FLOW PATTERNs
FLOW PATTERNs
NORMAL PROCEDURES
A330/A340
FLIGHT CREW STANDARD OPERATING PROCEDURES - COCKPIT PREPARATION
OPERATING MANUAL
FLOW PATTERN
Ident.: PRO-NOR-SOP-06-00019992.0001001 / 24 NOV 23
Applicable to: ALL
1
COCKPIT PREPARATION FLOW PATTERN
AT PUSHBACK/START CLEARANCE
Applicable to: ALL
Ident.: PRO-NOR-SOP-07-B-00024998.0001001 / 24 NOV 23
5
BEFORE START FLOW PATTERN
PUSHBACK/START CLEARANCE
PUSHBACK/START CLEARANCE.................................................................. OBTAIN PM
L2 Obtain ATC pushback/start clearance and ground crew clearance.
ATC
ATC..........................................................................................SET FOR OPERATION PM
L2 ATC is set in accordance with airport requirements.
Ident.: PRO-NOR-SOP-07-B-00011063.0002001 / 18 NOV 21
THRUST LEVERS
THRUST LEVERS ................................................................................................IDLE PF
CAUTION The engines start regardless of the thrust lever position. If the thrust levers are
not set to IDLE, then thrust rapidly increases to the corresponding thrust lever
position, causing a hazardous situation.
ACCU PRESSURE
ACCU PRESS indicator.................................................................................... CHECK PF
L2 The ACCU PRESS indication must be in the green band. If required, use the electric pump on blue
hydraulic system to recharge the brake accumulator.
L1
WARNING The blue electric pump pressurizes the blue hydraulic system. Get ground crew
clearance before using the electric pump.
Ident.: PRO-NOR-SOP-07-B-00011066.0002001 / 18 NOV 21
7
If pushback is required:
N/WS DISC MEMO................................................................... CHECK DISPLAYED PF
L2 In the case of pushback (towbarless or conventional), the nose wheel steering selector bypass
pin must be in the tow position. The N/WS DISC memo on the ECAM indicates this position.
L1 CAUTION If the ECAM does not display the N/WS DISC memo, but the ground crew
confirms that the tow pin is in the towing position, do not start the engines during
pushback in order to avoid possible damage to the nose landing gear upon
green hydraulic pressurization.
To dispatch the aircraft in this case, Refer to MMEL/MI-32-51 NWS Electrical
Deactivation Box.
BEFORE START C/L.............................................................................. COMPLETE PF-PM
PARK BRK handle...............................................................................................OFF PF
CAUTION Do not use brakes during pushback, unless required due to an emergency.
When pushback is completed:
PARK BRK handle.......................................................................................... ON PF
AFTER START
Applicable to: ALL
Ident.: PRO-NOR-SOP-09-A-00019960.0001001 / 03 NOV 22
APU BLEED
APU BLEED pb-sw.................................................................................................OFF PF
L2 This action enables to avoid ingestion of engine exhaust gases.
Ident.: PRO-NOR-SOP-09-A-00011045.0003001 / 03 NOV 22
ANTI-ICE
CAUTION In icing condition (Refer to LIM-ICE_RAIN Definition of Icing Conditions), the flight
crew must turn on the engine anti-ice and should not wait until seeing ice building
up.
ENG 1 and 2 ANTI-ICE pb-sw......................................................................AS RQRD PF
Engine anti-ice must be set to ON during all ground operations, when icing conditions exist or are
anticipated.
Ident.: PRO-NOR-SOP-09-A-00011046.0001001 / 09 NOV 21
APU
If the APU is not required:
APU MASTER SW pb-sw................................................................................ OFF PF
GROUND SPOILERS
GND SPLRS.......................................................................................................... ARM PM
Ident.: PRO-NOR-SOP-09-A-00011049.0001001 / 19 APR 22
RUDDER TRIM
RUD TRIM RESET pb.......................................................................................PRESS PM
L2 Press the RESET pb on the RUD TRIM panel.
L1 RUD TRIM.......................................................................................CHECK NEUTRAL PM
Note: After the reset, the flight crew may observe an indication of up to 0.6 ° (L or R) in the
RUD TRIM position indication.
Ident.: PRO-NOR-SOP-09-A-00011050.0001001 / 09 NOV 21
FLAPS
FLAPS lever................................................................................. SET FOR TAKEOFF PM
FLAPS.............................................................................................CHECK POSITION PM
L2 Check the position of the flaps on the ECAM upper display.
L1
If taxiing in icing conditions with rain, slush or snow:
Maintain the flaps retracted until the aircraft reaches the holding point of the takeoff runway.
This action prevents contamination of the slats/flaps mechanism.
Ident.: PRO-NOR-SOP-09-A-00011051.0003001 / 09 NOV 21
PITCH TRIM
PITCH TRIM......................................................................................................CHECK PM
L2 Check the takeoff CG on the PITCH TRIM handwheel using the ECAM’s CG indication.
Ident.: PRO-NOR-SOP-09-A-00011054.0001001 / 24 NOV 23
1
ECAM STATUS
ECAM STATUS.................................................................................................CHECK PF-PM
L2 The PM checks and the PF crosschecks that there is no status reminder (STS) on the E/WD
If STS appears on the E/WD, press the STS pb to display the STATUS page.
GROUND CREW
CLEAR TO DISCONNECT........................................................................ANNOUNCE PF
L2 The ground crew:
‐ Removes the chocks
‐ Nose wheel steering towing light on the nose landing gear checked off.
‐ Disconnects the interphone
‐ Makes the hand signal on the left or right side.
Ident.: PRO-NOR-SOP-09-A-00011068.0001001 / 09 NOV 21
TAXI
Ident.: PRO-NOR-SOP-10-A-00011941.0001001 / 09 NOV 21
Applicable to: ALL
TAXI CLEARANCE
TAXI clearance ................................................................................................OBTAIN PM
Ident.: PRO-NOR-SOP-10-A-00011942.0001001 / 09 NOV 21
Applicable to: ALL
EXTERIOR LIGHTS
L2 During taxi, the PF may request the PM to set the exterior lights.
L1 NOSE sw .............................................................................................................. TAXI PF
When crossing a runway:
STROBE sw.......................................................................................................ON PF
RWY TURN OFF & CAMERA sw .................................................................... ON PF
Ident.: PRO-NOR-SOP-10-A-00011943.0001001 / 09 NOV 21
Applicable to: ALL
PARK BRK
PARK BRK handle................................................................................................. OFF PF
BRAKES PRESSURE...................................................................... CHECK AT ZERO PF
L2 The flight crew may observe slight residual pressure on the triple indicator for a short period of
time.
Ident.: PRO-NOR-SOP-10-A-00011946.0002001 / 09 NOV 21
Applicable to: ALL
BRAKES
CAUTION If the aircraft was parked in wet conditions for a long time, the first brake
application at low speed is less effective.
BRAKE PEDALS............................................................................................... PRESS PF
BRAKES............................................................................................................ CHECK PF
BRAKE FAN pb .....................................................................................AS RQRD PM
L2 If an arc is displayed above the brake temperature on the WHEEL SD page, set to ON the BRAKE
FAN pb.
L1 BRAKES PRESSURE...................................................................... CHECK AT ZERO PM
FLIGHT CONTROLS
FLIGHT CONTROLS.........................................................................................CHECK PF-PM
L2 Check the flight controls at a convenient stage, before or during taxi.
Ident.: PRO-NOR-SOP-10-A-00011949.0001001 / 09 NOV 21
Applicable to: ALL
ATC CLEARANCE
ATC clearance.............................................................................................. CONFIRM PM
Ident.: PRO-NOR-SOP-10-A-00015138.0001001 / 24 NOV 23
Applicable to: ALL
1
AFS/FLIGHT INSTRUMENTS
F-PLN (SID,TRANS)......................................................................................... CHECK PM
L2 Carefully confirm that the ATC clearance agrees with the FMGS, if NAV mode is to be used.
L1 INITIAL CLIMB SPEED AND SPEED LIMIT.................................................... CHECK PM
L2 Use VERT REV at departure or at a CLB waypoint.
L1 CLEARED ALTITUDE ON FCU............................................................................. SET PM
L2 On the PFD, crosscheck and confirm the first cleared altitude.
L1 HDG ON FCU........................................................................ IF REQUIRED, PRESET PM
L2 If a heading is required by ATC after takeoff, in the case of a radar vector departure, preset the
heading on the FCU. NAV mode will be disarmed.
RWY TRK mode will keep the aircraft on the runway track.
L1 BOTH FD....................................................................................................CHECK ON PM
PFD/ND............................................................................................................. CHECK PF-PM
L2 Check that the PFD (e.g. airspeeds, initial target altitude, heading, FMA modes) and the ND
indications (SID) are in accordance with the departure.
L1 DEPARTURE BRIEFING.............................................................................. CONFIRM BOTH
AUTO BRK
AUTO BRK MAX pb-sw........................................................................................... ON PM
TERR ON ND
TERR ON ND ........................................................................................AS RQRD PF-PM
Consider selecting the radar display on the PF side, and TERR ON ND on the PM side only.
Ident.: PRO-NOR-SOP-10-A-00011952.0001001 / 28 NOV 23
Applicable to: ALL
3
ATC
ATC CODE/MODE..................................................... CONFIRM/SET FOR TAKEOFF PM
Ident.: PRO-NOR-SOP-10-A-00012083.0002001 / 15 NOV 21
Applicable to: ALL
TAXI - RADAR
Ident.: PRO-NOR-SOP-10-A-00015141.0003001 / 03 NOV 22
Applicable to: MSN 1224
WEATHER RADAR
RADAR..................................................................................................................... ON PM
L2 To check the departure path, set the MULTISCAN sw to MAN. The flight crew can then set the
radar to the AUTO position.
L1 PREDICTIVE WINDSHEAR SYSTEM.................................................................AUTO PM
Ident.: PRO-NOR-SOP-10-A-00015141.0004001 / 03 NOV 22
Applicable to: MSN 1741-1759
WEATHER RADAR
PREDICTIVE WINDSHEAR SYSTEM (1 or 2 ).................................................ON PM
RADAR CAPT DISPLAY mode selector................................................................. ALL PM
L2 30 s are necessary for the 3D buffer of the radar to be filled.
FINAL CHECK
T.O CONFIG pb ................................................................................................. TEST PM
L2 Press the T.O CONFIG on the ECP, and check that the EWD displays the T.O CONFIG NORMAL
memo.
L1 T.O MEMO ......................................................................................CHECK NO BLUE PM
L2 Check that the EWD does not display any blue line in the T.O memo section.
L1 CABIN REPORT .......................................................................................... RECEIVE PF-PM
L2 Check CABIN READY in the EWD, or obtain the cabin report from the purser.
Ident.: PRO-NOR-SOP-10-A-00024929.0001001 / 09 NOV 21
Applicable to: ALL
TAXI CHECKLIST
TAXI C/L.....................................................................................................COMPLETE PF-PM
BEFORE TAKEOFF
Applicable to: ALL
Ident.: PRO-NOR-SOP-11-A-00025077.0001001 / 09 NOV 21
BRAKE FANS
If the brake fans are set to ON:
BRAKE TEMPERATURE............................................................................CHECK PM
LINE-UP CLEARANCE
LINE-UP CLEARANCE.....................................................................................OBTAIN PM
Ident.: PRO-NOR-SOP-11-A-00012069.0001001 / 24 NOV 23
1
TCAS
TCAS Mode selector.................................................................................TA or TA/RA PM
L2 The flight crew should use the TA/RA mode as the default mode of the TCAS.
The flight crew may use the TA ONLY mode in specific airports, and for specific procedures
(identified by operators) that may provide resolution advisories that are neither wanted nor
appropriate (e.g. closely-spaced parallel or converging runways).
Ident.: PRO-NOR-SOP-11-A-00012077.0001001 / 09 NOV 21
TAKEOFF RUNWAY
TAKEOFF RUNWAY.....................................................................................CONFIRM PF-PM
L2 Confirm that the line up is performed on the intended runway and from the intended intersection.
Useful aids are:
‐ The runway markings
‐ The runway lights
Be careful that in low visibility, edge lights could be mixed up with the center line lights.
‐ The ILS signal
If the runway is ILS equipped, the flight crew can press the ILS pb (or LS pb): the LOC deviation
should be centered after line up
‐ The runway symbol on the ND
‐ The Runway Awareness and Advisory System .
Ident.: PRO-NOR-SOP-11-A-00012070.0001001 / 09 NOV 21
EXTERIOR LIGHTS
STROBE sw............................................................................................................. ON PF
L2 Set the STROBE sw to ON to cross or enter a runway.
The PF can request the PM to set the exterior lights.
Ident.: PRO-NOR-SOP-11-A-00012073.0001001 / 09 NOV 21
PACKS
PACK 1 pb-sw and PACK 2 pb-sw...............................................................AS RQRD PM
L2 Consider setting the packs to OFF, or the APU bleed pb-sw to ON. This will improve performance,
when using TOGA thrust.
If a takeoff is performed with the packs OFF : The packs must be set to OFF at least 20 s before
applying takeoff thrust.
In the case of a FLEX takeoff, setting the packs to OFF, or the APU bleed pb-sw ON, will reduce
takeoff EGT, and consequently reduce maintenance costs.
Use of the APU bleed is not permitted, if wing anti-ice is to be used.
Set the APU bleed pb-sw to ON at least 20 s before applying takeoff thrust. This will prevent the
ENG THRUST LOSS alert from triggering due to incorrect valve position.
Ident.: PRO-NOR-SOP-11-A-00012081.0001001 / 09 NOV 21
RNP AR DEPARTURE
GPS 1+2 on GPS MONITOR page.......................................... CHECK BOTH IN NAV PM
GPS PRIMARY on PROG page...................................................CHECK AVAILABLE PM
FMA................................................................................................................... CHECK PF-PM
L2 Verify NAV is armed.
Ident.: PRO-NOR-SOP-11-A-00012079.0001001 / 09 NOV 21
SLIDING TABLE/EFB
SLIDING TABLE................................................................................................. STOW PF-PM
ALL EFB transmitting mode..........................................................................AS RQRD PF-PM
L2 In accordance with the Operator's policy or, as required by operational regulations.
L1 ALL EFB (with no mounted equipment)............................................................. STOW PF-PM
L2 In flight, both flight crewmembers should not use EFB applications at the same time.
CABIN CREW
CABIN CREW...................................................................................................ADVISE PM
L2 Advise the cabin crew that takeoff is imminent.
Ident.: PRO-NOR-SOP-11-A-00012090.0001001 / 15 NOV 21
LINE-UP CHECKLIST
LINE-UP C/L.............................................................................................. COMPLETE PF-PM
TAKEOFF
Applicable to: ALL
Ident.: PRO-NOR-SOP-12-A-00021964.0001001 / 09 NOV 21
TAKEOFF CLEARANCE
TAKEOFF CLEARANCE.................................................................................. OBTAIN PM
Ident.: PRO-NOR-SOP-12-A-00021963.0001001 / 09 NOV 21
EXTERIOR LIGHTS
NOSE sw................................................................................................................. T.O PF
RWY TURN OFF sw................................................................................................ ON PF
LAND sw...................................................................................................................ON PF
Ident.: PRO-NOR-SOP-12-A-00012071.0016001 / 09 NOV 21
THRUST SETTING
The below procedure is the standard takeoff procedure. However, rolling takeoff is permitted.
TAKEOFF.................................................................................................. ANNOUNCE PF
THRUST........................................................................................................... 1.1 EPR PF
If the crosswind is at or below 20 kt and there is no tailwind:
SIDESTICK.................................................................................HALF FORWARD PF
L2 To counter the nose-up effect of setting engine takeoff thrust, apply half forward sidestick until
the airspeed reaches 80 kt. Release the sidestick gradually to reach neutral at 100 kt.
L1 BRAKES..................................................................................................RELEASE PF
THRUST LEVERS............................................................................ FLX or TOGA PF
L2 Once the thrust levers are set to FLX or TOGA detent, the Captain maintains the hand on the
thrust levers, until the aircraft reaches V1.
L1
In case of tailwind, or if crosswind is greater than 20 kt:
SIDESTICK................................................................................. FULL FORWARD PF
L2 To counter the nose-up effect of setting engine takeoff thrust, apply full forward sidestick until
the airspeed reaches 80 kt. Release the sidestick gradually to reach neutral at 100 kt.
L1 BRAKES..................................................................................................RELEASE PF
THRUST LEVERS............................................................................ FLX or TOGA PF
L2 Once the thrust levers are set to FLX or TOGA detent, the Captain maintains the hand on the
thrust levers, until the aircraft reaches V1.
L1
Note: The ENG SD page replaces the WHEEL SD page on the lower ECAM display.
CHRONO............................................................................................................START PM
DIRECTIONAL CONTROL.................................................................... USE RUDDER PF
PFD/ND......................................................................................................... MONITOR PM
L2 If GPS PRIMARY LOST, check on the ND the FMS position: i.e. that the aircraft is on the runway
centerline.
Ident.: PRO-NOR-SOP-12-A-00012072.0001001 / 09 NOV 21
BELOW 80 KT
TAKEOFF THRUST.......................................................................................... CHECK PM
L2 Check that the actual N1/EPR of the individual engines has reached the N1/EPR rating limit,
before the aircraft reaches 80 kt. Check EGT.
L1 THRUST SET............................................................................................ANNOUNCE PM
PFD and ENG indications.............................................................................MONITOR PM
L2 Scan airspeed, N1/EPR, and EGT throughout the takeoff.
Ident.: PRO-NOR-SOP-12-A-00025004.0001001 / 09 NOV 21
AT 80 KT
SIDESTICK....................................................................................................RELEASE PF
L2 Release the sidestick gradually to reach neutral at 100 kt.
Ident.: PRO-NOR-SOP-12-A-00012074.0001001 / 09 NOV 21
AT 100 KT
ONE HUNDRED KNOTS.......................................................................... ANNOUNCE PM
100 KT.................................................................................................. CROSSCHECK PF
L2 • The PF crosschecks and confirms the speed indicated on the PFD
• Below 100 kt, the Captain may decide to abort the takeoff, depending on the circumstances
• Above 100 kt, rejecting the takeoff is a more serious matter.
Ident.: PRO-NOR-SOP-12-A-00012076.0002001 / 09 NOV 21
AT V1
V1..................................................................................... MONITOR OR ANNOUNCE PM
L2 Monitor that the “V1” synthetic voice is triggered when reaching V1. If not, announce “V1”.
Ident.: PRO-NOR-SOP-12-A-00012078.0001001 / 09 NOV 21
AT VR
ROTATION........................................................................................................ORDER PM
ROTATION...................................................................................................PERFORM PF
L2 ‐ At VR, initiate the rotation with a positive sidestick input to achieve a continuous rotation rate of
about 3 °/s, towards a pitch attitude of 15 ° (12.5 °, if one engine is failed)
‐ Minimize lateral inputs on ground and during the rotation, to avoid spoiler extension. In strong
crosswind conditions, small lateral stick inputs may be used, if necessary, to aim at maintaining
wings level.
‐ After lift-off, follow the SRS pitch command bar.
L1
CAUTION If a tailstrike occurs, avoid flying at an altitude requiring a pressurized cabin, and
return to the originating airport for damage assessment.
Ident.: PRO-NOR-SOP-12-A-00012080.0003001 / 09 NOV 21
At F speed
FLAPS 1..................................................................................................... ORDER PF
FLAPS 1.................................................................................................... SELECT PM
At S speed
FLAPS 0..................................................................................................... ORDER PF
FLAPS 0.................................................................................................... SELECT PM
GND SPLRS..............................................................................................DISARM PM
L/G........................................................................................................ CHECK UP PM
NOSE sw..........................................................................................................OFF PM
RWY TURN OFF sw........................................................................................OFF PM
OTHER EXTERIOR LIGHTS..................................................................AS RQRD PM
L2 The flight crew can maintain the LAND sw set to ON, according to airline policy or regulatory
recommendations.
Ident.: PRO-NOR-SOP-12-A-00012092.0001001 / 18 AUG 10
CLIMB
Applicable to: ALL
Ident.: PRO-NOR-SOP-14-A-00012131.0001001 / 24 NOV 23
1
Normal vertical mode is CLB or OP CLB with managed speed active.
PF MCDU.........................................................................................................PERF CLB PF
L2 ‐ PF MCDU should be showing the PERF CLB page (allowing PF to monitor when the aircraft will
reach the FCU selected altitude) but the flight crew may select other pages such as F-PLN page
as may be tactically necessary
‐ The PROG page displays OPT FL and REC MAX FL. It is worth noting that this OPT FL is a
function of the cost index (CI).
‐ The displayed REC MAX FL gives the aircraft at least a 0.3 g buffet margin. The flight crew may
enter a cruise flight level above this level into the MCDU and the FMGS will accept it, provided that
it does not exceed the level at which the margin is reduced to 0.2 g.
L1 PM MCDU............................................................................................................... F-PLN PM
L2 PM MCDU should be showing the F-PLN page (allowing PM to enter any ATC long-term revisions to
the lateral or vertical flight plan).
L1
CLIMB SPEED MODIFICATIONS:
If a speed change is required by ATC, or for turbulence or operational considerations (e.g.
increase CLB rate):
Select the new speed with FCU SPD selection knob and pull.
Speed target is now selected.
To resume to MANAGED SPD profile:
Push FCU SPD selection knob. Speed target is now managed.
Note: The best rate of climb speed for long term situations lies between green dot and ECON
speed. Acceleration from green dot to ECON speed at high altitude can take a long
time.
EFIS Option:
The PF will select CSTR for grid MORA
The PM will select ARPT
Ident.: PRO-NOR-SOP-14-A-00012135.0001001 / 09 NOV 21
AT 10 000 FT AAL
LAND sw.................................................................................................................OFF PM
SEAT BELTS sw...........................................................................................AS RQRD PM
‐ MCDU predictions assume a return to the lateral F-PLN and descent flight path.
‐ Note that whenever the lateral mode is changed from NAV to HDG/TRK the vertical mode
reverts to V/S at the value pertaining at the time of the mode change.
‐ From time to time during stabilized descent, the flight crew may select FPA to check that the
remaining distance to destination is approximately the altitude change required divided by the
FPA in degrees.
‐ FPA (°) = Δ FL/DIST (NM)
DESCENT ADJUSTMENT
Applicable to: ALL
Ident.: PRO-NOR-SOP-17-A-00011967.0001001 / 09 NOV 21
DESCENT ADJUSTMENT
RATE of DESCENT...................................................................... ADJUST, AS RQRD PF
L2 To increase the rate of descent, increase the descent speed by using the selected speed, if
comfort and the ATC permit. It is more cost-effective (Time/Fuel) than using the speed brakes:
‐ Maintain a high speed as long as possible, provided that the ATC permits to fly above the speed
limits
‐ If the aircraft is high and at high speed, it is more efficient to keep the high speed until ALT* then
to decelerate at level-off, instead of combining descent and deceleration
‐ If the aircraft goes below the desired profile, use the selected speed and the V/S mode to adjust
the rate of descent.
In the OP DES mode, the flight crew can use the speed brakes to increase the rate of descent.
The flight crew can also use the speed brakes to maintain the required rate of descent, when
engine anti-ice is used.
In the DES mode, if the aircraft is on, or below the flight path and the ATC requires a higher rate
of descent, do not use the speed brakes because the rate of descent is imposed by the planned
flight path. Therefore, the A/THR may increase thrust to compensate for the increase in drag. In
this case, use the OP DES mode with speed brakes.
TERRAIN ON ND
TERR ON ND................................................................................................AS RQRD PF-PM
L2 ‐ In mountainous areas, consider displaying terrain on ND.
‐ If use of radar is required, consider selecting the radar display on the PF side, and TERR ON
ND on the PM side only.
‐ If NAV ACCURACY is LOW, do not use the TERR on ND.
Ident.: PRO-NOR-SOP-17-A-00011970.0002001 / 06 NOV 23
1
BAROMETRIC REFERENCE
When the aircraft approaches the transition level, and when cleared for an altitude:
BAROMETRIC REFERENCE................................................ SET/CROSSCHECK BOTH
L2 ‐ Set QNH on the EFIS control panel and on the standby altimeter
‐ Crosscheck the barometric reference settings and the altitude indications.
L1 Note: The flight crew must take into account any QNH change on the EFIS control panels,
standby altimeter and on the FMS PERF APPR page.
The flight crew should pay attention to a barometric reference that significantly
differs from the one used for approach preparation. That could be the symptom
of a barometric reference error. In this case the flight crew should consider the
confirmation of the barometric reference from all available sources.
AT 10 000 FT AAL
LAND sw................................................................................................................. SET PM
L2 LAND lights may be switched ON, depending on the airline policy or regulatory recommendation.
L1 SEAT BELTS sw...................................................................................................... ON PM
EFIS option pb..................................................................................................... CSTR PF-PM
L2 Select CSTR on both sides.
GO AROUND
Applicable to: ALL
Ident.: PRO-NOR-SOP-20-A-00011082.0008001 / 09 NOV 21
required. This enables to engage the GO-AROUND phase, with associated AP/FD modes.
The flight crew may use CL detent to have benefit of A/THR.
L1
Note: If the thrust levers are not set briefly to TOGA detent, the FMS does not engage the GO
AROUND phase, and flying over, or close to the airport (less than 7 NM) will sequence the
Destination waypoint in the F-PLN.
ROTATION.......................................................................................................PERFORM PF
L2 Initiate rotation towards 15 ° of pitch with all engines operative (approximately 12.5 ° if one engine is
out) to get a positive rate of climb then follow SRS Flight Director pitch orders.
When near the ground, avoid excessive rotation rate in order to prevent a tail strike.
L1 GO AROUND................................................................................................ ANNOUNCE PF
FLIGHT PARAMETERS................................................................................... MONITOR PM
FLAPS........................................................................................... RETRACT ONE STEP PM
FMA..................................................................................................CHECK/ANNOUNCE PF
L2 The following modes are displayed: MAN TOGA / SRS / GA TRK or NAV / A/THR.
Depending on the guidance modes during approach, NAV mode is either automatically armed or
automatically engaged.
For RNP AR, check that NAV mode engages immediately (minimum height 100 ft).
L1 POSITIVE CLIMB..........................................................................................ANNOUNCE PM
L/G UP.................................................................................................................. ORDER PF
L/G.................................................................................................................................UP PM
NAV or HDG mode........................................................................................... AS RQRD PF
GO AROUND ALTITUDE......................................................................................CHECK PM
Ident.: PRO-NOR-SOP-20-A-00011084.0001001 / 09 NOV 21
At F speed
FLAPS 1..................................................................................................... ORDER PF
AFTER LANDING
Ident.: PRO-NOR-SOP-21-A-00019950.0001001 / 09 NOV 21
Applicable to: ALL
GROUND SPOILERS
When the runway is vacated:
GND SPLRS..............................................................................................DISARM PF
EXTERIOR LIGHTS
L2
During taxi, the PF may request the PM to set the exterior lights.
L1 LAND sw.................................................................................................................OFF PF
When leaving the runway:
STROBE sw.................................................................................................. AUTO PF
NOSE sw.........................................................................................................TAXI PF
When crossing a runway:
STROBE sw.......................................................................................................ON PF
OTHER EXTERIOR LIGHTS........................................................................ AS RQRD PF
Ident.: PRO-NOR-SOP-21-A-00011017.0001001 / 09 NOV 21
Applicable to: MSN 1224
RADAR
RADAR....................................................................................................................OFF PM
Ident.: PRO-NOR-SOP-21-A-00011018.0001001 / 09 NOV 21
Applicable to: ALL
PREDICTIVE WINDSHEAR
PREDICTIVE WINDSHEAR SYSTEM ............................................................OFF PM
L2 Switching the radar and predictive windshear system OFF after landing avoids risk of radiating
persons at the gate area.
Ident.: PRO-NOR-SOP-21-A-00012821.0001001 / 15 NOV 21
Applicable to: MSN 1741-1759
FLAPS
FLAPS........................................................................................................... RETRACT PM
L2 ‐ Set the FLAPS lever to 0.
‐ If the approach was performed in icing conditions, or if the runway was contaminated with
slush or snow, do not retract the flaps until after engine shutdown, and after the ground crew
confirmed that flaps and slats are clear of obstruction due to ice.
‐ On ground, hot weather conditions may cause overheating to be detected around the bleed
ducts in the wings, resulting in AIR L(R) WING LEAK alert. Such warnings may be avoided
during transit by keeping the slats in CONF 1, when the OAT is above 30 °C.
Ident.: PRO-NOR-SOP-21-A-00011022.0001001 / 09 NOV 21
Applicable to: ALL
TCAS
TCAS.................................................................................................................... STBY PM
Ident.: PRO-NOR-SOP-21-A-00011023.0001001 / 09 NOV 21
Applicable to: ALL
ATC
ATC............................................................................................................... AS RQRD PM
L2 ATC is set in accordance with airport requirements.
Ident.: PRO-NOR-SOP-21-A-00011027.0001001 / 09 NOV 21
Applicable to: ALL
APU
APU MASTER SW pb-sw........................................................................................ ON PM
APU START pb........................................................................................................ ON PM
Note: APU start may be delayed until before engine shutdown. Before the flight crew shuts
down the engines, they must check that the AVAIL light of the APU START pb is on.
Ident.: PRO-NOR-SOP-21-A-00011024.0004001 / 03 NOV 22
Applicable to: ALL
ANTI ICE
CAUTION In icing conditions (Refer to LIM-ICE_RAIN Definition of Icing Conditions), the
flight crew must turn on the engine anti-ice and should not wait until seeing ice
building up.
BRAKE
BRAKE TEMPERATURE..............................................................................MONITOR PM
L2 ‐ Check the brake temperature for discrepancies and high temperature on the WHEEL SD page
‐ Maintenance action is due in the following cases:
• The temperature difference between two brakes of a gear is more than 150 °C, and the
temperature of one of these brakes is above or equal to 600 °C, or
• The temperature difference between two brakes of a gear is more than 150 °C, and the
temperature of one of these brakes is below or equal to 60 °C, or
• The difference between the average temperature of the left gear brakes and right brakes is
above or equal to 200 °C, or
• The temperature of one brake exceeds 800 °C.
PARKING
Ident.: PRO-NOR-SOP-22-A-00025018.0001001 / 10 MAY 22
Applicable to: ALL
PARK BRK
ACCU PRESS indicator.................................................................................... CHECK PF
L2 The ACCU PRESS indication must be in the green band. In case of low accumulator pressure,
chocks are required before engine shutdown.
ANTI ICE
ANTI ICE.................................................................................................................OFF PM
Ident.: PRO-NOR-SOP-22-A-00012191.0001001 / 09 NOV 21
Applicable to: ALL
APU BLEED
APU BLEED pb-sw.................................................................................................. ON PM
Set the APU BLEED pb-sw to ON immediately before engine shutdown to prevent engine exhaust
fumes from entering the air conditioning.
Ident.: PRO-NOR-SOP-22-A-00012192.0004001 / 24 NOV 23
Applicable to: ALL
1
ENGINES
If the APU is not available:
EXT PWR pb..................................................................................................... ON PF
No less than 1 min after high thrust operations:
All ENG MASTER LEVERS.............................................................................OFF PF
L2 The DOOR/OXY SD page is displayed on the lower ECAM display.
L1
Note: The flight crew must operate the engines at or near idle thrust for a cooling period of
1 min before engine shutdown, in order to thermally stabilize the engines.
Idle reverse thrust and normal thrust to maneuver during taxi (i.e. at or near idle), are
not considered as high thrust operations. Therefore, both of the following applies:
‐ If the flight crew used idle reverse thrust for landing and normal thrust to maneuver
during taxi after landing, the cooling period starts when the flight crew retards the
thrust lever during the flare
‐ If the flight crew used maximum reverse for landing, the cooling period starts when
the flight crew sets the thrust lever to idle reverse during the landing rollout.
Before engine shutdown, routine cooling periods that last less than the required time,
can result in engine degradation.
ENGINE PARAMETERS............................................................................ CHECK PF
L2 Check that engine parameters decrease.
EXTERIOR LIGHTS
WING sw.................................................................................................................OFF PF
BEACON sw........................................................................................................... OFF PF
L2 Turn off the beacon lights when all engines spooled down.
L1 OTHER EXTERIOR LIGHTS........................................................................ AS RQRD PF
L2 Wing lights may be used briefly for wing inspection. However, as this light can cause heat damage
to the jetway, it must be switched off, if the jetway is on the aircraft.
Ident.: PRO-NOR-SOP-22-A-00012195.0003001 / 09 NOV 21
Applicable to: MSN 1224-1741
EXTERIOR LIGHTS
WING sw.................................................................................................................OFF PF
BEACON sw........................................................................................................... OFF PF
L2 Turn off the beacon lights when all engines spooled down.
L1 OTHER EXTERIOR LIGHTS........................................................................ AS RQRD PF
L2 Wing lights may be used briefly for wing inspection. However, as this light can cause heat damage
to the jetway, it must be switched off, if the jetway is on the aircraft.
FUEL PUMPS
FUEL PUMPS.........................................................................................................OFF PM
Ident.: PRO-NOR-SOP-22-A-00012194.0001001 / 09 NOV 21
Applicable to: ALL
SLIDES
SLIDES..........................................................................................CHECK DISARMED PF
L2 Check that the slides are disarmed on the DOOR/OXY SD page. Warn the cabin crew, if any slide
is not disarmed.
Ident.: PRO-NOR-SOP-22-A-00012199.0001001 / 09 NOV 21
Applicable to: ALL
ATC
ATC.......................................................................................................................STBY PM
Ident.: PRO-NOR-SOP-22-A-00012196.0001001 / 09 NOV 21
Applicable to: ALL
SEAT BELTS
SEAT BELTS sw.................................................................................................... OFF PF
Ident.: PRO-NOR-SOP-22-A-00012200.0001001 / 09 NOV 21
Applicable to: ALL
IRS PERFORMANCE
IRS PERFORMANCE....................................................................................... CHECK PM
On the FMS POSITION/MONITOR page, check that the deviation does not exceed the following:
GROUND CONTACT
GROUND CONTACT.................................................................................ESTABLISH PF
L2 ‐ The flight crew should establish communication with the ground crew
‐ Check that chocks are in place.
FUEL QUANTITY
FUEL QUANTITY.............................................................................................. CHECK PM
L2 Check that the sum of the fuel on board and the fuel used is consistent with the fuel on board at
departure. If the flight crew detects a discrepancy that is not usual, maintenance action is due.
Ident.: PRO-NOR-SOP-22-A-00012203.0001001 / 05 MAY 22
Applicable to: ALL
BRAKE FAN
BRK FAN pb......................................................................................... AS RQRD PM
L2 Turn off the brake fans when they are no longer necessary.
Ident.: PRO-NOR-SOP-22-A-00012204.0001001 / 03 NOV 22
Applicable to: ALL
PARKING BRK
PARK BRK handle........................................................................................ AS RQRD PF
L2 If a temperature of one brake is above 300 °C (or above 150 °C with brake fan ON), the
parking brake should be released after the chocks are in place.
Releasing the parking brake prevents the critical structures from being exposed to high
temperature levels for an extended time. However, if operational conditions require (e.g. slippery
tarmac), the parking brake may remain applied.
The flight crew should not press the brake pedals before releasing the parking brake. However,
the flight crew must be prepared to press the brake pedals after parking brake release, if
necessary.
Ident.: PRO-NOR-SOP-22-A-00012208.0001001 / 18 NOV 21
Applicable to: ALL
PARKING CHECKLIST
PARKING C/L............................................................................................ COMPLETE PF-PM
Ident.: PRO-NOR-SOP-22-A-00012206.0001001 / 14 NOV 23
Applicable to: ALL
2
LOGBOOK
STATUS page................................................................................................... CHECK CM1
L2 Press the STS pb (ECAM control panel).
L1 LOGBOOK..................................................................................................COMPLETE CM1
L2 Complete the logbook according to the STATUS page.
Ident.: PRO-NOR-SOP-22-A-00021296.0001001 / 09 NOV 21
Applicable to: ALL
EFB
ALL EFB transmitting mode..........................................................................AS RQRD PF-PM
L2 In accordance with the Operator's policy or, as required by operational regulations.
L1
If performing transit stop:
CLEAR/CLOSE FLIGHT.............................................................................. APPLY PF-PM
Ident.: PRO-NOR-SOP-22-A-00012205.0001001 / 09 NOV 21
Applicable to: ALL
DISPLAY UNITS
DUs..........................................................................................................................DIM PF-PM
L2 Dim EFIS, ECAM and MCDU display units.