C@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

ATA SYSTEM: 27

TITLE: FLIGHT CONTROL - FLIGHT CONTROL PRIMARY COMPUTER -

INTRODUCE NEW FCPC STD P9/M18 ON A330 AIRCRAFT.

MODIFICATION No.: 53468S18201

This page transmits Revision No.01 of Service Bulletin No.A330-27-3148

ADDITIONAL WORK

**CONF ALL

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

REASON

Revision No. 01 issued to :

- delete SUBTASK 273148-730-001 001 Test after cancellation of the OEB No. 50 from Config. 01,

- add SUBTASK 273148-730-001 001 Test after cancellation of the OEB No. 50 to Config. 02.

CHANGES

**CONF 001

SUMMARY

MODIFICATIONS MODIFICATION CLASSIFICATION UPDATED

REASON/DESCRIPTION/OPERATIONAL

CONSEQUENCES

SUMMARY REASON UPDATED

EFFECTIVITY SUMMARY EFFECTIVITY UPDATED

REFERENCES / REPERCUSSIONS SUMMARY REFERENCES/REPERCUTIONS UPDATED

MANPOWER SUMMARY MANPOWER UPDATED

PLANNING INFORMATION

EFFECTIVITY EFFECTIVITY UPDATED

MSN Information EFFECTIVITY UPDATED

Configuration definition CONFIGURATION UPDATED

CONFIGURATION DESCRIPTION UPDATED

REASON

DATE: Jul 17/08 SERVICE BULLETIN No.: A330-27-3148

REVISION No.: 01 - Oct 09/08 Page: 1

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Advantages ADVANTAGES UPDATED

Operational/Maintenance

Consequences

OPERATIONAL/MAINTENANCE CONSEQUENCES

UPDATED

MANPOWER MANPOWER UPDATED

CONFIGURATION UPDATED

REFERENCES REFERENCES UPDATED

EXTERNAL REFERENCE UPDATED

PUBLICATION AFFECTED PUBLICATIONS AFFECTED UPDATED

INTERCHANGEABILITY/MIXABILITY INTERCHANGEABILITY/MIXABILITY

MATERIAL INFORMATION

LIST OF MATERIALS - OPERATOR

SUPPLIED

Components

COMP COMPA01 PARTSET UPDATED

PARTS TO BE RE-IDENTIFIED BY

OPERATOR

PARTS TO BY RE-IDENTIFIED BY OPERATOR UPDATED

TOOLING

Tooling - Price and Availability MATERIAL TOOL PRICE UPDATED

ACCOMPLISHMENT INSTRUCTIONS

Task MODIFICATION TASK SOLUTION REVISED

CAUTION UPDATED

Task associated data-001 MAN HOURS UPDATED

ELAPSED TIME UPDATED

Subtask 273148-010-001-001 SUBTASK SOLUTION REVISED

Subtask 273148-831-001-001 SUBTASK SOLUTION REVISED

Subtask 273148-831-002-001 SUBTASK SOLUTION REVISED

Subtask 273148-960-001-001 SUBTASK SOLUTION REVISED

MANPOWER RESSOURCE UPDATED

Subtask 273148-960-002-001 SUBTASK SOLUTION REVISED

MANPOWER RESSOURCE UPDATED

Subtask 273148-740-001-001 SUBTASK SOLUTION REVISED

Subtask 273148-710-001-001 SUBTASK SOLUTION REVISED

Subtask 273148-730-001-001 SUBTASK SOLUTION DELETED FOR APPLICABLE MSN

Subtask 273148-942-001-001 SUBTASK SOLUTION REVISED

**CONF 002

SUMMARY

MODIFICATIONS MODIFICATION CLASSIFICATION UPDATED

REASON/DESCRIPTION/OPERATIONAL

CONSEQUENCES

SUMMARY REASON UPDATED

EFFECTIVITY SUMMARY EFFECTIVITY UPDATED

REFERENCES / REPERCUSSIONS SUMMARY REFERENCES/REPERCUTIONS UPDATED

MANPOWER SUMMARY MANPOWER UPDATED

PLANNING INFORMATION

EFFECTIVITY EFFECTIVITY UPDATED

MSN Information EFFECTIVITY UPDATED

DATE: Jul 17/08 SERVICE BULLETIN No.: A330-27-3148

REVISION No.: 01 - Oct 09/08 Page: 2

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C@A330

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Configuration definition CONFIGURATION UPDATED

CONFIGURATION DESCRIPTION UPDATED

REASON

Advantages ADVANTAGES UPDATED

Operational/Maintenance

Consequences

OPERATIONAL/MAINTENANCE CONSEQUENCES

UPDATED

MANPOWER MANPOWER UPDATED

REFERENCES REFERENCES UPDATED

EXTERNAL REFERENCE UPDATED

PUBLICATION AFFECTED PUBLICATIONS AFFECTED UPDATED

INTERCHANGEABILITY/MIXABILITY INTERCHANGEABILITY/MIXABILITY

MATERIAL INFORMATION

LIST OF MATERIALS - OPERATOR

SUPPLIED

Components

COMP COMPA01 PARTSET UPDATED

PARTS TO BE RE-IDENTIFIED BY

OPERATOR

PARTS TO BY RE-IDENTIFIED BY OPERATOR UPDATED

TOOLING

Tooling - Price and Availability MATERIAL TOOL PRICE UPDATED

ACCOMPLISHMENT INSTRUCTIONS

Task MODIFICATION TASK SOLUTION REVISED

CAUTION UPDATED

Task associated data-002 MAN HOURS UPDATED

ELAPSED TIME UPDATED

Subtask 273148-010-001-001 SUBTASK SOLUTION REVISED

Subtask 273148-831-001-001 SUBTASK SOLUTION REVISED

Subtask 273148-831-002-001 SUBTASK SOLUTION REVISED

Subtask 273148-960-001-001 SUBTASK SOLUTION REVISED

MANPOWER RESSOURCE UPDATED

Subtask 273148-960-002-001 SUBTASK SOLUTION REVISED

MANPOWER RESSOURCE UPDATED

Subtask 273148-740-001-001 SUBTASK SOLUTION REVISED

Subtask 273148-710-001-001 SUBTASK SOLUTION REVISED

Subtask 273148-730-001-001 SUBTASK SOLUTION ADDED

Subtask 273148-942-001-001 SUBTASK SOLUTION REVISED

FILLING INSTRUCTIONS

**CONF ALL

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 revision

DATE: Jul 17/08 SERVICE BULLETIN No.: A330-27-3148

REVISION No.: 01 - Oct 09/08 Page: 3

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

REVISION SEQUENCE

ORIGINAL: Jul 17/08

REVISION No. : 01 - Oct 09/08

DATE: Jul 17/08 SERVICE BULLETIN No.: A330-27-3148

REVISION No.: 01 - Oct 09/08 Page: 4

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
C@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

ATA SYSTEM: 27

TITLE: FLIGHT CONTROL - FLIGHT CONTROL PRIMARY COMPUTER -

INTRODUCE NEW FCPC STD P9/M18 ON A330 AIRCRAFT.

**CONF ALL

MODIFICATIONS

MODIFICATION CLASSIFICATION

MAJOR 53468S18201

MINOR None

NOTE: 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.

REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES

New software standard P9/M18 on Flight Control Primary Computer (FCPC) 2K2 hardware was defined

in order to take into account the last FCPC software solutions.

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

FRANCE S.A.S. Service Bulletin No. LA2K2-27-007.

This Service Bulletin requires introduction of new software standard P9/M18 on FCPC hardware 2K2 by

means of On-Board Replaceable Module (OBRM) on the three FCPCs.

Accomplishment of this Service Bulletin introduces the following modifications :

- new elevator position monitoring,

- improvement of the monitoring of the flight control computer push button switches,

- improvement of monitoring to detect a Trimmable Horizontal Stabilizer Actuator (THSA) manual

command jamming,

- improvement of the double pressurization logic on elevator,

- new monitoring to avoid mixability between different FCPC standards,

DATE: Jul 17/08 SERVICE BULLETIN No.: A330-27-3148

REVISION No.: 01 - Oct 09/08 Page: 1

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C@A330

SERVICE BULLETIN

SUMMARY

- correction of the spurious Electronic Centralized Aircraft Monitoring (ECAM) warning "F/CTL PRIM

X FAULT" due to Digital Output (DGO) First In/First Out (FIFO) full issue (TFU 27.93.00.046),

- use of estimated true airspeed when temperature probes are inoperative,

- introduction of a speed/angle of attack estimation and monitoring,

- correction of the spurious ECAM warning "F/CTL RUD X SERVO FAULT" at engine start or engine

shut down (TFU 27.24.00.009).

The operational maintenance consequences of this Service Bulletin are the modification of the Flight

Crew Operating Manual (FCOM) Vol. 1.

The "new elevator position monitoring" function, that allow to cancel red Operations Engineering

Bulletin (OEB) No. 50, will be active at aircraft level only if Mod. No. 55697S18574 (FLIGHT

CONTROLS - FCSC - INTRODUCE FCSC STD L19M18 ON LR ENHANCED A/C (Service Bulletin No.

A330-27-3146)) is associated with FCPC P9/M18. It is anticipated that an Airworthiness Directive (AD)

will mandate modification of both Flight Control Secondary Computer (FCSC) and FCPC.

After AD issuance, this Service Bulletin will cancel red OEB No. 50 and Aircraft Flight Manual

(AFM) Temporary Revision (TR) 4.02.00/25 if associated with FCSC L19M18 (Service Bulletin No.

A330-27-3146). Operators having programmed an OEB reminder should delete the reminder(s) from

their system.

Only in case of these associations, the operational consequences of this Service Bulletin are the

modification of the Flight Manual (FM).

GENERAL EVALUATION

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

MATERIAL PRICE INFORMATION

**CONF 001

MATERIAL PRICE INFORMATION TABLE

TYPE MATERIAL QUANTITY

PER A/C

PRICE PER

A/C (USD)

MAINPARTS

COMP Component

COMPA01

See SB See SB FCPC

DATE: Jul 17/08 SERVICE BULLETIN No.: A330-27-3148

REVISION No.: 01 - Oct 09/08 Page: 2

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SERVICE BULLETIN

SUMMARY

**CONF 002

MATERIAL PRICE INFORMATION TABLE

TYPE MATERIAL QUANTITY

PER A/C

PRICE PER

A/C (USD)

MAINPARTS

COMP Component

COMPA01

See SB See SB FCPC

EFFECTIVITY

**CONF ALL

This Service Bulletin is applicable to this (these) operator(s) :

10V 46W 99Y AAR AEA CAL CCA CES CHH CPA CSN DAH DLH

EEZ EIN ETD EVA FWI HDA ISR IWD IYE JAI JST KFR KLM

LTU MAU MEA MPD MSR NWA QAF QFA QTR TAM TAP TCX THY

CONCURRENT REQUIREMENTS

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

following Service Bulletin or the equivalent production modification :

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

REFERENCES / REPERCUSSIONS

TFU 27.24.00.009

27.93.00.046

OEB 50

AOT None

SIL None

LINE MAINTENANCE AFFECTED No

LIFE LIMIT None

OTHERS None

NATURE OF THE WORK

AIRCRAFT NO

EQUIPMENT YES

HARD YES

SOFT YES

OBRM YES

DATE: Jul 17/08 SERVICE BULLETIN No.: A330-27-3148

REVISION No.: 01 - Oct 09/08 Page: 3

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C@A330

SERVICE BULLETIN

SUMMARY

MANPOWER

**CONF 001

Task 273148-831-801-001: MODIFICATION

TOTAL MANHOURS 5.00

ELAPSED TIME (HOURS) 4.00

C

Additional manhours related to Vendor SB; refer to:

On shelf 915VU, modify the FCPC (FIN 2CE1) AIRBUS FRANCE S.A.S. Service

Bulletin No. LA2K2-27-007

In electronic panel 800VU, modify the two FCPCs (FINs

2CE2 and 2CE3)

AIRBUS FRANCE S.A.S. Service

Bulletin No. LA2K2-27-007

**CONF 002

Task 273148-831-801-001: MODIFICATION

TOTAL MANHOURS 5.00

ELAPSED TIME (HOURS) 4.00

C

Additional manhours related to Vendor SB; refer to:

On shelf 915VU, modify the FCPC (FIN 2CE1) AIRBUS FRANCE S.A.S. Service

Bulletin No. LA2K2-27-007

In electronic panel 800VU, modify the two FCPCs (FINs

2CE2 and 2CE3)

AIRBUS FRANCE S.A.S. Service

Bulletin No. LA2K2-27-007

APPENDICES

**CONF ALL

Appendix 1 : Elapse Time Calculation

DATE: Jul 17/08 SERVICE BULLETIN No.: A330-27-3148

REVISION No.: 01 - Oct 09/08 Page: 4

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C@A330

SERVICE BULLETIN

SUMMARY

**CONF ALL

FR20

915VU

800VU

2CE1

2CE2

2CE3

A

B

A Z121 Z122 − 

B

G_SB_273148_5_AAAA_01_00

Figure A-FAAAA - Sheet 01

DATE: Jul 17/08 SERVICE BULLETIN No.: A330-27-3148

REVISION No.: 01 - Oct 09/08 Page: 5

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SERVICE BULLETIN

SUMMARY

This Page Intentionally Left Blank

DATE: Jul 17/08 SERVICE BULLETIN No.: A330-27-3148

REVISION No.: 01 - Oct 09/08 Page: 6

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Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
C@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

ATA SYSTEM: 27

TITLE: FLIGHT CONTROL - FLIGHT CONTROL PRIMARY COMPUTER -

INTRODUCE NEW FCPC STD P9/M18 ON A330 AIRCRAFT.

MODIFICATION No.: 53468S18201

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

**CONF ALL

A. EFFECTIVITY

NOTE: This modification is embodied before delivery on A330 aircraft MSN 0948,

0949, 0952, 0956, 0961, 0962, 0963, 0965 and subsequent.

(1) Models

330-201 330-202 330-203 330-223 330-243 330-302 330-303 330-323

330-342 330-343

(2) Effectivity by 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 0849-0855 0857-0863 0865-0869 0871 0873-0877 0879 0881-0885

0887-0893 0895-0896 0898-0901 0903-0909 0911 0913-0916 0918-0920 0922-0923

DATE: Jul 17/08 SERVICE BULLETIN No.: A330-27-3148

REVISION No.: 01 - Oct 09/08 Page: 1

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C@A330

SERVICE BULLETIN

0925-0928 0930-0932 0934-0937 0939-0947 0950-0951 0954 0957-0959 0964

(3) 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

10V 0863

46W 0871 0925

99Y 0747 0951

AAR 0640 0676 0708 0772 0803 0845

AEA 0733 0745 0749 0814 0931 0950

CAL 0602 0607 0641 0671 0675 0691 0699 0707 0714 0725 0752 0769

0805 0823 0838 0861 0920

CCA 0750 0756 0759 0780 0785 0797 0810 0815 0839 0860 0867 0873

0884 0890 0903 0909 0930 0941 0944 0957

CES 0713 0720 0728 0732 0735 0773 0777 0781 0782 0791 0821 0830

0836 0851 0862 0866 0916 0928 0936 0942

CHH 0875 0881 0906 0919

CPA 0669 0673 0679 0776 0850 0855 0895 0915 0959

CSN 0649 0652 0656 0664 0818 0840 0879 0889 0908 0935 0937 0954

0958 0964

DAH 0644 0647 0650 0653 0667

DLH 0570 0576 0579 0629 0636 0642 0645 0648 0687 0701 0896 0905

0913 0922

EEZ 0665 0802

EIN 0841 0847

ETD 0658 0688 0717 0724 0729 0730 0737 0788 0809 0824 0832 0852

0854 0868

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 0882 0885 0888 0901 0923 0932 0947

JST 0842 0853

KFR 0874 0891 0927 0939 0946

KLM 0682 0686 0703 0738 0770 0801 0811 0819 0834 0900

LTU 0739 0828 0911

MAU 0883

MEA 0926

MPD 0943

MSR 0600 0610 0666 0683 0696 0709 0726

DATE: Jul 17/08 SERVICE BULLETIN No.: A330-27-3148

REVISION No.: 01 - Oct 09/08 Page: 2

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SERVICE BULLETIN

OPERATOR MSN

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 0857 0858 0859 0865

QAF 0605

QFA 0553 0558 0564 0574 0593 0595 0603 0695 0705 0712 0887 0892

0898 0940 0945

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

0743 0746 0760 0789 0792 0813 0820 0826 0849 0893 0907 0918

TAM 0700 0869 0876

TAP 0877 0899 0904 0914 0934

TCX 0795

THY 0697 0704 0742 0754 0774

(4) Configuration by MSN

MSN CONFIGURATION

0524 0533 0542 0549 0552 0553 0558 0570 0571 0574 0576

0578 0579 0588 0591 0593 0595 0602 0603 0605 0607 0609

0612 0614 0618 0620 0621 0625 0629 0631 0632 0633 0637

0638 0640 0641 0645 0649 0652 0654 0656 0658 0662 0663

0665 0669 0670 0671 0673 0674 0675 0676 0679 0684 0687

0688 0690 0691 0692 0695 0697 0699 0704 0707 0708 0711

0712 0714 0716 0717 0718 0721 0722 0724 0725 0729 0730

0733 0734 0737 0739 0741 0742 0743 0745 0749 0751 0752

0754 0769 0772 0774 0776 0778 0784 0786 0788 0796 0799

0802 0803 0805 0806 0807 0809 0814 0817 0823 0824 0825

0827 0828 0831 0832 0833 0838 0841 0842 0843 0845 0847

0850 0851 0852 0854 0855 0857 0858 0859 0860 0861 0862

0863 0865 0866 0867 0868 0869 0871 0873 0874 0875 0876

0877 0879 0881 0882 0883 0884 0885 0887 0888 0889 0890

0891 0892 0893 0895 0896 0898 0899 0900 0901 0903 0904

0905 0906 0907 0908 0909 0911 0913 0914 0915 0916 0918

0919 0920 0922 0923 0925 0926 0927 0928 0930 0931 0932

0934 0935 0936 0937 0939 0941 0942 0943 0944 0946 0947

0950 0951 0954 0957 0958 0959 0964

002

0555 0564 0573 0587 0600 0610 0616 0623 0634 0636 0642

0644 0647 0648 0650 0653 0655 0659 0661 0664 0666 0667

0678 0680 0682 0683 0686 0693 0696 0700 0701 0703 0705

0709 0713 0720 0726 0728 0732 0735 0738 0746 0747 0750

0755 0756 0758 0759 0760 0770 0773 0777 0780 0781 0782

0785 0789 0791 0792 0795 0797 0801 0810 0811 0813 0815

0818 0819 0820 0821 0822 0826 0830 0834 0836 0839 0840

0849 0853 0940 0945

001 002

(5) Configuration definition

**CONF 001

Config. 01 is valid for aircraft on which Mod. No. 55697S18574 (INTRODUCE FCSC

STD L19M18 ON LR ENHANCED A/C (Service Bulletin No. A330-27-3146) is not

embodied.

DATE: Jul 17/08 SERVICE BULLETIN No.: A330-27-3148

REVISION No.: 01 - Oct 09/08 Page: 3

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SERVICE BULLETIN

**CONF 002

Config. 02 is valid for aircraft on which Mod. No. 55697S18574 (INTRODUCE FCSC

STD L19M18 ON LR ENHANCED A/C (Service Bulletin No. A330-27-3146)) is

embodied.

NOTE: Selection of config. 01 or config. 02 depends on the aircraft configuration.

(6) Material Effectivity

MATERIAL QTY PER A/C REMARK

Component COMPA01 1

B. CONCURRENT REQUIREMENTS

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

the following Service Bulletin or the equivalent production modification :

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

C. REASON

(1) History

New software standard P9/M18 on Flight Control Primary Computer (FCPC) 2K2

hardware was defined in order to take into account the last FCPC software solutions.

(2) Objective/Action

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

AIRBUS FRANCE S.A.S. Service Bulletin No. LA2K2-27-007.

This Service Bulletin requires introduction of new software standard P9/M18 on FCPC

hardware 2K2 by means of On-Board Replaceable Module (OBRM) on the three FCPCs.

(3) Advantages

Accomplishment of this Service Bulletin introduces the following modifications :

- new elevator position monitoring,

- improvement of the monitoring of the flight control computer push button switches,

- improvement of monitoring to detect a Trimmable Horizontal Stabilizer Actuator

(THSA) manual command jamming,

- improvement of the double pressurization logic on elevator,

- new monitoring to avoid mixability between different FCPC standards,

- correction of the spurious Electronic Centralized Aircraft Monitoring (ECAM) warning

"F/CTL PRIM X FAULT" due to Digital Output (DGO) First In/First Out (FIFO) full

issue (TFU 27.93.00.046),

- use of estimated true airspeed when temperature probes are inoperative,

DATE: Jul 17/08 SERVICE BULLETIN No.: A330-27-3148

REVISION No.: 01 - Oct 09/08 Page: 4

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SERVICE BULLETIN

- introduction of a speed/angle of attack estimation and monitoring,

- correction of the spurious ECAM warning "F/CTL RUD X SERVO FAULT" at engine

start or engine shut down (TFU 27.24.00.009).

(4) Operational/Maintenance Consequences

The operational maintenance consequences of this Service Bulletin are the modification

of the Flight Crew Operating Manual (FCOM) Vol. 1.

The "new elevator position monitoring" function, that allow to cancel red Operations

Engineering Bulletin (OEB) No. 50, will be active at aircraft level only if Mod. No.

55697S18574 (FLIGHT CONTROLS - FCSC - INTRODUCE FCSC STD L19M18 ON LR

ENHANCED A/C (Service Bulletin No. A330-27-3146)) is associated with FCPC P9/M18.

It is anticipated that an Airworthiness Directive (AD) will mandate modification of both

Flight Control Secondary Computer (FCSC) and FCPC.

After AD issuance, this Service Bulletin will cancel red OEB No. 50 and Aircraft Flight

Manual (AFM) Temporary Revision (TR) 4.02.00/25 if associated with FCSC L19M18

(Service Bulletin No. A330-27-3146). Operators having programmed an OEB reminder

should delete the reminder(s) from their system.

Only in case of these associations, the operational consequences of this Service Bulletin

are the modification of the Flight Manual (FM).

D. DESCRIPTION

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

- either you modify the three FCPCs by replacement or reprogramming of

their OBRMs as described in SUBTASK 273148-831-001 001 On shelf

915VU, modify the FCPC (FIN 2CE1) SUBTASK 273148-831-001 001

On shelf 915VU, modify the FCPC (FIN 2CE1) and in SUBTASK

273148-831-002 001 In electronic panel 800VU, modify the two FCPCs

(FINs 2CE2 and 2CE3) SUBTASK 273148-831-002 001 In electronic

panel 800VU, modify the two FCPCs (FINs 2CE2 and 2CE3) ,

- or you replace them as described in SUBTASK 273148-960-001 001 On

shelf 915VU, replace the FCPC (FIN 2CE1) SUBTASK 273148-960-001

001 On shelf 915VU, replace the FCPC (FIN 2CE1) and in SUBTASK

273148-960-002 001 In electronic panel 800VU, replace the two FCPCs

(FINs 2CE2 and 2CE3) SUBTASK 273148-960-002 001 In electronic

panel 800VU, replace the two FCPCs (FINs 2CE2 and 2CE3) .

To accomplish this Service Bulletin it is necessary to :

**CONF 001

Task 273148-831-801-001: MODIFICATION

(1) On shelf 915VU, modify the FCPC (FIN 2CE1)

(2) In electronic panel 800VU, modify the two FCPCs (FINs 2CE2 and 2CE3)

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(3) On shelf 915VU, replace the FCPC (FIN 2CE1)

(4) In electronic panel 800VU, replace the two FCPCs (FINs 2CE2 and 2CE3)

**CONF 002

Task 273148-831-801-001: MODIFICATION

(1) On shelf 915VU, modify the FCPC (FIN 2CE1)

(2) In electronic panel 800VU, modify the two FCPCs (FINs 2CE2 and 2CE3)

(3) On shelf 915VU, replace the FCPC (FIN 2CE1)

(4) In electronic panel 800VU, replace the two FCPCs (FINs 2CE2 and 2CE3)

**CONF ALL

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 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.

**CONF 001

Task 273148-831-801-001: MODIFICATION

Get Access 0.50

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Task 273148-831-801-001: MODIFICATION

On Aircraft

On shelf 915VU, replace the FCPC (FIN 2CE1) 1.00

In electronic panel 800VU, replace the two FCPCs

(FINs 2CE2 and 2CE3)

1.50

Tests 1.00

Close-Up 1.00

TOTAL MANHOURS 5.00

ELAPSED TIME (HOURS) 4.00

C

Additional manhours related to Vendor SB; refer to:

On shelf 915VU, modify the FCPC (FIN 2CE1) AIRBUS FRANCE S.A.S. Service

Bulletin No. LA2K2-27-007

In electronic panel 800VU, modify the two FCPCs

(FINs 2CE2 and 2CE3)

AIRBUS FRANCE S.A.S. Service

Bulletin No. LA2K2-27-007

NOTE: For detail concerning the elapse time calculation, refer to Appendix 1 : Elapse

Time Calculation .

**CONF 002

Task 273148-831-801-001: MODIFICATION

Get Access 0.50

On Aircraft

On shelf 915VU, replace the FCPC (FIN 2CE1) 1.00

In electronic panel 800VU, replace the two FCPCs

(FINs 2CE2 and 2CE3)

1.50

Tests 1.00

Close-Up 1.00

TOTAL MANHOURS 5.00

ELAPSED TIME (HOURS) 4.00

C

Additional manhours related to Vendor SB; refer to:

On shelf 915VU, modify the FCPC (FIN 2CE1) AIRBUS FRANCE S.A.S. Service

Bulletin No. LA2K2-27-007

In electronic panel 800VU, modify the two FCPCs

(FINs 2CE2 and 2CE3)

AIRBUS FRANCE S.A.S. Service

Bulletin No. LA2K2-27-007

**CONF ALL

H. WEIGHT AND BALANCE

Not Changed

I. ELECTRICAL LOAD DATA

Not Changed

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J. REFERENCES

**CONF 001

Aircraft Maintenance Manual (AMM) 12-34-24 22-97-00 27-93-34

27-96-00

ATA Common Support Data Dictionary (CSDD),

Chapter 2

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

Service Bulletin (SB) A330-27-3118

A330-27-3146

Vendor Service Bulletin (VSB) AIRBUS FRANCE S.A.S. Service

Bulletin No. LA2K2-27-007

AIRBUS FRANCE S.A.S. Service

Bulletin No. LA2K2-27-007

**CONF 002

Aircraft Maintenance Manual (AMM) 12-34-24 22-97-00 27-93-34

27-96-00 31-51-00

ATA Common Support Data Dictionary (CSDD),

Chapter 2

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

Service Bulletin (SB) A330-27-3118

A330-27-3146

Vendor Service Bulletin (VSB) AIRBUS FRANCE S.A.S. Service

Bulletin No. LA2K2-27-007

AIRBUS FRANCE S.A.S. Service

Bulletin No. LA2K2-27-007

**CONF ALL

K. PUBLICATION AFFECTED

Aircraft Wiring List (AWL)

Flight Crew Operating Manual (FCOM) VOL 1

Flight Manual (FM)

Illustrated Parts Catalog (IPC) 27-93-08 27-93-34

Aircraft Flight Manual (AFM) Temporary Revision (TR) 4.02.00/25

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

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

intermediate revision prior to Service Bulletin embodiment. For this purpose, please request

the intermediate revision by fax, telex or mail to :

SEDCC, AIRBUS - Customer Services Directorate

Fax No. : 33 (0) 5 61 93 28 06

Sita No. : TLSBP7X

E-mail : sb.reporting@airbus.com

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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

**CONF 001

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY REMARK

FCPC LA2K2B100D80000 LA2K2B100DB0000 03 See note(s) (1) (2) (3)

NOTE (1): For definitions of interchangeability codes in column INT., refer to ATA

Common Support Data Dictionary (CSDD), Chapter 2.

NOTE (2): Mixability not authorized. Replacement of the three FCPCs has to be done

simultaneously as per ACCOMPLISHMENT INSTRUCTIONS paragraph C.

NOTE (3): Only the mixability configuration(s) and condition(s) stated in this Service

Bulletin are approved.

**CONF 002

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY REMARK

FCPC LA2K2B100D80000 LA2K2B100DB0000 03 See note(s) (1) (2) (3)

NOTE (1): For definitions of interchangeability codes in column INT., refer to ATA

Common Support Data Dictionary (CSDD), Chapter 2.

NOTE (2): Mixability not authorized. Replacement of the three FCPCs has to be done

simultaneously as per ACCOMPLISHMENT INSTRUCTIONS paragraph C.

NOTE (3): Only the mixability configuration(s) and condition(s) stated in this Service

Bulletin are approved.

**CONF ALL

M. SPARES

FCPC LA2K2B100D80000

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This Page Intentionally Left Blank

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2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

(1) Procurement Addresses

Component COMPA01 Vendor parts are to be purchased from :

AIRBUS FRANCE S.A.S.

Avionics and simulation products

316, route de Bayonne

31060 TOULOUSE Cedex 09

FRANCE

Tel : (33) 5 61 93 55 55

Telex : AISPA 531546F

This Service Bulletin is the subject of an

AIRBUS monitored retrofit campaign.

(2) Price and Availability

Refer to the vendor Service Bulletin No. LA2K2-27-007 for the equipment modification

sales terms.

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

No Kit

D. LIST OF MATERIALS - OPERATOR SUPPLIED

(1) Consumable Materials

None

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(2) Components

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT REMARK

LA2K2B100DB0000 3 FCPC LA2K2B100D80000 03 (1)(2)(3)

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

Common Support Data Dictionary (CSDD), Chapter 2.

NOTE (1): Mixability not authorized. Replacement of the three FCPCs has to

be done simultaneously as per ACCOMPLISHMENT INSTRUCTIONS

paragraph C.

NOTE (2): Only the mixability configuration(s) and condition(s) stated in this Service

Bulletin are approved.

NOTE (3): Modification of removed equipment should be negotiated directly with

AIRBUS FRANCE S.A.S. as per instructions given in Service Bulletin No.

LA2K2-27-007.

(3) Equipment

None

E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

Refer to AIRBUS FRANCE S.A.S. Service Bulletin No. LA2K2-27-007

F. TOOLING

(1) Tooling - Price and Availability

To accomplish this Service Bulletin it is necessary to use the tools defined in AIRBUS

FRANCE S.A.S. Service Bulletin No. LA2K2-27-007.

(2) Tools

None

(3) Special Tools

None

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3. ACCOMPLISHMENT INSTRUCTIONS

Task 273148-831-801-001 - MODIFICATION

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

REPORT 606 ARE RECOMMENDED.

Task Associated Data

**CONF 001

Zone From 121 to 122

Modified FIN 2CE1 2CE2 2CE3

Access Door 811

Manpower

TOTAL MANHOURS 5.00

ELAPSED TIME (HOURS) 4.00

C

Additional manhours related to Vendor SB; refer

to:

AIRBUS FRANCE S.A.S. Service

Bulletin No. LA2K2-27-007

AIRBUS FRANCE S.A.S. Service

Bulletin No. LA2K2-27-007

**CONF 002

Zone From 121 to 122

Modified FIN 2CE1 2CE2 2CE3

Access Door 811

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Manpower

TOTAL MANHOURS 5.00

ELAPSED TIME (HOURS) 4.00

C

Additional manhours related to Vendor SB; refer

to:

AIRBUS FRANCE S.A.S. Service

Bulletin No. LA2K2-27-007

AIRBUS FRANCE S.A.S. Service

Bulletin No. LA2K2-27-007

A. GENERAL

**CONF 001

(1) Subtask 273148-839-001-001 - DOCUMENTATION

Manpower Resources

Skills NON SPECIFIC

Write in the applicable aircraft records that you have done all the work given in this

Service Bulletin.

**CONF 002

(1) Subtask 273148-839-001-001 - DOCUMENTATION

Manpower Resources

Skills NON SPECIFIC

Write in the applicable aircraft records that you have done all the work given in this

Service Bulletin.

B. PREPARATION

**CONF 001

(1) Subtask 273148-010-001-001 - Get access to the three FCPCs (FINs 2CE1, 2CE2 and

2CE3)

Work Zones and Access Panels

Zone Access/Work location

From 121 Access to open Door 811

To 122

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 12-34-24, Page Block 201

27-93-34, Page Block 401

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(a) Make sure that the aircraft is electrically grounded (Refer to AMM 12-34-24, Page

Block 201).

(b) Put the access platform(s) in position.

(c) Open the passenger/crew door(s).

(d) Do the preparation procedure as specified in the removal/installation of the three

FCPCs (FINs 2CE1, 2CE2 and 2CE3) (Refer to AMM 27-93-34, Page Block 401).

(e) If you modify the three FCPCs by replacement or reprogramming of their OBRMs

as described in SUBTASK 273148-831-001 001 On shelf 915VU, modify the FCPC

(FIN 2CE1) and in SUBTASK 273148-831-002 001 In electronic panel 800VU,

modify the two FCPCs (FINs 2CE2 and 2CE3) :

1 close the circuits breakers given in removal/installation of the three FCPCs

(FINs 2CE1, 2CE2 and 2CE3) (Refer to AMM 27-93-34, Page Block 401).

**CONF 002

(1) Subtask 273148-010-001-001 - Get access to the three FCPCs (FINs 2CE1, 2CE2 and

2CE3)

Work Zones and Access Panels

Zone Access/Work location

From 121 Access to open Door 811

To 122

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 12-34-24, Page Block 201

27-93-34, Page Block 401

(a) Make sure that the aircraft is electrically grounded (Refer to AMM 12-34-24, Page

Block 201).

(b) Put the access platform(s) in position.

(c) Open the passenger/crew door(s).

(d) Do the preparation procedure as specified in the removal/installation of the three

FCPCs (FINs 2CE1, 2CE2 and 2CE3) (Refer to AMM 27-93-34, Page Block 401).

(e) If you modify the three FCPCs by replacement or reprogramming of their OBRMs

as described in SUBTASK 273148-831-001 001 On shelf 915VU, modify the FCPC

(FIN 2CE1) and in SUBTASK 273148-831-002 001 In electronic panel 800VU,

modify the two FCPCs (FINs 2CE2 and 2CE3) :

1 close the circuits breakers given in removal/installation of the three FCPCs

(FINs 2CE1, 2CE2 and 2CE3) (Refer to AMM 27-93-34, Page Block 401).

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C. PROCEDURE

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

- either you modify the three FCPCs by replacement or reprogramming of

their OBRMs as described in SUBTASK 273148-831-001 001 On shelf

915VU, modify the FCPC (FIN 2CE1) SUBTASK 273148-831-001 001

On shelf 915VU, modify the FCPC (FIN 2CE1) and in SUBTASK

273148-831-002 001 In electronic panel 800VU, modify the two FCPCs

(FINs 2CE2 and 2CE3) SUBTASK 273148-831-002 001 In electronic

panel 800VU, modify the two FCPCs (FINs 2CE2 and 2CE3) below,

- or you replace them as described in SUBTASK 273148-960-001 001 On

shelf 915VU, replace the FCPC (FIN 2CE1) SUBTASK 273148-960-001

001 On shelf 915VU, replace the FCPC (FIN 2CE1) and in SUBTASK

273148-960-002 001 In electronic panel 800VU, replace the two FCPCs

(FINs 2CE2 and 2CE3) SUBTASK 273148-960-002 001 In electronic

panel 800VU, replace the two FCPCs (FINs 2CE2 and 2CE3) below.

**CONF 001

(1) Subtask 273148-831-001-001 - On shelf 915VU, modify the FCPC (FIN 2CE1)

Work Zones and Access Panels

Zone Access/Work location

From 121 Access to open Door 811

Work location 915VU

To 122

References

Aircraft Maintenance Manual (AMM) 27-93-34, Page Block 401

27-96-00, Page Block 501

Vendor Service Bulletin (VSB) AIRBUS FRANCE S.A.S. LA2K2-27-007

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

PRIM 1 (PRIM 2) (PRIM 3) pushbutton switch(es) is(are) pushed (the OFF and

FAULT legends of this (these) pusbutton switch(es) are off).

(b) Do the Built-In Test Equipment (BITE) test of the Electronic Flight Control Computer

(EFCS) (LRU IDENT) (Refer to AMM 27-96-00, Page Block 501) and make sure

that the PN of the FCPCs is :

LA2K2B100D80000.

(c) Open, safety and tag the circuit breakers given in removal/installation of the FCPCs

(FINs 2CE1, 2CE2 and 2CE3) (Refer to AMM 27-93-34, Page Block 401).

(d) In the avionics compartment, on the shelf 915VU, modify the FCPC (FINs 2CE1) by

replacement or reprogramming of the OBRMs.

Refer to AIRBUS FRANCE S.A.S. Service Bulletin No. LA2K2-27-007

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(e) Close the circuit breakers given in removal/installation of the three FCPCs (FINs

2CE1, 2CE2 and 2CE3) (Refer to AMM 27-93-34, Page Block 401).

(2) Subtask 273148-831-002-001 - In electronic panel 800VU, modify the two FCPCs (FINs

2CE2 and 2CE3)

Work Zones and Access Panels

Zone Access/Work location

From 121 Access to open Door 811

Work location 800VU

To 122

References

Aircraft Maintenance Manual (AMM) 27-93-34, Page Block 401

27-96-00, Page Block 501

Vendor Service Bulletin (VSB) AIRBUS FRANCE S.A.S. LA2K2-27-007

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

PRIM 1 (PRIM 2) (PRIM 3) pushbutton switch(es) is(are) pushed (the OFF and

FAULT legends of this (these) pusbutton switch(es) are off).

(b) Do the BITE test of the EFCS (LRU IDENT) (Refer to AMM 27-96-00, Page Block

501) and make sure that the PN of the FCPCs is :

LA2K2B100D80000.

(c) Open, safety and tag the circuit breakers given in removal/installation of the FCPCs

(FINs 2CE1, 2CE2 and 2CE3) (Refer to AMM 27-93-34, Page Block 401).

(d) In the avionics compartment, on the electronic panel 800VU, modify the three

FCPCs (FINs 2CE1, 2CE2 and 2CE3) by replacement or reprogramming of the

OBRMs.

Refer to AIRBUS FRANCE S.A.S. Service Bulletin No. LA2K2-27-007

(e) Close the circuit breakers given in removal/installation of the three FCPCs (FINs

2CE1, 2CE2 and 2CE3) (Refer to AMM 27-93-34, Page Block 401).

(3) Subtask 273148-960-001-001 - On shelf 915VU, replace the FCPC (FIN 2CE1)

Work Zones and Access Panels

Zone Access/Work location

From 121 Access to open Door 811

Work location 915VU

To 122

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

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Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD

LA2K2B100DB0000 1 FCPC

References

Aircraft Maintenance Manual (AMM) 27-93-34, Page Block 401

(a) In the avionics compartment, on the shelf 915VU, replace the FCPC (FIN 2CE1).

Refer to AMM 27-93-34, Page Block 401

1 Remove :

FIN 2CE1

1 FCPC LA2K2B100D80000

2 Install :

FIN 2CE1

1 FCPC LA2K2B100DB0000

(4) Subtask 273148-960-002-001 - In electronic panel 800VU, replace the two FCPCs (FINs

2CE2 and 2CE3)

Work Zones and Access Panels

Zone Access/Work location

From 121 Access to open Door 811

Work location 800VU

To 122

Manpower Resources

Manhours 1.50

Minimum number of person 1

Subtask elapsed time 1.50

Skills NON SPECIFIC

Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD

LA2K2B100DB0000 2 FCPC

References

Aircraft Maintenance Manual (AMM) 27-93-34, Page Block 401

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(a) In the avionics compartment on the electronic panel 800VU, replace the two FCPCs

(FINs 2CE2 and 2CE3).

Refer to AMM 27-93-34, Page Block 401

1 Remove :

FIN 2CE2

1 FCPC LA2K2B100D80000

FIN 2CE3

1 FCPC LA2K2B100D80000

2 Install :

FIN 2CE2

1 FCPC LA2K2B100DB0000

FIN 2CE3

1 FCPC LA2K2B100DB0000

**CONF 002

(1) Subtask 273148-831-001-001 - On shelf 915VU, modify the FCPC (FIN 2CE1)

Work Zones and Access Panels

Zone Access/Work location

From 121 Access to open Door 811

Work location 915VU

To 122

References

Aircraft Maintenance Manual (AMM) 27-93-34, Page Block 401

27-96-00, Page Block 501

Vendor Service Bulletin (VSB) AIRBUS FRANCE S.A.S. LA2K2-27-007

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

PRIM 1 (PRIM 2) (PRIM 3) pushbutton switch(es) is(are) pushed (the OFF and

FAULT legends of this (these) pusbutton switch(es) are off).

(b) Do the Built-In Test Equipment (BITE) test of the Electronic Flight Control Computer

(EFCS) (LRU IDENT) (Refer to AMM 27-96-00, Page Block 501) and make sure

that the PN of the FCPCs is :

LA2K2B100D80000.

(c) Open, safety and tag the circuit breakers given in removal/installation of the FCPCs

(FINs 2CE1, 2CE2 and 2CE3) (Refer to AMM 27-93-34, Page Block 401).

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(d) In the avionics compartment, on the shelf 915VU, modify the FCPC (FINs 2CE1) by

replacement or reprogramming of the OBRMs.

Refer to AIRBUS FRANCE S.A.S. Service Bulletin No. LA2K2-27-007

(e) Close the circuit breakers given in removal/installation of the three FCPCs (FINs

2CE1, 2CE2 and 2CE3) (Refer to AMM 27-93-34, Page Block 401).

(2) Subtask 273148-831-002-001 - In electronic panel 800VU, modify the two FCPCs (FINs

2CE2 and 2CE3)

Work Zones and Access Panels

Zone Access/Work location

From 121 Access to open Door 811

Work location 800VU

To 122

References

Aircraft Maintenance Manual (AMM) 27-93-34, Page Block 401

27-96-00, Page Block 501

Vendor Service Bulletin (VSB) AIRBUS FRANCE S.A.S. LA2K2-27-007

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

PRIM 1 (PRIM 2) (PRIM 3) pushbutton switch(es) is(are) pushed (the OFF and

FAULT legends of this (these) pusbutton switch(es) are off).

(b) Do the BITE test of the EFCS (LRU IDENT) (Refer to AMM 27-96-00, Page Block

501) and make sure that the PN of the FCPCs is :

LA2K2B100D80000.

(c) Open, safety and tag the circuit breakers given in removal/installation of the FCPCs

(FINs 2CE1, 2CE2 and 2CE3) (Refer to AMM 27-93-34, Page Block 401).

(d) In the avionics compartment, on the electronic panel 800VU, modify the three

FCPCs (FINs 2CE1, 2CE2 and 2CE3) by replacement or reprogramming of the

OBRMs.

Refer to AIRBUS FRANCE S.A.S. Service Bulletin No. LA2K2-27-007

(e) Close the circuit breakers given in removal/installation of the three FCPCs (FINs

2CE1, 2CE2 and 2CE3) (Refer to AMM 27-93-34, Page Block 401).

(3) Subtask 273148-960-001-001 - On shelf 915VU, replace the FCPC (FIN 2CE1)

Work Zones and Access Panels

Zone Access/Work location

From 121 Access to open Door 811

Work location 915VU

To 122

DATE: Jul 17/08 SERVICE BULLETIN No.: A330-27-3148

REVISION No.: 01 - Oct 09/08 Page: 20

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Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD

LA2K2B100DB0000 1 FCPC

References

Aircraft Maintenance Manual (AMM) 27-93-34, Page Block 401

(a) In the avionics compartment, on the shelf 915VU, replace the FCPC (FIN 2CE1).

Refer to AMM 27-93-34, Page Block 401

1 Remove :

FIN 2CE1

1 FCPC LA2K2B100D80000

2 Install :

FIN 2CE1

1 FCPC LA2K2B100DB0000

(4) Subtask 273148-960-002-001 - In electronic panel 800VU, replace the two FCPCs (FINs

2CE2 and 2CE3)

Work Zones and Access Panels

Zone Access/Work location

From 121 Access to open Door 811

Work location 800VU

To 122

Manpower Resources

Manhours 1.50

Minimum number of person 1

Subtask elapsed time 1.50

Skills NON SPECIFIC

Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD

LA2K2B100DB0000 2 FCPC

DATE: Jul 17/08 SERVICE BULLETIN No.: A330-27-3148

REVISION No.: 01 - Oct 09/08 Page: 21

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SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) 27-93-34, Page Block 401

(a) In the avionics compartment on the electronic panel 800VU, replace the two FCPCs

(FINs 2CE2 and 2CE3).

Refer to AMM 27-93-34, Page Block 401

1 Remove :

FIN 2CE2

1 FCPC LA2K2B100D80000

FIN 2CE3

1 FCPC LA2K2B100D80000

2 Install :

FIN 2CE2

1 FCPC LA2K2B100DB0000

FIN 2CE3

1 FCPC LA2K2B100DB0000

D. TEST

**CONF 001

(1) Subtask 273148-740-001-001 - Tests after replacement or reprogramming of the OBRMs

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 22-97-00, Page Block 501

27-93-34, Page Block 401

27-96-00, Page Block 501

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

make sure that the PRIM 1 (PRIM 2) (PRIM 3) pushbutton switch(es) is(are)

pushed (the OFF and FAULT legends of this (these) pusbutton switch(es) are off).

If a FAULT is present, do a reset with the concerned pushbutton switch. If FAULT

persists, replace the concerned computer (Refer to AMM 27-93-34, Page Block

401).

(b) Do the BITE test of the EFCS (LRU IDENT) (Refer to AMM 27-96-00, Page Block

501) and make sure that the PN of the FCPCs is :

PN LA2K2B100DB0000.

DATE: Jul 17/08 SERVICE BULLETIN No.: A330-27-3148

REVISION No.: 01 - Oct 09/08 Page: 22

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SERVICE BULLETIN

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

a visual check is acceptable).

(c) Do the BITE test of the EFCS (SYSTEM TEST) (Refer to AMM 27-96-00, Page

Block 501).

(d) If the airline operates the aircraft in Category (CAT) 3, do the LAND CAT III

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

(2) Subtask 273148-710-001-001 - Tests after replacement of the FCPCs

Work Zones and Access Panels

Zone Access/Work location

From 121

To 122

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 27-93-34, Page Block 401

(a) Do the test after the removal/installation of the FCPCs (FINs 2CE1, 2CE2 and

2CE3) (Refer to AMM 27-93-34, Page Block 401).

(3) Subtask 273148-730-001-001

Deleted

**CONF 002

(1) Subtask 273148-740-001-001 - Tests after replacement or reprogramming of the OBRMs

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 22-97-00, Page Block 501

27-93-34, Page Block 401

27-96-00, Page Block 501

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

make sure that the PRIM 1 (PRIM 2) (PRIM 3) pushbutton switch(es) is(are)

pushed (the OFF and FAULT legends of this (these) pusbutton switch(es) are off).

If a FAULT is present, do a reset with the concerned pushbutton switch. If FAULT

persists, replace the concerned computer (Refer to AMM 27-93-34, Page Block

401).

DATE: Jul 17/08 SERVICE BULLETIN No.: A330-27-3148

REVISION No.: 01 - Oct 09/08 Page: 23

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SERVICE BULLETIN

(b) Do the BITE test of the EFCS (LRU IDENT) (Refer to AMM 27-96-00, Page Block

501) and make sure that the PN of the FCPCs is :

PN LA2K2B100DB0000.

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

a visual check is acceptable).

(c) Do the BITE test of the EFCS (SYSTEM TEST) (Refer to AMM 27-96-00, Page

Block 501).

(d) If the airline operates the aircraft in Category (CAT) 3, do the LAND CAT III

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

(2) Subtask 273148-710-001-001 - Tests after replacement of the FCPCs

Work Zones and Access Panels

Zone Access/Work location

From 121

To 122

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 27-93-34, Page Block 401

(a) Do the test after the removal/installation of the FCPCs (FINs 2CE1, 2CE2 and

2CE3) (Refer to AMM 27-93-34, Page Block 401).

(3) Subtask 273148-730-001-001 - Test after cancellation of the OEB No. 50

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 31-51-00, Page Block 301

(a) On aircraft equipped with OEB REMINDER function, if the ECAM warning has been

flagged as described in OEB No. 50, the following codes should be deleted from

the Flight Warning Computer (FWC) database :

Refer to AMM 31-51-00, Page Block 301 ("delete OEB REMINDER information

from FWCs using MCDUs")

CODE WARN STS

PRIM 1 FAULT

27/90/050/113

NO YES

PRIM 1 PITCH FAULT

27/90/200/109

NO YES

ELEV SERVO FAULT

27/30/050/083

NO YES

DATE: Jul 17/08 SERVICE BULLETIN No.: A330-27-3148

REVISION No.: 01 - Oct 09/08 Page: 24

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SERVICE BULLETIN

G SYS LO PR

29/11/060/091

NO YES

E. CLOSE-UP

**CONF 001

(1) Subtask 273148-942-001-001 - Close access

Work Zones and Access Panels

Zone Access/Work location

From 121 Access to open Door 811

Work location 800VU

915VU

To 122

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 27-93-34, Page Block 401

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

(FINs 2CE1, 2CE2 and 2CE3) (Refer to AMM 27-93-34, Page Block 401).

(b) Close the passenger/crew door(s).

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

(d) Remove the access platform(s).

**CONF 002

(1) Subtask 273148-942-001-001 - Close access

Work Zones and Access Panels

Zone Access/Work location

From 121 Access to open Door 811

Work location 800VU

915VU

To 122

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 27-93-34, Page Block 401

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

(FINs 2CE1, 2CE2 and 2CE3) (Refer to AMM 27-93-34, Page Block 401).

DATE: Jul 17/08 SERVICE BULLETIN No.: A330-27-3148

REVISION No.: 01 - Oct 09/08 Page: 25

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C@A330

SERVICE BULLETIN

(b) Close the passenger/crew door(s).

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

(d) Remove the access platform(s).

DATE: Jul 17/08 SERVICE BULLETIN No.: A330-27-3148

REVISION No.: 01 - Oct 09/08 Page: 26

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SERVICE BULLETIN

Appendix 1 : Elapse Time Calculation

DATE: Jul 17/08 SERVICE BULLETIN No.: A330-27-3148

REVISION No.: 01 - Oct 09/08 Page: 1

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SERVICE BULLETIN

Appendix 1 : Elapse Time Calculation

**CONF ALL

**CONF ALL

ELAPSED TIME CALCULATION SERVICE BULLETIN No. A330−27−3148

5.0

4.0

2

TOTAL MANHOURS (MH)

ELAPSED TIME (ET)

NUMBER OF PEOPLE

NOTE:

STEPS

HOURS 0 5

MODIFICATION

IN 800 VU

CLOSE−UP

1

MH

0.5

ET

0.5

TEST

MODIFICATION

IN 915 VU

GET ACCESS

1

MH

1.5

ET

1.5

1

MH

1.0

ET

1.0

THIS CHART IS ONLY A PROPOSAL.

OPERATORS MAY DETERMINE THAT ANOTHER WAY

TO DO THE WORK IS MORE SUITABLE FOR THEM.

1 2 3 4

1

MH

1.0

ET

1.0

1

MH

1.0

ET

1.0

G_SB_273148_5_ABAA_01_00

Figure A-FABAA - Sheet 01

Elapse Time Calculation

DATE: Jul 17/08 SERVICE BULLETIN No.: A330-27-3148

REVISION No.: 01 - Oct 09/08 Page: 2

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SERVICE BULLETIN

REPORTING SHEET

TITLE: FLIGHT CONTROL - FLIGHT CONTROL PRIMARY COMPUTER -

INTRODUCE NEW FCPC STD P9/M18 ON A330 AIRCRAFT.

MODIFICATION No.: 53468S18201

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

embodiment:

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: Modification Operational Impact (MOI), if available YES/NO

Or : Intermediate 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: SDC32 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: Jul 17/08 SERVICE BULLETIN No.: A330-27-3148

REVISION No.: 01 - Oct 09/08 Page: 1

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SERVICE BULLETIN

QUALITY PERCEPTION FORM

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 further

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 Operator Supplied X Mod/Inspection

X Manpower X Industry support 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 : SEM4 Service Bulletins Management

FAX : (33) 5 61 93 42 51

Or via your Resident Customer Support Office.

DATE: Jul 17/08 SERVICE BULLETIN No.: A330-27-3148

REVISION No.: 01 - Oct 09/08 Page: 1

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