , surface to FL270
d)
well separated CB base FL100 tops to FL 270
Answer ;
a)
broken AC/CU base below FL100 tops FL150 , embedded isolated CB base below FL100 tops FL270
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
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Flight Planning & Monitoring
603.
( For this question use annex 033-11181A )
Annex 033-11181A
Which best describes the significant cloud , if any , forecast for the area southwest of BODO ( 67°N 014°E ) ;
a)
5 to 7 oktas CU and CB base below FL100 , tops FL180
b)
Nil
c)
3 to 7 oktas CU and CB base below FL100 , tops FL180
d)
5 to 7 oktas CU and CB base FL100 , tops FL180
Answer ;
a)
5 to 7 oktas CU and CB base below FL100 , tops FL180
----------------------------------------------------------------------------------------------------------------------------------------------------------------604.
( For this question use annex 033-12333A )
Annex 033-12333A
Which best describes the weather , if any , at LYON/SATOLAS at 1330 UTC ?
a)
frequent rain showers
b)
nil
c)
fog
d)
light rain associated with thunderstorms
Answer ;
d)
light rain associated with thunderstorms
Ateş Murat Üstünbıçak , ATPL
275
Flight Planning & Monitoring
----------------------------------------------------------------------------------------------------------------------------------------------------------------605.
( For this question use annex 033-12329A )
Annex 033-12329A
Which best describes the weather , if any , forecast for JOHANNESBURG/JAN SMUTS at 0400 UTC ?
a)
CAVOK
b)
rain associated with thunderstorms
c)
patches of fog
d)
mist and/or fog
Answer ;
c)
patches of fog
--------------------------------------------------------------------------------------------------------------------------------------------------------------606.
( For this question use annex 033-12320A )
Annex 033-12320A
Which describes the intensity of icing , if any , at FL 150 in the vicinity of TOULOUSE ( 44° N 01°E ) ?
a)
moderate
b)
moderate or severe
c)
light
d)
nil
Answer ;
b)
moderate or severe
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
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Flight Planning & Monitoring
607.
( For this question use annex 033-11181A )
Annex 033-11181A
Which describes the maximum intensity of icing , if any , at FL180 in the vicinity of CASABLANCA ( 33°N 008°W ) ?
a)
Moderate
b)
Nil
c)
Light
d)
Severe
Answer ;
d)
Severe
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
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Flight Planning & Monitoring
608.
( For this question use annex 033-12326A )
Annex 033-12320A
Which describes the maximum intensity of turbulence , if any , forecast for FL260 over TOULOUSE ( 44°N 001°E ) ?
a)
moderate
b)
severe
c)
light
d)
nil
Answer ;
b)
severe
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
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609.
( For this question use annex 033-11181A )
Annex 033-11181A
Which describes the worst hazard , if any , that could be associated with the type of feature at 38°N 015°E ?
a)
Severe attenuation in the HF R/T band
b)
Reduced visibility
c)
Engine flame out and windscreen damage
d)
There is no hazard
Answer ;
c)
Engine flame out and windscreen damage
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
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Flight Planning & Monitoring
610.
( For this question use annex 033- 11046A or Route Manual SID charts for ZURICH (10-3) )
Annex 033-11046A
Which is the correct ALBIX departure via AARAU for runway 16 ?
a)
ALBIX 6E
b)
ALBIX 6H
c)
ALBIX 7A
d)
ALBIX 7S
Answer ;
d)
ALBIX 7S
----------------------------------------------------------------------------------------------------------------------------------------------------------------611.
( For this question use annex 033- 11041A or Route Manual SID chart for MUNICH(10-3C ,10-3D) )
Which is the correct departure via KEMPTEN from runway 26L ?
a)
KEMPTEN THREE QUEBEC
b)
KEMPTEN THREE NOVEMBER
c)
KEMPTEN THREE ECHO
d)
KEMPTEN FIVE SIERRA
Answer ;
d)
KEMPTEN FIVE SIERRA
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
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Flight Planning & Monitoring
612.
( For this question use annex 033-12335A )
Annex 033-12335A
Which is the heaviest type of precipitation , if any , forecast for BORDEAUX/MERIGNAC at 1000 UTC ?
a)
heavy rain associated with thunderstorms
b)
nil
c)
light rain
d)
rain showers
Answer ;
c)
light rain
----------------------------------------------------------------------------------------------------------------------------------------------------------------613.
( For this question use annex 033-9729A , AERONAUTICAL CHART ICAO 1:500 000 STUTTGART (NO 47/6) or Route
Manual VFR+GPS chart ED-6 )
Route Manual VFR+GPS chart ED-6
Which navigation aid is located in position 48°23'N , 008°39'E ?
a)
VORTAC
b)
NDB
c)
VOR
d)
VOR/DME
Answer ;
c)
VOR
Ateş Murat Üstünbıçak , ATPL
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Flight Planning & Monitoring
----------------------------------------------------------------------------------------------------------------------------------------------------------------614.
( For this question use annex 033-9729A , 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 ?
a)
VOR
b)
VOR/DME
c)
TACAN
d)
NDB
Answer ;
b)
VOR/DME
----------------------------------------------------------------------------------------------------------------------------------------------------------------615.
( 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 )
Route Manual VFR+GPS chart ED-6
Which navigation aid is located in position 48°55'N , 009°20'E ?
a)
VOR/DME
b)
NDB
c)
TACAN
d)
VOR
Answer ;
a)
VOR/DME
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
Ateş Murat Üstünbıçak , ATPL
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616.
( For this question use annex 033-11202A )
Annex 033-11181A
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 ) ?
a)
None
b)
FL290
c)
FL 210
d)
FL250
Answer ;
d)
FL250
----------------------------------------------------------------------------------------------------------------------------------------------------------------617.
( For this question use TRM (VFR) , Aberdeen (Dyce) Area chart (10-1V) )
Which of the following frequencies is listed as available for contact with Aberdeen ATSU ?
a)
126.25
b)
119.87
c)
114.30
d)
135.17
Answer ;
d)
135.17
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
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Flight Planning & Monitoring
618.
( For this question use annex 033- 11044A or Route Manual SID chart for LONDON HEATHROW (10-3) )
Annex 033-11044A
Which of the following is a correct Minimum Safe Altitude ( MSA ) for the Airport ?
a)
East sector 2100 ft within 50 NM
b)
East sector 2300 ft within 50 NM
c)
West sector 2300 ft within 25 NM
d)
West sector 2100 ft within 25 NM
Answer ;
d)
West sector 2100 ft within 25 NM
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
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619.
( For this question use annex 033- 11048A or Route Manual SID chart for AMSTERDAM SCHIPHOL (10-3) )
Annex 033-11048A
Which of the following statements is correct for ANDIK departures from runway 19L ?
a)
The distance to ANDIK is 25 NM
b)
Cross ANDIK below FL60
c)
Contact SCHIPOL DEPARTURE 119.05 passing 2000 ft and report altitude
d)
Maximum IAS 250kt turning left at SPL 3.1 DME
Answer ;
c)
Contact SCHIPOL DEPARTURE 119.05 passing 2000 ft and report altitude
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-----------------------------------------------------------------------------------------------------------------------------------------------------------------
620.
Which of the following statements is relevant for forming route portions in integrated range flight planning ?
a)
Each reporting point requires a new segment.
b)
A small change of temperature ( 2°C ) can divide a segment.
c)
The distance from take-off up to the top of climb has to be known.
d)
No segment shall be more than 30 minutes of flight time.
Answer ;
c)
The distance from take-off up to the top of climb has to be known.
----------------------------------------------------------------------------------------------------------------------------------------------------------------621.
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.
a)
Both statements
b)
Statement 1 only
c)
Statement 2 only
d)
Neither statement
Answer ;
c)
Statement 2 only
----------------------------------------------------------------------------------------------------------------------------------------------------------------622.
Which of the following statements is(are) correct with regard to the advantages of computer flight plans ?
1.
The computer can file the ATC flight plan.
2.
Wind data used by the computer is always more up-to-date than that available to the pilot.
a)
Neither statement
b)
Statement 1 only
c)
Both statements
d)
Statement 2 only
Answer ;
b)
Statement 1 only
----------------------------------------------------------------------------------------------------------------------------------------------------------------623.
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 in-flight re-routing the computer produces a new plan.
a)
Both statements
b)
Statement 2 only
c)
Statement 1 only
d)
Neither statement
Answer ;
c)
Statement 1 only
----------------------------------------------------------------------------------------------------------------------------------------------------------------624.
Which of the following statements regarding filing a ATC flight plan is correct ?
a)
A flight plan should be filed when a national FIR boundary will be crossed.
b)
A flying college can file repetitive flight plan for VFR flights.
c)
In case of ATFM ( Air Traffic Flow Management ) the flight plan should be filed at least three hours in
advance of the EOBT.
d)
Any flight plan should be filed at least 10 minutes before departure.
Answer ;
c)
In case of ATFM ( Air Traffic Flow Management ) the flight plan should be filed at least three hours in
advance of the EOBT.
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
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625.
( For this question use annex 033-12343A or Flight Planning Manual MRJT 1 Figure 4.3.1C )
Annex 033-12343A
Within the limits of the data given , a mean temperature increase of 30°C will affect the trip time by approximately ;
a)
+5%
b)
-5%
c)
-7%
d)
+8%
Answer ;
b)
-5%
----------------------------------------------------------------------------------------------------------------------------------------------------------------626.
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 ?
a)
262°
b)
224°
c)
242°
d)
280°
Answer ;
d)
280°
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
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Flight Planning & Monitoring
627.
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
a)
800 kg
b)
500 kg
c)
1000 kg
d)
700 kg
Answer ;
a)
800 kg
----------------------------------------------------------------------------------------------------------------------------------------------------------------628.
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?
a)
The filed deviation is not accepted.
b)
You will get a separate clearance for the deviation.
c)
The route according to the flight plan is accepted.
d)
It is not allowed to file such a flight plan.
Answer ;
c)
The route according to the flight plan is accepted.
----------------------------------------------------------------------------------------------------------------------------------------------------------------629.
You must fly IFR on an airway orientated 135° magnetic with a MSA at 7800 ft. Knowing the QNH is 1025 hPa and the
temperature is ISA + 10°, the minimum flight level you must fly at is ;
a)
90
b)
75
c)
80
d)
70
Answer ;
a)
90
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
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