@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: 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 A330 aircraft,

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

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 ETOPS AFFECTED NO

STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED NO

NOTE (1): Service Bulletin must be accomplished.

MATERIAL PRICE INFORMATION

No Material

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SERVICE BULLETIN

SUMMARY

EFFECTIVITY

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

36V 38W 69X ABD ACA ACI AEA AFR AIC ALK ARG AZA AZU

BEL BER BGH CPA CRL CSA CSC DGA EDW EIN EVA FWI GFA

GIA GRL HDA HFY HVN KAL MAS MON OHY PAL QAF QFA QTR

RSY SAI SAS SYA TAE TAM TAP TCX THA THY TSC UAE USA

VKG WRC XAX XLF

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 533232-832-849-001: Inspection

TOTAL MANHOURS 1.00

ELAPSED TIME (HOURS) 1.00

APPENDICES

None

DATE: Nov 04/14 SERVICE BULLETIN No.: A330-53-3232

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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: 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

330-202 330-203 330-223 330-243 330-301 330-321 330-322 330-323

330-341 330-342 330-343

(2) Effectivity by MSN

0012 0017 0030 0037 0045 0050 0054-0055 0060 0062 0064-0067 0070-0072

0082-0083 0086-0087 0095-0096 0098-0099 0102 0106 0109 0111-0113 0116

0118-0122 0127 0132 0138 0140 0143-0144 0148 0153 0155 0162 0165 0171-0172

0177 0181 0183-0184 0188-0189 0191 0195 0198 0200 0203 0206 0209 0211 0219

0222-0224 0226 0229-0232 0234 0238 0240-0241 0244 0247-0251 0253-0256

0258-0259 0261-0262 0265-0267 0269 0271-0272 0275-0277 0279 0281 0283-0288

0290-0291 0293-0296 0299-0301 0303 0305-0306 0308-0309 0311-0317 0320

0322-0324 0326 0328 0330 0333-0334 0337-0340 0342-0346 0348-0351 0353

0356-0358 0361-0362 0364-0366 0368-0370 0372 0375 0380 0382 0384 0386

0388-0389 0392-0393 0396-0398 0400-0401 0403-0405 0407-0409 0412 0418-0423

0425 0427-0428 0432 0437 0439 0441 0443-0444 0448 0451-0452 0454-0456 0458

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SERVICE BULLETIN

0461-0463 0465-0466 0469 0472-0473 0476-0477 0479-0481 0484 0486-0487

0489-0491 0493-0494 0496-0498 0500-0513 0515-0516 0518-0519 0521-0522

0525-0527 0529-0530 0532 0535-0536 0539 0548 0550-0551 0565 0567-0568 0581

0584 0597 0627 0635 0657

(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

36V 0437 0451

38W 0401

69X 0494

ABD 0343

ACA 0277 0279 0284 0344 0400 0408 0412 0419

ACI 0507 0510

AEA 0461 0505 0526 0551 0597

AFR 0422 0443 0448 0458 0465 0481 0498 0500 0502 0503 0516 0519

0567 0584 0657

AIC 0353 0362

ALK 0303 0306 0311 0313 0404 0456 0627

ARG 0290 0300 0358 0364

AZA 0272 0339

AZU 0365 0372 0527 0532

BEL 0030 0037 0045 0082 0095 0229 0249 0324

BER 0288 0322 0403 0432 0444 0454 0469 0476 0493

BGH 0255

CPA 0102 0113 0121 0386 0389 0393 0418 0420 0421 0423 0439 0539

0548 0565

CRL 0285 0320

CSA 0425

CSC 0462

DGA 0240

EDW 0291

EIN 0269 0397

EVA 0530 0535

FWI 0253

GFA 0276 0281 0286 0287 0334 0340

GIA 0138 0140 0144 0148 0153 0165

GRL 0230

HDA 0012 0017 0071 0083 0099 0106 0109 0118 0155 0234 0244 0405

0479 0512 0581

HFY 0096 0127 0211 0262

HVN 0275 0294 0299 0366

KAL 0162 0172 0206 0219 0222 0226 0241 0256 0258 0267 0338 0350

0351 0368 0428 0484 0490 0550

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@A330

SERVICE BULLETIN

OPERATOR MSN

MAS 0067 0116 0119

MON 0261 0265

OHY 0072 0087 0098 0143

PAL 0183 0184 0188 0189 0191 0198 0200 0203

QAF 0487

QFA 0506 0508 0513 0522

QTR 0441 0473 0489 0511 0521

RSY 0120 0171

SAI 0055 0070 0086

SAS 0496 0497 0515 0568

SYA 0345

TAE 0348

TAM 0232 0238 0247 0259 0361 0466 0472

TAP 0181 0195 0223 0305 0308 0312 0317 0477 0486

TCX 0254 0266 0301 0398

THA 0050 0060 0062 0064 0065 0066 0112 0122 0209 0224 0231 0346

THY 0463 0504 0529

TSC 0111 0132 0177 0250 0271 0369 0407 0427 0480

UAE 0248 0251 0283 0293 0295 0314 0316 0326 0328 0382 0384 0392

0396 0409 0452 0455 0491 0509 0518 0525 0536

USA 0315 0323 0333 0337 0342 0370 0375 0380 0388

VKG 0309 0349 0356 0357

WRC 0296

XAX 0054 0330

XLF 0501 0635

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SERVICE BULLETIN

(4) Configuration by MSN

MSN CONFIGURATION

0012 0017 0030 0037 0045 0050 0054 0055 0060 0062 0064

0065 0066 0067 0070 0071 0072 0082 0083 0086 0087 0095

0096 0098 0099 0102 0106 0109 0111 0112 0113 0116 0118

0119 0120 0121 0122 0127 0132 0138 0140 0143 0144 0148

0153 0155 0162 0165 0171 0172 0177 0181 0183 0184 0188

0189 0191 0195 0198 0200 0203 0206 0209 0211 0219 0222

0223 0224 0226 0229 0230 0231 0232 0234 0238 0240 0241

0244 0247 0248 0249 0250 0251 0253 0254 0255 0256 0258

0259 0261 0262 0265 0266 0267 0269 0271 0272 0275 0276

0277 0279 0281 0283 0284 0285 0286 0287 0288 0290 0291

0293 0294 0295 0296 0299 0300 0301 0303 0305 0306 0308

0309 0311 0312 0313 0314 0315 0316 0317 0320 0322 0323

0324 0326 0328 0330 0333 0334 0337 0338 0339 0340 0342

0343 0344 0345 0346 0348 0349 0350 0351 0353 0356 0357

0358 0361 0362 0364 0365 0366 0368 0369 0370 0372 0375

0380 0382 0384 0386 0388 0389 0392 0393 0396 0397 0398

0400 0401 0403 0404 0405 0407 0408 0409 0412 0418 0419

0420 0421 0422 0423 0425 0427 0428 0432 0437 0439 0441

0443 0444 0448 0451 0452 0454 0455 0456 0458 0461 0462

0463 0465 0466 0469 0472 0473 0476 0477 0479 0480 0481

0484 0486 0487 0489 0490 0491 0493 0494 0496 0497 0498

0500 0501 0502 0503 0504 0505 0506 0507 0508 0509 0510

0511 0512 0513 0515 0516 0518 0519 0521 0522 0525 0526

0527 0529 0530 0532 0535 0536 0539 0548 0550 0551 0565

0567 0568 0581 0584 0597 0627 0635 0657

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

A330 aircraft, and with regards to previously embodied SRM Allowable Damage Limits

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

Bulletin.

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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 533232-832-849-001: Inspection

(1) Do a check of the Aircraft Records

E. COMPLIANCE

(1) Classification

MANDATORY: Service Bulletin must be accomplished.

(2) Accomplishment Timescale

Table 1, Config. 001 - A330-200 SRM Update of the Fuselage Door Surround Panel Corners ADL

Compliance time (Whichever occurs

Condition first/later)

Action

Threshold Grace period

Repetitive

interval

All Aircraft Identify records of

Structural Repair

Manual Allowable

Damage Limits (SRM

ADLs) for the LH and

RH Mid Pax door

surround areas.

12 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 2015

None None

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SERVICE BULLETIN

Table 1, Config. 001 - A330-200 SRM Update of the Fuselage Door Surround Panel Corners ADL

Compliance time (Whichever occurs

Condition first/later)

Action

Threshold Grace period

Repetitive

interval

No existing

ADL covered

by an SRM

version prior to

April 2013

revision

No further action

necessary within this

Service Bulletin

None None None

All Aircraft Identify records of

SRM ADLs for the

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 within this

Service Bulletin

None None None

Table 2, Config. 001 - A330-300 SRM Update of the Fuselage Door Surround Panel Corners ADL

Compliance time (Whichever occurs

Condition first/later)

Action

Threshold Grace period

Repetitive

interval

All Aircraft Identify records of

Structural Repair

Manual Allowable

Damage Limits (SRM

ADLs) for the LH and

RH Mid Pax Door, 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

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SERVICE BULLETIN

Table 2, Config. 001 - A330-300 SRM Update of the Fuselage Door Surround Panel Corners ADL

Compliance time (Whichever occurs

Condition first/later)

Action

Threshold Grace period

Repetitive

interval

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 within 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 the

update

- as per the new inspection instruction updated following this Service

Bulletin, only the schedule of the updated inspection instruction is

required to close the Service Bulletin, not the inspection itself.

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

issue date.

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.

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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 533232-832-849-001: 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

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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

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SERVICE BULLETIN

This Page Intentionally Left Blank

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SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS

Task 533232-832-849-001 - 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 533232-839-202-001 - 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

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SERVICE BULLETIN

C. PROCEDURE

(1) Subtask 533232-839-201-001 - 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 the 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 paragraph 3.A, 3.B or 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.

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SERVICE BULLETIN

D. TEST

None

E. CLOSE-UP

None

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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

DOOR CUT OUT CORNER AREAS

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

A A

G_SB_533232_6_BAAA_01_01

Figure A-GBAAA - Sheet 01

Identification of the SRM ADLs

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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

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.

IDENTIFY RECORDS OF SRM

ALLOWABLE DAMAGE LIMITS (ADL) FOR EACH RECORD,

FOLLOW THE INSTRUCTIONS BELOW

SUBSEQUENT SRM REVISIONS

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

01

02

01 02

− 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.

G_SB_533232_6_FAAA_01_05

Figure A-GFAAA - Sheet 01

Flowchart

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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 04/14 SERVICE BULLETIN No.: A330-53-3232

REVISION No.: 00 - Nov 04/14 Page: 1

6

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: Nov 04/14 SERVICE BULLETIN No.: A330-53-3232

REVISION No.: 00 - Nov 04/14 Page: 1

6

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