@A340

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: 53

TITLE: FUSELAGE - INSPECTION OF DOOR SURROUNDING SKIN PANELS

AT CUTOUT CORNER AREAS

**CONF ALL

MODIFICATIONS

None

REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES

Following changes in the Apr-13 revision of the Structural Repair Manual (SRM) for A340 aircraft, and

with regards to previously embodied SRM Allowable Damage Limits (ADL), AIRBUS is requiring the

operators to apply specific actions defined in this Service Bulletin.

This Service Bulletin is issued to instruct operators to examine their records and take the applicable

corrective action when necessary.

Accomplishment of this Service Bulletin will contribute to maintain the structural integrity of the door

surrounding skin panels at cutout corner areas.

GENERAL EVALUATION

EVALUATION TABLE

COMPLIANCE MANDATORY (1) CANCELS INSPECTION SB NO

POTENTIAL AD YES A/C OPERATION AFFECTED NO

RELIABILITY AFFECTED NO PAX COMFORT AFFECTED NO

COST SAVING NO LROPS AFFECTED NO

STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED NO

NOTE (1): Service Bulletin must be accomplished.

MATERIAL PRICE INFORMATION

No Material

DATE: Nov 25/14 SERVICE BULLETIN No.: A340-53-4222

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@A340

SERVICE BULLETIN

SUMMARY

EFFECTIVITY

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

06Y 15R 15T 31V 36V 56W 74W 83V 98X ABD AFR AIB ALD

ALK ARG BOE CAL CCA CPA DGA DLH F2I FIN GAF HFY I2L

IBE IRC IRM KAC LAN M3R MAU MDG MSR OAL PAL PUE QAF

RJA S3R SAA SAS SFB SLM SWR TAP THT THY UAE VCV VIR

XAX

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 534222-832-848-001: Inspection

TOTAL MANHOURS 1.00

ELAPSED TIME (HOURS) 1.00

APPENDICES

None

DATE: Nov 25/14 SERVICE BULLETIN No.: A340-53-4222

REVISION No.: 00 - Nov 25/14 Page: 2

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Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

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: 53

TITLE: FUSELAGE - INSPECTION OF DOOR SURROUNDING SKIN PANELS

AT CUTOUT CORNER AREAS

MODIFICATION No.: None

This document contains AIRBUS PROPRIETARY INFORMATION and shall at all times remain the

property of AIRBUS; no intellectual property right or licence is granted by AIRBUS in connection with

any information contained in it. It is delivered on the express condition that said document and the

information contained in it shall be treated as confidential, shall not be used for any purpose other than

that for which it is hereby delivered. It shall not be disclosed in whole or in part to third parties and shall

not be duplicated in any manner (except for the purposes of performing the tasks described hereunder

and provided that any recipient of such document shall comply with the conditions herein), without

AIRBUS prior written consent.

1. PLANNING INFORMATION

**CONF ALL

A. EFFECTIVITY

NOTE: This Service Bulletin is only applicable to aircraft on which Modification No.

49144S16279 has not been embodied.

(1) Models

340-211 340-212 340-213 340-311 340-312 340-313

(2) Effectivity by MSN

0002 0004 0006 0009 0014 0020 0022-0026 0029 0031-0035 0038 0041 0043-0044

0046-0047 0049 0051-0053 0056-0058 0061 0063 0074-0076 0078-0081 0084-0085

0089-0091 0093-0094 0101 0104 0114-0115 0117 0123 0125-0126 0128 0131

0134-0137 0139 0141-0142 0145-0147 0149-0152 0154 0156-0161 0163-0164

0166-0170 0173-0176 0178-0180 0182 0185-0187 0190 0192-0194 0196-0197 0199

0201-0202 0207-0208 0210 0212-0218 0220-0221 0227-0228 0233 0236-0237

0242-0243 0245-0246 0252 0257 0260 0263-0264 0268 0270 0273-0274 0278 0280

0282 0292 0297 0302 0304 0307 0310 0318-0319 0321 0325 0327 0329 0331-0332

0335 0347 0352 0354-0355 0359 0363 0367 0373-0374 0377-0379 0381 0385 0387

0390 0395 0399 0402 0406 0411 0413 0415 0424 0429-0430 0433-0435 0438 0442

0446-0447 0450 0459 0467 0470 0474 0483 0528 0538 0541 0545-0546 0554 0556

0559 0561-0562

DATE: Nov 25/14 SERVICE BULLETIN No.: A340-53-4222

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SERVICE BULLETIN

(3) Effectivity by Operator

The Operator/MSN relationship is provided for information only and is correct at the time

of issue in accordance with the information available to AIRBUS. Any future changes

resulting from transfer of an aircraft from one operator to another will not be reflected in

this list unless the Service Bulletin is revised for another reason.

OPERATOR MSN

06Y 0139 0149

15R 0151

15T 0009

31V 0093

36V 0024 0052

56W 0006

74W 0047 0051

83V 0216

98X 0429

ABD 0210

AFR 0029 0078 0084 0186 0207 0237 0245 0246 0260 0307 0310 0377

0399

AIB 0131 0141 0161 0182 0192 0199

ALD 0159 0178

ALK 0032 0033 0034 0367 0374 0381

ARG 0085 0094 0123 0126 0128 0170 0193 0373

BOE 0554

CAL 0402 0406 0411 0415 0433 0541

CCA 0201 0242 0243 0264

CPA 0136 0137 0142 0147 0157 0160 0208 0218 0220 0227 0228

DGA 0075 0081

DLH 0035 0053 0135 0158 0213 0233 0252 0297 0304 0321 0325 0327

0335 0347 0352 0354 0379 0390 0434 0447

F2I 0063 0074 0080 0257

FIN 0058 0168 0174

GAF 0274 0355

HFY 0117 0190 0202

I2L 0164

IBE 0125 0134 0145 0146 0217 0221 0329 0483

IRC 0002

IRM 0020 0056 0282

KAC 0089 0090 0101 0104

LAN 0359 0363 0442

M3R 0061

MAU 0076 0152 0194 0268

MDG 0319

MSR 0156

OAL 0280 0292

PAL 0173 0176 0187 0196 0302 0318 0332 0387 0459 0474

PUE 0212 0215

DATE: Nov 25/14 SERVICE BULLETIN No.: A340-53-4222

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@A340

SERVICE BULLETIN

OPERATOR MSN

QAF 0026 0528

RJA 0014 0022 0038 0043

S3R 0004

SAA 0197 0378

SAS 0167 0413 0424 0430 0435 0450 0467 0470

SFB 0046

SLM 0049

SWR 0150 0154 0169 0175 0179 0263 0538 0545 0546 0556 0559 0561

0562

TAP 0041 0044 0079 0091

THT 0385 0395 0438 0446

THY 0023 0025 0057 0115 0180 0270 0331

UAE 0163 0166 0185 0236

VCV 0031

VIR 0114 0214

XAX 0273 0278

(4) Configuration by MSN

MSN CONFIGURATION

0002 0004 0006 0009 0014 0020 0022 0023 0024 0025 0026

0029 0031 0032 0033 0034 0035 0038 0041 0043 0044 0046

0047 0049 0051 0052 0053 0056 0057 0058 0061 0063 0074

0075 0076 0078 0079 0080 0081 0084 0085 0089 0090 0091

0093 0094 0101 0104 0114 0115 0117 0123 0125 0126 0128

0131 0134 0135 0136 0137 0139 0141 0142 0145 0146 0147

0149 0150 0151 0152 0154 0156 0157 0158 0159 0160 0161

0163 0164 0166 0167 0168 0169 0170 0173 0174 0175 0176

0178 0179 0180 0182 0185 0186 0187 0190 0192 0193 0194

0196 0197 0199 0201 0202 0207 0208 0210 0212 0213 0214

0215 0216 0217 0218 0220 0221 0227 0228 0233 0236 0237

0242 0243 0245 0246 0252 0257 0260 0263 0264 0268 0270

0273 0274 0278 0280 0282 0292 0297 0302 0304 0307 0310

0318 0319 0321 0325 0327 0329 0331 0332 0335 0347 0352

0354 0355 0359 0363 0367 0373 0374 0377 0378 0379 0381

0385 0387 0390 0395 0399 0402 0406 0411 0413 0415 0424

0429 0430 0433 0434 0435 0438 0442 0446 0447 0450 0459

0467 0470 0474 0483 0528 0538 0541 0545 0546 0554 0556

0559 0561 0562

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

No Material Set

DATE: Nov 25/14 SERVICE BULLETIN No.: A340-53-4222

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SERVICE BULLETIN

B. CONCURRENT REQUIREMENTS

None

C. REASON

(1) History

Following changes in the Apr-13 revision of the Structural Repair Manual (SRM) for

A340 aircraft, and with regards to previously embodied SRM Allowable Damage Limits

(ADL), AIRBUS is requiring the operators to apply specific actions defined in this Service

Bulletin.

(2) Objective/Action

This Service Bulletin is issued to instruct operators to examine their records and take the

applicable corrective action when necessary.

(3) Advantages

Accomplishment of this Service Bulletin will contribute to maintain the structural integrity

of the door surrounding skin panels at cutout corner areas.

(4) Operational/Maintenance Consequences

None

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

Task 534222-832-848-001: Inspection

(1) Do a check of the Aircraft Records

E. COMPLIANCE

(1) Classification

MANDATORY: Service Bulletin must be accomplished.

DATE: Nov 25/14 SERVICE BULLETIN No.: A340-53-4222

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@A340

SERVICE BULLETIN

(2) Accomplishment Timescale

Table 1, Config. 001 - A340-200 and A340-300 SRM Update of the Fuselage Door Surround Panel

Corners ADL

Compliance time (Whichever occurs

Condition Action first/later)

Threshold Grace period

Repetitive interval

All Aircraft Identify records of

Structural Repair

Manual Allowable

damage Limits

(SRM ADL) for the

LH and RH Mid Pax

doors, Fwd cargo

door, LH and RH

emergency exit

door/Pax Door 3,

LH and RH Aft Pax

door, Aft cargo door

and Bulk cargo door

surround areas

24 months from

September 2014

See note (**)

None None

Existing ADL

covered by a

SRM version

prior to April

2013 revision

Update the

recorded inspection

threshold and

interval in line with

the value given in

the April 2013 or

subsequent SRM

revisions. See note

(*)

As soon as possible

before September

2016

None None

No existing

ADL covered

by an SRM

version prior to

April 2013

revision

No further action

necessary by this

Service Bulletin

None None None

NOTE: (*): Any new ADL inspection instruction following this update can be

achieved at the customers convenience:

- at any time within the Service Bulletin compliance time but no later

than any existing repair inspection already scheduled before this

update

- as per the new inspection instruction updated following this Service

Bulletin, only the schedule of updated inspection is required to close

this Service Bulletin, not the inspection itself.

NOTE: (**): It is recommended to check records within 6 months after the

Service Bulletin issue date.

DATE: Nov 25/14 SERVICE BULLETIN No.: A340-53-4222

REVISION No.: 00 - Nov 25/14 Page: 5

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@A340

SERVICE BULLETIN

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. It is anticipated that the AD will confirm the thresholds and

date given but reference should be made to the AD for confirmation of the mandated

accomplishment timescale.

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 534222-832-848-001: Inspection

On Aircraft

Do a check of the Aircraft Records 1.00

TOTAL MANHOURS 1.00

ELAPSED TIME (HOURS) 1.00

H. WEIGHT AND BALANCE

Not Changed

I. ELECTRICAL LOAD DATA

Not Changed

J. REFERENCES

Structural Repair Manual (SRM) 53-00-11 53-31-11 53-41-11

K. PUBLICATION AFFECTED

None

L. INTERCHANGEABILITY/MIXABILITY

Not Applicable

M. SPARES

None

DATE: Nov 25/14 SERVICE BULLETIN No.: A340-53-4222

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@A340

SERVICE BULLETIN

2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

None

B. INDUSTRY SUPPORT INFORMATION

AIRBUS will not provide industry support for accomplishment of this Service Bulletin.

C. LIST OF COMPONENTS

No Kit

D. LIST OF MATERIALS - OPERATOR SUPPLIED

None

E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

None

F. TOOLING

None

DATE: Nov 25/14 SERVICE BULLETIN No.: A340-53-4222

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SERVICE BULLETIN

This Page Intentionally Left Blank

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SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS

Task 534222-832-848-001 - Inspection

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: Manual titles given in the accomplishment instructions are referred to by acronyms.

Refer to paragraph 1.J., References, for the definition of acronyms.

NOTE: This Service Bulletin is classified mandatory or expected to be classified mandatory

by an Airworthiness Directive (AD). The paragraphs 3.C. and 3.D. in these

accomplishment instructions are Required for Compliance (RC) and must be done

to comply with the AD. Other paragraphs are recommended and may be deviated

from, done as part of other actions or done with accepted methods different from

those given in the Service Bulletin, as long as the RC paragraphs can be done and

the aircraft can be put back into a serviceable condition.

NOTE: The purpose of flow charts is to supplement the information given in the Procedure

and Compliance paragraphs and not to serve as the primary source for tasks or

compliance times given in this Service Bulletin.

Task Associated Data

Manpower

TOTAL MANHOURS 1.00

ELAPSED TIME (HOURS) 1.00

A. GENERAL

(1) Subtask 534222-839-202-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

B. PREPARATION

None

DATE: Nov 25/14 SERVICE BULLETIN No.: A340-53-4222

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SERVICE BULLETIN

C. PROCEDURE

(1) Subtask 534222-839-201-001 - Do a check of the Aircraft Records

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

References

Structural Repair Manual (SRM) 53-00-11, Page Block 101

53-31-11, Page Block 101

53-41-11, Page Block 101

Fig. A-GBAAA

Identification of SRM ADLs

Sheet 01

Fig. A-GFAAA

Flowchart

Sheet 01

NOTE: It is recommended to check the records within 6 months after Service

Bulletin issue date.

NOTE: Any new ADL inspection instruction following this update can be

achieved at the customers convenience:

- at any time within the Service Bulletin compliance time, but no later

than any existing repair inspection already scheduled before update

or

- as per the new inspection instruction updated following this Service

Bulletin, only the schedule of updated inspection is required to close

this Service Bulletin, not the inspection itself.

(a) Do a check of the aircraft records against the SRM ADL in accordance with

SRM 53-00-11, Page Block 101 paragraph 3.A, SRM 53-31-11, Page Block 101

paragraph 7.A and SRM 53-41-11, Page Block 101 paragraphs 3.A, 3.B and 3.C.

For procedure and location information, refer to Fig. A-GBAAA Sheet 01 and Fig.

A-GFAAA Sheet 01

1 If in the aircraft records, some damage are covered by an ADL from a SRM

revision prior to Apr-13 revision, update the recorded inspection threshold

and interval in line with the values given in the Apr-13 or subsequent SRM

revisions.

2 If in the aircraft records, there is no damage covered by an ADL from a

SRM revision prior to Apr-13 revision, then no further action is required in

accordance with this Service Bulletin.

DATE: Nov 25/14 SERVICE BULLETIN No.: A340-53-4222

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SERVICE BULLETIN

D. TEST

None

E. CLOSE-UP

None

DATE: Nov 25/14 SERVICE BULLETIN No.: A340-53-4222

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@A340

SERVICE BULLETIN

**CONF ALL

200 mm

(7.874 in)

200 mm

(7.874 in)

CORNER

AREA

A

TYPICAL

NOTE:

01 ONLY LH UPPER CORNER IS SHOWN, BUT THIS IS APPLICABLE TO ALL FOUR CORNERS.

LOCATION

FUSELAGE, DOOR CUT OUT AT CORNER AREAS

FORWARD CARGO DOOR, MID PAX DOOR,

EMERGENCY EXIT DOOR/PAX DOOR 3,

AFT CARGO DOOR, BULK CARGO DOOR

AND AFT PAX DOOR.

53−00−11 PB101 PARAGRAPH 3.A

53−31−11 PB101 PARAGRAPH 7.A

53−41−11 PB101 PARAGRAPHS 3.A, 3.B OR 3.C

SRM ADL REFERENCES

MID PAX

DOOR

EMERGENCY EXIT DOOR

PAX DOOR 3

01

A

FORWARD CARGO

DOOR 200 mm

(7.874 in)

MID PAX

DOOR

BULK CARGO

DOOR

AFT PAX

DOOR

AFT PAX

DOOR

AFT CARGO

DOOR

A A

A

A

A

DOOR CUT OUT CORNER AREAS

A A

F_SB_534222_6_BAAA_01_01

Figure A-GBAAA - Sheet 01

Identification of SRM ADLs

DATE: Nov 25/14 SERVICE BULLETIN No.: A340-53-4222

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SERVICE BULLETIN

**CONF ALL

EXISTING

ADL IS COVERED BY

A SRM VERSION PRIOR

TO APR−13 REVISION

YES

UPDATE THE RECORDED INSPECTION

THRESHOLD AND INTERVALS IN LINE WITH

THE VALUES GIVEN IN THE APR−13 OR

NO

NO FURTHER ACTION

AS PER THIS

SERVICE BULLETIN

IDENTIFY RECORDS OF SRM

ALLOWABLE DAMAGE LIMITS (ADL) FOR EACH RECORD,

FOLLOW THE INSTRUCTIONS BELOW

SUBSEQUENT SRM REVISIONS

01 02

NOTE: THE PURPOSE OF FLOW CHARTS IS TO SUPPLEMENT THE INFORMATION GIVEN IN THE

PROCEDURE AND COMPLIANCE PARAGRAPHS AND NOT TO SERVE AS THE PRIMARY 

SOURCE FOR TASKS OR COMPLIANCE TIMES GIVEN IN THIS SERVICE BULLETIN.

FOR THE ACCOMPLISHMENT TIMESCALE, REFER TO PARAGRAPH 1.E.(2)

ANY NEW ADL INSPECTION INSTRUCTIONS FOLLOWING THIS UPDATE CAN BE ACHIEVED 

AT THE OPERATORS CONVENIENCE:

− AT ANY TIME WITHIN THE SB COMPLIANCE TIME BUT NO LATER THAN ANY EXISTING 

REPAIR INSPECTION ALREADY SCHEDULED BEFORE UPDATE

− AS PER THE NEW INSPECTION INSTRUCTIONS UPDATED FOLLOWING THIS SB. 

ONLY THE SCHEDULE OF THE UPDATED INSPECTION INSTRUCTIONS IS REQUIRED

TO CLOSE THIS SB, NOT THE INSPECTION ITSELF.

01

02

F_SB_534222_6_FAAA_01_04

Figure A-GFAAA - Sheet 01

Flowchart

DATE: Nov 25/14 SERVICE BULLETIN No.: A340-53-4222

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SERVICE BULLETIN

REPORTING SHEET

TITLE: FUSELAGE - INSPECTION OF DOOR SURROUNDING SKIN PANELS

AT CUTOUT CORNER AREAS

MODIFICATION No.: None

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 25/14 SERVICE BULLETIN No.: A340-53-4222

REVISION No.: 00 - Nov 25/14 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: Nov 25/14 SERVICE BULLETIN No.: A340-53-4222

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