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CPL Test Series
Question Bank
Questions for INDIGO FLIGHT PLANNING (2108-2519)
Answer the following questions
Test Mode
Training Mode
1.
When using decision point procedure, you reduce the
holding fuel by 30%.
contingency fuel by adding contingency only from the burnoff between the decision airport and destination
contingency fuel by adding contingency only from the burnoff between decision point and destination
reserve fuel from 10% down to 5%.
2.
Given:Dry operating mass (DOM)= 33510 kgLoad= 7600 kgTrip fuel (TF)= 2040 kgFinal reserve fuel= 983 kgAlternate fuel= 1100 kgContingency fuel= 5% of trip fuelWhich of the listed estimated masses is correct?
Estimated take-off mass= 43295 kg
Estimated landing mass at destination= 43295 kg
Estimated take-off mass= 45233 kg
Estimated landing mass at destination= 43193 kg
3.
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
140 NM
120 NM
110 NM
130 NM
4.
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
1221 UTC
1203 UTC
1233 UTC
1213 UTC
5.
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
Statement 1 only
Statement 2 only
Both statements
Neither statement
6.
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?
It is not allowed to file such a flight plan
The filed deviation is not accepted
The route according to the flight plan is accepted
You will get a separate clearance for the deviation
7.
Given :Distance X to Y 2700 NMMach Number 0.75Temperature -45°CMean wind component 'on' 10 kt tailwindMean wind compontent 'back' 35 kt tailwindThe distance from X to the point of equal time (PET) between X and Y is
1313 NM
1425 NM
1386 NM
1350 NM
8.
The purpose of the decision point procedure is ?
To reduce the landing weight and thus reduce the structural stress on the aircraft
To reduce the minimum required fuel and therefore be able to increase the traffic load
To increase the safety of the flight
To increase the amount of extra fuel.
9.
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
at least equivalent to 45 minutes flying time
laid down by the operator, with the quantity being specified in the operating manual
at least equivalent to 30 minutes flying time
at least equivalent to the quantity required to fly to another aerodrome in the event that weather conditions so require
10.
An aeroplane is on an IFR flight. The flight is to be changed from IFR to VFR. Is it possible?
Yes, the pilot in command must inform ATC using the phrase ""cancelling my IFR flight"".
No, only ATC can order you to do this.
Yes, but only with permission from ATC.
No, you have to remain IFR in accordance to the filed flight plan
11.
An aeroplane has the following masses:ESTLWT= 50 000 kgTrip fuel= 4 300 kgContingency fuel= 215 kgAlternate fuel (final reserve included)= 2 100kgTaxi= 500 kgBlock fuel= 7 115 kgBefore departure the captain orders to make the block fuel 9 000 kg.The trip fuel in the operational flight plan should read
9 000 kg
6 185 kg.
4 300 kg.
6 400 kg.
12.
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
188 kg/h
267 kg/h
213 kg/h
200 kg/h
13.
For the purposes of Item 9 (Wake turbulence category) of the ATS flight plan, an aircraft with a maximum certificated take-off mass of 62000 kg is
heavy ""H""
unclassified ""U""
medium ""M""
light ""L""
14.
Given:Dry operating mass (DOM)= 33500 kgLoad= 7600 kgMaximum allowable take-off mass= 66200 kgStandard taxi fuel= 200 kgTank capacity= 16 100 kgThe maximum possible take-off fuel is
17 100 kg
15 900 kg
17 300 kg
16 300 kg
15.
Given :Distance A to B 3060 NMMean groundspeed 'out' 440 ktMean groundspeed 'back' 540 ktSafe Endurance 10 hoursThe time to the Point of Safe Return (PSR) is
5 hours 45 minutes
5 hours 30 minutes
5 hours 20 minutes
3 hours 55 minutes
16.
In the ATS flight plan Item 15 (Cruising speed), when not expressed as a Mach number, cruising speed is expressed as
CAS
Groundspeed
TAS
IAS
17.
For a repetitive flight plan (RPL) to be used, flights must take place on a regular basis on at least
10 occasions
30 occasions
50 occasions
20 occasions
18.
In the ATS flight plan Item 13, in a flight plan submitted before departure, the departure time entered is the
estimated take-off time
estimated off-block time
estimated time over the first point en route
allocated slot time
19.
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 kgFind: Maximum allowable take-off fuel
14400 kg
11400 kg
8600 kg
11100 kg
20.
On a ATC flight plan, to indicate that you will overfly the way-point ROMEO at 120 kt at flight level 085, you will write
ROMEO / K0120 FL085
ROMEO / FL085 N0120
ROMEO / F085 N0120
ROMEO / N0120 F085
21.
33.1.1.4 (2110) An aeroplane flies at an airspeed of 380 kt. lt 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
2h 35min
2h 10min
2h 32min
3h 00min
22.
An executive pilot is to carry out a flight to a French aerodrome, spend the night there and return the next day. Where will he find the information concerning parking and landing fees ?
in the GEN chapter of the French Aeronautical Information Publication (AIP)
in the AGA chapter of the French Aeronautical Information Publication (AIP)
in the FAL section of the French Aeronautical Information Publication (AIP)
by telephoning the aerodrome's local chamber of commerce, this type of information not being published
23.
A repetitive flight plan (RPL) is filed for a scheduled flight: Paris-Orly to Angouleme, Paris Orly as alternate. Following heavy snow falls, Angouleme airport will be closed at the expected time of arrival. The airline decides before departure to plan a re-routing of thatflight to Limoges
The RPL must be cancelled for that day and a specific flight plan has to be filed
It is not possible to plan another destination and the fIight has to be simply cancelled that day (scheduled flight and not chartered).
The pilot-in-command must advise ATC of his intention to divert to Limoges at least 15 minutes before the planned time of arrival
The airline's ""Operations "" Department has to tansmit a change in the RPL at the ATC office, at least half an hour before the planned time of departure.
24.
In the appropriate box of a flight plan, for endurance, one must indicate the time corresponding to
the required fuel for the flight
the total usable fuel on board minus reserve fuel
the required fuel for the flight plus the alternate and 45 minutes
the total usable fuel on board
25.
The cruising speed to write in the appropriate box of a flight plan is
calibrated air speed
true air speed
ground speed
indicated air speed
26.
In the ATS flight plan Item 15, a cruising speed of 470 knots will be entered as
N0470
N470
KN470
0470K
27.
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, additionnal fuel of
7380 kg.
8120 kg.
1845 kg
3500 kg.
28.
When completing an ATS flight plan for a flight commencing under IFR but possibly changing to VFR, the letters entered in Item 8 (FLIGHT RULES) would be
X
G
Y
N/S
29.
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 6 000 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?
13000 kg
13220 kg.
13370 kg
14500 kg
30.
An airway is marked 3500T 2100 a. This indicates that
the minimum enroute altitude (MEA) is 3500 ft
the airway base is 3500 ft MSL
the minimum obstruction clearance altitude (MOCA) is 3500 ft
the airway is a low level link route 2100 ft - 3500 ft MSL
31.
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
30
45
15
10
32.
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
1463 NM
1491 NM
1125 NM
1143 NM
33.
During an IFR flight in a Beech Bonanza the fuel indicators show that the remaining amount of fuel is 100 lbs after 38 minutes. The total amount of fuel at departure was 160 lbs. For the alternate fuel, 30 lbs is necessary. The planned fuel for taxi is 13 lbs. Final reserve fuel is estimated at 50 lbs. If the fuel flow remains the same, how many minutes can be flown to the destination with the remaining fuel?
4 minutes
12 minutes.
44 minutes
63 minutes.
34.
Find the time to the Point of Safe Return (PSR). Given: Maximum useable fuel 15000 kg, Minimum reserve fuel 3500 kg, TAS out 425 kt, Head wind component out 30 kt, TAS return 430 kt, Tailwind component return 20 kt, Average fuel flow 2150 kg/h
2 h 43 min
2 h 51 min
3 h 43 min
2 h 59 min
35.
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
30 minutes holding 1,500 feeI above aerodrome A
30 minutes holding 2,000 feet above aerodrome B
30 minutes holding 1,500 feet above aerodrome B
15 minutes holding 2,000 feet above aerodrome A
36.
You must fly IFR on an airway orientated 135° magnetic with a MSA at 7 800 ft. Knowing the QNH is 1 025 hPa and the temperature is ISA + 10°, the minimum flight level you must fly at is
80
75
70
90
37.
For a planned flight the calculated fuel is as follows:Flight time: 3h06minThe reserve fuel, at any time, should not be less than 30% of the remaining trip fuel.Taxi fuel: 8 kgBlock fuel: 118 kgHow much fuel should remain after 2 hours flight time?
27 kg trip fuel and 12 kg reserve fuel.
30 kg trip fuel and 9 kg reserve fuel
39 kg trip fuel and 12 kg reserve fuel
39 kg trip fuel and no reserve fuel
38.
In an ATS flight plan Item 15, in order to define a position as a bearing and distance from a VOR, the group of figures should consist of
VOR ident, magnetic bearing and distance in nautical miles
VOR ident, magnetic bearing and distance in kilometres
VOR ident, true bearing and distance in kilometres
full name of VOR, true bearing and distance in kilometres
39.
A helicopter is on a 150 NM leg to an off-shore oil rig. Its TAS is 130 kt with a 20 kt tailwind, its endurance is 3h30min without reserve. Upon reaching destination, it is asked to proceed outbound to locate a ship in distress, on a track which gives a 15 kt tailwind. Maintaining zero reserve on return to the oil rig, the helicopter can fly outbound for distance of
222.1 NM
160.3 NM
158.6 NM
224.5 NM
40.
In an ATS flight plan, Item 15 (route), a cruising pressure altitude of 32000 feet would be entered as
S3200
FL320
F320
32000
41.
The navigation plan reads:Trip fuel: 100 kgFlight time: 1h35minTaxi fuel: 3 kgBlock fuel: 181 kgThe endurance on the ICAO flight plan should read
2h 52min
1h 35min
2h 04min
2h 49min
42.
Which of the following statements is (are) correct with regard to the operation of flight planning computers ?1. The computer can file the ATC flight plan.2. In the event of inflight re-routing the computer produces a new plan
Statement 1 only
Neither statement
Both statements
Statement 2 only
43.
For a flight plan filed before the flight, the indicated time of departure is
the time at which the flight plan is filed
the time overhead the first reporting point after take-off.
the time of take-off
the estimated off-block time
44.
For a planned flight the calculated fuel is as follows:Flight time: 2h42minThe reserve fuel, at any time, should not be less than 30% of the remaining trip fuel.Taxi fuel: 9 kgBlock fuel: 136 kgHow much fuel should remain after 2 hours flight time?
33 kg trip fuel and 10 kg reserve fuel.
33 kg trip fuel and no reserve fuel.
25 kg trip fuel and 8 kg reserve fuel
23 kg trip fuel and 10 kg reserve fuel.
45.
For flight planning purposes the landing mass at alternate is taken as
Zero Fuel Mass plus Final Reserve Fuel and Alternate Fuel
Landing Mass at destination plus Alternate Fuel
Zero Fuel Mass plus Final Reserve Fuel.
Zero Fuel Mass plus Final Reserve Fuel and Contingency Fuel
46.
The required time for final reserve fuel for turbojet aeroplane is
30 min.
60 min
Variable with wind velocity
45 min.
47.
An appropriate flight level for IFR flight in accordance with semi-circular height rules on a course of 180° (M) is
FL95
FL105
FL100
FL90
48.
For turbojet engine driven aeroplane, given:Taxi fuel 600 kgFuel flow for cruise 10 000 kg/hFuel flow for holding 8 000 kg/hAlternate fuel 10 200 kgPlanned flight time to destination 6 hForecast visibility at destination 2000 mThe minimum ramp fuel required is
80 500 kg
79 200 kg
76 100 kg
77 800 kg
49.
A public transport aeroplane with reciprocating engines,is flying from PARlS to LYON. The final reserve corresponds to
2 hours at cruise consumption
30 minutes at holding speed
45 minutes at holding speed
1 hour at holding speed
50.
In the ATS flight plan item 15, it is necessary to enter any point at which a change of cruising speed takes place. For this purpose a ""change of speed"" is defined as
10 % TAS or 0.05 Mach or more
5% TAS or 0.01 Mach or more
20 knots or 0.05 Mach or more
20 km per hour or 0.1 Mach or more
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