Flight Planning _ Monitoring ( 629 Soru OK.b )

----------------------------------------------------------------------------------------------------------------------------------------------------------------A “current flight plan” is a ; filed flight plan with amendments and clearance included. a) b) flight plan in the course of which which radio radio communication communication should should be practised practised between between aeroplane and ATC. filed flight plan. c) flight plan with the correct time of departure. d)

001.

Answer ; a)

filed flight plan with amendments and clearance included. ----------------------------------------------------------------------------------------------------------------------------------------------------------------002. ( For this this question use anne !""-#$"%&A or Flight 'lanning anual )*T # Figure +.,.+ 

Annex 033-12367A 033-12367A A descent is planned at .&+$,! /0A1 from ",!!! ft to ,!!! ft. 2ow much fuel will be consumed during this descent 3 #,! 4g a) b) $&5 4g $6! 4g c) #+! 4g d) Answer ; a)

#,! 4g ----------------------------------------------------------------------------------------------------------------------------------------------------------------A descent is planned from &,!! ft A17 so as to arri8e at #!!! ft A17 % 9 from a :)TAC. :)TAC.
$&.# 9 -----------------------------------------------------------------------------------------------------------------------------------------------------------------

Ateş Murat Üstünbıçak , ATP ATPL L

#

Flight Planning & Monitoring Monitoring

004.

( For this this question use anne !""-+%$"A or Flight 'lanning anual >' # Figure "." 

Annex 033-4623A 033-4623A A flight has to be made with a multi engine piston aeroplane ( >' # . For the fuel calculations ta4e , ?1 gallons for the tai @ and an additional #" minutes at cruise condition to account for climb and descent. Calculated time from o8erhead to o8erhead is #h +&min. 'ower setting is +, @ $%!! )'. Calculated reser8e fuel is "! of the trip fuel. F7 #!!. Temperature -,BC. Find the minimum bloc4 fuel ; +&! ?1 gallons. a) "& ?1 gallons. b) +& ?1 gallons. c) %! ?1 gallons. d) Answer ; c)

+& ?1 gallons. -----------------------------------------------------------------------------------------------------------------------------------------------------------------


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005.

( For this this question use anne !""-+%$"A or Flight 'lanning anual >' # Figure "." 

Annex 033-4623A 033-4623A A flight has to be made with a multi engine piston aeroplane ( >' # . For the fuel calculations ta4e , ?1 gallons for the tai @ and an additional #" minutes at cruise condition to account for climb and descent. Calculated time from o8erhead to o8erhead is $ h "& min. 'ower setting is %, @ $,!! )'. Calculated reser8e fuel is "! of the trip fuel. F7 #$!. Temperature #BC. Find the minimum bloc4 fuel ; 6# ?1 gallons. a) &% ?1 gallons. b) 5% ?1 gallons. c) ##5 ?1 gallons. d) Answer ; a)

6# ?1 gallons. -----------------------------------------------------------------------------------------------------------------------------------------------------------------


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006.

( For this this question use anne !""-6&""A or Flight 'lanning anual 1>'# Figure $.$ Table Table $.$." 

Flight Planning Manual SEP1 Figure 2.2 Table 2.2.3 A flight has to be made with the single engine sample aeroplane. For the fuel calculation allow #! lbs fuel for start up and tai @ " minutes and # gallon of additional fuel to allow for the climb @ #! minutes and no fuel correction for the descent.'lanned flight time ( o8erhead to o8erhead  is !$ hours and "& minutes.)eser8e fuel "! of the trip fuel.'ower setting is $" in.2= ( or full throttle  @ $"!! )' @ $!BC lean. Flight le8el is ,! and the AT -,BC. The minimum bloc4 fuel is ; $%, lbs a) $,! lbs b) $!5 lbs c) $&! lbs d) Answer ; a)

$%, lbs -----------------------------------------------------------------------------------------------------------------------------------------------------------------


+


007.

( For this this question use anne !""-6&"$A or Flight 'lanning anual 1>'# Figure $.$ Table Table $.$.$ 

Annex 033-9732A 033-9732A A flight has to be made with the single engine sample aeroplane. For the fuel calculation allow #! lbs fuel for start up and tai @ " minutes and # gallon of additional fuel to allow for the climb @ #! minutes and no fuel correction for the descent.'lanned flight time ( o8erhead to o8erhead  is !" hours and #$ minutes.)eser8e fuel "! of the trip fuel.'ower setting is $, in.2= ( or full throttle  @ $#!! )' @ $!BC lean.Flight le8el is &! and the AT ##BC. ##BC. The minimum bloc4 fuel is ; $,$ lbs a) $5" lbs b) $%5 lbs c) $#, lbs d) Answer ; b)

$5" lbs -----------------------------------------------------------------------------------------------------------------------------------------------------------------


,


008.

( For this question use Flight 'lanning anual 1>'# Figure $.$ Table Table $.$." 

Flight Planning Manual SEP1 Figure 2.2 Table 2.2.3 A flight has to be made with the single engine sample aeroplane. For the fuel calculation allow #! lbs fuel for start up and tai @ " minutes and % lbs of additional fuel to allow for the climb @ #! minutes and no fuel correction for the descent. 'lanned flight time ( o8erhead to o8erhead  is !$ hours and "& minutes.)eser8e fuel "! of the trip fuel.'ower setting is $" in.2= ( or full throttle  @ $"!! )' @ $!BC lean. Flight le8el is ,! and the 1tandard aD ( 01A . The minimum bloc4 fuel is ; $,% lbs a) $%! lbs b) $&% lbs c) $5# lbs d) Answer ; c)

$&% lbs -----------------------------------------------------------------------------------------------------------------------------------------------------------------


%


009.

( For this question use Flight 'lanning anual 1>'# Figure $.$ Table $.$." 

Flight Planning Manual SEP1 Figure 2.2 Table 2.2.3 A flight has to be made with the single engine sample aeroplane. For the fuel calculation allow #! lbs fuel for start up and tai @ " minutes and #! lbs of additional fuel to allow for the climb @ #! minutes and no fuel correction for the descent. 'lanned flight time ( o8erhead to o8erhead  is !" hours and #$ minutes.)eser8e fuel "! of the trip fuel.'ower setting is $" in.2= ( or full throttle  @ $"!! )' @ $!BC lean. Flight le8el is &! and AT is 01A E $!C. The minimum bloc4 fuel is ; $56 lbs a) "$, lbs b) "!% lbs c) "+6 lbs d) Answer ; b)

"$, lbs -----------------------------------------------------------------------------------------------------------------------------------------------------------------


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010.

( For this question use anne !""-""!#A or Flight 'lanning anual >'# Figure ".# 

Annex 033-3301A 033-3301A A flight is to be made from one airport ( ele8ation "!!! ft  to another in a multi engine piston aeroplane ( >'# . The cruising le8el will be F7 ##!. The temperature at F7 ##! is 01A -#!B C. The temperature at the departure aerodrome is -#B C. Calculate the fuel to climb with miture rich ; #$ ?1 gallon a) 6 ?1 gallon b) " ?1 gallon c) % ?1 gallon d) Answer ; d)

% ?1 gallon -----------------------------------------------------------------------------------------------------------------------------------------------------------------


5


011.

( For this this question use anne !""-""$&A or Flight 'lanning anual >' # Figure ".$ 

Annex 033-3327A 033-3327A A flight is to be made in a multi engine piston aeroplane ( >'# . The cruising le8el will be ##!!! ft. The outside air temperature at F7 is -#, B C. The usable fuel is #$" ?1 gallons. The power is set to economic cruise. Find the range in 9 with +, min reser8e fuel at +,  power ; 5,$ 9 a) b) %!$ 9 %#! 9 c) &,$ 9 d) Answer ; d)

&,$ 9 -----------------------------------------------------------------------------------------------------------------------------------------------------------------


6


012.

( For this question use anne !""-""!$A or Flight 'lanning anual >'# Figure ".% 

Annex 033-3302A 033-3302A A flight is to be made to an airport @ pressure altitude "!!! ft @ in a multi engine piston aeroplane ( >'# . The forecast AT for the airport is -#B C. The cruising le8el will be F7 ##! @ where AT is -#!B C. Calculate the still air descent distance for ; #+, /0A1 @ )ate of descent #!!! ftmin @ =ears and flaps up ; a) "% 9 $! 9 b) $6 9 c) $, 9 d) Answer ; b)

$! 9 ----------------------------------------------------------------------------------------------------------------------------------------------------------------A Get aeroplane has a cruising fuel consumption of +!%! 4gh @ and "%6! 4gh during holding. 0f the destination is an isolated 013. airfield @ the aeroplane must carrD @ in addition to contingencD reser8es @ additional fuel of ; ",!! 4g. a) #5+, 4g. b) 5#$! 4g. c) d) &"5! 4g.

Answer ; c)

5#$! 4g. ----------------------------------------------------------------------------------------------------------------------------------------------------------------A Get aeroplane is to flD from A to H. The minimum final reser8e fuel must allow for ; 014. #, minutes hold at #,!! ft abo8e destination aerodrome ele8ation. a) b) "! minutes hold at #,!! ft abo8e mean sea le8el. "! minutes hold at #,!! ft abo8e destination aerodrome ele8ation @ when no alternate is required. c) $! minutes hold o8er alternate airfield. d)

Answer ; c)

"! minutes hold at #,!! ft abo8e destination aerodrome ele8ation @ when no alternate is required. ----------------------------------------------------------------------------------------------------------------------------------------------------------------A >TA) >TA) reads I 1A#+"! ",!!$/T &!!! 1/C $#!" J0!$+ K 015. TA) >TA) 3 runwaD in use a) period of 8aliditD b) temperaturedewpoint c) daDmonth d)

Answer ; c)

temperaturedewpoint -----------------------------------------------------------------------------------------------------------------------------------------------------------------


#!


016.

A public transport aeroplane with reciprocating engines @ the final reser8e should be ; fuel to flD for # hour at holding speed a) fuel to flD for "! minutes at holding speed b) c) fuel to flD for $ hours fuel to flD for +, minutes d)

Answer ; d)

fuel to flD for +, minutes ----------------------------------------------------------------------------------------------------------------------------------------------------------------A repetiti8e flight plan ( )'7  is filed for a scheduled flight @ 'aris-rlD to Angouleme @ 'aris rlD as alternate. Following 017. hea8D snow falls @ Angouleme airport will be closed at the epected time of arri8al. The airline decides before departure to t o plan a rerouting of that flight to 7imoges. The pilot-in-command must ad8ise ad8ise ATC of his intention to di8ert di8ert to 7imoges at least #, minutes minutes before before the a) planned time of arri8al. The )'7 must be cancelled for that daD and a specific flight plan plan has to be filed. b) The airlineLs airlineLs “perations” epartment has to transmit a change in in the )'7 at the ATC office @ at least half half an c) hour before the planned time of departure. 0t is not possible to plan plan another another destination destination and and the flight has to be simplD cancelled cancelled that daD ( scheduled scheduled d) flight and not chartered .

Answer ; b)

The )'7 must be cancelled for that daD and a specific flight plan has to be filed. ----------------------------------------------------------------------------------------------------------------------------------------------------------------018. A sector distance is +,! 9 long. The TA1 is +%! 4t. The wind component is ,! 4t tailwind.
Answer ; c)

+!% 9autical Air iles ( 9A  -----------------------------------------------------------------------------------------------------------------------------------------------------------------


##


019.

( For this question use anne !""-##$&!A 

Annex 033-11270A 033-11270A A turboGet aeroplane flies using the following data ; flight le8el I F7 ""! flight regime “7ong )ange”( 7)  mass #,% ,!! 4g tailwind component at this le8el I +! 4t
,"6 9 -----------------------------------------------------------------------------------------------------------------------------------------------------------------


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020.

( For this question use anne !""-##$#,A 

Annex 033-11215A 033-11215A A turboGet aeroplane is flDing using the following data ; optimum flight le8el @ ach !.5! @ mass of #6! !!! 4g temperature I 01A tailwind component I #!! 4t The fuel mileage and the fuel consumption per hour are ; &# 9#!!! 4g @ ,""! 4gh a) #!, 9#!!! 4g @ %,#, 4gh b) 5% 9#!!! 4g @ %,#, 4gh c) #!, 9#!!! 4g @ ,""! 4gh d) Answer ; d)

#!, 9#!!! 4g @ ,""! 4gh -----------------------------------------------------------------------------------------------------------------------------------------------------------------


#"


021.

( For this question use anne !""-##$#%A 

Annex 033-11216A 033-11216A A turboGet aeroplane is flDing using the following data ; flight le8el F7 $,! @ 7ong )ange ( 7)  cruise @ mass of #,! !!! 4g temperature I 01A head wind component I #!! 4t remaining flight time I # h +! min The ground distance that can be co8ered during the cruise flight is ; ++, 9 a) %#$ 9 b) $!"# 9 c) 5+# 9 d) Answer ; a)

++, 9 -----------------------------------------------------------------------------------------------------------------------------------------------------------------


#+


022.

( For this question use anne !""-##$!&A and !""-##$!&H 

Annex 033-11207A 033-11207A  033-11207! 033-11207! A turboGet aeroplane is prepared for a #"!! 9 flight at F7 ",! @ with a true airspeed of +%! 4t and a head wind of #%! 4t. The ta4e-off runwaD limitation is #&+ !!! 4g @ the planned departure mass is #%! !!! 4g. The departure fuel price is equal to !.6$ times the arri8al fuel price ( fuel price ratio K !.6$ . 0n order for the airline to optimiMe its sa8ings @ the additional fuel quantitD that must be loaded on board is ; "! !!! 4g a) #+ !!! 4g b) +$ !!! 4g c) #$ !!! 4g d) Answer ; b)

#+ !!! 4g -----------------------------------------------------------------------------------------------------------------------------------------------------------------


#,


023.

( For this question use anne !""-##$!5A 

Annex 033-1120"A 033-1120"A A turboGet aeroplane @ weighing $!! !!! 4g @ initiates its cruise at the optimum le8el at  !.5+ ( 01A @ C= K "& @ Total Anti 0ce 9 . A head wind of "! 4t is eperienced and @ after a distance of ,!! 9 @ se8ere icing is encountered and this requires an immediate descent. The aeroplane mass at start of descent is ; #6" !!! 4g a) #6" 5!! 4g b) #6$ ,!! 4g c) #6" +!! 4g d) Answer ; c)

#6$ ,!! 4g -----------------------------------------------------------------------------------------------------------------------------------------------------------------


#%


According to the chart the minimum obstruction clearance altitude ( CA  is 5,!! ft. The meteorological data gi8es an outside air temperature of -$!BC at F7 5,. The J92 @ gi8en bD a met. station at an ele8ation of +!!!ft @ is #!!" h'a.
024.

Answer ; a)

55!! ft. ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use anne anne !""- ##!+!A ##!+!A or )oute )oute anual anual 1TA) 1TA) charts charts for N?)0C2 (#!-$@#!-$A@#!-$H  025. Aeroplane arri8ing 8ia route H7 $N onlD @ should follow the following route to >/)9 int ; H7 )## )#### to =7/> int then T)A )-$+& inbound to >/)9 int a) 2C )!%& 8ia =7/> to >/)9 int b) <07 )!#5 outbound to >/)9 int c) d) T)A )$+& outbound to >/)9 int

Answer ; a)

H7 )### to =7/> int then T)A )-$+& inbound to >/)9 int ----------------------------------------------------------------------------------------------------------------------------------------------------------------After flDing for #% min at #!! 4t TA1 TA1 with a $! 4t tail wind component @ Dou ha8e to return to the airfield of departure. Oou Oou 026. will arri8e after ; a) $! min $+ min b) #% min c) #! min +! sec d) Answer ; b)

$+ min ----------------------------------------------------------------------------------------------------------------------------------------------------------------An aeroplane has the following masses ; 027. >1T71T7
Answer ; c)

+ "!! 4g. -----------------------------------------------------------------------------------------------------------------------------------------------------------------


#&


028.

( For this question use anne !""-""#$A or )oute anual chart >(20+ CAA->dition 

Annex 033-3312A 033-3312A An aeroplane has to flD from Abbe8ille ( ,!B!5.#P9 !!#B,#."P>  to Higgin ( ,#B#6.5P9 !!B!!.$P> . At Higgin Dou can find I #+#B. This is ; The a8erage true course of the great circle from Higgin to Abbe8ille. a) b) Te radial @ referenced to true north @ of Higgin to flD inbound. The magnetic course from Higgin to Abbe8ille. c) The magnetic course to flD inbound to Higgin. d) Answer ; c)

The magnetic course from Higgin to Abbe8ille. ----------------------------------------------------------------------------------------------------------------------------------------------------------------029. ( For this question use anne !""-""#$A or )oute anual chart >(20+ CAA->dition 

Annex 033-3312A 033-3312A An aeroplane has to flD from Abbe8ille ( ,!B!5.#P9 !!#B,#."P>  to Higgin ( ,#B#6.5P9 !!!B!!.$P> .
#!! 9 -----------------------------------------------------------------------------------------------------------------------------------------------------------------


#5


030.

( For this question use anne !""-""#$A or )oute anual chart >(20+ CAA->dition 

Annex 033-3312A 033-3312A An aeroplane has to flD from Abbe8ille ( ,!B!5.#P9 !!#B,#."P>  to Higgin ( ,#B#6.5P9 !!B!!.$P> .
F7 "!! ----------------------------------------------------------------------------------------------------------------------------------------------------------------031. ( For this question use anne !""-""#"A or )oute anual chart >(20+ CAA->dition 

Annex 033-3313A 033-3313A An aeroplane has to flD from 1alMburg ( +5B!!.$P9 !#$B,".%P>  to /lagenfurt ( +%B"&.,P9 !#+B"".5P> .
The airwaD ?H, can be used for flight tofrom /lagenfurt and 1alMburg. The airwaD ?H, cannot be used @ there is one waD traffic to the north. The airwaD ?H, is closed for southboud traffic abo8e F7$!!. The airwaD ?H, is closed in this direction ecept during the wee4ends.

Answer ; a)

The airwaD ?H, can be used for flight tofrom /lagenfurt and 1alMburg. -----------------------------------------------------------------------------------------------------------------------------------------------------------------


#6


( For this question question use anne !""-6A @ A>)9A?T0CA7 C2A)T 0CA #I ,!! !!! 1T?TT=A)T 1T?TT=A)T (9 +&% or )oute anual :F)E='1 chart >-% 

032.

#$ute Manual %F#&'PS %F#&'PS (hart E)-6 An aeroplane is flDing :F) and approaching position TA9= TA9= :)TAC :)TAC ( +5B"&P9 @ !!6B#%P>  at F7 !,, and magnetic course !6!B@ distance from :)TAC TA9= $! 9. 9ame the frequencD of the TA9= :)TAC ; +$$ 42M a) ##5.%! 2M b) ##$.,! 2M c) ##5.5! 2M d) Answer ; c)

##$.,! 2M ----------------------------------------------------------------------------------------------------------------------------------------------------------------An aeroplane is on an 0F) flight. The flight is to be changed from 0F) to :F). 0s it possible 3 033. 9o @ onlD ATC ATC can can order Dou to do this. a) Oes @ but onlD with permission from ATC. b) c) Oess @ the pilot in command must inform ATC Oe ATC using the phrase “cancelling mD 0F) flight”. 9o @ Dou ha8e to remain 0F) in accordance accordance to the filed flight plan. d)

Answer ; c)

Oes @ the pilot in command must inform ATC Oes ATC using the phrase “cancelling mD 0F) flight”. ----------------------------------------------------------------------------------------------------------------------------------------------------------------An aircraft flies at a TA1 TA1 of "5! 4t. 0t flies from A to H and bac4 to A. istance AH K +5! 9.
Answer ; a)

$ h ", min ----------------------------------------------------------------------------------------------------------------------------------------------------------------An aircraft @ following a $#,B true trac4 @ must flD o8er a #!%!! ft obstacle with a minimum obstacle clearance of #,!! ft. 035. /nowing the J92 recei8ed from an airport close bD @ which is almost at sea-le8el @ is #!", and the temperature is 01A -#,BC @ what is the minimum F7 the aircraft should flD at allowing for the temperature 8ariation 3 #$! a) b) #"! #+! c) #,! d)

Answer ; c)

#+! ----------------------------------------------------------------------------------------------------------------------------------------------------------------An aircraft has a maimum certificated ta4e-off mass of #"&!!! 4g but is operating at ta4e-off mass #",!!! 4g. 0n 0tem 6 of 036. the ATC ATC flight plan its wa4e turbulence categorD is ; hea8D “2”. a) medium “”. b) hea8Dmedium “2”. c) medium plus “E”. d)

Answer ; a)

hea8D “2”. -----------------------------------------------------------------------------------------------------------------------------------------------------------------


$!


( For this question use )oute anual chart >(20$  An aircraft has to flD from Aalborg ( ,&!%P9 !#!!!P>  to Hottna ( ,&+,P9 !#"+5P>  on airwaD ?)+%.
Answer ; a)

#"! 9 ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use anne !""-""#$A or )oute anual chart >(20+ CAA->dition  038.

Annex 033-3312A 033-3312A An aircraft has to flD from Abbe8ille ( ,!B!5.#P9 !!#B,#."P>  to Higgin ( ,#B#6.5P9 !!B!!.$P> . At Higgin Dou can find I #+#B. This is ; The magnetic course to flD inbound to Higgin. a) The magnetic course from Higgin to Abbe8ille. b) c) The radial @ referenced to true north @ of Higgin to flD inbound. The a8erage true course of the great circle from Higgin to Abbe8ille. d) Answer ; b)

The magnetic course from Higgin to Abbe8ille. ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use anne !""-""#$A or )oute anual chart >(20+ CAA->dition  039.

Annex 033-3312A 033-3312A An aircraft has to flD from Abbe8ille ( ,!B!5.#P9 !!#B,#."P>  to Higgin ( ,#B#6.5P9 !!!B!!.$P>.
%+9 "5 9 %$9 #!! 9

Answer ; d)

#!! 9 -----------------------------------------------------------------------------------------------------------------------------------------------------------------


$#


( For this question use )oute anual chart >(20$  An aircraft has to flD from A7A ( ,,$,P9 !#""+P>  to HAC/A ( ,&""P9 !##,6P>  on airwaDs ?H+, ?2+! and ?A6.
040.

Answer ; b)

#+" 9 ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use )oute anual chart >(20$  041. An aircraft has to flD from A7A ( ,,$,P9 !#""+P>  to '>T>) '> T>) ( ,%,!P9 !#"",P> . >cluding ):1 ):1 @ what is the lowest Flight 7e8el abo8e F7+!! that can be flown on an 0F) flight 'lan 3 F7 +$! a) F7 ++! b) F7 +#! c) F7 +"! d)

Answer ; d)

F7 +"! ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use )oute anual chart >(20$  042. An aircraft has to flD from A7A ( ,,$,P9 !#""+P>  to 1207709= (,&""P9 !#+!!P>.
#"#9 ----------------------------------------------------------------------------------------------------------------------------------------------------------------043. ( For this question use )oute anual chart >(20#  An aircraft has to flD from beacon H>9 ( ,&$6P9 !!&$$P<  to beacon A9 ( ,&#6P9 !!$#%P< .
Answer ; a)

!6" ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use )oute anual chart >(20#  044. An aircraft has to flD from =lasgow ( ,,,$P9 !!+$&P<  to Henbecula ( ,&$6P9 !!&$$P<  @ cruising at "$! 4t TA1. TA1. Assuming a headwind of +! 4t and cruise fuel consumption of $"!! 4gh @ what is the forecast fuel used for this flight 3 6&5 4g a) ###& 4g b) 5%6 4g c) $"!! 4g d)

Answer ; b)

###& 4g ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use )oute anual chart >(20#  045. An aircraft has to flD from =< (,,,$P9 !!+$&P<  to 091 091 ( ,&""P9 !!+!"P<  routing 8ia F09 F09 ( ,%$$P9 !!"$5P< . For Flight 'lanning purposes @ what is the trac4 distance for this flight 3 #!$ 9 a) &" 9 b) ++#9 c) ##& 9 d)

Answer ; d)

##& 9 -----------------------------------------------------------------------------------------------------------------------------------------------------------------


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( For this question use )oute anual chart >(20$  An aircraft has to flD from 09 ( ,,",P9 !#!"6P>  to 7A9:>TT>) ( ,&"6P9 !#$#&P> .
Answer ; d)

!$+ ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use Anne !""-""#"A or )oute anual chart >(20+ CAA->dition  047.

Annex 033-3313A 033-3313A An aircraft has to flD from 1alMburg ( +5B!!.$P9 !#$B,".%P>  to /lagenfurt ( +%B"&.,P9 !#+B"".5P> . At 1alMburg there is stated on the chart  ##".5 1H=. That means ; :)> 1H= will be deleted in the future and cannot be used for na8igation. a) :)> with identification 1H= frequencD ##".5 2M can be used. b) nlD the > > with with identification identification 1H= can be used @ for which frequencD ##".5 2M should be be tuned tuned @ :) c) is not a8ailable. 071> ##".5 2M of 1alMburg airport can be used for na8igation. d) Answer ; b)

:)> with identification 1H= frequencD ##".5 2M can be used. ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use anne !""-""#"A or )oute anual chart >(20+ CAA->dition  048.

Annex 033-3313A 033-3313A An aircraft has to flD from 1alMburg ( +5B!!.$P9 !#$B,".%P>  to /lagenfurt ( +%B"&.,P9 !#+B"".5P> .
The figure #".+ means that the minimum sector altitude ( 1A  is #"+!! ft. The figure #".+ means that the minimum enroute altitude ( >A  is #"+!! ft. The figure #!5 means that the minimum minimum obstacle clearance altitude ( CA CA  on this route is is #!5!! #!5!! ft abo8e 17. The figure #".+ means that the minimum minimum grid safe altitude in this sector is #"+!! #"+!! ft abo8e 17.

Answer ; d)

The figure #".+ means that the minimum grid safe altitude in this sector is #"+!! ft abo8e 17. -----------------------------------------------------------------------------------------------------------------------------------------------------------------


$"


049.

( For this question use Anne !""-""#"A or )oute anual chart >(20+ CAA->dition 

The airwaD ?H, cannot be used @ there is one waD traffic to the north. The airwaD ?H, is closed in this direction ecept during the wee4ends. The airwaD ?H, is closed for southbound traffic abo8e F7 $!!. The airwaD ?H, can be used for flights tofrom /lagenfurt and 1alMburg.

Answer ; d)

The airwaD ?H, can be used for flights tofrom /lagenfurt and 1alMburg. ----------------------------------------------------------------------------------------------------------------------------------------------------------------050. ( For this question use Anne !""-""#"A or )oute anual chart >(20+ CAA->dition 

The airwaD ?H, can be used for flights tofrom /lagenfurt and 1alMburg. The airwaD ?H, cannot be used @ there is one waD traffic to the north. The airwaD ?H, is closed in this direction ecept during the wee4ends. The airwaD ?H, is closed for southbound traffic abo8e F7$!!.

Answer ; a)

The airwaD ?H, can be used for flights tofrom /lagenfurt and 1alMburg. -----------------------------------------------------------------------------------------------------------------------------------------------------------------


$+


( For this question use )oute anual chart >(20$  An aircraft has to flD from 1207709= ( ,&""P9 !#+!!P>  to A7A ( ,,$,P9 !#""+P> .
Answer ; d)

"$!! ft ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use )oute anual chart >(20#  052. An aircraft has to flD from TA77A ( ,,"!P9 !!"$#P<  to F09 ( ,%$$P9 !!"$5P< . >cluding ):1 ):1 @ what is the first flight 7e8el abo8e F7+!! that can be flown on this leg on an 0F) flight 'lan 3 F7+#! a) F7+!! b) c) F7+"! F7+$! d)

Answer ; c)

F7+"! ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use )oute anual chart >(20#  053. An aircraft has to flD from the airport at Aberdeen ( ,&#6P9 !!$#%P<  to the airport at Henbecula ( ,&$6P9 !!&$$P< . =i8en ; Time to climb ## min Time to descend is #, min TC is at "< T is at %< TA1 TA1 $#! 4ts ( still air  Find the total GourneD time 3 +& min a) $5 min b) #% min c) ,+ min d)

Answer ; d)

,+ min ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use )oute anual chart >(20$  054. An aircraft has to flD from the beacon T9 ( ,,+%P9 !##$%P>  on a direct route to the beacon 2A) ( ,&,!P9 !#$+$P> .
Answer ; d)

!#5  #$6 9 ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use )oute anual chart >(20#  055. An aircraft has to flD from T0)>> ( ,%$6P9 !!%,"P<  direct to AH>)>>9 ( ,&#6P9 !!$#%P< .
Answer ; b)

,&!! ft ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use )oute anual chart >(20$  056. An aircraft has to flD on airwaDs from 09 ( ,,",P9 !#!"6P>  to HTT9A ( ,&+,P9 !#"+5P> . ) ?=, 12= ?2+$ HT c) 9 ?)#,% 1/A ?2+$ HT d)

Answer ; d)

9 ?)#,% 1/A ?2+$ HT -----------------------------------------------------------------------------------------------------------------------------------------------------------------


$,


( For this question use )oute anual chart >(20$  An aircraft has to flD on airwaDs from 1/A)A ( ,5$"P9 !#"#,P>  to 1:>A ( ,%#!P9 !#$"+P> . nce airborne @ if appro8ed @ which of the following is an acceptable route for this flight 3 1/A ?2+$ HT ?:"! 207 ?)# 1: a) 1/A ?H++ HA/ ?A6 'A'>) ?2+! 1: b) 1/A ?)#,% 7A: ?H+, 1: c) d) 1/A CT 1:

057.

Answer ; a)

1/A ?2+$ HT ?:"! 207 ?)# 1: ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use )oute anual chart >(20$  058. An aircraft has to flD on airwaDs from 1:>A (,%#!P9 !#$"+P> to 1/A)A (,5$"P9 !#"#,P>. ) ?A6 HA/ ?)#,% 1/A a) 1: ?2+! 'A'>) ?A6 HA/ ?H++ 1/A b) 1: ?H+, 7A: ?)#,% 1/A c) ?)# 207 ?:"! HT ?2+$ 1/A d) Answer ; b)

1: ?2+! 'A'>) ?A6 HA/ ?H++ 1/A ----------------------------------------------------------------------------------------------------------------------------------------------------------------An aircraft is flDing at AC2 !.5+ at F7 ""!. The static air temperature is -+5BC and the headwind component ,$ /t. At 059. #""5 ?TC the controller requests the pilot to cross the meridian of !"!< at #,!! ?TC. =i8en the distance to go is ,&! 9 @ the reduced AC2 9o. should be ; !.5! a) b) !.&5 !.&$ c) !.&% d)

Answer ; a)

!.5! ----------------------------------------------------------------------------------------------------------------------------------------------------------------060. ( For this question use )oute anual chart >(20$  An aircraft is flDing from HAC/A ( ,&B""P9 !##B,6P> to HTT9A ( ,&B+,P9 !#"B+5P>  on airwaD ?)+%.
Answer ; c)

2A)#%#  7A:!6$ ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use )oute anual chart >(20#  061. An aircraft is flDing 9orthbound on the direct route from >A9 C)11 that passes through position ,&B!!.!P9 !!"B#!.!P<. >cluding ):1 @ what is the first flight 7e8el abo8e F7+#! that can be used on an 0F) flight 'lan 3 F7+$! a) F7+"! b) F7++! c) F7+,! d)

Answer ; d)

F7+,! ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use )oute anual chart >(20#  062. An aircraft is flDing towards =< ( ,,,$P9 !!+$&<  on airwaD ?9%#, prior to an arri8al in the 7ondon F0). According to the information on the chart @ what is the most rele8ant frequencD to recei8e the broadcast weather for 7ondon F0) ( 9orth  3 #"".%& a) #$%.%! b) ##,.+ c) #$6.$$ d)

Answer ; b)

#$%.%! -----------------------------------------------------------------------------------------------------------------------------------------------------------------


%$Flight Planning & Monitoring Monitoring

An aircraft is in cruising flight at F7 !6, @ =1 #,,4t. The pilot intends to descend at ,!! ftmin to arri8e o8erhead the A9 :) at $!!! FT ( J92 #!"!h'a . The TA1 remains constant in the descent @ wind is negligible @ temperature standard. At which distance from A9 should the pilot commence the descent 3 "5 9 a) +5 9 b) +, 9 c) +# 9 d) 063.

Answer ; d)

+# 9 ----------------------------------------------------------------------------------------------------------------------------------------------------------------An aircraft is on an 0F) flight. The flight is to be changed from 0F) to :F). 0s it possible 3 064. 9o @ Dou ha8e to remain 0F) in accordance to the filed flight plan. a) 9o @ onlD ATC can order Dou to do this. b) c) Oes Oes @ but onlD with permission permissi on from ATC. Oess @ the pilot Oe pilot in command must inform ATC using the phrase phrase “cancelling “cancelling mD 0F) 0F) flight”. d)

Answer ; d)

Oes @ the pilot in command must inform ATC using the phrase “cancelling mD 0F) flight”. Oes ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this this question use anne !""-#$"%+A or Flight 'lanning anual )*T # Figure +.&.$  065.

Annex 033-12364A 033-12364A An aircraft on an etended range operation is required ne8er to be more than #$! minutes from an alternate @ based on # engine inoperati8e 7)C conditions in 01A.?sing the abo8e table and a gi8en mass of +!!!! 4g at the most critical point @ the maimum air distance to the rele8ant alternate is ; &", 9 a) 5#! 9 b) &6+ 9 c) 5&, 9 d) Answer ; a)

&", 9 -----------------------------------------------------------------------------------------------------------------------------------------------------------------


$&


An aircraft plans to depart 7ondon at #!!! ?TC and arri8e at unich ( >  at #$#, ?TC. 0n the ATC flight plan 0tem #% ( destination>>T  should be entered with ; a) >!$#, >$2#, b) >#+#, c) > AT !$#, d)

066.

Answer ; a)

>!$#, ----------------------------------------------------------------------------------------------------------------------------------------------------------------An airwaD is mar4ed ",!!T $#!!a. This indicates that ; 067. the minimum enroute altitude ( >A  is ",!! ft. a) the minimum obstruction clearance altitude ( CA  is ",!! ft. b) the airwaD base is ",!! ft 17. c) the airwaD is a low le8el lin4 route $#!! ft - ",!! ft 17. d)

Answer ; b)

the minimum obstruction clearance altitude ( CA  is ",!! ft. ----------------------------------------------------------------------------------------------------------------------------------------------------------------An airwaD is mar4ed ,!!! $6!!a. The notation ,!!! is the ; 068. base of the airwaD ( A=7  a) minimum enroute altitude ( >A  b) c) maimum authorised altitude ( AA  minimum holding altitude ( 2A  d)

Answer ; b)

minimum enroute altitude ( >A  ----------------------------------------------------------------------------------------------------------------------------------------------------------------An airwaD is mar4ed F7 5! #,!!a. This indicates that ; 069. a) the airwaD base is #,!! ft 17. #,!! ft 17 is the minimum radio reception altitude ( )A . b) the minimum enroute altitude ( >A  is F7 5!. c) the airwaDs etends from #,!! ft 17 to F7 5!. d)

Answer ; c)

the minimum enroute altitude ( >A  is F7 5!. ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use anne !""- ##!"#A or )oute anual chart >(20+ CAA->dition  070. An appropriate flight le8el for flight in ):1 airspace on airwaD ?=# from >)7A9=>9 >)7 ##+.6 ( +6B"6BP9 !##B!6P>  to F)A9/F?)T FF ## ##+.$ +.$ ( ,!B!"P9 !!5B"5P>  is ; F7"#! a) F7""! b) c) F7"!! F7$6! d) Answer ; c)

F7"!! ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use )oute anual chart >(7#  071. An appropriate flight le8el for flight on airwaD A$ from TA77A ##".5 ##".5 T7A ( ,,B"!P9 !!"B$#P<  to >A9 C)11 ##,.$ C1 ( ,+B+"P9 !!"B$!P<  is ; F7#!! a) F7,! b) F75! c) F76! d)

Answer ; d)

F76! ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use anne !""- ##!",A or )oute anual chart >(7$  072. An appropriate flight le8el for flight on airwaD H" from C2AT0779 C2AT0779 CT7 ##&.% ( +6B!5P9 !!"B",P>  to CAH)A0 CH ##$.% ( ,!B#+P9 !!"B!6P>  is ; F75! a) F7%! b) F7#&! c) F7,! d)

Answer ; c)

F7#&! -----------------------------------------------------------------------------------------------------------------------------------------------------------------


$5


( For this question use anne !""- ##!"$A or )oute anual chart >(7,  An appropriate flight le8el for flight on airwaD =6 from 1?H0 1?0 ##%.& ( ,$B$"P9 !#+B",P>  to CN>'09 CN> ##+., ( ,$B!5P9 !#%B++P>  is ; a) F7&! F7%! b) F75! c) F7,! d) 073.

Answer ; a)

F7&! ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use anne !""- ##!"&A or )oute anual chart >(7%  074. An appropriate flight le8el for flight on airwaD )#! from 9T>O  #!6.+ ( +6B$+P9 !!,B!5P>  to C2AT0779 C2AT0779 CT7 ##&.% ( +6B!5P9 !!"B",P>  is ; F7%! a) F7+! b) c) F7&! F7,! d)

Answer ; a)

F7%! ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use anne !""- ##!""A or )oute anual chart >(20, CAA->dition  075. An appropriate flight le8el for flight on airwaD ?=, in ):1 airspace from >9>9A1H09A71 >9 ##,." ( ++B"%P9 !!"B#!P>  to =A077AC =A0 ##,.5 ( +"B,&P9 !!#B,!P>  is ; F7$5! a) F7"!! b) F7"$! c) F7$6! d)

Answer ; d)

F7$6! ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use anne !""- ##!"!A or )oute anual chart >(20+ CAA->dition  076.

#$ute Manual (hart (hart E*+,4 An appropriate flight le8el for flight on airwaD ?)# from )TAC )TAC ( ,!B!!P9 !!$B!!P<  to 02?)1T 0 ##+.! ( ,#B!"P9 !!!B"&P<  is ; F7$%! a) F7$"! b) F7$,! c) F7$+! d) Answer ; c)

F7$,! -----------------------------------------------------------------------------------------------------------------------------------------------------------------


$6


( For this question use anne !""- ##!"+A or )oute anual chart >(20, CAA->dition  An appropriate flight le8el for flight on airwaD ?)$+ from 9A9T>1 9T1 ##&.$ ( +&B!6P9 !!#B"&P<  to CA>9 CA9 ##,.+ ( +6B#!P9 !!!B$&P<  is ; F7$&! a) F7$6! b) F7"!! c) d) F7"#! 077.

Answer ; c)

F7"!! ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use anne !""- ##!"%A or )oute anual chart >(7%  078. An appropriate flight le8el for flight on airwaD <"& from C2>H /= ##,.& ( ,!B!+P9 !#$B$+P>  to )09= )= ##+.& ( +6B!$P9 !#$B"$P>  is ; F75! a) F7&! b) F7+! c) F7,! d) Answer ; a)

F75! ----------------------------------------------------------------------------------------------------------------------------------------------------------------An appropriate flight le8el for 0F) flight in accordance with semi-circular height rules on a course of #5!B (   is ; 079. F76, a) F76! b) F7#!, c) d) F7#!!

Answer ; d)

F7#!! ----------------------------------------------------------------------------------------------------------------------------------------------------------------An 0F) flight is planned outside airwaDs on a course of $",B magnetic. The minimum safe altitude is &5!! ft. /nowing the 080. J92 is 66, h'a @ the temperature is 01A @ the minimum flight le8el Dou must flD is ; a) 6! 5! b) 5, c) #!! d)

Answer ; d)

#!! ----------------------------------------------------------------------------------------------------------------------------------------------------------------An operator shall ensure that calculation of usable fuel for an 0F)-flight with a turboGet aeroplane for which no destination 081. alternate is required includes @ tai fuel @ trip fuel @ contingencD fuel and fuel to flD for ; +, minutes minutes plus #, of the flight time planned planned to to be spent at cruising le8el or two hours whiche8er is less. a) +, minutes at holding speed at +,! m abo8e aerodrome ele8ation in standard conditions. b) +, minutes at holding speed at +,! m abo8e 17 in standard conditions. c) d) $ hours at normal cruise consumption.

Answer ; b)

+, minutes at holding speed at +,! m abo8e aerodrome ele8ation in standard conditions. -----------------------------------------------------------------------------------------------------------------------------------------------------------------


"!


082.


Annex 033-11207A 033-11207A  033-11207! 033-11207! Assuming a departuredestination fuel price ratio of !.6# @ the commander decides to optimiMe fuel tan4ering bD using the following data ; Cruise flight le8el I F7 ",! Air distance to be co8ered I $ ,!! 9 'lanned ta4e-off mass I $!! !!! 4g ( with the minimum prescribed fuel quantitD of "5 !!! 4g that includes a trip fuel of $6 !!! 4g  aimum landing mass I #5! !!! 4g aimum ta4e-off mass I $!, !!! 4g aimum tan4 capacitD I +! !!! 4g The additional fuel quantitD will be ; ! 4g a) $ !!! 4g b) c) " !!! 4g + !!! 4g d) Answer ; a)

! 4g -----------------------------------------------------------------------------------------------------------------------------------------------------------------


"#


083.


Annex 033-11207A 033-11207A  033-11207! 033-11207! Assuming a departuredestination fuel price ratio of !.6$ @ the commander decides to optimiMe fuel tan4ering bD using the following data ; Cruise flight le8el I F7 ",! Air distance to be co8ered I # 5"! 9 'lanned ta4e-off mass I #6! !!! 4g ( with a minimum prescribed fuel quantitD of "! !!! 4g that includes a trip fuel of $$ !!! 4g  aimum landing mass I #5! !!! 4g aimum ta4e-off mass I $!, !!! 4g aimum tan4 capacitD I +! !!! 4g The additional fuel quantitD will be ; #! !!! 4g a) #$ !!! 4g b) $! !!! 4g c) #, !!! 4g d) Answer ; a)

#! !!! 4g -----------------------------------------------------------------------------------------------------------------------------------------------------------------


"$


084.

( For this question use anne !""-##$##A !""-##$##A and !""-##$##H !""-##$##H 

Annex 033-1121 033-11211A 1A  033-11211 033-11211! ! Assuming the following data ; =round distance to be co8ered I # ,!! 9 Cruise flight le8el I F7 "#! Cruising speed I ach !.5$ ( true airspeed I +&! 4t  2ead wind component I +! 4t 'lanned destination landing mass I #+! !!! 4g Temperature Temperature I 01A E #,B C C= I "&  Total Total anti-ice I 9 'ac4 flow I 20 Fuel consumption for such a flight is ; $# &!! 4g a) $" ,!! 4g b) #6 6!! 4g c) $# ,!! 4g d) Answer ; b)

$" ,!! 4g -----------------------------------------------------------------------------------------------------------------------------------------------------------------


""


085.


Annex 033-1121 033-11211A 1A  033-11211 033-11211! ! Assuming the following data ; =round distance to be co8ered I $ ,!! 9 Cruise flight le8el I F7 ",! Cruising speed I ach !.5$ ( true airspeed I +&! 4t  Tailwind Tailwind component I +! 4t 'lanned destination landing mass I #,! !!! 4g Temperature Temperature I 01A C= I "& Total Total anti-ice I FF Air conditioning I normal Fuel consumption for such a flight is ; $5 "!! 4g a) $& 5!! 4g b) $6 $!! 4g c) $& !!! 4g d) Answer ; b)

$& 5!! 4g -----------------------------------------------------------------------------------------------------------------------------------------------------------------


"+


086.

( For this question use anne !""-##$#+A and !""-##$#+H 

Annex 033-1121 033-11211A 1A  033-11211 033-11211! ! Assuming the following data ; =round distance to be co8ered I $ %!! 9 Cruise flight le8el I F7 "&! Cruising speed I ach !.5$ ( true airspeed I +&! 4t 
"# ,!! 4g -----------------------------------------------------------------------------------------------------------------------------------------------------------------


",


087.


Annex 033-1121 033-11211A 1A  033-11211 033-11211! ! Assuming the following data ; =round distance to be co8ered I $ !!! 9 Cruise flight le8el I F7 ""! Cruising speedI ach !.5$ ( true airspeed I +&! 4t  2ead wind component I "! 4t 'lanned destination landing mass I #%! !!! 4g Temperature Temperature I 01A C= I "& Total Total anti-ice I 9 'ac4 flow I 20 Time needed to carrD out such a flight is ; , h !$ min a) + h #! min b) + h $% min c) + h +" min d) Answer ; d)

+ h +" min -----------------------------------------------------------------------------------------------------------------------------------------------------------------


"%


088.

etermine the Ta4e-off Ta4e-off ass for the following single engine aeroplane ; =i8en ; 1tandard >mptD ass #&%+ lbs ptional >quipment ", lbs 'ilot E Front seat passenger "!! lbs Cargo ass ",! lbs )amp Fuel K Hloc4 Fuel %! =al. Trip Fuel ", =al. Fuel densitD densitD % lbs=al. lbs=al. 1tart up and TaD Fuel #! lbs $5!6 lbs a) $%,6 lbs b) $&%+ lbs c) $&66 lbs d)

Answer ; d)

$&66 lbs ----------------------------------------------------------------------------------------------------------------------------------------------------------------uring a flight at night a position has to be reported to ATC. ATC. The aeroplane is at a distance of &,! 9 from the ground 089. station and at flight le8el ",!. The frequencD to be used is ; #$".6 2M. a) #&$5% 42M. b) c) ##""% 42M. ,%+6 42M. d)

Answer ; d)

,%+6 42M. ----------------------------------------------------------------------------------------------------------------------------------------------------------------uring a flight the fuel indicators show that the remaining amount of fuel is #!! lbs after "5 minutes. The total amount of 090. fuel at departure was #%! lbs. For the alternate fuel @ "! lbs is necessarD. The planned fuel for tai is #" lbs. Final reser8e fuel is estimated at ,! lbs. 0f the fuel flow remains the same @ how manD minutes can be flown to the destination with the remaining fuel 3 #$ minutes. a) + minutes. b) ++ minutes. c) %" minutes. d)

Answer ; a)

#$ minutes. ----------------------------------------------------------------------------------------------------------------------------------------------------------------uring a :F) flight at a na8igational chec4point the remaining usable fuel in tan4s is %! ?1 gallons. The reser8e fuel is #$ 091. ?1 gallons. According to the flight plan the remaining flight time is # h ", min. Calculate the highest acceptable rate of consumption possible for the rest of the trip ; a) $#." ?1 gallonshour "!." ?1 gallonshour b) "&.6 ?1 gallonshour c) "".! ?1 gallonshour d) Answer ; b)

"!." ?1 gallonshour ----------------------------------------------------------------------------------------------------------------------------------------------------------------uring an 0F) flight in a Heech HonanMa the fuel indicators show that the remaining amount of fuel is #!! lbs after "5 092. minutes. Fuel at ta4e off is #%!l bs. For the alternate fuel @ "! lbs is necessarD. The planned fuel for tai is #" lbs. Final reser8e fuel is estimated at ,! lbs. 0f the fuel flow remains the same @ how manD minutes can be flown to the destination with the remaining fuel 3 ++ minutes. a) %" minutes. b) c) #$ minutes. + minutes. d)

Answer ; c)

#$ minutes. ----------------------------------------------------------------------------------------------------------------------------------------------------------------uring an 0F) flight TA1 TA1 and time appear to de8iate from the data in the ATC ATC flight plan. The minimum de8iations @ that 093. should be reported to ATC ATC in order to conform to 'A91-)AC 'A91-)AC @ are ; TA1 TA1 , 4t and time , minutes. a) TA1 TA 1 , and time " minutes. b) TA1 TA1 " and time " minutes. c) TA1 TA1 #! 4t and time $ minutes. d) Answer ; b)

TA1 , and time " minutes. TA1 -----------------------------------------------------------------------------------------------------------------------------------------------------------------


"&


>cluding ):1 ):1 an appropriate flight le8el for 0F) flight in accordance with semicircular height rules on a course of #5!B (   is ; a) F7#!! F76! b) F76, c) F7#!, d) 094.

Answer ; a)

F7#!! ---------------------------------------------------------------------------------------------------------------------------------------------------------------->cluding ):1 ):1 an appropriate flight le8el for 0F) flight in accordance with semicircular height rules on a magnetic course 095. of $!!B is ; F7$6! a) F7"#! b) F7"!! c) d) F7"$! Answer ; b)

F7"#! ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use anne !""-6,&$A or Flight 'lanning anual )*T # Figure +.,.".#  096.

Annex 033-9572A 033-9572A Find I Air distance in 9autical Air iles ( 9A  for this leg and fuel consumption ; =i8en ; Flight time from top of climb at F7 $5! to the enroute point is +5 minutes. Cruise procedure is long range cruise. Temperature Temperature is 01A -,BC. The ta4e-off mass is ,%!!! 4g and climb fuel ##!! 4g. "+, 9A @ #66+ 4g a) "+, 9A @ $!!! 4g b) "+6 9A @ $!!! 4g c) "+, 9A @ $!!% 4g d) Answer ; a)

"+, 9A @ #66+ 4g -----------------------------------------------------------------------------------------------------------------------------------------------------------------


"5


097.

( For this question use anne !""-6,&#A or Flight 'lanning anual )*T # Figure +.,.".# 

Annex 033-9571A 033-9571A Find I Final fuel consumption for this leg ; =i8en ; 7ong range cruise Temperature Temperature -%"BC F7 ""! 0nitial gross mass enroute ,+#!! 4g 7eg flight time $6 min a) ##!& 4g ##!! 4g b) #!!! 4g c) #!6" 4g d) Answer ; d)

#!6" 4g ----------------------------------------------------------------------------------------------------------------------------------------------------------------Find the distance from waDpoint " ( <' "  to the critical point ; 098. =i8en ; distance from <' " to <' + I &,! 9 TA1 out +"! 4t TA1 return +$, 4t tailwind component out "! 4t head wind component return +! 4t +!5 9 a) "&, 9 b) +!" 9 c) "+$ 9 d)

Answer ; d)

"+$ 9 -----------------------------------------------------------------------------------------------------------------------------------------------------------------


"6


099.

Find the distance to the '09T F 1AF> )>T?)9 ( '1)  ; =i8en ; maimum useable fuel #,!!! 4g minimum reser8e fuel ",!! 4g utbound I TA1 +$, 4t @ head wind component "! 4t @ fuel flow $#,! 4gh )eturn I TA1 +"! 4t @ tailwind component $! 4t @ fuel flow $#,! 4gh ##$, 9 a) ##+" 9 b) #+%" 9 c) d) #+6# 9

Answer ; a)

##$, 9 ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this this question use anne !""-6,,&A or Flight 'lanning anual )*T # Figure +.,.".$ +.,.".$  100.

Annex 033-9557A 033-9557A Find the F?>7 F7< for the twin Get aeroplane with regard to the following data ; =i8en ; AC2 .&+ cruise Flight le8el "#! =ross mass I ,!!!! 4g 01A conditions $"!! 4gh a) $66+ 4gh b) #+6& 4gh c) ##,! 4gh d) Answer ; a)

$"!! 4gh -----------------------------------------------------------------------------------------------------------------------------------------------------------------


+!


101.

( For this question use annees annees !""-6,,+A and !""-6,,+H or Flight Flight 'lanning anual )*T # 'aragraph 'aragraph $.# and Figure

+.$.# 

Annex 033-9554A 033-9554A Find the F?>7 07>A=> '>9A7TO for the twin Get aeroplane with regard to the gi8en F70=2T 7>:>7 ; =i8en ; 7ong range cruise Cruise mass I ,"!!! 4g F7 "#! ! a) + b) #!  c) # d) Answer ; b)

+ -----------------------------------------------------------------------------------------------------------------------------------------------------------------


+#


102.

( For this this question use anne !""-6,,"A or Flight 'lanning anual )*T # Figure +.$.# +.$.# 

Annex 033-9550A 033-9550A Find the 'T0? A7T A7T0T?> 0T?> for the twin Get aeroplane. =i8en ; Cruise mass K ,!!!! 4g .&5 AC2 a) "%$!! ft "%&!! ft b) maimum operating altitude c) ",,!! ft d) Answer ; d)

",,!! ft -----------------------------------------------------------------------------------------------------------------------------------------------------------------


+$


103.

( For this this question use anne !""-6,,!A or Flight 'lanning anual )*T # Figure +.$.# +.$.# 

Annex 033-9550A 033-9550A Find the 'T0? A7T A7T0T?> 0T?> for the twin Get aeroplane ; =i8en ; Cruise mass I ,+!!! 4g 7ong range cruise or .&+ AC2 ""5!! ft a) b) maimum operating altitude "+,!! ft c) ","!! ft d) Answer ; c)

"+,!! ft -----------------------------------------------------------------------------------------------------------------------------------------------------------------


+"


104.

( For this question use anne !""-6,,!A or Flight 'lanning anual )*T # Figure +.$.$ 

Annex 033-9550A 033-9550A Find the 12)T 1 2)T 01TA9C> 01TA9C> C)?01> A7T0T?> A7T0T?> for the twin Get aeroplane ; =i8en ; Hra4e release mass I +!!!! 4g Temperature Temperature I 01A E $!BC Trip distance I #,! 9autical Air iles ( 9A  a) $&,!! ft "!!!! ft b) $#!!! ft c) $,!!! ft d) Answer ; b)

"!!!! ft -----------------------------------------------------------------------------------------------------------------------------------------------------------------


++


105.

( For this this question use anne !""-6,,!A or Flight 'lanning anual )*T # Figure +.$.$ +.$.$ 

Annex 033-9550A 033-9550A Find the 12)T 1 2)T 01TA9C> 01TA9C> C)?01> A7T0T?> A7T0T?> for the twin Get aeroplane ; =i8en ; Hra4e release mass I +,!!! 4g Temperature Temperature I 01A E $!BC Trip distance I ,! 9autical Air iles ( 9A  #$,!! ft a) ##!!! ft b) &,!! ft c) #!!!! ft d) Answer ; d)

#!!!! ft -----------------------------------------------------------------------------------------------------------------------------------------------------------------


+,


106.

( For this this question use anne !""-6,,%A or Flight 'lanning anual )*T # Figure +.#+ +.#+ 

Annex 033-9556A 033-9556A Find the 1'>C0F0C )A9=> for the twin Get aeroplane flDing below the optimum altitude ( range loss K %  and using the following data ; =i8en ; AC2 .&+ C)?01> Flight le8el I "#! =ross mass I ,!!!! 4g 01A conditions $66+ 9A#!!! 4g a) $5!& 9A#!!! 4g b) c) #&% 9A#!!! 4g #5& 9A#!!! 4g d) Answer ; c)

#&% 9A#!!! 4g ----------------------------------------------------------------------------------------------------------------------------------------------------------------Find the time to the 'oint of 1afe )eturn ( '1)  ; 107. =i8en ; aimum useable fuel #,!!! 4g inimum reser8e fuel ",!! 4g TA1 out +$, 4t 2ead wind component out "! 4t TA1 return +"! 4t Tailwind Tailwind component return $! 4t A8erage A8erage fuel flow $#,! 4gh $ h ,6 min a) $ h +" min b) $ h ,# min c) " h +" min d)

Answer ; c)

$ h ,# min -----------------------------------------------------------------------------------------------------------------------------------------------------------------


+%


108.

( For this this question use anne !""-6,%+A or Flight 'lanning anual )*T # Figure +.,.# +.,.# 

Annex 033-9564A 033-9564A Find I Time @ Fuel @ 1till Air istance and TA1 TA1 for an enroute climb $5!.&+ to F7 ",!. =i8en ; Hra4e release mass %+!!! 4g 01A E#!BC Airport ele8ation "!!! ft $, min @ #5&, 4g @ #+5 9autical Air iles ( 9A  @ "6# 4t a) $% min @ #6&, 4g @ #,& 9autical Air iles ( 9A  @ "66 4t b) $! min @ #&,! 4g @ ##& 9autical Air iles ( 9A  @ $55 4t c) $% min @ $!,! 4g @ #,& 9autical Air iles ( 9A  @ "66 4t d) Answer ; b)

$% min @ #6&, 4g @ #,& 9autical Air iles ( 9A  @ "66 4t -----------------------------------------------------------------------------------------------------------------------------------------------------------------


+&


109.

( For this question use anne !""-6,,5A 

Annex 033-955"A 033-955"A Finish the >9?)A9C>F?>7 CA7C?7AT09 CA7C?7AT09 and determine ATC ATC >9?)A9C> for a twin-Get aeroplane @ with the help of the table pro8ided. ContingencD is , of the planned trip fuel and fuel flow for etra fuel is $+!! 4gh ; ATC ATC >9?)A9C> >9?)A9C > I !"I"& a) ATC ATC >9?)A9C> >9?)A9C > I !"I,$ b) ATC AT C >9?)A9C >9?)A9C> > I !+I!& c) ATC ATC >9?)A9C> >9?)A9C > I !+I#$ d) Answer ; c)

ATC >9?)A9C ATC >9?)A9C> > I !+I!& ----------------------------------------------------------------------------------------------------------------------------------------------------------------Flight planning chart for an aeroplane @ states that the time to reach F7 #6! at a gi8en gross mass is $$ minutes and the 110. distance tra8elled is %% 9 ( no wind .
Answer ; c)

," 9 ----------------------------------------------------------------------------------------------------------------------------------------------------------------111. Flight planning chart for an aircraft states that the time to reach the cruising le8el at a gi8en gross mass is "% minutes and the distance tra8elled is #,& 9 ( Mero-wind .
Answer ; c)

#6" 9 -----------------------------------------------------------------------------------------------------------------------------------------------------------------


+5


112.

( For this question use )oute anual :F)E='1 chart >-% 

#$ute Manual %F#&'PS %F#&'PS (hart E)-6 FlDing from >'* 7A0C209=>9 airport ( +5B"!P9 @ !!6B"5P>  to >1N )TT<>07 N>'F>92A9 ( +5B#$P9 @ !!5B++P>  . Find magnetic course and the distance ; agnetic course !%" @ distance +# 9 a) agnetic course $+" @ distance %$ 9 b) agnetic course $+" @ distance +# 9 c) agnetic course !%" @ distance %$ 9 d) Answer ; c)

agnetic course $+" @ distance +# 9 -----------------------------------------------------------------------------------------------------------------------------------------------------------------


+6


113.


#$ute Manual %F#&'PS %F#&'PS (hart E)-6 FlDing from >'* 7A0C209=>9 airport ( +5B"!P9 @ !!6B"5P>  to >T >9=>9 airport ( +5B!"P9 @ !!6B$$P> . Find magnetic course and the distance ; agnetic course $!$ @ distance ++ 9 a) agnetic course $!$ @ distance $5 9 b) agnetic course !$$ @ distance ++ 9 c) agnetic course !$$ @ distance $5 9 d) Answer ; b)

agnetic course $!$ @ distance $5 9 -----------------------------------------------------------------------------------------------------------------------------------------------------------------


,!


114.


#$ute Manual %F#&'PS %F#&'PS (hart E)-6 FlDing from >1N )TT<>07 N>'F>92A9 ( +5B#$P9 @ !!5B++P>  to >'* 7A0C209=>9 airport ( +5B"!P9 @ !!6B"5P>  . etermine the highest obstacle within within a corridor , 9 left and , 9 right of the courseline courseline ; "%#$ ft a) b) $5,$ ft "&%! ft c) "$&5 ft d) Answer ; c)

"&%! ft -----------------------------------------------------------------------------------------------------------------------------------------------------------------


,#


115.


#$ute Manual %F#&'PS %F#&'PS (hart E)-6 FlDing from >1N )TT<>07 N>'F>92A9 ( +5B#$P9 @ !!5B++P>  to >'* 7A0C209=>9 airport ( +5B"!P9 @ !!6B"5P>  . Find magnetic course and the distance ; a) agnetic course $+"B @ distance +# 9 agnetic course !%"B @ distance +# 9 b) agnetic course $+"B @ distance %$ 9 c) agnetic course !%"B @ distance %$ 9 d) Answer ; b)

agnetic course !%"B @ distance +# 9 -----------------------------------------------------------------------------------------------------------------------------------------------------------------


,$


116.


#$ute Manual %F#&'PS %F#&'PS (hart E)-6 FlDing from >1N )TT<>07 N>'F>92A9 ( +5B#$P9 @ !!5B++P>  to >T >9=>9 airport ( +5B!"P9 @ !!6B$$P> . etermine the highest obstacle within a corridor , 9 left and , 9 right of the courseline ; "&%! ft a) b) $6$! ft """# ft c) $%!, ft d) Answer ; a)

"&%! ft ----------------------------------------------------------------------------------------------------------------------------------------------------------------117. ( For this question use )oute anual :F)E='1 chart >-% 

#$ute Manual %F#&'PS %F#&'PS (hart E)-6 FlDing from >1N )TT<>07 N>'F>92A9 ( +5B#$P9 @ !!5B++P>  to >T >9=>9 airport ( +5B!"P9 @ !!6B$$P> . Find magnetic course and the distance ; agnetic course $55B @ distance $& 9 a) agnetic course #!5B @ distance +! 9 b) agnetic course $55B @ distance +! 9 c) agnetic course #!5B @ distance $& 9 d) Answer ; d)

agnetic course #!5B @ distance $& 9 -----------------------------------------------------------------------------------------------------------------------------------------------------------------


,"


118.


#$ute Manual %F#&'PS %F#&'PS (hart E)-6 FlDing from >T >9=>9 airport ( +5B!"P9 @ !!6B$$P>  to >'* 7A0C209=>9 airport ( +5B"!P9 @ !!6B"5P> . etermine the highest obstacle within a corridor , 9 left and , 9 right of the courseline ; $,!& ft a) $#$! ft b) $5"5 ft c) $5&! ft d) Answer ; d)

$5&! ft -----------------------------------------------------------------------------------------------------------------------------------------------------------------


,+


119.


#$ute Manual %F#&'PS %F#&'PS (hart E)-6 FlDing from >T >9=>9 airport ( +5B!"P9 @ !!6B$$P>  to >'* 7A0C209=>9 airport ( +5B"!P9 @ !!6B"5P> . Find magnetic course and the distance ; agnetic course !$$B @ distance $5 9 a) agnetic course $!$B @ distance $5 9 b) c) agnetic course $!$B @ distance ++ 9 agnetic course !$$B @ distance ++ 9 d) Answer ; a)

agnetic course !$$B @ distance $5 9 -----------------------------------------------------------------------------------------------------------------------------------------------------------------


,,


120.


#$ute Manual %F#&'PS %F#&'PS (hart E)-6 FlDing from >T >9=>9 airport ( +5B!"P9 @ !!6B$$P>  to >1N )TT<>07 N>'F>92A9 ( +5B#$P9@ !!5B++P> . Find magnetic course and the distance ; agnetic course $55B @ distance +! 9 a) agnetic course #!5B @ distance $& 9 b) agnetic course $55B @ distance $& 9 c) agnetic course #!5B @ distance +! 9 d) Answer ; c)

agnetic course $55B @ distance $& 9 ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question question use Anne !""-6&$"A @ A>)9A?T0CA7 C2A)T 0CA #I,!! !!! 1T?TT=A)T 1T?TT=A)T (9 +&% or )oute 121. anual :F)E='1 chart >-% 

#$ute Manual %F#&'PS %F#&'PS (hart E)-6 FlDing from >)HAC2 airport ( +5B$#P9 @ !!6B,,P>  to '7T)09=>9 airport ( +5B""P9 @ !!5B,&P> . Find magnetic course and the distance ; agnetic course $5&B @ distance %! 9 a) agnetic course $,$B @ distance +# 9 b) agnetic course $5&B @ distance +# 9 c) agnetic course #!5B @ distance %! 9 d) Answer ; c)

agnetic course $5&B @ distance +# 9 -----------------------------------------------------------------------------------------------------------------------------------------------------------------


,%


( For this question question use Anne !""-6&$"A @ A>)9A?T0CA7 C2A)T 0CA #I,!! !!! 1T?TT=A)T 1T?TT=A)T (9 +&% or )oute anual :F)E='1 chart >-% 

122.

#$ute Manual %F#&'PS %F#&'PS (hart E)-6 FlDing from 'osition 10=A)09=>9 ( +5B!,P9 @ !!6B#"P>  to H0H>)AC2 airport ( +5B!&P9 @ !!6B+%P> . Find magnetic course and the distance ; agnetic course !5%B @ distance "$ 9 a) agnetic course $%&B @ distance $$ 9 b) c) agnetic course !6"B @ distance +# 9 agnetic course !5%B @ distance $$ 9 d) Answer ; d)

agnetic course !5%B @ distance $$ 9 ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question question use anne !""-6&$$A @ A>)9A?T0CA7 C2A)T 0CA #I,!! !!! 1T?TT=A)T (9 +&% or )oute 123. anual :F)E='1 chart >-% 

#$ute Manual %F#&'PS %F#&'PS (hart E)-6 FlDing from 1A?7=A? airport ( +5B!$P9 @ !!6B"#P>  to A7T>91TAT A7T>91TAT airport ( +&B,!P9 @ !#!B,"P> . Find magnetic course and the distance ; agnetic course #!$B @ distance ,% 9 a) agnetic course $5$B @ distance ,% 9 b) agnetic course !&5B @ distance 5$ 9 c) agnetic course #!$B @ distance 5$ 9 d) Answer ; a)

agnetic course #!$B @ distance ,% 9 -----------------------------------------------------------------------------------------------------------------------------------------------------------------


,&


( For this question use anne anne !""-6&"5A@ A>)9A?T0CA7 C2A)T 0CA #I,!! #I,!! !!! 1T?TT=A)T (9 +&% or )oute anual :F)E='1 chart >-%  FlDing :F) from '>0T09= ( +&B+5.!P9 @ !#!B,,.,P>  to 0>91TAT ( +&B"".,P9 @ !#!B#".!P>  determine the distance ; "% 9 a) ,5 9 b) "$ 9 c) +% 9 d)

124.

Answer ; c)

"$ 9 ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question question use anne !""-6&"&A @ A>)9A?T0CA7 C2A)T 0CA #I,!! !!! 1T?TT=A)T (9 +&% or )oute 125. anual :F)E='1 chart >-%  FlDing :F) from '>0T09= ( +&B+5.!P9 @ !#!B,,.,P>  to 0>91TAT ( +&B"".,P9 @ !#!B#".!P>  determine the magnetic course ; $+"B a) !%"B b) $,&B c) !&&B d)

Answer ; a)

$+"B ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question question use anne !""-6&"6A @ A>)9A?T0CA7 C2A)T 0CA #I,!! !!! 1T?TT=A)T (9 +&% or )oute 126. anual :F)E='1 chart >-%  FlDing :F) from '>0T09= ( +&B+5.!P9 @ !#!B,,.,P>  to 0>91TAT ( +&B"".,P9 @ !#!B#".!P> .etermine the minimum altitude within a corridor , 9 left and , 9 right of the courseline in order to staD #!!! ft clear of obstacles ; a) %6!! ft %%!! ft b) ,,!! ft c) ,"!! ft d)

Answer ; a)

%6!! ft -----------------------------------------------------------------------------------------------------------------------------------------------------------------


,5


( For this question question use anne !""-6&",A @ A>)9A?T0CA7 C2A)T 0CA #I,!! !!! 1T?TT=A)T (9 +&% or )oute anual :F)E='1 chart >-% 

127.

#$ute Manual %F#&'PS %F#&'PS (hart E)-6 FlDing :F) from :07709=>9 ( +5B!".,P9 @ !!5B$&.!P>  to F)>?>91TAT ( +5B$5.!P9 @ !!5B$+.!P>  determine the distance ; a) $5 9 $+ 4m b) +% 9 c) $+ 9 d) Answer ; d)

$+ 9 -----------------------------------------------------------------------------------------------------------------------------------------------------------------


,6


( For this question question use anne !""-6&"+A @ A>)9A?T0CA7 C2A)T 0CA #I,!! !!! 1T?TT=A)T (9 +&% or )oute anual :F)E='1 chart >-% 

128.

#$ute Manual %F#&'PS %F#&'PS (hart E)-6 FlDing :F) from :07709=>9 ( +5B!".,P9 @ !!5B$&.!P>  to F)>?>91TAT ( +5B$5.!P9 @ !!5B$+.!P>  determine the magnetic course. a) #&%B !!+B b) ",%B c) #5,B d) Answer ; c)

",%B ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question question use anne !""-6&"%A @ A>)9A?T0CA7 C2A)T 0CA #I,!! !!! 1T?TT=A)T (9 +&% or )oute 129. anual :F)E='1 chart >-%  FlDing :F) from :07709=>9 ( +5B!".,P9 @ !!5B$&.!P>  to F)>?>91TAT ( +5B$5.!P9 @ !!5B$+.!P> .etermine the minimum altitude within a corridor , 9 left and , 9 right of the courseline in order to staD #!!! ft clear of obstacles ; #,!! ft a) +$!! ft b) $6!! ft c) "6!! ft d)

Answer ; d)

"6!! ft -----------------------------------------------------------------------------------------------------------------------------------------------------------------


%!


Following in-flight depressurisation @ a turbine powered aeroplane is forced to di8ert to an en-route alternate airfield. 0f 130. actual flight conditions are as forecast @ the minimum quantitD of fuel remaining on arri8al at the airfield will be ; a) at least equi8alent to "! minutes flDing time. at least equi8alent to the quantitD quantitD required required to flD to another aerodrome in the e8ent that weather conditions so b) require. laid down bD the operator @ with the quantitD being specified in the operating manual. c) at least equi8alent to +, minutes flDing time. d) Answer ; a)

at least equi8alent to "! minutes flDing time. ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use anne !""-#$"+#A or Flight 'lanning anual )*T # Figure +.".#C  131.

Annex 033-12341A 033-12341A For a flight of #6!! ground nautical miles the following applD ; 2ead wind component #! 4t Temperature Temperature 01A -,BC Trip fuel a8ailable #,!!! 4g 7anding mass ,!!!! 4g
#&!!! ft


%#


----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this this question use anne !""-#$"++A or Flight 'lanning anual )*T # Figure +.".#C 

132.

Annex 033-12344A 033-12344A For a flight of $!!! ground nautical miles @ cruising at "!!!! ft @ within the limits of the data gi8en @ a headwind component of $, 4t will affect the trip time bD approimatelD ; -".% a) E$." b) E&.% c) E,." d) Answer ; c)

E&.%


%$


----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this this question use anne !""-#$",#A or Flight 'lanning anual )*T # Figure +."., 

133.

Annex 033-12351A 033-12351A For a flight of $+!! ground nautical miles the following applD ; Tail wind $, 4t Temperature Temperature 01A - #!BC Hra4e release mass %%!!! 4g The (a trip fuel and (b trip time respecti8elD are ; (a #+!!! 4g @ (b , hr ", min a) (a #,!!! 4g @ (b % hr !! min b) (a #,5!! 4g @ (b % hr $! min c) (a #+%!! 4g @ (b , hr +, min d) Answer ; a)

(a #+!!! 4g @ (b , hr ", min


%"


----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use anne !""-#$"+6A or Flight 'lanning anual )*T # Figure +.".#C 

134.

Annex 033-12349A 033-12349A For a flight of $+!! ground nautical miles the following applD ; Tail Tail wind component $, 4t Temperature Temperature 01A -#!BC Cruise altitude "#!!! ft 7anding mass ,$!!! 4g The (a trip fuel and (b trip time respecti8elD are ; (a #$!!! 4g @ (b , hr #, min a) (a #"%!! 4g @ (b % hr "! min b) (a #+$!! 4g @ (b , hr "! min c) (a #%$!! 4g @ (b , hr +, min d) Answer ; c)

(a #+$!! 4g @ (b , hr "! min


%+


----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use anne !""-#$"+6A or Flight 'lanning anual )*T # Figure +.".#C 

135.

Annex 033-12349A 033-12349A For a flight of $+!! ground nautical miles the following applD ; Temperature Temperature 01A -#!BC Cruise altitude $6!!! ft 7anding mass +,!!! 4g Trip fuel a8ailable #%!!! 4g
", 4t


%,


----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this this question use anne !""-#$""6A or Flight 'lanning anual )*T # Figure +.".#C +.".#C 

136.

Annex 033-12339A 033-12339A For a flight of $5!! ground nautical miles the following applD ; 2ead wind component #, 4t Temperature Temperature 01A E #,BC Cruise altitude ",!!! ft 7anding mass ,!!!! 4g The (a trip fuel and (b trip time respecti8elD are ; (a $!!!! 4g @ (b & hr !! min a) (a #%$!! 4g @ (b % hr $! min b) (a #&%!! 4g @ (b % hr ,! min c) (a #&!!! 4g @ (b % hr #! min d) Answer ; c)

(a #&%!! 4g @ (b % hr ,! min


%%


----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use anne !""-#$"+!A or Flight 'lanning anual )*T # Figure +."., 

137.

Annex 033-12340A 033-12340A For a flight of $5!! ground nautical miles the following applD ; 2ead wind component $! 4t Temperature Temperature 01A E #,BC Hra4e release mass %+&!! 4g The (a trip fuel and (b trip time respecti8elD are ; (a #,5!! 4g @ (b % hr #, min a) (a #&!!! 4g @ (b % hr +, min b) (a #%$!! 4g @ (b % hr $! min c) (a #5+!! 4g @ (b & hr !! min d) Answer ; b)

(a #&!!! 4g @ (b % hr +, min


%&


----------------------------------------------------------------------------------------------------------------------------------------------------------------( For the question use anne !""-#$"+%A or Flight Flight 'lanning anual )*T # Figure +.".#C +.".#C 

138.

Annex 033-12346A 033-12346A For a flight of $5!! ground nautical miles the following applD ; Tail Tail wind component +, 4t Temperature Temperature 01A - #!BC Cruise altitude $6!!! ft 7anding mass ,,!!! 4g The (a trip fuel (b trip time respecti8elD are ; (a #%!!! 4g @ (b % hr $, min a) (a #&#!! 4g @ (b % hr !& min b) (a $!!!! 4g @ (b % hr +! min c) (a #5!!! 4g @ (b , hr ,! min d) Answer ; b)

(a #&#!! 4g @ (b % hr !& min


%5


----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use anne !""-#$"+&A or Flight 'lanning anual )*T # Figure +."., 

139.

Annex 033-12347A 033-12347A For a flight of ",!! ground nautical miles the following applD ; Tail Tail wind component ,! 4t Temperature Temperature 01A E#!BC Hra4e release mass %,!!! 4g The (a trip fuel and (b trip time respecti8elD are ; (a $#5!! 4g @ (b 6 hr $, min a) (a #5#!! 4g @ (b & hr $! min b) (a #,5!! 4g @ (b % hr !! min c) (a #6!!! 4g @ (b & hr +,min d) Answer ; b)

(a #5#!! 4g @ (b & hr $! min


%6


----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use Anne !"#-##$$5A 

140.

Annex 033-1122"A 033-1122"A For a long distance flight at F7 "&! @ “7ong )ange” regime @ di8ided into four flight legs with the following specifications ; - segment AH - =round distance I $ !!! 9. headwind component I ,! 4t - segment HC - =round distance I # !!! 9. headwind component I "! 4t - segment C - =round distance I ,!! 9. tailwind component I &! 4t - segment > - =round distance I # !!! 9. headwind component I $! 4t The total air distance is approimatelD ; + ,5! 9 a) + 6+! 9 b) + 5!! 9 c) + 5$! 9 d) Answer ; c)

+ 5!! 9


&!


----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use Anne !""-##$$5A 

141.

Annex 033-1122"A 033-1122"A For a long distance flight at F7 "6! @ “7ong )ange” regime @ di8ided into four flight legs with the following characteristics ; - segment AH - =round distance I $ !!! 9. head wind component I ,! 4t - segment HC - =round distance I # !!! 9. head wind component I "! 4t - segment C - =round distance I ,!! 9. tail wind component I #!! 4t - segment > - =round distance I # !!! 9. head wind component I &! 4t The air distance of the entire flight is approimatelD ; , !+! 9 a) , #$! 9 b) + 6!! 9 c) + %"! 9 d) Answer ; c)

+ 6!! 9


&#


-----------------------------------------------------------------------------------------------------------------------------------------------------------------

142.

For a planned flight the calculated fuel is as follows ; Flight time I " h !% min The reser8e fuel @ at anD time @ should not be less than "! of the remaining trip fuel. Tai fuel I 5 4g Hloc4 fuel I ##5 4g 2ow much fuel should remain after $ hours flight time 3 "6 4g trip fuel and #$ 4g reser8e fuel. a) "! 4g trip fuel and 6 4g reser8e fuel. b) $& 4g trip fuel and #$ 4g reser8e fuel. c) "6 4g trip fuel and no reser8e fuel. d)

Answer ; b)

"! 4g trip fuel and 6 4g reser8e fuel. ----------------------------------------------------------------------------------------------------------------------------------------------------------------For a planned flight the calculated fuel is as follows ; 143. Flight time I $ h +$ min The reser8e fuel @ at anD time @ should not be less than "! of the remaining trip fuel. Tai fuel I 6 4g Hloc4 fuel I #"% 4g 2ow much fuel should remain after $ hours flight time 3 $, 4g trip fuel and 5 4g reser8e fuel. a) "" 4g trip fuel and no reser8e fuel. b) "" 4g trip fuel and #! 4g reser8e fuel. c) d) $" 4g trip fuel and #! 4g reser8e fuel.

Answer ; a)

$, 4g trip fuel and 5 4g reser8e fuel. ----------------------------------------------------------------------------------------------------------------------------------------------------------------For a repetiti8e ATC ATC flight plan ( )'7  to be used @ flights must ta4e t a4e place on a regular basis on at least ; 144. "! occasions. a) b) ,! occasions. $! occasions. c) #! occasions. d)

Answer ; d)

#! occasions. -----------------------------------------------------------------------------------------------------------------------------------------------------------------


&$


145.

( For this question use anne !"#-##$$6A 

Annex 033-11229A 033-11229A For a turboGet aeroplane flDing with a mass of #6! !!! 4g @ at ach !.5$ @ and 4nowing that the temperature at flight le8el F7 "&! is - ",B C @ the optimum flight altitude calculated using the anne is ; "&+!! ft a) "5%!! ft b) "+%!! ft c) "&5!! ft d) Answer ; a)

"&+!! ft ----------------------------------------------------------------------------------------------------------------------------------------------------------------For an ATC ATC flight plan filed before the flight @ the indicated tim e of departure is ; 146. the time at which the flight plan is filed. a) the time o8erhead the first reporting point after ta4e-off. b) the estimated off-bloc4 time. c) the time of ta4e-off. d)

Answer ; c)

the estimated off-bloc4 time.


&"


-----------------------------------------------------------------------------------------------------------------------------------------------------------------

147.

For flight planning purposes the landing mass at alternate is ta4en as ; Nero Fuel ass plus Final )eser8e Fuel and Alternate Fuel. a) Nero Fuel ass plus Final )eser8e Fuel and ContingencD Fuel. b) 7anding ass at destination plus Alternate Fuel. c) Nero Fuel ass plus Final )eser8e Fuel. d)

Answer ; b)

Nero Fuel ass plus Final )eser8e Fuel and ContingencD Fuel. ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use anne anne !""- ##!+,A ##!+,A or )oute )oute anual anual 1TA) 1TA) chart chart for A)0 HA)A*A1 (#!-$A@H  148.

Annex 033-11045A 033-11045A For runwaD "" arri8als from the east and south @ the 0nitial Approach Fi ( 0AF  inbound from airwaD ?)#! is ; C*9 a) T07 b) C>9TA c) d) :TH Answer ; d)

:TH -----------------------------------------------------------------------------------------------------------------------------------------------------------------


&+


149.

( For this this question use anne !""-#$"%+A or Flight 'lanning anual )*T # Figure +.&.$ 

Annex 033-12364A 033-12364A For the purpose of planning an etended range flight it is required that with a start of di8ersion mass of ,,!!! 4g a di8ersion of %!! nautical miles should be achie8ed in 6! minutes. ?sing the abo8e table @ the onlD listed cruise technique to meet that requirement is ; 7)C a) /0A1 .&+$6! b) /0A1 .&+""! c) d) /0A1 .&!$5! Answer ; c)

/0A1 .&+""! ---------------------------------------------------------------------------------------------------------------------------------------------------------------For the purposes of 0tem 6 (
Answer ; d)

medium “” ----------------------------------------------------------------------------------------------------------------------------------------------------------------For turboGet engine dri8en aeroplane @ gi8en ; 151. Tai Tai fuel %!! 4g Fuel flow for cruise #! !!! 4gh Fuel flow for holding 5 !!! 4gh Alternate fuel #! $!! 4g 'lanned flight time to destination % h Forecast 8isibilitD at destination $!!! m The minimum ramp fuel required is ; && 5!! 4g a) &% #!! 4g b) &6 $!! 4g c) 5! ,!! 4g d)

Answer ; a)

&& 5!! 4g


&,


-----------------------------------------------------------------------------------------------------------------------------------------------------------------

152.

From the options gi8en below select those flights which require ATC ATC flight plan notification ; #. AnD 'ubl 'ublic ic Trans ansport port flig flight ht.. $. AnD 0F) flight ". AnD flig flight ht which which is to to be carr carried ied out out in regio regions ns which which are are desig designat nated ed to ease ease the the pro8i pro8isio sionn of the the Alerting 1er8ice or the operations of 1earch and )escue. +. AnD cross-bo -border flights ,. AnD AnD fli fligh ghtt whic whichh in8 in8ol ol8e 8ess o8e o8erf rflD lDin ingg wat water er #@, a) $@+ b) "@+@, c) d) #@$@"

Answer ; b)

$@+ ----------------------------------------------------------------------------------------------------------------------------------------------------------------From which of the following would Dou epect to find details of the 1earch and )escue organisation and procedures 153. ( 1A)  3 a) 9TA A0' b) 10=>T c) ATCC ATCC broadcasts broadcast s d)

Answer ; b)

A0' ----------------------------------------------------------------------------------------------------------------------------------------------------------------From which of the following would Dou epect to find facilitation information regarding customs and health formalities 3 154. 9A:)A 9A:)A charts a) A0' b) ATCC c) 9TA d)

Answer ; b)

A0' ----------------------------------------------------------------------------------------------------------------------------------------------------------------From which of the t he following would Dou epect to find information regarding 4nown short unser8iceabilitD of :) @ TACA9 155. @ and 9H 3 ATCC ATCC broadcasts broadcast s a) b) A0' 10=>T c) 9TA d) Answer ; d)

9TA ----------------------------------------------------------------------------------------------------------------------------------------------------------------156. From which of the following would Dou epect to find the dates and times when temporarD danger areas are acti8e 3 10=>T a) 9TA and A0' b) )A9A: charts c) nlD A0' d)

Answer ; b)

9TA and A0' ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question question use anne !""-6&$#A @ A>)9A?T0CA7 C2A)T 0CA #I,!! !!! 1T?TT=A)T (9 +&% or )oute 157. anual :F)E='1 chart >-%  =i8e the frequencD of 1T?TT=A)T AT01 ; ##$.$,! 2M a) #",.&&, 2M b) #$%.#$, 2M c) #$%.#$, 42M d)

Answer ; c)

#$%.#$, 2M -----------------------------------------------------------------------------------------------------------------------------------------------------------------


&%


( For this question question use anne !""-6&$#A @ A>)9A?T0CA7 C2A)T 0CA #I,!! !!! 1T?TT=A)T (9 +&% or )oute anual :F)E='1 chart >-%  =i8e the frequencD of NQ)0C2 :7>T ; #$&.$! 2M a) #$&.$! 42M b) #$5.,$, 2M c) ##5.#! 2M d)

158.

Answer ; a)

#$&.$! 2M ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question question use anne !""-6&$#A @ A>)9A?T0CA7 C2A)T 0CA #I,!! !!! 1T?TT=A)T (9 +&% or )oute 159. anual :F)E='1 chart >-%  =i8e the name and frequencD of the Flight 0nformation 1er8ice for an aeroplane in position ( +&B,6P9 @ !#!B#+P>  ; F)A9/F?)T 09F)AT09 #$5.6, 2M a) b) >09=>9 09F)AT09 #$$.# 2M Q9C2>9 09F)AT09 #$%.6, 2M c) Q9C2>9 09F)AT09 #$!.%, 2M d)

Answer ; c)

Q9C2>9 09F)AT09 #$%.6, 2M ----------------------------------------------------------------------------------------------------------------------------------------------------------------160. ( For this this question use anne !""-6&#%A or Flight 'lanning anual 1>' # Figure $.+ 

Annex 033-9716A 033-9716A =i8en ; Aeroplane mass at start-up "%%" lbs A8iation A8iation gasoline ( densitD % lbsgal -fuel load &+ gal Ta4e-off Ta4e-off altitude sea le8el 2eadwind +! 4t Cruising altitude 5!!! ft 'ower setting full throttle $"!! )' $!BC lean of pea4 >=T Calculate the ground range ; %"" 9 a) ,+&., 9 b) &"! 9 c) 5++ 9 d) Answer ; a)

%"" 9


&&


----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use annees !""-##$$"A@ !""-##$$"H and !""-##$$"C  =i8en ; Ta4e-off Ta4e-off mass I #,! !!! 4g 'lanned cruise at F7 ",! 7ong range AC2 1tandard Atmosphere ( 01A  C= I "&  Co8ering an air distance of $ !!! 9 @ Dour trip fuel from ta4e-off to landing will be ; a) #6 %%! 4g $! $%! 4g b) $$ "%! 4g c) $# &%! 4g d)

161.

Answer ; c)

$$ "%! 4g ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this this question use anne !""-""!6A or Flight 'lanning anual )*T # Figure +.,.# +.,.#  162.

Annex 033-3307A 033-3307A =i8en ; mass at bra4e release ,& ,!! 4g temperature 01A -#!BC a8erage head wind component #% 4t initial cruise F7 $5! Find I Climb fuel ; #!+! 4g a) #$"5 4g b) #"5& 4g c) ##"5 4g d) Answer ; d)

##"5 4g


&5


----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this this question use anne !""-""!&A or Flight 'lanning anual )*T # Figure +.,.# +.,.# 

163.

Annex 033-3307A 033-3307A =i8en ; Hra4e release mass ,&,!! 4g Temperature Temperature 01A -#!BC A8erage A8erage headwind component #% 4t 0nitial F7 $5! Find I Climb fuel for enroute climb $5!.&+ ; #!+! 4g a) #$"5 4g b) ##"5 4g c) #"5& 4g d) Answer ; c)

##"5 4g


&6



164.

Annex 033-3307A 033-3307A =i8en ; estimated ta4e-off mass ,& ,!! 4g initial cruise F7 $5! a8erage temperature during climb 01A -#!BC; a8erage head wind component #5 4t Find I Climb time ; #, min a) #" min b) ## min c) #+ min d) Answer ; b)

#" min


5!



165.

Annex 033-3307A 033-3307A =i8en ; Hra4e release mass ,&,!! 4g 0nitial F7 $5! A8erage A8erage temperature during climb 01A -#!BC A8erage A8erage head wind component #5 4t Find I Climb time for enroute climb $5!.&+ ; ## min a) #" min b) #, min c) #+ min d) Answer ; b)

#" min


5#


----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use annees annees !""-""$!A @ !""-""$!H and !""-""$!C or Flight 'lanning anual anual )*T # Figures Figures +.$.# +.$.# @ +.$.$ and +.,.".$  166.

Annexe 033-3320A 033-3320A  033-3320!  033-3320/ 033-3320/ =i8en ; >stimated ta4e-off mass ,&!!! 4g =round distance #,! 9 Temperature Temperature 01A -#!BC Cruise at .&+ ach Find I Cruise altitude and epected true air speed ; ""6!! ft @ +$! 4t a) $+!!! ft @ ++, 4t b) "",!! ft @ +"! 4t c) $,!!! ft @ +", 4t d) Answer ; d)

$,!!! ft @ +", 4t


5$


----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use annees annees !""-""$!A @ !""-""$!H and !""-""$!C or Flight 'lanning anual anual )*T # Figures Figures +.$.# +.$.# @ +.$.$ and +.,.".$  167.

Annexe 033-3320A 033-3320A  033-3320!  033-3320/ 033-3320/ =i8en ; >stimated ta4e-off mass ,& !!! 4g 1till air distance #,! 9A utside air temperature ( AT  01A -#!/ Cruise at !.&+ ach. Find I Cruise altitude and epected true airspeed ; $$ !!! ft @ +,# 4t a) $, !!! ft @ +", 4t b) $, !!! ft @ ++, 4t c) $$ !!! ft @ ++# 4t d) Answer ; b)

$, !!! ft @ +", 4t


5"


-----------------------------------------------------------------------------------------------------------------------------------------------------------------

168.

( For this this question use anne !""-""!%A or Flight 'lanning anual )*T # Figure +.,.".# +.,.".# 

Annex 033-3306A 033-3306A =i8en ; Flight time from top of climb to the enroute point in F7$5! is +5 min. Cruise procedure is long range cruise ( 7)C . Temp I 01A -,B C Ta4e-off Ta4e-off mass I ,% !!! 4g Climb fuel I ##!! 4g Find I istance in nautical air miles ( 9A  for this leg and fuel consumption ; +"& 9A @$#!! 4g a) "+, 9A @$!!! 4g b) ",! 9A @$!!! 4g c) "+, 9A @$#!! 4g d) Answer ; b)

"+, 9A ;@$!!! 4g -----------------------------------------------------------------------------------------------------------------------------------------------------------------


5+


169.

( For this this question use anne !""-+&",A or Flight 'lanning anual 1>' # Figure $., 

Annex 033-4735A 033-4735A =i8en ; F7 &, 7ean miture Full throttle $"!! )' Ta4e-off Ta4e-off fuel I +++ lbs Ta4e-off Ta4e-off from 17 Find I >ndurance in hours and minutes ; !,I$! a) b) !,I#$ !+I+$ c) !,I$" d) Answer ; b)

!,I#$ -----------------------------------------------------------------------------------------------------------------------------------------------------------------


5,


170.

( For this this question use anne !""-""$#A or Flight 'lanning anual )*T # Figure +.".#.H +.".#.H 

Annex 033-3321A 033-3321A =i8en ; estimated Mero fuel mass ,! t estimated landing mass at alternate ,$ t final reser8e fuel $ t alternate fuel # t flight to destination @ distance &$! 9 @ true course ( TC  !"! @ <: "+!"! cruise I long range F7 ""! outside air temperature -"! B C. Find I >stimated trip fuel and time ; + &,! 4g @ !$I !! a) + 5!! 4g @ !#I +, b) + %!! 4g @ !$I !, c) + +!! 4g @ !$I !, d) Answer ; b)

$, !!! ft @ +", 4t


5%


-----------------------------------------------------------------------------------------------------------------------------------------------------------------

171.

( For this question use annees !""-6%6+A and !""-6%6+H or Flight 'lanning anual )*T # Figure +.,.".# and Figure

+.".#H 

Annexe 033-9694A 033-9694A  033-9694! =i8en ; Twin Get aeroplane Nero fuel mass ,!!!! 4g 7anding mass at alternate ,$!!! 4g Final reser8e fuel $!!! 4g Alternate fuel #!!! 4g Flight to destination I istance &$! 9 @ True course !"!B@ <: "+!B"! 4t 7ong range cruise @ F7 ""! utside air temperature -"!BC Find I >stimated trip fuel and time with simplified flight planning ; ++!! 4g @ !$ h !, min a) +5!! 4g @ !# h ,# min b) +&,! 4g @ !$ h !! min c) +%!! 4g @ !$ h !, min d) Answer ; b)

+5!! 4g @ !# h ,# min -----------------------------------------------------------------------------------------------------------------------------------------------------------------


5&


172.

( For this this question use anne !""-6%6&A or Flight 'lanning anual )*T # Figure +.+ 

Annex 033-9697A 033-9697A =i8en ; Twin Get aeroplane >stimated mass on arri8al at the alternate ,!!!! 4g >le8ation at destination aerodrome ",!! ft >le8ation at alternate aerodrome "! ft Find I Final reser8e fuel ; ##,! 4g a) b) ##5! 4g $"!! 4g c) $"%! 4g d) Answer ; b)

##5! 4g ----------------------------------------------------------------------------------------------------------------------------------------------------------------173. ( For this question use anne !""-6%6&A or Flight 'lanning anual )*T # Figure +.+ 

Annex 033-9697A 033-9697A =i8en ; Twin Get aeroplane >stimated mass on arri8al at the alternate ,!!!! 4g >stimated mass on arri8al at the destination ,$,$, 4g Alternate ele8ation 17 estination ele8ation #,!! ft Find I Final reser8e fuel and corresponding time ; ##5! 4g @ +, min a) ##5! 4g @ "! min b) $"%! 4g @ "! min c) $"%! 4g @ !# h !! min d) Answer ; b)

##5! 4g @ "! min -----------------------------------------------------------------------------------------------------------------------------------------------------------------


55


174.

( For this this question use anne !""-6%6&A or Flight 'lanning anual )*T # Figure +.+ 

Annex 033-9697A 033-9697A =i8en ; rD operating mass ", ,!! 4g >stimated load #$ !!! 4g ContingencD approach and landing fuel $ ,!! 4g >le8ation at departure aerodrome ,!! ft >le8ation at alternate aerodrome "! ft Find I Final reser8e fuel for a Get aeroplane ( holding  and gi8e the ele8ation which is rele8ant ; $ "%! 4g @ destination ele8ation a) b) # #5! 4g @ alternate ele8ation # #5! 4g @ destination ele8ation c) $ "%! 4g @ alternate ele8ation d) Answer ; b)

# #5! 4g @ alternate ele8ation -----------------------------------------------------------------------------------------------------------------------------------------------------------------


56


175.

( For this this question use anne !""-""$$A or Flight 'lanning anual )*T # Figure +.".% +.".% 

Annex 033-3322A 033-3322A =i8en ; >stimated drD operation mass ", ,!! 4g >stimated load #+ ,!! 4g Final reser8e fuel #$!! 4g istance to alternate 6, 9 A8erage A8erage true trac4 $#6B 2ead wind component #! 4t Find I Fuel and time to alternate ; 5!! 4g @ $+ min a) # #!! 4g @ ++ min b) # #!! 4g @ $, min c) 5!! 4g @ +! min d) Answer ; c)

# #!! 4g @ $, min -----------------------------------------------------------------------------------------------------------------------------------------------------------------


6!


176.

( For this this question use anne !""-""!,A or Flight 'lanning anual )*T # Figure +.,.".# +.,.".# 

Annex 033-3305A 033-3305A =i8en ; long range cruise I temp. -%"B C at F7 ""! initial gross mass enroute I ,+ #!! 4g leg flight time I $6 min Find I Fuel consumption for this leg ; # $!! 4g a) # %5! 4g b) # #!! 4g c) # !!! 4g d) Answer ; c)

# #!! 4g -----------------------------------------------------------------------------------------------------------------------------------------------------------------


6#


177.

( For this this question use anne !""-+&"%A or Flight 'lanning anual 1>' # Table Table $.$." 

Annex 033-4736A 033-4736A =i8en ; F7 &! AT -#6BC 7ean miture $"!! )' Find I Fuel flow in gallons per hour ( ='2  and TA1 ; a) #$.", ='2 @ TA1 I #,# 4t &".6! ='2 @ TA1 I #,6 4t b) ##.6, ='2 @ TA1 I #%! 4t c) #$.", ='2 @ TA1 I #,6 4t d) Answer ; d)

#$.", ='2 @ TA TA1 1 I #,6 4t -----------------------------------------------------------------------------------------------------------------------------------------------------------------


6$


178.

( For this this question use anne !""-+&"%A or Flight 'lanning anual 1>' # Table Table $.$." 

Annex 033-4736A 033-4736A =i8en ; F7 &, AT E#!BC 7ean miture $"!! )' Find I Fuel flow in gallons per hour ( ='2  and TA1 ; %5., ='2 @ TA1 I #%! 4t a) ##.% ='2 @ TA1 I #+" 4t b) c) ##.% ='2 @ TA1 I #%! 4t &#.# ='2 @ TA1 I #+" 4t d) Answer ; c)

##.% ='2 @ TA1 I #%! 4t -----------------------------------------------------------------------------------------------------------------------------------------------------------------


6"


179.

( For this this question use anne !""-6%6%A or Flight 'lanning anual )*T # Figure +.".% +.".% 

=i8en ;

Annex 033-9696A 033-9696A

Twin Get aeroplane rD operating mass ",,!! 4g Traffic load #+,!! 4g Final reser8e fuel #$!! 4g istance to alternate 6, 9 Tailwind Tailwind component #! 4t Find I Fuel required and trip time to alternate with simplified flight planning ( A7T>)9A A7T>)9AT> T> '7A9909=  ; #!!! 4g @ $+ min a) 5!! 4g @ !.+ hr b) #!!! 4g @ +! min c) 5!! 4g @ $+ min d) Answer ; a)

#!!! 4g @ $+ min -----------------------------------------------------------------------------------------------------------------------------------------------------------------


6+


180.

( For this this question use anne !""-6%6,A or Flight 'lanning anual )*T # Figure +."."C +."."C 

Annex 033-9695A 033-9695A =i8en ; Twin Get aeroplane =round distance to destination aerodrome is #%!! 9 2eadwind component ,! 4t F7 ""! Cruise .&5 ach 01A e8iation E$!BC and 7anding mass ,,!!! 4g Find I Fuel required and trip time with simplified flight planning ; ##%!! 4g @ !+ h #, min a) #$!!! 4g @ !" h ,# min b) ##+!! 4g @ !+ h #$ min c) #$+!! 4g @ !+ h !! min d) Answer ; d)

#$+!! 4g @ !+ h !! min -----------------------------------------------------------------------------------------------------------------------------------------------------------------


6,


181.

=i8en ; aimum allowable ta4e-off mass %++!! 4g aimum landing mass ,%$!! 4g aimum Mero fuel mass ,"!!! 4g rD operating mass ",,!! 4g Traffic load #+,!! 4g Trip fuel +6!! 4g Ta4e-off Ta4e-off fuel &+!! 4g Find I aimum additional load ; &!!! 4g a) b) "!!! 4g ,%!! 4g c) +!!! 4g d)

Answer ; b)

"!!! 4g ----------------------------------------------------------------------------------------------------------------------------------------------------------------182. =i8en ; aimum allowable ta4e-off mass %++!! 4g aimum landing mass ,%$!! 4g aimum Mero fuel mass ,"!!! 4g rD operating mass ",,!! 4g Traffic load #+,!! 4g Trip fuel +6!! 4g inimum Ta4e-off Ta4e-off Fuel &+!! 4g Find I aimum allowable ta4e-off fuel ; #++!! 4g a) ##+!! 4g b) 5%!! 4g c) d) ###!! 4g

Answer ; d)

###!! 4g ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use anne !""-6,&%A or )oute anual chart >(20, CAA->dition  183. =i8en ; 7eg oulins ( 9+% +$.+ >!!" "5.!   iGon ( 9+& #%." >!!, !,.6 . Find I )oute designator and total distance ; ?= $# @ $% 9 a) ?= $# @ %6 9 b) irect route @ %6 9 c)  @ ++ 9 d)

Answer ; c)

irect route @ %6 9 -----------------------------------------------------------------------------------------------------------------------------------------------------------------


6%


184.

( For this this question use anne !""-""$"A or Flight 'lanning anual )*T # Figure +."."C +."."C 

Annex 033-3323A 033-3323A =i8en ; ground distance to destination aerodrome # %!! 9 headwind component ,! 4t F7 ""! cruise !.&5 ach 01A E $! B C estimated landing weight ,,!!! 4g . Find I 1implified flight planning to determine estimated trip fuel and trip time ; #$ +!! 4g @ !+ h #$ min a) #$ +!! 4g @ !" h ,, min b) ## +!! 4g @ !+ h #$ min c) ## +!! 4g @ !" h ,, min d) Answer ; b)

#$ +!! 4g @ !" h ,, min -----------------------------------------------------------------------------------------------------------------------------------------------------------------


6&


185.

( For this this question use annees !""-""!&A or Flight 'lanning anual )*T # Figure +.,.# 

Annex 033-3307A 033-3307A =i8en ; bra4e release mass ,& ,!! 4g temperature 01A -#!BC head wind component #% 4t initial F7 $5! Find I 1till air distance ( 9A  and ground distance ( 9  for the climb ; %& 9A @ &# 9 a) %$ 9A @ ,6 9 b) &# 9A @ %& 9 c) ,6 9A @ %$ 9 d) Answer ; b)

%$ 9A @ ,6 9


65



186.

Annex 033-3307A 033-3307A =i8en ; Hra4e release mass ,&,!! 4g Temperature Temperature 01A -#!BC 2eadwind component #% 4t 0nitial F7 $5! Find I 1till air distance ( 9A  and ground distance ( 9  for the enroute climb $5!.&+ ; ,6 9A @ %$ 9 a) %$ 9A @ ,6 9 b) %$ 9A @ &# 9 c) &# 9A @ %& 9 d) Answer ; b)

%$ 9A @ ,6 9


66


----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this this question use anne !""-+&"&A or Flight 'lanning anual 1>' # Figure $.# 

187.

Annex 033-4737A 033-4737A =i8en ; F7 &, AT E,BC uring climb a8erage head wind component $! 4t Ta4e-off Ta4e-off from 17 with the initial i nitial mass of " %,! lbs. Find I 1till air distance ( 9A  and ground distance ( 9  using the graph “time @ fuel @ distance to climb” ; #% 9A. @ #5 9. a) b) #+ 9A. @ #5 9. #5 9A. @ #" 9. c) #5 9A. @ #, 9. d) Answer ; d)

#5 9A. @ #, 9. ----------------------------------------------------------------------------------------------------------------------------------------------------------------188. =i8en ; maimum allowable ta4e-off mass %+ +!! 4g maimum landing mass ,% $!! 4g maimum Mero fuel mass ," !!! 4g drD operating mass ", ,!! 4g estimated load #+ ,!! 4g estimated trip fuel + 6!!4g minimum ta4e-off fuel & +!! 4g Find the maimum allowable ta4e-off fuel ; #+ +!! 4g a) 5 %!! 4g b) ## +!! 4g c) ## #!! 4g d)

Answer ; d)

## #!! 4g


#!!


----------------------------------------------------------------------------------------------------------------------------------------------------------------=i8en ; aimum Ta4e-off Ta4e-off ass I %$ 5!! 4g aimum Nero Fuel ass I ,# $,! 4g aimum 7anding ass I ,+ 6!! 4g aimum Tai Tai ass I %" !,! 4g Trip fuel I # 5!! 4g Alternate fuel I # +!! 4g 2olding fuel ( final reser8e  I # $$, 4g rD perating ass I "+ !!! 4g Traffic 7oad I #" !!! 4g Catering I &,! 4g Haggage I " ,!! 4g Find the Ta4e-off ass ( T  ; ,#.,#, 4g a) b) ,,.&%, 4g ,$.$%, 4g c) ,#.+$, 4g d)

189.

Answer ; a)

,#.,#, 4g ----------------------------------------------------------------------------------------------------------------------------------------------------------------190. ( For this this question use anne !""-6&#,A or Flight 'lanning anual 1>' # Figure $.# 

Annex 033-9715A 033-9715A =i8en ; Ta4e-off Ta4e-off mass ",!! lbs eparture aerodrome pressure altitude $,!! ft AT E#!BC First cruising le8el I F7 F 7 #+! @ AT -,BC Find the time @ fuel and still air distance to climb ; $$ min @ %.& =A7 @ +, 9A a) $" min @ &.& =A7 @ ,! 9A b) $+ min @ &.& =A7 @ +& 9A c) #%., min @ +.6 =A7 @ "+., 9A d) Answer ; a)

$$ min @ %.& =A7 @ +, 9A


#!#


-----------------------------------------------------------------------------------------------------------------------------------------------------------------

191.

( For this question use anne !""-+&"&A or Flight 'lanning anual 1>' # Figure $.#

Annex 033-4737A 033-4737A =i8en ; F7 &, AT E,BC uring climb a8erage head wind component $! 4t Ta4e-off Ta4e-off from 17 with the initial i nitial mass of "%,! lbs. Find I Time and fuel to climb ; 6 min. @ $.& ?1= a) & min. @ $.% ?1= b) c) 6 min. @ "." ?1= #! min @ ".% ?1= d) Answer ; c)

6 min. @ "." ?1= -----------------------------------------------------------------------------------------------------------------------------------------------------------------


#!$


192.

( For this this question use anne !""-""!,A or Flight 'lanning anual )*T # Figure +.,.".# +.,.".# 

Annex 033-3305A 033-3305A =i8en ; F7 ""! 7ong range cruise AT -%"BC =ross mass ,! ,!! 4g Find I True airspeed ( TA1  +"# 4t a) +$! 4t b) +#5 4t c) +"" 4t d) Answer ; b)

+$! 4t -----------------------------------------------------------------------------------------------------------------------------------------------------------------


#!"


193.

( For this this question use anne !""-6%6#A or Flight 'lanning anual )*T # Figure +.,.".# +.,.".# 

Annex 033-9691A 033-9691A =i8en ; Twin Get aeroplane F7 ""! 7ong range cruise utside air temperature -%"BC =ross mass ,!,!! 4g Find I True air speed ( TA1  ; +"# 4t a) +#5 4t b) +"" 4t c) +$! 4t d) Answer ; d)

+$! 4t -----------------------------------------------------------------------------------------------------------------------------------------------------------------


#!+


194.

( For this this question use anne !""-6,&5A or Flight 'lanning anual )*T # Figure +.,.".# +.,.".# 

Annex 033-957"A 033-957"A =i8en ; 7ong range cruise AT -+,BC at F7 ",! =ross mass at the beginning of the leg +!!!! 4g =ross mass at the end of the leg "6!!! 4g Find I True air speed ( TA1 TA1  and cruise distance ( 9A  for a twin Get aeroplane ; TA1 +$" 4t @ $$& 9A a) TA1 +"" 4t @ $$& 9A b) TA1 +"" 4t @ ##%" 9A c) TA1 +$" 4t @ 6"% 9A d) Answer ; b)

TA1 +"" 4t @ $$& 9A -----------------------------------------------------------------------------------------------------------------------------------------------------------------


#!,


195.

( For this this question use anne !""-""#5A or Flight 'lanning anual )*T # Figure +.,.".# +.,.".# 

Annex 033-331"A 033-331"A =i8en ; long range cruise outside air temperature ( AT  -+, B C in F7 ",! mass at the beginning of the leg +! !!! 4g mass at the end of the leg "6 !!! 4g. Find I True airspeed ( TA1  at the end of the leg and the distance ( 9A  ; TA1 +"# 4t @ ##%" 9A a) TA1 +$" 4t @ $$& 9A b) TA1 +"# 4t @ $$& 9A c) TA1 +$" 4t @ 6"% 9A d) Answer ; c)

TA1 +"# 4t @ $$& 9A ----------------------------------------------------------------------------------------------------------------------------------------------------------------=i8en ; 196. True course ( TC  !#&B <: "+!B"! 4t True air speed ( TA1  +$! 4t Find I
Answer ; d)


#!%


197.

( For this question use 0mage #" 

,age 13 =i8en ; 'lanned and actual data as shown in the Flight 7og ecerpt. Actual =round 1peed ( =1  on the leg H>TA to =AA will be #!! /T. 0f all other flight parameters remain unchanged unchanged @ what fuel remaining should be epected at at waDpoint =AA 3 a) $%!! 4g $&&! 4g b) $5$! 4g c) $%5+ 4g d) Answer ; a)

$%!! 4g ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use 0mage +"  198.

,age 43 =i8en ; 'lanned and actual data as shown in the Flight 7og ecerpt. Actual =round 1peed ( =1  on the leg H>TA to =AA will be #!! /T. 0f all other flight parameters remain unchanged unchanged @ what fuel remaining should be epected at at waDpoint =AA 3 "#!6 4g a) ""6! 4g b) "!5! 4g c) $6,! 4g d) Answer ; d)

$6,! 4g


#!&


----------------------------------------------------------------------------------------------------------------------------------------------------------------199.

( For this question use 0mage ++ 

,age 44 =i8en ; 'lanned and actual data as shown in the Flight 7og ecerpt. Actual =round 1peed ( =1  on the leg H>TA to =AA will be #!, /T. 0f all other flight parameters remain unchanged unchanged @ what fuel remaining should be epected at at waDpoint =AA 3 a) "+"! 4g "+5! 4g b) "$%! 4g c) ""#5 4g d) Answer ; c)

"$%! 4g ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use 0mage +!  200.

,age 40 =i8en ; 'lanned and actual data as shown in the Flight 7og ecerpt. Actual =round 1peed ( =1  on the leg H>TA to =AA will be ##! /T. /T. 0f all other flight parameters remain unchanged unchanged @ what fuel remaining should be epected epected at waDpoint =AA 3 $#%! 4g a) $!!! 4g b) $"#! 4g c) $!%$ 4g d) Answer ; b)

$!!! 4g -----------------------------------------------------------------------------------------------------------------------------------------------------------------


#!5


201.

( For this question use 0mage +$ 

,age 42 =i8en ; 'lanned and actual data as shown in the Flight 7og ecerpt. Actual =round 1peed ( =1  on the leg H>TA to =AA will be ##! /T. /T. 0f all other flight parameters remain unchanged unchanged @ what fuel remaining should be epected epected at waDpoint =AA 3 a) $6!! 4g $%$, 4g b) $5$! 4g c) $&$" 4g d) Answer ; b)

$%$, 4g ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use 0mage +#  202.

,age 41 =i8en ; 'lanned and actual data as shown in the Flight 7og ecerpt. Actual =round 1peed ( =1  on the leg H>TA to =AA will be ##, /T. /T. 0f all other flight parameters remain unchanged unchanged @ what fuel remaining should be epected epected at waDpoint =AA 3 $+!! 4g a) $$"! 4g b) $,"! 4g c) $$&+ 4g d) Answer ; b)

$$"! 4g -----------------------------------------------------------------------------------------------------------------------------------------------------------------


#!6


203.

( For this question use 0mage 5 

,age " =i8en ; 'lanned and actual data as shown in the Flight 7og ecerpt. Arri8ing o8erhead =AA Dou Dou are cleared for direct routing to 0/>. The flight time for direct flight =AA to 0/> will be # hr !% mins @ assuming other flight data remains constant @ what fuel will be epected on arri8al o8erhead 0/>3 a) #!"% 4g #&!% 4g b) $%++ 4g c) #&$! 4g d) Answer ; b)

#&!% 4g ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use 0mage %  204.

,age 6 =i8en ; 'lanned and actual data as shown in the Flight 7og ecerpt. Arri8ing o8erhead =AA Dou Dou are cleared for direct routing to 0/>. The flight time for direct flight =AA to 0/> will be # hr !5 mins @ assuming other flight data remains constant @ what fuel will be epected on arri8al o8erhead 0/> 3 ,5$ 4g a) #$,! 4g b) $""5 4g c) #$&$ 4g d) Answer ; d)

#$&$ 4g -----------------------------------------------------------------------------------------------------------------------------------------------------------------


##!


205.

( For this question use 0mage " 

,age 3 =i8en ; 'lanned and actual data as shown in the Flight 7og ecerpt. Arri8ing o8erhead =AA Dou Dou are cleared for direct routing to 0/>. The flight time for direct flight =AA to 0/> will be # hr #! mins @ assuming other flight data remains constant @ what fuel will be epected on arri8al o8erhead 0/> 3 #,#! 4g a) b) "5! 4g $6#! 4g c) #"!! 4g d) Answer ; d)

#"!! 4g ----------------------------------------------------------------------------------------------------------------------------------------------------------------206. ( For this question use 0mage + 

,age 4 =i8en ; 'lanned and actual data as shown in the Flight 7og ecerpt. Arri8ing o8erhead =AA Dou Dou are cleared for direct routing to 0/>. The flight time for direct flight =AA to 0/> will be +! minutes @ assuming other flight data remains constant @ what fuel will be epected on arri8al o8erhead 0/> 3 #5,$ 4g a) #$%5 4g b) $%,$ 4g c) #6!! 4g d) Answer ; d)

#6!! 4g -----------------------------------------------------------------------------------------------------------------------------------------------------------------


### ###


207.

( For this question use 0mage 6 

,age 9 =i8en ; 'lanned and actual data as shown in the Flight 7og ecerpt. Arri8ing o8erhead =AA Dou Dou are cleared for direct routing to 0/>. The flight time for direct flight =AA to 0/> will be +$ minutes @ assuming other flight data remains constant @ what fuel will be epected on arri8al o8erhead 0/> 3 #+&, 4g a) b) $$+, 4g ##6, 4g c) %&! 4g d) Answer ; a)

#+&, 4g ----------------------------------------------------------------------------------------------------------------------------------------------------------------208. ( For this question use 0mage & 

,age 7 =i8en ; 'lanned and actual data as shown in the Flight 7og ecerpt. Arri8ing o8erhead =AA Dou Dou are cleared for direct routing to 0/>. The flight time for direct flight =AA to 0/> will be +, minutes @ assuming other flight data remains constant @ what fuel will be epected on arri8al o8erhead 0/> 3 #"5+ 4g a) $,$ 4g b) #!!$ 4g c) $!5$ 4g d) Answer ; a)

#"5+ 4g -----------------------------------------------------------------------------------------------------------------------------------------------------------------


##$


209.

( For this question use 0mage , 

,age 5 =i8en ; 'lanned and actual data as shown in the Flight 7og ecerpt. Arri8ing o8erhead =AA Dou Dou are cleared for direct routing to 0/>. The flight time for direct flight =AA to 0/> will be ,& minutes @ assuming other flight data remains constant @ what fuel will be epected on arri8al o8erhead 0/> 3 $"!, 4g a) b) #&$! 4g #+,! 4g c) &6! 4g d) Answer ; b)

#&$! 4g ----------------------------------------------------------------------------------------------------------------------------------------------------------------210. ( For this question use 0mage +, 

,age 45 =i8en ; 'lanned and actual data as shown in the Flight 7og ecerpt. 'ro8ided that flight conditions on the leg =AA to >7TA >7TA remain unchanged and fuel consumption remains unchanged @ what fuel remaining should be epected at waDpoint >7TA >7TA 3 +$$! 4g a) ++"! 4g b) "5!! 4g c) +"+! 4g d) Answer ; a)

+$$! 4g -----------------------------------------------------------------------------------------------------------------------------------------------------------------


##"


211.

( For this question use 0mage +% 

,age 46 =i8en ; 'lanned and actual data as shown in the Flight 7og ecerpt. 'ro8ided that flight conditions on the leg =AA to >7TA >7TA remain unchanged and fuel consumption remains unchanged @ what fuel remaining should be epected at waDpoint >7TA >7TA 3 a) +++! 4g +,#! 4g b) +%6! 4g c) +#%! 4g d) Answer ; c)

+%6! 4g ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use 0mage +&  212.

,age 47 =i8en ; 'lanned and actual data as shown in the Flight 7og ecerpt. 'ro8ided that flight conditions on the leg =AA to >7TA >7TA remain unchanged and fuel consumption remains unchanged @ what fuel remaining should be epected at waDpoint >7TA >7TA 3 +#+! 4g a) +&+! 4g b) +%+! 4g c) +,,! 4g d) Answer ; d)

+,,! 4g -----------------------------------------------------------------------------------------------------------------------------------------------------------------


##+


213.

( For this question use 0mage +5 

,age 4" =i8en ; 'lanned and actual data as shown in the Flight 7og ecerpt. 'ro8ided that flight conditions on the leg =AA to >7TA >7TA remain unchanged and fuel consumption remains unchanged @ what fuel remaining should be epected at waDpoint >7TA >7TA 3 a) +$,! 4g +&+, 4g b) ++&, 4g c) +%", 4g d) Answer ; c)

++&, 4g ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use 0mage +6  214.

,age 49 =i8en ; 'lanned and actual data as shown in the Flight 7og ecerpt. 'ro8ided that flight conditions on the leg =AA to >7TA >7TA remain unchanged and fuel consumption remains unchanged @ what fuel remaining should be epected at waDpoint >7TA >7TA 3 +5,! 4g a) +%+! 4g b) +&6! 4g c) +,,! 4g d) Answer ; b)

+%+! 4g -----------------------------------------------------------------------------------------------------------------------------------------------------------------


##,


215.

( For this question use 0mage ,! 

,age 50 =i8en ; 'lanned and actual data as shown in the Flight 7og ecerpt. 'ro8ided that flight conditions on the leg =AA to >7TA >7TA remain unchanged and fuel consumption remains unchanged @ what fuel remaining should be epected at waDpoint >7TA >7TA 3 ,!6! 4g a) ,!#! 4g b) +6+! 4g c) d) +%6! 4g Answer ; c)

+6+! 4g ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use 0mage ,,  216.

,age 55 =i8en ; 'lanning data as shown in the Flight 7og ecerpt ( Fuel 'lanning 1ection . After a bal4ed landing at the destination airport @ Dou ha8e to di8ert to the alternate airport with the gear etended. The re-calculated flight time to the alternate airport with the gear etended. The re-calculated flight time to the alternate due to the reduced speed is # h ,! min and the fuel flow will be 5+! 4gh. Final )eser8e Fuel remains unchanged.
,56! 4g


##%


----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use 0mage ,+ 

217.

,age 54 =i8en ; 'lanning data as shown in the Flight 7og ecerpt ( Fuel 'lanning 1ection . After a bal4ed landing at the destination airport @ Dou ha8e to di8ert to the alternate airport with the gear etended. The re-calculated flight time to the alternate due to the reduced speed is # h #! min and the fuel flow will be %!! 4gh. Final )eser8e Fuel remains unchanged.
,5+6 4g ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use 0mage #$  218.

,age 12 =i8en ; 'lanning data as shown in the Flight 7og ecerpt ( Fuel 'lanning 1ection . After a bal4ed landing at the destination airport @ Dou ha8e to di8ert to the alternate airport with the gear etended. The re-calculated flight time to the alternate due to the reduced speed is # h #! min and the fuel flow will be 6!! 4gh. Final )eser8e Fuel remains unchanged.
,65& 4g


##&


----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use 0mage ,$ 

219.

,age 52 =i8en ; 'lanning data as shown in the Flight 7og ecerpt ( Fuel 'lanning 1ection . After a bal4ed landing at the destination airport @ Dou ha8e to di8ert to the alternate airport with the gear etended. The re-calculated flight time to the alternate due to the reduced speed is # h $! min and the fuel flow will be &$! 4gh. Final )eser8e Fuel remains unchanged.
,5&+ 4g ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use 0mage ,"  220.

,age 53 =i8en ; 'lanning data as shown in the Flight 7og ecerpt ( Fuel 'lanning 1ection . After a bal4ed landing at the destination airport @ Dou ha8e to di8ert to the alternate airport with the gear etended. The re-calculated flight time to the alternate due to the reduced speed is # h $! min and the fuel flow will be &$! 4gh. Final )eser8e Fuel remains unchanged.
,%%6 4g


##5


----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use 0mage ,# 

221.

,age 51 =i8en ; 'lanning data as shown in the Flight 7og ecerpt ( Fuel 'lanning 1ection . After a bal4ed landing at the destination airport @ Dou ha8e to di8ert to the alternate airport with the gear etended. The re-calculated flight time to the alternate due to the reduced speed is # h "! min and the fuel flow will be %!! 4gh. Final )eser8e Fuel remains unchanged.
,%+$ 4g ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use 0mage #!  222.

,age 10 =i8en ; 'lanning data as shown in the Flight 7og ecerpt ( Fuel 'lanning 1ection . After a bal4ed landing at the destination airport @ Dou ha8e to di8ert to the alternate airport with the gear etended. The re-calculated flight time to the alternate due to the reduced speed is $ h $! min and the fuel flow will be &5! 4gh. Final )eser8e Fuel remains unchanged.
,++! 4g


##6


----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use Flight 'lanning anual )*T # Figure +.&." 

223.

Flight Planning Manual M#T 1 Figure Fi gure 4.7.3 =i8en ; i8ersion fuel a8ailable 5,!! 4g i8ersion cruise altitude #!!!! ft ass at point of di8ersion %$,!! 4g 2ead wind component ,! 4t Temperature Temperature 01A -,BC The (a maimum di8ersion distance @ and (b elapsed time alternate @ are approimatelD ; (a 5%! 9 @ (b " h $! min a) (a #!!! 9 @ (b " h +! min b) (a &%! 9 @ (b + h "! min c) (a ##"! 9 @ (b " h "! min d) Answer ; a)

(a 5%! 9 @ (b " h $! min


#$!


-----------------------------------------------------------------------------------------------------------------------------------------------------------------

224.

( For this this question use anne !""-#$"#$A or Flight 'lanning anual )*T # Figure +.".% 

Annex 033-12312A 033-12312A =i8en ; istance to Alternate I +!! 9 7anding mass at Alternate I ,! !!! 4g 2eadwind component I $, 4t The Alternate fuel required is ; $5!! 4g a) $,,! 4g b) $6!! 4g c) $%,! 4g d) Answer ; a)

$5!! 4g -----------------------------------------------------------------------------------------------------------------------------------------------------------------


#$#


225.

( For this this question use anne !""-#$"#$A or Flight 'lanning anual )*T # Figure +.".% +.".% 

Annex 033-12312A 033-12312A

=i8en ;

istance to Alternate +,! 9 7anding mass at Alternate I +, !!! 4g Tailwind Tailwind component I ,! 4t The Alternate fuel required is ; "!,! 4g a) $&,! 4g b) $6!! 4g c) $,!! 4g d) Answer ; d)

$,!! 4g ----------------------------------------------------------------------------------------------------------------------------------------------------------------=i8en ; 226. istance R to O $&!! 9 ach 9umber !.&, Temperature Temperature -+,BC ean wind component “on” #! 4t tailwind ean wind component “bac4” ", 4t tailwind The distance from R to the point of equal time ( '>T  between R and O is ; #",! 9 a) #"5% 9 b) #+$, 9 c) #"#" 9 d)

Answer ; b)

#"5% 9


#$$


----------------------------------------------------------------------------------------------------------------------------------------------------------------=i8en ; istance A to H $!,! 9 ean groundspeed “on” ++! 4t ean groundspeed “bac4” ,+! 4t The distance to the point of equal time ( '>T  between A and H is ; 6$! 9 a) #!$, 9 b) ##"! 9 c) d) ##," 9

227.

Answer ; c)

##"! 9 ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use Flight 'lanning anual )*T # Figure +.&."  228.

Flight Planning Manual M#T 1 Figure Fi gure 4.7.3 =i8en ; i8ersion distance %,! 9 i8ersion pressure altitude #% !!! ft ass at point of di8ersion ,& !!! 4g 2ead wind component $! 4t Temperature Temperature 01A E #,BC The di8ersion (a fuel required and (b time are approimatelD ; (a %$!! 4g @ (b $ h #! min a) (a ++!! 4g @ (b # h ", min b) (a +5!! 4g @ (b $ h !" min c) (a "6!! 4g @ (b # h +, min d) Answer ; c)

(a +5!! 4g @ (b $ h !" min


#$"


-----------------------------------------------------------------------------------------------------------------------------------------------------------------

229.

=i8enI rD operating mass (   I "",#! 4g Traffic 7oad I &%!! 4g Final reser8e fuel I 65" 4g Alternate fuel I ##!! 4g ContingencD fuel I #!$ 4g The estimated landing mass at alternate should be ; a) +$"#$ 4g. +$$#! 4g. b) +$!6" 4g. c) +$#6, 4g. d)

Answer ; d)

+$#6, 4g. ----------------------------------------------------------------------------------------------------------------------------------------------------------------=i8en ; 230. rD operating mass (   I ""!!! 4g Traffic 7oad I 5##! 4g Final reser8e fuel I 65" 4g Alternate fuel I ##!! 4g ContingencD fuel I #!$ 4g The estimated landing mass at alternate should be ; +###! 4g. a) +$$#! 4g. b) +$#6, 4g. c) +$"#$ 4g. d)

Answer ; c)

+$#6, 4g. ----------------------------------------------------------------------------------------------------------------------------------------------------------------=i8en ; 231. R K istance A to point of equal time ( '>T  between A and H > K >ndurance  K istance A to H  K =roundspeed “on” 2 K =roundspeed “bac4” The formula for calculating the distance R to point of equal time ( '>T  is ; RK2(E2 a) RK>2(E2 b) c) RK(E2 RK2(E2 d)

Answer ; a)

RK2(E2 -----------------------------------------------------------------------------------------------------------------------------------------------------------------


#$+


232.

( For this this question use anne !""-#$"!,A or Flight 'lanning anual )*T # Figure +.,.# +.,.# 

Annex 033-12305A 033-12305A =i8en ; Hra4e release mass I %$ !!! 4g Temperature Temperature I 01A E #,BC The fuel required for a climb from 1ea 7e8el to F7""! is ; #&!! 4g a) #&,! 4g b) #5!! 4g c) #%,! 4g d) Answer ; a)

#&!! 4g


#$,


-----------------------------------------------------------------------------------------------------------------------------------------------------------------

233.

( For this question use annees annees !""-#$"!%A and !""-#$"!%H or Flight 'lanning anual anual )*T # Figure Figure +.,.$ and +.,."." +.,."." 

Annexe 033-12306A 033-12306A  033-12306! =i8en ; Cruise ach !.&5 at F7"!! istance H - C I 5!! 9 Temperature Temperature I - ,,BC 2eadwind component I ,! 4t =ross mass at H I %+ ,!! 4g The fuel required from H - C is ; %!6! 4g a) +6&, 4g b) %#$, 4g c) +6+, 4g d) Answer ; a)

%!6! 4g -----------------------------------------------------------------------------------------------------------------------------------------------------------------


#


234.

( For this question use annees annees !""-#$"!5A and !""-#$"!5H or Flight 'lanning anual anual )*T )*T # Figure Figure +.,.$ and +.,.".+ 

Annexe 033-1230"A 033-1230"A  033-1230"! =i8en ; istance H - C I ",! 9 Cruise "!! /0A1 at F7 $#! Temperature Temperature I - +!BC Tailwind Tailwind component I &! 4t =ross mass at H I ," $!! 4g The fuel required from H - C is ; #6+! 4g a) $5!! 4g b) $%&! 4g c) #5#! 4g d) Answer ; a)

#6+! 4g -----------------------------------------------------------------------------------------------------------------------------------------------------------------


#$&


235.

( For this question use annees annees !""-#$"!&A and !""-#$"!&H or Flight 'lanning anual anual )*T # Figure Figure +.,.$ and +.,."." +.,."." 

Annexe 033-12307A 033-12307A  033-12307! =i8en ; istance H - C I #$!! 9 Cruise ach !.&5 at F7"!! Temperature Temperature e8iation from 01A I -#+BC Tailwind Tailwind component I +! 4t =ross mass at H I ,! $!! 4g The fuel required from H - C is ; ,5,! 4g a) %#,! 4g b) &!,! 4g c) &"!! 4g d) Answer ; b)

%#,! 4g -----------------------------------------------------------------------------------------------------------------------------------------------------------------


#$5


236.

( For this question use annees annees !""-#$"!$A and !""-#$"!$H or Flight 'lanning anual anual )*T # Figure Figure +.,.$ and +.,.".# +.,.".# 

Annexe 033-12302A 033-12302A  033-12302! =i8en ; istance C -  I %5! 9 7ong )ange Cruise at F7"+! Temperature Temperature e8iation from 01A I !B C 2eadwind component I %! 4t =ross mass at C I ++ &!! 4g The fuel required from C -  is ; "#!! 4g a) "+!! 4g b) "&!! 4g c) +!!! 4g d) Answer ; c)

"&!! 4g -----------------------------------------------------------------------------------------------------------------------------------------------------------------


#$6


237.

( For this question question use Annees !""-#$"!$A and !""-#$"!$H or Flight 'lanning anual anual )*T )*T # Figure +.,.$ and +.,.".# 

Annexe 033-12302A 033-12302A  033-12302! =i8en ; istance C -  I "$!! 9 7ong )ange Cruise at F7 "+! Temperature Temperature e8iation from 01A I E#$BC Tailwind Tailwind component I ,! 4t =ross mass at C I ,, !!! 4g The fuel required from C -  is ; #+ ,!! 4g a) #& ,!! 4g b) #& 5!! 4g c) #+ $!! 4g d) Answer ; a)

#+ ,!! 4g -----------------------------------------------------------------------------------------------------------------------------------------------------------------


#"!


238.

( For this question use annees annees !""-#$"!5A and !""-#$"!5H or Flight 'lanning anual anual )*T )*T # Figure Figure +.,.$ and +.,.".+ 

Annexe 033-1230"A 033-1230"A  033-1230"! =i8en ; istance C -  I ,+! 9 Cruise "!! /0A1 at F7 $#! Temperature Temperature e8iation from 01A I E$!BC 2eadwind component I ,! 4t =ross mass at C I %! !!! 4g The fuel required from C to  is ; "",! 4g a) "%5! 4g b) +$!! 4g c) +%$! 4g d) Answer ; c)

+$!! 4g -----------------------------------------------------------------------------------------------------------------------------------------------------------------


#"#


239.

( For this this question use anne !""-#$"!+A or Flight 'lanning anual )*T # Figure +.,.# +.,.# 

Annex 033-12304A 033-12304A =i8en ; Hra4e release mass I ,5 !!! 4g Temperature Temperature I 01A E #, The fuel required to climb from an aerodrome at ele8ation +!!! ft to F7"!! is ; #+,! 4g a) #$,! 4g b) #",! 4g c) #+!! 4g d) Answer ; b)

#$,! 4g


#"$


----------------------------------------------------------------------------------------------------------------------------------------------------------------=i8en ; Fuel densitD I !.&5 4gl rD operating mass I "",!! 4g Traffic load I #! %!! 4g aimum allowable ta4e-off mass I %%$!! 4g Tai Tai fuel I $!! 4g Tan4 Tan4 capacitD I $$ ,!! 7itres The maimum possible ta4e-off fuel is ; a) #& ",! 4g $# 6!! 4g b) #& ,,! 4g c) $$ #!! 4g d)

240.

Answer ; a)

#& ",! 4g ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use Flight 'lanning anual )*T # Figure +.&."  241.

Flight Planning Manual M#T 1 Figure Fi gure 4.7.3 =i8en ; istance to alternate 6,! 9 2ead wind component $! 4t ass at point of di8ersion ,!!!! 4g i8ersion fuel a8ailable ,5!! 4g The minimum pressure altitude at which the abo8e conditions maD be met is ; $$!!! ft a) #5!!! ft b) $!!!! ft c) $%!!! ft d) Answer ; a)

$$!!! ft


#""


----------------------------------------------------------------------------------------------------------------------------------------------------------------242.

=i8en ; F7 "&!  K !.&+ AT K -+&BC The TA1 is ; a) b) c) d)

+#, 4t +"+ 4t +$5 4t +$+ 4t

Answer ; b)

+"+ 4t ----------------------------------------------------------------------------------------------------------------------------------------------------------------=i8en ; 243. Course A to H !55B ( T  istance #$,! 9 ean TA1 ""! 4t ean <: "+!B%! 4t The time from A to the '>T between A and H is ; $ hours !$ minutes a) b) # hour ,+ minutes # hour "6 minutes c) # hour +" minutes d)

Answer ; d)

# hour +" minutes ----------------------------------------------------------------------------------------------------------------------------------------------------------------244. =i8en ; istance A to H "!%! 9 ean groundspeed “out” ++! 4t ean groundspeed “bac4” ,+! 4t 1afe >ndurance #! hours The time to the 'oint of 1afe )eturn ( '1)  is ; a) , hours $! minutes " hours ,, minutes b) , hours +, minutes c) , hours "# minutes d)

Answer ; d)

, hours "# minutes ----------------------------------------------------------------------------------------------------------------------------------------------------------------=i8en ; 245. istance from departure to destination $&! 9 True trac4 !"! <: #$!", TA1 #$, 4t T from the departure point 3 istance I #+# 9 Time I %5 min a) istance I #+# 9 Time I %, min b) istance I #"! 9 Time I %5 min c) istance I #", 9 Time I %5 min d)

Answer ; d)

istance I #", 9 Time I %5 min ----------------------------------------------------------------------------------------------------------------------------------------------------------------=i8en ; 246. istance from departure to destination ""5 9 True trac4 !+, <: $$,", TA1 #$! 4t T from the departure point 3 istance I #5, 9 Time I &$ min a) istance I #$! 9 Time I +% min b) istance I $#5 9 Time I 5, min c) istance I #%6 9 Time I 5, min d)

Answer ; b)

istance I #$! 9 Time I +% min -----------------------------------------------------------------------------------------------------------------------------------------------------------------


#"+


247.

=i8en ; istance from departure to destination ",! 9 True trac4 "$! <: ",!"! TA1 #"! 4t T from the departure point 3 istance I $#! 9 Time I #$$ min a) istance I #"6 9 Time I ,+ min b) c) istance I #"6 9 Time I 5# min istance I #$" 9 Time I &+ min d)

Answer ; a)

istance I $#! 9 Time I #$$ min ----------------------------------------------------------------------------------------------------------------------------------------------------------------=i8en ; 248. istance from departure to destination ,!! 9 True trac4 !6! <: !6!$! TA1 #,! 4t T from the departure point 3 istance I $,! 9 Time I 55 min a) b) istance I $5" 9 Time I #"# min istance I "5$ 9 Time I #&%min c) istance I $#& 9 Time I #!! min d)

Answer ; b)

istance I $5" 9 Time I #"# min ----------------------------------------------------------------------------------------------------------------------------------------------------------------249. =i8en ; istance from departure to destination 5&, 9 True trac4 $+! <: !%!,! TA1 ,!! 4t T from the departure point 3 a) istance I &#% 9 Time I &5 min istance I +5# 9 Time I %+ min b) istance I "6+ 9 Time I +" min c) istance I +"5 9 Time I ," min d)

Answer ; c)

istance I "6+ 9 Time I +" min ----------------------------------------------------------------------------------------------------------------------------------------------------------------=i8en ; 250. istance from departure to destination ##!! 9 True trac4 $5! <: #!!5! TA1 ++! 4t T from the departure point 3 istance I +,! 9 Time I ,$ min a) istance I %,! 9 Time I &, min b) istance I ,,! 9 Time I &, min c) istance I %,! 9 Time I #!5 min d)

Answer ; a)

istance I +,! 9 Time I ,$ min ----------------------------------------------------------------------------------------------------------------------------------------------------------------=i8en ; 251. istance from departure to destination $$!! 9 True trac4 #,! <: ""!,! TA1 +%! 4t T from the departure point 3 istance I 65! 9 Time I #++ min a) istance I ##!! 9 Time I #&6 min b) istance I ##$! 9 Time I #&6 min c) istance I 65! 9 Time I ##, min d)

Answer ; d)

istance I 65! 9 Time I ##, min -----------------------------------------------------------------------------------------------------------------------------------------------------------------


#",


252.

=i8en ; istance from departure to destination $5!! 9 True trac4 #+! <: #+!#!! TA1 ,!! 4t T from the departure point 3 istance I ##$! 9 Time I #"+ min a) istance I #+!! 9 Time I #%5 min b) istance I #%5! 9 Time I $,$ min c) d) istance I ##$! 9 Time I ##$ min

Answer ; c)

istance I #%5! 9 Time I $,$ min ----------------------------------------------------------------------------------------------------------------------------------------------------------------=i8en ; 253. istance from departure to destination I #,! 9 1afe >ndurance I ".$ h TA1 I 6! 4t =round 1peed ut I #!! 4t =round 1peed 2ome I 5! 4t
Answer ; d)

istance I #+$ 9 Time I 5, min ----------------------------------------------------------------------------------------------------------------------------------------------------------------254. =i8en ; istance from departure to destination I #5! 9 >ndurance I $ h TA1 I #$! 4t =round 1peed ut I #", 4t =round 1peed 2ome I #!, 4t
Answer ; b)

istance I ##5 9 Time I ," min ----------------------------------------------------------------------------------------------------------------------------------------------------------------=i8en ; 255. istance from departure to destination I $+! 9 1afe >ndurance I "., h TA1 I #$, 4t =round 1peed ut I ##! 4t =round 1peed 2ome I #+! 4t
Answer ; c)

istance I $#% 9 Time I ##5 min -----------------------------------------------------------------------------------------------------------------------------------------------------------------


#"%


256.

=i8en ; istance from departure to destination I ,!! 9 1afe >ndurance I + h TA1 I #+! 4t =round 1peed ut I #,! 4t =round 1peed 2ome I #"! 4t
Answer ; c)

istance I $&6 9 Time I ### min ----------------------------------------------------------------------------------------------------------------------------------------------------------------257. =i8en ; istance from departure to destination I 6,! 9 1afe >ndurance I "., h TA1 I "%! 4t =round 1peed ut I "$! 4t =round 1peed 2ome I +!! 4t
Answer ; b)

istance I %$$ 9 Time I ##& min ----------------------------------------------------------------------------------------------------------------------------------------------------------------=i8en ; 258. istance from departure to destination 6, 9 True trac4 #!, <: !%!#, TA1 #+! 4t T from the departure point 3 ,# 9 a) +&., 9 b) 5$ 9 c) ++ 9 d)

Answer ; a)

,# 9 ----------------------------------------------------------------------------------------------------------------------------------------------------------------=i8en ; 259. istance from departure to destination #+! 9 =1 ut 6! 4t =1 2ome 5! 4t T from the departure point 3 #$+ 9 a) %% 9 b) &! 9 c) &+ 9 d)

Answer ; b)

%% 9 ----------------------------------------------------------------------------------------------------------------------------------------------------------------=i8en ; 260. istance from departure to destination #,! 9 True trac4 #+$ <: $!!#, TA1 #"$ 4t T from the departure point 3 &6 9 a) #"+ 9 b) &, 9 c) &# 9 d)

Answer ; a)

&6 9


#"&


----------------------------------------------------------------------------------------------------------------------------------------------------------------261.

=i8en ; istance from departure to destination #,! 9 True trac4 !$! <: #5!"! TA1 #"! 4t T from the departure point 3 6# 9 a) b) ,6 9 &, 9 c) %, 9 d)

Answer ; b)

,6 9 ----------------------------------------------------------------------------------------------------------------------------------------------------------------262. =i8en ; istance from departure to destination #%, 9 True trac4 !,, <: "%!$! TA1 #!, 4t T from the departure point 3 a) &" 9 5" 9 b) 6$ 9 c) #"$ 9 d)

Answer ; c)

6$ 9 ----------------------------------------------------------------------------------------------------------------------------------------------------------------=i8en ; 263. istance from departure to destination #5! 9 True trac4 "#! <: !#!$! TA1 ##, 4t T from the departure point 3 6$ 9 a) 5$ 9 b) 6! 9 c) 65 9 d)

Answer ; d)

65 9 ----------------------------------------------------------------------------------------------------------------------------------------------------------------=i8en ; 264. istance from departure to destination $$! 9 True trac4 #&, <: $$!#! TA1 #", 4t T from the departure point 3 #!" 9 a) #"% 9 b) ##% 9 c) ##! 9 d)

Answer ; c)

##% 9 ----------------------------------------------------------------------------------------------------------------------------------------------------------------=i8en ; 265. istance from departure to destination $,! 9 =1 ut #"! 4t =1 2ome #!! 4t T from the departure point 3 #6$ 9 a) #!6 9 b) #+# 9 c) #$, 9 d)

Answer ; b)

#!6 9 -----------------------------------------------------------------------------------------------------------------------------------------------------------------


#"5


266.

=i8en ; istance from departure to destination $,% 9 =1 ut #%! 4t =1 2ome ##! 4t T from the departure point 3 #&% 9 a) #!+ 9 b) c) #$5 9 #,$ 9 d)

Answer ; b)

#!+ 9 ----------------------------------------------------------------------------------------------------------------------------------------------------------------=i8en ; 267. istance from departure to destination $5, 9 True trac4 "+5 <: $5!$, TA1 #$5 4t T from the departure point 3 #," 9 a) b) #$" 9 #"# 9 c) #+" 9 d)

Answer ; a)

#," 9 ----------------------------------------------------------------------------------------------------------------------------------------------------------------268. =i8en ; istance from departure to destination "#, 9 True trac4 "+" <: !#,#, TA1 #!! 4t T from the departure point 3 a) #&% 9 #+5 9 b) #"6 9 c) #%& 9 d)

Answer ; a)

#&% 9 ----------------------------------------------------------------------------------------------------------------------------------------------------------------=i8en ; 269. istance from departure to destination "+! 9 True trac4 "$! <: #%!+! TA1 ##! 4t T from the departure point 3 $#6 9 a) #$# 9 b) $$5 9 c) ##$ 9 d)

Answer ; d)

##$ 9 ----------------------------------------------------------------------------------------------------------------------------------------------------------------=i8en ; 270. istance from departure to destination "+! 9 =1 ut #,! 4t =1 2ome #$! 4t T from the departure point 3 #56 9 a) #,# 9 b) #&! 9 c) $&$ 9 d)

Answer ; b)

#,# 9 -----------------------------------------------------------------------------------------------------------------------------------------------------------------


#"6


271.

=i8en ; istance from departure to destination +", 9 =1 ut ##! 4t =1 2ome #"! 4t T from the departure point 3 #66 9 a) $"% 9 b) $#5 9 c) d) "%5 9

Answer ; b)

$"% 9 ----------------------------------------------------------------------------------------------------------------------------------------------------------------=i8en ; 272. istance from departure to destination +&! 9 True trac4 $"& <: "!!$, TA1 #$, 4t T from the departure point 3 $", 9 a) $#+ 9 b) c) $,% 9 $!, 9 d)

Answer ; c)

$,% 9 ----------------------------------------------------------------------------------------------------------------------------------------------------------------=i8en ; 273. istance from departure to destination ,!! 9 =1 ut 6, 4t =1 2ome #$, 4t T from the departure point 3 $#% 9 a) "5! 9 b) c) $5+ 9 $,! 9 d)

Answer ; c)

$5+ 9 ----------------------------------------------------------------------------------------------------------------------------------------------------------------=i8en ; 274. istance from departure to destination I #,! 9 1afe >ndurance I $.+ h True Trac4 I $,! <: I $5!#, TA1 I #$! 4t
Answer ; c)

#+$ 9 ----------------------------------------------------------------------------------------------------------------------------------------------------------------=i8en ; 275. istance from departure to destination I #5! 9 1afe >ndurance I $.5 h True Trac4 I !%, <: I $+,$, TA1 I #!! 4t
Answer ; d)

#"# 9 -----------------------------------------------------------------------------------------------------------------------------------------------------------------


#+!


276.

=i8en ; istance from departure to destination I #6! 9 1afe >ndurance I $.+ h True Trac4 I #$! <: I !"!+! TA1 I #"! 4t
Answer ; c)

#+5 9 ---------------------------------------------------------------------------------------------------------------------------------------------------------------=i8en ; 277. istance from departure to destination I $!! 9 1afe >ndurance I " h TA1 I #"! 4t =round 1peed ut I #,! 4t =round 1peed 2ome I ##! 4t
Answer ; c)

#6! 9 ----------------------------------------------------------------------------------------------------------------------------------------------------------------278. =i8en ; istance from departure to destination I $#! 9 1afe >ndurance I $., h True Trac4 I !", <: I $,!$! TA1 I #!, 4t
Answer ; d)

#$& 9 ----------------------------------------------------------------------------------------------------------------------------------------------------------------=i8en ; 279. istance from departure to destination I $#! 9 1afe >ndurance I "., h True Trac4 I "#! <: I $&!"! TA1 I #$! 4t
Answer ; b)

$!! 9 -----------------------------------------------------------------------------------------------------------------------------------------------------------------


#+#


280.

=i8en ; istance from departure to destination I $#, 9 1afe >ndurance I "." h True Trac4 I !!, <: I $6!#, TA1 I #$, 4t
Answer ; c)

$!, 9 ----------------------------------------------------------------------------------------------------------------------------------------------------------------=i8en ; 281. istance from departure to destination I $%! 9 1afe >ndurance I +.# h True Trac4 I#,! <: I #!!"! TA1 I ##! 4t
Answer ; c)

$#" 9 ----------------------------------------------------------------------------------------------------------------------------------------------------------------=i8en ; 282. istance from departure to destination I "!! 9 1afe >ndurance I + h TA1 I ##! 4t =round 1peed ut I #$! 4t =round 1peed 2ome I #!! 4t
Answer ; c)

$#5 9 ----------------------------------------------------------------------------------------------------------------------------------------------------------------=i8en ; 283. istance from departure to destination I "$! 9 1afe >ndurance I +." h True Trac4 I #$! <: I #5!+! TA1 I #"! 4t
Answer ; b)

$%$ 9 -----------------------------------------------------------------------------------------------------------------------------------------------------------------


#+$


284.

=i8en ; istance from departure to destination I ""! 9 1afe >ndurance I , h True Trac4 I #&! <: I #+!$, TA1 I #$, 4t
Answer ; c)

"!" 9 ----------------------------------------------------------------------------------------------------------------------------------------------------------------=i8en ; 285. istance from departure to destination I "%! 9 1afe >ndurance I +., h True Trac4 I "+, <: I $%!"! TA1 I #+! 4t
Answer ; a)

"!5 9 ----------------------------------------------------------------------------------------------------------------------------------------------------------------=i8en ; 286. istance from departure to destination I +!! 9 1afe >ndurance I $., h TA1 I ##, 4t =round 1peed ut I #"! 4t =round 1peed 2ome I #!, 4t
Answer ; c)

#+, 9 ----------------------------------------------------------------------------------------------------------------------------------------------------------------=i8en ; 287. istance from departure to destination I +#! 9 1afe >ndurance I ".% h True Trac4 I !,, <: I #5!", TA1 I #$! 4t
Answer ; c)

$!" 9 -----------------------------------------------------------------------------------------------------------------------------------------------------------------


#+"


288.

=i8en ; istance from departure to destination I +5! 9 1afe >ndurance I , h True Trac4 I "#, <: I #!!$! TA1 I ##, 4t
Answer ; d)

$5! 9 ----------------------------------------------------------------------------------------------------------------------------------------------------------------=i8en ; 289. istance from departure to destination I ,,! 9 >ndurance I ".% h True Trac4 I $!! <: I $$!#, TA1 I #"! 4t
Answer ; c)

$"# 9 ----------------------------------------------------------------------------------------------------------------------------------------------------------------=i8en ; 290. istance from departure to destination I #!!! 9 1afe >ndurance I + h TA1 I ,!! 4t =round 1peed ut I ,,! 4t =round 1peed 2ome I +,! 4t
Answer ; b)

66! 9 ----------------------------------------------------------------------------------------------------------------------------------------------------------------=i8en ; 291. istance from departure to destination I $!!! 9 >ndurance I , h TA1 I ,!! 4t =round 1peed ut I +5! 4t =round 1peed 2ome I ,$! 4t
Answer ; d)

#$+5 9 -----------------------------------------------------------------------------------------------------------------------------------------------------------------


#++


292.

=i8en ; istance from departure to destination I "&,! 9 1afe >ndurance I 6., h True Trac4 I "%! <: I "%!,! TA1 I +5! 4t
Answer ; c)

$$,, 9 ----------------------------------------------------------------------------------------------------------------------------------------------------------------=i8en ; 293. istance from departure to destination I +%"! 9 1afe >ndurance I #$.+ h True Trac4 I $+! <: I !%!5! TA1 I ,"! 4t
Answer ; b)

"$## 9 ----------------------------------------------------------------------------------------------------------------------------------------------------------------=i8en ; 294. istance from departure to destination I ,!!! 9 1afe >ndurance I #! h TA1 I +,! 4t =round 1peed ut I ,!! 4t =round 1peed 2ome I +!! 4t
Answer ; d)

$$$$ 9 ----------------------------------------------------------------------------------------------------------------------------------------------------------------=i8en ; 295. istance from departure to destination I %"+! 9 1afe >ndurance I #, h True Trac4 I !6! <: I $&!#!! TA1 I ,$! 4t
Answer ;

-----------------------------------------------------------------------------------------------------------------------------------------------------------------


#+,


296.

( For this question use Flight 'lanning anual )*T # Figure +.&." 

Flight Planning Manual M#T 1 Figure Fi gure 4.7.3 =i8en ; i8ersion distance &$! 9 Tail Tail wind component $, 4t ass at point of di8ersion ,,!!! 4g Temperature 01A i8ersion fuel a8ailable +$,! 4g
$,!!! ft


#+%


-----------------------------------------------------------------------------------------------------------------------------------------------------------------

297.

=i8en ; istance from departure to destination 6,! 9 =1 ut $&, 4t =1 2ome $$, 4t T from the departure point 3 a) "6 min #"6 min b) 6" min c) ##+ min d)

Answer ; c)

6" min ----------------------------------------------------------------------------------------------------------------------------------------------------------------=i8en ; 298. istance from departure to destination #"+, 9 =1 ut +5! 4t =1 2ome "%! 4t T from the departure point 3 a) #$5 min ,! min b) &$ min c) 6% min d)

Answer ; c)

&$ min ----------------------------------------------------------------------------------------------------------------------------------------------------------------=i8en ; 299. istance from departure to destination #5%! 9 =1 ut "%! 4t =1 2ome +!! 4t T from the departure point 3 a) #"$ min $$ min b) #+& min c) #%" min d)

Answer ; d)

#%" min ----------------------------------------------------------------------------------------------------------------------------------------------------------------=i8en ; 300. istance from departure to destination #6,! 9 =1 ut +!! 4t =1 2ome "!! 4t T from the departure point 3 a) #$, min $$" min b) #%& min c) $6 min d)

Answer ; a)

#$, min ----------------------------------------------------------------------------------------------------------------------------------------------------------------=i8en ; 301. istance from departure to destination $"5! 9 =1 ut +$! 4t =1 2ome ,$! 4t T from the departure point 3 #6 min a) #55 min b) #,$ min c) #$" min d)

Answer ; b)

#55 min -----------------------------------------------------------------------------------------------------------------------------------------------------------------


#+&


302.

=i8en ; istance from departure to destination $,!! 9 =1 ut ,+! 4t =1 2ome +&! 4t T from the departure point 3 #$6 min a) #&# min b) #+6 min c) d) $5 min

Answer ; a)

#$6 min ----------------------------------------------------------------------------------------------------------------------------------------------------------------=i8en ; 303. istance from departure to destination I #,!! 9 1afe >ndurance I +., h TA1 I +,! 4t =round 1peed ut I +5! 4t =round 1peed 2ome I +#! 4t
Answer ; b)

#$+ min ----------------------------------------------------------------------------------------------------------------------------------------------------------------304. =i8en ; istance from departure to destination I $+,! 9 1afe >ndurance I &., h TA1 I +#! 4t =round 1peed ut I "%! 4t =round 1peed 2ome I +%! 4t
Answer ; b)

$,$ min ----------------------------------------------------------------------------------------------------------------------------------------------------------------=i8en ; 305. istance from departure to destination I "!!! 9 1afe >ndurance I 5 h TA1 I ,$! 4t =round 1peed ut I %!! 4t =round 1peed 2ome I ++! 4t
Answer ; c)

$!" min -----------------------------------------------------------------------------------------------------------------------------------------------------------------


#+5


306.

=i8en ; rD operating mass (   I "",#! 4g Traffic 7oad I &%!! 4g Trip fuel ( TF  I $!+! 4g Final reser8e fuel I 65" 4g Alternate fuel I ##!! 4g ContingencD fuel I , of trip fuel stimated ta4e-off mass K +,$"" 4g. a) b) >stimated landing mass at destination K +"#6" 4g. >stimated landing mass at destination K +"$6, 4g. c) >stimated ta4e-off mass K +"$6, 4g. d)

Answer ; c)

>stimated landing mass at destination K +"$6, 4g. -----------------------------------------------------------------------------------------------------------------------------------------------------------------


#+6


307.

( For this question use annees !""-##$$+A @ !""-##$$+H and !""-##$$+C 

Annexe 033-11 033-11224A 224A  033-11224! 033-11224!  033-11224/ 033-11224/ =i8en ; Ta4e-off Ta4e-off mass I #,! !!! 4g 'lanned cruise at F7 ",! 7ong range AC2 1tandard Atmosphere ( 01A  C= I "&  Oou Oou ha8e to co8er an air distance of $ !!! 9. Oour Oour flight time will be ; $65 minutes a) "!+ minutes b) ",6 minutes c) $55 minutes d) Answer ; b)

"!+ minutes


#,!


----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this this question use Anne !""-#$"+,A or Flight 'lanning anual )*T # Figure +."., 

308.

Annex 033-12345A 033-12345A =i8en a trip time of about 6 hours @ within the limits of the data gi8en @ a temperature decrease of "!BC will affect the trip time bD approimatelD ; E" a) E & b) -+ c) -#! d) Answer ; b)

E &


#,#


----------------------------------------------------------------------------------------------------------------------------------------------------------------=i8en the following ;  K flight distance R K distance to 'oint of >qual Time =1o K groundspeed out =1r K groundspeed return The correct formula to find distance to 'oint of >qual Time is ; R K   =1r  ( =1o E =1r  a) R K ( $   =1o  ( =1o E =1r  b) c) R K ( $  E =1r  ( =1o E =1r  R K   =1o  ( =1o E =1r  d)

309.

Answer ; a)

R K   =1r  ( =1o E =1r  ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use anne.!""-#$"+$A or Flight 'lanning anual )*T # Figure +.".,  310.

Annex 033-12342A 033-12342A =i8en the following ; 2ead wind component ,! 4t Temperature Temperature 01A E #!BC Hra4e release mass %,!!! 4g Trip fuel a8ailable #5!!! 4g
$&+! 9


#,$


----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this this question use anne !""-#$"#!A or Flight 'lanning anual )*T # Figure +.+ +.+ 

311.

Annex 033-12310A 033-12310A 2709= '7A9909= ; The fuel required for "! minutes holding @ in a racetrac4 pattern @ at 'A #,!! ft @ mean gross mass +, !!! 4g @ is ; #"#! 4g a) #!6! 4g b) #!#! 4g c) $#5! 4g d) Answer ; b)

#!6! 4g ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this this question use anne !""-#$"#!A or Flight 'lanning anual )*T # Figure +.+ +.+  312.

Annex 033-12310A 033-12310A 2709= '7A9909= ; The fuel required for +, minutes holding @ in a racetrac4 pattern @ at 'A ,!!! ft @ mean gross mass +& !!! 4g @ is ; #!6! 4g a) #%", 4g b) c) ##$, 4g #%6! 4g d) Answer ; b)

#%", 4g ----------------------------------------------------------------------------------------------------------------------------------------------------------------2ow manD feet Dou ha8e to climb to reach F7 &, 3 313. =i8en ; F7 &, eparture aerodrome ele8ation #,!! ft J92 K #!$" h'a Temperature Temperature K 01A # h'a K "! ft a) %"!! ft. %%!! ft. b) &5!! ft. c) %!!! ft. d)

Answer ; a)

%"!! ft. ----------------------------------------------------------------------------------------------------------------------------------------------------------------2ow manD hours in ad8ance of >HT should a ATC ATC flight plan be filed in the case of flights into areas subGect to air traffic 314. flow management ( ATF  3 #I!! hour. a) "I!! hours. b) !I"! hours. c) $ hours. d)

Answer ; b)

"I!! hours.


#,"


----------------------------------------------------------------------------------------------------------------------------------------------------------------0f a pilot lands at an aerodrome other than the destination aerodrome specified in the flight plan @ he must ensure that the AT1 AT1 unit at the destination aerodrome is informed within a certain number of minutes of his planned >TA at destination. This number of minutes is ; #! a) "! b) #, c) +, d) 315.

Answer ; b)

"! ----------------------------------------------------------------------------------------------------------------------------------------------------------------0f CA1 is #6! 4ts @ Altitude 6!!! ft. Temp. 01A -#!BC @ True Course ( TC  ",!B @ <: "$!+! @ distance from departure to 316. destination is ",! 9 @ endurance " hours @ and actual time of departure is ##!, ?TC. The distance from departure to 'oint of >qual Time ( '>T  is ; #%& 9 a) b) $!" 9 #5" 9 c) #+& 9 d) Answer ; b)

$!" 9 ----------------------------------------------------------------------------------------------------------------------------------------------------------------317. 0f CA1 is #6! 4ts @ Altitude 6!!! ft. Temp. Temp. 01A -#!BC @ True Course ( TC  ",!B @ <: "$!+! @ distance from departure to destination is ",! 9 @ endurance " hours @ and actual time of departure is ##!, ?TC. The 'oint of >qual Time ( '>T  is reached at ; #$!" ?TC a) #$$# ?TC b) #$"" ?TC c) #$#" ?TC d)

Answer ; d)

#$#" ?TC ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use T) @ Harcelona Area chart (#!-#:  318. 0f routeing along the Harcelona :F) corridors from )eus )>' to 1A9 C>790 @ what is the maimum altitude a8ailable without changing 3 a) "!!! ft $!!! ft b) ",!! ft c) +,!! ft d) Answer ; b)

$!!! ft ----------------------------------------------------------------------------------------------------------------------------------------------------------------0f Dour destination airport has no 0CA indicator @ in the appropriate bo of Dour ATC ATC flight plan @ Dou write ; 319. RRRR a) NNNN b) AAAA c)  d)

Answer ; b)

NNNN ----------------------------------------------------------------------------------------------------------------------------------------------------------------0n a flight plan when the destination aerodrome is A and the alternate aerodrome is H @ the final reser8e fuel for a turboGet 320. engine aeroplane corresponds to ; "! minutes holding #.,!! feet abo8e aerodrome H a) b) "! minutes holding $.!!! feet abo8e aerodrome H #, minutes holding $.!!! feet abo8e aerodrome A c) "! minutes holding #.,!! feet abo8e aerodrome A d)

Answer ; a)

"! minutes holding #.,!! feet abo8e aerodrome H ----------------------------------------------------------------------------------------------------------------------------------------------------------------0n an ATC ATC flight plan 0tem #, @ in order to define a position as a bearing and distance from a :) @ the group of figures 321. should consist of ; full name of :) @ true bearing and distance in 4ilometres. a) :) ident @ magnetic bearing and distance in 4ilometres. b) :) ident @ magnetic bearing and distance in nautical miles. c) :) ident @ true bearing and distance in 4ilometres. d) Answer ; c)

:) ident @ magnetic bearing and distance in nautical miles. -----------------------------------------------------------------------------------------------------------------------------------------------------------------


#,+


322.

0n an ATC ATC flight plan 0tem #, ( route  @ a cruising pressure altitude of "$!!! feet would be entered as ; 1"$!! a) b) F7"$! F"$! c) "$!!! d)

Answer ; c)

F"$! ----------------------------------------------------------------------------------------------------------------------------------------------------------------323. 0n an ATC flight plan 0tem #, ( route  @ in terms of latitude and longitude@ a significant point at +#B",P north +B#,P east should be entered as ; +#B",P 9 !+B #,P> a) +#",9!!+#,> b) 9+#", >!!+#, c) 9!+#",>!+#, d) Answer ; b)

+#",9!!+#,> ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this this question use anne !""-+%#%A or Flight 'lanning anual )*T # Figure +.".% +.".%  324.

Annex 033-4616A 033-4616A 0n order to find A7T>)9AT> F?>7 and T0> T A7T>)9AT> @ the A>)'7A9> '>)AT09= A9?A7 shall be entered with ; distance in nautical miles ( 9  @ wind component @ Mero fuel mass. a) distance in nautical air miles ( 9A  @ wind component @ landing mass at alternate. b) distance in nautical miles ( 9 9  @ wind component @ drD operating operating mass plus holding fuel. c) distance in nautical miles ( 9  @ wind component @ landing mass at alternate. d) Answer ; d)

distance in nautical miles ( 9  @ wind component @ landing mass at alternate.


#,,


----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use anne !""-##&!$ A  The true course is !+$B. The 8ariation in the area is %B < and the wind is calm. The de8iation card is reproduced in the anne. 0n order to follow this course @ the pilot must flD a compass heading of ; !,$B a) !++B b) !+!B c) d) !,5B

325.

Answer ; a)

!,$B ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this this question use anne !""-+%#%A or Flight 'lanning anual )*T # Figure +.".% +.".%  326.

Annex 033-4616A 033-4616A 0n order to get alternate fuel and time @ the twin-Get aeroplane operations manual graph shall be entered with ; Flight time @ wind component @ landing mass at alternate. a) 1till air distance @ wind component @ Mero fuel mass. b) istance ( 9  @ wind component @ Mero fuel mass. c) istance ( 9  @ wind component @ landing mass at alternate. d) Answer ; d)

istance ( 9  @ wind component @ landing mass at alternate.


#,%


----------------------------------------------------------------------------------------------------------------------------------------------------------------327.

( For this question use annees !""-##$$%A and !""-##$$%H 

Annexe 033-112 033-11226A 26A  033-11226! 033-11226! 0n standard atmosphere @ assuming a mass of #6& !!! 4g @ in order to flD at F7 "&! and to be at the optimum altitude @ Dour ach number should be ; !.5! a) !.5+ b) the same as for 7)C (7ong )ange Cruise c) d) !.5$ Answer ; d)

!.5$ ----------------------------------------------------------------------------------------------------------------------------------------------------------------0n the appropriate bo of an ATC ATC flight plan @ for endurance @ one must indicate the time corresponding to ; 328. the required fuel for the flight plus the alternate and +, minutes. a) b) the total usable fuel on board. the total usable fuel on board minus reser8e fuel. c) the required fuel for the flight. d)

Answer ; b)

the total usable fuel on board. ----------------------------------------------------------------------------------------------------------------------------------------------------------------0n the appropriate bo of an ATC ATC flight plan form @ concerning equipment @ the letter to be used to indicate that the aircraft is 329. equipped with a mode A +!6% codes transponder with altitude reporting capabilitD is ; 1 a) C b) A c) ' d)

Answer ; b)

C -----------------------------------------------------------------------------------------------------------------------------------------------------------------


#,&


0n the appropriate bo of an ATC ATC flight plan form @ corresponding to the estimated time of departure @ the time indicated is is that at which the aircraft intends to ; go off bloc4s. a) pass the departure beacon. b) start-up. c) d) ta4e-off.

330.

Answer ; a)

go off bloc4s. ----------------------------------------------------------------------------------------------------------------------------------------------------------------0n the ATC ATC flight plan 0tem #! ( equipment  @ the letter to indicate the carriage of a ser8iceable transponder - mode A 331. ( + digits-+!6% codes  and mode C @ is ; a) ' C b) H c) A d)

Answer ; b)

C ----------------------------------------------------------------------------------------------------------------------------------------------------------------0n the ATC flight plan 0tem #! @ “standard equipment” is considered to be ; 332. :2F )TF @ AF @ :) and 071 a) :2F )TF @ AF @ :) and transponder b) :2F )TF @ :) @ 091 and transponder c) :2F )TF @ :) @ 071 and transponder d)

Answer ; a)

:2F )TF @ AF @ :) and 071 ----------------------------------------------------------------------------------------------------------------------------------------------------------------0n the ATC ATC flight plan 0tem #" @ in a flight plan submitted before departure @ the departure time entered is the ; 333. estimated time o8er the first point en route. a) estimated ta4e-off time. b) c) estimated off-bloc4 time. allocated slot time. d)

Answer ; c)

estimated off-bloc4 time. ----------------------------------------------------------------------------------------------------------------------------------------------------------------0n the ATC ATC flight plan 0tem #, @ a cruising speed of +&! 4nots will be entered as ; 334. a) /9+&! 9!+&! b) !+&!/ c) 9+&! d)

Answer ; b)

9!+&! ----------------------------------------------------------------------------------------------------------------------------------------------------------------0n the ATC ATC flight plan 0tem #, ( Cruising speed  @ when not epressed as a ach number @ cruising speed is epressed as ; 335. CA1 a) =roundspeed b) TA1 TA 1 c) 0A1 d)

Answer ; c)

TA1 TA1 ----------------------------------------------------------------------------------------------------------------------------------------------------------------0n the ATC flight plan 0tem #, @ for a flight along a designated route @ where the departure aerodrome is not on or connected 336. to that route ; it is not necessarD to indicate indicate the point of Goining that route route as it will be ob8ious to the a) AT1 unit. the letters “CT” should be entered @ followed bD the point of Goining the AT1 route b) the words “as cleared” should be entered c) it is necessarD onlD to gi8e the first reporting point on that route d) Answer ; b)

the letters “CT” should be entered @ followed bD the point of Goining the AT1 route -----------------------------------------------------------------------------------------------------------------------------------------------------------------


#,5


337. 0n the ATC ATC flight plan item #, @ it is necessarD to enter anD point at which a change of cruising speed ta4es place. For this purpose a “change of speed” speed” is defined as ; #!  TA1 TA1 or !.!, ach or more. a) $! 4m per hour or !.# ach or more. b) , TA TA1 1 or !.!# ach or more. c) $! 4nots or !.!, ach or more. d) Answer ; c)

, TA TA1 1 or !.!# ach or more. ----------------------------------------------------------------------------------------------------------------------------------------------------------------0n the ATC ATC flight plan item #, @ when entering a route for which standard departure ( 10 1 0  and standard arri8al ( 1TA)  338. procedures eist ; neither 10 nor 1TA) 1TA) should be entered. a) b) both should be entered in the ATC plan where appropriate. 10s should be entered but not 1TA)s. 1TA)s. c) 1TA)1 1TA)1 should be entered but not 10s. d) Answer ; b)

both should be entered in the ATC plan where appropriate. ----------------------------------------------------------------------------------------------------------------------------------------------------------------339. 0n the ATC flight plan 0tem #6 @ if the number of passengers to be carried is not 4nown when the plan is readD for filing ; “TH9” ( to be notified  maD be entered in the rele8ant bo. a) the plan maD not be filed until the information is a8ailable. b) an estimate maD be entered but that number maD not subsequentlD be eceeded. c) the plan should be filed with the rele8ant bo blan4. d)

Answer ; a)

“TH9” ( to be notified  maD be entered in the rele8ant bo. ----------------------------------------------------------------------------------------------------------------------------------------------------------------0n the AT1 AT1 flight plan @ for a non-scheduled flight which of the following letters should be entered in 0tem 5 ( TDpe TDpe of 340. Flight  ; = a) R b) c) 9 91 d) Answer ; c)

9 ----------------------------------------------------------------------------------------------------------------------------------------------------------------0n the AT1 flight plan item & @ for a radio radio equipped equipped aircraft aircraft @ the identifier identifier must must alwaDs alwaDs ; 341. a) be the )TF callsign to be used include an indication of the aircraft tDpe b) include the aircraft registration mar4ing c) include the operating agencD designator d)

Answer ; a)

be the )TF callsign to be used ----------------------------------------------------------------------------------------------------------------------------------------------------------------0n the AT1 flight plan plan 0tem #6 @ emergencD and sur8i8al sur8i8al equipment carried on the flight should be indicated bD ; 342. placing a tic4 in the rele8ant bo a) crossing out the bo rele8ant to anD equipment not carried b) listing the items carried on the “)>A)/1” line c) circling the rele8ant bo d)

Answer ; b)

crossing out the bo rele8ant to anD equipment not carried ----------------------------------------------------------------------------------------------------------------------------------------------------------------0n the cruise at F7 #,, at $%! 4t TA1 @ the pilot plans for a ,!! feetmin descent in order to flD o8erhead A9 :) at $ !!! 343. feet ( J92 #!"! . TA1 TA1 will remain constant during descent @ wind is negligible @ temperature is standard. The pilot must start the descent at a distance from A9 of ; #"! 9 a) ##! 9 b) #$! 9 c) #+! 9 d) Answer ; c)

#$! 9 -----------------------------------------------------------------------------------------------------------------------------------------------------------------


#,6


0n the e8ent that that 1>7CA7 @ is prescribed bD an appropriate appropriate authoritD @ in which section of the ATC flight plan will the 1>7CA7 code be entered 3 T2>) 09F)AT09 a) b) )?T> >J?0'>9T c) A0)C)AFT 0>9T0F0CAT09 0>9T0F 0CAT09 d)

344.

Answer ; a)

T2>) 09F)AT09 ----------------------------------------------------------------------------------------------------------------------------------------------------------------345. ( For this question use anne !""-###5"A !""-###5"A 

Annex 033-11 033-111"1A 0n the 8icinitD of 'A)01 ( +6B9 !!"B>  the tropopause is at about ; F7+!! a) F7",! b) F7"+! c) F7"5! d) Answer ; d)

F7"5! -----------------------------------------------------------------------------------------------------------------------------------------------------------------


#%!


346.

( For this question use anne !""-#$"$!A 

Annex 033-12320A 033-12320A 0n the 8icinitD of 12A999 ( ,$B 9 !!6B<  the tropopause is at about F7 ; "!! a) "%! b) c) ",! $&! d) Answer ; b)

"%! ----------------------------------------------------------------------------------------------------------------------------------------------------------------347. “0ntegrated range” cur8es or tables are presented in the Aeroplane perations anuals.Their purpose is ; a) to determine the fuel consumption for a certain still air distance considering the decreasing fuel flow with decreasing mass. to determine determine the optimum optimum speed speed considering the fuel cost cost as well as the time time related related cost cost of the aeroplane. aeroplane. b) to determine the still air distance for a wind components 8arDing with altitude. c) to determine the flight time for a certain leg under consideration of temperature de8iations. d)

Answer ; a)

to determine the fuel consumption for a certain still air distance considering the decreasing fuel flow with decreasing mass. ----------------------------------------------------------------------------------------------------------------------------------------------------------------0t is possible @ in flight @ to ; 348. #. file an ATC fl flight pl plan $. mod modifD ifD an an ac acti8 ti8e AT ATC fli fligght plan plan ". cance ncel an an ac acti8e ti8e ATC fli fligh ghtt pla plann +. clos lose an an ac acti8e ti8e ATC fli fligght pla plan
Answer ; a)

#@$@"@+


#%#


----------------------------------------------------------------------------------------------------------------------------------------------------------------0tem 6 of the ATC flight plan includes “9?H>) A9 TO'> F A0)C)AFT”. 0n this case “9?H>)” means ; the number of aircraft flDing in a group a) b) the registration number of the aircraft the number of aircraft which will separatelD be using a repetiti8e flight plan ( )'7  c) the 0CA tDpe designator number as set out in 0CA oc 5%+" d)

349.

Answer ; a)

the number of aircraft flDing in a group ----------------------------------------------------------------------------------------------------------------------------------------------------------------350. ( For this this question use anne !""-##$,"A @ !""-##$,"H @ !""-##$,"C and !""-##$," 

Annex 033-11253A 033-11253A  033-11253! 033-11253!  033-11253/ 033-11253/  033-11253) 033-11253) /nowing that ; ass at bra4e release I #6! !!! 4g 1elected cruise speed I !.5$ ach Flight leg distance I # ,!! 9 Cruise le8el I optimum Air conditioning I standard Anti-icing I FF Temperature Temperature I 01A C= I "& Assuming Mero wind @ the planned flight time from ta4e-off to landing needed to complete this flight will be ; $!" minutes a) #65 minutes b) $!6 minutes c) #6$ minutes d) Answer ; c)

$!6 minutes


#%$


----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use anne !""-##$,$A @ !""-##$,$H and !""-##$,$C 

351.

Annex 033-11252A 033-11252A  033-11252! 033-11252!  033-11252/ 033-11252/ /nowing that ; ass at bra4e release I $#! !!! 4g 1elected cruise speed I !.5$ ach Air distance I " !!! 9 Cruise le8el I optimum Air conditioning I standard Anti-icing I FF Temperature Temperature I 01A C= I "& Assuming Mero wind @ the planned flight time from ta4e-off to landing needed to complete this flight will be ; "6+ minutes a) +!! minutes b) "56 minutes c) "5" minutes d) Answer ; b)

+!! minutes


#%"


-----------------------------------------------------------------------------------------------------------------------------------------------------------------

352.

( For this this question use anne !""-##$,"A @ !""-##$,"H @ !""-##$,"C and !""-##$," 

Annex 033-11253A 033-11253A  033-11253! 033-11253!  033-11253/ 033-11253/  033-11253) 033-11253) /nowing that ; ass at bra4e release I #6! !!! 4g 1elected cruise speed I !.5$ ach Flight leg distance I # ,!! 9 Cruise le8el I optimum Air conditioning I standard Anti-icing I FF Temperature Temperature I 01A C= I "& Assuming Mero wind @ the planned landing mass at destination will be ; #&! $!! 4g a) #%6 $!! 4g b) #&# $!! 4g c) #&+ 5!! 4g d) Answer ; c)

#&# $!! 4g -----------------------------------------------------------------------------------------------------------------------------------------------------------------


#%+


353.

( For this question use anne !""-##$,$A @ !""-##$,$H @ and !""-##$,$C 

Annex 033-11252A 033-11252A  033-11252! 033-11252!  033-11252/ 033-11252/ /nowing that ; ass at bra4e release I $#! !!! 4g 1elected cruise speed I !.5$ ach Flight leg distance I " !!! 9 Cruise le8el I optimum Air conditioning I standard Anti-icing I FF Temperature Temperature I 01A C= I "& Assuming Mero wind @ the planned landing mass at destination will be ; #&$ "!! 4g a) #&! +!! 4g b) #&# "!! 4g c) #&% #!! 4g d) Answer ; a)

#&$ "!! 4g


#%,


-----------------------------------------------------------------------------------------------------------------------------------------------------------------

354.

ar4 the correct statement ; 0f a decision point procedure is applied for flight planning ; the trip fuel to the destination aerodrome is to be calculated 8ia the suitable enroute alternate. a) the trip fuel to the destination aerodrome is to be calculated 8ia the decision point. b) c) the fuel calculation is based on a contingencD fuel from departure aerodrome to the decision point. a destination alternate is not required. d)

Answer ; b)

the trip fuel to the destination aerodrome is to be calculated 8ia the decision point. ----------------------------------------------------------------------------------------------------------------------------------------------------------------inimum planned ta4e-off fuel is #%! 4g ( "! total reser8e fuel is included .Assume the groundspeed on this trip is 355. constant.
Answer ; b)

i8ersion to a nearbD alternate is necessarD @ because the remaining fuel is not sufficient. ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use anne !""-#!66#A or )oute anual chart >(20, CAA->dition  356. f the following @ the preferred airwaDs routing from AH01> AH01> AH ##".& ( +&B$%P9 !!#B!+P>  to A=>9 A=9 A=9 ( +"B,"BP9 !!!B,$P>  abo8e F7$!! is ; ?2+! F?C ?2$! '>)0C ?A"+ a) b) ?H#6 C=C ?A$, ?H#6 '0 ?H#6, c) ?A"+ d)

Answer ; d)

?A"+ ----------------------------------------------------------------------------------------------------------------------------------------------------------------357. ( For this question use anne !""-#!66$A or )oute anual chart >(20+ CAA->dition  f the following @ the preferred airwaDs routing from C7ACT9 C79 ##+.,, ( ,#B,#P9 !!#B!6P>  to 09A) 09 ##+." ( +5B",P9 !!$B!,P<  abo8e F7$+, is ; ?)#$ 0 ?A+& '> ?A+&, 1/? ?2### ?2### a) ?)#$ 0 ?)5 1A ?H## HA)7? ?<##, b) ?H$6 7A ?)# 0 ?A"+ 707A9 ?)6 c) d) ?H$6 7A ?)# )TA )TAC C ?)#+

Answer ; d)

?H$6 7A ?)# )TA )TAC C ?)#+ ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use anne !""-#!656A or )oute anual chart >(20+ CAA->dition  358. f the following @ the preferred airwaDs routing from F)A9/F?)T FF ##+.$ ( ,!B!"P9 !!5B"5P>  to //1O ( ,#B!%P9 !!$B"6P>  abo8e F7$+, @ on a
?)#! 9T ?H% H?H AT1 ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use anne !""-#!66!A or )oute anual chart >(20, CAA->dition  359. f the following @ the preferred airwaDs routing from A)T0=?>1 T= ##&." ( +"B$"P9 !!,B!,P>  to 1T ')>R 1') ##".6 ( +%B$5P9 !!%B$&P>  abo8e F7$+, is ; ?H$5+ :07A) ?H$5 a) ?A% 71A ?=,$ b) ?H$5 c) ?H$5$ =9 ?H+% d)

Answer ; d)

?H$5$ =9 ?H+% -----------------------------------------------------------------------------------------------------------------------------------------------------------------


#%%


( For this question use )oute anual chart 9A'  n a direct great circle course from )>O/*A:0/ )>O/*A:0/ ( %+B#!P 9 !$$B!!P<  to A1T>)A ( ,$B"$P9 !!+B,!P>  @ the (a a8erage true course @ and (b distance @ are ; (a ##5 @ (b #!6, 9 a) (a "## @ (b #5$+ 9 b) (a #+! @ (b #5$+ 9 c) (a #"# @ (b #!6, 9 d)

360.

Answer ; d)

(a #"# @ (b #!6, 9 ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use )oute anual chart 9A'  361. n a direct great circle course from 1hannon ( ,$B+"P 9 !!5B,"P<  to =ander ( +5B,+P 9 !,+B"$P<  @ the (a a8erage true course @ and (b distance @ are ; (a $5# @ (b #5&& 9 a) b) (a $5# @ (b $&"! 9 (a $++ @ (b #,$! 9 c) (a $%$ @ (b #&$! 9 d)

Answer ; d)

(a $%$ @ (b #&$! 9 ----------------------------------------------------------------------------------------------------------------------------------------------------------------362. n a gi8en path @ it is possible to chose between four flight le8els ( F7  @ each associated with a mandatorD flight ach 9umber (  . The flight conditions @ static static air temperature ( 1AT 1AT  and headwind headwind component ( 2
F7$&! ----------------------------------------------------------------------------------------------------------------------------------------------------------------n a :F) ATC ATC flight plan @ the total estimated time is ; 363. the estimated time from ta4e-off to o8erhead the destination airport @ plus #, minutes. a) the estimated time from ta4e-off to landing at the alternate airport. b) the estimated time required from ta4e-off to arri8e o8er the destination airport. c) d) the estimated time from engine start to landing at the destination airport.

Answer ; c)

the estimated time required from ta4e-off to arri8e o8er the destination airport. ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this this question use anne !""-#$","A or )oute anual chart , AT(20  364. n airwaD 'T1 ' from :igra ( %$B""+9 !!%B!$P>  @ the initial great circle grid course is ; a) "++ "," b) ",! c) "+& d)

Answer ; a)

"++ ----------------------------------------------------------------------------------------------------------------------------------------------------------------n an ATC ATC flight plan @ an aircraft indicated as “2” for “2ea8D” ; 365. is of the highest wa4e turbulence categorD categorD.. a) has a certified landing mass greater than or equal to #"% !!! 4g. b) has a certified ta4e-off mass greater than or equal to #+! !!! 4g. c) requires a runwaD length of at least $ !!!m at maimum certified ta4e-off mass. d)

Answer ; a)

is of the highest wa4e turbulence categorD categorD.. ----------------------------------------------------------------------------------------------------------------------------------------------------------------n an ATC ATC flight plan @ the letter “O” is used to indicate that the flight is carried out under the following flight rules ; 366. 0F) a) :F) followed bD 0F) b) :F) c) 0F) followed bD :F) d)

Answer ;


#%&


d)

0F) followed bD :F)

----------------------------------------------------------------------------------------------------------------------------------------------------------------n an ATC flight plan @ to indicate that Dou will o8erflD the waDpoint )> at #$! 4t at flight le8el !5, @ Dou will write ; )>F7!5,9!#$! a) )>/!#$!F7!5, b) c) )>F!5,9!#$! )>9!#$!F!5, d)

367.

Answer ; d)

)>9!#$!F!5, ----------------------------------------------------------------------------------------------------------------------------------------------------------------n an ATC ATC flight plan @ to indicate that Dou will o8erflD the waD-point TA9= TA9= at ",! 4ts at flight le8el $5! @ Dou write ; 368. a) TA9=9!",!F$5! TA9=T",!F$5! b) TA9=/!",!F7$5! c) TA9=F7$5!9!",! d)

Answer ; a)

TA9=9!",!F$5! ----------------------------------------------------------------------------------------------------------------------------------------------------------------n an ATC ATC flight plan @ Dou are required to indicate in the bo mar4ed “speed” the planned pl anned speed for the first part of the 369. cruise or for the entire cruise.This speed is ; The estimated ground speed. a) The indicated airspeed. b) The equi8alent airspeed. c) d) The true airspeed.

Answer ; d)

The true airspeed. ----------------------------------------------------------------------------------------------------------------------------------------------------------------n an 0F) na8igation chart @ in a #B quadrant of longitude and latitude @ appears the following information “5!”. This means 370. that within this quadrant ; a) the minimum safe altitude is 5!!! ft the minimum flight le8el is F7 5! b) the altitude of the highest obstacle is 5!!! ft c) the floor of the airwaD is at 5!!! ft d) Answer ; a)

the minimum safe altitude is 5!!! ft ----------------------------------------------------------------------------------------------------------------------------------------------------------------n an instrument approach chart @ a minimum sector altitude ( 1A is defined in relation to a radio na8igation facilitD. 371.
Answer ; b)

$, 9 -----------------------------------------------------------------------------------------------------------------------------------------------------------------


#%5


372.

( For this question use anne !""-#$"$5A 

Annex 033-12320A 033-12320A 8er 799 ( ,#B9 !!!B><  @ the lowest F7 listed which is unaffected bD CAT is ; a) $&! $"! b) "%! c) "#! d) Answer ; b)

$"! ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use 0mage #+  373.

,age 14 'lanned and actual data as shown in the Flight 7og ecerpt. Actual =round 1peed ( =1  on the leg H>TA to =AA will be #!, /T. 0f all other flight parameters remain unchanged unchanged @ what fuel remaining should be epected at at waDpoint =AA 3 "$,! 4g a) "+"! 4g b) ""#5 4g c) "+5! 4g d) Answer ; a)

"$,! 4g


#%6


-----------------------------------------------------------------------------------------------------------------------------------------------------------------

374.

( For this question use 0mage ## 

,age 11 11 'lanned and actual data as shown in the Flight 7og ecerpt. Actual =round 1peed ( =1  on the leg H>TA to =AA will be ##! /T. /T. 0f all other flight parameters remain unchanged unchanged @ what fuel remaining should be epected epected at waDpoint =AA 3 a) $%$, 4g $6!! 4g b) $5$! 4g c) $&$" 4g d) Answer ; a)

$%$, 4g ----------------------------------------------------------------------------------------------------------------------------------------------------------------'lanning a flight from 'aris ( Charles de =aulle  to 7ondon (2eathrow for a twin S Get aeroplane. 375. 'replanning ; aimum Ta4e-off Ta4e-off ass I %$ 5!! 4g aimum Nero Fuel ass I ,# $,! 4g aimum 7anding ass I ,+ 6!! 4g aimum Tai Tai ass I %" !,! 4g Assume the following preplanning results ; Trip fuel I # 5!! 4g Alternate fuel I # +!! 4g 2olding fuel ( final reser8e  I # $$, 4g rD perating ass I "+ !!! 4g Traffic 7oad I #" !!! 4g Catering I &,! 4g Haggage I " ,!! 4g Find the Ta4e-off ass ( T  ; ,, &%, 4g. a) ,$ $%, 4g. b) c) ,# +$, 4g. ,# ,#, 4g. d)

Answer ; d)

,# ,#, 4g. -----------------------------------------------------------------------------------------------------------------------------------------------------------------


#&!


376.

( For this this question use anne !""-"6#!A or Flight 'lanning anual )*T # Figure +.+ 

Annex 033-3910A 033-3910A 'lanning a flight from 'aris Charles de =aulle to 7ondon 2eathrow for a twin-Get aeroplane. 'replanning ; rD perating ass (   I "+ !!! 4g Traffic 7oad I #" !!! 4g The holding is planned at # ,!! ft abo8e alternate ele8ation. The alternate ele8ation is $,% ft. The holding is planned for "! minutes with no reductions. etermine the >stimated 7anding ass at alternate anchester ; $ $,! 4g. a) b) +5 #$, 4g. +6 $,! 4g. c) +5 %&, 4g. d) Answer ; b)

+5 #$, 4g. ----------------------------------------------------------------------------------------------------------------------------------------------------------------377. ( For this question use annees annees !""-"6#$A and !""-"6#$H or )oute )oute anual chart >(20+ >(20+ CAA->dition and Flight planning planning manual Figure +.".$A  'lanning a flight from 'aris Charles de =aulle ( 9+6 !!.6 >!!$ "%.6  to 7ondon 2eathrow ( 9,# $6.$
# &+! 4g. ----------------------------------------------------------------------------------------------------------------------------------------------------------------378. ( For this question use annees annees !""-"6##A and !""-"6##H !""-"6##H or )oute )oute anual anual chart >(20+ CAA->dition and Flight Flight planning planning manual Figure +.".%  'lanning a flight from 'aris Charles de =aulle ( 9+6 !!.6 >!!$ "%.6  to 7ondon 2eathrow ( 9,# $6.$ stimated 7anding ass at alternate is about ,! !!! 4g. Find the alternate fuel and the according time ; # "!! 4g and $5 minutes. a) # $!! 4g and $% minutes. b) # +,! 4g and "$ minutes. c) # %!! 4g and "% minutes. d) Answer ; c)

# +,! 4g and "$ minutes.


#&#


-----------------------------------------------------------------------------------------------------------------------------------------------------------------

379.

( For this this question use annees !""-##!&"A @ !""-##!&"H @ !""-##!&"C and !""-##!&" 

Annex 033-11073A 033-11073A


Annex 033-11073! 033-11073!

#&$


Annex 033-11073/ 033-11073/

Annex 033-11073) 033-11073)

'lanning a AC2 !.5$ cruise at F7 "6! @ the estimated landing mass is #%! !!! 4g @ the ground distance is $ 5!! 9 and the mean tailwind is #!! 4t @ 01A conditions. Fuel consumption will be ; $% 6,! 4g a) $$ 5%! 4g b) "! ##& 4g c) $+ 6!! 4g d) Answer ; a)

$% 6,! 4g -----------------------------------------------------------------------------------------------------------------------------------------------------------------


#&"


380.

( For this this question use annees !""-##!&"A @ !""-##!&"H @ !""-##!&"C and !""-##!&" 

Annex 033-11073A 033-11073A


Annex 033-11073! 033-11073!

#&+


Annex 033-11073/ 033-11073/

Annex 033-11073) 033-11073)

'lanning a AC2 !.5$ cruise at F7 "6! @ the estimated landing mass is #%! !!! 4g. The ground distance is $ 5!! 9 and the mean wind is equal to Mero. 01A conditions. Fuel consumption will be ; "! ##& 4g a) $& ,&& 4g b) "! "&# 4g c) "$ %,& 4g d) Answer ; d)

"$ %,& 4g -----------------------------------------------------------------------------------------------------------------------------------------------------------------


#&,


381.

( For this question use anne anne !""-6&!"A or )oute anual 10 chart chart $!-" for 'A)01 'A)01 Charles-de-=aulle 

Annex 033-9703A 033-9703A 'lanning an 0F)-flight from 'aris ( Charles de =aulle  )
$+., 9 -----------------------------------------------------------------------------------------------------------------------------------------------------------------


#&%


382.

( For this this question use anne !""-6&!"A or )oute anual chart 10 'A)01 'A)01 Charles-e-=aulle Charles-e-=aulle ($!-" 

Annex 033-9703A 033-9703A 'lanning an 0F) flight from 'aris ( Charles de =aulle  to 7ondon ( 2eathrow . Find the ele8ation of the departure aerodrome ; $#& ft. a) $ ft. b) $%5 ft. c) "5& ft. d) Answer ; d)

"5& ft. -----------------------------------------------------------------------------------------------------------------------------------------------------------------


#&&


383.

( For this this question use anne !""-6&#!H or )oute anual chart 1TA) 1TA) 799 2eathrow (#!-$ 

Annex 033-9710! 033-9710! 'lanning an 0F) flight from 'aris ( Charles de =aulle  to 7ondon ( 2eathrow . Find the ele8ation of the destination aerodrome ; #!! ft. a) 5! ft. b) && ft. c) #&& ft. d) Answer ; b)

5! ft. -----------------------------------------------------------------------------------------------------------------------------------------------------------------


#&5


384.

( For this this question use anne !""-6&!!A or Flight 'lanning anual )*T # Figure +.,.# +.,.# 

Annex 033-9700A 033-9700A 'lanning an 0F)-flight from 'aris ( Charles de =aulle  to 7ondon ( 2eathrow  for the twin Get aeroplane. =i8en ; >stimated Ta4e-off Ta4e-off ass ( T  ,$!!! 4g Airport ele8ation "5& ft F7 $5! <: $5!B+! 4t 01A e8iation -#!BC A8erage True Course "+!B Find I Time to the top of climb ( TC  ; #, min a) " min b) #$ min c) ## min d) Answer ; d)

## min


#&6


-----------------------------------------------------------------------------------------------------------------------------------------------------------------

( For this question use anne !""-"6!5A or )oute anual chart >(20+ CAA->dition  'lanning an 0F) flight from 'aris Charles de =aulle ( 9+6 !!.6 >!!$ "%.6  to 7ondon 2eathrow ( 9,# $6.$
385.

Answer ; b)

5! ft. ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use anne !""-"6!6A or )oute anual chart >(20+ CAA->dition  386. 'lanning an 0F) flight from 'aris Charles de =aulle ( 9+6 !!.6 >!!$ "%.6  to 7ondon 2eathrow ( 9,# $6.$
Answer ; b)

$!& 9. ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this this question use anne !""-6&!6A or 10 chart 'aris Charles de =aulle $!-"  387. 'lanning an 0F)-flight from 'aris Charles de =aulle to 7ondon. 10 is AHH 5A. Assume :ariation :ariation "B< @ TA1 TA1 +"!4ts @ <: $5!+! and distance to top of climb ,! 9. etermine the magnetic course @ ground speed and wind correction angle from top of climb to AHH ##%.% ; a) C "+6B @ =1 +#+ 4t @
C "+6B @ =1 +#+ 4t @
Answer ; d)

&+., 9 -----------------------------------------------------------------------------------------------------------------------------------------------------------------


#5!


389.

( For this this question use anne !""-6&!+A or Flight 'lanning anual )*T # Figure +.,.+ +.,.+ 

Annex 033-9704A 033-9704A 'lanning an 0F)-flight from 'aris to 7ondon for the twin Get aeroplane. =i8en ; >stimated 7anding ass +6&!! 4g F7 $5! <: $5!B+! 4t A8erage True Course "$!B 'rocedure for descent .&+ $,! /0A1 etermine the distance from the top of descent to 7ondon ( ele8ation 5! ft  ; 6& 9 a) 5& 9 b) &% 9 c) %, 9 d) Answer ; c)

&% 9 -----------------------------------------------------------------------------------------------------------------------------------------------------------------


#5#


390.

( For this this question use anne !""-6&!%A or Flight 'lanning anual )*T # Figure +.,.+ +.,.+ 

Annex 033-9706A 033-9706A 'lanning an 0F)-flight from 'aris to 7ondon for the twin Get aeroplane. =i8en ; >stimated 7anding ass +6&!! 4g F7 $5! <: $5!B+! 4t A8erage True Course "$!B 'rocedure for descent .&+ $,! /0A1 etermine the fuel consumption from the top of descent to 7ondon ( ele8ation 5! ft  ; "$! 4g a) $%" 4g b) $#! 4g c) $&" 4g d) Answer ; d)

$&" 4g -----------------------------------------------------------------------------------------------------------------------------------------------------------------


#5$


391.

( For this this question use anne !""-6&!5A or Flight 'lanning anual )*T # Figure +.,.".$ +.,.".$ 

Annex 033-970"A 033-970"A 'lanning an 0F)-flight from 'aris to 7ondon for the twin Get aeroplane. =i8en ; =ross mass ,!!!! 4g F7 $5! 01A e8iation -#!BC Cruise procedure ach !.&+ etermine the TA1 ; +$& 4t a) +"! 4t b) ++! 4t c) +#& 4t d) Answer ; b)

+"! 4t -----------------------------------------------------------------------------------------------------------------------------------------------------------------


#5"


392.

( For this this question use anne !""-6&!,A or Flight 'lanning anual )*T # Figure +.,.+ +.,.+ 

Annex 033-9705A 033-9705A 'lanning an 0F)-flight from 'aris to 7ondon for the twin Get aeroplane. =i8en ; >stimated 7anding ass +6&!! 4g F7 $5! <: $5!B+! 4t A8erage True Course "$!B 'rocedure for descent .&+ $,! /0A1 etermine the time from the top of descent to 7ondon ( ele8ation 5! ft  ; #& min a) #! min b) 5 min c) #6 min d) Answer ; d)

#6 min -----------------------------------------------------------------------------------------------------------------------------------------------------------------


#5+


393.

( For this this question use anne !""-6&!!A or Flight 'lanning anual )*T # Figure +.,.# +.,.# 

Annex 033-9700A 033-9700A 'lanning an 0F)-flight from 'aris to 7ondon for the twin Get aeroplane. =i8en ; >stimated Ta4e-off Ta4e-off ass ( T  ,$!!! 4g Airport ele8ation "5& ft F7 $5! <: $5!B+! 4t 01A e8iation -#!BC A8erage True Course "+!B Find I Fuel to the top of climb ( TC  ; #,!! lbs a) ##!! 4g b) #!!! lbs c) #!!! 4g d) Answer ; d)

#!!! 4g -----------------------------------------------------------------------------------------------------------------------------------------------------------------


#5,


394.

( For this question use anne anne !""-6%66A and !""-6%66H or Flight Flight 'lanning anual )*T # 'aragraph 'aragraph ,.# and Figure

+.,.# 

Annex 033-9699A 033-9699A  033-9699! 'lanning an 0F)-flight from 'aris to 7ondon for a twin Get aeroplane. =i8en ; >stimated Ta4e-off Ta4e-off ass ( T  ,$!!! 4g Airport ele8ation "5& ft F7 $5! <: $5!B+! 4t 01A-e8iation -#!BC A8erage True Course "+!B Find I =round distance to the top of climb ( TC  ; ," 9 a) ,% 9 b) +& 9 c) ,! 9 d) Answer ; d)

,! 9


#5%


----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use annees annees !""-"6!5A @ !""-6&#!H and !""-6&#!C or )oute anual chart >(20+ CAA->dition @ 1TA) 1TA) #!-$ and 0nstrument approach chart ##-+ 071 > )wD $&) for 7ondon 2eathrow  'lanning an 0F)-flight from 'aris to 7ondon ( 2eathrow . Assume ; 1TA) is H0= $A :ariation ,B < >n-route TA1 +"! 4ts <: $5!+! escent distance &%9 etermine the magnetic course @ ground speed and wind correction angle from AHH ##%.% ( 9,! !5.# >!!# ,#."  to top of descent ; C #+#B @ =1 "6% 4t @
Answer ; d)

C "$#B @ =1 "6% 4t @ )wD $&) for 7ondon (2eathrow 

Annex 033-3301A 033-3301A 'lanning an 0F)-flight from 'aris to 7ondon ( 2eathrow .9ame the identifier and frequencD of the initial approach fi ( 0AF  of the H0= $A arri8al route ; H0= ##,.# 42M a) >' "#% 42M b) C/ ##,." 2M c) H0= ##,.# 2M d) Answer ; d)

H0= ##,.# 2M


#5&


-----------------------------------------------------------------------------------------------------------------------------------------------------------------

397.

( For this question use anne !""-##$%$A 

Annex 033-11262A 033-11262A 'rior to an 0F) flight @ when filling in the 0CA flight plan @ the time information which should be entered in bo #" I “Time” is ; planned ta4e-off time. a) the time of flight plan filing. b) estimated off-bloc4 time. c) planned engine start time. d) Answer ; c)

estimated off-bloc4 time. -----------------------------------------------------------------------------------------------------------------------------------------------------------------


#55


398.

( For this question use anne !""-##$%$A 

Annex 033-11262A 033-11262A 'rior to an 0F) flight @ when filling in the 0CA flight plan @ the time information which should be entered in bo #% I “Total estimated time” is the time elapsed from ; ta4e-off until reaching the 0AF ( 0nitial Approach Fi  of the destination aerodrome. a) ta4e-off until landing. b) tai-out prior to ta4e-off until taiing completion after landing. c) taiing until the 0AF ( 0nitial Approach Fi  of the destination aerodrome. d) Answer ; a)

ta4e-off until reaching the 0AF ( 0nitial Approach Fi  of the destination aerodrome. -----------------------------------------------------------------------------------------------------------------------------------------------------------------


#56


399.

( For this this question use anne !""-6,%$A or Flight 'lanning anual )*T # Figure +.,.".# +.,.".# 

Annex 033-9562A 033-9562A The aeroplane gross mass at top of climb is %#,!! 4g. The distance to be flown is "5, 9 at F7 ",! and AT -,+." BC. The wind component is +! 4t tailwind. ?sing long range cruise procedure what fuel is required 3 $!,! 4g a) $$,! 4g b) $",! 4g c) $#,! 4g d) Answer ; d)

$#,! 4g ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use anne !""- ##!#%A or )oute anual chart >(7,  400. The airwaD intersection at )99>HO ( ,%B#5P9 !#,B#%P>  is mar4ed bD ; a TACA9 callsign )9 a) a fan mar4er callsign 7' b) an 9H callisign 9 c) an 9H callsign 7F d)

Answer ; c)

an 9H callisign 9 -----------------------------------------------------------------------------------------------------------------------------------------------------------------


#6!


401.

( For this question use anne !""-#$"#6A 

Annex 033-12314A 033-12314A The approimate mean wind component ( 4t  along true course #5!B from ,!B9 to +!B9 at !!,B < is ; tail wind ,, 4t a) tail wind &! 4t b) tail wind +! 4t c) d) headwind ,, 4t Answer ; a)

tail wind ,, 4t -----------------------------------------------------------------------------------------------------------------------------------------------------------------


#6#


402.

( For this question use anne !""-###6$A !""-###6$A 

Annex 033-11 033-11190A The approimate mean wind component ( 4t  at ach !.&5 along true course $&!B at ,!B9 from !!!B to !#!B< is ; +! 4t headwind component a) ", 4t tailwind component b) $, 4t tailwind component c) ,, 4t headwind component d) Answer ; a)

+! 4t headwind component ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use anne !""-#$"&"A or )oute anual chart 9A'  403. The a8erage magnetic course from A ( %+B9 !!%B>  to C ( %$B9 !$!B<  is ; $&6B a) b) $&#B $+&B c) $,6B d)

Answer ; b)

$&#B ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use anne !""-#$"%5A or )oute anual chart 9A'  404. The a8erage magnetic course from C ( %$B9 !$!B<  to H ( ,5B9 !!+B>  is ; ##6B a) ##5B b) !66B c) #!6B d)

Answer ; a)

##6B -----------------------------------------------------------------------------------------------------------------------------------------------------------------


#6$


405.

( For this question use anne !""-#$"&+A or )oute anual chart 9A'  The a8erage true course from A ( %+B9 !!%B>  to C ( %$B9 !$!B<  is ; !&6B a) b) $&#B $+&B c) $,6B d)

Answer ; d)

$,6B ----------------------------------------------------------------------------------------------------------------------------------------------------------------406. ( For this question use anne !""-#$"%6A or )oute anual chart 9A'  The a8erage true course from C ( %$B9 !$!B<  to H ( ,5B9 !!+B>  is ; #!6B a) ##6B b) #$!B c) !66B d)

Answer ; a)

#!6B ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use T) @ Athinai (2ellini4on Approach chart ($6-#  407. The callsign and frequencD to use to obtain start up clearance is ; Approach ##6.#! a) b) Tower ##5.#! =round #$#.&! c) AT01 #$".+! d)

Answer ; c)

=round #$#.&! -----------------------------------------------------------------------------------------------------------------------------------------------------------------


#6"


408.

( For this question use anne anne !""- ##!+6A ##!+6A or )oute )oute anual anual 1TA) 1TA) charts charts for ?90C2 (#!-$A@H 

Annex 033-11049A 033-11049A The correct arri8al route and 0nitial Approach Fi ( 0AF  for an arri8al from the west 8ia TA9= for runwaD !5 7) is ; 9= #T @ 0AF )/07 a) /H #T @ 0AF )/07 b) AA7>9 #T @ 0AF )/07 c) AA7>9 #T @ 0AF H= d) Answer ; c)

AA7>9 #T @ 0AF )/07


#6+


----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question question use anne !""- ##!%"A ##!%"A or )oute anual chart 'A)01 'A)01 C2A)7>1 > > =A?77> =A?77> 071 )wD $& ($#-$ 

409.

Annex 033-11063A 033-11063A The crossing altitude and descent instruction for a propeller aircraft at C?70>)1 ( C7  are ; Cross at F7&! descend to +!!! ft a) Cross at F7%! and maintain b) Cross at F7%! descend to +!!! ft c) Cross at F75! descend to F7&! d) Answer ; c)

Cross at F7%! descend to +!!! ft


#6,


----------------------------------------------------------------------------------------------------------------------------------------------------------------410.

The cruising speed to write in the appropriate bo of an ATC ATC flight plan is ; calibrated air speed. a) true air speed. b) ground speed. c) indicated air speed. d)

Answer ; b)

true air speed. ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question question use anne !""- ##!,5A ##!,5A or )oute anual chart 799 799 2>AT2) 2>AT2)< < 071 071 > )wD !67 (##-$  411.

Annex 033-1105"A 033-1105"A The ecision Altitude ( A  for a 071 straight-in landing is ; +!! ft a) $!! ft b) +5! ft c) $5! ft d) Answer ; d)

$5! ft -----------------------------------------------------------------------------------------------------------------------------------------------------------------


#6%


412.

( For this question use )oute anual chart >(20#  The direct distance from T0)>> ##&.& T0) ( ,%B"!P9 !!%B,"P<  to 09:>)9>11 #!6.$ 091 ( ,&B"$P9 !!+B!"P<  is ; $!+ 9 a) ##$ 9 b) #6$ 9 c) d) "%! 4m

Answer ; a)

$!+ 9 ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use anne !""-#$"&$A or )oute anual chart 9A'  413. The distance ( 9  from A ( %+B9 !!%B>  to C ( %$B9 !$!B<  is ; a) &$! %6! b) #,6! c) #++! d)

Answer ; a)

&$! ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use Anne !""-#$"&&A or )oute anual chart 9A'  414. The distance ( 9  from C ( %$B9 !$!B<  to H ( ,5B9 !!+B>  is ; &%! a) &&, b) &$, c) d) &!!

Answer ; a)

&%! ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use )oute anual chart >(7#  415. The distance on airwaD H+ from '7> 2077 ##$.# '7 to 12A'' ( ,+B"!P9 !!$B"5P<  is ; a) "! 9 ,# 9 b) "# 9 c) +6 9 d)

Answer ; d)

+6 9 ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use T) (:F) @ Aberdeen Aberdeen 0nformation 'age (#6-"  416. The >ast Apron and >astern TwD ha8e restricted access. The maimum permitted wingspan ; is $! ft. a) is the same as a Heech $!!. b) does not applD to helicopters. c) d) is $! m.

Answer ; d)

is $! m. ----------------------------------------------------------------------------------------------------------------------------------------------------------------The final reser8e fuel for aeroplanes with turbine engines is ; 417. fuel to flD for +, minutes at holding speed at #!!! ft ( "!! m  abo8e aerodrome ele8ation ele8ation in standard standard a) conditions. fuel to flD for "! minutes at holding speed at #,!! ft ( +,! m  abo8e aerodrome ele8ation ele8ation in standard standard b) conditions. fuel to flD for +, minutes at holding speed at #,!! ft ( +,! m  abo8e aerodrome ele8ation ele8ation in standard standard c) conditions. fuel to flD for %! minutes at holding speed at #,!! ft ( +,! m  abo8e aerodrome ele8ation ele8ation in standard standard d) conditions.

Answer ; b)

fuel to flD for "! minutes at holding speed at #,!! ft ( +,! m  abo8e aerodrome ele8ation in standard conditions. -----------------------------------------------------------------------------------------------------------------------------------------------------------------


#6&


418.

( For this this question use anne !""-6,+"A or Flight 'lanning anual )*T # Figure +.+ 

Annex 033-9543A 033-9543A The final reser8e fuel ta4en from the 2709= '7A9909= table for the twin Get aeroplane is based on the following parameters ; a) pressure altitude @ aeroplane mass and flaps up with minimum drag airspeed. pressure altitude @ aeroplane mass and flaps down with maimum range speed. b) pressure altitude @ aeroplane mass and flaps up with maimum range speed. c) pressure altitude @ aeroplane mass and flaps down with minimum drag airspeed. d) Answer ; a)

pressure altitude @ aeroplane mass and flaps up with minimum drag airspeed. ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use )oute anual chart >(20+ CAA->dition  419. The first ( lowest  a8ailable flight le8el for flight on airwaD ?=# from >)7A9=>9 >)7 ##+.6 ( +6B"6BP9 !##B!6P>  to F)A9/F?)T F)A9/F?)T FF ##+.$ ##+.$ ( ,!B!"P9 !!5B"5P>  is ; F7"$! a) F7"!! b) c) F7$6! F7"#! d)

Answer ; b)

F7"!! ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use )oute anual chart >(20+ CAA->dition  420. The first ( lowest  a8ailable flight le8el for flight on airwaD ?=, from >9>-9A1H09A71 >9 ##,." ( ++B"%P9 !!"B#!P>  to =A077AC =A0 ##,.5 ( +"B,&P9 !!#B,!P>  is ; F7$6! a) F7"!! b) F7$5! c) F7"#! d)

Answer ; a)

F7$6! -----------------------------------------------------------------------------------------------------------------------------------------------------------------


#65


421.

( For this question use anne !""-##$"6A and !"#-##$"6H 

Annexe 033-112 033-11239A 39A  031-11239! 031-11239! The flight crew of a turboGet aeroplane prepares a flight using the following data ; Flight leg distance I " ,!! 9 Flight le8el F7 "#! @ true airspeed I +,! 4t 2eadwind component at this le8el I ,, 4t 0nitiallD planned ta4e-off mass ( without etra fuel on board  I #5! !!! 4g Fuel price I !."! l at departure The commander maD carrD a fuel quantitD of 5 !!! 4g in addition to that which is necessarD. For this fuel transport operation to be cost effecti8e@ the maimum fuel price at arri8al must be ; !.$5 l a) !.$& l b) !.$% l c) !."" l d) Answer ; b)

!.$& l -----------------------------------------------------------------------------------------------------------------------------------------------------------------


#66


422.

( For this question use anne !""-##$"6A and !"#-##$"6H 

Annexe 033-112 033-11239A 39A  031-11239! 031-11239! The flight crew of a turboGet aeroplane prepares a flight using the following data ; Flight leg distance I " ,!! 9 Flight le8el F7 "#! @ true airspeed I +,! 4t 2eadwind component at this le8el I ,, 4t 0nitiallD planned ta4e-off mass ( without etra fuel on board  I #5! !!! 4g Fuel price I !.$& l at destination The commander maD carrD on board 5 !!! 4g more fuel than that which is necessarD. For this fuel transport operation to be cost effecti8e @ the maimum fuel price at departure must be ; !.$5 l a) !."! l b) !.$6 l c) !.$+ l d) Answer ; b)

!."! l -----------------------------------------------------------------------------------------------------------------------------------------------------------------


$!!


423.

( For this question use anne !""-##$+#A 

Annex 033-11241A 033-11241A The flight crew of a turboGet aeroplane prepares a flight using the following data ; Flight le8el F7 "&! at “7ong )ange” ( 7)  cruise regime ass at bra4e release I $#$ 5!! 4g Flight leg ground distance I $ ,!! 9 Temperatures Temperatures I 01A C= I "& 2eadwind component I "! 4t “Total “Total anti-ice” set on “9” for the entire flight 9o requested climb and descent descent correction of the fuel consumption The fuel consumption ( from ta4e-off to landing  is ; "+ +"! 4g a) "! ++! 4g b) "$ +5! 4g c) $5 &$! 4g d) Answer ; a)

"+ +"! 4g


$!#


----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use annees !""-##$!+A @ !""-##$!+H and !""-##$!+C 

424.

The flight crew of a turboGet aeroplane prepares a flight using the following data ; Flight leg ground distance I + !!! 9 Flight le8el F7 "&! I “7ong range” flight regime >ffecti8e wind at this le8el I head wind of ,! 4t Temperature I 01A Centre of gra8itD ( C=  I "&  'ac4 flow I 7< ( 7  Anti ice I FF )eference landing mass I #+! !!! 4g Tai Tai fuel I ,!! 4g Annexe 033-11 033-11204A 204A  033-11204! 033-11204!  033-11204/ 033-11204/ Final reser8e fuel I $ +!! 4g The fuel quantitD which must be loaded on board the aircraft is ; ,# 5%! 4g a) +# 6,! 4g b) ,$ !%! 4g c) +% "+! 4g d) Answer ; a)

,# 5%! 4g


$!$


----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use anne !""-##$"5A 

425.

Annex 033-1123"A 033-1123"A The flight crew of a turboGet aeroplane prepares a flight using the following data ; Flight le8el F7 "&! at “7ong )ange” ( 7)  cruise regime ( 'rescribed  mass at bra4e release I $!+ ,!! 4g Flight leg ground distance I $ !!! 9 Temperatures Temperatures I 01A 2eadwind component I &! 4t “Total “Total anti-ice” set on “9” for the entire flight 9o requested climb and descent descent correction of the fuel consumption The fuel required from ta4e-off to landing is ; $& &&! 4g a) $$ #%! 4g b) $! 6!! 4g c) $6 ++! 4g d) Answer ; d)

$6 ++! 4g


$!"


----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use anne !""-##$&$A 

426.

Annex 033-11272A 033-11272A The flight crew of a turboGet aeroplane prepares a flight using the following data ; Ta4e-off Ta4e-off mass I #%5 ,!! 4g Flight leg ground distance I $ !!! 9 Flight le8el F7 "&! @ “7ong )ange” flight regime Tailwind Tailwind component at this le8el I "! 4t Total Total anti-ice set on “9” Fied tai fuel I ,!! 4g @ final reser8e I $ !!! 4g 0gnore alternate fuel. The effects of climb and descent are not corrected for consumption. The prescribed quantitD of trip fuel for the flight leg is ; $" !!! 4g a) $" "!! 4g b) $! ,!! 4g c) $$ ,!! 4g d) Answer ; c)

$! ,!! 4g


$!+


----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use anne !""-##$&#A 

427.

Annex 033-11271A 033-11271A The flight crew of a turboGet aeroplane prepares a flight using the following data ; Ta4e-off Ta4e-off mass I $#! ,!! 4g Flight leg ground distance I $ ,!! 9 Flight le8el F7 ""! @ “7ong )ange” flight regime Tailwind Tailwind component at this le8el I &! 4t Total Total anti-ice set on “9” Fied tai fuel I ,!! 4g @ final reser8e I $ +!! 4g 0gnore alternate fuel. The effects of climb and descent are not corrected for consumption. The quantitD of fuel that must be loaded at the par4ing area is ; "! $!! 4g a) "6 &,! 4g b) "# 5+! 4g c) "# "+! 4g d) Answer ; c)

"# 5+! 4g


$!,


-----------------------------------------------------------------------------------------------------------------------------------------------------------------

428.

( For this question use anne !""-##$+,A and !""-##$+,H 

Annex 033-11245A 033-11245A  033-11245! 033-11245! The flight crew of a turboGet aeroplane prepares a flight using the following data ; Flight leg air distance I $ &!! 9 Flight le8el F7 "#! @ true airspeed I +&! 4t Tailwind Tailwind component at this le8el I ", 4t 0nitiallD planned ta4e-off mass ( without etra fuel on board  I #5! !!! 4g Fuel price I !.$5 >urol at departure @ !.$% >urol at destination To maimiMe sa8ings @ the commander chooses to carrD etra fuel in addition to that which is necessarD. The optimum quantitD of fuel which should be carried in addition to the prescribed quantitD is ; The fuel transport operation is not recommended in this case. a) % !!! 4g. b) c) #! !!! 4g. + !!! 4g. d) Answer ; a)

The fuel transport operation is not recommended in this case. -----------------------------------------------------------------------------------------------------------------------------------------------------------------


$!%


429.


Annex 033-11245A 033-11245A  033-11245! 033-11245! The flight crew of a turboGet aeroplane prepares a flight using the following data ; Flight leg air distance I $ &!! 9 Flight le8el F7 "#! @ true airspeed I +&! 4t Tailwind Tailwind component at this le8el I ", 4t 0nitiallD planned ta4e-off mass ( without etra fuel on board  I #6, !!! 4g Fuel price I !.$5 >urol at departure @ !.$% >urol at destination To maimiMe sa8ings @ the commander chooses to carrD etra fuel in addition to that which is necessarD. The optimum quantitD of fuel which should be carried in addition to the prescribed quantitD is ; , !!! 4g. a) b) #! !!! 4g. 5 !!! 4g. c) The fuel transport operation is not recommended in this case. d) Answer ; d)



$!&


430.

( For this question use Anne !""-##$+,A and !""-##$+,H 

Annex 033-11245A 033-11245A  033-11245! 033-11245! The flight crew of a turboGet aeroplane prepares a flight using the following data ; Flight leg distance I " ,!! 9 Flight le8el F7 "#! @ true airspeed I +,! 4t 2eadwind component at this le8el I -,, 4t 0nitiallD planned ta4e-off mass ( without etra fuel on board  I #5! !!! 4g Fuel price I !."! >urol at departure @ !.$& >urol at destination To maimiMe sa8ings @ the commander chooses to carrD etra fuel in addition to that which is necessarD. ?sing the appended anne @ the optimum quantitD of fuel which should be carried in addition to the prescribed quantitD is ; a) The fuel transport operation is not recommended in this case. $$ !!! 4g. b) #, !!! 4g. c) 5 !!! 4g. d) Answer ; a)



$!5


431.

( For this question use Anne !""-##$+,A and !""-##$+,H 

Annex 033-11245A 033-11245A  033-11245! 033-11245! The flight crew of a turboGet aeroplane prepares a flight using the following data ; Flight leg distance I " ,!! 9 Flight le8el F7 "#! @ true airspeed I +,! 4t 2eadwind component at this le8el I , 4t 0nitiallD planned ta4e-off mass ( without etra fuel on board  I #5! !!! 4g Fuel price I !.", ?1 ollarsl at departure @ !."#, ?1 ollarsl at destination To maimiMe sa8ings @ the commander chooses to carrD etra fuel in addition to that which is necessarD. ?sing the appended anne @ the optimum quantitD of fuel which should be carried in addition to the prescribed quantitD is ; The fuel transport operation is not recommended in this case. a) $$ !!! 4g. b) c) #, !!! 4g. 5 !!! 4g. d) Answer ; a)



$!6


432.


Annex 033-11245A 033-11245A  033-11245! 033-11245! The flight crew of a turboGet aeroplane prepares a flight using the following data ; Flight leg distance I + !!! 9 Flight le8el F7 "#! @ true airspeed I +,! 4t 2eadwind component at this le8el I ,! 4t 0nitiallD planned ta4e-off mass ( without etra fuel on board  I #&! !!! 4g Fuel price I !.$& >urol at departure @ !."! >urol at destination To maimiMe sa8ings @ the commander chooses to carrD etra fuel in addition to that which is necessarD. ?sing the appended anne @ the optimum quantitD of fuel which should be carried in addition to the prescribed quantitD is ; #5 !!! 4g. a) 5 !!! 4g. b) c) The fuel transport operation is not recommended in this case. "$ !!! 4g. d) Answer ; b)

5 !!! 4g. -----------------------------------------------------------------------------------------------------------------------------------------------------------------


$#!


433.


Annex 033-11245A 033-11245A  033-11245! 033-11245! The flight crew of a turboGet aeroplane prepares a flight using the following data ; Flight leg distance I " ,!! 9 Flight le8el F7 "#! @ true airspeed I +,! 4t 2eadwind component at this le8el I - ,, 4t 0nitiallD planned ta4e-off mass ( without etra fuel on board  I #5! !!! 4g Fuel price I !."! >urol at departure @ !.$& >urol at destination To maimiMe sa8ings @ the commander decides to carrD etra fuel in addition to that which is necessarD. ?sing the appended anne @ the optimum quantitD of fuel which should be carried in addition to the prescribed quantitD is ; a) #, !!! 4g $$ !!! 4g b) The fuel transport operation is not recommended in this case. c) 5 !!! 4g d) Answer ; c)



$##


434.

( For this this question use anne !""-#$",!A or Flight 'lanning anual )*T # Figure +."., +."., 

Annex 033-12350A 033-12350A The following applD ; Tail Tail wind component #! 4t Temperature Temperature 01A E#!BC Hra4e release mass %"!!! 4g Trip fuel a8ailable $!!!! 4g
"&+! 9


$#$


----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use anne !""-#$"+5A or Flight 'lanning anual )*T # Figure +."., 

435.

Annex 033-1234"A 033-1234"A The following applD ; Temperature Temperature 01A E#,BC Hra4e release mass %$!!! 4g Trip time , hr $! min
#",!! 4g


$#"


-----------------------------------------------------------------------------------------------------------------------------------------------------------------

436.

The following fuel consumption figures are gi8en for a Get aeroplane 1tandard tai fuel I %!! 4g. A8erage A8erage cruise consumption I #! !!! 4gh. 2olding fuel consumption at #,!! ft abo8e alternate airfield ele8ation I 5!!! 4gh. Flight time from departure to destination I % hours Fuel for di8ersion to alternate I #! $!! 4g. The minimum ramp fuel load is ; &6 5!! 4g. a) b) && $!! 4g. &+ 5!! 4g. c) && 5!! 4g. d)

Answer ; d)

&& 5!! 4g. ----------------------------------------------------------------------------------------------------------------------------------------------------------------437. ( For this question use anne !""-#$""!A 

Annex 033-12330A 033-12330A The forecast period co8ered bD the 'A)01C2A)7>1->-=A?77> 'A)01C2A)7>1->-=A?77> TAFs TAFs totals ( hours  ; $& a) $! b) c) #5 6 d) Answer ; a)

$& -----------------------------------------------------------------------------------------------------------------------------------------------------------------


$#+


438.

( For this question question use anne !""- ##!%&A ##!%&A or )oute anual chart ?90C2 ?90C2 9H > )wD $%7 approach (#%-" 

Annex 033-11067A 033-11067A The frequencD and identifier of the 9H for the published approaches are ; ##$." ?9 a) +!! 1< b) ""5 9< c) #!5.% 1 d) Answer ; b)

+!! 1<


$#,


-----------------------------------------------------------------------------------------------------------------------------------------------------------------

439.

The fuel burn of an aircraft turbine engine is $$! lh with a fuel densitD of !.5! .0f the densitD is !.&, @ the fuel burn will beI a) $!% lh #&% lh b) $$! lh c) $", lh d)

Answer ; d)

$", lh ----------------------------------------------------------------------------------------------------------------------------------------------------------------The fuel burn off is $!! 4gh with a relati8e fuel densitD of !.5 .0f the relati8e densitD is !.&, @ the fuel burn will be ; 440. #55 4gh a) $%& 4gh b) $#" 4gh c) $!! 4gh d)

Answer ; d)

$!! 4gh ----------------------------------------------------------------------------------------------------------------------------------------------------------------The fuel plan gi8es a trip fuel of %, ?1 gallons. The alternate fuel @ final reser8e included @ is #& ?1 gallons. ContingencD 441. fuel is , of the trip fuel. The usable fuel at departure is 6" ?1 gallons. At a certain moment the fuel consumed according to the fuel gauges is +! ?1 gallons and the distance flown is half of the total distance. Assume that fuel consumption doesnLt change.
The remaining fuel is not sufficient to reach the destination with reser8es intact. ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use )oute anual chart >(20$  442. The identifier of the radio na8igation aid at ( ,%B!%P9 !#$B#,P>  is ; 9)A a) 9A b) c) 1:!+
Answer ; b)

9A ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use )oute anual chart >(20$  443. The identifier of the radio na8igation aid at ( ,%B!&P9 !#$B,5P>  is ; A) a) 1:!" b) 1: c) A1T) d)

Answer ; a)

A) -----------------------------------------------------------------------------------------------------------------------------------------------------------------


$#%


444.

( For this question use anne anne !""- ##!%+A ##!%+A or )oute )oute anual anual chart ?90C2 ?90C2 071 )wD $%) (##-+ 

Annex 033-11064A 033-11064A The 071 frequencD and identifier are ; #!5." 09< a) #!5.& 01< b) #!5." 01< c) #!5.& 09< d) Answer ; d)

#!5.& 09<


$#&


----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question question use anne !""- ##!%,A ##!%,A or )oute anual chart 'A)01 'A)01 C2A)7>1 > > =A?77> =A?77> 071 )wD #! ($#-5 

445.

Annex 033-11065A 033-11065A The 071 localiMer course is ; !55B a) ##5B b) $%5B c) #!!B d) Answer ; a)

!55B


$#5


-----------------------------------------------------------------------------------------------------------------------------------------------------------------

( For this this question use anne !""-#$",%A or )oute anual chart , AT(20  The initial great circle course from position A ( 5!B!!P9 #&!B!!P>  to position H ( &,B!!P9 !##B>  is #&&B ( = . The final grid course at position H will be ; #&$B ( =  a) b) ","B ( =  #&&B ( =  c) #6+B ( =  d)

446.

Answer ; c)

#&&B ( =  ----------------------------------------------------------------------------------------------------------------------------------------------------------------447. ( For this this question use anne !""-#$",,A or )oute anual chart , AT(20  The initial great circle true course from /efla8i4 ( %+B!!P9 !$$B"%P <  to :igra ( %$B""P9 !!%B!$P>  measures !5+B. n a polar enroute chart where the grid is aligned aligned with the !!!B meridian the initial grid course will be ; #!%B a) !5!B b) !%%B c) d) !6%B Answer ; a)

#!%B ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use anne !""- #!66%A or )oute anual chart >(7,  448. The initial magnetic coursedistance from >>7> >>7 ##$.+ ( ,"B#!P9 !!%B+!P>  to <>7= ( ,+B#5P9 !!&B$,P>  on airwaD A& is ; !$"B +& 9 a) !$"B #,& 9 b) !$+B $! 9 c) !$+B &" 9 d) Answer ; d)

!$+B &" 9 ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use anne !""-#$"&,A or )oute anual chart 9A'  449. The initial magnetic course from A ( %+B9 !!%B>  to C ( %$B9 !$!B<  is ; $&,B a) $%&B b) c) $%$B $&#B d)

Answer ; a)

$&,B ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use anne !""-#$"&!A or )oute anual chart 9A'  450. The initial magnetic course from C ( %$B9 !$!B<  to H ( ,5B9 !!+B>  is ; ##"B a) !5!B b) !65B c) ##%B d)

Answer ; d)

##%B ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use )oute anual chart >(20#  451. The initial magnetic course from 09:>)9>11 #!6.$ 091 ( ,&B"$P9! !+B!"P<  direct to T0)>> ##&.& T0) ( ,%B"!P9 !!%B,"P<  is ; $"!B a) $#5B b) $++B c) $"&B d) Answer ; c)

$++B -----------------------------------------------------------------------------------------------------------------------------------------------------------------


$#6


( For this question use )oute anual chart >(20#  The initial magnetic course from T0)>> ##&.& T0) ( ,%B"!P9 !!%B,"P<  direct to 09:>)9>11 #!6.$ 091 ( ,&B"$P9 !!+B!"P<  is ; $"% a) b) !%+ !+5 c) !,% d) 452.

Answer ; b)

!%+ ----------------------------------------------------------------------------------------------------------------------------------------------------------------453. ( For this question use )oute anual chart >(20#  The initial magnetic course from T0)>> ##&.& T0) ( ,%B"!P9 !!%B,"P<  direct to 1T)9
!#6 ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use anne !""-#$"&%A or )oute anual chart 9A'  454. The initial true course from A ( %+B9 !!%B>  to C ( %$B9 !$!B<  is ; a) $&#B $+%B b) $&,B c) $%&B d)

Answer ; a)

$&#B ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use anne !""-#$"&#A or )oute anual chart 9A'  455. The initial true course from C ( %$B9 !$!B<  to H ( ,5B9 !!+B>  is ; $&5B a) ##%B b) !65B c) d) !5!B

Answer ; c)

!65B ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use )oute anual chart >(20#  456. The initial true course from 09:>)9>11 #!6.$ 091 ( ,&B"$P9 !!+B!"P<  direct to T0)>> ##&.& T0) ( ,%B"!P9 !!%B,"P<  is ; $#5B a) $"!B b) $++B c) $"&B d)

Answer ; d)

$"&B ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use )oute anual chart >(20#  457. The initial true course from T0)>> ##&.& T0) ( ,%B"!P9 !!%B,"P<  direct to 09:>)9>11 #!6.$ 091 ( ,&B"$P9 !!+B!"P<  is ; !,+B a) !+5B b) $"%B c) !%$B d)

Answer ; a)

!,+B -----------------------------------------------------------------------------------------------------------------------------------------------------------------


$$!


458.

( For this question use )oute anual chart >(20#  The initial true course from T0)>> ##&.& T0) ( ,%B"!P9 !!%B,"P<  direct to 1T)9
 is ; a) b) c) d)

!#6B !!"B !##B #6$B

Answer ; c)

!##B ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use anne !""-#$""#A  459.

Annex 033-12331A 033-12331A The lowest cloud conditions ( o4tasft  at H)>A?R>)0=9AC at #""! ?TC were ; # to $ at "!!! a) " to + at $!!! b) " to + at 5!! c) # to + at "!!! d) Answer ; a)

# to $ at "!!! -----------------------------------------------------------------------------------------------------------------------------------------------------------------


$$#


460.

( For this question use anne anne !""- ##!%%A ##!%%A or )oute )oute anual anual chart N?)0C2 N?)0C2 071 071 )wD #% (##-$ (##-$ 

Annex 033-11066A 033-11066A The lowest published authorised ):) for an 071 approach glide slope out @ all other aids ser8iceable @ aircraft categorD A is ; &$!m a) 5!!m b) #,!!m c) %!!m d) Answer ; a)

&$!m


$$$


-----------------------------------------------------------------------------------------------------------------------------------------------------------------

461.

( For this question use anne !""- #!66&A or )oute anual chart >(7$  The magnetic coursedistance from CAH)A0 CH ##$.% ( ,!B#+P9 !!"B!6P>  to TA7?9 ( +6B""P9 !!"B$,P>  on airwaD

H" is ; a) b) c) d)

"+6B  $% 9 #%6B  %5 9 #%6B  +$ 9 "+6B  +$ 9

Answer ; c)

#%6B  +$ 9 ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use )oute anual chart >(7#  462. The magnetic coursedistance from >A9 C)11 ##,.$ C1 ( ,+B+"P9 !!"B$!P 2077 ##$.# '7 ( ,"B+,P9 !!$B!%P<  on airwaD A$ is ; #+6  &" 9 a) #,,  &" 9 b) "$6  ," 9 c) #+"  ," 9 d)

Answer ; a)

#+6  &" 9 ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use anne !""- #!66"A or )oute anual chart >(20+ CAA->dition  463. The magnetic coursedistance from 09/>71H?27 /H ##&.5 ( +6B!6P9 !#!B#+P>  to >)7A9=>9 >)7 ##+.6 ( +6B"6P9 !##B!6P>  on airwaD ?)## is ; a) !,!B  +& 9 $"!B  6&9 b) !,$B  6& 9 c) #""B  5, 9 d)

Answer ; a)

!,!B  +& 9 ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use anne !""- ##!!"A or )oute anual chart >(20, CAA->dition  464. The magnetic coursedistance from >7HA >7H ##+.& ( +$B++P9 !#!B$+P>  to 1'>N0 ( +"B+6P9 !!6B"+P>  on airwaD ?A", is ; ""$B  &% 9 a) ""$B  ##5 9 b) c) "$$B  %! 9 #,$B  +$ 9 d)

Answer ; a)

""$B  &% 9 ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use anne !""- #!66,A or )oute anual chart >(7,  465. The magnetic coursedistance from >7H> 7H> ##,.# ( ,"B"6P9 !!6B"%P>  to 7?9? ( ,+B,!P9 !!6B#6P>  on airwaD 2#$ is ; ",$B  &$ 9 a) ""6B  5! 9 b) ""6B  #$, 9 c) ",$B  6% 9 d)

Answer ; a)

",$B  &$ 9 ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use anne !""- #!66+A or )oute anual chart >(7%  466. The magnetic coursedistance from =)1T>9J?09 =TJ ###.$, ###.$, ( +6B!!P9 !!%B+"P>  to 7099A ( +6B+#P9 !!%B#,P>  on airwaD )& is ; #,&B  ,5 9 a) ""&B  +% 9 b) ""&B  ,5 9 c) ""&B  "# 9 d) Answer ; b)

""&B  +% 9 -----------------------------------------------------------------------------------------------------------------------------------------------------------------


$$"


( For this question use anne !""- ##!!+A or )oute anual chart >(20, CAA->dition  The magnetic coursedistance from 70=>1 7= ##+., ( +,B+6P9 !!#B!$P>  to C7>)9T F>))A9 CF ##&., ( +,B+&P9 !!"B##P>  on airwaD ?=$$ is ; !+%B  &! 9 a) ##"B  #+$ 9 b) c) !%&B  #$$ 9 !6+B  6! 9 d)

467.

Answer ; d)

!6+B  6! 9 ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use )oute anual chart >(7#  468. The magnetic coursedistance from '7> 2077 ##$.# '7 ( ,"B++P9 !!$B!%P< to TA77A TA77A ##".5 T7A ( ,,B"!P9 !!"B$#P<  on airwaD H+ is ; "+"  ##+ 9 a) ""&  ##+ 9 b) #,&  #!% 9 c) #%"  #!% 9 d)

Answer ; a)

"+"  ##+ 9 ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use anne !""- ##!!$A or )oute anual chart >(20+ CAA->dition  469. The magnetic coursedistance from 1A7NH?)= 1H= ##".5 ( +5B!!P9 !#$B,+P>  to 1TA?H 1TA?H ( +5B++P9 !#$B"5P>  on airwaD ?H, is ; a) "+%B  +" 9 #%%B  %+ 9 b) "+%B  +, 9 c) "+%B  %+ 9 d) Answer ; c)

"+%B  +, 9 ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use anne !""- ##!!#A or )oute anual chart >(20+ CAA->dition  470. The magnetic coursedistance from 1T ')>R 1') ##".6 ( +%B$5P9 !!%B$&P>  to F)0H?)= F)0 ##,.# ( +%B+&P9 !!&B#+P>  on airwaD ?=%! is ; !+5B  +% 9 a) !+#B  &5 9 b) c) !%#B  $5 9 !%#B  "& 9 d)

Answer ; d)

!%#B  "& 9 ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use )oute anual chart >(7#  471. The magnetic coursedistance from TA77A ##".5 T7A ( ,,B"!P9 !!"B$#P<  to >A9 C)11 ##,.$ C1 ( ,+B+"P9 !!"B$!P<  on airwaD A$ is ; #5,B  #5 9 a) !!,B  #5 9 b) #5,B  +& 9 c) !!,B  +& 9 d)

Answer ; c)

#5,B  +& 9 ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use anne !""- ##!!!A or )oute anual chart >(20+ CAA->dition  472. The magnetic coursedistance from TA9= T= ##$., ##$., ( +5B"&P9 !!6B#%P>  to 09/>71H?27 /H ##&.5 ( +6B!6P9 !#!B#+>  on airwaD ?)## is ; #"$B  +" 9 a) #!,B  #!, 9 b) !,$B  ,! 9 c) !!&B  %! 9 d)

Answer ; c)

!,$B  ,! 9 -----------------------------------------------------------------------------------------------------------------------------------------------------------------


$$+


( For this question use anne !""- #!666A or )oute anual chart >(20+ CAA->dition  The magnetic coursedistance from T)>9T T9T ##,.& ( ,"B!"P9 !!#B+!P<  to O O
473.

Answer ; b)

$6&B  ,& 9 ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use Anne !""- #!665A or )oute anual chart >(7#  474. The magnetic coursedistance from O O
$&6B  5, 9 ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use )oute anual chart >(7#  475. The magnetic course from >A9 C)11 ##,.$ C1 ( ,+B+"P9 !!"B$!P ##+.$, 9>< ( ,,B!$P9 !!#B+#P<  on airwaD <6## is ; !5" a) $%" b) c) !&& $,& d)

Answer ; c)

!&& ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use T) @ Harcelona Area chart (#!-#:  476. The maimum altitude that maD be used to transit the whole :F) corridor from )>?1 to 1A9 C>790 is ; $!!! ft a) +,!! ft b) "!!! ft c) ",!! ft d)

Answer ; a)

$!!! ft ----------------------------------------------------------------------------------------------------------------------------------------------------------------The maimum permissible ta4e-off mass of an aircraft for the 7 wa4e turbulence categorD on an ATC ATC flight plan is ; 477. $ &!! 4g a) & !!! 4g b) , &!! 4g c) d) #! !!! 4g

Answer ; b)

& !!! 4g -----------------------------------------------------------------------------------------------------------------------------------------------------------------


$$,


478.


Annex 033-12320A 033-12320A The maimum wind 8elocitD ( B 4t  immediatelD north of T?901 ( "%B9 !#!B>  is ; $,!5, a) $5!##! b) #5!#!, c) #6!6, d) Answer ; d)

#6!6, -----------------------------------------------------------------------------------------------------------------------------------------------------------------


$


479.

( For this question use anne !""-###5#A !""-###5#A 

The maimum wind 8elocitD ( B "!!#!! a) b) "!!#%! "!!#+! c) $6!##! d)

Annex 033-11 033-111"1A 4t  shown in the 8icinitD of ?90C2 ( +5B9 !#$B>  is is ;

Answer ; c)

"!!#+! -----------------------------------------------------------------------------------------------------------------------------------------------------------------


$$&


480.

( For this question question use anne !""- ##!%$A ##!%$A or )oute anual chart 799 799 2>AT2) 2>AT2)< < 071 071 > )wD !6) (##-# 

Annex 033-11062A 033-11062A The inimum escent Altitude ( A  for an 071 glide slope out @ is ; +5! ft a) +!, ft b) $&, ft c) $!! ft d) Answer ; a)

+5! ft -----------------------------------------------------------------------------------------------------------------------------------------------------------------


$$5


( For this question use anne !""-##!$"A or )oute anual chart >(20, CAA->dition  The minimum enroute altitude a8ailable on airwaD ?)#%! from 90C> 9 0C> 90N ##$.+ ( +"B+%P9 !!&B#,P>  to HA1T0A HTA ##%.$ ( +$B"$P9 !!6B$6P>  is ; F7$%! a) F7$#! b) c) F7$,! F7$!! d)

481.

Answer ; c)

F7$,! ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use )oute anual chart >(7#  482. The minimum enroute altitude ( >A  that can be maintained continuouslD on ad8isorD route <6## from 9> ##+.$, 9>< ( ,,B!$P9 !!#B$+P<  to >A9 C)11 ##,.$ C1 ( ,+B+"P9 !!"B$!P<  is ; +&!! ft a) F7#,! b) +,$! ft c) F7,! d)

Answer ; d)

F7,! ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use )oute anual chart >(7#  483. The minimum enroute altitude ( >A  that can be maintained continuouslD on airwaD H$$% from TA77A ##".5 ##".5 T7A ( ,,B"! 9!!"B$#P<  to reporting point A9=?1 ( ,%B+$P9!!"B!"P<  is ; a) ,!!! ft F75! b) F7&! c) ,,!! ft d) Answer ; c)

F7&! ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use anne !""- ##!$&A or )oute anual chart >(7$  484. The minimum enroute altitude ( >A  that can be maintained continuouslD on airwaD =+ from *>)1>O *1O ##$.$ ##$.$ ( +6B#"P9 !!$B!"P<  to 70NA ( +6B",P9 !!+B$!P<  is ; $5!! ft 17 a) #!!! ft 17 b) c) F7%! F7#+! d)

Answer ; d)

F7#+! ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use )oute anual chart >(7#  485. The minimum enroute altitude ( >A  that can be maintained continuouslD on airwaD 7%!$ from TA77A TA77A ##".5 ##".5 T7A ( ,,B"!9 !!"B$#P<  to 9> ##+.$, 9>< ( ,,B!$P9!!#B$+P<  is ; F7$!! a) "6!! ft b) "#!! ft c) F7#!! d) Answer ; a)

F7$!! ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use )oute anual chart >(7,  486. The minimum enroute altitude that can be maintained continuouslD on airwaD H%,2%, from R9 ( ,,B$&P9 !#5B#!P>  to )99> )> ##$.! ##$.! ( ,,B!+P9 !#+B+%P> !#+B+%P>  is ; #!!! ft a) F7%! b) F7#!! c) $,!! ft d) Answer ; c)

F7#!! -----------------------------------------------------------------------------------------------------------------------------------------------------------------


$$6


( For this question use anne !""- ##!$,A or )oute anual chart >(7#  The minimum enroute altitude that can be maintained continuouslD on airwaD =# from 1T)?H7> 1T? ##".# ( ,$B!!P9 !!,B!$P<  to H)>C9 HC9 ##&.+, ( ,#B+"P9 !!"B#%P<  is ; a) +#!!ft 17 F75! b) F7##! c) $6!! ft 17 d)

487.

Answer ; c)

F7##! ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use anne !""-##!$6A or )oute anual chart >(7,  488. The minimum enroute altitude that can be maintained continuouslD on airwaD =$+ from /7*A ( ,%B !!P9 !#%B+6P>  to )99> )> ##$.! ( ,,B!+P9 !#+B+%P>  is ; F7#!! a) #!!!ft b) c) $,!! ft F7%! d)

Answer ; a)

F7#!! ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use anne !""- ##!$+A or )oute anual chart >(20+ CAA->dition  489. The minimum enroute altitude that can be maintained continuouslD on airwaD ?A"+ from O A77A1>O
F7$6! -----------------------------------------------------------------------------------------------------------------------------------------------------------------


$"!


490.

( For this question question use anne !""- ##!%!A ##!%!A or )oute anual chart A)0 A)0 HA)A*A1 HA)A*A1 071 071 > )wD "" (##-# 

Annex 033-11060A 033-11060A The minimum glide slope interception altitude for a full 071 is ; ",!! ft a) +!!! ft b) $!%& ft c) #,%& ft d) Answer ; b)

+!!! ft -----------------------------------------------------------------------------------------------------------------------------------------------------------------


$"#


491.

( For this question question use anne !""- ##!+$A ##!+$A or )oute anual 1TA) 1TA) chart for 799 2>AT2)< 2>AT2)< (#!-$ 

Annex 033-11042A 033-11042A The minimum holding altitude ( 2A  and maimum holding speed ( 0A1  at 2A at C/2A C/ ##,." are ; 6!!!ft and $,!4t a) &!!!ft and $,!4t b) &!!! ft and $$!4t c) 6!!!ft and $$!4t d) Answer ; c)

&!!! ft and $$!4t -----------------------------------------------------------------------------------------------------------------------------------------------------------------


$"$


492.

( For this question question use anne !""- ##!,6A ##!,6A or )oute anual chart A1T>)A 1C20'27 071 > )wD $$ (##-% 

Annex 033-11059A 033-11059A The issed Approach procedure is to climb to an altitude of (i .................... on a trac4 of (ii ..................... (i "!!! ft @ (ii #%!B a) (i $!! ft @ (ii $$"B b) (i "!!! ft @ (ii $$"B c) (i $!!! ft @ (ii #%!B d) Answer ; d)

(i $!!! ft @ (ii #%!B -----------------------------------------------------------------------------------------------------------------------------------------------------------------


$""


493.

The na8igation plan reads ; Trip fuel I #!! 4g Flight time I # h ", min Tai fuel I " 4g Hloc4 fuel I #5# 4g The endurance on the 0CA flight plan should read ; $ h !+ min a) # h ", min b) c) $ h +6 min $ h ,$ min d)

Answer ; c)

$ h +6 min ----------------------------------------------------------------------------------------------------------------------------------------------------------------The na8igation plan reads ; 494. Trip fuel I #"% 4g Flight time I $ h +, min Calculated reser8e fuel I "! of trip fuel Fuel in tan4 is minimum ( no etra fuel on board  Tai fuel I " 4g The endurance on the 0CA flight plan should read ; a) " h "5 min " h "+ min b) $ h +6 min c) $ h +, min d)

Answer ; b)

" h "+ min ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use anne !""- ##!#,A or )oute anual chart >(7,  495. The 9H at >9/ ( ,$B+6P9 !#,B,!P>  can be identified on ; Channel ++! @ HF off a) FrequencD ++! 42M @ HF off b) FrequencD ++! 42M @ HF on c) d) Channel ++! @ HF on

Answer ; c)

FrequencD ++! 42M @ HF on ----------------------------------------------------------------------------------------------------------------------------------------------------------------The planned departure time from the par4ing area is #5#, ?TC. The estimated ta4e-off time is #5$, ?TC. The flight plan 496. must be filed with ATC at the latest at ; a) #&,, ?TC #&$, ?TC b) #&#, ?TC c) #&+, ?TC d)

Answer ; c)

#&#, ?TC ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use anne !""-##&#&A  497.

Annex 033-11717A 033-11717A The planned flight is o8er a distance of ++! 9. Hased on the wind charts at altitude the following components are found ; F7,! I -"! 4t @ F7#!! I -,! 4t @ F7#5! I -&! 4t The perations anual in appendi details the aircraftLs performances. ither F7 !,! or F7 #!! a) F7 #5! b) F7 !,! c) F7 #!! d) Answer ; b)

F7 #5!


$"+


-----------------------------------------------------------------------------------------------------------------------------------------------------------------

498.

The purpose of the decision point procedure is ; to increase the safetD of the flight. a) to reduce the landing weight and thus reduce the structural stress on the aircraft. b) to reduce the minimum required fuel and therefore be able to increase the traffic load. c) to increase the amount of etra fuel. d)

Answer ; c)

to reduce the minimum required fuel and therefore be able to increase the traffic load. ----------------------------------------------------------------------------------------------------------------------------------------------------------------The quantitD of fuel which is calculated to be necessarD for a Get aeroplane to flD 0F) from departure aerodrome to the 499. destination aerodrome is ,",$ 4g. Fuel consumption in holding mode is %!!! 4gh. Alternate fuel is +"5! 4g. ContingencD should be , of trip fuel.
Answer ; c)

#"!!! 4g. -----------------------------------------------------------------------------------------------------------------------------------------------------------------


$",


500.

( For this question use anne anne !""- ##!%#A ##!%#A or )oute )oute anual anual chart A1T>)A *AA 090?1 (#!- 

Annex 033-11061A 033-11061A The )adio Altimeter minimum altitude for a CAT CAT $ 071 > approach to )wD !#7 is ; "!! ft a) #!! ft b) #55 ft c) 55 ft d) Answer ; b)

#!! ft


$"%


----------------------------------------------------------------------------------------------------------------------------------------------------------------501.

( For this question use )oute anual chart >(20$  The radio na8igation aid at ( ,&B+,P9 !#"B+5P>  is a ; :) @ frequencD ",, 2M. a) :) @ frequencD ",, 42M b) 9H @ frequencD ",, 2M. c) 9H @ frequencD ",, 42M. d)

Answer ; d)

9H @ frequencD ",, 42M. ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use anne !""- ##!#$A or )oute anual chart >(7#  502. The radio na8igation aid at H>7FA1T H>7FA1T C0TO ( ,+B"&P9 !!,B,"P<  is ; an 9H @ frequencD +$! 42M @ 9T continuous operation a) an 9H @ frequencD +$! 42M @ continuous operation b) c) a fan mar4er @ frequencD +$! 42M a TACA9 @ channel +$! d)

Answer ; a)

an 9H @ frequencD +$! 42M @ 9T continuous operation ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use anne !""- ##!#!A or )oute anual chart >(20+ CAA->dition  503. The radio na8igation aid at C20==0A ( +,B!+P9 !#$B#&P>  is a ; :) @ frequencD ##+.# 2M @ and TACA9 TACA9 frequencD +!5 2M a) :) @ frequencD ##+.# 2M @ and TACA9 TACA9 channel +!5 b) :)> onlD @ frequencD ##+.# 2M c) :)> @ frequencD ##+.# 2M @ and 9H frequencD +!5 42M d)

Answer ; d)

:)> @ frequencD ##+.# 2M @ and 9H frequencD +!5 42M ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use )oute anual chart >(7#  504. The radio na8igation aid at 7>>1 H)AF) ( ,"B,$P9 !!#B"6P<  is ; an 9H @ frequencD +!$., 42M @ 9T continuous operation a) a TACA9 TACA9 @ channel +!$., b) c) a fan mar4er @ frequencD +!$., 42M an 9H @ frequencD +!$., 42M @ continuous operation d)

Answer ; a)

an 9H @ frequencD +!$., 42M @ 9T continuous operation ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use Anne !""- ##!#"A or )oute anual chart >(7#  505. The radio na8igation aid at 12A999 ( ,$B+"P9 !!5B,"P<  is ; an 9H @ frequencD ",$ 42M a) a :) onlD @ frequencD ##"." 2M b) a TACA9 @ frequencD frequenc D ##"." 42M c) a :)> @ frequencD ##"." 2M d)

Answer ; d)

a :)> @ frequencD ##"." 2M ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use )oute anual chart >(7#  506. The radio na8igation aid at 1T AHH1 ( ,,B,,P9 !!$B#$P<  is ; a TACA9 @ channel ##$., a) a :)> @ frequencD ##$., 2M b) c) an 9H @ frequencD ##$., 2M a :) onlD @ frequencD ##$., 2M d)

Answer ; b)

a :)> @ frequencD ##$., 2M ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use anne !""- ##!!&A or )oute anual chart >(20+ CAA->dition  507. The radio na8igation aid at 1T 0N0>) ( +5B"59 !!+B,"P>  is a ; :) @ frequencD ##+.! 2M @ and TACA9 TACA9 channel 5& a) TACA9 TA CA9 @ channel 5& @ frequencD ##+.! 2M b) TACA9 @ channel ##+.! c) TACA9 TACA9 @ channel 5& @ and 9H frequencD ##+.! 42M d)

Answer ; b)

TACA9 @ channel 5& @ frequencD ##+.! 2M TACA9 -----------------------------------------------------------------------------------------------------------------------------------------------------------------


$"&


508.

( For this question use anne !""- ##!!5A or )oute anual chart >(20+ CAA->dition  The radio na8igation aid at T'C70FF> ( ,+B#$P9 !!#B$$P<  is a ; :)TAC :)TAC @ frequencD ##".& 2M @ and an 9H frequencD 6$ 42M. a) TACA9 TA CA9 onlD @ channel 5+ @ ( frequencD ##".& 2M  b) TACA9 TACA9 @ channel 5+ @ and a :) frequencD ##".& 2M onlD. c) TACA9 TACA9 @ channel 5+ @ and an 9H frequencD 6$ 42M onlD. d)

Answer ; b)

TACA9 onlD @ channel 5+ @ ( frequencD ##".& 2M  TACA9 ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use anne !""- ##!!5A or )oute anual chart >(20+ CAA->dition  509. The radio na8igation aid at N?)0C2 ( +&B"%P9 !!5B+6P>  is ; a :) onlD @ frequencD ##,.! 2M a) an 9H onlD @ frequencD ##,.! 42M b) c) a TACA9 @ frequencD frequenc D ##,.! 2M a :)> @ frequencD ##,.!2M d)

Answer ; a)

a :) onlD @ frequencD ##,.! 2M ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this this question use anne !""- ##!##A ##!##A or )oute anual chart >(20+ CAA->dition CAA->dition  510. The radio na8igation aid on airwaD ?=+ at 7?R>?07 ( +&B+#P9 !!%B#5P>  is a ; :)> onlD @ identifier 7?7 a) :) onlD @ identifier 7?7 b) :) @ identifier 7?7 @ frequencD paired with TACA9 TACA9 identifier 7R0 c) :)> and 9H @ identifier 7R0 d)

Answer ; b)

:) onlD @ identifier 7?7 ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use anne !""- ##!!%A or )oute anual chart >(20+ CAA->dition  511. The radio na8igation aid ser8ing 1T)A1H?)= ( +5B"!P9 !!&B"+P>  is a ; :) onlD @ frequencD ##,.% 2M a) > onlD @ channel ##,.% b) c) :)TACA9 :)TA CA9 @ frequencD ##,.% 2M TACA9 TACA9 onlD @ frequencD ##,.% 2M d)

Answer ; c)

:)TACA9 @ frequen frequencD cD ##,.% 2M ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use anne !""- ##!!6A or )oute anual chart >(20+ CAA->dition  512. The radio na8igation aid 1TA ( ,#B+,P9 !!+B#,P>  is ; a :)> @ on channel "5% a) a TACA9 @ on channel "5% b) a :) @ frequencD "5% 2M c) an 9H @ frequencD "5% 42M d)

Answer ; d)

an 9H @ frequencD "5% 42M ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use )oute anual chart >(20$  513. The radio na8igation aid(s at ( ,,B$%P9 !##B"5P>  isare ; :)> @ frequencD #$5.&, 2M. a) 9H @ frequencD ##$.5 ##$.5 42M. b) c) :)> @ frequencD ##$.5 2M. :)> @ frequencD #$5.#, 2M. d)

Answer ; c)

:)> @ frequencD ##$.5 2M. ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use )oute anual chart >(20$  514. The radio na8igation aid(s at ( ,,B,6P9 !#+B!%P>  isare ; :)> @ frequencD ##%.6 2M. a) 9H @ frequencD ##%.6 ##%.6 42M. b) 9H @ frequencD "%" 42M. c) :) @ frequencD "%" 42M. d)

Answer ; c)

9H @ frequencD "%" 42M. -----------------------------------------------------------------------------------------------------------------------------------------------------------------


$"5


515.

( For this question use )oute anual chart >(20$  The radio na8igation aid(s at ( ,%B!6P9 !#"B#+P>  isare ; :)> @ frequencD ##%.6 2M. a) :) @ frequencD ##%.$ 2M. b) :) @ frequencD ##%.6 2M. c) :)> @ frequencD ##%.$ 2M. d)

Answer ; c)

:) @ frequencD ##%.6 2M. ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use )oute anual chart >(20$  516. The radio na8igation aid(s at ( ,%B#&P9 !#!B+&P>  isare ; :) @ frequencD "&+ 2M. a) :)> @ frequencD "&+ 42M. b) c) 9H@ frequencD "&+ 42M @ for TemporarD TemporarD ?se ( T? T? . 9H @ frequencD "&+ 42M. d)

Answer ; d)

9H @ frequencD "&+ 42M. ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use )oute anual chart >(20#  517. The radio na8igation aid(s at ( ,&B"$P9 !!+B!"P<  isare ; :)> @ frequencD #!6.$ 2M. a) :)> @ frequencD #!6.$ 42M. b) :) @ frequencD #!6.$ 2M @ no > a8ailable. c) :) @ frequencD #!6.$ 2M @ for 091 update onlD. d)

Answer ; a)

:)> @ frequencD #!6.$ 2M. ----------------------------------------------------------------------------------------------------------------------------------------------------------------The required time for final reser8e fuel for turboGet aeroplane is ; 518. :ariable :ariable with wind 8elocitD. 8elocit D. a) %! min. b) +, min. c) d) "! min.

Answer ; d)

"! min. -----------------------------------------------------------------------------------------------------------------------------------------------------------------


$"6


519.

( For this question question use anne !""- ##!+"A ##!+"A or )oute anual 1TA) 1TA) charts for 'A)01 'A)01 C2A)7>1 > > =A?77> ($!-$ 

Annex 033-11043A 033-11043A The route distance from C20>:)>1 ( C0:  to H?)199> ( H19  is ; 55 9 a) 5" 9 b) &" 9 c) 6% 9 d) Answer ; d)

6% 9 -----------------------------------------------------------------------------------------------------------------------------------------------------------------


$+!


520.

( For this question use anne anne !""- ##!+&A ##!+&A or )oute )oute anual anual 10 chart chart for A1T>)A 1C20'27 (#!-"H 

Annex 033-11047A 033-11047A The route distance from runwaD $& to A)9> is ; ", 9 a) ,6 9 b) ,$ 9 c) %& 9 d) Answer ; d)

%& 9


$+#


-----------------------------------------------------------------------------------------------------------------------------------------------------------------

The still air distance in the climb is #56 9autical Air iles ( 9A  and time "! minutes.
521.

Answer ; b)

#&+ 9 ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use anne !""-#$"$!A  522.

Annex 033-12320A 033-12320A The surface sDstem o8er :0>99A ( +5B9 !#%B>  is a ; cold front mo8ing west a) cold front mo8ing east b) c) warm front mo8ing north stationarD occluded front d) Answer ; b)

cold front mo8ing east -----------------------------------------------------------------------------------------------------------------------------------------------------------------


$+$


523.


Annex 033-111 033-111"1A "1A The surface weather sDstem o8er >ngland ( ,"B9 !!$B<  is ; a cold front mo8ing east a) b) a warm front mo8ing southeast an occluded front mo8ing east c) a depression mo8ing north d) Answer ; c)

an occluded front mo8ing east ----------------------------------------------------------------------------------------------------------------------------------------------------------------524. ( For this question use anne !""-#$""$A 

Annex 033-12332A 033-12332A The surface wind 8elocitD ( B 4t  at at 'A)0 'A)01C2A)7>1->-=A?77> 1C2A)7>1->-=A?77> at #""! ?TC was ; #5!#$ a) "!!!, b) $&!!+ c) $&!!5 d) Answer ; c)

$&!!+


$+"


-----------------------------------------------------------------------------------------------------------------------------------------------------------------

525.

( For this question use anne !""-##&!+A  True Air Air speed I #&! 4t 9 to re-route to A) 8ia T=*. The gi8en wind conditions remaining constant. The fuel consumption during the turn is $! litres. The total fuel consumption at position o8erhead A) will be ; # "$% litres a) b) # #5$ litres # %!! litres c) # ,+, litres d)

Answer ; d)

# ,+, litres ----------------------------------------------------------------------------------------------------------------------------------------------------------------526. The Trip Fuel for a Get aeroplane to flD from the departure aerodrome to the destination aerodrome is ,",! 4g. Fuel consumption in holding mode is %!!! 4gh. The quantitD of fuel which is needed to carrD out one go-around and land on the alternate airfield is +"5! 4g. The destination aerodrome has a single runwaD.
#" $"! 4g ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question refer to 0mage #  527.

,age 1 The true course is !+$B. The 8ariation in the area is %B < and the wind is calm. The de8iation card is reproduced in the anne. 0n order to follow this course@ the pilot must flD a compass heading of ; !,$ a) !+! b) !++ c) !,5 d) Answer ; a)

!,$ ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use anne !""- ##!#+A or )oute anual chart >(7,  528. The :) and TACA9 on airwaD =6 at 19AH)?C/ ( ,$B#$P9 !!5B#&P>  are ; frequencD paired @ and ha8e different identifiers a) b) 9T frequencD paired @ and ha8e different identifiers 9T frequencD paired @ and ha8e the same identifier c) frequencD paired @ and ha8e the same identifier d)

Answer ; b)

9T frequencD paired @ and ha8e different identifiers -----------------------------------------------------------------------------------------------------------------------------------------------------------------


$++


529.

( For this question use anne !""-###6!A !""-###6!A 

Annex 033-111 033-11190A 90A The wind direction and 8elocitD ( B 4t  at +!B9 !+!B> is ; "!!&, a) ""!5, b) ""!&, c) d) #,!&, Answer ; c)

""!&, -----------------------------------------------------------------------------------------------------------------------------------------------------------------


$+,


530.


Annex 033-11 033-11190A The wind direction and 8elocitD ( B 4t  at ,!B9 !+!B> is ; a) $!!&! !$!&! b) !$!5! c) ",!&! d) Answer ; b)

!$!&! -----------------------------------------------------------------------------------------------------------------------------------------------------------------


$+%


531.


Annex 033-11 033-11190A The wind direction and 8elocitD ( B 4t  at %!B9 !#,B< is ; $6!#,, a) $6!#5, b) ##!#,, c) "$!#,, d) Answer ; a)

$6!#,, -----------------------------------------------------------------------------------------------------------------------------------------------------------------


$+&


532.

( For this question use anne !""-###56A !""-###56A 

Annex 033-11 033-111"1A The wind 8elocitD o8er 0TA7O is ; ##! 4t at F7"5! maimum 8elocitD not shown on chart a) a maimum of ##! 4t at F7"5! b) #"! 4t at F7"5! maimum 8elocitD not shown on chart c) a maimum of #%! 4t at F7 "5! d) Answer ; b)

a maimum of ##! 4t at F7"5! -----------------------------------------------------------------------------------------------------------------------------------------------------------------


$+5


533.

( For this question use anne !""-#$"#+A 

Annex 033-12314A 033-12314A The <: ( B a) b) c) d)

4t  at +!B9 !$!B< is ; #,,+! ""++! #",+! "#!+!

Answer ; d)

"#!+! -----------------------------------------------------------------------------------------------------------------------------------------------------------------


$+6


534.


Annex 033-12314A 033-12314A The <: ( B a) b) c) d)

4t  at ,!B9!#,B< is ; "#!5, "#!&, $6!&, #!!&,

Answer ; c)

$6!&, -----------------------------------------------------------------------------------------------------------------------------------------------------------------


$,!


535.


Annex 033-12314A 033-12314A The <: <: ( B a) b) c) d)

4t  at %!B 9!#,B < is ; "!!%! ##,%! "$!%! "!!&!

Answer ; a)

"!!%! ----------------------------------------------------------------------------------------------------------------------------------------------------------------536. ( For this question refer to 0mage $ 

,age 2 True Air speed I#&! 4t @ 9 to re-route to A) 8ia T=*. The gi8en wind conditions remaining constant. The fuel consumption during the turn is $! litres. The total fuel consumption at position o8erhead A) will be ; # %!! litres a) # #5$ litres b) # ,+, litres c) # "$% litres d) Answer ; c)

# ,+, litres


$,#


-----------------------------------------------------------------------------------------------------------------------------------------------------------------

537.

?nless otherwise shown on charts for standard instrument departure the routes are gi8en with ; a) true headings magnetic course b) magnetic headings c) true course d)

Answer ; b)

magnetic course ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this this question use anne !""-#$"%+A or Flight 'lanning anual )*T # Figure +.&.$  538.

Annex 033-12364A 033-12364A ?sing the abo8e table @ in 01A conditions and at a speed of .&!$5! /0A1 @ in an elapsed time of 6! minutes an aircraft with mass at point of di8ersion +5!!! 4g could di8ert a distance of ; ,5+ 9 a) %!" 9 b) %!5 9 c) ,%" 9 d) Answer ; a)

,5+ 9 -----------------------------------------------------------------------------------------------------------------------------------------------------------------


$,$


539.

( For this question use Flight 'lanning anual 1>' # Figure $." Table $.".# 

Flight Planning Manual SEP 1 Figure 2.3 Table 2.3.1 ?sing the 'ower 1etting Table @ for the single engine aeroplane@ determine the cruise TA1 and fuel flow ( lbshr  with full throttle and cruise lean miture in the following conditions ; =i8en ; AT I "BC 'ressure altitude I %!!! ft 'ower I Full throttle  $#.! in2g  $#!! )' #"% 4t and ,%.6 lbshr a) #"# 4t and ,%.6 lbshr b) c) #$, 4t and ,,.& lbshr #"+ 4t and ,,.& lbshr d) Answer ; d)

#"+ 4t and ,,.& lbshr -----------------------------------------------------------------------------------------------------------------------------------------------------------------


$,"


540.

( For this question use Flight 'lanning anual 1>' # Figure $.$ Table $.$." 

Flight Planning Manual SEP 1 Figure 2.2 Table 2.2.3 ?sing the 'ower 1etting Table @ for the single engine aeroplane @ determine the cruise TA1 TA1 and fuel flow ( lbshr  with full throttle and cruise lean miture in the following conditions ; =i8en ; AT I #"BC 'ressure altitude I 5!!! ft )' I $"!! #%! 4t and &#.# lbshr a) b) #%! 4t and %6." lbshr #,6 4t and &#.& lbshr c) #,5 4t and &+.+ lbshr d) Answer ; b)

#%! 4t and %6." lbshr -----------------------------------------------------------------------------------------------------------------------------------------------------------------


$,+


541.

( For this question use Flight 'lanning anual 1>' # Figure $.$ Table $.$." 

Flight Planning Manual SEP 1 Figure 2.2 Table 2.2.3 ?sing the 'ower 1etting Table @ for the single engine aeroplane @ determine the manifold pressure and fuel flow ( lbshr  with full throttle and cruise lean miture in the following conditions ; =i8en ; AT I #"BC 'ressure altitude I 5!!! ft )' I $"!! $$.+ in.2g and %6." lbshr a) b) $$.+ in.2g and &#.# lbshr $$.+ in.2g and &".5 lbshr c) $".! in.2g and %6.! lbshr d) Answer ; a)

$$.+ in.2g and %6." lbshr -----------------------------------------------------------------------------------------------------------------------------------------------------------------


$,,


542.

( For this question use Flight 'lanning anual 1>' # Figure $.+ Table $.+ 

Flight Planning Manual SEP 1 Figure 2.4 Table 2.4 ?sing the )ange 'rofile iagramm @ for the single engine aeroplane @ determine the range@ with +, minutes reser8e @ in the following conditions ; =i8en ; .A.T. I 01A E#%BC 'ressure altitude I +!!! ft 'ower I Full throttle  $,.! in2g  $#!! )' 5%, 9 a) &"6 9 b) 6## 9 c) d) 5,# 9 Answer ; a)

5%, 9 ----------------------------------------------------------------------------------------------------------------------------------------------------------------:F) flights shall not be flown o8er the congested areas of cities at a height less than ; 543. #!!! ft abo8e the highest obstacle within a radius of %!! m from the aircraft. a) b) the highest obstacle. $!!! ft abo8e the highest obstacle within a radius of %!! ft from the aircraft. c) ,!! ft abo8e the highest obstacle. d)

Answer ; a)

#!!! ft abo8e the highest obstacle within a radius of %!! m from the aircraft. ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use )oute anual chart chart >(7#  544. A9 C)11 ##,.$ C1 ( ,+B+"P9 !!"B$!P<  to TA77A TA77A ##".5 T7A ( ,,B"!P9 !!"B$#P<  on airwaD A$ 3 +, and "6 a) +, and +! b) +$ and +! c) +$ and "6 d)

Answer ; b)

+, and +!


$,%


----------------------------------------------------------------------------------------------------------------------------------------------------------------545.

( For this question use T) (:F) @ Aberdeen Aberdeen (Dce 0nformation 'age (#6-% 
Answer ; d)

(i 2$ @ (ii 2+ ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use T) @ >sbGerg Aerodrome chart (#6-$  546. sbGerg 3 5,"! ft  +, ft a) 5,"! m  +, m b) c) $%!! ft  #+5 ft $%!! m  +, m d)

Answer ; d)

$%!! m  +, m ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use )oute anual chart chart >(7#  547. 1/ ( ,,B#5P9 !!"B#$P<  3 #%"  "6 9 a) "+"  ,$ 9 b) "+"  ##+ 9 c) #%"  ,$ 9 d)

Answer ; b)

"+"  ,$ 9 ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use T) (:F) @ Aberdeen (Dce Area chart (#6-,  548.
Answer ; a)

##+."! or #$#.5, ----------------------------------------------------------------------------------------------------------------------------------------------------------------549. ( For this question use )oute anual :F)E='1 chart >-%  9 airport ( +&B$5P9 @ !!5B""P>  3 #,&$ ft a) #+#% ft b) #!!! m c) #+$# ft d)

Answer ; b)

#+#% ft ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use T) @ e /ooD Area chart (#6-#  550.
Answer ; c)

(i #!6.&! @ (ii $#% ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use T) (:F) @ Aberdeen Aberdeen (Dce Area Area chart (#6-,  551.
Answer ; c)

#$#.5, -----------------------------------------------------------------------------------------------------------------------------------------------------------------


$,&


552.

( For this question use )oute anual chart >(20#  )>>9 ( ,&#6P9 !!$#%P<  to T0)>> ( ,%"!P9 !!%,"P<  3 a) $+& $%! b) $," c) $%& d)

Answer ; b)

$%! ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use T) (:F) @ Aberdeen Aberdeen (Dce Area Area chart (#!-#:  553.
Answer ; d)

##6.5& ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use T) @ >sbGerg Area chart (#6-#  554.
Answer ; b)

!5! (  +.$ 9 ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use T) (:F) @ Aberdeen Aberdeen (Dce 0nformation 'age (#6-%  555.
Answer ; d)

2% ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use anne !""-###65A !""-###65A  556.
Answer ; c)

#!!! ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use anne !""-#$""+A  557.

Annex 033-12334A 033-12334A 3 nil a) #5!! b) !5!! c) #"!! d) Answer ; b)

#5!!


$,5


----------------------------------------------------------------------------------------------------------------------------------------------------------------558.

( For this question use T) (:F) @ Aberdeen (Dce Area chart (#!-#: 
Answer ; d)

#&"" ft ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use T) (:F) @ Aberdeen Aberdeen (Dce Area Area chart (#!-#:  559.
Answer ; b)

$#!, ft ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use T) @ Athinai (2ellini4on Approach chart ($6-#  560. shown at the northern end of 2ellini4on airfield 3 $6+ 29 a) ",& /:) b) ##+.+! AT2 c) $&, 2/ d)

Answer ; c)

##+.+! AT2 ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use T) @ :F) directorD for =reece (&-"  561.
Answer ; d)

(i 7T K ?TC E $ 2ours @ (ii 7T K ?TC E " 2ours ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use T) @ :F) directorD for 9etherlands (&-"  562.
Answer ; c)

(i 7T S # 2our K ?TC @ (ii 7T S $ 2ours K ?TC ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use )oute anual chart >(7#  563. A9 C)11 ##,.$ C1 ( ,+B+"P9 !!"B$!P ##+.$, 9>< ( ,,B!$P9 !!#B+#P<  3 F7,! a) b) F7#,! +$!! ft c) +&!! ft d)

Answer ; b)

F7#,! ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use T) @ Athinai Athinai (2ellini4on Area Area chart ($6-#  564.
Answer ; b)

"!! ft -----------------------------------------------------------------------------------------------------------------------------------------------------------------


$,6


565.


Annex 033-11 033-11190A
-$ ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use )oute anual chart chart >(20$  566. 3 a) oppler :) @ ident 1?' and 9H @ ident > 9H @ ident > and :) @ ident ident :>O b) 9H onlD @ ident > c) :) onlD @ ident :>O d)

Answer ; c)

9H onlD @ ident > ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use )oute anual chart >(20$  567. TT>) (,&"6P9 !#$#&P>  3 oppler :) onlD with identification 7A: a8ailable on frequencD ##+.% 2M. a) :)> and 9H with identification 7A: a8ailable a8ailable on frequencD ##+.% 2M. b) > onlD with identification 7A: a8ailable on frequencD ##+.% 2M. c) :)> with identification 7A: a8ailable on frequencD ##+.% 2M. d)

Answer ; d)

:)> with identification 7A: a8ailable on frequencD ##+.% 2M.


$%!


-----------------------------------------------------------------------------------------------------------------------------------------------------------------

568.

( For this question use T) @ e /ooD Area Area chart (#6-#  /O 3 ".,!! ft a) b) #.,!! ft ".!!! ft c) "$.5!! ft d)

Answer ; b)

#.,!! ft ----------------------------------------------------------------------------------------------------------------------------------------------------------------569. ( For this question use )oute anual chart >(7#  nroute Altitude ( >A  on airwaD <6## from >A9 C)11 ##,.$ C1 ( ,+B+"P9 !!"B$!P ##+.$, 9>< ( ,,B!$P9 !!#B+#P<  3 F7#,! a) +&!! ft b) F7,! c) d) +$!! ft

Answer ; c)

F7,! ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use T) (:F) @ Aberdeen Aberdeen (Dce 0nformation 'age (#6-%  570.
Answer ; c)

$ /m ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use T) @ Athinai Athinai (2ellini4on 7anding Chart ($6-$  571. a) "&B,".5P9 $"B+".&P> b) "&B,+.5P9 $"B++.&P> c) d) "&B,+.$P9 $"B++."P>

Answer ; b)

"&B,".5P9 $"B+".&P> ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use T) @ >sbGerg Aerodrome chart (#6-$  572. sbGerg 3 a) ,,B"$.+P9 !!5B"+.6P< ,,B"$.+P9 !!5B"+.6P> b) ,,B"#.%P9 !!5B"".#P< c) ,,B"#.%P9 !!5B"".#P> d)

Answer ; d)

,,B"#.%P9 !!5B"".#P> ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use or T) @ 1abadell Area chart (#6-#  573.
Answer ; a)

##5.%, -----------------------------------------------------------------------------------------------------------------------------------------------------------------


$%#


574.


Annex 033-12314A 033-12314A 3 -#! a) E$ b) -,, c) E#! d) Answer ; a)

-#! ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use T) @ Athinai (2ellini4on Approach chart ($6-#  575.
Answer ; c)

#6 9 ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use T) @ >sbGerg Area chart (#6-#  576. 1/) to o8erhead >sbGerg 3 "!5 (  $6 9 a) "!5 (  $6 /m b) "!5 (T  $6 9 c) "!5 (T  $6 /m d)

Answer ; a)

"!5 (  $6 9 -----------------------------------------------------------------------------------------------------------------------------------------------------------------


$%$


577.

( For this question use T) @ Athinai (2ellini4on Approach chart ($6-# 

Athinai * +ellini$n  Ar$a(h (hart * 29-1  a) "> b) "< c) ,< d) Answer ; b)

">


$%"


----------------------------------------------------------------------------------------------------------------------------------------------------------------578.

( For this question use anne !""-###6,A !""-###6,A 

Annex 033-111 033-11195A 95A 2  3 a) " to + at ,!! , to & at #$!! b) , to & at ,!! c) , to & at $!!! d) Answer ; c)

, to & at ,!! ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use anne !""-#$"$6A  579.

Annex 033-12329A 033-12329A 1H?)=*A9 1?T1 at !"!! ?TC 3 a) " to + at 5!! " to + at +!! b) , to & at 5!! c) , to & at +!! d) Answer ; d)

, to & at +!! ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use anne !""-#$""%A  580.

Annex 033-12336A 033-12336A A?R>)0=9AC at #%!! ?TC 3 "! a) , b) $, c) #! d) Answer ; a)

"! -----------------------------------------------------------------------------------------------------------------------------------------------------------------


$%+


581.


Annex 033-12314A 033-12314A to !#!B> at +,B9 3 -,! a) -,+ b) -,$ c) d) -+5 Answer ; a)

-,! -----------------------------------------------------------------------------------------------------------------------------------------------------------------


$%,


582.


Annex 033-11 033-11190A 3 -+& a) -+% b) -+6 c) d) -,! Answer ; a)

-+& -----------------------------------------------------------------------------------------------------------------------------------------------------------------


$%%


583.


#$ute Manual %F#&'PS %F#&'PS (hart E)-6 '* 7A0C209=>9 airport ( +5B"!P9 @ !!6B"5P>  3 +" a) +% b) c) +!$ m $+"+ ft d) Answer ; a)

+" ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use )oute anual :F)E='1 chart >-%  584.

#$ute Manual %F#&'PS %F#&'PS (hart E)-6 T >9=>9 airport ( +5B!"P9 @ !!6B$$P>  3 +% a) ##$! m b) +" c) #5#6 ft d) Answer ; a)

+%


$%&


----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use anne !""-#$""$A 

585.

Annex 033-12332A 033-12332A 1->-=A?77> 'A)01C2A)7>1->-=A?77> at $#!! ?TC 3 5!!! m a) %!!! m b) #! 4m c) $!!! m d) Answer ; b)

%!!! m ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use anne !""-###6%A !""-###6%A  586.

Annex 033-111 033-11196A 96A =77  3 a) #,!! #!!!! b) ,!!! c) $$!! d) Answer ; a)

#,!! ----------------------------------------------------------------------------------------------------------------------------------------------------------------( ?se )oute anual chart >(20#  587. frequencD #!6.5 2M. b) :) and > on frequencD #!6.5. c) d) TACA9 TACA9 range and bearing on Channel ",.

Answer ; b)

The range element onlD of TACA9 TACA9 on > frequencD #!6.5 2M. ----------------------------------------------------------------------------------------------------------------------------------------------------------------stimated ta4e-off mass c) aimum certified ta4e-off mass d)

Answer ; d)

aimum certified ta4e-off mass ----------------------------------------------------------------------------------------------------------------------------------------------------------------
Answer ; b)

"! minutes or more.


$%5


----------------------------------------------------------------------------------------------------------------------------------------------------------------
590.

Answer ; c)

"! minutes flDing time or "&! 4m. ----------------------------------------------------------------------------------------------------------------------------------------------------------------
Answer ; a)

# @ $ @ " @ +. ----------------------------------------------------------------------------------------------------------------------------------------------------------------
Answer ; d)

!#,, ----------------------------------------------------------------------------------------------------------------------------------------------------------------uropean > uropean destination @ cloc4 times are to be epressed in ; 593. a) 7ocal mean time 7ocal standard time b) Central >uropean Time c) ?TC d)

Answer ; d)

?TC ----------------------------------------------------------------------------------------------------------------------------------------------------------------1  would be ; R a) = b) 91 c) d) O

Answer ; d)

O ----------------------------------------------------------------------------------------------------------------------------------------------------------------” c) “NNNN” followed bD an entrD in 0tem #5 d) Answer ; d)

“NNNN” followed bD an entrD in 0tem #5 ----------------------------------------------------------------------------------------------------------------------------------------------------------------
Answer ; d)

estimated off-bloc4 time. -----------------------------------------------------------------------------------------------------------------------------------------------------------------


$%6


597.

Answer ; c)

contingencD fuel bD adding contingencD onlD from the burnoff between decision point and destination. ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use anne !""-###5#A !""-###5#A  598.

Annex 033-11 033-111"1A 9=2AN0 ( "$B9 !$!B>  3 7ight a) 9il b) 1e8ere c) oderate d) Answer ; b)

9il -----------------------------------------------------------------------------------------------------------------------------------------------------------------


$&!


599.


Annex 033-11 033-111"1A 1T ( +,B9 !$%B>  3 1e8ere a) 9il b) oderate c) 7ight d) Answer ; c)

oderate -----------------------------------------------------------------------------------------------------------------------------------------------------------------


$&#


600.

( For this question use anne.!""-#$"$!A 

Annex 033-12320A 033-12320A )709 ( ,"B 9 !#"B>  3 se8ere a) nil b) moderate c) light d) Answer ; c)

moderate -----------------------------------------------------------------------------------------------------------------------------------------------------------------


$&$


601.


Annex 033-12320A 033-12320A  3 , to & o4tas C? and AC base F7#!! tops F7#5! a) " to + o4tas C? and AC base F7#!! tops F7#%! b) c) " to + o4tas C? and AC base below F7#!! tops F7#5! , to & o4tas C? and AC base below F7#!! tops F7#5! d) Answer ; d)

, to & o4tas C? and AC base below F7#!! tops F7#5! -----------------------------------------------------------------------------------------------------------------------------------------------------------------


$&"


602.


Annex 033-12320A 033-12320A ( ++B9!!#B>  3 bro4en ACC? base below F7#!! tops F7#,! @ embedded isolated CH base below F7#!! tops F7$&! a) , to & o4tas C? and AC base below F7#!! tops to F7$&! b) isolated CH embedded in laDer cloud @ surface to F7$&! c) d) well separated CH base F7#!! tops to F7 $&! Answer ; a)

bro4en ACC? base below F7#!! tops F7#,! @ embedded isolated CH base below F7#!! tops F7$&! -----------------------------------------------------------------------------------------------------------------------------------------------------------------


$&+


603.


Annex 033-11 033-111"1A  ; , to & o4tas C? and CH base below F7#!! @ tops F7#5! a) b) 9il " to & o4tas C? and CH base below F7#!! @ tops F7#5! c) , to & o4tas C? and CH base F7#!! @ tops F7#5! d) Answer ; a)

, to & o4tas C? and CH base below F7#!! @ tops F7#5! ----------------------------------------------------------------------------------------------------------------------------------------------------------------604. ( For this question use anne !""-#$"""A 

Annex 033-12333A 033-12333A
light rain associated with thunderstorms


$&,


----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use anne !""-#$"$6A 

605.

Annex 033-12329A 033-12329A 1H?)=*A9 1?T1 at !+!! ?TC 3 CA:/ a) rain associated with thunderstorms b) c) patches of fog mist andor fog d) Answer ; c)

patches of fog --------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use anne !""-#$"$!A  606.

Annex 033-12320A 033-12320A ( ++B 9 !#B>  3 moderate a) moderate or se8ere b) light c) nil d) Answer ; b)

moderate or se8ere -----------------------------------------------------------------------------------------------------------------------------------------------------------------


$&%


607.


Annex 033-11 033-111"1A
1e8ere -----------------------------------------------------------------------------------------------------------------------------------------------------------------


$&&


608.

( For this question use anne !""-#$"$%A 

Annex 033-12320A 033-12320A ( ++B9 !!#B>  3 moderate a) se8ere b) c) light nil d) Answer ; b)

se8ere -----------------------------------------------------------------------------------------------------------------------------------------------------------------


$&5


609.


Annex 033-11 033-111"1A 3 1e8ere attenuation in the 2F )T band a) )educed 8isibilitD b) c) >ngine flame out and windscreen damage There is no haMard d) Answer ; c)

>ngine flame out and windscreen damage -----------------------------------------------------------------------------------------------------------------------------------------------------------------


$&6


610.

( For this this question use anne !""- ##!+%A or )oute anual 10 charts charts for N?)0C2 (#!-" 

Annex 033-11046A 033-11046A a) A7H0R %2 b) A7H0R &A c) A7H0R &1 d) Answer ; d)

A7H0R &1 ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this this question use anne !""- ##!+#A or )oute anual 10 chart chart for ?90C2(#!-"C ?90C2(#!-"C @#!-"  611. 'T>9 from runwaD $%7 3 />'T>9 T2)>> J?>H>C a) />'T>9 T2)>> 9:>H>) b) />'T>9 T2)>> >C2 c) />'T>9 F0:> 10>))A d)

Answer ; d)

/>'T>9 F0:> 10>))A -----------------------------------------------------------------------------------------------------------------------------------------------------------------


$5!


612.

( For this question use anne !""-#$"",A 

Annex 033-12335A 033-12335A A?R>)0=9AC at #!!! ?TC 3 hea8D rain associated with thunderstorms a) nil b) light rain c) rain showers d) Answer ; c)

light rain ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question question use anne !""-6&$6A @ A>)9A?T0CA7 C2A)T 0CA #I,!! !!! 1T?TT=A)T (9 +&% or )oute 613. anual :F)E='1 chart >-% 

#$ute Manual %F#&'PS %F#&'PS (hart E)-6 3 :)TAC a) 9H b) :) c) :)> d) Answer ; c)

:)


$5#


----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question question use anne !""-6&$6A @ A>)9A?T0CA7 C2A)T 0CA #I,!! !!! 1T?TT=A)T (9 +&% or )oute anual :F)E='1 chart >-%  3 :) a) :)> b) TACA9 c) d) 9H

614.

Answer ; b)

:)> ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question question use anne !""-6A @ A>)9A?T0CA7 C2A)T 0CA #I,!! !!! 1T?TT=A)T (9 +&% or )oute 615. anual :F)E='1 chart >-% 

#$ute Manual %F#&'PS %F#&'PS (hart E)-6 3 :)> a) 9H b) TACA9 c) :) d) Answer ; a)

:)> -----------------------------------------------------------------------------------------------------------------------------------------------------------------


$5$


616.

( For this question use anne !""-##$!$A 

Annex 033-11 033-111"1A )709 ( ,"B9 #"B>  3 9one a) F7$6! b) F7 $#! c) d) F7$,! Answer ; d)

F7$,! ----------------------------------------------------------------------------------------------------------------------------------------------------------------( For this question use T) (:F) @ Aberdeen Aberdeen (Dce Area Area chart (#!-#:  617.
Answer ; d)

#",.#& -----------------------------------------------------------------------------------------------------------------------------------------------------------------


$5"


618.

( For this question use anne anne !""- ##!++A ##!++A or )oute )oute anual anual 10 chart chart for 799 2>AT2)< 2>AT2)< (#!-" 

Annex 033-11044A 033-11044A ast sector $#!! ft within ,! 9 a) >ast sector $"!! ft within ,! 9 b)


$5+


619.

( For this question use anne anne !""- ##!+5A ##!+5A or )oute )oute anual anual 10 chart chart for A1T>)A 1C20'27 (#!-" 

Annex 033-1104"A 033-1104"A 'A >'A)T?)> )T?)> ##6.!, passing $!!! ft and report altitude c) aimum 0A1 $,!4t turning left at 1'7 ".# > d) Answer ; c)

Contact 1C20'7 >'A >'A)T?)> )T?)> ##6.!, passing $!!! ft and report altitude


$5,


-----------------------------------------------------------------------------------------------------------------------------------------------------------------

620.

ach reporting point requires a new segment. A small change of temperature ( $BC  can di8ide a segment. b) The distance from ta4e-off up to the top of climb has to be 4nown. c) 9o segment shall be more than "! minutes of flight time. d)

Answer ; c)

The distance from ta4e-off up to the top of climb has to be 4nown. ----------------------------------------------------------------------------------------------------------------------------------------------------------------
Answer ; c)

1tatement $ onlD ----------------------------------------------------------------------------------------------------------------------------------------------------------------622.
Answer ; b)

1tatement # onlD ----------------------------------------------------------------------------------------------------------------------------------------------------------------
Answer ; c)

1tatement # onlD ----------------------------------------------------------------------------------------------------------------------------------------------------------------HT. AnD flight plan should be filed at least #! minutes before departure. d)

Answer ; c)

0n case of ATF ( Air Traffic Flow anagement  the flight plan should be filed at least three hours in ad8ance of the >HT. -----------------------------------------------------------------------------------------------------------------------------------------------------------------


$5%


625.

( For this question use anne !""-#$"+"A or Flight 'lanning anual )*T # Figure +.".#C 

Annex 033-12343A 033-12343A
-, ----------------------------------------------------------------------------------------------------------------------------------------------------------------Oou Oou are flDing a constant compass heading of $,$B. :ariation :ariation is $$B> @ de8iation is "B< and Dour 091 is showing a drift of 626. 6B right. True trac4 is 3 $%$B a) $$+B b) $+$B c) $5!B d) Answer ; d)

$5!B -----------------------------------------------------------------------------------------------------------------------------------------------------------------


$5&


627.

Oou Oou are to determine the maimum fuel load which can be carried in the following conditions ; - drD operating mass I $5!! 4g - trip fuel I "!! 4g - traffic load I +!! 4g - maimum ta4e-off mass I +$!! 4g - maimum landing mass I "&!! 4g 5!! 4g a) ,!! 4g b) c) #!!! 4g &!! 4g d)

Answer ; a)

5!! 4g ----------------------------------------------------------------------------------------------------------------------------------------------------------------Oou Oou ha8e a flight plan 0F) from Amsterdam to 7ondon. 0n the flight plan it is noted that Dou will de8iate from the AT1 AT1 route 628. passing the F0) boundarD Amsterdam7ondon. The The airwaD clearance reads @ Cleared Cleared to 7ondon 8ia flight planned route.
The route according to the flight plan is accepted. ----------------------------------------------------------------------------------------------------------------------------------------------------------------Oou Oou must flD 0F) on an airwaD orientated #",B magnetic with a 1A at &5!! ft. /nowing the J92 is #!$, h'a and the 629. temperature is 01A E #!B@ the minimum flight le8el Dou must flD at is ; 6! a) b) &, 5! c) &! d)

Answer ; a)

6! -----------------------------------------------------------------------------------------------------------------------------------------------------------------


$55


Flight Planning _ Monitoring ( 629 Soru OK.b )

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