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Question Bank
Questions for INDIGO FLIGHT PLANNING (2108-2519)
Answer the following questions
Test Mode
Training Mode
1.
On a VFR flight plan, the total estimated time is
the estimated time from take-off to overhead the destination airport
the estimated time from take-off to landing at the alternate airport
the estimated time from take-off to overhead the destination airport, plus 15 minutes
the estimated time from engine start to landing at the destination airport
2.
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
3 h 43 min
2 h 59 min
2 h 51 min
3.
An aeroplane is flying from an airport to another.In cruise, the calibrated airspeed is I50 kt, true airspeed 180 kt, average groundspeed 210 kt, the speed box on the filed flight plan shall be filled as follows
N0180
K0210
K0180
K0150
4.
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 AGA chapter of the French Aeronautical Information Publication (AIP)
by telephoning the aerodrome's local chamber of commerce, this type of information not being published
in the FAL section of the French Aeronautical Information Publication (AIP)
in the GEN chapter of the French Aeronautical Information Publication (AIP)
5.
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
70
80
90
75
6.
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
4 300 kg.
6 185 kg.
9 000 kg
6 400 kg.
7.
A public transport aeroplane with reciprocating engines,is flying from PARlS to LYON. The final reserve corresponds to
45 minutes at holding speed
1 hour at holding speed
30 minutes at holding speed
2 hours at cruise consumption
8.
Given the following:D = flight distance X = distance to Point of Equal TimeGSo = groundspeed outGSr = groundspeed return The correct formula to find distance to Point of Equal Time is
X = (D/2) + GSr / (GSo + GSr)
X = D x GSr / (GSo + GSr)
X = D x GSo / (GSo + GSr)
X = (D/2) x GSo / (GSo + GSr)
9.
You are to determine the maximum fuel load which can be carried in the following conditions :- dry operating mass : 2800 kg- trip fuel : 300 kg- payload : 400 kgmaximum take-off mass : 4200 kg- maximum landing mass : 3700 kg
800 kg
1000 kg
700 kg
500 kg
10.
On an ATC flight plan, to indicate that you will overfly the way-point TANGO at 350 kts at flight level 280, you write
TANGO / FL280 N0350
TANGO / K0350 FL280
TANGO / N0350 F280
TANGO / KT350 F280
11.
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
17 300 kg
15 900 kg
16 300 kg
17 100 kg
12.
How many hours in advance of departure time should a flight plan be filed in the case of flights into areas subject to air traffic flow management (ATFM)?
1:00 hour
3:00 hours.
0:30 hours
0:10 hours.
13.
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 kgFind: Maximum additional load
5600 kg
7000 kg
3000 kg
4000 kg
14.
Given :Course A to B 088° (T)distance 1250 NMMean TAS 330 ktMean W/V 340°/60 ktThe time from A to the PET between A and B is
1 hour 54 minutes
1 hour 42 minutes
1 hour 39 minutes
2 hours 02 minutes
15.
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
224.5 NM
158.6 NM
16.
The fuel burn off is 200 kg/h with a relative fuel density of 0,8. If the relative density is 0,75, the fuel burn will be
213 kg/h
200 kg/h
267 kg/h
188 kg/h
17.
An operator (turbojet engine) shall ensure that calculation up of usable fuel for a flight for which no destination alternate is required includes, taxi fuel, trip fuel, contingency fuel and fuel to fly for
2 hours at normal cruise consumption
30 minutes at holding speed at 450 m above aerodrome elevation in standard conditions
45 minutes plus 15% of the flight time planned to be spent at cruising level or two hours whichever is less
30 minutes at holding speed at 450 m above MSL in standard conditions
18.
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?
193 NM
203 NM
188 NM
174 NM
19.
An airway is marked 3500T 2100 a. This indicates that
the minimum obstruction clearance altitude (MOCA) is 3500 ft
the minimum enroute altitude (MEA) is 3500 ft
the airway base is 3500 ft MSL
the airway is a low level link route 2100 ft - 3500 ft MSL
20.
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
Y
X
G
N/S
21.
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
22.
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?
12 minutes.
63 minutes.
4 minutes
44 minutes
23.
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
24.
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 = 0The flight level allowing the highest ground speed is
FL290
FL270
FL330
FL370
25.
In the ATS flight plan Item 15, a cruising speed of 470 knots will be entered as
0470K
N470
N0470
KN470
26.
When completing an ATS flight plan, an elapsed time (Item 16) of 1 hour 55 minutes should be entered as
1H55
155
115M
115
27.
Given: Maximum allowable take-off mass 64 400 kg, maximum landing mass 56200 kg, maximum zero fuel mass 53 000 kg, dry operating mass 35 500 kg, estimated load 14 500 kg, estimated trip fuel 4 900 kg, minimum take-off fuel 7 400 kg.Find: maximum additional load
5 600 kg
3 000 kg
4 000 kg
7 000 kg
28.
An aircraft, following a 215° true track, must fly over a 10 600 ft obstacle with a minimum obstacle clearance of 1 500 ft. Knowing the QNH received from an airport close by, which is almost at sea-level, is 1035 and the temperature is ISA -15°C, the minimum flight level will be
140
130
150
120
29.
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
1203 UTC
1213 UTC
1221 UTC
1233 UTC
30.
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
1125 NM
1491 NM
1143 NM
31.
Which of the following statements regarding filing a flight plan is correct?
Any flight plan should be filed at least 10 minutes before departure
In case of flow control the flight plan should be filed at least three hours in advance of the time of departure.
A flying college can file repetitive flight plan for VFR flights
A flight plan should be filed when a national FIR boundary will be crossed
32.
Unless otherwise shown on charts for standard instrument departure the routes are given with
true course
magnetic course
magnetic headings
true headings
33.
To carry out a VFR flight to an off-shore platform, the minimum fuel quantity on board is
at least equal to that defined for IFR flights
that defined for VFR flights over land increased by 5 %
that defined for VFR flights over land increased by 10 %
identical to that defined for VFR flights over land
34.
The maximum permissible take-off mass of an aircraft for the L wake turbulence category on a flight plan is
10 000 kg
7 000 kg
2 700 kg
5 700 kg
35.
A ""current flight plan"" is a
flight plan with the correct time of departure
filed flight plan with amendments and clearance included
filed flight plan
flight plan in the course of which radio communication should be practised between aeroplane and ATC
36.
In the ATS flight plan, for a non-scheduled flight which of the following letters schould be entered in Item 8 (Type of Flight)
G
N
X
N/S
37.
An airway is marked 5000 2900a. The notation 5000 is the
minimum holding altitude (MHA)
maximum authorised altitude (MAA)
minimum enroute altitude (MEA)
base of the airway (AGL)
38.
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 49min
2h 04min
2h 52min
1h 35min
39.
Given :Distance A to B 2050 NMMean groundspeed 'on' 440 ktMean groundspeed 'back' 540 ktThe distance to the point of equal time (PET) between A and B is
920 NM
1130 NM
1153 NM
1025 NM
40.
Given: True course (TC) 017°, W/V 340°/30 kt, True air speed (TAS) 420 ktFind: Wind correction angle (WCA) and ground speed (GS)
WCA -2°, GS 426 kt
WCA +2°, GS 396 kt
WCA -2°, GS 396 kt
WCA +2°, GS 416 kt
41.
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 ?
262°
224°
242°
280°
42.
For a repetitive flight plan (RPL) to be used, flights must take place on a regular basis on at least
20 occasions
50 occasions
10 occasions
30 occasions
43.
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 kgFind the maximum allowable take-off fuel
11 400 kg
8 600 kg
14 400 kg
11 100 kg
44.
The purpose of the decision point procedure is ?
To reduce the minimum required fuel and therefore be able to increase the traffic load
To increase the amount of extra fuel.
To increase the safety of the flight
To reduce the landing weight and thus reduce the structural stress on the aircraft
45.
An aircraft plans to depart London at 1000 UTC and arrive at Munich (EDDM) at 1215 UTC. In the ATS flight plan Item 16 (destination/EET) should be entered with
EDDM 0215
EDDM 2H15
EDDM 1215
EDDM 1415
46.
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?
25 kg trip fuel and 8 kg reserve fuel
33 kg trip fuel and 10 kg reserve fuel.
33 kg trip fuel and no reserve fuel.
23 kg trip fuel and 10 kg reserve fuel.
47.
For a flight to an off-shore platform, an alternate aerodrome is compulsory, except if :1 - flight duration does not exceed two hours2 - during the period from two hours before to two hours after the estimated landing time, the forecast conditions of ceiling and visibility are not less than one and a half times the applicable minima3 - the platform is available and no other flight either from or to the platform is expected between the estimated time of departure and one half hour after the estimated landing timeThe combination which regroups all of the correct statements is
2 - 3
02-Jan
1 - 3
2001-02-03
48.
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
3500 kg.
8120 kg.
7380 kg.
1845 kg
49.
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
79 200 kg
77 800 kg
76 100 kg
80 500 kg
50.
When completing an ATS flight plan for a European destination, clock times are to be expressed in
Central European Time
local standard time
Local mean time
UTC
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