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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

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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

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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

MAJOR 30439P6703 31040P6954 33299P8256 35522P9122 36766P9906

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

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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

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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

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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

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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

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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

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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

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(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

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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

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**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

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(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

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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

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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

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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

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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

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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 prior

to 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

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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

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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

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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

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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

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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

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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

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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

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(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

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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

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- 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

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**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

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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

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(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

DATE: Oct 31/13 SERVICE BULLETIN No.: A320-22-1461

REVISION No.: 07 - Mar 23/15 Page: 23

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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

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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

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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

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(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.

DATE: Oct 31/13 SERVICE BULLETIN No.: A320-22-1461

REVISION No.: 07 - Mar 23/15 Page: 27

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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

DATE: Oct 31/13 SERVICE BULLETIN No.: A320-22-1461

REVISION No.: 07 - Mar 23/15 Page: 28

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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

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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

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- 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

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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

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**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

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(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

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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

DATE: Oct 31/13 SERVICE BULLETIN No.: A320-22-1461

REVISION No.: 07 - Mar 23/15 Page: 35

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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

DATE: Oct 31/13 SERVICE BULLETIN No.: A320-22-1461

REVISION No.: 07 - Mar 23/15 Page: 36

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(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

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(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

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- 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

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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

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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

DATE: Oct 31/13 SERVICE BULLETIN No.: A320-22-1461

REVISION No.: 07 - Mar 23/15 Page: 41

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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

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**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

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**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

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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

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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

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(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

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**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

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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

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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

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SERVICE BULLETIN

QUALITY PERCEPTION FORM

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

that you provide us will be used to analyse areas of difficulties and to take corrective action to further

improve the quality of our Service Bulletins.

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

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

- Quality rating of this SB 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

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