@A330

SERVICE BULLETIN

SUMMARY

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

This summary is for information only and is not approved for modification of the aircraft.

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 21

TITLE: AIR CONDITIONING - GENERAL - INSTALL NEW BONDING BRACKETS

AFTER FRAME64 LH BETWEEN P33-P34

**CONF ALL

MODIFICATIONS

MODIFICATION CLASSIFICATION

MAJOR None

MINOR 201681D50373

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

Maintenance experiences have shown that the bonding lead from the isolation valve 283HN to Frame

(FR)64, between Stringer (STGR)33 and STGR34, is too close to the electrical harness 5871VB and

chafing might be possible.

The chafing might lead to a non-closure of the isolation valve 283HN through a short circuit of the

isolation valve by contact of the chafed bonding lead and wire harness 5871VB.

This Service Bulletin details the installation of a new bonding bracket and new bonding lead at

STGR33, between FR64 and FR65.

The accomplishment of this Service Bulletin will avoid possible chafing between the bonding lead and

the electrical harness 5871VB and ensure the reliability of the isolation valve 283HN.

GENERAL EVALUATION

EVALUATION TABLE

COMPLIANCE MANDATORY (1) CANCELS INSPECTION SB NO

POTENTIAL AD YES A/C OPERATION AFFECTED NO

RELIABILITY AFFECTED YES PAX COMFORT AFFECTED NO

COST SAVING NO ETOPS AFFECTED NO

DATE: Aug 04/11 SERVICE BULLETIN No.: A330-21-3160

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SERVICE BULLETIN

SUMMARY

EVALUATION TABLE

STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED NO

NOTE (1): Service Bulletin must be accomplished.

MATERIAL PRICE INFORMATION

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 213160D01R01 1 45.00 Bracket, Rivet, Bonding Lead, Screw,

Washer, Nut

EFFECTIVITY

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

CRK ETD THY

CONCURRENT REQUIREMENTS

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 YES

EQUIPMENT NO

HARD NO

SOFT NO

OBRM NO

MANPOWER

Task 213160-831-848-001: Modification

TOTAL MANHOURS 3.00

ELAPSED TIME (HOURS) 3.00

APPENDICES

None

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SERVICE BULLETIN

SUMMARY

**CONF ALL

Z160 B

A

B

283HN

FR73

FR62

A

FR64

FR63

FR62

STGR34

STGR35

STGR33

FR61

283HN

G_SB_213160_6_SAAA_01_00

NEW

BONDING

BRACKET

Figure A-GSAAA - Sheet 01

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SERVICE BULLETIN

SUMMARY

This Page Intentionally Left Blank

DATE: Aug 04/11 SERVICE BULLETIN No.: A330-21-3160

REVISION No.: 00 - Aug 04/11 Page: 4

6

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@A330

SERVICE BULLETIN

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 21

TITLE: AIR CONDITIONING - GENERAL - INSTALL NEW BONDING BRACKETS

AFTER FRAME64 LH BETWEEN P33-P34

MODIFICATION No.: 201681D50373

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

330-243F

(2) Effectivity by MSN

1004 1032 1051 1062 1070

(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

CRK 1051 1062

ETD 1032 1070

THY 1004

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SERVICE BULLETIN

(4) Configuration by MSN

MSN CONFIGURATION

1004 1032 1051 1062 1070 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

Consumable CMLD01 1

Kit 213160D01R01 1

B. CONCURRENT REQUIREMENTS

None

C. REASON

(1) History

Maintenance experiences have shown that the bonding lead from the isolation valve

283HN to Frame (FR)64, between Stringer (STGR)33 and STGR34, is too close to the

electrical harness 5871VB and chafing might be possible.

The chafing might lead to a non-closure of the isolation valve 283HN through a short

circuit of the isolation valve by contact of the chafed bonding lead and wire harness

5871VB.

(2) Objective/Action

This Service Bulletin details the installation of a new bonding bracket and new bonding

lead at STGR33, between FR64 and FR65.

(3) Advantages

The accomplishment of this Service Bulletin will avoid possible chafing between the

bonding lead and the electrical harness 5871VB and ensure the reliability of the isolation

valve 283HN.

(4) Operational/Maintenance Consequences

None

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

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SERVICE BULLETIN

Task 213160-831-848-001: Modification

(1) Modify the bonding lead installation

E. COMPLIANCE

(1) Classification

MANDATORY: Service Bulletin must be accomplished.

(2) Accomplishment Timescale

This Service Bulletin has been classified Mandatory. It is expected that an Airworthiness

Directive (AD) published by the European Aviation Safety Agency (EASA) will be issued

to confirm this classification. The accomplishment timescale, which has not yet been

defined, will be given in the AD.

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 213160-831-848-001: Modification

Get Access 1.00

On Aircraft

Modify the bonding lead installation 0.75

Tests 0.25

Close-Up 1.00

TOTAL MANHOURS 3.00

ELAPSED TIME (HOURS) 3.00

H. WEIGHT AND BALANCE

Not Changed

I. ELECTRICAL LOAD DATA

Not Changed

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SERVICE BULLETIN

J. REFERENCES

Aircraft Maintenance Manual (AMM) 06-20-00 06-30-00 06-31-53

20-28-00 24-41-00 25-53-00

25-80-00 50-14-00 52-30-00

Elec. Std. Practices Manual (ESPM) 20-51-20 20-51-21 20-55-00

Standards Manual (SM)

Structural Repair Manual (SRM) 51-42-11 51-44-00 51-44-11

K. PUBLICATION AFFECTED

Illustrated Parts Catalog (IPC) 21-28-04

L. INTERCHANGEABILITY/MIXABILITY

Not Applicable

M. SPARES

None

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SERVICE BULLETIN

2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

(1) Procurement Addresses

Kit 213160D01R01 Customers with aircraft shown in the

effectivity of this Service Bulletin should send

a purchase order to AIRBUS. Quote the

number of this Service Bulletin. The address

is:

Airbus Material, Logistic and Suppliers

Weg beim Jaeger 150

D-22335 Hamburg

Germany

For ordering by internet:

http//spares.airbus.com

For ordering modification kits by fax: +49 40

50 76 25 90

For ordering single spares by fax: +49 40 50

76 25 12

(2) Price and Availability

Kit 213160D01R01

Cost 45.00 USD

Availability 90 calendar days from receipt of order

The Kit availability given above is the standard lead time from the date of your purchase

order. If you require Kits before this time, please include a retrofit planning schedule with

your order so that we can try to comply with your requirements.

The sales terms (costs and availability) are estimated in relation to economic conditions

at the issue date of the Service Bulletin.

B. INDUSTRY SUPPORT INFORMATION

AIRBUS will share the costs of accomplishment of this Service Bulletin by providing the kits at

no charge for orders placed before first issue date.

For the accomplishment of this Service Bulletin before Dec-2014, AIRBUS will credit the

manhours indicated in this Service Bulletin at the agreed in-house warranty labor rate for

claims received not later than 90 days after completion of the last affected aircraft of your

fleet.

DATE: Aug 04/11 SERVICE BULLETIN No.: A330-21-3160

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SERVICE BULLETIN

C. LIST OF COMPONENTS

Kit 213160D01R01

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

NOTES

1 NAS1801-3-7 2 SCREW

2 MS21042-3 1 NUT

3 NAS1149C0332R 3 WASHER

6 EN6081D4-06 5 RIVET

7 ABS1577A05 1 BRACKET

8 E0089-10-280NN 1 LEAD

NOTE: If you find part numbers of hardware components in the related kit(s) which

you cannot identify in the LIST OF COMPONENTS of this Service Bulletin,

refer to Standards Manual (SM). The SM will give you the correct part number

to part number relationship.

D. LIST OF MATERIALS - OPERATOR SUPPLIED

(1) Consumable Materials

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO CML

MAT. No.

QTY PER A/C SEE

NOTES

Cleaning Solvent 11-016 As required

Lint-Free Cotton Cloth 19-003 As required

(2) Components

None

(3) Equipment

None

E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

None

F. TOOLING

None

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SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS

Task 213160-831-848-001 - Modification

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

INCLUDED IN THE REFERENCED PROCEDURES.

CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP

ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY

AND MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENANCE

WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING,

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

THIS:

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

NECESSARY ON WIRING AND COMPONENTS.

REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND OTHER

CONTAMINATION.

THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION

AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION.

IN CASE OF CONTAMINATION REFER TO ESPM 20-55-00.

Task Associated Data

Zone

160

Manpower

TOTAL MANHOURS 3.00

ELAPSED TIME (HOURS) 3.00

A. GENERAL

(1) Subtask 213160-910-201-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-20-00, Page Block 001

06-30-00, Page Block 001

06-31-53, Page Block 001

50-14-00, Page Block 001

Structural Repair Manual (SRM) 51-44-00

(a) For identification of zones (Refer to AMM 06-20-00, Page Block 001).

(b) For Stringer (STGR) identification (Refer to AMM 06-30-00, Page Block 001).

(c) For Frame (FR) identification (Refer to AMM 06-31-53, Page Block 001).

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SERVICE BULLETIN

(d) For sidewall panel identification (Refer to AMM 50-14-00, Page Block 001).

(e) For fastener hole diameter and drill and deburr data (Refer to SRM 51-44-00).

(2) Subtask 213160-839-201-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Bulletin.

B. PREPARATION

(1) Subtask 213160-941-201-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 24-41-00-860-801

Task 25-53-00-000-801

Task 25-80-00-000-801

Task 52-30-00-010-801

Fig. A-GBAAA

Modify the lead bonding installation

Sheet 01

Sheet 02

Fig. A-GBBAA

Modify the lead bonding installation

Sheet 01

Sheet 02

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

24-41-00-860-801).

(b) Put the access platform in position at the Aft cargo-compartment door.

(c) Open the Aft cargo-compartment door (Refer to AMM Task 52-30-00-010-801).

(d) If a Cargo Loading System (CLS) is installed, put a warning notice in position on

the control panel to tell persons not to operate the CLS.

(e) Remove the access panel 151TW (Refer to AMM Task 25-53-00-000-801).

(f) In the work area, zone 160, as shown on Fig. A-GBAAA Sheet 01 and

Fig. A-GBBAA Sheet 01, remove the insulation blankets (Refer to AMM Task

25-80-00-000-801).

DATE: Aug 04/11 SERVICE BULLETIN No.: A330-21-3160

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SERVICE BULLETIN

C. PROCEDURE

(1) Subtask 213160-831-201-001 - Modify the bonding lead installation

Work Zones and Access Panels

Zone Access/Work location

160 Work location from Frame 64 to Frame 65

Stringer 34

Manpower Resources

Manhours 0.75

Minimum number of person 1

Subtask elapsed time 0.75

Skills AIRFRAME

Material necessary to do the job

Kit 213160D01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 NAS1801-3-7 2 SCREW

2 MS21042-3 1 NUT

3 NAS1149C0332R 3 WASHER

6 EN6081D4-06 5 RIVET

7 ABS1577A05 1 BRACKET

8 E0089-10-280NN 1 LEAD

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Cleaning Solvent 11-016 As required

Lint-Free Cotton Cloth 19-003 As required

References

Aircraft Maintenance Manual (AMM) Task 20-28-00-912-801

25-80-00, Page Block 801

Elec. Std. Practices Manual (ESPM) 20-51-20

20-51-21

Structural Repair Manual (SRM) 51-42-11

51-44-11

Fig. A-GBAAA

Modify the lead bonding installation

Sheet 01

Sheet 02

Fig. A-GBBAA

Modify the lead bonding installation

Sheet 01

Sheet 02

(a) As shown on Fig. A-GBAAA Sheet 01 and Fig. A-GBAAA Sheet 02, View C and D,

remove:

2 Nut Item (2) Discard

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SERVICE BULLETIN

4 Washer Item (3) Discard

2 Screw Item (1) Discard

1 Lead Bonding Item (4) Discard

(b) As shown on Fig. A-GBAAA Sheet 02, at FR64, remove:

2 Rivet Item (6) Discard

1 Bracket Item (5) Discard

(c) As shown on Fig. A-GBAAA Sheet 02, View E, close the holes with:

2 Rivet EN6081D4-06 Item 6

(Refer to SRM 51-42-11).

(d) Install the new bracket at STGR34, between FR64 and FR65 LH, as shown on Fig.

A-GBBAA Sheet 01 and Fig. A-GBBAA Sheet 02, View D, Section A-A.

1 At STGR34 make marks to show the position of the holes.

2 Drill the pilot hole at STGR34 with a diameter of 2.4mm (0.094inch) (Refer to

SRM 51-44-11).

3 Temporarily install:

1 Bracket ABS1577A05 Item 7

NOTE: Use the new hole at STGR34.

4 Transfer drill the holes from the bracket, item 7, to STGR34 with a diameter of

3.3mm (0.13inch) (Refer to SRM 51-44-11).

5 Remove the bracket and deburr the holes at STGR34 and the bracket, item 7

(Refer to SRM 51-44-11).

6 Clean the contact surface of the STGR34 LH and the bracket, item 7, with:

Lint-Free Cotton

Cloth

19-003 As required

and

Cleaning Solvent 11-016 As required

7 Install:

1 Bracket ABS1577A05 Item 7

3 Rivet EN6081D4-06 Item 6

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SERVICE BULLETIN

(Refer to SRM 51-42-11).

NOTE: Do the electrical bonding of the rivets (Refer to ESPM

20-51-20) and (Refer to AMM Task 20-28-00-912-801).

(e) Perform a cutout in the insulation blanket in position of the new bracket, item 7, for

installation of the insulation blanket (Refer to AMM 25-80-00, Page Block 801).

(f) As shown on Fig. A-GBBAA Sheet 02, View C and D, install:

1 Lead Bonding E0089-10-280NN Item 8

with:

2 Screw NAS1801-3-7 Item 1

3 Washer NAS1149C0332R Item 3

1 Nut MS21042-3 Item 2

and do the electrical bonding (Refer to ESPM 20-51-21).

D. TEST

(1) Subtask 213160-760-201-001 - Low current test

Manpower Resources

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) Task 20-28-00-720-801

(a) Do the low current test of the new bonding lead and the new bracket (Refer to

AMM Task 20-28-00-720-801).

E. CLOSE-UP

(1) Subtask 213160-942-201-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 25-53-00-400-801

Task 25-80-00-400-801

Task 52-30-00-410-801

Fig. A-GBBAA

Modify the lead bonding installation

Sheet 01

Sheet 02

Fig. A-GBAAA

Modify the lead bonding installation

Sheet 01

Sheet 02

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SERVICE BULLETIN

(a) Make sure that the work areas are clean and clear of tools and other items of

equipment.

(b) In the work area, install the insulation blankets (Refer to AMM Task

25-80-00-400-801).

(c) Install the access panel 151TW (Refer to AMM Task 25-53-00-400-801).

(d) If installed, remove the warning notice from the CLS.

(e) Close the Aft cargo-compartment door (Refer to AMM Task 52-30-00-410-801).

(f) Remove the access platform(s).

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**CONF ALL

B Z160

A

283HN

FR73

FR62

A

STGR33

FR64

FR63

FR62

STGR34

STGR35

FR61

B

C

283HN

D E

G_SB_213160_6_BAAA_01_01

Figure A-GBAAA - Sheet 01

Modify the lead bonding installation

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SERVICE BULLETIN

**CONF ALL

C

D

(2)

(3)

(4)

(3)

(1)

(2)

(4)

(1)

(3)

(6)

(5)

FR64

(3)

6

FR64

E

BEFORE

AFTER

G_SB_213160_6_BAAA_02_02

Figure A-GBAAA - Sheet 02

Modify the lead bonding installation

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SERVICE BULLETIN

**CONF ALL

Z160

G_SB_213160_6_BBAA_01_00

B

A

B

C

283HN

FR73

FR62

A

FR64

FR63

FR62

STGR34

STGR35

STGR33

FR61

283HN

A

A D

Figure A-GBBAA - Sheet 01

Modify the lead bonding installation

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SERVICE BULLETIN

**CONF ALL

C D

100.0 mm

(3.94 in)

14.0 mm

(0.55 in)

STGR34

FR64

A A

1

3

8

7

2

3

8

3

1

7

STGR34

6

G_SB_213160_6_BBAA_02_03

Figure A-GBBAA - Sheet 02

Modify the lead bonding installation

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SERVICE BULLETIN

REPORTING SHEET

TITLE: AIR CONDITIONING - GENERAL - INSTALL NEW BONDING BRACKETS

AFTER FRAME64 LH BETWEEN P33-P34

MODIFICATION No.: 201681D50373

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.

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Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

QUALITY PERCEPTION FORM

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

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

improve the quality of our Service Bulletins.

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

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

- Quality rating of this SB 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: Aug 04/11 SERVICE BULLETIN No.: A330-21-3160

REVISION No.: 00 - Aug 04/11 Page: 1

6

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