DGCA CPL AIR NAVIGATION

DGCA CPL/ATPL - GENERAL NAVIGATION

Hi ,

This DGCA-aligned General Navigation quiz is designed to evaluate your conceptual clarity, calculation accuracy, and exam readiness exactly as required for DGCA CPL / ATPL examinations.

The quiz covers:

  • True, Magnetic & Compass direction conversions

  • Wind correction angle, drift & triangle of velocities

  • IAS, TAS & Ground Speed relationships

  • Chart projections and applied navigation logic

  • Common DGCA trap concepts and recurring exam mistakes

Each question is structured to test application over memorisation, helping you identify the precise gaps that affect DGCA performance.

🎯 Who should take this quiz:

  • DGCA CPL / ATPL aspirants

  • Students facing difficulty in General Navigation

  • Repeat exam candidates

  • Pilots aiming for strong GN fundamentals


🚀 Online Coaching (Instructor-Led)

Students who need structured guidance and exam-oriented teaching can enrol in online General Navigation coaching, where I personally teach and mentor students with a focus on:

  • Clear concept breakdowns

  • DGCA-style numerical problem solving

  • Shortcuts, logic building & exam strategy

📞 For Online Classes Enquiries:
Capt. Louis Lobo
📱 9004751779

Prepare with clarity. Train with purpose.
Master General Navigation for DGCA—the right way.

 

1 / 386

What is the approximate compression of the Earth?

2 / 386

The following rhumb line tracks and distances are flown; starting from E in latitude 50°N.

E to F 000°(T) 300 NM

F to G 090°(T) 300 NM

G to H 180°(T) 300 NM

What is the rhumb line bearing and distance of H from E?

3 / 386

An aircraft flies for 1000 nm along a rhumb line track of 090°(T) from C at 36°00’N 174°45’E to D. What is the longitude of D?

4 / 386

A flight is to be made along the parallel of latitude from A at 48°00’N 04°00’W to B at 48°00’N 02°27’E. Calculate the distance

5 / 386

An aircraft at position 2700N 17000W travels 3000 km on a track of 180°(T), then 3000 km on

a track of 090°(T), then 3000 km on a track of 000°(T), then 3000 km on a track of 270°(T).

What is its final position?

6 / 386

A and B are both in the Southern hemisphere and the convergency of their meridians is 8°. The initial great circle track from A to B is 094°(T).

If the position of B is 23°00’S 20°00’W, what is the position of A?

7 / 386

Calculate the convergency between positions A (55°30’N 04°35’W) and B  (64°00’N 22°37’W).

8 / 386

Position X 64°00’S 11°50’W. Position Y 64°00’S 05°10’W.

Give:

The approximate initial great circle track from Y to X.

9 / 386

A and B are in the same hemisphere.

The initial great circle track from B to A is 268°(T) and the initial great circle

track from A to B is 092°(T).

i)In which hemisphere are A and B?

ii)What is the rhumb line track from A to B?

10 / 386

In what latitude is the convergency between two meridians on the Earth

equal to twice their convergency in latitude 20°N?

11 / 386

The great circle track from A to B measures 227°(T) at A and 225°(T) at B.

What is the convergency of the meridians through A and B and in which

hemisphere are they?

12 / 386

The great circle bearing of position B in latitude 30°00’S from position A (30°00’S

165°00’E) is 100°(T).

What is:

a. The great circle track from B to A?

b.The longitude of position B ?

13 / 386

The convergency of the meridians through M and N which are in the Southern

hemisphere is 12°.

If the rhumb line track from M to N is 249°(T), what is the great circle track:

from M to N?

14 / 386

An aircraft flying VFR using visual navigation crosses two parallel roads at right

angles to the track. For what purpose could that information be used?

15 / 386

Which of the following would be most useful as a visual checkpoint when

planning a flight?

16 / 386

refer to Appendix A. What is the symbol for an unlighted

obstacle?

17 / 386

You are flying a VFR route and have become uncertain of your position. Which is

the best course of action?

18 / 386

You are flying an airway with a centre line QDM of 137 °(M) towards VOR/DME ‘A’.

Your RMI reads 141°(M)/DME 90 NM.

Are you left or right of centre line?

19 / 386

On the approach to London Heathrow runway 27, glide slope 3°, you reduce speed

from 150 kt to 120 kt. What change should you make to your ROD to maintain glide

slope?

20 / 386

You are approaching Innsbruck, Austria on a glide slope of 3.5°. What height (QFE)

should you be at 2 miles range

21 / 386

An aircraft is flying due South. At 1000 hrs, point P bears 267°(T) from the aircraft.

At 1006 hrs, point P bears 275°(T) from the aircraft. If the aircraft has a ground

speed of 120 kt, estimate the range of the aircraft from point P.

22 / 386

Approaching London City airport (glide slope 5.5°), you reduce ground speed from 120 kt to

110 kt. What change should you make to your ROD to maintain the glide slope?

23 / 386

Approaching London Heathrow (3° glide slope), an aircraft decreases speed from 140 kt to 120

kt. What change in the ROD must be made to maintain the glide slope?

24 / 386

An aircraft is flying from Oxford to Cambridge, planned track 074°(M), distance

70 NM, heading 065°(M). Having flown 30 NM, the pilot ‘pinpoints’ the aircraft

position overhead Cranfield, 4 NM left of planned track

What was the expected drift?

25 / 386

An aircraft leaves A to fly to B, 95 NM distance. Having flown 35 NM, the aircraft

position is found from a ‘pinpoint’ (a geographical point over which the aircraft has

flown); the pinpoint is 7 NM right of track.

What alteration of heading is required to fly direct to B?

26 / 386

If an aircraft is 2 miles off required track at a range of 40 NM, what is the angle off

track (track error)?

27 / 386

If an aircraft is 3° off required track at a range of 120 NM, how far in nautical miles

(NM) is the aircraft off required track?

28 / 386

You are flying from S to T, which is a required track of 272°(T). You find that your

position is 50 NM from T and 5 NM right of the required track. What track must you

fly to arrive overhead T?

29 / 386

You are flying from Q to R, which is a required track of 125°(T). You find that your

position is 40 NM from R and 2 NM left of the required track. What track must you

fly to arrive overhead R?

30 / 386

You are flying an instrument approach to an airfield and the required glide slope

angle is 2.5°. You are correctly on the glide slope and you are passing a height of

1000 feet QFE. What is your range from the touchdown point? (Assume 1 NM =

6000 feet).

31 / 386

You are flying an instrument approach to an airfield and the required glide slope

angle is 3.00°. What height should you be passing when you are exactly 2 nautical

miles from the touchdown point? (NOTE: For this question, assume 1 NM = 6000

feet).

32 / 386

A surveyor places himself 660 metres from a mast and measures an elevation angle

of 4° to the top of the mast. What is the height of the mast?

33 / 386

You are flying from N to P, which is a required track of 315°(T). You find that your

position is 40 NM outbound from N and 6 NM left of the required track. What is

your track made good?

34 / 386

You are flying from L to M, which is a required track of 220°(T). You find that your

position is 45 NM outbound from L and 3 NM right of the required track. What is

your track made good?

35 / 386

You are flying from J to K, which is a required track of 045°(T). You find that your

position is 80 NM outbound from J and 4 NM left of the required track. What is

your track made good?

36 / 386

You are flying from G to H. You find that your position is 30 NM outbound from G

and 4 NM left of the required track. What is your track error angle?

37 / 386

You are flying from E to F. You find that your position is 90 NM outbound from E

and 6 NM right of the required track. What is your track error angle?

38 / 386

You are flying from C to D. You find that your position is 120 NM outbound from C

and 8 NM right of the required track. What is your track error angle?

39 / 386

You are flying from A to B. You find that your position is 60 NM outbound from A

and 7 NM left of the required track. What is your track error angle?

40 / 386

On a particular take-off, you can accept up to 10 knots tailwind. The runway QDM

is 047, the variation is 17°E and the ATIS gives the wind direction as 210. What is

the maximum wind strength you can accept?

41 / 386

If variation is West, then:

42 / 386

What is a line of equal magnetic variation?

43 / 386

What is the dip angle at the South Magnetic Pole?

44 / 386

What is the maximum possible value of dip angle?

45 / 386

Isogonal lines converge as follows:

46 / 386

The value of magnetic variation on a chart changes with time. This is due to:

47 / 386

The angle between True North and Magnetic North is known as:

48 / 386

The agonic line:

49 / 386

The value of variation:

50 / 386

Where is a compass most effective?

51 / 386

Which of these is a correct statement about the Earth’s magnetic field?

52 / 386

At the magnetic equator:

53 / 386

What is the definition of magnetic variation?

54 / 386

The sensitivity of a direct reading magnetic compass is

55 / 386

A Rhumb Line cuts all meridians at the same angle. This gives:

56 / 386

Any Meridian Line is a:

57 / 386

You are at position A at 54°20’N 002°30’W. Given a ch.lat of 16°20’N and a ch.long

of 20°30’W to B, what is the position of B?

58 / 386

What is the difference in nautical miles from position A (41°25’N)

to position B (79°30’N)? Both are on the same meridian.

59 / 386

Given that the compression value of the Earth is 1/297 and that the semi-major

axis of the Earth, measured at the axis of the Equator, is 6378.4 km, what is the

semi-minor (i.e. radius) axis of the Earth measured at the axis of the Poles?

60 / 386

A great circle has its North vertex at 70N 130E. What is the position of its South

vertex?

61 / 386

A Graticule is the name given to:

62 / 386

Your position is 5833N 17400W. You fly exactly 6 NM eastwards. What is your new

position?

63 / 386

An aircraft is flying around the Earth eastwards along the 60N parallel of latitude

at a ground speed of 240 knots. At what ground speed would another aircraft

have to fly eastwards along the Equator to fly once round the Earth in the same

journey time?

64 / 386

An aircraft departs a point 0400N 17000W and flies 600 NM South, followed by

600 NM East, then 600 NM North, then 600 NM West. What is its final position?

65 / 386

An aircraft at position 50N 006E travels 300 NM due South, then travels 300 NM

due East, then 300 NM due North and then 300 NM due West. What is the

aircraft’s final position relative to its start point?

66 / 386

An aircraft starts at position 0410S 17822W and heads true north for 2950 NM,

then turns 90 degrees left, and maintains a rhumb line track for 314 kilometres.

What is its final position?

67 / 386

Aircraft S leaves position 36°N 10°E at 1522 hours, and flies a rhumb line track of

090°(T) at ground speed 470 kt until it reaches the 13°E meridian when it turns

onto a track of 180°(T) at a ground speed of 460 kt.

Aircraft T leaves position 30°N 10°E at 1522 hours and flies a rhumb line track of

090°(T) at ground speed 150 kt,

1.  Which aircraft reaches position 30°N 13°E first?

68 / 386

Aircraft Q, ground speed 301 kt flies parallel of latitude 46°N through 10° of

longitude. Aircraft R, ground speed 364 kt flies between the same meridians in the

same time as aircraft Q.

What is the latitude of the track of aircraft R?

69 / 386

An aircraft leaves position L in latitude 37°S and makes good the following tracks

and ground speeds:

L to M 270°(T) 310 kt M to N 180°(T) 280 kt N to P 090°(T) 250 kt

P is due south of L

M is reached 80 minutes after leaving L

P is reached 93.5 minutes after leaving N

Calculate the distance and time from M to N.

70 / 386

At which latitude is the departure in NM. between two points equal to:

i.

At Equator

their difference in longitude in minutes?

71 / 386

An aircraft leaves J (36°00’S 130°14’E) at 0946 UTC, flying a rhumb line track of 270°

at Flight Level 100, temperature 0°C, Mach No. 0.81, wind component 35 kt tail.

What is the aircraft’s position at 1004 UTC?

72 / 386

In which latitude is a difference in longitude of 44°10’ the equivalent of a

departure of 2295 NM?

73 / 386

What is the track and distance measured along the parallel of latitude of 80°S from

176°15’W to 179°45’E?

74 / 386

An aircraft is flying at FL200, the OAT is 0°C. When the actual air pressure on an

airfield at MSL is placed on the subscale of the altimeter the indicated altitude is 19 300 ft. What is the aircraft’s True Altitude?

75 / 386

An aircraft at position 8500N 02000E flies a rhumb line track of 075°(T). What will be its path over the Earth?

76 / 386

An aircraft homing to a VOR/DME loses 2500 feet in 11.1 NM change of DME range.

What is the gradient of the slope?

77 / 386

The orbit of the Earth round the Sun is elliptical. An ellipse has 2 foci. Which of the following is a correct statement?

78 / 386

The distance A to B is 90 NM in a straight line. You are 60 NM from A when you fix

your position 4 NM to the left of track. What correction do you need to make to arrive at B?

79 / 386

How many nautical miles are travelled in 1 minute 45 seconds at a ground speed of 135 knots?

80 / 386

Given: FL350, Mach 0.80, OAT -55°(C), calculate values for TAS and LSS

81 / 386

Given: Position A is 60N 020W, Position B is 60N 021W, and Position C is 59N 020W, what are, respectively, the distances from A to B and from A to C?

82 / 386

Fuel flow per hr is 22 US.gal, total fuel on board is 83 imp.gal. What is the endurance?

83 / 386

Given:

TAS = 485 kt, OAT = ISA +10°C, FL410. Calculate the Mach Number.

84 / 386

The rhumb line distance between points A (60°00’N 002°30’E) and B (60°00’N 007°30’W) is:

85 / 386

The angle between the true great circle track and the true rhumb line track joining

the following points: A (60S 165W) and B (60S 177E) at the place of departure A?

86 / 386

 

During a low level flight 2 parallel roads are crossed at right angles by an aircraft. The time between these roads can be used to check the aircraft:

87 / 386

 

Given: True course 300°

Drift 8°R

Variation 10°W

Deviation -4°

Calculate the compass heading.

88 / 386

The distance between two waypoints is 200 NM.

To calculate compass heading the pilot used 2°E magnetic variation instead of 2°W.

Assuming that the forecast W/V applied, what will the off track distance be at the second waypoint?

89 / 386

Given:

IAS 120 kt

FL80

OAT +20°(C)

What is the TAS?

90 / 386

On a direct Mercator chart, a rhumb line appears as a

91 / 386

Isogonals are lines of equal:

92 / 386

A compass swing is performed in order to correct for:

93 / 386

What is the meaning of the term ‘standard time’?

94 / 386

What rate of descent is required to maintain a 3.5° glide slope at a ground speed of 150 knots?

95 / 386

On the Polar Stereographic projection, a great circle appears as:

96 / 386

What is the formula for conversion angle?

97 / 386

You are at FL150 and the SAT is -5°(C). You are over an airport with an elevation of 720 feet. The QNH is 1003. Assume 27 feet = 1 hPa. What is your true height?

98 / 386

On which chart projection is it not possible to show the North Pole?

99 / 386

On a Lambert’s chart the constant of the cone is 0.80. A is at 53N 04W. You plan

to fly to B. The initial Lambert’s chart straight-line track is 070(T) and the rhumb line track from A to B is 080(T). What is the longitude of B?

100 / 386

On a Lambert chart, the convergence factor is .78585. What is the parallel of tangency?

101 / 386

Lines of latitude on a chart are always

102 / 386

Given: Runway direction 083°(M), Surface W/V 045/35 kt. Calculate the effective headwind component.

103 / 386

On a conformal chart, the standard parallels are 41° 20’N and 11° 40’N. What is the constant of the cone?

104 / 386

What is the shortest distance between Point ‘A’ (3543N 00841E) and Point ‘B’ (5417N 17119W)?

105 / 386

What is the duration of civil twilight?

106 / 386

An aircraft flies 100 stat.m in 20 minutes. How long does it take to fly 215 NM?

107 / 386

What is the diameter of the Earth?

108 / 386

Given: Heading 165(M), Variation 25W, Drift 10°R, G/S 360 knots. At ‘A’ your

relative bearing to an NDB is 325R. Five minutes later, at ‘B’, the relative bearing is 280(R). What is the true bearing and distance from ‘B’ to the NDB?

109 / 386

At 0422 you are 185 NM from a VOR at FL370. You need to descend at a mean

descent rate of 1800’/min to be at FL80 overhead the VOR. Your ground speed in

the level cruise is currently 320 knots. In the descent your mean G/S will be 232 knots. What is the latest time to commence descent?

110 / 386

What is the chart convergence factor on a Polar Stereographic chart?

111 / 386

Please refer to Appendix A. What does symbol 9 represent?

112 / 386

How do rhumb lines (with the exception of meridians) appear on a Polar Stereographic chart?

113 / 386

On a chart, meridians at 45N are shown every 10 degrees apart. This is shown on the chart by a distance of 14 cm. What is the scale?

114 / 386

Given that the value of ellipticity of the Earth is 1/297 and that the semi-major axis

of the Earth, measured at the axis of the Equator is 6378.4 km, what is the semi- minor axis of the Earth measured at the axis of the Poles?

115 / 386

An aircraft at position 0000N/S 16327W flies a track of 225°(T) for 70 NM. What is its new position?

116 / 386

A Lambert conformal conic chart has a constant of the cone of 0.80.

A straight line course drawn on this chart from A (53°N 004°W) to B is 080° at A; course at B is 092°. What is the longitude of B?

117 / 386

TAS = 240 knots. Track is 180°(T). The relative bearing from an NDB is 315(R) at 1410. At 1420 the bearing has changed to 270(R). What is your distance from the NDB at 1420?

118 / 386

Your position is 5833N 17400W. You fly exactly 6 NM westwards. What is your new position?

119 / 386

The chart that is generally used for navigation in polar areas is based on a:

120 / 386

Convert 80 metres/sec into knots.

121 / 386

Given: Aircraft height = 2500 feet, ILS GP angle = 3°, at what approximate distance from the threshold can you expect to intercept the glide-path?

122 / 386

At what times of the year does the length of the hours of daylight change most rapidly?

123 / 386

At what latitude does the maximum difference between geodetic and geocentric latitude occur?

124 / 386

If variation is East, then

125 / 386

An aircraft is flying around the Earth eastwards along the 60N parallel of latitude

at a ground speed of 360 knots. At what ground speed would another aircraft have to fly eastwards along the Equator to fly once round the Earth in the same journey time?

126 / 386

An island is observed to be 15°(T)o the left.

The aircraft heading is 120°(M), variation 17°(W).

The bearing (°T) from the aircraft to the island is:

127 / 386

 

Given: Track 198°, Heading 184°, TAS 427 kt and GS 453kt, what are the W/V and Drift Angle?

128 / 386

Please refer to Appendix A.

What is the chart symbol for a lightship?

129 / 386

What is the effect on the Mach number and TAS in an aircraft that is climbing with constant CAS?

130 / 386

What is the rhumb line track from A (4500N 01000W) to B (4830N 00500W)?

131 / 386

What is the reason for seasonal changes in climate?

132 / 386

What is a line of equal grivation?

133 / 386

What is the dip angle at the North Magnetic Pole?

134 / 386

Civil Twilight occurs between:

135 / 386

An aircraft’s compass must be swung:

136 / 386

An aircraft is at 5530N 03613W, where the variation is 15W. It is tuned to a VOR located at 5330N 03613W, where the variation is 12W. What VOR radial is the aircraft on?

137 / 386

You leave A to fly to B, 475 NM away, at 1000 hours. Your ETA at B is 1130. At

1040, you are 190 NM from A. What ground speed is required to arrive on time at B?

138 / 386

What is the weight in kilograms of 380 US Gallons at a Specific Gravity of 0.78?

139 / 386

Given: For take-off an aircraft requires a headwind component of at least 10 kt

and has a cross-wind limit of 35 kt. The angle between the wind direction and the runway is 45°. Calculate the maximum and minimum allowable wind speeds.

140 / 386

Given: Runway direction 083°(M), Surface W/V 035/35 kt. Calculate the effective crosswind component.

141 / 386

Given:

Magnetic heading 311°

Drift is 10° left

Relative bearing of NDB 270. What is the magnetic bearing of the NDB measured from the aircraft?

142 / 386

What is the maximum possible value of Dip Angle at either Pole?

143 / 386

At 1000 hours an aircraft is on the 310 radial from a VOR/DME, at 40 nautical miles

range. At 1015 the radial and range are 040/40 NM. What is the aircraft’s track and ground speed?

144 / 386

An aircraft departs a point 0400N 17000W and flies 240 NM South, followed by 240 NM East, then 240 NM North, then 240 NM West. What is its final position?

145 / 386

Position A is 55N 30W. Position B is 54N 20W. The great circle track from A to B, measured at A, is 100°(T). What is the rhumb line bearing from A to B?

146 / 386

Isogonal lines converge as follows:

147 / 386

The value of magnetic variation on a chart changes with time. This is due to

148 / 386

Position A is at 70S 030W, position B is 70S 060E. What is the great circle track of B from A, measured at A?

149 / 386

The angle between the plane of the Equator and the plane of the Ecliptic is:

150 / 386

An aircraft is at 10°N and is flying North at 444 km/hour. After 3 hours the latitude is

151 / 386

The angle between True North and Magnetic North is known as:

152 / 386

What is the highest latitude on the Earth at which the Sun can be vertically overhead?

153 / 386

On a particular direct Mercator wall chart, ‘the full length of the parallel of latitude at 53N is 133 cm long. What is the scale of the chart at 30S?

154 / 386

You fly from 49N to 58N along the 180 E/W meridian. What is the distance in kilometres?

155 / 386

A rhumb line is:

156 / 386

You are homing to overhead a VORTAC and will descend from 7500 QNH to be

1000 AMSL by 6 NM DME. Your ground speed is 156 knots and the ROD will be 1000 feet/min. At what range from the VORTAC do you commence the descent?

157 / 386

An aircraft at FL370 is required to commence descent at 120 NM from a VOR and to

cross the facility at FL130. If the mean GS for the descent is 288 kt, the minimum rate of descent required is:

158 / 386

An aircraft at position 2700N 17000W travels 3000 km on a track of 180°(T), then

3000 km on a track of 090°(T), then 3000 km on a track of 000°(T), then 3000 km on a track of 270°(T). What is its final position?

159 / 386

Ground speed is 540 knots. 72 NM to go. What is time to go?

160 / 386

The relative bearing to a beacon is 090°R. Three minutes later, at a ground speed

of 180 knots, it has changed to 135°R. What was the distance of the closest point of approach of the aircraft to the beacon?

161 / 386

You are on an ILS 3-degree glide slope which passes over the runway threshold at

50 feet. Your DME range is 25 NM from the threshold. What is your height above

the runway threshold elevation? (Use the 1 in 60 rule and 6000 feet = 1 nautical mile)

162 / 386

How does scale change on a normal Mercator chart?

163 / 386

The pressure alt is 29 000 feet and the SAT is -55°(C). What is density altitude?

164 / 386

What is the highest latitude listed below at which the Sun will rise above the horizon and set every day?

165 / 386

In which month does aphelion occur?

166 / 386

At 65 NM from a VOR you commence a descent from FL330 in order to arrive over the VOR at FL80. Your mean ground speed in the descent is 240 knots. What rate of descent is required?

167 / 386

On a 5% glide slope your groundspeed is 150 kt. What should be your rate of descent to maintain the glide slope?

168 / 386

The agonic line:

169 / 386

On a particular take-off, you can accept up to 10 knots tailwind. The runway QDM

is 047, the variation is 17°E and the ATIS gives the wind direction as 210. What is the maximum wind strength you can accept?

170 / 386

Your pressure altitude is FL55, the QNH is 998, and the SAT is +30°(C). What is density altitude?

171 / 386

You are heading 345°(M), the variation is 20°E, and you take a radar bearing of 30° left of the nose from an island. What bearing do you plot from the island?

172 / 386

Heading is 156°(T), TAS is 320 knots, W/V is 130/45 and the Variation is 10°W. What is your magnetic track?

173 / 386

The scale on a Lambert’s conformal conic chart

174 / 386

On a direct Mercator chart, great circles are shown as

175 / 386

On a chart, 90.74 km is represented by 7.0 centimetres. What is the scale?

176 / 386

A Lambert’s Conical conformal char

177 / 386

The main reason that day and night, throughout the year, have different durations is due to the:

178 / 386

5 hours 20 minutes and 20 seconds time difference is equivalent to which change of longitude?

179 / 386

In which months is the difference between apparent noon and mean noon the greatest?

180 / 386

By what amount must you change your rate of descent given a 10 knot decrease in headwind on a 3° glide slope?

181 / 386

You are heading 080°(T) when you get a range and bearing fix from your AWR on a headland at 185 NM 30° left of the nose. What true bearing do you plot on the chart?

182 / 386

An aircraft starts at position 0410S 17822W and heads true north for 2950 NM,

then turns 90 degrees right, and maintains a rhumb line track for 314 kilometres. What is its final position?

183 / 386

Given:

Airport elevation is 1000 feet.

QNH is 988 hPa

What is the approximate airport pressure altitude?

184 / 386

An aircraft is at FL140 with an IAS of 210 and a true OAT of -5°(C). The wind

component is -35 knots. When the aircraft is at 150 NM from a reporting point,

ATC request the crew to lose 5 minutes by the time they get to the beacon. How much do they need to reduce IAS?

185 / 386

A useful method of a pilot resolving, on a visual flight, any uncertainty in the aircraft’s position is to maintain visual contact with the ground and:

186 / 386

Isogrivs are lines that connect positions that have:

187 / 386

A-C = 50nm (A-B = 30nm, B-C=20nm)

ATA A is 1010. ETA B is 1030. ETA C is 1043.

ATA B is 1027. What is revised ETA C?

188 / 386

An aircraft leaves at 0900UTC on a 250 NM journey with a planned ground speed

of 115 knots. After 74 NM the aircraft is 1.5 minutes behind the planned schedule. What is the revised ETA at the destination?

189 / 386

Grivation is the combination of

190 / 386

The value of variation

191 / 386

Where is a compass most effective?

192 / 386

Which of these is a correct statement about the Earth’s magnetic field?

193 / 386

At the magnetic equator

194 / 386

What is the definition of magnetic variation?

195 / 386

An aircraft at position 60°N 005°W tracks 090°(T) for 315 km. On completion of the flight the longitude will be:

196 / 386

The sensitivity of a direct reading magnetic compass is:

197 / 386

You are flying 090°(C) heading. Deviation is 2W and Variation is 12E. Your TAS is 160 knots. You are flying the 070 radial outbound from a VOR and you have gone 14 NM in 6 minutes. What is the W/V?

198 / 386

An aircraft flies a great circle track from 56°N 070°W to 62°N 110°E. The total distance travelled is:

199 / 386

Required course 045°(T), W/V = 190 /30, FL = 55 @ ISA, Variation = 15°W. CAS = 120 knots. What is mag heading and G/S?

200 / 386

Course 040°(T), TAS 120 kt, Wind speed = 30 knots. From which direction will the wind give the greatest drift?

201 / 386

‘ISA Dev = +30°C, Pressure alt = 5000 feet. What is true alt?

202 / 386

G/S = 240 knots, Distance go = 530 NM. What is time to go?

203 / 386

Pressure Altitude is 28 000 feet, OAT = -45°C, Mach No = 0.46, W/V = 270/85, Track = 200°T. What is the drift and groundspeed?

204 / 386

A South Polar Stereographic chart is overprinted with a false grid aligned with the

prime meridian. At position 87S 123W the true track of an aircraft is 179°. What will the grid track be?

205 / 386

Question

206 / 386

 

A North Polar Stereographic chart is overprinted with a false grid aligned with the prime meridian. At position 80N 135E the grid track is 235°, will the true track be:

207 / 386

Sunrise/sunset twilight tables in the Air Almanac are listed for a sea level

situation. An aircraft flying at FL350 would experience sunrise _____________ ,sunset ___________ and the length of twilight would ____________

208 / 386

Between 60N and 60S, the minimum duration of Civil Twilight is?

209 / 386

Nautical twilight and astronomic twilight are the twilight periods that follow

civil twilight. Nautical twilight occurs when the Sun is between _________ and ____________ below the sensible horizon:

210 / 386

Civil twilight is

211 / 386

On Mid-winter Day in the Northern hemisphere, the Sun will be overhead:

212 / 386

On Mid-summer Day in the Southern hemisphere, the Sun will be overhead:

213 / 386

A ship at longitude 83E observes sunrise at a Zone Time of 0500 ZT on Zone Date 15th May. What is the UTC?

214 / 386

Zone Time (ZT) is used

215 / 386

Local Mean Time (LMT) always changes by a day when crossing:

216 / 386

The definition of Local Mean Time (LMT) is:

217 / 386

Without using the Air Almanac, convert 153°30’ of arc of longitude into time

218 / 386

 

A star has a Greenwich Hour Angle (GHA) of 220°. Which meridian is the star transiting (crossing)?

219 / 386

The Hour Angle (Greenwich Hour Angle) of a celestial body is analogous/ equivalent on the Earth to ________?

220 / 386

‘The Calendar Year and the Tropical Year are of different lengths. The difference

is adjusted partly by using leap years every fourth calendar year. However, some years are not designated as leap years’. Which of the following years will be a leap year?

221 / 386

What is the length of a Sidereal Year?

222 / 386

The maximum difference between mean time and apparent time is:

223 / 386

The maximum difference between mean noon (1200LMT) and real/apparent noon occurs in ________?

224 / 386

A sidereal day is

225 / 386

‘The length of daylight/night depends upon the declination of the Sun and the

latitude of the observer’. When is the rate of change of the length of daylight greatest?

226 / 386

The declination of a celestial body (the Sun) measured on the Celestial Sphere is analogous (equivalent) to ________________ on the Earth?

227 / 386

What is the angle between the Equinoctial and the Ecliptic?

228 / 386

In the situation given above in Question 5, the Sun will be overhead:

229 / 386

When it is the Winter Solstice in the Southern hemisphere, the Declination of the Sun is:

230 / 386

When do the ‘equinoxes’ occur?

231 / 386

Viewed from the North Celestial Pole (above the North Pole), the Earth orbits the Sun:

232 / 386

When does aphelion occur?

233 / 386

When does perihelion occur?

234 / 386

On a Lambert’s chart the constant of the cone is 0.80. A is at 53N 04W. You plan to

fly to B. The initial Lambert’s chart straight-line track is 070°(T) and the rhumb line track from A to B is 082°(T). What is the longitude of B?

235 / 386

On a Lambert chart, the constant of the cone is .78585. What is the parallel of tangency?

236 / 386

Scale on a Lambert conformal chart is:

237 / 386

On a conformal chart, the standard parallels are 41°20’N and 11°40’N. What is the constant of the cone?

238 / 386

Scale on a Lambert’s conformal conic chart

239 / 386

Question

240 / 386

A Lambert’s conformal chart extends from 29°N to 45°N. Standard parallels are

A Lambert’s conical conformal chart has standard parallels at 63N and 41N. What is the constant of the cone?

241 / 386

Sunrise/sunset twilight tables in the Air Almanac are listed for a sea level

situation. An aircraft flying at FL350 would experience sunrise _____________ ,sunset ___________ and the length of twilight would ____________

242 / 386

Between 60N and 60S, the minimum duration of Civil Twilight is?

243 / 386

Nautical twilight and astronomic twilight are the twilight periods that follow

civil twilight. Nautical twilight occurs when the Sun is between _________ and____________ below the sensible horizon:

244 / 386

Civil twilight is

245 / 386

On Mid-winter Day in the Northern hemisphere, the Sun will be overhead:

246 / 386

On Mid-summer Day in the Southern hemisphere, the Sun will be overhead:

247 / 386

A ship at longitude 83E observes sunrise at a Zone Time of 0500 ZT on Zone Date 15th May. What is the UTC?

248 / 386

Zone Time (ZT) is used

249 / 386

Local Mean Time (LMT) always changes by a day when crossing

250 / 386

The definition of Local Mean Time (LMT) is

251 / 386

Without using the Air Almanac, convert 153°30’ of arc of longitude into time.

252 / 386

A star has a Greenwich Hour Angle (GHA) of 220°. Which meridian is the star transiting (crossing)?

253 / 386

The Hour Angle (Greenwich Hour Angle) of a celestial body is analogous/equivalent on the Earth to ________?

254 / 386

The Calendar Year and the Tropical Year are of different lengths. The difference

is adjusted partly by using leap years every fourth calendar year. However, some years are not designated as leap years’. Which of the following years will be a leap year?

255 / 386

What is the length of a Sidereal Year?

256 / 386

The maximum difference between mean time and apparent time is

257 / 386

The maximum difference between mean noon (1200LMT) and real/apparent noon occurs in ________?

258 / 386

A sidereal day is

259 / 386

‘The length of daylight/night depends upon the declination of the Sun and the

latitude of the observer’. When is the rate of change of the length of daylight greatest?

260 / 386

The declination of a celestial body (the Sun) measured on the Celestial Sphere is analogous (equivalent) to ________________ on the Earth?

261 / 386

What is the angle between the Equinoctial and the Ecliptic?

262 / 386

When it is the Winter Solstice in the Southern hemisphere, the Declination of the Sun is

263 / 386

When do the ‘equinoxes’ occur?

264 / 386

Viewed from the North Celestial Pole (above the North Pole), the Earth orbits the Sun:

265 / 386

When does aphelion occur?

266 / 386

When does perihelion occur?

267 / 386

On a Lambert’s chart the constant of the cone is 0.80. A is at 53N 04W. You plan to

fly to B. The initial Lambert’s chart straight-line track is 070°(T) and the rhumb line track from A to B is 082°(T). What is the longitude of B?

268 / 386

On a Lambert chart, the constant of the cone is .78585. What is the parallel of tangency?

269 / 386

Scale on a Lambert conformal chart is:

270 / 386

On a conformal chart, the standard parallels are 41°20’N and 11°40’N. What is the constant of the cone?

271 / 386

Scale on a Lambert’s conformal conic chart

272 / 386

A Lambert’s conformal chart extends from 29°N to 45°N. Standard parallels are

A Lambert’s conical conformal chart has standard parallels at 63N and 41N. What is the constant of the cone?

273 / 386

How does scale change on a normal Mercator chart?

274 / 386

Mercator charts use ................... projections

275 / 386

On a Mercator chart, a rhumb line appears as a:

276 / 386

A non-perspective chart:

277 / 386

On a chart, meridians at 43N are shown every 10 degrees apart. This is shown on the chart by a distance of 14 cm. What is the approximate scale?

278 / 386

On a particular direct Mercator wall chart, the 180W to 180E parallel of latitude at 53N is 133 cm long. What is the scale of the chart at 30S?

279 / 386

On a chart, 49 nautical miles is represented by 7.0 centimetres. What is the scale?

280 / 386

An aircraft starts at position 0410S 17822W and tracks true north for 2950 NM,

then turns 90 degrees left, and maintains a rhumb line track for 314 kilometres. What is the final position?

281 / 386

An aircraft flies directly from 56N 020W to 56N 030W. The initial Great Circle track from 020W is:

282 / 386

You are on an ILS 3-degree glide slope which passes over the runway threshold at

50 feet. Your DME range is 25 NM from the threshold. What is your height above

the runway threshold elevation? (Use the 1 in 60 rule and 6000 feet = 1 nauticalmile)

283 / 386

By what amount must you change your rate of descent given a 10 knot increase in headwind on a 3° glide slope?

284 / 386

A pilot receives the following signals from a VOR DME station.

Radial = 180° +/- 1°, distance = 200 NM

What is the approximate maximum error?

285 / 386

You are flying from A to B, planned track 245°(M), distance 225 NM. Your ground

speed is 180 knots. After 15 minutes flying, you fix your position as 3 NM left of planned track. Which of the following statements is correct?

286 / 386

Airfield elevation is 1000 feet. The QNH is 988. Use 27 feet per hectopascal. What is pressure altitude?

287 / 386

Convert 70 metres/sec into knots.

288 / 386

An aircraft is climbing at a constant CAS in ISA conditions. What will be the effect on TAS and Mach No.?

289 / 386

You leave A to fly to B, 475 NM away, at 1000 hours. Your ETA at B is 1130. At

1040, you are 190 NM from A. What ground speed is required to arrive on time at B?

290 / 386

You are flying at a True Mach No. of .72 in a SAT of -45°C. At 1000 hours you are

100 NM from the CPT DME and your ETA at CPT is 1012. ATC ask you to slow down

to be at CPT at 1016. What should your new Mach No be if you reduce speed at 100 NM to go?

291 / 386

Course 040°(T), TAS 120 kt, wind speed = 30 knots. From which direction will the wind give the greatest drift?

292 / 386

G/S = 240 knots, distance to go = 500 NM. What is time to go?

293 / 386

An aircraft is maintaining a 5.2% gradient on a flat terrain. Its height at 7 NM from the runway is approximately:

294 / 386

Given: TAS 140 kt, heading 005°(T), W/V 265/25, calculate the drift and groundspeed.

295 / 386

Given: TAS 200 kt, Track 110°(T), W/V 015/40, calculate heading (°T) and ground speed

296 / 386

Given: IAS 120 knots, FL80, OAT +20°C. What is the TAS?

297 / 386

You plan to land on R/W 14. The met forecast wind velocity is 110/30. Variation is 30°W. What crosswind do you expect?

298 / 386

You are flying at FL330 at Mach No. 0.9, Ambient temperature is ISA +15. What is your TAS?

299 / 386

You are flying at 400 kt TAS, Indicated temperature -50°C. What is your COAT?

300 / 386

You plan to take off from Khamis Mushayt, Saudi Arabia, elevation 6500 ft. The ambient temperature is +25°C. What is your density altitude?

301 / 386

Pressure altitude is 27 000 feet, OAT = -35°C, Mach No. = 0.45, W/V = 270/85, Track= 200°(T). What is drift and ground speed?

302 / 386

Given:

True Track = 352°(T)

Variation = 11°W

Deviation = - 5°

Drift = 10°R

What is heading °(C)?

303 / 386

One purpose of a compass calibration is to reduce the difference, if any, between:

304 / 386

The value of magnetic variation on a chart changes with time. This is due to:

305 / 386

At the magnetic equator:

306 / 386

At a specific location, the value of magnetic variation:

307 / 386

You plan to fly a track (course) of 348°(T), Drift is 17°port, Variation is 32°W.Deviation is 4°E. What compass heading should you fly?

308 / 386

Given that the value of ellipticity of the Earth is 1/297 and that the semi-major axis

of the Earth, measured at the axis of the Equator is 6378.4 km, what is the semi- major axis of the Earth measured at the axis of the Poles?

309 / 386

SAT = +35°C. Pressure alt (corrected for barometric error) = 5000 feet. What is true alt?

310 / 386

The circumference of the Earth is approximately?

311 / 386

An aircraft is at latitude 10N and is flying south at 444 km/hour. After 3 hours the latitude is:

312 / 386

An aircraft at latitude 02°20’N tracks 180°(T) for 685 km. What is its latitude at the end of the flight?

313 / 386

What is the shortest distance in kilometres between Cairo (30°17’N 030°10’E) and Durban(29°48’S 030°10’E)?

314 / 386

Required course 045°(T), W/V = 190°(T)/30, FL=55@ISA, Variation = 15°E. CAS =120 knots. What is magnetic heading and G/S?

315 / 386

The maximum difference between geodetic and geocentric latitude occurs at about?

316 / 386

How much is the polar diameter of the Earth different from the equatorial diameter?

317 / 386

An ICAO nautical mile is defined as:

318 / 386

A great circle has a northern vertex of 50N 100W. the southern vertex is:

319 / 386

On a particular direct Mercator wall chart, the 180°W to 180°E parallel of latitude at 53°N is 133 cm long. What is the scale of the chart at 30°S?

320 / 386

The scale of a Mercator chart is 1:3 500 000 in latitude 52N. What is the spacing, in centimetres, between meridians 1° apart?

321 / 386

On a Mercator chart the spacing of meridians 1° apart is 5.42 cm. What is the scale of the chart as a representative fraction in latitude 56N ?

322 / 386

On a Mercator chart the spacing of meridians 1° apart is 2.82 cm. In which latitude will the scale be 1:2 319 000 ?

323 / 386

The scale of a Mercator chart is 1:3 500 000 at 52N. Give the length in inches of a straight line on the chart from A (58N 42E) to B (58N 34E).

324 / 386

A Mercator is to be constructed at a scale of 1:2 237 000 in latitude 44N. What is the required spacing in centimetres between meridians 1° apart ?

325 / 386

The chart length between meridians 1° apart is 3.2 inches. What is the scale of the chart as a representative fraction at 50N ?

326 / 386

On a Mercator chart, the scale at 15°N is 1:1 500 000. What is the scale at 47°S?

327 / 386

On a Mercator chart, the scale at 50°N is 1:4 500 000. What is the scale at the Equator?

328 / 386

On a Mercator chart, the scale at the Equator is 1:3 500 000. What is the scale at

37°S?

329 / 386

At 40N, the scale of Mercator chart is 1:10 000 000. What is the distance in centimetres between the 160E and 160W meridians at 20S?

330 / 386

On a Mercator chart, the chart length between two meridians, 160E and 160W, is 30 cm at 30S. What is the scale of the chart at 30S?

331 / 386

On a Mercator chart, the scale at 54S is 1:2 000 000. What is the scale at 25N?

332 / 386

If the scale of a Mercator chart at 52S is 1:2 000 000, what is the scale at the Equator?

333 / 386

If the scale of a Mercator chart at the Equator is 1:1 000 000, what is the scale at 60N (or S)?

334 / 386

At 60S on a Mercator chart, chart convergence is:

335 / 386

On a Mercator chart, the rhumb line track from Durban (30S 032E) to Perth (30S 116E) is 090°(T). What is the great circle track from Perth to Durban?

336 / 386

If the rhumb line track from Turin (45N 008E) to Khartoum (15N 032E) is 145°(T), what is the direction of the great circle track measured at Turin?

337 / 386

The angle between a straight line on a Mercator chart and the corresponding great circle is:

338 / 386

On a direct Mercator, with the exception of the meridians and the Equator, great circles are represented as:

339 / 386

On a direct Mercator, great circles can be represented as:

340 / 386

On a normal Mercator chart, rhumb lines are represented as:

341 / 386

A direct Mercator graticule is:

342 / 386

A normal Mercator chart is a ________________ projection?

(i) Cylindrical

(ii) Perspective

(iii) Non-perspective

(iv) Conformal

(v) Conical

(vi) Azimuthal

The correct combination of the above statements is:

343 / 386

On a chart, one centimetre represents 3.5 kilometres

a. Give the scale as a representative fraction

b.What is the length in inches on the chart which would represent the distance flown in 4 minutes at a ground speed of 204 kilometres per hour?

344 / 386

On a chart 5 centimetres represents 7 nautical miles

a. b. Give the scale of this chart as a representative fraction

Determine the distance in inches on this chart which would represent the

distance flown by an aircraft in 5 minutes at a groundspeed of 156 knots.

345 / 386

The representative fraction of a chart is given as 1: 1 000 000

What is the chart length of a line representing an Earth distance of 50 kilometres on this chart? give your answer in both centimetres and inches

346 / 386

The representative fraction of a chart is given as 1: 500 000 (Half Mil Chart)

a. how many (1) centimetres and (2) inches would represent 30 kilometres on the ground?

347 / 386

Give the scale, as a representative fraction, of the following charts:-

a. One centimetre represents five kilometres

348 / 386

Your position is 5833N 17400W. You fly exactly 6 NM eastwards. What is your new position?

349 / 386

An aircraft is flying around the Earth eastwards along the 60N parallel of latitude

at a ground speed of 240 knots. At what ground speed would another aircraft

have to fly eastwards along the Equator to fly once round the Earth in the same

journey time?

350 / 386

An aircraft departs a point 0400N 17000W and flies 600 NM South, followed by

600 NM East, then 600 NM North, then 600 NM West. What is its final position?

351 / 386

An aircraft at position 50N 006E travels 300 NM due South, then travels 300 NM

due East, then 300 NM due North and then 300 NM due West. What is the

aircraft’s final position relative to its start point?

352 / 386

An aircraft starts at position 0410S 17822W and heads true north for 2950 NM,

then turns 90 degrees left, and maintains a rhumb line track for 314 kilometres.

What is its final position?

353 / 386

An aircraft leaves J (36°00’S 130°14’E) at 0946 UTC, flying a rhumb line track of 270°

at Flight Level 100, temperature 0°C, Mach No. 0.81, wind component 35 kt tail.

What is the aircraft’s position at 1004 UTC?

354 / 386

An aircraft leaves J (36°00’S 130°14’E) at 0946 UTC, flying a rhumb line track of 270°

at Flight Level 100, temperature 0°C, Mach No. 0.81, wind component 35 kt tail.

What is the aircraft’s position at 1004 UTC?

355 / 386

In which latitude is a difference in longitude of 44°10’ the equivalent of a

departure of 2295 NM?

356 / 386

What is the track and distance measured along the parallel of latitude of 80°S from

176°15’W to 179°45’E?

357 / 386

The following rhumb line tracks and distances are flown; starting from E in latitude

50°N.

E to F 000°(T) 300 NM

F to G 090°(T) 300 NM

G to H 180°(T) 300 NM

What is the rhumb line bearing and distance of H from E?

358 / 386

An aircraft flies for 1000 nm along a rhumb line track of 090°(T) from C at 36°00’N

174°45’E to D. What is the longitude of D?

359 / 386

A flight is to be made along the parallel of latitude from A at 48°00’N 04°00’W to B

at 48°00’N 02°27’E. Calculate the distance.

360 / 386

An aircraft at position 2700N 17000W travels 3000 km on a track of 180°(T), then 3000 km on

a track of 090°(T), then 3000 km on a track of 000°(T), then 3000 km on a track of 270°(T).

What is its final position?

361 / 386

A and B are both in the Southern hemisphere and the convergency of their meridians is 8°. The initial great circle track from A to B is 094°(T).

If the position of B is 23°00’S 20°00’W, what is the position of A?

362 / 386

The initial great circle track from B to A is 245°(T) and the rhumb line track from A

to B is 060°(T).

If the mean latitude between A and B is 53° and the longitude of B is 02°15’E, what

is the longitude of A?

363 / 386

Calculate the convergency between positions A (55°30’N 04°35’W) and

B (64°00’N 22°37’W).

364 / 386

Position X 64°00’S 11°50’W. Position Y 64°00’S 05°10’W.

Give:

a. The convergency between the meridians of X and Y.

b. The approximate initial great circle track from Y to X.

365 / 386

C and D are in the same hemisphere.

The initial great circle track from C to D is 063°(T) and the rhumb line track

from D to C is 240°(T).

i) In which hemisphere are C and D?

ii) What is the approximate initial great circle track from D to C?

366 / 386

 A and B are in the same hemisphere.

The initial great circle track from B to A is 268°(T) and the initial great circle

track from A to B is 092°(T).

i) In which hemisphere are A and B?

367 / 386

In what latitude is the convergency between two meridians on the Earth

equal to twice their convergency in latitude 20°N?

368 / 386

The great circle track from A to B measures 227°(T) at A and 225°(T) at B.

What is the convergency of the meridians through A and B and in which

hemisphere are they?

369 / 386

The rhumb line from position D (30°00’N 179°00’W) to position C is 090°(T).

The initial great circle track from C to D is 287°(T).

What is:

a. The great circle track from D to C?

b. The approximate latitude and longitude of position C ?

370 / 386

The great circle bearing of position B in latitude 30°00’S from position A (30°00’S

165°00’E) is 100°(T).

What is:

a. The longitude of position B ?

371 / 386

The great circle bearing of position B in latitude 30°00’S from position A (30°00’S

165°00’E) is 100°(T).

What is:

a. The great circle track from B to A?

372 / 386

The convergency of the meridians through M and N which are in the Southern

hemisphere is 12°.

If the rhumb line track from M to N is 249°(T), what is the great circle track:

a. from M to N?

373 / 386

The difference between great circle direction and Rhumb Line direction joining two given

points is called

374 / 386

The initial great circle track from C (3600N 01500E) to D (latitude 4200N) is 300°(T) and the

final great circle track at D is 295°(T).

a. What is the longitude of D?

375 / 386

What does symbol 3 represent?

376 / 386

Which of the following would be most useful as a visual checkpoint when

planning a flight?

377 / 386

An aircraft flying VFR using visual navigation crosses two parallel roads at right

angles to the track. For what purpose could that information be used?

378 / 386

Which of the following is the symbol for an exceptionally high (over 1000 feet

AGL) lighted obstruction?

379 / 386

You are flying a VFR route and have become uncertain of your position. Which is

the best course of action?

380 / 386

You are flying an airway with a centre line QDM of 137 °(M) towards VOR/DME ‘A’.

Your RMI reads 141°(M)/DME 90 NM.

a. Are you left or right of centre line?

b. What is your distance off the airway centre line?

381 / 386

On the approach to London Heathrow runway 27, glide slope 3°, you reduce speed

from 150 kt to 120 kt. What change should you make to your ROD to maintain glide

slope?

382 / 386

You are approaching Rota, Spain on runway 28 which has a glide slope of 2.6°. At

what height should you be at 4 miles range?

383 / 386

You are approaching Innsbruck, Austria on a glide slope of 3.5°. What height (QFE)

should you be at 2 miles range?

384 / 386

An aircraft is flying due South. At 1000 hrs, point P bears 267°(T) from the aircraft.

At 1006 hrs, point P bears 275°(T) from the aircraft. If the aircraft has a ground

speed of 120 kt, estimate the range of the aircraft from point P.

385 / 386

Approaching London City airport (glide slope 5.5°), you reduce ground speed from 120 kt to

110 kt. What change should you make to your ROD to maintain the glide slope?

386 / 386

You are flying from Q to R, which is a required track of 125°(T). You find that your

position is 40 NM from R and 2 NM left of the required track. What track must you

fly to arrive overhead R?

Your score is

The average score is 16%

0%