MSFS 2024 · Airliner

FlyByWire A380X Startup Checklist

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Weight & Balance
Takeoff DistanceLanding Distance

FlyByWire A380X Startup Notes

The A380X powers up on four batteries, not two: BAT 1, ESS BAT, BAT 2 and the APU battery. Ground power surprises people next, because the airplane needs at least two external units to carry the network, and FlyByWire's SOP switches them on in the order 2, 3, 1, 4 so the displays come up faster. Set all three IR selectors to NAV early; alignment runs a realistic eight minutes unless you change it on the flyPad. And the FMS has no keypad - its pages live on the MFD, driven by the KCCU trackball.

Fuel and payload are the classic trap. They load exclusively through the flyPad EFB, and the sim's own weight and balance sliders snap back within seconds, so pilots set a load that never arrives and then meet an amber INITIALIZE WEIGHT/CG on the FMS. Engine start needs the APU running with APU bleed on, and the SOP asks for a ten second pause after IGN START so the FADEC can finish its engine tests before you lift the masters one at a time. Treat the SOP's OIT and laptop pages as background reading; the terminal is still largely inoperative in this alpha.

Common mistakes

  • Loading fuel in the sim's panel instead of the flyPad EFB
  • Connecting a single ground power unit when two are the minimum
  • Lifting the engine masters inside the ten second wait after IGN START

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FlyByWire A380XMSFS 2024 · Startup Checklist · 315 steps · 20 phases
DATE PILOT TAIL
PHS 1 - Pre-Flight Planning10 steps
01Route and OFPGENERATEDNOTE: The SOP expects a company flight plan, received via ACARS or inserted manually on the OIS FLT OPS STS page.
02Departure and Destination Weather (METAR / TAF)REVIEWEDNOTE: Check runway in use, wind, ceiling, visibility, and freezing levels at origin, destination, and enroute.
03Alternate AirfieldsSELECTEDNOTE: Pick suitable alternates with adequate weather, runway length, and A380-capable parking.
04NOTAMsREVIEWEDCAUTION: The SOP calls for NOTAMs to be taken into account when computing preliminary takeoff performance, and for unavailable navaids to be deselected on the FMS POSITION/NAVAIDS page.
05Block FuelCONFIRMEDNOTE: Trip plus taxi plus contingency plus alternate plus final reserve. The SOP also has the crew check RTE RSV / FINAL and MIN FUEL AT DEST against regulation.
06MEL / CDL ItemsCHECKEDNOTE: SOP: check dispatch conditions via the Logbook status panel of the OPS Library, and verify MEL and CDL items are activated in the performance applications.
07ZFW / ZFWCGOBTAINEDCAUTION: SOP caution: some speeds on the PFD are based on ZFW and ZFWCG. If expected values are entered, the captain is responsible for inserting the actual values.
08Gross Weight CGWITHIN OPERATIONAL LIMITSNOTE: SOP: verify the ECAM GWCG is within limits using the OIS loadsheet application. If the loadsheet takeoff CG and the ECAM GWCG differ by more than 1 percent, re-check the entered values.
09SID / STAR / ApproachBRIEFEDNOTE: Review the planned departure, arrival, and approach including altitude and speed constraints.
10Preliminary Takeoff PerformanceCOMPUTEDNOTE: SOP: initialize the T.O PERF application on the OIS, obtain airfield data, insert outside conditions and aircraft configuration, then compute and review the result.
PHS 2 - Initial Power Up13 steps
01Engine Master Switches 1, 2, 3, 4OFFNOTE: Verify on the pedestal.
02Engine StarterNORM
03Both WipersOFF
04All Batteries (BAT 1, ESS BAT, BAT 2, APU BAT)ONNOTE: Verify the OFF lights extinguish when the battery buttons are pressed.
05External Power (2, 3, 1, 4)ONCAUTION: SOP: activate the external power units in the order 2 - 3 - 1 - 4, which gives a shorter display-unit start time. The aircraft needs at least two external power units to power the whole electrical network. Under high electrical load, consider a third and fourth unit, or set CABIN FANS and COOLG to OFF.
06Cockpit LightsAS REQUIREDNOTE: Set the standby compass and ANN light BRIGHT or DIM, then the pedestal flood, ambient and integ light knobs, then display unit brightness.
07Captain and First Officer LaptopsONNOTE: Slide the ON/OFF switch near the OIS to the right and hold for 2 seconds. The laptops take around 5 minutes to start.
08Backup LaptopONNOTE: On the first officer's lateral console. Needed to run the automatic data loading operations.
09Control Device and Keyboards 1 and 2 (KCCU)ON
10Onboard Information TerminalONNOTE: Turn the OIT knob to start the terminal, then adjust brightness.
11OIT Side - NSS AVNCSSELECTNOTE: Initializes the network server systems avionics. Log in as pilot as soon as possible - the NSS AVNCS connection can take a few minutes.
12OIT Side - FLT OPSSELECTNOTE: Log in as pilot, then start NAV CHARTS and OPS LIBRARY.
13Initial DataSENDNOTE: Send the initialization request to the airline ground station via the INIT Data button after checking the input and display data.
PHS 3 - Aircraft Status and APU Start13 steps
01ECAM RCLPRESSNOTE: Press and hold the RCL pushbutton on the ECAM Control Panel for at least 3 seconds to recall all previously cleared or cancelled ECAM alerts.
02Cleared or Cancelled AlertsCHECKCAUTION: Verify all alerts and make sure they are resolved before taking off.
03MEL / CDL ItemsCHECK AND NOTE CDLNOTE: Verify the ECAM recall notes and the maintenance release status via NSS AVNCS.
04Aircraft AcceptancePERFORMNOTE: Verify VHF3 Data mode is active, then sign the acceptance in the flight acceptance report. It can be signed later but must be before the end of Cockpit Preparation.
05RMP 1 and 2ON
06Standby Radio NavigationOFF
07Communication FrequenciesTUNENOTE: SOP recommendation: VHF 1 for active ATC and emergency frequencies, VHF 2 for ATIS, VHF 3 for ACARS.
08APU Fire and Engine 1-4 Fire PushbuttonsCHECK IN AND GUARDED
09APU and Engine AgentsOFF
10Fire TestPRESS AND HOLDNOTE: Verify a constant repetitive chime, the master warning flashing, ECAM ENG 1(2)(3)(4) FIRE / APU FIRE / MLG BAY FIRE messages, all fire pushbuttons red, squib and disch lights illuminated, and all engine master panel fire lights on.
11APU Master SwitchON
12APU StartONNOTE: Ensure the APU flap is fully open on the APU system display page.
13External PowerAS REQUIREDNOTE: SOP recommends keeping the external power units ON to reduce APU load in hot weather.
PHS 4 - Cockpit Preparation41 steps
01All White LightsOFFNOTE: Scan the overhead panel bottom to top, left to right. While scanning, check that the only amber lights are the GEN FAULT lights.
02RCDR GND CTLON
03EVAC CAPT / CAPT and PURSCAPTAIN
04Probe and Window HeatAUTONOTE: Only set to ON in cold weather conditions.
05All IR Mode (ADIRS)NAVCAUTION: Complete a full alignment if this is the first flight of the day, the crew has changed, GPS is not available for all segments, or long segments with low navaid coverage are expected. Ensure at least one IRS remains operative during refuelling.
06ELTARMED
07Reset Buttons (Left and Right)CHECK PUSHEDNOTE: Verify none are in the outward position.
08STROBEAUTO
09BEACONOFF
10NAVON
11Remaining Exterior LightsAS REQUIRED
12SEAT BELTSONNOTE: Set to ON once refuelling is complete.
13NO SMOKINGAUTO
14EMER EXIT LightARM
15Engine StartNORM
16APU BleedONCAUTION: Do not use APU bleed if a high pressure ground air unit is connected. Check the bleed page of the system display - pressure in the bleed system means the ground air unit is connected.
17XBLEEDAUTO
18AIR FLOWNORM
19CKPT TemperatureAS REQUIREDNOTE: SOP recommends approximately 21.5 degC.
20CABIN TemperaturePURS SELNOTE: Cabin temperature can only be controlled from the flight attendant panel.
21ELEC DC SD PageDISPLAY
22All Batteries (BAT 1, ESS BAT, BAT 2, APU BAT)OFF THEN ONNOTE: After resetting all batteries to ON, verify the current charge of each is below 60 A and decreasing.
23TRIM TK FEEDAUTO
24Maintenance Panel - All LightsOFF
25Cargo Air Cond SelectorsAS REQUIRED
26RMP 3ONNOTE: STBY RAD NAV key OFF.
27CVR TestPRESSNOTE: The test fails if the ECAM alert RECORDER CVR FAULT appears 5 seconds after the press.
28Switching SelectorsNORMNOTE: Attitude heading, air data and FMS selectors all NORM.
29ISISCHECKNOTE: Adjust brightness, then verify airspeed, barometric setting, altitude, attitude and heading.
30L/G GRVTYOFF
31ClockCHECK AND SETNOTE: Reset the elapsed time and chronometer.
32A-SKIDON
33Parking BrakeONCAUTION: Do not set the parking brake if the brakes are hot and chocks are in place - this improves brake cooling. Verify brake pressure descends to zero on the triple pressure indicator.
34Body Accumulators PressureCHECK / REINFLATENOTE: Verify the pressure is in the green band. Press ACCU REINFLATE if needed.
35Thrust LeversIDLE
36Thrust Reverser LeversSTOWED
37Engine Masters 1, 2, 3 and 4OFF
38Cockpit Door SwitchNORM
39ATC COM - Message RecordERASE ALLNOTE: Erase CPDLC messages from the previous flight to avoid confusion in the message history.
40ATC ClearanceOBTAINNOTE: Then prepare the appropriate navigation charts on the clipboard.
41SURV Default SettingsSELECTNOTE: Verify transponder AUTO, squawk correct, TCAS TA/RA and NORM, all TAWS modes ON, weather radar AUTO with elevation/tilt AUTO, Mode WX, TURB AUTO, GAIN AUTO, WX ON VD ON, and PRED W/S AUTO.
PHS 5 - FMS Initialization33 steps
01Flight Plan InitializationCOMPLETENOTE: Enter the flight number exactly as filed in the ICAO flight plan. Cost index varies with company policy.
02WindsENTERNOTE: Use the forecast wind from the computerized flight plan.
03IRS 1, 2 and 3CHECK NAV OR ALIGNNOTE: Verify on the FMS POSITION/IRS page. If GPS is unavailable or failed, set the IRS to ALIGN.
04DepartureSELECT / CHECKNOTE: Ensure the correct runway, SID and TRANS on the FMS departure page.
05NavaidsCHECKNOTE: Verify VOR, ILS and ADF tuned by the FMS on the POSITION/NAVAIDS page. Deselect any navaids shown unavailable by NOTAM.
06ZFW / ZFWCGINSERT
07Block FuelINSERTNOTE: The fuel is automatically redistributed.
08RTE RSV / FINAL and MIN FUEL AT DESTCHECK / INSERT
09Preliminary Takeoff Performance DataINSERTNOTE: On the takeoff panel of the FMS ACTIVE/PERF page.
10V1, VR and V2INSERT
11TOGA / FLEX / DERATEDSELECT / INSERT
12FlapsSELECT
13Anti-IceINSERT
14Thrust Reduction / Acceleration AltitudeSET OR CHECK
15Noise ProcedureACKNOWLEDGE
16Transition AltitudeAS APPROPRIATE
17EO ACCEL AltitudeSET OR CHECK
18Derated ClimbINSERT AS APPROPRIATE
19Preselected SpeedsAS REQUIRED
20Active Flight PlanCHECK AND COMPLETENOTE: Verify waypoints, routes, departure, arrival, and vertical climb speed limits or constraints. Verify the total distance is similar to the computerized flight plan.
21Secondary Flight PlanAS APPROPRIATENOTE: Used to anticipate a runway change, an immediate return, or an emergency landing at the nearest airport. Ensure any past secondary flight plans are deleted.
22Route SummaryVERIFIED
23FMS InitializationCROSSCHECKNOTE: Verify airfield data, IRS alignment status, fuel and payload data, takeoff performance and flight plan.
24Barometric ReferenceSETNOTE: Set QNH on the EFIS control panel and the ISIS. Verify the two PFDs differ by no more than 20 ft, and the ISIS and PFD by no more than 30 ft. A 0.01 inHg difference between PFD and ISIS QNH is normal.
25ND Mode and RangeAS REQUIREDNOTE: ARC mode if the departure is roughly on runway heading; NAV mode if the change of direction is above 70 degrees.
26Weather RadarOFFCAUTION: Ensure no personnel and no metallic obstacle are within 20 feet of the aircraft. The radar starts emitting automatically when the first engine is started and weather display is selected.
27Flight DirectorON
28NORTH REFMAGNOTE: Ensure the TRUE message does not appear on the PFD or the HDG/TRK display.
29SPD/MACH, HDG/TRK, V/S/FPA WindowsDASHED
30ALT WindowINITIAL CLEARANCE ALTITUDE
31Oxygen Mask TestPERFORMNOTE: Set INT/RAD to INT on the RMP, test the mask, and verify the blinker turns yellow with audible oxygen flow. Check REGUL PR LO is not displayed on the DOOR SD page.
32Sliding WindowsCLOSED / LOCKEDNOTE: Verify the green part of the unlock pushbutton is visible.
33Takeoff BriefingPERFORMNOTE: Cover the planned course for normal and abnormal operations during takeoff, plus any other operational risks.
PHS 6 - Before Start22 steps
01Security InspectionCOMPLETE
02Cockpit PreparationCOMPLETE
03OxygenSET
04Gear Pins and CoversREMOVE
05Final LoadsheetCHECKNOTE: Verify the loadsheet data is accurate and compare ZFW / ZFWCG with the values entered in the FMS. The captain crosschecks both FMS.
06Fuel QuantityCHECKNOTE: Verify fuel on board on the system display corresponds to the flight plan and the loadsheet.
07THS in FMS ACTIVE/PERFT.O CG INSERTEDNOTE: Insert the takeoff centre of gravity from the loadsheet, then crosscheck. If the ECAM GWCG is outside operational limits, set AUTO GND XFR ON and wait for FUEL AUTO GND XFR COMPLETED. Do not launch the automatic ground transfer while the aircraft is moving.
08Final LoadsheetSIGN AND EXPORT
09T.O DataSETNOTE: Confirm the OIS final takeoff performance is still valid, or recompute. Crosscheck the takeoff speeds, flex temperature and takeoff configuration on both FMS.
10AltimeterSET
11Seats, Seat Belts, Harnesses, Rudder Pedals, ArmrestsADJUSTNOTE: The pilot's eyes should be in line with the red and white ball.
12Head Up DisplayDEPLOY AND ADJUSTNOTE: Declutter mode is recommended. Crosswind mode is not recommended on the ground.
13MFDIN TAKEOFF CONFIGURATIONNOTE: PF has the takeoff panel of ACTIVE/PERF, PM has the active flight plan page.
14External PowerCHECK AVAILABLENOTE: Push the external power pushbutton to show the AVAIL light before requesting disconnection.
15Low Pressure Ground CartsCHECK DISCONNECTEDNOTE: Disconnect before engine start to avoid faulty triggers.
16Pushback / Start-Up ClearanceOBTAIN
17Windows and DoorsCLOSENOTE: Verify on the DOOR system display that the doors are locked and the windows closed.
18SlidesCHECK ARMED
19SignsON / AUTO
20BeaconONNOTE: Set to ON when cleared for pushback.
21Thrust LeversIDLECAUTION: If a lever is beyond the idle detent it can damage the engine at start-up.
22Park BrakeSET AS REQUIREDCAUTION: If no pushback is required, set ON and verify pressure above 3,500 PSI on the triple pressure indicator. If pushback is required, set OFF and check the N/W STEER DISC memo is displayed. If the memo is absent but the ground crew confirms the tow pin is in the towing position, do not proceed with the pushback.
PHS 7 - Engine Start7 steps
01Engine Start SelectorIGN STARTNOTE: The engine page appears on the system display. Wait 10 seconds before setting the engine masters ON - this allows a series of fault-detection tests on the engines.
02Start Engines 1 and 2ANNOUNCENOTE: Any engine can be started first, at the pilot's discretion.
03Engine Master 1, then 2ONNOTE: Set the masters ON when all amber crosses and messages disappear from the engine parameters on the EWD and the SD engine page. The FADEC automatically cranks the engine for 20 seconds when N2 reaches 20 percent.
04Engine Idle ParametersCHECK NORMALNOTE: At ISA sea level with bleeds OFF the SOP gives approximately: throttle 3 percent, EGT around 455 degC, N1 approximately 20 percent, N2 approximately 66 percent, fuel flow around 1,400 lb/hr (635 kg/hr).
05Start Engines 3 and 4ANNOUNCE
06Engine Master 3, then 4ONCAUTION: Engine vibration at start is normal - up to 5 units over the N2 vibration limit is tolerated briefly during the start sequence only, due to thermal stabilization.
07ENG 2(3) REVERSER FAULTCHECK NOT DISPLAYEDNOTE: If the alert appears, set the engine start selector to NORM to reset FADEC electrical power, then back to IGN START when XX appears on the ENG parameters. If the message reappears the aircraft requires maintenance.
PHS 8 - After Start12 steps
01Engine Start SelectorNORMCAUTION: Prevents continuous ignition on the ground. The wheel page replaces the engine page on the system display. Wait 3 minutes before taking off to prevent thermal shock.
02APU BleedOFFNOTE: The APU bleed valves close and all engine bleed valves open automatically.
03All Engine Anti-IceAS REQUIREDCAUTION: Set ON when icing conditions are expected, or standing water, slush, ice or snow is on the taxiway or runway with OAT below 10 degC. Ice shedding requires an engine run-up at least every 30 minutes of taxi and before takeoff: park brake ON, then 60 percent N1 on two symmetric engines, then the other two. Abort the run-up if the aircraft starts to move.
04APU Master SwitchOFFNOTE: If the APU is no longer required.
05Ground SpoilersARMNOTE: Pull the ground spoilers lever to the outward position.
06Rudder TrimZERONOTE: If not zero, press the RESET button on the rudder trim panel.
07FlapsSETNOTE: Set the takeoff position and verify on the slats/flaps display on the PFD. If taxiing in icing conditions, delay flap extension until the runway holding point.
08Pitch TrimCHECKNOTE: Verify the pitch trim is at the takeoff position shown on the PFD.
09ECAM StatusCHECKNOTE: If a status reminder is displayed, press STS on the ECAM control panel.
10Ground EquipmentCLEARNOTE: Announce clear to disconnect. The ground crew removes chocks and tow pin, disconnects the interphone, and gives a hand signal from one side of the aircraft.
11N/W STEER DISC MemoCHECK NOT DISPLAYED
12Flight ControlsCHECKNOTE: Perform with flaps at the takeoff configuration. Check pitch, then roll, then yaw, holding each input long enough for full travel. Callouts: FULL UP, FULL DOWN, NEUTRAL, FULL LEFT, FULL RIGHT, NEUTRAL. For rudder, press PEDAL DISC to disconnect nosewheel steering first.
PHS 9 - Taxi17 steps
01Taxi ClearanceOBTAIN
02ETACS Taxi CameraAS REQUIREDNOTE: On the EFIS control panel. To acknowledge a ramp coordinator signal, turn the turnoff lights ON then OFF.
03ND Range SelectorZOOMNOTE: Activates the onboard airport navigation system (OANS). If DATABASE CYCLE NOT VALID appears, swap the active and second database.
04Nose LightsTAXI
05RWY TURN OFF and CameraAS REQUIRED
06Parking BrakeOFFNOTE: Verify no pressure on the triple pressure indicator.
07Thrust LeversAS REQUIREDCAUTION: No more than 10 percent thrust is needed at heavy weight on an uphill taxi slope. Excessive thrust can damage airport signalisation. If more thrust is needed, add it on the outer engines to prevent foreign object ingestion.
08BrakesCHECKCAUTION: The first brake application after the aircraft has been parked in wet conditions for an extended period may be less effective. Taxi at 10 to 20 kt in a straight line and 8 to 10 kt in a sharp turn. If speed is exceeded, brake to 10 kt and let the aircraft accelerate again.
09Nosewheel SteeringAS REQUIREDNOTE: Use smooth, progressive input. Maximum steering angle is 70 degrees.
10ATC ClearanceCONFIRM
11Takeoff DataCHECK / UPDATENOTE: If the runway or conditions changed, access T.O PERF, select or enter the new runway and conditions, recompute, and crosscheck. Update V1/VR/V2, flex temperature and flaps in the FMS, then set the flaps lever to the new takeoff position.
12Takeoff BriefingCONFIRMNOTE: Same as the briefing at the gate, with any new clearance or conditions added.
13Autobrake RTOARMNOTE: The RTO ARM light illuminates and BRK RTO appears on the FMA. Above 72 kt the RTO brake applies maximum braking if the thrust levers are set to idle; below that speed it will not activate.
14ATC CodeCONFIRM / SET
15T.O CONFIGTESTNOTE: Press the TO CONFIG pushbutton on the ECAM control panel. The EWD displays T.O CONFIG NORMAL if everything is in order.
16T.O MemoNO BLUE LINE
17CabinREADYNOTE: Verify the CABIN READY message on the EWD or obtain the report from the chief flight attendant.
PHS 10 - Before Takeoff11 steps
01Takeoff or Line-Up ClearanceOBTAIN
02Cabin CrewADVISENOTE: Make the takeoff signal to the cabin around 3 minutes before the estimated takeoff time.
03Packs 1 and 2AS REQUIREDCAUTION: SOP recommends packs OFF, or APU BLEED ON, to improve engine performance and reduce EGT for takeoff. Do not use APU BLEED if wing anti-ice is in use.
04Exterior LightsSETNOTE: RWY TURN OFF and camera ON, landing light ON, nose light T.O.
05ETACS TaxiOFFNOTE: If the ETACS was used during the taxi.
06ND RangeAS REQUIREDNOTE: Set the minimum range to the first waypoint after departure. Weather radar on the PF side, terrain on the PM side. TRAF ON.
07Approach PathCHECK CLEAR OF TRAFFIC
08StrobeONNOTE: Set to ON when crossing or entering a runway.
09Takeoff RunwayCONFIRMNOTE: Confirm by runway markings, runway lights, ILS signal, and the runway symbol on the ND.
10Sliding TableSTOWED
11TCASTA/RANOTE: TA ONLY is recommended where TA/RA is inappropriate, such as converging or parallel runways.
PHS 11 - Takeoff14 steps
01TakeoffANNOUNCENOTE: The SOP recommends performing a rolling takeoff.
02Throttle25 PERCENTNOTE: Apply 25 percent thrust first. For a standing takeoff apply the brakes; for a rolling takeoff release them.
03Thrust LeversFLX OR TOGACAUTION: If crosswind is above 23 kt and/or there is a tailwind, set 50 percent thrust first and only advance to FLX or TOGA at 20 kt ground speed.
04ChronometerSTART
05Directional ControlUSE RUDDER
06FMAMAN FLX OR MAN TOGANOTE: The lateral mode is not displayed until liftoff unless an ILS is tuned for the departure runway.
07Takeoff ThrustCHECKNOTE: Each engine should reach the thrust rating, indicated by a blue dot, before 80 knots.
08Before 80 Knots - Thrust SetANNOUNCECAUTION: Scan the PFD and engine indications. Reject the takeoff if any parameter indicates an abnormal situation.
09100 KnotsANNOUNCEWARNING: Rejecting the takeoff above 100 knots is a considerably more serious case than below it.
10V1MONITOR OR ANNOUNCE
11VR - Rotation12.5 DEG NOSE UPNOTE: Rotate toward a pitch attitude of 12.5 degrees, or 10 degrees with an engine failed, then follow the SRS pitch command bar. With the HUD, rotate to bring the inverted T toward the horizon line. NAV engages at 30 ft if armed; otherwise RWY TRK engages at 50 ft.
12Positive ClimbANNOUNCENOTE: Announced only when the vertical speed is positive and the radio altitude has increased.
13Landing GearUP
14AutopilotAS REQUIREDNOTE: Engage AP1 or AP2 above 100 ft AGL.
PHS 12 - After Takeoff / Climb14 steps
01Thrust Reduction Altitude - Thrust LeversCLNOTE: The cruise SD page replaces the engine page at 1,500 ft or at the thrust reduction altitude.
02Packs 1 and 2ONNOTE: If they were set OFF for takeoff.
03At F Speed - Flaps 1SETNOTE: For takeoffs in CONFIG 1+F the F speed does not appear.
04At S Speed - FlapsZERO
05Exterior LightsSETNOTE: Switch OFF the nose light and the runway turn off and camera.
06Ground SpoilersDISARM
07APU Bleed and APU MasterOFFNOTE: If the APU was used to supply the air conditioning.
08TCASTA/RANOTE: If the takeoff was performed in TA ONLY mode.
09Anti-IceAS REQUIREDNOTE: Set ON when icing conditions are expected with total air temperature at or below 10 degC. In the climb, set ON in icing conditions unless the static air temperature is below -40 degC.
10Cruise Flight LevelSET AS REQUIRED
11At 10,000 ft - Landing LightOFF
12At 10,000 ft - Seat Belts SignsAS REQUIREDNOTE: SOP recommends keeping the signs ON until the cruise phase, unless company policy states otherwise.
13Optimal / Maximum AltitudeCHECKNOTE: On the FMS cruise page.
14Transition Altitude - Barometric ReferenceSTANDARD SET / CROSSCHECKNOTE: The barometric setting flashes on the PFD at the transition altitude. Set STD on the EFIS control panel and on the ISIS.
PHS 13 - Cruise5 steps
01ALT CRZ on FMACHECKNOTE: Verify the aircraft is cruising at the level inserted on the CRZ panel of the FMS ACTIVE/PERF page. Change the FMS cruise level if the selected AFS altitude is below it.
02ECAM MemoREVIEW
03SD PagesREVIEWCAUTION: Pay close attention to engine oil pressure. Oil quantity can decrease rapidly in cruise due to temperature variation, particularly early in the flight. Monitor the bleed and electrical SD pages.
04Flight ProgressCHECK
05Step Flight LevelAS APPROPRIATENOTE: Proceed with step climbs as planned in the flight plan.
PHS 14 - Descent Preparation16 steps
01Weather and Landing InformationOBTAINNOTE: Start the preparation 80 nautical miles before the top of descent. Check destination and alternate weather and the runway to be used.
02Landing ElevationCHECKNOTE: Displayed on the cruise page of the system display.
03Barometric ReferencePRESET
04ECAM STATUS / STATUS MORECHECKNOTE: Note any failure or system degradation affecting landing capability, approach or descent. Check ALERTS IMPACTING LDG PERF on the STATUS MORE page.
05Landing PerformanceCHECKNOTE: Click the SYNCHRO ECAM button, then enter the estimated landing conditions and aircraft status in the OIS, compute, and compare the result with airline policy or local regulation.
06FMS ACTIVE/F-PLN Arrival PageINSERT / CHECKNOTE: Insert APPR, STAR, TRANS and APPR VIA. If NO FLS FOR THIS APPR appears, the approach is a non-precision approach without the FMS landing system function.
07DES Panel of FMS ACTIVE/PERFINSERT / CHECKNOTE: The managed speed profile defaults to a 250 kt speed limit below 10,000 ft. This can be altered on the FMS VERT REV page.
08APPR Panel of FMS ACTIVE/PERFINSERT / CHECKNOTE: Enter destination QNH, temperature and wind (do not enter gust values), then the minimum altitude to the nearest ten feet. Any runway or arrival change resets the minimum. Verify the landing configuration - FLAPS 3 may be chosen over FLAPS FULL depending on runway length, go-around performance, windshear, severe turbulence or system failure.
09GA Panel of FMS ACTIVE/PERFCHECKNOTE: Verify the thrust reduction altitude and the acceleration altitude.
10FMS POSITION/NAVAIDSCHECKNOTE: Verify VOR/ADF idents on the NDs and the ILS/GLS ident on the PFDs, plus frequency and course for an ILS/GLS approach.
11Secondary Flight PlanAS REQUIREDNOTE: Prepare an alternative runway or holding plan. Remember to set the new minimum and navaids when selecting it.
12Runway Exit and BTVSELECTCAUTION: BTV is recommended on dry or wet runways. It is not recommended on a contaminated runway, with an inoperative thrust reverser, or with any failure affecting landing performance. Set ND mode PLAN, range ZOOM, then select the runway and exit. Crosscheck the OANS runway length against the charts - the difference must not exceed 115 feet.
13Autobrake / BTVSELECT AS REQUIREDNOTE: Available modes are BTV, BRK LO, BRK 2, BRK 3 and BRK HI. SOP recommends autobrake mode 3 on a contaminated runway, and HI if BTV is unavailable or the runway is short.
14Landing BriefingPERFORM
15Descent ClearanceOBTAIN
16Cleared Altitude on AFS Control PanelSETCAUTION: Set the cleared altitude if it is above the safe altitude. If the safe altitude is higher, refer to ATC and set the safe altitude.
PHS 15 - Descent9 steps
01DescentINITIATENOTE: Engage DES mode at the top of descent shown on the ND or the FMS active flight plan page. The top of descent is calculated so the aircraft reaches VAPP at 1,000 ft AGL. It is not displayed in heading or track mode.
02Altitude KnobPUSHNOTE: At the top of descent.
03Rate of DescentADJUST AS REQUIREDCAUTION: Increase the selected speed if ATC allows, and maintain a high speed as long as possible for a fuel-efficient descent. Speed brakes are not recommended, and combining descent with deceleration is not recommended. Speed brakes may be used in OP DES but not in DES mode.
04At 20,000 ft - Cabin CrewADVISENOTE: SOP technique: use the seat belt sign selector to sound 3 chimes (select auto then on) and make the announcement 'Cabin crew, prepare for landing'.
05Terrain and Weather RadarAS REQUIRED
06At 10,000 ft - Landing LightsON
07At 10,000 ft - Seat Belts SignON
08CSTRONNOTE: Displays altitude constraints on the ND.
09LS PushbuttonAS REQUIREDNOTE: Press for an ILS/GLS, ILS G/S out, LOC only, LOC B/C, or non-precision approach flown with the FMS landing system.
PHS 16 - Approach23 steps
01Approach PhaseCHECK / ACTIVATENOTE: Activates automatically when flying over the DECEL pseudo waypoint in NAV mode. In heading or track mode, activate it 15 nautical miles from touchdown.
02PositioningCHECKNOTE: Use VERT DEV on the PFD in NAV mode, or the energy circle on the ND in HDG or TRK mode.
03Managed SpeedCHECKNOTE: The aircraft decelerates automatically at the DECEL pseudo waypoint when managed speed is active and NAV, LOC* or LOC is engaged.
04Landing Data and MinimaSET
05AltimeterQNH SET
06APPR Mode on AFS Control PanelPRESSNOTE: Press when ATC clears the approach. LOC and glideslope modes engage approximately 3 seconds after activation.
07Autopilot 1 + 2ONNOTE: Engage both autopilots when APPR mode is engaged. Check the approach capability on the FMA: CAT2, CAT3 SINGLE, CAT3 DUAL or AUTO LAND.
08Approaching Green Dot - Flaps 1SETNOTE: Set before 3 nautical miles from the final approach fix. Verify the aircraft decelerates toward the S speed. Aim to be on the glideslope with flaps 1 at S speed at or above 2,500 ft AGL. If the aircraft is high or not decelerating, extend the landing gear - speed brakes have limited effect at low speed.
09Below VFE Next, 2,500 ft AGL Minimum - Flaps 2SETNOTE: Verify deceleration toward the F speed. If the glideslope interception is below 2,000 ft AGL, set flaps 2 at one dot below the glideslope.
10After Flaps 2, 2,000 ft AGL Minimum - Landing GearDOWN
11Auto BrakeCONFIRMCAUTION: Be prepared for changing runway conditions. If using BTV, land on the runway set in BTV - landing on a different runway switches the autobrake automatically to HI on short final.
12Ground SpoilersARMNOTE: Arm by pulling the spoilers lever.
13Exterior LightsSET
14Below VFE Next - Flaps 3SET
15Wheel SD PageCHECKNOTE: Appears below 800 ft AGL or at gear extension. Verify five green landing gear indications and at least one green triangle on each gear, showing the strut locked down.
16Below VFE Next - Flaps FullSETNOTE: Verify the aircraft is decelerating toward the approach speed.
17AutothrottleCHECK IN SPEED MODE OR OFF
18Sliding TableSTOWED
19Landing MemoNO BLUE LINE
20CabinREADYNOTE: CABIN READY on the EWD, or a report from the chief flight attendant.
21At 350 ft AGL - LAND on FMAANNOUNCENOTE: Also check the ILS or GLS course on the PFD. At 500 ft AGL and below with BTV selected, the PM adjusts the ND range to display the OANS dry and wet lines.
22Minimum + 100 ftANNOUNCE ONE HUNDRED ABOVE
23Minimum - Landing or Go-AroundANNOUNCECAUTION: Maintain a stabilized flight path until the flare. At 50 ft, one dot below the glideslope is 7 ft below it. Do not duck under the glideslope.
PHS 17 - Landing13 steps
01Autopilot (manual landing)OFFNOTE: Disengage for a manual landing but keep the autothrottle speed mode engaged. If the autopilot is still engaged at minimum minus 50 ft, the FMA displays DISCONNECT AP FOR LDG.
02At approximately 40 ft RA - FlareINITIATENOTE: For a stabilized approach the normal flare height is 40 ft above ground level. Monitor pitch and bank - excessive angles risk a wing or tail strike.
03Thrust LeversIDLECAUTION: Move the thrust levers to idle as the main landing gear touches down. The ground spoilers will not extend if two or more thrust levers remain above the IDLE detent.
04Automatic Landing - FMACHECK FLARE / THROTTLE IDLE / ROLL OUTNOTE: FLARE between 50 and 40 ft RA, THROTTLE IDLE at approximately 30 ft, an automatic RETARD callout at 10 ft, then ROLL OUT at touchdown. With AUTO ROLL OUT, keep the autopilot engaged until the end of the roll out.
05DerotationINITIATENOTE: As soon as the main landing gear touches down.
06Reverser LeversPULLNOTE: Select MAX REV as soon as the landing gear touches down. If reverser use is limited for operational reasons, maintain IDLE REV until taxi speed. With one reverser failed the opposite engine reverser can still be used.
07Ground SpoilersCHECK EXTENDEDCAUTION: Check on the slats/flaps display at the bottom of the PFD. If they do not deploy, verify all thrust levers are at the IDLE detent, then set both reversers to MAX REV and press the brake pedals. Unarmed spoilers deploy automatically on thrust reverser activation.
08Auto BrakeCHECK / ANNOUNCENOTE: Verify the mode on the FMA: BTV, BRK LO, BRK 2, BRK 3 or BRK HI. The autobrake does not activate if the ground spoilers are not extended.
09Autopilot (auto rollout)DISCONNECT BEFORE 20 KT
1080 Knots - Reverser LeversIDLECAUTION: Avoid high reverse thrust at low speed unless the KEEP MAX REVERSE callout sounds or in an emergency.
11Directional ControlMONITORNOTE: Do not use the nosewheel steering control handle before reaching taxi speed.
12At Taxi Speed - Reverser LeversSTOWCAUTION: Stow the reversers before leaving the runway. Reverse thrust on taxiways is not recommended except in an emergency.
13Auto BrakeDISARMNOTE: Use one of the autothrottle instinctive disconnect pushbuttons. In BTV mode the autobrake disarms automatically at 10 knots.
PHS 18 - After Landing12 steps
01Ground SpoilersDISARM
02FlapsRETRACT TO 0
03APU Master SwitchONNOTE: The start sequence can be delayed to the engine shutdown sequence, but the SOP recommends doing it as early as possible.
04APU StartONNOTE: Verify the FLAP OPEN message on the APU SD page.
05Engine Start SelectorCHECK NORM
06Anti-IceAS REQUIREDNOTE: Turn ON when taxiing in cold conditions below 3 degC. Engine ground idle is increased when engine anti-ice is active.
07Landing LightsOFF
08StrobeAUTONOTE: Switch to AUTO when leaving the runway.
09Nose LightTAXI
10Runway Turn Off Lights and CameraAS REQUIRED
11Weather RadarCHECK OFFNOTE: Switches off automatically 60 seconds after landing.
12Brake TemperatureMONITORCAUTION: Monitor on the WHEEL SD page. Check for discrepancies and for temperatures higher than 500 degC.
PHS 19 - Parking16 steps
01Anti-IceOFF
02APU BleedONNOTE: Set ON before shutting the engines down to prevent engine exhaust fumes spreading into the air conditioning system.
03Parking BrakeONCAUTION: Avoid applying the parking brake if any brake temperature is above 500 degC.
04Engine Master Switches 1, 2, 3 and 4OFFCAUTION: After high thrust operations such as maximum reverse at landing, run the engines at idle for 3 minutes before shutdown for thermal stability of the hot section. If the APU is not available, connect external power before the shutdown sequence.
05Elapsed TimeSTOP
06Seat BeltsOFF
07SlidesCHECK DISARMEDNOTE: Verify on the DOOR/OXY SD page. If any slides are armed, advise the cabin crew.
08BeaconOFFNOTE: Turn OFF once all engines have spooled down.
09Other Exterior LightsAS REQUIRED
10Ground ContactESTABLISHEDNOTE: Verify with the ground crew that the chocks are in place.
11Fuel PumpsOFFNOTE: A white OFF light appears on the buttons.
12Head Up DisplaySTOW
13Fuel QuantityCHECKNOTE: Verify the fuel remaining is consistent with the prediction.
14Parking BrakeAS REQUIREDCAUTION: If a BRAKE HOT alert appears, ensure the chocks are placed and release the parking brake. Leave the parking brake set when winds including gusts exceed 30 knots, the ramp slope is excessive, or the surface is wet.
15OIS - All ApplicationsCLOSENOTE: Then exit the session so the FLT OPS STS page initializes for the next flight.
16Logbook - Flight ClosurePERFORMNOTE: Set the OIT side to NSS AVNCS and verify VHF 3 DATA mode is active before closing the electronic flight.
PHS 20 - Securing the Aircraft14 steps
01Parking BrakeONNOTE: Keeping the parking brake ON reduces leaks in the hydraulic system.
02Oxygen Crew SupplyOFF
03ADIRS (1 + 2 + 3)OFFCAUTION: Do not turn the ADIRS off during turnarounds at airports above 70 degrees North latitude - this avoids excessive alignment time. Wait 10 seconds before turning the electrical supply off so the system remembers the last data.
04Exterior LightsOFF
05Ground ServicingAS REQUIREDNOTE: Set GND SERVICING to ON if the ground crew requires electrical power.
06APU BleedOFF
07External PowerAS REQUIREDNOTE: At least two external power units are needed to supply the entire electrical network. Verify the APU load is below 50 percent, otherwise a third unit is required or the APU must be kept running.
08APU Master SwitchOFFNOTE: Turn OFF after all passengers have disembarked.
09Emergency Exit LightsOFF
10No SmokingOFF
11All LaptopsOFFNOTE: Click SWITCH OFF LAPTOP on the LOGIN page. The NSS shuts down automatically when the aircraft electrical supply is down.
12Onboard Information TerminalOFF
13All Batteries (BAT 1, ESS BAT, BAT 2, APU BAT)OFFCAUTION: Wait until the APU flap is closed before shutting off the APU battery.
14Cockpit WaylightON IF NECESSARYNOTE: If OFF is selected, the waylight turns off after 60 seconds, leaving time to leave the cockpit.
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