@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 FORWARD PASSENGER DOOR

SURROUNDING SKIN PANELS AT CUTOUT CORNER AREAS

**CONF ALL

MODIFICATIONS

None

REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES

Following changes in Apr-2013 revision of SRM A340-200/-300 and with regards to previously

embodied SRM ADL (allowable damage limits), Airbus is requiring the operators to apply specific

actions defined in this Service Bulletin.

This Service Bulletin requires the operators to identify records of SRM ADL (allowable damage limits) at

corners of skin surrounding forward PAX door cutout.

It is recommended to check records in the specified areas within 6 months after SB issue date. In case

of existing SRM ADL recorded prior to Apr-2013 SRM revision, please contact AIRBUS Repair Support

(SEOE) for further instructions.

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

surrounding forward PAX door cutout.

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.

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SERVICE BULLETIN

SUMMARY

MATERIAL PRICE INFORMATION

No Material

EFFECTIVITY

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

06Y 15R 83V 98X ABD AFR AIB ALK ARG BOE CAL CCA CPA

DLH F2I FIN G8E GAF HFY I2L IBE IRM KAC LAN MAU MDG

MSR OAL PAL PUE QAF SAA SAS SVW SWR THT THY UAE 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 NO

EQUIPMENT NO

HARD NO

SOFT NO

OBRM NO

MANPOWER

Task 534223-832-801-001: Inspection

TOTAL MANHOURS 2.00

APPENDICES

None

DATE: Sep 26/14 SERVICE BULLETIN No.: A340-53-4223

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@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 FORWARD PASSENGER 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 Mod.

No.40347S10187 (FUSELAGE - NOSE FORWARD FUSELAGE MODIFY

DOOR NR 1 SURROUND) is embodied.

(1) Models

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

(2) Effectivity by MSN

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 0225 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 0544-0546 0554 0556 0559 0561-0562 0582 0585

0590 0598 0643 0646 0651 0668 0793 0800 0835 0844 0921 0938 0955

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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

83V 0216

98X 0429

ABD 0210

AFR 0186 0207 0237 0245 0246 0260 0307 0310 0377 0399

AIB 0131 0141 0161 0182

ALK 0367 0374 0381

ARG 0123 0126 0128 0170 0193 0373

BOE 0554

CAL 0402 0406 0411 0415 0433 0541

CCA 0192 0199 0201 0242 0243 0264

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

DLH 0135 0158 0213 0233 0252 0297 0304 0321 0325 0327 0335 0347

0352 0354 0379 0390 0434 0447

F2I 0257

FIN 0168 0174 0835 0844 0921 0938

G8E 0414

GAF 0274 0355

HFY 0117 0190 0202

I2L 0164

IBE 0125 0134 0145 0146 0217 0221 0329 0483

IRM 0282

KAC 0101 0104

LAN 0359 0363 0442

MAU 0152 0194 0268 0793 0800

MDG 0319

MSR 0156 0159 0178

OAL 0280 0292

PAL 0173 0176 0187 0196 0302 0318 0332 0387 0459 0474

PUE 0212 0215

QAF 0528

SAA 0197 0378 0544 0582 0590 0643 0646 0651

SAS 0167 0413 0424 0430 0435 0450 0467 0470

SVW 0955

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

0562 0585 0598

THT 0385 0395 0438 0446 0668

THY 0115 0180 0270 0331

UAE 0163 0166 0185 0236

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SERVICE BULLETIN

OPERATOR MSN

VIR 0114 0214 0225

XAX 0273 0278

(4) Configuration by MSN

MSN CONFIGURATION

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 0225 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 0414 0415 0424

0429 0430 0433 0434 0435 0438 0442 0446 0447 0450 0459

0467 0470 0474 0483 0528 0538 0541 0544 0545 0546 0554

0556 0559 0561 0562 0582 0585 0590 0598 0643 0646 0651

0668 0793 0800 0835 0844 0921 0938 0955

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

B. CONCURRENT REQUIREMENTS

None

C. REASON

(1) History

Following changes in Apr-2013 revision of SRM A340-200/-300 and with regards to

previously embodied SRM ADL (allowable damage limits), Airbus is requiring the

operators to apply specific actions defined in this Service Bulletin.

(2) Objective/Action

This Service Bulletin requires the operators to identify records of SRM ADL (allowable

damage limits) at corners of skin surrounding forward PAX door cutout.

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SERVICE BULLETIN

It is recommended to check records in the specified areas within 6 months after SB

issue date. In case of existing SRM ADL recorded prior to Apr-2013 SRM revision,

please contact AIRBUS Repair Support (SEOE) for further instructions.

(3) Advantages

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

of the skin surrounding forward PAX door cutout.

(4) Operational/Maintenance Consequences

None

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

Task 534223-832-801-001: Inspection

(1) Check if ADL have been recorded at Corners of Skin Surrounding Forward PAX

Doors, LH and RH Side

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. It is anticipated that the AD will confirm the thresholds

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

accomplishment timescale.

DATE: Sep 26/14 SERVICE BULLETIN No.: A340-53-4223

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SERVICE BULLETIN

Table 1, Config. 001 - Inspection of SRM allowable damage limits records at corners of skin

surrounding forward PAX door

Compliance time (whichever occurs

later)

Condition Action

Threshold

(whichever occurs

fist)

Grace period

(whichever occurs

fist)

Repetitive interval

All aircraft Check the aircraft

maintenance

program

documentation for

existing ADL in the

related sections in

accordance with

the Subtask

534223-832-001-001

Before Sep-2015

for ADL with a

Temporary Life

Limit

and

Before Sep-2016

for ADL with a

Permanent

Acceptance

See NOTE (*)

None None

No existing ADL

covered by a SRM

version prior to

Apr-2013 revision

No further action

necessary within

this Service

Bulletin

None None None

ADL detected with

a temporary life

limit and covered

by a SRM version

prior to Apr-2013

revision

Contact AIRBUS

with detailed repair

report for specific

assessment and

follow their

instructions

As soon as

possible before

Sep-2015

See NOTE (**)

None None

ADL detected with

a permanent

acceptance and

covered by a SRM

version prior to

Apr-2013 revision

Contact AIRBUS

with detailed repair

report for specific

assessment and

follow their

instructions

As soon as

possible before

Sep-2016

See NOTE (**)

None None

NOTE (*): It is recommended to check records within 6 months after SB Issue Date.

NOTE (**): It is recommended to contact Airbus 6 months before the end of the

Compliance Time.

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.

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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 534223-832-801-001: Inspection

On Aircraft

Check if ADL have been recorded at Corners of Skin

Surrounding Forward PAX Doors, LH and RH Side

2.00

TOTAL MANHOURS 2.00

H. WEIGHT AND BALANCE

Not Changed

I. ELECTRICAL LOAD DATA

Not Changed

J. REFERENCES

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

Structural Repair Manual (SRM) 53-11-11

K. PUBLICATION AFFECTED

None

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

None

(2) Price and Availability

None

B. INDUSTRY SUPPORT INFORMATION

AIRBUS will not provide industry support for accomplishment of the 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

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SERVICE BULLETIN

This Page Intentionally Left Blank

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SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS

Task 534223-832-801-001 - Inspection

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/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.

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.

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.

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SERVICE BULLETIN

Task Associated Data

Manpower

TOTAL MANHOURS 2.00

A. GENERAL

(1) Subtask 534223-839-001-001 - 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

C. PROCEDURE

(1) Subtask 534223-832-001-001 - Check if ADL have been recorded at Corners of Skin

Surrounding Forward PAX Doors, LH and RH Side

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills NON SPECIFIC

References

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

Fig. A-FBAAA

Area with ADL submitted to assessment

Sheet 01

Fig. A-FFAAA

Flow Chart

Sheet 01

NOTE: For the accomplishment timescale, refer to 1.E.(2).

(a) Check in the aircraft maintenance program documentation if ADL have been

recorded at corners of skin surrounding forward PAX doors, LH and RH side,

according to SRM 53-11-11, Page Block 101 paragraph 4.D.

Refer to Fig. A-FBAAA and Flow Chart Fig. A-FFAAA

1 If some ADL covered by a SRM version prior to Apr-2013 revision are found,

contact AIRBUS with detailed repair report for specific assessment and follow

their instructions.

2 If no ADL covered by a SRM version prior to Apr-2013 revision is found, no

further action is required.

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SERVICE BULLETIN

D. TEST

None

E. CLOSE-UP

None

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SERVICE BULLETIN

**CONF ALL

350 mm

(13.779 in)

60 mm

(2.362 in)

260 mm

(10.236 in)

FR1

FR17

A

TYPICAL

Z831

01 AREA ON WHICH ADL ARE SUBMITTED TO ASSESSMENT

NOTE:

01

Z841

Z220 A

LH SIDE SHOWN

RH SIDE SYMMETRICAL

B

A

FR13

FR17

B

B

F_SB_534223_5_BAAA_01_00

Figure A-FBAAA - Sheet 01

Area with ADL submitted to assessment

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SERVICE BULLETIN

**CONF ALL

CHECK THE AIRCRAFT MAINTENANCE PROGRAM DOCUMENTATION

FOR EXISTING ADL AT CORNERS OF SKIN SURROUNDING

YES COVERED BY A SRM VERSION PRIOR TO

EXISTING ADL

CONTACT AIRBUS

WITH DETAILED REPAIR

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

NO FURTHER ACTION WITHIN

THIS SERVICE BULLETIN

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

01

FORWARD PAX DOORS, LH AND RH SIDE, IN ACCORDANCE WITH

APR−2013 REVISION ?

01

REPORT FOR SPECIFIC

ASSESSMENT AND

QUESTION

ACTION

FINDING

SUBTASK 534223−832−001−001

FOLLOW THEIR INSTRUCTIONS

NO

F_SB_534223_5_FAAA_01_00

Figure A-FFAAA - Sheet 01

Flow Chart

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SERVICE BULLETIN

REPORTING SHEET

TITLE: FUSELAGE - INSPECTION OF FORWARD PASSENGER 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: Sep 26/14 SERVICE BULLETIN No.: A340-53-4223

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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: Sep 26/14 SERVICE BULLETIN No.: A340-53-4223

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