@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 CAA02 INSTEAD OF FAC B621, 622, 623.

**CONF ALL

MODIFICATIONS

MODIFICATION CLASSIFICATION

MAJOR None

MINOR 157158P14838

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.

The Service Bulletin consists in installing FAC CAA02 standard in place of FAC B0621, B0622 or

B0623 standards.

Accomplishment of this Service Bulletin will satisfy the operator’s request.

FAC CAA02 provides dataloading capacity and improved performance. It includes the software

improvement of the FAC B0621 (ROPS) and of the FAC B0622/B0623 (Sharklets tunings for the A320

Sharklets family) with ROPS improvements.

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 NO

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SUMMARY

NOTE (1): Service Bulletin for convenience or option.

MATERIAL PRICE INFORMATION

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Component COMPA01 1 See SB FACs, Media

EFFECTIVITY

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

AAL

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

CONCURRENT REQUIREMENTS

For MSN 5678 5698 5704 5745 5753 5761 5781 5786 5788-5789 5798 5810 5827

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

following Service Bulletin(s):

Service Bulletin No. None

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 YES

OBRM NO

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SERVICE BULLETIN

SUMMARY

MANPOWER

Task 221502-831-801-001: Modification

TOTAL MANHOURS 2.25

ELAPSED TIME (HOURS) 2.25

APPENDICES

None

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SUMMARY

**CONF ALL

FR1

FR24A

Z120

A

A

OF THE FACs

REPLACEMENT

1CC2

1CC1

80VU

N_SB_221502_5_SAAA_01_00

Figure A-FSAAA - Sheet 01

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SUMMARY

**CONF ALL

A

1CCMD1

A

N_SB_221502_5_SBAA_01_00

Figure A-FSBAA - Sheet 01

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SERVICE BULLETIN

SUMMARY

This Page Intentionally Left Blank

DATE: Nov 14/14 SERVICE BULLETIN No.: A320-22-1502

REVISION No.: 00 - Nov 14/14 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 CAA02 INSTEAD OF FAC B621, 622, 623.

MODIFICATION No.: 157158P14838

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

319-115

(2) Effectivity by MSN

5678 5698 5704 5745 5753 5761 5781 5786 5788-5789 5798 5810 5827

(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

AAL 5678 5698 5704 5745 5753 5761 5781 5786 5788 5789 5798 5810

5827

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(4) Configuration by MSN

MSN CONFIGURATION

5678 5698 5704 5745 5753 5761 5781 5786 5788 5789 5798

5810 5827

001

(5) Configuration definition

**CONF 001

Config. 001 is valid for all the aircraft given in the effectivity of this Service Bulletin as a

standard configuration.

(6) Material Effectivity

MATERIAL QTY PER A/C SEE NOTES

Component COMPA01 1

B. CONCURRENT REQUIREMENTS

For MSN 5678 5698 5704 5745 5753 5761 5781 5786 5788-5789 5798 5810 5827

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

the following Service Bulletin(s):

Service Bulletin No. None

C. REASON

(1) History

This Service Bulletin is issued further to an operator’s request.

(2) Objective/Action

The Service Bulletin consists in installing FAC CAA02 standard in place of FAC B0621,

B0622 or B0623 standards.

(3) Advantages

Accomplishment of this Service Bulletin will satisfy the operator’s request.

FAC CAA02 provides dataloading capacity and improved performance. It includes the

software improvement of the FAC B0621 (ROPS) and of the FAC B0622/B0623

(Sharklets tunings for the A320 Sharklets family) with ROPS improvements.

(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

To accomplish this Service Bulletin it is necessary to :

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Task 221502-831-801-001: Modification

(1) Replace the FACs 1CC1 and 1CC2 in the Electronics rack 80VU.

(2) Install the media disk 1CCMD1 in the storage box.

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.

Task 221502-831-801-001: Modification

Get Access 0.50

On Aircraft

Replace the FACs 1CC1 and 1CC2 in the Electronics

rack 80VU.

0.50

Install the media disk 1CCMD1 in the storage box. 0.25

Tests 0.50

Close-Up 0.50

TOTAL MANHOURS 2.25

ELAPSED TIME (HOURS) 2.25

H. WEIGHT AND BALANCE

Manufacturers Empty Weight -3.4 KG (-7.4956 LB)

Effect on Balance -31.827 KGM (-230.204 LB.FT )

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I. ELECTRICAL LOAD DATA

Not Changed

J. REFERENCES

Aircraft Maintenance Manual (AMM) 12-34-24 22-66-34 31-32-00

ATA Common Support Data Dictionary (CSDD),

Chapter 2

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

K. PUBLICATION AFFECTED

Aircraft Wiring List (AWL)

Flight Crew Operating Manual (FCOM)

Illustrated Parts Catalog (IPC)

Master Minimum Equipment List (MMEL)

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).

L. INTERCHANGEABILITY/MIXABILITY

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE

NOTES

FacFlight Augmentation

Computer

B397BAM0622 C13206AA00 03 NO (1) (2) (3)

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

Common Support Data Dictionary (CSDD), Chapter 2.

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

Bulletin are approved.

NOTE (1): When the old P/N B397BAM0622 is removed, it can be replaced by:

- the old P/N B397BAM0622,

- the new P/N C13206AA00, provided that the LRU IDENT of the spare

FAC is C13206AA02, refer to NOTE (3).

NOTE (2): When the new P/N C13206AA00 with LRU IDENT C13206AA02 is removed, it

can be replaced only by the P/N C13206AA00 with LRU IDENT C13206AA02.

NOTE (3): P/N C13206AA02 is created to represent the complete computer (hardware

P/N C13206AA00 and software P/N G2856AAA02) and is displayed when

LRU IDENT is performed on aircraft.

In case the LRU IDENT of the spare FAC is different, if Mod. No.

153590P12462 is embodied, FAC software uploading can be performed as

per AMM.

M. SPARES

Fac-Flight Augmentation

Computer

B397BAM0622

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2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

(1) Procurement Addresses

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:

Component COMPA01 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

C13206AA00 2 FAC B397BAM0622 03

F1422927 1 MEDIA (1)

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

Common Support Data Dictionary (CSDD), Chapter 2.

NOTE (1): The disk FIN 1CCMD1 contains the software FINs 1CC1SW1 and

1CC2SW1 (PN G2856AAA02).

(3) Equipment

None

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E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

None

F. TOOLING

None

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3. ACCOMPLISHMENT INSTRUCTIONS

Task 221502-831-801-001 - Modification

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

INCLUDED IN THE REFERENCED PROCEDURES.

CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP

ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY

AND MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENANCE

WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING,

COMPONENTS AND THE WORK AREA AS CLEAN AS POSSIBLE. TO DO

THIS:

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

NECESSARY ON WIRING AND COMPONENTS

- REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND

OTHER CONTAMINATION.

THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION

AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION.

IF THERE IS CONTAMINATION REFER TO ESPM 20-55-00.

NOTE: The accomplishment instructions of this Service Bulletin include procedures given

in other documents or in other sections of the Service Bulletin. When the words

"refer to" are used and the operator has a procedure accepted by the local

authority he belongs to, the accepted alternative procedure can be used. When the

words "in accordance with" are used then the given procedure must be followed.

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

close-up steps to add flexibility yo 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

Zone

120 210

Modified FIN

1CC1 1CC2 1CCMD1

Access

Door 824

Manpower

TOTAL MANHOURS 2.25

ELAPSED TIME (HOURS) 2.25

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A. GENERAL

(1) Subtask 221502-839-001-001 - 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.

B. PREPARATION

(1) Subtask 221502-941-001-001 - 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

NOTE: The items given in this note 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.

(a) Make sure that the aircraft is electrically grounded, refer to AMM Task

12-34-24-869-002.

(b) Do the job set-up procedure as specified in the removal of the FACs (1CC1,

1CC2), refer to AMM Task 22-66-34-000-002.

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C. PROCEDURE

(1) Subtask 221502-960-001-001 - Replace the FACs 1CC1 and 1CC2 in the Electronics

rack 80VU.

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 824

Work location Electrical panel 80VU

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills NON SPECIFIC

Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

C13206AA00 2 FAC

References

Aircraft Maintenance Manual (AMM) Task 22-66-34-000-002

Task 22-66-34-400-002

Fig. A-FBAAA

Location of the two FACs 1CC1 and

1CC2

Sheet 01

(a) Remove:

Refer to AMM Task 22-66-34-000-002.

FIN 1CC1

1 FacFlight Augmentation

Computer

B397BAM0622

and

FIN 1CC2

1 FacFlight Augmentation

Computer

B397BAM0622

(b) Install:

Refer to AMM Task 22-66-34-400-002.

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FIN 1CC1

1 FacFlight Augmentation

Computer

C13206AA00

and

FIN 1CC2

1 FacFlight Augmentation

Computer

C13206AA00

(2) Subtask 221502-470-001-001 - Install the media disk 1CCMD1 in the storage box.

Work Zones and Access Panels

Zone Access/Work location

210

Manpower Resources

Manhours 0.25

Minimum number of person 1

Subtask elapsed time 0.25

Skills NON SPECIFIC

Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

F1422927 1 MEDIA (1)

NOTE (1): The disk FIN 1CCMD1 contains the software FINs 1CC1SW1 and

1CC2SW1 (PN G2856AAA02).

References

Fig. A-FBBAA

Location of the storage box in the

cockpit.

Sheet 01

(a) Install:

FIN 1CCMD1

1 Disk-Fac Operational

Program

F1422927

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D. TEST

(1) Subtask 221502-941-002-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 22-66-34-400-002

(a) Remove the safety clip(s) and/or tag(s) and close/unlock this (these) circuit

breaker(s) as specified after the installation of the FAC (1CC1, 1CC2), refer to

AMM Task 22-66-34-400-002.

(2) Subtask 221502-700-001-001 - Procedure

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 22-66-34-400-002

Task 31-32-00-860-001

(a) Do the Line Replaceable Unit (LRU) identification:

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

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

2 Procedure:

ACTION RESULT

1. On the SYSTEM REPORT/TEST page:

- Push the line key adjacent to the Automatic

Flight System (AFS) indication

- The AFS main menu page comes into view

2. On the AFS main menu pages:

- Push the line key adjacent to the LRU IDENT

indication

- The AFS/LRU IDENTIFICATION page comes

into view

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ACTION RESULT

3. On the AFS/LRU IDENTIFICATION page:

- Make sure that the PN of the two FACs is

C13206AA02

NOTE: In case of the LRU

IDENTIFICATION of the FACs is

different, if MOD 153590 is

embodied, FAC software uploading

can be performed

4. Print the AFS/LRU IDENTIFICATION page (if

the printer is not available, a visual check is

acceptable)

3 Close-up:

a On the MCDU, push the line key adjacent to the RETURN indication until

the CFDS MENU page comes into view.

b On the MCDU, set the bright (BRT) knobs to OFF position.

(b) Do the test procedure as specified after the installation of the FAC (1CC1, 1CC2),

refer to AMM Task 22-66-34-400-002.

E. CLOSE-UP

(1) Subtask 221502-942-001-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 22-66-34-400-002

(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 after the installation of the FAC (1CC1,

1CC2), refer to AMM Task 22-66-34-400-002.

(c) Put the aircraft back to its initial configuration.

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**CONF ALL

FR1

FR24A

Z120

A

A

1CC2

1CC1

80VU

N_SB_221502_5_BAAA_01_00

Figure A-FBAAA - Sheet 01

Location of the two FACs 1CC1 and 1CC2

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**CONF ALL

A

1CCMD1

A

N_SB_221502_5_BBAA_01_00

Figure A-FBBAA - Sheet 01

Location of the storage box in the cockpit.

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SERVICE BULLETIN

REPORTING SHEET

TITLE: AUTO FLIGHT - FLIGHT AUGMENTATION COMPUTER (FAC) - INSTALL

FAC CAA02 INSTEAD OF FAC B621, 622, 623.

MODIFICATION No.: 157158P14838

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: Nov 14/14 SERVICE BULLETIN No.: A320-22-1502

REVISION No.: 00 - Nov 14/14 Page: 1

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@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: Nov 14/14 SERVICE BULLETIN No.: A320-22-1502

REVISION No.: 00 - Nov 14/14 Page: 1

5

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