Vayudoot Aviation

1.
From which of the following would you expect to find information regarding known short unserviceability of VOR, TACAN, and NDB ?

AIP (Air Information Publication)

NOTAM

ATCC broadcasts

SIGMET

2.
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 10 %

that defined for VFR flights over land increased by 5 %

identical to that defined for VFR flights over land

3.
Given:Dry operating mass (DOM)= 33000 kgLoad= 8110 kgFinal reserve fuel= 983 kgAlternate fuel= 1100 kgContingency fuel 102 kgThe estimated landing mass at alternate should be

42312 kg

42210 kg

41110 kg

42195 kg

4.
On an ATC flight plan, an aircraft indicated as ""H"" for ""Heavy""

has a certified take-off mass greater than or equal to 140 000 kg

is of the highest wake turbulence category

requires a runway length of at least 2 000m at maximum certified take-off mass

has a certified landing mass greater than or equal to 136 000 kg

5.
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°

242°

280°

224°

6.
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

16 300 kg

17 300 kg

15 900 kg

7.
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

4000 kg

3000 kg

7000 kg

8.
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

16 min

24 min

10 min 40 sec

20 min

9.
The planned departure time from the parking area is 1815 UTCThe estimated takeoff time is 1825 UTCThe IFR flight plan must be filed with ATC at the latest at

1745 UTC

1725 UTC

1715 UTC

1755 UTC

10.
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""

medium ""M""

light ""L""

unclassified ""U""

11.
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 / K0350 FL280

TANGO / FL280 N0350

TANGO / N0350 F280

TANGO / KT350 F280

12.
A ""current flight plan"" is a

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

flight plan with the correct time of departure

13.
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 landing mass at destination= 43295 kg

Estimated landing mass at destination= 43193 kg

Estimated take-off mass= 45233 kg

Estimated take-off mass= 43295 kg

14.
If your destination airport has no ICAO indicator, in the appropriate box of your flight plan, you write

AAAA

////

XXXX

ZZZZ

15.
A descent is planned from 7500 ft MSL so as to arrive at 1000 ft MSL 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

15,0 NM

27,1 NM

11,7 NM

30,2 NM

16.
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

1386 NM

1313 NM

1425 NM

1350 NM

17.
The cruising speed to write in the appropriate box of a flight plan is

true air speed

calibrated air speed

ground speed

indicated air speed

18.
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

Statement 1 only

Statement 2 only

Both statements

Neither statement

19.
On an ATC flight plan, the letter ""Y"" is used to indicate that the flight is carried out under the following flight rules

IFR

VFR

IFR followed by VFR

VFR followed by IFR

20.
For a repetitive flight plan (RPL) to be used, flights must take place on a regular basis on at least

20 occasions

10 occasions

50 occasions

30 occasions

21.
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

22.
Unless otherwise shown on charts for standard instrument departure the routes are given with

magnetic headings

true headings

magnetic course

true course

23.
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 396 kt

WCA -2°, GS 426 kt

WCA +2°, GS 396 kt

WCA +2°, GS 416 kt

24.
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

500 kg

800 kg

700 kg

1000 kg

25.
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

158.6 NM

224.5 NM

160.3 NM

222.1 NM

26.
A VFR flight planned for a Piper Seneca III. At a navigational checkpoint the remaining usable fuel in tanks is 60 US gallons. The alternate fuel is 12 US gallons. According to the flight plan the remaining flight time is 1h35min. Calculate the highest rate of consumption possible for the rest of the trip

37.9 US gallons/hour

21.3 US gallons/hour

30.3 US gallons/hour

33.0 US gallons/hour

27.
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

1 - 3

02-Jan

2001-02-03

2 - 3

28.
In the ATS flight plan item 15, when entering a route for which standard departure (SID) and standard arrival (STAR) procedures exist

SIDs should be entered but not STARs

both should be entered in the ATS plan where appropriate

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

STARS should be entered but not SIDs

29.
An aircraft is in cruising flight at FL 095, IAS 155kt. The pilot intends to descend at 500 ft/min to arrive overhead the MAN VOR at 2 000 FT (QNH 1 030hPa). The TAS remains constant in the descent, wind is negligeable, temperature standard. At which distance from MAN should the pilot commence the descent?

45 NM

40 NM

48 NM

42 NM

30.
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?

511 Nautical Air Miles (NAM)

414 Nautical Air Miles (NAM)

499 Nautical Air Miles (NAM)

406 Nautical Air Miles (NAM)

31.
In the ATS 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

C

P

A

B

32.
During an IFR flight TAS and time appear to deviate from the data in the flight plan. The minimum deviations, that should be reported to ATC in order to conform to PANS-RAC, are

TAS 10 kt and time 2 minutes

TAS 3% and time 3 minutes

TAS 5% and time 3 minutes.

TAS 5 kt and time 5 minutes

33.
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

79 800 kg

77 800 kg

74 800 kg

77 200 kg

34.
In an ATS flight plan, Item 15 (route), a cruising pressure altitude of 32000 feet would be entered as

F320

FL320

32000

S3200

35.
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 airway is a low level link route 2100 ft - 3500 ft MSL

the minimum obstruction clearance altitude (MOCA) is 3500 ft

36.
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

11 100 kg

8 600 kg

11 400 kg

14 400 kg

37.
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

167 NM

147 NM

203 NM

183 NM

38.
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 42 minutes

1 hour 54 minutes

2 hours 02 minutes

1 hour 39 minutes

39.
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 2H15

EDDM 0215

EDDM 1415

EDDM 1215

40.
The required time for final reserve fuel for turbojet aeroplane is

60 min

45 min.

Variable with wind velocity

30 min.

41.
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.

1845 kg

3500 kg.

8120 kg.

42.
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

The pilot-in-command must advise ATC of his intention to divert to Limoges at least 15 minutes before the planned time of arrival

It is not possible to plan another destination and the fIight has to be simply cancelled that day (scheduled flight and not chartered).

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.

43.
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

44.
When calculating the fuel required to carry out a given flight, one must take into account :1 - the wind2 - foreseeable airborne delays3 - other weather forecasts4 - any foreseeable conditions which may delay landingThe combination which provides the correct statement is

03-Jan

1 - 2 - 3

03-Jan

1 - 2 - 3 - 4

45.
In an ATS flight plan Item 15 (route), in terms of latitude and longitude, a significant point at 41°35' north 4°15' east should be entered as

4135N00415E

41°35' N 04° 15'E

N04135E0415

N4135 E00415

46.
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 x GSo / (GSo + GSr)

X = (D/2) x GSo / (GSo + GSr)

X = (D/2) + GSr / (GSo + GSr)

X = D x GSr / (GSo + GSr)

47.
Given : true track 017, W/V 340/30, TAS 420 ktFind : wind correction angle (WCA) and ground speed (GS)

WCA +2° , GS 396 kt

WCA +2° , GS 416 kt

WCA -2° , GS 396 kt

WCA -2° , GS 426 kt

48.
An airway is marked 5000 2900a. The notation 5000 is the

minimum enroute altitude (MEA)

base of the airway (AGL)

minimum holding altitude (MHA)

maximum authorised altitude (MAA)

49.
The Trip Fuel for a jet aeroplane to fly from the departure aerodrome to the destination aerodrome is 5 350 kg. Fuel consumption in holding mode is 6 000 kg/ h. The quantity of fuel which is needed to carry out one go-around and land on the alternate airfield is 4 380 kg. The destination aerodrome has a single runway.What is the minimum quantity of fuel which should be on board at take-off?

10 000 kg

12 700 kg

13 000 kg

13 050 kg

50.
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 feet above aerodrome B

30 minutes holding 2,000 feet above aerodrome B

30 minutes holding 1,500 feeI above aerodrome A

15 minutes holding 2,000 feet above aerodrome A

Question Bank

Questions for INDIGO FLIGHT PLANNING (2108-2519)

From which of the following would you expect to find information regarding known short unserviceability of VOR, TACAN, and NDB ?

To carry out a VFR flight to an off-shore platform, the minimum fuel quantity on board is

Given:Dry operating mass (DOM)= 33000 kgLoad= 8110 kgFinal reserve fuel= 983 kgAlternate fuel= 1100 kgContingency fuel 102 kgThe estimated landing mass at alternate should be

On an ATC flight plan, an aircraft indicated as ""H"" for ""Heavy""

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 ?

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

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

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

The planned departure time from the parking area is 1815 UTCThe estimated takeoff time is 1825 UTCThe IFR flight plan must be filed with ATC at the latest at

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

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 ""current flight plan"" is a

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?

If your destination airport has no ICAO indicator, in the appropriate box of your flight plan, you write

A descent is planned from 7500 ft MSL so as to arrive at 1000 ft MSL 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

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

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

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

On an ATC flight plan, the letter ""Y"" is used to indicate that the flight is carried out under the following flight rules

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

Which of the following statements regarding filing a flight plan is correct?

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

Given: True course (TC) 017°, W/V 340°/30 kt, True air speed (TAS) 420 ktFind: Wind correction angle (WCA) and ground speed (GS)

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

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

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?

In the ATS 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

During an IFR flight TAS and time appear to deviate from the data in the flight plan. The minimum deviations, that should be reported to ATC in order to conform to PANS-RAC, are

In an ATS flight plan, Item 15 (route), a cruising pressure altitude of 32000 feet would be entered as

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

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

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

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

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

The required time for final reserve fuel for turbojet aeroplane is

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

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

When calculating the fuel required to carry out a given flight, one must take into account :1 - the wind2 - foreseeable airborne delays3 - other weather forecasts4 - any foreseeable conditions which may delay landingThe combination which provides the correct statement is

In an ATS flight plan Item 15 (route), in terms of latitude and longitude, a significant point at 41°35' north 4°15' east should be entered as

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

Given : true track 017, W/V 340/30, TAS 420 ktFind : wind correction angle (WCA) and ground speed (GS)

An airway is marked 5000 2900a. The notation 5000 is the

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