A320-Taxi and Before Ckeck-List

PFPF PNFPNFTAXI & BEFORE T/O

A320 - Version 05a

PFPF PNFPNF1. TAXI INITIATION

Observe ECAM MEMO :

PARKING BRAKE release

( Slight residual pressure may beindicated for a short period of time )

When Taxi clearance obtained:

NOSE LIGHT....TAXI

PARKING BRAKE..................OFF

THRUST LEVERS..AS RQRD

ANNOUNCE.BRAKE CHECK

BRAKE PEDALPRESS

FLT CTLCHECK

TAXI CLEARANCE.....OBTAIN

ELAPSED TIME .................AS RQRD

BRAKE PRESSURE...........CHECK ZERO

ANNOUNCE..PRESSURE ZERO

FLT CTL..CHECK

Before Taxiing:

NW STRG DISC..CHECK not displayed onright ECAM MEMO

PFPF PNFPNF2. TAXI : CLEARANCE CONFIRMATION

When ATC clearance obtained: ATC CLEARANCE..CONFIRM

TERR ON NDAS RQRD

1. RADAR / PWS...ON / AUTO

2. ATC..SET

3. AUTOBRAKEMAX

4. T/O CONFIG..PRESS

5. T/O MEMO.CHECK NO BLUE

1 2

3

4

5

PFPF PNFPNF3. TAXI CHECKS

FCU ALT.....CHECK

If ATC requests to maintain runway heading or incase of a radar vector procedure :

HDG....SET

FLIGHT INSTRUMENTS..CHECK

T/O BRIEFING..CONFIRM

FLIGHT INSTRUMENTSCHECK

CABIN REPORTRECEIVE (CM1)

BEFORE T/O C/L down to the line

PFPF PNFPNF4. BEFORE TAKE OFF

If brake fans running:

BRAKE TEMP BELOW 150C.CHECK

BRAKE FANSOFF

TAKE OFF/LINE UP CLEARANCE..OBTAIN

ENGINE MODE SEL....AS RQRD

TCAS..TA or TA/RA

PACKS 1 + 2..AS RQRD

SLIDING TABLE.....STOW

APPROACH PATH CLEAR OF TRAFFIC.CHECK

CABIN CREW.ADVISE

EXTERIOR LIGHTS..SET

SLIDING TABLE...STOW

minimize bird strike hazardduring takeoff

BEFORE T/O C/L below the line

PFPF PNFPNF

THE END...THE END...

PFPF PNFPNFFLIGHT CONTROLS CHECK

Rudder check

FULL UP

FULL DOWN

NEUTRAL

FULL LEFT

FULL RIGHT

NEUTRAL

FULL LEFT

FULL RIGHT

NEUTRAL

PF moves the flight controls

PNF announces :

Bothelevators

ailerons

PF checks that PNF calls are in accordancewith the sidestick orders

PNF applies full sidestick deflections andsilently checks full travels and correct sense




2. ATC..SET

3. AUTOBRAKEMAX

4. TO CONFIG...PRESS

5. TO MEMO..CHECK NO BLUE

1 2

3

4

5

FMGS updatesTAKEOFF DATA updates

- Gross Weight and CG on FUEL PRED- F-PLN (runway in use)- Flaps levers (Take-off position)- V1,VR,V2 (reinsert)- FLEX T/O temperature (reinsert)

If takeoff data / ATC clearance has changed, (or in case of RWY change)

update takeoff data and FMGS :

- F-PLN- Initial climb and speed limit



TERR ON NDAS RQRD


2. ATC..SET

3. AUTOBRAKEMAX



1 2

3

4

5

If use of radar is required, consider selecting theradar display on the PF side, and TERR ON NDon the PNF side only.



TERR ON NDAS RQRD


2. ATC..SET

3. AUTOBRAKEMAX



1 2

3

4

5

Switch the Radar ON and the PWS to AUTO aslate as possible to avoid hazardous emissions toground staff

Switch the Radar ON and the PWS to AUTO aslate as possible to avoid hazardous emissions toground staff



TERR ON NDAS RQRD


2. ATC..SET

3. AUTOBRAKEMAX



1 2

3

4

5

Set the appropriate ATC configuration for takeoff:

ATC: AUTOALT RPTG: ONATC code setTCAS: TA or TA/RATraffic sel: ABV

Set the appropriate ATC configuration for takeoff:

ATC: AUTOALT RPTG: ONATC code setTCAS: TA or TA/RATraffic sel: ABV



TERR ON NDAS RQRD


2. ATC..SET

3. AUTOBRAKEMAX



1 2

3

4

5

Autobrake may be armed with PARKING BRK ON.

Autobrake may be armed with PARKING BRK ON.

ECAM WHEEL page

AUTO BRKMAX



TERR ON NDAS RQRD


2. ATC..SET

3. AUTOBRAKEMAX



1 2

3

4

5

Check that ECAM upper display showsT.O CONFIG NORMAL

Check that ECAM upper display showsT.O CONFIG NORMAL

PFPF PNFPNF

This disarms NAV mode.

Then RWY TRK will engage at 30 ft RA and will keep the aircraft on the current TRK.

This disarms NAV mode.

Then RWY TRK will engage at 30 ft RA and will keep the aircraft on the current TRK.

HEADING PRESET

Usual case :

If HDG preset :

CLB NAV

OP CLB

FMA

PFPF PNFPNFAddress any changes in the clearance

Make as extensive use as possible of the displays

TO BRIEFING CONFIRMATION FLOW

Address any changes in the clearance

Make as extensive use as possible of the displays

TO BRIEFING CONFIRMATION FLOW

PERFpage

F-PLNpage

12

3

456

7 RWY/SIDGW

CONF

FLXSel ALT

V1

V2

VR( optional)

TO BRIEFING CONFIRMATION

PFPF PNFPNFlimitation: 300C

auto ignition temperature of the hydraulic fluid

BRAKE TEMPERATURE LIMITATION

Without brake fan: Rely on HOT BRAKE ECAM caution (triggered at 300C)

With brake fans running:

The fans blow on the temperature sensor, and modifies the indication

The crew cannot rely on the ECAM caution (linked to indicated value).

Brake temperature must be checked

If indicated value is above 150C: delay takeoff

Indication on ECAM : 150 CActual Brake temperature :300 C




BRAKE FANSOFF



TCAS..TA or TA/RA




CABIN CREW.ADVISE




BEFORE T/O C/L below the line

Conditions for selecting IGN/START prior to takeoff :

Consider igniters wear in case of continuous ignition

Conditions for selecting IGN/START prior to takeoff :

Consider igniters wear in case of continuous ignition

ONENG ANTI ICEautomatically

Heavy rain or severe turbulencesexpected after takeoff

Runway with standing water

IAECFM




BRAKE FANSOFF



TCAS..TA or TA/RA




CABIN CREW.ADVISE




BEFORE T/O C/L below the lineKnown nearby traffic, in visual contact

Significant potential for unwanted or inappropriateresolution advisories

The FAA recommendsselecting TA mode




BRAKE FANSOFF



TCAS..TA or TA/RA




CABIN CREW.ADVISE




BEFORE T/O C/L below the lineConsider selecting packs

OFF or APU bleed ON

Improved performance(TOGA)

Reduced EGT (FLEX)

Use of APU bleed is not allowed, if wing anti-ice is to be used.

Documents

A320-Taxi and Before Ckeck-List