A320 Take-Off Performance Calculator

Normal Checklist:

BEFORE START

COCKPIT PREP COMPLETED

GEAR PINS and COVERS REMOVED

SIGNS ON/AUTO

ADIRS NAV

FUEL QUANTITY ______ KG.LB

TO DATA SET

BARO REF SET (BOTH)

MCDU WEIGHTS (LMC) ENTERED

WINDOWS/DOORS CLOSED (BOTH)

BEACON ON

THR LEVERS IDLE

PARKING BRAKE AS RQRD

AFTER START

ANTI ICE AS RQRD

ECAM STATUS CHECKED

PITCH TRIM ______% SET

RUDDER TRIM ZERO

BEFORE TAKEOFF

FLIGHT CONTROLS CHECKED (BOTH)

FLT INST CHECKED (BOTH)

BRIEFING CONFIRMED

FLAP SETTING CONF _____ (BOTH)

V1 / VR / V2 / FLX TEMP _____ (BOTH)

ATC SET

ECAM MEMO TO NO BLUE

- AUTO BRK MAX
- SIGNS ON
- CABIN READY
- SPLRS ARM
- FLAPS TO
- TO CONFIG NORM

TAKEOFF RWY _____ CONFIRM (BOTH)

CABIN CREW ADVISED

TCAS TA OR TA/RA

ENG MODE SEL AS RQRD

PACKS AS RQRD

AFTER TAKEOFF / CLIMB

LDG GEAR UP

FLAPS RETRACTED

PACKS ON

BARO REF _____ SET (BOTH)

APPROACH

BRIEFING CONFIRMED

ECAM STATUS CHECKED

SEAT BELTS ON

BARO REF _____ SET (BOTH)

MINIMUM _____ SET (BOTH)

ENG MODE SEL AS RQRD

LANDING

CABIN CREW ADVISED

A/THR SPEED/OFF

AUTOBRAKE AS RQRD

ECAM MEMO LDG NO BLUE

- LDG GEAR DN
- SIGNS ON
- CABIN READY
- SPLRS ARM
- FLAPS SET

AFTER LANDING

FLAPS RETRACTED

SPOILERS DISARMED

APU START

RADAR OFF/STBY

PREDICTIVE WINDSHEAR SYSTEM OFF

PARKING

APU BLEED ON

ENGINES OFF

SEAT BELTS OFF

EXT LT AS RQRD

FUEL PUMPS OFF

PARK BRK and CHOCKS AS RQRD

Consider HEAVY RAIN

SECURING THE AIRCRAFT

ADIRS OFF

OXYGEN OFF

APU BLEED OFF

EMER EXIT LT OFF

SIGNS OFF

APU AND BAT OFF

Consider COLD WEATHER

Supplementary Procedures:

ONE ENGINE TAXI - DEPARTURE

BRAKE ACCU PRESS CHECK

ENG 1 START

X BLEED OPEN

Apply the normal "AFTER START" procedures, but:

- Keep the APU running

- APU bleed should be switched off

- Perform the ECAM status, engine anti-icing and wing anti-icing checks after both engines have been started

Before releasing parking brake:
Y ELEC PUMP ON

Apply the normal "TAXI" procedures, but:

- Delay flight control checks until both engines have been started

- Do not arm autobrake before flight control check

Before ENG 2 start:
Y ELEC PUMP OFF

APU BLEED ON

No less than 2 minutes before takeoff:
ENGINE 2 START

X BLEED AUTO
Continue with "AFTER START" procedures

FLIGHT CONTROLS CHECK

AUTO BRK MAX

ONE ENGINE TAXI - ARRIVAL

APU START

After minimum cooling period of 3 minutes
APU AVAIL and taxi in a straight line:

ENG 2 SHUT DOWN

Y ELEC PUMP ON

At parking:
Y ELEC PUMP OFF

ENG 1 SHUT DOWN

DE-ICING ON GROUND

Do not move flaps, slats, ailerons, spoilers or elevators if they are not free of ice

Before spraying fluid:
CAB PRESS MODE SEL CHECK AUTO

ENG BLEED 1 + 2 OFF

APU BLEED OFF

DITCHING pb ON

THRUST LEVERS CHECK IDLE

READY FOR SPRAYING INFORM GND CREW

Upon completion of the spraying operation:
DITCHING pb OFF

OUTFLOW VALVE CHECK OPEN

ENG BLEED 1 + 2 ON

Switch ENG bleed ON, preferably after vacating the de-icing area. If fuselage has been sprayed consider APU BLEED OFF for Take-Off.

PITOTS ans STATIC (gnd crew) CHECK

GROUND EQUIPMENT REMOVE

DEICING REPORT RECEIVED

APU BLEED AS RQRD

NORMAL PROCEDURE RESUME

Pay special attention to the flight control check.

ASU ENGINE START

Refer to FCOM, if ENG1 will be started first and/or if external pneumatic PWR is used to start second ENG

Before connecting external pneumatic PWR:
PACKS 1 and 2 OFF

Before start:
APU BLEED OFF

ENG BLEED (both engines) OFF

X BLEED OPEN

Cleared to start and min. 30 psi air pressure
ENG 2 START

External pneumatic PWR unit removed
PACKS 1 and 2 ON

ENG 2 BLEED ON

XBLEED ENG START for ENG 1 APPLY

CROSSBLEED ENGINE START

Caution: Do not perform the crossbleed engine start procedure during pushback.

Simultaneous use of ENG bleed & external pneumatic PWR supply is prohibited.

APU BLEED OFF

ENGINE BLEED (running engine) CHECK ON

ENGINE BLEED (receiving engine) OFF

X-BLEED OPEN

Cleared to start
Confirm area is clear of obstacles & ensure increased power jet wake does not constitute any hazard to people or installation behind the aircraft

THRUST LVR (supplying engine) OPEN

Adjust initially to 30 PSI & min. 25 PSI during start.

RECEIVING ENGINE START

After start
THRUST LVR (supplying engine) IDLE

X-BLEED AUTO

ENGINE BLEED (receiving engine) ON

PACKS Check ON

Trim by cabin section

You can go back to the previous layout by resizing the window. The A319 IAE has been added.

Use this page to add runways and intersections.
Metric units only!