Sep ZONE TEMPERATURE SELS ed Adjusts the temperature for the associated zone PACK FLOW SEL Note that each increment on the zone temperature sel scale is 2 degrees which ives a selectable range from 18 degrees at COLD to 30 dagrees at HOT. Permits the selection of pack flow according to the umber of passengers and ambient conditions: PACK Ps sw ] RAMARPSSW | HOTAIR PE SW Pack flow control valve prea oon aaa Hot air pressure valve automaticaly controlled automaticaly controled Hot air pressure valve and trim air valves closed, Pack tow contol vehe RAW ARinet dosed dosed Packtow cont vale RAM At open [Be essere ° Duct overeat is detected trovaneal es a RZ etUy‘The pressure regulating valve regulates hot air pressure, Controls the forward inlet and outlet ‘The pressure reguiating valve isolation valves and the extraction cee fan. A duct overheat is detected. a ees ‘The isolation valves and the trim air valve are [Fezal|) closed, and the extraction fanis stooped. Either inlet or outlet valve is notinthe selected position, Controls the aft inlet and outlet 'solalion valves and the extraction fan. ‘The isolation valves are open and the extraction fan runs. ‘Adjusts the temperature for ‘The isolation valves and the the respective cargo trim air valve are closed, and compartment. the extraction fans stopped Either inlet or outlet valve is Select any yellow button notin the selacted position for reviow. AIRBUS “AIR CONDITIONINGVENTILATION ‘The two cabin fans run, ‘The two cabin fans are stopped. Select any yellow button for reviow. C71 )=10 Meee Ly yee etPACK OUTLET TEMPERATURE Nomally green Becomes amber if temperature above limits PACK BY PASS VALVE POSITION This indication is green = Cold -valve fully closed, H = Hot -vaive fully open PACK FLOW Normally green Becomes amber if pack flow control vale is closed Select any yellow button for review, Eye PACK FLOW CONTROL RAM AIR INLET Fully open in fight, Fully open on ground Fuly closed Intransit PACK COMPRESSOR OUTLET TEMPERATURE VALVE VaWve not closed | — es onirol pasition with control position Valve not closed, disagree B Valve fuly closed, disagresZONE CONTROLLER CABIN FAN FAULT INDICATION FAULTINDICATION No indication: normal operation, Appears ifa fault ina [cabin re-circulation fault fans detected Zone controller Primary zone controler fault ZONE TEMPERATURE ZONE DUCT This indication is green TEMPERATURE Normally green, becomes amber wen above limits HOT AIR PRESSURE REGULATING VALVE Valve not closed, disagree with control position. ZONE TRIM AIR VALVE POSITION Normally green, becomes ‘amber when the valve Falls Valve fuly closed and pb at AUTO > = Coid- vale fully closed H= Hot -valve ful open. ‘Valve tuly closed, disagree with control position J SaCARGO COMPARTMENT TEMPERATURE This indication is green ZONE INDICATION This indication is white DUCTINLET ‘TEMPERATURE Normally green Becomes amber when above limits Select any yellow button Te INLETISOLATION VALVE — TRIM AIR VALVE This indication is green Cold - vate closed Hot - valve open OUTLETISOLATION VALVE Valve open. aoYouhav AIR COr indications, |ZG aesThe sw, spring loaded to neutral, controls the outflow valve position ‘and the vertical speed Swnich UP. moves the vaive to the open position. CT ey Cty COR oa ae rr cy cy ‘Switch DN: moves the valve to the closed position. In AUTO made, the outflow valve is controlled by one system. Both automatic systems are faulty. ese cae wae) AIRBUS Coy 3 |e rr cd aa AUTO position: the pressurization system uses the FMGS data to build an optimized pressure schedule ‘Other positions: instead of using the FMGS, the pressurization schedule uses the selected value for landing elevation, ‘The system operates normally, Closure of + The outflow valve, + The emergency ram air inlet, + The avionics ventilation inet, and extract valves, + The pack flow contol valves and, + The FWD cargo outlet isol vave.LDG ELEV AUTOIMAN The landing elevation is provided by the FMGS, and Is based upon elevation of destination airport. The LOG ELEV selis in AUTO. fo | ‘The landing elevation is, ‘manually selected and allows auto pressurization when FMGS information is not available. The LDG ELEV sel isnotin AUTO CABIN DIFFERENTIAL PRESSURE Cabin differential pressure in nocral range Cabin differential pressure out of normal range. The value pulses in green for advisory Exe on Select any yellow button for review. LANDING ELEVATION Can be automatically selected by the FMGS or manually selected by the pilot CABIN ALTITUDE Cabin alitude in normal range. Cabin altitude above lit. ‘The value puises in green before tuming red (advisory) Cabin vertical [Cabin vertical speed in normal speed out of normal range range. The value pulses in green for advisoryACTIVE SYSTEM INDICATION ee The MODE SEL sw isin MAN position PACK INDICATION Select any yellow button for review. (OUTFLOW VALVE POSITION The valve is operating normally SAFETY VALVEPOSITION | Both safety valves are fully closed Atleast one of the safety valves is not closed, The vane is fully ‘open in fight.CN eee CON You have reviewed al the PRESSURIZATION controls and indications, Have some fun with the quiz!Select any yellow button for review. VENTILATION Ce ame Le ci | A u T ° ‘AUTO position CLOSED CRCUT configuation ‘AUTO position yy OPEN CIRCUIT configuration: + On the ground at T.0 power or The inlet and outlet valves open, Bon the ground, in fight and, the fan and the ground cooling HS Thrustlevers not at TO power __* Skintemperature below a unt start automatically wth E a speciied value +The AIC on the ground, + /Skan temperature abovea_ INTERMEDIATE configuration: + Both engines stopped specified vale + On the ground at 7.0 power or and, in fight and, + High temperature of + Skin temperature above a Avionics venation ai. OVD position Cee FAULT position’ A failure is detected: ‘In the ground cooling ry When etther pb sw is in the OVRD position, the system is in CLOSED. ft] configuration and adds air from the air conditioning system (with the blower in [eiise} Jp4 OVRD position, its fan stops). it Wen bop switches ae inte OVRD poston, a fos ram the ir aac cenaitonng sytem and ten overboard. One extattan continues to pT run The sytem sn SMOKE cowigraton F) blowing pressure is ow, F) computer problem or, stops, the valves close and $1 duct overheat, Hj smoke warming is activated, the fan st © computer problem or, a nee ‘smoke warning is acivated. GAIRBUS © VENTWATO!button for review. PCr VENT INDICATION Normal cispiy. DE ei ™ Blower fat + Exract faut or, “ AVNCS SYS. faut. INLET VALVE POSITION The INLET vale admits outside airinto the Valve position Vale position disagree disagree. INLET AND EXTRACT INDICATIONS Normally white. ‘The corresponding indication tus ‘amber in case of blower fault or extract fault Vai fuly closed Valve fully open. Vat position Valve partially open. p ps unknown,yellow button for review. PoC GND COOL INDICATION Nommal display. The inlet or the outlet valve is not fully closed when at least one engine is runing or in 7 flight ent INLETIOUTLET VALVES POSITION.| You have reviewed all the VENTILATION controls and indications,7 Ve TsO ee ede enThis is a pb sw, used for togating between speed (SPD) and Mach number (MACH) indications (Ret ‘SPDIMACH INDICATIONS) This sel knob has three functions: Display of the speed or Mach selected by the crew. + To change the crew selected speed when tuned, + To activate the crew selected speed when pulled, and, + To retunto managed speed when pushed. Solact any yellow button for review.Displays the heading or track selected This sel knob has three functions Pushed to: by the crew, + To change the crew selected + Display or hide the Flight heading or track when tuned, Path Vector (bird) on the + To activate the crew selected PFD, heading or track when pulled, and, Toggle between FD + To retun to the managed lateral crossbars referenced to fight plan when pushes aircraft attitude symbol and Fight Path Director referenced to the FPV, “Toggle between HDG- WIS reference targets and TRKFPA reference targets in the HOGITRK and V/S-FPA windows Select any yellow button for reviow.The altitude window akways shows the This Sel knob has three functions This pb is used for the display of the atitude set by the crew selected and actual atitudes, in meters, + To change the crew selected ‘onthe Primaty Flight Displays (PFDs). attitude when tuned, + To distegard the verical profile ‘nin pulled, and, + To retum to the vertical profile when pushed ‘The outer ring enables to select altitude increments either of 100 or 1000 ft per click Select any yollow button for review. AIRBUS © AUTOFLIGHT- Controls & Indications,Here again, the VIS-FPA sal Displays VIS or FPA, knob has three functions: Selected VS + Turned, to change the VIS cr FPA, * Pushed, an immediate Selected FPA level offis ordered, and, + Pulled, to select a VIS or anFPA a | Sotec any yoloy buiton forrviewThe LOG pb is used for intercepting and trackang the localzer independently of the glide. The EXPED pb allows you to clear a Specified altitude or to match a constraint In cimb, the — target speediMach will be green dot, in ‘descent 80/340. When selected, green lights are displayed on the pb. ‘The APPR pb enabies the inlercepfion and tracking of an ILS. t also allows a NON PRECISION APPR ta be followed in MANAGED NAV. Solect any yellow button for review.Engages or disengages autopilot ‘Arms, activates or disconnects the auto, functions. Comes on green when the thrust, Comes on green ifthe ATHR is AP is engaged. ‘aimed or active. Solect any yellow button for review.Used for switching the FD on or of Used for the display of the related information on the ND. Solect any yellow button for review.SCREEN (DISPLAY) ‘The screen is used for the display of various paces accessible through the function keys. It comprises A itle fine, where the name of the age is shown, Six pails of labeldata lines, A scratchpad line used to enter data in the FMGCs orto display messages {fom the same FMGCs LINE SELECTKEYS Six keys, called Line Select Keys abbreviated LSK, are located on both sides of the screen ANNUNCIATORS: HB FM?" Fotied on means that FM has failed [EN 2" trotted on means that FM2 has failed ig ND tgtted on means tat the on side FM detects an independent mode of operation, ROY" lighted on means that BB iicou has nrished its power up testaterits BRT knob was tumed to ON BRIGHTNESS KNOB The brightness knob is used for increasing or decreasing the brightness. This knob is also used for switching the MCDU off any yellow button for review. eaFUNCTION KEYS INT A allows the fight plan to be initialized and the IRS to be aligned. INIT_B allows the flight crew to initialize the ZFW and ZFWCG and to do the fuel planning before engines are started FUEL PRED shows the fuel prediction for the fight and is also used for entering fuel data once the engines are started F-PLN page A displays the time, speed and alitude predictions at each ‘waypoint ofthe active F-PLN. F-PLN page B shows the wind forecast and estimated fuel on board for each waypoint of the F-PLN. Both pages also display the distance, beanng and tack between these waypoints, DIR to page allows the modification of the F-PLN by creating a direct leg from the current AIC position to the selected waypoint ATC COMM: refer to FANS course any yellow button for review. FUNCTION KEYS DATA calls a group of monitor pages such {5 position monitor, IRS and GPS monitor. It also calls a set of reference pages allowing the interrogation af the NAV database PERF pages allow the crew to optimize the SPDIMACH targets for each phase of fiat PROG pages enable the crew to monitor the progress of the flight, to crosscheckiupdate the FM position, to alter the CRZ FL of the aircraft. RAD NAV displays the tadio_navaids curently autotuned by the system. ft also allows the pilot to salact other navaids. SEC F-PLNallows the creation, intialization and modification of a secondary fight plan AIRPORT allows the crew, on F-PLN page ‘A. to switch between the destination airport, alierate aiport and origin alrport SweLEFT ANNUNCIATORS FAIL" lighted on means that the MCDU has failed the MCDU to display penpherals This light tells the pilot trat the FM has an important message to deliver. i Comes on while the crew is using ALPHA-NUMERICAL KEYBOARD These keys are used for writing data in the FMGGs via the scratchpad | RIGHT ANNUNCIATOR Indicates thatthe pilot should call up a peripheral inked to the MCDU (such as ACARS or CFDS), ADDITIONAL FUNCTION KEYS. CLR allows deta, in the scratchoad (messages or inserted data) or within certain displayed pages, to be cleared OVEY (overty) allows a selected ‘waypoint to be overtiown Lea‘The ATHR can only work when the thrust levers are set forward of the IDLE detent up CL wah bol saan coercive arct to MCT, in case of single engine operation. ‘Away totum the ATHR OFF is to press ‘either one of the two THR instinctive disconnect pushbuttons located on the thrust levers.You have reviewed all the AUTOFLIGHT controls.by V) 512109Displays the standby frequency. Exchanges the active and standby frequencies, and sets the new active frequency. for ‘Shows the active frequency of the solectad radio. Selects the STBY frequency. Solacts the radio fo tune, The selected key comes on green. ‘When a radio normally releted to an RMP is tuned by another RMP, the SEL light comes on. ‘while on both RMPS. Controls the RMP power supply. Select any yellow button for review.respective channel is selected and the knob ‘comes on. INT: communication between cockpit crew members and ground personnel Neutral disconnects microphones from transmission. Reception is osmal, RAD: Connects boom or oxygen ‘mask microphones to the facility ‘selected on the ACP by pressing ‘and holding in the RAD position. Note: the sw is spring loaded from the RAD to the neutral position ‘Allows suppression of navigation ident signals (VORADF) (ON ight comes on green when pushed. Used to select the reception channel and adjust the related audio levels. When released out, the Tight Pen) VC f Bi re VOC Pushing the key selects the related channel for transmission and the three green lights come on. ‘The channel is deselected by pushing the key again or selecting another channel. Select any yellow button for review. Used for PA ‘announcement via ‘boom, oxygen or hand mike, Itmust be pressed ‘and held to use the PAsystem, Extinguishes the amber ight inthe CALL, MECH, and ATT transmission keys. LV] -] =] 0 Mero Set‘When the MECH pb is pressed, When one of the cabin call pushbuttons is pressed, a light comes on, and a horn a“CAPTAIN CALL’ message appears atthe ‘sounds to alert the ground appropriate cabin station, and a highfiow chime ‘mechanic. ‘sounds inthe cabin. When the emergency pb sw is selected on, the ON ght flashes white, and the CALL light flashes amber. ‘An “emergency call” message appears on all fight attendant panels, and three high/low chimes sound through all cabin loudspeakers. ‘fan emergency calls inated from the cabin, he ON light flashes white, the CALL light flashes amber, and three long buzzers sound in the cockot. ‘Select any yellow button for review. ‘SAIRBUS “COMMUNICATION:Prior to starfing the engine, the CVR can be selected ON by pressing this pb ‘The CVR ERASE pb enables the complete ‘erasure of he disk when the aircraft is on the (ground, wit the parking brake ON. RCDR CE [ae Rico ‘The CVR TEST pb, when pressed and held until tone is heard, allows the crew to fest the CVR. ifthe system and the parkang brake are on. ‘When pressed for 2 seconds, the CVR ERASE pb enables. the complete erasure of the memory if ‘he aircraft is on the ground, ‘the partang brake is on, and ‘Select any yellow button for review. ‘the GND CTL pb is switched on, S AIRBUSa FOOOOC es Oe) rc VOOOOOC ‘You have reviewed all the COMMUNICATIONS indications and controlsBAT1 AND 2 INDICATION a When switched OFF For the parameters and the boxtitle, see the general rule R11 AND ZINDICATION For the parameters and the box tile, see the general ule GEN 1 AND 2 INDICATION a EXT PWR INDICATION amber when eave engine pe 7 when not available. Gea] 80x cisplayed when fea] 2valable. For the parameters and the . box title, see the general rule For the parameters and the “GEN Indication, see the general rule Engine running and parameters in notmal range GEN in amber when ANE switched OFF GENERAL RULE For the folowing components BAT, TR, GEN, APU GEN, STATINV and EXT NR, a sneral rule can be applied: -aparameterbecomes amber hen tsvaueis outotrange: ERs is accompanies by te boriteaspayedin amoer: RN *allthe units are displayed in cyan Ey TeBATTERY CONNECTION LINES In green when the battery is connected, HH othervise, not cisoayes HEB charging current > 1.4 HEB Discharge curren 1.0 Select any yellow button for review. CONNECTION LINES Green ine when two ‘components ate connected, HE otrcrise not islayed BUS BAR INDICATION Normally displayed in green. APU GEN INDICATION "APU MASTER sw OFF white “APU GEN’ indication Inamber when not supplied *APU MASTER sw ON: Note: DC BATin amber when voltage < 25 V. ‘An amber “SHED” indication parameters in normal range. appears when AC or DC SHED ESS BUS is off ‘APU GEN pb sw OFF: amber “APU GEN’and white OFF ~ APU GEN pb sw ON For the parameters, see the general ule.‘Select any ye ESS TRINDICATION Parameters not displayed Ball» normal configuration (ESS TR contactor open). ‘When in use, same logic as for the TR 1 and 2 indications IDG INDICATION a 4” or *2" indication in amber: " relative engine not runing, otherwise Fanaa white eer +1DG" in amber if oll outlettemp. > 1 cillow press, IDG disconnected. Otherwise white GALLEY SHED INDICATION inwhite BREEREIEA ot oieriemperature Fe PSY 2% OFF or if galeys are eee ert automatically shed, +advisory between 147°C and 185°C. storing a loss of one camber if> 184° C. generator EB pears wnan 06 aiscomected || Not displayed in normal Wana {1222S hen10G low pressure configuration. and relative engine running ‘normally green, Engine running and parameters in normal range. eyo EMER GEN INDICATION Parameters not isplayed in nomal configuration EE When in use For the parameters and the box ttle, see the general rue. STATIC INVERTER INDICATION Not displayed in rnoxmal configuration. ig BERNA] Appear ony curing talic inverter test Eun For the parameters, see the general rule.BAT‘ AND 2 INDICATION Each battery voltage is indicated in white The battery voltag= indications are LCDs and are wired directy to the batteries. Note: The minimum eequied baton vokage i 25 51 sy Each BAT pb sw controis its related battery. a battery. The battery is OFF Select any yelion button for review. eaTianozPesws | ‘The related Battery Charge Limiter (BCL) automatically controls the connectionidisconnection of the corresponding ‘When the charging current increases at an abnormal rateEXT PWRPB SW The EXT PWR pb sw controls the external ower source No external power is connected or the parameters are out ofthe normal range. Extemal power is connected and available The parameters are in the normal range. External power is supplying the electrical system, GEN 1 AND 2, APU PB SWs ‘The GEN pb switches control the related generators. The related generator is managed by the system. The related generator is fauly The related generator is OFF. Select any yelion button for review.BUS TIE PB SW ‘The BUS TIE pb sw enables the crew to isolate one side of he system fram the other. The system automatically manages the different power sources Both sides are isolated, | caLLey pe sw The load of any generator is above 100% of rated output ‘The galley supply is OFF. The GALLEY pb sw controls the galley supply. ‘The galley supply is managed by the system Select any yellow button for review. IDG from its drive shaft ACESS FEED PB SW ‘The AC ESS FEED pb sw enables the crew to switch the supply af AG ESS BUS from AC BUS 1 to AC BUS 2 ACESS BUS is supplied from AC BUS 1. When AC ESS BUS is not supplied. ACESS BUS is supplied from AC BUS 2 |. 0c 4 AND 2 GUARDED PB swe “The IDG guarded pb switches enables the crew to disconnect an ‘The related IDG is connected to its drive shal ‘The FAULT light comes on in case of IDG oil overheat or IDG oil low pressure. ‘CAUTION Press the IDG pb sw until the GEN FAULT light comes on but not more than 3 seconds to avoid damage to the disengage solenoid Fa Frm >The GEN 1 LINE pb comes ‘on when smoke is detected in the avionies bay, ra | Comes onredin case of emergency ‘generator maifunction OFF postion enables the crew toisolate generator 1 curing a ‘smoke dil. Generator 1's disconnected from the system. Saray Cod Pe Ceo) EJ ‘The EMER GEN TEST guarded pb is In AUTO position, the RAT Is, mainly operated by maintenance crew to automatically extended by the system in test ine emergency generator. case of emergency electrical supply cconaitions When pressed, the RAT extension is ‘manually selected and the emergency generator is coupled to the circuit ifthe gear is up.satay Cog tal Ce!CABIN SYSTEMS CONTROLS & ale oe SAIRBUS © CABINS! >FORWARD AND AFT DOORS Indicates the status of the door. Used when operating the door. Used to aim and disarm the evacuation device ‘Near this window, there are two warning indicators: *+ One indicator illuminates ‘white when the slide is armed and the door handle moved up, Has to be pushed to unlock the + One indicator flashes red in door from its open positon. case of cabin pressunzation when both engines are off and the door is disarmed Inwich the emergency opening cylinder and the pressure gage are a Used fo open and clase the door. ‘An evacuation device is stowed in a container on the lower part of the door. Select any yellow button for review. CoN) Te Meters ee ee "ae eeOVERWING EMERGENCY EXITS Acoverfiap protects the Opening instructions are placarded control handle onthe ext frame. Aside armed indication illuminates \hite when the cover fap is removed, Select any yellow button for review. CFV ieee on een easHANDSET KEYBOARD ‘The emergency call pb is used to call the cockpit in case of an ‘emergency situation. ‘The reset pb is used to reset a call ‘The captain cal pb is used for normal calls from cabin 0 cockpit. Select any yellow button for review. Ces Eur eectEVAC PANEL EVAC Dee Grd ye Cer) ‘The evacuation command ‘can be activated from the cockpit only Used to switch on the evacuation ‘command system. ‘The evacuation command can be activated trom either the purser station, orthe Used to shut of the evacuation hom ee inthe cockpit. Select any yellow button for review. Coy V1 s1 0 Meer EEN eee a cre aFORWARD AND OVERWING HANDSET AFT DOORS EMERGENCY EXITS KEYBOARD om ty EVAC PANEL You have reviewed the main cabin controls. Have some fun with the quiz !FIRE Panel New) Discharges the related fire extinguisher Enables fire detection and bottle when pushed. ‘Normally in and guarded. ‘extinguishing system to be tested. Notactive, as long as the FIRE ‘When pressed, indications Rahes RST ‘Gomes on red independently of canbe checked on the FIRE the pb postion as long as the panel (FIRE pb, SQUIB and respective engine fre warning is DISCH ight) and, f AC power activated, available, on the MASTER The related extinguisher botte is ‘WARN ight and the ECAM. ready to be activated. ‘When released out + Aural waming is canceled, + Squibs are armed, n the re extinguisher + Fuel, hydraulic, air bleed and botle is depressurized Fee ee anesare cies Note: this action is raversible eae review AIRBUS “FIRE PROTECTION - Controls & indications [SeCARGO SMOKE Panel eT elt © Select any yellow button for review. LFV) 120 Mea aha tO se eet ‘When pressed, the fire agent is. discharged in the respective ‘compartment (FWD or AFT). Enables smoke detection and ‘extinguishing system to be tested. When pressed for at least 3 seconds, Unt tis released indications can be checked on the ECAM and on the CARGO SMOKE panel red SMOKE lights come on twice and DISCH lights come on amber) Not: the CARGO VENT ISOLATION. VALVES wil lose, Te)S AIRBUS ENG Panel Re Eee eis. Py Py Identifies the engine to be shut down, FIRE PROTECTION Select any yollow button for review. Ae ew MS Fen >S AIRBUS EXTERNAL POWER Panel ( \When pressed, in the event of an APU fire, the automatic shutdown is confirmed and the extemal hom willbe silenced. aon eae eee tar | ‘Comes on red in case of APU fire. Select any yollow button for review. eaEMER ELEC PWR Panel ee seno eh aor) Ce eto Indicates detection of smoke in. the avionees bay, Generator is disconnected from all electrical buses. itremains running and supplies one fuel pump in each wing tank. Select any yollow button for review. EW eae neeVENTILATION Panel VENTILATION Cem Ls) Both FAULT lights come on amber ‘along with ECAM warning when ‘smoke is defected in the avionics ventilation duct. Select any yollow button for review. Te CF) )=(0 Me aa ah ea ec tar |FIRE Panel ‘You have reviewed allthe contro's ‘and indications conceming the FIRE PROTECTION chapter EXTERN \L POWER Panel era C CARGO SMOKE Panel Cod Some BLOWER EXTRACT GND.COOL_ | CABF 0 rT i i Q 8 S AIRBUSQ =} j ry ES nN r)ares ae ee a ___SPOLERINDICATION | BE Sepgnsstymeteitan SPO BRK ais dergees i Retracted Ey Fawronencerectes The movements are ‘symbolized by @ aren index a Faulty when retracted or moving infront of a white inhibited scale ‘The index becomes amber in case of failure of both hydraulic actuators or loss of related computers. Neutral position in clean configuration. Normally displayed in green. Rudder symbol and scale become amber in case of low pressure in all Neutral position when flaps are hydraulic circus. extended and there is a 5 degree aileron drop. Rudder travel iriters at high speed are indicated by while dashes on the rudder scale.Normally in green ea Becomes amberin case of computer failure, switched OFF orboth FCDCs failed. Cena GEN "ormaty in white Becomes amber it Asean Becomes amber in case of failure of both hydraulic actuators. Be HE 72) inven a Normally blue Becomes amber if rudder trim reset has failedNormally in green Becomes amber in case of actuator failure (hydraulic ce | low pressure, jamming). e ox i Identical to rudder hydraulic indication a iw na Becomes amber in case of hycraulic low pressure. Select any yellow button for review.Identical tothe ECAM F/CTL page. ‘Select the yellow button for review.Select any yellow button for review. *S" and "F” appear: Normally in white, In amber in case of loss of both hydraulic systems or slats or flaps fault Replaces *F* if WIB is applied to flaps. Replaces “S' if WTB is, applied to slats. Replaces *S" when alpha/speed lock function is activated *S" and*F" nat displayed in clean configuration. "0," "14F",°2',°3 or FULL” appears: White dots indicate selectable positions. Not displayed in clean configuration Cyan indicate selected position position is reached. ‘0"is, not displayed in clean Green indicate current configuration. position Incyan during tansi Ee Inamber in case of loss of, both hydraulic systems, WTB application or sats or flaps fault. 7S == LaeRed barber pole scale indicates Green bars indicate Fi High speed protection Le) =. Lae ‘The top of the amber barber pole scale indicates Alpha prot speed The top of the red solid scale indicates Alpha max speed Select any yellow button for review.‘An amber “A FLOOR’ indication on the PFD and on the EWD indicate that the Alpha floor protection is active and has automatically set maximum power on the autothrust.Double green dasives on each side of the bank angle sscale indicate the bank angle protection imi. Double amber crosses indicate that the pratecton HEM Smnatlgreencesnes on Eee the PFD pitch scale Indicate the pitch atitude protection limits Double amber crosses Indicate that the protection is lost _ zs = weThe four white comers on the PFD show the max side stick deflection. (On the ground, the white cross on the PED indicates the combined First Officer Captain side stick deflection, Note: does NOT indicate suraces defection CLL | LL =. LS Lecal‘The red take-over pb sw allows a pilot to disconnect the autopilot of, by pressing and holding it more than 40 s, to deactivate the opposite side stick and obtain ful control ‘To recover control, a pilot simply has to momentafly press his take-over pb sw Inthe A220 family the side sticks allow the pilots to achieve martal roll and pitch control They are springoeded to neutral and receive no feedback from the fight controls. Select any yellow button for review.RUDDER PEDALS RUDDER PEDAL ADJUSTER The rudder ped: ‘manual yaw control. The udder pedals remain stationary regardless of any autopilot input allow The rudder pedal adjuster is used to adjust the position ofthe rudder pedals Select any yellow button for review 7 : = Sale‘Select the yellow button for review. ‘The rudder PEDALS DISC button on the nase wheel Sieering handle enables the rudder pedal movements to be cisconnected from the nose wheel steeringSPEED BRAKE LEVER } ‘The speed brake lever authorizes the pilot: * To arm the ground spoilers by pulling onitand + To control the speed brakes position by pushing and mowing the lever to the required position WHITE BAND. ‘A mihite band appearing around the base of the speed brake lever indicates that the ground spoilers are armed [saeco nostro | : _ as easDisplays the current rudder tim ra RETRACT Co Control the operation ofthe left and right Janding lights ‘The ON position causes the extension of the associated light which comes on automatically when fully extended, ‘The OFF position causes the associated light to go off but remain extended. ‘The RETRACT position tums off and retracts the associated light. ‘Select any yellow button for reviow. a ni a 7 VU eee tae edSIGNS panel When the EMER EXIT LT sels inthe OFF position, he OFF EMERGENCY EXIT LT is amber. ‘When moved from ON to OFF or ‘OFF to ON position, ‘NO ‘SMOKING? and “EXIT signs inthe ‘cabin go off of come on and alow tone sounds. ‘The AUTO position causes the *NO SMOKING” and "EXIT" signs to come on when the landing gear is extended and to go aff when the ‘gears retracted ee ON pn ee ure e * on (Oe oFF cere When moved from ON to OFF or the ON poston, emergency OFF to ON position, FASTEN igtting comes on. SEAT BELT signs in the cabin and “RETURN TO SEAT’ signs in the. Perea es escape lavatones go off or come on anda ng EXT sigs and overnend low tone sounds, ‘emergency lighting automaticaly come ‘onthe normal electrical system is lost Inthe OFF position, emergency lighting willbe oft Select any yellow button for review 7 VU eee tae edSEAT BELTS AND NO SMOKING MEMO MESSAGE MEMO messages When the ‘SEAT BELTS" signs are ON or when the ‘NO SMOKING" signs are ON, a related memo message appears on the E/WD. STROBE LT OFF MEMO MESSAGE LDGLTMEMO MESSAGE Ifthe strobe Ights are OFF in fight When the lancing lights are the STROBE LT OFF memo message extended, the LDG LT memo v0. message Is displayed in green on the ENVD. is displayed in green on the fect any yellow but ZS LowaREADING LT panel INT LT panel EXT LT panel enero ye MAIN PANEL INSTR AND PEDESTAL LIGHTIN panel Perrone a Module complete 7 Vil siUyFee ue |svsseknos | seLavs Presents the data corresponding to OFF: display off 1.2.3: system selected for data See eco eer is amuy selector knob positions DATA SEL KNOB Selects the information to be displayed in the display: sts status and ‘information for abnoxmal situations, EVERETT WIND ‘true wind ‘Can be used for data entry such as direction and speed, present position or heading in ATT mode. HOG true heading and minutes remaining before alignment is complete, PPOs present latitude and ONBATLIGHT longitude, ‘Comes on amber when at least one IR THIS true track and ts supplied by the battenes only. talso {ground speed, ‘come on fora few seconds att the beginning of the alignment. TEST tests the display. Select any yellow button for reviow. Teil Re dello ek enn Mae wadSteady when a fault has been detected Flashing if atitude and heading information may be recovered in ATT mode Steady when the IR is aligning, Flashing i “IR alignment faut or, + difference between position at shut down and entered position exceeds 10 of latitude or longitude, ‘no position entry after 10 min. ADIRU nol energized No data availabe. LJ] NAV ‘Normal position Supplies ful inertia data. ATT IR supplies only attitude and heading information. (In case Been oe a Air Date ouput ciscomecied Se ree AIRBUS © NAVIGATION= Controls & indications cn)Receiver 1 data is displayed on the left hand side and rece'ver 2 data on the right hand side White color is reserved for VOR information while green is for ADF. The following data is displayed smal picture of the associated pointer, 4st line: sselecied nav aid 2nd ine: snay aid identifier. 31d kine: “DME distance. ‘nothing if automaticaly tuned by FMGC Ifa VOR does not have DME, the DME indication is replaced by green dashes. ADFS are shown as green pointers while VORs are white pointers. Select any yellow button for reviow _ ZS = Dawe‘Selects a navigation display for the Selects the range scale forthe onside: onside ND. ND. eu a a oF (Outer ting for unit selection (in Hg or Pa). {nner ring for value selecton. Select ADF or VOR pointer for the Puling the knob gives the reference onside ND, exceptin PLAN mode. setting (STD). Turning itthen has no effect. Pushing it from STD recals the last QNH selection Select any yellow button for reviow.MCDU RAD NAV PAGE Navaids autotuned by the FMGS. Navaids manually tuned on the RMP. Solect any yellow button for reviow. SlewsteyMy —————_ co Navaids automatically tuned. Navigation stand-by mode engaged. Navaid tuning is no longer available from the MCDUs. Nate: when an RMP ic used te tune an ILS/DME, the PFDs do not ‘splay tho DME cistanco, ‘Show the active and stand-by frequencies, or the course. Ifthe STBY/CRS window is displaying a Course, then depressing the transfer key displays the active frequency in both windows. ‘Two concentric knobs controt the display in the STBY/CRS window. ‘The course setting is done through the imer knob only. Select any yellow button for reviow.Indicate the DME distance or dashes ifan ADF, ora VOR without DME, is Indicate the magnetic bearing ta selected the station received by VOR orland ADF receivers. Positioned according to ADIRU 1 heading infomation. Select VOR 1 of ADF 1 forthe dashed pointer and VOR 2 or ADF 2 for the double pointer. Select any yellow button for reviow.Heading signal from ADIRU 4 not val. Signal fom VOR 2 or ADF 2 receiver invalid, The fauty system is incicated by the sel position (here ADF 2). ‘Signal from VOR 1 or ADF 4 receiver invalid. The faulty system is indicated by the sel position (here VOR 1). | Solect any yellow button for reviow.(ram uaa ea Radio height above the around, in feet. Displayed from 0 to 2500 ft Select any yellow button for reviow.GPWS SYS fault Inhibits “TOO LOW FLAPS" waring in case of landing in CONF 3. GPWS SYS off. Aline messages are inhibited, ary coy ry Che eeu eee Inhibits the Terrain Awareness Inhibits the "Gide Slope" warnings Inhibits flap wamings in case of a Display (TAD) and Terrain landing with a reduced ap setting Clearance Floor (TCF) modes, and (following a failure). does net affect the basic GPWS modes 1105 Select any yellow button for reviow.GPWS GISPB Comes on when a warning is acivated, assocated with a speaiic voice warming, Associated with glide siope alerts Pressing this pb sw during such an aller stops the aural waming and switches off the pb sw. Note: pressing this pb sw continually in fight or on «gound launches atest sequence of either some or all ura and cual varings LOUDSPEAKERS Give the GPWS aural warnings even iftumed off. Select any yellow button for reviowThese memos appear to remind the crew ofthe inhibition of some flaps warnings. When a landing in CONF 3 has been chosen, When a landing with a reduced flap setting is imposed after @ faire Select any yellow button for reviow SS SweThe TCAS controls are detailed in a ‘The transponder controls work ike any specific couse conventional transponder. Select any yellow button for reviow.WX Weather mode. it shows the intensity of preciprtations, 2 sia ee WX/TURB — Shows the turbulence areas in magenta in precipitation areas. ‘The radar operates in ground ‘mapping made. Adjusts the sensitivity ofthe radar receiver. Conitols the Predicive Windshear Controls the antenna tit in retain to function. the honzon. Select any yellow button for reviow.Fitted on top of the windshield centor post in a closed compartment It may be pulled down for use,‘roll scaleirol index, side sip index, ‘pitch scale, ‘pitch limit indicator, yed aircralt symbol, ‘glide scale and index, ocalzer scale and index ‘actual airspeed reference tangle, ‘mach number, in green, when greater than 0.5, “speed bugs. salltude indication, sNEG appears in white for negative altitudes, saltude bugs. eee ana Selected barometric pressire or standard pressure are displayed inbiue. Select any yellow button for reviow.Used to display, activate or inhibit the bugs function ‘The glide slope and the locabzar a bm devation scales appear when this JALT(x 100) pbis pressed Enable access fram box to al another. ‘barometric selection knob or, ‘bugs selection knob. Four speed bugs values (in knots) can be selected by the crew ‘Two speed bugs values (X 100) can be selected by the crew. Select any yellow button for reviow.You have reviewed all the navigation indications and7 Vi leiyComes on white when the cabin OXYGEN Panel ‘oxygen mask doors are activated. Inthe AUTO position, the mask doors ‘open automatically when the cabin altitude exceeds 14 000. Conirois the crew oxygen supply vale. Asstt ‘When the vale is open, low pressure ! IES ongenis suppiiedto the masks, When the guard is ited andthe pb is pressed, the mask doors also open, | egardess ofthe cabin aide ‘When in the OFF positon, the vaWe is closedBLINKER FLOWMETER Crew Oxygen Mask ‘When testing oxygen flow and Storage Box ‘onygen overpressure, the flow Indicator flashes yellow 10 indicate the oxygen is flowing. PRESS TO TEST AND RESET CONTROL This lever has two functions: + Itprovides an oxygen flow test, + retracts the OXY ON flag. This stops the mask oxygen ow and deactivates the OXY ON FLAG mask mike. This flag lets the crew know that the oxygen supply vaive is open and the mike Is energized. Note: to got back the normal interphone reset the oxygen system ‘Select any yellow button for review. RELEASE LEVERS Enable the pilot to exact the oxygen mask from its container by pressing the levers and pulling out Italso inflates the hamess. SUPPLY SEL Enables the pilot io select cither 100% or diluted ‘oxygen tothe mask EMERGENCY PRESSURE SEL ‘Supplies oxygen at @ continuous pressure (overpressure) to the masks. 5-7 SSEECAM DOOR Page range. notmalin al cases, (Oxygen low pressure is detected, orthe OXYGEN GSE Pressure CREW SUPPLY pb swis abnormally ow. Cal OFF, maintenance Gi, Anamber tale appears 2s an alert tothe REGULLOPR ieee pital the oxygen ‘quantity ts below 1500 psi Appears only when a low pressure is detected in he circuit to the mask. ct any yellow button for review. / me SweECAM DOOR Page range. notmalin al cases, (Oxygen low pressure is detected, orthe OXYGEN GSE Pressure CREW SUPPLY pb swis abnormally ow. Cal OFF, maintenance Gi, Anamber tale appears 2s an alert tothe REGULLOPR ieee pital the oxygen ‘quantity ts below 1500 psi Appears only when a low pressure is detected in he circuit to the mask. ct any yellow button for review. / me SweOXYGEN Panel Crew Oxygen Mask Storage Box XYGEN controls and indications.AIR COND panel ENG BLEED PB SW ‘The ENG BLEED pushbuttons are in the ighis out position, meaning that the ENG BLEED valves are aulomalically controlled ‘The ENG BLEED vaves and HP valves are closed, Afailure has been detected inthe ENG BLEED system (associated with an ECAM caution) APU BLEED PB SW ‘The APU BLEED pb swis inthe lights out position, meaning thatthe APU BLEED vale is closed, APU BLEED valve is open An APU leak is detected The APU BLEED valve closes Select any yellow button for review. X BLEED SEL ‘The X BLEED selector isin the AUTO Position meaning that the X BLEED valve ts automatically cortrolied I yell The X BLEED valve is Se entire ererl ‘Tne X BLEED valve is manually closedAPU BLEED VALVE ‘The APU BLEED vale is indicated provided the APU MASTER SWis ON ‘The APU BLEED vate i nal fly open. The APU BLEED vabve i 7) fully open (APU BLEED ‘memo also appears on the EMD) ENG BLEED VALVES BLEED valve open BLEED valve fuly closed BLEED valve disagree in ‘open position. BLEED valve disagree in losed position Baws ECAM BLEED page (1/2) X BLEED VALVE wi X BLEED valve is normally closed [BE «BLEED vane is normally = open mz X BLEED vave is in transit. X BLEED valve disagree in iosed position X BLEED vane disaaree in ‘open position HP VALVES The HP valves are controlled automatically HP valve not ful closed. > ee HP valve disagree in closed Postion. Soleo‘The GND HP connection indication is always displayed in white when the aircraft's on the ground whether the GND unit is connected or not. Itdoes NOT confirm that high pressure air is actually connected. Note: GND HP airis connected, do NOT use APU BLEED! ee Becomes amber when ‘engine N2 below idle ECAM BLEED page (2/2) The precooler inlet Es oe. eal overpressure detection The precooler outiet temperature is normally BE Sessa ee re Seen LS = DwAIR COND panel | You have reviewed all the BLEED | controis and indications. — See7a) 0 ee ae eaAPU Panel Controls the power supply of the APU and allows the start sequence to begin when the START pb swis pushed When selected OFF + The APU shuts down after a cooling period. When pressed ON + The APU ait inlet flap opens, + The ECAM APU page is, displayed FAULT light comes on when an auiomalic or an emergency shut down occurs. Select any yellow button for review. When pressed ON, the APU starting sequence Is initiated. ‘The AVAIL light comes on green meaning that the APU 's available to supply elecincal ower andlor bleed air Note: During the APU shutdown sequence (including 2 cool dow paid), the AVAIL light erains on During tis cool dowm period, you can stop the shutdown sequence by pressing the MASTER SW po beck to ON presides AVAIL i stil displayedECAM APU Page (1/2) Displayed in green, The APU is available to These indications give supply electrical power information on the APU andlor bleed air. generator parameters. For more details, please see the ATA 24 ELECTRICAL chapter. Valve is open. Valve s fully closed Valve fuly closed if APU bleed ON, Displays the available bleed air pressure in green. ‘Select any yellow button for review.APU N INDICATION Displayed in green when the APU peed is normal Amber or dif out oflimits APU EGTINDICATION Displayed in ‘green at normal operating temperatures. Amber of red when out of mits. Note: The red range varies dung start cr ECAM APU Page (2/2) er aac Select any yellow button for review FUEL LO PR INDICATION Displayed in amber when an APU fuel low pressure i detected. Noe: Eventhough thi in amber. tig an adisoy FLAP OPEN INDICATION Displayed in green when the APU air inlet flap is, fully open LOW OIL LEVEL INDICATION Advisory displayed when ri caida an APU oll low quantity is ES ccteccc Not Minimum quantity allows normal APU operation for an sional 10 hous Wie aeAPU Panel ECAM APU Page = feEW cet T= _ ==+ When closed and locked. mora Bel -vresins Door indication appears when associated door nat locked. + Appears beside the relative door When slide armed * Otherwise not + Otherwise not displayed displayed. ‘Select any yellow button for review. ~~ SS -- DwelePerera ‘You have reviewed all the door indications Have some fun with the quizUR F Deer) en C7110 eda aSe NSE Mor) ne ON position of th 2 switches is used to aulomatically stat the engin NGMASTE eed eee Te)Enable to select REVERSE thrust from forward idle position Mowing the thrust lover back into the forward thrust area will stow the reversers, The THRUST LEVERS are used to manualy set a Thrust Lever Angle (LA), Selected TLA is the reference for FADEC computation ofthe thrust rating mit and EPR. ‘The autothrust can be disconnected by using this two red buttons. yn esoAVTHR OPERATING RANGE DETENTS ‘There are five positions defined by datenis ar AUTH operating range with Ras TOGA: _ Max TakeOf thrust (or Go Around thrust) FLX MCT: Max Continuous Thrust (orfiex takeof) cL: Max CLimb thrust 0 Idle thrust Tile veverse thrust AVTHR operating range with 2 pete ~~ FULL Max reverse thrust Note: There is no ile reverse detent Select any yellow button for review. Za stty‘Manual start is initiated, Manual start sequence is. stopped. ‘Select any yellow button for reviewFUEL USED INDICATION FUEL FILTER INDICATION The CLOG message appears amber in case of excessive pressure loss across the fuel The fuel used value is displayed ingreen tis reset to zero at engine start. The two last digits Eten are dashed i the indication is fiter inaccurate OIL FILTER INDICATION The CLOG message appears amber in case of excessive Ere eu eee pressure lass acrass the main oil Normally areen, the indication pence pulses green above 140 decrees \creasing) or 135 degrees, (decreasing) Becomes amber when above 140 degrees for more than 1 minutes ( abave 155 degrees without delay VIB INDICATION The N1 and N2 indications are normally green. N1 pulses above Band N2 pulses above 4 3 NACELLE TEMPERATURE Pulses green above 240 degrees.OIL QUANTITY INDICATION Tne oil quantity is displayed in green The indication pulses when oil quanity drops below three quarts (decreasing). OIL PRESSURE INDICATION Normally green, the indication pulses green above 90 PSI or below 16 PSI Becomes red below 13 PS! ENGINE BLEED PRESSURE Normally displayed green, tums amber below 21 psi or if overpressure, IGNITION INDICATION During start sequence, A or B is displayed in green depending on the selected igniter. In continuous ianition or manual start mode, A+B is displayed in green START VALVE POSITION Bl Valve dosed wy Valve openIDLE/AFLOOR INDICATION IDLE Is displayed green when, in flight, both engines are at ide. It flashes fist for 10 seconds, then it fays steady aA AFLOOR is displayed in amber when the function is active N1 INDICATION EGTINDICATION N2 INDICATION CHECK MESSAGE In case of discrepancy between an indication and an EGT, Nt, N2 or FF value, a CHECK is displayed y yellow button ‘THRUST LIMIT MODE TOGA, FLX, MCT, CL OR MREV elected mode is displayed in blue N1 RATING LIMIT The N1 rating limtis displayed in When FLEX is selected the corresponding temperature is displayed in blue In MREV mode, the N1 rating limit is replaced by amber crosses. FUEL FLOW INDICATION The Fuel Flow is displayed in green. DA &Limit value of N1. corresponding to the ful forward thrust lever Postion. Predicted N1 corresponding to the thrust lever position. ‘Appears and remains in red at the highest N1 attained. ‘disappears after a new start on ‘ground or after maintenance ‘action, This red arc shows the prohibited area of operation Displayed in green, it hows the difference between the actual N1 ‘and the N1 command value. Four N1 command ares join the current N1 needle to the Nt command needle ttis only displayed with ATHR, engaged, and agtaomin geen [SESH The N1 trend triangle shows When Ni value is cagraded, the the N1 direction. last digit is amber dashed Needle pulses red or amber if ‘tis onWy displayed with ATHR value is out of normal range engaged DAPredicted N1 corresponding to the thrust ever position Limit value of N1. corresponding to the ful forward thrust lever Postion. This red arc shows the prohibited area of operation, ‘Appears green when the reversers are fully deployed In fight with one reverser unlocked, itflashes amber for 9 seconds then remains steady‘Amber index appears at 725 deorees Celsius during engine start, then at 915 degrees Celsius lect any yellow button for review ‘The red line indicates the maximum value reached ‘twill only disappear after a new take off or after maintenance action. ‘The red are begins at 950 degrees Celsius and contnues tothe end of the scale. ‘Actual EGT is displayed green in analog and digital form, Their color changes amber, then red above the normal range The needle pulses in the amber or red rangeN2 digital indicator green. During a start sequence, itis displayed on a gray background ‘normaly in Ittums red witha red cross above the normal range (105%) The red cross will only disappear after a new take off or after @ maintenance action When N2 value is degraded, t digit is dashed amber.have eviewediRe ENGNE |] raband scans |