fmgs a320 user guide

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JeeHellWare A320 FMGS

User Guide

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!AB"# $F %$&!#&!Click on a chapter below to jump there.

Recent additions are marked with the following symbol !

1. Fore'ord......................................................................................(

2.)nstru*ent a++li,ations...............................................................6

2.1 - F ri*ar Flit is+la4 ....................................................................62.1.1 - General View.....................................................................................................62.1.2 - Attitude Indicator................................................................................................72.1.3 - Speed Tape........................................................................................................8

2.1.4 - Altitude indications.............................................................................................2.1.! - Vertical Speed..................................................................................................1"2.1.6 - #eadin$ Tape...................................................................................................1"2.1.7 - %li$&t 'at& Vector.............................................................................................112.1.8 - %li$&t (irector )%(*..........................................................................................122.1. - I+S and V(,V deiation Scales......................................................................142.1.1" - %li$&t ode Annunciator )%A*.....................................................................1!2.1.11 - %la$s and /essa$es......................................................................................16

2.2 - &a5iation is+la &4...........................................................................12.2.1 - General............................................................................................................172.2.2 - I+S 0ose /ode................................................................................................182.2.3 - V0 0ose /ode..............................................................................................12.2.4 - AV /odes )0ose and Arc*.............................................................................2"2.2.! - 'lan /ode........................................................................................................222.2.6 - ,G'S............................................................................................................232.2.7 - TAS................................................................................................................242.2.8 - &rono/etre....................................................................................................27

2.3 - #nine / Warnin is+la #/W...............................................................282.3.1 - General............................................................................................................282.3.2 - ,n$ine 'ara/eters..........................................................................................2

2. - Sste*/Status is+la S4.....................................................................31

2.4.1 - General............................................................................................................312.4.2 - ,GI,...........................................................................................................332.4.3 - B+,,(.............................................................................................................34


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2.4.4 - ABI '0,SS50,.........................................................................................3!2.4.! - ,+,T0IA+...................................................................................................362.4.6 - #(0A5+I....................................................................................................372.4.7 - %5,+................................................................................................................382.4.8 - A'5..................................................................................................................32.4. - AI0 (ITIIG.......................................................................................4"2.4.1" - (0G,............................................................................................412.4.11 - #,,+...........................................................................................................422.4.12 - %+IG#T T0+S.....................................................................................432.4.13 - 05IS,.........................................................................................................44

2.( - Flit %ontrol Unit F%U 4.........................................................................(2.!.1 - General............................................................................................................4!2.!.2 - ,%IS panel......................................................................................................472.!.3 - Auto-%li$&t ontrol...........................................................................................482.!.4 - Air9us %5 p&ilosop&:....................................................................................!"

2.6 - $5eread +anel.........................................................................................(2

2.6.1 - General ;.......................................................................................................!22.6.2 - Anti-ice< +i$&ts< A'5< a9in 'ressure< ...........................................................!62.6.3 - ,/er$enc: ,lectric 'ower< G'S. ................................................................!82.6.4 - Air conditionin$.................................................................................................!2.6.! - anual ,n$ine Start........................................................................................6"2.6.6 - ,+, panel......................................................................................................612.6.7 - #:draulic.........................................................................................................622.6.8 - %uel..................................................................................................................632.6. - Auto Bra=e )optional on V#( application*....................................................632.6.1" - ,n$ine Start )optional on V#( application*................................................642.6.11 - A(I0S.............................................................................................................6!2.6.12 - Add-on enu inter>ace...................................................................................67

2. - M%U.........................................................................................................682.7.1 - General............................................................................................................682.7.2 - STAT5S pa$e..................................................................................................722.7.3 - IIT A pa$e......................................................................................................732.7.4 - I( pa$e......................................................................................................742.7.! - IIT B pa$e......................................................................................................7!2.7.6 - %'+ pa$e.......................................................................................................762.7.7 - (5'+IAT, pa$e............................................................................................8"2.7.8 - +ateral 0eision 'a$e......................................................................................81

2.7. - V,0TIA+ 0,VISI pa$e............................................................................"2.7.1" - (I0 T pa$e..................................................................................................12.7.11 - ',0% pa$es...................................................................................................2


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2.7.12 - '0G pa$es..................................................................................................!2.7.13 - 0A(I AV pa$e..........................................................................................62.7.14 - S, %'+ pa$es...........................................................................................72.7.1! - (5 ,5 pa$e.....................................................................................1""2.7.16 - (ATA pa$e...................................................................................................1"2

2.8 - A/F and A/!H7 loi,...........................................................................1062.8.1 - A'%( /odes.................................................................................................1"62.8.2 - AT#0 /odes.................................................................................................1132.8.3 - %A................................................................................................................114

2. - Stand-B instru*ents.............................................................................11(2..1 - General...........................................................................................................11!2..2 - Standard ec&anical Instru/ents.................................................................11!2..3 - ((0I............................................................................................................1162..4 - loc=&rono/eter........................................................................................1172..! - ISIS.................................................................................................................1182..6 - Triple Bra=e Indicator.....................................................................................11

3.FMGS o+erations 9 "FB$ to "FM& ........................................120

3.1 - General.....................................................................................................120

3.2 - re:lit....................................................................................................1223.2.1 - IIT A.............................................................................................................1223.2.2 - %'+..............................................................................................................1233.2.3 - +a route (,'A0T50,...................................................................................1263.2.4 - A00IVA+ pa$es and S, %-'+ .................................................................123.2.! - 0A( AV pa$e..............................................................................................123.2.6 - IIT B ? %uel Settin$s....................................................................................13"

3.2.7 - ',0% pa$es...................................................................................................1333.2.8 - ,n$ine Start and Ta@i.....................................................................................13!

3.3 - !A;# $FF +ase.....................................................................................136

3. - %li*< ase.............................................................................................10

3.( - %ruise +ase...........................................................................................11

3.6 - es,ent ase........................................................................................1(0

3. - A++roa, and landin............................................................................1(1


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1. Fore'ord

$"2% &'() software is a freeware solution to replicate the real $irbus $"2%*s &light'anagement + (uidance )ystem ,&'()- and main electronic instruments for 'icrosoft*s&light )imulator .

0f you hae any uestions remarks or else you can contact me through e3mail ,jeehell at jeehell.org- or through mycockpit.org forums ,4nglish- or aircockpit.com forums,&rench-.

he present guide will depict eery functions implemented in the software and describe allinstruments.

he standard operations will be e6plained on a sample flight between oulouse ,7&89-and :ice ,7&':-.

A!!#&!)$& 9

!is so:t'are is ele5ent da*ae o,,urred to our sste*= ) 'on?t ta>e an lia


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2. )nstru*ent a++li,ations

2.1 - PFD (Primary Flight Display)

2.1.1 - General View

,1- 3 $ttitude 0ndicator ,$


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2.1.2 - Attitude Indicatr

his is the heart of the P&


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2.1.! - "peed #ape

,1- = 0$) inde6

,2- = $ctual 'ach number shown if greater than '%.5

,"- = 0$) target. 0f speed target is out of scale range then the numeric alue isshown either aboe or below the scale in the same color as the inde6.

,#- = 'a6imum 0$) red and black ribbon moing according to aircraft ma6imumspeeds ,>&4 >74 ''9 >'9-.

,5- = 0$) trend. )hows the 0$) to be reached in 1%s if acceleration is constant.

,;- = >7) speed this amber ribbon starts at 3protection speed and stops at the>7) speed ,lowest selectable speed-.

,?- 3 3protection ribbon. Ranges from >stall to >3protection. 0f 0$) drops inside

this ribbon 3protection automatically engages and 9($ is applied.

,- = )tall speed ribbon.

,D- = &laps retraction speed

,1%- = :e6t flap setting >&4

,11- = Rotation speed ,>r- ,not a real alue s&own-

,12- 3 (reen dot best lift/drag ration in clean configuration

,1"- = 1 ,not a real alue s&own-.


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2.1.$ - Altitude indicatins

,1- = $ctual altitude ,in respect to the barometric setting- ,2- = $ltitude target. 0f the target is out of scale range then the numeric alue is

shown either aboe or below the scale in the same color as the inde6.

,"- = (round altitude ribbon

,#- = Radio altimeter


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2.1.% - Vertical "peed

he green line is an analog indicator and moes along the >/) scale. 7imits areE2%%%ft/min. he green number is the >/) in hundreds of ft/min ,here >/) is then A11%%ft/min-.

2.1.& - 'eading #ape

,1- = 'agnetic heading inde6

,2- = 'agnetic heading target. 0f target is out of scale range then the numeric alueis shown either left or right of the scale in the same color as the inde6.

,"- = $ctual magnetic track


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2.1. - Flight Path Vectr

he &light Path >ector ,&P>- is only shown when in rack/&P$ mode ,see &CF section-

,1- = &light Path $ngle

,2- =


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2.1. - Flight Directr (FD)

HG - V/S *ode 9

0n G/) mode the &< shows two green bars pitch and roll. o follow the &9R data block. )hown only if a alid signal is receied on :$> receier. 0tshows freuency course selected ,through 'C page- and 0:4/''9in descent-

,15- = G


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2.%.$ - Air:us F47 philsphy

he &'() (uidance part is controlled ia the $uto &light Control panel.

)elected mode means the pilots decide of the trajectory of the $C& whereas 'anaged

means the &'() computes the trajectory according to the &P7: entered ia the 'C


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0ntentionnally left blank


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2.& - erhead panel

2.&.1 - General ;

he oerhead panel is the main pilot/aircraft interface concerning the aircraft systems suchas bleed air electric power or hydraulic circuits. 0t is diided in smaller groups of switchespush3buttons indicators etc according to the concerned system.

&or the sake of readability oer a computer screen 0 decided to diide the oerhead panelin two which we*ll call the lower + upper oerhead panels ,please note the upper 9>GG< panelbetween Iday modeJ and Inight modeJ.

"o'er $5eread


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U++er $5eread

Please note that when you launch the 9>G *odemeaning

4ngines will stop running

$ll power sources are shut off ,electrical and pneumatics-.

0n that state all korryes and indicators are switched 9&&. 0t looks closely to the9>G< status when in3flight and eerything is working correctly e6cept that thebattery oltage displays are 9&& as well. #5ertin re*ains o:: until ou,onne,t #D! W7= or ou s'it, one


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2.&.2 - Anti-ice; +ights; AP7; 4a:in Pressure; ...

$ll those functions are located on the same sub3panel

A&!) )%# 9 o operate the wing or engine anti3ice systems simply click on thecorresponding korry. he blue $& label will show up.

Probe/@indow Geat actiates the windshield heating and the arious probes ,Pitot $o$$ etc-. @hen on $F9 mode ,no light- the heating is automatic and will be on as longas the aircraft is in the air. 0f $& the heating will be on een on the ground.

#D! "! and S)G&S 9he e6terior lights and interior signs are uite simply operated clickthe labels. &or the right side landing light you hae to click on inisible spots placed in thesame way as for the left side one. Please do not use &) standards &)F0PC offsets forlights only those 0 proide.

AU 9if starting condition are met you first hae to turn $&the master switch then pushthe start korry. @hen $PF power is aailable the green AVA)"label comes up.


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%AB)& 7#SS 9Cabin pressure is managed either automatically or manually.

0f you want to use automatic mode make sure '9/) C7. his switch is spring3loaded to neutral position. hereare two different calculators managing pressuriLation you can switch bymaintaining '9


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2.&.! - ,mergency ,lectric Pwer; GP3".

#M#7 #"#% W7 9 he emergency electric power is produced by a generator drien bythe Ram $ir urbine ,R$-. he R$ automatically deploys in flight when all othergenerators are lost. o manually e6tend it unguard the red switch and push the korry. heR$ cannot be stowed in flight it needs maintenance actions on the ground. he korry tothe left is not pushable it simply shows the status of the emergency generator. 4'4R(4: 4) is not operational.

GWS 9he (P@) korrys arm/disarm the following system ,from left to right-

)K) oerall (P@) system.

(/) '9


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2.&.$ - Air cnditining

A)7 %$& 9his panel allows the management of bleed air used for air conditioning andengine starting.

8leed air can be obtained from different sources

(:< GP if on the ground and engine bleeds are not aailable ,click (:< GP labelto actiate or see the add3on menu-

$PF 8744< if $PF is running

4:( 1 8744< + 4:( 2 8744< if corresponding engine is running

he bleed air is then used either to feed the start ales or the P$CHs which arecompressors to cool air then regulating cabin temperature.

he O38leed ale is used to proide bleed air to one side if not aailable on the other,e6ample $PF bleed to feed engine 2 start ale-. hree positions )hut $uto or open.

Kou can select the flow of the P$CHs with the P$CH &79@ rotary.

Kou can select target temperature in the cabin with the three rotaries labeled C9CHP0&@< C$80: and $& C$80:. hey are not animated. o select the temperature you canclick on the cold ,1BC- or hot labels ,"%BC- or the green arrow ,2#BC-. o selectintermediate temperatures left or right click to respectiely increase/decrease temperatureby 1BC.

G9 $0R opens/closes the hot air ale used to regulate the cold air coming from the

P$CHs.


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%A7G$ H#A! 9his panel controls the temperature in the cargo hold compartments.emperature is selected in the same way as the cabin compartments. he korrys control

the cargo hot air ale and the isolation ales.

2.&.% - /anual ,ngine "tart

hese guarded korrys are used to start the engines manually see later on.


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2.&.& - ,+,4 panel

#"#% 9his panel is used to manage electric generation and distribution.

8$ 1 + 2 are used to connect the batteries to the


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2.&. - 'ydraulic

H 9here are " hydraulic circuits on the $"2% family

(reen pressuriLed thanks to the 4:( 1 Pump

8lue pressuriLed by an electric pump or an emergency pump powered by the R$

Kellow pressuriLed thanks to the 4:( 2 Pump or an electric pump

0n case of low pressure in green or yellow circuit the Power ransfer Fnit ,PF- canpressuriLe the two simultaneously ,on ground with one running or pump failure in flight-.

Kou can e6tend the R$ here as well ia the red guarded switch.


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2.&. - Fuel

FU#" 9his panel manages the fuel pumps and the fuel O3bleed. 0f all pumps are 9: and'9


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2.&.1 - ,ngine "tart (ptinal n V'D applicatin)

7ocated on the Pedestal on the real $C& this panel is optionally displayed by going in the

right click menu.

o start an engine automatically

'ake sure start ale has pressure

)elect '9G


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2.&.11 - ADI"

,1- = 7C< display

,2- =


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his panel is used to control the $


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2.&.12 - Add-n /enu inter=ace

)ome options are only related to ground handling such as connection of ground GPground P@R and stowing of the R$. o simulate ground crew communications thesoftware adds " items in the $dd3on menu in the &) tool bar

4O P@R connects/disconnects the e6ternal electrical power.

(:< GP connects/disconnects the ground high pressure supply.

R$ stows the ram air turbine ,een in flight unrealistically-.


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2. - /4D7

2..1 - General

he 'ultifunction Control +


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,1- 3 7eft )election Heys ,7)H-.

,2- 3 Right )election Heys ,R)H-.

,"- = $lphanumeric keyboard

,#- = 'C


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Kou can either simply use your own keyboard ,see table ne6t page-- while making surethe 'C


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he "eft Selection ;eys will be called "S;?s.

he 7ight Selection ;eys will be of course the 7S;?s.

&irst line 7)H is thus "S;1 etc...

8elow line number ; is a line called )cratchpad S. $ll data we want to enter using the7)H/R)H must first be typed in the )cratchpad. hen to transfer the data to the line we

push the corresponding 7)H/R)H.

he orange suares signal data input necessary for a correct &P7: setup.

8lue data fields is usually modificable data.

(reen fields are usually calculated and cannot be be changed by the pilots.

;e


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2..2 - "#A#7" page

his is the page that shows up when you launch the 'C


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2..! - I0I# A page

his page is brought up by pressing the 0:0 key on the 'C


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0f a &R9'/9 couple is entered A")G& )7SS in 37 push the R)H" to initialiLe the 0R)and display all attitude and position data on P&< and :< ,if $


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1" to (" 9enter different winds for different altitudes. )ynta6 OOO/KK/YYY whereOOO is true wind direction KK is wind speed in knots and YYY is a flight leel,1%%%ft is thus &71%-

(7 9no effect

6" 9cancel any new alue entered and back to 0:0 $ page

67 9$ccepts new alues entered and back to 0:0 $ page.

2..% - I0I# 6 page

$lso called 0:0 &uel Prediction. 9nce a route has been entered you need to enter herefuels alues in order to initialiLe fuel calculations. )&)! Bis accessed on ground ia Rightor 7eft arrow when 0:0 $ is shown. ,the arrows in title line indicate you can switch pages-.

1" 90nput ta6i fuel in tons

17 9 input here the Y&@C( ,Yero &uel @eight Center of (raity- and the Y&@,Yero &uel @eight in tons-. )ynta6

Y&@/Y&@C( if you want to change both alues

Y&@ or /Y&@C( if you only want to change one alue.

2" 9 flight plan fuel in tons and in time. 2.;/%%5% means the flight plan route willneed 2.; tons of fuel and will last %%h5%min without any resere

27 9otal fuel before start3up in tons. Kou can uplink it ia R)H"

3" 9Route fuel resere input a percentage of route fuel to consider as resere fuel.Kou can only input a percentage but the 'C


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37 9Fse R)H" to get Y&@C( Y&@ and block fuel ia datalink.

" 9$lternate route trip fuel and duration.

7 9ake 9ff @eight as calculated the following way 9@ Z Y&@ A block = ta6i

(" 9&inal resere. 0nput synta6 OOKK where OO is hours and KK minutes. 4en ifthere are Leroes input four number ,e6 %%"% for "% minutes-. he number shown

before resere time is weight euialent in tons ,here 1.% tons for "% minutesresere-.

(7 97anding @eight as calculated in the following way 7@ Z 9@ = R4

6" 946tra fuel in tons and time ,here 1.1 tons %% hours "" minutes-. 46tra Z block = ta6i = trip = R4 = R)> = $7:

2..& - FP+0 page

his page is where the flight plan route is entered including )0


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,"- = )peed constraint ,magenta if met amber otherwise-

6"hows destination predictions ,time of arrial distance to go and estimated fuelon board-.

$ normal flight plan has more than 5 points so you can scroll through all points ia theertical arrows

6"is resered for destination airport.

@hen on the ground and &P7: hasn*t been scrolled down 1"shows departure airport.

o add a waypoint enter the name of the waypoint ,>9R :


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0f you want to insert 8$R)9 before $'&9F point push 7)H ne6t to $'&9F here is whatwill happen

he line labels between two points show the magnetic track and the distance in nauticalmiles between the two points.


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he numbers on the right are the speed and altitude profiles at each point in knots andfeet. hey are shown only when calculation is possible when weight and speeds data areinput.

0f nothing is entered in the scratchpad pushing a 7)H will prompt the "ateral 7e5isionpage and a R)H will prompt the Verti,al 7e5isionpage. 0f an airport is displayed on the

corresponding line R)H won*t hae any effect.

!o delete a 'a+oint=push C7R button then the adjacent 7)H.

Kou can as well add a waypoint with latitude and longitude place/bearing/distance orplace3bearing/place3bearing. )ynta6 is

+AT+ where

+ATstarts with the letter : or ) ,:orth or )outh- then one or two digits fordegrees of arc then two digits for minutes of arc and eentually a decimalpart for minutes of arc

+starts with the letter 4 or @ ,4ast or @est- then one to three digits for

degrees of arc then two digits for minutes of arc and eentually a decimalpart for minutes of arc.

#@a*+le 9:##%1./4%%?15 stands for ##B1.* :orth and %%?B15* 4ast

'lace9earin$(istance where

'laceis the 0< of a >9R :


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2.. - D7P+I4A#, page

0f you insert a waypoint 0< ,>9R :


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2.. - +ateral eisin Page

"A! 7#V F7$M +ae9

$ccessed ia 7)H 1 to 5 in &P7: page. his page allows you to modify the lateraltrajectory from the selected point.

3" 9Push 7)H" to add an holding circuit at the selected point.

37 9enter a new waypoint in the scratchpad then push R)H" to add that waypointa>terthe selected point.

" 9actiates the $7: &P7: starting at the actie point.

7 9Changes the destination airport and deletes all points downstream from theselected one.

(7 9 click R)H5 to enter the airways page to follow airways to another point.

"S;6to go back to &P7 page.


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H$" A! +ae 9

$ccessed ia preceding page. 0t allows you to add an holding pattern at a point withdesired characteristics

1" 9inbound magnetic course toward holding fi6.

2" 9direction of turns. R for right and 7 for left.

3" 9outbound track length either in time or distance

input OO.O for time in decimal minutes

input /KK.K for decimal nautical miles

Press 7S;6to insert the holding pattern or "S;6to cancel.


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A)7WAS +ae 9

his pages is accessed ia lateral reision page. 0t allows you to add to the flight planseeral waypoints from airways easily

&irst enter an airway which connects at the selected reision point and push 7)H1.

hen you can successiely enter airways which connect with the preceding oneia 7)H 2 to 5. he connecting point between two $@K is automatically entered inR1 to #.

9nce you hae selected all the $@Ks you need enter the last waypoint of the last$@K ia the R)Hs1 to 5 ,according to the number of $@Ks used-.

0n the screenshot aboe $@K F'?"" was entered then F:?1. hose two connect at(0P:9 point. @e wanted to e6it F:?1 at 9'$)0 so we entered it in R2 line.

@hen you are happy with the $@Ks entered push R)H; to accept the route or 7)H; toget back to lateral reision page.

$ll the points along the selected $@Ks to the last point are automatically entered in the&P7: ,in our e6ample all points between 8$R)9 and 9'$)0 on F'?"" then F:?1-


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#A7!U7# F7$M 9

0n &P7: page if 17 displays the departure airport pushing 7)H1 prompts this page.

Push 7)H1 again to access departure R@K selection page


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he first line shows dashes if it*s the first time this pages is accessed during preflight. helines 2 to 5 show the aailable runways at departure $P with length in meters 07)freuency and course if aailable.

0f a R@K and )0< had preiously been selected the ne6t page shows up instead withgreen characters in line1

o select a R@K simply push the 7)H adjacent to it. 0f more than # R@Ks are aailable


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you can scroll with ertical arrows. @hen selecting a runway it prompts you automaticallyto the )0< selection page

0n the same way you can select the desired )0< ia 7)H 2 to 5 and scroll with erticalarrows if more than # are aailable. @hen selected the arrow before the )0< namedisappears ,here 89


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A77)VA" !$ +ae 9

0n &P7: page pushing 7)H; prompts the ne6t page

&rom that page you can access the )$R and approach selection pages. Pushing R)H1prompts the approach selection page

)elect the desired approach with 7)H " to 5. Kou can scroll if more than " are aailableusing the ertical arrows keys. 4ach procedure is for 9:4 R@K only and the length in

meters as well as 07) data ,if aailable- are displayed. Clicking the desired 7)H promptsthe )$R selection page


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he aailable )$Rs are selectable with 7)H " to 5. o connect a )$R to the approach

procedure you may need to add a I>0$J. o do so push the 7)H2


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:otehe >0$s aailable depend on the approach procedure selected and in fact connectthe 0$& to the final segments of the approach procedure. he )$Rs connect the en3routephase to the 0$&.

)elect the >0$ you need ia 7)H 2 to 5. 0$* if you don*t need any >0$. )ome approach procedures cancome without any ia.

9nce you*e selected your >0$ ,or no >0$- and your )$R you might hae to chosebetween )$R transitions in the same way as )0< transition using the R)H" to 5.

9nce you*re done push R)H; to insert the terminal procedures in the &P7:.


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2..* - V,#I4A+ ,VI"I0 page

0n &P7: page pushing R)H1 to 5 prompts this page if scratchpad is empty.

2" 9C78 or


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2..1 - DI # page

Push )7key on 'C


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2..11 - P,F pages

hose pages are accessed ia the #7Fkey on the 'Cr and >2 in knots

" 9ransition altitude in feet

(" 9 hrust reduction altitude and acceleration altitude synta6

OOOO/KKKK where OOO and KKKK are the altitude alue of respectielyGR R4< and $CC altitude. 46 1%%%/1%%%.

$CC altitude shouldn*t be inferior to GR R4< altitude.

17shows the departure runway if it has already been entered ia departure lateralreision page.

37asks for take off flaps settings. >1/>r/>2 lower limit depends on that alue andchanging it for a lower alue ,2 to 1 for e6ample- will resets those speed alues.

7 9&le6ible take3off temperature ,BC- if you want to use &74O operations. 4ntryrange is aboe 9$ or R4& and below ;BC ,R4& depends on pressurealtitude-.


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Pushing 7S;6will prompt the ne6t phase of flight P4R& page P4R& C78.

#7F %"B +ae 9

his page is directly accessible when in C78 mode. 0t is no longer accessible once cruisephase is reached.

1"shows the speed mode that will automatically engage after setting the thrustleers at the C78 notch on initial climb ,for more details see the &'() section-.

2"72 shows the cost inde6 that is input from 0:0 $ page.

3"is the managed speed law. he 0$) alue changes according to the C78 )P mode engaged

&CF altitude aboe $C& current altitude

$C& not flying an altitude constraint

(/) mode is not actieC78 mode *anuall enaeswhen pilot pushes the altitude selector knob on the &CF

and conditions aboe are met.


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(isen$a$e/ent conditions ,one is enough-

:$> mode disengages ,ertical mode reerts to 9P C78-

$nother ertical mode engages

Pilot selects an altitude lower than current $C& altitude. ,ertical mode reerts to>/) mode-

$ %"B *ode 9

open climb mode controls the aircraft pitch to maintain the target speed ,managed orselected- but disregards any &P7: altitude constraint.

#nae*entconditions &CF altitude must be higher than actual $C& altitude A&,oneof the following-

Pilot pulls the altitude selector knob

$C& reaches $CC $7 with C78 armed and :$> not engaged

:$> mode lost when C78 is engaged

(isen$a$e/ent conditions ,one is enough-

$ny other ertical mode engaged

&CF altitude set lower than actual $C& altitude. ,ertical mode reerts to >/)mode-

#S *ode 9

this mode controls the aircraft pitch to fly along a calculated ertical profile which takes intoaccount the &P7: waypoint speed and altitude constraints and thus reuire the :$>mode to be engaged. he aim of the profile is to maintain idle thrust to reduce fuelconsumption. he target speed is maintained with a 32% knots error margin.

Ar*in conditions ,all of the following-

&CF altitude below current altitude

:$> engaged.

(isar/in$ conditions ,one is enough-

$nother ertical mode is engaged

&CF altitude higher than or eual to $C& altitude.

#nae*entconditions ,all of the following - :$> mode engaged

&CF altitude below $C& current altitude


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$C& not flying an altitude constraint

9 (/) 7$: mode lost when /)mode-

A"!I= A"! %S!7I *odes 9

$ltitude and altitude constraint acuire modes.

#nae*ent automatically when in C78 9P C78


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A"!= A"! %S!7 *odes 9

$ltitude hold modes. hey maintain either the &CF altitude of the constraint altitude ifertical profile is managed.

Ar*in conditions wheneer target altitude is different than actual altitude.

#nae*ent automatically if altitude is within 2%ft of target altitude.

(isen$a$e/entconditions any other ertical mode engages.

V/S FA *odes 9

hese modes maintain a constant >/) or a constant flight path angle. Kou can switchbetween the two with the G/) = RH &P$ pushbutton on &CF.

#nae*entconditions,one is enough-

Pull >/) &P$ selector knob or push it ,for immediate leel off- )elect a higher altitude than current $C& altitude in


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AP5FD cmmn mdes

e $ :: *odes 5erti,al S7S and lat e ral 7W4 9

hese modes enaeduring take off.

)R) mode maintains >2A1% knots by adjusting pitch X it disen$a$es when reaching$cceleration $ltitude ,$CC $7-.

R@K mode is not modeled yet.

)"S A++roa,es *odes 9

hese are the following modes9

ertical (/) or (/)[

lateral 79C or 79C[

7$:


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7$"" $U! enaeson touch down.

& on re,ision A ++roa,es 5erti,al F)&A" C lat e ral A &AV4 9

)elected approach is non307).

his two modes ar*by pressing $PPR pushbutton.

$PP :$> enaeswith same conditions as :$> mode

&0:$7 enaesif armed and$PP :$> is engaged.

hey both disen$a$e if $PPR pushbutton is pushed again or another ertical mode isengaged.


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2..2 - A5#' mdes

$uto hrust ,$/GR- controls the engines N:1 setting. 0t is used either to maintain aconstant :1 setting ,GRF) mode- or to adjust speed/mach ,)P44


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2..! - F/A

he &light 'ode $nnunciator displays the current ar*edand enaed$P/&< and $/GRmodes

Columns ,1- ,2- and ,"- ,respectiely A/!H7 5erti,al mode and lateral mode-show in green the modes engaged and in blue the modes armed. @hite is used

when $/GR is armed but not engaged. Column ,#- shows $pproach capabilities.

Column ,5- shows $P/&< and $/GR status in white if engaged in blue if armed.

9n the picture aboe taken during take off roll we can see that thrust leers are set at9($ )R) is enaed C78 :$> and $/GR are ar*ed.

will be later engaged.


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2.* - "tand-6y instruments

2.*.1 - General

Kou now hae the choice to install and run each specific standby instrument duringinstallation ,see )nstallation Guide chapter "-.

he following chapter will describe briefly each of them and list the keyboard shortcutsaailable. here are also &)F0PC and joysticks commands possible.

2.*.2 - "tandard /echanical Instruments

he usual mechanical stand3by instruments are included

0ndicated $irspeed 0ndicator

$ltimeter ,feet or meters-

$rtificial GoriLon.

8arometric settings is changed using $S or S keys.


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2.*.! - DD/I

he 9R1/$9R2/$


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2.*.$ - 4lc$file in the )8K folder.


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2.*.% - I"I"

he 0)0) ,0ntegrated )tandby instruments )ystem- is a small P&< with 0$) altimeter andattitude information

Kou can show 07) scales ,aboe right picture- by pressing "S.

he baro3pressure is adjusted as well with $S and S. Kou can switch back tostandard 1%1"hpa pressure using MS.

he speed and altitude scales can show reference bugs. o do that you need to enter the8ugs menu using BS


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hen using and -keys you can naigate through the different bug bo6es. Kou can adjustthe desired bug ,the bo6 circled in magenta- using the $S and S keys ,the samekeys used for baro3pressure- and enable/disable it with MS.

2.*.& - #riple 6ra


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3. FMGS o+erations 9 "FB$ to "FM&

!.1 - General

0n this chapter we*ll be flying an imaginary flight from oulouse38lagnac ,7&89- to :iceRiiera ,7&':-. 0*ll try to describe most of the &'() functions throughout that flight.

Remember that a:ter laun,in te so:t'are= te air,ra:t 'ill Estate=which means all systems are inoperatie ,4lectrical pneumatics hydraulics fueletc...-. 0t is thus normal to get black screens only...

9f course there is an e6haustie flightdeck preparation procedure described in the aircraftmanualsX if you later want to stick as close as possible to the real operations you can finda lot of material on the web ,check out www.smartcockpit.com-.

&or our discoery flight we will first connect an e6ternal electrical power source ,no

please refrain from plugin your computer F)8 port into the wall socket LL- Checkchapter 2.;.;if necessary

9pen &) $dd3ons S menu and chose 4O P@R S.

9n the 9>G


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7et*s start the $PF ,seechapter 2.;.2-. @e can follow the spool up on the )


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!.2 - Pre=light

!.2.1 - I0I# A

)o here we are at the gate in 7&89. he P$O are slowly boarding the aircraft and wenow hae to start setting the &'() up with today*s flight.

&irst thing will be to align the 0R) so we can get a map on the :< and the P&< showingattitude data. o do so go to the 0:0 $ page in the 'C


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!.2.2 - FP+0

!e :ollo'in +aes are onl *eant as an e@a*+le te *a e5ol5e in te :uture=+arti,ularl due to ne' na5iation data u+dates 'itout an *odi:i,ations done totis uide.

9ur 9ps gae us the routing to :ice

AF7)% G3 FJ7 2( M!G G01 MJ N302 AB"A;

7et*s go to the &P7: page. &or the moment it looks like

Fse the up arrow ,- of the 'C


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ype $&R0C in the )cratchpad then insert it by clicking on "S;3to put it in place of &3P7:


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Push the "S;ne6t to $&R0C to prompt the lateral reision page at $&R0C point.

)elect $0R@$K) page ,7S;(-.

ype ("D in 17 ,"S;1- then &\R in 1R ,7S;1-.

&rom &\R we*ll follow the K25 airway ,2"- until '( ,27-.

$


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"says I333&P7:


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)ince we*ll be flying in ertical managed mode the white dot ne6t to the altitude window ison.

8ack to the 'C


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0nsert the departure procedure in the 'PK &P7: ,6"- nous obtenons la page suiante

8y clicking on 67 ,'PK 0:)4R- we accept the temporary flight plan.

&aisons le une nouelle fois d]filer jusu*^ l*]cran ci3dessous il nous faut supprimer lepoint $&R0C en ",C7R puis "S;- puis la


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!.2.$ - AIVA+ pages and ",4 F-P+0

9ur flight plan is now almost complete X we will hae to modify it for our arrial in 7&': onthe same principles as for the departure procedure.

he )4C &3P7: ,)econdary &light Plan- may be used to prepare for an emergency returnto oulouse after take off.

0 won*t go into such details as this document is meant only to be a Oui,> dis,o5er guideto \eeGell@are $"2% &'() X your personal knowledge and research will allow you tobenefit from the multiple features not presented here and get a ery realistic e6perience.

!.2.% - AD 0AV page

:ow we*ll tune the radio naigation aids to be able to follow the )0< een in case of 0R)failure.

(o to R$< :$> page on the 'C9Rs freuency respectiely 11?.?% and 115.%.

@e*ll input 9F in >9R1 and ($0 in >9R2.

@e can also manually insert the 07) of R@K"27.

4en if the autotune is functional it is best to manually insert the naaids to not losethe setting when needed..


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!.2.& - I0I# 6 Fuel "ettings

(o back to 0:0 $ page then with one of the horiLontal arrows switch to 0:0 8.

&uel and weight inputs are comple6 for beginners and een for adanced users.

)n real o+erations=the data to input depend on numerous parameters such as aircraft loaf,passengers fret- altitude winds at different altitudes on the &P7: alternate routemargins ,ta6in time holding before landing V-. Companies and piltos hae the data...which is not easily in the reach of simmers.

@eight and balance ,passengers cargo holds- and fuel distribution in the tanks obey tostrict rules and will impact the center of graity of the aircraft and thus its ability to fly.

Flit Si*ulatoruses the data,P$O and cargo Loning fuel- from the flight model shippedwith my software.

his data ,isible in the $ircraft / &uel and payload S menu- correspond to tereal distri


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7et*s go back to 0:0 8 page

JeeHellWare A320 FMGS has a ery simple solution for those who want to uickly flywihtout doing any payload calculations the software has a feature to import the fuel andpayload data of the flight model directly into the 'C


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For ad5an,ed users= there are third party add3ons which will allow you to conduct the fullweight and balance calculations. Kou*ll hae to

Change the fuel and payload S of &light )imulator to make them stick to your loadsheet S

&ill the 0:0 8 page accordingly.

:ote the &'() use the *etri, unit tons4= whereas &light )imulator can use pounds,7bs- or gallons X you can change &) settings to display Hgs.

Ho'e5er ou +ro,eed remember what you insert in the &'() are +redi,tions and

what you insert in &) is the a,tualdata.

:ote also that after engine start 0:0 8 is no longer aailable X you*ll hae to prompt &F47PR4< page if necessary.


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!.2. - P,F pages

:ow on to P4R& pages the first one is !A;# $FF +ae.

Gere also this data comes from comple6 charts and calculations. he numbers greatly

depend on the weight weather conditions runway state etc... 7e:eren,e s+eeds 9 0f you use a software such as opCat you can use it to

determine the >1 >r and >2 speeds and enter them in the ake 9ff page.9therwise you*ll hae to enter plausible alues according to the stall speed of theaircraft. Fsually >1 at 120 >ts >r at 130 >ts and >2 at 18 >tsis mostly 9H.

!ransition altitude 9 his depends on the departure airport. 0n oulouse it is at5%%%ft.

!rust 7edu,tion and A,,eleration altitudes 9he default alue is 15%% / 15%%aboe the airport ,the 'C


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Push now 7S;6key to call ne@t +ae 9 %"B.

0f you look at our )0< on the :


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!.2. - ,ngine "tart and #aBi

Passengers are seated luggage and cargo loaded cabin and holds doors are closed


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!.! - #AC, FF phase

9nce cleared for take off slowly moe the thrust leers to 5%N of :1 and check ,as onthe picture below- both engines hae the same :1.

:ow moe the leers into the &7O / 'C detent sicne we used a &74O 4'P in P4R&

$H4 9&& page. Gadn*t we entered that &7O temperature we*d hae to moe the thrustleers into 9($ detent.

9n the &'$ '$: &7O 52 S must be displayed in the first column


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0f you hae copilot he will call the reference speeds such as %kts >1 and >r. Check onthe P&< that your speed scale agrees with the callouts. )R)/R@K is engaged while C78and :$> are armed.

:otice the white bo6 with the white cross on the P&


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ground the cross marks the stick deflection ,ertically and laterally- and the bo6 showsthe delfection limits.

Reaching >r pull +roressi5el on the stick to achiee an initial pitch of around ?B thenafter lift off aim towards appro6imately 15B pitch up.

9nce >/) is positie retract the landing gear and follow the &< orders to match the )R)guidance.

Kou can engage the $P when airborne for more than 5 seconds. $P will keep >2A1% knots.

@han reaching the hrust Reduction $ltitude 7>R C78 message starts flashing on the&'$ in the first column

Kou must now put back the thrust leers into the C7 detent.

$/GR will now fully engage ,white on the &'$ last column- and reduce the :1N to the:1 settings reuired for the climb phase.

$P/&< will use the pitch to maintain the desired speed. )ince the $CC $7 is the same asthe GR R4< $7 the aircraft will accelerate towards our selected speed.

@hen reaching the $CC $7 the $P/&< commands a pitch decrease to allow the aircraftto accelerate aboe the 3) speed. his speed marks the minimum speed at which we can

retract the slats.


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GR C78 C78 and :$> are engaged on the &'$ and so are $P and $/GR.


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!.$ - 4lim: Phase

@hen the tight turn is done we go into managed speed mode by pushing the )P< knobon the &CF ,which now shows a dashed speed window with a white dot-. 8elow &71%%

we*ll be limited to 25% kts.

@hen passing 5%%%ft ,our transition altitude- pull the Q:G knob to switch the barometersetting to )< ,1%1" mb or 2D.D2 inGg-.

Passing &71%% will accelerate aboe the 25% kts limit to reach our climb speed. he pitchgoes down to allow that acceleration and so will the >/) until it can go up again when wemeet our target speed.

4n3route control clears us to our cruising altitude &7"1% select "1%%% in the altitudewindow of the &CF ,and push the $7 selector knob if you were already in $7 mode-.&7"1% target will be displayed on the P&< altitude scale.

@hen approaching &7"1% >/) will reduce to capture the altitude. &'$ will now show themodes '$CG $7 CRY and :$> engaged.

0f the '


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!.% - 4ruise phase


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$ bit later the 'C


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@e can now fill the $PPR P4R& page by pushing the P4R& key then clicking twice on7S;6,:4O PG$)4- fill in the Q:G ,1%1?- temperature ,15B- wind ,2%%/1%- transitionaltitude ,5%%% ft as indicated by the apporach chart- and also the '


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)hortly after '$RR0 fi6 ,see ne6t page- $C clears us directly to '(.


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Call


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$t the same time the aircraft banks left to join the new actie waypoint.

:otice the arrow symbol just before '( this it the op of descent S calculated by the&'(). 0t*s the point where descent phase should be started to follow the optimum flight

profile.


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8y datalink our company adises us the current procecure in :ice is the 07) %#7. @e canfinish filling in the 'C


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9ur last Ien routeJ waypoint is $87$H and the charts show we hae to follow the $87$;R)$R click on "S;( and you*ll get the following screen

he $PPR >0$ here is automatically filled in ,if the &'() can determine the correct >0$route-. 9therwise you*d hae to check the paper charts $87$H 5R ends at 'F) so wemust put the 'F) >0$ to correctly join the 07)%#7 $PPR.

7et*s insert our arrial route by clicking "S;6 then 7S;6.

@hile in the &P7: page don*t forget to clear any &3P7:


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!.& - Descent Phase

@e*e been cleared to descend to &712%. )elect 12%%% on the &CF and push the $7knob to engage managed descent.

his way we force the descent before reaching the 9


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Manaed des,ent s+eed is constantly adjusted by the &'() to try it*s best atmaintaining the descent profile symboliLed by the >/ target. $ll that keeping enginesat idle.

:ote that an aircraft can hardly descent and slow down at the same time. his is why it willreduce it*s >/) to match a speed constraint such as 25% kts below &71%% or a lower

speed asked by the $C.

)peaking of constraints notice that 12%%% is displayed in magenta on the P&


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@hen speed is below the >&4 of first flaps setting select flaps 1.


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he 07) should be perfectly followed until the threshold. 0t may happen there is a little glideor localiLer deiation. 0f it happens you hae to land manually.

Right before touching down retard the thrust leers to 0 '$O detent- to slow the aircraft down more efficiently.he auto3brake will also actiate automatically.


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9n the ground if rollout mode is giing bad guidance use the rudder pedals to control theaircraft.

$t ?% kts put the thrust leers back into R4> 0


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