JeeHellWare A320 FMGS User Guide B38 Version
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1. Fore'ord.......... Fore'ord................... ................... ................... ............................ ................................................( .............................( 2.)nstru*ent a++li,ations........... a++li,ations.................... .................. ................... ..................................6 ........................6 2.1 - F ri*ar Flit is+la4 .............. ....................... ................. .............................................6 .....................................6 2.1.1 - General View.....................................................................................................6 2.1.2 - Attitude Indicator................................................................................................7 2.1.3 - Speed Tape...................................................................................................... Tape...................................................................................................... ..8 2.1.4 - Altitude indications............................................................................................. 2.1.! - Vertical Speed..................................................................................................1" 2.1.6 - #eadin$ Tape.................................................................................................. Tape.................................................................................................. .1" 2.1.7 - %li$&t 'at& Vector......................................................................................... ....11 2.1.8 - %li$&t (irector )%(*..........................................................................................12 2.1. - I+S and V(,V deiation Scales......................................................................14 2.1.1" - %li$&t ode Annunciator )%A*.....................................................................1! 2.1.11 2.1.1 1 - %la$s and /essa$es................................................................................. .....16
2.2 - &a5iation is+la &4..................... &4............................. ................. ................. .....................................1 .............................1 2.2.1 - General............................................................................................................17 2.2.2 - I+S 0ose /ode................................................................................................18 2.2.3 - V0 0ose /ode..............................................................................................1 2.2.4 - AV /odes )0ose and Arc*.............................................................................2" 2.2.! - 'lan /ode........................................................................................................22 2.2.6 - ,G'S............................................................................................................23 2.2.7 - TAS................................................................................................................24 2.2.8 - &rono/etre....................................................................................................27
2.3 - #nine / Warnin is+la #/W................................................. #/W............................. .................................. ..............28 28 2.3.1 - General............................................................................................................28 2.3.2 - ,n$ine 'ara/eters..........................................................................................2
2. - Sste*/Status is+la S4..................... S4............................. ................. ................. ...............................31 .......................31 2.4.1 - General............................................................................................................31 2.4.2 - ,GI,...........................................................................................................33 2.4.3 - B+,,(.............................................................................................................34
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1. Fore'ord.......... Fore'ord................... ................... ................... ............................ ................................................( .............................( 2.)nstru*ent a++li,ations........... a++li,ations.................... .................. ................... ..................................6 ........................6 2.1 - F ri*ar Flit is+la4 .............. ....................... ................. .............................................6 .....................................6 2.1.1 - General View.....................................................................................................6 2.1.2 - Attitude Indicator................................................................................................7 2.1.3 - Speed Tape...................................................................................................... Tape...................................................................................................... ..8 2.1.4 - Altitude indications............................................................................................. 2.1.! - Vertical Speed..................................................................................................1" 2.1.6 - #eadin$ Tape.................................................................................................. Tape.................................................................................................. .1" 2.1.7 - %li$&t 'at& Vector......................................................................................... ....11 2.1.8 - %li$&t (irector )%(*..........................................................................................12 2.1. - I+S and V(,V deiation Scales......................................................................14 2.1.1" - %li$&t ode Annunciator )%A*.....................................................................1! 2.1.11 2.1.1 1 - %la$s and /essa$es................................................................................. .....16
2.2 - &a5iation is+la &4..................... &4............................. ................. ................. .....................................1 .............................1 2.2.1 - General............................................................................................................17 2.2.2 - I+S 0ose /ode................................................................................................18 2.2.3 - V0 0ose /ode..............................................................................................1 2.2.4 - AV /odes )0ose and Arc*.............................................................................2" 2.2.! - 'lan /ode........................................................................................................22 2.2.6 - ,G'S............................................................................................................23 2.2.7 - TAS................................................................................................................24 2.2.8 - &rono/etre....................................................................................................27
2.3 - #nine / Warnin is+la #/W................................................. #/W............................. .................................. ..............28 28 2.3.1 - General............................................................................................................28 2.3.2 - ,n$ine 'ara/eters..........................................................................................2
2. - Sste*/Status is+la S4..................... S4............................. ................. ................. ...............................31 .......................31 2.4.1 - General............................................................................................................31 2.4.2 - ,GI,...........................................................................................................33 2.4.3 - B+,,(.............................................................................................................34
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2.4.4 - ABI '0,SS50,.........................................................................................3! 2.4.! - ,+,T0IA+...................................................................................................36 2.4.6 - #(0A5+I....................................................................................................37 2.4.7 - %5,+................................................................................................................38 2.4.8 - A'5..................................................................................................................3 2.4. - AI0 (ITIIG.......................................................................................4" 2.4.1" - (0G,............................................................................................41 2.4.11 2.4.1 1 - #,,+...........................................................................................................42 2.4.12 - %+IG#T T0+S.....................................................................................43 2.4.13 - 05IS,.........................................................................................................44
2.( - Flit %ontrol Unit F%U 4....... 4................ ................. ................. ................. ................. ................. ....................... ...............( ( 2.!.1 - General............................................................................................................4! 2.!.2 - ,%IS panel...................................................................................... ......... ................ .......47 47 2.!.3 - Auto-%li$&t ontrol...........................................................................................48 2.!.4 - Air9us %5 p&ilosop&:....................................................................................!"
2.6 - $5eread +anel....... +anel................ ................. ................. ................. ................. ................. ................. ...............................(2 ......................(2 2.6.1 - General ;....................................................................................................... !2 2.6.2 - Anti-ice< +i$&ts< A'5< a9in 'ressure< ...........................................................!6 2.6.3 - ,/er$enc: ,lectric 'ower< 'ower< G'S. .............................................................. ..!8 2.6.4 - Air conditionin$.................................................................................................! 2.6.! - anual ,n$ine Start........................................................................................6" 2.6.6 - ,+, panel......................................................................................................61 2.6.7 - #:draulic................................................................................................ ......... .........62 62 2.6.8 - %uel..................................................................................................................63 2.6. - Auto Bra=e )optional on V#( application*....................................................63 2.6.1" - ,n$ine Start )optional on V#( application*................................................64 2.6.11 2.6.1 1 - A(I0S.............................................................................................................6! 2.6.12 - Add-on enu inter>ace...................................................................................67
2. - M%U....... M%U................ ................. ................. ................. ................. ................. ................. ...............................................68 ......................................68 2.7.1 - General............................................................................................................68 2.7.2 - STAT5S pa$e..................................................................................................72 2.7.3 - IIT A pa$e......................................................................................................73 2.7.4 - I( pa$e......................................................................................................74 2.7.! - IIT B pa$e......................................................................................................7! 2.7.6 - %'+ pa$e.......................................................................................................76 2.7.7 - (5'+IAT, pa$e............................................................................................8" 2.7.8 - +ateral 0eision 'a$e......................................................................................81 2.7. - V,0TIA+ 0,VISI pa$e............................................................................" 2.7.1" - (I0 T pa$e..................................................................................................1 2.7.11 2.7.1 1 - ',0% pa$es............................................................................................. ......2
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2.7.12 - '0G pa$es..................................................................................................! 2.7.13 - 0A(I AV pa$e..........................................................................................6 2.7.14 - S, %'+ pa$es...........................................................................................7 2.7.1! - (5 ,5 pa$e.....................................................................................1"" 2.7.16 - (ATA pa$e.......................................................................................... .........1"2
2.8 - A/F and A/!H7 loi,...........................................................................106 2.8.1 - A'%( /odes.................................................................................................1"6 2.8.2 - AT#0 /odes................................................................................................ .113 2.8.3 - %A................................................................................................................114
2. - Stand-B instru*ents.............................................................................11( 2..1 - General...........................................................................................................11! 2..2 - Standard ec&anical Instru/ents.................................................................11! 2..3 - ((0I.................................................................................................... ........116 2..4 - loc=&rono/eter........................................................................................117 2..! - ISIS.............................................................................................................. ...118 2..6 - Triple Bra=e Indicator.....................................................................................11
3.FMGS o+erations 9 "FB$ to "FM& ........................................120 3.1 - General.....................................................................................................120 3.2 - re:lit....................................................................................................122 3.2.1 - IIT A.............................................................................................................122 3.2.2 - %'+..............................................................................................................123 3.2.3 - +a route (,'A0T50,...................................................................................126 3.2.4 - A00IVA+ pa$es and S, %-'+ ........................................................ .........12 3.2.! - 0A( AV pa$e..............................................................................................12 3.2.6 - IIT B ? %uel Settin$s....................................................................................13" 3.2.7 - ',0% pa$es...................................................................................................133 3.2.8 - ,n$ine Start and Ta@i.....................................................................................13!
3.3 3. 3.( 3.6 3. -
!A;# $FF +ase.....................................................................................136 %li*< ase.............................................................................................10 %ruise +ase...........................................................................................11 es,ent ase........................................................................................1(0 A++roa, and landin............................................................................1(1
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1. Fore'ord $"2% &'() software is a freeware solution to replicate the real $irbus $"2%*s &light 'anagement + (uidance )ystem ,&'()- and main electronic instruments for 'icrosoft*s &light )imulator . 0f you hae any uestions remarks or else you can contact me through e3mail ,jeehell ≪ at ≫ jeehell.org- or through mycockpit.org forums ,4nglish- or aircockpit.com forums ,&rench-. he present guide will depict eery functions implemented in the software and describe all instruments. he standard operations will be e6plained on a sample flight between oulouse ,7&89and :ice ,7&':-.
A!!#&!)$& 9 •
•
•
!is so:t'are is < no *eans related to Air
ind or aeronauti,al ,erti:i,ation= el e5ent da*ae o,,urred to our sste*= ) 'on?t ta>e an lia. !e use and distri te "i,ense.t@t :ile to >no' 'at are te rits ou a5e 'it tis 5ersion.
JeeHell A320 FMGS %o+rit 2011-201 Jean "u, &itard - All rits reser5ed %renc& translation and editorial support 9: ic&el 'icue )2"14*
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2. )nstru*ent a++li,ations 2.1 - PFD (Primary Flight Display) 2.1.1 - General View
• • • • • • •
,1- 3 $ttitude 0ndicator ,$<0,2- = )peed ape ,"- = >ertical )peed ,#- = $ltitude ape ,5- = Compass ape ,;- = 8arometric )etting ,?- 3 &light 'ode $nnunciator ,&'$-
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2.1.2 - Attitude Indicatr his is the heart of the P&<. 0t shows the $C& attitude ,pitch bank sideslip-.
• • • • •
,1- = $ircraft reference symbol ,2- = Roll inde6 ,"- = )ideslip inde6 ,#- = Pitch limits of the &ly38y3@ire ,&8@- ,A"%B/315B,5- = 8ank limits of &8@
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2.1.! - "peed #ape
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,1- = 0$) inde6 ,2- = $ctual 'ach number shown if greater than '%.5 ,"- = 0$) target. 0f speed target is out of scale range then the numeric alue is shown either aboe or below the scale in the same color as the inde6. ,#- = 'a6imum 0$) red and black ribbon moing according to aircraft ma6imum speeds ,>&4 >74 ''9 >'9-. ,5- = 0$) trend. )hows the 0$) to be reached in 1%s if acceleration is constant. ,;- = >7) speed this amber ribbon starts at α3protection speed and stops at the >7) speed ,lowest selectable speed-. ,?- 3 α3protection ribbon. Ranges from >stall to >α3protection. 0f 0$) drops inside this ribbon α3protection 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
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,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 are E2%%%ft/min. he green number is the >/) in hundreds of ft/min ,here >/) is then A11%% ft/min-.
2.1.& - 'eading #ape
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,1- = 'agnetic heading inde6 ,2- = 'agnetic heading target. 0f target is out of scale range then the numeric alue is 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<(3>/) mode the &< shows two green bars pitch and roll. o follow the &< guidance center the $C& symbol on both bars.
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!ra,>/FA *ode 9
0n H/&P$ mode the &< shows the &light Path on the &P< to achiee the correct pitch attitude and roll in order to get the &P< horiLontal.
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2.1.* - I+" and VD,V deiatin "cales )"S trae,tor de5iation 9
he 07) scales appear when an 07) freuency is entered either ia the 'C
,1- = 7ocaliLer Course
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Verti,al e5iation V / #V 9
he > / <4> inde6 appears at the engagement of descent ,at 9< or on manual actiation of <4) mode-.
2.1.1 - Flight /de Annunciatr (F/A) he &'$ is a summary of &'() mode status and will be discussed later on in the $P/&< and $/GR section.
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2.1.11 - Flags and messages
Gere are all the flags currently implemented. hey appear when the corresponding data is not aailable which means that the $<0R) are not operational check on the 9>G< to switch them on and align them.
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2.2 - 0aigatin Display (0D) 2.2.1 - General he :< has fie modes each representing different data • • • • •
07) rose mode >9R rose mode :$> rose mode :$> arc mode P7$: mode.
:$> arc and rose modes display the same data but arc only shows the D%B forward sector whereas rose modes show a ";%B sector. here are si6 range selections which do not affect the data displayed • • • • • •
1%:' 2%:' #%:' %:' 1;%:' "2%:'.
:< mode and range can be selected ia the 4&0) panels ne6t to the &CF.
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2.2.2 - I+" se mde
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,1- = $ircraft symbol ,2- = 'agnetic heading inde6 ,yellow line,"- = 'agnetic track ,green line and diamond shape,#- = (round )peed rue $ir)peed and wind at the aircraft. he green arrow represents the wind direction relatie to aircraft direction. ,5- = 07) data block.
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2.2.! - V se mde
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,1- = Geading target ,2- 3 >9R data block. )hown only if a alid signal is receied on :$> receier. 0t shows freuency course selected ,through 'C page- and 0< ,"- = Course
Captain :< show :$> 1 indications &9 :< shows :$> 2 indications.
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2.2.$ - 0AV mdes (se and Arc)
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,1- = $ctie &light Plan track. his green line is continuous if :$> mode is engaged and broken otherwise. ,2- = $ctie point. he magenta number is a constraint ,here below &71%%-. ,"- = :on actie point. ,#- = )econdary &light Plan ,if 'C
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,1- = 8earing 1 pointer and :$>1 data block ,2- = 8earing 2 pointer and :$>2 data block ,"- = Cross rack 4rror. 1.D7 means the $C& is 1.D:' to the left of the &P7: track. ,on this picture the $C& is flying in reerse direction of the &P7:...-
he bearing pointers appear in all modes e6cept Plan mode. he color is green for $<&s and white for >9Rs. Kou can select to display them or not ia the 4&0).
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2.2.% - Plan mde
he P7$: mode shows a map centered on the 2nd line point in the 'C
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2.2.& - ,GP3" @hen errain 9n :< is selected the :< displays ,in all modes- the terrain eleation according to the aircraft reference altitude in colors. he aircraft reference altitude is the $C& altitude or the altitude e6pected in "%s if descending more than 1%%% ft/minute.
Color code • • •
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Kou can switch 9:/9&& the 4(P@) ia the 'C
2.2. - #4A" he raffic Collision $oidance )ystem ,C$)- use the transponders of all aircraft in the icinity to detect risks of collision. 0t represents on the :< the position of other traffic to help acuire a situation awareness. 0t can detect traffic #%:' from $C& position and EDD%%ft from $C& altitude. here are four leels of risk each represented by a different symbol on :< • •
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,1- = pro6imate no collision risk. 0ntruder within ;:' laterally and E12%%ft ertically ,2- = raffic $disory ,$- potential collision risk. 4stimated ti me of closest position M #%s ,"- = Resolution $disory ,R$- real collision risk. 4stimated time of closest position M 25s ,#- = 9ther intruder no risks of collision
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&or each type of symbol the number below is the altitude difference in hundred of feet and the arrow is the ertical trend ,the difference between the two aircraft ertical speed-. &or $ alerts there is an aural warning *R$&&0C R$&&0C* and if the :< range or mode is not adeuate an amber flag appears on the :<. &or R$ alerts there is an aural warning *C70'8 C70'8* or *<4)C4:< <4)C4:<* and a isual aid on the P&< ertical speed indicator. 0f the :< range or mode is not adeuate a red flag appears on the :<. @hen an R$ is oer an aural message *Clear of conflict* is played.
0n order for the C$) to function you need to set your transponder on mode C and the C$) on any mode besides )8K. Kou can do so ia the 'C
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C$) modes are • • •
S!B C$) does not proide any traffic information !A only $ alerts are proided ,R$s are treated as as-. !A/7A all intruders displayed
00t is possible to inhibit pro6imates and other intruders ia the 'C
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•
A"" Pro6imates and intruders are shown at all times if within E2?%%ft. !H7! pro6imates and intruders are shown only if within E2?%%ft $:< a $ or R$ is present. ABV ,aboe- Pro6imates and intruders are shown at all times if within ADD%%ft and 32?%%ft B"W ,below- Pro6imates and intruders are shown at all times if within 3DD%%ft and A2?%%ft.
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2.2. - 4hrnmetre 8oth CP and &/9 :
here is only one control for it located on the glare3shield panel on the real aircraft. 0n the software you hae two ways to actiate it either push C on the keyboard while the :< window is focused or through the &)F0PC offset ;;<% ,see table-. 9ne push starts and shows the chronometer the second push freeLes it and the third push resets and hides the chronometer.
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2.! - ,ngine 5 3arning Display ,53D 2.!.1 - General he 4/@< usually displayed on the upper 4C$' presents arious important informations on the $C& systems. 0t is diided into four parts • • •
he upper left part part is resered for engine parameters. he upper right part is for fuel and flaps. he lower two parts are for 4C$' failure warning and memo messages. &or the time being only a few messages and C/7 are displayed.
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2.!.2 - ,ngine Parameters &1 9 his indicator shows the :1 in percentage to the ma6imum :1.
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,1- = $nalog pointer ,2- = :umerical alue ,"- = )mall white circle position of thrust leer ,#- = $mber line ma6 :1 ,5- = ransient :1 difference between commanded and actual :1. 9nly displayed with $/GR on. ,;- = 'a6 permissible :1 starts at 1%# N it*s the prohibited area of :1.
#G! 9 his indicator shows the 46haust (as emperature in Celsius degrees.
• • • •
,1- = $nalog pointer ,2- = :umerical alue ,"- 3 'a6imum permissible 4( ,starts at D5%BC,#- = 'a6imum 4( ,D15BC-.
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&2 and Fuel Flo' 9 :2 is in percentage of ma6imum :2. &uel flow is in kg/hour.
"e5er settin 9 0t shows the hrust rating mode according to leers position and the ma6imum N:1 alue $/GR can delier when in that position. 0f the leers are not in a defined notch only the numerical alue appears.
Fuel $n Board F$B4 and :la+s 9 he &98 ,&uel 9n 8oard- shows the total fuel on3board in kg. •
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he &lap indicator shows the flaps ,&- and slats ,)- settings. he green triangles show the actual position. he blue ones the selected position ,ia pedestal leer- they disappear when selected and actual positions match. he te6t below the indicator is the selected flaps position. 0t*s green when selected and actual positions match and blue when flaps/slats are i n transit.
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2.$ - "ystem5"tatus Display ("D) 2.$.1 - General he )< is usually displayed on the lower 4C$' on the main panel. 0t displays information on most aircraft systems through a set of system pages in a total of 12 pages. Gere is a list of the pages with the corresponding keypress to access it ,with )< page focused- • • • • • • • • • • •
4ngine ,48leed ,8Cabin pressure ,P4lectric power ,7Gydraulic ,G&uel ,& $PF ,$ $ir conditioning ,9
here are additional keyboard shortcuts for this window • •
• • •
K and F arm/disarm the ground spoilers is the 9 C9:&0( button on the 4C$' control panel ,4CP located on the pedestalR is the RC7 button of the 4CP 8$CH)P$C4 is the C7R button of the 4CP <47 is the 4'4R C$:C button of the 4CP
he selection of a page can be either manual or automatic. 8y default it*s automatic and the page displayed depends on the flight phase and aircraft configuration. o manually select a page push the key as in the list aboe. o get back to automatic selection push the same key again. 0f a page is displayed as a result of a failure you cannot manually oerride it to display another system page. he description of the pages in this chapter is intended to remain brief. $lmost eery indicators and labels are modeled. &or an in3depth description of )< pages and aircraft systems 0 suggest you read material such as &C9's ,www.smartcockpit.com -.
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he display is usually organiLed like in this picture
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,1- = )ystem Page aries according to the selected page ,either automatically or manually,2- = Permanent data shows the otal and )tatic $ir emperature ,$ + )$- the (load FC time and the (ross @eight ,(@-.
:ow let*s see each page independently.
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2.$.2 - ,0GI0, his page show arious information for each engine in addition to the 4@<.
• • • • • •
,1- = &uel used in kilograms ,2- = 9il uantity in N ,"- = 9il pressure in P)0 ,#- = 9il temperature in BC ,5- = )tart ale position ,here closed,;- = :1 fan ibrations
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2.$.! - 6+,,D 0t displays the status of the air bleed system.
• • • • • • • • • •
,1- = Gigh Pressure ale ,2- = 4ngine 8leed ale ,"- = 4ngine bleed pressure and temperature ,#- = Pack flow control ale and flow indicator ,5- = Pack compressor outflow temperature ,;- = Pack by3pass ale ,?- = Pack outlet temperature ,- = R$' air ale ,D- = O38leed ale ,1%- = $PF bleed ale
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2.$.$ - 4A6I0 P,""7, 0t displays the cabin pressuriLation system status.
•
• • • • •
,1- = 7anding runway eleation either selected manually or automatically ,cf oerhead,2- = Pressure difference P ,P)0-. ,"- = Cabin ertical speed ,ft/min,#- = Cabin altitude ,feet,5- = )afety ale ,;- = Packs status
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2.$.% - ,+,4#I4A+ his page shows the electric power generation and distribution to the different buses.
•
• • • • • • • • •
,1- = :ormal electric generation status ,oltage load and freuency-. 4ngine 1+2 generators $PF electric generator and ground power. ,2- = $C buses 1 + 2 ,"- = $C essential bus ,#- = ransformer3Rectifier 1 + 2 ,5- =
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2.$.& - '8DA7+I4 his page shows the hydraulic system status.
• • • • • • •
,1- = Gydraulic flui pressure in ( 8 and K circuits ,2- = Power ransfer Fnit ,PF-. ,"- = R$ drien electric pump ,#- = Gydraulic pumps ,5- = &ire ale ,;- = Gydraulic fluid uantity ,?- = Kellow electric pump
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2.$. - F7,+ his page displays the fuel system status.
• • • • • • • • • •
,1- = &uel used in kilograms ,2- = 4ngine 7ow Pressure fuel ale ,"- = &uel 9n 8oard in kilograms ,#- = $PF low pressure fuel ale ,5- = &uel O3feed ale ,;- = @ing tanks fuel pumps ,?- = Center tank fuel pumps ,- = 9uter wing tanks fuel uantity ,D- = 0nner wing tanks fuel uantity ,1%- = Center tank fuel uantity
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2.$. - AP7 his page shows the $u6iliary Power Fnit status.
• • • • • •
,1- = $PF electric generator status ,2- = $PF fan : in percentage of ma6imum : ,"- = $PF 46haust (as emperature ,#- = $PF bleed ale ,5- = $PF bleed air pressure in P)0 ,;- = $PF flap indication ,appears if flap open only-
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2.$.* - AI 40DI#I0I0G his page shows the air conditioning status.
• • • • • • • • •
,1- = Cockpit forward + aft compartments actual temperature ,BC,2- = Cockpit forward + aft compartments desired temperature ,BC,"- = rim air ales position ,#- = &orward + aft cargo compartments actual temperature ,BC,5- 3 &orward + aft cargo compartments desired temperature ,BC,;- = Cargo trim air ale ,?- = Cabin hot air ale ,- = Cargo isolations ales ,D- = Cargo hot air ale
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2.$.1 - D598G,0 his page shows the status of cabin + cargo doors.
• • • •
,1- = &orward doors ,2- = 4mergency escape doors and slides arming indication ,"- = $ft doors ,#- = Cargo door
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2.$.11 - 3',,+ his page shows the status of the landing gear the brakes and the spoilers.
• • • • •
,1- = 7anding gear and gear bay doors status ,2- = 8rake temperature ,"- = $utobrake Ready indication ,#- = $utobrake status ,5- = )poilers indication. Gere fully retracted.
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2.$.12 - F+IG'# 40#+" his page shows the position of the flight controls as well as the functioning of releant hydraulic circuits.
• • • • •
,1- = )peed brakes. Gere left )bs are retracted and right )bs are e6tended. ,2- = 7 + R $ilerons and corresponding hydraulic circuit ,8 + (-. ,"- = Pitch rim and corresponding hydraulic circuits ,( + K-. ,#- = 4leators and corresponding hydraulic circuits ,( 8 K,5- = Rudder and corresponding hydraulic circuits ,( 8 K-
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2.$.1! - 47I", his page shows a summary of engine air conditioning and pressuriLation status.
• • • • • • • •
,1- = &uel used in kilograms ,2- = 9il uantity in N ,"- = Pressure P in P)0. ,#- = Cabin compartments temperature ,5- = 4ngine :1 ibrations ,;- = 7anding eleation in feet ,?- = Cabin ertical speed ,ft/min,- = Cabin altitude
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2.% - Flight 4ntrl 7nit (F47 ) 2.%.1 - General he &CF is located on the glare3shield. 0t is one of the main interface between the pilots and the &'() along with the 'C
he software logic implemented regarding switches ans selectors is uite intuitie Si*+le s'it,es are pushed with a single click ,left or right7otar en,oders ,G<( )P< $7 >) and Q:G- • • •
urn with the mouse3wheel Push with left click Pull with right click.
7otar s'it,es as :< range and modes switches turn right with a right click and left with a left click. Kou can click the te6t ne6t to rotaries or :$> selectors to select what you want directly ,i.e. click on *$RC* to set :< in $RC mode on *inG(* to set Q:G in inG( or on *$<&* to set na pointers to $<&.-
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7es+onse ti*e is not al'as i**ediate ,due to networking delays- so do not triple or uadruple click... Master Warnin C Master %aution located on the glare3shield are not displayed but functional. •
•
• •
•
0f you disconnect the $P through the &CF the caalry charge S will sound until :ou press t&e aster arnin$ 9utton TT 0n the same way if you disconnect $/GR through the &CF button a single chime will sound and an 4C$' alert will show up on 4/@<. 0f GR leers are in C7 gate the :1 alue deliered by the &$<4C will be locked shown by an amber IGR 7HJ on the &'$. To unloc= t&e t&rust< :ou &ae to /oe t&e T#0 leers out o> t&e + $ate. To re/oe t&e ,A /essa$es< :ou &ae to pus& t&e pus&-9utton. 'aster @arning + 'aster Caution switches can be controlled by an &)F0PC offset see the Ad5an,ed Users Manual S for an offsets list. hey can also be controlled through keyboard shortcuts on the &CF window ,'aster @arning @ S et 'aster Caution C S-.
!e standard +ro,edure to dis,onne,t Auto ilot and Auto !rust $P red ake 9er button on both sticks or keyboard shortcut $ S. $/GR red 0nstinctie R or keyboard shortcut S. • •
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2.%.2 - ,FI" panel
•
,1- = $dditional :< data display ,only one can be engagedC)R shows constraints in magenta ne6t to flight plan points @P ,@aypoints- shows fi6es that are not in the &P7: :<8 shows :<8) that are not in the &P7: >9R shows >9Rs and <'4s that are not in the &P7: $RP shows airports ,2- = :< range selection ,"- = :< mode selection ,#- = :< bearing pointers selection ,5- = 07) scales on P&< ,;- = &< bars on P&< ,?- = oggles barometric pressure between standard ,pull- and Q:G ,push,- = Q:G displays in mb or in.Gg. 0f set to standard it reads I)
• • • • • • •
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2.%.! - Aut-Flight 4ntrl
• •
•
,1- = )P'$CG switch click to switch between )P< and 'ach mode ,2- = )peed display shows selected speed or 'ach number if in selected mode otherwise shows dashes ,U U U- and a white dot ne6t to it shows up. ,"- = )peed control Pull to enter selected speed mode Push to enter managed speed mode 'ouse3wheel changes alue by 1knot or %.%1 'ach ,#- = Geading displayshows selected heading or track if in selected mode otherwise shows dashes ,U U U- and a white dot ne6t to it shows up. ,5- = G<( control Pull to enter selected lateral mode Push to enter managed lateral mode 'ouse3wheel changes alue by 1B. ,;- = $ltitude
•
•
• • •
•
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•
@hen in managed mode the white dot shows up. ,?- = $ltitude control Pull to enter selected ertical mode Push to enter ertical managed mode 'ouse3wheel changes the alue by 1%%ft or 1%%%ft ,- = >ertical speed display )hows the selected ertical speed / &light Path $ngle or dashes,U U U U U- if ertical mode is either managed or 9P C78/<4) ,D- = >/) control 7eel3off push >) / &P$ pull 'ouse3wheel change alue by 1%% ft/min or by %.1B ,1%- = $PPR button click to engage the approaches modes 79C or (/) if 07) approach entered in &P7: $PP3:$> / &0:$7 modes if non precision approach selected ,11- = 79C pushbutton arm/disarms 79C only mode ,12- = $/GR pushbutton arms/disarms $/GR. o disarm/disengage $GR use the instinctie buttons ,located on the GR leers on the real $C&,1"- = $P1 + $P2 push buttons engage/disengage auto pilot. o disarm/disengage $GR use the instinctie button ,located on the stick on the real $C&,1#- = 4OP4< pushbutton engages e6pedite mode ,green dot in climb >:4/''9 in descent,15- = G<( / RH selector click to switch between G<(3>/) and RH3&P$ lateral modes. he corresponding modes show up aboe G<( and >) displays. ,1;- = 'etric $7 switch ,to toggle the display of altitude in meters on P&< and )<-. • • •
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2.%.$ - 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 $C& whereas 'anaged means the &'() computes the trajectory according to the &P7: entered ia the 'C
ou can read /ore a9out selected/ana$ed< $uidance /ana$e/ent in t&e A'%( and AT#0 c&apter .
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2.& - erhead panel 2.&.1 - General ; he oerhead panel is the main pilot/aircraft interface concerning the aircraft systems such as bleed air electric power or hydraulic circuits. 0t is diided in smaller groups of switches push3buttons indicators etc according to the concerned system. &or the sake of readability oer a computer screen 0 decided to diide the oerhead panel in two which we*ll call the lower + upper oerhead panels ,please note the upper 9>G< here has nothing to do with the circuit breakers panel on the real $"2%-. •
•
•
he lower panel is launched wheneer you launch the oerhead software. 0f you close this panel the software will close as well. Kou can fire up the upper panel with a right click on the panel then I)how upper 9>G
he main type of switch is the IkorryJ. 0t*s a pushbutton with one or two leds built3in. •
•
Fsually the lower part is the state of a function.
here are 2 or 3 +ositions s'it,es such as this one for the strobe light. Kou can choose the position you want by clicking on the label directly. )o for e6ample if you want to set the
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strobe light to automatic mode just click the I$F9J label to its right ,red arrow-
he same principle goes for the rotar
Click the labels 9r left/right click the rotary
)ome of the rotaries ,such as cabin temperature or landing leation- won*t moe een if clicked. o see the alue selected just moe the mouse cursor oer the rotary and a small label with the alue will appear. 9n the upper 9>G< you can show two additional panel 'i, are not +la,ed on te $VH on te a,tual air,ra:t. hey are the $uto38rake panel and the 4ngine start panel. )ince my software simulates the real operations of engine start and auto3brake it seemed necessary to hae those controls in handy. Goweer if you prefer to only use the &)F0PC offsets you can hide them ia the options window of the oerhead panel ,accessible ia a right click on the lower 9>G<-.
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)ome switches are uarded you can only operate them when unguarded. o do so simply click on the coer. o guard the switch back simply click on the remaining isible part. 0f you use the &)F0PC offsets guarded/unguarded state is ignored. he gray spots mark where you can imagine there is a korry that will maybe be filled in later on... 9ne of the gray spots on the lower left part of the lower panel is called R$0: RP7: S just ne6t to the @0P4R selector. 8y clicking on it you will in fact switch the 9>G< panel between Iday modeJ and Inight modeJ.
"o'er $5eread
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U++er $5eread
Please note that when you launch the 9>G< it will default to ,old and dar> *ode meaning • • •
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 the 9>G< status when in3flight and eerything is working correctly e6cept that the battery 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 4a:in Pressure; ... $ll those functions are located located on the same sub3panel sub3panel
A&!) )%# )%# 9 o oper operat ate e the the wing wing or engi engine ne anti3 anti3ic ice e syst system ems s simp simply ly clic click k on the the corresponding 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 long as the aircraft is in the air. 0f $& $& the heating will be on een on the ground. #D! "! and S)G&S 9 he 9 he e6terior lights and interior signs are uite simply operated click the labels. &or the right side landing light you hae to click on inisible spots placed in the same way as for the left side one. Please do not use &) standards &)F0PC offsets for lights only those 0 proide. AU 9 if 9 if starting condition are met you first hae to turn $& $& the the master switch then push the start korry korr y. @hen $PF power is aailable the green AVA)" AVA)" label label comes up.
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%AB)& 7#SS 9 Cabin 9 Cabin pressure is managed either automatically automatically or manually. manually. •
•
0f you want to use automatic mode make sure '9<4 )47 korry is not illuminated. Kou can select the landing eleation with the rotary ,eihter automatic by clicking $F9 label or manually manually with left/right clicks-. 0f you want to control pressure manually make sure '$: is illuminated then select the cabin climb rate by clicking and maintaining mouse button down on the up or right label of '$: >/) C7. his switch is spring3loaded to neutral position. here are are two two dif differe ferent nt calc calcul ulat ator ors s mana managi ging ng pres pressu suri riLa Lati tion on you can can swit switch ch by maintaining '9<4 )47 button pushed down 1% seconds.
9ther functions are not yet modeled.
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2.&.! - ,mergency ,lectric Pwer; GP3". #M#7 #"#% W7 9 he emergency electric power is produced by a generator drien by the the Ram Ram $ir $ir urbi urbine ne ,R$ ,R$-. he he R$ R$ auto automa matic tical ally ly depl deploy oys s in flig flight ht when when all all othe other r generators are lost. o manually e6tend it unguard the red switch and push the korry. he R$ cannot be stowed in flight it needs maintenance actions on the ground. he korry to the left is not pushable it simply shows the status of the emergency generator. 4'4R (4: 4) is not operational.
GWS 9 he 9 he (P@) korrys arm/disarm the following system ,from left to right- )K) oerall (P@) system. (/) '9<4 glideslope S announcement. &7$P '9<4 too low flaps S announcement. 7<( &7$P " if landing configuration is flap " and not flaps full then arm this korry to aoid unnecessary warnings on final approach. • • • •
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2.&.$ - Air cnditining
A)7 %$& 9 his panel allows the management of bleed air used for air conditioning and engine starting. 8leed air can be obtained from different sources •
• •
(:< GP if on the ground and engine bleeds are not aailable ,click (:< GP label to 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 are compressors 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 can click on the cold ,1BC- or hot labels ,"%BC- or the green arrow ,2#BC-. o select intermediate temperatures left or right click to respectiely increase/decrease temperature by 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! 9 his 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
#"#% 9 his 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 9 here 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- can pressuriLe 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#" 9 his panel manages the fuel pumps and the fuel O3bleed. 0f all pumps are 9: and '9<4 )47 is not '$: then pumps are operated automatically by the aircraft. 9therwise the center pumps are operated. O38leed allows fuel from one side to feed the opposite engine.
2.&.* - Aut 6ra
AU!$/B7; 9 7ocated on the main instrument panel on the actual aircraft it controls the auto3brake and anti3skid systems. Click the korrys to select the leel of auto3brake desired ,push again to deactiate auto3 brake-. he $/)H0< switch is straight forward...
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2.&.1 - ,ngine "tart (ptinal n V'D applicatin)
7ocated on the Pedestal on the real $C& this panel is optionally displayed by going in the right click menu. o start an engine automatically • • •
'ake sure start ale has pressure )elect '9<4 0(:/)$R. )elect '$)4R switch 9:.
o start an engine manually • • • •
'ake sure start ale has pressure )elect '9<4 0(:/)$R. )elect 4:( '$: )$R 9: ,lower 9>G<)elect '$)4R switch 9: when :2W2%N.
he fuel 7P and GP ales are operated automatically. o abort start or stop an engine select '$)4R switch off.
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2.&.11 - ADI"
• • • • • • •
,1- = 7C< display ,2- =
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his panel is used to control the $<0R) $ir
•
he $
o work correctly the 0Rs need to be IalignedJ. •
•
•
Put the 0Rs mode selector on :$> then the I$70(:J light comes on. @hen it comes off the corresponding 0R is aligned. &ull alignment takes around 1% minutes. here is a fast alignment feature which takes only "%s. o do so when on :$> switch back to 9&& then :$> again in less than 5 seconds. &ast alignment is always possible unlike on the real $C&.
he $ mode is not yet fully functional the $<0R) will only proide $ir data. 7ater on it will be possible to enter manually the G<( when in $ he keyboard is not working either and the only way to initialiLe the 0R) position is ia the 0:0 page on the 'C
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2.&.12 - Add-n /enu inter=ace
)ome options are only related to ground handling such as connection of ground GP ground P@R and stowing of the R$. o simulate ground crew communications the software 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-. ,"- = $lphanumeric keyboard ,#- = 'C
he 'C
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Kou can either simply use your own keyboard ,see table ne6t page-- while making sure the 'C
7ine number one has two captions le>t caption ,here C9 R4 S- and ri$&t caption ,here &R9'/9 S-. @e*ll name 1" the left caption line X he right caption line will be 17. 9n the same principle we*ll name the lines 2" 3" etc... 4ach line has a switch •
hese are named 7ine )election keys
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Beta 38.3
• • •
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 the 7)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
A,tion $ 3 Y %3D A ,if pushed twice it*ll output a 3 3 / 7)H1 3 7)H; R)H1 3 R)H; $rrow keys &irst line of page key ,left to right)econd line of page key ,left to right9erfly 8right or
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2..2 - "#A#7" page his is the page that shows up when you launch the 'C
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2..! - I0I# A page
his page is brought up by pressing the 0:0 key on the 'C
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17 - F7$M / !$ 9 input 9 input airports 0C$9 code for departure and arrial separated by / S ,e6ample 4(77/7&P(-. 1" - %$ 7!# 9 Company 9 Company Route 4nter here the name of the company company route you want to used. 27 empty. 27 empty. 2" - A"!& / %$ 7!# 9 4ither 9 4ither enter the $7: $7: 0C$9 code or I/JAC9R4 from arrial to $7:. :ot mandatory. 3" - F"! &B7 9 input 9 input here your flight number ,e6 8$@"1C4 or $&D%5G0-. $&D%5G0-. 7 et " 9 longitude 9 longitude and latitude ,cannot be changed(7 - W)& 9 push 9 push R)H5 to prompt the winds page. (" - %$S! )&#D 67 - !7$$ 9 ropopause 9 ropopause altitude. 8y default ";%D%ft you can change it but no effect on flight profile. 6" - %7 F" / !#M 9 Cruise 9 Cruise flight leel has to input here. he number after the I/J automa automatic tically ally update updates s to predic predictt temper temperatu ature re at cruisi cruising ng altitu altitude de accord according ing to tropopause altitude.
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0f a &R9'/9 couple is entered A")G& )7S S )7S S in 37 37 push the R)H" to initialiLe the 0R) and display all attitude and position data on P&< and :< ,if $<0R) are 9: and alignment is finished-.
2..$ - 3I0D page 9nly the climb wind page is modeled for the moment and it is pure eyecandy it doesn*t hae any effect on flight profile. his page is accessed ia 0:0 $ page.
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1" to (" 9 enter 9 enter different winds for different altitudes. )ynta6 OOO/KK/YYY where OOO is true wind direction KK is wind speed in knots and YYY is a flight leel ,1%%%ft is thus &71%(7 9 no 9 no effect 6" 9 cancel 9 cancel any new alue entered and back to 0:0 $ page 67 9 $ccepts 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 here fuels alues in order to initialiLe fuel calculations. )&)! calculations. )&)! B is B is accessed on ground ia Right or 7eft arrow when 0:0 $ is shown. ,the arrows in title line indicate you can switch pages-. • •
1" 9 0nput 9 0nput 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 ) 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 will need 2.; tons of fuel and will last %%h5%min without any resere 27 9 otal 9 otal fuel before start3up in tons. Kou can uplink it ia R)H" 3" 9 Route 9 Route 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 9 Fse R)H" to get Y&@C( Y&@ and block fuel ia datalink. " 9 $lternate route trip fuel and duration. 7 9 ake 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 if there are Leroes input four number ,e6 %%"% for "% minutes-. he number shown before resere time is weight euialent in tons ,here 1.% tons for "% minutes resere-. (7 9 7anding @eight as calculated in the following way 7@ Z 9@ = R4 6" 9 46tra 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< )$R and approach procedure. 0t can be accessed ia F"& key on 'C
,1- = 9erfly point ,2- = $ltitude constraint ,magenta if met amber otherwise-
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,"- = )peed constraint ,magenta if met amber otherwise6" hows destination predictions ,time of arrial distance to go and estimated fuel on board-.
$ normal flight plan has more than 5 points so you can scroll through all points ia the ertical 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 :<8 fi6- in the scratchpad then push the 7)H adjacent to the point you want to insert the waypoint before
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0f you want to insert 8$R)9 before $'&9F point push 7)H ne6t to $'&9F here is what will happen
he line labels between two points show the magnetic track and the distance in nautical miles between the two points.
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he numbers on the right are the speed and altitude profiles at each point in knots and feet. hey are shown only when calculation is possible when weight and speeds data are input. 0f nothing is entered in the scratchpad pushing a 7)H will prompt the "ateral 7e5ision page and a R)H will prompt the Verti,al 7e5ision page. 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 or place3bearing/place3bearing. )ynta6 is •
+AT+ where +AT starts with the letter : or ) ,:orth or )outh- then one or two digits for degrees of arc then two digits for minutes of arc and eentually a decimal part 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 decimal part for minutes of arc. #@a*+le 9 :##%1./4%%?15 stands for ##B1.* :orth and %%?B15* 4ast 'lace9earin$(istance where 'lace is the 0< of a >9R :<8 or &0O 9earin$ is the magnetic bearing in degrees distance is the distance in nautical miles #@a*+le 9 $YR/%D%/5 is the point 5:' east of $YR >9R. place1-9earin$1place2-9earin$2 where place1 is the 0< of a >9R :<8 or fi6 number1 9earin$1 is the bearing from place1 place2 is the 0< of a >9R :<8 or fi6 number2 9earin$2 is the bearing from place2 #@a*+le 9 C()3%D%/$YR31% is the the crossing between the %D%B radial from C() and the 1%B radial of $YR. •
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2.. - D7P+I4A#, page 0f you insert a waypoint 0< ,>9R :<8 or fi6- which corresponds to seeral points worldwide the ne6t page is prompted
0t lists the fie nearest points in increasing distance from $C&. o select the desired waypoint push the adjacent 7)H.
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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 lateral trajectory from the selected point. • •
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3" 9 Push 7)H" to add an holding circuit at the selected point. 37 9 enter a new waypoint in the scratchpad then push R)H" to add that waypoint a>ter the selected point. " 9 actiates the $7: &P7: starting at the actie point. 7 9 Changes the destination airport and deletes all points downstream from the selected one. (7 9 click R)H5 to enter the airways page to follow airways to another point. "S;6 to 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 with desired characteristics • • •
1" 9 inbound magnetic course toward holding fi6. 2" 9 direction of turns. R for right and 7 for left. 3" 9 outbound track length either in time or distance input OO.O for time in decimal minutes input /KK.K for decimal nautical miles Press 7S;6 to insert the holding pattern or "S;6 to 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 plan seeral waypoints from airways easily • •
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&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 one ia 7)H 2 to 5. he connecting point between two $@K is automatically entered in R1 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; to get 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. he lines 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 with green 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 automatically to the )0< selection page
0n the same way you can select the desired )0< ia 7)H 2 to 5 and scroll with ertical arrows if more than # are aailable. @hen selected the arrow before the )0< name disappears ,here 89
he line 1 updates and if for that particular )0< transitions are aailable you can select one with the R)H1 to 5 ,here none are aailable-. 9nce eerything is selected and erified push R)H; to insert the )0< in the &P7:.
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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)H1 prompts the approach selection page
)elect the desired approach with 7)H " to 5. Kou can scroll if more than " are aailable using 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 prompts the )$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 connect the 0$& to the final segments of the approach procedure. he )$Rs connect the en3route phase 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 can come without any ia. 9nce you*e selected your >0$ ,or no >0$- and your )$R you might hae to chose between )$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" 9 C78 or <4) )peed limitations by default 25%kts below &71%%. 3" 9 input speed constraint at point. 37 9 input altitude constraint at point ,A/3 signs for minimum/ma6imun altitude no sign for e6act altitude-. • •
0f no alue is entered blue brackets appear ,like $7 C)R aboe-. 9therwise the numeric alue appears in magenta ,like )P< C)R aboe-.
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2..1 - DI # page Push )7 key on 'C
Kou can either scroll through the &P7: points in lines 2 to 5 or directly enter any point name in 71. hen you need to select a <0R 9 mode with R)H 2 to 5 •
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)7#%! !$ either deletes all points between $C& position and selected &P7: point ,if in &P7:- or insert the new point instead of current actie &P7: followed by a %'+ discontinuit: ,if not a &P7: point-. AB#AM !S do the same as <0R4C 9 but insert reference points on the new track abeam the old &P7: points. 7A)A" )& allows you to join the waypoint after intercepting a specified radial to it. he $C& will fly in G<(/RH mode until the radial is intercepted and :$> mode engaged. 0t*s up to the pilot to select a alid heading to intercept the radial. 7A)A" $U! allows you to intercept a radial outbound the specified point. he $C& will fly in G<(/RH mode until the radial is intercepted and :$> mode engaged. 0t*s up to the pilot to select a alid heading to intercept the radial.
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2..11 - P,F pages hose pages are accessed ia the #7F key on the 'C
his page can be accessed only during preflight • • •
1" 3" 9 Reference speeds >1 >r and >2 in knots " 9 ransition altitude in feet (" 9 hrust reduction altitude and acceleration altitude synta6 OOOO/KKKK where OOO and KKKK are the altitude alue of respectiely GR R4< and $CC altitude. 46 1%%%/1%%%. $CC altitude shouldn*t be inferior to GR R4< altitude. 17 shows the departure runway if it has already been entered ia departure lateral reision page. 37 asks for take off flaps settings. >1/>r/>2 lower limit depends on that alue and changing 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. 4ntry range is aboe 9$ or R4& and below ;BC ,R4& depends on pressure altitude-. •
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Pushing 7S;6 will 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 cruise phase is reached. •
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1" shows the speed mode that will automatically engage after setting the thrust leers 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< 70' alue ,by default 25% kts below &71%% see 7$ R4> pages to change those alues-. " 9 input here an indicated airspeed if you want to fly with selected speed after 9 ,to follow $C clearance for e6ample or if e6pecting tight turns-.
0f there is an asterisk ,[- before the 0$) in lines " or # means that the corresponding mode is not actie ,in picture aboe selected mode is actie and there is an asterisk at 3"-.
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#7F %7 et #S +aes 9 hose pages resemble P4R& climb and thus won*t be detailed here.
#7F A7 +ae 9
his page allows you to input approach data. • • •
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1" 9 $rrial airport Q:G 2" 9 $rrial airport temperature in BC 3" 9 arrial airport surface wind. )ynta6 OOO/KK where OOO is direction in degrees and KK speed in knots " 9 arrial airport transition altitude in feet (" 9 $pproach speed 27 9 'inimum
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2..12 - PG pages his set of pages is accessed ia 7$G key on 'C
• • • •
1" shows the CRY leel chosen in 0:0 $ page " shows the bearing and distance to the point selected in R# ,>9R :<8 or fi67ines 5 and 7ines ; are dummy for the moment. 27 9 /<4> numerical alues
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2..1! - ADI 0AV page
his page is accessed ia the 7A &AV key on 'C9Rs 07) ans :<8s-. :aaids can no longer be tuned from within &). &)F0PC controls will be added soon. 1" 9 >9R1 0&reuency 17 9 >9R2 0&reuency 2" 9 >9R1 course selector 27 9 >9R2 course selector 3" 9 07) 0&reuency " 9 07) magnetic track (" 9 :<81 0&reuency 6" 9 :<82 0&reuency • • • • • • • •
o tune a naaid either input the 0< or the freuency in the 0
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2..1$ - ",4 FP+0 pages he )4C &P7: key on the 'C
"S;1 9 copies the actie &P7: in the )4C &P7:. he display switches then to )4C &P7: page. 7S;1 9 accesses the secondary 0:0 $ page. ,)4C 0:0 $ has the same layout as 0:0 $-. he display switches then to )4C &P7: page. "S;2 9 accesses the )4C &P7: page ,same layout as &P7: page but all lines are white instead of green-. 9nce a )4C &P7: has been created the )4C 0:<4O page becomes ,see ne6t page-
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he 0:0 prompt at R1 disappears. o create a new )4C &P7: ia 0:0 $ page you*d hae to delete the e6isting one with "S;3 I<4744 )4CJ. he "S; actiates the )4C &P7:. he )4C &P7: becomes &P7: and &P7: becomes )4C &P7:.
S#% F"& +ae 9
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$ll &P7: sub3pages are aailable in the )4C &P7: ,lateral and ertical reisions )0< $PPR )$R selection-. @hen the 'C
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2..1% - /4D7 /,07 page
his paged is accessed ia the 'C
"S;1 will "S;1 will prompt the C$) page "S;2 will "S;2 will switch on/off 4(P@) Ierrain Ierrain 9n :
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he C$) page is used to set transponder tr ansponder and C$) modes. )ee C$) description.
his page allows allows you to moe each line to match your your hardware hardware faceplate faceplate ,if you hae one...-. Click on corresponding 7)H ,respectiely R)H- to moe line up ,resp. down-. o moe the itle line click on left or right arrows to moe scratchpad line click on up and down arrows ,or use corresponding &)F0PC offsets-.
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2..1& - DA#A page A!A )&#D +ae 9 Kou can access this page with the A!A key A!A key on the 'C
his page allows you to access arious other pages • • • •
"S;1 9 Position 9 Position 'onitoring "S;2 9 0R) 9 0R) monitoring "S;3 9 (P) 9 (P) monitoring "S; 9 $/C 9 $/C )tatus ,already described in chapter 2.?.2-
&or the moment all 0R) &'(C and (P) will compute the e6act alue of position G<( and track there is no drift implemented nor any possibility to induce a position error, in 0:0 $ page for e6ample-.
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osition Monitor +ae 9
0t shows the position computed by both &'(C the (P) and a mi6 from the " 0R). 0t also displays the status of the 0R) ,whether in $70(: :$> $ or 9&& mode-. 0n3flight you can press the 7)H; to freeLe the display for a better readability.
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)7S Monitor +ae 9
Gere is the detail of the 0R) 2 as in Position monitor Page you can freeLe the details ,here froLen at %D1 FC-. 0t displays latitude longitude track heading ground speed win. I:4O 0R)J prompt will display the ne6t 0R) ,or 0R)1 if you*re currently in 0R)"-.
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2. - AP5FD and A5#' lgic 2..1 - AP5FD mdes he $uto3Pilot ,$P- and the &light
Kou must first ar* it 0t will then enae by itself when the conditions for engagement are met.
$ few modes work in conjunction with the $uto hrust ,$/GR-. 0n the following pages you,ll find a list of the different modes with their ar*in and enae*ent conditions.
+ateral 0aigatin mdes
HG or !7; *odes 9 these modes allow to fly along the heading or track selected by the pilot in the &CF G<(/RH window. Kou can switch between G<( or RH with the G<( >/) = RH &P$ pushbutton on the &CF. #nae*ent ,one of the following is enough- • • • •
Pulling G<( selector knob on the &CF :$> mode automatically disengaged &0:$7 mode lost when in $PP :$> mode 79C or 79C[ mode lost
(isen$a$e/ent conditions engagement of any other lateral mode.
&AV *ode9 his mode guides the aircraft along the lateral flight plan entered in the 'C
$C& on the ground and no other lateral mode armed
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Pushing the G<( selector knob on the &CF
(isar/in$ conditions ,one is enough- • •
Pulling G<( selector knob on the &CF 7$:< mode engages
#nae*ent conditions ,one is enough- • • •
$t "% ft radio3altitude if armed on the ground @ith a <0R 9 order. 0n3flight when armed and near the &P7: track.
(isen$a$e/ent condition $n other lateral mode is engaged.
Vertical 0aigatin mdes
%"B *ode9 this mode controls the aircraft pitch to fly at either a selected or managed speed up to an altitude selected in the &CF altitude window. 0t takes into account the &P7: waypoints speed and altitude constraints and thus reuire the :$> mode to be engaged. Ar*in conditions ,one is enough- •
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on the ground or when )R) mode is engaged no other ertical mode is engaged and $CC47 $7 is below &CF altitude in3flight when &CF altitude is aboe current aircraft altitude.
(isar/in$ condition ,one is enough- • •
$nother ertical mode is engaged &CF altitude lower than or eual to $C& altitude.
#nae*ent conditions ,all of the following- :$> mode engaged &CF altitude aboe $C& current altitude $C& not flying an altitude constraint (/) mode is not actie C78 mode *anuall enaes when 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 or selected- but disregards any &P7: altitude constraint. #nae*ent conditions &CF altitude must be higher than actual $C& altitude A& ,one of 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 into account 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 fuel consumption. 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*ent conditions ,all of the following - • •
:$> mode engaged &CF altitude below $C& current altitude
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$C& not flying an altitude constraint 9 (/) 7$:< and &0:$7 mode not actie.
<4) mode *anuall enaes when pilot pushes the altitude selector knob on the &CF and conditions aboe are met. (isen$a$e/ent conditions ,one is enough- • • •
:$> mode disengages ,ertical mode reerts to 9P<4) $nother ertical mode engages Pilot selects an altitude higher than current $C& altitude. ,ertical mode reerts to >/) mode-
$#& #S%#&! *ode $ #S4 9 9pen descent mode controls the aircraft pitch to maintain the target speed ,managed or selected- but disregards any &P7: altitude constraint. #nae*ent conditions &CF altitude must be lower than actual $C& altitude A& ,one of the following- • •
Pilot pulls the altitude selector knob :$> mode lost when <4) is engaged
(isen$a$e/ent conditions ,one is enough- • •
$ny other ertical mode engaged &CF altitude set higher than actual $C& altitude. ,ertical mode reerts to >/) mode-
A"!I= A"! %S!7I *odes 9 $ltitude and altitude constraint acuire modes. #nae*ent automatically when in C78 9P C78 <4) 9P <4) or >/) modes and the $C& is in the altitude capture Lone around the &CF altitude target or constraint altitude ,in <4) or C78 modes only-. (isen$a$e/ent &CF altitude is modified and $C& is no longer in capture Lone or if $7 or $7 C)R engage.
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A"!= A"! %S!7 *odes 9 $ltitude hold modes. hey maintain either the &CF altitude of the constraint altitude if ertical 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/ent conditions any other ertical mode engages.
V/S FA *odes 9 hese modes maintain a constant >/) or a constant flight path angle. Kou can switch between the two with the G<( >/) = RH &P$ pushbutton on &CF. #nae*ent conditions ,one is enough- • • •
Pull >/) &P$ selector knob or push it ,for immediate leel off)elect a higher altitude than current $C& altitude in <4) or 9P <4) modes. )elect a lower altitude than current $C& altitude in C78 or 9P C78 modes.
(isen$a$e/ent conditions ,one is enough- • •
Pulling or pushing altitude selector knob Reaching &CF altitude
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AP5FD cmmn mdes
!a>e $:: *odes 5erti,al S7S and lateral 7W4 9 hese modes enae during 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 modes 9 • • • • •
ertical (/) or (/)[ lateral 79C or 79C[ 7$:< &7$R4 R977 9F.
)elected approach must be 07). "$%I enaes when $PPR has been pushed and $C& is in the localiLer interception Lone. 0t disen$a$es when 79C engages or $C& loses localiLer signal or $PPR pushbuton is pushed a second time to cancel approach mode. "$% enaes when $C& is established on localiLer beam. 0t then follows the localiLer. 0t disen$a$es when 7$:< mode engages 79C signal is lost or $PPR button pushed again. G/SI enaes engages when $PPR has been pushed and $C& intercepts the glideslope signal. 0t disen$a$es when (/) engages or $C& loses glidepath signal or $PPR pushbuton is pushed a second time to cancel approach mode. G/S enaes when $C& is established on (/) beam. 0t then follows the glidepath. 0t disen$a$es when 7$:< mode engages (/) signal is lost or $PPR button pushed again. "A& enaes when $C& established on (P and localiser and R$ is inferior to #%%ft. F"A7# enaes when in 7$:< mode and R$≤#%ft.
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7$"" $U! enaes on touch down.
&on re,ision A++roa,es 5erti,al F)&A" C lateral A &AV4 9 )elected approach is non307). his two modes ar* by pressing $PPR pushbutton. $PP :$> enaes with same conditions as :$> mode &0:$7 enaes if armed and $PP :$> is engaged. hey both disen$a$e if $PPR pushbutton is pushed again or another ertical mode is engaged.
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2..2 - A5#' mdes $uto hrust ,$/GR- controls the engines N:1 setting. 0t is used either to maintain a constant :1 setting ,GRF) mode- or to adjust speed/mach ,)P44'$CG mode-. • •
@hen $P/&< is not engaged $/GR always operates in )P44'$CG mode. @hen $P/&< is engaged $/GR can operate either in )P44'$CG or GRF) mode according to the $P/&< modes engaged.
Ar*in conditions of $/GR ,one is enough- • •
$/GR pushbutton pushed on &CF )etting thrust leers to 9($ notch
#nae*ent conditions of $/GR ,all of the following- • •
hrust leers between idle and C7 notches $/GR is armed
$/GR operates in GRF) modes while $P/&< ertical modes is one of the following •
)R)[ C78 9P C78 <4) en 0<74 9P <4). 0t deliers a thrust between idle power and the ma6imum thrust setting materialiLed by thrust leers position ,C78 'C 9($...-.
$/GR operates in )P44'$CG modes while $P/&< ertical modes is one of the following • • • •
$P/&< not engaged $7 X $7 C)R X $7[ X $7 C)R[ X $7 CRY <4) ,when in geometric path>/) = &P$ X (/)[ X (/) X &0:$7.
(isen$a$e/ent conditions of $/GR ,one is enough- • •
&CF $/GR pushbutton. hrust leers at idle notch.
@hen disengaged $/GR is not re3armed you need to re3arm $/GR manually.
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2..! - F/A he &light 'ode $nnunciator displays the current ar*ed and enaed $P/&< and $/GR modes
•
• •
Columns ,1- ,2- and ,"- ,respectiely A/!H7 5erti,al mode and lateral modeshow 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 at 9($ )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 during installation ,see )nstallation Guide chapter "-. he following chapter will describe briefly each of them and list the keyboard shortcuts aailable. 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- as well as the bearing to selected naaid ,>9R or $<&-. he heading rose is moing and it*s top arrow shows the magnetic heading of the aircraft. @ith a righ3click you can display some options •
•
Check $<& option to use either >9Rs or :<8s input on the <9R1/$<&1 by using F1 and F2 keys respectiely. $nd you can switch between >9R2/$<&2 by using F3 and F keys. Fncheck $<& option to only use it as a >9R receier ,as on the picture aboe-
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2.*.$ - 4lc<54hrnmeter
he clock is a digital ersion. 0t can show the current (' hour as well as the date ,using $ 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 and attitude 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 to standard 1%1"hpa pressure using M S. he speed and altitude scales can show reference bugs. o do that you need to enter the 8ugs menu using B S
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hen using and - keys you can naigate through the different bug bo6es. Kou can adjust the desired bug ,the bo6 circled in magenta- using the $ S and S keys ,the same keys used for baro3pressure- and enable/disable it with M S.
2.*.& - #riple 6ra
• •
,1- = 8rakes $ccumulator Pressure ,2- 3 8rakes pressure applied. hey*ll show the pressure only if the brakes are powered by the yellow hydraulic circuit ,in case of ( failure or $7: braking law-.
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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 :ice Riiera ,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 E state= which means all systems are inoperatie ,4lectrical pneumatics hydraulics fuel etc...-. 0t is thus normal to get black screens only... 9f course there is an e6haustie flightdeck preparation procedure described in the aircraft manualsX if you later want to stick as close as possible to the real operations you can find a 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- Check chapter 2.;.; if necessary • • • •
9pen &) $dd3ons S menu and chose 4O P@R S. 9n the 9>G< a green AVA)" light goes on on the 4O P@R korry. Click on that Horry which will turn it to $&. :ow all our instruments are powering up.
Click now on all korries which hae a white 9&& indication lit X you must switch all those indictions off.
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7et*s start the $PF ,see chapter 2.;.2-. @e can follow the spool up on the )< followed by the AVA)" indication on the $PF )$R korry on the 9>G) X the aircraft is now producing its own electricity. @e*ll remoe the 4O P@R ,click on the 4OP P@R korry to switch it from $& to AVA)" then click again on 4O P@R in the &) addon menu-. :ow we hae to align the 0R). Check the chapter 2.;.11 for that then we can moe on to the 'C
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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 we now 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&< showing attitude data. o do so go to the 0:0 $ page in the 'C
0:0 $ should look like
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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 to tis 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;3 to put it in place of &3 P7: <0)C9:0:F0K S. @e get the following screen
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Push the "S; ne6t "S; ne6t to $&R0C to prompt the lateral reision page at $&R0C point. )elect $0R@$K) page ,7S;( ,7S;(-. -. ype ("D in 17 ,"S;1 ,"S;1- - then &\R in 1R ,7S;1 ,7S;1-. -. &rom &\R we*ll follow the K25 airway ,2" ,2"-- until '( ,27 ,27-. -. $
•
he 'C
Click now on 7S;6 to 7S;6 to insert this routing in the 'C
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" says " says I333&P7: <0)C9:0:F0K333J. his message appears eery time the software cannot cannot link the lateral lateral reisi reision on with with the &P7: ,here ,here betwe between en the last $@K point and 7&':- so it happens when the last point of a new leg is different to the point after it in the &P7: seuence. @e can remoe the discontinuity C7R key "S; "S; then 'PK 0:)4R S ,7S;6 ,7S;6-. -. Kou now hae an almost complete &P7: only lacking departure and arrial procedures.
!.2.! - +a rute D,PA#7, 8y now boarding is almost oer oer and it*s time ti me to call the deliery for our 0&R clearance. oday the R@K in use is "27 ,we listened to the $0)- and the deliery controller answers >AF!2; start up t 0ice is appred; s?uaw< $$!&; AFI4 %6 departure; initial F+ 1$; reprt =r push :ac<@.
7et*s first enter the transponder code ,ia &)- then in the &CF set the altitude to 1#%%%ft as initially cleared and push to managed mode
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)ince we*ll be flying in ertical managed mode the white dot ne6t to the altitude window is on. 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 le point $&R0C en " ,C7R puis "S;- puis la <0)C9:0:F0K en 3" ,C7R puis "S;3- et enfin 7S;6 pour 'PK 0:)4R.
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!.2.$ - 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&': on the same principles as for the departure procedure. he )4C &3P7: ,)econdary &light Plan- may be used to prepare for an emergency return to oulouse after take off. 0 won*t go into such details as this document is meant only to be a Oui,> dis,o5er guide to \eeGell@are $"2% &'() X your personal knowledge and research will allow you to benefit from the multiple features not presented here and get a ery realistic e6perience.
!.2.% - AD 0AV page :ow we*ll tune the radio naigation aids to be able to follow the )0< een in case of 0R) failure. (o to R$< :$> page on the 'C
@e need 9F and ($0 >9Rs 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 lose the 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 route margins ,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 to strict rules and will impact the center of graity of the aircraft and thus i ts ability to fly. Flit Si*ulator uses the data ,P$O and cargo Loning fuel- from the flight model shipped with my software. •
his data ,isible in the $ircraft / &uel and payload S menu- correspond to te real 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 fly wihtout doing any payload calculations the software has a feature to import the fuel and payload data of the flight model directly into the 'C
9f course the data you*ll get is the default setting of &) it is ery unrealistic on most occasions ,particularly on short trips-. @e then get a screen as in the ne6t picture ,data may ary-
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For ad5an,ed users= there are third party add3ons which will allow you to conduct the full weight 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,tual data. :ote also that after engine start 0:0 8 is no longer aailable X you*ll hae to prompt &F47 PR4< 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 the aircraft. Fsually >1 at 120 >ts >r at 130 >ts and >2 at 18 >ts is mostly 9H. !ransition altitude 9 his depends on the departure airport. 0n oulouse it is at 5%%%ft. !rust 7edu,tion and A,,eleration altitudes 9 he default alue is 15%% / 15%% aboe the airport ,the 'C
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Push now 7S;6 key to call ne@t +ae 9 %"B. 0f you look at our )0< on the :< you can see a 1%B right turn just after departure •
•
•
•
@ith such tight turns it is a good idea to fly at a l ower speed than the usual 25% kts below 1% %%% feet. @e*ll put a limitation at 21% kts by using the pre3selected speed feature. )imply enter 21% in ". he dashes on the speed window of the &CF should hae been replaced by the >2 speed which means we are now in selected speed mode. @hen the 1%B turn is done we*ll switch back to managed speed mode.
Kou should hae the following screen
he following P4R& pages are for later phases of flight and not useful for now.
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!.2. - ,ngine "tart and #aBi Passengers are seated luggage and cargo loaded cabin and holds doors are closed <99R / 9OK page on the )< confirms that ,this page is not yet operational in the software though-. @e are ready to go we just need to ask startup pushback and ta6i clearancesT 4ngine start is done as described in chapter 2.;.1% first engine nB2 then :B1 while monitoring the )< indications. $fter start3up put the flaps leer on position 1 4@< shows 1A& ,one step of slats and one step of flaps-. Check the flight goerns on the )< ,moe the rudder and stick in all directions-. $rm the spoilers. )elect auto3brake on '$O so in case of R9 ,rejected take off only before >1- we get a fast braking answer.
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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 on the 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& $H4 9&& page. Gadn*t we entered that &7O temperature we*d hae to moe the thrust leers into 9($ detent. 9n the &'$ '$: &7O 52 S must be displayed in the first column
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0f you hae copilot he will call the reference speeds such as %kts >1 and >r. Check on the P&< that your speed scale agrees with the callouts. )R)/R@K is engaged while C78 and :$> are armed.
:otice the white bo6 with the white cross on the P&<. his indication is only isible on the
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ground the cross marks the stick deflection ,ertically and laterally- and the bo6 shows the delfection limits. Reaching >r pull +roressi5el on the stick to achiee an initial pitch of around ?B then after 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 as the GR R4< $7 the aircraft will accelerate towards our selected speed. @hen reaching the $CC $7 the $P/&< commands a pitch decrease to allow the aircraft to accelerate aboe the 3) speed. his speed marks the minimum speed at which we can retract the slats.
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GR C78 C78 and :$> 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< knob on 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 barometer setting to )< ,1%1" mb or 2D.D2 inGg-. Passing &71%% will accelerate aboe the 25% kts limit to reach our climb speed. he pitch goes down to allow that acceleration and so will the >/) until it can go up again when we meet our target speed. 4n3route control clears us to our cruising altitude &7"1% select "1%%% in the altitude window 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 the modes '$CG $7 CRY and :$> engaged. 0f the '
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!.% - 4ruise phase
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$ bit later the 'C
@e can get the weather informations using the '4$R feature simulating an $C$R) link push 'C
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@e can now fill the $PPR P4R& page by pushing the P4R& key then clicking twice on 7S;6 ,:4O PG$)4- fill in the Q:G ,1%1?- temperature ,15B- wind ,2%%/1%- transition altitude ,5%%% ft as indicated by the apporach chart- and also the '<$ ,"%% ft-. he 'C
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)hortly after '$RR0 fi6 ,see ne6t page- $C clears us directly to '(.
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Call <0R 9 page on the 'C
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$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 can finish filling in the 'C
@e*ll fly the 07)%#7 the first in the list so click on "S;3.
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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 we must put the 'F) >0$ to correctly join the 07)%#7 $PPR. 7et*s insert our arrial route by clicking "S;6 then 7S;6. @hile in the &P7: page don*t forget to clear any &3P7: <0)C9:0:F0K as we did on the departure. @e can check the complete route on the :< using the P7$: mode ,mode selector on the 4&0)- and scrolling the &P7: using the 'C
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Version 38.3
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User Guide
06 / 03 / 201
A320 FMGS Beta 38.3
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!.& - Descent Phase @e*e been cleared to descend to &712%. )elect 12%%% on the &CF and push the $7 knob to engage managed descent. his way we force the descent before reaching the 9<. :ote the 9< is only displayed as a reference the aircraft will not descend by itself when oerflying the 9< we hae to tell it to do so.
Version 38.3
JeeHellWare
User Guide
06 / 03 / 201
A320 FMGS Beta 38.3
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Manaed des,ent s+eed is constantly adjusted by the &'() to try it*s best at maintaining the descent profile symboliLed by the >/<4> target. $ll that keeping engines at idle. :ote that an aircraft can hardly descent and slow down at the same time. his is why it will reduce 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&<. his is a constraint included in the charts which is also in the naigation database of the &'() ,)peed and altitude constraints are displayed in magenta on the :< by selecting C)R on the 4&0) panel-. his is handy as in fact we had selected 1%%%% on the &CF instead of 12%%%. Crosschecking the instruments allows us to correct and now 12%%% is displayed blue on the P&<. Sele,ted *odes can used when managed modes cannot follow the ertical profile or if the $C remoes the constraint on a portion of our route. @ith strong rear wind sometimes the flight profile is too steep and so the pilot will hae to do its best to get back on it. Ge can use the s+eed es , _ deflection ma6 with autopilot on- to hel increase the descent rate. his must be aoided at lower altitude/low speeds. Check the $0) to erify and eentually refresh the arrial conditions. Q:G is still 1%1? temperature rose to 1;B and wind is now 2%%B/11 kts. 4nter these modifications in the $PPR P4R& page X $pproach speed >app is now 1## knots. he managed descent looks good so far X at 0P0H we are re3cleared down &7% ,managed mode will automatically reduce our speed to 25% kts below &71%%-. 4nter %%% on the &CF ,the white dot confirms we are in managed mode-. $t 'F) we are cleared at 5%%% ft and asked to slow down to 2"% kts. 4nter 5%%% ft on the $7 window then 2"% kts and pull the )P< selector to go into selected speed mode.
!. - Apprach and landing he approach controller in :ice clears us for the full 07) approach. @hile passing the <4C47 pseudo point marked by a circled magenta < lmanaged speed becomes >app and if we go back into managed speed mode ,push on the )P< selector- the aircraft will slow down towards >app. 7et*s go in managed speed mode. )elect #%%% feet on the &CF ,(lide path interception altitude- to reach that altitude ,set as a constraint at :0122 point- and the &'() will finsih the job almost by itself.
Version 38.3
JeeHellWare
User Guide
06 / 03 / 201
A320 FMGS Beta 38.3
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@hen speed is below the >&4 of first flaps setting select flaps 1. page. 9n the P&< display the 07) deiation scales by pushing the 07) button on the 4&0) panel. Push $PPR button on the &CF and monitor 79C and (70<4 capture on the &'$ and 07) scales. Push on $P2 ,if $P1 is engaged or ice3ersa- to engage the second autopilot ,possible only during 07) approach as a backup means-. $t around 2%%%ft select flaps " then lower the landing gear. &inally e6tend flaps at &F77. @e can do an autoland just let the $P do the rest. $P/&< capacity is displayed in the #th &'$ column. Gere we hae C$"
Version 38.3
JeeHellWare
User Guide
06 / 03 / 201
A320 FMGS Beta 38.3
Page 15" / 155
he 07) should be perfectly followed until the threshold. 0t may happen there is a little glide or localiLer deiation. 0f it happens you hae to land manually. Right before touching down retard the thrust leers to 0<74 detent. $t touch down the spoilers will e6tend automatically as they were armed. Fse the reerse thrust ,put the thrust leers to R4> '$O detent- to slow the aircraft down more efficiently. he auto3brake will also actiate automatically.
Version 38.3
JeeHellWare
User Guide
06 / 03 / 201
A320 FMGS Page 15# / 155
Beta 38.3
9n the ground if rollout mode is giing bad guidance use the rudder pedals to control the aircraft. $t ?% kts put the thrust leers back into R4> 0<74 then use the differential brakes ,on the pedals- to disengage the auto3brake. @hen speed is controlled put the leers into 0<74 detent. Kou still hae to acate the runway ,you may now use the tiller to ta6i- disarm the spoilers retract the flaps and follow tower instructions to get to your parking position...
Celco/e to I, T, (DAE50... e &ae arried at our destination... 'lease =eep readin$ t&is docu/ent until t&e aircra>t doors are opened... ote t&is is onl: a >irst approac& at Fee#ellare A32" %GS< oluntaril: si/pli>ied. ou can learn /ore 9: :oursel> 9: researc&in$ t&e net< or real /anuals to i/proe :our >l:in$ e@perience wit& t&is so>tware. our e@perience can also 9e $reatl: en&anced 9: addin$ ot&er so>tware or &ardware< co/pati9le wit& t&e %GS /ain so>tware. T&ese are presented in t&eC ,Bperts Guide )separate docu/ent< currentl: 9ein$ re-written and soon aaila9le< &oep>ull:...*. e &ope :ou enHo:ed :our >li$&t wit& us...