# 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



# MANDATORYMANDATORYMANDATORY
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 5

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# C @A330 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 5

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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 5

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# C @A330 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

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# 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. 

# MANDATORYMANDATORYMANDATORY
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 5

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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 5

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# C @A330 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 5

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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 5

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# C @A330 SERVICE BULLETIN SUMMARY

**CONF ALL

FR20

915VU

800VU 2CE1

2CE2

2CE3 

## A

**B** − Z121 Z122 

### A **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 5

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# C @A330 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 5

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# 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



# MANDATORYMANDATORYMANDATORY
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 5

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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 5

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# C @A330 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 5

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# C @A330 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 5

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# C @A330 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)

DATE: Jul 17/08 SERVICE BULLETIN No.: A330-27-3148 REVISION No.: 01 - Oct 09/08 Page: 5 5

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# C @A330 SERVICE BULLETIN (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. EASA21J.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

DATE: Jul 17/08 SERVICE BULLETIN No.: A330-27-3148 REVISION No.: 01 - Oct 09/08 Page: 6 5

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# C @A330 SERVICE BULLETIN

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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# C @A330 SERVICE BULLETIN

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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# C @A330 SERVICE BULLETIN 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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# C @A330 SERVICE BULLETIN

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# C @A330 SERVICE BULLETIN

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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# C @A330 SERVICE BULLETIN (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 toAIRBUS 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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# C @A330 SERVICE BULLETIN

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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# C @A330 SERVICE BULLETIN
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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# C @A330 SERVICE BULLETIN (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 toAMM 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 toAMM 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 @A330 SERVICE BULLETIN

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 toAMM 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 toAIRBUS FRANCE S.A.S. Service Bulletin No. LA2K2-27-007
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# C @A330 SERVICE BULLETIN (e) Close the circuit breakers given in removal/installation of the three FCPCs (FINs 2CE1, 2CE2 and 2CE3) (Refer toAMM 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 toAMM 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 toAIRBUS 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 toAMM 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 DATE: Jul 17/08 SERVICE BULLETIN No.: A330-27-3148 REVISION No.: 01 - Oct 09/08 Page: 17 5

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# C @A330 SERVICE BULLETIN
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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# C @A330 SERVICE BULLETIN (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 toAMM 27-93-34, Page Block 401).

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# C @A330 SERVICE BULLETIN (d) In the avionics compartment, on the shelf 915VU, modify the FCPC (FINs 2CE1) by replacement or reprogramming of the OBRMs. Refer toAIRBUS 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 toAMM 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 toAMM 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 toAIRBUS 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 toAMM 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

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# C @A330 SERVICE BULLETIN
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 5

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# C @A330 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.

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# C @A330 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 toAMM 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 toAMM 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 5

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# C @A330 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 toAMM 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 toAMM 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 5

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# C @A330 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 toAMM 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 toAMM 27-93-34, Page Block 401).
DATE: Jul 17/08 SERVICE BULLETIN No.: A330-27-3148 REVISION No.: 01 - Oct 09/08 Page: 25 5

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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 5

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# C @A330 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 5

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# C @A330 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. 4 3 2 1 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 5

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# C @A330 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 5

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# C @A330 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 5

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