w c o m ww . docutr a c k A320€Flight€Deck...

Flight Deck Documentation AIRBUS A320

12.11.06 Ralf Anderseck Seite 1

A320 Flight DeckDocumentation

By: Ralf Anderseck 25.2.2002

Source: http://www.meriweather.com by jerome meriweather

1 Flight Deck A320

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Inhaltsverzeichnis

1 Flight Deck A320__________________________________________________________ 1

2 Overhead Panel A320 ______________________________________________________ 3SVCE INT OVRD Switch ________________________________________________________ 8

Avionics COMPT LT Switch _____________________________________________________ 8

Data Display Window __________________________________________________________ 12SYS Selector _______________________________________________________________________ 12SEC Switch ________________________________________________________________________ 13FAC Switch ________________________________________________________________________ 13GEN 1 Line Switch __________________________________________________________________ 13MAN ON Switch ____________________________________________________________________ 14

3 Glareshield______________________________________________________________ 294 Center Instrument Panel___________________________________________________ 29

5 Control Pedestral_________________________________________________________ 296 Rudder Pedals ___________________________________________________________ 29

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2 Overhead Panel A3202.1 Overhead Fuse Panel

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2.1.1. Captain's and F/O'sRead Light Control(A320)

Ajustable Light

Reading Light KnobControls the intensity of the overhead ReadingLight.

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2.1.2. Gasper Panel (A320)

Gasper Air Vents

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2.1.3. Fuse Panel (A320)

There are no hotspots on this panel. I left it asis because it's pretty selfexplanatory. Thelettering above each breaker explains whatcircuit it accesses.

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2.1.4. Pedestal Floor Light

Auto Switching Control

Enables the Captain or First Officer to useACP 3 in case of ACP 1 or 2 failure.

• CAPT 3 The Captain makes audioselections on ACP 3 and ACP 1 isdeactivated.

• NORM Each crewmember usesrespective dedicated equipment.

• F/O 3 The First Officer makes audioselections on ACP 3 and ACP 2 isdeactivated.

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2.1.5. Maintenance Panel(A320)

CVR HeadSet

Audio Jack for monitoring the operation of theCockpit Voice Recorder. Used by MaintenanceTech Personnel.

Maintenance Oxygen Switch

• TMR Reset Switch Resets controlcircuit when selected ON, and ON lightilluminates. PASSENGER SYS ONLight goes off.

• TMR Reset Fault Light Illuminateswith a failure to deenergize theoxygen mask door latches.

•SVCE INT OVRD Switch

• AUTO Enables communication to theinterphone jacks. The function isinoperative when the landing gear isnot compressed.

• ON Used by Maintenance to allowcommunication when the landing gearis not compressed. The ON lightilluminates.

•Avionics COMPT LT Switch

• AUTO Causes the avionicscompartment lighting to come on

automatically when the avionicscompartment door is opened.

• ON Turns the avionics compartmentlighting on.

HYD

Blue Pump OVRD Switch (Guarded)• ON The Blue electric pump is

energized, provided the BLUE ELECPUMP switch, located on the hydraulicpanel, is in AUTO.

Leak Measurement Valve Switches(Guarded)

Used for Maintenance ground test only. Whenthe light is on, portions of the Hydraulic systemare inoperative.

APU Auto Extinguishing Panel

APU TEST Switch

Tests APU Fire Warning, auto extinguishingand shutdown circuits. For test, MASTERswitch must be ON and TEST switch must beheld down for 10 seconds. The OK light comeson to indicate a successful test.

Reset Switch

Resets test circuit.

ENGENG FADEC GND PWRSwitches (Guarded)

• ON Supply the associated FADECwith ground power, provided the ENGFIRE switch is not released.

• Off Disconnect ground power.

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2.1.6. Captain's and F/O'sRead Light Control(A320)

Ajustable Light

Reading Light KnobControls the intensity of the overhead Reading Light.

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2.2. Overhead Panel 2

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2.2.1. OBS Audio ENT ( A320 )

OBS Audio ENTObserver Audio

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2.2.2. ADIRS Control Display Panel(A320)

Data Display Window

Displays the data selected by the DATASelector. Keyboard entry overrides the display.

Data Selector• Test Displays all 8s in data display

window and illuminates ENT and CLRkeys.

• TK/GS Displays true track andgroundspeed.

• PPOS Displays present latitude andlongitude.

• WIND Displays true Wind directionand speed.

• HDG Displays true Heading andminutes remaining until alignment iscompleted.

• STS Displays system statusmessage code.

SYS Selector• OFF Blanks data display window.• 1, 3 or 2 Displays data for associated

IRS.Data Entry KeyboardAllows entry of preset position or heading inATT mode, in the selected system.

• Alpha Keys Select N, S, E, W forpresent position entry or H for headingentry in ATT mode.

• Numeric Keys Key in present positionor present magnetic heading in ATTmode, to the data display window.

• ENT Key Illuminates when and alphakey is selected. Enters keyed data intothe ADIRS when pushed.

• CLR Key Illuminates when keyeddata is of an unreasonable value.Clears keyed (but not yet entered)data from display window whenpushed.

ON BAT LightIlluminates amber when one or more ADIRUsis supplied by airplane battery only. Alsoilluminates for a few seconds at the beginningof the alignment.

IR Lights 1, 2 & 3 toptop• FAULT Illuminates amber when a

Fault affects the associated IR.Flashes if attitude and headinginformation is recoverable in the ATTmode.

• ALIGN Illuminates white when theassociated IR is operating normally inthe ALIGN mode.Flashes if:

• IR alignment fault detected.• No present position entry has

been made after ten minutes.• Difference between position at

shut down and enteredposition exceeds 1° of latitudeor longitude.

IR Mode Selector toptop• OFF Deactivates associated ADIRU.

Both ADR and IR data are notavailable,

• NAV Provides full inertial data toairplane system.

• ATT Provides only attitude andheading data if loss of navigationcapability occurs. Heading must beentered via the ADIRS Control DisplayUnit and must be reset frequently.

ADR Lights 1, 2 & 3 toptop• FAULT Illuminates amber when a

fault is detected in the associated airdata reference part.

OFF Switch Disconnects air data output toassociated ADR. IR is not affected.

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“2.2.3 EVAC Controls (A320)“ \|32.2.3 EVAC Controls (A320)

Flight Controls

ELAC Switch• ON Engages the associated elevator

and aileron computer.• OFF Disengages associated

computer.• Fault Light Illuminates amber:

• When a failure is detected• During ELAC power up test.

SEC Switch• ON Engages the associated spoiler

and elevator and aileron computer.• OFF Disengages associated

computer.• Fault Light Illuminates amber when a

failure is detected.FAC Switch

• ON Engages the associated flightaugmentation computer.

• OFF Disengages associatedcomputer.

• Fault Light Illuminates amber when afailure is detected.

•EVACCommand SwitchON Activates evacuation alert. The EVAClight flashes and horn sounds in the cockpit.EVAC lights flash at forward and AFT FlightAttendant panels and Evacuation tone soundsin the cabin. Pushing the COMMAND switch asecond time cancels the Evacuation alert.Horn Shut OFF SwitchSilences the Evacuation Horn in the cockpitwhen pushed.CAPT and CAPT/PURS Switch (WiredGuard)Safety wired to the CAPT/PURS position.Allows activation of an Evacuation alert fromthe cockpit or cabin.

EMER ELEC PWREMER GEN Test SwitchNormally used by Maintenance.GEN 1 Line Switch

• OFF Causes the GEN 1 linecontactor to open. A fuel pump in each

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wing tank remains powered by GEN 1and GEN 2 powers AC bus 1.

• Smoke Light Illuminates amber whenSmoke is detected in the avionicsVentilation systen.

RAT & ENER GEN Fault Light Illuminates red with a loss of power to ACbuses 1 and 2 if:

• The emergency generator is notsupplying electrical power, and

• the nose gear is up.MAN ON Switch

• AUTO The RAT extendsautomatically, provided AC bus 1 and2 are not electrically powered andspeed is above 100 knots. If theLanding Gear is up, the emergencygenerator is hydraulically powered bythe blue system.

• ON The RAT extends. Emergencygenerators coupling occurs providedthe landing gear is up.

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2.2.4. Ground Proximity WarningSystem (GPWS) &Cockpit Voice Recorder (RCDR) (A320 )

GPWS

TERR• OFF Inhibits the GPWS enhanced

modes.• FAULT Illuminates when failure is

detected with the enhanced modes.SYS Switch

• OFF All GPWS warnings areinhibited.

• FAULT Light Illuminates amber whena GPWS malfunction is detected. AllGPWS warning are inhibited.

G/S ModeInhibits the GPWS glide slope mode.

FLAP ModeInhibits the GPWS Flap Mode to preventnuisance warnings when landing with otherthan landing flaps.

LDG FLAP 3• ON Inhibits the GPWS Flap Mode to

prevent nuisance warnings whenlanding with flaps 3.

RCDRGND CTL Switch (Springloaded)Any power interruption may cause the GNDCTL switch to revert to AUTO.

• ON Energizes the cockpit voicerecorder (CVR) and digital flight datarecorder (DFDR). The ON lightilluminates.

• AUTO CVR and DFDR areautomatically energized illuminates.

• On the ground for the first fiveminutes following electricalpower application.

• On the ground with at leastone engine running.

• In flight.The CVR and DFDR stop automatically fiveminutes after the last engine is shut down.

CVR Erase SwitchErases tape when pushed for two seconds,provided the airplane is on the ground and theparking brake handle is on.

CVR Test SwitchWhen pushed and held, the CVR test isactivated provided the CVR is energized andthe parking brake handle is on. During the test,a low frequency tone is heard through thecockpit loudspeakers.

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2.2.5. Oxygen Panel, Calls Panel &Rain Repellent & Wiper Controls (A320 )

Oxygen Panel

Video IN UseIlluminates when cabin Video System isoperating.

Mask MAN ON Switch (RedGuarded)

• AUTO Oxygen mask doors openautomatically when cabin altitudeexceeds 14,000 feet.

• ON When pressed, Oxygen maskdoors open.

Passenger SYS ON LightIlluminates when Oxygen mask doors open.Remains on until the OXYGEN TMR RESETswitch is pushed on the overhead maintenancepanel.

Crew Supply Switch• ON Oxygen supply valve is open.

Low Oxygen pressure is supplied tothe masks.

• OFF Oxygen supply valve is closedand OFF light illuminates.

•Calls PanelMECH SwitchInitiates call to ground personnel. When

pushed, the COCKPIT CALL light illuminateson the external service interphone panel, andan external horn sounds. When released, theexternal horn is silenced. The COCKPIT CALLlight remains illuminated until the RESETswitch, located on the external serviceinterphone panel, is pushed.

FWD/AFT SwitchesWhen pushed:

• A pink light illuminates at thecorresponding Flight Attendant areacall panel.

• A "CAPTAIN CALL" message appearson the corresponding Flight Attendantindication panel.

• A high/low chime sounds through thecorresponding loudspeaker.

EMER Switch (Guarded)When selected ON:

• The ON light flashes.• The CALL light flashes.• A pink light flashes at all Flight

Attendant area call panels.• A "EMERGENCY CALL" message

appears on all Attendant indicationpanels.

• A high/low chime sounds through allloudspeakers.

If an emergency call is initiated from the cabin:• The ON light flashes.• The CALL light flashes.• Three long buzzers sound in the

cockpit.Reset is achieved when the Flight Attendanthangs up the handset.

Wiper ControlsRain RPLNT SwitchDeactivated

Wiper SelectorControls operation of the respective Wiper.When selected OFF, the Wiper stops out ofview.

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2.2.6. Engine / APU Fire ControlPanel ( A320 )

ENG 1 & 2 Fire Switches ( guarded )When released out, an electrical signal:

• Cancels aural warning• Arms squibs• Deactivates generator• Closes the following valves

• Fuel LP• Engine fuel return• Hydraulic bleed• Pack flow control•

ENG 1 & 2 Fire LightsIlluminate independently of the switch positionas long as the respective engine fire warning isactivated.

ENG 1 & 2 Agent 1/2 SwitchesArms when the corresponding ENG FIREswitch is released out. SQUIB lights illuminateto facilitate identification of the agent switch tobe activated. When the AGENT switch ispushed momentarily:

• Bottle is discharged• Related DISCH light illuminates•

ENG 1 & 2 TEST SwitchesTest the fire detection and extinguishingsystem operation.

• Activates ECAM ENG FIRE warning• Activates continuous chime• Illuminates the following:

• Flashing MASTER WARNlights

• ENG FIRE switch• SQUIB lights• DISCH lights• FIRE lights on engine start

and ignition panel•

APU Fire Switch ( guarded )When released out:

• Cancels aural warning• APU shuts down• Squib is armed• Squib light illuminates• Fuel LP valve is closed• APU bleed and crossbleed valves are

closed• APU generator is deactivated•

APU Fire Light

APU Fire light illuminates independently ofswitch position when the APU fire warning isactivated.

APU Agent SwitchArms by pushing the APU FIRE switch. SQUIBlight illuminates. When the AGENT switch ispushing momentarily:

• Bottle is discharged• DISCH light illuminates•

APU TEST SwitchTests fire detection and extinguishing systemoperation.Does not cause automatic shutdown ofAPU.

• Activates ECAM APU FIRE warning• Activates continuous chime• Illuminates the following:

• Flashing MASTER WARNlights

• APU FIRE switch on APUFIRE Panel

• SQUIB lightDISCH light

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2.2.7. Hydraulic Control & Fuel Panels ( A320 )

Hydraulic Control Panel

ENG 1 & 2 Pump Switch & Light• Switch

• ON The Pump Pressurizesthe system when the Engine isrunning.

• OFF The Pump isdepressurized. Powergeneration stops.

• LightIlluminates amber to indicate:

• Reservoir low level• Reservoir overheat• Reservoir low air pressure• Pump low pressure

Extinguishes when the ENG PUMPswitch is selected OFF, except duringan overheat; in which case, the lightremains on as long as the overheat ispresent.

RAT MAN ON Switch ( red Guard )When pushed, the RAM Air Turbine extends.The RAT extends automatically in flight with aloss of AC buses 1 and 2.

Blue ELEC Pump Switch & Fault Light (Guarded )

• Switch• AUTO The Pump is

energized, provided AC poweris available:

• In flight• On the ground,

provided one engine isrunning or the BLUEPUMP OVRD switchhas been pressed.

• OFF The Pump is deenergized.

• Fault Light Illuminates amber toindicate:


Extinguishes when the BLUE ELECPUMP switch is selected OFF, exceptduring an overheat; in which case, thelight remains on as long as theoverheat is present.

PTU Switch & Fault Light• Switch

• AUTO The reversible motorpump is armed and bothyellow and green electrohydraulic valves are open. ThePTU runs automatically whenthe differential pressurebetween the green and yellowsystems is more than 500 psi.

• OFF Both green and yellowPTU electrohydraulic valvesare energized and close.Power transfer stops.


• Green or yellow reservoiroverheat

• Green or yellow reservoir lowair pressure

• Green or yellow reservoir lowlevel

Extinguishes when the PTU switch isselected OFF, except during anoverheat; in which case, the light

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remains on as long as the overheat ispresent.

Yellow ELEC Pump & Fault Light• Switch

• ON The Pump is energized.If electrical power is removed,the pump remains deenergized at the next electricalpower application.

• OFF The Pump is deenergized. It is automaticallyenergized when the forward oraft cargo door lever isoperated. During cargo dooroperation, all other yellowsystem users are inhibited,except for the No. 2 enginethrust reverser and the brakeaccumulator.



Extinguishes when the YELLOWELEC PUMP switch is selected OFF,except during an overheat; in whichcase, the light remains on as long asthe overheat is present.

Fuel Panel

X FEED Switch & Open Light• Switch

• OFF Closes Crossfeed valve.• ON Open Crossfeed valve.

ON illuminates white.• Open Light Illuminates green when

Crossfeed valve is fully open.•

ENG 1 & 2 L/R TK Pumps Switch & FaultLights

• Switch

• ON Energize associatedTank Pump; fuel feeds onlywhen center Tank Pumps'delivery pressure drops belowthreshold.

• OFF Deactivate associatedTank Pump.

• Fault Lights Illuminates amber whenthe delivery pressure drops. Inhibitedwhen OFF selected.

•CTR TK 1 & 2 Pump Switches & FaultLights

• Switch• ON Activates associated

Center Tank Pump. If MANmode is selected on MODESEL switch.

• OFF Deactivate associatedCenter Tank Pump.

• Fault Lights Illuminates amber whenthe associated Pump is operating anddelivery pressure drops.

•Mode SEL Switch & Fault Lights

• Switch• AUTO Center Tank Pumps

control is automatic:• Pumps operate at

engine start for twominutes

• Pumps operateprovided slats areretracted

• Pumps automaticallyturn off five minutesafter Center Tank lowlevel is reached

• MAN Allows manual controlof Center Tank Pumps withCTR TK PUMP switches.

• Fault Lights Illuminates amber whenCenter Tank has more than 550pounds of fuel and the left or right wingTank has less than 11,000 pounds.

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2.2.8. Electrical Control Panel ( A320 )

BAT 1/2 Indication Window

Display the Battery voltage

BAT 1/2 SwitchesControls the operation of the correspondingbattery charge limiter.

• AUTO The Batteries areautomatically connected to the DCBAT bus during the following:

• APU starting• Battery charging• Below 100 knots on the

ground with a loss of ACbuses 1 and 2

• OFF The Battery charge limiter is notoperating and the batery line contactoris open. The OFF light illuminateswhite provided the DC BAT bus ispowered. The HOT BAT buses remainpowered.

• Fault Light Illuminates amber whenthe charging current for thecorresponding battery increases at anabnormal rate. In addition, the batterycontactor opens.

•

AC ESS Feed SwitchEnables the AC ESS BUS to be powered viaAC BUS 2 instead of AC BUS 1.

• Normal AC ESS BUS is suppliedfrom AC BUS 1.

• ALTN AC ESS BUS is supplied fromAC BUS 2.

• Fault Light Illuminates amber whenthe AC ESS BUS is not electricallypowered.

•Galley Switch

• AUTO The Galleys are electricallypowered. The main Galley bus isautomatically shed when only onegenerator is operating, except on theground when the APU or externalpower is available.

• OFF The Galleys are not electricallypowered.

• Fault Light Illuminates amber whenany generator load is above 100% ofits rated output.

•IDG 1/2 SwitchesGuarded and normally springloaded out. Whenpushed, the IDG is disconnected from its driveshaft and can only be reconnected byMaintenance.

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GEN 1/2 Switches• ON The Generator field is energized

and the line contactor closes providedelectrical parameters are normal.

• OFF The Generator field is deenergized and the line contactoropens. The fault circuit is reset.

• Fault Light Illuminates amber if aprotection trip is initiated by theGenerator control unit (GCU), or theline contactor opens without selectingthe respective GEN switch OFF.

•APU GEN Switch

• ON The Generator field is energizedand the line contactor closes providedelectrical parameters are normal andthe EXT PWR line contactor is open.The bus tie contactor (1 and/or 2)automatically closes if generators 1and/or 2 are not operating.

• OFF The Generator field is deenergized and the line contactoropens. The fault circuit is reset.

• Fault Light Illuminates amber if aprotection trip is initiated by theGenerator control unit (GCU), or theline contactor opens without selectingthe APU GEN switch OFF. The APUGEN FAULT light is inhibited whenAPU speed is low.

•BUS TIE Switch

• AUTO The Bus Tie contactors openor close automatically to maintainpower supply to AC buses 1 and 2.

One contactor is closed when oneenginedriven generator supplies theassociated AC bus and the APUgenerator or external power suppliesthe other side.

Both contactors are closed in case ofone enginedriven generator, orexternal power supply.

• OFF Both Bus Tie contactors areopen.

•EXT PWR SwitchWhen pushed with the EXT PWR AVAIL lightilluminated:

• External Power line contactor closes• AVAIL light goes off• ON light illuminates

When pushed with the EXT PWR ON lightilluminated:

• External Power line contactor opens• ON light goes off• AVAIL light illuminates

AVAIL Light Illuminates green providedExternal Power is plugged in and electricalparameters are normal.

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2.2.9. Air Conditioning & Pneumatic Controls ( A320 )

Air Conditioning

PACK Flow SelectorPermits selection of Pack Flow according tonumber of passengers and ambient conditions.

Zone Temperature SelectorsAdjust Temperature for associated Zone.

HOT AIR Switch• ON Automatically controls zone Hot

Air pressure regulating valve.• OFF Closes Hot Air pressure

regulating valve and trim air valvesand resets fault circuit.

• Fault Light Illuminates amber whenduct overheat is detected. If thisoccurs, the zone Hot Air pressureregulating valve and trim air valvesautomatically close. The FAULT lightstay on until ;power temperature issensed with the switch off.

•

PACK 1/2 Switches• ON Automatically controls Pack Flow

control valve. Valve regulates flow,except in the following conditions:

• Upstream pressure is belowminimum

• Compressor outlet overheat• During Engine Start sequence

with ENG MODE selector setto IGN/START or CRANK and:

• Either ENG MASTERswitch is ON

• The start valve is open• N2 is less than 50%

• Corresponding fire switch isdepressed

• DITCHING switch is selectedON

• OFF Closes Pack Flow control valve.• Fault Light Illuminates amber when

Pack Flow control valve positiondisagrees with selected position, or ifcompressor outlet overheats

•RAM AIR Switch (Guarded)

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• ON Illuminates when selected on. Ifthe DITCHING switch is in its normalguarded position:

• Ram Air inlet opens• Normal outflow valve control is

maintained if differentialpressure is greater than orequal to 1 psi

• Outflow valve opens ifdifferential pressure is lessthan 1 psi.

• OFF Closes Ram Air inlet.Pneumatic

ENG BLEED 1/2 Switches• ON Opens Bleed valve provided:

• Upstream pressure is above 8psi

• APU BLEED switch is OFF orAPU Bleed valve is closed

• There is no leak, overpressure or overtemperaturedetected

• ENG FIRE switch not releasedout

• Engine start valve is closed• OFF Closes Bleed valve and HP

valve. OFF light illuminates white.• Fault Light Illuminates amber to

indicate:• Overpressure downstream of

Bleed valve• Bleed overheat• Wing or engine leak on

associated side• Bleed valve not closed during

Engine Start• Bleed valve not closed with

APU Bleed ONAPU BLEED Switch

• ON Opens APU Bleed valve providedN is greater than 95% and there is noleak on APU or left side Bleed.

• OFF Closes APU valve.• Fault Light Illuminates amber when

APU leak is detected.•

X BLEED Selector• AUTO Opens crossbleed valve if

APU Bleed valve is open; closescrossbleed valve if APU Bleed valve isclosed or an air leak is detected.

• OPEN Opens crossbleed valveSHUT Closes crossbleed valve

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2.2.10. Anti Ice Control, Window Heat & Cabin Press Panel(A320)

Anti Ice

WingControls Wing Anti Ice system simultaneouslyon both Wings.

• ON• "ON" light illuminates• "WING A. ICE" message

appear on ECAM MEMOdisplay

• Wing Anti Ice valves openprovided pneumatic supply isavailable. On the ground, thevalves open for 30 secondsonly

• OFF• "ON" light goes OFF• Wing Anti Ice valves close

• Fault Light Illuminates when either ofthe following occur:

• Wing Anti Ice valve positiondisagrees with selectedposition.

• Low pressure is detected.•

ENG 1 / 2Controls the respective engine antiice system.

• ON• "ON" light illuminates• "ENG A. ICE" message

appear on ECAM MEMOdisplay

• Engine Anti Ice valves openprovided Engine bleed air isavailable.

• Continuous ignition is providedwhen the valve is open

• OFF• "ON" light goes OFF• Engine Anti Ice valves close

• Fault Light Illuminates if Engine AntiIce valve position disagrees withswitch position.

Probe/Window Heat

Probe/Window Heat• AUTO Provides automatic Heating of

Probes and Windows:• Inflight• On the ground provided one

engine is running. (TATProbes excluded)

• ON Provides Heating of Probes andWindows:

•Cabin PRESS

MAN V/S CTL SwitchControls the outflow valve position via themanual motor, when MODE SEL switch ispositioned to MAN. Spring loaded to neutral.Switch must be held in position until target V/Sis reached, as outflow valve operation is slow.

• UP Moves valve towards openposition.

• DN Moves valve towards closedposition.

•Mode SEL Switch

• Auto Automatic mode is operating.Outflow valve is controlled by onesystem at a time.

• MAN Allows manual control by theMAN V/S CTL switch. Illuminates whitewhen selected. The cabin altitudeindication on the ECAM PRESS pagemay fluctuate when switching fromAUTO to MAN.

• Fault Light Illuminates amber onlywhen fault detected in both automaticsystems.

LDG ELEV Selector• Auto (Detent) Pressurization system

uses FMGSdetermined landingelevation to optimize pressureschedule.

• Other Positions Pressurizationsystem uses selected value for landingelevation reference in the event of an

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FMGC failure or incorrect landingelevation in the database. Actual valueis displayed on the ECAM CRUISEand PRESS pages.

•Ditching Switch ( Guarded )

• Normal Selects normal systemoperation.

• ON Commands operating system toclose the outflow valve, emergencyram air inlet, avionics ventilation inletand extract valves and pack flowcontrol valve.

Outflow valve will not automatically

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2.2.11. Lighting & APU Control Panel ( A320 )

Exterior Lights

Strobe LightsControls the operation of the white strobelights located on each wing tip and below theAPU tail cone.

• OFF Turns lights OFF• AUTO Causes strobe lights to come

on automatically when the nose gearshock absorber is not compressed.

• ON Turns lights ON•

Beacon LightsControls the operation of the red Beacon lightslocated on the top and bottom of the fuselage.

• OFF Turns lights OFF• ON Turns lights ON•

Wing LightsControls the operation of the wing illuminationlights located on each side of the forwardfuselage. The lights illuminate the wing leadingedge and engine air intake.


NAV & LOGO LightsControls the operation of the navigation lights.Dual navigation lights are located on eachwingtip and on the APU tail cone.

• OFF Turns lights OFF• 1 Turns first set of navigation lights

ON• 2 Turns second set of navigation

lights ON•

RWY Turn OFF LightsControls the operation of the Runway turnofflights located on the nose gear strut.


Land L / RControls the operation of the Left and RightLanding lights located inboard of the engines.

• RETRACT Causes the respectivelight to retract and turn off.

• OFF Causes the respective light togo off. (but remain extended)

• ON Causes the respective light toextend. The light comes onautomatically when fully extended..

•NoseControls the operation of the taxi and takeofflights located on the nose gear strut.

• OFF Turns the taxi and takeoff lightsOFF.

• TAXI Turns the taxi lights ON.• T.O. Turns the taxi and takeoff lights

ON.•

APU Control

Master SwitchWhen selected ON:

• On illuminates blue• ECB powerup test is initiated• APU air inlet flap opens• APU fuel isolation valve opens• APU fuel pump runs• ECAM APU page is displayed

When selected OFF:• On light extinguishes• APU START switch AVAIL light

extinguishes• APU shuts down after two minutes for

cooling• APU air inlet flap closes•

START SwitchWhen selected ON:

• On illuminates blue• The APU starter is energized after air

inlet flap is fully open• Ignition occurs

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• At a preset N, the starter is deenergized and ignition ceases

At 95% N:• On light extinguishes• AVAIL light illuminates green• The APU is available to supply Bleed

Air and/or Electrical power• After 10 seconds the ECAM APU page

disappears.•

Interior Lighting Control

OVHD INTEG LTControls the intensity of the overhead integrallighting.

Ice IND & STBY CompassControls the operation of the ice indicator andstandby compass integral lighting.

Dome Light• OFF Turns Dome light OFF• DIM Reduces Dome lighting intensity• BRT Selects both Dome lights on

high intensityANN Light

• TEST Causes all flight deckannunciator lights to illuminate. Allliquid crystal displays (LCDs) indicate"8"s.

• DIM Reduces the illumination ofAnnunciator lights

• BRT Increases the illumination of theAnnunciator lights for normaloperation.

Emergency Lighting / Signs Control

Seat Belts Lights• OFF Turns signs off and associated

chime sounds.• ON Causes FASTEN SEAT BELT

signs (in cabin) and RETURN TOYOUR SEAT sign (in lavatories) toilluminate. Associated chime sounds.

•No Smoking Lights

• OFF Turns NO SMOKING and EXITsigns off and associated chimesounds.

• AUTO Causes NO SMOKING andEXIT to come on when the landinggear is extended and to go off whenthe gear is retracted.. Associatedchime sounds when the signs come onand go off.UPDATE Currently the NOSMOKING sign is always illuminatedand needs to remain in Auto to allowfor Emergency exit battery charging.

• ON Causes NO SMOKING signs toilluminate and associated chimesounds. The EXIT signs may or maynot illuminate, depending on whichCabin Attendant Module (CAM) isinstalled.

•EMER EXIT LT

• ON Causes overhead emergencylights, EXIT signs and escape pathlighting system to illuminate.

• ARM Causes overhead emergencylights to automatically illuminate if ACbus 1 or DC ESS SHED bus fails, or ifthe emergency generator is operatingdue to normal aircraft electrical powerfailure.

Escape path lighting and EXIT signsautomatically illuminate if DC ESSSHED bus fails or normal aircraftelectrical power fails without theemergency generator operating.

EXIT sign also automatically illuminatewhen cabin altitude exceeds 11,300feet and may illuminate when the NOSMOKING switch is selected ON,independent of EMER EXIT LTselector.

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2.2.12. a320 Throttle Controls Transmission Switches

When pushed in, selected the associatedchannel for transmission and the three greenlines illuminate. The channel is deselected bypushing the switch again or selecting anotherchannel.

• VHF/HF When pushed, allowscommunication on applicabletransceiver. "CALL" flashes when aSELCAL is received on the applicableradio.

• INT When pushed, allowscommunication on the flight interphonesystem. "MECH" flashes when a call isreceived from the external serviceinterphone panel. Light goes off after60 seconds if not reset.

• CAB When pushed, allowscommunication on the Cabininterphone system or serviceinterphone. "ATT" flashes when a callis received from a Flight Attendantstation. Light goes off after 60 secondsif not reset.

• PA Used for PA transmission viaboom, oxygen mask or hand mike.The transmission switch must bepressed and held to use the PAsystem. PA announcements can alsobe made using the cockpit handsetwithout selecting the PA transmissionswitch.

Reception KnobsSelect reception channels and adjustassociated audio levels. When knob isreleased out, the respective channel isselected and the knob illuminates.

INT / RAD SwitchOperates as a presstotalk switch for boon oroxygen mask microphones.

• INT The interphone is "hot" betweencockpit crew members, regardless ofthe transmission switch selection. TheINT knob must be selected forreception.

• Neutral Disconnects microphonesfrom transmission. Reception isnormal.

• RAD Connects boom or maskmicrophones to facility selected on theACP. Springloaded to the neutralposition.

ON Voice SwitchInhibits ADF and VOR IDENT signals. Switchilluminates when pushed in.

Reset SwitchExtinguishes lights in the CALL, MECH andATT transmission switches.

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2.2.13. Radio Management Panel (RMP) ( A320 )

Frequency Displays Windows• ACTIVE Shows the active frequency

of the selected radio (which isidentified by the illuminated radioselection key).

• STBY/CRS Displays the NAV courseor standby radio frequency. Thisfrequency is activated by pushing thetransfer switch, and is changed byrotating the frequency selector knobs.

•Transfer Switch (Arrow)When pushed, exchanges the active andstandby frequencies, and tunes the new activefrequency.

Radio Selection Switches (VHF, HF & AM)When pushed, the ACTIVE window displaysthe tuned frequency and the STBY/CRSwindow displays the Standby frequency.

SEL IndicatorIlluminates on both RMPs when a transceivernormally associated with an RMP is tuned byanother RMP.

Frequency Selector KnobsSelects the course or standby radio frequency.Displayed in STBY/CRS window.Inner knob controls decimal values.

NAV Switch (Guarded)When pressed on RMP 1 or 2, the radionavigation backup mode engages.Removes autotuning from the FMGC and theVOC, ILS and ADF receivers are controlled bythe RMP.The switch illuminates green when pushed.Pushing switch a second time returns controlto the FMGC.

STBY NAV Selection Switches (VOR, ILS,MLS & ADF)When the NAV switch is selected, enablestuning of the selected navaid via the frequencyselector knobs.Each RMP tunes its respective VOR.Tuning an ILS on either RMP tunes both ILSreceivers, if both RMPs are in the standby NAVmode.The ADF can only be tuned on RMP 1.

BFO SwitchWhen selected, the Beat Frequency Oscillatormode becomes active, provided the ADFreceiver is selected.

ON/OFF SwitchControls the power supply to the RadioManagement

.

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2.2.14. Flight Controls & Cargo Heat(A320)

Flight Controls

ELAC Switch• ON Engages the associated elevator

and aileron computer.• OFF Disengages associated

computer.• Fault Light Illuminates amber:

• When a failure is detected• During ELAC power up test.•

SEC 2/3 Switch• ON Engages the associated spoiler

and elevator and aileron computer.• OFF Disengages associated

computer.• Fault Light Illuminates amber when a

failure is detected.•

FAC Switch• ON Engages the associated flight

augmentation computer.• OFF Disengages associated

computer.

• Fault Light Illuminates amber when afailure is detected.

Cargo Heat

HOT AIR Switch• AUTO Automatically controls Cargo

Heat pressure regulating valve.• OFF Closes Cargo Heat pressure

regulating valve and reset fault circuit.• Fault Light Illuminates amber when

duct overheat is detected andextinguishes when temperature dropsand OFF is selected. System thenresets with ISOL VALVE switch ON.

•AFT ISOL Valve Switch

• AUTO Opens inlet and outletIsolation valves and activatesextraction fan provided there is nosmoke detected in the AFT cargocompartment.

• OFF Closes inlet and outlet Isolationvalves and turns off extraction fan.

• Fault Light Illuminates amber wheneither inlet or outlet valve is in

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disagreement with the selectedposition.

•Temperature SelectorAdjust temperature for AFT Cargocompartment.

• COLD Approximately 40°F• HOT Approximately 80°F• Center Approximately 60°F

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2.2.15. Cargo Smoke Panel ( A320 )

A320 Cargo Smoke Panel

Smoke Light (red) FWD / AFTIlluminates when smoke is detected inrespective Cargo compartment. Activated byboth loops or by one loop if the other is faulty.Activation of the AFT CARGO SMOKE lightalso closes the AFT Cargo inlet and outletisolation valves and shuts off the AFT Cargoextraction fan.

A320 TEST Button• Tests smoke detectors in sequence.• Tests SMOKE lights twice with

associated ECAM.• Closes ventilation system isolation

valves.• Tests DISCH lights.

•DISCH Agent 2 Light (amber)

• Illuminates 60 minutes after Agent 1 isdischarged in the FWD or AFTcompartment.

• Extinguishes when Agent 2 isdischarged.

•DISCH Lights 1 & 2 (amber)Illuminate when associated extinguishing agenthas been discharged.

DISCH ( red Guarded )Discharges associated agent (1 or 2) in therespective Cargo compartment (FWD or AFT).

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2.2.16. Ventilation Panel, Engine Start & Rain Repellent & Wiper Controls ( A320 )

Ventilation PanelBlower/Extract SwitchesWhen both switches are in AUTO:

• On ground before takeoff powerapplied: the Ventilation system is inopen circuit configuration.

• On ground after takeoff power applied,or in flight: the Ventilation system is inclosed circuit configuration.

• In flight, Ventilation system can be inthe intermediate configuration if skintemperature is above flight threshold.

When either switches are in OVRD:• The system goes to closed circuit

configuration.• Air from Air Conditioning system is

added to Ventilation system.• text

When both switches are in OVRD:• Air is provided from the Air

Conditioning system and thenextracted overhead.

• The blower fan stops.CAB Fans Switch

• ON Activates the two cabinrecirculation fans.

• OFF Stops the two cabin recirculationfans.

Engine Manual Start / N1 Mode Panel

ENG MAN Start Switches

• ON• The start valve opens,

provided the ENG MODEselector is in CRANK orIGN/START and N2 is lessthan 10%.

• Both pack valves close.• The ON light illuminates blue.

• OFF The start valve is closed unlessa start cycle is in progress.

•ENG N1 Mode Switches

• ON Thrust control reverts from thenormal (EPR) control mode to thealternate (N1) control mode. When anautomatic reversion to the N1 rated orunrated mode occurs, selecting theswitch confirms the mode. The ONlight illuminates blue.

• OFF The normal (EPR) control modeis selected, if available.

•Wiper Controls

Wiper SelectorControls operation of the respective Wiper.When selected OFF, the Wiper stops out ofview.

Rain RPLNT Switch

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3 Glareshield

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3.1. a320 ACARS IDU AUTO Land

Auto LandIlluminates below 200 feet RA in the LANDmode when any one of the following occurs:

• Both Autopilots are off.• Excessive localizer deviation or glide

slope deviation.• Loss of localizer signal above 15 feet

RA or loss of glide slope signal above100 feet RA.

Master WARN LightFlash red for level 3 Warnings. Accompaniedby an aural Warning.The lights extinguish when:

• Either MASTER WARN light ispushed.

• The Warn no longer exists.• The CLR key on the ECAM Control

Panel is pushed.• The EMER CANC key on the ECAM

Control Panel is pushed.The aural Warning stops when:


• The Warning no longer exists.• The EMER CANC key on the ECAM

Control Panel is pushed.

Master CAUT LightIlluminate amber for level 2 cautions.Accompanied by a single chime.The lights extinguish when:

• Either MASTER CAUT light is pushed.• The Caution no longer exists.

• The CLR key on the ECAM ControlPanel is pushed.

• The EMER CANC key on the ECAMControl Panel is pushed.

CHRONO Switch• First push causes Chronometer time to

display in boxed format in lowerleftcomer of onside ND. Operatesindependently of clock Chronometerand other ND Chronometer.

• Second push freezes the displayedvalue.

• Third push resets the Chronometerand removes the display.

Side Stick Priority LightsArrow LightIlluminates red in front of pilot losing authority.Extinguishes when sidestick activation is reestablished by:

• Release of other priority switch in lessthan 30 seconds.

• Pushing either priority switchmomentarily to cancel a latchedpriority condition.

•Captain's LightIlluminates green to indicate associatedSidestick has established priority by activationof its priority switch and the opposite Sidestickis not in neutral.Extinguishes when the opposite ( F/O Light ) isreturned to neutral.

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3.2. a320 EFIS

Barometric WindowDisplays Barometric reference.

Barometric SelectorProvides selection of Barometric reference.The outer knob selects units of reference ininches of mercury (In Hg) or Hectopascals(hPa). The inner knob provides selection of thereference value displayed in the Barometricwindow and on the PFD. At airplane powerup,either 1013 hPa or 29.92 In Hg is displayed.

When the selector is pulled, the standardBarometric reference setting (1013 hPa/29.92In Hg) is displayed in the Barometric windowand "STD" is displayed on the PFD. Pushingthe knob enables selection of a newBarometric reference.

FD SwitchWhen pushed, the respective flight directorcommand bars or flight path vector/flight pathdirector is displayed on the associated PFDand the switch illuminates.

ILS SwitchWhen pressed, the localizer and glide slope

scales are displayed on the PFD and theswitch illuminates. Deviation symbols aredisplayed when a valid ILS signal is beingreceived.

Data Display Switches (5)Display optional data in addition to the datapermanently displayed in the PLAN, ARC andROSE NAV modes. Only one switch can beactivated at a time, The selected switch isilluminates.

Mode SelectorProvides selection of desired navigationdisplay.

Range SelectorProvides selection of desired Range on therespective ND. In the event of a mode orRange data failure, the ND defaults to ROSENAV with an 80 nm Range.

VOR/ADF Selector 1&2Provides selection of VOR and/or ADF bearingpointers and DME on respective ND in anymode except PLAN. Corresponding navaiddata characteristics are shown.

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3.3. a320 Flight Control Unit

FCU Window

SPD / MACH WindowDisplays dashes when the speed/Mach ismanaged. Displays selected speed from theFCU or preselected speed from the MCDU.

Managed Speed LightIlluminates to indicate an FMGS managedspeed is being flown.

Heading / Track WindowDisplays dashes when LNAV is engaged.

LAT LightIlluminates to indicate managed lateral mode iseither armed or engaged.

Flight Director Display ModeIndicates that the flight director is in eitherHDG V/S or TRK FPA display mode.

ALT WindowDisplays altitude selected with the altitudeknob. The window never displays dashes,even when VNAV is engaged.

LVL / CH LightIlluminates to indicate managed vertical modeis either armed or engaged.

V/S / FPA WindowDisplays the vertical speed or flight path angleselected using the vertical speed/flight pathangle knob. The applicable mode is controlledwith the HDGV/S TRKFPA switch.

Switches / Knobs left to rightSPD / MACH SwitchWhen pushed, changes the value in theSPD/MACH window from airspeed to Mach,and viceversa.

Speed / MACH SwitchWhen rotated, changes the value displayed inthe SPD/MACH window.

When pulled, the selected speed displayed inthe SPD/MACH window engages.

When pushed, FMGS managed speedengages, the managed speed light illuminatesand dashes appear in the SPD/MACH window.

Heading / Track KnobWhen rotated, changes the value displayed inthe HDG/TRK window.When pulled, the selected heading/trackdisplayed in the HDG/TRK window engages.If a heading is selected prior to pulling theknob, the airplane turns in the shortestdirection to the selected heading.If a heading is selected after pulling the knob,the airplane turns to the new heading in thedirection the knob is turned.If the knob is pulled during a turn, the airplanerolls out on the existing heading.

When pushed, LNAV engaes, the LAT lightillumonates and dashes appear in theHDG/TRK window.

LOC SwitchArms, engages, or disengages the LOC mode.It takes a minimum of 3 seconds after armingfor the LOC to engage in the capture mode

Flight Director Mode SwitchWhen pushed, changes betweenheading/vertical speed and track/flight pathangle display modes of both flight directors.

AP SwitchesEngages/disengage selected autopilot.Illuminate green when the autopilot isengaged.

A/THR SwitchArms or deactivates autothrottle system.Illuminates green if the autothrottle is armed orengaged.

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Altitude KnobChanges the altitude displayed in the ALTwindow.The inner knob rotates to change the altitudevalue.The outer knob provides selection of 100 or1000 foot increments.

When pulled, the open climb or open descentengages.

When pushed, VNAV engages and theLVL/CH light illuminates.

EXPED SwitchEngages the EXPED mode to reach thealtitude window with maximum verticalgradient. The expedite mode can only bedisengaged by the engagement of anothermode.

Metric ALT SwitchWhen pushed, the FCU altitude is displayed inmeters on ECAM.

Vertical Speed / Flight Path Angle KnobWhen rotated, selects the vertical speed orflight path angle displayed in the V/S / FPAwindow.When the knob is pulled, vertical speedengages.When the knob is pushed, the airplaneimmediately levels off.

APPR SwitchArms, engages or disengages the followingmodes:LOC and G/S modes if an ILS approach hasbeen slected from the MCDU database.APP NAV, FINAL and FINAL APP modes if anonprecision approach has been selectedfrom the MCDU database.

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3.4. a320 EFIS

Barometric Window

Displays Barometric reference.

Barometric SelectorProvides selection of Barometric reference.The outer knob selects units of reference ininches of mercury (In Hg) or Hectopascals(hPa). The inner knob provides selection of thereference value displayed in the Barometricwindow and on the PFD. At airplane powerup,either 1013 hPa or 29.92 In Hg is displayed.

When the selector is pulled, the standardBarometric reference setting (1013 hPa/29.92In Hg) is displayed in the Barometric windowand "STD" is displayed on the PFD. Pushingthe knob enables selection of a newBarometric reference.

FD SwitchWhen pushed, the respective flight directorcommand bars or flight path vector/flight pathdirector is displayed on the associated PFDand the switch illuminates.

ILS SwitchWhen pressed, the localizer and glide slope

scales are displayed on the PFD and theswitch illuminates. Deviation symbols aredisplayed when a valid ILS signal is beingreceived.

Data Display Switches (5)Display optional data in addition to the datapermanently displayed in the PLAN, ARC andROSE NAV modes. Only one switch can beactivated at a time, The selected switch isilluminates.

Mode SelectorProvides selection of desired navigationdisplay.

Range SelectorProvides selection of desired Range on therespective ND. In the event of a mode orRange data failure, the ND defaults to ROSENAV with an 80 nm Range.

VOR/ADF Selector 1&2Provides selection of VOR and/or ADF bearingpointers and DME on respective ND in anymode except PLAN. Corresponding navaiddata characteristics are shown.

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3.5. a320 ACARS IDU AUTO Land

Illuminates below 200 feet RA in the LANDmode when any one of the following occurs:

• Both Autopilots are off.• Excessive localizer deviation or glide

slope deviation.• Loss of localizer signal above 15 feet

RA or loss of glide slope signal above100 feet RA.

Master WARN LightFlash red for level 3 Warnings. Accompaniedby an aural Warning.The lights extinguish when:


• The Warn no longer exists.• The CLR key on the ECAM Control

Panel is pushed.• The EMER CANC key on the ECAM

Control Panel is pushed.The aural Warning stops when:


• The Warning no longer exists.• The EMER CANC key on the ECAM

Control Panel is pushed.

Master CAUT LightIlluminate amber for level 2 cautions.Accompanied by a single chime.The lights extinguish when:

• Either MASTER CAUT light is pushed.• The Caution no longer exists.

• The CLR key on the ECAM ControlPanel is pushed.

• The EMER CANC key on the ECAMControl Panel is pushed.

CHRONO Switch• First push causes Chronometer time to

display in boxed format in lowerleftcomer of onside ND. Operatesindependently of clock Chronometerand other ND Chronometer.

• Second push freezes the displayedvalue.

• Third push resets the Chronometerand removes the display.

Side Stick Priority LightsArrow LightIlluminates red in front of pilot losing authority.Extinguishes when sidestick activation is reestablished by:

• Release of other priority switch in lessthan 30 seconds.

• Pushing either priority switchmomentarily to cancel a latchedpriority condition.

Captain's LightIlluminates green to indicate associatedSidestick has established priority by activationof its priority switch and the opposite Sidestickis not in neutral.Extinguishes when the opposite ( F/O Light ) isreturned to neutral.

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4 Center Instrument Panel

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4.1. Gasper Air Vent & Speaker(A320)

Gasper Air Vent

Speaker

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4.2. Captain's Forward Panel(A320)

GPWS G / S• GPWS Illuminates red when any

GPWS mode from 1 through 4 isactivated and an aural warningsounds.

• G / S Illuminates amber when GPWSmode 5 is activated and the "GlideSlope" aural warning sounds. Pressingthe switch silences the "Glide Slope"warning and turns off the G/S light.

•PFD Brightness Control KnobManually adjusts onside PFD brightness.When PFD is selected OFF, the PFD image isauto,atically displayed on the onside ND. (NDmay be recovered by pushing the PFD/NDXFR switch.)

PFD/ND XFR SwitchInterchanges the onside PFD and NDdisplays.

ND Brightness Control KnobManually adjusts onside ND brightness. Outerknob controls the brightness of the weatherradar image only. Inner knob controls thegeneral brightness of the ND symbology.

Loud Speaker KnobAdjust loudspeaker audio volume. Aural alert,CVR test, and voice message level are notcontrolled by these knobs.

Console/Floor Lighting SelectorControls the intensity of the side consoles,

briefcase areas and the floor around the pilotseats

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4.3. Captain's Primary Flight Display (PFD)(A320)

Flight Mode AnnunciationsDisplays 5 columns 3 lines of flight modeannunciations and messages

PFD Airspeed Indications

Overspeed Protection SymbolIndicates in green the speed (VMO + 6 knots /Mmo + 0.01) at which Overspeed protectionactivates.

VMAXDefined by the lower end of a red and blackstrip along the speed scale. Represents thelowest of VMC ( or MMC ), VFE, or VLE if thelanding gear is extended. Computed by theFACs.

Green Dot SpeedAppears while flying in the clean configuration.Represents the best lifttodrag, as computedby the FACs.

Speed Indicators• F Minimum Flap Retraction Speed

Appears in green next to the minimumspeed for selecting position 1 when theFLAPS selector is in position 3 or 2.Computed by the FACs.

• S Minimum Slat Retraction Speed Appears in green next to the minimumspeed for selecting position 0 when theFLAPS selector is in position 1.Computed by the FACs.

• 1 Decision Speed (V1) Appears inblue next to the speed entered by thecrew through the MCDU. When out ofindication range, appears on upperpart of scale. Disappears after liftoff.

•Actual Airspeed Reference LineIndicates the actual airspeed where the scalevalue moves in front of the line. Airspeedindication starts from 30 knots.

Speed Trend ArrowStarting from the airspeed reference line,points to the speed value which will be attainedin 10 seconds if the acceleration remainsconstant. Appears only when speed differenceis greater than two knots. Disappears whenspeed difference is less than one knot, or ifFACs fail

Target Airspeed PointerPoints to the target airspeed value or theairspeed corresponding to the target Machnumber. The pointer is magenta when the

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target airspeed is the value computed by theFMGC in managed speed mode. The pointer isblue when the target airspeed is manuallyentered on the FMGC or manually entered onthe FCU. When the target airspeed is out ofthe speed tape range, the target speed value isdisplayed above or below the speed tape innumeric form.

Minimum Selectable Speed (VLS)Represents 1.13 stall speed (VS) duringtakeoff or following touch and go as computedby the FACs.

Alpha Protection SpeedRepresents the speed corresponding to theangle of attack at which alpha protectionactivates, as computed in pitch normal law bythe FACs.

Mach NumberDisplays when number is greater than .5.

ILS InformationThe following appears when an ILS frequencyand course have been selected in the MCDUand when the ILS switch on the EFIS controlpanel is pushed:

• ILS identification as decoded from theILS receiver.

• ILS frequency.• DME distance if a DME is colocated.

PFD Attitude Indications

Fixed Airplane Symbol

Pitch ScaleProvides graduations between 80° nose upand 80° nose down with 2.5° incrementsbetween 10° nose down and 30° nose up.

Roll IndexPoints to angle of bank on roll scale.

Roll ScaleProvides graduations at 0, 10, 20, 30 and 45degrees of bank.

Side Slip Index / Beta TargetIndicates lateral acceleration on the groundand side slip in flight as provided by ADIRS.Reaches stop at .3Gs.

Bank Angle Limit IndicatorIndicates bank angle limitation in green at ±67°on roll scale. Replaced by amber "X" with lossof normal law.

Glide Slope Deviation ScaleAppears when ILS switch is pushed. Flashes

continuously when the deviation exceeds onedot for two seconds or more (above 100 feetRA).

Glide Slope Deviation Index and LocalizerIndexAppear when glide slope and localizer signalsare valid if deviation scales are displayed.

Localizer ScaleAppears when ILS switch is pushed. Flashescontinuously when the deviation exceeds onefourth dot for two seconds or more (above 15feet RA).

Target Altitude or Selected FL IndicatorIndicates the FCUselected target altitude orthe selected flight level.

Altitude IndicationDisplays altitude in green on a white movingscale. "NEG" appears in window to indicatenegative altitude. Window changes from yellowto amber if the airplane deviates from theselected altitude or flight level. Numerical valuechanges from green to amber when theairplane flies below any MDA entered in theMCDU.

Barometric Reference IndicationIndicates that either STD or QNH has beenselected as barometric reference.

PFD Vertical Speed IndicationsLabel

Vertical Speed ScaleDisplays white on grey. Graduated each 500feet per minute.

Digital Vertical Speed IndicationDisplays green. Disappears when verticalspeed is less than 200 feet per minute.Window surrounding indication becomesamber to indicate inertial data has beenreplaced by barometric information.

Analog Vertical Speed PointerDisplays green. If vertical speed exceeds 2000feet per minute, pointer positions to end ofscale. Speed indicators becoming amber if anyof the following occur:

• Vertical speed exceeds 6000 fpm.• Vertical speed exceeds 2000 fpm

descent and radio altitude is between2500 and 1000 feet.

• Vertical exceeds 1200 fpm descentand radio altitude is less than 1000feet.

PFD Heading IndicationsLabelActual Track Diamond

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Indicates the actual track on the heading scalein green.

Selected Heading or Track IndexPoints to the selected heading or track on theheading scale.

ILS Course PointerAppears when an ILS frequency and coursehave been selected and when ILS switch ispushed.

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4.4. Captain's Navigation Display (ND)(A320)

Groundspeed and True AirspeedDisplays airplane speeds in green asdetermined by ADIRS.

Wind Direction / SpeedDisplays wind direction and speed with respectto true north in numeric form and wind directionin respect to magnetic north in green arrowform. Dashes indicate no wind data received.

APP MassagesDisplayed in green when an ILS or VORapproach has been selected on the MCDU.

TO Waypoint Information• Identification (Tille) Displays

in white.• Track To Go (011) Displays in

green.• Distance To Go (5.5nm)

Displays in green.

• Estimated Time of Arrival(05:36) Displays in green.

Arc Mode Range MarksDisplays range scale selected on the EFIScontrol panel (10 to 320 nm) in white.

Weather Radar ImageDisplays when radar is operating in all modesexcept PLAN. The echo colors correspond tothe precipitation rate.

Chronometer IndicationDisplays elapsed time in white when onsidechronometer is started.

ILS Marker BeaconFlashes blue for outer marker, amber formiddle marker and white for inner marker.RunwayDisplays selected Runway as oriented runwaysymbol. Down to scale if range 10, 20 or 40 nmis selected.

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Holding PatternDisplays active Holding Pattern.

VOR/DME NavaidDisplays green if a current waypoint, white if itis the TO waypoint, blue when tuned fordisplay and magenta when not a part of theflight plan but displayed as option as selectedon the FCU.

Left/Right Navaid DisplaysDisplay the following information for theselected Navaid, the left side for receiver oneand the right side for receiver two:

• Type of Navaid (ADF in green or VORin white).

• Shape and color of the associatedbearing pointer.

• Navaid identification (or frequency if noidentification is available).

• DME distance if a DME is colocatedto the selected VOR.

• Method of tuning• M for Navaid manualy tuned

through the MCDU• R for Navaid tuned from an

RMP.Airplane Symbol

WaypointsActive waypoint displays white, all othersgreen. Others magenta when WPT displayselected.

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4.5. Standby Airspeed Standby Altimeter

Standby AirspeedConnected directly to the standby pitot andstatic source. Airspeed bugs are requiredequipment but may be deferred if missing.

Standby AltimeterConnected directly to the standby staticsource. Altimeter bugs are required equipmentbut may be deferred if missing.

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4.6. Standby Attitude Indicator(A320)

TERR on NDButton is used when the terrain counter isdisplayed on the ND.

Attitude IndicatorIndication remains available for five minutesafter total electrical failure.

Red FlagFlag appears with failure of indicator or powersupply.

Caging KnobWhen pulled, centers and levels the horizon.(Airplane should be level for this action.)

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4.7. Digital Distance & Radio Magnetic Indicator (DDRMI)(A320)

VOR DME CountersIndicate DME distance to the VORs tuned onthe RAD NAV or PROG page or RMP.

HDG FlagAppears when the following occur:

• ADIRS heading signal is invalid.• RMI fails.• Power supply fails.

Bearing Pointers• Indicate the Magnetic Bearing to VOR

1.• Indicate the Magnetic Bearing to VOR

2 or ADF 1 as selected by theVOR/ADF selectors.

Compass CardDisplays the bearing scale. Normally suppliedfrom ADIRU 1.

VOR/ADF FlagsAppears when:

• Selected VOR or ADF receiver fails.• ADIRS heading signal is invalid.• RMI fails.• Power supply fails.

Associate pointer remains at the valid position.

VOR/ADF SelectorsAllows selection of VOR 2 or ADF 1 on thedouble pointer.

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4.8. Primary Engine Display (Engine/Warning Display)

Upper Left SectionEPR

Actual EPR Digital Indicator

Actual EPR Pointer

EPR Command ArcDisplays difference between EPR pointer andEPR command value. This transient arc is onlydisplayed with the A/THR engaged.

Maximum EPR (Red Mark)Displays the EPR limit value corresponding tothe fullforward throttle position.

Throttle Indication (circle)Displays the predicted EPR corresponding tothe throttle position.

REV IndicationAppears when one reverser cowl is not stowedor is unlocked or inadvertently deployed. Inflight, REV flashes for 9 seconds and thenremains steady. The indication changes to

green when the doors are fully deployed.

EGT

Actual EGT Pointer and IndicationDisplays green. Pulse amber when EGTexceeds 610°C. Pulse red when EGT exceeds635°C.

Maximum Permissible EGTRepresented by red line. If 635°C is exceeded,a red mark appears at maximum valuereached. It will only disappear at the nexttakeoff or by Maintenance action.

Maximum EGTDisplays amber at 610°C. Not shown duringengine start sequence.

N1

Actual N1 Pointer and IndicationDisplays green. Pulse amber when N1 exceedsN1 rating limit. Pulse red when N1 equals orexceeds 100%.

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Maximum Permissible N1Represented by red line. If 100% is exceeded,a red mark appears at maximum valuereached. It will only disappear at the nexttakeoff or by Maintenance action.

Upper Right Section

Thrust Limit ModeDisplays selected status. In flight (or on theground with engine stopped), the selectedmode corresponds to the detent of the mostadvanced throttle.

EPR Rating LimitIn flight, displays value computed by theFADEC receiving the highest actual EPR. Onthe ground the value is computed by theFADEC receiving the most advanced throttleposition.

Fexible Takeoff TemperatureDisplays Fexible Takeoff Temperature selectedthrough the MCDUs when FLX mode selected.

F.F. IndicationDisplays Fuel Flow to each engine (pounds perhour).

FOB IndicationIndicates total fuel on board. An amber halfbox appears around FOB when quantity shownis not fully usable due to transfer valve failureor loss of center tank pumps.

FlapDisplays when slats or flaps not fully retracted.

• White when selected position isreached.

• Blue when flaps or slats are in transit.• Becomes amber with:

• Loss of both supplyinghydraulic systems, except onground with both engines shutdown.

• Blue when flaps or slats are intransit.

• Application of wing tip brakes.• Failure of slats or flaps.

S, F IndicationDisplays green. Becomes amber with:

• Loss of both supplying hydraulicsystems, except on ground with bothengines shut down.


Actual Position TriangleDisplays green. Becomes amber with:

• Loss of both supplying hydraulicsystems, except on ground with bothengines shut down.


Selectable PositionsDisplay white. Not displayed in cleanconfiguration.

Selected Position TriangleDisplay blue. Disappears when selectedposition is reached.

Flap Lever PositionDisplay green when selected position (0, 1+F,1, 2, 3, or FULL) is reached. Zero notdisplayed when clean confifuration is reached.Indication displays blue during transit.

Lower Left Section

Memo/Failure Information• Displays memos during normal

operation.• When system failure is detected,

displays independent failure andrequired action.

• Once action is performed, displaysindependent and primary failure.

• When ECAM CLR key is pushed,previous memo information reappears.

Lower Right Section

Memo/Failure Information• Displays memos during normal

operation.• When system failure is detected,

memos remain displayed until the crewperforms required action.

• Once required action is performed,displays secondary failure.

• When ECAM CLR key is pushed asecond time, previous memoinformation reappears.

• When ECAM CLR key is pushed athird time, status reminder ("STS")appears.

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4.9. Secondary Engine Display (System/Status Display)

Screen Left

F.USED IndicationDisplays fuel used as computed by theFADEC. The value is frozen at engineshutdown and is reset at engine start on theground. The last two digits are dshed if the fuelused indication is inaccurate due to loss of fuelflow for more than one minute.

OIL Quantity IndicationDisplays Oil Quantity inquarts. Represented bypointer and digital display. Indication pulsesbelow 5 quarts (decreasing) or 7 quarts(increasing).

OIL Pressure IndicationRepresented by pointer and digital display. Thedigital indication pulses if oil pressure exceeds390 psi (increasing) or 385 (decreasing). Bothindications become amber below 80 psi andred below 60 psi.

OIL Temperature IndicationDisplays Oil Temperature in °C. The indicationpulses above 156°C (increasing) or 150°C(decreasing). It becomes amber if thetemperature exceeds 156°C for more than 15minutes or instantaneously when above165°C.

IGN IndicationDisplays during start sequence. The selectedIgnitors "A" or "B" or "AB" are displayed whensupplied.

Start Valve IndicationDisplays positive of start valve. A horizontalline through the circle signifies the valve is fullyopen. A vertical line signifies the valve is fullyclosed.

Engine Bleed PressureDisplays Bleed Pressure upstream from theprecooler. The value becomes amber below 21psi when N2 exceeds 10% with the engine startvalve not closed or when Bleed overpressureis detected.

Screen RightVIB IndicationsDisplays N1 and N2 Vibration levels. Theindication pulses above 5.0. The data is alsodisplayed on the ECAM cruise page.

OIL Filter IndicationDisplays Filter status. An amber CLOGmassage appears in case of excessivepressure loss across the main oil scavenge.

F.Filter IndicationDisplays fuel Filter status. An amber CLOGmassage appears in case of excessivepressure loss across the fuel filter.

Permanent Data

TAT, SAT & GWMessage Area.

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4.10. Landing Gear Indicator, AutoBrake, Antiskid &NoseWheel Steering System (A320)

LDG Gear LightsDisplay proximity detector information receivedfrom LGCIU 1. The LDG GEAR indicator paneldoes not illuminate when LGCIU 1 is notelectrically powered.

• UNLK Illuminate red if the gear is notlocked in the selected position.

• Lights Illuminate geen if the gear islocked down.

AUTO/BRK SwitchesArm the required deceleration rate. The ONlight illuminates blue to indicate positivearming. The DECEL light illuminates greenwhen actual airplane deceleration correspondsto 80% of the selected rate.

• LO Selected for landing. If thedeceleration rate from reverse thrust isnot adequate, progressive pressure isapplied to the brakes four secondsafter ground spoiler deployment toprovide a fixed deceleration rate.

• MED Selected for landing. If thedeceleration rate from reverse thrust isnot adequate, progressive pressure isapplied to the brakes two secondsafter ground spoiler deployment toprovide a fixed deceleration rate.

• MAX Selected for takeoff. During anaborted takeoff, maximum brakepressure is applied when groundspoilier deployment occurs.

A/SKID & N/W STRG Switch• ON

• If green hydraulic pressure isavailable:

• Antiskid is available.• Nosewheel steering is

available.• If green hydraulic pressure is

lost:• Yellow hydraulic

pressure takes overautomatically tosupply the brakes.

• Antiskid remainsavailable.

• Nosewheel steering islost.

• OFF• Yellow hydraulic pressure

supplies the brakes.• Brake pressure must be

limited by referring to the tripleindicator to avoid wheellocking.

• Differential braking remainsavailable via the pedals.

• Antiskid is deactivated.• Nosewheel steering is lost.

TERR ON NDDisplays a "Terrain Map Display" on the ND foraircraft equipped with Enhanced GroundProximity Warning System (EGPWS).

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4.11. Landing Gear Selector(A320)

Landing Gear LeverProvides electrical signals to the two LGCIUswhich control the green hydraulic supply.

• UP Retracts landing gear. When thegear doors open, the main wheels areautomatically braked by the normalbrake system. The nose wheel arestopped by a brake band in the gearwell during door closure. When thelever is UP, the hydraulic supply isautomatically cut off above 260 KIAS

• DOWN Extends the landing gear.The system remains pressurized ifgreen hydraulic pressure is available.An interlock mechanism preventsunsafe retraction by locking the lever

in the DOWN position when any gearshock absorber is compressed or thenosewheel steering is not centered.

DOWN ArrowIlluminates red associated with ECAM "GEARNOT DOWN" warning if the landing gear is notdownlocked with any one of the following:

• Radio altitude less than 750 feet andboth engine's N1 below 75%.

• Radio altitude less than 750 feet andFlaps 3 or FULL selected.

• Flaps FULL selected with both radioaltimeters failed

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4.12. Clock(A320)

CHR ButtonFirst push starts Sweep Second Hand and minutesdisplay in the ET/CHR indicator. Second push stopssecond hand and freezes minutes display. Thirdpush resets second hand to the 12 o'clock positionand blanks CHR indicator.

DATE ButtonSets the Chronometer in the Date Mode. Thedate is set by positioning the UTC Selector toHSD (day), MSM (month) and HLDY (year).Return the UTC Selector to the RUN position.Pressing the DATE button again will resumethe display of UTC time.

ET CounterDisplays elapsed and chronograph time.Chronograph time display has priority over

elapsed time.

Sweep Second HandIndicates Chronometer seconds.

ET Selector• RUN Starts the elapsed time counter.• HOLD Freezes counter time.• RESET Resets counter to zero.

UTC SelectorSets the time.

• RUN Clock will begin normaloperation.

• HLDY Hold• MSM Minutes• HSD Hours

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4.13. Brakes & Accumulator Pressure Triple Indicator(A320)

ACCU PRESS IndicationDisplays the brake accumulator pressure.

BRAKES Pressure IndicationDisplays the yellow hydraulic system pressurethat is supplied to the left and right brakes

.

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4.14. F/O's Primary Flight Display Flags (PFD)(A320)

SPD Sel FlagIndicates failure of selected speed data.

V1 INOP FlagIndicates V1 signal is not valid.

SI FlagIndicates loss of side slip data.

Check ATT FlagIndicates at least a 5 discrepancy in attitudedata between PFDs. Appears on both PFDs inamber.

ALT SELIndicates selected altitude data failure.

Check ALT FlagAppears in amber when the differencebetween both PFD's altitude indications isgreater than 250 feet (QNH), or 500 feet(STD). Inhibited when CAPT and F/O ADRbarometric references disagree.

SPD FlagIndicates speed data failure.

FD FlagIndicates both FMGCs have failed or both FDshave disengaged with FD switches on.

ATT Flag

Indicates attitude data failure.

FPV FlagIndicates drift angle or flight path angle are notvalid when in TRKFPA mode.

G/S FlagIndicates Glide Slope receiver failure.

ALT FlagIndicates altitude data failure.

V/S FlagIndicates Vertical Speed data failure.

V/DEV FlagIndicates Vertical Deviation data failure andILS switch not pushed.

DH FlagIndicates in amber that decision height hasbeen reached.

RA FlagIndicates failure of both radio altimeters.

LOC FlagIndicates failure of Localizer receiver.

SPD LIM FlagAppears when both FACs are inoperative.Indicates the following speed data is lost: VLS,

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S, F, green dot, VTREND, VMAX OP, VMAX,VFE NEXT, VSW.

MACH FlagIndicates Mach data failure.

ILS FlagIndicates ILS frequency is not available or thatboth localizer and glide slope signals havefailed.

DME FlagIndicates DME distance is not available.

HDG FlagIndicates Heading data failure.

Check HDG FlagIndicates at least a 5 discrepancy in Headingdata between PFDs. Appears on both PFDs inamber

.

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4.15. F/O's Navigation Display Flags (ND)(A320)

VOR Course FlagIndicates VOR course data failure in red.

Check HDG FlagAppears inamber when a discrepancy of atleast 5° between both NDs is detected by theflight warning computer (FWC).

HDG FlagIndicates heading data failure in red. Flashesfor the first nine seconds.

LOC FlagIndicates localizer data failure in red. Flashesfor the first nine seconds.

Center Message Area• MODE Change Appears in

green when a discrepancy is detectedbetween the selected mode on theEFIS control panel and the mode sentfrom the onside FMGC, or while anew page is being prepared by theDMC for display. Has priority over"RANGE Change" message.

• RANGE Change Appears ingreen when a range discrepancy isdetected.

• MAP NOT AVAIL Appears inred when "CHANGE" message isdisplayed more than six seconds, or toindicate FMGC failure, or to indicatethat the airplane position provided byFMGC is not valid.

VOR FlagIndicates VOR bearing is not valid. Flashes forthe first nine seconds.

G/S FlagIndicates G/S data failure in red. Flashes forthe first nine seconds.

VOR/ADF/DME FlagIndicates failure of a navigation receiver in red.Flashes for the first nine seconds.

Other Message AreaIndicates incomplete map data. If the numberof images exceeds capacity, the FMGC mightshed some optional data from the display.

• MAP Partly Displayed text• NAV ACCUR DOWNGRAD

or NAV ACCUR UPGRAD text

• SPECIF VOR / D UNAVAIL text

• Check ADF1, Check VOR1,Check ILS1 text

• Set Offside RNG / MODEtext

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4.16. F/O's Forward Panel(A320)

GPWS G / S• GPWS Illuminates red when any

GPWS mode from 1 through 4 isactivated and an aural warningsounds.

• G / S Illuminates amber when GPWSmode 5 is activated and the "GlideSlope" aural warning sounds. Pressingthe switch silences the "Glide Slope"warning and turns off the G/S light.

ND Brightness Control KnobManually adjusts onside ND brightness. Outerknob controls the brightness of the weatherradar image only. Inner knob controls thegeneral brightness of the ND symbology.

PFD/ND XFR SwitchInterchanges the onside PFD and NDdisplays.

PFD Brightness Control KnobManually adjusts onside PFD brightness.When PFD is selected OFF, the PFD image isauto,atically displayed on the onside ND. (NDmay be recovered by pushing the PFD/NDXFR switch.)

Console/Floor Lighting SelectorControls the intensity of the side consoles,briefcase areas and the floor around the pilotseats.

Loud Speaker KnobAdjust loudspeaker audio volume. Aural alert,CVR test, and voice message level are notcontrolled by these knobs.

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4.17. Gasper Air Vent & Speaker(A320)

Gasper Air Vent

Speaker

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5 Control Pedestral

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5.1. Switching Panel(A320)

ATT HDG Selector• CAPT 3 IR 3 replaces IR 1.• NORM

• IR 1 supplies data to PFD 1, ND 1 and RMI/VOR DME.• IR 2 supplies data to PFD 2 and ND 2.

• F/O 3 IR 3 replaces IR 2.

AIR Data Selector• CAPT 3 ADR 3 replaces ADR 1.• NORM

• ADR 1 supplies data to PFD 1, ND 1 and RMI/VOR DME.• ADR 2 supplies data to PFD 2 and ND 2.

• F/O 3 ADR 3 replaces ADR 2.

EIS DMC Selector• CAPT 3 DMC 3 replaces DMC 1.• NORM

• DMC 1 supplies data to PFD 1, ND 1 and upper ECAM display.• DMC 2 supplies data to PFD 2 and ND 2 and lower ECAM display.

• F/O 3 DMC 3 replaces DMC 2.

ECAM / ND XFR Selector• CAPT Transfers SD to Captain's ND.• NORM SD appears on lower ECAM display.• F/O Transfers SD to 1st Officer's ND.

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5.2. Electronic Centralized Aircraft Monitoring (ECAM) Panel (A320)

ECAM Control KnobsSelects respective display on/off and controlbrightness. When the upper ECAM display isselected OFF, the E/WD automaticallytransfers to the lower ECAM display.

T.O. CONFIG KeyWhen pushed, simulates takeoff powerapplication to trigger a warning if the airplane isnot properly configured for takeoff. If theairplane is properly configured, the"T.O.CONFIG NORMAL" message in thetakeoff memo displays green.

EMER CANC Key ( RED )When pushed:

• Warnings: Present aural warning iscancelled. MASTER WARN lightsextinguish. ECAM message display isnot affected.

• Cautions: Present Cautions iscancelled for remainder of flight.STATUS page is automaticallydisplayed. "CANCELLED CAUTION"message and the title of the inhibitionis suppressed after AC powerapplication until first engine start, butcan be manually recalled by pushingRCL key for more than 3 seconds.

System Page Keys ( 11 Keys )When pushed, the related system pageappears on the lower ECAM display.Illuminates after manual selection or when anadvisory is detected. If pushed a second timewhile illuminated, the system page for thepresent phase of flight or current warningappears.

Left / Right CLR KeysIlluminates when an ECAM warning, caution,or status message is displayed. When anIlluminated CLR key is pushed, the ECAMdisplay will change.

STS KeyIlluminates when ECAM STATUS page isdisplayed. When pushed, the STATUS page isdisplayed on the ECAM lower display. Whenpushed with no present status messages,"NORMAL" appears for five seconds. TheSTATUS page may be cleared by pushing theSTS key a second time or by pushing the CLRkey.

RCL KeyWhen pushed, Recalls warning and cautionmassages that have been suppressed with theCLR key or automatic flight phase inhibition."NORMAL" appears for five seconds with nocurrent warnings or cautions. When pushed formore then three seconds, caution messagessuppressed by the EMER CANC key areRecalled.ALL KeyWhen pushed and held, all system pages aredisplayed in succession at onesecondintervals. If the ECAM control panel fails, pushand hold the ALL Key until the desired systempage appears and then release the key tomaintain the display.If only one ECAM screen is available,repeatedly pressing the ALL Key will cycle tothe desired page.

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5.3. a320 Throttle Controls

AutoThrottleAutoThrottle System (A/THR), using inputs from the FMGC, controls thrustbased on airplane speed, altitude andconfiguration. The throttles do not move whenthe Autothrottle System is in use. The systemis armed in flight by pushing the A/THR switchon the FCU when the throttles are not in theengagement range.

Transmit signals to the FADEC, whichcomputes and displays the thrust rating limitand EPR. The throttle can only be movedmanually. There are five lever positions defineby stops or detents: Reverse Idle, Forward Idle, Climb (CL), Continuous Thrust (FLX/MCT) and TakeOff / Go Around (TO/GA)

Autothrottle Disconnect Switches ( RedButtons )When pressed, disconnects the autothrottlesystem.

Select Reverse Thrust by overriding the stop

fitted at the FWD IDLE position. The stop isreset when the throttle is selected back toforward thrust.

Pitch Trim WheelsProvides mechanical control of horizontalstabilizer trim. Trim wheels have priority overelectrical control. Use of trim wheels does notdisconnect the ELACs, as the overridemechanism ensures that the computers remainsynchronized with the manually selectedposition.

Trim wheels must be utilized when pitch directlaw is in effect.

Pitch trim is automatically reset to 0 followingtouchdown as the pitch attitude becomes lessthan 2.5°.Trim Position ScalesIndicate trim position in degrees. Normal rangeis marked by a green band.CG ScalesIndicate relation between CG location andpitch trim setting prior takeoff

.

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5.4. A320 Engine Start & Ignition Panel

ENG MASTER Switches 1 & 2• ON LP fuel valve opens, provided the ENG FIRE switch is in.

During and automatic start, the HP fuel valve opens, provided the ENG MODE selector is atIGN/START.During a manual start, the HP fuel valve opens, provided the ENG MODE selector is atIGN/START and the ENG MAN START switch is ON.

• OFF Closes the HP and LP fuel valves. Resets both channels of the FADEC.ENG Mode Selector

• NORM Continuous ignition A + B is selected when the engine is running and one of thefollowing is met:

• FLEX or TO/GA thrust is selected on the ground• TO/GA thrust is selected in flight• ENG ANTI ICE switch is ON• Engine surge or stall occurs in flight• FLAPS lever position is other then "0" in flight

• CRANK The start valve opens provided the ENG MAN START switch is ON and N2 is lessthan 10%. Ignition is not supplied.

• IGN / START Provides continuous ignition if the ENG MASTER switch is ON and N2 is at idleor greater.During and automatic start, on airplanes placarded :EXTENDED DRY CRANK", expectignition and fuel flow 50 seconds after ENG MASTER switch is selected ON.On airplanes without the placard, expect ignition and fuel flow between approximately 15%and 20% N2.During a manual start the HP fuel valve is open and ignition is selected when the ENGMASTER switch is selected ON.

FIRE LightIlluminates when the respective fire warning is activated and during engine fire test.FAULT LightIlluminates amber in the event of an automatic start abort, or a disagreement between the HP fuelvalve position of FADEC channel A and B.

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5.5. Speed Brake, Trim and Flap Lever Panels( A320 )

Speed Brake

Speed Brake LeverLever provides the following speed brake andground spoiler functions:

• Manually pushing lever down and aftinflight, selects surface position ofSpeed Brakes. A "hard point: isprovided at the 1/2 position.

• Speed Brake deflection is limited toapproximately 1/2 with an autopilotengaged, regardless of lever position.

• Pulling the lever up to the RET positionarms the ground spoilers toautomatically extend for landing orwhen executing a rejected takeoff.

•Trim

RUD Trim SelectorControls the Rudder Trim actuator whichmoves the neutral point of the articial feel at arate of 1 degree per second of rudder travel.Selector is deactivated with A/P engaged.

RUD Trim Position IndicatorDisplays Rudder Trim direction (L or R) andvalue (0° to 20°).

RUD Trim RESET SwitchWhen pushed, the FAC commands the RudderTrim actuator to the zero trim position.

Flaps

Flap LeverCommands flaps and slats for simultaneousoperation to selected position. Lever must bepulled out of detent prior to positioning.Detents are provided at positions 1 and 3 toavoid excessive flap/slat travel by a singleaction.

When the flap lever is in any position otherthen "0" in flight, idle RPM is increased(approach idle) and continuous ignition isactivated.

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5.6. A320 Parking Brake & Landing Gears Gravity Extension

Parking Brake System

Parking Brake HandleSets the Parking Brake by pulling the handleand then turning it clockwise. Activation of theParking Brake deactivates all other brakingmodes. "PARK BRK" is displayed on theECAM memo page.

Landing Gear Gravity Extension SystemGravity Gear EXTN HandleProvides Landing Gear extension in the eventof electrical, hydraulic or mechanical failure.The handle must be extended and then rotatedclockwise three turns to shut off hydraulicpressure, open the doors and unlock the gear.

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5.7. MultifunctionControl Display Unit (MCDU) ( A320 )

To me, the MCDU, Mulifunction Control Display Unit is the heart of the A320/319. Everythingthat the airbus can do, can be controled from this unit. The few pages above, that I have manageto highlight are just a small sample of the many pages that you can access from the MCDU.

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Line Select Keys

Identified as 1L 6L and 1R 6R, provideaccess to the onside data for the left and rightdata fields. The keys transfer data from thescratch pad to the line next to key if acceptableto FMGC. If a caret ( < or > ) appears next to

the key, selecting the key accesses anotherMCDU page.

Fail / FMGC AnnunciatorThe Fail Annunciator illuminates when theMCDU has stopped operating properly. Thedisplay screen blanks, and "FMC FAIL"appears.The FMGC Annunciator illuminates when theFMGC is not linked to the MCDU and theFMGC requests the display. Return to theFMGC via the MCDU MENU key.

MCDU Menu AnnunciatorIlluminates when a system linked to the MCDUrequests the display. The system can bechanged with the MCDU MENU key.

MCDU Page Formats and ColorsPage Formats

Large Font EntryRepresents pilot entries or modifiable data.

Small Font EntryRepresents predicted, defaulted, or FMGCcalculated values.

Line LabelIdentifies the data displayed directly under thislabel line (in small font).

Data LineContains box prompts, dashes, brackets andcomputergenerated data (displayed in smallfont), or pilotentered data (displayed in largefont).

Box Prompts ()Indicates that data entry is required forminimum FMGS operation. The data is enteredvia the scratch pad and replaces the boxprompts when the associated line select key ispressed. The box prompt entry appears inlarge font.

Dashes ( )Indicates that data entry is not usually requiredor that data is being calculated by the FMGC.The calculated data will appear in small font.

Brackets ( [ ] )Indicates that data entry is optional.

Vertical Slew Prompts ()Indicates that the latitude/longitude valuebelow the prompts can be increased ordecreased. The slew prompts also appear inthe last two spaces of the scratch [ad toindicate that the display can be scrolled up ordown.

Asterisk ( * )Indicates that pushing the applicable line selectkey will change the parameters which affectthe airplanes active situation.

Page Prompts ( < or > )Indicates that another MCDU page isaccessible when the associated line select keyis pressed.

Overfly Triangle ()Appears next to a qaypoint identifier on the FPLN page to indicate that the airplane mustoverfly the waypoint.

MCDU ColorsThe MCDU uses extensive colors to conveyspecific information and to assist inidentification and recongnition of various typesof data. The colors used on the MCDU arematched with flight plan data that is graphically

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displayed on the Navigation Display (ND). Thisprovides easy recognition of a particular typeof flight plan on either the MCDU or the ND.

BLUEinforms the crew that data entry is allowed.Pilotentered data is shown in large font andFMSgenerated data is shown in small font.Blue information includes modifiable/selectabledata, entry brackets (no default data exists),missed approach waypoints and activealternate flight plan data.

MAGENTAidentifies constraints. Magenta informationincludes VNAV altitude/speed/time constraintsthat will be met, altitude/speed/time constraintvalues and climb and descent speed limits.

GREENis used for FMSgenerated data that is notmodifiable such as active flight plan data(except "TO" waypoint and destination data)

AMBERsignifies that the item being displayed isimportant and requires immediate attention.Amber information includes VNAValtitude/speed/time constraints that will bemissed, mandatory data, major scratch padmessage and "INSERT/ERASE" prompts.

YELLOWindicates a temporary flight plan display.

WHITEis used t

Line Select Keys

o display data that clarifiespage operations, including page titles, datafield labals, dashed data fields (no dataavailable), minor scratch pad messages,secondary flight plan data, activeIdentified as 1L 6L and 1R 6R, provideaccess to the onside data for the left and rightdata fields. The keys transfer data from thescratch pad to the line next to key if acceptableto FMGC. If a caret ( < or > ) appears next tothe key, selecting the key accesses anotherMCDU page.

ht plan "TO" waypoint and predictions, activeflight plan destination and predictions and page

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Function and Mode Keys

Provides access to the DIR TO page whichenables the pilot to proceed directly from thepresent position to a designated waypoint.

Provides access to the PROGRESS pagewhich displays active flight data concerning theflight plan for the phase of flight during whichPROG is selected. Allows the crew to updatethe flight management position and providesbearing and distance to a specified waypoint.

Provides access to the PERFORMANCEpages which display the performanceparameters for the current phase of flight.

Provides access to the flight plan initializationINIT A and B pages. Used to initialize theFMGC parameters. The INIT B page is onlyavailable on the ground prior to engine start.

Provides access to the DATA INDEX page,which enables access to a menu for variouspages concerning airplane position and status,runways, waypoints, routes and stored data.

Provides access to the FLIGHT PLAN pages,which contain a legbyleg description of theactive flight plan route. Destination and arrivalinformation is also available on applicable flightplan pages.

Provides access to the radio navigation(RADIO NAV) which enables navaids displayand tuning.

Provides access to the FUEL PRED page forreview of fuel and time predictions based onthe active flight plan and display of GW / CGand FOB.

Provides access to the SEC INDEX page

which displays a legbyleg description of thesecondary flight plan route. Destination andarrival information is also available onapplicable flight plan pages.

Currently BLANK

Provides access to the MCDU MENU page,which enables access to systems that use theMCDU for display.

Provides access to the active flight plan page ifanother page is displayed on the MCDU or, if

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the FPLN page is already displayed, thedisplay cycles between the origin anddestination.

Provides access to additional pages of relatedinformation when another page is required tocomplete data display. This capability isindicated by the additional page arrow on theMCDU page title line. The NEXT PAGEfunction wraps around from the last page to thefirst page.

Used to scroll the display up and down whenpages are longer than the available space onthe CRT (indicated by arrows in the last twospaces of the scratch pad). These keys arealso used for changing data )latitude/longitude)by a set amount.When pushed, clears messages and data fromthe scratch pad or an individual data field.

rovides access to the DIR TO page whichenables the pilot to proceed directly from thepresent position to a designated waypoint.

Alphanumeric Keys

Enable entry of letters and numbers into thescratch pad. The slash key " / " is used toseparate pairs of entries in the same data field.

OVFY Key

When pushed, aappears in the scratch pad.Line selecting the waypoint to be overflowncauses theto appear next to that waypointdesignator in the FPLN, and the lateral flight

plan is modified so that the airplane directlyoverflies the waypoint. The overfly functionprovides for flight directly over a waypoint whilemaintaining LNAV.

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5.8. Radio Management Panel (RMP) ( A320 )

Frequency Displays Windows• ACTIVE Shows the active frequency

of the selected radio (which isidentified by the illuminated radioselection key).

• STBY/CRS Displays the NAV courseor standby radio frequency. Thisfrequency is activated by pushing thetransfer switch, and is changed byrotating the frequency selector knobs.

•Transfer Switch (Arrow)When pushed, exchanges the active andstandby frequencies, and tunes the new activefrequency.

Radio Selection Switches (VHF, HF & AM)When pushed, the ACTIVE window displaysthe tuned frequency and the STBY/CRSwindow displays the Standby frequency.

SEL IndicatorIlluminates on both RMPs when a transceivernormally associated with an RMP is tuned byanother RMP.

Frequency Selector KnobsSelects the course or standby radio frequency.Displayed in STBY/CRS window.Inner knob controls decimal values.

NAV Switch (Guarded)When pressed on RMP 1 or 2, the radionavigation backup mode engages.Removes autotuning from the FMGC and theVOC, ILS and ADF receivers are controlled bythe RMP.The switch illuminates green when pushed.Pushing switch a second time returns controlto the FMGC.

STBY NAV Selection Switches (VOR, ILS,MLS & ADF)When the NAV switch is selected, enablestuning of the selected navaid via the frequencyselector knobs.Each RMP tunes its respective VOR.Tuning an ILS on either RMP tunes both ILSreceivers, if both RMPs are in the standby NAVmode.The ADF can only be tuned on RMP 1.

BFO SwitchWhen selected, the Beat Frequency Oscillatormode becomes active, provided the ADFreceiver is selected.

ON/OFF SwitchControls the power supply to the RadioManagement

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5.9. a320 Throttle Controls

When pushed in, selected the associatedchannel for transmission and the three greenlines illuminate. The channel is deselected bypushing the switch again or selecting anotherchannel.

• VHF/HF When pushed, allowscommunication on applicabletransceiver. "CALL" flashes when aSELCAL is received on the applicableradio.

• INT When pushed, allowscommunication on the flight interphonesystem. "MECH" flashes when a call isreceived from the external serviceinterphone panel. Light goes off after60 seconds if not reset.

• CAB When pushed, allowscommunication on the Cabininterphone system or serviceinterphone. "ATT" flashes when a callis received from a Flight Attendantstation. Light goes off after 60 secondsif not reset.

• PA Used for PA transmission viaboom, oxygen mask or hand mike. Thetransmission switch must be pressedand held to use the PA system. PAannouncements can also be madeusing the cockpit handset withoutselecting the PA transmission switch.

Reception KnobsSelect reception channels and adjustassociated audio levels. When knob isreleased out, the respective channel isselected and the knob illuminates.

INT / RAD SwitchOperates as a presstotalk switch for boon oroxygen mask microphones.

• INT The interphone is "hot" betweencockpit crew members, regardless ofthe transmission switch selection. TheINT knob must be selected forreception.

• Neutral Disconnects microphonesfrom transmission. Reception isnormal.

• RAD Connects boom or maskmicrophones to facility selected on theACP. Springloaded to the neutralposition.

ON Voice SwitchInhibits ADF and VOR IDENT signals. Switchilluminates when pushed in.

Reset SwitchExtinguishes lights in the CALL, MECH andATT transmission switches.

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5.10. Instrument Panel & Pedestal Lighting Controls

Flood LT Main PNL KnobControls the intensity of the Center InstrumentPanel flood lighting.

INTEG LT Main PNL & PED KnobControls the intensity of the Main Panel andControl Pedestal intgral lighting.

Door UnlockControls the Flight Deck Door and is used bythe pilots to keep that door locked at specificaltitudes during phases of the flight.

Flood LT PED KnobControls the intensity of the Control Pedestal

flood lighting.

AIDS PrintAircraft Integrated Data System ( AIDS ) allowsthe airline to record and montior all availableparameters which are on the aircraft buses.The button can be programmed ( over theMCDU ) to trigger paper reports, DARrecordings or ACARS transmissions of a selectamount of parameters.

DFDR EventWhen pressed, an event flag will be written onthe DFDR.

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5.11.WX Radar Control Panel(A320)

Both the A320 & A319SYS SwitchActivates Weather Radar to display on ND inany mode except PLAN.

A320 Image/A319 Mode Selector• WX Provides 180° display of

continuously updated Weather Radarinformation.

• MAP text• A320 WX/TURB Provides 180°

display of Turbulence and Weather to40nm and Weather only beyond 40nm.

• A319 WX+T Provides 180 display ofTurbulence and Weather to 40nm andWeather only beyond 40 nm.

GAIN KnobAllows automatic Gain adjustment whenpositioned to AUTO and manual adjustment upto MAX.

TILT KnobControls antenna Tilt angle with reference tohorizon. Tilt angle is displayed on lowerrightcorner of ND.Clockwise rotation commands Tilt up andcounterclockwise commands Tilt down.

Just the A319PWS Switch

• OFF Deactivates PWS• AUTO Activates PWS provided:

• One engine is operating• The airplane is below 2300

feet RA• The TCAS/XPDR switch is in

any position other than STBYGND CLTR SPRS Switch

• ON Suppresses the ground echo onthe screen.

• OFF Normal switch position.

•

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5.12. A320 Cabin Handset

PA AllWhen pushed, the Passenger Address system provides cabin announcement capability from thecockpit. Volume output is automatically increased when an engine is operating.CAPT. SwitchWhen pushed, the ATT light illuminates on all ACPs and a buzzer sounds in the cockpit. "CAPTAIN"message is displayed at the respective Flight Attendant Interphone panel

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5.13 F/O´s FMC look 5.7

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5.14 F/O´s Radio look 5.8

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5.15. F/O´s Throttle Control look 5.9

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5.16. F/O´s Light Control look 5.11

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5.17. TCAS/ATC Control Panel(A320)

Above/Below Switches• N Vertical coverage of 2700' Above

and Below airplane altitude.• Above/Below Vertical coverage of

9900' Above or Below airplanealtitude. Opposite altitude remains2700'.

DEACTDeActivate

Transponder Code Indicator(Window)Displays current Transponder Code.

TCAS/XPDR Selector• STBY TCAS and the transponders

are in the warmup cycle. Message"TCAS STBY" will appear in green onupper ECAM.

• XPDR The transponder is ON andTCAS is in the warmup cycle.

• TA The ATC/TCAS system is ON andall Proximate Traffic and TrafficAdvisory functions of TCAS areoperable. Resolution Advisories andvertical guidance function are inhibited.Target symbols will be visible onlywhen a TA is active.

• TA/RA The ATC/TCAS system is ONand all Proximate Traffic, TrafficAdvisory and Resolution Advisoryfunctions of TCAS are operable.Target symbols will be visible onlywhen a TA or RA is active.

• TFC The ATC/TCAS system is ONand all transponder equipped airplaneswithin 40 nm and the altitude sliceselected by the ABOVE/BELOWswitch are displayed full time: Other,Proximate, TA and RA traffic.

Code Selector KnobSelects TCAS/ATC Code.

ATC Fail Light (red)Indicates a failure of the selected transponder.

IDENT ButtonAccording to Kevin Camilleri A320 F/O, when aaircraft, during a flight, is handed over toanother controller, that controller may requestthe crew to "IDENT" by saying e.g. "American590 squawk ident." The crew can push thisbutton which will send a signal to the groundradars and highlight the aircraft on the ATCscreen. The controller can then confirm thatthe target is actually the aircraft he just spoketo.

Transponder Selector• 1 Selects transponder 1 and ADR 1• 2 Selects transponder 2 and ADR 2

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5.18. ACARS Data Printer(A320)

SLEW SwitchAdvances the paper when pushed

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5.19. A320 SideStick

Takeover (Priority) SwitchWhen pressed:

• Disconnects autopilot• When held in, deactivates the other

Sidestick and allows full singularcontrol. Holding switch for more than30 seconds latches the system,allowing the switch to be releasedwithout losing priority.

A deactivated stick can be reactivatedat any time by momentarily pushingeither priority switch.

If the priority switches on bothsidesticks are pushed, the last oneactivated assumes priority.

• Illuminates Glareshield SIDE STICKPRIORITY lights and activates"PRIORITY LEFT" or "PRIORITY

RIGHT" audio voice messageaccording to control configuration.

Transmit SwitchOperates as a pushtotalk switch for boom oroxygen mask microphones.

• Neutral Boom and maskmicrophones are disconnected fromtransmission, although reception isnormal. Switch is springloaded toneutral.

• Transmit When selected, providestransmission to the facility selected onthe ACP transmission switch. Iftransmit is selected on the sidestickwhen the ACP INT/RAD switch is setto INT, the transmit function haspriority over the interphone function.

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6 Rudder Pedals

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7 Acronyms & DefinitionsAACARS Aircraft Communications Addressingand Reporting SystemACFT AircraftACPT AcceptADF Automatic Direction FinderADS Automatic Dependent SurveillanceAES Airborne Earth StationAEIS Automatic Enroute Information ServiceAFDS Autopilot Flight Director SystemAFN ATS Facilities NotificationAFTN Aeronautical Fixed TelecommunicationsNetworkAGL Above Ground LevelALT AltitudeALTM AltimeterALTN AlternateANP Actual Navigation PerformanceAPT AirportAPU Auxiliary Power UnitATC Air Traffic ControlATIS Automatic Terminal Information Service

BBF Boarded FuelBKN BrokenBLK Blank

CCentigradeCANC/RCL Cancel / RecallCDU Control Display UnitCLB ClimbCLR ClearCNS Communication, Navigation andSurveillanceCPDLC Control ler/Pilot DatalinkCommunications (ICAO)CRZ Cruise

DDARPS Dynamic Air Route Planning SystemDES DescendDEST DestinationDNLNK Downlink

EECS Environmental Control SystemEFIS Electronic Flight Instrument SystemEICAS Engine Indicating and Crew AlertingSystemEMER EmergencyEST EstimateETA Estimate Time of ArrivalETD Estimate Time of DepartureETE Estimate Time EnrouteETR Estimate Time Remaining

FFANS 1 Future Air Navigation System 1FMCS Flight Management Computer SystemFOB Fuel on BoardFPF Flight Plan ForecastFPT Flight Plan Time

GGNSS Global Navigation Satellite SystemGPS Global Positioning SystemGPWS Ground Proximity Warning SystemGOSSU Global Positioning System SensorUnit

HHDG HeadingHF High FrequencyHGA High Gain AntennaHPA Hectopascals

IIAS Indicated AirspeedIDG Integrated Drive GeneratorsIN Inches of MercuryINMARSAT International Maritime Satellite

J

K KT Knots

LLAT LatitudeLDG LandingLNAV Lateral NavigationLONG Longitude

MM MachMCDU Multifunction Control Display UnitMCP Mode Control PanelMFD Multifunction Display

NND Navigation DisplayNM Nautical Mile

O

PPFC Primary Flight ComputersPFD Primary Flight Display

Q

R

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RAIM Receiver Autonomous Integrity MonitorRNP Required Navigation PerformanceRTA Required Time Of ArrivalRWY Runway

SSATCOM Satellite CommunicationSATNAV Satellite NavigationSELCAL Selective CallingSTAB Stabilizer

TTCAS Traffic Collision Avoidance SystemTDM Track Detail MessageTWDL Two Way Datalink

UUPLNIK Uplink

VV1 Takeoff Decision SpeedV2 Scheduled Takeoff Target SpeedVHF Very High FrequencyVNAV Vertical NavigationVOR VHF Omnidirectional Range

WWPT Waypoint

X

Y

Z

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Date post:	05-Feb-2018
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