A330

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

MANDATORY MANDATORY MANDATORY MANDATORY

ATA SYSTEM : 27

TITLE : FLIGHT CONTROLS - FCSC - INTRODUCE FCSC STD L19M18 ON A330 A/C.

MODIFICATION No. : 55697S18547

This page transmits Revision No. 01 of Service Bulletin No. A330-27-3146

ADDITIONAL WORK

No additional work is required by this revision for aircraft modified by any previous issue.

REASON

Revision No. 01 issued to update paragraphs PUBLICATION AFFECTED, LIST OF

MATERIALS-OPERATORS SUPPLIED and TEST.

CHANGES

SUMMARY :

- REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES

. Para. REASON updated.

- EFFECTIVITY

. Effectivity updated and operator ISR added.

PLANNING INFORMATION :

- EFFECTIVITY

. 1.A. Effectivity updated and operator ISR added.

- REASON

. 1.C. Para. REASON updated.

- PUBLICATIONS AFFECTED

. 1.K. FCOM added.

DATE : Jun 01/07 SERVICE BULLETIN No. : A330-27-3146

REVISION No. : 01 - Sep 03/08 Page : 1 of 2

Printed in France © AIRBUS 2008 All rights reserved
A330

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

MATERIAL INFORMATION :

- LIST OF MATERIALS - OPERATOR SUPPLIED

. 2.D. NOTE (01) cancelled.

ACCOMPLISHMENT INSTRUCTIONS :

- TESTS

. 3.C. PN LA2B00300A30000 becomes LA2B00300A40000.

FILING INSTRUCTIONS

This Service Bulletin has been generated electronically and is reissued as a complete document.

Replace the complete document.

Put this Revision Transmittal Sheet in front of the Service Bulletin.

HISTORY OF PREVIOUS REVISIONS

No previous revisions.

REVISION SEQUENCE

ORIGINAL : Jun 01/07

REVISION No. : 01 - Sep 03/08

DATE : Jun 01/07 SERVICE BULLETIN No. : A330-27-3146

REVISION No. : 01 - Sep 03/08 Page : 2

Printed in France © AIRBUS 2008 All rights reserved
A330

SERVICE BULLETIN

SUMMARY

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

This summary is for information only and is

not approved for modification of the aircraft

MANDATORY MANDATORY MANDATORY MANDATORY

ATA SYSTEM : 27

TITLE : FLIGHT CONTROLS - FCSC - INTRODUCE FCSC STD L19M18 ON A330 A/C.

MODIFICATION No. : 55697S18547

REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES

New software standard L19/M18 on Flight Control Secondary Computer was defined in order to take into

account the last FCSC software evolutions.

This Service Bulletin is published to inform all operators of A330 aircraft of the issue of AIRBUS FRANCE

SAS Service Bulletin No. LA2B0-27-005.

This Service Bulletin recommends introducing new software "L19/M18" PN LA2B00300A40000 on the

two FCSC by means of On Board Replace Module (OBRM) replacement or reprogramming or FCSCs

replacement.

Accomplishment of this Service Bulletin introduces the improvements that follow :

- modification of others computers monitoring

- new elevator position monitoring function, which cancels the OEB 50.

- correction of spurious alarm of Pedal Feel and Trim Unit (PFTU).

- modification of parameters record when computer fault.

NOTE : To take into account the "new elevator position monitoring" function at aircraft level, this new

FCSC needs to be associated with Flight Control Primary Computer (FCPC) P9/M18. A future AD

will mandate the modification of both FCSC and FCPC to permit the cancellation of red OEB 50

NOTE : FCSC STD L19/M18 can be installed on basic aircraft.

DATE : Jun 01/07 SERVICE BULLETIN No. : A330-27-3146

REVISION No. : 01 - Sep 03/08 Page : 1 of 4

Printed in France © AIRBUS 2008 All rights reserved
A330

SERVICE BULLETIN

SUMMARY

EVALUATION TABLE

COMPLIANCE Mandatory CANCELS INSPECTION SB No

POTENTIAL AD Yes A/C OPERATION AFFECTED Yes

RELIABILITY AFFECTED No PAX COMFORT AFFECTED No

COST SAVING No ETOPS AFFECTED No

STRUCTURAL LIFE EXTN No VENDOR SB INVOLVED Yes

KIT PRICE (USD) No Kit

MODIFICATION CLASSIFICATION

MAJOR 55697S18547

MINOR None

As per EASA IR 21, a minor change is one that has no appreciable effect on the mass, balance, structural

strength, reliability, operational characteristics affecting the airworthiness of the product. All other changes

are major changes.

EFFECTIVITY

This Service Bulletin is applicable to these operators :

99Y AAR AEA CAL CCA CES CPA CSN DAH DLH EEZ EIN ETD EVA FWI HDA ISR IWD IYE JAI JST

KLM LTU MSR NWA QAF QFA QTR TAM TCX THY

NOTE : This modification is embodied before delivery on aircraft MSN 0850-0852, 0854-0939,

0941-0944, 0946-1000, 1002-1054, 1056 and subsequent.

CONCURRENT REQUIREMENTS

Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishment of the following

Service Bulletin(s) or the equivalent production modification(s):

Service Bulletin No. A330-27-3120 Mod. No. 52378S18007

DATE : Jun 01/07 SERVICE BULLETIN No. : A330-27-3146

REVISION No. : 01 - Sep 03/08 Page : 2

Printed in France © AIRBUS 2008 All rights reserved
A330

SERVICE BULLETIN

SUMMARY

Service Bulletin No. A330-27-3132 Mod. No. 49965S16501

Mod. No. 51341S16795

Mod. No. 53503S18051

Mod. No. 53504S18052

Service Bulletin No. A330-27-3017 Mod. No. 42983S12314

Service Bulletin No. A330-27-3118 Mod. No. 52017S16877

REFERENCES/REPERCUSSIONS

TFU : 27.22.00.004

27.90.00.033

OEB : 50-3

AOT : None

SIL : None

LIFE LIMIT : None

LINE MAINTENANCE AFFECTED : No

OTHERS : None

NATURE OF THE WORK

AIRCRAFT : NO

EQUIPMENT : YES

HARD : YES

SOFT : NO

OBRM : YES

MANPOWER

Config. 01, on aircraft :

TOTAL MANHOURS 2.5

ELAPSED TIME (HOURS) 2.5

NOTE : For other manhours required for the accomplishment of this Service Bulletin, refer to AIRBUS

FRANCE SAS Service Bulletin No. LA2B0-27-005.

MATERIAL INFORMATION

AIRCRAFT DATA

None

DATE : Jun 01/07 SERVICE BULLETIN No. : A330-27-3146

REVISION No. : 01 - Sep 03/08 Page : 3

Printed in France © AIRBUS 2008 All rights reserved
A330

SERVICE BULLETIN

SUMMARY

APPENDICES

None

DATE : Jun 01/07 SERVICE BULLETIN No. : A330-27-3146

REVISION No. : 01 - Sep 03/08 Page : 4

Printed in France © AIRBUS 2008 All rights reserved
A330

SERVICE BULLETIN

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

MANDATORY MANDATORY MANDATORY MANDATORY

ATA SYSTEM : 27

TITLE : FLIGHT CONTROLS - FCSC - INTRODUCE FCSC STD L19M18 ON A330 A/C.

MODIFICATION No. : 55697S18547

This document contains AIRBUS PROPRIETARY INFORMATION and shall at all times remain the property

of AIRBUS; no intellectual property right or licence is granted by AIRBUS in connection with any information

contained in it. It is delivered on the express condition that said document and the information contained in

it shall be treated as confidential, shall not be used for any purpose other than that for which it is hereby

delivered. It shall not be disclosed in whole or in part to third parties and shall not be duplicated in any

manner (except for the purposes of performing the tasks described hereunder and provided that any recipient

of such document shall comply with the conditions herein), without AIRBUS’ prior written consent.

1. PLANNING INFORMATION

A. EFFECTIVITY

(1) Models

330-202 330-203 330-223 330-243 330-302 330-303 330-323 330-342 330-343

(2) Aircraft

(a) Effectivity by MSN

This Service Bulletin is applicable to aircraft MSN :

0524 0533 0542 0549 0552 0553 0555 0558 0564 0570 0571 0573 0574 0576 0578

0579 0587 0588 0591 0593 0595 0600 0602 0603 0605 0607 0609 0610 0612 0614

0616 0618 0620 0621 0623 0625 0629 0631-0634 0636-0638 0640-0642 0644 0645

0647-0650 0652-0656 0658 0659 0661-0667 0669-0671 0673-0676 0678-0680

0682-0684 0686-0688 0690-0693 0695-0697 0699-0701 0703-0705 0707-0709

0711-0714 0716-0718 0720-0722 0724-0726 0728-0730 0732-0735 0737-0739

0741-0743 0745-0747 0749-0752 0754-0756 0758-0760 0769 0770 0772-0774

0776-0778 0780-0782 0784-0786 0788 0789 0791 0792 0795-0797 0799 0801-0803

0805-0807 0809-0811 0813-0815 0817-0828 0830-0834 0836 0838-0843 0845

0847 0849 0853 0940 0945 1001 1055

NOTE : This modification is embodied before delivery on aircraft MSN

0850-0852, 0854-0939, 0941-0944, 0946-1000, 1002-1054, 1056

and subsequent.

DATE : Jun 01/07 SERVICE BULLETIN No. : A330-27-3146

REVISION No. : 01 - Sep 03/08 Page : 1 of 14

Printed in France © AIRBUS 2008 All rights reserved
A330

SERVICE BULLETIN

(b) Effectivity by Operator

The Operator/MSN relationship is provided for information only and is correct at the

time of issue in accordance with the information available to AIRBUS. Any future

changes resulting from transfer of an aircraft from one operator to another will not be

reflected in this list unless the Service Bulletin is revised for another reason.

OPERATOR MSN

99Y 0747

AAR 0640 0676 0708 0772 0803 0845 1001 1055

AEA 0733 0745 0749 0814

CAL 0602 0607 0641 0671 0675 0691 0699 0707 0714 0725 0752

0769 0805 0823 0838

CCA 0750 0756 0759 0780 0785 0797 0810 0815 0839

CES 0713 0720 0728 0732 0735 0773 0777 0781 0782 0791 0821

0830 0836

CPA 0669 0673 0679 0776

CSN 0649 0652 0656 0664 0818 0840

DAH 0644 0647 0650 0653 0667

DLH 0570 0576 0579 0629 0636 0642 0645 0648 0687 0701

EEZ 0665 0802

EIN 0841 0847

ETD 0658 0688 0717 0724 0729 0730 0737 0788 0809 0824 0832

EVA 0555 0573 0587 0634 0655 0661 0678 0693 0755

FWI 0758

HDA 0654 0662 0692 0716 0741 0786

ISR 0822

IWD 0670 0833

IYE 0625 0632

JAI 0751 0807 0825 0831

JST 0842 0853

DATE : Jun 01/07 SERVICE BULLETIN No. : A330-27-3146

REVISION No. : 01 - Sep 03/08 Page : 2

Printed in France © AIRBUS 2008 All rights reserved
A330

SERVICE BULLETIN

OPERATOR MSN

KLM 0682 0686 0703 0738 0770 0801 0811 0819 0834

LTU 0739 0828

MSR 0600 0610 0666 0683 0696 0709 0726

NWA 0524 0533 0542 0549 0552 0578 0588 0591 0609 0614 0618 0620

0621 0631 0633 0663 0674 0690 0718 0722 0778 0784 0796

0799 0806 0817 0827 0843

QAF 0605

QFA 0553 0558 0564 0574 0593 0595 0603 0695 0705 0712 0940 0945

QTR 0571 0612 0616 0623 0637 0638 0659 0680 0684 0711 0721 0734

0743 0746 0760 0789 0792 0813 0820 0826 0849

TAM 0700

TCX 0795

THY 0697 0704 0742 0754 0774

(c) Effectivity by MSN and Kit/Configuration

The Kits and configurations applicable to these MSNs are given at the end of this list

0524 0533 0542 0549 0552-0553 0555 0558 0564 0570-0571 0573-0574 0576

0578-0579 0587-0588 0591 0593 0595 0600 0602-0603 0605 0607 0609-0610 0612

0614 0616 0618 0620-0621 0623 0625 0629 0631-0634 0636-0638 0640-0642

0644-0645 0647-0650 0652-0656 0658-0659 0661-0667 0669-0671 0673-0676

0678-0680 0682-0684 0686-0688 0690-0693 0695-0697 0699-0701 0703-0705

0707-0709 0711-0714 0716-0718 0720-0722 0724-0726 0728-0730 0732-0735

0737-0739 0741-0743 0745-0747 0749-0752 0754-0756 0758-0760 0769-0770

0772-0774 0776-0778 0780-0782 0784-0786 0788-0789 0791-0792 0795-0797

0799 0801-0803 0805-0807 0809-0811 0813-0815 0817-0828 0830-0834 0836

0838-0843 0845 0847 0849 0853 0940 0945 1001 1055

KIT No. QTY PER A/C CONFIGURATION

None 01

NOTE : Config. 01 is valid for all the aircraft given in the effectivity of this Service

Bulletin as a standard configuration.

(3) Spares

FCSC LA2B00300A30000

DATE : Jun 01/07 SERVICE BULLETIN No. : A330-27-3146

REVISION No. : 01 - Sep 03/08 Page : 3

Printed in France © AIRBUS 2008 All rights reserved
A330

SERVICE BULLETIN

B. CONCURRENT REQUIREMENTS

Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishment of the

following Service Bulletin(s) or the equivalent production modification(s):

Service Bulletin No. A330-27-3120 Mod. No. 52378S18007

Service Bulletin No. A330-27-3132 Mod. No. 49965S16501

Mod. No. 51341S16795

Mod. No. 53503S18051

Mod. No. 53504S18052

Service Bulletin No. A330-27-3017 Mod. No. 42983S12314

Service Bulletin No. A330-27-3118 Mod. No. 52017S16877

C. REASON

(1) History

New software standard L19/M18 on Flight Control Secondary Computer was defined in

order to take into account the last FCSC software evolutions.

(2) Objective/Action

This Service Bulletin is published to inform all operators of A330 aircraft of the issue of

AIRBUS FRANCE SAS Service Bulletin No. LA2B0-27-005.

This Service Bulletin recommends introducing new software "L19/M18" PN

LA2B00300A40000 on the two FCSC by means of On Board Replace Module (OBRM)

replacement or reprogramming or FCSCs replacement.

(3) Advantages

Accomplishment of this Service Bulletin introduces the improvements that follow :

- modification of others computers monitoring

- new elevator position monitoring function, which cancels the OEB 50.

- correction of spurious alarm of Pedal Feel and Trim Unit (PFTU).

- modification of parameters record when computer fault.

NOTE : To take into account the "new elevator position monitoring" function at aircraft

level, this new FCSC needs to be associated with Flight Control Primary

Computer (FCPC) P9/M18. A future AD will mandate the modification of both

FCSC and FCPC to permit the cancellation of red OEB 50

NOTE : FCSC STD L19/M18 can be installed on basic aircraft.

(4) Operational/Maintenance Consequences

Accomplishment of this Service Bulletin cancels the OEB if associated with FCPC P9/M18.

AFM is thus impacted only in the case of these associations

DATE : Jun 01/07 SERVICE BULLETIN No. : A330-27-3146

REVISION No. : 01 - Sep 03/08 Page : 4

Printed in France © AIRBUS 2008 All rights reserved
A330

SERVICE BULLETIN

Accomplishment of this Service Bulletin cancels the FCOM TR 335-2.

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

(1) Config. 01

NOTE : To accomplish this Service Bulletin, you have two possibilities :

- either you modify the FCSCs as described in ACCOMPLISHMENT INSTRUCTIONS

paragraph B.(1).(a) below,

- or you replace them as described in ACCOMPLISHMENT INSTRUCTIONS

paragraph B.(1).(b) below.

NOTE : For the modification of the FCSCs by replacement or by reprogramming of their

OBRMs, refer to AIRBUS FRANCE SAS Service Bulletin No. LA2B0-27-005.

(a) In the forward shelf 915VU (for FIN 3CE1) and in the main rack 800VU (for FIN

3CE2), modify the FCSCs by replacement or reprogramming of their OBRMs.

(b) In the forward shelf 915VU (for FIN 3CE1 ) and in the main rack 800VU (for FIN

3CE2 ), replace the FCSCs (FIN 3CE1 and 3CE2 )

E. COMPLIANCE

(1) Classification

Mandatory

(2) Accomplishment Timescale

Accomplishment of this Service Bulletin is expected to be rendered mandatory by the issue

of an Airworthiness Directive (AD) published by the European Aviation Safety Agency

(EASA). The accomplishment timescale, which has not yet been defined, will be given in

the AD.

F. APPROVAL

Approved under the EASA Design Organisation Approval No. EASA.21J.031.

If an aircraft listed in the effectivity has a modification or repair embodied that is not of AIRBUS

origin, and which affects the content of this Service Bulletin, the operator is responsible for

obtaining approval by its airworthiness authority for any adaptation necessary before incorporation

of the Service Bulletin.

G. MANPOWER

The manpower estimates given in this Service Bulletin are based on the direct labor cost to do the

work. These estimates assume that the work will be done by experienced personnel, and may

need to be revised upwards to suit operator’s circumstances. The estimates do not include the

time to prepare, plan or inspect the work. Manufacture and procurement of parts and tools, drying

times for paints, sealants, etc, and general administration work are also not included.

DATE : Jun 01/07 SERVICE BULLETIN No. : A330-27-3146

REVISION No. : 01 - Sep 03/08 Page : 5

Printed in France © AIRBUS 2008 All rights reserved
A330

SERVICE BULLETIN

Config. 01 , on aircraft :

Get access 0.5

Replacement of the two FCSCs 1.0

Test 0.5

Close-Up 0.5

TOTAL MANHOURS 2.5

ELAPSED TIME (HOURS) 2.5

NOTE : For other manhours required for the accomplishment of this Service Bulletin, refer to

AIRBUS FRANCE SAS Service Bulletin No. LA2B0-27-005.

H. WEIGHT AND BALANCE

Not changed

I. ELECTRICAL LOAD DATA

Not changed

J. REFERENCES

Aircraft Maintenance Manual (AMM) : 12-34-24 22-97-00 27-94-34 27-96-00

52-10-00

Elec. Std. Practices Manual (ESPM) : 20-55-00

Service Bulletin No. A330-27-3017

Service Bulletin No. A330-27-3118

Service Bulletin No. A330-27-3120

Service Bulletin No. A330-27-3132

AIRBUS FRANCE SAS LA2B0-27-005

K. PUBLICATIONS AFFECTED

Aircraft Maintenance Manual (AMM) : 27-90-00

Trouble Shooting Manual (TSM) : 27-95-00

Aircraft Wiring Lists (AWL)

Illustrated Parts Catalog (IPC) : 27-94-08 27-94-34

Flight Crew Operating Manual (FCOM) : VOL 1 VOL 3

DATE : Jun 01/07 SERVICE BULLETIN No. : A330-27-3146

REVISION No. : 01 - Sep 03/08 Page : 6

Printed in France © AIRBUS 2008 All rights reserved
A330

SERVICE BULLETIN

If FCSC L19M18 is installed with FCPC P9/M18 (Mod. No. 53468S18201 or Service Bulletin No.

A330-27-3148) VOL 1 is impacted.

This Service Bulletin has an operational impact. Please inform AIRBUS, at least four weeks in

advance, in case you need of your operational documentation to be amended by an intermediate

revision prior to SB embodiment.

For this purpose, please request the intermediate revision by fax, telex or mail to :

SDC3, AIRBUS - Customer Services Directorate

Fax No. (33) 5 61 93 28 06

Sita No. TLSBP7X

E-mail sb.reporting@airbus.com

These amendments will be confirmed by the next normal revision of operational documentation,

once your Service Bulletin accomplishment report has been sent, as usual, to our Customer

Services Directorate (SDC3).

L. INTERCHANGEABILITY/MIXABILITY

DESCRIPTION OLD PART No. NEW PART No. INT MIXABILITY

FCSC LA2B00300A30000 LA2B00300A40000 03 (02)(03)

NOTE : For definitions of interchangeability codes in column INT. refer to ATA Common

Support Data Dictionary (CSDD), Chapter 2.

NOTE(01) Interchangeability code becomes 01 provided that the two FCSCs are replaced at

the same time.

NOTE(02) Not authorized, replacement of the two FCSCs has to be done simultaneously as per

ACCOMPLISHMENT INSTRUCTIONS paragraph B of this Service Bulletin.

NOTE(03) Only the mixability configuration(s) and condition(s) stated in this Service Bulletin

are approved.

DATE : Jun 01/07 SERVICE BULLETIN No. : A330-27-3146

REVISION No. : 01 - Sep 03/08 Page : 7

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SERVICE BULLETIN

This Page Intentionally Left Blank

DATE : Jun 01/07 SERVICE BULLETIN No. : A330-27-3146

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A330

SERVICE BULLETIN

2. MATERIAL INFORMATION

A. MATERIAL - PRICE AND AVAILABILITY

This Service Bulletin is the subject of an AIRBUS retrofit campaign.

B. INDUSTRY SUPPORT INFORMATION

For the organisation of this retrofit, operators are kindly requested to contact AIRBUS retrofit

management department.

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1, Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel :(33) 5 67 19 06 22

E-mail :monitored.retrofit@airbus.com

Fax :(33) 5 61 93 27 45

Modification of parts/equipment is at no charge for the Operator. The man-hours indicated in this

Service Bulletin will remain at the Operators’ cost.

C. LIST OF COMPONENTS

None

D. LIST OF MATERIALS - OPERATOR SUPPLIED

(1) Consumable Materials

None

(2) Components

ITEM NEW PART No. QTY UM KEYWORD ITEM OLD PART No. INT INST DISP

LA2B00300A40000 2 FCSC LA2B00300A30000 03

NOTE : For definitions of interchangeability codes in column INT. refer to ATA Common

Support Data Dictionary (CSDD), Chapter 2.

E. PARTS TO BE RE-IDENTIFIED BY THE OPERATOR

None

F. TOOLING - PRICE AND AVAILABILITY

None

DATE : Jun 01/07 SERVICE BULLETIN No. : A330-27-3146

REVISION No. : 01 - Sep 03/08 Page : 9

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A330

SERVICE BULLETIN

G. SPECIAL TOOLS

None

DATE : Jun 01/07 SERVICE BULLETIN No. : A330-27-3146

REVISION No. : 01 - Sep 03/08 Page : 10

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A330

SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS

A. GENERAL

WARNING : MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONS

INCLUDED IN THE REFERENCED PROCEDURES.

CAUTION : ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP ELECTRICAL

WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY AND MECHANICALLY

SERVICEABLE). WHEN YOU DO MAINTENANCE WORK, REPAIRS OR

MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING, COMPONENTS AND

THE WORK AREA AS CLEAN AS POSSIBLE. TO DO THIS:

PUT PROTECTION, SUCH AS PLASTIC SHEETING, CLOTHS, ETC; AS

NECESSARY ON WIRING AND COMPONENTS.

REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND OTHER

CONTAMINATION.

THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION AND

DAMAGE TO THE ELECTRICAL WIRING INSTALLATION.

IN CASE OF CONTAMINATION REFER TO ESPM 20-55-00.

CAUTION : THE ELECTROSTATIC DISCHARGE PRECAUTIONS DESCRIBED IN ARINC

606 ARE RECOMMENDED.

(1) Preparation

(a) Config. 01

1 Electrically ground the aircraft (Refer to AMM 12-34-24, Page block 201)

2 Put the access platform in position.

3 Open the access door 811 (Refer to AMM 52-10-00, Page block 201)

4 Do the preparation procedure as specified in the removal/installation of the

FCSCs (FIN 3CE1 and 3CE2 ) (Refer to AMM 27-94-34, Page block 401)

(2) Standard Practices

None

B. MODIFICATION

(1) Config. 01

NOTE : To accomplish this Service Bulletin, you have two possibilities :

- either you modify the FCSCs as described in ACCOMPLISHMENT INSTRUCTIONS

paragraph B.(1).(a) below,

- or you replace them as described in ACCOMPLISHMENT INSTRUCTIONS

paragraph B.(1).(b) below.

DATE : Jun 01/07 SERVICE BULLETIN No. : A330-27-3146

REVISION No. : 01 - Sep 03/08 Page : 11

Printed in France © AIRBUS 2008 All rights reserved
A330

SERVICE BULLETIN

NOTE : For the modification of the FCSCs by replacement or by reprogramming of their

OBRMs, refer to AIRBUS FRANCE SAS Service Bulletin No. LA2B0-27-005.

(a) In the forward shelf 915VU (for FIN 3CE1) and in the main rack 800VU (for FIN

3CE2), modify the FCSCs by replacement or reprogramming of their OBRMs.

1 On the FLT CTL section of the overhead panel 241VU (212VU), make sure that

the SEC1 (SEC2) push-button switches are pushed (the OFF and FAULT

legends of these push-button switches are off).

2 Make sure that these circuit breakers are closed :

For FIN 3CE1 :

PANEL DESIGNATION FIN LOCATION

742VU FCSC 1 NORM 10CE1 70 C

742VU FCSC 1 STBY 9CE 77 G

For FIN 3CE2 :

PANEL DESIGNATION FIN LOCATION

722VU FCSC 2 10CE2 39 T

742VU FCSC2 STBY SPLY 41CE 66 D

721VU PRINTER 1TP 02 D

3 Do the BITE test of the Electrical Flight Control System (EFCS) (Line

Replaceable Unit (LRU) identification) (Refer to AMM 27-96-00, Page block 501)

and make sure that the PN LA2B00300A30000 of the FCSC (on the second

page) is in accordance with the vendor Service Bulletin.AIRBUS FRANCE

SASLA2B0-27-005

NOTE : Print the LRU identification page (if the printer is not available, a

visual check is acceptable).

4 Open, safety and tag the circuit breakers given in the removal/installation of

the Flight Control Secondary Computer (FCSC) (FINs 3CE1 and 3CE2) (Refer

to AMM 27-94-34, Page block 401)

5 Replace or reprogram the OBRMs on the FCSCs (FINs 3CE1 and 3CE2)

as per the vendor Service Bulletin.

6 Close the circuit breakers given in the removal/installation of the Flight Control

Secondary Computer (FCSC) (FINs 3CE1 and 3CE2) (Refer to AMM 27-94-34,

Page block 401).

(b) In the forward shelf 915VU (for FIN 3CE1 ) and in the main rack 800VU (for FIN

3CE2 ), replace the FCSCs (FIN 3CE1 and 3CE2 )

Refer to AMM 27-94-34, Page block 401.

1 Remove :

2 FCSC LA2B00300A30000

DATE : Jun 01/07 SERVICE BULLETIN No. : A330-27-3146

REVISION No. : 01 - Sep 03/08 Page : 12

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A330

SERVICE BULLETIN

2 Install :

2 FCSC LA2B00300A40000

C. TEST

(1) Config. 01

(a) Tests after replacement or reprogramming of the OBRMs

1 After power-up, on the FLT CTL section of the overhead panel 241VU (212VU),

make sure that the SEC1 (SEC2) push-button switch(es) is (are) pushed (the

OFF and FAULT legends of this (these) push-button switch(es) is (are) off).

2 If a FAULT is present, do a reset with the concerned push-button switch. If

FAULT persists, replace the concerned computer (Refer to AMM 27-94-34,

Page block 401.

3 Make sure that these circuit breakers are closed :

For FIN 3CE1 :

PANEL DESIGNATION FIN LOCATION

742VU FCSC 1 NORM 10CE1 70 C

742VU FCSC 1 STBY 9CE 77 G

For FIN 3CE2 :

PANEL DESIGNATION FIN LOCATION

722VU FCSC 2 10CE2 39 T

742VU FCSC2 STBY SPLY 41CE 66 D

721VU PRINTER 1TP 02 D

4 Do the BITE Test of the Electrical Flight Control System (EFCS) (Line

Replaceable Unit (LRU) identification) (Refer to AMM 27-96-00, Page block 501)

and make sure that the PN LA2B00300A40000 of the FCSC (on the second

page) is in accordance with the vendor Service Bulletin.AIRBUS FRANCE

SASLA2B0-27-005

NOTE : Print the LRU identification page (if the printer is not available, a

visual check is acceptable).

5 Do the BITE Test of the Electrical Flight Control System (EFCS) (SYSTEM

TEST), (Refer to AMM 27-96-00, Page block 501)

6 If the airline operates the aircraft in CAT 3 conditions, do the LAND CAT III

capability test, (Refer to AMM 22-97-00, Page block 501)

(b) Test after replacements of the EFCSs.

1 Do the test after removal/installation of the Flight Control Secondary Computer

(FCSC) FIN 3CE1 and 3CE2, (Refer to AMM 27-94-34, Page block 401)

DATE : Jun 01/07 SERVICE BULLETIN No. : A330-27-3146

REVISION No. : 01 - Sep 03/08 Page : 13

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A330

SERVICE BULLETIN

D. CLOSE UP

(1) Config. 01

(a) Do the close-up procedure as specified in the removal/installation of the FCSCs (FIN

3CE1 and 3CE2 ) (Refer to AMM 27-94-34, Page block 401)

(b) Restore the systems and the aircraft to normal operating condition.

(c) Make sure that the work areas are clean and clear of tools and other items of

equipment.

(d) Close the access door 811 (Refer to AMM 52-10-00, Page block 201)

(e) Remove the access platform(s).

E. DOCUMENTATION

Write in the applicable aircraft records that you have done all the work given in the Service Bulletin.

DATE : Jun 01/07 SERVICE BULLETIN No. : A330-27-3146

REVISION No. : 01 - Sep 03/08 Page : 14

Printed in France © AIRBUS 2008 All rights reserved
A330

SERVICE BULLETIN

REPORTING SHEET

TITLE : FLIGHT CONTROLS - FCSC - INTRODUCE FCSC STD L19M18 ON A330 A/C.

MODIFICATION No. : 55697S18547

Please complete the appropriate item (A or B):

A - SB WILL BE embodied .................................................................. YES/NO (if NO please comment)

If YES, aircraft concerned (as per SB effectivity by default) and planned dates (month/year) of embodiement:

.............................................................................................................................................................................

.............................................................................................................................................................................

B - SB HAS BEEN embodied on aircraft: ............................................................................................................

.............................................................................................................................................................................

.............................................................................................................................................................................

Operator comments:............................................................................................................................................

.............................................................................................................................................................................

.............................................................................................................................................................................

From Airline: ........................................................................................................................................................

Name/Title: ..........................................................................................................................................................

Signature:..................... Date: .....................................................

If operational documentation is affected (see Paragraph 1.K of this SB): If information is needed prior to next

normal revision or prior to SB embodiment, please indicate required service(s):

Either : Advance data................................................................................... YES/NO

Or : Intermediate/Temporary revision ..................................................... YES/NO

Important Information: This SB will only be incorporated in your maintenance and operational documentation

if this sheet is returned to Airbus and signed by a duly authorised representative. With the next feasible

revision, this will result in

- updating of maintenance documentation to show pre and post SB data.

- updating of maintenance and operational documentation to show post SB data

after embodiment.

If this SB requires previous or simultaneous accomplishment of other SBs, Airbus shall automatically include

them in the manual revisions. Refer to SIL 00-037 for detailed information.

Please return this completed sheet to:

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX FRANCE

Attn: SEDCC1 Technical Data and Documentation Services

FAX: (+33) 5 61 93 28 06

e-mail: sb.reporting@airbus.com

Or via your Resident Customer Support Office.

Alternatively, SB lists via letters or fax are also accepted.

DATE : Jun 01/07 SERVICE BULLETIN No. : A330-27-3146

REVISION No. : 01 - Sep 03/08 Page : 1 of 1

Printed in France © AIRBUS 2008 All rights reserved
A330

SERVICE BULLETIN

REPORTING QUALITY

TITLE : FLIGHT CONTROLS - FCSC - INTRODUCE FCSC STD L19M18 ON A330 A/C.

MODIFICATION No. : 55697S18547

Use this form to tell us what is your perception of the quality of this Service Bulletin.The reported data that you

provide us will be used to analyse areas of difficulties and to take corrective action to futher improve the quality

of our Service Bulletins.

We thank you for the time you have taken in completing this form.

(Please rate on a scale of 1 to 4, with 4 being the highest score)

-Quality rating of this SB 4 3 2 1

-Quality rating of the Accomplishment Instructions 4 3 2 1

-Quality rating of the Illustrations 4 3 2 1

-Is this SB easy to understand ? Y / N

If you have had difficulties in the accomplishment of this SB please quote below the area(s) and give a short

description of the issue.

Planning Material Instructions

X Effectivity X Kit Content X Preparation

X Reason X List of Materials X Mod/Inspection

X Manpower Operator Supplied X Test

X References X Re-identification X Close-up

X Publication X Tooling X Illustrations

Comments :

Operator : Date:

Name/Title :

Please return this form to:

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX FRANCE

Attn: SEMB Service Bulletins Management

FAX: (+33) 5 61 93 42 51

Or via your Resident Customer Support Office.

DATE : Jun 01/07 SERVICE BULLETIN No. : A330-27-3146

REVISION No. : 01 - Sep 03/08 Page : 1 of 1

Printed in France © AIRBUS 2008 All rights reserved