PFPF PNFPNFCommon 340

BEFORE START…

…ENGINE START…

…AFTER START

A340 - Version 03b

PFPF PNFPNFCommon 3401.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/Ldown to the line COMPLETED”

PFPF PNFPNFCommon 3401.b. BEFORE START

CAUTION ! DO NOT PERFORM the pushback if NW STRG DISC notdisplayed on the ECAM MEMO to avoid damages to the nose landing gear.

The BRAKE ACCU PRESSmust be in the green band When PARKING BRAKE is ON:

brake pressure is shownPARK BRK MEMO is displayed

NW STRG DISC MEMO........……….………..CHECK

WINDOWS and DOORS…….……CHECK CLOSED

THR LEVERS……………………….…………..…IDLE

PARKING BRAKE ACCU PRESS………..…CHECK

PARKING BRAKE……………………………..……ON

ORDER…….”BEFORE START C/L below the line”

GROUND CREW COMMUNICATION…ESTABLISH

PUSHBACK/START CLEARANCE……….OBTAIN

WINDOWS…………………………………….CHECK

BEACON……………………………………………ON

BEFORE START C/L below the line….PERFORMANNOUNCE…………………”BEFORE START C/L

COMPLETE”

PFPF PNFPNFA340-3002. AUTOMATIC ENGINE START SEQUENCE

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

BLEED PRESSURE…………………………CHECK

ANNOUNCE…………..”STARTING ENGINE 1&2”

MASTER SW 1 then 2…..………………………..ONSTART VALVE OPENSN2 INCREASES (N3 for RR)IGNITERFUEL FLOWEGTN1OIL PRESSSTART VALVE CLOSE

• 50% N2

ENG IDLE PARAMETERS……..CHECK NORMAL

ANNOUNCE…………..”STARTING ENGINE 3&4”REPEAT START SEQUENCE FOR ENG 3&4..…..

..CHECK

Check BLEED PRESSURE on ECAM page.

ECAM ENGINE page

XX.X XX.X

Start ENG 3 & 4 ONCE

AVAIL is displayed for

both ENG 1 & ENG 2

PFPF PNFPNFCommon 3403.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

5.

ENGINE WHEEL

ENG START SELback to NORM

ECAMPedestal

OverheadPanel

5

6

4

1

2

3

PFPF PNFPNFCommon 3403.b. AFTER START

To stabilize engine hot section temperature:

If icing conditions :

2 min minimum ator near IDLE

Enginestarted

High power

t

NWS TOWING FAULT LT extinguished…CHECK

AFTER START C/L

engines started

Observe the ECAM MEMO:

t (min.)0 2

PFPF PNFPNFCommon 3402. AUTOMATIC ENGINE START SEQUENCE

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

BLEED PRESSURE…………………………CHECK

ANNOUNCE…………..”STARTING ENGINE 1&2”

MASTER SW 1 then 2…..………………………..ONSTART VALVE OPENSN2 INCREASES (N3 for RR)IGNITERFUEL FLOWEGTN1OIL PRESSSTART VALVE CLOSE

• 50% N2 (GE)• Between 43% and 48% N2 (PW)• 50% N3 (RR)

ENG IDLE PARAMETERS……..CHECK NORMAL

ANNOUNCE…………..”STARTING ENGINE 3&4”REPEAT START SEQUENCE FOR ENG 3&4..…..

..CHECK

Check BLEED PRESSURE on ECAM page.

ECAM ENGINE page

ENG 2 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).

ENG 2 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).

PFPF PNFPNFA340-3002. AUTOMATIC ENGINE START SEQUENCE

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

BLEED PRESSURE…………………………CHECK

ANNOUNCE…………..”STARTING ENGINE 1&2”

MASTER SW 1 then 2…..………………………..ONSTART VALVE OPENSN2 INCREASES (N3 for RR)IGNITERFUEL FLOWEGTN1OIL PRESSSTART VALVE CLOSE

• 50% N2

ENG IDLE PARAMETERS……..CHECK NORMAL

ANNOUNCE…………..”STARTING ENGINE 3&4”REPEAT START SEQUENCE FOR ENG 3&4..…..

..CHECK

Check BLEED PRESSURE on ECAM page.

ECAM ENGINE page

XX.X XX.X

Start ENG 3 & 4 ONCE

AVAIL is displayed for

both ENG 1 & ENG 2

Each pilot monitors one engine.

Engine 1 & 2 start sequence :

ENG 1 MASTER switchON

ENG 2 MASTER switchON

Permits correct operation ofthe NO Break Power Transfer

PFPF PNFPNFA340-3002. AUTOMATIC ENGINE START SEQUENCE

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

BLEED PRESSURE…………………………CHECK

ANNOUNCE…………..”STARTING ENGINE 1&2”

MASTER SW 1 then 2…..………………………..ONSTART VALVE OPENSN2 INCREASES (N3 for RR)IGNITERFUEL FLOWEGTN1OIL PRESSSTART VALVE CLOSE

• 50% N2

ENG IDLE PARAMETERS……..CHECK NORMAL

ANNOUNCE…………..”STARTING ENGINE 3&4”REPEAT START SEQUENCE FOR ENG 3&4..…..

..CHECK

Check BLEED PRESSURE on ECAM page.

ECAM ENGINE page

XX.X XX.X

Start ENG 3 & 4 ONCE

AVAIL is displayed for

both ENG 1 & ENG 2

NORMAL ENGINE IDLE PARAMETERSAT ISA SEA LEVEL

N1…………………about 20%

EGT……………….about 400° C

N2…………………about 60%

FF…………………about 300 kg/h (660 lb/h)

PFPF PNFPNFCommon 3403.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

5.

ENGINE WHEEL

ENG START SELback to NORM

ECAMPedestal

OverheadPanel

5

6

4

1

2

3

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 PNFPNFA340-300

Set Takeoff CG on the pitch trim wheel

For this purpose, use the actual CG indicated on theECAM :

The Takeoff CG value must be within the green bandlimits.

PITCH TRIM SET

PFPF PNFPNFCommon 340

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

OAT or TAT 10° C with visiblemoisture in the air, standingwater, slush, ice or snow on

the taxiways or runways

ICINGICINGCONDITIONSCONDITIONS

expected

ENG ANTI ICEmust be ON

Engine anti-ice•

Wing anti-ice

WING ANTI ICErecommended

Prevent ice formation

Ice accumulation on thewing leading edges

Ice accumulation on thevisual ice indicator or on

the windshield wipers

OR

OR

WHEN ARE ENG & WING ANTI ICE REQUIRED ?

PFPF PNFPNFCommon 3403.b. AFTER START

To stabilize engine hot section temperature:

If icing conditions :

2 min minimum ator near IDLE

Enginestarted

High power

t

NWS TOWING FAULT LT extinguished…CHECK

AFTER START C/L

engines started

Observe the ECAM MEMO:

t (min.)0 2

If nosewheel steering has exceeded 93°

NO GO

Maintenance action required

Illumination of the redoversteer warning light

FAULT

FAULT

PFPF PNFPNFCommon 3403.b. AFTER START

To stabilize engine hot section temperature:

If icing conditions :

2 min minimum ator near IDLE

Enginestarted

High power

t

NWS TOWING FAULT LT extinguished…CHECK

AFTER START C/L

engines started

Observe the ECAM MEMO:

t (min.)0 2

NW STRG still disconnected+

at least 1 engine running

PFPF PNFPNFCommon 3403.b. AFTER START

To stabilize engine hot section temperature:

If icing conditions :

2 min minimum ator near IDLE

Enginestarted

High power

t

NWS TOWING FAULT LT extinguished…CHECK

AFTER START C/L

engines started

Observe the ECAM MEMO:

t (min.)0 2

On ground, perform an ENGINE RUN-UP (70% N1 minimum)for approximately 15 sec prior to higher thrust in order to

centrifuge any ice from the engine’s rotating parts

If icing conditions > 30minOR

Significant engine vibration•