061 - General Navigation

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GENERAL NAVIGATIONsubj Domanda RispostaA RispostaB RispostaC RispostaD Check

061 An aircraft departs from position A (0410' S 17822'W) and flies northward

followin the meridian for 2!"0 #$% &t then flies westward alon the parallel oflatitde for 82 #$ to position % *he coordinates of position are+

4"00'# 1728', "20'# 16!22W 4"00'# 16!22W "20'# 1728',

061 *he anle -etween the tre reat.circle trac/ and the tre rhm-.line trac/oinin the followin points A (60 S 16" W) (60 S 177 ,) at the place ofdepartre A is

7%8 ! 1"%6 "%2

061 3ien Wa5point 1% 60S 00W Wa5point 2% 60S 020W What will -e theapproimate latitde shown on the displa5 nit of an inertial naiation s5stem atlonitde 02"W+

06006'S 06011'S 0"!4!'S 06000'S

061 What is the time reired to trael alon the parallel of latitde 60 # -etween

meridians 010 , and 00 W at a rondspeed of 480 /t+

2 9 0 $ 1 9 1" $ 1 9 4" $ " 9 00 $

061 3ien ale for the flattenin of the ,arth is 1:2!8% ,arth's semi.maor ais asmeasred at the eator eals 678%4 /m% What is the semi.minor ais (/m) ofthe earth at the ais of the poles+

6 "6%! 6 78%4 6 67%0 6 !!%!

061 ;osition A is located on the eator at lonitde 1000,% ;osition is located

100 #$ from A on a -earin of 22"(*)% *he coordinates of position are

0111'S 1284!', 0111'# 1111', 0111'S 1111', 0111'# 1284!',

061 &n order to fl5 from position A (1000'# 0000'W) to position (000'#0"000'W) maintainin a constant tre corse it is necessar5 to fl5

a rhm- line trac/ the constant aerae drift rote the reat.circle rote a straiht line plotted on a 280 #$ is to the ,ast of A 9eired lonitde of position A+

8!', 4!"7', "1"1', 40',

061 ?n a polar stereoraphic proection chart showin the Soth ;ole a straiht lineoins position A (70S 06",) to position (70S 02"W)% *he tre corse on

departre from position A is approimatel5

22" 2"0 1" 1"


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061 ?n a direct $ercator proection the distance measred -etween two meridians

spaced " apart at latitde 60# is 8 cm% *he scale of this chart at latitde 60# isapproimatel5

1 "00 000 1 4 7"0 000 1 7 000 000 1 6 000 000

061 *wo positions plotted on a polar stereoraphic chart A (80# 000) and (70#102W) are oined -5 a straiht line whose hihest latitde is reached at 0"W%At point the tre corse is

20 02 247 0"

061 3ien $anetic headin 11 =rift anle 10 left 9elatie -earin of #= 270What is the manetic -earin of the #= measred from the aircraft+

221 208 211 180

061 3ien the followin *re trac/ 1!2 $anetic ariation 7, =rift anle " leftWhat is the manetic headin reired to maintain the ien trac/+

1!0 1!4 204 180

061 3ien the followin $anetic headin 060 $anetic ariation 8W =riftanle 4 riht What is the tre trac/+

0"6 064 048 072

061 An aircraft is followin a tre trac/ of 048 at a constant *AS of 210 /t% *hewind elocit5 is "0 : 0 /t% *he 3S and drift anle are

1!2 /t 7 riht 200 /t %" riht 1!2 /t 7 left 22" /t 7 left

061 3ien B< "0 $ach 0%80 ?A* .""% alclate the ales for *AS and local

speed of sond ( 2"(*) : 120/t alclate the drift anle+

6 left 6 riht ! left left

061 3ien *re eadin > 180 *AS > "00 /t W:C 22" : 100 /t alclate the 3S+ 4" /t 600 /t "" /t 4"0 /t

061 3ien *re headin > 10 *AS > 200 /t 3S > 176 /t =rift anle 7 riht%alclate the W:C+

270 : /t 60 : /t 0!0 : /t 180 : /t

061 &f an aeroplane was to circle arond the ,arth followin parallel 60# at a rond

speed of 480 /t% &n order to circle arond the ,arth alon the eator in the sameamont of time it shold fl5 at a rond speed of

!60 /t 240 /t ""0 /t 480 /t

061 3ien *re eadin > 0!0 *AS > 180 /t 3S > 180 /t =rift " riht alclatethe W:C+ 00" : 1" /t 1!0 : 1" /t "" : 1" /t 18" : 1" /t

061 3ien *re eadin > 0!0 *AS > 200 /t W:C > 220 : 0 /t% alclate the3S+

220 /t 20 /t 180 /t 200 /t

061 An aeroplane is fl5in at *AS 180 /t on a trac/ of 0!0% *he W:C is 04" : "0/t%ow far can the aeroplane fl5 ot from its -ase and retrn in one hor+

8" #$ 88 #$ "6 #$ 176 #$

061 *he followin information is displa5ed on an &nertial #aiation S5stem 3S "20

/t *re =3 0!0 =rift anle " riht *AS 480 /t% SA* (static air te mperatre)."1% *he W:C -ein eperienced is

20 : 60 /t 22" : 60 /t 220 : 60 /t 2" : 60 /t

061 *he reported srface wind from the ontrol *ower is 240:" /t% 9nwa5 0(00)% What is the cross.wind component+

0 /t 24 /t 27 /t 21 /t

061 An aircraft passes position A (6000'# 12000'W) on rote to position (6000'# 1400'W)% What is the reat circle trac/ on departre from A+

27! 288 261 270

061 A reat circle trac/ oins position A ("!S 141W) and (61S 148W)% What isthe difference -etween the reat circle trac/ at A and +

&t increases -5 6 &t decreases -5 6 &t increases -5 &t decreases -5

061 What is the lonitde of a position 6 #$ to the east of "842'# 0!400'W+ 0!48%"'W 0!"4%0'W 0!"%1'W 0!412%0'W

061 An aircraft is maintainin a "%2D radient is at 7 #$ from the rnwa5 on a flatterrainE its heiht is approimatel5

2210 B* 680 B* 18!0 B* 640 B*

061 An aircraft is descendin down a 6D slope whilst maintainin a 3:S of 00 /t%*he rate of descent of the aircraft is approimatel5

1800 B*:$ 10800 B*:$ 600 B*:$ !00 B*:$

061 *he anle -etween the plane of the ecliptic and the plane of eator isapproimatel5

2%" 2"% 27%" 66%"

061 *he dration of ciil twiliht is the time -etween snset and when the centre ofthe sn is 6 -elow the tre hori@on

areed -5 the internationalaeronatical athorities which is 12mintes

needed -5 the sn to moe from theapparent heiht of 0 to the apparentheiht of 6

-etween snset and when the centreof the sn is 12 -elow the trehori@on

061 ?n the 27th of Be-rar5 at "2S and 040, the snrise is at 024 F*% ?n thesame da5 at "2S and 0"W the snrise is at

074 F* 024 F* 214 F* 0"2 F*

061 An aeroplane flies from A ("!S 142W) to (61S 148W) with a *AS of 480 increases -5 " aries -5 10 decreases -5 6 aries -5 4


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/t% *he atopilot is enaed and copled with an &nertial #aiation S5stem in

which A trac/ is actie% ?n rote A the tre trac/

061 *he rhm-.line distance -etween points A (6000'# 0020',) and (6000'#

0070'W) is

00 #$ 4"0 #$ 600 #$ 1"0 #$

061 An aircraft is oer position ? (""0'# 0601"'W) where GG9 C?9 ("0'#0601"'W) can -e receied% *he manetic ariation is 1W at ? and 28W at

GG9% What is the radial from GG9+

028 208 01 2

061 3ien *AS > 48" /t ?A* > &SA H10 B< 410% alclate the $ach #m-er+ 0%82" 0%!0 0%8" 0%87

061 (Bor this estion se anne 061.1818A) Assme a #orth polar stereoraphicchart whose rid is alined with the 3reenwich meridian% An aircraft flies from

the eoraphic #orth pole for a distance of 480 #$ alon the 110, meridianthen follows a rid trac/ of 1"4 for a distance of 00 #$% &ts position is now

approimatel5

8000'# 080, 784"'# 087, 7!1"'# 074, 701"'# 080,

061 3ien A polar stereoraphic chart whose rid is alined with the @ero meridian%3rid trac/ 44 4!0 /t% ?n the fliht -etween Aand the eialent headwind is .20 /t% ?n the retrn le -etween and A theeialent headwind is H40 /t% What distance from A alon the rote A to isthe ;oint of ,al *ime (;,*)+

"0 #$ 470 #$ 4"" #$ "00 #$

061 3ien A= > Air distance 3= > 3rond distance *AS > *re Airspeed 3S >3rondspeed Which of the followin is the correct formla to calclate ronddistance (3=) one+

3= > (A= L 3S):*AS 3= > (A= . *AS):*AS 3= > A= L (3S .*AS):3S 3= > *AS:(3S L A=)

061 An aircraft is fl5in with the aid of an inertial naiation s5stem (S) connectedto the atopilot% *he followin two points hae -een entered in the S

compter W;* 1 60# 00W W;* 2 60# 020W When 02"W is passed thelatitde shown on the displa5 nit of the inertial naiation s5stem will -e

600"%7'# 6000%0'# "!4!%0'# 6011%0'#

061 *he drift of the a@imth 5ro on an inertial nit indces an error in the position

ien -5 this nit% KtK -ein the elapsed time% *he total error is

proportional to t proportional to the sare of time tM proportional to t:2 sinsoNdal

061 With reference to inertial naiation s5stems a *AS inpt is reired to proide a W:C read ot not reired reired for ;olar naiation reired for rhm- line naiation

061 *he platform of an inertial naiation s5stem (S) is maintained at riht anlesto the local ertical -5 appl5in corrections for the effects of

aircraft manoeres earth rotationtransport wander and coriolis

5roscopic inertia earth rotation andreal drift

ertical elocities earth precessioncentrifal forces and transport drift

moement in the 5awin planesecondar5 precession and pendlososcillation

061 An aircraft traels from point A to point sin the atopilot connected to theaircraft's inertial s5stem% *he coordinates of A (4"S 010W) and (4"S

00W) hae -een entered% *he tre corse of the aircraft on its arrial at tothe nearest deree is

277 284 26 270

061 Some inertial reference and naiation s5stems are /nown as KstrapdownK% *his

means that

the 5roscopes and accelerometers

-ecome part of the nit's fitre to theaircraft strctre

onl5 the 5ros and not the

accelerometers -ecome part of thenit's fitre to the aircraft strctre

5ros and accelerometers are monted

on a sta-ilised platform in the aircraft

5ros and accelerometers need

satellite information inpt to o-tain aertical reference

061 As the S position of the departre aerodrome coordinates "2%7'#1!46%'W are inpt instead of "2%7'# 1!46%',% When the aircrafts-seentl5 passes point "2# 180W the lonitde ale shown on the S

will -e

0!! 2%6'W 0!! 2%6', 080 27%4', 080 27%4'W


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061 &n order to maintain an accrate ertical sin a pendlos s5stem an aircraft

inertial platform incorporates a deice

with dampin and a period of 84%4 $ withot dampin and a period of

84%4 $

withot dampin and a period of 84%4

S,

with dampin and a period of 84%4

S,

061 *he oter mar/er of an &


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061 (Bor this estion se anne 061.226A) When it is 0600 Standard *ime in

Jeensland (Astralia) the Standard *ime in awaii (FSA) is

1000 1200 0200 0600

061 *he chart distance -etween meridians 10 apart at latitde 6" #orth is %7"

inches% *he chart scale at this latitde approimates

1 " 000 000 1 6 000 000 1 2 "00 000 1 000 000

061 ?n a


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061 3ien ;ressre Altitde 2!000 B* ?A* .""% alclate the =ensit5 Altitde+ 27"00 B* 1000 B* "00 B* 26000 B*

061 3ien ompass eadin 0!0 =eiation 2W Cariation 12, *AS 160 /t%Whilst maintainin a radial 070 from a C?9 station the aircraft flies a ronddistance of 14 #$ in 6 $% What is the W:C (*)+

160:"0 /t 40:2" /t 40:!8 /t 1"":2" /t

061 ow man5 #$ wold an aircraft trael in 1 $ 4" S, if 3S is 1" /t+ %!4 2%6 %2" !%0

061;arallels of latitde on a =irect $ercator chart are parallel straiht lines neall5 spaced parallel straiht lines eall5 spaced arcs of concentric circles eall5 spaced straiht lines conerin a-oe the

pole

061 A chart has the scale 1 1 000 000% Brom A to on the chart measres 1%" inches(one inch eals 2%"4 centimetres) the distance from A to in #$ is

20%6 8%1 44%" "4%2

061ontor lines on aeronatical maps and charts connect points hain the same eleation a-oe sealeel

with the same ariation hain the same lonitde of eal latitde

061 A 9hm- line is a line on the srface of the earth cttinall meridians at the same anle

the shortest distance -etween twopoints on a ;ol5conic proection

an5 straiht line on a


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061 3ien $anetic trac/ > 1" P =3 > 01 P($) CA9 > "PW *AS > 22" /t

*he aircraft flies "0 #$ in 12 $% alclate the W:C(*)+

1!0 P:6 /t "" P:1" /t 1!" P:61 /t 1!" P:6 /t

061 ?ne prpose of compass cali-ration is to determine the deiation on an5 headin on a ien headin at an5 latitde on # S , and W onl5

061 An island appears 0 to the left of the centre line on an air-orne weather radar

displa5% What is the tre -earin of the aircraft from the island if at the time ofo-seration the aircraft was on a manetic headin of 276 with the maneticariation 12W+

0"4 18 24 08

061 3ien *re trac/ 180 =rift 89 ompass headin 1!" =eiation .2 alclate

the ariation%

21W 2"W "W !W

061ompass deiat ion is de fine d a s the anle -e twe en $a ne tic #or th a nd ompa ss #or th *re #or th a nd $a net ic #orth *re #or th a nd ompass #or th the hor i@ ontal a nd the total intensit5

of the earth's manetic field

061 3ien *re corse 00 drift 89 ariation 10W deiation .4 alclate thecompass headin%

06 22 2!4 278

061 3ien tre trac/ "2 ariation 11 W deiation is ." drift 109% alclate thecompass headin+

"8 46 018 02"

061 3ien tre trac/ 070 ariation 0W deiation H1 drift 109 alclate thecompass headin+

08! 0!1 100 101

061 *he anle -etween *re #orth and $anetic #orth is called ariation deiation compass error drift

061 =eiation applied to manetic headin ies compass headin tre headin manetic corse manetic trac/

061 A natical mile is 18"2 metres 160! metres 1012 metres 1"00metres

061 An aircraft flies the followin rhm- line trac/s and distances from position0400'# 0000'W 600 #$ Soth then 600 #$ ,ast then 600 #$ #orth then600 #$ West% *he final position of the aircraft is

0400'# 02!"8'W 0400'# 0002'W 0400'# 0000'W 0"8'# 0002'W

061 What is the final position after the followin rhm- line trac/s and distances hae-een followed from position 6000'# 0000'W+ Soth for 600 #$ ,ast for600 #$ #orth for 600 #$ West for 600 #$% *he final position of the

aircraft is

6000'# 0!000'W 6000'# 0000', "!00'# 06000'W "!00'# 0!000'W

061 3ien *AS > 270 /t *re =3 > 270 Actal wind 20"(*):0/t alclate

the drift anle and 3S+

69 . 2"!/t 6< . 2"6/t 69 . 2"1/t 89 . 2"!/t

061 3ien *AS > 270 /t *re =3 > 14" Actal wind > 20"(*):0/t% alclatethe drift anle and 3S+

6< . 2"6 /t 69 . 2"1 /t 89 . 261 /t 69 . 2"! /t

061 3ien *AS > 470 /t *re =3 > 17 W:C > 04"(*):4"/t alclate the drift

anle and 3S+

"< . 470 /t 9 . 470 /t "< . 47" /t "9 . 47" /t

061 3ien *AS > 140 /t *re =3 > 02 W:C > 04"(*):4"/t alclate the driftanle and 3S+

16< . 1"6 /t !9 . 14 /t !< . 146 /t 189 . 146 /t

061 3ien *AS > 2!0 /t *re =3 > 171 W:C > 10(*):0/t alclate the driftanle and 3S+

4< . 14 /t 49 . 10 /t 49 . 14 /t 4< . 10 /t

061 3ien *AS > 48" /t *re =3 > 226 W:C > 110(*):!"/t% alclate the drift

anle and 3S+

!9 . " /t 79 . "1 /t !9 . 4 /t 8< . 4" /t

061 3ien *AS > 1!0 /t *re =3 > 08" W:C > 110(*):"0/t% alclate the driftanle and 3S+

8< . 146 /t 7< . 1"6 /t 4< . 168 /t 4< . 14" /t

061 3ien *AS > 12 /t *re =3 > 2"7 W:C > 0!"(*):"/t% alclate the driftanle and 3S+

49 . 16" /t 29 . 166 /t 4< . 167 /t < . 166 /t

061 3ien *AS > 70 /t *re =3 > 181 W:C > 0!"(*):"/t% alclate the tretrac/ and 3S+

186 . 70 /t 176 . 70 /t 1!2 . 70 /t 18! . 70 /t

061 3ien *AS > 7" /t *re =3 > 124 W:C > 10(*):""/t% alclate the tretrac/ and 3S+

12 . 20 /t 12" . 22 /t 126 . 20 /t 12" . 18 /t

061 3ien *AS > 12" /t *re =3 > "" W:C > 20(*):0/t% alclate the tretrac/ and 3S+

00" . 102 /t 4" . 100 /t 48 . 102 /t 002 . !8 /t

061 3ien *AS > 1!8 /t =3 (*) > 180 W:C > "!:2"% alclate the *rac/(*)

and 3S+

180 . 22 /t 17! . 220 /t 181 . 180 /t 180 . 18 /t


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061 3ien *AS > 1" /t =3 (*) > 278 W:C > 140:20/t alclate the *rac/ (*)

and 3S+

28 . 1"0 /t 27! . 1"2 /t 272 . 121 /t 27" . 1"0 /t

061 3ien *AS > 22" /t =3 (*) > 12 W:C > 0!0:60/t% alclate the *rac/

(*) and 3S+

14 . 178 /t 14 . 188 /t 120 . 1!0 /t 128 . 180 /t

061 3ien *AS > 480 /t =3 (*) > 040 W:C > 0!0:60/t% alclate the *rac/(*) and 3S+

04 . 44" /t 028 . 41" /t 02 . 42" /t 06 . 4" /t

061 3ien *AS > 1"" /t =3 (*) > 216 W:C > 0!0:60/t% alclate the *rac/

(*) and 3S%

21 . 1!6 /t 224 . 17" /t 222 . 181 /t 226 . 186 /t

061 3ien *AS > 170 /t =3(*) > 100 W:C > "0:0/t% alclate the *rac/ (*)and 3S+

10! . 182 /t 0!1 . 18 /t 10 . 178 /t 0!8 . 178 /t

061 3ien *AS > 2" /t =3 (*) > 076 W:C > 040:40/t% alclate the drift anleand 3S+

79 . 204 /t 7< . 26! /t "< . 2"" /t "9 . 207 /t

061 3ien *AS > 440 /t =3 (*) > 4! W:C > 040:40/t% alclate the drift and3S+

4< . 41" /t 2< . 420 /t 6< . !" /t "< . 8" /t

061 3ien *AS > 46" /t =3 (*) > 124 W:C > 170:80/t% alclate the drift and3S+

8< . 41" /t < . 41" /t 4< . 400 /t 6< . 400 /t

061 3ien *AS > !" /t =3 (*) > 07" W:C > 10:20/t% alclate the drift and3S+

!9 . 108 /t 10< . 104 /t !< . 10" /t 89 . 104 /t

061 3ien *AS > 140 /t =3 (*) > 00" W:C > 26":2"/t% alclate the drift and3S+

109 . 146 /t !9 . 140 /t 119 . 142 /t 119 . 140 /t

061 3ien *AS > 1!0 /t =3 (*) > "" W:C > 16":2"/t% alclate the drift and3S+

1< . 21" /t 1< . 22" /t 19 . 17" /t 19 . 16" /t

061 3ien *AS > 20 /t =3 (*) > 2"0 W:C > 20":10/t% alclate the drift and3S+

29 . 22 /t 2< . 224 /t 1< . 22" /t 19 . 221 /t

061 3ien *AS > 20" /t =3 (*) > 180 W:C > 240:2"/t% alclate the drift and

3S+

6< . 1!4 /t 7< . 1!2 /t < . 1!0 /t 4< . 1!" /t

061 3ien *AS > 2"0 /t =3 (*) > 02! W:C > 0":4"/t% alclate the drift and3S+

1< . 20" /t 19 . 20" /t 1< . 26" /t 19 . 2!" /t

061 3ien *AS > 12 /t =3 (*) > 0" W:C > 20":1"/t% alclate the *rac/

(*) and 3S+

0"0 . 14" /t 0"7 . 144 /t 0"2 . 14 /t 0"1 . 144 /t

061 3ien *AS > !0 /t =3 (*) > "" W:C > 120:20/t% alclate the *rac/ (*)

and 3S+

46 . 102 /t 006 . !" /t "8 . 101 /t "! . 102 /t

061 3ien *AS > 48" /t =3 (*) > 168 W:C > 10:7"/t% alclate the *rac/(*) and 3S+

174 . 428 /t 17 . 424 /t 17" . 420 /t 17" . 42 /t

061 3ien *AS > 1"" /t *rac/ (*) > 0" W:C > 160:18/t% alclate the =3

(*) and 3S+

01 . 16! /t 0" . 16! /t 0! . 170 /t 0! . 141 /t

061 3ien *AS > 10 /t *rac/ (*) > 00 W:C > 1!0:40/t% alclate the =3(*) and 3S+

001 . 170 /t 002 . 17 /t "! . 166 /t "7 . 168 /t

061 3ien *AS > 227 /t *rac/ (*) > 16 W:C > 20":1"/t% alclate the =3(*) and 3S+

12 . 22 /t 11 . 20 /t 1 . 2" /t 10 . 2 /t

061 3ien *AS > 46" /t *rac/ (*) > 007 W:C > 00:80/t% alclate the =3(*) and 3S+

"8 . 428 /t 001 . 4" /t 017 . 4!0 /t "7 . "02 /t

061 3ien *AS > 200 /t *rac/ (*) > 07 W:C > 210:20/t% alclate the =3(*) and 3S+

077 . 214 /t 07! . 211 /t 07" . 21 /t 077 . 210 /t

061 3ien *AS > 200 /t *rac/ (*) > 110 W:C > 01":40/t% alclate the =3(*) and 3S+

0!! . 1!! /t 121 . 207 /t 121 . 1!! /t 0!7 . 201 /t

061 3ien *AS > 270 /t *rac/ (*) > 260 W:C > 27":0/t% alclate the =3(*) and 3S+

262 . 241 /t 262 . 27 /t 264 . 241 /t 264 . 27 /t

061 3ien *re =3 > 07 *AS > 20 /t *rac/ (*) > 1 3S > 210 /t%alclate the W:C+

260:0/t 2"7:"/t 2"":2"/t 26":0/t

061 3ien *re =3 > 2 *AS > 480 /t *rac/ (*) > 240 3S > "2 /t%alclate the W:C+

110:7"/t 11":70/t 110:80/t 10":7"/t

061 3ien *re =3 > 1 *AS > 22" /t *rac/ (*) > 144 3S > 206 /t% 07":4"/t 070:40/t 070:4"/t 07":"0/t


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alclate the W:C+

061 3ien *re =3 > 074 *AS > 20 /t *rac/ (*) > 066 3S > 242 /t%alclate the W:C+

180:"/t 180:0/t 18":"/t 180:40/t

061 3ien *re =3 > 206 *AS > 140 /t *rac/ (*) > 207 3S > 1" /t%alclate the W:C+

180:0"/t 000:0"/t 000:10/t 180:10/t

061 3ien *re =3 > 0"4 *AS > 4"0 /t *rac/ (*) > 0"! 3S > 416 /t%alclate the W:C+

010:"0/t 00":"0/t 010:""/t 010:4"/t

061 3ien *re =3 > 14" *AS > 240 /t *rac/ (*) > 1"0 3S > 210 /t%alclate the W:C+

11":"/t 60:"/t 180:"/t 2!":"/t

061 3ien *re =3 > 002 *AS > 10 /t *rac/ (*) > " 3S > 12 /t%

alclate the W:C+

0!":20/t 0!0:1"/t 0!0:20/t 0!":2"/t

061 3ien *re =3 > 0" *AS > 24" /t *rac/ (*) > 046 3S > 220 /t%alclate the W:C+

40:"0/t ":4"/t ":""/t 40:4"/t

061 3ien corse reired > 08" (*) Borecast W:C 00:100/t *AS > 470 /t=istance > 26" #$% alclate the tre =3 and fliht time+

07" ! $ 076 4 $ 0!6 2! $ 0!" 1 $

061 3ien *re corse from A to > 0!0 *AS > 460 /t W:C > 60:100/t

Aerae ariation > 10, =eiation > .2% alclate the compass headin and3S+

06! . 448 /t 068 . 460 /t 078 . 4"0 /t 070 . 4" /t

061 Bor a landin on rnwa5 2 (227 manetic) srface W:C reported -5 the A*&Sis 180:0/t% CA9 is 1,% alclate the cross wind component+

22 /t 26 /t 1" /t 20 /t

061 3ien $aimm allowa-le tailwind component for landin 10 /t% ;lannedrnwa5 0" (047 manetic)% *he direction of the srface wind reported -5 A*&S210% Cariation is 17,% alclate the maimm allowa-le wind speed that can

-e accepted withot eceedin the tailwind limit+

11 /t 18 /t 8 /t 1" /t

061 3ien $aimm allowa-le crosswind component is 20 /t% 9nwa5 06 9WG

J=$ 06($)% Wind direction 100($) alclate the maimm allowa-le windspeed+

/t 7 /t 26 /t 2" /t

061 3ien *re corse A to > 2"0 =istance A to > 1" #$ *AS > 4"0 /t%

W:C > 200:60/t% ,*= A > 06"0 F*% What is the ,*A at +

076 F* 070 F* 0810 F* 0716 F*

061 3ien 3S > "10 /t% =istance A to > 4 #$ What is the time ($) from A to

+

" 4 6 7

061 3ien 3S > 122 /t% =istance from A to > !8" #$% What is the time from A to+

8 9 04 $ 7 9 48 $ 7 9 4! $ 8 9 10 $

061 3ien 3S > 26 /t% =istance from A to > "4 #$ What is the ti me from A to

+

1 9 0 $ 1 9 0! $ 1 9 10 $ 1 9 40 $

061 3ien 3S > 4" /t% =istance from A to > 1!20 #$% What is the time from Ato +

4 9 2" $ 9 2" $ 9 26 $ 4 9 10 $

061 3ien 3S > 4" /t% =istance from A to > "60 #$% What is the time from Ato +

10 9 1! $ 10 9 0" $ 11 9 00 $ 11 9 02 $

061 3ien 3S > 480 /t% =istance from A to > "60 #$% What is the time from A

to +

11 9 10 $ 11 9 06 $ 11 9 07 $ 11 9 1" $

061 3ien 3S > !" /t% =istance from A to > 480 #$% What is the time from A to+

" 9 0 $ 4 9 "! $ " 9 00 $ " 9 08 $

061 3ien 3S > 10" /t% =istance from A to > 10 #$% What is the time from A to+

00 9 "! $ 00 9 "7 $ 00 9 "8 $ 01 9 01 $

061 3ien 3S > 120 /t% =istance from A to > 84 #$% What is the time from A to+

00 9 42 $ 00 9 4 $ 00 9 44 $ 00 9 4" $

061 3ien 3S > 1" /t% =istance from A to > 4 #$% What is the time from A to+

9 12 $ 9 2" $ 9 1! $ 9 20 $

061 A straiht line is drawn on a


10/23


and to cross the facilit5 at B


11/23


is the minimm rate of descent reired+

061 An aircraft o-tains a relatie -earin of 1" from an #= at 080% At 0840 therelatie -earin from the same #= is 270% Assmin no drift and a 3S of 240

/t what is the approimate rane from the #= at 0840+

40 #$ "0 #$ 60 #$ 0 #$

061 *he eialent of 70 m:sec is approimatel5 16 /t 14" /t 210 /t " /t

061 An aircraft at B


12/23


061 A fliht is to -e made from 'A' 4!S 180,:W to '' "8S 180,:W% *he distance

in /ilometres from 'A' to '' is approimatel5

1000 1222 "40 804

061 An aircraft at position 60# 00"W trac/s 0!0(*) for 1" /m% ?n completion of

the fliht the lonitde will -e

00040', 00"1"', 00210'W 0001"',

061 *he 'departre' -etween positions 60# 160, and 60# '' is !00 #$% What isthe lonitde of ''+

170W 140W 14", 17",

061 An aircraft at latitde 0220'# trac/s 180(*) for 68" /m% ?n completion of the

fliht the latitde will -e

0"0'S 0410'S 040'S 0!0"'S

061 An aircraft at latitde 10 Soth flies north at a 3S of 8!0 /m:r% What will itslatitde -e after 1%" 9+

0200'# 121"'# 2200'# 0"0'#

061 An aircraft at latitde 10#orth flies soth at a rondspeed of 44" /m:r% Whatwill -e its latitde after 9+

0200'S 121"'S 2200'S 0"0'S

061 *he main reason for montin the detector nit of a remote readin compass inthe wintip of an aeroplane is

to minimise the amont of deiationcased -5 aircraft manetism andelectrical circits

to maimise the nits eposre tothe earth's manetic field

to ensre that the nit is in the mostaccessi-le position on the aircraft forease of maintenance

-5 hain detector nits on -othwintips to cancel ot the deiationeffects cased -5 the aircraft

strctre

061?n a tra nse rse $e rc ator char t the sc ale is ea ct l5 cor re ct alon the me ridia ns of ta ne nc 5 e a tor and paral le l of oriin me ridian of ta ne nc 5 a nd the pa ra llel oflatitde perpendiclar to it

prime meridian and the eator

061 ?n a transerse $ercator chart with the eception of the ,ator parallels of

latitde appear as

ellipses straiht lines h5per-olic lines para-olas

061An ?-lie $ercator proection is sed specificall5 to prodce charts of the reat circle rote -etween

two points

radio naiational charts in

eatorial reions

toporaphical maps of lare east: west

etent

plottin charts in eatorial reions

061 *ranserse $ercator proections are sed for maps of lare north:soth etent maps of lare east:west etent ineatorial areas

radio naiation charts in eatorialareas

plottin charts in eatorial areas

061 3ien =istance A to > 120 #$ After 0 #$ aircraft is #$ to the left of

corse% What headin alteration shold -e made in order to arrie at point ''+

8 riht 6 riht 4 riht 8 left

061 An aircraft was oer 'A' at 14" hors fl5in direct to ''% 3ien =istance 'A' to'' 2!00 #$ *re airspeed 470 /t $ean wind component 'ot' H"" /t $ean wind

component '-ac/' .7" /t *he ,*A for reachin the ;oint of ,al *ime (;,*)-etween 'A' and '' is

16"7 1744 1846 1721

061 An aircraft was oer 'A' at 14" hors fl5in direct to ''% 3ien =istance 'A' to'' 2!00 #$ *re airspeed 470 /t $ean wind component 'ot' H"" /t $ean windcomponent '-ac/' .7" /t Safe endrance ! 9 0 $ *he distance from 'A' to

the ;oint of Safe 9etrn (;S9) 'A' is

2141 #$ 1611 #$ 17"! #$ 2844 #$

061 3ien =istance 'A' to '' 2484 #$ 3rondspeed 'ot' 420 /t 3rondspeed '-ac/'"00 /t *he time from 'A' to the ;oint of ,al *ime (;,*) -etween 'A' and '' is

1! $ 16 $ 17 $ 18 $

061 3ien =istance 'A' to '' 2484 #$ $ean rondspeed 'ot' 420 /t $eanrondspeed '-ac/' "00 /t Safe endrance 08 9 0 $ *he distance from 'A'

to the ;oint of Safe 9etrn (;S9) 'A' is

1!40 #$ 1!08 #$ 176 #$ 160 #$

061 An aircraft was oer 'J' at 120 hors fl5in direct to '9'% 3ien =istance 'J' to

'9' 016 #$ *re airspeed 480 /t $ean wind component 'ot' .!0 /t $ean windcomponent '-ac/' H7" /t *he ,*A for reachin the ;oint of ,al *ime (;,*)-etween 'J' and '9' is

17"2 17"6 1820 1742

061 An aircraft was oer 'J' at 120 hors fl5in direct to '9'% 3ien =istance 'J' to'9' 016 #$ *re airspeed 480 /t $ean wind component 'ot' .!0 /t $ean windcomponent '-ac/' H7" /t Safe endrance 1000 9 *he distance from 'J' to the

;oint of Safe 9etrn (;S9) 'J' is

22!0 #$ 270 #$ 110 #$ 1"10 #$

061 3ien =istance 'A' to '' 1!7 #$ 3rondspeed 'ot' 40 /t 3rondspeed '-ac/'8" /t *he time from 'A' to the ;oint of ,al *ime (;,*) -etween 'A' and '' is

10 $ 14" $ 162 $ 181 $

061 3ien =istance 'A' to '' 1!7 #$ 3rondspeed 'ot' 40 /t 3rondspeed '-ac/'

8" /t Safe endrance 7 9 20 $ *he distance from 'A' to the ;oint of Safe9etrn (;S9) 'A' is

14!0 #$ 1664 #$ 16!8 #$ 1422 #$

061 3ien =istance 'A' to '' 246 #$ 3rondspeed 'ot' 6" /t 3rondspeed '-ac/'480 /t *he time from 'A' to the ;oint of ,al *ime (;,*) -etween 'A' and '' is

21! $ 2!0 $ 1!7 $ 167 $


13/23


061 3ien =istance 'A' to '' 246 #$ 3rondspeed 'ot' 6" /t 3rondspeed '-ac/'

480 /t Safe endrance 8 9 0 $ *he time from 'A' to the ;oint of Safe9etrn (;S9) 'A' is

2!0 $ 21! $ 1!7 $ 20! $

061 3ien =istance 'J' to '9' 1760 #$ 3rondspeed 'ot' 4" /t 3rondspeed '-ac/'8" /t *he time from 'J' to the ;oint of ,al *ime (;,*) -etween 'J' and '9' is

114 $ 110 $ 106 $ 102 $

061 3ien =istance 'J' to '9' 1760 #$ 3rondspeed 'ot' 4" /t 3rondspeed '-ac/'

8" /t Safe endrance ! 9 *he distance from 'J' to the ;oint of Safe 9etrn(;S9) -etween 'J' and '9' is

188 #$ 11 #$ 1467 #$ 1642 #$

061 3ien =istance 'A' to '' 62 #$ 3rondspeed 'ot' 70 /t 3rondspeed '-ac/'00 /t *he time from 'A' to the ;oint of ,al *ime (;,*) -etween 'A' and '' is

26 $ 288 $ 2 $ 28 $

061 A rond featre was o-sered on a relatie -earin of 1" and $ later on arelatie -earin of 270% *he W:C is calmE aircraft 3S 180 /t% What is theminimm distance -etween the aircraft and the rond featre+

! #$ 12 #$ #$ 6 #$

061 An island is o-sered to -e 1" to the left% *he aircraft headin is 120($)ariation 17(W)% *he -earin (*) from the aircraft to the island is

088 122 268 02

061 An aircraft is planned to fl5 from position 'A' to position '' distance 480 #$ atan aerae 3S of 240 /t% &t departs 'A' at 1000 F*% After fl5in 1"0 #$ alontrac/ from 'A' the aircraft is 2 $ -ehind planned time% Fsin the actal 3Seperienced what is the reised ,*A at ''+

1206 120 11" 11"7

061 An aircraft is planned to fl5 from position 'A' to position '' distance 20 #$ at

an aerae 3S of 180 /t% &t departs 'A' at 1200 F*% After fl5in 70 #$ alontrac/ from 'A' the aircraft is $ ahead of planned time% Fsin the actal 3Seperienced what is the reised ,*A at ''+

1 F* 1401 F* 147 F* 140 F*

061 An aircraft is planned to fl5 from position 'A' to position '' distance 2"0 #$ atan aerae 3S of 11" /t% &t departs 'A' at 0!00 F*% After fl5in 7" #$ alontrac/ from 'A' the aircraft is 1%" $ -ehind planned time% Fsin the actal 3S

eperienced what is the reised ,*A at ''+

111" F* 1110 F* 1044 F* 10"0 F*

061 3ien $anetic trac/ > 07" =3 > 066($) CA9 > 11, *AS > 27" /t

Aircraft flies 48 #$ in 10 $% alclate the tre W:C +

40:4" /t 20:"0 /t 210:1" /t 180:4" /t

061 3ien $anetic trac/ > 210 $anetic =3 > 21" CA9 > 1", *AS > 60/t Aircraft flies 64 #$ in 12 $% alclate the tre W:C+

26":"0 /t 1!":"0 /t 2":"0 /t 00:0 /t

061 3ien =istance 'A' to '' is 47" #$ ;lanned 3S 1" /t A*= 1000 F* 1040

F* . fi o-tained 1!0 #$ a lon trac/% What 3S mst -e maintained from thefi in order to achiee planned ,*A at ''+

40 /t 60 /t% 00 /t 20 /t%

061 3ien =istance 'A' to '' is 2" #$ ;lanned 3S 1" /t A*= 110 F* 120"F* . fi o-tained 16" #$ a lon trac/% What 3S mst -e maintained from the

fi in order to achiee planned ,*A at ''+

"" /t 7" /t !" /t " /t

061 3ien =istance 'A' to '' is 100 #$ Bi o-tained 40 #$ alon and 6 #$ to theleft of corse% What headin alteration mst -e made to reach ''+

1" 9iht ! 9iht 6 9iht 18 9iht

061 3ien =istance 'A' to '' is !0 #$ Bi o-tained 60 #$ alon and 4 #$ to the

riht of corse% What headin alteration mst -e made to reach ''+

12


14/23


accelerometer of an inertial naiation s5stem (S) in #AC $?=, is latitde

061 Which of the followin lists which compares an &nertial 9eference S5stem thattilises 9in


15/23


061 (Bor this estion se anne 061.12"4!A to 061.1261A) What is the radial and

=$, distance from 9O C?9:=$, (#"1"0%4 W0082!%7) to position #"20W007"0+

0! . 48 #$ 024 . 4 #$ 02 . 48 #$ 017 . 4 #$

061 (Bor this estion se anne 061.12"4!A to 061.1261A) What is the radial and=$, distance from 9O C?9:=$, (#"1"0%4 W0082!%7) to position #"140W0070+

11 . 8 #$ 104 . 76 #$ 2! . ! #$ 106 . 8 #$

061 (Bor this estion se anne 061.12"4!A to 061.1261A) What is the radial and=$, distance from SA C?9:=$, (#"24% W008"%1) to position #"00W00!40+

0! . #$ 0"7 . 27 #$ 2! . #$ 24 . 17 #$

061 (Bor this estion se anne 061.12"4!A to 061.1261A) What is the radial and=$, distance from SA C?9:=$, (#"24% W008"%1) to position #"10

W0080+

0" . 0 #$ 070 . "8 #$ 207 . 1 #$ 01! . 1 #$

061 (Bor this estion se anne 061.12"4!A to 061.1261A) What is the radial and=$, distance from SA C?9:=$, (#"24% W008"%1) to position #"220

W00810+

1! . " #$ 12! . 46 #$ 12 . 6 #$ 212 . 26 #$

061 (Bor this estion se anne 061.12"4!A to 061.1261A) What is the radial and=$, distance from SA C?9:=$, (#"24% W008"%1) to position #"210W00!20+

214 . 7 #$ "4 . 4 #$ 1!8 . 7 #$ 46 . 4 #$


=$, distance from ?# C?9:=$, (#""4%8 W0084!%1) to position #"40W00!00+

"8 . 6 #$ 214 . 26 #$ 04! . 4" #$ 16! . " #$

061 (Bor this estion se anne 061.12"4!A to 061.1261A) What is the radial and=$, distance from ?# C?9:=$, (#""4%8 W0084!%1) to position #"400

W00800+

088 . 2! #$ 20 . 8 #$ 0!4 . 64 #$ 260 . 0 #$

061 (Bor this estion se anne 061.12"4!A to 061.1261A) What is the radial and=$, distance from ?# C?9:=$, (#""4%8 W0084!%1) to position #"40

W00820+

140 . 2 #$ 11! . 42 #$ 11 . 22 #$ 240 . 24 #$


=$, distance from ?# C?9:=$, (#""4%8 W0084!%1) to position #"0W00!0+

2 . " #$ 16" . 27 #$ " . 4 #$ 02" . 8 #$


=$, distance from ,< C?9:=$, (#"4!%7 W0061%8) to position #"410W00710+

26 . 44 #$ 22 . 6 #$ 20 . 44 #$ . 6 #$

061 (Bor this estion se anne 061.12"4!A to 061.1261A) What is the radial and=$, distance from ,< C?9:=$, (#"4!%7 W0061%8) to position #"440W0070+

278 . 44 #$ 0!0 . 46 #$ 278 . 10 #$ 0!8 . 4" #$

061 (Bor this estion se anne 061.12"4!A to 061.1261A) What is the radial and=$, distance from ,< C?9:=$, (#"4!%7 W0061%8) to position #""00W00700+

1" . 4 #$ 2!6 . 6" #$ 126 . #$ 222 . 48 #$

061 (Bor this estion se anne 061.12"4!A to 061.1261A) What is the aeraetrac/ ($) and distance -etween W*= #= (#"211% W0070"%0) and O,9

#= (#"210%! W00!1%")+

278 . !0 #$ 0!0 . !1 #$ 270 . 8! #$ 0!8 . !0 #$

061 (Bor this estion se anne 061.12"4!A to 061.1261A) What is the aeraetrac/ ($) and distance -etween 9O C?9 (#"1"0%4 W0082!%7) and 9#

#= (#"18%1 W008"6%")+

"7 . 8! #$ 16! . !1 #$ 4! . !0 #$ 177 . !2 #$

061 (Bor this estion se anne 061.12"4!A to 061.1261A) What is the aeraetrac/ ($) and distance -etween 9# #= (#"18%1 W008"6%") and W*=

#= (#"211% W0070"%0)+

142 . !" #$ 1" . !4 #$ 1" . !6 #$ 22 . !" #$

061 (Bor this estion se anne 061.12"4!A to 061.1261A) What is the aeraetrac/ ($) and distance -etween W*= #= (#"211% W0070"%0) and A 27 B*)

1680 B* 20 B* 680 B* . 20 B*

061 *he circmference of the parallel of latitde at 60# is approimatel5 10 800 #$ 18 706 #$ 20 000 #$ 4 641 #$

061 $ornin iil twiliht -eins when the centre of the sn is 6 -elow the

celestial hori@on

the centre of the sn is 12 -elow the

celestial hori@on

the centre of the sn is 18 -elow the

celestial hori@on

the sn's pper ede is tanential to

the celestial hori@on

061 Seasons are de to the inclination of the polar ais with the

ecliptic plane

,arth's elliptical or-it arond the

Sn

,arth's rotation on its polar ais aria-le distance -etween ,arth and

Sn061 3ien ;osition 'A' #60 W020 ;osition '' #60 W021 ;osition '' #"! W020%

What are respectiel5 the distances from A to and from A to +0 #$ and 60 #$ "2 #$ and 60 #$ 60 #$ and 0 #$ 60 #$ and "2 #$

061 3ien *re altitde !000 B* ?A* .2 AS 200 /t% What is the *AS+ 220 /t 21" /t 200 /t 210 /t

061 3ien An aircraft is fl5in a trac/ of 2""($) 22"4 F* it crosses radial 60

from a C?9 station 200 F* it crosses radial 0 from the same station% At200 F* the distance -etween the aircraft and the station is

the same as it was at 22"4 F* reater than it was at 22"4 F* randoml5 different than it was at 22"4

F*

less than it was at 22"4 F*

061 *he distance -etween two wa5points is 200 #$ *o calclate compass headinthe pilot sed 2, manetic ariation instead of 2W% Assmin that the forecastW:C applied what will the off trac/ distance -e at the second wa5point+

14 #$ 7 #$ 0 #$ 21 #$

061 *he scale on a


19/23


061 ;arallels of latitde ecept the eator are 9hm- lines 3reat circles -oth 9hm- lines and 3reat circles are neither 9hm- lines nor 3reat

circles

061 3ien B


20/23


wa5.point A to % *he inertial s5stems' entral =ispla5 Fnits (=F) shows .

L*O on S 1 > 0 . L*O on S 2 > 8< (L*O > cross trac/) Brom thisinformation it can -e dedced that

061 (Bor this estion se anne 061.12"4!A to 061.1261A) What is the radial and=$, distance from 9O C?9:=$, (#"1"0%4 W0082!%7) to position #"220W00810+

00 . #$ 048 . 40 #$ 014 . #$ 220 . 40 #$

061 (Bor this estion se anne 061.12"4!A to 061.1261A) What is the radial and=$, distance from 9O C?9:=$, (#"1"0%4 W0082!%7) to position #"210W00!20+

11 . 8 #$ "0 . 22 #$ 2!" . 8 #$ 170 . 22 #$

061 (Bor this estion se anne 061.12"4!A to 061.1261A) What is the aeraetrac/ ($) and distance -etween A< C?9 (#"18%0 W00626%!) and S


21/23


061 (Bor this estion se anne 061.12"4!A to 061.1261A) 3ien SA

C?9:=$, (#"24% W008"%1) radial 120:" #$% What is the aircraftposition+

#"20 W00800 #"00 W00!4" #"22" W0080" #"2"0 W00!"0

061 (Bor this estion se anne 061.12"4!A to 061.1261A) 3ien SAC?9:=$, (#"24% W008"%1) radial 16":6 #$% What is the aircraft

position+

#"210 W0080 #"208 W00840 #"1" W00!1" #"17 W00!08

061 (Bor this estion se anne 061.12"4!A to 061.1261A) 3ien SAC?9:=$, (#"24% W008"%1) radial 22:2 #$% What is the aircraft

position+

#"220 W00!0 #"0" W0081" #"228 W00!" #"0 W00810

061 (Bor this estion se anne 061.12"4!A to 061.1261A) 3ien SAC?9:=$, (#"24% W008"%1) radial 02":4! #$% What is the aircraft

position+

#"0 W0080 #"28 W00820 #"1"" W00!1" #"200 W0!2"

061 (Bor this estion se anne 061.12"4!A to 061.1261A) 3ien SAC?9:=$, (#"24% W008"%1) radial 048:22 #$% What is the aircraft

position+

#"00 W080 #"2"8 W0082" #"22" W00!17 #"228 W00!20

061 (Bor this estion se anne 061.12"4!A to 061.1261A 3ien SA C?9#"24% W008"%1 9O C?9 #"1"0%4 W0082!%7 Aircraft position #"220W00!10 Which of the followin lists two radials that are applica-le to the aircraft

position+

SA 214 9O 0 SA 02" 9O 141 SA 20" 9O 21 SA 0 9O 14!

061 (Bor this estion se anne 061.12"4!A to 061.1261A) 3ien SA C?9#"24% W008"%1 9O C?9 #"1"0%4 W0082!%7 Aircraft position #"20W00820 Which of the followin lists two radials that are applica-le to the aircraft

position+

SA 11 9O 017 SA 04 9O 18! SA 12 9O 1!7 SA 124 9O 00!

061 (Bor this estion se anne 061.12"4!A to 061.1261A) 3ien SA C?9#"24% W008"%1 9O C?9 #"1"0%4 W0082!%7 Aircraft position #"20W00!0 Which of the followin lists two radials that are applica-le to the aircraft

position+

SA 248 9O 2" SA 068 9O 14" SA 060 9O 18 SA 240 9O 17

061 (Bor this estion se anne 061.12"4!A to 061.1261A) 3ien SA C?9#"24% W008"%1 ?# C?9 #""4%8 W0084!%1 Aircraft position #"0W00800 Which of the followin lists two radials that are applica-le to the aircraft

position+

SA 042 ?# 18 SA 21 ?# 10 SA 0 ?# 10 SA 221 ?# 18

061 (Bor this estion se anne 061.12"4!A to 061.1261A) 3ien SA C?9#"24% W008"%1 ?# C?9 #""4%8 W0084!%1 Aircraft position #"20W00!"0 Which of the followin lists two radials that are applica-le to the aircraft

position+

SA 2" ?# 2" SA 17 ?# 046 SA 17 ?# 226 SA 14" ?# 0""

061 (Bor this estion se anne 061.12"4!A to 061.1261A) 3ien SA C?9(#"24% W008"%1) =$, "0 #$ 9O C?9 (#"1"0%4 W0082!%7) =$, 41

#$ Aircraft headin 270($) oth =$, distances increasin% What is the

aircraft position+

#"200 W00!" #"21" W00!40 #"21" W0074" #"2" W007"0

061 (Bor this estion se anne 061.12"4!A to 061.1261A) 3ien SA C?9

(#"24% W008"%1) =$, 41 #$ 9O C?9 (#"1"0%4 W0082!%7) =$, 0

#$ Aircraft headin 270($) oth =$, distances decreasin% What is theaircraft position+

#"21" W0080" #"20" W00!1" #"21" W00!1" #"22" W00810

061 (Bor this estion se anne 061.12"4!A to 061.1261A) 3ien 9# C?9(#"18%1 W008"6%") =$, 18 #$ SA C?9 (#"24% W008"%1) =$, 0

#$ Aircraft headin 270($) oth =$, distances decreasin% What is the

aircraft position+

#"10 W0080 #"2"2 W00!2 #"07 W00!2 #""" W0082"

061 (Bor this estion se anne 061.12"4!A to 061.1261A) 3ien 9# C?9

(#"18%1 W008"6%") =$, 4 #$ SA C?9 (#"24% W008"%1) =$, 26#$ Aircraft headin 0!0($) oth =$, distances increasin% What is theaircraft position+

#"2"" W0081" #"2"0 W000 #"0" W00!0 #"10 W00820

061 (Bor this estion se anne 061.12"4!A to 061.1261A) 3ien ?# C?9(#""4%8 W0084!%1) =$, 0 #$ 9# C?9 (#"18%1 W008"6%") =$, 2"

#$ Aircraft headin 270($) oth =$, distances decreasin% What is theaircraft position+

#"0 W00820 #"4 W00!2" #"" W00!2" #"7 W00820


22/23


061 (Bor this estion se anne 061.12"4!A to 061.1261A) 3ien 9O

C?9:=$, (#"1"0%4 W0082!%7) Oerr5 aerodrome (#"210%! W00!1%4) What isthe 9O radial and =$, distance when oerhead Oerr5 aerodrome+

07 . 4 #$ 11! . 44 #$ 127 . 4" #$ 2!! . 42 #$

061 (Bor this estion se anne 061.12"4!A to 061.1261A) 3ien SAC?9:=$, (#"24% W008"%1) irr aerodrome (#"04 W007"4) What is theSA radial and =$, distance when oerhead irr aerodrome+

068 . 41 #$ 248 . 42 #$ 060 . 42 #m 240 . 41 #$

061 (Bor this estion se anne 061.12"4!A to 061.1261A) 3ien SAC?9:=$, (#"24% W008"%1) onnemara aerodrome (#"14 W00!28) Whatis the SA radial and =$, distance when oerhead onnemara aerodrome+

. 7 #$ 1"4 . 8 #$ 26 . 7 #$ 146 . 8 #$

061 (Bor this estion se anne 061.12"4!A to 061.1261A) 3ien ?#C?9:=$, (#""4%8 W0084!%1) astle-ar aerodrome (#""1 W00!17) What is

the ?# radial and =$, distance when oerhead astle-ar aerodrome+

26" . 17 #$ 077 . 18 #$ 2"7 . 17 #$ 086 . 18 #$

061 (Bor this estion se anne 061.12"4!A to 061.1261A) 3ien ?#C?9:=$, (#""4%8 W0084!%1) A--e5 Shrle aerodrome (#"" W007!)

What is the ?# radial and =$, distance when oerhead A--e5 Shrleaerodrome+

12 . 46 #$ 116 . 47 #$ 2!6 . 46 #$ 04 . 47 #$

061 (Bor this estion se anne 061.12"4!A to 061.1261A) What featre is shownon the chart at position #"211 W00!1+

O,99G:Barranfore aerodrome Waterford #= onnemara aerodrome ;nchestown aerodrome

061 (Bor this estion se anne 061.12"4!A to 061.1261A) What featre is shown

on the chart at position #"212 W00612+

*FSOA9 9?O


23/23


aeronatical chart s5m-ols indicates a C?9*A+

061 (Bor this estion refer to anne 061.12621A to 061.1268A) Whichaeronatical chart s5m-ol indicates a Bliht &nformation 9eion (B&9) -ondar5+

1 4 "

061 (Bor this estion refer to anne 061.12621A to 061.1268A) Whichaeronatical chart s5m-ol indicates a ontrol one -ondar5+

4 " 2

061 (Bor this estion refer to anne 061.12621A to 061.1268A) Whichaeronatical chart s5m-ol indicates an ncontrolled rote+

4 " 2

061 (Bor this estion refer to anne 061.12621A to 061.1268A) Whichaeronatical chart s5m-ol indicates the -ondar5 of adisor5 airspace+

" 2 4

061 (Bor this estion refer to anne 061.12621A to 061.1268A) Which

aeronatical chart s5m-ol indicates a non.complsor5 reportin point+

6 7 8 1"

061 (Bor this estion refer to anne 061.12621A to 061.1268A) Whichaeronatical chart s5m-ol indicates a complsor5 reportin point+

7 8 1" 6

061 (Bor this estion refer to anne 061.12621A to 061.1268A) Whichaeronatical chart s5m-ol indicates a Wa5.point+

8 1" 6 7


aeronatical chart s5m-ol indicates an nlihted o-stacle+

! 10 11 12

061 (Bor this estion refer to anne 061.12621A to 061.1268A) Whichaeronatical chart s5m-ol indicates a lihted o-stacle+

10 11 12 !


aeronatical chart s5m-ol indicates a rop of nlihted o-stacles+

11 12 1 !


aeronatical chart s5m-ol indicates a rop of lihted o-stacles+

12 ! 10 11

061 (Bor this estion refer to anne 061.12621A to 061.1268A) Whichaeronatical chart s5m-ol indicates an eceptionall5 hih nlihted o-stacle+

1 14 ! 11

061 (Bor this estion refer to anne 061.12621A to 061.1268A) Whichaeronatical chart s5m-ol indicates an eceptionall5 hih lihted o-stacle+

14 10 12 1

061 (Bor this estion refer to anne 061.12621A to 061.1268A) What is themeanin of aeronatical chart s5m-ol #o% 1"+

Aeronatical rond liht Cisal reference point a@ard to aerial naiation

Date post:	04-Jun-2018
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