# Airbus Service Bulletin A330-57-3116

## Copies (2)

Copies the FAA filed in AD dockets on regulations.gov, newest revision first. A newer revision may exist.

- Revision 01 ("A330-57-3116 R02"), 643 pages: PDF https://openairdocs.org/files/sha256/3f/03/3f038c0cd31ee701e8b85909dbdd9dc5e21df22a541b36720a57b4cabbfa2f76; text https://openairdocs.org/service-documents/airbus/a330-57-3116/file/3f038c0cd31e.md. Rights: © Airbus S.A.S. Filed by the FAA in regulations.gov docket FAA-2018-0113, the docket of AD 2019-16-07. Not covered by OpenAirDocs’ CC0 dedication.
- FAA-2016-6899 SB A330-57-3116 R00 ("FAA-2016-6899 SB A330-57-3116 R00"), 118 pages: PDF https://openairdocs.org/files/sha256/9f/2e/9f2e56fec9b90f77acbbaa54a9d84d2ec05d8e28f4027b1c7e5fbb924da0acb2; text https://openairdocs.org/service-documents/airbus/a330-57-3116/file/9f2e56fec9b9.md. Rights: © Airbus S.A.S. Filed by the FAA in regulations.gov docket FAA-2016-6899; AD 2016-12-09 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication.

## Details

- Manufacturer: [Airbus](https://openairdocs.org/service-documents/airbus.md)
- Type: Service bulletin (Service Bulletin)
- Number: A330-57-3116
- Latest revision known: A330-57-3116, Revision 01, dated November 23, 2016 (OpenAirDocs)
- Page: https://openairdocs.org/service-documents/airbus/a330-57-3116

## ADs that cite it (2) (OpenAirDocs)

Newest first, with the revision each names, as OpenAirDocs read it from the AD's text.

- [AD 2016-12-09](https://openairdocs.org/ad/2016-12-09.md), effective Jun 29, 2016: No revision named
- [AD 2016-09-11](https://openairdocs.org/ad/2016-09-11.md), effective Jun 13, 2016: No revision named

Also cited in [2 proposed ADs](https://openairdocs.org/service-documents/airbus/a330-57-3116/proposed.md).

## Text (643 pages)

Revision 01, the newest copy. Rights: © Airbus S.A.S. Filed by the FAA in regulations.gov docket FAA-2018-0113, the docket of AD 2019-16-07. Not covered by OpenAirDocs’ CC0 dedication. Each page's text from the PDF; open the PDF at a page with #page=N.

### Page 1

@A330
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET
AIRBUS
CUSTOMER SERVICES DIRECTORATE
1 Rond Point Maurice Bellonte
31707 BLAGNAC CEDEX
FRANCE
T e l:( 3 3 )56 19 33 33 3
Telex : AIRBU 530526F
F a x:( 3 3 )56 19 34 25 1
MANDATORY
 MANDATORY
 MANDATORY
ATA SYSTEM: 57
TITLE: WINGS - CENTER WING BOX - I NSPECTION OF FASTENER HOLES AT
FRAME 40 VERTICAL WEB BELOW INTRADOS
MODIFICATION No.: None
This page transmits Revision No.02 of Service Bulletin No.A330-57-3116
ADDITIONAL WORK
**CONF ALL
No additional work is required by this revision for aircraft modified by any previous issue.
REASON
Revision No. 02 issued to:
- Increase the effectivity
- Update maintenance thresholds and intervals.
CHANGES
The main changes of this revision are:
- Kit 573116A06R00, Kit 573116A07R00 and Kit 573116A08R00 created
- Effectivity updated
- CML references added and updated
- COMPLIANCE paragraph updated
- Illustrations created and updated
- Minors changes applied.
DATE: Mar 12/13 SERVICE BULLETIN No.: A330-57-3116
REVISION No.: 02 - Feb 05/18 Page: 1
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 2

@A330
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET
FRONT MATTER
WINGS - CENTER WING BOX -
INSPECTION OF FASTENER HOLES AT
FRAME 40 VERTICAL WEB BELOW
INTRADOS
CONFIGURATION UPDATED
 R
SUMMARY
REASON/DESCRIPTION/OPERATIONAL
CONSEQUENCES
REASON UPDATED
 R
MATERIAL PRICE INFORMATION
 MATERIAL PRICE INFORMATION TABLE
UPDATED
R
MATERIAL PRICE INFORMATION TABLE
UPDATED
R
MATERIAL PRICE INFORMATION TABLE
UPDATED
R
MATERIAL PRICE INFORMATION TABLE
UPDATED
R
MATERIAL PRICE INFORMATION TABLE
UPDATED
R
EFFECTIVITY
 OPERATOR LIST UPDATED
 R
PLANNING INFORMATION
EFFECTIVITY
 EFFECTIVITY RELATED INFORMATION
UPDATED
R
Configuration definition
CONF 001
 CONFIGURATION DEFINITION UPDATED
 R
CONF 004
 CONFIGURATION DEFINITION UPDATED
CONFIGURATION DESCRIPTION UPDATED
R
CONF 005
 CONFIGURATION DEFINITION UPDATED
 R
Material Effectivity
 MATERIAL EFFECTIVITY UPDATED
MATERIAL SET QUANTITY UPDATED
MATERIAL SET UPDATED
R
MATERIAL EFFECTIVITY UPDATED
MATERIAL SET QUANTITY UPDATED
MATERIAL SET UPDATED
R
MATERIAL EFFECTIVITY UPDATED
MATERIAL SET QUANTITY UPDATED
MATERIAL SET UPDATED
R
REASON
Objective/Action
 OBJECTIVE/ACTION UPDATED
 R
COMPLIANCE
Accomplishment Timescale
 ACCOMPLISHMENT TIMESCALE UPDATED
 R
Accomplishment Timescale
 ACCOMPLISHMENT TIMESCALE UPDATED
 R
Accomplishment Timescale
 ACCOMPLISHMENT TIMESCALE UPDATED
 R
Accomplishment Timescale
 ACCOMPLISHMENT TIMESCALE UPDATED
 R
Accomplishment Timescale
 ACCOMPLISHMENT TIMESCALE UPDATED
 R
MANPOWER
 MANPOWER UPDATED
 R
MANPOWER UPDATED
 R
MANPOWER UPDATED
 R
DATE: Mar 12/13 SERVICE BULLETIN No.: A330-57-3116
REVISION No.: 02 - Feb 05/18 Page: 2
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 3

@A330
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET
MANPOWER UPDATED
 R
MANPOWER UPDATED
 R
MANPOWER UPDATED
 R
PUBLICATION AFFECTED
 PUBLICATIONS AFFECTED UPDATED
 R
MATERIAL INFORMATION
MATERIAL - PRICE AND AVAILABILITY
Procurement Addresses
 PROCUREMENT ADDRESSES UPDATED
MATERIAL SET UPDATED
R
Price and Availability
 PRICE AND AVAILABILITY UPDATED
MATERIAL AVAILABILITY UPDATED
MATERIAL PRICE UPDATED
MATERIAL SET UPDATED
R
INDUSTRY SUPPORT INFORMATION
 INDUSTRY SUPPORT INFORMATION UPDATED
 R
LIST OF COMPONENTS
 LIST OF COMPONENTS UPDATED
 R
Kit 573116A06R00
 PART MATERIAL SET ADDED
 N
Kit 573116A07R00
 PART MATERIAL SET ADDED
 N
Kit 573116A08R00
 PART MATERIAL SET ADDED
 N
LIST OF MATERIALS - OPERATOR
SUPPLIED
Consumable Materials
Consumable CMLA01
 CONSUMABLE MATERIAL SET UPDATED
CONSUMABLE UPDATED
QUANTITY UPDATED
R
ACCOMPLISHMENT INSTRUCTIONS
TASK 573116- 839-801-001-Check the
existence of an RDAS in the area of FR40
Pre Service Bulletin No. A330-57-3132
Subtask 573116-839-003-001
 SUBTASK SOLUTION UPDATED
 R
Subtask 573116-839-003-001
 SUBTASK SOLUTION UPDATED
 R
Subtask 573116-839-003-001
 SUBTASK SOLUTION UPDATED
 R
Subtask 573116-839-003-001
 SUBTASK SOLUTION UPDATED
 R
Subtask 573116-839-003-001
 SUBTASK SOLUTION UPDATED
 R
TASK 573116- 832-801-001-Special
Detailed Inspection of the Holes of FR40
Pre Service Bulletin No. A330-57-3132
TASK SOLUTION UPDATED
NOTE UPDATED
R
Subtask 573116-941-001-001
 SUBTASK SOLUTION UPDATED
NOTE UPDATED
R
Subtask 573116-941-003-001
 SUBTASK SOLUTION UPDATED
PANEL UPDATED
FIN UPDATED
R
Subtask 573116-941-004-001
 SUBTASK SOLUTION UPDATED
PANEL UPDATED
R
Subtask 573116-210-001-001
 SUBTASK SOLUTION UPDATED
 R
Subtask 573116-941-001-001
 SUBTASK SOLUTION UPDATED
NOTE UPDATED
R
Subtask 573116-941-003-001
 SUBTASK SOLUTION UPDATED
PANEL UPDATED
FIN UPDATED
R
DATE: Mar 12/13 SERVICE BULLETIN No.: A330-57-3116
REVISION No.: 02 - Feb 05/18 Page: 3
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 4

@A330
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET
Subtask 573116-941-004-001
 SUBTASK SOLUTION UPDATED
PANEL UPDATED
R
Subtask 573116-210-001-001
 SUBTASK SOLUTION UPDATED
 R
Subtask 573116-941-001-001
 SUBTASK SOLUTION UPDATED
NOTE UPDATED
R
Subtask 573116-941-003-001
 SUBTASK SOLUTION UPDATED
PANEL UPDATED
FIN UPDATED
R
Subtask 573116-941-004-001
 SUBTASK SOLUTION UPDATED
PANEL UPDATED
R
Subtask 573116-210-001-001
 SUBTASK SOLUTION UPDATED
 R
Subtask 573116-941-001-001
 SUBTASK SOLUTION UPDATED
NOTE UPDATED
R
Subtask 573116-941-003-001
 SUBTASK SOLUTION UPDATED
PANEL UPDATED
FIN UPDATED
R
Subtask 573116-941-004-001
 SUBTASK SOLUTION UPDATED
PANEL UPDATED
R
Subtask 573116-210-001-001
 SUBTASK SOLUTION UPDATED
 R
Subtask 573116-941-001-001
 SUBTASK SOLUTION UPDATED
NOTE UPDATED
R
Subtask 573116-941-003-001
 SUBTASK SOLUTION UPDATED
PANEL UPDATED
FIN UPDATED
R
Subtask 573116-941-004-001
 SUBTASK SOLUTION UPDATED
PANEL UPDATED
R
Subtask 573116-210-001-001
 SUBTASK SOLUTION UPDATED
 R
Subtask 573116-832-001-001
 SUBTASK SOLUTION UPDATED
NOTE UPDATED
R
Subtask 573116-832-002-001
 SUBTASK SOLUTION UPDATED
NOTE UPDATED
R
Subtask 573116-420-001-001
 SUBTASK SOLUTION UPDATED
KEYWORD UPDATED
ITEM NUMBER UPDATED
PART NUMBER UPDATED
QUANTITY UPDATED
CONSUMABLE UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
PART NUMBER DESCRIPTION UPDATED
MATERIAL LIST UPDATED
REFERENCES UPDATED
NOTE UPDATED
R
DATE: Mar 12/13 SERVICE BULLETIN No.: A330-57-3116
REVISION No.: 02 - Feb 05/18 Page: 4
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 5

@A330
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET
Subtask 573116-420-002-001
 SUBTASK SOLUTION UPDATED
KEYWORD UPDATED
ITEM NUMBER UPDATED
PART NUMBER UPDATED
QUANTITY UPDATED
CONSUMABLE UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
PART NUMBER DESCRIPTION UPDATED
MATERIAL LIST UPDATED
REFERENCES UPDATED
NOTE UPDATED
R
Subtask 573116-833-001-001
 SUBTASK SOLUTION UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
REFERENCES UPDATED
R
Subtask 573116-833-002-001
 SUBTASK SOLUTION UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
REFERENCES UPDATED
R
Subtask 573116-833-005-001
 SUBTASK SOLUTION UPDATED
KEYWORD UPDATED
ITEM NUMBER UPDATED
PART NUMBER UPDATED
QUANTITY UPDATED
CONSUMABLE UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
PART NUMBER DESCRIPTION UPDATED
MATERIAL LIST UPDATED
REFERENCES UPDATED
NOTE UPDATED
R
Subtask 573116-833-006-001
 SUBTASK SOLUTION UPDATED
KEYWORD UPDATED
ITEM NUMBER UPDATED
PART NUMBER UPDATED
QUANTITY UPDATED
CONSUMABLE UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
PART NUMBER DESCRIPTION UPDATED
MATERIAL LIST UPDATED
REFERENCES UPDATED
NOTE UPDATED
R
Subtask 573116-832-003-001
 SUBTASK SOLUTION UPDATED
NOTE UPDATED
R
Subtask 573116-832-004-001
 SUBTASK SOLUTION UPDATED
NOTE UPDATED
R
Subtask 573116-832-017-001
 SUBTASK SOLUTION UPDATED
NOTE UPDATED
R
DATE: Mar 12/13 SERVICE BULLETIN No.: A330-57-3116
REVISION No.: 02 - Feb 05/18 Page: 5
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 6

@A330
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET
Subtask 573116-832-018-001
 SUBTASK SOLUTION UPDATED
NOTE UPDATED
R
Subtask 573116-420-003-001
 SUBTASK SOLUTION UPDATED
KEYWORD UPDATED
ITEM NUMBER UPDATED
PART NUMBER UPDATED
QUANTITY UPDATED
CONSUMABLE UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
PART NUMBER DESCRIPTION UPDATED
MATERIAL LIST UPDATED
REFERENCES UPDATED
NOTE UPDATED
R
Subtask 573116-420-004-001
 SUBTASK SOLUTION UPDATED
KEYWORD UPDATED
ITEM NUMBER UPDATED
PART NUMBER UPDATED
QUANTITY UPDATED
CONSUMABLE UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
PART NUMBER DESCRIPTION UPDATED
MATERIAL LIST UPDATED
REFERENCES UPDATED
NOTE UPDATED
R
Subtask 573116-420-009-001
 SUBTASK SOLUTION UPDATED
KEYWORD UPDATED
ITEM NUMBER UPDATED
PART NUMBER UPDATED
QUANTITY UPDATED
CONSUMABLE UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
PART NUMBER DESCRIPTION UPDATED
MATERIAL LIST UPDATED
REFERENCES UPDATED
NOTE UPDATED
R
Subtask 573116-420-010-001
 SUBTASK SOLUTION UPDATED
KEYWORD UPDATED
ITEM NUMBER UPDATED
PART NUMBER UPDATED
QUANTITY UPDATED
CONSUMABLE UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
PART NUMBER DESCRIPTION UPDATED
MATERIAL LIST UPDATED
REFERENCES UPDATED
NOTE UPDATED
R
DATE: Mar 12/13 SERVICE BULLETIN No.: A330-57-3116
REVISION No.: 02 - Feb 05/18 Page: 6
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 7

@A330
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET
Subtask 573116-833-003-001
 SUBTASK SOLUTION UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
REFERENCES UPDATED
R
Subtask 573116-833-004-001
 SUBTASK SOLUTION UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
REFERENCES UPDATED
R
Subtask 573116-833-017-001
 SUBTASK SOLUTION UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
REFERENCES UPDATED
R
Subtask 573116-833-018-001
 SUBTASK SOLUTION UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
REFERENCES UPDATED
R
Subtask 573116-833-007-001
 SUBTASK SOLUTION UPDATED
CONSUMABLE UPDATED
QUANTITY UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
MATERIAL LIST UPDATED
REFERENCES UPDATED
NOTE UPDATED
R
Subtask 573116-833-008-001
 SUBTASK SOLUTION UPDATED
CONSUMABLE UPDATED
QUANTITY UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
MATERIAL LIST UPDATED
REFERENCES UPDATED
NOTE UPDATED
R
Subtask 573116-833-019-001
 SUBTASK SOLUTION UPDATED
KEYWORD UPDATED
ITEM NUMBER UPDATED
PART NUMBER UPDATED
QUANTITY UPDATED
CONSUMABLE UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
PART NUMBER DESCRIPTION UPDATED
MATERIAL LIST UPDATED
REFERENCES UPDATED
NOTE UPDATED
R
DATE: Mar 12/13 SERVICE BULLETIN No.: A330-57-3116
REVISION No.: 02 - Feb 05/18 Page: 7
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 8

@A330
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET
Subtask 573116-833-020-001
 SUBTASK SOLUTION UPDATED
KEYWORD UPDATED
ITEM NUMBER UPDATED
PART NUMBER UPDATED
QUANTITY UPDATED
CONSUMABLE UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
PART NUMBER DESCRIPTION UPDATED
MATERIAL LIST UPDATED
REFERENCES UPDATED
NOTE UPDATED
R
Subtask 573116-832-001-005
 SUBTASK SOLUTION UPDATED
NOTE UPDATED
R
Subtask 573116-832-002-005
 SUBTASK SOLUTION UPDATED
NOTE UPDATED
R
Subtask 573116-420-001-001
 SUBTASK SOLUTION UPDATED
KEYWORD UPDATED
ITEM NUMBER UPDATED
PART NUMBER UPDATED
QUANTITY UPDATED
CONSUMABLE UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
PART NUMBER DESCRIPTION UPDATED
MATERIAL LIST UPDATED
REFERENCES UPDATED
NOTE UPDATED
R
Subtask 573116-420-002-001
 SUBTASK SOLUTION UPDATED
KEYWORD UPDATED
ITEM NUMBER UPDATED
PART NUMBER UPDATED
QUANTITY UPDATED
CONSUMABLE UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
PART NUMBER DESCRIPTION UPDATED
MATERIAL LIST UPDATED
REFERENCES UPDATED
NOTE UPDATED
R
Subtask 573116-833-001-001
 SUBTASK SOLUTION UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
REFERENCES UPDATED
R
Subtask 573116-833-002-001
 SUBTASK SOLUTION UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
REFERENCES UPDATED
R
DATE: Mar 12/13 SERVICE BULLETIN No.: A330-57-3116
REVISION No.: 02 - Feb 05/18 Page: 8
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 9

@A330
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET
Subtask 573116-833-005-001
 SUBTASK SOLUTION UPDATED
KEYWORD UPDATED
ITEM NUMBER UPDATED
PART NUMBER UPDATED
QUANTITY UPDATED
CONSUMABLE UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
PART NUMBER DESCRIPTION UPDATED
MATERIAL LIST UPDATED
REFERENCES UPDATED
NOTE UPDATED
R
Subtask 573116-833-006-001
 SUBTASK SOLUTION UPDATED
KEYWORD UPDATED
ITEM NUMBER UPDATED
PART NUMBER UPDATED
QUANTITY UPDATED
CONSUMABLE UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
PART NUMBER DESCRIPTION UPDATED
MATERIAL LIST UPDATED
REFERENCES UPDATED
NOTE UPDATED
R
Subtask 573116-832-001-005
 SUBTASK SOLUTION UPDATED
NOTE UPDATED
R
Subtask 573116-832-002-005
 SUBTASK SOLUTION UPDATED
NOTE UPDATED
R
Subtask 573116-420-001-001
 SUBTASK SOLUTION UPDATED
KEYWORD UPDATED
ITEM NUMBER UPDATED
PART NUMBER UPDATED
QUANTITY UPDATED
CONSUMABLE UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
PART NUMBER DESCRIPTION UPDATED
MATERIAL LIST UPDATED
REFERENCES UPDATED
NOTE UPDATED
R
DATE: Mar 12/13 SERVICE BULLETIN No.: A330-57-3116
REVISION No.: 02 - Feb 05/18 Page: 9
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 10

@A330
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET
Subtask 573116-420-002-001
 SUBTASK SOLUTION UPDATED
KEYWORD UPDATED
ITEM NUMBER UPDATED
PART NUMBER UPDATED
QUANTITY UPDATED
CONSUMABLE UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
PART NUMBER DESCRIPTION UPDATED
MATERIAL LIST UPDATED
REFERENCES UPDATED
NOTE UPDATED
R
Subtask 573116-833-001-001
 SUBTASK SOLUTION UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
REFERENCES UPDATED
R
Subtask 573116-833-002-001
 SUBTASK SOLUTION UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
REFERENCES UPDATED
R
Subtask 573116-833-005-001
 SUBTASK SOLUTION UPDATED
KEYWORD UPDATED
ITEM NUMBER UPDATED
PART NUMBER UPDATED
QUANTITY UPDATED
CONSUMABLE UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
PART NUMBER DESCRIPTION UPDATED
MATERIAL LIST UPDATED
REFERENCES UPDATED
NOTE UPDATED
R
Subtask 573116-833-006-001
 SUBTASK SOLUTION UPDATED
KEYWORD UPDATED
ITEM NUMBER UPDATED
PART NUMBER UPDATED
QUANTITY UPDATED
CONSUMABLE UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
PART NUMBER DESCRIPTION UPDATED
MATERIAL LIST UPDATED
REFERENCES UPDATED
NOTE UPDATED
R
Subtask 573116-832-017-003
 SUBTASK SOLUTION UPDATED
NOTE UPDATED
R
Subtask 573116-832-018-003
 SUBTASK SOLUTION UPDATED
NOTE UPDATED
R
DATE: Mar 12/13 SERVICE BULLETIN No.: A330-57-3116
REVISION No.: 02 - Feb 05/18 Page: 10
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 11

@A330
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET
Subtask 573116-420-009-002
 SUBTASK SOLUTION UPDATED
KEYWORD UPDATED
ITEM NUMBER UPDATED
PART NUMBER UPDATED
QUANTITY UPDATED
CONSUMABLE UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
PART NUMBER DESCRIPTION UPDATED
MATERIAL LIST UPDATED
REFERENCES UPDATED
NOTE UPDATED
R
Subtask 573116-420-010-002
 SUBTASK SOLUTION UPDATED
KEYWORD UPDATED
ITEM NUMBER UPDATED
PART NUMBER UPDATED
QUANTITY UPDATED
CONSUMABLE UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
PART NUMBER DESCRIPTION UPDATED
MATERIAL LIST UPDATED
REFERENCES UPDATED
NOTE UPDATED
R
Subtask 573116-833-017-001
 SUBTASK SOLUTION UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
REFERENCES UPDATED
R
Subtask 573116-833-018-001
 SUBTASK SOLUTION UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
REFERENCES UPDATED
R
Subtask 573116-833-019-002
 SUBTASK SOLUTION UPDATED
KEYWORD UPDATED
ITEM NUMBER UPDATED
PART NUMBER UPDATED
QUANTITY UPDATED
CONSUMABLE UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
PART NUMBER DESCRIPTION UPDATED
MATERIAL LIST UPDATED
REFERENCES UPDATED
NOTE UPDATED
R
DATE: Mar 12/13 SERVICE BULLETIN No.: A330-57-3116
REVISION No.: 02 - Feb 05/18 Page: 11
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 12

@A330
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET
Subtask 573116-833-020-002
 SUBTASK SOLUTION UPDATED
KEYWORD UPDATED
ITEM NUMBER UPDATED
PART NUMBER UPDATED
QUANTITY UPDATED
CONSUMABLE UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
PART NUMBER DESCRIPTION UPDATED
MATERIAL LIST UPDATED
REFERENCES UPDATED
NOTE UPDATED
R
Subtask 573116-700-002-001
 SUBTASK SOLUTION UPDATED
PANEL UPDATED
FIN UPDATED
R
Subtask 573116-700-002-001
 SUBTASK SOLUTION UPDATED
PANEL UPDATED
FIN UPDATED
R
Subtask 573116-700-002-001
 SUBTASK SOLUTION UPDATED
PANEL UPDATED
FIN UPDATED
R
Subtask 573116-700-002-001
 SUBTASK SOLUTION UPDATED
PANEL UPDATED
FIN UPDATED
R
Subtask 573116-700-002-001
 SUBTASK SOLUTION UPDATED
PANEL UPDATED
FIN UPDATED
R
Subtask 573116-942-001-001
 SUBTASK SOLUTION UPDATED
CONSUMABLE UPDATED
FIN UPDATED
PANEL UPDATED
MATERIAL LIST UPDATED
R
Subtask 573116-942-002-001
 SUBTASK SOLUTION UPDATED
PANEL UPDATED
R
Subtask 573116-942-001-001
 SUBTASK SOLUTION UPDATED
CONSUMABLE UPDATED
FIN UPDATED
PANEL UPDATED
MATERIAL LIST UPDATED
R
Subtask 573116-942-002-001
 SUBTASK SOLUTION UPDATED
PANEL UPDATED
R
Subtask 573116-942-001-001
 SUBTASK SOLUTION UPDATED
CONSUMABLE UPDATED
FIN UPDATED
PANEL UPDATED
MATERIAL LIST UPDATED
R
Subtask 573116-942-002-001
 SUBTASK SOLUTION UPDATED
PANEL UPDATED
R
DATE: Mar 12/13 SERVICE BULLETIN No.: A330-57-3116
REVISION No.: 02 - Feb 05/18 Page: 12
5
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### Page 13

@A330
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET
Subtask 573116-942-001-001
 SUBTASK SOLUTION UPDATED
CONSUMABLE UPDATED
FIN UPDATED
PANEL UPDATED
MATERIAL LIST UPDATED
R
Subtask 573116-942-002-001
 SUBTASK SOLUTION UPDATED
PANEL UPDATED
R
Subtask 573116-942-001-001
 SUBTASK SOLUTION UPDATED
CONSUMABLE UPDATED
FIN UPDATED
PANEL UPDATED
MATERIAL LIST UPDATED
R
Subtask 573116-942-002-001
 SUBTASK SOLUTION UPDATED
PANEL UPDATED
R
TASK 573116- 839-802-001-Check the
existence of an RDAS in the area of FR40
Post Service Bulletin No. A330-57-3132
Subtask 573116-839-004-001
 SUBTASK SOLUTION UPDATED
 R
Subtask 573116-839-004-001
 SUBTASK SOLUTION UPDATED
 R
Subtask 573116-839-004-001
 SUBTASK SOLUTION UPDATED
 R
Subtask 573116-839-004-001
 SUBTASK SOLUTION UPDATED
 R
Subtask 573116-839-004-001
 SUBTASK SOLUTION UPDATED
 R
TASK 573116- 832-802-001-Special
Detailed Inspection of the Holes of FR40
Post Service Bulletin No. A330-57-3132
TASK SOLUTION UPDATED
NOTE UPDATED
R
Subtask 573116-941-005-001
 SUBTASK SOLUTION UPDATED
NOTE UPDATED
R
Subtask 573116-941-007-001
 SUBTASK SOLUTION UPDATED
PANEL UPDATED
FIN UPDATED
R
Subtask 573116-941-008-001
 SUBTASK SOLUTION UPDATED
PANEL UPDATED
R
Subtask 573116-941-005-001
 SUBTASK SOLUTION UPDATED
NOTE UPDATED
R
Subtask 573116-941-007-001
 SUBTASK SOLUTION UPDATED
PANEL UPDATED
FIN UPDATED
R
Subtask 573116-941-008-001
 SUBTASK SOLUTION UPDATED
PANEL UPDATED
R
Subtask 573116-941-005-001
 SUBTASK SOLUTION UPDATED
NOTE UPDATED
R
Subtask 573116-941-007-001
 SUBTASK SOLUTION UPDATED
PANEL UPDATED
FIN UPDATED
R
Subtask 573116-941-008-001
 SUBTASK SOLUTION UPDATED
PANEL UPDATED
R
Subtask 573116-941-005-001
 SUBTASK SOLUTION UPDATED
NOTE UPDATED
R
DATE: Mar 12/13 SERVICE BULLETIN No.: A330-57-3116
REVISION No.: 02 - Feb 05/18 Page: 13
5
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### Page 14

@A330
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET
Subtask 573116-941-007-001
 SUBTASK SOLUTION UPDATED
PANEL UPDATED
FIN UPDATED
R
Subtask 573116-941-008-001
 SUBTASK SOLUTION UPDATED
PANEL UPDATED
R
Subtask 573116-941-005-001
 SUBTASK SOLUTION UPDATED
NOTE UPDATED
R
Subtask 573116-941-007-001
 SUBTASK SOLUTION UPDATED
PANEL UPDATED
FIN UPDATED
R
Subtask 573116-941-008-001
 SUBTASK SOLUTION UPDATED
PANEL UPDATED
R
Subtask 573116-832-009-001
 SUBTASK SOLUTION UPDATED
NOTE UPDATED
R
Subtask 573116-832-010-001
 SUBTASK SOLUTION UPDATED
NOTE UPDATED
R
Subtask 573116-420-005-003
 SUBTASK SOLUTION UPDATED
KEYWORD UPDATED
ITEM NUMBER UPDATED
PART NUMBER UPDATED
QUANTITY UPDATED
CONSUMABLE UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
PART NUMBER DESCRIPTION UPDATED
MATERIAL LIST UPDATED
REFERENCES UPDATED
NOTE UPDATED
R
Subtask 573116-420-006-001
 SUBTASK SOLUTION UPDATED
KEYWORD UPDATED
ITEM NUMBER UPDATED
PART NUMBER UPDATED
QUANTITY UPDATED
CONSUMABLE UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
PART NUMBER DESCRIPTION UPDATED
MATERIAL LIST UPDATED
REFERENCES UPDATED
NOTE UPDATED
R
Subtask 573116-833-009-001
 SUBTASK SOLUTION UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
REFERENCES UPDATED
R
Subtask 573116-833-010-001
 SUBTASK SOLUTION UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
REFERENCES UPDATED
R
DATE: Mar 12/13 SERVICE BULLETIN No.: A330-57-3116
REVISION No.: 02 - Feb 05/18 Page: 14
5
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### Page 15

@A330
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET
Subtask 573116-833-013-001
 SUBTASK SOLUTION UPDATED
KEYWORD UPDATED
ITEM NUMBER UPDATED
PART NUMBER UPDATED
QUANTITY UPDATED
CONSUMABLE UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
PART NUMBER DESCRIPTION UPDATED
MATERIAL LIST UPDATED
REFERENCES UPDATED
NOTE UPDATED
R
Subtask 573116-833-014-001
 SUBTASK SOLUTION UPDATED
KEYWORD UPDATED
ITEM NUMBER UPDATED
PART NUMBER UPDATED
QUANTITY UPDATED
CONSUMABLE UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
PART NUMBER DESCRIPTION UPDATED
MATERIAL LIST UPDATED
REFERENCES UPDATED
NOTE UPDATED
R
Subtask 573116-832-011-001
 SUBTASK SOLUTION UPDATED
NOTE UPDATED
R
Subtask 573116-832-012-001
 SUBTASK SOLUTION UPDATED
NOTE UPDATED
R
Subtask 573116-832-021-001
 SUBTASK SOLUTION UPDATED
NOTE UPDATED
R
Subtask 573116-832-022-001
 SUBTASK SOLUTION UPDATED
NOTE UPDATED
R
Subtask 573116-420-007-001
 SUBTASK SOLUTION UPDATED
KEYWORD UPDATED
ITEM NUMBER UPDATED
PART NUMBER UPDATED
QUANTITY UPDATED
CONSUMABLE UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
PART NUMBER DESCRIPTION UPDATED
MATERIAL LIST UPDATED
REFERENCES UPDATED
NOTE UPDATED
R
DATE: Mar 12/13 SERVICE BULLETIN No.: A330-57-3116
REVISION No.: 02 - Feb 05/18 Page: 15
5
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### Page 16

@A330
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET
Subtask 573116-420-008-001
 SUBTASK SOLUTION UPDATED
KEYWORD UPDATED
ITEM NUMBER UPDATED
PART NUMBER UPDATED
QUANTITY UPDATED
CONSUMABLE UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
PART NUMBER DESCRIPTION UPDATED
MATERIAL LIST UPDATED
REFERENCES UPDATED
NOTE UPDATED
R
Subtask 573116-420-011-001
 SUBTASK SOLUTION UPDATED
KEYWORD UPDATED
ITEM NUMBER UPDATED
PART NUMBER UPDATED
QUANTITY UPDATED
CONSUMABLE UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
PART NUMBER DESCRIPTION UPDATED
MATERIAL LIST UPDATED
REFERENCES UPDATED
NOTE UPDATED
R
Subtask 573116-420-012-001
 SUBTASK SOLUTION UPDATED
KEYWORD UPDATED
ITEM NUMBER UPDATED
PART NUMBER UPDATED
QUANTITY UPDATED
CONSUMABLE UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
PART NUMBER DESCRIPTION UPDATED
MATERIAL LIST UPDATED
REFERENCES UPDATED
NOTE UPDATED
R
Subtask 573116-833-025-001
 SUBTASK SOLUTION UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
REFERENCES UPDATED
R
Subtask 573116-833-026-001
 SUBTASK SOLUTION UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
REFERENCES UPDATED
R
Subtask 573116-833-027-001
 SUBTASK SOLUTION UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
REFERENCES UPDATED
R
DATE: Mar 12/13 SERVICE BULLETIN No.: A330-57-3116
REVISION No.: 02 - Feb 05/18 Page: 16
5
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### Page 17

@A330
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET
Subtask 573116-833-022-001
 SUBTASK SOLUTION UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
REFERENCES UPDATED
R
Subtask 573116-833-015-001
 SUBTASK SOLUTION UPDATED
KEYWORD UPDATED
ITEM NUMBER UPDATED
PART NUMBER UPDATED
QUANTITY UPDATED
CONSUMABLE UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
PART NUMBER DESCRIPTION UPDATED
MATERIAL LIST UPDATED
REFERENCES UPDATED
NOTE UPDATED
R
Subtask 573116-833-016-001
 SUBTASK SOLUTION UPDATED
KEYWORD UPDATED
ITEM NUMBER UPDATED
PART NUMBER UPDATED
QUANTITY UPDATED
CONSUMABLE UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
PART NUMBER DESCRIPTION UPDATED
MATERIAL LIST UPDATED
REFERENCES UPDATED
NOTE UPDATED
R
Subtask 573116-833-023-001
 SUBTASK SOLUTION UPDATED
KEYWORD UPDATED
ITEM NUMBER UPDATED
PART NUMBER UPDATED
QUANTITY UPDATED
CONSUMABLE UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
PART NUMBER DESCRIPTION UPDATED
MATERIAL LIST UPDATED
REFERENCES UPDATED
NOTE UPDATED
R
DATE: Mar 12/13 SERVICE BULLETIN No.: A330-57-3116
REVISION No.: 02 - Feb 05/18 Page: 17
5
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### Page 18

@A330
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET
Subtask 573116-833-024-001
 SUBTASK SOLUTION UPDATED
KEYWORD UPDATED
ITEM NUMBER UPDATED
PART NUMBER UPDATED
QUANTITY UPDATED
CONSUMABLE UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
PART NUMBER DESCRIPTION UPDATED
MATERIAL LIST UPDATED
REFERENCES UPDATED
NOTE UPDATED
R
Subtask 573116-832-009-001
 SUBTASK SOLUTION UPDATED
NOTE UPDATED
R
Subtask 573116-832-010-001
 SUBTASK SOLUTION UPDATED
NOTE UPDATED
R
Subtask 573116-420-005-003
 SUBTASK SOLUTION UPDATED
KEYWORD UPDATED
ITEM NUMBER UPDATED
PART NUMBER UPDATED
QUANTITY UPDATED
CONSUMABLE UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
PART NUMBER DESCRIPTION UPDATED
MATERIAL LIST UPDATED
REFERENCES UPDATED
NOTE UPDATED
R
Subtask 573116-420-006-001
 SUBTASK SOLUTION UPDATED
KEYWORD UPDATED
ITEM NUMBER UPDATED
PART NUMBER UPDATED
QUANTITY UPDATED
CONSUMABLE UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
PART NUMBER DESCRIPTION UPDATED
MATERIAL LIST UPDATED
REFERENCES UPDATED
NOTE UPDATED
R
Subtask 573116-833-009-001
 SUBTASK SOLUTION UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
REFERENCES UPDATED
R
Subtask 573116-833-010-001
 SUBTASK SOLUTION UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
REFERENCES UPDATED
R
DATE: Mar 12/13 SERVICE BULLETIN No.: A330-57-3116
REVISION No.: 02 - Feb 05/18 Page: 18
5
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### Page 19

@A330
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET
Subtask 573116-833-013-001
 SUBTASK SOLUTION UPDATED
KEYWORD UPDATED
ITEM NUMBER UPDATED
PART NUMBER UPDATED
QUANTITY UPDATED
CONSUMABLE UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
PART NUMBER DESCRIPTION UPDATED
MATERIAL LIST UPDATED
REFERENCES UPDATED
NOTE UPDATED
R
Subtask 573116-833-014-001
 SUBTASK SOLUTION UPDATED
KEYWORD UPDATED
ITEM NUMBER UPDATED
PART NUMBER UPDATED
QUANTITY UPDATED
CONSUMABLE UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
PART NUMBER DESCRIPTION UPDATED
MATERIAL LIST UPDATED
REFERENCES UPDATED
NOTE UPDATED
R
Subtask 573116-832-021-001
 SUBTASK SOLUTION UPDATED
NOTE UPDATED
R
Subtask 573116-832-022-001
 SUBTASK SOLUTION UPDATED
NOTE UPDATED
R
Subtask 573116-420-011-002
 SUBTASK SOLUTION UPDATED
KEYWORD UPDATED
ITEM NUMBER UPDATED
PART NUMBER UPDATED
QUANTITY UPDATED
CONSUMABLE UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
PART NUMBER DESCRIPTION UPDATED
MATERIAL LIST UPDATED
REFERENCES UPDATED
NOTE UPDATED
R
DATE: Mar 12/13 SERVICE BULLETIN No.: A330-57-3116
REVISION No.: 02 - Feb 05/18 Page: 19
5
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### Page 20

@A330
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET
Subtask 573116-420-012-002
 SUBTASK SOLUTION UPDATED
KEYWORD UPDATED
ITEM NUMBER UPDATED
PART NUMBER UPDATED
QUANTITY UPDATED
CONSUMABLE UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
PART NUMBER DESCRIPTION UPDATED
MATERIAL LIST UPDATED
REFERENCES UPDATED
NOTE UPDATED
R
Subtask 573116-833-027-001
 SUBTASK SOLUTION UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
REFERENCES UPDATED
R
Subtask 573116-833-022-001
 SUBTASK SOLUTION UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
REFERENCES UPDATED
R
Subtask 573116-833-023-002
 SUBTASK SOLUTION UPDATED
KEYWORD UPDATED
ITEM NUMBER UPDATED
PART NUMBER UPDATED
QUANTITY UPDATED
CONSUMABLE UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
PART NUMBER DESCRIPTION UPDATED
MATERIAL LIST UPDATED
REFERENCES UPDATED
NOTE UPDATED
R
Subtask 573116-833-024-002
 SUBTASK SOLUTION UPDATED
KEYWORD UPDATED
ITEM NUMBER UPDATED
PART NUMBER UPDATED
QUANTITY UPDATED
CONSUMABLE UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
PART NUMBER DESCRIPTION UPDATED
MATERIAL LIST UPDATED
REFERENCES UPDATED
NOTE UPDATED
R
Subtask 573116-832-021-001
 SUBTASK SOLUTION UPDATED
NOTE UPDATED
R
Subtask 573116-832-022-001
 SUBTASK SOLUTION UPDATED
NOTE UPDATED
R
Subtask 573116-420-011-004
 SUBTASK SOLUTION ADDED
 N
Subtask 573116-420-012-004
 SUBTASK SOLUTION ADDED
 N
DATE: Mar 12/13 SERVICE BULLETIN No.: A330-57-3116
REVISION No.: 02 - Feb 05/18 Page: 20
5
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### Page 21

@A330
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET
Subtask 573116-420-011-002
 SUBTASK SOLUTION DELETED FOR
APPLICABLE MSN
D
Subtask 573116-420-012-002
 SUBTASK SOLUTION DELETED FOR
APPLICABLE MSN
D
Subtask 573116-833-027-001
 SUBTASK SOLUTION UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
REFERENCES UPDATED
R
Subtask 573116-833-022-001
 SUBTASK SOLUTION UPDATED
CONFIGURATION UPDATED
FIGURE REFERENCE UPDATED
REFERENCES UPDATED
R
Subtask 573116-833-023-004
 SUBTASK SOLUTION ADDED
 N
Subtask 573116-833-024-004
 SUBTASK SOLUTION ADDED
 N
Subtask 573116-833-023-002
 SUBTASK SOLUTION DELETED FOR
APPLICABLE MSN
D
Subtask 573116-833-024-002
 SUBTASK SOLUTION DELETED FOR
APPLICABLE MSN
D
Subtask 573116-700-001-001
 SUBTASK SOLUTION UPDATED
PANEL UPDATED
FIN UPDATED
R
Subtask 573116-700-001-001
 SUBTASK SOLUTION UPDATED
PANEL UPDATED
FIN UPDATED
R
Subtask 573116-700-001-001
 SUBTASK SOLUTION UPDATED
PANEL UPDATED
FIN UPDATED
R
Subtask 573116-700-001-001
 SUBTASK SOLUTION UPDATED
PANEL UPDATED
FIN UPDATED
R
Subtask 573116-700-001-001
 SUBTASK SOLUTION UPDATED
PANEL UPDATED
FIN UPDATED
R
Subtask 573116-942-004-001
 SUBTASK SOLUTION UPDATED
CONSUMABLE UPDATED
FIN UPDATED
PANEL UPDATED
MATERIAL LIST UPDATED
R
Subtask 573116-942-005-001
 SUBTASK SOLUTION UPDATED
PANEL UPDATED
R
Subtask 573116-942-004-001
 SUBTASK SOLUTION UPDATED
CONSUMABLE UPDATED
FIN UPDATED
PANEL UPDATED
MATERIAL LIST UPDATED
R
Subtask 573116-942-005-001
 SUBTASK SOLUTION UPDATED
PANEL UPDATED
R
DATE: Mar 12/13 SERVICE BULLETIN No.: A330-57-3116
REVISION No.: 02 - Feb 05/18 Page: 21
5
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### Page 22

@A330
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET
Subtask 573116-942-004-001
 SUBTASK SOLUTION UPDATED
CONSUMABLE UPDATED
FIN UPDATED
PANEL UPDATED
MATERIAL LIST UPDATED
R
Subtask 573116-942-005-001
 SUBTASK SOLUTION UPDATED
PANEL UPDATED
R
Subtask 573116-942-004-001
 SUBTASK SOLUTION UPDATED
CONSUMABLE UPDATED
FIN UPDATED
PANEL UPDATED
MATERIAL LIST UPDATED
R
Subtask 573116-942-005-001
 SUBTASK SOLUTION UPDATED
PANEL UPDATED
R
Subtask 573116-942-004-001
 SUBTASK SOLUTION UPDATED
CONSUMABLE UPDATED
FIN UPDATED
PANEL UPDATED
MATERIAL LIST UPDATED
R
Subtask 573116-942-005-001
 SUBTASK SOLUTION UPDATED
PANEL UPDATED
R
Fig. A-FCBAA
Fig. A-FCBAA Sheet 04
 SHEET UPDATED
 R
Fig. A-FCBAB
Fig. A-FCBAB Sheet 04
 SHEET UPDATED
 R
Fig. A-FCBAC
Fig. A-FCBAC Sheet 04
 SHEET UPDATED
 R
Fig. A-FCCAA
Fig. A-FCCAA Sheet 04
 SHEET UPDATED
 R
Fig. A-FCCAB
Fig. A-FCCAB Sheet 04
 SHEET UPDATED
 R
Fig. A-FFAAA
Fig. A-FFAAA Sheet 01
 SHEET UPDATED
 R
Fig. A-FFAAB
Fig. A-FFAAB Sheet 01
 SHEET UPDATED
 R
Fig. A-FFAAC
Fig. A-FFAAC Sheet 01
 SHEET UPDATED
 R
Fig. A-FFAAD
Fig. A-FFAAD Sheet 01
 SHEET UPDATED
 R
Fig. A-FFAAE
Fig. A-FFAAE Sheet 01
 SHEET UPDATED
 R
Fig. A-FFBAA
Fig. A-FFBAA Sheet 01
 SHEET UPDATED
 R
Fig. A-FFBAB
DATE: Mar 12/13 SERVICE BULLETIN No.: A330-57-3116
REVISION No.: 02 - Feb 05/18 Page: 22
5
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### Page 23

@A330
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET
Fig. A-FFBAB Sheet 01
 SHEET UPDATED
 R
Fig. A-FFBAC
Fig. A-FFBAC Sheet 01
 SHEET UPDATED
 R
Fig. A-FFBAD
Fig. A-FFBAD Sheet 01
 SHEET UPDATED
 R
Fig. A-FFBAE
Fig. A-FFBAE Sheet 01
 SHEET UPDATED
 R
Fig. A-FIAAA
 FIGURE SOLUTION ADDED
 N
Fig. A-FIAAA Sheet 01
 SHEET ADDED
 N
Appendix 01 - Lower Bound Table
Fig. A-FAAAA
Fig. A-FAAAA Sheet 01
 SHEET UPDATED
 R
Fig. A-FAAAB
Fig. A-FAAAB Sheet 01
 SHEET UPDATED
 R
Fig. A-FAAAC
Fig. A-FAAAC Sheet 01
 SHEET UPDATED
 R
Fig. A-FAAAD
Fig. A-FAAAD Sheet 01
 SHEET UPDATED
 R
FILING INSTRUCTIONS
This Service Bulletin has been generated electronically and is reissued as a complete document.
Replace the complete document.
Put this Revision Transmittal Sheet in front of the Service Bulletin.
HISTORY OF PREVIOUS REVISIONS
Revision No. 01 issued to:
Increase the effectivity
Reduce the inspection area
Update maintenance thresholds and intervals.
REVISION SEQUENCE
ORIGINAL: Mar 12/13
REVISION No. : 01 - Nov 23/16
REVISION No. : 02 - Feb 05/18
DATE: Mar 12/13 SERVICE BULLETIN No.: A330-57-3116
REVISION No.: 02 - Feb 05/18 Page: 23
5
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### Page 24

@A330
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET
This Page Intentionally Left Blank
DATE: Mar 12/13 SERVICE BULLETIN No.: A330-57-3116
REVISION No.: 02 - Feb 05/18 Page: 24
5
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### Page 25

@A330
SERVICE BULLETIN
SUMMARY
AIRBUS
CUSTOMER SERVICES DIRECTORATE
1 Rond Point Maurice Bellonte
31707 BLAGNAC CEDEX
FRANCE
T e l:( 3 3 )56 19 33 33 3
Telex : AIRBU 530526F
F a x:( 3 3 )56 19 34 25 1
This summary is for information only and is not approved for modification of the aircraft.
MANDATORY
 MANDATORY
 MANDATORY
ATA SYSTEM: 57
TITLE: WINGS - CENTER WING BOX - I NSPECTION OF FASTENER HOLES AT
FRAME 40 VERTICAL WEB BELOW INTRADOS
**CONF ALL
MODIFICATIONS
None
REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES
During ALI 57.11.04 inspections tasks on the rear fitting of the Frame 40 between stringer 38 and 39
LH/RH side, cracks have been found on the fasteners next to the one to be inspected (for the
configuration PRE MOD 44360). After reaming at second oversize of the subjected hole, the crack is
still present.
This Service Bulletin mandates the Inspection of the fasteners holes at Frame 40 Vertical Web between
stringer 38 and 39 below Intrados, left and right sides for all A330 aircraft post-modification 44360
embodiments. The aim of this Inspection Service Bulletin (ISB) is to implement the corrective inspection
necessary to the in-service aircraft.
For aircraft previously inspected as per Technical Disposition Ref. LR57D11023270 or
LR57D11029173, next inspection is due based on interval value given in this ISB or dedicated RDAS
instructions requirements in case of deviations to the TD instructions.
The procedure as described in this Service Bulletin is to be performed if no AIRBUS repair and/or repair
improvement has been previously performed in the same area. In case of repairs performed previously,
please contact AIRBUS Repair Support department of further instruction.
Accomplishment of this ISB will permit early detection of cracks on the Frame 40 Vertical Web between
stringer 38 and 39 below Intrados, left and right sides and will ensure that the structural integrity of the
area is maintained.
The Task ALI 57.11.04 applicable to aircraft post-modification 44360 will be superseded by
accomplishment of this Service Bulletin No. A330-57-3116.
DATE: Mar 12/13 SERVICE BULLETIN No.: A330-57-3116
REVISION No.: 02 - Feb 05/18 Page: 1
5
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### Page 26

@A330
SERVICE BULLETIN
SUMMARY
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
**CONF 001
MATERIAL PRICE INFORMATION TABLE
MATERIAL SET
 QTY PER
A/C
PRICE PER
A/C (USD)
MAIN PARTS
Kit 573116A01R06
 2
 388.00
 Bolts, Nuts
Kit 573116A03R02
 2
 7,340.00
 Bolts, Nuts
Kit
 573116A07R00
 2
 2,800.00
 Bolts, Nuts
TOTAL
 10,528.00
**CONF 002
MATERIAL PRICE INFORMATION TABLE
MATERIAL SET
 QTY PER
A/C
PRICE PER
A/C (USD)
MAIN PARTS
Kit 573116A02R04
 2
 266.00
 Bolts, Nuts
Kit 573116A03R02
 2
 7,340.00
 Bolts, Nuts
Kit
 573116A08R00
 2
 2,700.00
 Bolts, Nuts
TOTAL
 10,306.00
**CONF 003
MATERIAL PRICE INFORMATION TABLE
MATERIAL SET
 QTY PER
A/C
PRICE PER
A/C (USD)
MAIN PARTS
Kit 573116A01R06
 2
 388.00
 Bolts, Nuts
Kit 573116A03R02
 2
 7,340.00
 Bolts, Nuts
Kit
 573116A07R00
 2
 2,800.00
 Bolts, Nuts
TOTAL
 10,528.00
DATE: Mar 12/13 SERVICE BULLETIN No.: A330-57-3116
REVISION No.: 02 - Feb 05/18 Page: 2
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 27

@A330
SERVICE BULLETIN
SUMMARY
**CONF 004
MATERIAL PRICE INFORMATION TABLE
MATERIAL SET
 QTY PER
A/C
PRICE PER
A/C (USD)
MAIN PARTS
Kit 573116A01R06
 2
 388.00
 Bolts, Nuts
Kit 573116A03R02
 2
 7,340.00
 Bolts, Nuts
Kit
 573116A07R00
 2
 2,800.00
 Bolts, Nuts
TOTAL
 10,528.00
**CONF 005
MATERIAL PRICE INFORMATION TABLE
MATERIAL SET
 QTY PER
A/C
PRICE PER
A/C (USD)
MAIN PARTS
Kit 573116A01R06
 2
 388.00
 Bolts, Nuts
Kit
 573116A06R00
 2
 100.00
 Nuts
TOTAL
 488.00
EFFECTIVITY
**CONF ALL
This Service Bulletin is applicable to this (these) operator(s) :
01Q
 12P 18P 36V
 38W 39V
 41N 43P 44W
 56O
 64N AAF
 AAL
AAR AAW ACA ACI AEA AFL AFR AIB ALD
 ALK ARG ASL ASY
AVA AZA AZU BEC BEL BER CAL CBJ CCA CEB CES CHH CPA
CRK CRL CSA CSC CSN CSZ
 D2F
 DAH DAL DGA DLH EDW EIN
ETD EVA EVE F2I FBU FIN FJI FWI GCR GFA GIA GRL HAL
HDA HFY HKC
 HVN I2L
 IAW IBE IRA
 JAI JAV KAC KAL KLM
LAA LKE
 LNI MAS MAU MEA MLM MNB
 MOV MSR NMB NWS
 OBS
OHY OMA ONE P2C
 PAL PLM QAF QFA QTR RNA
 RSF RSY
 RWD
RZO SAA SAF SAI SAS SEY SIA SVA SWR SXD TAE TAM TAP
TAR TBA TCX THA THY TNA TOW TPA
 TPU
 TSC U6A
 UAE UAF
VIR VKG VOZ WOW WRC XAX XLF
CONCURRENT REQUIREMENTS
None
REFERENCES / REPERCUSSIONS
TFU
 57.11.00.007
OEB
 None
AOT
 None
SIL
 None
ISI
 None
LINE MAINTENANCE AFFECTED
 No
LIFE LIMIT
 None
OTHER
 OIT Ref. 999.0082/12
DATE: Mar 12/13 SERVICE BULLETIN No.: A330-57-3116
REVISION No.: 02 - Feb 05/18 Page: 3
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 28

@A330
SERVICE BULLETIN
SUMMARY
OTHER
 OIT Ref. 999.0086/11
NATURE OF THE WORK
AIRCRAFT
 YES
EQUIPMENT
 NO
HARD
 NO
SOFT
 NO
OBRM
 NO
MANPOWER
**CONF 001
Task 573116-839-801-001: Check the existence of an RDAS in the area of FR40 Pre Service
Bulletin No. A330-57-3132
TOTAL MANHOURS
 1.00
ELAPSED TIME (HOURS)
 1.00
Task 573116-832-801-001: Special Detailed Inspection of the Holes of FR40 Pre Service
Bulletin No. A330-57-3132
TOTAL MANHOURS
 56.00
ELAPSED TIME (HOURS)
 26.00
Task 573116-839-802-001: Check the existence of an RDAS in the area of FR40 Post Service
Bulletin No. A330-57-3132
TOTAL MANHOURS
 1.00
ELAPSED TIME (HOURS)
 1.00
Task 573116-832-802-001: Special Detailed Inspection of the Holes of FR40 Post Service
Bulletin No. A330-57-3132
TOTAL MANHOURS
 56.00
ELAPSED TIME (HOURS)
 26.00
**CONF 002
Task 573116-839-801-001: Check the existence of an RDAS in the area of FR40 Pre Service
Bulletin No. A330-57-3132
TOTAL MANHOURS
 1.00
ELAPSED TIME (HOURS)
 1.00
Task 573116-832-801-001: Special Detailed Inspection of the Holes of FR40 Pre Service
Bulletin No. A330-57-3132
TOTAL MANHOURS
 64.00
ELAPSED TIME (HOURS)
 28.75
Task 573116-839-802-001: Check the existence of an RDAS in the area of FR40 Post Service
Bulletin No. A330-57-3132
TOTAL MANHOURS
 1.00
DATE: Mar 12/13 SERVICE BULLETIN No.: A330-57-3116
REVISION No.: 02 - Feb 05/18 Page: 4
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 29

@A330
SERVICE BULLETIN
SUMMARY
Task 573116-839-802-001: Check the existence of an RDAS in the area of FR40 Post Service
Bulletin No. A330-57-3132
ELAPSED TIME (HOURS)
 1.00
Task 573116-832-802-001: Special Detailed Inspection of the Holes of FR40 Post Service
Bulletin No. A330-57-3132
TOTAL MANHOURS
 64.00
ELAPSED TIME (HOURS)
 28.75
**CONF 003
Task 573116-839-801-001: Check the existence of an RDAS in the area of FR40 Pre Service
Bulletin No. A330-57-3132
TOTAL MANHOURS
 1.00
ELAPSED TIME (HOURS)
 1.00
Task 573116-832-801-001: Special Detailed Inspection of the Holes of FR40 Pre Service
Bulletin No. A330-57-3132
TOTAL MANHOURS
 56.00
ELAPSED TIME (HOURS)
 26.00
Task 573116-839-802-001: Check the existence of an RDAS in the area of FR40 Post Service
Bulletin No. A330-57-3132
TOTAL MANHOURS
 1.00
ELAPSED TIME (HOURS)
 1.00
Task 573116-832-802-001: Special Detailed Inspection of the Holes of FR40 Post Service
Bulletin No. A330-57-3132
TOTAL MANHOURS
 56.00
ELAPSED TIME (HOURS)
 26.00
**CONF 004
Task 573116-839-801-001: Check the existence of an RDAS in the area of FR40 Pre Service
Bulletin No. A330-57-3132
TOTAL MANHOURS
 1.00
ELAPSED TIME (HOURS)
 1.00
Task 573116-832-801-001: Special Detailed Inspection of the Holes of FR40 Pre Service
Bulletin No. A330-57-3132
TOTAL MANHOURS
 56.00
ELAPSED TIME (HOURS)
 26.00
Task 573116-839-802-001: Check the existence of an RDAS in the area of FR40 Post Service
Bulletin No. A330-57-3132
TOTAL MANHOURS
 1.00
ELAPSED TIME (HOURS)
 1.00
DATE: Mar 12/13 SERVICE BULLETIN No.: A330-57-3116
REVISION No.: 02 - Feb 05/18 Page: 5
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 30

@A330
SERVICE BULLETIN
SUMMARY
Task 573116-832-802-001: Special Detailed Inspection of the Holes of FR40 Post Service
Bulletin No. A330-57-3132
TOTAL MANHOURS
 49.00
ELAPSED TIME (HOURS)
 23.75
**CONF 005
Task 573116-839-801-001: Check the existence of an RDAS in the area of FR40 Pre Service
Bulletin No. A330-57-3132
TOTAL MANHOURS
 1.00
ELAPSED TIME (HOURS)
 1.00
Task 573116-832-801-001: Special Detailed Inspection of the Holes of FR40 Pre Service
Bulletin No. A330-57-3132
TOTAL MANHOURS
 49.00
ELAPSED TIME (HOURS)
 23.75
Task 573116-839-802-001: Check the existence of an RDAS in the area of FR40 Post Service
Bulletin No. A330-57-3132
TOTAL MANHOURS
 1.00
ELAPSED TIME (HOURS)
 1.00
Task 573116-832-802-001: Special Detailed Inspection of the Holes of FR40 Post Service
Bulletin No. A330-57-3132
TOTAL MANHOURS
 49.00
ELAPSED TIME (HOURS)
 23.75
APPENDICES
**CONF ALL
Appendix 01 - Lower Bound Table
Appendix 02 - Inspection Report
DATE: Mar 12/13 SERVICE BULLETIN No.: A330-57-3116
REVISION No.: 02 - Feb 05/18 Page: 6
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 31

@A330
SERVICE BULLETIN
SUMMARY
**CONF 001 thru 004
A
A
HOLES TO BE INSPECTED.
FR40
B
FR40
FR47
STGR38
STGR39
STGR40
STGR37
CENTER WING BOX
LOWER PANEL REFERENCE
LH SHOWN
RH SYMMETRICAL
VIEW LOOKING AFT
,  Z141 Z142
FASTENER NOT AFFECTED.
NOTE:
B
G_SB_573116_5_SAAA_01_04
Figure A-FSAAA - Sheet 01
DATE: Mar 12/13 SERVICE BULLETIN No.: A330-57-3116
REVISION No.: 02 - Feb 05/18 Page: 7
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 32

@A330
SERVICE BULLETIN
SUMMARY
**CONF 005
A
A
HOLE TO BE INSPECTED.
FR40
B
FR40
FR47
STGR38
STGR39
STGR40
STGR37
CENTER WING BOX
LOWER PANEL REFERENCE
LH SHOWN
RH SYMMETRICAL
VIEW LOOKING AFT
FASTENER NOT AFFECTED.
NOTE:
B
Z141
Z142
LH
RH
G_SB_573116_5_SAAB_01_00
Figure A-FSAAB - Sheet 01
DATE: Mar 12/13 SERVICE BULLETIN No.: A330-57-3116
REVISION No.: 02 - Feb 05/18 Page: 8
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 33

@A330
SERVICE BULLETIN
AIRBUS
CUSTOMER SERVICES DIRECTORATE
1 Rond Point Maurice Bellonte
31707 BLAGNAC CEDEX
FRANCE
T e l:( 3 3 )56 19 33 33 3
Telex : AIRBU 530526F
F a x:( 3 3 )56 19 34 25 1
MANDATORY
 MANDATORY
 MANDATORY
ATA SYSTEM: 57
TITLE: WINGS - CENTER WING BOX - I NSPECTION OF FASTENER HOLES AT
FRAME 40 VERTICAL WEB BELOW INTRADOS
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.
44360S13013 (WING - CENTER WING - M ODIFY FR40 AND FRONT SPAR
(ADAPTATION SOLUTION)) or 44360S13482 (WING - CENTER WING -
MODIFY FR40 AND FRONT SPAR (SE RIAL SOLUTION)) is embodied.
(1) Models
330-202 330-203 330-223 330-223F
 330-243 330-243F
 330-301 330-302
330-303 330-322 330-323 330-342 330-343 330-941
(2) Effectivity by MSN
0177 0181 0195 0200 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 0295-0296 0300-0301
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 0461-0463 0465-0466 0469 0472-0473
0476-0477 0479-0481 0484 0486-0487 0489-0491 0493-0494 0496-0498 0500-0513
DATE: Mar 12/13 SERVICE BULLETIN No.: A330-57-3116
REVISION No.: 02 - Feb 05/18 Page: 1
5
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### Page 34

@A330
SERVICE BULLETIN
0515-0516 0518-0519 0521-0522 0524-0527 0529-0530 0532-0533 0535-0536 0539
0542 0548-0553 0555 0558 0564-0565 0567-0568 0570-0571 0573-0574 0576
0578-0579 0581 0584 0587-0588 0591 0593 0595 0597 0600 0602-0603 0605 0607
0609-0610 0612 0614 0616 0618 0620-0621 0623 0625 0627 0629 0631-0638
0640-0642 0644-0645 0647-0650 0652-0659 0661-0667 0669-0671 0673-0676
0678-0680 0682-0684 0686-0688 0690-0693 0695-0697 0699-0701 0703-0705
0707-0709 0711-0714 0716-0718 0720-0722 0724-0726 0728-0730 0732-0735
0737-0739 0741-0743 0745-0747 0749-0752 0754-0756 0758-0760 0769-0770
0772-0774 0776-0778 0780-0782 0784-0786 0788-0789 0791-0792 0795-0797 0799
0801-0803 0805-0807 0809-0811 0813-0815 0817-0828 0830-0834 0836 0838-0843
0845 0847 0849-0855 0857-0863 0865-0869 0871 0873-0877 0879 0881-0885
0887-0893 0895-0896 0898-0901 0903-0909 0911 0913-0916 0918-0920 0922-0923
0925-0928 0930-0932 0934-0937 0939-0952 0954 0956-0959 0961-0971 0973-0980
0982-0986 0988-0992 0994-0998 1000-1004
 1006-1016 1018-1023 1025-1026
1028-1029 1031-1039
 1041-1049 1051-1055
 1057-1063
 1065-1067 1069-1078
1080-1082 1084-1090 1092-1101
 1103-1108 1110 1112 1114-1116
 1118 1120
1123-1124 1126-1127 1129-1133 1135-1138
 1141 1143 1145-1151 1153 1155-1157
1159-1161 1163-1165
 1167-1175
 1177-1178 1180-1181
 1183-1184 1186-1193
1195-1196 1198-1206 1208-1241 1243-1252 1254-1256 1258-1272 1274-1423
1425-1521
 1523-1651
 1653-1660 1662-1681 1684-1701 1703-1704 1706 1708-1716
1718-1794 1796-1806 1809 1814 1816
 1825 1830
 1833
 1835
 1838-1843
 1845-1846
1848-1849
 1851-1852
 1854-1857
 1859-1860
 1862-1864
 1866-1869
 1871-1875
1877-1883
 1885-1886
 1889
 1891
 1893-1894
 1896
 1899
 1902
 1906
(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
01Q
 1830
12P
 1787 1848
 1883
 1891
18P
 1321
36V
 1164
38W
 0401
39V
 0255
41N
 1676
43P
 1053
44W
 0979
 1002
56O
 0231
64N
 1751
AAF
 0444
 0493
AAL
 0315 0323 0333 0337 0342 0370 0375 0380 0388 1011 1022 1041
1069 1076 1095 1100 1415 1417 1441 1455 1480 1502 1512 1526
AAR
 0640 0676 0708 0772 0803 0845 1001 1055 1151 1211 1326 1340
1435 1464 1518
AAW
 1043 1472 1535
ACA
 0277 0279 0284 0344 0400 0408 0412 0419
ACI
 0507 0510
DATE: Mar 12/13 SERVICE BULLETIN No.: A330-57-3116
REVISION No.: 02 - Feb 05/18 Page: 2
5
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### Page 35

@A330
SERVICE BULLETIN
OPERATOR
 MSN
AEA
 0461 0505 0526 0733 0745 0749 0814 0931 0950 0992 1097 1574
AFL
 0963 0973 1014 1045 1047 1058 1065 1072 1077 1103 1232 1247
1264 1270 1284 1299 1301 1323 1328 1345 1356 1371
AFR
 0422 0443 0448 0458 0465 0481 0498 0500 0502 0503 0516 0519
0567 0584 0657
AIB
 0871
ALD
 0326
 0328
 0392
ALK
 0303 0306 0311 0313 0456 0627 1564 1583 1604 1650 1669 1687
1689
ARG
 0290 0300 0358 0364 0587 0634
 1605 1623 1737 1748
ASL
 0885
ASY
 0747 0892 0898 0951 0969 1036 1183
AVA
 1009 1016 1073 1208 1224 1279 1342 1357
 1400
AZA
 0272 0339 0825 0831 1123 1135 1218 1225 1252 1283 1308 1313
1327 1354
AZU
 0365
 0372
 0462 0494 0527 0529 0532
BEC
 0863
BEL
 0229 0249 0291
 0324 1085
BER
 0288 0322 0739
CAL
 0602 0607 0641 0671 0675 0691 0699 0707 0714 0725 0752 0769
0805 0823 0838 0861 0920 1177 1272 1278 1346 1367 1450 1539
CBJ
 0988 1020 1028 1052 1753 1763 1775 1782 1862
 1880
CCA
 0750 0756 0759 0780 0785 0797 0810 0815 0839 0860 0867 0873
0884 0890 0903 0909 0930 0941 0944 0957 1087 1110 1130 1187
1199 1216 1237 1260 1282 1304 1330 1333 1353 1373 1383 1396
1413 1434 1444 1459 1471 1493 1509 1525 1538 1541 1563 1570
1587 1658 1673 1685 1695 1752 1765 1786 1802
CEB
 1420 1445 1495 1527 1552 1602 1712 1789
CES
 0713 0720 0728 0732 0735 0773 0777 0781 0782 0791 0821 0830
0836 0851 0862 0866 0916 0928 0936 0942 1262 1267 1280 1291
1303 1324 1331 1372 1375 1402 1421 1429 1440 1461 1468 1479
1484 1500 1520 1537 1547 1551 1569 1588 1595 1603 1617 1632
1639 1655 1664 1788 1796 1798 1801 1804 1809 1816
 1833
 1841
1842
 1868
 1869
 1873
 1881
CHH
 0875 0881 0906 0982 1159 1168 1178 1190 1255 1325 1438 1532
1558 1573 1591 1614 1634 1656 1663 1677 1686 1703 1855
 1860
1871
 1875
 1893
 1896
 1899
CPA
 0386 0389 0393 0418 0420 0421 0423 0439 0539 0548 0565 0679
0776 0850 0855 0895 0915 0959 1163 1196 1222 1239 1285 1317
1343 1349 1362 1366 1387 1409 1436 1443 1618 1621
CRK
 0396
 0452
 1031 1034 1039 1042 1051
 1054 1059 1062
 1099 1105
1107 1115
 1124 1146
 1157
 1277 1286 1322 1358 1369 1384 1398
1668 1863
 1874
 1902
CRL
 0285 0320 1359 1376
CSA
 0425
CSC
 1082 1138 1241 1397 1432 1528 1579 1662 1746 1780 1825 1856
DATE: Mar 12/13 SERVICE BULLETIN No.: A330-57-3116
REVISION No.: 02 - Feb 05/18 Page: 3
5
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### Page 36

@A330
SERVICE BULLETIN
OPERATOR
 MSN
CSN
 0649 0652 0656 0664 0818 0840 0879 0889 0908 0935 0937 0954
0958 0964 1096 1116 1129 1202 1220 1233 1244 1297 1309 1335
1392 1425 1430 1494 1519 1536 1575 1593 1625 1636 1645 1699
1714 1760 1776 1793 1814 1846
 1852
 1885
 1894
CSZ
 1839
 1867
 1879
 1889
D2F
 0209
 0968
 1112
DAH
 0644 0647 0650 0653 0667 1613 1630 1649
DAL
 0524 0533 0542 0549 0552 0578 0588 0591 0609 0614 0618 0620
0621 0631 0633 0663 0674 0690 0718 0722 0778 0784 0796 0799
0806 0817 0827 0843 0857 0858 0859 0865 1627 1628 1637 1679
1701 1716 1720 1721 1769 1783
DGA
 0240 1735
DLH
 0570 0576 0579 0629 0636 0642 0645 0648 0687 0701 0896 0905
0913 0922 0989 1292 1305 1314 1497
EDW
 1193 1711
EIN
 0269 0330 0397 0841 0847 0985 1025 1106 1742 1744 1791
ETD
 0658 0688 0717 0724 0729 0730 0737 0788 0809 0824 0832 0852
0854 0868 0975 0991 1032
 1070
 1071 1081 1167 1205 1226 1245
1414
 1486 1521 1524
 1772
EVA
 0678 0693 0755 1254 1268 1274 1684 1690 1767 1778 1794 1806
EVE
 0670
 0802 1691
F2I
 0200
FBU
 1727
FIN
 0994 1007 1013 1023 1067 1078 1088 1173
FJI
 1394 1416 1465 1692
FWI
 0253 0343
 0758 0965 1021 1265
GCR
 0919 1756 1758 1773 1805 1840
 1849
GFA
 0276 0281 0286 0287 0334 0340
GIA
 1184 1214 1261 1288 1364 1410 1446 1474 1548 1560 1577 1585
1654 1671 1698 1709 1723 1733
GRL
 0230
HAL
 1104 1114 1171 1217 1259 1295 1302 1310 1316 1389 1399 1404
1422 1469 1488 1496 1511 1530 1565 1606 1615 1672 1732
HDA
 0234 0244 0405 0479 0512 0581 0669 0673 1457 1503 1523
 1545
1557
 1567
 1598
HFY
 0211 0262 1008 1878
HKC
 1175
 1320
HVN
 0366 0943 0962 1019 1256 1266
I2L
 0275
 0454
 0828
 0911
IAW
 1339
IBE
 1377 1385 1405 1426 1437 1490 1507 1515 1694 1700 1710 1719
1728 1736 1740 1747 1755 1761 1777 1784 1835
 1854
 1864
 1877
1882
IRA
 1540
 1586
JAI
 0888 0923 0947 0956 1351 1361 1370 1391
JAV
 0409
KAC
 1626 1643 1653 1678 1681
DATE: Mar 12/13 SERVICE BULLETIN No.: A330-57-3116
REVISION No.: 02 - Feb 05/18 Page: 4
5
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### Page 37

@A330
SERVICE BULLETIN
OPERATOR
 MSN
KAL
 0206 0219 0222 0226 0241 0256 0258 0267 0338 0350 0351 0368
0428 0484 0490 0550 1133 1155 1200 1203 1393 1556 1576 1590
1611 1638 1647
KLM
 0682 0686 0703 0738 0770 0801 0925 1161 1287 1294 1300 1381
1580
LAA
 1412 1505 1543
LKE
 1838
 1843
 1851
 1866
LNI
 1675 1680 1693
MAS
 0665
 0822
 1136
 1148
 1180
 1209 1219 1229 1234 1243 1281 1318
1336 1337 1347 1388 1395 1431 1470 1489
MAU
 0883 1057
MEA
 0926 0984 0995 0998 1725
MLM
 0451
MNB
 1332
MOV
 0535 0655
 0661
MSR
 0600 0610 0666 0683 0696 0709 0726 1143 1230 1238 1246
NMB
 1451 1466
NWS
 1213
 1221
OBS
 0833
OHY
 0316 0345 0353 0362 0404 0437 0491
 0509
 0525
 0625 0632
OMA
 1038 1044 1049 1063 1093 1120 1227 1572 1582 1599
ONE
 1492
 1506
 1508
 1608 1657
P2C
 0891
 0927
PAL
 1449 1456 1460 1463 1467 1475 1482 1504 1510 1531 1546 1553
1559 1566 1568
PLM
 0261 0265 0469
 0551
QAF
 0487 0605
QFA
 0506 0508 0513 0522 0553 0558 0564 0574 0593 0595 0603 0695
0705 0712 0842 0853 0887 0940 0945 0976 1061 1094 1169 1174
1198 1251 1258 1365
QTR
 0441 0473 0489 0511 0521 0571 0623 0637 0638 0659 0680 0711
0721 0734 0743 0746 0760 0789 0792 0813 0820 0826 0849 0893
0907 0918 1350
 1386
 1406
 1578
 1584
 1594
 1688
 1708
RNA
 1872
RSF
 0980 0996 1235 1379 1478 1516
RSY
 0283
 0293
 0295
 0946
RWD
 1741 1759
RZO
 0970
SAA
 1191 1210 1223 1236 1249 1271 1745 1754 1757 1779 1792
SAF
 1667 1762 1799 1857
 1886
SAI
 0811 0819 0834 0900
SAS
 0496 0497 0515 0568 1660 1665 1697 1715
SEY
 0751 0807
SIA
 0978 0983 0986 1010 1132 1149 1156 1382 1401 1427 1447 1453
1477 1485 1517 1544 1562 1597 1609 1633 1648 1666
DATE: Mar 12/13 SERVICE BULLETIN No.: A330-57-3116
REVISION No.: 02 - Feb 05/18 Page: 5
5
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### Page 38

@A330
SERVICE BULLETIN
OPERATOR
 MSN
SVA
 1108 1127 1137 1141 1147 1153 1189 1192 1454 1462 1473 1513
1724 1726 1729 1731 1734 1738 1739 1743 1749 1764 1766 1770
1774 1781 1790 1797 1800 1803
SWR
 1000 1018 1026 1029 1084 1089 1101 1145 1181 1188 1276 1290
1355 1403
SXD
 0504
 0530 0555 0573 0612
 0616
 0684
TAE
 0348
TAM
 0232 0238 0247 0259 0361 0466 0472 0700
TAP
 0181 0195 0223 0305 0308 0312 0317 0477 0486 0877 0899 0904
0914 0934 0997
 1006
 1012
 1015
 1906
TAR
 1631 1641
TBA
 1730 1771 1785 1845
 1859
TCX
 0254 0266 0301 0398 0948 0967
THA
 0346 0990 1003 1035 1037 1060 1074 1086 1090 1263 1269 1289
1338 1348 1374 1408
THY
 0463 0697 0704 0742 0754 0774 0869 0874 0876 0882 0901 0932
0939 0949 0961 0977 1004
 1092
 1118 1150 1160 1170 1172 1204
1212 1228 1240 1298 1307 1311 1344
 1418
 1442
 1458 1476 1483
1487 1491
 1499 1501 1514 1529 1542
 1550
 1554
 1571 1592
 1616
1620 1622 1629 1635
 1640 1642 1644 1651
 1696 1704 1706 1713
1718 1722
 1750
 1768
TNA
 1378
TOW
 1033 1046 1248 1275 1312 1334 1363 1390 1419 1439 1498 1555
1601 1610
TPA
 1368
 1380
 1428
 1534
TPU
 1448
TSC
 0177 0248 0250 0251 0271 0314
 0369 0407 0427 0455
 0480 0518
0536
 0795 0966 0971
U6A
 0224
UAE
 0382 0384
UAF
 1080 1186 1250
VIR
 0403
 0432
 0476
 1195 1201 1206 1215 1231 1296 1315 1329 1341
1352
VKG
 0309 0349 0356 0357
VOZ
 1293 1306 1319 1407 1452 1561
WOW
 1098 1607 1624
WRC
 0296
XAX
 0654 0662 0692 0716 0741 0786 0952 0974 1048 1066 1075 1126
1131 1165 1411 1423 1433 1481 1533 1549 1581 1589 1596 1600
1612 1619 1646 1659 1670 1674
XLF
 0501 0597
 0635 1360
DATE: Mar 12/13 SERVICE BULLETIN No.: A330-57-3116
REVISION No.: 02 - Feb 05/18 Page: 6
5
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### Page 39

@A330
SERVICE BULLETIN
(4) Configuration by MSN
MSN
 CONFIGURATION
0177 0200 0209
 0224 0231 0234 0240 0244 0248 0251 0261
0265 0283 0285 0288
 0293 0295 0301 0306 0313 0314 0316
0320 0326 0328 0345 0346 0348 0365 0369 0372 0382 0384
0386 0389 0392 0393 0396 0403
 0405 0409 0418 0420 0421
0422 0423 0425
 0432 0437 0439 0441 0443 0444
 0448 0451
0452 0454 0455 0458 0465 0469
 0472 0473 0476 0477
 0479
0481 0486
 0489 0491 0493
 0498 0500 0503 0506
 0507 0508
0509 0510 0511 0512 0522
002
0181 0195 0206 0211 0219 0222 0223 0226 0229 0230 0232
0238 0241 0247 0249 0250 0253 0254 0255 0256 0258 0259
0262 0266 0267 0269 0271 0272 0275 0276 0277 0279 0281
0284 0286 0287 0290 0291 0296 0300 0303 0305 0308 0309
0311 0312 0315 0317 0322 0323 0324 0330 0333 0334 0337
0338 0339 0340 0342 0343 0344 0349 0350 0351 0353 0356
0357 0358 0361 0362 0364 0366 0368 0370 0375 0380 0388
0397 0398 0400 0401 0404 0407 0408 0412 0419 0427 0428
0456 0461 0462 0463 0466 0480 0484 0487 0490 0494 0496
0497 0501 0502 0504 0505
001 002
0513 0515 0516 0518 0519 0521 0524 0525 0526 0527 0529
0530 0532 0533 0535 0536 0539 0542 0548 0549 0550 0551
0552 0553 0555 0558 0564 0565 0567 0568 0570 0571 0573
0574 0576 0578 0579 0581 0584 0587 0588 0591 0593 0595
0597 0600 0602 0603 0605 0607 0609 0610 0612 0614 0616
0618 0620 0621 0623 0625 0627 0629 0631 0632 0633 0634
0635 0636 0637 0638 0640 0641 0642 0644 0645 0647 0648
0649 0650 0652 0653 0654 0655 0656 0657 0658 0659 0661
0662 0663 0664 0665 0666 0667 0669 0670 0671 0673 0674
0675 0676 0678 0679 0680 0682 0683 0684 0686 0687 0688
0690 0691 0692 0693 0695 0696 0697 0699 0700 0701 0703
0704 0705 0707 0708 0709 0711 0712 0713 0714 0716 0717
0718 0720 0721 0722 0724 0725 0726 0728 0729 0730 0732
0733 0734 0735 0737 0738 0739 0741 0742 0743 0745 0746
0747 0749 0750 0751 0752 0754 0755 0756 0758 0759 0760
0769 0770 0772 0773 0774 0776 0777 0778 0780 0781 0782
0784 0785 0786 0788 0789 0791 0792 0795 0796 0797 0799
0801 0802 0803 0805 0806 0807 0809 0810 0811 0813 0814
0815 0817 0818 0819 0820 0821 0822 0823 0826
003
DATE: Mar 12/13 SERVICE BULLETIN No.: A330-57-3116
REVISION No.: 02 - Feb 05/18 Page: 7
5
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### Page 40

@A330
SERVICE BULLETIN
MSN
 CONFIGURATION
0824 0825 0827 0828 0830 0831 0832 0833 0834 0836 0838
0839 0840 0841 0842 0843 0845 0847 0849 0850 0851 0852
0853 0854 0855 0857 0858 0859 0860 0861 0862 0863 0865
0866 0867 0868 0869 0871 0873 0874 0875 0876 0877 0879
0881 0882 0883 0884 0885 0887 0888 0889 0890 0891 0892
0893 0895 0896 0898 0899 0900 0901 0903 0904 0905 0906
0907 0908 0909 0911 0913 0914 0915 0916 0918 0919 0920
0922 0923 0925 0926 0927 0928 0930 0931 0932 0934 0935
0936 0937 0939 0940 0941 0942 0943 0944 0945 0946 0947
0948 0949 0950 0951 0952 0954 0956 0957 0958 0959 0961
0962 0963 0964 0965 0966 0967 0968 0969 0970 0971 0973
0974 0975 0976 0977 0978 0979 0980 0982 0983 0984 0985
0986 0988 0989 0990 0991 0992 0994 0995 0996 0997 0998
1000 1001 1002 1003 1004
 1006 1007 1008 1009 1010 1011
1012 1013 1014 1015 1016 1018 1019 1020 1021 1022 1023
1025 1026 1028 1029 1031 1032
 1033 1034 1035 1036 1037
1038 1039 1041 1042 1043 1044 1045 1046 1047 1048 1049
1051
 1052 1053 1054 1055 1057 1058 1059 1060 1061 1062
1063 1065 1066 1067 1069 1070
 1071 1072 1073 1074 1075
1076 1077 1078 1080 1081 1082 1084 1085 1086 1087 1088
1089 1090 1092
 1093 1094 1095 1096 1097 1098 1099 1100
1101 1103 1104 1105 1106 1107 1108 1110 1112 1114 1115
1116 1118 1120 1123 1124 1126 1127 1129 1130 1131 1132
1133 1135 1136
 1137 1138 1141 1143 1145 1146 1147 1148
1149 1150 1151 1153 1155 1156 1157 1159 1160 1161 1163
1164
 1165 1167 1168 1169 1170 1171 1172 1173 1174 1175
1177 1178 1180
 1181 1183 1184 1186 1187 1188 1189 1190
1191 1192 1193 1195 1196 1198 1199 1200 1201 1202 1203
1204 1205 1206 1208 1209 1210 1211 1212 1213 1214 1215
1216 1217 1218 1219 1220 1221 1222 1223 1224 1225 1226
1227 1228 1229 1230 1231 1232 1233 1234 1235 1236 1237
1238 1239 1240 1241 1243 1244 1245 1246 1247 1248 1249
1250 1251 1252 1254 1255 1256 1258 1259 1260 1261 1262
1263 1264 1265 1266 1267 1268 1269 1270 1271 1272 1274
1275 1276 1277 1278 1279 1280 1281 1282 1283 1284 1285
1286 1287 1288 1289 1290 1291 1292 1293 1294 1295 1296
1297 1298 1299 1300 1301 1302 1303 1304 1305 1306 1307
1308 1309 1310 1311 1312 1313 1314 1315 1316 1317 1318
1319 1320
 1321 1322 1323 1324 1325 1326 1327 1328 1329
1330 1331 1332
 1333 1334 1335 1336 1337 1338 1339 1340
1341 1342 1343 1344
 1345 1346 1347 1348 1349 1350
 1351
1352 1353 1354 1355 1356 1357 1358 1359 1360 1361 1362
1363 1364 1365 1366 1367 1368
 1369 1370 1371 1372 1373
1374 1375 1376 1377 1378 1379 1380
 1381 1382 1383 1384
1385 1386
 1387 1388 1389 1390 1391 1392 1393 1394 1395
1396 1397 1398 1399 1400 1401 1402 1403 1404 1405 1406
1407 1408 1409 1410 1411 1412 1413 1414
 1415 1416 1417
1418
 1419 1420 1421 1422 1423 1425 1426 1427 1428
 1429
1430 1431 1432 1433 1434 1435 1436 1437 1438 1439 1440
004
DATE: Mar 12/13 SERVICE BULLETIN No.: A330-57-3116
REVISION No.: 02 - Feb 05/18 Page: 8
5
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### Page 41

@A330
SERVICE BULLETIN
MSN
 CONFIGURATION
1441
 1442
 1443
 1444
 1445
 1446
 1447
 1448
 1449
 1450
 1451
1452
 1453
 1454
 1455
 1456
 1457
 1458
 1459
 1460
 1461
 1462
1463
 1464
 1465
 1466
 1467
 1468
 1469
 1470
 1471
 1472
 1473
1474
 1475
 1476
 1477
 1478
 1479
 1480
 1481
 1482
 1483
 1484
1485
 1486
 1487
 1488
 1489
 1490
 1491
 1492
 1493
 1494
 1495
1496
 1497
 1498
 1499
 1500
 1501
 1502
 1503
 1504
 1505
 1506
1507
 1508
 1509
 1510
 1511
 1512
 1513
 1514
 1515
 1516
 1517
1518
 1519
 1520
 1521
 1523
 1524
 1525
 1526
 1527
 1528
 1529
1530
 1531
 1532
 1533
 1534
 1535
 1536
 1537
 1538
 1539
 1540
1541
 1542
 1543
 1544
 1545
 1546
 1547
 1548
 1549
 1550
 1551
1552
 1553
 1554
 1555
 1556
 1557
 1558
 1559
 1560
 1561
 1562
1563
 1564
 1565
 1566
 1567
 1568
 1569
 1570
 1571
 1572
 1573
1574
 1575
 1576
 1577
 1578
 1579
 1580
 1581
 1582
 1583
 1584
1585
 1586
 1587
 1588
 1589
 1590
 1591
 1592
 1593
 1594
 1595
1596
 1597
 1598
 1599
 1600
 1601
 1602
 1603
 1604
 1605
 1606
1607
 1608
 1609
 1610
 1611
 1612
 1613
 1614
 1615
 1616
 1617
1618
 1619
 1620
 1621
 1622
 1623
 1624
 1625
 1626
 1627
 1628
1629
 1630
 1631
 1632
 1633
 1634
 1635
 1636
 1637
 1638
 1639
1640
 1641
 1642
 1643
 1644
 1645
 1646
 1647
 1648
 1649
 1650
1651
 1653
 1654
 1655
 1656
 1657
 1658
 1659
 1660
 1662
 1663
1664
 1665
 1666
 1667
 1668
 1669
 1670
 1671
 1672
 1673
 1674
1675
 1676
 1677
 1678
 1679
 1680
 1681
 1684
 1685
 1686
 1687
1688
 1689
 1690
 1691
 1692
 1693
 1694
 1695
 1696
 1697
 1698
1699
 1700
 1701
 1703
 1704
 1706
 1708
 1709
 1710
 1711
 1712
1713
 1714
 1715
 1716
 1718
 1719
 1720
 1721
 1722
 1723
 1724
1725
 1726
 1727
 1728
 1729
 1730
 1731
 1732
 1733
 1734
 1735
1736
 1737
 1738
 1739
 1740
 1741
 1742
 1743
 1744
 1745
 1746
1747
 1748
 1749
 1750
 1751
 1752
 1760
004
1753 1754 1755 1756 1757 1758 1759 1761 1762 1763 1764
1765 1766 1767 1768
 1769 1770 1771 1772
 1773 1774 1775
1776 1777 1778 1779 1780 1781 1782 1783 1784 1785 1786
1787 1788 1789 1790 1791 1792 1793 1794 1796 1797 1798
1799 1800 1801 1802 1803 1804 1805 1806 1809 1814 1816
1825 1830
 1833
 1835
 1838
 1839
 1840
 1841
 1842
 1843
 1845
1846
 1848
 1849
 1851
 1852
 1854
 1855
 1856
 1857
 1859
 1860
1862
 1863
 1864
 1866
 1867
 1868
 1869
 1871
 1872
 1873
 1874
1875
 1877
 1878
 1879
 1880
 1881
 1882
 1883
 1885
 1886
 1889
1891
 1893
 1894
 1896
 1899
 1902
 1906
005
(5) Configuration definition
**CONF 001
Config. 001 is valid for aircraft on which:
- MOD No. 49202S16307 is not embodied,
and on which:
- Service Bulletin No. A330-57-3083 (MOD No. 52094S17923) is not accomplished.
**CONF 002
Config. 002 is valid for aircraft on which:
- MOD No. 49202S16307 is not embodied,
and on which:
DATE: Mar 12/13 SERVICE BULLETIN No.: A330-57-3116
REVISION No.: 02 - Feb 05/18 Page: 9
5
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### Page 42

@A330
SERVICE BULLETIN
- Service Bulletin No. A330-57-3083 (MOD No. 52094S17923) is accomplished.
or
- MOD No. 49202S16307 and
- MOD No. 50755S16633 are embodied,
and on which:
- Service Bulletin No. A330-57-3083 (MOD No. 52094S17923) is accomplished.
**CONF 003
Config. 003 is valid for aircraft on which:
- MOD No. 49202S16307 is embodied,
and on which:
- MOD No. 55306S18660 is not embodied.
**CONF 004
Config. 004 is valid for aircraft on which:
- MOD No. 55306S18660 is embodied,
and on which:
- MOD No. 205225S33534 is not embodied.
or
- MOD No. 55792S18775 is embodied,
and on which:
- MOD No. 205225S33534 is not embodied.
**CONF 005
Config. 005 is valid for aircraft on which:
- MOD No. 205225S33534 is embodied.
(6) Material Effectivity
**CONF 001, 003 thru 004
MATERIAL
 QTY PER A/C
 SEE NOTES
Kit 573116A01R06
 2
Kit 573116A03R02
 2
Kit
 573116A07R00
 2
 (1
)
Consumable CMLA01
 1
NOTE
 (1)
:K i t
 573116A07R00 is only necessary if Kit 573116A01R03 has been
received and not installed on aircraft at the time of Service Bulletin
Revision No. 02 issuance.
**CONF 002
MATERIAL
 QTY PER A/C
 SEE NOTES
Kit 573116A02R04
 2
Kit 573116A03R02
 2
Kit
 573116A08R00
 2
 (1
)
Consumable CMLA01
 1
NOTE
 (1)
:K i t
 573116A08R00 is only necessary if Kit 573116A01R03 has been
received and not installed on aircraft at the time of Service Bulletin
Revision No. 02 issuance.
DATE: Mar 12/13 SERVICE BULLETIN No.: A330-57-3116
REVISION No.: 02 - Feb 05/18 Page: 10
5
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### Page 43

@A330
SERVICE BULLETIN
**CONF 005
MATERIAL
 QTY PER A/C
 SEE NOTES
Kit 573116A01R06
 2
Kit
 573116A06R00
 2
 (1
)
Consumable CMLA01
 1
NOTE
 (1)
:K i t
 573116A06R00 is only necessary if Kit 573116A01R03 has been
received and not installed on aircraft at the time of Service Bulletin
Revision No. 02 issuance.
**CONF ALL
B. CONCURRENT REQUIREMENTS
None
C. REASON
(1) History
During ALI 57.11.04 inspections tasks on the rear fitting of the Frame 40 between
stringer 38 and 39 LH/RH side, cracks have been found on the fasteners next to the
one to be inspected (for the configuration PRE MOD 44360). After reaming at second
oversize of the subjected hole, the crack is still present.
(2) Objective/Action
This Service Bulletin mandates the Inspection of the fasteners holes at Frame 40
Vertical Web between stringer 38 and 39 below Intrados, left and right sides for all A330
aircraft post-modification 44360 embodiments. The aim of this Inspection Service Bulletin
(ISB) is to implement the corrective inspection necessary to the in-service aircraft.
For aircraft previously inspected as per Technical Disposition Ref. LR57D11023270 or
LR57D11029173, next inspection is due based on interval value given in this ISB or
dedicated RDAS instructions requirements in case of deviations to the TD instructions.
The procedure as described in this Service Bulletin is to be performed if no AIRBUS
repair and/or repair improvement has been previously performed in the same area.
In case of repairs performed previously, please contact AIRBUS Repair Support
department of further instruction.
(3) Advantages
Accomplishment of this ISB will permit early detection of cracks on the Frame 40 Vertical
Web between stringer 38 and 39 below Intrados, left and right sides and will ensure that
the structural integrity of the area is maintained.
(4) Operational/Maintenance Consequences
The Task ALI 57.11.04 applicable to aircraft post-modification 44360 will be superseded
by accomplishment of this Service Bulletin No. A330-57-3116.
DATE: Mar 12/13 SERVICE BULLETIN No.: A330-57-3116
REVISION No.: 02 - Feb 05/18 Page: 11
5
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### Page 44

@A330
SERVICE BULLETIN
D. DESCRIPTION
To accomplish this Service Bulletin it is necessary to :
**CONF 001
Task 573116-839-801-001: Check the existence of an RDAS in the area of FR40 Pre Service
Bulletin No. A330-57-3132
(1) Check the existence of an RDAS in the area of FR40
Task 573116-832-801-001: Special Detailed Inspection of the Holes of FR40 Pre Service
Bulletin No. A330-57-3132
(1) Depending on the Check of the RDAS, Do a Special Detailed Inspection of the
Fastener Holes H38, H39, H43 and H25 of FR40, LH side
(2) Depending on the Check of the RDAS, Do a Special Detailed Inspection of the
Fastener Holes H38, H39, H43 and H25 of FR40, RH side
(3) Depending on the Check of the RDAS, Remove the Fasteners from Holes H38, H39,
H43 and H25, LH Side
(4) Depending on the Check of the RDAS, Remove the Fasteners from Holes H38, H39,
H43 and H25, RH Side
(5) Depending on the Check of the RDAS, Do a Rotating Probe Inspection of the
Fastener Holes H38, H39, H43 and H25 of FR40, LH Side
(6) Depending on the Check of the RDAS, Do a Rotating Probe Inspection of the
Fastener Holes H38, H39, H43 and H25 of FR40, RH Side
(7) Depending on the Inspection Results, install the New same Fasteners to the Holes
H38, H39, H43 and H25 in transition fit, LH Side
(8) Depending on the Inspection Results, install the New same Fasteners to the Holes
H38, H39, H43 and H25 in transition fit, RH Side
(9) Depending on the Inspection Results, oversize the Holes H38, H39, H43 and H25 to
the First Oversize in comparison with the current Hole diameter, LH Side
(10) Depending on the Inspection Results, oversize the Holes H38, H39, H43 and H25
to the First Oversize in comparison with the current Hole diameter, RH Side
(11) Depending on the Inspection Results, install the New Fasteners to the Holes H38,
H39, H43 and H25 in transition fit, LH Side
(12) Depending on the Inspection Results, install the New Fasteners to the Holes H38,
H39, H43 and H25 in transition fit, RH Side
Task 573116-839-802-001: Check the existence of an RDAS in the area of FR40 Post
Service Bulletin No. A330-57-3132
(1) Check the existence of an RDAS in the area of FR40
DATE: Mar 12/13 SERVICE BULLETIN No.: A330-57-3116
REVISION No.: 02 - Feb 05/18 Page: 12
5
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### Page 45

@A330
SERVICE BULLETIN
Task 573116-832-802-001: Special Detailed Inspection of the Holes of FR40 Post Service
Bulletin No. A330-57-3132
(1) Depending on the Check of the RDAS, Do a Special Detailed Inspection of the
Fastener Holes H38, H39, H43 and H25 of FR40, LH side
(2) Depending on the Check of the RDAS, Do a Special Detailed Inspection of the
Fastener Holes H38, H39, H43 and H25 of FR40, RH side
(3) Depending on the Check of the RDAS, Remove the Fasteners from Holes H38, H39,
H43 and H25, LH Side
(4) Depending on the Check of the RDAS, Remove the Fasteners from Holes H38, H39,
H43 and H25, RH Side
(5) Depending on the Check of the RDAS, Do a Rotating Probe Inspection of the
Fastener Holes H38, H39, H43 and H25 of FR40, LH Side
(6) Depending on the Check of the RDAS, Do a Rotating Probe Inspection of the
Fastener Holes H38, H39, H43 and H25 of FR40, RH Side
(7) Depending on the Inspection Results, install the New same Fasteners to the Holes
H38, H39, H43 and H25 in transition fit, LH Side
(8) Depending on the Inspection Results, install the New same Fasteners to the Holes
H38, H39, H43 and H25 in transition fit, RH Side
(9) Depending on the Inspection Results, oversize the Holes H38, H39, H43 and H25 to
the First Oversize in comparison with the current Hole diameter, LH Side
(10) Depending on the Inspection Results, oversize the Holes H38, H39, H43 and H25
to the First Oversize in comparison with the current Hole diameter, RH Side
(11) Depending on the Inspection Results, install the New Fasteners to the Holes H38,
H39, H43 and H25 in transition fit, LH Side
(12) Depending on the Inspection Results, install the New Fasteners to the Holes H38,
H39, H43 and H25 in transition fit, RH Side
**CONF 002
Task 573116-839-801-001: Check the existence of an RDAS in the area of FR40 Pre Service
Bulletin No. A330-57-3132
(1) Check the existence of an RDAS in the area of FR40
Task 573116-832-801-001: Special Detailed Inspection of the Holes of FR40 Pre Service
Bulletin No. A330-57-3132
(1) Depending on the Check of the RDAS, Do a Special Detailed Inspection of the
Fastener Holes H38, H39 and H43 of FR40, LH side
(2) Depending on the Check of the RDAS, Do a Special Detailed Inspection of the
Fastener Holes H38, H39 and H43 of FR40, RH side
DATE: Mar 12/13 SERVICE BULLETIN No.: A330-57-3116
REVISION No.: 02 - Feb 05/18 Page: 13
5
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### Page 46

@A330
SERVICE BULLETIN
(3) Depending on the Check of the RDAS, Do a Special Detailed Inspection of the
Fastener Hole H25 of FR40, LH side
(4) Depending on the Check of the RDAS, Do a Special Detailed Inspection of the
Fastener Hole H25 of FR40, RH side
(5) Depending on the Check of the RDAS, Remove the Fasteners from Holes H38, H39
and H43, LH Side
(6) Depending on the Check of the RDAS, Remove the Fasteners from Holes H38, H39
and H43, RH Side
(7) Depending on the Check of the RDAS, Remove the Fastener from Hole H25, LH
Side
(8) Depending on the Check of the RDAS, Remove the Fastener from Hole H25, RH
Side
(9) Depending on the Check of the RDAS, Do a Rotating Probe Inspection of the
Fastener Holes H38, H39 and H43 of FR40, LH Side
(10) Depending on the Check of the RDAS, Do a Rotating Probe Inspection of the
Fastener Holes H38, H39 and H43 of FR40, RH Side
(11) Depending on the Check of the RDAS, Do a Rotating Probe Inspection of the
Fastener Hole H25 of FR40, LH Side
(12) Depending on the Check of the RDAS, Do a Rotating Probe Inspection of the
Fastener Hole H25 of FR40, RH Side
(13) Depending on the Inspection Results, install the New same Fasteners to the Holes
H38, H39 and H43 in transition fit, LH Side
(14) Depending on the Inspection Results, install the New same Fasteners to the Holes
H38, H39 and H43 in transition fit, RH Side
(15) Depending on the Inspection Results, install the New same Fastener to the Hole
H25 in transition fit, LH Side
(16) Depending on the Inspection Results, install the New same Fastener to the Hole
H25 in transition fit, RH Side
(17) Depending on the Inspection Results, oversize the Holes H38, H39 and H43 to the
First Oversize in comparison with the current Hole diameter, LH Side
(18) Depending on the Inspection Results, oversize the Holes H38, H39 and H43 to the
First Oversize in comparison with the current Hole diameter, RH Side
(19) Depending on the Inspection Results, oversize the Hole H25 to the First Oversize in
comparison with the current Hole diameter, LH Side
(20) Depending on the Inspection Results, oversize the Hole H25 to the First Oversize in
comparison with the current Hole diameter, RH Side
DATE: Mar 12/13 SERVICE BULLETIN No.: A330-57-3116
REVISION No.: 02 - Feb 05/18 Page: 14
5
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SERVICE BULLETIN
(21) Depending on the Inspection Results, install the New Fasteners to the Holes H38,
H39 and H43 in transition fit, LH Side
(22) Depending on the Inspection Results, install the New Fasteners to the Holes H38,
H39 and H43 in transition fit, RH Side
(23) Depending on the Inspection Results, install the New Fastener to the Hole H25 in
transition fit, LH Side
(24) Depending on the Inspection Results, install the New Fastener to the Hole H25 in
transition fit, RH Side
Task 573116-839-802-001: Check the existence of an RDAS in the area of FR40 Post
Service Bulletin No. A330-57-3132
(1) Check the existence of an RDAS in the area of FR40
Task 573116-832-802-001: Special Detailed Inspection of the Holes of FR40 Post Service
Bulletin No. A330-57-3132
(1) Depending on the Check of the RDAS, Do a Special Detailed Inspection of the
Fastener Holes H38, H39 and H43 of FR40, LH side
(2) Depending on the Check of the RDAS, Do a Special Detailed Inspection of the
Fastener Holes H38, H39 and H43 of FR40, RH side
(3) Depending on the Check of the RDAS, Do a Special Detailed Inspection of the
Fastener Hole H25 of FR40, LH side
(4) Depending on the Check of the RDAS, Do a Special Detailed Inspection of the
Fastener Hole H25 of FR40, RH side
(5) Depending on the Check of the RDAS, Remove the Fasteners from Holes H38, H39
and H43, LH Side
(6) Depending on the Check of the RDAS, Remove the Fasteners from Holes H38, H39
and H43, RH Side
(7) Depending on the Check of the RDAS, Remove the Fastener from Hole H25, LH
Side
(8) Depending on the Check of the RDAS, Remove the Fastener from Hole H25, RH
Side
(9) Depending on the Check of the RDAS, Do a Rotating Probe Inspection of the
Fastener Holes H38, H39 and H43 of FR40, LH Side
(10) Depending on the Check of the RDAS, Do a Rotating Probe Inspection of the
Fastener Holes H38, H39 and H43 of FR40, RH Side
(11) Depending on the Check of the RDAS, Do a Rotating Probe Inspection of the
Fastener Hole H25 of FR40, LH Side
(12) Depending on the Check of the RDAS, Do a Rotating Probe Inspection of the
DATE: Mar 12/13 SERVICE BULLETIN No.: A330-57-3116
REVISION No.: 02 - Feb 05/18 Page: 15
5
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@A330
SERVICE BULLETIN
Fastener Hole H25 of FR40, RH Side
(13) Depending on the Inspection Results, install the New same Fasteners to the Holes
H38, H39 and H43 in transition fit, LH Side
(14) Depending on the Inspection Results, install the New same Fasteners to the Holes
H38, H39 and H43 in transition fit, RH Side
(15) Depending on the Inspection Results, install the New same Fastener to the Hole
H25 in transition fit, LH Side
(16) Depending on the Inspection Results, install the New same Fastener to the Hole
H25 in transition fit, RH Side
(17) Depending on the Inspection Results, oversize the Holes H38, H39 and H43 to the
First Oversize in comparison with the current Hole diameter, LH Side
(18) Depending on the Inspection Results, oversize the Holes H38, H39 and H43 to the
First Oversize in comparison with the current Hole diameter, RH Side
(19) Depending on the Inspection Results, oversize the Hole H25 to the First Oversize in
comparison with the current Hole diameter, LH Side
(20) Depending on the Inspection Results, oversize the Hole H25 to the First Oversize in
comparison with the current Hole diameter, RH Side
(21) Depending on the Inspection Results, install the New Fasteners to the Holes H38,
H39 and H43 in transition fit, LH Side
(22) Depending on the Inspection Results, install the New Fasteners to the Holes H38,
H39 and H43 in transition fit, RH Side
(23) Depending on the Inspection Results, install the New Fastener to the Hole H25 in
transition fit, LH Side
(24) Depending on the Inspection Results, install the New Fastener to the Hole H25 in
transition fit, RH Side
**CONF 003
Task 573116-839-801-001: Check the existence of an RDAS in the area of FR40 Pre Service
Bulletin No. A330-57-3132
(1) Check the existence of an RDAS in the area of FR40
Task 573116-832-801-001: Special Detailed Inspection of the Holes of FR40 Pre Service
Bulletin No. A330-57-3132
(1) Depending on the Check of the RDAS, Do a Special Detailed Inspection of the
Fastener Holes H38, H39, H43 and H25 of FR40, LH side
(2) Depending on the Check of the RDAS, Do a Special Detailed Inspection of the
Fastener Holes H38, H39, H43 and H25 of FR40, RH side
DATE: Mar 12/13 SERVICE BULLETIN No.: A330-57-3116
REVISION No.: 02 - Feb 05/18 Page: 16
5
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### Page 49

@A330
SERVICE BULLETIN
(3) Depending on the Check of the RDAS, Remove the Fasteners from Holes H38, H39,
H43 and H25, LH Side
(4) Depending on the Check of the RDAS, Remove the Fasteners from Holes H38, H39,
H43 and H25, RH Side
(5) Depending on the Check of the RDAS, Do a Rotating Probe Inspection of the
Fastener Holes H38, H39, H43 and H25 of FR40, LH Side
(6) Depending on the Check of the RDAS, Do a Rotating Probe Inspection of the
Fastener Holes H38, H39, H43 and H25 of FR40, RH Side
(7) Depending on the Inspection Results, install the New same Fasteners to the Holes
H38, H39, H43 and H25 in transition fit, LH Side
(8) Depending on the Inspection Results, install the New same Fasteners to the Holes
H38, H39, H43 and H25 in transition fit, RH Side
(9) Depending on the Inspection Results, oversize the Holes H38, H39, H43 and H25 to
the First Oversize in comparison with the current Hole diameter, LH Side
(10) Depending on the Inspection Results, oversize the Holes H38, H39, H43 and H25
to the First Oversize in comparison with the current Hole diameter, RH Side
(11) Depending on the Inspection Results, install the New Fasteners to the Holes H38,
H39, H43 and H25 in transition fit, LH Side
(12) Depending on the Inspection Results, install the New Fasteners to the Holes H38,
H39, H43 and H25 in transition fit, RH Side
Task 573116-839-802-001: Check the existence of an RDAS in the area of FR40 Post
Service Bulletin No. A330-57-3132
(1) Check the existence of an RDAS in the area of FR40
Task 573116-832-802-001: Special Detailed Inspection of the Holes of FR40 Post Service
Bulletin No. A330-57-3132
(1) Depending on the Check of the RDAS, Do a Special Detailed Inspection of the
Fastener Holes H38, H39, H43 and H25 of FR40, LH side
(2) Depending on the Check of the RDAS, Do a Special Detailed Inspection of the
Fastener Holes H38, H39, H43 and H25 of FR40, RH side
(3) Depending on the Check of the RDAS, Remove the Fasteners from Holes H38, H39,
H43 and H25, LH Side
(4) Depending on the Check of the RDAS, Remove the Fasteners from Holes H38, H39,
H43 and H25, RH Side
(5) Depending on the Check of the RDAS, Do a Rotating Probe Inspection of the
Fastener Holes H38, H39, H43 and H25 of FR40, LH Side
(6) Depending on the Check of the RDAS, Do a Rotating Probe Inspection of the
DATE: Mar 12/13 SERVICE BULLETIN No.: A330-57-3116
REVISION No.: 02 - Feb 05/18 Page: 17
5
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### Page 50

@A330
SERVICE BULLETIN
Fastener Holes H38, H39, H43 and H25 of FR40, RH Side
(7) Depending on the Inspection Results, install the New same Fasteners to the Holes
H38, H39, H43 and H25 in transition fit, LH Side
(8) Depending on the Inspection Results, install the New same Fasteners to the Holes
H38, H39, H43 and H25 in transition fit, RH Side
(9) Depending on the Inspection Results, oversize the Holes H38, H39, H43 and H25 to
the First Oversize in comparison with the current Hole diameter, LH Side
(10) Depending on the Inspection Results, oversize the Holes H38, H39, H43 and H25
to the First Oversize in comparison with the current Hole diameter, RH Side
(11) Depending on the Inspection Results, install the New Fasteners to the Holes H38,
H39, H43 and H25 in transition fit, LH Side
(12) Depending on the Inspection Results, install the New Fasteners to the Holes H38,
H39, H43 and H25 in transition fit, RH Side
**CONF 004
Task 573116-839-801-001: Check the existence of an RDAS in the area of FR40 Pre Service
Bulletin No. A330-57-3132
(1) Check the existence of an RDAS in the area of FR40
Task 573116-832-801-001: Special Detailed Inspection of the Holes of FR40 Pre Service
Bulletin No. A330-57-3132
(1) Depending on the Check of the RDAS, Do a Special Detailed Inspection of the
Fastener Holes H38, H39, H43 and H25 of FR40, LH side
(2) Depending on the Check of the RDAS, Do a Special Detailed Inspection of the
Fastener Holes H38, H39, H43 and H25 of FR40, RH side
(3) Depending on the Check of the RDAS, Remove the Fasteners from Holes H38, H39,
H43 and H25, LH Side
(4) Depending on the Check of the RDAS, Remove the Fasteners from Holes H38, H39,
H43 and H25, RH Side
(5) Depending on the Check of the RDAS, Do a Rotating Probe Inspection of the
Fastener Holes H38, H39, H43 and H25 of FR40, LH Side
(6) Depending on the Check of the RDAS, Do a Rotating Probe Inspection of the
Fastener Holes H38, H39, H43 and H25 of FR40, RH Side
(7) Depending on the Inspection Results, install the New same Fasteners to the Holes
H38, H39, H43 and H25 in transition fit, LH Side
(8) Depending on the Inspection Results, install the New same Fasteners to the Holes
H38, H39, H43 and H25 in transition fit, RH Side
DATE: Mar 12/13 SERVICE BULLETIN No.: A330-57-3116
REVISION No.: 02 - Feb 05/18 Page: 18
5
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### Page 51

@A330
SERVICE BULLETIN
(9) Depending on the Inspection Results, oversize the Holes H38, H39, H43 and H25 to
the First Oversize in comparison with the current Hole diameter, LH Side
(10) Depending on the Inspection Results, oversize the Holes H38, H39, H43 and H25
to the First Oversize in comparison with the current Hole diameter, RH Side
(11) Depending on the Inspection Results, install the New Fasteners to the Holes H38,
H39, H43 and H25 in transition fit, LH Side
(12) Depending on the Inspection Results, install the New Fasteners to the Holes H38,
H39, H43 and H25 in transition fit, RH Side
Task 573116-839-802-001: Check the existence of an RDAS in the area of FR40 Post
Service Bulletin No. A330-57-3132
(1) Check the existence of an RDAS in the area of FR40
Task 573116-832-802-001: Special Detailed Inspection of the Holes of FR40 Post Service
Bulletin No. A330-57-3132
(1) Depending on the Check of the RDAS, Do a Special Detailed Inspection of the
Fastener Hole H25 of FR40, LH side
(2) Depending on the Check of the RDAS, Do a Special Detailed Inspection of the
Fastener Hole H25 of FR40, RH side
(3) Depending on the Check of the RDAS, Remove the Fastener from Hole H25, LH
Side
(4) Depending on the Check of the RDAS, Remove the Fastener from Hole H25, RH
Side
(5) Depending on the Check of the RDAS, Do a Rotating Probe Inspection of the
Fastener Hole H25 of FR40, LH Side
(6) Depending on the Check of the RDAS, Do a Rotating Probe Inspection of the
Fastener Hole H25 of FR40, RH Side
(7) Depending on the Inspection Results, install the New same Fastener to the Hole H25
in transition fit, LH Side
(8) Depending on the Inspection Results, install the New same Fastener to the Hole H25
in transition fit, RH Side
(9) Depending on the Inspection Results, oversize the Hole H25 to the First Oversize in
comparison with the current Hole diameter, LH Side
(10) Depending on the Inspection Results, oversize the Hole H25 to the First Oversize in
comparison with the current Hole diameter, RH Side
(11) Depending on the Inspection Results, install the New Fastener to the Hole H25 in
transition fit, LH Side
(12) Depending on the Inspection Results, install the New Fastener to the Hole H25 in
DATE: Mar 12/13 SERVICE BULLETIN No.: A330-57-3116
REVISION No.: 02 - Feb 05/18 Page: 19
5
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@A330
SERVICE BULLETIN
transition fit, RH Side
**CONF 005
Task 573116-839-801-001: Check the existence of an RDAS in the area of FR40 Pre Service
Bulletin No. A330-57-3132
(1) Check the existence of an RDAS in the area of FR40
Task 573116-832-801-001: Special Detailed Inspection of the Holes of FR40 Pre Service
Bulletin No. A330-57-3132
(1) Depending on the Check of the RDAS, Do a Special Detailed Inspection of the
Fastener Hole H25 of FR40, LH side
(2) Depending on the Check of the RDAS, Do a Special Detailed Inspection of the
Fastener Hole H25 of FR40, RH side
(3) Depending on the Check of the RDAS, Remove the Fastener from Hole H25, LH
Side
(4) Depending on the Check of the RDAS, Remove the Fastener from Hole H25, RH
Side
(5) Depending on the Check of the RDAS, Do a Rotating Probe Inspection of the
Fastener Hole H25 of FR40, LH Side
(6) Depending on the Check of the RDAS, Do a Rotating Probe Inspection of the
Fastener Hole H25 of FR40, RH Side
(7) Depending on the Inspection Results, install the New same Fastener to the Hole H25
in transition fit, LH Side
(8) Depending on the Inspection Results, install the New same Fastener to the Hole H25
in transition fit, RH Side
(9) Depending on the Inspection Results, oversize the Hole H25 to the First Oversize in
comparison with the current Hole diameter, LH Side
(10) Depending on the Inspection Results, oversize the Hole H25 to the First Oversize in
comparison with the current Hole diameter, RH Side
(11) Depending on the Inspection Results, install the New Fastener to the Hole H25 in
transition fit, LH Side
(12) Depending on the Inspection Results, install the New Fastener to the Hole H25 in
transition fit, RH Side
Task 573116-839-802-001: Check the existence of an RDAS in the area of FR40 Post
Service Bulletin No. A330-57-3132
(1) Check the existence of an RDAS in the area of FR40
Task 573116-832-802-001: Special Detailed Inspection of the Holes of FR40 Post Service
DATE: Mar 12/13 SERVICE BULLETIN No.: A330-57-3116
REVISION No.: 02 - Feb 05/18 Page: 20
5
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### Page 53

@A330
SERVICE BULLETIN
Bulletin No. A330-57-3132
(1) Depending on the Check of the RDAS, Do a Special Detailed Inspection of the
Fastener Hole H25 of FR40, LH side
(2) Depending on the Check of the RDAS, Do a Special Detailed Inspection of the
Fastener Hole H25 of FR40, RH side
(3) Depending on the Check of the RDAS, Remove the Fastener from Hole H25, LH
Side
(4) Depending on the Check of the RDAS, Remove the Fastener from Hole H25, RH
Side
(5) Depending on the Check of the RDAS, Do a Rotating Probe Inspection of the
Fastener Hole H25 of FR40, LH Side
(6) Depending on the Check of the RDAS, Do a Rotating Probe Inspection of the
Fastener Hole H25 of FR40, RH Side
(7) Depending on the Inspection Results, install the New same Fastener to the Hole H25
in transition fit, LH Side
(8) Depending on the Inspection Results, install the New same Fastener to the Hole H25
in transition fit, RH Side
(9) Depending on the Inspection Results, oversize the Hole H25 to the First Oversize in
comparison with the current Hole diameter, LH Side
(10) Depending on the Inspection Results, oversize the Hole H25 to the First Oversize in
comparison with the current Hole diameter, RH Side
(11) Depending on the Inspection Results, install the New Fastener to the Hole H25 in
transition fit, LH Side
(12) Depending on the Inspection Results, install the New Fastener to the Hole H25 in
transition fit, RH Side
**CONF ALL
E. COMPLIANCE
(1) Classification
MANDATORY: Service Bulletin must be accomplished.
(2) Accomplishment Timescale
**CONF 001
This Service Bulletin has been classified Mandatory by the issue of an Airworthiness
Directive (AD) published by the European Av iation Safety Agenc y (EASA). The AD must
be used as the reference document for the mandated accomplishment timescale.
DATE: Mar 12/13 SERVICE BULLETIN No.: A330-57-3116
REVISION No.: 02 - Feb 05/18 Page: 21
5
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### Page 54

@A330
SERVICE BULLETIN
Table 1, Config. 001 - Check the existence of an RDAS in the area of the Fastener Holes H38, H39,
H43 and H25 of Frame 40, Pre Service Bulletin No. A330-57-3132, LH and RH sides
Compliance Time
Condition
 Action
Threshold
(whichever
occurs first)
Grace period
 Repetitive
Interval
(whichever
occurs first)
A330-300
Weight
Variant (WV)
010 series
Flight Cycles
(FC) optimized
set: within 18201
FC / 59458
Flight Hours (FH)
from entry into
service
or
FH optimized
set: within 14101
FC / 95418 FH
from entry into
service
See NOTE (*)
A330-300
WV020 series
except
WV022
FC optimized
set: within 19388
FC / 63333 FH
from entry into
service
or
FH optimized
set: within 15020
FC / 101637 FH
from entry into
service
See NOTE (*)
All aircraft
A330-300
WV022
Check the
existence of an
RDAS in the
area of Frame
40, LH and RH
sides in
accordance with
TASK
573116-839-801
FC optimized
set: within 18900
FC / 61740 FH
from entry into
service
or
FH optimized
set: within 14642
FC / 99081 FH
from entry into
service
See NOTE (*)
24 months
from Sep
30/16
None
DATE: Mar 12/13 SERVICE BULLETIN No.: A330-57-3116
REVISION No.: 02 - Feb 05/18 Page: 22
5
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### Page 55

@A330
SERVICE BULLETIN
Table 1, Config. 001 - Check the existence of an RDAS in the area of the Fastener Holes H38, H39,
H43 and H25 of
 Frame 40, Pre Service Bulletin No. A330-57-3132, LH and RH sides
Compliance Time
Condition
 Action
Threshold
(whichever
occurs first)
Grace period
 Repetitive
Interval
(whichever
occurs first)
All aircraft
 A330-200
WV020 series
Check the
existence of an
RDAS in the
area of
 Frame
40, LH and RH
sides in
accordance with
TASK
573116-839-801
FC optimized
set: within 17988
FC / 62957 FH
from entry into
service
or
FH optimized
set: within 13436
FC / 87334 FH
from entry into
service
See NOTE (*)
24 months
from Sep
30/16
None
Existing RDAS
 Contact
AIRBUS
Before next flight
 None
 None
No existing RDAS
 Do a special
detailed
inspection of
the fastener
holes of the
area of Frame
40, LH and RH
sides in
accordance with
TASK
573116-832-801
Refer to table 2
NOTE (*): For FH and FC optimization on A330/A340 aircraft, operators shall select the set that better
suits aircraft operation and utilization (refer to OIT 999.0086/11).
DATE: Mar 12/13 SERVICE BULLETIN No.: A330-57-3116
REVISION No.: 02 - Feb 05/18 Page: 23
5
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### Page 56

@A330
SERVICE BULLETIN
Table 2, Config. 001 - Do a Special Detailed Inspection of the Fastener Holes H38, H39, H43 and H25
of the area of Frame 40, Pre Service Bulletin No. A330-57-3132, LH and RH sides
Compliance Time
Condition
 Action
Threshold
(whichever
occurs first)
Grace period
 Repetitive
Interval
(whichever
occurs first)
All aircraft
 All A330WV
 D oas p e c i a l
detailed
inspection of the
fastener holes
of the area of
Frame 40, LH
and RH sides in
accordance with
TASK
573116-832-801
Before next flight
 None
 None
DATE: Mar 12/13 SERVICE BULLETIN No.: A330-57-3116
REVISION No.: 02 - Feb 05/18 Page: 24
5
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### Page 57

@A330
SERVICE BULLETIN
Table 2, Config. 001 - Do a Special Detailed Inspection of the Fastener Holes H38, H39, H43 and H25
of the area of Frame 40, Pre Service Bulletin No. A330-57-3132, LH and RH sides
Compliance Time
Condition
 Action
Threshold
(whichever
occurs first)
Grace period
 Repetitive
Interval
(whichever
occurs first)
All A330WV
 Install the new
same fasteners,
LH and/or RH
sides in
accordance with
SUBTASKS
573116-420-001
for LH side
and/or
573116-420-002
for RH side
And
Before next flight
 None
 None
A330-300
WV010 series
FC optimized
set: 3913 FC /
12782 FH
or
FH optimized
set: 3143 FC /
21267 FH
See NOTE (*)
A330-300
WV020 series
except
WV022
FC optimized
set: 4178 FC /
13649 FH
or
FH optimized
set: 3356 FC /
22710 FH
See NOTE (*)
No crack found
A330-300
WV022
Repeat the
special detailed
inspection, LH
and RH sides in
accordance with
TASK
573116-832-801
None
 None
FC optimized
set: 4085 FC /
13343 FH
or
FH optimized
set: 3281 FC /
22201 FH
See NOTE (*)
DATE: Mar 12/13 SERVICE BULLETIN No.: A330-57-3116
REVISION No.: 02 - Feb 05/18 Page: 25
5
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### Page 58

@A330
SERVICE BULLETIN
Table 2, Config. 001 - Do a Special Detailed Inspection of the Fastener Holes H38, H39, H43 and H25
of the area of Frame 40, Pre Service Bulletin No. A330-57-3132, LH and RH sides
Compliance Time
Condition
 Action
Threshold
(whichever
occurs first)
Grace period
 Repetitive
Interval
(whichever
occurs first)
A330-200
WV020 series
Repeat the
special detailed
inspection, LH
and RH sides in
accordance with
TASK
573116-832-801
None
 None
 FC optimized
set: 3911 FC /
13688 FH
or
FH optimized
set: 3160 FC /
20537 FH
See NOTE (*)
Or
No crack found
All A330WV
 Apply Service
Bulletin No.
A330-57-3132
Refer to table 4
See NOTE (**)
Crack found and
fasteners
installed to first
oversize after
first inspection
All A330WV
 Contact
AIRBUS
Before next flight
 None
 None
DATE: Mar 12/13 SERVICE BULLETIN No.: A330-57-3116
REVISION No.: 02 - Feb 05/18 Page: 26
5
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### Page 59

@A330
SERVICE BULLETIN
Table 2, Config. 001 - Do a Special Detailed Inspection of the Fastener Holes H38, H39, H43 and H25
of the area of Frame 40, Pre Service Bulletin No. A330-57-3132, LH and RH sides
Compliance Time
Condition
 Action
Threshold
(whichever
occurs first)
Grace period
 Repetitive
Interval
(whichever
occurs first)
Oversize the
holes to first
oversize
diameter in
comparison with
the current hole
diameter, LH
and/or RH sides
in accordance
with SUBTASKS
573116-833-001
for LH side
and/or
573116-833-002
for RH side
And
Before next flight
 None
 None
Crack found and
fastener not
installed to first
oversize after
first inspection
All A330WV
Do a rotating
probe inspection
of the fastener
holes, LH and/or
RH sides in
accordance with
SUBTASKS
573116-832-005
for LH side
and/or
573116-832-006
for RH side
Refer to table 3
NOTE (*): For FH and FC optimization on A330/A340 aircraft, operators shall select the set that better
suits aircraft operation and utilization (refer to OIT 999.0086/11).
NOTE (**): It is recommended to apply the Service Bulletin No. A330-57-3132 after the lower bound,
refer to Appendix 01 - Lower Bound Table in order to have a terminative solution for all bores.
DATE: Mar 12/13 SERVICE BULLETIN No.: A330-57-3116
REVISION No.: 02 - Feb 05/18 Page: 27
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 60

@A330
SERVICE BULLETIN
Table 3, Config. 001 - Do a Rotating Probe Inspection of the Fastener Holes H38, H39, H43 and H25
of Frame 40, Pre Service Bulletin No. A330-57-3132, LH and/or RH sides
Compliance Time
Condition
 Action
Threshold
(whichever
occurs first)
Grace period
 Repetitive
Interval
(whichever
occurs first)
All aircraft
 All A330WV
 Do a rotating
probe inspection
of the fastener
holes, LH
and/or RH sides
in accordance
with
SUBTASKS
573116-832-005
for LH side
and/or
573116-832-006
for RH side
Before next flight
 None
 None
Crack found
 All A330WV
 Contact
AIRBUS
Before next flight
 None
 None
DATE: Mar 12/13 SERVICE BULLETIN No.: A330-57-3116
REVISION No.: 02 - Feb 05/18 Page: 28
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

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