033 - flight planning & flight monitoring

8/13/2019 033 - Flight Planning & Flight Monitoring

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FLIGHT PLANNING AND FLIGHT MONITORINGsubj Domanda RispostaA RispostaB RispostaC RispostaD Chec

033 An aircraft is flying at MACH 0.84 at FL 330. The static air temperature is -48C an thehea!in c"mp"nent #$ %t. At &338 'TC the c"ntr"ller re(uests the pil"t t" cr"ss themeriian "f 030) at 'TC. *i+en the istance t" g" is #,0 M the reuceMACH ". sh"ul /e

0.80 0.,8 0.,1 0.,$

033 2n a gi+en path it is p"ssi/le t" ch"se /et!een f"ur flight le+els FL each ass"ciate!ith a manat"ry flight Mach um/er M. The flight c"niti"ns static air temperature5AT an hea!in c"mp"nent H)C are gi+en /el"! FL 3,0 - M 6 0.80 Ts 6 -10CH)C 6 - 7t FL 330 - M 6 0.,8 Ts 6 -10C H)C6 - # 7t FL $0 - M 6 0.80 Ts 6-##C H)C 6 - 7t FL $,0 - M 6 0.,1 Ts 6 -43C H)C 6 0 The flight le+el all"!ingthe highest gr"un spee is

FL$,0 FL$0 FL330 FL3,0

033A pu/lic transp"rt aer"plane !ith recipr"cating engines the final reser+e sh"ul /e fuel t" fly f"r 4# minutes fuel t" fly f"r $ h"urs fuel t" fly f"r & h"ur at h"ling speefuel t" fly f"r 30 minutes at h"lingspee

033 9n a flight plan !hen the estinati"n aer"r"me is A an the alternate aer"r"me is : thefinal reser+e fuel f"r a tur/";et engine aer"plane c"rresp"ns t"

30 minutes h"ling feeta/"+e aer"r"me :

30 minutes h"ling $000 feet a/"+eaer"r"me :

minutes h"ling $000 feet a/"+eaer"r"me A

30 minutes h"ling feeta/"+e aer"r"me A

033 The Trip Fuel f"r a ;et aer"plane t" fly fr"m the eparture aer"r"me t" the estinati"naer"r"me is # 3#0 7g. Fuel c"nsumpti"n in h"ling m"e is 1 000 7gi fuel 100 7g Fuel fl"! f"r cruise &0 0007gperiences a hea!in c"mp"nent 6 10 7t. The!in remains c"nstant. The urati"n "f the flight !ill /e

$h 3#min 3h 00min $h &0min $h 3$min

033 2n an ATC flight plan y"u are re(uire t" inicate in the /"> mar7e spee theplanne spee f"r the first part "f the cruise "r f"r the entire cruise. This spee is

The true airspee The e(ui+alent airspee The inicate airspee The estimate gr"un spee

033 F"ll"!ing in-flight epressurisati"n a tur/ine p"!ere aer"plane is f"rce t" i+ert t" anen-r"ute alternate airfiel. 9f actual flight c"niti"ns are as f"recast the minimum(uantity "f fuel remaining "n arri+al at the airfiel !ill /e

at least e(ui+alent t" 30 minutesflying time

at least e(ui+alent t" the (uantityre(uire t" fly t" an"ther aer"r"me inthe e+ent that !eather c"niti"ns s"re(uire

lai "!n /y the "perat"r !ith the(uantity /eing specifie in the"perating manual

at least e(ui+alent t" 4# minutesflying time

033 During a flight at night a p"siti"n has t" /e rep"rte t" ATC. The aer"plane is at aistance "f ,#0 M fr"m the gr"un stati"n an at flight le+el 3#0. The fre(uency t" /euse is

#14 7HE. &&331 7HE. &,$81 7HE. &$3. MHE.

033 An aer"plane has the f"ll"!ing masses @5TL)T6 #0 000 7g Trip fuel6 4 300 7gC"ntingency fuel6 $ 7g Alternate fuel final reser+e inclue6 $ &007g Ta>i6 #00 7g:l"c7 fuel6 , & 7g :ef"re eparture the captain "rers t" ma7e the /l"c7 fuel 0007g. The trip fuel in the "perati"nal flight plan sh"ul rea

4 300 7g. 1 &8# 7g. 000 7g. 1 400 7g.

033 Acc"ring t" the chart the minimum "/structi"n clearance altitue M2CA is 8#00 ft.The mete"r"l"gical ata gi+es an "utsie air temperature "f -$0C at FL 8#. The Hgi+en /y a met. stati"n at an e le+ati"n "f 4000ft is &003 h?a. )hat is the minimum

8800 ft. 8#00 ft. &$800 ft. 8$00 ft.


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pressure altitue !hich sh"ul /e fl"!n acc"ring t" the gi+en M2CA=

033 During a flight the fuel inicat"rs sh"! that the remaining am"unt "f fuel is &00 l/s after38 minutes. The t"tal am"unt "f fuel at eparture !as &10 l/s. F"r the alternate fuel 30l/s is necessary. The planne fuel f"r ta>i is &3 l/s. Final reser+e fuel is estimate at #0l/s. 9f the fuel fl"! remains the same h"! many minutes can /e fl"!n t" the estinati"n!ith the remaining fuel=

&$ minutes. 13 minutes. 44 minutes. 4 minutes.

033 During an 9F flight TA5 an time appear t" e+iate fr"m the ata in the ATC flightplan. The minimum e+iati"ns that sh"ul /e rep"rte t" ATC in "rer t" c"nf"rm t"?A5-AC are

TA5 #G an t ime 3 minutes. TA5 3G an t ime 3 minutes . TA5 # 7t an t ime # minutes . TA5 &0 7t an t ime $ minu tes.

033 H"! many h"urs in a+ance "f @2:T sh"ul a ATC flight plan /e file in the case "f

flights int" areas su/;ect t" air traffic fl"! management ATFM=

300 h"urs. &00 h"ur. 030 h"urs. $ h"urs.

033 A current flight plan is a file flight plan !ith amenmentsan clearance inclue.

file flight plan. flight plan !ith the c"rrect time "feparture.

flight plan in the c "urse "f !hichrai" c"mmunicati"n sh"ul /e

practise /et!een aer"plane anATC.

033)hich "f the f"ll"!ing statements regaring filing a ATC flight plan is c"rrect= 9n case "f ATFM Air Traffic Fl"!Management the flight plansh"ul /e file at least three h"ursin a+ance "f the @2:T.

Any flight plan sh"ul /e file at least&0 minutes /ef"re eparture.

A flight plan sh"ul /e file !hen anati"nal F9 /"unary !ill /ecr"sse.

A flying c"llege can file repetiti+eflight plan f"r F flights.

033 An aircraft is "n an 9F flight. The flight is t" /e change fr"m 9F t" F. 9s itp"ssi/le=

Ies the pil"t in c"mman mustinf"rm ATC using the phrasecancelling my 9F flight.

" y"u ha+e t" remain 9F inacc"rance t" the file flight plan.

" "nly ATC can "rer y"u t" "this.

Ies /ut "nly !ith permissi"n fr"mATC.

033 I"u ha+e an ATC flight plan 9F fr"m Amsteram t" L"n"n. 9n the flight plan it isn"te that y"u !ill e+iate fr"m the AT5 r"ute passing the F9 /"unaryAmsterami fuel trip fuelc"ntingency fuel an fuel t" fly f"r

4# minutes at h"ling spee at 4#0m a/"+e aer"r"me ele+ati"n instanar c"niti"ns

$ h"urs at n"rmal cruise c"nsumpti"n 4# minutes plus G "f the flighttime planne t" /e spent at cruisingle+el "r t!" h"urs !hiche+er is less

4# minutes at h"ling spee at 4#0m a/"+e M5L in stanarc"niti"ns

033F flights shall n"t /e fl"!n "+er the c"ngeste areas "f cities at a height less than &000 ft a/"+e the highest "/stacle!ithin a raius "f 100 m fr"m theaircraft.

$000 ft a/"+e the highest "/stacle!ithin a raius "f 100 ft fr"m theaircraft.

#00 ft a/"+e the highest "/stacle. the highest "/stacle.

033 H"! many feet y"u ha+e t" clim/ t" reach FL ,#= *i+en FL ,#J eparture aer"r"meele+ati"n ftJ H 6 &0$3 h?aJ temperature 6 95AJ & h?a 6 30 ft

1300 ft. 1000 ft. 1100 ft. ,800 ft.

033 The re(uire time f"r final reser+e fuel f"r tur/";et aer"plane is 30 min. 4# min. 10 min. aria/le !ith !in +el"city.

033 *i+en Dry "perating mass D2M6 33#&0 7g Traffic L"a6 ,100 7g Final reser+e fuel683 7g Alternate fuel6 &&00 7g C"ntingency fuel &0$ 7g The estimate laning mass at

alternate sh"ul /e

4$ 7g. 4$03 7g. 4$$&0 7g. 4$3&$ 7g.

033 *i+en Dry "perating mass D2M6 33000 7g Traffic L"a6 8&&0 7g Final reser+e fuel683 7g Alternate fuel6 &&00 7g C"ntingency fuel &0$ 7g The estimate laning mass atalternate sh"ul /e

4$ 7g. 4&&&0 7g. 4$$&0 7g. 4$3&$ 7g.

033 *i+en Dry "perating mass D2M6 33#&0 7g Traffic L"a6 ,100 7g Trip fuel TF6$040 7g Final reser+e fuel6 83 7g Alternate fuel6 &&00 7g C"ntingency fuel6 #G "ftrip fuel )hich "f the liste estimate masses is c"rrect=

@stimate laning mass atestinati"n6 43$# 7g.

@stimate ta7e-"ff mass6 4#$33 7g. @stimate laning mass atestinati"n6 43&3 7g.

@stimate ta7e-"ff mass6 43$# 7g.

033 *i+en Fuel ensity 6 0,8 7gimum all"!a/le ta7e-"ff mass 6 11$00 7g Ta>i fuel 6 $00 7g Tan7 capacity 6 $$#00 Litres The ma>imum p"ssi/le ta7e-"ff fuel is

&, 3#0 7g $$ &00 7g &, ##0 7g $& 00 7g

033 The (uantity "f fuel !hich is calculate t" /e necessary f"r a ;et aer"plane t" fly 9Ffr"m eparture aer"r"me t" the estinati"n aer"r"me is #3#$ 7g. Fuel c"nsumpti"n inh"ling m"e is 1 000 7g


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"ff=

033 The f"ll"!ing fuel c"nsumpti"n figures are gi+en f"r a ;et aer"plane -stanar ta>i fuel100 7g. -a+erage cruise c"nsumpti"n &0 000 7gture rich.

1 '5 gall"n '5 gall"n &$ '5 gall"n 3 '5 gall"n

033 F"r this (uesti"n use anne> 033-330$A "r Flight ?lanning Manual M@?& Figure 3.1 Aflight is t" /e mae t" an airp"rt pressure altitue 3000 ft in a multi e ngine pist"naer"plane M@?&. The f"recast 2AT f"r the airp"rt is -& C. The cruising le+el !ill /eFL &&0 !here 2AT is -&0 C. Calculate the still air escent istance f"r &4# %9A5 ate"f escent &000 ft 033-3301A "r Flight ?lanning Manual MKT & Figure4.#.3.& *i+en flight time fr"m t"p "f clim/ t" the enr"ute p"int in FL$80 is 48 min.Cruise pr"ceure is l"ng range cruise LC. Temp. 95A -# C Ta7e-"ff mass #1 000 7gClim/ fuel & &00 7g Fin istance in nautical air miles AM f"r this leg an fuelc"nsumpti"n

34# AMJ $000 7g 3#0 AMJ $000 7g 34# AMJ $&00 7g 43, AMJ $&00 7g

033 F"r this (uesti"n use anne> 033-330,A "r Flight ?lanning Manual MKT & Figure 4.#.&*i+en estimate ta7e-"ff mass #, #00 7gJ initial cruise FL $80J a+erage temperatureuring clim/ 95A -&0CJ a+erage hea !in c"mp"nent &8 7t Fin clim/ time

&3 min && min min &4 min

033 F"r this (uesti"n use anne>es 033-3308A "r Flight ?lanning Manual MKT & Figure

4.#.& *i+en /ra7e release mass #, #00 7g temperature 95A -&0CJ hea !inc"mp"nent &1 7t initial FL $80 Fin still air istance AM an gr"un istance Mf"r the clim/

1$ AMJ # M # AMJ1$ M 1, AMJ ,& M ,& AMJ1, M

033 F"r this (uesti"n use anne> 033-330A "r Flight ?lanning Manual MKT & Figure 4.#.&*i+en mass at /ra7e release #, #00 7gJ temperature 95A -&0CJ a+erage hea !inc"mp"nent &1 7t initial cruise FL $80 Fin clim/ fuel

&&38 7g &$38 7g &38, 7g &040 7g

033 *i+en true c"urse TC 0&,J ) 033-33&$A "r "ute Manual chart @H94 CAA-@iti"n Anaer"plane has t" fly fr"m A//e+ille #008.&B 00&.3B@ t" :iggin #&&.8B0000.$B@. )hat is the first FL a/"+e FL$# that can /e fl"!n "n an 9F flight plan =

FL 3&0 FL 330 FL 3$0 FL 300


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033 F"r this (uesti"n use anne> 033-33&3A "r "ute Manual chart @H94 CAA-@iti"n Anaircraft has t" fly fr"m A//e+ille #008.&B 00&.3B@ t" :iggin #&&.8B00000.$B@. )hat is the istance "f this leg =

&00 M 38 M 14M 1$M

033 F"r this (uesti"n use anne> 033-33&4A "r "ute Manual chart @H94 CAA-@iti"n Anaircraft has t" fly fr"m A//e+ille #008.&B 00&.3B@ t" :iggin #&&.8B0000.$B@. At :iggin y"u can fin &4&. This is

The magnetic c"urse fr"m :iggint" A//e+ille.

The magnetic c"urse t" fly in/"un t":iggin.

The a+erage true c"urse "f the greatcircle fr"m :iggin t" A//e+ille.

The raial reference t" true n"rth"f :iggin t" fly in/"un.

033 F"r this (uesti"n use anne> 033-33A "r "ute Manual chart @H94 CAA-@iti"n Anaircraft has t" fly fr"m 5alE/urg 4800.$B 0&$#3.1B@ t" %lagenfurt 413,.#B0&433.8B@. )hich statement is c"rrect =

The air!ay ':# can /e use f"rflights t"


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G p"!er.

033 'nless "ther!ise sh"!n "n charts f"r stanar instrument eparture the r"utes are gi+en!ith

magnetic c"urse magnetic heaings true c"urse true heaings

033 Flight planning chart f"r an aircraft states that the time t" reach the cruising le+el at agi+en gr"ss mass is 31 minutes an the istance tra+elle is , M Eer"-!in. )hat!ill /e the istance tra+elle !ith an a+erage tail!in c"mp"nent "f 107t =

&3 M &$8 M , M $$8 M

033 I"u are flying a c"nstant c"mpass heaing "f $#$. ariati"n is $$@ e+iati"n is 3)an y"ur 95 is sh"!ing a rift "f right. True trac7 is =

$80 $$4 $4$ $1$

033 The purp"se "f the ecisi"n p"int pr"ceure is t" reuce the minimum re(uirefuel an theref"re /e a/le t"

increase the traffic l"a.

t" reuce the laning !eight an thusreuce the structural stress "n the

aircraft.

t" increase the safety "f the flight. t" increase the am"unt "f e>tra fuel.

033 )hen using ecisi"n p"int pr"ceure y"u reuce the c"ntingency fuel /y aingc"ntingency "nly fr"m the /urn"ff

/et!een ecisi"n p"int anestinati"n.

c"ntingency fuel /y aing c"ntingency"nly fr"m the /urn"ff /et!een theecisi"n airp"rt an estinati"n.

reser+e fuel fr"m &0G "!n t" #G. h"ling fuel /y 30G.

033 9f CA5 is &0 7ts Altitue 000 ft. Temp. 95A - &0C True C"urse TC 3#0 ) 033-30,A "r "ute Manual chart 5TA L2D2Heathr"! &0-$ ?lanning a 9F flight fr"m ?aris Charles e *aulle t" L"n"nHeathr"!. Fin the ele+ati"n "f the estinati"n aer"r"me.

80 ft. ,, ft. &,, ft. &00 ft.

033 F"r this (uesti"n use anne> 033-308A "r "ute Manual chart @H94 CAA-@iti"n?lanning a 9F flight fr"m ?aris Charles e *aulle 4 00. @00$ 31. t" L"n"nHeathr"! #& $.$ )000 $,.. Fin the a+erage true c"urse fr"m ?aris t" L"n"n.

3$$. &4$. 330. 343.

033 F"r this (uesti"n use anne> 033-30A "r "ute Manual chart @H94 CAA-@iti"n?lanning a 9F flight fr"m ?aris Charles e *aulle 4 00. @00$ 31. t" L"n"nHeathr"! #& $.$ )000 $,.. Determine the preplanning istance /y calculating theirect istance plus &0G. The preplanning istance is

$0, M. &88 M. 308 M. $&8 M.

033 F"r this (uesti"n use anne> 033-3&0A "r Flight ?lanning Manual MKT & Figure 4.4?lanning a flight fr"m ?aris Charles e *aulle t" L"n"n Heathr"! f"r a t!in - ;etaer"plane. ?replanning Dry 2perating Mass D2M 34 000 7g Traffic L"a &3 000 7gThe h"ling is planne at & #00 ft a/"+e alternate ele+ati"n. The alternate ele+ati"n is$#1 ft. The h"ling is planne f"r 30 minutes !ith n" reucti"ns. Determine the@stimate Laning Mass at alternate Manchester.

48 &$# 7g. 4 $#0 7g. $ $#0 7g. 48 1,# 7g.

033 F"r this (uesti"n use anne>es 033-3&&A an 033-3&&: "r "ute Manual chart @H94CAA-@iti"n an Flight planning manual Figure 4.3.1 ?lanning a flight fr"m ?arisCharles e *aulle 4 00. @00$ 31. t" L"n"n Heathr"! #& $.$ )000 $,. f"ra t!in - ; et aer"plane. The alternate airp"rt is Manchester #3 $&.4 )00$ .,?replanning The !in fr"m L"n"n t" Manchester is $#0es 033-3&$A an 033-3&$: "r "ute Manual chart @H94CAA-@iti"n an Flight planning manual Figure 4.3.$A ?lanning a flight fr"m ?arisCharles e *aulle 4 00. @00$ 31. t" L"n"n Heathr"! #& $.$ )000 $,. f"ra t!in - ; et aer"plane. ?replanning ?"!er setting Mach6 0.,4 ?lanne flight le+el FL

& ,40 7g. & ##0 7g. & 00 7g. & 4#0 7g.


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$80 The Laning Mass in the fuel graph is #0 000 7g The trip istance use f"rcalculati"n is $00 M The !in fr"m ?aris t" L"n"n is $80imum er" Fuel Mass#& $#0 7g Ma>imum Laning Mass #4 00 7g Ma>imum Ta>i Mass 13 0#0 7g Assumethe f"ll"!ing preplanning results Trip fuel & 800 7g Alternate fuel & 400 7g H"lingfuel final reser+e & $$# 7g Dry 2perating Mass 34 000 7g Traffic L"a &3 000 7gCatering ,#0 7g :aggage 3 #00 7g Fin the Ta7e-"ff Mass T2M

#& # 7g. ## ,1# 7g. #& 4$# 7g. #$ $1# 7g.

033 F"r this (uesti"n use anne> 033-41&1A "r Flight ?lanning Manual MKT & Figure 4.3.19n "rer t" get alternate fuel an time the t!in -;et aer"plane "perati"ns manual graphshall /e entere !ith

Distance M !in c"mp"nentlaning mass at alternate.

5till air istance !in c"mp"nent Eer"fuel mass.

Flight time !in c "mp"nentlaning mass at alternate.

Distance M !in c "mp"nentEer" fuel mass.

033 The na+igati"n plan reas Trip fuel &00 7g Flight time &h3#min Ta>i fuel 3 7g :l"c7fuel &8& 7g The enurance "n the 9CA2 flight plan sh"ul rea

$h 4min &h 3#min $h 04min $h #$min

033 The na+igati"n plan reas Trip fuel &31 7g Flight time $h4#min Calculate reser+efuel 30G "f trip fuel Fuel in tan7 is minimum n" e>tra fuel "n /"ar Ta>i fuel 3 7gThe enurance "n the 9CA2 flight plan sh"ul rea

3h34min $h4#min $h4min 3h38min

033 F"r a planne flight the calculate fuel is as f"ll"!s Flight time 3h01min The reser+efuel at any time sh"ul n"t /e less than 30G "f the remaining trip fuel. Ta>i fuel 8 7g:l"c7 fuel &&8 7g H"! much fuel sh"ul remain after $ h"urs flight time=

30 7g trip fuel an 7g reser+efuel.

3 7g trip fuel an &$ 7g reser+e fuel. $, 7g trip fuel an &$ 7g reser+efuel.

3 7g trip fuel an n" reser+e fuel.

033 F"r a planne flight the calculate fuel is as f"ll"!s Flight time $h4$min The reser+efuel at any time sh"ul n"t /e less than 30G "f the remaining trip fuel. Ta>i fuel 7g:l"c7 fuel &31 7g H"! much fuel sh"ul remain after $ h"urs flight time=

$# 7g trip fuel an 8 7g reser+efuel.

33 7g trip fuel an &0 7g reser+e fuel. $3 7g trip fuel an &0 7g reser+efuel.

33 7g trip fuel an n" reser+e fuel.

033 Minimum planne ta7e-"ff fuel is &10 7g 30G t"tal reser+e fuel is inclue. Assumethe gr"unspee "n this trip is c"nstant. )hen the aircraft has "ne half the istance theremaining fuel is ,0 7g. 9s i+ersi"n t" a near/y alternate necessary=

Di+ersi"n t" a near/y alternate isnecessary /ecause the remainingfuel is n"t sufficient.

Di+ersi"n t" a near/y alternate is n"tnecessary /ecause the reser+e fuel hasn"t /een use c"mpletely.

Di+ersi"n t" a near/y alternate is n"tnecessary /ecause it is all"!e t"calculate !ith"ut reser+e fuel.

Di+ersi"n t" a near/y alternate isnecessary unless the captainecies t" c"ntinue "n his "!n

resp"nsi/ility.033 F"r this (uesti"n use anne> 033-41$$A "r Flight ?lanning Manual M@? & Figure 3.3 A

flight has t" /e mae !ith a multi engine pist"n aer"plane M@? &. F"r the fuelcalculati"ns ta7e # '5 gall"ns f"r the ta>i an an aiti"nal &3 minutes at cruisec"niti"n t" acc"unt f"r clim/ an escent. Calculate time fr"m "+erhea t" "+erhea is&h4,min. ?"!er setting is 4#G $100 ?M. Calculate reser+e fuel is 30G "f the tripfuel. FL &00. Temperature -#C. Fin the minimum /l"c7 fuel.

4, '5 gall"ns. 3, '5 gall"ns. 10 '5 gall"ns. 4,0 '5 gall"ns.

033 F"r this (uesti"n use anne> 033-41$3A "r Flight ?lanning Manual M@? & Figure 3.3 Aflight has t" /e mae !ith a multi engine pist"n aer"plane M@? &. F"r the fuelcalculati"ns ta7e # '5 gall"ns f"r the ta>i an an aiti"nal &3 minutes at cruisec"niti"n t" acc"unt f"r clim/ an escent. Calculate time "+erhea t" "+erhea is$h3,min. ?"!er setting is 1#G $#00 ?M. Calculate reser+e fuel is 30G "f the tripfuel. FL &$0. Temperature &C. Fin the minimum /l"c7 fuel.

& '5 gall"ns. 81 '5 gall"ns. ,1 '5 gall"ns. &&8 '5 gall"ns.

033 F"r this (uesti"n use anne> 033-4,3#A "r Flight ?lanning Manual 5@? & Figure $.#*i+en FL ,# Lean mi>ture Full thr"ttle $300 ?M Ta7e-"ff fuel 444 l/s Ta7e-"ff fr"m

M5L Fin @nurance in h"urs.

0#&$ 0#$0 044$ 0#$3

033 F"r this (uesti"n use anne> 033-4,31A "r Flight ?lanning Manual 5@? & Ta/le $.$.3*i+en FL ,# 2AT &0C Lean mi>ture $300 ?M Fin Fuel fl"! in gall"ns per h"ur*?H an TA5.

&&.1 *?H TA5 &10 7t &&.1 *?H TA5 &43 7t ,&.& *?H TA5 &43 7t 18.# *?H TA5 &10 7t

033 F"r this (uesti"n use anne> 033-4,3,A "r Flight ?lanning Manual 5@? & Figure $.&*i+en FL ,# 2AT #C During clim/ a+erage hea !in c"mp"nent $0 7t Ta7e-"fffr"m M5L !ith the initial mass "f 3 1#0 l/s. Fin Time an fuel t" clim/.

min. 33 '5* &0 min. 31 '5* , min. $1 '5* min. $, '5*

033 F"r this (uesti"n use anne> 033-4,38A "r Flight ?lanning Manual 5@? & Figure $.&*i+en FL ,# 2AT #C During clim/ a+erage hea !in c"mp"nent $0 7t Ta7e-"fffr"m M5L !ith the initial mass "f 3 1#0 l/s. Fin 5till air istance AM an gr"unistance M using the graph time fuel istance t" clim/.

&8 AM. M. &1 AM. &8 M. &8 AM. &3 M. &4 AM. &8 M.

033 9ntegrate range cur+es "r ta/les are presente in the Aer"plane 2perati"ns Manuals.Their purp"se is

t" etermine the fuel c "nsumpti"nf"r a certain still air istancec"nsiering the ecreasing fuel

t" etermine the flight time f"r a certainleg uner c"nsierati"n "f temperaturee+iati"ns.

t" etermine the still air istance f"ra !in c"mp"nents +arying !ithaltitue.

t" etermine the "ptimum speec"nsiering the fuel c"st as !ell asthe time relate c"st "f the


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fl"! !ith ecreasing mass. aer"plane.

033 F"r this (uesti"n use anne> 033-#43A "r Flight ?lanning Manual MKT & Figure 4.4The final reser+e fuel ta7en fr"m the H2LD9* ?LA9* ta/le f"r the t!in ;etaer"plane is /ase "n the f"ll"!ing parameters

pressure altitue aer"plane massan flaps up !ith minimum ragairspee

pressure altitue aer"plane mass anflaps "!n !ith ma>imum range spee

pressure altitue aer"plane mass anflaps up !ith ma>imum range spee

pressure altitue aer"plane massan flaps "!n !ith minimum ragairspee

033F"r fl ight planning purp"ses the laning mass at alternate is ta7en as er" Fuel Mass plus Final eser+eFuel.

Laning Mass at estinati"n plusAlternate Fuel.

er" Fuel Mass plus Final eser+eFuel an Alternate Fuel.

er" Fuel Mass plus Final eser+eFuel an C"ntingency Fuel.

033 F"r this (uesti"n use anne> 033-#41A "r Flight ?lanning Manual MKT & Figure 4.3.19n "rer t" fin ALT@AT@ F'@L an T9M@ T2 ALT@AT@ the A@2?LA@2?@AT9* MA'AL shall /e entere !ith

istance in nautical miles M!in c"mp"nent laning mass atalternate

istance in nautical air miles AM!in c"mp"nent laning mass atalternate

istance in nautical miles M!in c"mp"nent Eer" fuel mass

istance in nautical miles M!in c"mp"nent ry "peratingmass plus h"ling fuel

033 T he final re ser+e fuel f"r ae r"planes !ith tur/ine engines is fuel t" fly f"r 30 minute s a t

h"ling spee at ft 4#0 ma/"+e aer"r"me ele+ati"n instanar c"niti"ns.

fuel t" fly f"r 4# minutes at h"ling

spee at ft 4#0 m a/"+eaer"r"me ele+ati"n in stanarc"niti"ns.

fuel t" fly f"r 4# minutes at h"ling

spee at &000 ft 300 m a/"+eaer"r"me e le+ati"n in stanarc"niti"ns.

fuel t" fly f"r 10 minutes at h"ling

spee at ft 4#0 m a/"+eaer"r"me ele+ati"n in stanarc"niti"ns.

033 )hich "f the f"ll"!ing statements is rele+ant f"r f"rming r"ute p"rti"ns in integraterange flight planning=

The istance fr"m ta7e-"ff up t"the t"p "f clim/ has t" /e 7n"!n.

" segment shall /e m"re than 30minutes "f flight time.

@ach rep"rting p"int re(uires a ne!segment.

A small change "f temperature $C can i+ie a segment.

033 F"r this (uesti"n use anne> 033-##0A "r Flight ?lanning Manual MKT & Figure 4.$.$Fin the 5H2T D95TAC@ C'95@ ALT9T'D@ f"r the t!in ;et aer"plane. *i+en:ra7e release mass64#000 7g Temperature695A $0C Trip istance6#0 autical AirMiles AM

&0000 ft ,#00 ft &$#00 ft &&000 ft

033 F"r this (uesti"n use anne> 033-##&A "r Flight ?lanning Manual MKT & Figure 4.$.$Fin the 5H2T D95TAC@ C'95@ ALT9T'D@ f"r the t!in ;et aer"plane. *i+en:ra7e release mass640000 7g Temperature695A $0C Trip istance6 auticalAir Miles AM

30000 ft $#000 ft $&000 ft $,#00 ft

033 F"r this (uesti"n use anne> 033-##$A "r Flight ?lanning Manual MKT & Figure 4.$.&Fin the 2?T9M'M ALT9T'D@ f"r the t!in ;et aer"plane. *i+en Cruise mass6#40007g L"ng range cruise "r .,4 MACH

34#00 ft 33800 ft 3#300 ft ma>imum "perating altitue

033 F"r this (uesti"n use anne> 033-##3A "r Flight ?lanning Manual MKT & Figure 4.$.&Fin the 2?T9M'M ALT9T'D@ f"r the t!in ;et aer"plane. *i+en Cruise mass6#00007g .,8 MACH

3##00 ft 31$00 ft 31,00 ft ma>imum "perating altitue

033 F"r this (uesti"n use anne>es 033-##4A an 033-##4: "r Flight ?lanning ManualMKT & ?aragraph $.& an Figure 4.$.& Fin the F'@L M9L@A*@ ?@ALTI f"r thet!in ;et aer"plane !ith regar t" the gi+en FL9*HT L@@L . *i+en L"ng range cruiseCruise mass6#3000 7g FL 3&0

4 G & G &0 G 0 G

033 F"r this (uesti"n use anne> 033-##1A "r Flight ?lanning Manual MKT & Figure 4.&4Fin the 5?@C9F9C A*@ f"r the t!in ;et aer"plane flying /el"! the "ptimum altituerange l"ss 6 1G an using the f"ll"!ing ata. *i+en MACH .,4 C'95@ Flight le+el6 3&0 *r"ss mass 6 #0000 7g 95A c"niti"ns

&,1 AM


8/30


l"ng range cruise pr"ceure !hat fuel is re(uire=

033 Fin the istance fr"m !ayp"int 3 )? 3 t" the critical p"int. *i+en istance fr"m )?3 t" )? 4 6 ,#0 M TA5 "ut 430 7t TA5 return 4$# 7t Tail!in c"mp"nent "ut 30 7thea !in c"mp"nent return 40 7t

34$ M 3,# M 408 M 403 M

033 F"r this (uesti"n use anne> 033-#14A "r Flight ?lanning Manual MKT & Figure 4.#.&Fin Time Fuel 5till Air Distance an TA5 f"r an enr"ute clim/ $80imum usea/le fuel 7gMinimum reser+e fuel 3#00 7g TA5 "ut 4$# 7t Hea !in c"mp"nent "ut 30 7t TA5return 430 7t Tail!in c"mp"nent return $0 7t A+erage fuel fl"! $ 7g 033-#,&A "r Flight ?lanning Manual MKT & Figure4.#.3.& Fin Final fuel c"nsumpti"n f"r this leg *i+en L"ng range cruise Temperature-13C FL 330 9nitial gr"ss mass enr"ute #4&00 7g Leg flight time $ min

&03 7g &&0, 7g &&00 7g &000 7g

033 F"r this (uesti"n use anne> 033-#,$A "r Flight ?lanning Manual MKT & Figure4.#.3.& Fin Air istance in autical Air Miles AM f"r this leg an fuelc"nsumpti"n *i+en Flight time fr"m t"p "f clim/ at FL $80 t" the enr"ute p"int is 48minutes. Cruise pr"ceure is l"ng range cruise. Temperature is 95A -#C. The ta7e-"ffmass is #1000 7g an clim/ fuel &&00 7g.

34# AMJ &4 7g 34 AMJ $000 7g 34# AMJ $000 7g 34# AMJ $001 7g

033 F"r this (uesti"n use anne> 033-#,3A "r Flight ?lanning Manual MKT & Figure 4.#.&*i+en :ra7e release mass #,#00 7g 9nitial FL $80 a+erage temperature uring clim/95A -&0C a+erage hea !in c"mp"nent &8 7t Fin Clim/ time f"r enr"ute clim/$80 033-#,4A "r Flight ?lanning Manual MKT & Figure 4.#.&*i+en :ra7e release mass #,#00 7g Temperature 95A -&0C Hea!in c"mp"nent &17t 9nitial FL $80 Fin 5till air istance AM an gr"un istance M f"r theenr"ute clim/ $80 033-#,#A "r Flight ?lanning Manual MKT & Figure 4.#.&*i+en :ra7e release mass #,#00 7g Temperature 95A -&0C A+erage hea!inc"mp"nent &1 7t 9nitial FL $80 Fin Clim/ fuel f"r enr"ute clim/ $80 033-#,1A "r "ute Manual chart @H9# CAA-@iti"n*i+en Leg M"ulins41 4$.4 @003 38.0pecte true air spee

$#000 ft 43# 7t $4000 ft 44# 7t 33#00 ft 430 7t 3300 ft 4$0 7t

033 F"r this (uesti"n use anne> 033-1&A "r Flight ?lanning Manual MKT & Figure4.#.3.& *i+en t!in ;et aer"plane FL 330 L"ng range cruise 2utsie air temperature-13C *r"ss mass #0#00 7g Fin True air spee TA5

4$0 7t 433 7t 43& 7t 4&8 7t

033 *i+en Ma>imum all"!a/le ta7e-"ff mass 14400 7g Ma>imum laning mass #1$00 7gMa>imum Eer" fuel mass #3000 7g Dry "perating mass 3##00 7g Traffic l"a &4#007g Trip fuel 400 7g Minimum Ta7e-"ff Fuel ,400 7g Fin Ma>imum all"!a/le ta7e-"ff fuel

&&&00 7g &&400 7g &4400 7g 8100 7g

033 *i+en Ma>imum all"!a/le ta7e-"ff mass 14400 7g Ma>imum laning mass #1$00 7gMa>imum Eer" fuel mass #3000 7g Dry "perating mass 3##00 7g Traffic l"a &4#007g Trip fuel 400 7g Ta7e-"ff fuel ,400 7g Fin Ma>imum aiti"nal l"a

3000 7g 4000 7g ,000 7g #100 7g

033 F"r this (uesti"n use anne>es 033-14A an 033-14: "r Flight ?lanning ManualMKT & Figure 4.#.3.& an Figure 4.3.&: *i+en t!in ;et aer"plane er" fuel mass#0000 7g Laning mass at alternate #$000 7g Final reser+e fuel $000 7g Alternate fuel

4800 7g 0& h #& min 4400 7g 0$ h 0# min 4,#0 7g 0$ h 00 min 4100 7g 0$ h 0# min


9/30


&000 7g Flight t" estinati"n Distance ,$0 M True c"urse 030 ) 033-,0$A "r "ute Manual 59D chart $0-3 f"r ?A95Charles-e-*aulle ?lanning an 9F-flight fr"m ?aris t" L"n"n. Determine the istance"f the eparture r"ute A:: 8A.

,4.# M ,$.# M #1 M 83 M

033 F"r this (uesti"n use anne> 033-,03A "r "ute Manual 59D chart $0-3 f"r ?A95Charles-e-*aulle ?lanning an 9F-flight fr"m ?aris Charles e *aulle )I $, t"L"n"n. *i+en Distance fr"m ?A95 Charles-e-*aulle t" t"p "f clim/ #0 MDetermine the istance fr"m the t"p "f clim/ T2C t" A:: &&1.1.

$4.# M 33 M 31.# M 3& M

033 F"r this (uesti"n use anne> 033-,04A "r Flight ?lanning Manual MKT & Figure4.#.4 ?lanning an 9F-flight fr"m ?aris t" L"n"n f"r the t!in ;et aer"plane. *i+en@stimate Laning Mass 4,00 7g FL $80 )


10/30


033 F"r this (uesti"n use anne>es 033-,0,A 033-,0,: "r "ute Manual chart @H94CAA-@iti"n 9nstrument appr"ach chart L2D2 Heathr"! 9L5 DM@ !y $,?lanning an 9F-flight fr"m ?aris t" L"n"n Heathr"! +ia initial appr"ach fi> 9AF:iggin 2 . *i+en istance fr"m t"p "f escent T2D t" !y $, is ,1 MDetermine the istance fr"m A:: &&1.1 t" T2D.

4 M 10 M &00 M ## M

033 F"r this (uesti"n use anne> 033-,08A "r Flight ?lanning Manual MKT & Figure4.#.3.$ ?lanning an 9F-flight fr"m ?aris t" L"n"n f"r the t!in ;et aer"plane. *i+en*r"ss mass #0000 7g FL $80 95A De+iati"n -&0C Cruise pr"ceure Mach 0.,4Determine the TA5

430 7t 440 7t 4$, 7t 4&, 7t

033 F"r this (uesti"n use anne> 033-,0A "r 59D chart ?aris Charles e *aulle $0-3 ?lanning an 9F-flight fr"m ?aris Charles e *aulle t" L"n"n. 59D is A:: 8A. Assume

ariati"n 3 ) TA5 4307ts ) 033-,A "r Flight ?lanning Manual 5@? & Figure $.&*i+en Ta7e-"ff mass 3#00 l/s eparture aer"r"me pressure altitue $#00 ft 2AT

&0C First cruising le+el FL &40 2AT -#C Fin the time fuel an still air istance t"clim/.

$$ min 1., *AL 4# AM $4 min ,., *AL 4, AM &1.# min 4. *AL 34.# AM $3 min ,., *AL #0 AM

033 F"r this (uesti"n use anne> 033-,&1A "r Flight ?lanning Manual 5@? & Figure $.4*i+en Aer"plane mass at start-up 3113 l/s A+iati"n gas"line ensity 1 l/s 033-,$&A A@2A'T9CAL CHAT 9CA2 0005T'TT*AT 2 4, 033-,$3A A@2A'T9CAL CHAT 9CA2 0005T'TT*AT 2 4,


11/30


033 F"r this (uesti"n use anne> 033-,$,A A@2A'T9CAL CHAT 9CA2 0005T'TT*AT 2 4,i 3 minutes an & gall"n "f aiti"nalfuel t" all"! f"r the clim/ &0 minutes an n" fuel c"rrecti"n f"r the escent. ?lanneflight time "+erhea t" "+erhea is 03 h"urs an &$ minutes. eser+e fuel 30G "f thetrip fuel. ?"!er setting is $# in.H* "r full thr"ttle $&00 ?M $0C lean. Flight le+elis ,0 an the 2AT &&C. The minimum /l"c7 fuel is

$83 l/s $18 l/s $#$ l/s $ l/s

033 F"r this (uesti"n use anne> 033-,33A "r Flight ?lanning Manual 5@?& Figure $.$Ta/le $.$.3 A flight has t" /e mae !ith the single engine sample aer"plane. F"r the fuelcalculati"n all"! &0 l/s fuel f"r start up an ta>i 3 minutes an & gall"n "f aiti"nalfuel t" all"! f"r the clim/ &0 minutes an n" fuel c"rrecti"n f"r the escent. ?lanneflight time "+erhea t" "+erhea is 0$ h"urs an 3, minutes. eser+e fuel 30G "f thetrip fuel. ?"!er setting is $3 in.H* "r full thr"ttle $300 ?M $0C lean. Flight le+elis #0 an the 2AT -#C. The minimum /l"c7 fuel is

$1# l/s $08 l/s $,0 l/s $#0 l/s

033 F"r this (uesti"n use anne> 033-,34A A@2A'T9CAL CHAT 9CA2 0005T'TT*AT 2 4, 033-,31A A@2A'T9CAL CHAT 9CA2 0005T'TT*AT 2 4,


12/30


033 F"r this (uesti"n use anne> 033- &00A "r "ute Manual chart @H9# CAA-@iti"n2f the f"ll"!ing the preferre air!ays r"uting fr"m MAT9*'@5 MT* &&,.343$3B 00#0#B@ t" 5T ?@O 5? &&3. 41$8B 001$,B@ a/"+e FL$4# is

':$8$ D* ':41 ':$84 9LA ':$8 ':$8 'A1 L5A '*#$

033 F"r this (uesti"n use anne> 033-&0&A "r "ute Manual chart @H9# CAA-@iti"n2f the f"ll"!ing the preferre air!ays r"uting fr"m AM:295@ AM: &&3., 4,$1B00&04B@ t" A*@ A* 43#3B 000#$B@ a/"+e FL$00 is

'A34 ':& ?29 ': 'H40 F2'C2 'H$0 ?@9C 'A34 ':& C*C 'A$#

033 F"r this (uesti"n use anne> 033- &0$A "r "ute Manual chart @H94 CAA-@iti"n2f the f"ll"!ing the preferre air!ays r"uting fr"m CLACT2 CL &&4.## #&B00&0B@ t" D9AD D9 &&4.3 483#B 00$0#B) a/"+e FL$4# is

':$ LAM '& 2TAC '&4 '&$ M9D 'A4, D?@ 'A4,#52%M' 'H&&&

'&$ M9D '8 5AM ':&&:AL' ')&

':$ LAM '& M9D 'A34L9LA '

033 F"r this (uesti"n use anne> 033- &03A "r "ute Manual chart @H94 CAA-@iti"nThe magnetic c"urse 033- &&008A "r "ute Manual chart @H94 CAA-@iti"nThe rai" na+igati"n ai at '9CH 4,31B 0084B@ is

a 2 "nly fre(uency &.0 MHE a 2


13/30


The rai" na+igati"n ai 5TAD #&4#B 004B@ is

033 F"r this (uesti"n use anne> 033- &&0&0A "r "ute Manual chart @H94 CAA-@iti"nThe rai" na+igati"n ai at CH92**9A 4#04B 0&$&,B@ is a

2 033- &&0&4A "r "ute Manual chart @L2# The 2 an

TACA "n air!ay * at 25A:'C% #$&$B 008&,B@ are

2T fre(uency paire an ha+e

ifferent ientifiers

fre(uency paire an ha+e ifferent

ientifiers

2T fre(uency paire an ha+e the

same ientifier

fre(uency paire an ha+e the

same ientifier033 F"r this (uesti"n use anne> 033- &&0A "r "ute Manual chart @L2# The D: at

D@%2 #$4B 0#0B@ can /e ientifie "nFre(uency 440 7HE :F2 "n Channel 440 :F2 "n Channel 440 :F2 "ff Fre(uency 440 7HE :F2 "ff

033 F"r this (uesti"n use anne> 033- &&0&1A "r "ute Manual chart @L2# The air!ayintersecti"n at 2@:I #1&8B 0&1B@ is mar7e /y

an D: callisign a TACA callsign 2 a fan mar7er callsign L? an D: callsign LF

033 Fr"m !hich "f the f"ll"!ing !"ul y"u e>pect t" fin inf"rmati"n regaring 7n"!nsh"rt unser+icea/ility "f 2 TACA an D: =

2TAM A9? 59*M@T ATCC /r"acasts

033 Fr"m !hich "f the f"ll"!ing !"ul y"u e>pect t" fin the ates an times !hentemp"rary anger areas are acti+e

2TAM an A9? 2nly A9? 59*M@T ADpect t" fin etails "f the 5earch an escue"rganisati"n an pr"ceures 5A =

A9? ATCC /r"acasts 2TAM 59*M@T

033 Fr"m !hich "f the f"ll"!ing !"ul y"u e>pect t" fin facilitati"n inf"rmati"n regaringcust"ms an health f"rmalities =

A9? A 033- &&0$&A "r "ute Manual chart @H94 CAA-@iti"nAer"planes intening t" use air!ay '&4 sh"ul cr"ss *9:52 intersecti"n #04#B

00$30B) at "r a/"+e

FL$#0 FL&40 FL&10 FL$00

033 An air!ay is mar7e 3#00T $&00 a. This inicates that the minimum "/structi"n clearancealtitue M2CA is 3#00 ft

the minimum enr"ute altitue M@A is3#00 ft

the air!ay /ase is 3#00 ft M5L the air!ay is a l"! le+el lin7 r"ute$&00 ft - 3#00 ft M5L

033 F"r this (uesti"n use anne> 033- &&0$3A "r "ute Manual chart @H9# CAA-@iti"nThe minimum enr"ute altitue a+aila/le "n air!ay '&10 fr"m 9C@ 9 &&$.44341B 00,B@ t" :A5T9A :TA &&1.$ 4$3$B 00$B@ is

FL$#0 FL$00 FL$&0 FL$10

033 F"r this (uesti"n use anne> 033- &&0$4A "r "ute Manual c hart @H94 CAA-@iti"nThe minimum enr"ute altitue that can /e maintaine c"ntinu"usly "n air!ay 'A34fr"m )ALLA5@I )AL &&4.& #3$3B 00308B) t" M9DH'5T M9D &&4.0#&03B 0003,B) is

FL$0 FL$4# FL$#0 FL330

033 F"r this (uesti"n use anne> 033- &&0$#A "r "ute Manual chart @L2& The minimumenr"ute altitue that can /e maintaine c"ntinu"usly "n air!ay *& fr"m 5T'M:L@5T' &&3.& #$00B 00#0$B) t" :@C2 :C &&,.4# #&43B 003&1B) is

FL&&0 FL80 4&00ft M5L $00 ft M5L

033 An air!ay is mar7e FL 80 a. This inicates that the minimum enr"ute altitueM@A is FL 80.

the air!ay /ase is ft M5L. the air!ays e>tens fr"m ftM5L t" FL 80.

ft M5L is the minimum rai"recepti"n altitue MA.

033 F"r this (uesti"n use anne> 033- &&0$,A "r "ute Manual chart @L2$ The minimumenr"ute altitue M@A that can /e maintaine c"ntinu"usly "n air!ay *4 fr"m K@5@IK5I &&$.$ 4&3B 00$03B) t" L9AD 43#B 004$0B) is

FL&40 FL10 $800 ft M5L &000 ft M5L

033An air!ay is mar7e #000 $00a. The n"tati"n #000 is the minimum enr"ute alti tue M@A ma>imum auth"rise alt itue MAA minimum h"ling alti tue MHA /ase "f the air!ay A*L

033 F"r this (uesti"n use anne> 033- &&0$A "r "ute Manual chart @L2# The minimumenr"ute altitue that can /e maintaine c"ntinu"usly "n air!ay *$4 fr"m %2LKA #100B 0&14B@ t" 2@ 2@ &&$.0 ##04B 0&441B@ is

FL&00 FL10 &000ft $#00 ft

033 F"r this (uesti"n use anne> 033- &&030A "r "ute Manual chart @H94 CAA-@iti"nAn appr"priate flight le+el f"r flight "n air!ay '& fr"m 2TAC #000B 00$00B)t" M9DH'5T M9D &&4.0 #&03B 0003,B) is

FL$#0 FL$10 FL$40 FL$30

033 F"r this (uesti"n use anne> 033- &&03&A "r "ute Manual chart @H94 CAA-@iti"nAn appr"priate flight le+el f"r flight in 5M airspace "n air!ay '*& fr"m@LA*@ @L &&4. 43B 0&&0B@ t" FA%F'T FFM &&4.$ #003B

FL300 FL$0 FL3&0 FL330


14/30


00838B@ is

033 F"r this (uesti"n use anne> 033- &&03$A "r "ute Manual chart @L2# Anappr"priate flight le+el f"r flight "n air!ay * fr"m 5':9 5'9 &&1., #$$3B0&43#B@ t" C@M?9 C@ &&4.# #$08B 0&144B@ is

FL,0 FL#0 FL10 FL80

033 F"r this (uesti"n use anne> 033- &&033A "r "ute Manual chart @H9# CAA-@iti"nAn appr"priate flight le+el f"r flight "n air!ay '*# in 5M airspace fr"m M@D@-

A5:9AL5 M@ &.3 4431B 003&0B@ t" *A9LLAC *A9 &.8 43#,B00B@ is

FL$0 FL$80 FL300 FL3$0

033 F"r this (uesti"n use anne> 033- &&034A "r "ute Manual chart @H9# CAA-@iti"nAn appr"priate flight le+el f"r flight "n air!ay '$4 fr"m AT@5 T5 &&,.$4,0B 00&3,B) t" CA@ CA &.4 4&0B 000$,B) is

FL3&0 FL$0 FL300 FL$,0

033 F"r this (uesti"n use anne> 033- &&03#A "r "ute Manual chart @L2$ Anappr"priate flight le+el f"r flight "n air!ay :3 fr"m CHAT9LL2 CTL &&,.1 408B0033#B@ t" CAM:A9 CM: &&$.1 #0&4B 0030B@ is

FL,0 FL80 FL10 FL#0

033 F"r this (uesti"n use anne> 033- &&031A "r "ute Manual chart @L21 Anappr"priate flight le+el f"r flight "n air!ay )3, fr"m CH@: 2%* &., #004B0&$$4B@ t" 2D9* D* &&4., 40$B 0&$3$B@ is

FL80 FL40 FL#0 FL,0

033 F"r this (uesti"n use anne> 033- &&03,A "r "ute Manual chart @L21 Anappr"priate flight le+el f"r flight "n air!ay &0 fr"m M2TM@DI MMD &0.44$4B 00#08B@ t" CHAT9LL2 CTL &&,.1 408B 0033#B@ is

FL10 FL,0 FL#0 FL40

033 @>cluing 5M an appr"priate flight le+el f"r 9F flight in acc"rance !ith semi-circular height rules "n a c"urse "f &80 M is

FL&00 FL0 FL# FL&0#

033 @>cluing 5M an appr"priate flight le+el f"r 9F flight in acc"rance !ith semi-circular height rules "n a magnetic c"urse "f $00 is

FL3&0 FL3$0 FL$0 FL300

033 F"r this (uesti"n use anne> 033- &&040A "r "ute Manual 5TA charts f"r '9CH&0-$&0-$A&0-$: Aer"plane arri+ing +ia r"ute :LM $ "nly sh"ul f"ll"! thef"ll"!ing r"ute t" @%2 int

:LM &&& t" *2L%@ int thenTA -$4, in/"un t" @%2int

TA $4, "ut/"un t" @%2 int )9L 0&8 "ut/"un t" @%2 int H2C 01, +ia *2L%@ t" @%2int

033 F"r this (uesti"n use anne> 033- &&04&A "r "ute Manual 59D chart f"r M'9CH&0-3C&0-3D )hich is the c"rrect eparture +ia %@M?T@ fr"m run!ay $1L =

%@M?T@ F9@ 59@A %@M?T@ TH@@ @CH2 %@M?T@ TH@@ '@:@C %@M?T@ TH@@ 2@M:@

033 F"r this (uesti"n use anne> 033- &&04$A "r "ute Manual 5TA chart f"r L2D2H@ATH2) &0-$D The minimum h"ling altitue MHA an ma>imum h"lingspee 9A5 at MHA at 2C%HAM 2C% &.3 are

,000 ft an $$07t 000ft an $$07t ,000ft an $#07t 000ft an $#07t

033 F"r this (uesti"n use anne> 033- &&043A "r "ute Manual 5TA charts f"r ?A95CHAL@5 D@ *A'LL@ $0-$ The r"ute istance fr"m CH9@@5 C9 t":2'52@ :5 is

1 M 83 M 88 M ,3 M

033 F"r this (uesti"n use anne> 033- &&044A "r "ute Manual 59D chart f"r L2D2H@ATH2) &0-3 )hich "f the f"ll"!ing is a c"rrect Minimum 5afe AltitueM5A f"r the Airp"rt=

)est sect"r $&00 ft !ithin $# M )est sect"r $300 ft !ithin $# M @ast sect"r $&00 ft !ithin #0 M @ast sect"r $300 ft !ithin #0 M

033 F"r this (uesti"n use anne> 033- &&04#A "r "ute Manual 5TA chart f"r MAD9D:AAKA5 &0-$A: F"r run!ay 33 arri+als fr"m the east an s"uth the 9nitialAppr"ach Fi> 9AF in/"un fr"m air!ay '&0 is

T: CK C@TA M2T9L

033 F"r this (uesti"n use anne> 033- &&041A "r "ute Manual 59D charts f"r '9CH &0-3 )hich is the c"rrect AL:9O eparture +ia AAA' f"r run!ay &1=

AL:9O ,5 AL:9O ,A AL:9O 1H AL:9O 1@

033 F"r this (uesti"n use anne> 033- &&04,A "r "ute Manual 59D chart f"rAM5T@DAM 5CH9?H2L &0-3: The r"ute istance fr"m run!ay $, t" A@M is

1, M 3# M # M #$ M

033 F"r this (uesti"n use anne> 033- &&048A "r "ute Manual 59D chart f"rAM5T@DAM 5CH9?H2L &0-3 )hich "f the f"ll"!ing statements is c"rrect f"rAD9% epartures fr"m run!ay &L=

C"ntact 5CH9?2L D@?AT'@&&.0# passing $000 ft an rep"rtaltitue

Cr"ss AD9% /el"! FL10 The istance t" AD9% is $# M Ma>imum 9A5 $#07t turning left at5?L 3.& DM@

033 F"r this (uesti"n use anne> 033- &&04A "r "ute Manual 5TA charts f"r M'9CH&0-$A: The c"rrect arri+al r"ute an 9nitial Appr"ach Fi> 9AF f"r an arri+al fr"mthe !est +ia TA*2 f"r run!ay 08 L H O 6 PPPPP 2 H D > 2 O 6 PPPPP 2 H @ > 2 > H O 6 PPPPPPPP 2 H D > 2 > H O 6 PPPPPPPP 2 H


15/30


033 *i+en C"urse A t" : 088 T istance &$#0 M Mean TA5 330 7t Mean ) 033- &&0#8A "r "ute Manual chart L2D2H@ATH2) 9L5 DM@ !y 0L &&-$ The Decisi"n Altitue DA f"r a 9L5straight-in laning is

$80 ft $00 ft 400 ft 480 ft

033 F"r this (uesti"n use anne> 033- &&0#A "r "ute Manual chart AM5T@DAM5CH9?H2L 9L5 DM@ !y $$ &&-1 The Misse Appr"ach pr"ceure is t" clim/ t" analtitue "f i------------ "n a trac7 "f ii ----------

i $000 ft ii &10 i $00 ft ii $$3 i 3000 ft ii &10 i 3000 ft ii $$3

033 F"r this (uesti"n use anne> 033- &&010A "r "ute Manual chart MAD9D :AAKA59L5 DM@ !y 33 &&-& The minimum glie sl"pe intercepti"n altitue f"r a full 9L5is

4000 ft 3#00 ft $01, ft , ft

033 F"r this (uesti"n use anne> 033- &&01&A "r "ute Manual chart AM5T@DAM KAAM99M'M5 &0-O The ai" Altimeter minimum altitue f"r a CAT $ 9L5 DM@appr"ach t" !y 0&L is

&00 ft 88 ft 300 ft &88 ft

033 F"r this (uesti"n use anne> 033- &&01$A "r "ute Manual chart L2D2H@ATH2) 9L5 DM@ !y 0 &&-& The Minimum Descent Altitue MDA f"ran 9L5 glie sl"pe "ut is

480 ft 40# ft $,# ft $00 ft

033 F"r this (uesti"n use anne> 033- &&013A "r "ute Manual chart ?A95 CHAL@5 D@*A'LL@ 9L5 !y $, $&-$ The cr"ssing altitue an escent instructi"n f"r a

pr"peller aircraft at C2'L2MM9@5 CLM are

Cr"ss at FL10 escen t" 4000 ft Cr"ss at FL,0 escen t" 4000 ft Cr"ss at FL80 escen t" FL,0 Cr"ss at FL10 an maintain

033 F"r this (uesti"n use anne> 033- &&014A "r "ute Manual chart M'9CH 9L5 !y$1 &&-4 The 9L5 fre(uency an ientifier are

&08., 9M) &08., 9M5) &08.3 9M) &08.3 9M5)

033 F"r this (uesti"n use anne> 033- &&01#A "r "ute Manual chart ?A95 CHAL@5 D@*A'LL@ 9L5 !y &0 $&-8 The 9L5 l"caliEer c"urse is

088 &00 &&8 $18

033 F"r this (uesti"n use anne> 033- &&011A "r "ute Manual chart '9CH 9L5 !y &1&&-$ The l"!est pu/lishe auth"rise f"r an 9L5 appr"ach glie sl"pe "ut all"ther ais ser+icea/le aircraft categ"ry A is

,$0m 100m 800m m

033 F"r this (uesti"n use anne> 033- &&01,A "r "ute Manual chart M'9CH D: DM@!y $1L appr"ach &1-3 The fre(uency an ientifier "f the D: f"r the pu/lisheappr"aches are

400 M5) 338 M) &08.1 DM5 &&$.3 M'

033 )hich "f the f"ll"!ing statements is are c"rrect !ith regar t" c"mputer flight plans &.The c"mputer ta7es acc"unt "f /a !eather "n the r"ute an as e>tra fuel. $. Thec"mputer calculates alternate fuel sufficient f"r a misse appr"ach clim/ cruise escentan appr"ach an laning at the estinati"n alternate.

5tatement $ "nly :"th statements 5tatement & "nly either statement

033 F"r this (uesti"n use anne>es 033-&&0,3A 033-&&0,3: 033-&&0,3C an 033-&&0,3D?lanning a MACH 08$ cruise at FL 30 the estimate laning mass is &10 000 7gJ thegr"un istance is $ 800 M an the mean tail!in is &00 7tJ 95A c"niti"ns. Fuelc"nsumpti"n !ill /e

$1 #0 7g $$ 810 7g $4 00 7g 30 &&, 7g

033 F"r this (uesti"n use anne>es 033-&&0,4A 033-&&0,4: 033-&&0,4C an 033-&&0,4D?lanning a MACH 08$ cruise at FL 30 the estimate laning mass is &10 000 7g. Thegr"un istance is $ 800 M an the mean !in is e(ual t" Eer". 95A c"niti"ns. Fuelc"nsumpti"n !ill /e

3$ 1#, 7g 30 &&, 7g $, #,, 7g 30 3,& 7g


16/30


033 F"r this (uesti"n use anne> 033-&&&8&A )hich escri/es the !"rst haEar if any thatc"ul /e ass"ciate !ith the type "f feature at 38 0@ =

@ngine flame "ut an !inscreenamage

5e+ere attenua ti"n in the HF 033-&&&83A 9n the +icinity "f ?A95 4 003@ thetr"p"pause is at a/"ut

FL400 FL340 FL3#0 FL380

033 F"r this (uesti"n use anne> 033-&&&84A )hich escri/es the ma>imum intensity "ficing if any at FL&80 in the +icinity "f CA5A:LACA 33 008) =

5e+ere M"erate Light il

033 F"r this (uesti"n use anne> 033-&&&8#A )hich /est escri/es the significant cl"u ifany f"recast f"r the area s"uth!est "f :2D2 1, 0&4@

# t" , "7tas C' an C: /ase /el"!FL&00 t"ps FL&80

# t" , "7tas C' an C: /ase FL&00t"ps FL&80

3 t" , "7tas C' an C: /ase /el"!FL&00 t"ps FL&80

il

033 F"r this (uesti"n use anne> 033-&&&81A )hich /est escri/es /e ma>imum intensity"f icing if any a t FL in the +icinity "f :'CHA@5T 4# 0$1@ = M"erate Light 5e+ere il

033 F"r this (uesti"n use anne> 033-&&&8,A )hich /est escri/es the ma>imum intensity"f CAT if any f"recast f"r FL330 "+er :@*HA9 3$ 0$0@ =

il Light M"erate 5e+ere

033 F"r this (uesti"n use anne> 033-&&&88A The ma>imum !in +el"city 033-&&&8A )hat is the earliest time 'TC if any thatthunerst"rms are f"recast f"r D2HA 2T:D =

&000 0800 0100 il f"recast

033 A M@TA reas 5A&430 3#00$%T ,000 5%C $& 033-&&$0,A an 033-&&$0,: A tur/";et aer"plane isprepare f"r a &300 M flight at FL 3#0 !ith a true airspee "f 410 7t an a hea !in"f &10 7t. The ta7e-"ff run!ay limitati"n is &,4 000 7g the planne eparture mass is&10 000 7g. The eparture fuel price is e(ual t" 0.$ times the arri+al fuel price fuel

price rati" 6 0.$. 9n "rer f"r the airline t" "ptimiEe its sa+ings the aiti"nal fuel(uantity that must /e l"ae "n /"ar is

&4 000 7g 30 000 7g 4$ 000 7g &$ 000 7g


17/30


033 F"r this (uesti"n use anne> 033-&&$08A A tur/";et aer"plane !eighing $00 000 7ginitiates its cruise at the "ptimum le+el at M 0.84 95A C*63,G T"tal Anti 9ce 2. Ahea !in "f 30 7t is e>perience an after a istance "f #00 M se+ere icing isenc"untere an this re(uires an immeiate escent. The aer"plane mass at start "fescent is

&$ #00 7g &3 000 7g &3 400 7g &3 800 7g

033 F"r this (uesti"n use anne> 033-&&$0A an 033-&&$0: Assuming aepartureimum tan7 capacity 40

000 7g The aiti"nal fuel (uantity !ill /e

0 7g 3 000 7g $ 000 7g 4 000 7g

033 F"r this (uesti"n use anne> 033-&&$&0A an 033-&&$&0: Assuming aepartureimum tan7 capacity 40 000 7gThe aiti"nal fuel (uantity !ill /e

&0 000 7g $0 000 7g &$ 000 7g 000 7g

033 F"r this (uesti"n use anne> 033-&&$&&A an 033-&&$&&: Assuming the f"ll"!ingata . *r"un istance t" /e c"+ere $ 000 M . Cruise flight le+el FL 330 . Cruisingspee Mach 0.8$ true airspee 4,0 7t . Hea !in c"mp"nent 30 7t . ?lanneestinati"n laning mass &10 000 7g . Temperature 95A . C* 3,G . T"tal anti-ice2 . ?ac7 fl"! H9 Time neee t" carry "ut such a flight is

4 h 43 min 4 h $1 min # h 0$ min 4 h &0 min

033 F"r this (uesti"n use anne> 033-&&$&$A an 033-&&$&$: Assuming the f"ll"!ingata . *r"un istance t" /e c"+ere & #00 M . Cruise flight le+el FL 3&0 . Cruisingspee Mach 0.8$ true airspee 4,0 7t . Hea !in c"mp"nent 40 7t . ?lanneestinati"n laning mass &40 000 7g . Temperature 95A C . C* 3, G . T"talanti-ice 2 . ?ac7 fl"! H9 Fuel c"nsumpti"n f"r such a flight is

$3 #00 7g $& #00 7g $& ,00 7g & 00 7g

033 F"r this (uesti"n use anne> 033-&&$&3A an 033-&&$&3: Assuming the f"ll"!ingata . *r"un istance t" /e c"+ere $ #00 M . Cruise flight le+el FL 3#0 . Cruisingspee Mach 0.8$ true airspee 4,0 7t . Tail!in c"mp"nent 40 7t . ?lanneestinati"n laning mass 000 7g . Temperature 95A . C* 3,G . T"tal anti-ice 2FF. Air c"niti"ning n"rmal Fuel c"nsumpti"n f"r such a flight is

$, 800 7g $, 000 7g $8 300 7g $ $00 7g

033 F"r this (uesti"n use anne> 033-&&$&4A an 033-&&$&4: Assuming the f"ll"!ingata . *r"un istance t" /e c"+ere $ 100 M . Cruise flight le+el FL 3,0 . Cruisingspee Mach 0.8$ true airspee 4,0 7t . )in Eer" !in uring flight . ?lanneestinati"n laning mass &40 000 7g . Temperature 95A C . C* 3, G . T"talanti-ice 2 . Air c"niti"ning n"rmal Fuel c"nsumpti"n f"r such a flight is

3& #00 7g $ &00 7g $ 4007g $, 400 7g

033 F"r this (uesti"n use anne> 033-&&$A A tur/";et aer"plane is flying using thef"ll"!ing ata . "ptimum flight le+el Mach 0.80 mass "f &0 000 7g . temperature 95A. tail!in c"mp"nent &00 7t The fuel mileage an the fuel c"nsumpti"n per h"ur are

&0# M


18/30


altitue y"ur Mach num/er sh"ul /e

033 F"r this (uesti"n use anne> 033-&&$$8A F"r a l"ng istance flight at FL 30 L"ngange regime i+ie int" f"ur flight legs !ith the f"ll"!ing characteristics - segmentA: - *r"un istance $ 000 M. hea !in c"mp"nent #0 7t - segment :C - *r"unistance & 000 M. hea !in c"mp"nent 30 7t - segment CD - *r"un istance #00

M. tail !in c"mp"nent &00 7t - segment D@ - *r"un istance & 000 M. hea !inc"mp"nent ,0 7t The air istance "f the entire flight is appr">imately

4 00 M # &$0 M 4 130 M # 040 M

033 F"r this (uesti"n use anne> 03&-&&$$A F"r a tur/";et aer"plane flying !ith a mass "f&0 000 7g at Mach 0.8$ an 7n"!ing that the temperature at flight le+el FL 3,0 is -3# C the "ptimum flight altitue calculate using the anne> is

3,400 ft 3,800 ft 34100 ft 38100 ft

033 F"r this (uesti"n use anne> 03&-&&$3&A F"r a l"ng istance flight at FL 3,0 L"ng

ange regime i+ie int" f"ur flight legs !ith the f"ll"!ing specificati"ns - segmentA: - *r"un istance $ 000 M. hea!in c"mp"nent #0 7t - segment :C - *r"unistance & 000 M. hea!in c"mp"nent 30 7t - segment CD - *r"un istance #00

M. tail!in c"mp"nent ,0 7t - segment D@ - *r"un istance & 000 M. hea!inc"mp"nent $0 7t The t"tal air istance is appr">imately

4 800 M 4 40 M 4 #80 M 4 8$0 M

033 F"r this (uesti"n use anne> 033-&&$38A The flight cre! "f a tur/";et aer"planeprepares a flight using the f"ll"!ing ata - Flight le+el FL 3,0 at L"ng ange Lcruise regime - ?rescri/e mass at /ra7e release $04 #00 7g - Flight leg gr"unistance $ 000 M - Temperatures 95A - Hea!in c"mp"nent ,0 7t - T"tal anti-iceset "n 2 f"r the entire flight - n" re(ueste clim/ an escent c"rrecti"n "f the fuelc"nsumpti"n The fuel re(uire fr"m ta7e-"ff t" laning is

$ 440 7g $, ,,0 7g $0 00 7g $$ &10 7g

033 F"r this (uesti"n use anne> 033-&&$3A an 03&-&&$3: The flight cre! "f a tur/";etaer"plane prepares a flight using the f"ll"!ing ata - Flight leg istance 3 #00 M -Flight le+el FL 3&0 true airspee 4#0 7t - Hea!in c"mp"nent at this le+el ## 7t -9nitially planne ta7e-"ff mass !ith"ut e>tra fuel "n /"ar &80 000 7g - Fuel price

0.30 Qimum fuel price at arri+al must /e

0.$, Qtra fuel "n /"ar &80 000 7g - Fuel price0.30 @ur"tra fuel "n /"ar &,0 000 7g - Fuel price0.$, @ur"


19/30


anne> the "ptimum (uantity "f fuel !hich sh"ul /e carrie in aiti"n t" the prescri/e(uantity is

033 F"r this (uesti"n use anne> 033-&&$4#A an 033-&&$4#: The flight cre! "f a tur/";etaer"plane prepares a flight using the f"ll"!ing ata - Flight leg istance 3 #00 M -Flight le+el FL 3&0 true airspee 4#0 7t - Hea!in c"mp"nent at this le+el # 7t -9nitially planne ta7e-"ff mass !ith"ut e>tra fuel "n /"ar &80 000 7g - Fuel price0.3# Qtra fuel in aiti"n t" that !hich is necessary. 'sing the appeneanne> the "ptimum (uantity "f fuel !hich sh"ul /e carrie in aiti"n t" the prescri/e(uantity is

The fuel transp"rt "perati"n is n"trec"mmene in this case.

$$ 000 7g 000 7g 8 000 7g

033 F"r this (uesti"n use anne> 033-&&$#$A 033-&&$#$: an 033-&&$#$C %n"!ing that .

Mass at /ra7e release $&0 000 7g . 5electe cruise spee 0.8$ Mach . Air istance 3000 M . Cruise le+el "ptimum . Air c"niti"ning stanar . Anti-icing 2FF .Temperature 95A . C* 3,G Assuming Eer" !in the planne flight time fr"m ta7e-"fft" laning neee t" c"mplete this flight !ill /e

400 minutes 383 minutes 34 minutes 38 minutes

033 F"r this (uesti"n use anne> 033-&&$#3A 033-&&$#3: 033-&&$#3C an 033-&&$#3D%n"!ing that . Mass at /ra7e release &0 000 7g . 5electe cruise spee 0.8$ Mach .Flight leg istance & #00 M . Cruise le+el "ptimum . Air c"niti"ning stanar . Anti-icing 2FF . Temperature 95A . C* 3,G Assuming Eer" !in the planne flight timefr"m ta7e-"ff t" laning neee t" c"mplete this flight !ill /e

$0 minutes &$ minutes &8 minutes $03 minutes

033 F"r this (uesti"n use anne> 033-&&$#4A 033-&&$#4: 033-&&$#4C an 033-&&$#4D%n"!ing that . Mass at /ra7e release &0 000 7g . 5electe cruise spee 0.8$ Mach .Flight leg istance & #00 M . Cruise le+el "ptimum . Air c"niti"ning stanar . Anti-icing 2FF . Temperature 95A . C* 3,G Assuming Eer" !in the planne laningmass at estinati"n !ill /e

&,& $00 7g &1 $00 7g &,0 $00 7g &,4 800 7g

033 F"r this (uesti"n use anne> 033-&&$##A 033-&&$##: an 033-&&$##C %n"!ing

that . Mass at /ra7e release $&0 000 7g . 5electe cruise spee 0.8$ Mach . Flight legistance 3 000 M . Cruise le+el "ptimum . Air c"niti"ning stanar . Anti-icing2FF . Temperature 95A . C* 3, Assuming Eer" !in the planne laning mass a testinati"n !ill /e

&,$ 300 7g &,0 400 7g &,& 300 7g &,1 &00 7g

033 F"r this (uesti"n use anne> 033-&&$#A an 033-&&$#: The flight cre! "f a tur/";etaer"plane prepares a flight using the f"ll"!ing ata - Flight leg air istance $ ,00 M -Flight le+el FL 3&0 true airspee 4,0 7t - Tail!in c"mp"nent at this le+el 3# 7t -9nitially planne ta7e-"ff mass !ith"ut e>tra fuel "n /"ar &80 000 7g - Fuel price0.$8 @ur"tra fuel "n /"ar 000 7g - Fuel price0.$8 @ur"iing until the 9AF 9nitialAppr"ach Fi> "f the estinati"naer"r"me.

033 F"r this (uesti"n use anne> 033-&&$,0A A tur/";et aer"plane flies using the f"ll"!ingata . flight le+el FL 330 flight regime L"ng ange L mass #00 7g .tail!in c"mp"nent at this le+el 40 7t )ith a remaining flight time "f & h &0 min thegr"un istance that can /e c"+ere /y the aer"plane at cruising spee is

#3 M 43 M 4,& M #&8 M

033 F"r this (uesti"n use anne> 033-&&$,&A The flight cre! "f a tur/";et aer"planeprepares a flight using the f"ll"!ing ata . Ta7e-"ff mass $&0 #00 7g . Flight leggr"un istance $ #00 M . Flight le+el FL 330J L"ng ange flight regime . Tail!in

3& 840 7g 3& 340 7g 30 $00 7g 3 ,#0 7g


20/30


c"mp"nent at this le+el ,0 7t . T"tal anti-ice set "n 2 . Fi>e ta>i fuel #00 7gJ finalreser+e $ 400 7g . 9gn"re alternate fuel. The effects "f clim/ an escent are n"tc"rrecte f"r c"nsumpti"n. The (uantity "f fuel that must /e l"ae at the par7ing areais

033 F"r this (uesti"n use anne> 033-&&$,$A The flight cre! "f a tur/";et aer"planeprepares a flight using the f"ll"!ing ata . Ta7e-"ff mass &18 #00 7g . Flight leggr"un istance $ 000 M . Flight le+el FL 3,0J L"ng ange flight regime . Tail!inc"mp"nent at this le+el 30 7t . T"tal anti-ice set "n 2 . Fi>e ta>i fuel #00 7gJ finalreser+e $ 000 7g . 9gn"re alternate fuel. The effects "f clim/ an escent are n"tc"rrecte f"r c"nsumpti"n. The prescri/e (uantity "f trip fuel f"r the flight leg is

$0 #00 7g $3 000 7g $$ #00 7g $3 300 7g

033 2n an ATC flight plan an aircraft inicate as H f"r Hea+y is "f the highest !a7e tur/ulence

categ"ry

has a certifie laning mass greater than

"r e(ual t" &31 000 7g

has a certifie ta7e-"ff mass greater

than "r e(ual t" &40 000 7g

re(uires a run!ay length "f at least

$ 000m at ma>imum certifie ta7e-"ff mass

033 9f y"ur estinati"n airp"rt has n" 9CA2 inicat"r in the appr"priate /"> "f y"ur ATCflight plan y"u !rite

AAAA OOOO cept if & -flight urati"n "es n"t e>cee t!" h"urs $ - uring the peri" fr"m t!" h"urs /ef"re t"t!" h"urs after the estimate laning time the f"recast c"niti"ns "f ceiling an+isi/ility are n"t less than "ne an a half times the applica/le minima 3 - the platf"rm isa+aila/le an n" "ther flight either fr"m "r t" the platf"rm is e>pecte /et!een theestimate time "f eparture an "ne half h"ur after the estimate laning time Thec"m/inati"n !hich regr"ups all "f the c"rrect statements is

& - $ - 3 & - $ & - 3 $ - 3

033 )hen calculating the fuel re(uire t" carry "ut a gi+en flight "ne must ta7e int" acc"unt& - the !in $ - f"reseea/le air/"rne elays 3 - "ther !eather f"recasts 4 - any

f"reseea/le c"niti"ns !hich may elay laning The c"m/inati"n !hich pr"+ies thec"rrect statement is

& $ 3 4 & 3 $ 4 & $ 3

033F"r an ATC flight plan file /ef"re the flight the inicate time "f eparture is the estimate "ff-/l"c7 time the time at !hich the flight plan is file. the time "f ta7e-"ff. the time "+erhea the first rep"rtingp"int after ta7e-"ff.

033 The cruising spee t" !rite in the appr"priate /"> "f an ATC flight plan is true air spee inicate air spee gr"un spee cali/rate air spee

033 9n the appr"priate /"> "f an ATC flight plan f"r enurance "ne must inicate the timec"rresp"ning t"

the t"tal usa/le fuel "n /"ar the re(uire fuel f"r the flight the re(uire fuel f"r the flight plusthe alternate an 4# minutes

the t"tal usa/le fuel "n /"ar minusreser+e fuel

033 The fuel /urn "f an aircraft tur/ine engine is $$0 l


21/30


033 9n the appr"priate /"> "f an ATC flight plan f"rm c"ncerning e(uipment the letter t" /euse t" inicate that the aircraft is e(uippe !ith a m"e A 401 c"es transp"ner !ithaltitue rep"rting capa/ility is

C ? 5 A

033 F"r this (uesti"n use anne> 033-&&,0$ A The true c"urse is 04$. The +ariati"n in thearea is 1 ) an the !in is calm. The e+iati"n car is repr"uce in the anne>. 9n"rer t" f"ll"! this c"urse the pil"t must fly a c"mpass heaing "f

0#$ 0#8 040 044

033 F"r this (uesti"n use anne> 033-&&,04A True Air spee &,0 7t )in in the area$,0


22/30


033 F"r this (uesti"n use anne> 033-&$$,1A 9n the ATC flight plan 9tem f"r a flightal"ng a esignate r"ute !here the eparture aer"r"me is n"t "n "r c"nnecte t" thatr"ute

the letters DCT sh"ul /eentere f"ll"!e /y the p"int "f

;"ining the AT5 r"ute

it is necessary "nly t" gi+e the firstrep"rting p"int "n that r"ute

the !"rs as cleare sh"ul /eentere

it is n"t necessary t" inicate thep"int "f ;"ining that r"ute as it !ill/e "/+i"us t" the AT5 unit.

033 F"r this (uesti"n use anne> 033-&$$,,A 9n the e+ent that 5@LCAL is prescri/e /y anappr"priate auth"rity in !hich secti"n "f the ATC flight plan !ill the 5@LCAL c"e /eentere =

2TH@ 9F2MAT92 @'9?M@T 2'T@ A9CAFT 9D@T9F9CAT92

033 An aircraft has a ma>imum certificate ta7e-"ff mass "f &3,000 7g /ut is "perating atta7e-"ff mass &3#000 7g. 9n 9tem "f the ATC flight plan its !a7e tur/ulence categ"ryis

hea+y H hea+ypresse in

'TC L"cal mean time l"cal stanar time Central @ur"pean Time

033 9n the AT5 flight plan f"r a n"n-scheule flight !hich "f the f"ll"!ing letters sh"ul /eentere in 9tem 8 Type "f Flight

033-&$$8#A 9n the ATC flight plan item , f"r a rai"e(uippe aircraft the ientifier must al!ays

/e the TF callsign t" /e use inclue the aircraft registrati"n mar7ing inclue the "perating agencyesignat"r

inclue an inicati"n "f the aircrafttype

033 9n the ATC flight plan item it is necessary t" enter any p"int a t !hich a change "fcruising spee ta7es place. F"r this purp"se a change "f spee is efine as

#G TA5 "r 0.0& Mach "r m"re &0 G TA5 "r 0.0# Mach "r m"re $0 7m per h"ur "r 0.& Mach "r m"re $0 7n"ts "r 0.0# Mach "r m"re

033 9n the ATC flight plan item !hen entering a r"ute f"r !hich stanar eparture 59Dan stanar arri+al 5TA pr"ceures e>ist

/"th sh"ul /e entere in the ATCplan !here appr"priate

59Ds sh"ul /e entere /ut n"t 5TAs 5TA5 sh"ul /e entere /ut n"t59Ds

neither 59D n"r 5TA sh"ul /eentere

033 )hen an ATC flight plan has /een su/mitte f"r a c"ntr"lle flight the flight plansh"ul /e amene "r cancelle in the e+ent "f the "ff-/l"c7 time /eing elaye /y

30 minutes "r m"re 4# minutes "r m"re 10 minutes "r m"re 0 minutes "r m"re

033 F"r this (uesti"n use anne> 033-&$$8A 9n the ATC flight plan 9tem & emergencyan sur+i+al e(uipment carrie "n the flight sh"ul /e inicate /y

cr"ssing "ut the /"> rele+ant t" anye(uipment n"t carrie

circ ling the re le+ant /"> placing a ti c7 in the re le+ant /"> li sting the it ems carr ie "n the@MA%5 line

033 )hen c"mpleting an ATC flight plan f"r a flight c"mmencing uner 9F /ut p"ssi/lychanging t" F the letters e ntere in 9tem 8 FL9*HT 'L@5 !"ul /e

I

the plan sh"ul /e file !ith therele+ant /"> /lan7

an estimate may /e entere /ut thatnum/er may n"t su/se(uently /ee>ceee

the plan may n"t /e file until theinf"rmati"n is a+aila/le

033 9n an ATC flight plan 9tem in "rer t" efine a p"siti"n as a /earing an istancefr"m a 2 the gr"up "f figures sh"ul c"nsist "f

2 ient magnetic /earing anistance in nautical miles

2 ient true /earing an istance in7il"metres

2 ient magnetic /earing anistance in 7il"metres

full name "f 2 true /earing anistance in 7il"metres

033 An aircraft plans t" epart L"n"n at &000 'TC an arri+e at Munich @DDM at &$

'TC. 9n the ATC flight plan 9tem &1 estinati"n


23/30


033 F"r a repetiti+e ATC flight plan ?L t" /e use flights must ta7e place "n a regular/asis "n at least

&0 "ccasi"ns $0 "ccasi"ns 30 "ccasi"ns #0 "ccasi"ns

033 9n the ATC flight plan 9tem &0 e(uipment the letter t" inicate the carriage "f aser+icea/le transp"ner - m"e A 4 igits-401 c"es an m"e C is

C : A ?

033 F"r this (uesti"n use anne>es 033-&$30$A an 033-&$30$: "r Flight ?lanning ManualMKT & Figure 4.#.$ an 4.#.3.& *i+en Distance C - D 3$00 M L"ng ange Cruiseat FL 340 Temperature De+iati"n fr"m 95A &$C Tail!in c"mp"nent #0 7t *r"ssmass at C ## 000 7g The fuel re(uire fr"m C - D is

&4 #00 7g &4 $00 7g &, 800 7g &, #00 7g

033 F"r this (uesti"n use anne>es 033-&$303A an 033-&$303: "r Flight ?lanning ManualMKT & Figure 4.#.$ an 4.#.3.& *i+en Distance C - D 180M L"ng ange Cruise atFL340 Temperature De+iati"n fr"m 95A 0 C Hea!in c"mp"nent 10 7t *r"ss mass

at C 44 ,00 7g The fuel re(uire fr"m C - D is

3,00 7g 3400 7g 3&00 7g 4000 7g

033 F"r this (uesti"n use anne> 033-&$304A "r Flight ?lanning Manual MKT & Figure4.#.& *i+en :ra7e release mass #8 000 7g Temperature 95A The fuel re(uire t"clim/ fr"m an aer"r"me at ele+ati"n 4000 ft t" FL300 is

&$#0 7g &400 7g &4#0 7g &3#0 7g

033 F"r this (uesti"n use anne> 033-&$30#A "r Flight ?lanning Manual MKT & Figure4.#.& *i+en :ra7e release mass 1$ 000 7g Temperature 95A C The fuel re(uiref"r a clim/ fr"m 5ea Le+el t" FL330 is

&,00 7g &1#0 7g &,#0 7g &800 7g

033 F"r this (uesti"n use anne>es 033-&$301A an 033-&$301: "r Flight ?lanning ManualMKT & Figure 4.#.$ an 4.#.3.3

100 7g 1&$# 7g 4,# 7g 44# 7g

033 F"r this (uesti"n use anne>es 033-&$30,A an 033-&$30,: "r Flight ?lanning ManualMKT & Figure 4.#.$ an 4.#.3.3 *i+en Distance : - C &$00 M Cruise Mach 0.,8 atFL300 Temperature De+iati"n fr"m 95A -&4C Tail!in c"mp"nent 40 7t *r"ss massat : #0 $00 7g The fuel re(uire fr"m : - C is

1 7g #8#0 7g ,300 7g ,0#0 7g

033 F"r this (uesti"n use anne>es 033-&$308A an 033-&$308: "r Flight ?lanning ManualMKT & Figure 4.#.$ an 4.#.3.4 *i+en Distance C - D #40 M Cruise 300 %9A5 at

FL $&0 Temperature De+iati"n fr"m 95A $0C Hea!in c"mp"nent #0 7t *r"ssmass at C 10 000 7g The fuel re(uire fr"m C t" D is

41$0 7g 4$00 7g 33#0 7g 3180 7g

033 F"r this (uesti"n use anne>es 033-&$30A an 033-&$30: "r Flight ?lanning ManualMKT & Figure 4.#.$ an 4.#.3.4 *i+en Distance : - C 3#0 M Cruise 300 %9A5 atFL $&0 Temperature - 40C Tail!in c"mp"nent ,0 7t *r"ss mass at : #3 $00 7g Thefuel re(uire fr"m : - C is

&8&0 7g &40 7g $800 7g $1,0 7g

033 F"r this (uesti"n use anne> 033-&$3&0A "r Flight ?lanning Manual MKT & Figure 4.4- H2LD9* ?LA9* The fuel re(uire f"r 30 minutes h"ling in a racetrac7

pattern at ?A ft mean gr"ss mass 4# 000 7g is

&00 7g &0&0 7g &3&0 7g $&80 7g

033 F"r this (uesti"n use anne> 033-&$3&&A "r Flight ?lanning Manual MKT & Figure 4.4- H2LD9* ?LA9* The fuel re(uire f"r 4# minutes h"ling in a racetrac7

pattern at ?A #000 ft mean gr"ss mass 4, 000 7g is

&13# 7g &00 7g &10 7g &&$# 7g

033 F"r this (uesti"n use anne> 033-&$3&$A "r Flight ?lanning Manual MKT & Figure4.3.1 *i+en Distance t" Alternate 4#0 M Laning mass at Alternate 4# 000 7gTail!in c"mp"nent #0 7t The Alternate fuel re(uire is

$#00 7g $,#0 7g 30#0 7g $00 7g

033 F"r this (uesti"n use anne> 033-&$3&3A "r Flight ?lanning Manual MKT & Figure4.3.1 *i+en Distance t" Alternate 400 M Laning mass at Alternate #0 0007gHea!in c"mp"nent $# 7t The alternate fuel re(uire is

$800 7g $##0 7g $00 7g $1#0 7g

033 F"r this (uesti"n use anne> 033-&$3&4A The ) 033-&$3&8A The )


24/30


033 F"r this (uesti"n use anne> 033-&$3$0A )hich /est escri/es the significant cl"uf"recast f"r the area east "f Tunis 310&0@ =

# t" , "7tas C' an AC /ase/el"! FL&00 t"ps FL&80

3 t" 4 "7tas C' an AC /ase /el"!FL&00 t"ps FL&80

# t" , "7tas C' an AC /ase FL&00t"ps FL&80

3 t" 4 "7tas C' an AC /aseFL&00 t"ps FL&10

033 F"r this (uesti"n use anne>.033-&$3$&A )hich /est escri/es the ma>imum intensity"f icing if any a t FL&10 in the +icinity "f :@L9 #3 0&3@ =

m"erate se+ere light nil

033 F"r this (uesti"n use anne> 033-&$3$$A )hich escri/es the intensity "f icing if anyat FL in the +icinity "f T2'L2'5@ 44 0&@ =

m"erate m"erate "r se+ere light nil

033 F"r this (uesti"n use anne> 033-&$3$3A The surface system "+er 9@A480&1@ is a

c"l fr"nt m"+ing east !arm fr"nt m"+ing n"rth stati"nary "cclue fr"nt c"l fr"nt m"+ing !est

033 F"r this (uesti"n use anne> 033-&$3$4A 9n the +icinity "f 5HA2 #$ 00)the tr"p"pause is at a/"ut FL

310 3#0 300 $,0

033 F"r this (uesti"n use anne> 033-&$3$#A )hich /est escri/es the significant cl"uf"recast "+er T2'L2'5@ 4400&@ =

/r"7en AC 033-&$3$,A The ma>imum !in +el"city 033-&$340A "r Flight ?lanning Manual MKT & Figure4.3.# F"r a flight "f $800 gr"un nautical miles the f"ll"!ing apply Hea !inc"mp"nent $0 7t Temperature 95A C :ra7e release mass 14,00 7g The a trip fuelan / trip time respecti+ely are

a &,000 7g / 1hr 4# min a 7g / 1hr min a &1$00 7g / 1hr $0 min a &8400 7g / ,hr 00 min

033 F"r this (uesti"n use anne> 033-&$34&A "r Flight ?lanning Manual MKT & Figure4.3.&C F"r a flight "f &00 gr"un nautical miles the f"ll"!ing apply Hea !inc"mp"nent &0 7t Temperature 95A -#C Trip fuel a+aila/le 7g Laning mass#00007g )hat is the minimum cruise le+el pressure altitue !hich may /e planne =

&,000 ft $$000 ft &4000 ft &0000 ft

033 F"r this (uesti"n use anne>.033-&$34$A "r Flight ?lanning Manual MKT & Figure4.3.# *i+en the f"ll"!ing Hea !in c"mp"nent #0 7t Temperature 95A &0C :ra7erelease mass 1#0007g Trip fuel a+aila/le &80007g )hat is the ma>imum p"ssi/le trip

$,40 M 3&00 M 3480 M $#40 M


25/30


istance =

033 F"r this (uesti"n use anne> 033-&$343A "r Flight ?lanning Manual MKT & Figure4.3.&C )ithin the limits "f the ata gi+en a mean temperature increase "f 30C !illaffect the trip time /y appr">imately

-#G #G 8G -,G

033 F"r this (uesti"n use anne> 033-&$344A "r Flight ?lanning Manual MKT & Figure4.3.&C F"r a flight "f $000 gr"un nautical miles cruising at 30000 ft !ithin the limits"f the ata gi+en a hea!in c"mp"nent "f $# 7t !ill affect the trip time /yappr">imately

,.1G #.3G $.3G -3.1G

033 F"r this (uesti"n use anne> 033-&$34#A "r Flight ?lanning Manual MKT & Figure4.3.# *i+en a trip time "f a/"ut h"urs !ithin the limits "f the ata gi+en atemperature ecrease "f 30C !ill affect the trip time /y appr">imately

,G 3G -4G -&0G

033 F"r the (uesti"n use anne> 033-&$341A "r Flight ?lanning Manual MKT & Figure4.3.&C F"r a flight "f $800 gr"un nautical miles the f"ll"!ing apply Tail !inc"mp"nent 4#7t Temperature 95A - &0C Cruise altitue $000ft Laning mass ##0007gThe a trip fuel / trip time respecti+ely are

a &,&007g / 1hr 0, min a &80007g /#hr #0 min a $00007g / 1hr 40 min a &10007g / 1hr $# min

033 F"r this (uesti"n use anne> 033-&$34,A "r Flight ?lanning Manual MKT & Figure4.3.# F"r a flight "f 3#00 gr"un nautical miles the f"ll"!ing apply Tail !inc"mp"nent #0 7t Temperature 95A &0C :ra7e release mass 1#0007g The a trip fuelan / trip time respecti+ely are

a &8&00 7g / ,hr $0 min a 7g / 1hr 00 min a $&800 7g / hr $# min a &000 7g / ,hr 4#min

033 F"r this (uesti"n use anne> 033-&$348A "r Flight ?lanning Manual MKT & Figure4.3.# The f"ll"!ing apply Temperature 95A C :ra7e release mass 1$0007g Triptime #hr $0 min )hat is the trip fuel =

&3#007g &30007g &3$007g &38007g

033 F"r this (uesti"n use anne> 033-&$34A "r Flight ?lanning Manual MKT & Figure4.3.&C F"r a flight "f $400 gr"un nautical miles the f"ll"!ing apply Temperature 95A-&0C Cruise altitue $000ft Laning mass 4#0007g Trip fuel a+aila/le &10007g )hatis the ma>imum hea!in c"mp"nent !hich may /e accepte =

3# 7t t ,07t 0

033 F"r this (uesti"n use anne> 033-&$3#0A "r Flight ?lanning Manual MKT & Figure4.3.# The f"ll"!ing apply Tail !in c"mp"nent &07t Temperature 95A &0C :ra7erelease mass 130007g Trip fuel a+aila/le $00007g )hat is the ma>imum p"ssi/le tripistance =

3,40 M 3140 M 3#00 M 3$#0 M

033 F"r this (uesti"n use anne> 033-&$3#&A "r Flight ?lanning Manual MKT & Figure4.3.# F"r a flight "f $400 gr"un nautical miles the f"ll"!ing apply Tail !in $#7tTemperature 95A - &0C :ra7e release mass 110007g The a trip fuel an / trip timerespecti+ely are

a &40007g / #hr 3# min a g /1hr $0 min a &41007g / #hr 4# min a g / 1hr 00 min

033 F"r this (uesti"n use anne> 033-&$3#3A "r "ute Manual chart # ATH9 2n air!ay?T5 ? fr"m igra 1$334 0010$B@ the initial great circle gri c"urse is

344 3#3 34, 3#0

033 F"r this (uesti"n use anne> 033-&$3#4A "r "ute Manual chart A? 2n a irect greatcircle c"urse fr"m 5hann"n #$43B 008#3B) t" *aner 48#4B0#43$B) the aa+erage true c"urse an / istance are

a $1$ / &,$0 M a $8& / $,30 M a $44 / $0 M a $8& / &8,, M

033 F"r this (uesti"n use anne> 033-&$3##A "r "ute Manual chart # ATH9 The initialgreat circle true c"urse fr"m %efla+i7 1400B 0$$31B ) t" igra 1$33B 0010$B@

measures 084. 2n a p"lar enr"ute chart !here the gri is aligne !ith the 000 meriianthe initial gri c"urse !ill /e

&01 080 01 011

033 F"r this (uesti"n use anne> 033-&$3#1A "r "ute Manual chart # ATH9 The initialgreat circle c"urse fr"m p"siti"n A 8000B &,000B@ t" p"siti"n : ,#00B 0&&@ is&,, *. The final gri c"urse at p"siti"n : !ill /e

&,, * &4 * &,$ * 3#3 *

033 F"r this (uesti"n use anne> 033-&$3#A "r Flight ?lanning Manual MKT & Figure4.,.3 *i+en Di+ersi"n istance ,$0M Tail !in c"mp"nent $#7t Mass at p"int "fi+ersi"n ##0007g Temperature 95A Di+ersi"n fuel a+aila/le 4$#07g )hat is theminimum pressure altitue at !hich the a/"+e c"niti"ns may /e met =

$0000ft $1000ft &1000ft &4#00ft

033 F"r this (uesti"n use anne> 033-&$310A "r Flight ?lanning Manual MKT & Figure4.,.3 *i+en Di+ersi"n istance 1#0 M Di+ersi"n pressure altitue &1 000 ft Mass at

p"int "f i+ersi"n #, 000 7g Hea !in c"mp"nent $0 7t Temperature 95A C Thei+ersi"n a fuel re(uire an / time are appr">imately

a 48007g / $h 03min a 3007g / &h 4#min a 1$007g / $h &0min a 44007g / &h 3#min


26/30


033 F"r this (uesti"n use anne> 033-&$31&A "r Flight ?lanning Manual MKT & Figure4.,.3 *i+en Distance t" alternate #0 M Hea !in c"mp"nent $0 7t Mass at p"int "fi+ersi"n #00007g Di+ersi"n fuel a+aila/le #8007g The minimum pressure altitue at!hich the a/"+e c"niti"ns may /e met is

$$000ft $0000ft $1000ft &8000ft

033 F"r this (uesti"n use anne> 033-&$314A "r Flight ?lanning Manual MKT & Figure4.,.$ F"r the purp"se "f planning an e>tene range flight it is re(uire that !ith a start"f i+ersi"n mass "f ##0007g a i+ersi"n "f 100 nautical miles sh"ul /e achie+e in 0minutes. 'sing the a/"+e ta/le the "nly liste cruise techni(ue t" meet that re(uirementis

M


27/30


&$0 7t )hat is the istance an time "f the ?@T fr"m the eparture p"int=

033 *i+en Distance fr"m eparture t" estinati"n $#1 M *5 2ut &10 7t *5 H"me &&0 7t)hat is the istance "f the ?@T fr"m the eparture p"int=

&04 M $ M &$8 M &,1 M

033 *i+en Distance fr"m eparture t" estinati"n $,0 M True trac7 030 )


28/30


033 *i+en Distance fr"m eparture t" estinati"n 43# M *5 2ut &&0 7t *5 H"me &30 7t)hat is the istance "f the ?@T fr"m the eparture p"int=

$31 M & M $&8 M 318 M

033 *i+en Distance fr"m eparture t" estinati"n &40 M *5 2ut 0 7t *5 H"me 80 7t)hat is the istance "f the ?@T fr"m the eparture p"int=

11 M ,4 M ,0 M &$4 M

033 *i+en Distance fr"m eparture t" estinati"n #00 M True trac7 00 )


29/30


033 *i+en Distance fr"m eparture t" estinati"n M @nurance 3$ h TA5 0 7t*r"un 5pee 2ut &00 7t *r"un 5pee H"me 80 7t )hat is the istance an time "fthe ?5 fr"m the eparture p"int=

Distance &4$ M Time 8# min Distance 1, M Time #0 min Distance ,& M Time 4, min Distance 8 M Time # min

033 *i+en Distance fr"m eparture t" estinati"n 3$0 M @nurance 43 h True Trac7&$0 )


30/30


033 *i+en Distance fr"m eparture t" estinati"n 310 M @nurance 4# h True Trac734# )

033 - flight planning & flight monitoring

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