Airbus A320 SOP 04Takeoff

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TAKE OFF

PF

2.TAKE OFF RUN

1.TAKE OFF INITIATION AND POWER SET

3.ROTATION

4.THRUST REDUCTION

PNF

5.ACCELERATION

ACCEL ALT

F

6.AFTER TAKE OFF

S

THR RED ALT L/G UP POWER

80 kt

100 kt

V1

VR

A320 - Version 06d

PF

PNF 1. TAKEOFF INITIATION AND POWER SET

ANNOUNCE………………………….….”TAKE OFF”

CHRONO……………………………………......START

BRAKES………..…………………………...RELEASE THRUST LEVERS… … 1) From IDLE to 50 % N1 (1.05 EPR) … 2) From Both engines THR stabilized to T/O THR

¾ ECAM SD auto - switching

WHEEL

¾ Computer inhibits warnings and cautions.

ENGINE

T.O. INHIBIT

CHRONO……………………………………...START

PF

PNF 2. TAKEOFF RUN

ANNOUNCE FMA…………………………………….

FMA…………………………………………. CHECK ANNOUNCE…………………………..”CHECKED”

N1(EPR)……………………………………..CHECK BEFORE 80 kt

ANNOUNCE…………………….…”POWER SET”

AT 100 kt

ANNOUNCE………...”ONE HUNDRED KNOTS”

ANNOUNCE…………………………...”CHECKED”

PF

Limit

PNF SAME SPEED INDICATION

Limit

80 kt

100 kt

PF

PNF 3.a. ROTATION

AT V1

ANNOUNCE……………………….………..”V1”

At VR

ANNOUNCE…………………..….…”ROTATE”

ROTATION………………………………..PERFORM WHEN V/S positive and RA positive

ANNOUNCE…………...….…”POSITIVE CLB”

ORDER……………………………..…...”GEAR UP” L/G……………………………………….……..UP ANNOUNCE……………………..…”GEAR UP” GRND SPLR…………………………....DISARM EXTERIOR LIGHTS……………………..…..SET ORDER…………………………..”AUTOPILOT ON” A/P………………………..…...ON (on PF SIDE) ¾ AP is available 5 sec after lift off (100 ft). L/G UP 10

10

VR 80 kt

100 kt

V1 Note: With CFM engines, IGNITION is displayed only if IGN/START mode has been selected.

PF

PNF 3.b. PRESELECTED HEADING

ANNOUNCE FMA ……………………....”AP 1 (or 2)”

FMA………………………….………..…..CHECKED ANNOUNCE……………………………”CHECKED”

If RWY TRK mode is engaged: HDG…………………………………PULL or MANAGE

¾RWY TRK mode keeps the aircraft on the runway track memorized at 30 ft RA.

Pull HDG Knob To maintain runway HDG

Or

Push HDG Knob: NAV mode is engaged

PF

PNF 4. THRUST REDUCTION

FMA When LVR CLB flashing on FMA THRUST LEVERS………………………………....CL

FMA If takeoff was performed with packs off: PACKS 1 and 2 …………….………...……….ON ¾ 1500 ft AGLor 2 min after lift off : T.O. INHIBIT

L/G UP

THR RED ALT

¾ ECAM SD auto – switching :

VR ENG

CRZ

PF

PNF 5. ACCELERATION

At acceleration altitude

FMA At F speed with positive speed trend ANNOUNCE…………..”SPEED CHECKED”

ORDER……………………………...…”FLAPS 1”

FLAPS 1………………………………SELECT CONFIRM……………….…………“FLAPS 1” At S speed with positive speed trend ANNOUNCE……….....”SPEED CHECKED”

ORDER……………………………...…”FLAPS 0”

FLAPS 0…………………………...…SELECT CONFIRM………………………... “FLAPS 0”

THR RED ALT

ACCEL ALT

F

S

¾ Target speed change 1st CLB SPD CLIMB phase

V2

PF

PNF 6. AFTER TAKEOFF

APU BLEED/MASTER SW…..…….AS RQRD

ENG MODE SEL…………………….AS RQRD

TCAS…………………………………..…TA/RA

ANTI ICE……………...……………...AS RQRD

PF

PNF 7. TRANSITION ALT

At transition altitude : ANNOUNCE……………………….”PULL STANDARD” BARO REF ...……………......……...PULL STANDARD

BARO REF ...……………...……….…PULL STANDARD ANNOUNCE...……..”STANDARD CROSS-CHECKED”

ANNOUNCE…………………....”PASSING FL XX, now” ALT ...…………….....………………………….….CHECK ANNOUNCE………………………….….….”CHECKED”

AFTER T/O CLIMB C/L

PF

PNF

THE END...

PF

PNF 2. TAKEOFF RUN

ANNOUNCE FMA……………………………………. Typical Typical announcement announcement is is ::

FMA…………………………………………. CHECK ANNOUNCE…………………………..”CHECKED”

“MAN TOGA (or MAN FLX XX), SRS, RWY, A/THR blue” N1(EPR)……………………………………..CHECK BEFORE 80 kt

ANNOUNCE…………………….…”POWER SET”

AT 100 kt

ANNOUNCE………...”ONE HUNDRED KNOTS”

ANNOUNCE…………………………...”CHECKED”

PF

Limit

PNF SAME SPEED INDICATION

Limit

80 kt

100 kt

PF

PNF 3.a. ROTATION

AT V1

ANNOUNCE……………………….………..”V1”

At VR

ANNOUNCE…………………..….…”ROTATE”

ROTATION………………………………..PERFORM WHEN V/S positive and RA positive

ANNOUNCE…………...….…”POSITIVE CLB”

ORDER……………………………..…...”GEAR UP” ¾ ¾ Set Set NOSE NOSE and and RWY RWY TURN TURN OFF OFF lights lights switches switches to to OFF OFF ¾ ¾ LAND LAND lights lights should should be be left left ON ON

L/G……………………………………….……..UP ANNOUNCE……………………..…”GEAR UP” GRND SPLR…………………………....DISARM EXTERIOR LIGHTS……………………..…..SET

ORDER…………………………..”AUTOPILOT ON” A/P………………………..…...ON (on PF SIDE) ¾ AP is available 5 sec after lift off (100 ft). L/G UP 10

10

VR 80 kt

100 kt

V1 Note: With CFM engines, IGNITION is displayed only if IGN/START mode has been selected.

PF

PNF 4. THRUST REDUCTION

FMA When LVR CLB flashing on FMA THRUST LEVERS………………………………....CL THR THR RED RED ALT ALT ~~ 1500 1500 ft ft AGL AGL is is the the default default value value of of the the FMS, FMS, ItIt can can be be modified modified by by the the pilot pilot as as required required by by the the procedure procedure

FMA If takeoff was performed with packs off: PACKS 1 and 2 …………….………...……….ON ¾ 1500 ft AGLor 2 min after lift off : T.O. INHIBIT

L/G UP

THR RED ALT

¾ ECAM SD auto – switching :

VR ENG

CRZ

PF

ONE PACK

PNF

4. THRUST REDUCTION ¾ Do not select PACK 1 ON before reducing Takeoff Thrust, otherwise :

FMA When LVR CLB flashing on FMA

EGT

THRUST LEVERS………………………………....CL ¾

FMA Second pack selection is delayed until clean configuration. ONE PACK……………………...………………….ON • It may be selected earlier, in order to avoid ECAM caution activation, •

but not earlier than 10 seconds after PACK 1 ON, for passenger comfort ¾ 1500 ft AGLor 2 min after lift off :

¾ If

Above 1500 ft L/G UP

THR RED ALT

AIR PACK X T.O. OFFINHIBIT

¾ ECAM SD auto – switching :

VR ENG

CRZ

PF

FLAPS

PNF

5. ACCELERATION At acceleration altitude

FMA ¾ For T/O inspeed CONFtrend 1+F minimum flap retraction speed “F” is not displayed. At F speed with positive ANNOUNCE…………..”SPEED CHECKED”

ORDER……………………………...…”FLAPS 1”

FLAPS 1………………………………SELECT CONFIRM……………….…………“FLAPS 1” At S speed with positive speed trend ¾ When CONF 1+F is selected, auto retraction of flaps to CONF 11 occurs at 210 kt ANNOUNCE……….....”SPEED CHECKED” ORDER……………………………...…”FLAPS 0” FLAPS 0…………………………...…SELECT CONFIRM………………………... “FLAPS 0” 2ND PACK………………………………….ON ¾ Announce “FLAPS X” as soon as the proper position has been selected THR RED ALT

ACCEL ALT

F

S

¾ Target speed change 1st CLB SPD CLIMB phase

V2

PF FLIGHT PHASE SWITCHING CONDITIONSPNF 5. ACCELERATION At acceleration altitude

FMA At F speed with positive speed trend Preflight

Take Off

Climb

ORDER……………………………...…”FLAPS 1”

Cruise

Des

Approach

Go Around or Done

ANNOUNCE…………..”SPEED CHECKED”

FLIGHT PHASES

OPTIMUM SPEED PROFILE

SWITCHING CONDITIONS TO NEXT PHASE FLAPS 1………………………………SELECT

PREFLIGHT

/

SRS take off mode engaged and

At S speed with positive speed trend

N1> 85% (EPR >= 1.25) or CONFIRM……………….…………“FLAPS 1” Ground Speed > 90 kt

V2 (V2 + 10)

TAKE OFF

At acceleration altitude or by engagement of another vertical mode

ANNOUNCE……….....”SPEED CHECKED”

ORDER……………………………...…”FLAPS 0”

Reaching cruise FL FLAPS 0…………………………...…SELECT

CLIMB

ECON CLB SPD / MACH

CRUISE

ECON CRZ MACH

CONFIRM………………………... “FLAPS At descent initiation (if distance to DEST0” < 200 NM and no step descent)

2ND PACK………………………………….ON - Over flying (DECEL) pseudo waypoint with NAV (or DESCENT

THR RED ALT

ACCEL ALT

ECON DES MACH / SPD

F

S

APPROACH

Vapp (GS Min)

GO AROUND

Vapp or current SPD whichever is greater. Green Dot at ACC ALT

CLIMB phase

DONE

LOC*/LOC) mode engaged and altitude < 7200 ft AGL - Manual activation of the approach phase.

¾ Target speed change

1. To Go Around : when thrust levers at TO.GA detent or 2. To Done: 30 seconds after landing or 3. To Climb: when inserting a new CRZ FL

1. To Approach : Manual activation of the approach phase or 1st CLB SPD 2. To Climb: Above acceleration altitude by - Selecting ALTN or - inserting NEW DEST and CRZ FL

V2

/

To preflight when INIT or PERF key depressed

PF

PNF 6. AFTER TAKEOFF

APU BLEED/MASTER SW…..…….AS RQRD

ENG MODE SEL…………………….AS RQRD

TCAS…………………………………..…TA/RA

ANTI ICE……………...……………...AS RQRD

Select Select :: ¾ ¾ APU APU BLEED BLEED to to OFF, OFF,

¾ ¾ IGN, IGN,

ifif APU APU

has has been been used used during during T/O T/O

in in case case of of

severe severe turbulence turbulence or or heavy heavy rain rain

¾ ¾ TA/RA, TA/RA,

ifif TA TA

has has been been used used during during T/O T/O

¾ ¾ ENG ENG ANTI ANTI ICE, ICE,

in in case case of of

expected expected icing icing conditions conditions