# @A318/A319/A320/A321 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 ATA SYSTEM: 22 

### TITLE: AUTO FLIGHT - FLIGHT AUGMENTATION COMPUTER (FAC) - INSTALL FAC B623 (SHARKLET PROJECT) MODIFICATION No.: 30439P6703 31040P6954 33299P8256 35522P9122 36766P9906 38777P10777 160011P12126 160065P13119 This page transmits Revision No.07 of Service Bulletin No.A320-22-1461 ADDITIONAL WORK **CONF ALL No additional work is required by this revision for aircraft modified by any previous issue. REASON Revision No. 07 issued to add aircraft MSN 5760 and 5799 for operator GCR. CHANGES The main changes of this revision are: - Effectivity extended - CONCURRENT REQUIREMENTS paragraph updated. SUMMARY EFFECTIVITY OPERATOR LIST UPDATED R CONCURRENT REQUIREMENTS CONCURRENT REQUIREMENTS UPDATED R PLANNING INFORMATION EFFECTIVITY EFFECTIVITY RELATED INFORMATION UPDATED R Configuration definition CONF 001 CONFIGURATION DEFINITION UPDATED R CONCURRENT REQUIREMENTS CONCURRENT SB LIST UPDATED R FILING INSTRUCTIONS This Service Bulletin has been generated electronically and is reissued as a complete document. Replace the complete document.

DATE: Oct 31/13 SERVICE BULLETIN No.: A320-22-1461 REVISION No.: 07 - Mar 23/15 Page: 1 5

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# @A318/A319/A320/A321 SERVICE BULLETIN REVISION TRANSMITTAL SHEET Put this Revision Transmittal Sheet in front of the Service Bulletin. HISTORY OF PREVIOUS REVISIONS Revision No. 01 issued to add aircraft MSN 5538 for operator MLM, aircraft MSN 5528 for operator TAM and aircraft MSN 5715 and 5747 for PAL. Revision No. 02 issued to add aircraft MSN 5559 and 5607 for operator SBI. Revision No. 03 issued to add aircraft MSN 5605 and 5662 for operator MDL and aircraft MSN 4858, 4930, 4968, 5010, 5078 and 5127 for operator QTR. Revision No. 04 issued to add aircraft MSN 5488 for operator VOI, and aircraft MSN 5562 for operator CQH. Revision No. 05 issued to add aircraft MSN 5485 for operator EVA, aircraft MSN 5446 for operator CQH and aircraft MSN 5630 5656 and 5722 for operator CBJ. Revision No. 06 issued to add aircraft for operators 15T, AFL, CHB, MLM, JBU, TAP, TBA and THY. REVISION SEQUENCE ORIGINAL: Oct 31/13 REVISION No. : 01 - Feb 25/14 REVISION No. : 02 - Apr 30/14 REVISION No. : 03 - Jul 17/14 REVISION No. : 04 - Sep 15/14 REVISION No. : 05 - Nov 13/14 REVISION No. : 06 - Jan 21/15 REVISION No. : 07 - Mar 23/15

DATE: Oct 31/13 SERVICE BULLETIN No.: A320-22-1461 REVISION No.: 07 - Mar 23/15 Page: 2 5

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# @A318/A319/A320/A321 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. ATA SYSTEM: 22 

### TITLE: AUTO FLIGHT - FLIGHT AUGMENTATION COMPUTER (FAC) - INSTALL FAC B623 (SHARKLET PROJECT) **CONF ALL MODIFICATIONS MODIFICATION CLASSIFICATION 30439P6703 31040P6954 33299P8256 35522P9122 36766P9906 MAJOR 38777P10777 160011P12126 160065P13119 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 This Service Bulletin is issued further to an operator’s request. In the frame of Sharklet upgrade, this Service Bulletin allows the installation of the Flight Augmentation Computer (FAC) PN B397BAM0623. For A/C which have a sharklet upgrade, modifications are required to adjust computation of the Weight, CG and Characteristic speeds. Accomplishment of this Service Bulletin will satisfy the operator’s request. The operational/maintenance consequences of this Service Bulletin are covered by the update of the affected publications detailed in "PLANNING INFORMATION". GENERAL EVALUATION EVALUATION TABLE COMPLIANCE OPTIONAL (1) CANCELS INSPECTION SB NO POTENTIAL AD NO 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 NOTE (1): Service Bulletin for convenience or option.

DATE: Oct 31/13 SERVICE BULLETIN No.: A320-22-1461 REVISION No.: 07 - Mar 23/15 Page: 1 5

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# @A318/A319/A320/A321 SERVICE BULLETIN SUMMARY MATERIAL PRICE INFORMATION **CONF 001 MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Component COMPA01 1 See SB FAC **CONF 002 MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Component COMPA02 1 See SB FAC **CONF 003 MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Component COMPA03 1 See SB FAC **CONF 004 MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Component COMPA04 1 See SB FAC EFFECTIVITY **CONF ALL This Service Bulletin is applicable to this (these) operator(s) :

15T AFL BEC CBJ CHB CQH EVA GCR JBU MLM MON PAL QTR SBI TAM TAP TBA TCX TGW THY VOI NOTE: This Service Bulletin is written for the operators listed above. The modification in this Service Bulletin can be done by other operators. If other operators want to do this modification, use the RFC/RMO procedure and write to : AIRBUS CUSTOMER SERVICES DIRECTORATE SC Department 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE

DATE: Oct 31/13 SERVICE BULLETIN No.: A320-22-1461 REVISION No.: 07 - Mar 23/15 Page: 2 5

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# @A318/A319/A320/A321 SERVICE BULLETIN SUMMARY CONCURRENT REQUIREMENTS For MSN 1904 1915 1927 1948 2006 2020 2031 2042 2063 2075 2099 2125 2132 3488 3517 3554 3572 3622 3659 3707 3724 3760 3769 3800 3811 3883 4021 4095 4106 4145 4578 4612 4622 4629 4647 4665 4695 4755 4766 4774 4790 4801 4846 4858 4904 4930 4968 5010 5060 5078 5127 5142 5157 5256 5446 5450-5451 5465 5485 5488 5490 5528-5529 5536 5538 5546 5559 5562-5563 5565 5572 5578 5580 5582 5584-5585 5603 5605-5607 5614 5626 5630 5633 5656 5662-5663 5667 5679 5689 5715 5722 5740 5747 5760 5799 5873 5921 Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishment of the following Service Bulletin(s) : Service Bulletin No. None For MSN 1667 1756 1765 1799 1816 2178 Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishment of the following Service Bulletin(s) : Service Bulletin No. A320-22-1102 NOTE: Service Bulletin No. A320-22-1102 (AUTO FLIGHT - FLIGHT AUGMENTATION COMPUTER - INSTALL FAC STANDARD BAM0617). For MSN 1856 1909 1996 2156 2164 2395 2401 2404 2414 2452 2522 2602 2609 2626 2631 2655 2738-2739 2928 2934 2941 2984 3010 3142 3164 3185 3208 3239 3257 3259 3303 3308 3341 3558 3567 3603 3654 3718-3719 3896 3931 3949 Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishment of the following Service Bulletin(s) : Service Bulletin No. A320-22-1278 NOTE: Service Bulletin No. A320-22-1278 (AUTO FLIGHT - FAC (FLIGHT AUGMENTATION COMPUTER) - INTRODUCE FAC SOFTWARE STANDARD BAM0620). REFERENCES / REPERCUSSIONS TFU None OEB None AOT None SIL None LINE MAINTENANCE AFFECTED No LIFE LIMIT None OTHER None NATURE OF THE WORK AIRCRAFT NO EQUIPMENT YES HARD YES SOFT NO OBRM YES DATE: Oct 31/13 SERVICE BULLETIN No.: A320-22-1461 REVISION No.: 07 - Mar 23/15 Page: 3 5

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# @A318/A319/A320/A321 SERVICE BULLETIN SUMMARY MANPOWER **CONF 001 Task 221461-831-801-001: Modification by Replacement or by Reprogramming of the OBRMs. TOTAL MANHOURS 1.50 ELAPSED TIME (HOURS) 1.50 Additional manhours related to Vendor SB; refer to: In the Main Rack 80VU, Modify the two FACs (1CC1, 1CC2) by Replacement or by Reprogramming of their OBRMs. THALES Service Bulletin No. B397BAM-22-046 THALES Service Bulletin No. B397BAM-22-048 Task 221461-831-802-001: Modification by Replacement of the FACs. TOTAL MANHOURS 2.50 ELAPSED TIME (HOURS) 2.50 **CONF 002 Task 221461-831-801-001: Modification by Replacement or by Reprogramming of the OBRMs. TOTAL MANHOURS 1.50 ELAPSED TIME (HOURS) 1.50 Additional manhours related to Vendor SB; refer to: In the Main Rack 80VU, Modify the two FACs (1CC1, 1CC2) by Replacement or by Reprogramming of their OBRMs. THALES Service Bulletin No. B397BAM-22-046 THALES Service Bulletin No. B397BAM-22-048 Task 221461-831-802-001: Modification by Replacement of the FACs. TOTAL MANHOURS 2.50 ELAPSED TIME (HOURS) 2.50 **CONF 003 Task 221461-831-801-001: Modification by Replacement or by Reprogramming of the OBRMs. TOTAL MANHOURS 1.50 ELAPSED TIME (HOURS) 1.50 Additional manhours related to Vendor SB; refer to: In the Main Rack 80VU, Modify the two FACs (1CC1, 1CC2) by Replacement or by Reprogramming of their OBRMs. THALES Service Bulletin No. B397BAM-22-044 THALES Service Bulletin No. B397BAM-22-046 THALES Service Bulletin No. B397BAM-22-048

DATE: Oct 31/13 SERVICE BULLETIN No.: A320-22-1461 REVISION No.: 07 - Mar 23/15 Page: 4 5

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# @A318/A319/A320/A321 SERVICE BULLETIN SUMMARY Task 221461-831-802-001: Modification by Replacement of the FACs. TOTAL MANHOURS 2.50 ELAPSED TIME (HOURS) 2.50 **CONF 004 Task 221461-831-801-001: Modification by Replacement or by Reprogramming of the OBRMs. TOTAL MANHOURS 1.50 ELAPSED TIME (HOURS) 1.50 Additional manhours related to Vendor SB; refer to: In the Main Rack 80VU, Modify the two FACs (1CC1, 1CC2) by Replacement or by Reprogramming of their OBRMs. THALES Service Bulletin No. B397BAM-22-046 THALES Service Bulletin No. B397BAM-22-048 Task 221461-831-802-001: Modification by Replacement of the FACs. TOTAL MANHOURS 2.50 ELAPSED TIME (HOURS) 2.50 APPENDICES **CONF ALL Appendix 01: Retrofitted Modifications

DATE: Oct 31/13 SERVICE BULLETIN No.: A320-22-1461 REVISION No.: 07 - Mar 23/15 Page: 5 5

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# @A318/A319/A320/A321 SERVICE BULLETIN SUMMARY

**CONF ALL

FR1 Z120 FR24A



## A 80VU 

### A

1CC2

1CC1 FAC

−2

FAC

−1 84VU UPGRADE OF

83VU THE FAC

−1 AND FAC

−2

N_SB_221461_5_SAAA_01_00 Figure A-FSAAA - Sheet 01

DATE: Oct 31/13 SERVICE BULLETIN No.: A320-22-1461 REVISION No.: 07 - Mar 23/15 Page: 6 5

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# @A318/A319/A320/A321 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 ATA SYSTEM: 22 

### TITLE: AUTO FLIGHT - FLIGHT AUGMENTATION COMPUTER (FAC) - INSTALL FAC B623 (SHARKLET PROJECT) MODIFICATION No.: 30439P6703 31040P6954 33299P8256 35522P9122 36766P9906 38777P10777 160011P12126 160065P13119 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 (1) Models 319-112 319-115 319-132 320-214 320-232 320-233 321-211 321-231 (2) Effectivity by MSN 1667 1756 1765 1799 1816 1856 1904 1909 1915 1927 1948 1996 2006 2020 2031 2042 2063 2075 2099 2125 2132 2156 2164 2178 2395 2401 2404 2414 2452 2522 2602 2609 2626 2631 2655 2738-2739 2928 2934 2941 2984 3010 3142 3164 3185 3208 3239 3257 3259 3303 3308 3341 3488 3517 3554 3558 3567 3572 3603 3622 3654 3659 3707 3718-3719 3724 3760 3769 3800 3811 3883 3896 3931 3949 4021 4095 4106 4145 4578 4612 4622 4629 4647 4665 4695 4755 4766 4774 4790 4801 4846 4858 4904 4930 4968 5010 5060 5078 5127 5142 5157 5256 5446 5450-5451 5465 5485 5488 5490 5528-5529 5536 5538 5546 5559 5562-5563 5565 5572 5578 5580 5582 5584-5585 5603 5605-5607 5614 5626 5630 5633 5656 5662-5663 5667 5679 5689 5715 5722 5740 5747 5760 5799 5873 5921

DATE: Oct 31/13 SERVICE BULLETIN No.: A320-22-1461 REVISION No.: 07 - Mar 23/15 Page: 1 5

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# @A318/A319/A320/A321 SERVICE BULLETIN (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 15T 3164 AFL 5536 5565 5572 5578 5580 5585 5614 5873 5921 BEC 5538 CBJ 5630 5656 5722 CHB 5626 5679 5740 CQH 5446 5562 EVA 5485 GCR 5760 5799 JBU 1904 1915 1927 1948 2006 2020 2031 2042 2063 2075 2099 2125 2132 3488 3517 3554 3572 3622 3659 3707 3724 3760 3800 3811 4578 4612 4647 4904 5060 5142 MLM 4622 MON 5582 5606 PAL 5715 5747 QTR 4858 4930 4968 5010 5078 5127 SBI 5559 5607 TAM 5528 TAP 1667 1756 1765 1799 1816 2178 3769 3883 4021 4095 4106 4145 TBA 4766 4801 4846 5157 5256 5451 5529 5563 TCX 5603 TGW 5605 5662 THY 1856 1909 1996 2156 2164 2395 2401 2404 2414 2452 2522 2602 2609 2626 2631 2655 2738 2739 2928 2934 2941 2984 3010 3142 3185 3208 3239 3257 3259 3303 3308 3341 3558 3567 3603 3654 3718 3719 3896 3931 3949 4629 4665 4695 4755 4774 4790 5450 5465 5490 5546 5584 5633 5663 5667 5689 VOI 5488 (4) Configuration by MSN MSN CONFIGURATION 1667 1756 1765 1799 1816 2178 3488 3517 3554 3572 3622 3659 3707 3724 3760 3800 3811 4578 4612 4647 4904 5060 5142 004

1856 1909 1996 2156 2164 2395 2401 2404 2414 2452 2522 2602 2609 2626 2631 2655 2738 2739 2928 2934 2941 2984 3010 3142 3185 3208 3239 3257 3259 3303 3308 3341 3558 3567 3603 3654 3718 3719 3769 3883 3896 3931 3949 4021 4095 4106 4145 5536 5565 5572 5578 5580 5585 5614 5873 5921 002

1904 1915 1927 1948 2006 2020 2031 2042 2063 2075 2099 2125 2132 003

DATE: Oct 31/13 SERVICE BULLETIN No.: A320-22-1461 REVISION No.: 07 - Mar 23/15 Page: 2 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

MSN CONFIGURATION 3164 4622 4629 4665 4695 4755 4766 4774 4790 4801 4846 4858 4930 4968 5010 5078 5127 5157 5256 5446 5450 5451 5465 5485 5488 5490 5528 5529 5538 5546 5559 5562 5563 5582 5584 5603 5605 5606 5607 5626 5630 5633 5656 5662 5663 5667 5679 5689 5715 5722 5740 5747 5760 5799 001

(5) Configuration definition **CONF 001 Config. 001 is valid for aircraft equipped with FAC P/N B397BAM0620. For the retrofitted modifications after accomplishment of this Service Bulletin, refer to Appendix 01: Retrofitted Modification. **CONF 002 Config. 002 is valid for aircraft equipped with FAC P/N B397BAM0619. For the retrofitted modifications after accomplishment of this Service Bulletin, refer to Appendix 01: Retrofitted Modification. **CONF 003 Config. 003 is valid for aircraft equipped with FAC P/N B397BAM0513. For the retrofitted modifications after accomplishment of this Service Bulletin, refer to Appendix 01: Retrofitted Modification. **CONF 004 Config. 004 is valid for aircraft equipped with FAC P/N B397BAM0617. For the retrofitted modifications after accomplishment of this Service Bulletin, refer to Appendix 01: Retrofitted Modification. (6) Material Effectivity **CONF 001 MATERIAL QTY PER A/C SEE NOTES Component COMPA01 1 **CONF 002 MATERIAL QTY PER A/C SEE NOTES Component COMPA02 1 **CONF 003 MATERIAL QTY PER A/C SEE NOTES Component COMPA03 1 **CONF 004 MATERIAL QTY PER A/C SEE NOTES Component COMPA04 1

DATE: Oct 31/13 SERVICE BULLETIN No.: A320-22-1461 REVISION No.: 07 - Mar 23/15 Page: 3 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

**CONF ALL B. CONCURRENT REQUIREMENTS For MSN 1904 1915 1927 1948 2006 2020 2031 2042 2063 2075 2099 2125 2132 3488 3517 3554 3572 3622 3659 3707 3724 3760 3769 3800 3811 3883 4021 4095 4106 4145 4578 4612 4622 4629 4647 4665 4695 4755 4766 4774 4790 4801 4846 4858 4904 4930 4968 5010 5060 5078 5127 5142 5157 5256 5446 5450-5451 5465 5485 5488 5490 5528-5529 5536 5538 5546 5559 5562-5563 5565 5572 5578 5580 5582 5584-5585 5603 5605-5607 5614 5626 5630 5633 5656 5662-5663 5667 5679 5689 5715 5722 5740 5747 5760 5799 5873 5921 Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishment of the following Service Bulletin(s) : Service Bulletin No. None For MSN 1667 1756 1765 1799 1816 2178 Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishment of the following Service Bulletin(s) : Service Bulletin No. A320-22-1102 NOTE: Service Bulletin No. A320-22-1102 (AUTO FLIGHT - FLIGHT AUGMENTATION COMPUTER - INSTALL FAC STANDARD BAM0617). For MSN 1856 1909 1996 2156 2164 2395 2401 2404 2414 2452 2522 2602 2609 2626 2631 2655 2738-2739 2928 2934 2941 2984 3010 3142 3164 3185 3208 3239 3257 3259 3303 3308 3341 3558 3567 3603 3654 3718-3719 3896 3931 3949 Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishment of the following Service Bulletin(s) : Service Bulletin No. A320-22-1278 NOTE: Service Bulletin No. A320-22-1278 (AUTO FLIGHT - FAC (FLIGHT AUGMENTATION COMPUTER) - INTRODUCE FAC SOFTWARE STANDARD BAM0620). C. REASON (1) History This Service Bulletin is issued further to an operator’s request. (2) Objective/Action In the frame of Sharklet upgrade, this Service Bulletin allows the installation of the Flight Augmentation Computer (FAC) PN B397BAM0623. For A/C which have a sharklet upgrade, modifications are required to adjust computation of the Weight, CG and Characteristic speeds.

DATE: Oct 31/13 SERVICE BULLETIN No.: A320-22-1461 REVISION No.: 07 - Mar 23/15 Page: 4 5

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# @A318/A319/A320/A321 SERVICE BULLETIN (3) Advantages Accomplishment of this Service Bulletin will satisfy the operator’s request. (4) Operational/Maintenance Consequences The operational/maintenance consequences of this Service Bulletin are covered by the update of the affected publications detailed in "PLANNING INFORMATION". D. DESCRIPTION NOTE: To accomplish this Service Bulletin, you have two possibilities : - Either you modify the FACs by replacement or by reprogramming of the OBRMs as described in TASK 221461-831-801 001 Modification by Replacement or by Reprogramming of the OBRMs. - Or you replace them as described in TASK 221461-831-802 001 Modification by Replacement of the FACs. To accomplish this Service Bulletin it is necessary to : **CONF 001 Task 221461-831-801-001: Modification by Replacement or by Reprogramming of the OBRMs. (1) In the Main Rack 80VU, Modify the two FACs (1CC1, 1CC2) by Replacement or by Reprogramming of their OBRMs. Task 221461-831-802-001: Modification by Replacement of the FACs. (1) Replace the FACs (1CC1, 1CC2) **CONF 002 Task 221461-831-801-001: Modification by Replacement or by Reprogramming of the OBRMs. (1) In the Main Rack 80VU, Modify the two FACs (1CC1, 1CC2) by Replacement or by Reprogramming of their OBRMs. Task 221461-831-802-001: Modification by Replacement of the FACs. (1) Replace the FACs (1CC1, 1CC2) **CONF 003 Task 221461-831-801-001: Modification by Replacement or by Reprogramming of the OBRMs. (1) In the Main Rack 80VU, Modify the two FACs (1CC1, 1CC2) by Replacement or by Reprogramming of their OBRMs.

DATE: Oct 31/13 SERVICE BULLETIN No.: A320-22-1461 REVISION No.: 07 - Mar 23/15 Page: 5 5

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# @A318/A319/A320/A321 SERVICE BULLETIN Task 221461-831-802-001: Modification by Replacement of the FACs. (1) Replace the FACs (1CC1, 1CC2) **CONF 004 Task 221461-831-801-001: Modification by Replacement or by Reprogramming of the OBRMs. (1) In the Main Rack 80VU, Modify the two FACs (1CC1, 1CC2) by Replacement or by Reprogramming of their OBRMs. Task 221461-831-802-001: Modification by Replacement of the FACs. (1) Replace the FACs (1CC1, 1CC2) **CONF ALL E. COMPLIANCE (1) Classification OPTIONAL: Service Bulletin for convenience or option. (2) Accomplishment Timescale In accordance with operators’ maintenance schedule. F. APPROVAL The technical content of this document is approved under the authority of 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 221461-831-801-001: Modification by Replacement or by Reprogramming of the OBRMs. Get Access 0.50 Tests 0.50 Close-Up 0.50 DATE: Oct 31/13 SERVICE BULLETIN No.: A320-22-1461 REVISION No.: 07 - Mar 23/15 Page: 6 5

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# @A318/A319/A320/A321 SERVICE BULLETIN
Task 221461-831-801-001: Modification by Replacement or by Reprogramming of the OBRMs.

TOTAL MANHOURS 1.50 ELAPSED TIME (HOURS) 1.50 Additional manhours related to Vendor SB; refer to: In the Main Rack 80VU, Modify the two FACs (1CC1, 1CC2) by Replacement or by Reprogramming of their OBRMs. THALES Service Bulletin No. B397BAM-22-046 THALES Service Bulletin No. B397BAM-22-048 Task 221461-831-802-001: Modification by Replacement of the FACs. Get Access 0.50 On Aircraft Replace the FACs (1CC1, 1CC2) 1.00 Tests 0.50 Close-Up 0.50 TOTAL MANHOURS 2.50 ELAPSED TIME (HOURS) 2.50 **CONF 002 Task 221461-831-801-001: Modification by Replacement or by Reprogramming of the OBRMs. Get Access 0.50 Tests 0.50 Close-Up 0.50 TOTAL MANHOURS 1.50 ELAPSED TIME (HOURS) 1.50 Additional manhours related to Vendor SB; refer to: In the Main Rack 80VU, Modify the two FACs (1CC1, 1CC2) by Replacement or by Reprogramming of their OBRMs. THALES Service Bulletin No. B397BAM-22-046 THALES Service Bulletin No. B397BAM-22-048 Task 221461-831-802-001: Modification by Replacement of the FACs. Get Access 0.50 On Aircraft Replace the FACs (1CC1, 1CC2) 1.00 Tests 0.50 Close-Up 0.50 TOTAL MANHOURS 2.50 ELAPSED TIME (HOURS) 2.50 **CONF 003 Task 221461-831-801-001: Modification by Replacement or by Reprogramming of the OBRMs. Get Access 0.50 DATE: Oct 31/13 SERVICE BULLETIN No.: A320-22-1461 REVISION No.: 07 - Mar 23/15 Page: 7 5

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# @A318/A319/A320/A321 SERVICE BULLETIN
Task 221461-831-801-001: Modification by Replacement or by Reprogramming of the OBRMs. Tests 0.50 Close-Up 0.50 TOTAL MANHOURS 1.50 ELAPSED TIME (HOURS) 1.50 Additional manhours related to Vendor SB; refer to: In the Main Rack 80VU, Modify the two FACs (1CC1, 1CC2) by Replacement or by Reprogramming of their OBRMs. THALES Service Bulletin No. B397BAM-22-044 THALES Service Bulletin No. B397BAM-22-046 THALES Service Bulletin No. B397BAM-22-048 Task 221461-831-802-001: Modification by Replacement of the FACs. Get Access 0.50 On Aircraft Replace the FACs (1CC1, 1CC2) 1.00 Tests 0.50 Close-Up 0.50 TOTAL MANHOURS 2.50 ELAPSED TIME (HOURS) 2.50 **CONF 004 Task 221461-831-801-001: Modification by Replacement or by Reprogramming of the OBRMs. Get Access 0.50 Tests 0.50 Close-Up 0.50 TOTAL MANHOURS 1.50 ELAPSED TIME (HOURS) 1.50 Additional manhours related to Vendor SB; refer to: In the Main Rack 80VU, Modify the two FACs (1CC1, 1CC2) by Replacement or by Reprogramming of their OBRMs. THALES Service Bulletin No. B397BAM-22-046 THALES Service Bulletin No. B397BAM-22-048 Task 221461-831-802-001: Modification by Replacement of the FACs. Get Access 0.50 On Aircraft Replace the FACs (1CC1, 1CC2) 1.00 Tests 0.50 Close-Up 0.50 TOTAL MANHOURS 2.50 ELAPSED TIME (HOURS) 2.50

DATE: Oct 31/13 SERVICE BULLETIN No.: A320-22-1461 REVISION No.: 07 - Mar 23/15 Page: 8 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

**CONF ALL H. WEIGHT AND BALANCE Not Changed I. ELECTRICAL LOAD DATA Not Changed J. REFERENCES **CONF 001 Aircraft Maintenance Manual (AMM) 12-34-24 20-15-00 22-62-00 22-66-34 22-96-00 22-97-00 31-32-00 52-41-00 ATA Common Support Data Dictionary (CSDD), Chapter 2 Elec. Std. Practices Manual (ESPM) 20-55-00 Service Bulletin (SB) A320-22-1278 Service Information Letter (SIL) SIL 00-022 Vendor Service Bulletin (VSB) THALES Service Bulletin No. B397BAM-22-046 THALES Service Bulletin No. B397BAM-22-048 **CONF 002 Aircraft Maintenance Manual (AMM) 12-34-24 20-15-00 22-62-00 22-66-34 22-96-00 22-97-00 31-32-00 52-41-00 ATA Common Support Data Dictionary (CSDD), Chapter 2 Elec. Std. Practices Manual (ESPM) 20-55-00 Service Bulletin (SB) A320-22-1278 Service Information Letter (SIL) SIL 00-022 Vendor Service Bulletin (VSB) THALES Service Bulletin No. B397BAM-22-046 THALES Service Bulletin No. B397BAM-22-048 **CONF 003 Aircraft Maintenance Manual (AMM) 12-34-24 20-15-00 22-62-00 22-66-34 22-96-00 22-97-00 31-32-00 52-41-00 ATA Common Support Data Dictionary (CSDD), Chapter 2 Elec. Std. Practices Manual (ESPM) 20-55-00 Service Information Letter (SIL) SIL 00-022

DATE: Oct 31/13 SERVICE BULLETIN No.: A320-22-1461 REVISION No.: 07 - Mar 23/15 Page: 9 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

Vendor Service Bulletin (VSB) THALES Service Bulletin No. B397BAM-22-044 THALES Service Bulletin No. B397BAM-22-046 THALES Service Bulletin No. B397BAM-22-048 **CONF 004 Aircraft Maintenance Manual (AMM) 12-34-24 20-15-00 22-62-00 22-66-34 22-96-00 22-97-00 31-32-00 52-41-00 ATA Common Support Data Dictionary (CSDD), Chapter 2 Elec. Std. Practices Manual (ESPM) 20-55-00 Service Bulletin (SB) A320-22-1102 Service Information Letter (SIL) SIL 00-022 Vendor Service Bulletin (VSB) THALES Service Bulletin No. B397BAM-22-046 THALES Service Bulletin No. B397BAM-22-048 **CONF ALL K. PUBLICATION AFFECTED

Aircraft Wiring List (AWL) Flight Crew Operating Manual (FCOM) Illustrated Parts Catalog (IPC) 22-66-34 22-67-08 Trouble Shooting Manual (TSM) 22-66-00 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 a revision priorto Service Bulletin embodiment. For this purpose, please request the revision by e-mail, online through the SB Reporting service or alternatively by fax to: SEDOR4 - AIRBUS Customer Services Technical Data Fax No.: (33) 5 61 93 28 06 E-mail: sb.reporting@airbus.com SB Reporting service is accessible on-line through AIRBUSWorld from: - My on-line services’ section, available on all AIRBUSWorld pages - The Maintenance & Engineering Community, in: . Modify and Upgrade page - Access SB and VSB section. 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 Aircraft In-Service Data (SEDOR4). DATE: Oct 31/13 SERVICE BULLETIN No.: A320-22-1461 REVISION No.: 07 - Mar 23/15 Page: 10 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

L. INTERCHANGEABILITY/MIXABILITY **CONF 001 DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE NOTES FAC B397BAM0620 B397BAM0623 03 NO NOTE: For definitions of interchangeability codes in column INT., refer to ATA Common Support Data Dictionary (CSDD), Chapter 2. NOTE: 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 SEE NOTES FAC B397BAM0619 B397BAM0623 03 NO NOTE: For definitions of interchangeability codes in column INT., refer to ATA Common Support Data Dictionary (CSDD), Chapter 2. NOTE: Only the mixability configuration(s) and condition(s) stated in this Service Bulletin are approved. **CONF 003 DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE NOTES FAC B397BAM0513 B397BAM0623 03 NO NOTE: For definitions of interchangeability codes in column INT., refer to ATA Common Support Data Dictionary (CSDD), Chapter 2. NOTE: Only the mixability configuration(s) and condition(s) stated in this Service Bulletin are approved. **CONF 004 DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE NOTES FAC B397BAM0617 B397BAM0623 03 NO NOTE: For definitions of interchangeability codes in column INT., refer to ATA Common Support Data Dictionary (CSDD), Chapter 2. NOTE: Only the mixability configuration(s) and condition(s) stated in this Service Bulletin are approved.

DATE: Oct 31/13 SERVICE BULLETIN No.: A320-22-1461 REVISION No.: 07 - Mar 23/15 Page: 11 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

**CONF ALL M. SPARES FAC B397BAM0513 FAC B397BAM0617 FAC B397BAM0619 FAC B397BAM0620

DATE: Oct 31/13 SERVICE BULLETIN No.: A320-22-1461 REVISION No.: 07 - Mar 23/15 Page: 12 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

2. MATERIAL INFORMATION **CONF ALL A. MATERIAL - PRICE AND AVAILABILITY (1) Procurement Addresses Component COMPA01 Component COMPA02 Component COMPA03 Component COMPA04 The material is included in the commercial offer of the Letter Agreement, and as such will be supplied by AIRBUS Upgrade Services. To facilitate the material reception, Airline Customers are requested to contact: AIRBUS Upgrade Services Attn Key Account Manager (KAM) (2) Price and Availability Sales terms must be agreed between the Customer and AIRBUS in accordance with the RFC (or RFC/RMO) procedure. B. INDUSTRY SUPPORT INFORMATION Industry Support terms must be agreed between the Customer and AIRBUS in accordance with the RFC (or RFC/RMO) procedure. C. LIST OF COMPONENTS No Kit D. LIST OF MATERIALS - OPERATOR SUPPLIED (1) Consumable Materials None (2) Components Component COMPA01 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES B397BAM0623 2 FAC B397BAM0620 03 NOTE: For definitions of interchangeability codes in column INT., refer to ATA Common Support Data Dictionary (CSDD), Chapter 2. Component COMPA02 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES B397BAM0623 2 FAC B397BAM0619 03 DATE: Oct 31/13 SERVICE BULLETIN No.: A320-22-1461 REVISION No.: 07 - Mar 23/15 Page: 13 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

NOTE: For definitions of interchangeability codes in column INT., refer to ATA Common Support Data Dictionary (CSDD), Chapter 2. Component COMPA03 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES B397BAM0623 2 FAC B397BAM0513 03 NOTE: For definitions of interchangeability codes in column INT., refer to ATA Common Support Data Dictionary (CSDD), Chapter 2. Component COMPA04 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES B397BAM0623 2 FAC B397BAM0617 03 NOTE: For definitions of interchangeability codes in column INT., refer to ATA Common Support Data Dictionary (CSDD), Chapter 2. (3) Equipment None E. PARTS TO BE RE-IDENTIFIED BY OPERATOR None F. TOOLING (1) Tooling - Price and Availability To accomplish this Service Bulletin, it is necessary to use the tools defined in Vendor Service Bulletin (Refer to THALES Service Bulletin No. B397BAM-22-044, B397BAM-22-046 and B397BAM-22-048). (2) Tools None (3) Special Tools None

DATE: Oct 31/13 SERVICE BULLETIN No.: A320-22-1461 REVISION No.: 07 - Mar 23/15 Page: 14 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS Task 221461-831-801-001 - Modification by Replacement or by Reprogramming of the OBRMs. WARNING: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONS INCLUDED IN THE REFERENCED PROCEDURES. CAUTION: REFER TO AMM 20-15-00, Page Block 201 and SIL 00-022) FOR ELECTRONIC DISCHARGE PRECAUTIONS. 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. NOTE: The accomplishment instructions of this Service Bulletin refer to procedures included in other AIRBUS documents. When the words ’refer to’ are used and the operator has an accepted alternative procedure, the accepted alternative procedure can be used. When the words ’in accordance with’ are included in the instruction, the procedure in the AIRBUS document must be used. NOTE: The access and close-up instructions, not comprising return to service tests, in this Service Bulletin do not constitute or affect the technical intent of the Service Bulletin. Operators can therefore, as deemed necessary, omit or add access and/or close-up steps to add flexibility to their maintenance operations as long as the technical intent of the Service Bulletin is met within the set parameters. NOTE: Manual titles given in the accomplishment instructions are referred to by acronyms. Refer to paragraph 1.J., References, for the definition of acronyms. Task Associated Data **CONF 001 Zone 120 210 Modified FIN 1CC1 1CC2

DATE: Oct 31/13 SERVICE BULLETIN No.: A320-22-1461 REVISION No.: 07 - Mar 23/15 Page: 15 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

Access Door 824 831 Manpower TOTAL MANHOURS 1.50 ELAPSED TIME (HOURS) 1.50 Additional manhours related to Vendor SB; refer to: THALES Service Bulletin No. B397BAM-22-046 THALES Service Bulletin No. B397BAM-22-048 **CONF 002 Zone 120 210 Modified FIN 1CC1 1CC2 Access Door 824 831 Manpower TOTAL MANHOURS 1.50 ELAPSED TIME (HOURS) 1.50 Additional manhours related to Vendor SB; refer to: THALES Service Bulletin No. B397BAM-22-046 THALES Service Bulletin No. B397BAM-22-048 **CONF 003 Zone 120 210 Modified FIN 1CC1 1CC2 Access Door 824 831 Manpower TOTAL MANHOURS 1.50 ELAPSED TIME (HOURS) 1.50 Additional manhours related to Vendor SB; refer to: THALES Service Bulletin No. B397BAM-22-044 THALES Service Bulletin No. B397BAM-22-046 THALES Service Bulletin No. B397BAM-22-048 **CONF 004 Zone 120 210

DATE: Oct 31/13 SERVICE BULLETIN No.: A320-22-1461 REVISION No.: 07 - Mar 23/15 Page: 16 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

Modified FIN 1CC1 1CC2 Access Door 824 831 Manpower TOTAL MANHOURS 1.50 ELAPSED TIME (HOURS) 1.50 Additional manhours related to Vendor SB; refer to: THALES Service Bulletin No. B397BAM-22-046 THALES Service Bulletin No. B397BAM-22-048 **CONF ALL A. GENERAL **CONF 001 (1) Subtask 221461-839-001-001 - Administrative Manpower Resources Skills NON SPECIFIC (a) Write in the applicable aircraft records that you have done all the work given in this Service Bulletin. **CONF 002 (1) Subtask 221461-839-001-001 - Administrative Manpower Resources Skills NON SPECIFIC (a) Write in the applicable aircraft records that you have done all the work given in this Service Bulletin. **CONF 003 (1) Subtask 221461-839-001-001 - Administrative Manpower Resources Skills NON SPECIFIC (a) Write in the applicable aircraft records that you have done all the work given in this Service Bulletin. **CONF 004 (1) Subtask 221461-839-001-001 - Administrative Manpower Resources Skills NON SPECIFIC DATE: Oct 31/13 SERVICE BULLETIN No.: A320-22-1461 REVISION No.: 07 - Mar 23/15 Page: 17 5

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# @A318/A319/A320/A321 SERVICE BULLETIN (a) Write in the applicable aircraft records that you have done all the work given in this Service Bulletin. **CONF ALL B. PREPARATION **CONF 001 (1) Subtask 221461-941-001-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 12-34-24-869-002 Task 52-41-00-010-002 (a) Make sure that the aircraft is electrically grounded (Refer to AMM Task 12-34-24-869-002). (b) The following items shall be considered as the basic Aircraft configuration before you start a maintenance task: - Aircraft on the ground resting on landing gear (the ground safety locks and the wheel chocks are in position on the landing gear). - Engine shut down, thrust reversers closed and locked. - Aircraft in clean configuration. - Parking brake applied. - Aircraft electrical network de-energized. - Hydraulic systems depressurized. - Access to the cockpit and cabin is available. - All circuit breakers are in closed position. - All controls in NORM, AUTO or OFF position. (c) Open the Avionic Compartment Door 824 (Refer to AMM Task 52-41-00-010-002). **CONF 002 (1) Subtask 221461-941-001-001 - Job Set-up Manpower Resources Skills NON SPECIFIC

DATE: Oct 31/13 SERVICE BULLETIN No.: A320-22-1461 REVISION No.: 07 - Mar 23/15 Page: 18 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

References Aircraft Maintenance Manual (AMM) Task 12-34-24-869-002 Task 52-41-00-010-002 (a) Make sure that the aircraft is electrically grounded (Refer to AMM Task 12-34-24-869-002). (b) The following items shall be considered as the basic Aircraft configuration before you start a maintenance task: - Aircraft on the ground resting on landing gear (the ground safety locks and the wheel chocks are in position on the landing gear). - Engine shut down, thrust reversers closed and locked. - Aircraft in clean configuration. - Parking brake applied. - Aircraft electrical network de-energized. - Hydraulic systems depressurized. - Access to the cockpit and cabin is available. - All circuit breakers are in closed position. - All controls in NORM, AUTO or OFF position. (c) Open the Avionic Compartment Door 824 (Refer to AMM Task 52-41-00-010-002). **CONF 003 (1) Subtask 221461-941-001-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 12-34-24-869-002 Task 52-41-00-010-002 (a) Make sure that the aircraft is electrically grounded (Refer to AMM Task 12-34-24-869-002). (b) The following items shall be considered as the basic Aircraft configuration before you start a maintenance task: - Aircraft on the ground resting on landing gear (the ground safety locks and the wheel chocks are in position on the landing gear). - Engine shut down, thrust reversers closed and locked.

DATE: Oct 31/13 SERVICE BULLETIN No.: A320-22-1461 REVISION No.: 07 - Mar 23/15 Page: 19 5

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# @A318/A319/A320/A321 SERVICE BULLETIN - Aircraft in clean configuration. - Parking brake applied. - Aircraft electrical network de-energized. - Hydraulic systems depressurized. - Access to the cockpit and cabin is available. - All circuit breakers are in closed position. - All controls in NORM, AUTO or OFF position. (c) Open the Avionic Compartment Door 824 (Refer to AMM Task 52-41-00-010-002). **CONF 004 (1) Subtask 221461-941-001-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 12-34-24-869-002 Task 52-41-00-010-002 (a) Make sure that the aircraft is electrically grounded (Refer to AMM Task 12-34-24-869-002). (b) The following items shall be considered as the basic Aircraft configuration before you start a maintenance task: - Aircraft on the ground resting on landing gear (the ground safety locks and the wheel chocks are in position on the landing gear). - Engine shut down, thrust reversers closed and locked. - Aircraft in clean configuration. - Parking brake applied. - Aircraft electrical network de-energized. - Hydraulic systems depressurized. - Access to the cockpit and cabin is available. - All circuit breakers are in closed position. - All controls in NORM, AUTO or OFF position. (c) Open the Avionic Compartment Door 824 (Refer to AMM Task 52-41-00-010-002).

DATE: Oct 31/13 SERVICE BULLETIN No.: A320-22-1461 REVISION No.: 07 - Mar 23/15 Page: 20 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

**CONF ALL C. PROCEDURE **CONF 001 (1) Subtask 221461-831-001-002 - In the Main Rack 80VU, Modify the two FACs (1CC1, 1CC2) by Replacement or by Reprogramming of their OBRMs. Work Zones and Access Panels Zone Access/Work location 120 Access Door 824 Work location Electrical panel 80VU 210 Access Door 831 References Aircraft Maintenance Manual (AMM) Task 22-96-00-710-001 Task 31-32-00-860-001 Vendor Service Bulletin (VSB) THALES B397BAM-22-046 THALES B397BAM-22-048 (a) Do the operational test of the AFS (Refer to AMM Task 22-96-00-710-001). (b) Do the Line Replaceable Unit (LRU) identification test: 1 Job set-up:
a Do the procedure to get access to the SYSTEM REPORT/TEST Menu page (Refer to AMM Task 31-32-00-860-001). b Make sure that these circuit breakers are closed: PANEL DESIGNATION FIN LOCATION SEE NOTES 121VU PTR/SPLY 6TW 21 J (01) 121VU PTR/SPLY 6TW 20 K (01) 49VU AUTO FLT/FAC1/28VDC 5CC1 04 B 49VU AUTO FLT/FAC1/26VAC 14CC1 03 B 121VU AUTO FLT/FAC2/28VDC 5CC2 19 M 121VU AUTO FLT/FAC2/26VAC 14CC2 18 M NOTE (01): The location of the CB depends on the A/C configuration. 2 Procedure: ACTION RESULT 1. On the SYSTEM REPORT/TEST page : - Push the line key adjacent to the AFS indication. - The AFS MAIN MENU page comes into view 2. On the AFS MAIN MENU page : - Push the line key adjacent to the LRU IDENT

indication. - The AFS/LRU IDENTIFICATION page comes into view.

DATE: Oct 31/13 SERVICE BULLETIN No.: A320-22-1461 REVISION No.: 07 - Mar 23/15 Page: 21 5

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# @A318/A319/A320/A321 SERVICE BULLETIN
3. On the AFS/LRU IDENTIFICATION page : - Make sure that the P/N of the two FACs is

B397BAM0620 4. Print the AFS/LRU IDENTIFICATION page (if the printer is not available, a visual check is acceptable) 3 Close-up:
a Put the aircraft back to its initial configuration. b On the Multipurpose Control and Display Unit (MCDU), push the line key adjacent to the RETURN indication until the Centralized Fault Display Unit (CFDS) MENU page comes into view. (c) Open, safety and tag these circuit breakers : PANEL DESIGNATION FIN LOCATION SEE NOTES 49VU AUTO FLT/FAC1/28VDC 5CC1 04 B 49VU AUTO FLT/FAC1/26VAC 14CC1 03 B 121VU AUTO FLT/FAC2/28VDC 5CC2 19 M 121VU AUTO FLT/FAC2/26VAC 14CC2 18 M (d) Replace or reprogram the OBRMs on the FACs (1CC1, 1CC2) Refer to THALES Service Bulletin No. B397BAM-22-046 and THALES Service Bulletin No. B397BAM-22-048. **CONF 002 (1) Subtask 221461-831-001-006 - In the Main Rack 80VU, Modify the two FACs (1CC1, 1CC2) by Replacement or by Reprogramming of their OBRMs. Work Zones and Access Panels Zone Access/Work location 120 Access Door 824 Work location Electrical panel 80VU 210 Access Door 831 References Aircraft Maintenance Manual (AMM) Task 22-96-00-710-001 Task 31-32-00-860-001 Vendor Service Bulletin (VSB) THALES B397BAM-22-046 THALES B397BAM-22-048 (a) Do the operational test of the AFS (Refer to AMM Task 22-96-00-710-001).

DATE: Oct 31/13 SERVICE BULLETIN No.: A320-22-1461 REVISION No.: 07 - Mar 23/15 Page: 22 5

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# @A318/A319/A320/A321 SERVICE BULLETIN (b) Do the Line Replaceable Unit (LRU) identification test: 1 Job set-up:
a Do the procedure to get access to the SYSTEM REPORT/TEST Menu page (Refer to AMM Task 31-32-00-860-001). b Make sure that these circuit breakers are closed: PANEL DESIGNATION FIN LOCATION SEE NOTES 121VU PTR/SPLY 6TW 21 J (01) 121VU PTR/SPLY 6TW 20 K (01) 49VU AUTO FLT/FAC1/28VDC 5CC1 04 B 49VU AUTO FLT/FAC1/26VAC 14CC1 03 B 121VU AUTO FLT/FAC2/28VDC 5CC2 19 M 121VU AUTO FLT/FAC2/26VAC 14CC2 18 M NOTE (01): The location of the CB depends on the A/C configuration. 2 Procedure: ACTION RESULT 1. On the SYSTEM REPORT/TEST page : - Push the line key adjacent to the AFS indication. - The AFS MAIN MENU page comes into view 2. On the AFS MAIN MENU page : - Push the line key adjacent to the LRU IDENT

indication. - The AFS/LRU IDENTIFICATION page comes into view. 3. On the AFS/LRU IDENTIFICATION page : - Make sure that the P/N of the two FACs is

B397BAM0619 4. Print the AFS/LRU IDENTIFICATION page (if the printer is not available, a visual check is acceptable) 3 Close-up:
a Put the aircraft back to its initial configuration. b On the Multipurpose Control and Display Unit (MCDU), push the line key adjacent to the RETURN indication until the Centralized Fault Display Unit (CFDS) MENU page comes into view. (c) Open, safety and tag these circuit breakers : PANEL DESIGNATION FIN LOCATION SEE NOTES 49VU AUTO FLT/FAC1/28VDC 5CC1 04 B 49VU AUTO FLT/FAC1/26VAC 14CC1 03 B 121VU AUTO FLT/FAC2/28VDC 5CC2 19 M
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# @A318/A319/A320/A321 SERVICE BULLETIN

PANEL DESIGNATION FIN LOCATION SEE NOTES 121VU AUTO FLT/FAC2/26VAC 14CC2 18 M (d) Replace or reprogram the OBRMs on the FACs (1CC1, 1CC2) Refer to THALES Service Bulletin No. B397BAM-22-046 and THALES Service Bulletin No. B397BAM-22-048. **CONF 003 (1) Subtask 221461-831-001-005 - In the Main Rack 80VU, Modify the two FACs (1CC1, 1CC2) by Replacement or by Reprogramming of their OBRMs. Work Zones and Access Panels Zone Access/Work location 120 Access Door 824 Work location Electrical panel 80VU 210 Access Door 831 References Aircraft Maintenance Manual (AMM) Task 22-96-00-710-001 Task 31-32-00-860-001 Vendor Service Bulletin (VSB) THALES B397BAM-22-044 THALES B397BAM-22-046 THALES B397BAM-22-048 (a) Do the operational test of the AFS (Refer to AMM Task 22-96-00-710-001). (b) Do the Line Replaceable Unit (LRU) identification test: 1 Job set-up:
a Do the procedure to get access to the SYSTEM REPORT/TEST Menu page (Refer to AMM Task 31-32-00-860-001). b Make sure that these circuit breakers are closed: PANEL DESIGNATION FIN LOCATION SEE NOTES 121VU PTR/SPLY 6TW 21 J (01) 121VU PTR/SPLY 6TW 20 K (01) 49VU AUTO FLT/FAC1/28VDC 5CC1 04 B 49VU AUTO FLT/FAC1/26VAC 14CC1 03 B 121VU AUTO FLT/FAC2/28VDC 5CC2 19 M 121VU AUTO FLT/FAC2/26VAC 14CC2 18 M NOTE (01): The location of the CB depends on the A/C configuration. 2 Procedure: ACTION RESULT

DATE: Oct 31/13 SERVICE BULLETIN No.: A320-22-1461 REVISION No.: 07 - Mar 23/15 Page: 24 5

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# @A318/A319/A320/A321 SERVICE BULLETIN
1. On the SYSTEM REPORT/TEST page : - Push the line key adjacent to the AFS indication. - The AFS MAIN MENU page comes into view 2. On the AFS MAIN MENU page : - Push the line key adjacent to the LRU IDENT

indication. - The AFS/LRU IDENTIFICATION page comes into view. 3. On the AFS/LRU IDENTIFICATION page : - Make sure that the P/N of the two FACs is

B397BAM0513 4. Print the AFS/LRU IDENTIFICATION page (if the printer is not available, a visual check is acceptable) 3 Close-up:
a Put the aircraft back to its initial configuration. b On the Multipurpose Control and Display Unit (MCDU), push the line key adjacent to the RETURN indication until the Centralized Fault Display Unit (CFDS) MENU page comes into view. (c) Open, safety and tag these circuit breakers : PANEL DESIGNATION FIN LOCATION SEE NOTES 49VU AUTO FLT/FAC1/28VDC 5CC1 04 B 49VU AUTO FLT/FAC1/26VAC 14CC1 03 B 121VU AUTO FLT/FAC2/28VDC 5CC2 19 M 121VU AUTO FLT/FAC2/26VAC 14CC2 18 M (d) Replace or reprogram the OBRMs on the FACs (1CC1, 1CC2) Refer to THALES Service Bulletin No. B397BAM-22-044, THALES Service Bulletin No. B397BAM-22-046 and THALES Service Bulletin No. B397BAM-22-048. **CONF 004 (1) Subtask 221461-831-001-007 - In the Main Rack 80VU, Modify the two FACs (1CC1, 1CC2) by Replacement or by Reprogramming of their OBRMs. Work Zones and Access Panels Zone Access/Work location 120 Access Door 824 Work location Electrical panel 80VU 210 Access Door 831 References Aircraft Maintenance Manual (AMM) Task 22-96-00-710-001 Task 31-32-00-860-001

DATE: Oct 31/13 SERVICE BULLETIN No.: A320-22-1461 REVISION No.: 07 - Mar 23/15 Page: 25 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

References Vendor Service Bulletin (VSB) THALES B397BAM-22-046 THALES B397BAM-22-048 (a) Do the operational test of the AFS (Refer to AMM Task 22-96-00-710-001). (b) Do the Line Replaceable Unit (LRU) identification test: 1 Job set-up:
a Do the procedure to get access to the SYSTEM REPORT/TEST Menu page (Refer to AMM Task 31-32-00-860-001). b Make sure that these circuit breakers are closed: PANEL DESIGNATION FIN LOCATION SEE NOTES 121VU PTR/SPLY 6TW 21 J (01) 121VU PTR/SPLY 6TW 20 K (01) 49VU AUTO FLT/FAC1/28VDC 5CC1 04 B 49VU AUTO FLT/FAC1/26VAC 14CC1 03 B 121VU AUTO FLT/FAC2/28VDC 5CC2 19 M 121VU AUTO FLT/FAC2/26VAC 14CC2 18 M NOTE (01): The location of the CB depends on the A/C configuration. 2 Procedure: ACTION RESULT 1. On the SYSTEM REPORT/TEST page : - Push the line key adjacent to the AFS indication. - The AFS MAIN MENU page comes into view 2. On the AFS MAIN MENU page : - Push the line key adjacent to the LRU IDENT

indication. - The AFS/LRU IDENTIFICATION page comes into view. 3. On the AFS/LRU IDENTIFICATION page : - Make sure that the P/N of the two FACs is

B397BAM0617 4. Print the AFS/LRU IDENTIFICATION page (if the printer is not available, a visual check is acceptable) 3 Close-up:
a Put the aircraft back to its initial configuration. b On the Multipurpose Control and Display Unit (MCDU), push the line key adjacent to the RETURN indication until the Centralized Fault Display Unit (CFDS) MENU page comes into view.

DATE: Oct 31/13 SERVICE BULLETIN No.: A320-22-1461 REVISION No.: 07 - Mar 23/15 Page: 26 5

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# @A318/A319/A320/A321 SERVICE BULLETIN (c) Open, safety and tag these circuit breakers : PANEL DESIGNATION FIN LOCATION SEE NOTES 49VU AUTO FLT/FAC1/28VDC 5CC1 04 B 49VU AUTO FLT/FAC1/26VAC 14CC1 03 B 121VU AUTO FLT/FAC2/28VDC 5CC2 19 M 121VU AUTO FLT/FAC2/26VAC 14CC2 18 M (d) Replace or reprogram the OBRMs on the FACs (1CC1, 1CC2) Refer to THALES Service Bulletin No. B397BAM-22-046 and THALES Service Bulletin No. B397BAM-22-048. **CONF ALL D. TEST **CONF 001 (1) Subtask 221461-710-001-001 - Test after Removal or Reprogramming of the OBRMs of the FACs Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 22-62-00-710-001 Task 22-96-00-710-001 Task 22-97-00-710-001 Task 31-32-00-860-001 Vendor Service Bulletin (VSB) THALES B397BAM-22-046 THALES B397BAM-22-048 (a) Do the LRU identification test : 1 Job Set-up
a Do the procedure to get access to the SYSTEM REPORT/TEST Menu page (Refer to AMM Task 31-32-00-860-001). b Make sure that these circuit breakers are closed : PANEL DESIGNATION FIN LOCATION SEE NOTES 121VU PTR/SPLY 6TW 21 J (01) 121VU PTR/SPLY 6TW 20 K (01) 49VU AUTO FLT/FAC1/28VDC 5CC1 04 B 49VU AUTO FLT/FAC1/26VAC 14CC1 03 B 121VU AUTO FLT/FAC2/28VDC 5CC2 19 M 121VU AUTO FLT/FAC2/26VAC 14CC2 18 M NOTE (01): The location of the CB depends on the A/C configuration.

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# @A318/A319/A320/A321 SERVICE BULLETIN

2 Procedure : ACTION RESULT - On the SYSTEM REPORT/TEST page :

. Push the line key adjacent to the AFS

indication. - The AFS MAIN MENU page comes into view.

- On the AFS MAIN MENU page :

. Push the line key adjacent to the LRU IDENT

indication. - The AFS/LRU IDENTIFICATION page comes into view. - On the AFS/LRU IDENTIFICATION page :

. Make sure that the new PN of the two FACs is

B397BAM0623. - Print the AFS/LRU IDENTIFICATION page (if

the printer is not available, a visual check is acceptable). 3 Close-up :
a Put the aircraft back to its initial configuration. b On the MCDU, push the line key adjacent to the RETURN indication until the CFDS MENU page comes into view. (b) Do the operational test of the AFS (Refer to AMM Task 22-96-00-710-001). NOTE: If the airline operates the aircraft in CATIII conditions, do the Land CATIII capability test (Refer to AMM Task 22-97-00-710-001). NOTE: If you remove the FACs after this CFDS indication : YD ACTR 3CC1 (2), you must do the test with the hydraulic pressure available (Green for the FAC1, Yellow for the FAC2). NOTE: As an alternative, you can do this operational test without the CFDS (Refer to AMM Task 22-62-00-710-001). **CONF 002 (1) Subtask 221461-710-001-001 - Test after Removal or Reprogramming of the OBRMs of the FACs Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 22-62-00-710-001 Task 22-96-00-710-001 Task 22-97-00-710-001 Task 31-32-00-860-001

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# @A318/A319/A320/A321 SERVICE BULLETIN

References Vendor Service Bulletin (VSB) THALES B397BAM-22-046 THALES B397BAM-22-048 (a) Do the LRU identification test : 1 Job Set-up
a Do the procedure to get access to the SYSTEM REPORT/TEST Menu page (Refer to AMM Task 31-32-00-860-001). b Make sure that these circuit breakers are closed : PANEL DESIGNATION FIN LOCATION SEE NOTES 121VU PTR/SPLY 6TW 21 J (01) 121VU PTR/SPLY 6TW 20 K (01) 49VU AUTO FLT/FAC1/28VDC 5CC1 04 B 49VU AUTO FLT/FAC1/26VAC 14CC1 03 B 121VU AUTO FLT/FAC2/28VDC 5CC2 19 M 121VU AUTO FLT/FAC2/26VAC 14CC2 18 M NOTE (01): The location of the CB depends on the A/C configuration. 2 Procedure : ACTION RESULT - On the SYSTEM REPORT/TEST page :

. Push the line key adjacent to the AFS

indication. - The AFS MAIN MENU page comes into view.

- On the AFS MAIN MENU page :

. Push the line key adjacent to the LRU IDENT

indication. - The AFS/LRU IDENTIFICATION page comes into view. - On the AFS/LRU IDENTIFICATION page :

. Make sure that the new PN of the two FACs is

B397BAM0623. - Print the AFS/LRU IDENTIFICATION page (if

the printer is not available, a visual check is acceptable). 3 Close-up :
a Put the aircraft back to its initial configuration. b On the MCDU, push the line key adjacent to the RETURN indication until the CFDS MENU page comes into view. (b) Do the operational test of the AFS (Refer to AMM Task 22-96-00-710-001). NOTE: If the airline operates the aircraft in CATIII conditions, do the Land
DATE: Oct 31/13 SERVICE BULLETIN No.: A320-22-1461 REVISION No.: 07 - Mar 23/15 Page: 29 5

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# @A318/A319/A320/A321 SERVICE BULLETIN CATIII capability test (Refer to AMM Task 22-97-00-710-001). NOTE: If you remove the FACs after this CFDS indication : YD ACTR 3CC1 (2), you must do the test with the hydraulic pressure available (Green for the FAC1, Yellow for the FAC2). NOTE: As an alternative, you can do this operational test without the CFDS (Refer to AMM Task 22-62-00-710-001). **CONF 003 (1) Subtask 221461-710-001-002 - Test after Removal or Reprogramming of the OBRMs of the FACs Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 22-62-00-710-001 Task 22-96-00-710-001 Task 22-97-00-710-001 Task 31-32-00-860-001 Vendor Service Bulletin (VSB) THALES B397BAM-22-044 THALES B397BAM-22-046 THALES B397BAM-22-048 (a) Do the LRU identification test : 1 Job Set-up
a Do the procedure to get access to the SYSTEM REPORT/TEST Menu page (Refer to AMM Task 31-32-00-860-001). b Make sure that these circuit breakers are closed : PANEL DESIGNATION FIN LOCATION SEE NOTES 121VU PTR/SPLY 6TW 21 J (01) 121VU PTR/SPLY 6TW 20 K (01) 49VU AUTO FLT/FAC1/28VDC 5CC1 04 B 49VU AUTO FLT/FAC1/26VAC 14CC1 03 B 121VU AUTO FLT/FAC2/28VDC 5CC2 19 M 121VU AUTO FLT/FAC2/26VAC 14CC2 18 M NOTE (01): The location of the CB depends on the A/C configuration. 2 Procedure : ACTION RESULT - On the SYSTEM REPORT/TEST page :

. Push the line key adjacent to the AFS

indication. - The AFS MAIN MENU page comes into view.

DATE: Oct 31/13 SERVICE BULLETIN No.: A320-22-1461 REVISION No.: 07 - Mar 23/15 Page: 30 5

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# @A318/A319/A320/A321 SERVICE BULLETIN
- On the AFS MAIN MENU page :

. Push the line key adjacent to the LRU IDENT

indication. - The AFS/LRU IDENTIFICATION page comes into view. - On the AFS/LRU IDENTIFICATION page :

. Make sure that the new PN of the two FACs is

B397BAM0623. - Print the AFS/LRU IDENTIFICATION page (if

the printer is not available, a visual check is acceptable). 3 Close-up :
a Put the aircraft back to its initial configuration. b On the MCDU, push the line key adjacent to the RETURN indication until the CFDS MENU page comes into view. (b) Do the operational test of the AFS (Refer to AMM Task 22-96-00-710-001). NOTE: If the airline operates the aircraft in CATIII conditions, do the Land CATIII capability test (Refer to AMM Task 22-97-00-710-001). NOTE: If you remove the FACs after this CFDS indication : YD ACTR 3CC1 (2), you must do the test with the hydraulic pressure available (Green for the FAC1, Yellow for the FAC2). NOTE: As an alternative, you can do this operational test without the CFDS (Refer to AMM Task 22-62-00-710-001). **CONF 004 (1) Subtask 221461-710-001-001 - Test after Removal or Reprogramming of the OBRMs of the FACs Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 22-62-00-710-001 Task 22-96-00-710-001 Task 22-97-00-710-001 Task 31-32-00-860-001 Vendor Service Bulletin (VSB) THALES B397BAM-22-046 THALES B397BAM-22-048 (a) Do the LRU identification test : 1 Job Set-up
a Do the procedure to get access to the SYSTEM REPORT/TEST Menu page (Refer to AMM Task 31-32-00-860-001). DATE: Oct 31/13 SERVICE BULLETIN No.: A320-22-1461 REVISION No.: 07 - Mar 23/15 Page: 31 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

b Make sure that these circuit breakers are closed : PANEL DESIGNATION FIN LOCATION SEE NOTES 121VU PTR/SPLY 6TW 21 J (01) 121VU PTR/SPLY 6TW 20 K (01) 49VU AUTO FLT/FAC1/28VDC 5CC1 04 B 49VU AUTO FLT/FAC1/26VAC 14CC1 03 B 121VU AUTO FLT/FAC2/28VDC 5CC2 19 M 121VU AUTO FLT/FAC2/26VAC 14CC2 18 M NOTE (01): The location of the CB depends on the A/C configuration. 2 Procedure : ACTION RESULT - On the SYSTEM REPORT/TEST page :

. Push the line key adjacent to the AFS

indication. - The AFS MAIN MENU page comes into view.

- On the AFS MAIN MENU page :

. Push the line key adjacent to the LRU IDENT

indication. - The AFS/LRU IDENTIFICATION page comes into view. - On the AFS/LRU IDENTIFICATION page :

. Make sure that the new PN of the two FACs is

B397BAM0623. - Print the AFS/LRU IDENTIFICATION page (if

the printer is not available, a visual check is acceptable). 3 Close-up :
a Put the aircraft back to its initial configuration. b On the MCDU, push the line key adjacent to the RETURN indication until the CFDS MENU page comes into view. (b) Do the operational test of the AFS (Refer to AMM Task 22-96-00-710-001). NOTE: If the airline operates the aircraft in CATIII conditions, do the Land CATIII capability test (Refer to AMM Task 22-97-00-710-001). NOTE: If you remove the FACs after this CFDS indication : YD ACTR 3CC1 (2), you must do the test with the hydraulic pressure available (Green for the FAC1, Yellow for the FAC2). NOTE: As an alternative, you can do this operational test without the CFDS (Refer to AMM Task 22-62-00-710-001).

DATE: Oct 31/13 SERVICE BULLETIN No.: A320-22-1461 REVISION No.: 07 - Mar 23/15 Page: 32 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

**CONF ALL E. CLOSE-UP **CONF 001 (1) Subtask 221461-942-001-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 52-41-00-410-002 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Close the Avionic Compartment Door 824 (Refer to AMM Task 52-41-00-410-002). (c) Restore the systems and the aircraft to normal operating condition. **CONF 002 (1) Subtask 221461-942-001-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 52-41-00-410-002 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Close the Avionic Compartment Door 824 (Refer to AMM Task 52-41-00-410-002). (c) Restore the systems and the aircraft to normal operating condition. **CONF 003 (1) Subtask 221461-942-001-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 52-41-00-410-002 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Close the Avionic Compartment Door 824 (Refer to AMM Task 52-41-00-410-002).
DATE: Oct 31/13 SERVICE BULLETIN No.: A320-22-1461 REVISION No.: 07 - Mar 23/15 Page: 33 5

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# @A318/A319/A320/A321 SERVICE BULLETIN (c) Restore the systems and the aircraft to normal operating condition. **CONF 004 (1) Subtask 221461-942-001-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 52-41-00-410-002 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Close the Avionic Compartment Door 824 (Refer to AMM Task 52-41-00-410-002). (c) Restore the systems and the aircraft to normal operating condition.

DATE: Oct 31/13 SERVICE BULLETIN No.: A320-22-1461 REVISION No.: 07 - Mar 23/15 Page: 34 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

Task 221461-831-802-001 - Modification by Replacement of the FACs. **CONF ALL 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. NOTE: The accomplishment instructions of this Service Bulletin refer to procedures included in other AIRBUS documents. When the words ’refer to’ are used and the operator has an accepted alternative procedure, the accepted alternative procedure can be used. When the words ’in accordance with’ are included in the instruction, the procedure in the AIRBUS document must be used. NOTE: The access and close-up instructions, not comprising return to service tests, in this Service Bulletin do not constitute or affect the technical intent of the Service Bulletin. Operators can therefore, as deemed necessary, omit or add access and/or close-up steps to add flexibility to their maintenance operations as long as the technical intent of the Service Bulletin is met within the set parameters. NOTE: Manual titles given in the accomplishment instructions are referred to by acronyms. Refer to paragraph 1.J., References, for the definition of acronyms. Task Associated Data **CONF 001 Zone 120 210 Modified FIN 1CC1 1CC2 Access Door 824 831 Manpower TOTAL MANHOURS 2.50
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# @A318/A319/A320/A321 SERVICE BULLETIN
ELAPSED TIME (HOURS) 2.50 **CONF 002 Zone 120 210 Modified FIN 1CC1 1CC2 Access Door 824 831 Manpower TOTAL MANHOURS 2.50 ELAPSED TIME (HOURS) 2.50 **CONF 003 Zone 120 210 Modified FIN 1CC1 1CC2 Access Door 824 831 Manpower TOTAL MANHOURS 2.50 ELAPSED TIME (HOURS) 2.50 **CONF 004 Zone 120 210 Modified FIN 1CC1 1CC2 Access Door 824 831 Manpower TOTAL MANHOURS 2.50 ELAPSED TIME (HOURS) 2.50 **CONF ALL A. GENERAL **CONF 001 (1) Subtask 221461-839-002-001 - Administrative Manpower Resources Skills NON SPECIFIC

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# @A318/A319/A320/A321 SERVICE BULLETIN (a) Write in the applicable aircraft records that you have done all the work given in this Service Bulletin. **CONF 002 (1) Subtask 221461-839-002-001 - Administrative Manpower Resources Skills NON SPECIFIC (a) Write in the applicable aircraft records that you have done all the work given in this Service Bulletin. **CONF 003 (1) Subtask 221461-839-002-001 - Administrative Manpower Resources Skills NON SPECIFIC (a) Write in the applicable aircraft records that you have done all the work given in this Service Bulletin. **CONF 004 (1) Subtask 221461-839-002-001 - Administrative Manpower Resources Skills NON SPECIFIC (a) Write in the applicable aircraft records that you have done all the work given in this Service Bulletin. **CONF ALL B. PREPARATION **CONF 001 (1) Subtask 221461-941-002-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 12-34-24-869-002 Task 22-66-34-000-002 Task 52-41-00-010-002 (a) Make sure that the aircraft is electrically grounded (Refer to AMM Task 12-34-24-869-002).

DATE: Oct 31/13 SERVICE BULLETIN No.: A320-22-1461 REVISION No.: 07 - Mar 23/15 Page: 37 5

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# @A318/A319/A320/A321 SERVICE BULLETIN (b) Do the preparation procedure as specified in the removal of the FAC (1CC1, 1CC2) (Refer to AMM Task 22-66-34-000-002). (c) The following items shall be considered as the basic Aircraft configuration before you start a maintenance task: - Aircraft on the ground resting on landing gear (the ground safety locks and the wheel chocks are in position on the landing gear). - Engine shut down, thrust reversers closed and locked. - Aircraft in clean configuration. - Parking brake applied. - Aircraft electrical network de-energized. - Hydraulic systems depressurized. - Access to the cockpit and cabin is available. - All circuit breakers are in closed position. - All controls in NORM, AUTO or OFF position. (d) Open the Avionic Compartment Door 824 (Refer to AMM Task 52-41-00-010-002). **CONF 002 (1) Subtask 221461-941-002-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 12-34-24-869-002 Task 22-66-34-000-002 Task 52-41-00-010-002 (a) Make sure that the aircraft is electrically grounded (Refer to AMM Task 12-34-24-869-002). (b) Do the preparation procedure as specified in the removal of the FAC (1CC1, 1CC2) (Refer to AMM Task 22-66-34-000-002). (c) The following items shall be considered as the basic Aircraft configuration before you start a maintenance task: - Aircraft on the ground resting on landing gear (the ground safety locks and the wheel chocks are in position on the landing gear). - Engine shut down, thrust reversers closed and locked.

DATE: Oct 31/13 SERVICE BULLETIN No.: A320-22-1461 REVISION No.: 07 - Mar 23/15 Page: 38 5

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# @A318/A319/A320/A321 SERVICE BULLETIN - Aircraft in clean configuration. - Parking brake applied. - Aircraft electrical network de-energized. - Hydraulic systems depressurized. - Access to the cockpit and cabin is available. - All circuit breakers are in closed position. - All controls in NORM, AUTO or OFF position. (d) Open the Avionic Compartment Door 824 (Refer to AMM Task 52-41-00-010-002). **CONF 003 (1) Subtask 221461-941-002-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 12-34-24-869-002 Task 22-66-34-000-002 Task 52-41-00-010-002 (a) Make sure that the aircraft is electrically grounded (Refer to AMM Task 12-34-24-869-002). (b) Do the preparation procedure as specified in the removal of the FAC (1CC1, 1CC2) (Refer to AMM Task 22-66-34-000-002). (c) The following items shall be considered as the basic Aircraft configuration before you start a maintenance task: - Aircraft on the ground resting on landing gear (the ground safety locks and the wheel chocks are in position on the landing gear). - Engine shut down, thrust reversers closed and locked. - Aircraft in clean configuration. - Parking brake applied. - Aircraft electrical network de-energized. - Hydraulic systems depressurized. - Access to the cockpit and cabin is available. - All circuit breakers are in closed position.

DATE: Oct 31/13 SERVICE BULLETIN No.: A320-22-1461 REVISION No.: 07 - Mar 23/15 Page: 39 5

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# @A318/A319/A320/A321 SERVICE BULLETIN - All controls in NORM, AUTO or OFF position. (d) Open the Avionic Compartment Door 824 (Refer to AMM Task 52-41-00-010-002). **CONF 004 (1) Subtask 221461-941-002-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 12-34-24-869-002 Task 22-66-34-000-002 Task 52-41-00-010-002 (a) Make sure that the aircraft is electrically grounded (Refer to AMM Task 12-34-24-869-002). (b) Do the preparation procedure as specified in the removal of the FAC (1CC1, 1CC2) (Refer to AMM Task 22-66-34-000-002). (c) The following items shall be considered as the basic Aircraft configuration before you start a maintenance task: - Aircraft on the ground resting on landing gear (the ground safety locks and the wheel chocks are in position on the landing gear). - Engine shut down, thrust reversers closed and locked. - Aircraft in clean configuration. - Parking brake applied. - Aircraft electrical network de-energized. - Hydraulic systems depressurized. - Access to the cockpit and cabin is available. - All circuit breakers are in closed position. - All controls in NORM, AUTO or OFF position. (d) Open the Avionic Compartment Door 824 (Refer to AMM Task 52-41-00-010-002).

DATE: Oct 31/13 SERVICE BULLETIN No.: A320-22-1461 REVISION No.: 07 - Mar 23/15 Page: 40 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

**CONF ALL C. PROCEDURE **CONF 001 (1) Subtask 221461-831-002-002 - Replace the FACs (1CC1, 1CC2) Work Zones and Access Panels Zone Access/Work location 120 Access Door 824 Work location Electrical panel 80VU 210 Access Door 831 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 SEE NOTES B397BAM0623 2 FAC References Aircraft Maintenance Manual (AMM) Task 22-66-34-000-002 Task 22-66-34-400-002 (a) Remove: Refer to AMM Task 22-66-34-000-002 FIN 1CC1 1 FAC B397BAM0620 FIN 1CC2 1 FAC B397BAM0620 (b) Install: Refer to AMM Task 22-66-34-400-002 FIN 1CC1 1 FAC B397BAM0623 FIN 1CC2 1 FAC B397BAM0623

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# @A318/A319/A320/A321 SERVICE BULLETIN

**CONF 002 (1) Subtask 221461-831-002-004 - Replace the FACs (1CC1, 1CC2) Work Zones and Access Panels Zone Access/Work location 120 Access Door 824 Work location Electrical panel 80VU 210 Access Door 831 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 COMPA02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES B397BAM0623 2 FAC References Aircraft Maintenance Manual (AMM) Task 22-66-34-000-002 Task 22-66-34-400-002 (a) Remove: Refer to AMM Task 22-66-34-000-002 FIN 1CC1 1 FAC B397BAM0619 FIN 1CC2 1 FAC B397BAM0619 (b) Install: Refer to AMM Task 22-66-34-400-002 FIN 1CC1 1 FAC B397BAM0623 FIN 1CC2 1 FAC B397BAM0623

DATE: Oct 31/13 SERVICE BULLETIN No.: A320-22-1461 REVISION No.: 07 - Mar 23/15 Page: 42 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

**CONF 003 (1) Subtask 221461-831-002-005 - Replace the FACs (1CC1, 1CC2) Work Zones and Access Panels Zone Access/Work location 120 Access Door 824 Work location Electrical panel 80VU 210 Access Door 831 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 COMPA03 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES B397BAM0623 2 FAC References Aircraft Maintenance Manual (AMM) Task 22-66-34-000-002 Task 22-66-34-400-002 (a) Remove: Refer to AMM Task 22-66-34-000-002 FIN 1CC1 1 FAC B397BAM0513 FIN 1CC2 1 FAC B397BAM0513 (b) Install: Refer to AMM Task 22-66-34-400-002 FIN 1CC1 1 FAC B397BAM0623 FIN 1CC2 1 FAC B397BAM0623

DATE: Oct 31/13 SERVICE BULLETIN No.: A320-22-1461 REVISION No.: 07 - Mar 23/15 Page: 43 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

**CONF 004 (1) Subtask 221461-831-002-006 - Replace the FACs (1CC1, 1CC2) Work Zones and Access Panels Zone Access/Work location 120 Access Door 824 Work location Electrical panel 80VU 210 Access Door 831 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 COMPA04 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES B397BAM0623 2 FAC References Aircraft Maintenance Manual (AMM) Task 22-66-34-000-002 Task 22-66-34-400-002 (a) Remove: Refer to AMM Task 22-66-34-000-002 FIN 1CC1 1 FAC B397BAM0617 FIN 1CC2 1 FAC B397BAM0617 (b) Install: Refer to AMM Task 22-66-34-400-002 FIN 1CC1 1 FAC B397BAM0623 FIN 1CC2 1 FAC B397BAM0623

DATE: Oct 31/13 SERVICE BULLETIN No.: A320-22-1461 REVISION No.: 07 - Mar 23/15 Page: 44 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

**CONF ALL D. TEST **CONF 001 (1) Subtask 221461-700-001-001 - Testing Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 22-66-34-400-002 (a) Job Set-up: 1 Remove the safety clips and tags and close the circuit breakers as specified after the installation of the FAC (1CC1, 1CC2) (Refer to AMM Task 22-66-34-400-002). (b) Procedure: 1 Do the test after the installation of the FACs (Refer to AMM Task 22-66-34-400-002). **CONF 002 (1) Subtask 221461-700-001-001 - Testing Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 22-66-34-400-002 (a) Job Set-up: 1 Remove the safety clips and tags and close the circuit breakers as specified after the installation of the FAC (1CC1, 1CC2) (Refer to AMM Task 22-66-34-400-002). (b) Procedure: 1 Do the test after the installation of the FACs (Refer to AMM Task 22-66-34-400-002). **CONF 003 (1) Subtask 221461-700-001-001 - Testing Manpower Resources Skills NON SPECIFIC
DATE: Oct 31/13 SERVICE BULLETIN No.: A320-22-1461 REVISION No.: 07 - Mar 23/15 Page: 45 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

References Aircraft Maintenance Manual (AMM) Task 22-66-34-400-002 (a) Job Set-up: 1 Remove the safety clips and tags and close the circuit breakers as specified after the installation of the FAC (1CC1, 1CC2) (Refer to AMM Task 22-66-34-400-002). (b) Procedure: 1 Do the test after the installation of the FACs (Refer to AMM Task 22-66-34-400-002). **CONF 004 (1) Subtask 221461-700-001-001 - Testing Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 22-66-34-400-002 (a) Job Set-up: 1 Remove the safety clips and tags and close the circuit breakers as specified after the installation of the FAC (1CC1, 1CC2) (Refer to AMM Task 22-66-34-400-002). (b) Procedure: 1 Do the test after the installation of the FACs (Refer to AMM Task 22-66-34-400-002). **CONF ALL E. CLOSE-UP **CONF 001 (1) Subtask 221461-942-002-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 22-66-34-400-002 Task 52-41-00-410-002 (a) Make sure that the work areas are clean and clear of tools and other items of equipment.
DATE: Oct 31/13 SERVICE BULLETIN No.: A320-22-1461 REVISION No.: 07 - Mar 23/15 Page: 46 5

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# @A318/A319/A320/A321 SERVICE BULLETIN (b) Do the close-up procedure as specified in the installation of the FACs (Refer to AMM Task 22-66-34-400-002). (c) Close the Avionic Compartment Door 824 (Refer to AMM Task 52-41-00-410-002). (d) Restore the systems and the aircraft to normal operating condition. **CONF 002 (1) Subtask 221461-942-002-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 22-66-34-400-002 Task 52-41-00-410-002 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Do the close-up procedure as specified in the installation of the FACs (Refer to AMM Task 22-66-34-400-002). (c) Close the Avionic Compartment Door 824 (Refer to AMM Task 52-41-00-410-002). (d) Restore the systems and the aircraft to normal operating condition. **CONF 003 (1) Subtask 221461-942-002-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 22-66-34-400-002 Task 52-41-00-410-002 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Do the close-up procedure as specified in the installation of the FACs (Refer to AMM Task 22-66-34-400-002). (c) Close the Avionic Compartment Door 824 (Refer to AMM Task 52-41-00-410-002). (d) Restore the systems and the aircraft to normal operating condition.

DATE: Oct 31/13 SERVICE BULLETIN No.: A320-22-1461 REVISION No.: 07 - Mar 23/15 Page: 47 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

**CONF 004 (1) Subtask 221461-942-002-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 22-66-34-400-002 Task 52-41-00-410-002 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Do the close-up procedure as specified in the installation of the FACs (Refer to AMM Task 22-66-34-400-002). (c) Close the Avionic Compartment Door 824 (Refer to AMM Task 52-41-00-410-002). (d) Restore the systems and the aircraft to normal operating condition.

DATE: Oct 31/13 SERVICE BULLETIN No.: A320-22-1461 REVISION No.: 07 - Mar 23/15 Page: 48 5

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# @A318/A319/A320/A321 SERVICE BULLETIN Appendix 01: Retrofitted Modifications **CONF ALL MOD Config. 001 Config. 002 Config. 003 Config. 004 160011P12126 X X X X 160065P13119 X X X X 38777P10777 X X X 36766P9906 X X 35522P9122 X X 33299P8256 X 31040P6954 X 30439P6703 X NOTE: X is used for the retrofitted modifications after accomplishment of this service bulletin.

DATE: Oct 31/13 SERVICE BULLETIN No.: A320-22-1461 REVISION No.: 07 - Mar 23/15 Page: 1 5

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# @A318/A319/A320/A321 SERVICE BULLETIN REPORTING SHEET 

### TITLE: AUTO FLIGHT - FLIGHT AUGMENTATION COMPUTER (FAC) - INSTALL FAC B623 (SHARKLET PROJECT) MODIFICATION No.: 30439P6703 31040P6954 33299P8256 35522P9122 36766P9906 38777P10777 160011P12126 160065P13119 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: Oct 31/13 SERVICE BULLETIN No.: A320-22-1461 REVISION No.: 07 - Mar 23/15 Page: 1 5

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# @A318/A319/A320/A321 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 4321 - Quality rating of the Accomplishment Instructions 4321 - Quality rating of the Illustrations 4321 - 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: Oct 31/13 SERVICE BULLETIN No.: A320-22-1461 REVISION No.: 07 - Mar 23/15 Page: 1 5

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