Before After Start

8/18/2019 Before After Start

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PFPF PNFPNFA330

BEFORE START…

…ENGINE START…

…AFTER START

A330 - Version 03



PFPF PNFPNFA330

1.a. BEFORE START

LOADSHEET……………..………………….CHECK

COCKPIT DOOR………..………………….CLOSED

Confirm any takeoff weight limitation.

Ask for external power disconnection

TAKEOFF DATA.........…………..…ENTER/REVISE

SEAT BELTS…………………………………ADJUST

MCDU………………………………………...PERF TO

ORDER….”BEFORE START C/L down to the line”

TAKEOFF DATA.........……………………XCHECK

SEAT BELTS……………………………….ADJUST

MCDU………………………………………….F-PLN

EXT PWR………………………………………..OFF

BEFORE START down to the line..…PERFORM

ANNOUNCE………………..”BEFORE START C/L

down to the line COMPLETED”





PFPF PNFPNFA330

2. AUTOMATIC ENGINE START SEQUENCE

ENG START SEL.........………………….IGN/START

BLEED PRESSURE…………………………CHECK

ANNOUNCE……………....”STARTING ENGINE 1”

MASTER SW 1…………………………………….ON

START VALVE OPENS

N2 INCREASES (N3 for RR)

IGNITER

FUEL FLOW

EGT

N1OIL PRESS

START VALVE CLOSE

• 50% N2 (GE)

• Between 43% and 48% N2 (PW)

• 50% N3 (RR)

ENG IDLE PARAMETERS……..CHECK NORMAL

ANNOUNCE……………...”STARTING ENGINE 2”REPEAT START SEQUENCE FOR ENG 2………..

..CHECK

Check BLEED PRESSURE on ECAM page. ECAM ENGINE page

RRGE PW

Start ENG 2 ONCE AVAIL is displayed

for ENG 1 XX.X



PFPF PNFPNFA330

3.a. AFTER START

ENG START SEL…………………….……NORM

APU BLEED………………………………….OFF

ECAM STATUS…………………….………CHECKECAM DOOR PAGE…...………………….CHECK

ANNOUNCE….……”CLEAR TO DISCONNECT”

1. GND SPLRS…………………………………ARM

2. RUD TRIM…………………………………RESET

3. FLAPS…………………………………………SET

4. PITCH TRIM…………………………………..SET

ENG ANTI ICE…………………………AS RQRDWING ANTI ICE………………………..AS RQRD

6. APU MASTER SW……………………………OFF

End of START sequence : Signal for PNF actions

Pedestal

Overhead

Panel

5.

5

6

4

1

2

3

ENGINE WHEEL

ENG START SEL

back to NORM

ECAM



PFPF PNFPNFA330

3.b. AFTER START

To stabilize engine hot section temperature:

If icing conditions :

3 min (GE) / 5 min (PW & RR) / 3 min (RR if

engines have been stopped for 1.5 hr or less)

minimum at or near IDLE

Engine

startedHigh power

t

GE : RR : PW :

engines started

Observe the ECAM MEMO:

NWS TOWING FAULT LT extinguished…CHECK

AFTER START C/L

t (min.)0 2



PFPF PNFPNFA330

2. AUTOMATIC ENGINE START SEQUENCE




MASTER SW 1…………………………………….ON

START VALVE OPENS


IGNITER

FUEL FLOW

EGT

N1OIL PRESS

START VALVE CLOSE

• 50% N2 (GE)


• 50% N3 (RR)



..CHECK



for ENG 1

RRGE PW

ENG 1 is started first because it powers the blue hydraulic system, which pressurizes the parking

brake.

DO NOT SET the MASTER switch ON before all amber crosses and messages have disappeared on

engine parameters (upper ECAM display).


brake.



Select “IGN

START”

Set ENG master

switch to ONWait 3 sec.



PFPF PNFPNFA3302. AUTOMATIC ENGINE START SEQUENCE




MASTER SW 1…………………………………….ON

START VALVE OPENS


IGNITER

FUEL FLOW

EGT

N1OIL PRESS

START VALVE CLOSE

• 50% N2 (GE)


• 50% N3 (RR)



..CHECK



for ENG 1

RRGE PW

DO NOT SET the MASTER switch ON before EGT amber crosses and messages have disappeared on



brake.

DO NOT SET the MASTER switch ON before EGT amber crosses and messages have disappeared on



brake.

Starting a hot engine

(1st start: EGT>100°C

2nd start: EGT>150°C)

EEC performs a dry crank to

reduce engine temperature



PFPF PNFPNFA3302. AUTOMATIC ENGINE START SEQUENCE




MASTER SW 1…………………………………….ON

START VALVE OPENS


IGNITER

FUEL FLOW

EGT

N1OIL PRESS

START VALVE CLOSE

• 50% N2 (GE)


• 50% N3 (RR)



..CHECK



for ENG 1

RRGE PW


brake.




brake.





PFPF PNFPNFA330

GE:

N1………………………about 23%

EGT…………………….about 360° C

N2………………………about 63%

FF………………………about 550 kg/h (1210 lb/h)

PW:

EPR……………………about 1.010%

EGT……………………about 320° C

N1………………………about 23%

RR:

EPR……………………about 1.015%

EGT……………………about 380° C

N1………………………about 22.6%N2………………………about 47%

NORMAL ENGINE IDLE PARAMETERS

AT ISA SEA LEVEL

FF…………………about 580 kg/h (1280 lb/h)

N2…………………about 59%

FF…………………about 820 kg/h (1800 lb/h)

N3…………………about 63%

Upper ECAM

Lower ECAM



PFPF PNFPNFA3303.a. AFTER START

ENG START SEL…………………….……NORM

APU BLEED………………………………….OFF

ECAM STATUS…………………….………CHECK

ECAM DOOR PAGE…...………………….CHECK

ANNOUNCE….……”CLEAR TO DISCONNECT”

1. GND SPLRS…………………………………ARM

2. RUD TRIM…………………………………RESET

3. FLAPS…………………………………………SET

4. PITCH TRIM…………………………………..SET

ENG ANTI ICE…………………………AS RQRD

WING ANTI ICE………………………..AS RQRD

6. APU MASTER SW……………………………OFF

End of START sequence : Signal for PNF actions

Pedestal

Overhead

Panel

5.

5

6

4

1

2

3

ENGINE WHEEL

ENG START SEL

back to NORM

ECAM

Turn APU BLEED OFF just after engine start

to avoid ingesting engine exhaust gases.

Turn APU BLEED OFF just after engine start

to avoid ingesting engine exhaust gases.



PFPF PNFPNFA330

Set Takeoff CG on the pitch trim wheel

For this purpose, use the actual CG indicated on the

ECAM :

The Takeoff CG value must be within the green band

limits.

PITCH TRIM SET

4



PFPF PNFPNFA330

WHEN ARE ENG & WING ANTI ICE REQUIRED ?

CAUTION ! In icing conditions, minimise flight duration with the slats extended.

OAT or TAT 10° C with visible

moisture in the air, standingwater, slush, ice or snow on

the taxiways or runways

ICING ICING

CONDITIONS CONDITIONS

expected

ENG ANTI ICE

must be ON

Engine anti-ice•

Wing anti-ice

WING ANTI ICE

recommended

Prevent ice formation

Ice accumulation on the

wing leading edges

Ice accumulation on thevisual ice indicator or on

the windshield wipers

OR

OR



PFPF PNFPNFA3303.b. AFTER START






Engine

startedHigh power

t

GE : RR : PW :

engines started



AFTER START C/L

t (min.)0 2

If nosewheel steering has exceeded 93°

NO GO

Maintenance action required

FAULT

FAULT

Illumination of the red

oversteer warning light









Engine

startedHigh power

t

GE : RR : PW :

engines started



AFTER START C/L

t (min.)0 2

NW STRG still disconnected+

at least 1 engine running









Engine

startedHigh power

t

GE : RR : PW :

engines started



AFTER START C/L

t (min.)0 2

On ground, perform an ENGINE RUN-UP (60% N1 minimum)for approximately 30 sec prior to higher thrust in order to

centrifuge any ice from the engine’s rotating parts

If icing conditions > 30min

OR

Significant engine vibration•

ENG ANTI ICEON

Continuous ignitionautomatically selected•









Engine

startedHigh power

t

GE : RR : PW :

engines started



AFTER START C/L

t (min.)0 2

On ground, perform an ENGINE RUN-UP (50% N1recommended) for 10 sec prior to take off in order to

centrifuge any ice from the engine’s rotating parts

If holding on the ground, perform it once every hour

If icing conditions

&

OAT 1° C•









Engine

startedHigh power

t

GE : RR : PW :

engines started



AFTER START C/L

t (min.)0 2

On ground, perform PERIODIC ENGINE RUN-UP (50% N1recommended) to centrifuge any ice from the engine’s

rotating parts at intervals not greater than 15 min.If icing conditions

&OAT 3° C

Take off should be preceded by a STATIC RUN-UP (50% N1recommended) with observation of all primary parameters

•

ENG ANTI ICEON

Continuous ignitionautomatically selected•

Date post:	07-Jul-2018
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