Professione Volare
Domande Navigation
Data:
Nome Allievo:
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169) What is the time required to travel along the parallel of 172) The constant of the cone, on a Lambert chart where the
latitude 60° N between meridians 010° E and 030° W at a convergence angle between longitudes 010°E and 030°W
groundspeed of 480 kt? is 30°, is:
A 5 HR 00 MIN A 0.50
B 2 HR 30 MIN B 0.64
1 HR 15 MIN 0.75
C C
D 1 HR 45 MIN D 0.40
162) (For this question use annex 061-2326A to 061-2326D) 177) What is the final position after the following rhumb line
When it is 0600 Standard Time in Queensland (Australia) tracks and distances have been followed from position
the Standard Time in Hawaii (USA) is: 60°00'N 030°00'W?
South for 3600 NM,
East for 3600 NM,
A 1200
North for 3600 NM,
West for 3600 NM.
B 0200
The final position of the aircraft is:
0600
C
A 59°00'N 090°00'W
D 1000
B 60°00'N 090°00'W
60°00'N 030°00'E
C
175) A line drawn on a chart which joins all points where the
value of magnetic variation is zero is called an:
D 59°00'N 060°00'W
A isotach
170) An aircraft at latitude 10°North flies south at a
B agonic line
groundspeed of 445 km/HR.
What will be its latitude after 3 HR?
aclinic line
C
A 03°50'S
D isogonal
B 02°00'S
174) Given:
12°15'S
C
Airport elevation is 1000 ft.
QNH is 988 hPa.
D 22°00'S
What is the approximate airport pressure altitude?
(Assume 1 hPa = 27 FT)
A 1680 FT 178) (For this question refer to annex 061-12608A)
What feature is shown on the chart at position N5417
W01005?
B 320 FT
A Belmullet aerodrome
680 FT
C
B Carnmore aerodrome
D - 320 FT
Clonbullogue aerodrome
C
173) (For this question refer to annex 061-12618A)
D EAGLE ISLAND LT.H. NDB
Which of the aeronautical chart symbols indicates a
basic, non-specified, navigation aid?
A 3
B 5
6
C
D 2
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168) Given: 164) Given:
Distance 'A' to 'B' 2484 NM TAS = 465 kt,
Groundspeed 'out' 420 kt Track (T) = 007°,
Groundspeed 'back' 500 kt W/V = 300/80kt.
The time from 'A' to the Point of Equal Time (PET) Calculate the HDG (°T) and GS?
between 'A' and 'B' is:
A 357 - 430 kt
A 193 MIN
B 358 - 428 kt
B 163 MIN
001 - 432 kt
C
173 MIN
C
D 000 - 430 kt
D 183 MIN
193) (For this question use annex 061-12593A)
167) An island is observed to be 15° to the left. Given:
The aircraft heading is 120°(M), variation 17°(W). SHA VOR N5243.3 W00853.1
The bearing °(T) from the aircraft to the island is: CON VOR N5354.8 W00849.1
Aircraft position N5320 W00950
Which of the following lists two radials that are
A 302
applicable to the aircraft position?
B 088
A SHA 325°
CON 235°
122
C
B SHA 137°
D 268
CON 046°
SHA 317°
C
CON 226°
166) Which of the following statements concerning earth
magnetism is completely correct?
D SHA 145°
CON 055°
A An isogonal is a line which connects places with the same
magnetic variation; the agonic line is the line of zero
magnetic dip
171) The distance between positions A and B is 180 NM. An
aircraft departs position A and after having travelled 60
B An isogonal is a line which connects places of equal dip; the
NM, its position is pinpointed 4 NM left of the intended
aclinic is the line of zero magnetic dip
track. Assuming no change in wind velocity, what
An isogonal is a line which connects places with the same alteration of heading must be made in order to arrive at
C
magnetic variation; the aclinic connects places with the position B?
same magnetic field strength
A 2° Left
D An isogonal is a line which connects places with the same
magnetic variation; the aclinic is the line of zero magnetic dip
B 4° Right
6° Right
C
165) The rhumb line track between position A (45°00'N,
010°00'W) and position B (48°30'N, 015°00'W) is
D 8° Right
approximately:
A 300
185) (For this question refer to annex 061-12609A)
Which of the following lists all the aeronautical chart
B 345
symbols shown at position N5150.4 W00829.7?
315
C
A VOR: DME: NDB:compulsory reporting point
D 330
B VOR: DME: NDB: ILS
civil airport: VOR: DME: compulsory reporting point
C
D civil airport: VOR: non-compulsory reporting point
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231) A Lambert conformal conic chart has a constant of the 188) Given:
cone of 0.75. M 0.80,
The initial course of a straight line track drawn on this OAT -50°C,
chart from A (40°N 050°W) to B is 043°(T) at A; course at FL 330,
B is 055°(T). GS 490 kt,
What is the longitude of B? VAR 20°W,
Magnetic heading 140°,
Drift is 11° Right.
A 36°W
Calculate the true W/V?
B 38°W
A 025°/45 kt
41°W
C
B 020°/95 kt
D 34°W
025°/47 kt
C
D 200°/95 kt
191) Given:
true track 352°
variation 11° W
deviation is -5° 176) Given:
drift 10°R. Distance A to B is 360 NM.
Calculate the compass heading? Wind component A - B is -15 kt,
Wind component B - A is +15 kt,
TAS is 180 kt.
A 346°
What is the distance from the equal-time-point to B?
B 018°
A 180 NM
025°
C
B 170 NM
D 358°
165 NM
C
D 195 NM
190) An aircraft departs from position A (04°10' S 178°22'W)
and flies northward following the meridian for 2950 NM.
It then flies westward along the parallel of latitude for
382 NM to position B. 186) Given:
The coordinates of position B are? TAS = 155 kt,
Track (T) = 305°,
W/V = 160/18kt.
A 53°20'N 169°22W
Calculate the HDG (°T) and GS?
B 45°00'N 169°22W
A 305 - 169 kt
53°20'N 172°38'E
C
B 309 - 170 kt
D 45°00'N 172°38'E
309 - 141 kt
C
D 301 - 169 kt
189) On a chart, the distance along a meridian between
latitudes 45°N and 46°N is 6 cm. The scale of the chart is
approximately:
161) (For this question refer to annex 061-12604A)
What feature is shown on the chart at position N5211
A 1 : 1 850 000
W00931?
B 1 : 1 000 000
A Punchestown aerodrome
1 : 185 000
C
B KERRY/Farranfore aerodrome
D 1 : 18 500 000
Waterford NDB
C
D Connemara aerodrome
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184) The distance between two waypoints is 200 NM, 179) A flight is to be made from 'A' 49°S 180°E/W to 'B' 58°S,
To calculate compass heading, the pilot used 2°E 180°E/W.
magnetic variation instead of 2°W. The distance in kilometres from 'A' to 'B' is
Assuming that the forecast W/V applied, what will the off approximately:
track distance be at the second waypoint?
A 804
A 21 NM
B 1000
B 14 NM
1222
C
7 NM
C
D 540
D 0 NM
187) Given:
183) (For this question use annex 061-9437A) TAS = 485 kt,
Complete line 1 of the 'FLIGHT NAVIGATION LOG'; True HDG = 226°,
positions 'A' to 'B'. W/V = 110°(T)/95kt.
What is the HDG°(M) and ETA? Calculate the drift angle and GS?
A 282° - 1128 UTC A 9°R - 533 kt
B 282° - 1114 UTC B 7°R - 531 kt
268° - 1128 UTC 9°R - 433 kt
C C
D 268° - 1114 UTC D 8°L - 435 kt
182) An aircraft departing A(N40º 00´ E080º 00´) flies a 137) Given :
constant true track of 270º at a ground speed of 120 kt. ETA to cross a meridian is 2100 UTC
What are the coordinates of the position reached in 6 GS is 441 kt
HR? TAS is 491 kt
At 2010 UTC, ATC requests a speed reduction to cross
the meridian at 2105 UTC.
A N40º 00´ E060º 00´
The reduction to TAS will be approximately:
B N40º 00´ E068º 10´
A 75 kt
N40º 00´ E064º 20´
C
B 60 kt
D N40º 00´ E070º 30´
40 kt
C
D 90 kt
181) On which of the following chart projections is it NOT
possible to represent the north or south poles?
A Transverse Mercator 163) On a Lambert conformal conic chart, with two standard
parallels, the quoted scale is correct:
B Polar stereographic
A along the parallel of origin
Direct Mercator
C
B along the prime meridian
D Lambert's conformal
along the two standard parallels
C
D in the area between the standard parallels
180) Which of the following correctly lists the order of
available selections of the Mode Selector switches of an
inertial reference system (IRS) mode panel?
A OFF - ALIGN - ATT - NAV
B OFF - ALIGN - NAV - ATT
OFF - ON - ALIGN - NAV
C
D OFF - STBY - ALIGN - NAV
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143) The angle between the plane of the ecliptic and the 145) Given:
plane of equator is approximately : Distance 'A' to 'B' 2484 NM
Mean groundspeed 'out' 420 kt
Mean groundspeed 'back' 500 kt
A 27.5°
Safe endurance 08 HR 30 MIN
The distance from 'A' to the Point of Safe Return (PSR)
B 66.5°
'A' is:
23.5°
C
A 1736 NM
D 25.3°
B 1630 NM
1940 NM
C
142) (For this question refer to annex 061-12632A)
Which aeronautical chart symbol indicates a group of
D 1908 NM
lighted obstacles?
A 12
138) The ICAO definition of ETA is the:
B 9
A estimated time of arrival at destination
10
C
B actual time of arrival at a point or fix
D 11
estimated time of arrival at an en-route point or fix
C
141) Given: D estimated time en route
TAS = 200 kt,
Track (T) = 073°,
W/V = 210/20kt.
146) Given:
Calculate the HDG (°T) and GS?
Position A 45°N, ?°E
Position B 45°N, 45°15'E
A 079 - 211 kt
Distance A-B = 280 NM
B is to the East of A
B 075 - 213 kt
Required: longitude of position A?
077 - 210 kt
C
A 49°57'E
D 077 - 214 kt
B 51°51'E
40°33'E
C
140) Given:
An aircraft is on final approach to runway 32R (322°); D 38°39'E
The wind velocity reported by the tower is 350°/20 kt.;
TAS on approach is 95 kt.
In order to maintain the centre line, the aircraft's
136) At the magnetic equator, when accelerating after take off
heading (°M) should be :
on heading West, a direct reading compass :
A 328°
A underreads the heading
B 322°
B indicates a turn to the south
316°
C
indicates the correct heading
C
D 326°
D overreads the heading
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135) Given: GS = 480 kt. 131) Given:
Distance from A to B = 5360 NM. Magnetic track = 075°,
What is the time from A to B? HDG = 066°(M),
VAR = 11°E,
TAS = 275 kt
A 11 HR 15 MIN
Aircraft flies 48 NM in 10 MIN.
Calculate the true W/V °?
B 11 HR 10 MIN
A 340°/45 kt
11 HR 06 MIN
C
B 320°/50 kt
D 11 HR 07 MIN
210°/15 kt
C
134) Given:
D 180°/45 kt
True track 180°
Drift 8°R
Compass heading 195°
Deviation -2° 139) (For this question refer to annex 061-12624A)
Calculate the variation? Which aeronautical chart symbol indicates an
uncontrolled route?
A 21°W
A 3
B 25°W
B 4
5°W
C
5
C
D 9°W
D 2
133) In which of the following situations is the FMC present
position of a B737-400 Electronic Flight Instrument 153) With reference to inertial navigation systems, a TAS
System likely to be least accurate? input is:
A On final approach A required for Polar navigation
B Just after take-off B required for rhumb line navigation
At top of climb required to provide a W/V read out
C C
D At top of descent D not required
132) (For this question refer to annex 061-12626A) 160) (For this question use annex 061-12564A)
Which aeronautical chart symbol indicates a non- What is the average track (°M) and distance between
compulsory reporting point? WTD NDB (N5211.3 W00705.0) and KER NDB (N5210.9
W00931.5)?
A 15
A 098° - 90 NM
B 6
B 278° - 90 NM
7
C
090° - 91 NM
C
D 8
D 270° - 89 NM
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159) Given: 144) As the INS position of the departure aerodrome,
TAS = 250 kt, coordinates 35°32.7'N 139°46.3'W are input instead of
HDG (T) = 029°, 35°32.7'N 139°46.3'E. When the aircraft subsequently
W/V = 035/45kt. passes point 52°N 180°W, the longitude value shown on
Calculate the drift and GS? the INS will be:
A 1L - 205 kt A 080° 27.4'W
B 1R - 205 kt B 099° 32.6'W
1L - 265 kt 099° 32.6'E
C C
D 1R - 295 kt D 080° 27.4'E
158) Complete the following statement regarding magnetic 154) Given:
variation. TAS = 170 kt,
The charted values of magnetic variation on earth HDG(T) = 100°,
normally change annually due to: W/V = 350/30kt.
Calculate the Track (°T) and GS?
A magnetic pole movement causing numerical values at all
locations to increase or decrease A 091 - 183 kt
B magnetic pole movement causing numerical values at all
B 103 - 178 kt
locations to increase.
098 - 178 kt
C
a reducing field strength causing numerical values at all
C
locations to decrease.
D 109 - 182 kt
D an increasing field strength causing numerical values at all
locations to increase.
194) When decelerating on a westerly heading in the
Northern hemisphere, the compass card of a direct
157) Given: reading magnetic compass will turn :
Runway direction 230°(T),
Surface W/V 280°(T)/40 kt.
A anti-clockwise giving an apparent turn towards the north
Calculate the effective cross-wind component?
B clockwise giving an apparent turn toward the south
A 26 kt
anti-clockwise giving an apparent turn towards the south
C
B 31 kt
D clockwise giving an apparent turn towards the north
36 kt
C
D 21 kt
152) (For this question refer to annex 061-12602A)
Given:
CON VOR/DME (N5354.8 W00849.1)
156) An aircraft is planned to fly from position 'A' to position Castlebar aerodrome (N5351 W00917)
'B',distance What is the CON radial and DME distance when
320 NM, at an average GS of 180 kt. It departs 'A' at 1200 overhead Castlebar aerodrome?
UTC.
After flying 70 NM along track from 'A', the aircraft is 3
A 086° - 18 NM
MIN ahead of planned time.
Using the actual GS experienced, what is the revised
B 265° - 17 NM
ETA at 'B'?
077° - 18 NM
C
A 1333 UTC
D 257° - 17 NM
B 1401 UTC
1347 UTC
C
D 1340 UTC
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151) What is the source of magnetic variation information in 147) (For this question use annex 061-12561A)
a Flight Management System (FMS)? What is the radial and DME distance from BEL VOR/DME
(N5439.7 W00613.8) to position N5410 W00710?
A Magnetic variation information is stored in each IRS
memory; it is applied to the true heading calculated by the A 333° - 36 NM
respective IRS
B 236° - 44 NM
B The main directional gyro which is coupled to the magnetic
sensor (flux valve) positioned in the wingtip
223° - 36 NM
C
The FMS calculates MH and MT from the FMC position
C
D 320° - 44 NM
D Magnetic variation is calculated by each IRS based on the
respective IRS position and the aircraft magnetic heading
155) An aircraft is maintaining a 5.2% gradient is at 7 NM from
the runway, on a flat terrain; its height is approximately:
150) Given:
A 3640 FT
True HDG = 035°,
TAS = 245 kt,
Track (T) = 046°, B 2210 FT
GS = 220 kt.
Calculate the W/V?
680 FT
C
A 340/45kt
D 1890 FT
B 340/50kt
207) An aircraft was over 'Q' at 1320 hours flying direct to 'R'.
335/45kt
C
Given:
Distance 'Q' to 'R' 3016 NM
D 335/55kt
True airspeed 480 kt
Mean wind component 'out' -90 kt
Mean wind component 'back' +75 kt
Safe endurance 10:00 HR
149) A ground feature appears 30° to the left of the centre line
The distance from 'Q' to the Point of Safe Return (PSR)
of the CRT of an airborne weather radar. If the heading
'Q' is:
of the aircraft is 355° (M) and the magnetic variation is
15° East, the true bearing of the aircraft from the feature
A 2370 NM
is:
A 310° B 1310 NM
B 130° 1510 NM
C
160° D 2290 NM
C
D 220°
200) (For this question use annex 061-12555A)
What is the radial and DME distance from SHA
VOR/DME (N5243.3 W00853.1) to position N5220
148) The constant of cone of a Lambert conformal conic
W00810?
chart is quoted as 0.3955.
At what latitude on the chart is earth convergency
A 129° - 46 NM
correctly represented?
A 66°42' B 132° - 36 NM
B 68°25' 212° - 26 NM
C
21°35' D 139° - 35 NM
C
D 23°18'
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213) Route 'A' (44°N 026°E) to 'B' (46°N 024°E) forms an angle 215) (For this question use annex 061-12579A)
of 35° with longitude 026°E. Average magnetic variation Given:
between 'A' and 'B' is 3°E. SHA VOR (N5243.3 W00853.1) radial 223°,
What is the average magnetic course from 'A' to 'B'? CRK VOR (N5150.4 W00829.7) radial 322°.
What is the aircraft position?
A 328°
A N5220 W00920
B 032°
B N5230 W00910
038°
C
N5210 W00910
C
D 322°
D N5210 W00930
212) Given: Waypoint 1. 60°S 030°W
Waypoint 2. 60°S 020°W 208) (For this question use annex 061-12592A)
What will be the approximate latitude shown on the Given:
display unit of an inertial navigation system at longitude SHA VOR N5243.3 W00853.1
025°W? CON VOR N5354.8 W00849.1
Aircraft position N5330 W00800
Which of the following lists two radials that are
A 060°00'S
applicable to the aircraft position?
B 060°06'S
A SHA 042°
CON 138°
060°11'S
C
B SHA 213°
D 059°49'S
CON 310°
SHA 033°
C
CON 130°
211) An aircraft at FL290 is required to commence descent
when 50 NM from a VOR and to cross that VOR at FL80.
D SHA 221°
Mean GS during descent is 271kt.
CON 318°
What is the minimum rate of descent required?
A 1900 FT/MIN
216) (For this question refer to annex 061-12617A)
Which of the aeronautical chart symbols indicates an
B 2000 FT/MIN
NDB?
1700 FT/MIN
C
A 4
D 1800 FT/MIN
B 6
2
C
210) Given:
Maximum allowable tailwind component for landing 10
D 3
kt.
Planned runway 05 (047° magnetic).
The direction of the surface wind reported by ATIS 210°.
Variation is 17°E. 206) Given: GS = 135 kt.
Calculate the maximum allowable windspeed that can Distance from A to B = 433 NM.
be accepted without exceeding the tailwind limit? What is the time from A to B?
A 8 kt A 3 HR 12 MIN
B 15 kt B 3 HR 25 MIN
11 kt 3 HR 19 MIN
C C
D 18 kt D 3 HR 20 MIN
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205) (For this question use annex 061-12568A) 209) When accelerating on a westerly heading in the northern
What is the average track (°M) and distance between hemisphere, the compass card of a direct reading
KER NDB (N5210.9 W00931.5) and CRN NDB (N5318.1 magnetic compass will turn:
W00856.5)?
A anti-clockwise giving an apparent turn towards the north
A 197° - 71 NM
B anti-clockwise giving an apparent turn towards the south
B 205° - 71 NM
clockwise giving an apparent turn towards the north
C
017° - 70 NM
C
D clockwise giving an apparent turn towards the south
D 025° - 70 NM
223) Given: GS = 435 kt.
204) The rhumb-line distance between points A (60°00'N Distance from A to B = 1920 NM.
002°30'E) and B (60°00'N 007°30'W) is: What is the time from A to B?
A 150 NM A 4 HR 10 MIN
B 300 NM B 4 HR 25 MIN
450 NM 3 HR 25 MIN
C C
D 600 NM D 3 HR 26 MIN
203) The north and south magnetic poles are the only 1) Given:
positions on the earth's surface where: true track 070°
variation 30°W
deviation +1°
A a freely suspended compass needle will stand vertical
drift 10°R
Calculate the compass heading?
B isogonals converge
A 100°
a freely suspended compass needle will stand horizontal
C
B 101°
D the value of magnetic variation equals 90°
089°
C
202) The resultant of the first integration from the
D 091°
north/south accelerometer of an inertial navigation
system (INS) in the NAV MODE is:
A velocity along the local meridian 229) Given:
Distance 'Q' to 'R' 1760 NM
Groundspeed 'out' 435 kt
B groundspeed
Groundspeed 'back' 385 kt
The time from 'Q' to the Point of Equal Time (PET)
change latitude
C
between 'Q' and 'R' is:
D latitude
A 102 MIN
B 114 MIN
192) (For this question use annex 061-12552A)
What is the radial and DME distance from CRK
110 MIN
C
VOR/DME (N5150.4 W00829.7) to position N5140
W00730?
D 106 MIN
A 293° - 39 NM
B 106° - 38 NM
113° - 38 NM
C
D 104° - 76 NM
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228) The sensors of an INS measure: 199) The reported surface wind from the Control Tower is
240°/35 kt. Runway 30 (300°).
What is the cross-wind component?
A precession
A 21 kt
B acceleration
B 30 kt
velocity
C
24 kt
C
D the horizontal component of the earth's rotation
D 27 kt
227) (For this question refer to annex 061-12614A)
Which of the aeronautical chart symbols indicates a
222) When is the magnetic compass most effective?
VOR/DME?
A 2 A In the region of the magnetic South Pole.
B 6 B In the region of the magnetic North Pole.
7 On the geographic equator
C C
D 1 D About midway between the magnetic poles
226) Given: 221) On a Direct Mercator, rhumb lines are:
TAS = 485 kt,
OAT = ISA +10°C,
A curves convex to the equator
FL 410.
Calculate the Mach Number?
B straight lines
A 0.90
curves concave to the equator
C
B 0.85
D ellipses
0.87
C
D 0.825
220) (For this question use annex 061-12584A)
Given:
SHA VOR/DME (N5243.3 W00853.1) radial 120°/35 NM.
What is the aircraft position?
214) Parallels of latitude on a Direct Mercator chart are :
A N5225 W00805
A straight lines converging above the pole
B N5250 W00950
B parallel straight lines unequally spaced
N5230 W00800
C
parallel straight lines equally spaced
C
D N5300 W00945
D arcs of concentric circles equally spaced
219) Given:
224) (For this question use annex 061-12587A) True course 300°
Given: drift 8°R
SHA VOR/DME (N5243.3 W00853.1) radial 025°/49 NM. variation 10°W
What is the aircraft position? deviation -4°
Calculate the compass heading?
A N5155 W00915
A 322°
B N5200 W0925
B 294°
N5330 W00830
C
278°
C
D N5328 W00820
D 306°
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218) The convergence factor of a Lambert conformal conic 201) (For this question use annex 061-12583A)
chart is quoted as 0.78535. Given:
At what latitude on the chart is earth convergency SHA VOR (N5243.3 W00853.1) radial 143°,
correctly represented? CRK VOR (N5150.4 W00829.7) radial 050°.
What is the aircraft position?
A 52°05'
A N5155 W00810
B 80°39'
B N5205 W00805
38°15'
C
N5200 W00800
C
D 51°45'
D N5210 W00800
217) The value of magnetic variation:
455) (For this question refer to annex 061-12600A)
Given:
A varies between a maximum of 45° East and 45° West
SHA VOR/DME (N5243.3 W00853.1)
Birr aerodrome (N5304 W00754)
B cannot exceed 90° What is the SHA radial and DME distance when
overhead Birr aerodrome?
has a maximum of 180°
C
A 240° - 41 NM
D must be 0° at the magnetic equator
B 068° - 41 NM
248° - 42 NM
C
225) Which of the following statements concerning the
position indicated on the Inertial Reference System (IRS)
D 060° - 42 Nm
display is correct?
A The positions from the two IRSs are compared to obtain a
'best position' which is displayed on the IRS
454) Given:
Pressure Altitude 29000 FT,
B It is not updated once the IRS mode is set to NAV
OAT -55°C.
Calculate the Density Altitude?
It is constantly updated from information obtained by the
C
FMC
A 27500 FT
D It is updated when 'go-around' is selected on take-off
B 31000 FT
33500 FT
C
449) Given :
A is N55° 000°
D 26000 FT
B is N54° E010°
The average true course of the great circle is 100°.
The true course of the rhumbline at point A is:
453) Given:
Direct Mercator chart with a scale of 1 : 200 000 at
A 107°
equator;
Chart length from 'A' to 'B', in the vicinity of the equator,
B 100°
11 cm.
What is the approximate distance from 'A' to 'B'?
096°
C
A 21 NM
D 104°
B 22 NM
14 NM
C
D 12 NM
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452) (For this question use annex 061-12565A) 448) (For this question refer to annex 061-12637A)
What is the average track (°M) and distance between Which aeronautical chart symbol indicates an
CRK VOR (N5150.4 W00829.7) and CRN NDB (N5318.1 aeronautical ground light?
W00856.5)?
A 15
A 349° - 90 NM
B 16
B 177° - 92 NM
10
C
357° - 89 NM
C
D 14
D 169° - 91 NM
447) (For this question use annex 061-9440A)
457) On a Direct Mercator chart, meridians are: Complete line 4 of the 'FLIGHT NAVIGATION LOG',
positions 'G' to 'H'.
What is the HDG°(M) and ETA?
A inclined, equally spaced, straight lines that meet at the
nearer pole
A HDG 354° - ETA 1326 UTC
B parallel, unequally spaced, vertical straight lines
B HDG 034° - ETA 1336 UTC
inclined, unequally spaced, curved lines that meet at the
C
HDG 344° - ETA 1303 UTC
C
nearer pole
D HDG 344° - ETA 1336 UTC
D parallel, equally spaced, vertical straight lines
446) Given:
450) Given:
Distance 'A' to 'B' 3623 NM
Compass Heading 090°,
Groundspeed 'out' 370 kt
Deviation 2°W,
Groundspeed 'back' 300 kt
Variation 12°E,
The time from 'A' to the Point of Equal Time (PET)
TAS 160 kt.
between 'A' and 'B' is:
Whilst maintaining a radial 070° from a VOR station,
the aircraft flies a ground distance of 14 NM in 6 MIN.
A 238 MIN
What is the W/V °(T)?
A 160°/50 kt
B 263 MIN
B 340°/25 kt
288 MIN
C
340°/98 kt
C D 323 MIN
D 155°/25 kt
445) (For this question refer to annex 061-12606A)
What feature is shown on the chart at position N5311
W00637?
458) A Rhumb line is :
A Clonbullogue aerodrome
A any straight line on a Lambert projection
B Punchestown aerodrome
B a line convex to the nearest pole on a Mercator projection
Connemara aerodrome
C
a line on the surface of the earth cutting all meridians at the
C
same angle
D KERRY/Farranfore aerodrome
D the shortest distance between two points on a Polyconic
projection
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444) (For this question use annex 061-12595A) 198) Given: GS = 345 kt.
Given: Distance from A to B = 3560 NM.
SHA VOR (N5243.3 W00853.1) DME 41 NM, What is the time from A to B?
CRK VOR (N5150.4 W00829.7) DME 30 NM,
Aircraft heading 270°(M),
A 11 HR 02 MIN
Both DME distances decreasing.
What is the aircraft position?
B 10 HR 19 MIN
A N5205 W00915
10 HR 05 MIN
C
B N5215 W00915
D 11 HR 00 MIN
N5225 W00810
C
197) For a landing on runway 23 (227° magnetic) surface
D N5215 W00805
W/V reported by the ATIS is 180/30kt.
VAR is 13°E.
Calculate the cross wind component?
195) (For this question use annex 061-12557A)
What is the radial and DME distance from CON
A 15 kt
VOR/DME (N5354.8 W00849.1) to position N5430
W00900?
B 20 kt
A 358° - 36 NM
22 kt
C
B 214° - 26 NM
D 26 kt
049° - 45 NM
C
196) (For this question use annex 061-12403A)
D 169° - 35 NM
An aircraft on radial 315° at a range of 150 NM from
MYGGENES NDB (N6206 W00732) is at position:
451) A ground feature was observed on a relative bearing of
A N6345 W01125
315° and 3 MIN later on a relative bearing of 270°.
The W/V is calm; aircraft GS 180 kt.
B N6040 W00320
What is the minimum distance between the aircraft and
the ground feature?
N6320 W01205
C
A 6 NM
D N6020 W00405
B 9 NM
469) Fuel flow per HR is 22 US-GAL, total fuel on board is 83
12 NM
C
IMP GAL.
What is the endurance?
D 3 NM
A 2 HR 15 MIN
465) Given:
B 4 HR 32 MIN
True heading = 310°
TAS = 200 kt
3 HR 12 MIN
C
GS = 176 kt
Drift angle 7° right.
D 3 HR 53 MIN
Calculate the W/V?
A 180° / 33 kt
468) A ground feature was observed on a relative bearing of
B 270° / 33 kt
325° and five minutes later on a relative bearing of 280°.
The aircraft heading was 165°(M), variation 25°W, drift
10°Right and GS 360 kt. When the relative bearing was
360° / 33 kt
C
280°, the distance and true bearing of the aircraft from
the feature was:
D 090° / 33 kt
A 40 NM and 290°
B 30 NM and 060°
30 NM and 240°
C
D 40 NM and 110°
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456) (For this question use annex 061-9441A) 462) In northern hemisphere, during an acceleration in an
Complete line 5 of the 'FLIGHT NAVIGATION LOG', easterly direction, the magnetic compass will indicate:
positions 'J' to 'K'.
What is the HDG°(M) and ETA?
A a decrease in heading
A HDG 337° - ETA 1422 UTC
B an increase in heading
B HDG 320° - ETA 1412 UTC
an apparent turn to the South
C
HDG 337° - ETA 1322 UTC
C
D a heading of East
D HDG 320° - ETA 1432 UTC
461) (For this question use annex 061-12574A)
What is the average track (°T) and distance between
466) An aircraft at FL370, M0.86, OAT -44°C, headwind WTD NDB (N5211.3 W00705.0) and SLG NDB (N5416.7
component 110 kt, is required to reduce speed in order W00836.0)?
to cross a reporting point 5 MIN later than planned.
If the speed reduction were to be made 420 NM from the
A 156° - 136 NM
reporting point, what Mach Number is required?
B 164° - 138 NM
A M0.79
336° - 137 NM
C
B M0.81
D 344° - 139 NM
M0.73
C
D M0.75
460) Which of the following statements concerning the
operation of an Inertial Navigation System (INS)/Inertial
Reference System (IRS) is correct?
128) Isogrives are lines that connect positions that have:
A NAV mode must be selected on the runway just prior to
take-off
A the same horizontal magnetic field strength
B NAV mode must be selected prior to the loading of
B the same variation
passengers and/or freight
NAV mode must be selected when the alignment procedure
C
O° magnetic dip
C
is commenced
D the same grivation
D NAV mode must be selected prior to movement of the
aircraft off the gate
464) Given: GS = 95 kt.
Distance from A to B = 480 NM.
459) (For this question use annex 061-12589A)
What is the time from A to B?
Given:
SHA VOR N5243.3 W00853.1
A 5 HR 03 MIN
CRK VOR N5150.4 W00829.7
Aircraft position N5220 W00910
B 4 HR 59 MIN Which of the following lists two radials that are
applicable to the aircraft position?
5 HR 00 MIN
C
A SHA 212°
CRK 328°
D 5 HR 08 MIN
B SHA 025°
CRK 141°
463) (For this question use annex 061-12582A)
SHA 205°
Given: C
SHA VOR (N5243.3 W00853.1) radial 129°, CRK 321°
CRK VOR (N5150.4 W00829.7) radial 047°.
D SHA 033°
What is the aircraft position?
CRK 149°
A N5210 W00750
B N5205 W00755
N5220 W00750
C
D N5215 W00755
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467) An aircraft at FL370 is required to commence descent at 45) Given:
120 NM from a VOR and to cross the facility at FL130. If True HDG = 133°,
the mean GS for the descent is 288 kt, the minimum rate TAS = 225 kt,
of descent required is: Track (T) = 144°,
GS = 206 kt.
Calculate the W/V?
A 920 FT/MIN
A 075/50kt
B 960 FT/MIN
B 075/45kt
860 FT/MIN
C
070/40kt
C
D 890 FT/MIN
D 070/45kt
40) (For this question refer to annex 061-12607A)
What feature is shown on the chart at position N5351
W00917? 44) Which one of the following is an advantage of a remote
reading compass as compared with a standby compass?
A Brittas Bay aerodrome
A It senses the magnetic meridian instead of seeking it,
increasing compass sensitivity
B Castlebar aerodrome
B It is lighter than a direct reading compass because it
Connaught aerodrome
C
employs, apart from the detector unit, existing aircraft
equipment
D Connemara aerodrome
It eliminates the effect of turning and acceleration errors by
C
pendulously suspending the detector unit
33) Given:
D It is more reliable because it is operated electrically and
Distance 'A' to 'B' is 100 NM,
power is always available from sources within the aircraft
Fix obtained 40 NM along and 6 NM to the left of course.
What heading alteration must be made to reach 'B'?
43) For a given track the:
A 9° Right
Wind component = +45 kt
Drift angle = 15° left
B 6° Right
TAS = 240 kt
What is the wind component on the reverse track?
18° Right
C
A -55 kt
D 15° Right
B -45 kt
46) The direct reading magnetic compass is made aperiodic
C -35 kt
(dead beat) by:
D -65 kt
A using the lowest acceptable viscosity compass liquid
B using long magnets
48) An island appears 30° to the left of the centre line on an
airborne weather radar display. What is the true bearing
pendulous suspension of the magnetic assembly
C
of the aircraft from the island if at the time of
observation the aircraft was on a magnetic heading (MH)
D keeping the magnetic assembly mass close to the compass
of 020° with the magnetic variation (VAR) 25°W?
point and by using damping wires
A 145°
B 195°
205°
C
D 325°
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41) The two standard parallels of a conical Lambert 37) Which of the following statements concerning the loss
projection are at N10°40'N and N41°20'. of alignment by an Inertial Reference System (IRS) in
The cone constant of this chart is approximatively : flight is correct?
A 0.66 A The IRS has to be coupled to the remaining serviceable
system and a realignment carried out in flight
B 0.18
B The mode selector has to be rotated to ATT then back
through ALIGN to NAV in order to obtain an in-flight
0.44
C
realignment
D 0.90
It is not usable in any mode and must be shut down for the
C
rest of the flight
D The navigation mode, including present position and ground
49) (For this question use annex 061-1818A)
speed outputs, is inoperative for the remainder of the flight
Assume a North polar stereographic chart whose grid is
aligned with the Greenwich meridian.
An aircraft flies from the geographic North pole for a
distance 36) The platform of an inertial navigation system (INS) is
of 480 NM along the 110°E meridian, then follows a grid maintained at right angles to the local vertical by
track applying corrections for the effects of:
of 154° for a distance of 300 NM.
Its position is now approximately: A aircraft manoeuvres, earth rotation, transport wander and
coriolis
A 70°15'N 080°E
B gyroscopic inertia, earth rotation and real drift
B 80°00'N 080°E
vertical velocities, earth precession, centrifugal forces and
C
transport drift
78°45'N 087°E
C
D movement in the yawing plane, secondary precession and
D 79°15'N 074°E
pendulous oscillation
39) Given: GS = 105 kt.
35) Assuming zero wind, what distance will be covered by
Distance from A to B = 103 NM.
an aircraft descending 15000 FT with a TAS of 320 kt and
What is the time from A to B?
maintaining a rate of descent of 3000 FT/MIN?
A 00 HR 57 MIN
A 38.4 NM
B 00 HR 58 MIN
B 16.0 NM
01 HR 01 MIN
C
26.7 NM
C
D 00 HR 59 MIN
D 19.2 NM
38) Given:
130) The purpose of compass check swing is to:
TAS = 235 kt,
HDG (T) = 076°
A measure the angle between Magnetic North and Compass
W/V = 040/40kt.
North
Calculate the drift angle and GS?
B cancel out the vertical component of the earth's magnetic
A 5R - 207 kt
field
B 7R - 204 kt
cancel out the horizontal component of the earth's magnetic
C
field
7L - 269 kt
C
D cancel out the effects of the magnetic fields found on board
D 5L - 255 kt the aeroplane
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42) During a low level flight 2 parallel roads that are crossed 60) Given:
at right angles by an aircraft. The time between these True HDG = 145°,
roads can be used to check the aircraft: TAS = 240 kt,
Track (T) = 150°,
GS = 210 kt.
A position
Calculate the W/V?
B track
A 295/35kt
drift
C
B 115/35kt
D groundspeed
360/35kt
C
D 180/35kt
56) (For this question refer to annex 061-12625A)
Which aeronautical chart symbol indicates the boundary
of advisory airspace?
59) (For this question use annex 061-12554A)
What is the radial and DME distance from SHA
A 5
VOR/DME (N5243.3 W00853.1) to position N5310
W00830?
B 2
A 070° - 58 NM
3
C
B 207° - 31 NM
D 4
019° - 31 NM
C
63) (For this question refer to annex 061-12619A)
D 035° - 30 NM
Which of the aeronautical chart symbols indicates a
TACAN?
A 2 47) (For this question use annex 061-12560A)
What is the radial and DME distance from CON
VOR/DME (N5354.8 W00849.1) to position N5330
B 6
W00930?
7
C
A 165° - 27 NM
D 1
B 335° - 43 NM
025° - 38 NM
C
62) Given:
TAS = 227 kt,
D 233° - 35 NM
Track (T) = 316°,
W/V = 205/15kt.
Calculate the HDG (°T) and GS?
57) One of the errors inherent in a ring laser gyroscope
occurs at low input rotation rates tending towards zero
A 313 - 235 kt
when a phenomenon known as 'lock-in' is experienced.
What is the name of the technique, effected by means of
B 310 - 233 kt
a piezo-electric motor, that is used to correct this error?
312 - 232 kt
C
A dither
D 311 - 230 kt
B cavity rotation
zero drop
C
61) What is the chart distance between longitudes 179°E
and 175°W on a direct Mercator chart with a scale of 1 :
D beam lock
5 000 000 at the equator?
A 106 mm
B 167 mm
72 mm
C
D 133 mm
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32) Double integration of the output from the east/west 52) (For this question refer to annex 061-12603A)
accelerometer of an inertial navigation system (INS) in Given:
the NAV MODE give: CON VOR/DME (N5354.8 W00849.1)
Abbey Shrule aerodrome (N5335 W00739)
What is the CON radial and DME distance when
A vehicle longitude
overhead Abbey Shrule aerodrome?
B distance north/south
A 296° - 46 NM
velocity east/west
C
B 304° - 47 NM
D distance east/west
124° - 46 NM
C
D 116° - 47 NM
55) (For this question use annex 061-9439A)
Complete line 3 of the 'FLIGHT NAVIGATION LOG',
positions 'E' to 'F'.
What is the HDG°(M) and ETA? 51) An Oblique Mercator projection is used specifically to
produce:
A HDG 106° - ETA 1215 UTC
A charts of the great circle route between two points
B HDG 115° - ETA 1145 UTC
B radio navigational charts in equatorial regions
HDG 105° - ETA 1205 UTC
C
topographical maps of large east/ west extent
C
D HDG 095° - ETA 1155 UTC
D plotting charts in equatorial regions
54) Which one of the following, concerning great circles on
a Direct Mercator chart, is correct? 50) (For this question use annex 061-1829A and the data for
1300 UTC)
1300 UTC DR position 37°30'N 021°30'W alter heading
A They are all curves concave to the equator
PORT SANTO NDB (33°03'N 016°23'W)
TAS 450 kt,
B They approximate to straight lines between the standard
Forecast W/V 360°/30kt.
parallels
Calculate the ETA at PORT SANTO NDB?
They are all curves convex to the equator
C
A 1354
D With the exception of meridians and the equator, they are
B 1348
curves concave to the equator
1344
C
53) Given the following:
D 1341
Magnetic heading: 060°
Magnetic variation: 8°W
Drift angle: 4° right
What is the true track?
58) Given :
True altitude 9000 FT,
A 072°
OAT -32°C,
CAS 200 kt.
B 056°
What is the TAS?
064°
C A 210 kt
D 048° B 220 kt
215 kt
C
D 200 kt
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8) (For this question use annex 061-12597A) 12) (For this question use annex 061-12566A)
Given: What is the average track (°M) and distance between
CRN VOR (N5318.1 W00856.5) DME 34 NM, CRN NDB (N5318.1 W00856.5) and WTD NDB (N5211.3
SHA VOR (N5243.3 W00853.1) DME 26 NM, W00705.0)?
Aircraft heading 090°(M),
Both DME distances increasing.
A 322° - 95 NM
What is the aircraft position?
B 142° - 95 NM
A N5250 W0030
315° - 94 NM
C
B N5305 W00930
D 135° - 96 NM
N5310 W00820
C
D N5255 W00815
11) The angle between Magnetic North and Compass North
is called:
34) A course of 120°(T) is drawn between 'X' (61°30'N) and
A magnetic variation
'Y' (58°30'N) on a Lambert Conformal conic chart with a
scale of 1 : 1 000 000 at 60°N.
B alignment error
The chart distance between 'X' and 'Y' is:
compass deviation
C
A 33.4 cm
D compass error
B 38.5 cm
36.0 cm
C
16) Which of the following statements is correct concerning
the effect of turning errors on a direct reading compass?
D 66.7 cm
A Turning errors are greatest on east/west headings, and are
least at high latitudes
14) Given:
True HDG = 233°, B Turning errors are greatest on north/south headings, and
TAS = 480 kt, are least at high latitudes
Track (T) = 240°,
GS = 523 kt. Turning errors are greatest on east/west headings, and are
C
Calculate the W/V? greatest at high latitudes
D Turning errors are greatest on north/south headings, and
A 110/75kt
are greatest at high latitudes
B 115/70kt
9) An aircraft was over 'Q' at 1320 hours flying direct to 'R'.
110/80kt
C
Given:
Distance 'Q' to 'R' 3016 NM
D 105/75kt
True airspeed 480 kt
Mean wind component 'out' -90 kt
Mean wind component 'back' +75 kt
13) (For this question use annex 061-12576A) The ETA for reaching the Point of Equal Time (PET)
What is the average track (°T) and distance between BAL between 'Q' and 'R' is:
VOR (N5318.0 W00626.9) and CRN NDB (N5318.1
W00856.5)? A 1756
A 272° - 89 NM
B 1820
B 270° - 90 NM
1742
C
278° - 89 NM
C
D 1752
D 268° - 91 NM
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17) Given: 4) On a Direct Mercator chart, a rhumb line appears as a:
Distance 'Q' to 'R' 1760 NM
Groundspeed 'out' 435 kt
A straight line
Groundspeed 'back' 385 kt
Safe endurance 9 HR
The distance from 'Q' to the Point of Safe Return (PSR) B small circle concave to the nearer pole
between 'Q' and 'R' is:
spiral curve
C
A 1313 NM
D curve convex to the nearer pole
B 1467 NM
1642 NM
C
3) (For this question use annex 061-12567A)
What is the average track (°M) and distance between
D 1838 NM
WTD NDB (N5211.3 W00705.0) and BAL VOR (N5318.0
W00626.9)?
A 026° - 71 NM
7) Given:
TAS = 95 kt,
HDG (T) = 075°, B 018° - 153 NM
W/V = 310/20kt.
Calculate the drift and GS?
206° - 71 NM
C
A 8R - 104 kt
D 198° - 72 NM
B 9R - 108 kt
2) On a Transverse Mercator chart, scale is exactly correct
10L - 104 kt
C
along the:
D 9L - 105 kt
A datum meridian and meridian perpendicular to it
B prime meridian and the equator
6) Which of the following statement is correct concerning
gyro-compassing of an inertial navigation system (INS)?
meridian of tangency
C
A Gyro-compassing of an INS is possible in flight because it
D Equator, parallel of origin and prime vertical
cannot differentiate between movement induced and
misalignment induced accelerations.
B Gyro-compassing of an INS is not possible in flight 10) (For this question refer to annex 061-12631A)
because it can differentiate between movement induced and Which aeronautical chart symbol indicates a group of
misalignment induced accelerations. unlighted obstacles?
Gyro-compassing of an INS is not possible in flight because
C A 11
it cannot differentiate between movement induced and
misalignment induced accelerations.
B 12
D Gyro-compassing of an INS is possible in flight because it
13
C
can differentiate between movement induced and
misalignment induced accelerations.
D 9
5) Given:
TAS = 140 kt,
24) (For this question refer to annex 061-12613A)
True HDG = 302°,
Which of the following lists all the aeronautical chart
W/V = 045°(T)/45kt
symbols shown at position N5211 W00705?
Calculate the drift angle and GS?
A NDB: ILS
A 9°L - 146 kt
B civil airport: NDB
B 18°R - 146 kt
VOR: NDB
C
16°L - 156 kt
C
D civil airport: ILS
D 9°R - 143 kt
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31) Given: 27) (For this question use annex 061-12575A)
course required = 085° (T), What is the average track (°T) and distance between
Forecast W/V 030/100kt, SHA VOR (N5243.3 W00853.1) and CON VOR (N5354.8
TAS = 470 kt, W00849.1)?
Distance = 265 NM.
Calculate the true HDG and flight time?
A 002° - 72 NM
A 096°, 29 MIN
B 010° - 71 NM
B 095°, 31 MIN
358° - 72 NM
C
075°, 39 MIN
C
D 006° - 71 NM
D 076°, 34 MIN
15) Where and when are the IRS positions updated?
30) (For this question use annex 061-12558A)
A Only on the ground during the alignment procedure
What is the radial and DME distance from CON
VOR/DME (N5354.8 W00849.1) to position N5400
W00800? B During flight IRS positions are automatically updated by the
FMC
A 260° - 30 NM
IRS positions are updated by pressing the 'Take-off/ Go-
C
around' button at the start of the take-off roll
B 088° - 29 NM
D Updating is normally carried out by the crew when over-
320° - 8 NM
C
flying a known position (VOR station or NDB)
D 094° - 64 NM
25) (For this question use annex 061-12594A)
Given:
SHA VOR (N5243.3 W00853.1) DME 50 NM,
29) An aircraft was over 'A' at 1435 hours flying direct to 'B'.
CRK VOR (N5150.4 W00829.7) DME 41 NM,
Given:
Aircraft heading 270°(M),
Distance 'A' to 'B' 2900 NM
Both DME distances increasing.
True airspeed 470 kt
What is the aircraft position?
Mean wind component 'out' +55 kt
Mean wind component 'back' -75 kt
A N5215 W00745
The ETA for reaching the Point of Equal Time (PET)
between 'A' and 'B' is:
B N5235 W00750
A 1846
N5200 W00935
C
B 1721
D N5215 W00940
1657
C
D 1744
66) Approximately how many nautical miles correspond to
12 cm on a map with a scale of 1 : 2 000 000?
28) Given: A 329
Distance 'A' to 'B' 1973 NM
Groundspeed 'out' 430 kt
B 43
Groundspeed 'back' 385 kt
Safe endurance 7 HR 20 MIN
130
C
The distance from 'A' to the Point of Safe Return (PSR)
'A' is:
D 150
A 1490 NM
B 1664 NM
1698 NM
C
D 1422 NM
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23) Permanent magnetism in aircraft arises chiefly from: 19) An aircraft at FL370 is required to commence descent
when
100 NM from a DME facility and to cross the station at
A exposure to the earth's magnetic field during normal
FL120.
operation
If the mean GS during the descent is 396 kt, the
minimum
B the combined effect of aircraft electrical equipment and the
rate of descent required is approximately:
earth's magnetic field
A 1550 FT/MIN
the effect of internal wiring and exposure to electrical storms
C
B 1650 FT/MIN
D hammering, and the effect of the earth's magnetic field,
whilst under construction
2400 FT/MIN
C
D 1000 FT/MIN
22) An aircraft passes position A (60°00'N 120°00'W) on
route to position B (60°00'N 140°30'W).
What is the great circle track on departure from A?
18) Which of the following is an occasion for carrying out a
A 279° compass swing on a Direct Reading Compass?
A After an aircraft has passed through a severe electrical
B 288°
storm, or has been struck by lightning
261°
C
B Before an aircraft goes on any flight that involves a large
change of magnetic latitude
D 270°
After any of the aircraft radio equipment has been changed
C
due to unserviceability
21) Given:
D Whenever an aircraft carries a large freight load regardless
TAS = 465 kt,
of its content
HDG (T) = 124°,
W/V = 170/80kt.
Calculate the drift and GS?
26) The annunciator of a remote indicating compass system
A 4L - 400 kt is used when:
A setting the 'heading' pointer
B 6L - 400 kt
B synchronising the magnetic and gyro compass elements
8L - 415 kt
C
compensating for deviation
D 3L - 415 kt C
D setting local magnetic variation
20) (For this question use annex 061-12580A)
Given:
SHA VOR (N5243.3 W00853.1) radial 205°,
105) Concerning direct reading magnetic compasses, in the
CRK VOR (N5150.4 W00829.7) radial 317°.
northern hemisphere, it can be said that :
What is the aircraft position?
A on a Westerly heading, a longitudinal deceleration causes
A N5210 W00910
an apparent turn to the North
B on an Easterly heading, a longitudinal acceleration causes
B N5118 W00913
an apparent turn to the North
N5205 W00915
C
on an Easterly heading, a longitudinal acceleration causes
C
an apparent turn to the South
D N5215 W00917
D on a Westerly heading, a longitudinal acceleration causes
an apparent turn to the South
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64) In the B737-400 Flight Management System the CDUs 108) Given:
are used during preflight to: True HDG = 054°,
TAS = 450 kt,
Track (T) = 059°,
A manually initialize the Flight Director System and FMC with
GS = 416 kt.
dispatch information
Calculate the W/V?
B manually initialize the IRSs, FMC and Autothrottle with
dispatch information A 010/55kt
manually initialize the IRSs and FMC with dispatch
C
B 010/45kt
information
010/50kt
C
D automatically initialize the IRSs and FMC with dispatch
information
D 005/50kt
111) The horizontal component of the earth's magnetic field:
113) (For this question use annex 061-12572A)
What is the average track (°T) and distance between
A is approximately the same at magnetic latitudes 50°N and
SLG NDB (N5416.7 W00836.0) and CFN NDB (N5502.6
50°S
W00820.4)?
B weakens with increasing distance from the magnetic poles
A 020° - 46 NM
weakens with increasing distance from the nearer magnetic
C
B 348° - 46 NM
pole
191° - 45 NM
C
D is approximately the same at all magnetic latitudes less than
60°
D 011° - 47 NM
110) Which one of the following statements is correct
concerning the appearance of great circles, with the
106) Given:
exception of meridians, on a Polar Stereographic chart
True HDG = 206°,
whose tangency is at the pole ?
TAS = 140 kt,
Track (T) = 207°,
A The higher the latitude the closer they approximate to a
GS = 135 kt.
straight line
Calculate the W/V?
B Any straight line is a great circle
A 000/10kt
They are complex curves that can be convex and/or concave
C
B 180/10kt
to the Pole
180/05kt
C
D They are curves convex to the Pole
D 000/05kt
109) What is the ISA temperature value at FL 330?
114) What is the highest latitude listed below at which the
A -56°C sun will reach an altitude of 90° above the horizon at
some time during the year?
B -66°C
A 45°
C -81°C
B 66°
D -50°C
0°
C
D 23°
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104) Given: 100) An aircraft flies the following rhumb line tracks and
Position 'A' is N00° E100°, distances
Position 'B' is 240°(T), 200 NM from 'A'. from position 04°00'N 030°00'W :
What is the position of 'B'? 600 NM South,
then 600 NM East,
then 600 NM North,
A N01°40' E097°07'
then 600 NM West.
The final position of the aircraft is:
B S01°40' E101°40'
A 03°58'N 030°02'W
N01°40' E101°40'
C
B 04°00'N 029°58'W
D S01°40' E097°07'
04°00'N 030°02'W
C
103) Given:
D 04°00'N 030°00'W
TAS = 140 kt,
HDG (T) = 005°,
W/V = 265/25kt.
Calculate the drift and GS? 99) A negative (westerly) magnetic variation signifies that :
A 9R - 140 kt
A Compass North is West of Magnetic North
B 11R - 142 kt
B True North is East of Magnetic North
11R - 140 kt
C
True North is West of Magnetic North
C
D 10R - 146 kt
D Compass North is East of Magnetic North
102) On a direct Mercator projection, the distance measured
107) The term drift refers to the wander of the axis of a gyro
between two meridians spaced 5° apart at latitude 60°N
in:
is 8 cm.
The scale of this chart at latitude 60°N is approximately:
A any plane
A 1 : 7 000 000
B the horizontal plane
B 1 : 6 000 000
the vertical plane
C
1 : 3 500 000
C
D the vertical and horizontal plane
D 1 : 4 750 000
121) Given the following:
True track: 192°
101) Given:
Magnetic variation: 7°E
TAS = 190 kt,
Drift angle: 5° left
True HDG = 085°,
What is the magnetic heading required to maintain the
W/V = 110°(T)/50kt.
given track?
Calculate the drift angle and GS?
A 204°
A 8°L - 146 kt
B 180°
B 7°L - 156 kt
190°
C
4°L - 168 kt
C
D 194°
D 4°L - 145 kt
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232) What is the name given to an Inertial Reference System 124) Given:
(IRS) which has the gyros and accelerometers as part of True Heading = 090°
the unit's fixture to the aircraft structure? TAS = 180 kt
GS = 180 kt
Drift 5° right
A Ring laser
Calculate the W/V?
B Strapdown
A 360° / 15 kt
Rigid
C
B 190° / 15 kt
D Solid state
010° / 15 kt
C
D 180° / 15 kt
127) At 0422 an aircraft at FL370, GS 320kt,
is on the direct track to VOR 'X' 185 NM distant.
The aircraft is required to cross VOR 'X' at FL80.
For a mean rate of descent of 1800 FT/MIN at a mean GS 112) A chart has the scale 1 : 1 000 000. From A to B on the
of 232 kt, chart measures 1.5 inches (one inch equals 2.54
the latest time at which to commence descent is: centimetres), the distance from A to B in NM is :
A 0454 A 44.5
B 0445 B 54.2
0448 20.6
C C
D 0451 D 38.1
126) Given: 122) At 0020 UTC an aircraft is crossing the 310° radial at 40
TAS = 135 kt, NM of a VOR/DME station.
HDG (°T) = 278, At 0035 UTC the radial is 040° and DME distance is 40
W/V = 140/20kt NM.
Calculate the Track (°T) and GS? Magnetic variation is zero.
The true track and ground speed are :
A 279 - 152 kt
A 080° - 226 kt
B 282 - 148 kt
B 088° - 232 kt
275 - 150 kt
C
085° - 226 kt
C
D 283 - 150 kt
D 090° - 232 kt
125) The maximum difference between geocentric and
geodetic latitude occurs at about: 96) An aircraft at FL120, IAS 200kt, OAT -5° and wind
component +30kt, is required to reduce speed in order
to cross a reporting point 5 MIN later than planned.
A 0° North and South (equator)
Assuming flight conditions do not change, when 100 NM
from the reporting point IAS should be reduced to:
B 45° North and South
A 174 kt
60° North and South
C
B 159 kt
D 90° North and South
165 kt
C
D 169 kt
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120) Given: 116) Given:
Chart scale is 1 : 1 850 000. TAS = 230 kt,
The chart distance between two points is 4 centimetres. HDG (T) = 250°,
Earth distance is approximately : W/V = 205/10kt.
Calculate the drift and GS?
A 100 NM
A 2L - 224 kt
B 4 NM
B 1L - 225 kt
40 NM
C
1R - 221 kt
C
D 74 NM
D 2R - 223 kt
119) On a Direct Mercator chart a great circle will be
represented by a: 115) Given: GS = 122 kt.
Distance from A to B = 985 NM.
What is the time from A to B?
A complex curve
A 8 HR 10 MIN
B curve convex to the equator
B 8 HR 04 MIN
straight line
C
7 HR 48 MIN
C
D curve concave to the equator
D 7 HR 49 MIN
118) The Earth can be considered as being a magnet with the:
123) If an aeroplane was to circle around the Earth following
A red pole near the north pole of the earth and the direction of
parallel 60°N at a ground speed of 480 kt. In order to
the magnetic force pointing straight up from the earth's
circle around the Earth along the equator in the same
surface
amount of time, it should fly at a ground speed of:
B blue pole near the north pole of the earth and the direction of
A 480 kt
the magnetic force pointing straight down to the earth's
surface
B 960 kt
red pole near the north pole of the earth and the direction of
C
240 kt
the magnetic force pointing straight down to the earth's C
surface
D 550 kt
D blue pole near the north pole of the earth and the direction of
the magnetic force pointing straight up from the earth's
surface
72) (For this question use annex 061-12556A)
What is the radial and DME distance from SHA
VOR/DME (N5243.3 W00853.1)
117) On a Lambert conformal conic chart, the distance
to position N5210 W00920?
between parallels of latitude spaced the same number of
degrees apart :
A 346° - 34 NM
A is constant between, and expands outside, the standard
B 214° - 37 NM
parallels
354° - 34 NM
B expands between, and reduces outside, the standard C
parallels
D 198° - 37 NM
is constant throughout the chart
C
D reduces between, and expands outside, the standard
parallels
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79) When turning right from 330°(C) to 040°(C) in the 98) In an Inertial Navigation System (INS), Ground Speed
northern hemisphere, the reading of a direct reading (GS) is calculated:
magnetic compass will:
A from TAS and W/V from RNAV data
A over-indicate the turn and liquid swirl will increase the effect
B by integrating gyro precession in N/S and E/W directions
B under-indicate the turn and liquid swirl will increase the effect respectively
by integrating measured acceleration
C
over-indicate the turn and liquid swirl will decrease the effect
C
D from TAS and W/V from Air Data Computer (ADC)
D under-indicate the turn and liquid swirl will decrease the
effect
73) Given:
78) An aircraft travels 2.4 statute miles in 47 seconds. Half way between two reporting points the navigation
What is its groundspeed? log gives the following information:
TAS 360 kt,
W/V 330°/80kt,
A 131 kt
Compass heading 237°,
Deviation on this heading -5°,
B 160 kt
Variation 19°W.
What is the average ground speed for this leg?
183 kt
C
A 354 kt
D 209 kt
B 373 kt
77) The chart that is generally used for navigation in polar
360 kt
C
areas is based on a:
D 403 kt
A Lambert conformal projection
B Stereographical projection
82) Given:
True course from A to B = 090°,
Direct Mercator projection
C
TAS = 460 kt,
W/V = 360/100kt,
D Gnomonic projection
Average variation = 10°E,
Deviation = -2°.
Calculate the compass heading and GS?
76) What are, in order of highest priority followed by lowest,
A 068° - 460 kt
the two levels of message produced by the CDU of the
B737-400 Electronic Flight Instrument System?
B 078° - 450 kt
A Alerting and Advisory
070° - 453 kt
C
B Urgent and Routine
D 069° - 448 kt
Priority and Alerting
C
D Urgent and Advisory
71) The scale on a Lambert conformal conic chart :
A is constant across the whole map
75) Position A is located on the equator at longitude
130°00E.
B varies slightly as a function of latitude and longitude
Position B is located 100 NM from A on a bearing of
225°(T).
is constant along a parallel of latitude
C
The coordinates of position B are:
D is constant along a meridian of longitude
A 01°11'N 128°49'E
B 01°11'S 128°49'E
01°11'N 131°11'E
C
D 01°11'S 131°11'E
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70) (For this question use annexes 061-2305A and 061- 74) On a Direct Mercator chart at latitude 15°S, a certain
2305B) length represents a distance of 120 NM on the earth.
When it is 1000 Standard Time in Kuwait, the Standard The same length on the chart will represent on the earth,
Time in Algeria is: at latitude 10°N, a distance of :
A 0700 A 124.2 NM
B 0800 B 118.2 NM
1200 122.3 NM
C C
D 1300 D 117.7 NM
69) The circumference of the parallel of latitude at 60°N is 88) When an aircraft on a westerly heading on the northern
approximately: hemisphere accelerates, the effect of the acceleration
error causes the magnetic compass to:
A 34 641 NM
A lag behind the turning rate of the aircraft
B 10 800 NM
B indicate a turn towards the south
18 706 NM
C
to turn faster than the actual turning rate of the aircraft
C
D 20 000 NM
D indicate a turn towards the north
68) An island appears 45° to the right of the centre line on
an airborne weather radar display. What is the true 65) An aeroplane is flying at TAS 180 kt on a track of 090°.
bearing of the aircraft from the island if at the time of The W/V is 045° / 50kt.
observation the aircraft was on a magnetic heading (MH) How far can the aeroplane fly out from its base and
of 215° with the magnetic variation (VAR) 21°W? return in one hour?
A 239° A 85 NM
B 329° B 88 NM
059° 56 NM
C C
D 101° D 176 NM
67) (For this question refer to annex 061-12634A) 95) An aircraft at FL390 is required to descend to cross a
Which aeronautical chart symbol indicates an DME facility at FL70. Maximum rate of descent is 2500
exceptionally high lighted obstacle? FT/MIN, mean GS during descent is 248 kt. What is the
minimum range from the DME at which descent should
commence?
A 13
A 63 NM
B 14
B 68 NM
10
C
53 NM
C
D 12
D 58 NM
129) 265 US-GAL equals? (Specific gravity 0.80)
A 862 kg
B 895 kg
940 kg
C
D 803 kg
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94) (For this question use annex 061-9442A) 80) On a Lambert chart (standard parallels 37°N and 65°N),
Complete line 6 of the 'FLIGHT NAVIGATION LOG', with respect to the straight line drawn on the map
positions 'L' to 'M'. between A ( N49° W030°) and B (N48° W040°), the:
What is the HDG°(M) and ETA?
A rhumb line is to the north, the great circle is to the south
A HDG 064° - ETA 1449 UTC
B great circle and rhumb line are to the south
B HDG 075° - ETA 1452 UTC
great circle and rhumb line are to the north
C
HDG 070° - ETA 1459 UTC
C
D great circle is to the north, the rhumb line is to the south
D HDG 075° - ETA 1502 UTC
89) On a Lambert Conformal Conic chart great circles that
93) Given: are not meridians are:
TAS = 485 kt,
HDG (T) = 168°,
A curves concave to the pole of projection
W/V = 130/75kt.
Calculate the Track (°T) and GS?
B straight lines within the standard parallels
A 173 - 424 kt
curves concave to the parallel of origin
C
B 175 - 420 kt
D straight lines regardless of distance
175 - 432 kt
C
81) Which one of the following describes the appearance of
D 174 - 428 kt
rhumb lines, except meridians, on a Polar Stereographic
chart?
92) Given:
A Straight lines
Distance 'A' to 'B' 1973 NM
Groundspeed 'out' 430 kt
B Curves concave to the Pole
Groundspeed 'back' 385 kt
The time from 'A' to the Point of Equal Time (PET)
Ellipses around the Pole
C
between 'A' and 'B' is:
D Curves convex to the Pole
A 181 MIN
B 130 MIN
87) Given:
TAS = 270 kt,
145 MIN
C
Track (T) = 260°,
W/V = 275/30kt.
D 162 MIN
Calculate the HDG (°T) and GS?
A 264 - 241 kt
91) Given:
TAS = 270 kt,
B 264 - 237 kt
True HDG = 270°,
Actual wind 205°(T)/30kt,
262 - 241 kt
C
Calculate the drift angle and GS?
D 262 - 237 kt
A 6L - 256kt
B 6R - 251kt
86) (For this question use annex 061-2304A)
The UTC of sunrise on 6 December at WINNIPEG
8R - 259kt
C
(Canada) (49°50'N 097°30'W) is:
D 6R - 259kt
A 2230
B 1413
0930
C
D 0113
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85) An aircraft at FL140, IAS 210 kt, OAT -5°C and wind 90) (For this question use annex 061-12598A)
component minus 35 kt, is required to reduce speed in Given:
order to cross a reporting point 5 MIN later than CON VOR (N5354.8 W00849.1) DME 30 NM,
planned. CRN VOR (N5318.1 W00856.5) DME 25 NM,
Assuming that flight conditions do not change, when Aircraft heading 270°(M),
150 NM from the reporting point the IAS should be Both DME distances decreasing.
reduced by: What is the aircraft position?
A 25 kt A N5330 W00820
B 30 kt B N5343 W00925
15 kt N5335 W00925
C C
D 20 kt D N5337 W00820
84) Given: 400) At what approximate date is the earth furthest from the
TAS = 375 kt, sun (aphelion)?
True HDG = 124°,
W/V = 130°(T)/55kt.
A End of December
Calculate the true track and GS?
B Beginning of January
A 125 - 322 kt
End of September
C
B 126 - 320 kt
D Beginning of July
125 - 318 kt
C
D 123 - 320 kt
393) (For this question refer to annex 061-12635A)
What is the meaning of aeronautical chart symbol No.
15?
83) Given:
IAS 120 kt,
A Lighthouse
FL 80,
OAT +20°C.
B Aeronautical ground light
What is the TAS?
Visual reference point
C
A 141 kt
D Hazard to aerial navigation
B 102 kt
120 kt
C
406) An island appears 30° to the left of the centre line on an
airborne weather radar display. What is the true bearing
D 132 kt
of the aircraft from the island if at the time of
observation the aircraft was on a magnetic heading of
276° with the magnetic variation 12°W?
97) The azimuth gyro of an inertial unit has a drift of
0.01°/HR.
A 054°
After a flight of 12 HR with a ground speed of 500 kt, the
error on the aeroplane position is approximately :
B 318°
A 60 NM
234°
C
B 12 NM
D 038°
1 NM
C
D 6 NM
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405) (For this question use annex 061-12559A) 401) Which component of the B737-400 Flight Management
What is the radial and DME distance from CON System (FMS) is used to enter flight plan routeing and
VOR/DME (N5354.8 W00849.1) to position N5340 performance parameters?
W00820?
A Multi-Function Control Display Unit
A 240° - 24 NM
B Flight Management Computer
B 140° - 23 NM
Inertial Reference System
C
119° - 42 NM
C
D Flight Director System
D 311° - 22 NM
409) Given:
404) Given: aircraft height 2500 FT,
True course A to B = 250° ILS GP angle 3°.
Distance A to B = 315 NM At what approximate distance from THR can you expect
TAS = 450 kt. to capture the GP?
W/V = 200°/60kt.
ETD A = 0650 UTC.
A 7.0 NM
What is the ETA at B?
B 13.1 NM
A 0716 UTC
14.5 NM
C
B 0736 UTC
D 8.3 NM
0730 UTC
C
D 0810 UTC
399) Which of the following statements concerning the
alignment procedure for Inertial Navigation
Systems(INS)/Inertial Reference Systems (IRS) at mid-
403) The 'departure' between positions 60°N 160°E and 60°N latitudes is correct?
'x' is 900 NM.
What is the longitude of 'x'?
A INS/IRS can only be aligned in NAV mode
A 145°E
B INS/IRS can be aligned in either the ALIGN or NAV mode
B 175°E
INS/IRS can only be aligned in the ALIGN mode
C
170°W
C
D INS/IRS can be aligned in either the ALIGN or ATT mode
D 140°W
398) (For this question use annex 061-12400A)
What are the average magnetic course and distance
408) (For this question refer to annex 061-12623A) between
Which aeronautical chart symbol indicates a Control INGO VOR (N6350 W01640) and Sumburg VOR (N5955 W
Zone boundary? 00115)?
A 3 A 117° - 494 NM
B 4 B 130° - 440 NM
5 131° - 494 NM
C C
D 2 D 118° - 440 NM
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397) (For this question refer to annex 061-12620A) 402) The principle of 'Schuler Tuning' as applied to the
Which of the aeronautical chart symbols indicates a operation of Inertial Navigation Systems/ Inertial
VORTAC? Reference Systems is applicable to:
A 1 A both gyro-stabilised platform and 'strapdown' systems
B 3 B only gyro-stabilised systems
6 both gyro-stabilised and laser gyro systems but only when
C C
operating in the non 'strapdown' mode
D 7
D only to 'strapdown' laser gyro systems
396) (For this question refer to annex 061-12610A)
416) What additional information is required to be input to an
Which of the following lists all the aeronautical chart
Inertial Navigation System (INS) in order to obtain an
symbols shown at position N5318.0 W00626.9?
W/V readout?
A military airport: VOR: NDB
A Mach Number
B VOR: DME: danger area
B TAS
military airport: VOR: DME
C
IAS
C
D civil airport: VOR: DME
D Altitude and OAT
395) Isogonals converge at the:
230) On a Lambert Conformal chart the distance between
meridians 5° apart along latitude 37° North is 9 cm. The
A North and South magnetic poles only scale of the chart at that parallel approximates:
A 1 : 6 000 000
B North and South geographic and magnetic poles
B 1 : 5 000 000
Magnetic equator
C
1 : 3 750 000
D North magnetic pole only C
D 1 : 2 000 000
424) The automatic flight control system (AFCS) in an aircraft
is coupled to the guidance outputs from an inertial
navigation system (INS).
422) (For this question use annex 061-12402A)
The aircraft is flying between inserted waypoints No. 3
What are the initial true course and distance between
(55°00'N 020°00'W) and No.4 (55°00'N 030°00'W).
positions N5800 W01300 and N6600 E00200?
With DSRTK/STS selected on the CDU, to the nearest
whole degree, the initial track read-out from waypoint
A 042° - 635 NM
No. 3 will be:
B 032° - 470 NM
A 266°
036° - 638 NM
C
B 270°
D 029° - 570 NM
274°
C
D 278°
421) An aircraft at latitude 10° South flies north at a GS of 890
km/HR.
What will its latitude be after 1.5 HR?
A 03°50'N
B 02°00'N
12°15'N
C
D 22°00'N
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420) (For this question use annex 061-12549A) 392) What is the longitude of a position 6 NM to the east of
What is the radial and DME distance from CRK 58°42'N 094°00'W?
VOR/DME (N5150.4 W00829.7) to position N5220
W00810?
A 093°53.1'W
A 014° - 33 NM
B 094°12.0'W
B 220° - 40 NM
093°48.5'W
C
030° - 33 NM
C
D 093°54.0'W
D 048° - 40 NM
415) The following points are entered into an inertial
navigation system (INS).
419) An aircraft at FL350 is required to cross a VOR/DME WPT 1: 60°N 30°W
facility at WPT 2: 60°N 20°W
FL110 and to commence descent when 100 NM from the WPT 3: 60°N 10°W
facility. The inertial navigation system is connected to the
If the mean GS for the descent is 335 kt, the minimum automatic pilot on route (1-2-3).
rate of The track change when passing WPT 2 will be
descent required is: approximately:
A 1290 FT/MIN A a 4° decrease
B 1340 FT/MIN B a 9° decrease
1390 FT/MIN zero
C C
D 1240 FT/MIN D a 9° increase
407) Given: 414) Given:
Magnetic track = 210°, TAS = 200 kt,
Magnetic HDG = 215°, Track (T) = 110°,
VAR = 15°E, W/V = 015/40kt.
TAS = 360 kt, Calculate the HDG (°T) and GS?
Aircraft flies 64 NM in 12 MIN.
Calculate the true W/V?
A 121 - 199 kt
A 300°/30 kt
B 097 - 201 kt
B 265°/50 kt
099 - 199 kt
C
195°/50 kt
C
D 121 - 207 kt
D 235°/50 kt
413) (For this question use annex 061-12581A)
Given:
417) On a transverse Mercator chart, the scale is exactly SHA VOR (N5243.3 W00853.1) radial 120°,
correct along the: CRK VOR (N5150.4 W00829.7) radial 033°.
What is the aircraft position?
A prime meridian and the equator
A N5220 W00750
B meridians of tangency
B N5240 W00750
equator and parallel of origin
C
N5230 W00800
C
D meridian of tangency and the parallel of latitude
perpendicular to it D N5225 W00805
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412) (For this question use annex 061-12550A) 394) Given:
What is the radial and DME distance from CRK Distance 'A' to 'B' 2346 NM
VOR/DME (N5150.4 W00829.7) to position N5210 Groundspeed 'out' 365 kt
W00920? Groundspeed 'back' 480 kt
The time from 'A' to the Point of Equal Time (PET)
between 'A' and 'B' is:
A 311° - 38 NM
A 219 MIN
B 350° - 22 NM
B 290 MIN
295° - 38 NM
C
197 MIN
C
D 170° - 22 NM
D 167 MIN
411) The angle between True North and Magnetic North is
called :
374) Given:
TAS = 205 kt,
A compass error
HDG (T) = 180°,
W/V = 240/25kt.
B drift
Calculate the drift and GS?
variation
C
A 3L - 190 kt
D deviation
B 4L - 195 kt
6L - 194 kt
C
410) Given:
Runway direction 305°(M),
D 7L - 192 kt
Surface W/V 260°(M)/30 kt.
Calculate the cross-wind component?
A 18 kt 373) The sensitivity of a direct reading compass varies:
B 21 kt
A directly with the vertical component of the earth's magnetic
field
24 kt
C
B inversely with both vertical and horizontal components of the
D 27 kt earth's magnetic field
inversely with the vertical component of the earth's magnetic
C
field
418) An aircraft takes-off from an airport 2 hours before
sunset. The pilot flies a track of 090°(T), W/V 130°/ 20 kt,
D directly with the horizontal component of the earth's
TAS 100 kt. In order to return to the point of departure
magnetic field
before sunset, the furthest distance which may be
travelled is:
372) (For this question use annex 061-12401A)
A 105 NM
What are the average magnetic course and distance
between
B 84 NM
position N6000 W02000 and Sumburg VOR (N5955 W
00115)?
97 NM
C
A 105° - 562 NM
D 115 NM
B 091° - 480 NM
091° - 562 NM
C
368) What is the local mean time, position 65°25'N 123°45'W
at 2200 UTC?
D 105° - 480 NM
A 0615
B 0815
1345
C
D 2200
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371) The Great Circle bearing of 'B' (70°S 060°E), from 'A' (70° 366) Given:
S 030° W), is approximately: True Heading = 090°
TAS = 200 kt
W/V = 220° / 30 kt.
A 135°(T)
Calculate the GS?
B 150°(T)
A 180 kt
090°(T)
C
B 200 kt
D 315°(T)
220 kt
C
D 230 kt
376) 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°(T). 365) An aircraft equipped with an Inertial Navigation System
What is the longitude of B? (INS) flies with INS 1 coupled with autopilot 1. Both
inertial navigation systems are navigating from way-
point A to B. The inertial systems' Central Display Units
A 008°E
(CDU) sho shows:
- XTK on INS 1 = 0
B 019°E
- XTK on INS 2 = 8L
(XTK = cross track)
011°E
C
From this information it can be deduced that:
D 009°36'E
A only inertial navigation system No. 1 is drifting
B the autopilot is unserviceable in NAV mode
369) The distance measured between two points on a
navigation map is 42 mm (millimetres). The scale of the
at least one of the inertial navigaton systems is drifting
C
chart is 1:1 600 000.
The actual distance between these two point is
D only inertial navigation system No. 2 is drifting
approximately:
A 67.20 NM
364) 5 HR 20 MIN 20 SEC corresponds to a longitude
difference of:
B 3.69 NM
A 78°45'
36.30 NM
C
B 80°05'
D 370.00 NM
81°10'
C
377) A pilot receives the following signals from a VOR DME
D 75°00'
station:
radial 180°+/- 1°, distance = 200 NM.
What is the approximate error?
363) A straight line on a Lambert Conformal Projection chart
for normal flight planning purposes:
A +/- 7 NM
A is approximately a Great Circle
B +/- 3.5 NM
B is a Loxodromic line
+/- 1 NM
C
is a Rhumb line
C
D +/- 2 NM
D can only be a parallel of latitude
367) In order to fly from position A (10°00'N, 030°00'W) to
position B (30°00'N, 050°00'W), maintaining a constant
true course, it is necessary to fly:
A a straight line plotted on a Lambert chart
B a rhumb line track
the constant average drift route
C
D the great-circle route
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362) (For this question use annex 061-9438A) 390) Seasons are due to the:
Complete line 2 of the 'FLIGHT NAVIGATION LOG',
positions 'C' to 'D'.
A inclination of the polar axis with the ecliptic plane
What is the HDG°(M) and ETA?
B Earth's elliptical orbit around the Sun
A HDG 188° - ETA 1229 UTC
Earth's rotation on its polar axis
B HDG 193° - ETA 1249 UTC C
D variable distance between Earth and Sun
HDG 183° - ETA 1159 UTC
C
D HDG 193° - ETA 1239 UTC
389) Deviation applied to magnetic heading gives:
370) Which of the following lists, which compares an Inertial
A magnetic course
Reference System that utilises Ring Laser Gyroscopes
(RLG) instead of conventional gyroscopes, is
B magnetic track
completely correct?
compass heading
C
A There is little or no 'spin up' time and it does not suffer from
'lock in' error
D true heading
B There is little or no 'spin up' time and it is insensitive to
gravitational ('g') forces
388) The standard parallels of a Lambert's conical
The platform is kept stable relative to the earth
C
orthomorphic projection are 07°40'N and 38°20' N.
mathematically rather than mechanically but it has a longer
The constant of the cone for this chart is:
'spin up' time
A 0.60
D It does not suffer from 'lock in' error and it is insensitive to
gravitational ('g') forces
B 0.92
0.42
384) Given: C
TAS = 132 kt,
HDG (T) = 053°, D 0.39
W/V = 205/15kt.
Calculate the Track (°T) and GS?
387) (For this question refer to annex 061-12628A)
A 050 - 145 kt
Which aeronautical chart symbol indicates a Way-point?
B 057 - 144 kt
A 15
052 - 143 kt
C
B 6
D 051 - 144 kt
7
C
D 8
391) The resultant of the first integration of the output from
the east/west accelerometer of an inertial navigation
system (INS) in NAV MODE is:
375) (For this question use annex 061-12577A)
What is the average track (°T) and distance between BAL
A vehicle longitude
VOR (N5318.0 W00626.9) and CFN NDB (N5502.6
W00820.4)?
B departure
A 335° - 128 NM
velocity along the local parallel of latitude
C
B 325° - 126 NM
D change of longitude
320° - 127 NM
C
D 327° - 124 NM
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385) On the 27th of February, at 52°S and 040°E, the sunrise 381) Given:
is at 0243 UTC. True HDG = 002°,
On the same day, at 52°S and 035°W, the sunrise is at: TAS = 130 kt,
Track (T) = 353°,
GS = 132 kt.
A 0243 UTC
Calculate the W/V?
B 2143 UTC
A 090/20kt
0523 UTC
C
B 095/25kt
D 0743 UTC
095/20kt
C
D 090/15kt
425) Given: GS = 236 kt.
Distance from A to B = 354 NM
What is the time from A to B?
380) (For this question refer to annex 061-12636A)
What is the meaning of aeronautical chart symbol No.
A 1 HR 30 MIN
16?
B 1 HR 09 MIN
A Off-shore lighthouse
1 HR 10 MIN
C
B Lightship
D 1 HR 40 MIN
Off-shore helicopter landing platform
C
D Shipwreck showing above the surface at low tide
383) Given:
FL250,
OAT -15 ºC,
TAS 250 kt. 379) What is the ratio between the litre and the US-GAL ?
Calculate the Mach No.?
A 1 litre equals 3.78 US-GAL
A 0.44
B 1 US-GAL equals 4.55 litres
B 0.39
1 litre equals 4.55 US-GAL
C
0.40
C
D 1 US-GAL equals 3.78 litres
D 0.42
378) In a remote indicating compass system the amount of
382) The flight log gives the following data :
deviation caused by aircraft magnetism and electrical
"True track, Drift, True heading, Magnetic variation,
circuits may be minimised by:
Magnetic heading, Compass deviation, Compass
heading"
A the use of repeater cards
The right solution, in the same order, is :
B positioning the master unit in the centre of the aircraft
A 125°, 2°R, 123°, 2°W, 121°, -4°, 117°
using a vertically mounted gyroscope
B 119°, 3°L, 122°, 2°E, 120°, +4°, 116° C
D mounting the detector unit in the wingtip
115°, 5°R, 120°, 3°W, 123°, +2°, 121°
C
D 117°, 4°L, 121°, 1°E, 122°, -3°, 119°
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386) The main reason for usually mounting the detector unit 495) For a distance of 1860 NM between Q and R, a ground
of a remote indicating compass in the wingtip of an speed "out" of 385 kt, a ground speed "back" of 465 kt
aeroplane is to: and an endurance of 8 HR (excluding reserves) the
distance from Q to the point of safe return (PSR) is:
A place it in a position where there is no electrical wiring to
cause deviation errors A 930 NM
B place it where it will not be subjected to electrical or
B 1865 NM
magnetic interference from the aircraft
1685 NM
C
reduce the amount of deviation caused by aircraft
C
magnetism and electrical circuits
D 1532 NM
D facilitate easy maintenance of the unit and increase its
exposure to the Earth's magnetic field
494) The chart distance between meridians 10° apart at
latitude 65° North is 3.75 inches. The chart scale at this
490) (For this question use annex 061-12588A) latitude approximates:
Given:
SHA VOR/DME (N5243.3 W00853.1) radial 048°/22 NM.
A 1 : 5 000 000
What is the aircraft position?
B 1 : 6 000 000
A N5258 W00825
1 : 2 500 000
C
B N5225 W00917
D 1 : 3 000 000
N5228 W00920
C
D N5300 W0830
493) The automatic flight control system (AFCS) in an aircraft
is coupled to the guidance outputs from an inertial
navigation system (INS) and the aircraft is flying from
483) (For this question use annex 061-12405A) waypoint No. 2 (60°00'S 070°00'W) to No. 3 (60°00'S
Which of the following beacons is 185 NM from 080°00'W).
AKRABERG (N6124 W00640)? Comparing the initial track (°T) at 070°00'W and the final
track (°T) at 080°00'W, the difference between them is
A KIRKWALL (N5858 W 00254) that the initial track is approximately:
A 5° less than the final one
B STORNOWAY (N5815 W00617)
B 9° less than the final one
SUMBURGH (N5955 W00115)
C
5° greater than the final one
C
D SAXAVORD (N6050 W00050)
D 9° greater than the final one
496) Given:
Distance 'A' to 'B' is 475 NM,
Planned GS 315 kt, 498) What indication, if any, is given in the B737-400 Flight
ATD 1000 UTC, Management System if radio updating is not available?
1040 UTC - fix obtained 190 NM along track.
What GS must be maintained from the fix in
A A warning message is displayed on the EHSI and MFDU
order to achieve planned ETA at 'B'?
B A warning message is displayed on the IRS displays
A 320 kt.
A warning message is displayed on the Flight Director
C
B 340 kt
System
360 kt. D No indication is given so long as the IRS positions remain
C
within limits
D 300 kt
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491) (For this question use appendix ) 487) The circumference of the earth is approximately:
Given:
TAS is120 kt.
A 5400 NM
ATA 'X' 1232 UTC,
ETA 'Y' 1247 UTC,
ATA 'Y' is 1250 UTC. B 10800 NM
What is ETA 'Z'?
21600 NM
C
A 1302 UTC
D 43200 NM
B 1257 UTC
1300 UTC
C
486) (For this question refer to annex 061-12616A)
Which of the aeronautical chart symbols indicates a
D 1303 UTC
VOR?
A 6
499) An aircraft in the northern hemisphere makes an
accurate rate one turn to the right/starboard. If the initial B 2
heading was 330°, after 30 seconds of the turn the direct
reading magnetic compass should read:
3
C
A more or less than 060° depending on the pendulous
D 5
suspension used
B less than 060°
485) With reference to an inertial navigation system (INS), the
initial great circle track between computer inserted
060°
C
waypoints will be displayed when the control display
unit (CDU) is selected to:
D more than 060°
A DSRTK/STS
489) The following information is displayed on an Inertial
B HDG/DA
Navigation System:
GS 520 kt,
TK/GS
C
True HDG 090°,
Drift angle 5° right,
D XTK/TKE
TAS 480 kt.
SAT (static air temperature) -51°C.
The W/V being experienced is:
423) The nominal scale of a Lambert conformal conic chart is
A 320° / 60 kt
the:
B 225° / 60 kt A scale at the standard parallels
220° / 60 kt
C B mean scale between pole and equator
D 325° / 60 kt mean scale between the parallels of the secant cone
C
D scale at the equator
488) Given:
Distance 'A' to 'B' is 325 NM,
Planned GS 315 kt,
492) On a Direct Mercator chart at latitude of 45°N, a certain
ATD 1130 UTC,
length represents a distance of 90 NM on the earth.
1205 UTC - fix obtained 165 NM along track.
The same length on the chart will represent on the earth,
What GS must be maintained from the fix in
at latitude 30°N, a distance of :
order to achieve planned ETA at 'B'?
A 73.5 NM
A 355 kt
B 78 NM
B 375 kt
45 NM
C
395 kt
C
D 110 NM
D 335 kt
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506) (For this question refer to annex 061-12605A) 509) (For this question use annex 061-12563A)
What feature is shown on the chart at position N5212 What is the radial and DME distance from BEL VOR/DME
W00612? (N5439.7 W00613.8) to position N5500 W00700?
A Clonbullogue aerodrome A 126° - 33 NM
B TUSKAR ROCK LT.H. NDB B 222° - 48 NM
WTD NDB 315° - 34 NM
C C
D KERRY/Farranfore aerodrome D 296° - 65 NM
513) Contour lines on aeronautical maps and charts connect 497) Waypoints can be entered in an INS memory in different
points : formats.
In which of the following formats can waypoints be
entered into all INSs?
A with the same variation
A by waypoints name
B having the same longitude
B geographic coordinates
of equal latitude
C
bearing and distance
C
D having the same elevation above sea level
D hexadecimal
512) (For this question refer to annex 061-12621A)
Which aeronautical chart symbol indicates a Flight
Information Region (FIR) boundary? 507) Given:
TAS = 470 kt,
True HDG = 317°
A 5
W/V = 045°(T)/45kt
Calculate the drift angle and GS?
B 1
A 3°R - 470 kt
3
C
B 5°L - 475 kt
D 4
5°R - 475 kt
C
511) The equivalent of 70 m/sec is approximately:
D 5°L - 470 kt
A 145 kt
482) Given:
B 210 kt AD = Air distance
GD = Ground distance
TAS = True Airspeed
35 kt
C
GS = Groundspeed
Which of the following is the correct formula to calculate
D 136 kt
ground distance (GD) gone?
A GD = (AD - TAS)/TAS
510) Two positions plotted on a polar stereographic chart, A
(80°N 000°) and B (70°N 102°W) are joined by a straight
B GD = AD X (GS -TAS)/GS
line whose highest latitude is reached at 035°W.
At point B, the true course is:
GD = TAS/(GS X AD)
C
A 023°
D GD = (AD X GS)/TAS
B 247°
305°
C
D 203°
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505) What is the meaning of the term "standard time" ? 500) Isogonic lines connect positions that have:
A It is the time zone system applicable only in the USA A 0° variation
B It is an expression for local mean time B the same elevation
It is another term for UTC the same angle of magnetic dip
C C
D It is the time set by the legal authorities for a country or part D the same variation
of a country
508) (For this question refer to annex 061-12601A)
504) Given:
Given:
Distance 'A' to 'B' is 90 NM,
SHA VOR/DME (N5243.3 W00853.1)
Fix obtained 60 NM along and 4 NM to the right of
Connemara aerodrome (N5314 W00928)
course.
What is the SHA radial and DME distance when
What heading alteration must be made to reach 'B'?
overhead Connemara aerodrome?
A 4° Left
A 154° - 38 NM
B 8° Left
B 326° - 37 NM
12° Left
C
146° - 38 NM
C
D 16° Left
D 333° - 37 NM
503) The lines on the earth's surface that join points of equal
432) Given:
magnetic variation are called:
Runway direction 210°(M),
Surface W/V 230°(M)/30kt.
A isogrives
Calculate the cross-wind component?
B isoclines A 10 kt
isogonals B 19 kt
C
D isotachs 16 kt
C
D 13 kt
502) Given:
Magnetic heading 311°
Drift angle 10° left
484) A useful method of a pilot resolving, during a visual
Relative bearing of NDB 270°
flight, any uncertainty in the aircraft's position is to
What is the magnetic bearing of the NDB measured from
maintain visual contact with the ground and:
the aircraft?
A set heading towards a line feature such as a coastline,
A 211°
motorway, river or railway
B 180° B fly the reverse of the heading being flown prior to becoming
uncertain until a pinpoint is obtained
221°
C
fly expanding circles until a pinpoint is obtained
C
D 208°
D fly reverse headings and associated timings until the point of
departure is regained
501) Isogonals are lines of equal :
438) The great circle distance between position A (59°34.1'N
008°08.4'E) and B (30°25.9'N 171°51.6'W) is:
A magnetic variation.
A 10 800 NM
B compass deviation.
B 5 400 NM
pressure.
C
10 800 km
C
D wind velocity.
D 2 700 NM
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437) Given: 433) Given:
Aircraft at FL 150 overhead an airport TAS = 440 kt,
Elevation of airport 720 FT. HDG (T) = 349°
QNH is 1003 hPa. W/V = 040/40kt.
OAT at FL150 -5°C. Calculate the drift and GS?
What is the true altitude of the aircraft?
(Assume 1 hPa = 27 FT)
A 2L - 420 kt
A 15 840 FT
B 6L - 395 kt
B 14 160 FT
5L - 385 kt
C
14 720 FT
C
D 4L - 415 kt
D 15 280 FT
441) At 60° N the scale of a direct Mercator chart is 1 : 3 000
000.
436) (For this question refer to annex 061-12615A) What is the scale at the equator?
Which of the aeronautical chart symbols indicates a
DME?
A 1 : 6 000 000
A 5
B 1 : 3 000 000
B 6
1 : 3 500 000
C
2
C
D 1 : 1 500 000
D 3
431) (For this question refer to annex 061-12629A)
Which aeronautical chart symbol indicates an unlighted
435) (For this question use annex 061-12596A) obstacle?
Given:
CRN VOR (N5318.1 W00856.5) DME 18 NM,
A 12
SHA VOR (N5243.3 W00853.1) DME 30 NM,
Aircraft heading 270°(M),
B 9
Both DME distances decreasing.
What is the aircraft position?
10
C
A N5355 W00825
D 11
B N5310 W00830
430) A straight line on a chart 4.89 cm long represents 185
N5252 W00923
C
NM.
The scale of this chart is approximately :
D N5307 W00923
A 1 : 7 000 000
440) (For this question refer to annex 061-12599A)
B 1 : 3 500 000
Given:
CRK VOR/DME (N5150.4 W00829.7)
1 : 6 000 000
C
Kerry aerodrome (N5210.9 W00931.4)
What is the CRK radial and DME distance when
D 1 : 5 000 000
overhead Kerry aerodrome?
A 127° - 45 NM
429) A direct reading compass should be swung when:
B 299° - 42 NM
A the aircraft is stored for a long period and is frequently
307° - 43 NM
C
moved
D 119° - 44 NM
B the aircraft has made more than a stated number of landings
there is a large, and permanent, change in magnetic latitude
C
D there is a large change in magnetic longitude
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428) On a Lambert conformal conic chart the convergence of 481) The alignment time, at mid-latitudes, for an Inertial
the meridians: Reference System using laser ring gyros is
approximately:
A is zero throughout the chart
A 5 MIN
B varies as the secant of the latitude
B 10 MIN
equals earth convergency at the standard parallels
C
20 MIN
C
D is the same as earth convergency at the parallel of origin
D 2 MIN
427) On a Polar Stereographic chart, the initial great circle
course from A 70°N 060°W to B 70°N 060°E is 480) Given: GS = 510 kt.
approximately: Distance A to B = 43 NM
What is the time (MIN) from A to B?
A 150° (T)
A 5
B 210° (T)
B 4
030° (T)
C
6
C
D 330° (T)
D 7
426) Given:
TAS = 270 kt, 479) At latitude 60°N the scale of a Mercator projection is 1 : 5
True HDG = 145°, 000 000. The length on the chart between 'C' N60°
Actual wind = 205°(T)/30kt. E008° and 'D' N60° W008° is:
Calculate the drift angle and GS?
A 19.2 cm
A 8°R - 261 kt
B 17.8 cm
B 6°R - 259 kt
16.2 cm
C
6°L - 256 kt
C
D 35.6 cm
D 6°R - 251 kt
478) Given:
434) An aircraft travels 100 statute miles in 20 MIN, how long An aircraft is flying a track of 255°(M),
does it take to travel 215 NM? 2254 UTC, it crosses radial 360° from a VOR station,
2300 UTC, it crosses radial 330° from the same station.
At 2300 UTC, the distance between the aircraft and the
A 50 MIN
station is :
B 100 MIN
A less than it was at 2254 UTC
90 MIN
C
B the same as it was at 2254 UTC
D 80 MIN
greater than it was at 2254 UTC
C
D randomly different than it was at 2254 UTC
474) What is the value of the convergence factor on a Polar
Stereographic chart?
A 0.0 477) An aircraft is over position HO (55°30'N 060°15'W), where
YYR VOR (53°30'N 060°15'W) can be received. The
magnetic variation is 31°W at HO and 28°W at YYR.
B 1.0
What is the radial from YYR?
0.866
C
A 028°
D 0.5
B 208°
031°
C
D 332°
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439) (For this question use annex 061-12569A) 472) Given:
What is the average track (°M) and distance between True Heading = 180°
BAL VOR (N5318.0 W00626.9) and SLG NDB (N5416.7 TAS = 500 kt
W00836.0)? W/V 225° / 100 kt
Calculate the GS?
A 128° - 99 NM
A 535 kt
B 308° - 98 NM
B 450 kt
316° - 96 NM
C
435 kt
C
D 262° - 86 NM
D 600 kt
475) A Mercator chart has a scale at the equator = 1 : 3 704
000. 471) Which of the following can all be stored as five letter
What is the scale at latitude 60° S? waypoint identifiers through the CDU of a B737-400
Electronic Flight Instrument System?
A 1 : 7 408 000
A Waypoint names; navaid frequencies; runway codes; airport
ICAO identifiers
B 1 : 3 208 000
B Waypoint names; navaid positions; airport ICAO identifiers;
1 : 185 200
C
airport names
D 1 : 1 852 000
Waypoint names; navaid identifiers; runway numbers; airport
C
ICAO identifiers
D Airway names; navaid identifiers; airport names; waypoint
359) On a Mercator chart, at latitude 60°N, the distance
code numbers
measured between W002° and E008° is 20 cm. The scale
of this chart at latitude 60°N is approximately:
470) An aircraft obtains a relative bearing of 315° from an
A 1 : 5 560 000
NDB at 0830. At 0840 the relative bearing from the same
position is 270°.
B 1 : 556 000
Assuming no drift and a GS of 240 kt, what is the
approximate range from the NDB at 0840?
1 : 2 780 000
C
A 30 NM
D 1 : 278 000
B 40 NM
473) (For this question use annex 061-12591A)
50 NM
C
Given:
SHA VOR N5243.3 W00853.1
D 60 NM
CRK VOR N5150.4 W00829.7
Aircraft position N5230 W00930
Which of the following lists two radials that are
applicable to the aircraft position? 443) During the initial alignment of an inertial navigation
system (INS) the equipment:
A SHA 068°
CRK 145° A will not accept a 10° error in initial latitude but will accept a
10° error in initial longitude
B SHA 060°
CRK 138° B will accept a 10° error in initial latitude but will not accept a
10° error in initial longitude
SHA 240°
C
will not accept a 10° error in initial latitude or initial longitude
CRK 137° C
D SHA 248°
D will accept a 10° error in initial latitude and initial longitude
CRK 325°
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442) Given: 277) The duration of civil twilight is the time:
Course 040°(T),
TAS is 120 kt,
A between sunset and when the centre of the sun is 6° below
Wind speed 30 kt.
the true horizon
Maximum drift angle will be obtained for a wind
direction of:
B agreed by the international aeronautical authorities which is
12 minutes
A 130°
needed by the sun to move from the apparent height of 0° to
C
B 145°
the apparent height of 6°
115°
C D between sunset and when the centre of the sun is 12° below
the true horizon
D 120°
276) Given:
TAS = 220 kt;
476) On a direct Mercator projection, at latitude 45° North, a
Magnetic course = 212 º,
certain length represents 70 NM.
W/V 160 º(M)/ 50kt,
At latitude 30° North, the same length represents
Calculate the GS?
approximately:
A 186 kt
A 70 NM
B 290 kt
B 81 NM
246 kt
C
86 NM
C
D 250 kt
D 57 NM
275) (For this question use annex 061-12551A)
271) Given:
What is the radial and DME distance from CRK
ILS GP angle = 3.5 DEG,
VOR/DME (N5150.4 W00829.7) to position N5230
GS = 150 kt.
W00750?
What is the approximate rate of descent?
A 017° - 43 NM
A 1000 FT/MIN
B 039° - 48 NM
B 700 FT/MIN
024° - 43 NM
C
800 FT/MIN
C
D 023° - 48 NM
D 900 FT/MIN
274) When accelerating on an easterly heading in the
264) An aircraft takes off from the aerodrome of BRIOUDE
Northern hemisphere, the compass card of a direct
(altitude 1 483 FT, QFE = 963 hPa, temperature = 32°C).
reading magnetic compass will turn :
Five minutes later, passing 5 000 FT on QFE, the second
altimeter set on 1 013 hPa will indicate approximately :
A clockwise giving an apparent turn toward the south
A 6 400 FT
B anti-clockwise giving an apparent turn toward the north
B 6 800 FT
anti-clockwise giving an apparent turn toward the south
C
6 000 FT
C
D clockwise giving an apparent turn toward the north
D 4 000 FT
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279) An aircraft travels from point A to point B, using the 268) Given:
autopilot connected to the aircraft's inertial system. The Distance A to B = 120 NM,
coordinates of A (45°S 010°W) and B (45°S 030°W) have After 30 NM aircraft is 3 NM to the left of course.
been entered. What heading alteration should be made in order to
The true course of the aircraft on its arrival at B, to the arrive at point 'B'?
nearest degree, is:
A 4° right
A 277°
B 8° left
B 284°
8° right
C
263°
C
D 6° right
D 270°
267) An Agonic line is a line that connects:
272) A direct Mercator graticule is based on a projection that
is :
A positions that have the same variation
A spherical
B points of equal magnetic dip
B concentric
points of equal magnetic horizontal field strength
C
cylindrical
C
D positions that have 0° variation
D conical
266) An aircraft at FL350 is required to descend to cross a
DME facility at FL80.
280) Which is the highest latitude listed below at which the
Maximum rate of descent is 1800 FT/MIN and mean GS
sun will rise above the horizon and set every day?
for descent is 276 kt.
The minimum range from the DME at which descent
A 62°
should start is:
B 66°
A 49 NM
68°
C
B 59 NM
D 72°
69 NM
C
D 79 NM
270) A straight line drawn on a chart measures 4.63 cm and
represents 150 NM.
The chart scale is:
361) The main reason that day and night, throughout the
year, have different duration, is due to the:
A 1 : 5 000 000
A gravitational effect of the sun and moon on the speed of
B 1 : 1 000 000
rotation of the earth
1 : 6 000 000
C B inclination of the ecliptic to the equator
D 1 : 3 000 000
earth's rotation
C
D relative speed of the sun along the ecliptic
269) 730 FT/MIN equals:
A 1.6 m/sec
B 2.2 m/sec
3.7 m/sec
C
D 5.2 m/sec
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273) Given : 292) On a polar stereographic projection chart showing the
Position 'A' N60 W020, South Pole, a straight line joins position A (70°S 065°E)
Position 'B' N60 W021, to position B (70°S 025°W).
Position 'C' N59 W020. The true course on departure from position A is
What are, respectively, the distances from A to B and approximately:
from A to C?
A 135°
A 60 NM and 30 NM
B 315°
B 60 NM and 52 NM
225°
C
30 NM and 60 NM
C
D 250°
D 52 NM and 60 NM
291) Civil twilight is defined by :
287) An island appears 30° to the right of the centre line on
an airborne weather radar display. What is the true
A sun upper edge tangential to horizon
bearing of the aircraft from the island if at the time of
observation the aircraft was on a magnetic heading (MH)
of 355° with the magnetic variation (VAR) 15°E? B sun altitude is 6° below the celestial horizon
A 160°
sun altitude is 12° below the celestial horizon
C
B 190°
D sun altitude is 18° below the celestial horizon
220°
C
290) Given:
D 130°
The coordinates of the heliport at Issy les Moulineaux
are:
N48°50' E002°16.5'
The coordinates of the antipodes are :
294) Given:
FL120,
A S48°50' W177°43.5'
OAT is ISA standard,
CAS is 200 kt,
B S48°50' E177°43.5'
Track is 222°(M),
Heading is 215°(M),
Variation is 15°W.
S41°10' W177°43.5'
C
Time to fly 105 NM is 21 MIN.
What is the W/V?
D S41°10' E177°43.5'
A 050°(T) / 70 kt.
278) Given:
B 040°(T) / 105 kt.
TAS = 125 kt,
True HDG = 355°,
055°(T) / 105 kt .
C
W/V = 320°(T)/30kt.
Calculate the true track and GS?
D 065°(T) / 70 kt.
A 348 - 102 kt
293) What is the validity period of the 'permanent' data base B 002 - 98 kt
of aeronautical information stored in the FMC In the
B737-400 Flight Management System?
005 - 102 kt
C
A 28 days
D 345 - 100 kt
B one calendar month
3 calendar months
C
D 14 days
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288) Which of the following statements concerning the 284) (For this question use annex 061-12573A)
earth's magnetic field is completely correct? What is the average track (°T) and distance between
WTD NDB (N5211.3 W00705.0) and FOY NDB (N5234.0
W00911.7)?
A The earth's magnetic field can be classified as transient,
semi-permanent or permanent
A 286° - 81 NM
B Dip is the angle between total magnetic field and vertical
field component
B 294° - 80 NM
The blue pole of the earth's magnetic field is situated in
C
075° - 81 NM
C
North Canada
D 277° - 83 NM
D At the earth's magnetic equator, the inclination varies
depending on whether the geograhic equator is north or
south of the magnetic equator
283) What is the value of the magnetic dip at the magnetic
south pole ?
263) A great circle track joins position A (59°S 141°W) and B
(61°S 148°W).
A 90°
What is the difference between the great circle track at A
and B?
B 45°
A It increases by 3°
60°
C
B It decreases by 3°
D 0°
It increases by 6°
C
282) (For this question use annex 061-12578A)
D It decreases by 6°
What is the average track (°T) and distance between
CRN NDB (N5318.1 W00856.5) and EKN NDB (N5423.6
W00738.7)?
286) (For this question use annex 061-1828A and the data for
1215 UTC)
A 044° - 82 NM
1215 UTC LAJES VORTAC (38°46'N 027°05'W) RMI reads
178°,
B 035° - 80 NM
range 135 NM.
Calculate the aircraft position at 1215 UTC?
042° - 83 NM
C
A 40°50'N 027°40'W
D 036° - 81 NM
B 41°00'N 028°10'W
281) An aircraft at latitude 02°20'N tracks 180°(T) for 685 km.
41°05'N 027°50'W
C
On completion of the flight the latitude will be:
D 40°55'N 027°55'W
A 04°10'S
B 04°30'S
285) Assume a Mercator chart.
The distance between positions A and B, located on the
09°05'S
C
same parallel and 10° longitude apart, is 6 cm. The scale
at the parallel is 1 : 9 260 000.
D 03°50'S
What is the latitude of A and B?
A 0°
289) On a Lambert Conformal Conic chart earth convergency
B 45° N or S
is most accurately represented at the:
60° N or S A Equator
C
D 30° N or S B parallel of origin
north and south limits of the chart
C
D standard parallels
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239) An aircraft at FL310, M0.83, temperature -30°C, is 243) How long will it take to fly 5 NM at a groundspeed of 269
required to reduce speed in order to cross a reporting Kt ?
point five minutes later than planned.
Assuming that a zero wind component remains
A 1 MIN 07 SEC
unchanged, when 360 NM from the reporting point Mach
Number should be reduced to:
B 1 MIN 55 SEC
A M0.78
2 MIN 30 SEC
C
B M0.80
D 0 MIN 34 SEC
M0.74
C
242) Given:
D M0.76
TAS = 198 kt,
HDG (°T) = 180,
W/V = 359/25.
265) An aircraft is planned to fly from position 'A' to position Calculate the Track(°T) and GS?
'B',
distance 480 NM at an average GS of 240 kt. It departs
A 180 - 223 kt
'A' at 1000 UTC.
After flying 150 NM along track from 'A', the aircraft is 2
B 179 - 220 kt
MIN behind planned time.
Using the actual GS experienced, what is the revised
181 - 180 kt
C
ETA at 'B'?
D 180 - 183 kt
A 1203
B 1153
247) At what approximate latitude is the length of one minute
of arc along a meridian equal to one NM (1852 m)
1157
C
correct?
D 1206
A 30°
B 45°
245) The main advantage of a remote indicating compass
over a direct reading compass is that it:
0°
C
A has less moving parts
D 90°
B requires less maintenance
240) (For this question refer to annex 061-12638A)
is able to magnify the earth's magnetic field in order to attain
C
Which aeronautical chart symbol indicates a lightship?
greater accuracy
D senses, rather than seeks, the magnetic meridian A 10
B 12
244) Given:
14
C
TAS = 290 kt,
True HDG = 171°,
W/V = 310°(T)/30kt D 16
Calculate the drift angle and GS?
A 4°L - 314 kt
248) ATT Mode of the Inertial Reference System (IRS) is a
back-up mode providing:
B 4°R - 310 kt
A only attitude and heading information
4°R - 314 kt
C
B only attitude information
D 4°L - 310 kt
navigation information
C
D altitude, heading and position information
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238) At what approximate date is the earth closest to the sun 234) Given:
(perihelion)? TAS = 132 kt,
True HDG = 257°
W/V = 095°(T)/35kt.
A Beginning of July
Calculate the drift angle and GS?
B End of June
A 2°R - 166 kt
Beginning of January
C
B 4°L - 167 kt
D End of March
3°L - 166 kt
C
D 4°R - 165 kt
237) How many NM would an aircraft travel in 1 MIN 45 SEC if
GS is 135 kt?
A 3.94 233) Given:
TAS = 225 kt,
HDG (°T) = 123°,
B 2.36
W/V = 090/60kt.
Calculate the Track (°T) and GS?
3.25
C
A 120 - 190 kt
D 39.0
B 128 - 180 kt
236) Given:
134 - 178 kt
C
TAS = 472 kt,
True HDG = 005°,
D 134 - 188 kt
W/V = 110°(T)/50kt.
Calculate the drift angle and GS?
A 7°R - 491 kt 241) An island is observed by weather radar to be 15° to the
left.
The aircraft heading is 120°(M) and the magnetic
B 7°L - 491 kt
variation 17°W.
What is the true bearing of the aircraft from the island?
7°R - 487 kt
C
A 268°
D 6°L - 487 kt
B 302°
235) The automatic flight control system is coupled to the
088°
C
guidance outputs from an inertial navigation system.
Which pair of latitudes will give the greatest difference
D 122°
between initial track read-out and the average true
course given, in each case, a difference of longitude of
10°?
255) Given:
TAS = 370 kt,
A 30°S to 25°S
True HDG = 181°,
W/V = 095°(T)/35kt.
B 60°N to 60°N
Calculate the true track and GS?
60°N to 50°N
C
A 189 - 370 kt
D 30°S to 30°N
B 186 - 370 kt
176 - 370 kt
C
D 192 - 370 kt
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262) An aircraft in the northern hemisphere is making an 246) An aircraft flies a great circle track from 56° N 070° W to
accurate rate one turn to the right. 62° N 110° E.
If the initial heading was 135°, after 30 seconds the The total distance travelled is?
direct reading magnetic compass should read:
A 1788 NM
A more or less than 225° depending on the pendulous
suspension used
B 2040 NM
B more than 225°
3720 NM
C
225°
C
D 5420 NM
D less than 225°
256) Given:
For take-off an aircraft requires a headwind component
261) (For this question refer to annex 061-12612A)
of at least 10 kt and has a cross-wind limitation of 35 kt.
Which of the following lists all the aeronautical chart
The angle between the wind direction and the runway is
symbols shown at position N5318.1 W00856.5?
60°,
Calculate the minimum and maximum allowable wind
A civil airport: VOR: DME: non-compulsory reporting point
speeds?
B VOR: DME: NDB: compulsory reporting point A 15 kt and 43 kt
civil airport: NDB: DME: non-compulsory reporting point B 18 kt and 50 kt
C
D VOR: DME: NDB: compulsory reporting point 20 kt and 40 kt
C
D 12 kt and 38 kt
260) (For this question refer to annex 061-12627A)
Which aeronautical chart symbol indicates a
compulsory reporting point?
297) The Local Mean Time at longitude 095°20'W, at 0000
UTC, is :
A 7
A 0621:20 previous day
B 8
B 1738:40 same day
15
C
0621:20 same day
C
D 6
D 1738:40 previous day
259) The total length of the 53°N parallel of latitude on a
direct Mercator chart is 133 cm. What is the approximate
254) How is the radio position determined by the FMC in the
scale of the chart at latitude 30°S?
B737-400 Electronic Flight Instrument System?
A 1 : 25 000 000
A DME/DME or VOR/DME
B 1 : 30 000 000
B DME ranges and/ or VOR/ADF bearings
1 : 18 000 000
C
VOR/DME range and bearing
C
D 1 : 21 000 000
D DME/DME
258) Given:
253) An aircraft is descending down a 12% slope whilst
TAS = 155 kt,
maintaining a GS of 540 kt.
HDG (T) = 216°,
The rate of descent of the aircraft is approximately:
W/V = 090/60kt.
Caslculate the Track (°T) and GS?
A 4500 FT/MIN
A 226 - 186 kt
B 3900 FT/MIN
B 231 - 196 kt
6500 FT/MIN
C
224 - 175 kt
C
D 650 FT/MIN
D 222 - 181 kt
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252) Given: GS = 120 kt. 257) Given:
Distance from A to B = 84 NM. TAS = 480 kt,
What is the time from A to B? HDG (°T) = 040°,
W/V = 090/60kt.
Calculate the Track (°T) and GS?
A 00 HR 42 MIN
A 034 - 445 kt
B 00 HR 43 MIN
B 028 - 415 kt
00 HR 44 MIN
C
032 - 425 kt
C
D 00 HR 45 MIN
D 036 - 435 kt
251) In which two months of the year is the difference
between the transit of the Apparent Sun and Mean Sun
across the Greenwich Meridian the greatest? 336) The diameter of the Earth is approximately:
A June and December
A 12 700 km
B April and August
B 6 350 km
February and November
C
18 500 km
C
D March and September
D 40 000 km
250) Given:
295) The parallels on a Lambert Conformal Conic chart are
TAS 487kt,
represented by:
FL 330,
Temperature ISA + 15.
A straight lines
Calculate the MACH Number?
B parabolic lines
A 0.81
hyperbolic lines
B 0.84 C
D arcs of concentric circles
0.76
C
D 0.78
342) Which of the following statements concerning the
aircraft positions indicated on a triple fit Inertial
Navigation System (INS)/ Inertial Reference System
249) An aircraft at FL350 is required to commence descent
(IRS) on the CDU is correct?
when 85 NM from a VOR and to cross the VOR at FL80.
The mean GS for the descent is 340 kt.
A The positions will be the same because they are an average
What is the minimum rate of descent required?
of three different positions
A 1700 FT/MIN
B The positions will only differ if one of the systems has been
decoupled because of a detected malfunction
B 1800 FT/MIN
The positions will only differ if an error has been made when
C
1900 FT/MIN
C inputting the present position at the departure airport
D The positions are likely to differ because they are calculated
D 1600 FT/MIN
from different sources
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341) Two points A and B are 1000 NM apart. TAS = 490 kt. 337) (For this question refer to annex 061-12633A)
On the flight between A and B the equivalent headwind Which aeronautical chart symbol indicates an
is -20 kt. exceptionally high unlighted obstacle?
On the return leg between B and A, the equivalent
headwind is +40 kt.
A 9
What distance from A, along the route A to B, is the the
Point of Equal Time (PET)?
B 11
A 530 NM
13
C
B 470 NM
D 14
455 NM
C
345) On a transverse Mercator chart, with the exception of
D 500 NM
the Equator, parallels of latitude appear as:
A straight lines
340) Given:
TAS = 90 kt,
B hyperbolic lines
HDG (T) = 355°,
W/V = 120/20kt.
parabolas
C
Calculate the Track (°T) and GS?
D ellipses
A 359 - 102 kt
B 346 - 102 kt
335) At 47° North the chart distance between meridians 10°
apart is 5 inches.
006 - 95 kt
C
The scale of the chart at 47° North approximates:
D 358 - 101 kt
A 1 : 6 000 000
B 1 : 8 000 000
339) At a specific location, the value of magnetic variation:
1 : 3 000 000
C
A depends on the magnetic heading
D 1 : 2 500 000
B depends on the true heading
varies slowly over time
C
334) Gyrocompassing of an inertial reference system (IRS) is
accomplished with the mode selector switched to:
D depends on the type of compass installed
A ALIGN
B STBY
344) An aircraft at position 60°N 005°W tracks 090°(T) for 315
km.
ATT/REF
On completion of the flight the longitude will be: C
A 000°15'E D ON
B 000°40'E
333) During initial alignment an inertial navigation system is
005°15'E
C
north aligned by inputs from:
D 002°10'W A vertical accelerometers and the north gyro
B horizontal accelerometers and the east gyro
the aircraft remote reading compass system
C
D computer matching of measured gravity magnitude to gravity
magnitude of initial alignment
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332) Given: 352) (For this question use annex 061-12404A)
true track is 348°, An aircraft on radial 110° at a range of 120 NM from
drift 17° left, SAXAVORD VOR (N6050 W00050) is at position:
variation 32° W,
deviation 4°E.
A N6127 W00443
What is the compass heading?
B N6010 E00255
A 359°
N6109 E00255
C
B 337°
D N6027 E00307
033°
C
D 007°
514) Which FMC/CDU page normally appears on initial power
application to the B737-400 Electronic Flight Instrument
System?
331) Given:
TAS = 130 kt,
A IDENT
Track (T) = 003°,
W/V = 190/40kt.
B INITIAL
Calculate the HDG (°T) and GS?
POS INIT
C
A 002 - 173 kt
D PERF INIT
B 359 - 166 kt
357 - 168 kt
C
358) Given:
value for the ellipticity of the Earth is 1/297.
D 001 - 170 kt
Earth's semi-major axis, as measured at the equator,
equals 6378.4 km.
What is the semi-minor axis (km) of the earth at the axis
330) (For this question use annex 061-12586A) of the Poles?
Given:
SHA VOR/DME (N5243.3 W00853.1) radial 232°/32 NM. A 6 356.9
What is the aircraft position?
B 6 378.4
A N5228 W00935
6 367.0
C
B N5303 W00810
D 6 399.9
N5220 W00930
C
D N5305 W00815
357) Which of the following lists all the methods that can be
used to enter 'Created Waypoints' into the CDU of a
B737-400 Electronic Flight Instrument System?
338) The angle between the true great-circle track and the
true rhumb-line track joining the following points: A (60°
A Identifier bearing/distance; place bearing/place bearing;
S 165° W) B (60° S 177° E), at the place of departure A,
latitude and longitude; waypoint name
is:
B Identifier bearing/distance; place distance/place distance;
A 7.8° along-track displacement; latitude and longitude
Identifier bearing/distance; place bearing/place bearing;
C
B 9°
along-track displacement; latitude and longitude
15.6°
C
D Identifier bearing/distance; place bearing/place distance;
along/across-track displacement; latitude and longitude
D 5.2°
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356) (For this question refer to annex 061-12611A) 351) Given:
Which of the following lists all the aeronautical chart Distance 'A' to 'B' 2346 NM
symbols shown at position N5416.7 W00836.0? Groundspeed 'out' 365 kt
Groundspeed 'back' 480 kt
Safe endurance 8 HR 30 MIN
A VOR: DME: NDB: non-compulsory reporting point
The time from 'A' to the Point of Safe Return (PSR) 'A' is:
B civil airport: NDB: DME: compulsory reporting point
A 197 MIN
VOR: DME: NDB: compulsory reporting point
C
B 209 MIN
D civil airport: VOR: DME: non-compulsory reporting point
290 MIN
C
D 219 MIN
355) Parallels of latitude, except the equator, are:
A Rhumb lines
350) (For this question use annex 061-12562A)
What is the radial and DME distance from BEL VOR/DME
B Great circles (N5439.7 W00613.8) to position N5440 W00730?
A 278° - 10 NM
both Rhumb lines and Great circles
C
B 098° - 45 NM
D are neither Rhumb lines nor Great circles
278° - 44 NM
C
343) What is the effect on the Mach number and TAS in an
D 090° - 46 NM
aircraft that is climbing with constant CAS?
A Mach number increases; TAS increases
349) Given:
B Mach number remains constant; TAS increases FL 350,
Mach 0.80,
OAT -55°C.
Mach number decreases; TAS decreases
C
Calculate the values for TAS and local speed of sound
(LSS)?
D Mach number increases; TAS remains constant
A 461 kt , LSS 296 kt
353) From the departure point, the distance to the point of
B 461 kt , LSS 576 kt
equal time is :
237 kt, LSS 296 kt
C
A proportional to the sum of ground speed out and ground
speed back
D 490 kt, LSS 461 kt
B inversely proportional to the total distance to go
inversely proportional to ground speed back
C 348) (For this question refer to annex 061-12630A)
Which aeronautical chart symbol indicates a lighted
obstacle?
D inversely proportional to the sum of ground speed out and
ground speed back
A 11
B 12
327) Given:
TAS = 197 kt,
True course = 240°, 9
C
W/V = 180/30kt.
Descent is initiated at FL 220 and completed at FL 40.
D 10
Distance to be covered during descent is 39 NM.
What is the approximate rate of descent?
A 1500 FT/MIN
B 1400 FT/MIN
800 FT/MIN
C
D 950 FT/MIN
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347) Given: 310) Given:
True HDG = 307°, A polar stereographic chart whose grid is aligned with
TAS = 230 kt, the zero meridian.
Track (T) = 313°, Grid track 344°,
GS = 210 kt. Longitude 115°00'W,
Calculate the W/V? Calculate the true course?
A 257/35kt A 049°
B 255/25kt B 229°
265/30kt 099°
C C
D 260/30kt D 279°
346) A pilot accidently turning OFF the INS in flight, and then 309) (For this question use annex 061-12571A)
turns it back ON a few moments later. Following this What is the average track (°T) and distance between
incident: CON VOR (N5354.8 W00849.1) and BEL VOR (N5439.7
W00613.8)?
A everything returns to normal and is usable
A 071° - 100 NM
B the INS is usable in NAV MODE after a position update
B 113° - 97 NM
it can only be used for attitude reference
C
293° - 98 NM
C
D no useful information can be obtained from the INS
D 063° - 101 NM
354) The angular difference, on a Lambert conformal conic
chart, between the arrival and departure track is equal 308) Given:
to: Magnetic heading = 255°
VAR = 40°W
GS = 375 kt
A earth convergence
W/V = 235°(T) / 120 kt
Calculate the drift angle?
B conversion angle
A 9° left
difference in longitude
C
B 16° right
D map convergence
7° left
C
303) (For this question use annex 061-12585A)
D 7° right
Given:
SHA VOR/DME (N5243.3 W00853.1) radial 165°/36 NM.
What is the aircraft position?
307) An aircraft is flying with the aid of an inertial navigation
system (INS) connected to the autopilot. The following
A N5210 W00830
two points have been entered in the INS computer:
WPT 1: 60°N 030°W
B N5208 W00840
WPT 2: 60°N 020°W
When 025°W is passed the latitude shown on the
N5315 W00915
C
display unit of the inertial navigation system will be:
D N5317 W00908
A 59°49.0'N
B 60°11.0'N
60°05.7'N
C
D 60°00.0'N
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306) Given: 302) The purpose of the Flight Management System (FMS),
Magnetic track = 315 º, as for example installed in the B737-400, is to provide:
HDG = 301 º(M),
VAR = 5ºW,
A both manual navigation guidance and performance
TAS = 225 kt,
management
The aircraft flies 50 NM in 12 MIN.
Calculate the W/V(°T)? B continuous automatic navigation guidance and performance
management
A 195 º/61 kt
manual navigation guidance and automatic performance
C
management
B 195 º/63 kt
D continuous automatic navigation guidance as well as manual
190 º/63 kt
C
performance management
D 355 º/15 kt
301) (For this question use annex 061-12590A)
Given:
329) The main reason for mounting the detector unit of a SHA VOR N5243.3 W00853.1
remote reading compass in the wingtip of an aeroplane CRK VOR N5150.4 W00829.7
is: Aircraft position N5230 W00820
Which of the following lists two radials that are
applicable to the aircraft position?
A by having detector units on both wingtips, to cancel out the
deviation effects caused by the aircraft strucure
A SHA 131°
B to minimise the amount of deviation caused by aircraft CRK 017°
magnetism and electrical circuits
B SHA 304°
to maximise the units exposure to the earth's magnetic field CRK 189°
C
SHA 312°
C
D to ensure that the unit is in the most accessible position on
CRK 197°
the aircraft for ease of maintenance
D SHA 124°
CRK 009°
304) An aircraft at FL330 is rerquired to commence descent
when 65 NM from a VOR and to cross the VOR at FL100.
The mean GS during the descent is 330 kt.
300) An aeroplane flies from A (59°S 142°W) to B (61°S
What is the minimum rate of descent required?
148°W) with a TAS of 480 kt.
The autopilot is engaged and coupled with an Inertial
A 1850 FT/MIN
Navigation System in which AB track is active.
On route AB, the true track:
B 1950 FT/MIN
A varies by 4°
1650 FT/MIN
C
B increases by 5°
D 1750 FT/MIN
varies by 10°
C
313) An island appears 60° to the left of the centre line on an
D decreases by 6°
airborne weather radar display. What is the true bearing
of the aircraft from the island if at the time of
observation the aircraft was on a magnetic heading (MH)
299) In a navigation chart a distance of 49 NM is equal to 7
of 276° with the magnetic variation (VAR) 10°E?
cm. The scale of the chart is approximately:
A 086°
A 1 : 1 300 000
B 226°
B 1 : 700 000
026°
C
1 : 130 000
C
D 046°
D 1 : 7 000 000
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298) An aircraft is following a true track of 048° at a constant 296) A Lambert conformal conic projection, with two
TAS of 210 kt. standard parallels:
The wind velocity is 350° / 30 kt.
The GS and drift angle are:
A shows lines of longitude as parallel straight lines
A 225 kt, 7° left
B the scale is only correct along the standard parallels
B 192 kt, 7° right
shows all great circles as straight lines
C
200 kt, 3.5° right
C
D the scale is only correct at parallel of origin
D 192 kt, 7° left
326) Which of the following lists the first three pages of the
FMC/CDU normally used to enter data on initial start-up
360) Some inertial reference and navigation systems are of the B737-400 Electronic Flight Instrument System?
known as "strapdown".
This means that:
A POS INIT - RTE - IDENT
A gyros and accelerometers need satellite information input to
B IDENT - RTE - DEPARTURE
obtain a vertical reference
POS INIT - RTE - DEPARTURE
C
B the gyroscopes and accelerometers become part of the
unit's fixture to the aircraft structure
D IDENT - POS INIT - RTE
only the gyros, and not the accelerometers, become part of
C
the unit's fixture to the aircraft structure
325) (For this question use annex 061-12570A)
D gyros and accelerometers are mounted on a stabilised
What is the average track (°M) and distance between
platform in the aircraft
CRN NDB (N5318.1 W00856.5) and BEL VOR (N5439.7
W00613.8)?
305) Given:
A 237° - 130 NM
TAS = 190 kt,
HDG (T) = 355°,
B 057° - 126 NM
W/V = 165/25kt.
Calculate the drift and GS?
089° - 95 NM
C
A 1R - 175 kt
D 229° - 125 NM
B 1R - 165 kt
324) On a Mercator chart, the scale:
1L - 215 kt
C
D 1L - 225 kt
A varies as 1/2 cosine of the co-latitude
B varies as 1/cosine of latitude (1/cosine= secant)
319) An aircraft was over 'A' at 1435 hours flying direct to 'B'.
Given:
varies as the sine of the latitude
C
Distance 'A' to 'B' 2900 NM
True airspeed 470 kt
D is constant throughout the chart
Mean wind component 'out' +55 kt
Mean wind component 'back' -75 kt
Safe endurance 9 HR 30 MIN
The distance from 'A' to the Point of Safe Return (PSR)
323) In order to maintain an accurate vertical using a
'A' is: pendulous system, an aircraft inertial platform
incorporates a device:
A 2141 NM
A without damping and a period of 84.4 SEC
B 1611 NM
B with damping and a period of 84.4 SEC
1759 NM
C
with damping and a period of 84.4 MIN
C
D 2844 NM
D without damping and a period of 84.4 MIN
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322) Compass deviation is defined as the angle between: 318) (For this question use annex 061-12553A)
What is the radial and DME distance from SHA
VOR/DME (N5243.3 W00853.1) to position N5300
A True North and Compass North
W00940?
B the horizontal and the total intensity of the earth's magnetic
A 324° - 17 NM
field
B 309° - 33 NM
Magnetic North and Compass North
C
057° - 27 NM
C
D True North and Magnetic North
D 293° - 33 NM
311) Given:
Runway direction 083°(M),
317) Given:
Surface W/V 035/35kt.
Maximum allowable crosswind component is 20 kt.
Calculate the effective headwind component?
Runway 06, RWY QDM 063°(M).
Wind direction 100°(M)
A 27 kt
Calculate the maximum allowable windspeed?
B 31 kt
A 25 kt
34 kt
C
B 33 kt
D 24 kt
31 kt
C
D 26 kt
320) The drift of the azimuth gyro on an inertial unit induces
an error in the position given by this unit. "t" being the
elapsed time.
316) Given:
The total error is:
True HDG = 074°,
TAS = 230 kt,
A proportional to t
Track (T) = 066°,
GS = 242 kt.
B proportional to the square of time, t²
Calculate the W/V?
proportional to t/2
C A 180/40kt
D sinusoîdal
B 180/35kt
180/30kt
C
312) An aircraft is planned to fly from position 'A' to position
'B', D 185/35kt
distance 250 NM at an average GS of 115 kt. It departs
'A' at 0900 UTC.
After flying 75 NM along track from 'A', the aircraft is 1.5
315) Transverse Mercator projections are used for:
MIN behind planned time.
Using the actual GS experienced, what is the revised
ETA at 'B'?
A maps of large north/south extent
A 1044 UTC
B maps of large east/west extent in equatorial areas
B 1050 UTC
radio navigation charts in equatorial areas
C
1115 UTC
C
D plotting charts in equatorial areas
D 1110 UTC
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314) Given:
Required course 045°(M);
Variation is 15°E;
W/V is 190°(T)/30 kt;
CAS is 120 kt at FL 55 in standard atmosphere.
What are the heading (°M) and GS?
A 056° and 137 kt
B 055° and 147 kt
036° and 151 kt
C
D 052° and 154 kt
328) Assuming mid-latitudes (40° to 50°N/S).
At which time of year is the relationship between the
length
of day and night, as well as the rate of change of
declination
of the sun, changing at the greatest rate?
A Summer solstice and spring equinox
B summer solstice and winter solstice
Winter solstice and autumn equinox
C
D Spring equinox and autumn equinox
321) (For this question use annex 061-2325A to 061-2325D)
An aircraft takes off from Guam at 2300 Standard Time
on 30 April local date.
After a flight of 11 HR 15 MIN it lands at Los Angeles
(California).
What is the Standard Time and local date of arrival
(assume summer time rules apply)?
A 1715 on 30 April
B 1215 on 1 May
1315 on 1 May
C
D 1615 on 30 April
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