@A330

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 52

TITLE: DOORS-SERVICE DOORS-MODIFICATION OF LATCHING MECHANISM

OF POTABLE WATER SERVICE PANEL

MODIFICATION No.: 201938D50416 201938D50379 201939D59871 201939D59870 203344D50725

203563D50740

This page transmits Revision No.01 of Service Bulletin No.A330-52-3086

ADDITIONAL WORK

**CONF ALL

Additional work is required by this revision for aircraft modified by any previous issue of this Service

Bulletin to correct the adjusting stud installation and the sealant application.

REASON

Revision No. 01 issued to introduce a new Door Assy equipped with a new adjusting stud and new LISI

latches, to introduce additional work for the adjusting stud and to introduce minor changes.

CHANGES

FRONT MATTER

MODIFICATIONS MODIFICATION NUMBER(S) UPDATED R

SUMMARY

MODIFICATIONS MODIFICATION CLASSIFICATION UPDATED R

MATERIAL PRICE INFORMATION MATERIAL PRICE INFORMATION TABLE

UPDATED

R

MATERIAL PRICE INFORMATION TABLE

UPDATED

R

MATERIAL PRICE INFORMATION TABLE

UPDATED

R

EFFECTIVITY OPERATOR LIST UPDATED R

REFERENCES / REPERCUSSIONS REFERENCES/REPERCUSSIONS TABLE

UPDATED

R

MANPOWER MANPOWER UPDATED R

MANPOWER UPDATED R

MANPOWER UPDATED R

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 1

6

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

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

APPENDICES APPENDICES UPDATED R

Fig. A-GSAAA

Fig. A-GSAAA Sheet 01 SHEET UPDATED R

PLANNING INFORMATION

EFFECTIVITY EFFECTIVITY RELATED INFORMATION

UPDATED

R

Configuration definition

CONF 001 CONFIGURATION DEFINITION UPDATED R

Material Effectivity MATERIAL EFFECTIVITY UPDATED

MATERIAL SET UPDATED

MATERIAL SET QUANTITY UPDATED

R

MATERIAL EFFECTIVITY UPDATED

MATERIAL SET UPDATED

MATERIAL SET QUANTITY UPDATED

R

MATERIAL EFFECTIVITY UPDATED

MATERIAL SET UPDATED

MATERIAL SET QUANTITY UPDATED

R

COMPLIANCE

Accomplishment Timescale ACCOMPLISHMENT TIMESCALE UPDATED R

MANPOWER MANPOWER UPDATED R

MANPOWER UPDATED

CONFIGURATION UPDATED

R

MANPOWER UPDATED

CONFIGURATION UPDATED

R

MANPOWER UPDATED

CONFIGURATION UPDATED

R

WEIGHT AND BALANCE WEIGHT AND BALANCE UPDATED R

Minor editorial or document structure change R

Minor editorial or document structure change R

Minor editorial or document structure change R

REFERENCES REFERENCED DOCUMENTATION UPDATED R

REFERENCED DOCUMENTATION UPDATED R

REFERENCED DOCUMENTATION UPDATED R

PUBLICATION AFFECTED PUBLICATIONS AFFECTED UPDATED R

INTERCHANGEABILITY/MIXABILITY INTERCHANGEABILITY/MIXABILITY UPDATED R

INTERCHANGEABILITY/MIXABILITY UPDATED R

INTERCHANGEABILITY/MIXABILITY 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

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 2

6

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

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Kit 523086D01R03 PART MATERIAL SET UPDATED

MATERIAL SET LABEL UPDATED

PART NUMBER UPDATED

R

Kit 523086D02R05 PART MATERIAL SET UPDATED

MATERIAL SET LABEL UPDATED

PART NUMBER UPDATED

R

Kit 523086D03R04 PART MATERIAL SET UPDATED

MATERIAL SET LABEL UPDATED

PART NUMBER UPDATED

R

LIST OF MATERIALS - OPERATOR

SUPPLIED

Consumable Materials

Consumable CMLD10 CONSUMABLE MATERIAL SET UPDATED

CONSUMABLE UPDATED

QUANTITY UPDATED

R

Components COMPONENTS UPDATED R

Component COMPD04 PART MATERIAL SET ADDED N

PARTS TO BE RE-IDENTIFIED BY

OPERATOR

PARTS TO BE RE-IDENTIFIED BY OPERATOR

UPDATED

R

Reidentified part set REIDD07 PART MATERIAL SET ADDED N

Reidentified part set REIDD08 PART MATERIAL SET ADDED N

Reidentified part set REIDD09 PART MATERIAL SET ADDED N

ACCOMPLISHMENT INSTRUCTIONS

TASK 523086- 831-848-001-Modification TASK SOLUTION UPDATED

NOTE UPDATED

R

Task associated data - 001 MAN HOURS UPDATED

ELAPSED TIME UPDATED

R

Task associated data - 002 MAN HOURS UPDATED

ELAPSED TIME UPDATED

R

Task associated data - 003 MAN HOURS UPDATED

ELAPSED TIME UPDATED

R

Subtask 523086-910-201-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

Subtask 523086-910-201-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

Subtask 523086-910-201-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

Subtask 523086-941-201-001 SUBTASK SOLUTION UPDATED R

Subtask 523086-941-201-001 SUBTASK SOLUTION UPDATED R

Subtask 523086-941-201-001 SUBTASK SOLUTION UPDATED R

Subtask 523086-831-201-001 SUBTASK SOLUTION ADDED N

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 3

6

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

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Subtask 523086-420-201-001 SUBTASK SOLUTION UPDATED

CONSUMABLE UPDATED

QUANTITY UPDATED

REFERENCED DOCUMENTATION UPDATED

CONFIGURATION UPDATED

FIGURE REFERENCE UPDATED

MATERIAL LIST UPDATED

REFERENCES UPDATED

R

Subtask 523086-420-202-001 SUBTASK SOLUTION UPDATED

CONSUMABLE UPDATED

MATERIAL LIST UPDATED

R

Subtask 523086-420-206-001 SUBTASK SOLUTION UPDATED

PART NUMBER UPDATED

FIGURE REFERENCE UPDATED

MATERIAL LIST UPDATED

R

Subtask 523086-420-203-001 SUBTASK SOLUTION UPDATED

CONSUMABLE UPDATED

QUANTITY UPDATED

REFERENCED DOCUMENTATION UPDATED

MATERIAL LIST UPDATED

REFERENCES UPDATED

R

Subtask 523086-420-204-001 SUBTASK SOLUTION UPDATED

CONSUMABLE UPDATED

MATERIAL LIST UPDATED

R

Subtask 523086-820-201-001 SUBTASK SOLUTION UPDATED

CONSUMABLE UPDATED

QUANTITY UPDATED

FIGURE REFERENCE UPDATED

REFERENCED DOCUMENTATION UPDATED

CONFIGURATION UPDATED

MATERIAL LIST UPDATED

R

Subtask 523086-916-201-001 SUBTASK SOLUTION UPDATED

CONSUMABLE UPDATED

MATERIAL LIST UPDATED

R

Subtask 523086-420-205-001 SUBTASK SOLUTION UPDATED

CONSUMABLE UPDATED

MATERIAL LIST UPDATED

R

Subtask 523086-831-201-002 SUBTASK SOLUTION ADDED N

Subtask 523086-420-201-002 SUBTASK SOLUTION UPDATED

CONSUMABLE UPDATED

QUANTITY UPDATED

REFERENCED DOCUMENTATION UPDATED

CONFIGURATION UPDATED

FIGURE REFERENCE UPDATED

MATERIAL LIST UPDATED

REFERENCES UPDATED

R

Subtask 523086-420-202-002 SUBTASK SOLUTION UPDATED

CONSUMABLE UPDATED

MATERIAL LIST UPDATED

R

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 4

6

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

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Subtask 523086-420-206-002 SUBTASK SOLUTION UPDATED

PART NUMBER UPDATED

FIGURE REFERENCE UPDATED

MATERIAL LIST UPDATED

R

Subtask 523086-420-203-002 SUBTASK SOLUTION UPDATED

CONSUMABLE UPDATED

QUANTITY UPDATED

REFERENCED DOCUMENTATION UPDATED

MATERIAL LIST UPDATED

REFERENCES UPDATED

R

Subtask 523086-420-204-002 SUBTASK SOLUTION UPDATED

CONSUMABLE UPDATED

MATERIAL LIST UPDATED

R

Subtask 523086-820-201-001 SUBTASK SOLUTION UPDATED

CONSUMABLE UPDATED

QUANTITY UPDATED

FIGURE REFERENCE UPDATED

REFERENCED DOCUMENTATION UPDATED

CONFIGURATION UPDATED

MATERIAL LIST UPDATED

R

Subtask 523086-916-201-001 SUBTASK SOLUTION UPDATED

CONSUMABLE UPDATED

MATERIAL LIST UPDATED

R

Subtask 523086-420-205-002 SUBTASK SOLUTION UPDATED

CONSUMABLE UPDATED

MATERIAL LIST UPDATED

R

Subtask 523086-831-201-003 SUBTASK SOLUTION ADDED N

Subtask 523086-420-201-003 SUBTASK SOLUTION UPDATED

CONSUMABLE UPDATED

QUANTITY UPDATED

REFERENCED DOCUMENTATION UPDATED

CONFIGURATION UPDATED

FIGURE REFERENCE UPDATED

MATERIAL LIST UPDATED

REFERENCES UPDATED

R

Subtask 523086-420-202-003 SUBTASK SOLUTION UPDATED

CONSUMABLE UPDATED

MATERIAL LIST UPDATED

R

Subtask 523086-420-206-003 SUBTASK SOLUTION UPDATED

PART NUMBER UPDATED

FIGURE REFERENCE UPDATED

MATERIAL LIST UPDATED

R

Subtask 523086-420-203-003 SUBTASK SOLUTION UPDATED

CONSUMABLE UPDATED

QUANTITY UPDATED

REFERENCED DOCUMENTATION UPDATED

MATERIAL LIST UPDATED

REFERENCES UPDATED

R

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 5

6

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

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Subtask 523086-420-204-003 SUBTASK SOLUTION UPDATED

CONSUMABLE UPDATED

MATERIAL LIST UPDATED

R

Subtask 523086-820-201-001 SUBTASK SOLUTION UPDATED

CONSUMABLE UPDATED

QUANTITY UPDATED

FIGURE REFERENCE UPDATED

REFERENCED DOCUMENTATION UPDATED

CONFIGURATION UPDATED

MATERIAL LIST UPDATED

R

Subtask 523086-916-201-001 SUBTASK SOLUTION UPDATED

CONSUMABLE UPDATED

MATERIAL LIST UPDATED

R

Subtask 523086-420-205-003 SUBTASK SOLUTION UPDATED

CONSUMABLE UPDATED

MATERIAL LIST UPDATED

R

Subtask 523086-700-201-001 SUBTASK SOLUTION UPDATED R

Subtask 523086-700-201-001 SUBTASK SOLUTION UPDATED R

Subtask 523086-700-201-001 SUBTASK SOLUTION UPDATED R

Subtask 523086-942-201-001 SUBTASK SOLUTION UPDATED R

Subtask 523086-942-201-001 SUBTASK SOLUTION UPDATED R

Subtask 523086-942-201-001 SUBTASK SOLUTION UPDATED R

TASK 523086- 831-849-001-Modification -

ADDITIONAL WORK for aircraft modified

by the original issue

TASK SOLUTION ADDED N

Task associated data - 001 TASK ASSOCIATED DATA ADDED N

Task associated data - 002 TASK ASSOCIATED DATA ADDED N

Task associated data - 003 TASK ASSOCIATED DATA ADDED N

Subtask 523086-910-202-001 SUBTASK SOLUTION ADDED N

Subtask 523086-839-202-001 SUBTASK SOLUTION ADDED N

Subtask 523086-910-202-001 SUBTASK SOLUTION ADDED N

Subtask 523086-839-202-001 SUBTASK SOLUTION ADDED N

Subtask 523086-910-202-001 SUBTASK SOLUTION ADDED N

Subtask 523086-839-202-001 SUBTASK SOLUTION ADDED N

Subtask 523086-941-202-001 SUBTASK SOLUTION ADDED N

Subtask 523086-941-202-001 SUBTASK SOLUTION ADDED N

Subtask 523086-941-202-001 SUBTASK SOLUTION ADDED N

Subtask 523086-831-202-001 SUBTASK SOLUTION ADDED N

Subtask 523086-831-203-001 SUBTASK SOLUTION ADDED N

Subtask 523086-831-202-002 SUBTASK SOLUTION ADDED N

Subtask 523086-831-203-001 SUBTASK SOLUTION ADDED N

Subtask 523086-831-202-003 SUBTASK SOLUTION ADDED N

Subtask 523086-831-203-001 SUBTASK SOLUTION ADDED N

Subtask 523086-700-202-001 SUBTASK SOLUTION ADDED N

Subtask 523086-700-202-001 SUBTASK SOLUTION ADDED N

Subtask 523086-700-202-001 SUBTASK SOLUTION ADDED N

Subtask 523086-942-202-001 SUBTASK SOLUTION ADDED N

Subtask 523086-942-202-001 SUBTASK SOLUTION ADDED N

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 6

6

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

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Subtask 523086-942-202-001 SUBTASK SOLUTION ADDED N

Fig. A-GBAAA

Fig. A-GBAAA Sheet 02 SHEET UPDATED R

Fig. A-GBBAA

Fig. A-GBBAA Sheet 02 SHEET UPDATED R

Fig. A-GBBAA Sheet 03 SHEET UPDATED R

Fig. A-GBBAA Sheet 04 SHEET UPDATED R

Fig. A-GBBAA Sheet 05 SHEET UPDATED R

Fig. A-GBCAA FIGURE SOLUTION UPDATED R

Fig. A-GBCAA Sheet 02 SHEET UPDATED R

Fig. A-GBCAA Sheet 03 SHEET UPDATED R

Fig. A-GBCAA Sheet 04 SHEET ADDED N

Fig. A-GBDAA FIGURE SOLUTION ADDED N

Fig. A-GBDAA Sheet 01 SHEET ADDED N

Fig. A-GBDAA Sheet 02 SHEET ADDED N

Fig. A-GBDAA Sheet 03 SHEET ADDED N

Fig. A-GBEAA FIGURE SOLUTION ADDED N

Fig. A-GBEAA Sheet 01 SHEET ADDED N

Fig. A-GBEAA Sheet 02 SHEET ADDED N

Fig. A-GBEAA Sheet 03 SHEET ADDED N

Appendix 01 - Elapsed Time Assumption

Fig. A-GGAAA

Fig. A-GGAAA Sheet 01 SHEET UPDATED R

Appendix 02 - Status of the aircraft after accomplishment of the Service Bulletin A330-52-3086

APPENDIX CONTENT APPENDIX CONTENT ADDED N

FILLING 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

No previous revision

REVISION SEQUENCE

ORIGINAL: Apr 27/12

REVISION No. : 01 - Apr 25/14

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 7

6

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

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

This Page Intentionally Left Blank

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 8

6

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

SERVICE BULLETIN

SUMMARY

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

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

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 52

TITLE: DOORS-SERVICE DOORS-MODIFICATION OF LATCHING MECHANISM

OF POTABLE WATER SERVICE PANEL

**CONF ALL

MODIFICATIONS

MODIFICATION CLASSIFICATION

MAJOR None

MINOR 201938D50416 201938D50379 201939D59871 201939D59870 203344D50725

203563D50740

NOTE: As per EASA IR 21, a minor change is one that has no appreciable effect on the

mass, balance, structural strength, reliability, operational characteristics affecting the

airworthiness of the product. All other changes are major changes.

REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES

Several cases have been reported in which the potable water service panel access door 164AR has

been lost during flight. In one case, on an A340 aircraft the THS leading edge has been hit, in a second

case, on an A330 aircraft the door was presumed to have caused damage to the THS.

Investigations have shown difficulties with the latching mechanism of the potable water service panel

access door, which can lead to a potential unsafe condition. The potential unsafe condition could cause

possible injury to persons and damage to property on ground and potential loss of the potable water

service panel access door on runway.

The Inspection Service Bulletin A330-52-3077 was issued to inspect the access door 164AR, 154AR

and 171AL. The Modification Service Bulletin A330-52-3076 was issued as the final repair solution to

the Inspection Service Bulletin A330-52-3077. Further occurrences of access door 164AR lost during

flight have shown that the Modification Service Bulletin A330-52-3076 is not the definitive final repair

solution for this access door. Therefore, this mandatory Modification Service Bulletin, A330-52-3086, is

issued as the final repair solution for the access door 164AR. The loss of this door is classified to be a

potential unsafe condition.

To avoid further occurrences the design of the latching mechanism of the potable water service panel

access door has to be modified to mitigate the risk.

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 1

6

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

SERVICE BULLETIN

SUMMARY

This Service Bulletin mandates the operator to install a modified potable water service panel access

door with reinforced hinge screws and more robust latches, including an additional third latch.

After accomplishment of this Service Bulletin the handling and reliability of the potable water service

panel access door is improved.

This Service Bulletin meets the safety intent by making sure that the potable water service panel

access door can be correctly latched.

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 523086D01R03 1 15,280.00 Door, attachment parts

Component COMPD04 See SB Stud-adjusting

**CONF 002

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 523086D02R05 1 15,280.00 Door, attachment parts

Component COMPD04 See SB Stud-adjusting

**CONF 003

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 523086D03R04 1 15,280.00 Door, attachment parts

Component COMPD04 See SB Stud-adjusting

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 2

6

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

SERVICE BULLETIN

SUMMARY

EFFECTIVITY

**CONF ALL

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

11S 31V 36V 38W 39V 69X AAR AAW ABD ACA ACI AEA AFL

AFR AIB AIC ALK ARA ARG ASY AVA AWW AZA BEC BEL BER

CAL CCA CES CHH CPA CRK CRL CSA CSC CSN DAH DAL DGA

DLH EDW EIN ETD EVA EVE FIN FWI GFA GIA GRL HAL HDA

HFY HVN I2L ISS IYE JAI JST KAL KLM MAS MAU MEA MON

MSR OHY OMA PAL QAF QFA QTR RJA RSF RSY SAA SAI SAS

SIA SVA SWR SYA TAE TAM TAP TCX THA THY TOW TSC UAE

UAF USA VIR VKG VOZ WRC XAX XLF

CONCURRENT REQUIREMENTS

None

REFERENCES / REPERCUSSIONS

TFU 52.42.00.015

OEB None

AOT None

SIL None

LINE MAINTENANCE AFFECTED No

LIFE LIMIT None

OTHER SBIT 13-0016

NATURE OF THE WORK

AIRCRAFT YES

EQUIPMENT NO

HARD NO

SOFT NO

OBRM NO

MANPOWER

**CONF 001

Task 523086-831-848-001: Modification

TOTAL MANHOURS 13.50

ELAPSED TIME (HOURS) 12.00

Task 523086-831-849-001: Modification - ADDITIONAL WORK for aircraft modified by the

original issue

TOTAL MANHOURS 7.50

ELAPSED TIME (HOURS) 7.50

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 3

6

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

SERVICE BULLETIN

SUMMARY

**CONF 002

Task 523086-831-848-001: Modification

TOTAL MANHOURS 13.50

ELAPSED TIME (HOURS) 12.00

Task 523086-831-849-001: Modification - ADDITIONAL WORK for aircraft modified by the

original issue

TOTAL MANHOURS 7.50

ELAPSED TIME (HOURS) 7.50

**CONF 003

Task 523086-831-848-001: Modification

TOTAL MANHOURS 13.50

ELAPSED TIME (HOURS) 12.00

Task 523086-831-849-001: Modification - ADDITIONAL WORK for aircraft modified by the

original issue

TOTAL MANHOURS 7.50

ELAPSED TIME (HOURS) 7.50

APPENDICES

**CONF ALL

Appendix 01 - Elapsed Time Assumption

Appendix 02 - Status of the aircraft after accomplishment of the Service Bulletin A330-52-3086

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 4

6

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

SERVICE BULLETIN

SUMMARY

**CONF ALL

FR70

FR69

164AR

Z160

A

B

A

NEW 

POTABLE WATER

FR69

FR70

STGR50RH

B

SERVICE DOOR

164AR

G_SB_523086_6_SAAA_01_02

Figure A-GSAAA - Sheet 01

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 5

6

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

SERVICE BULLETIN

SUMMARY

This Page Intentionally Left Blank

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 6

6

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

SERVICE BULLETIN

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 52

TITLE: DOORS-SERVICE DOORS-MODIFICATION OF LATCHING MECHANISM

OF POTABLE WATER SERVICE PANEL

MODIFICATION No.: 201938D50416 201938D50379 201939D59871 201939D59870 203344D50725

203563D50740

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

The intent of this modification is achieved in production on MSN 1309 and subsequent

through modification 201715 or 201796.

(1) Models

330-202 330-203 330-223 330-243 330-301 330-302 330-303 330-321

330-322 330-323 330-341 330-342 330-343

(2) Effectivity by MSN

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

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

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

0177 0181 0183-0184 0188-0189 0191 0195 0198 0200 0203 0205-0206 0209 0211

0219 0222-0224 0226 0229-0232 0234 0238 0240-0241 0244 0247-0251 0253-0256

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

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

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

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

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

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 1

6

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

SERVICE BULLETIN

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 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 0926-0928 0930-0932 0934-0937

0939-0952 0954 0956-0959 0961-0971 0973-0980 0982-0986 0988-0992 0994-1003

1006-1016 1018-1023 1025-1026 1028-1029 1031 1033-1039 1041-1049 1052-1055

1057-1061 1063 1065-1067 1069 1071-1078 1080-1082 1084-1090 1093-1101

1103-1108 1110 1112 1114 1116 1118 1120 1123-1124 1126-1127 1129-1133 1135

1137-1138 1141 1143 1145-1147 1149-1151 1153 1155-1157 1159-1161 1163 1165

1167-1174 1177-1178 1181 1183-1184 1186-1193 1195-1196 1198-1206 1208-1241

1243-1252 1254-1256 1258-1272 1274-1304

(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

11S 1053

31V 0205

36V 0437 0451

38W 0401

39V 0939

69X 0494

AAR 0640 0676 0708 0772 0803 0845 1001 1055 1151 1211

AAW 0999 1043

ABD 0343

ACA 0277 0279 0284 0344 0400 0408 0412 0419

ACI 0507 0510

AEA 0461 0505 0526 0551 0597 0670 0733 0745 0749 0814 0931 0950

0992 1097

AFL 0963 0973 1014 1045 1047 1058 1065 1072 1077 1103 1232 1247

1264 1270 1284 1299 1301

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

0567 0584 0657

AIB 0871

AIC 0353 0362

ALK 0303 0306 0311 0313 0404 0456 0627

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SERVICE BULLETIN

OPERATOR MSN

ARA 0874 0891 0927

ARG 0290 0300 0358 0364

ASY 0747 0951 0969 1036 1183

AVA 0948 0967 1009 1016 1073 1208 1224 1279

AWW 0255

AZA 0272 0339 1123 1135 1218 1225 1252 1283

BEC 0863

BEL 0030 0037 0045 0082 0095 0229 0249 0324

BER 0288 0322 0403 0432 0444 0454 0469 0476 0493 0665 0739 0822

0828 0911

CAL 0602 0607 0641 0671 0675 0691 0699 0707 0714 0752 0769 0805

0823 0838 0861 0920 1177 1272 1278

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

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

CHH 0875 0881 0906 0919 0982 1159 1168 1178 1190 1255

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

0548 0565 0679 0776 0850 0855 0895 0915 0959 1163 1196 1222

1239 1285

CRK 1031 1034 1039 1042 1054 1059 1277 1286

CRL 0285 0320

CSA 0425

CSC 0462 1082 1138 1241

CSN 0649 0652 0656 0664 0818 0840 0879 0889 0908 0935 0937 0954

0958 0964 1096 1116 1129 1202 1220 1233 1244 1297

DAH 0644 0647 0650 0653 0667

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

DGA 0240

DLH 0570 0576 0579 0629 0636 0642 0645 0648 0687 0701 0896 0905

0913 0922 0989 1292

EDW 0291 1193

EIN 0269 0397 0841 0847 0985 1025 1106

ETD 0658 0688 0717 0724 0729 0730 0737 0751 0788 0807 0809 0824

0825 0831 0832 0852 0854 0868 0885 0888 0975 0991 1071 1081

1167 1205 1226 1245

EVA 0530 0535 0555 0573 0587 0634 0655 0661 0678 0693 0755 1254

1268 1274

EVE 0833

FIN 0994 1007 1013 1023 1067 1078 1088 1173

FWI 0253 0758 0965 1021 1265

GFA 0276 0281 0286 0287 0334 0340

GIA 0138 0140 0144 0148 0153 0165 0988 1020 1028 1052 1184 1214

1261 1288

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

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@A330

SERVICE BULLETIN

OPERATOR MSN

GRL 0230

HAL 1104 1114 1171 1217 1259 1295 1302

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

0479 0512 0581 0669 0673

HFY 0096 0127 0211 0262 1008

HVN 0275 0294 0299 0366 0943 0946 0962 1019 1256 1266

I2L 0527 0532 0725

ISS 0802

IYE 0625 0632

JAI 0923 0947 0956

JST 0506 0513 0522 0842 0853 0940 0945 1198 1251

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

0351 0368 0428 0484 0490 0550 1133 1155 1200 1203

KLM 0682 0686 0703 0738 0770 0801 0811 0819 0834 0900 1161 1287

1294 1300

MAS 0067 0116 0119 1209 1219 1229 1234 1243 1281

MAU 0883 1057

MEA 0926 0984 0995 0998

MON 0261 0265

MSR 0600 0610 0666 0683 0696 0709 0726 1143 1230 1238 1246

OHY 0072 0087 0098 0143

OMA 1038 1044 1049 1063 1093 1120 1227

PAL 0183 0184 0188 0189 0191 0198 0200 0203

QAF 0487 0605

QFA 0508 0553 0558 0564 0574 0593 0595 0603 0695 0705 0712 0887

0892 0898 0976 1061 1094 1169 1174 1258

QTR 0441 0473 0489 0511 0521 0571 0612 0616 0623 0637 0638 0659

0680 0684 0711 0721 0734 0743 0746 0760 0789 0792 0813 0820

0826 0849 0893 0907 0918

RJA 0970 0979 1002

RSF 0980 0996 1235

RSY 0120 0171

SAA 1191 1210 1223 1236 1249 1271

SAI 0055 0070 0086

SAS 0496 0497 0515 0568

SIA 0978 0983 0986 0997 1006 1010 1012 1015 1085 1098 1099 1105

1107 1124 1132 1146 1149 1156 1157

SVA 1108 1127 1137 1141 1147 1153 1189 1192

SWR 1000 1018 1026 1029 1084 1089 1101 1145 1181 1188 1276 1290

SYA 0345

TAE 0348

TAM 0232 0238 0247 0259 0361 0466 0472 0477 0486 0700 0876 0949

0961 0968 0977 1112 1118 1213 1221

TAP 0181 0195 0223 0305 0308 0312 0317 0877 0899 0904 0914 0934

TCX 0254 0266 0301 0398

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

0990 1003 1035 1037 1060 1074 1086 1090 1263 1269 1289

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@A330

SERVICE BULLETIN

OPERATOR MSN

THY 0463 0504 0529 0697 0704 0742 0754 0774 0869 0882 0901 0932

1150 1160 1170 1172 1204 1212 1228 1240 1298

TOW 1033 1046 1248 1275

TSC 0111 0132 0177 0250 0271 0369 0407 0427 0480 0795 0966 0971

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

0396 0409 0452 0455 0491 0509 0518 0525 0536

UAF 1080 1186 1250

USA 0315 0323 0333 0337 0342 0370 0375 0380 0388 1011 1022 1041

1069 1076 1095 1100

VIR 1195 1201 1206 1215 1231 1296

VKG 0309 0349 0356 0357

VOZ 0365 0372 1293

WRC 0296

XAX 0054 0330 0654 0662 0692 0716 0741 0786 0952 0974 1048 1066

1075 1126 1131 1165

XLF 0501 0635

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SERVICE BULLETIN

(4) Configuration by MSN

MSN CONFIGURATION

0012 0017 0030 0037 0045 0050 0054 0055 0060 0062 0064

0065 0066 0067 0070 0071 0072 0082 0083 0086 0087 0095

0096 0098 0099 0102 0106 0109 0111 0112 0113 0116 0118

0119 0120 0121 0122 0127 0132 0138 0140 0143 0144 0148

0153 0155 0162 0165 0171 0172 0177 0181 0183 0184 0188

0189 0191 0195 0198 0200 0203 0205 0206 0209 0211 0219

0222 0223 0224 0226 0229 0230 0231 0232 0234 0238 0240

0241 0244 0247 0248 0249 0250 0251 0253 0254 0255 0256

0258 0259 0261 0262 0265 0266 0267 0269 0271 0272 0275

0276 0277 0279 0281 0283 0284 0285 0286 0287 0288 0290

0291 0293 0294 0295 0296 0299 0300 0301 0303 0305 0306

0308 0309 0311 0312 0313 0314 0315 0316 0317 0320 0322

0323 0324 0326 0328 0330 0333 0334 0337 0338 0339 0340

0342 0343 0344 0345 0346 0348 0349 0350 0351 0353 0356

0357 0358 0361 0362 0364 0365 0366 0368 0369 0370 0372

0375 0380 0382 0384 0386 0388 0389 0392 0393 0396 0397

0400 0403 0405 0407 0408 0409 0412 0418 0419 0420 0421

0422 0423 0425 0427 0428 0432 0437 0439 0441 0443 0444

0448 0451 0452 0454 0456 0458 0461 0462 0463 0465 0466

0469 0472 0473 0476 0477 0479 0480 0481 0484 0486 0487

0489 0490 0491 0493 0494 0496 0497 0498 0500 0501 0502

0503 0504 0505 0506 0507 0508 0509 0510 0511 0512 0513

0515 0516 0518 0519 0521 0522 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

0751 0755 0807 0825 0831 0863 0882 0885 0888 0901 0923

0932 0947 0952 0956 0974 1048 1053 1066 1075 1108 1126

1127 1131 1133 1137 1141 1147 1153 1155 1165 1189 1191

1192 1195 1200 1201 1203 1206 1209 1210 1215 1219 1223

1229 1231 1234 1236 1240 1243 1249 1271 1281 1296

001

0398 0401 0404 0455 002

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SERVICE BULLETIN

MSN CONFIGURATION

0733 0734 0735 0737 0738 0739 0741 0742 0743 0745 0746

0747 0749 0750 0752 0754 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 0809 0810 0811 0813 0814 0815 0817 0818

0819 0820 0821 0822 0823 0824 0826 0827 0828 0830 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 0865 0866 0867 0868 0869 0871 0873 0874 0875

0876 0877 0879 0881 0883 0884 0887 0889 0890 0891 0892

0893 0895 0896 0898 0899 0900 0903 0904 0905 0906 0907

0908 0909 0911 0913 0914 0915 0916 0918 0919 0920 0922

0926 0927 0928 0930 0931 0934 0935 0936 0937 0939 0940

0941 0942 0943 0944 0945 0946 0948 0949 0950 0951 0954

0957 0958 0959 0961 0962 0963 0964 0965 0966 0967 0968

0969 0970 0971 0973 0975 0976 0977 0978 0979 0980 0982

0983 0984 0985 0986 0988 0989 0990 0991 0992 0994 0995

0996 0997 0998 0999 1000 1001 1002 1003 1006 1007 1008

1009 1010 1011 1012 1013 1014 1015 1016 1018 1019 1020

1021 1022 1023 1025 1026 1028 1029 1031 1033 1034 1035

1036 1037 1038 1039 1041 1042 1043 1044 1045 1046 1047

1049 1052 1054 1055 1057 1058 1059 1060 1061 1063 1065

1067 1069 1071 1072 1073 1074 1076 1077 1078 1080 1081

1082 1084 1085 1086 1087 1088 1089 1090 1093 1094 1095

1096 1097 1098 1099 1100 1101 1103 1104 1105 1106 1107

1110 1112 1114 1116 1118 1120 1123 1124 1129 1130 1132

1135 1138 1143 1145 1146 1149 1150 1151 1156 1157 1159

1160 1161 1163 1167 1168 1169 1170 1171 1172 1173 1174

1177 1178 1181 1183 1184 1186 1187 1188 1190 1193 1196

1198 1199 1202 1204 1205 1208 1211 1212 1213 1214 1216

1217 1218 1220 1221 1222 1224 1225 1226 1227 1228 1230

1232 1233 1235 1237 1238 1239 1241 1244 1245 1246 1247

1248 1250 1251 1252 1254 1255 1256 1258 1259 1260 1261

1262 1263 1264 1265 1266 1267 1268 1269 1270 1272 1274

1275 1276 1277 1278 1279 1280 1282 1283 1284 1285 1286

1287 1288 1289 1290 1291 1292 1293 1294 1295 1297 1298

1299 1300 1301 1302 1303 1304

003

(5) Configuration definition

**CONF 001

Conf. 001 is valid for all aircraft which have not embodied Modification No. 48133 ,

53630 and 54779 and all aircraft which have not embodied Modification No. 48133 but

have embodied Modification No. 54779 which cancels the embodiment of Modification

No. 53630.

**CONF 002

Conf. 002 is valid for all aircraft which have embodied Modification No. 48133 but have

not embodied Modification No. 53630 and 54779.

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

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@A330

SERVICE BULLETIN

**CONF 003

Conf. 003 is valid for all aircraft which have embodied Modification No. 53630 but have

not embodied Modification No. 48133 and 54779.

The following table gives further information of the configuration description

MOD Config. 001 Config. 002 Config. 003

48133 - - x -

53630 - x - x

54779 - x - -

Configuration/Modification/Service Bulletin Cross Reference Chart

(6) Material Effectivity

**CONF 001

MATERIAL QTY PER A/C SEE NOTES

Kit 523086D01R03 1

Component COMPD04 As required (1)

Reidentified part set REIDD05 1

Reidentified part set REIDD07 As required (2)

Consumable CMLD10 As required

NOTE (1): The matset Comp 523086D04 is applicable only for operators which

have already matset Kit 523086D01R02, Kit 523086D02R02 or Kit

523086D03R02 on stock or which have already accomplished this

Service Bulletin at the original issue and have to do the additional work.

NOTE (2): The part set Reid 523086D07 is to be used only for operators which

have already matset Kit 523086D01R02 on stock or which have already

accomplished this Service Bulletin at the original issue and have to do

the additional work.

**CONF 002

MATERIAL QTY PER A/C SEE NOTES

Kit 523086D02R05 1

Component COMPD04 As required (1)

Reidentified part set REIDD05 1

Reidentified part set REIDD08 As required (2)

Consumable CMLD10 As required

NOTE (1): The matset Comp 523086D04 is applicable only for operators which

have already matset Kit 523086D01R02, Kit 523086D02R02 or Kit

523086D03R02 on stock or which have already accomplished this

Service Bulletin at the original issue and have to do the additional work.

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

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SERVICE BULLETIN

NOTE (2): The part set Reid 523086D08 is to be used only for operators which

have already matset Kit 523086D02R02 on stock or which have already

accomplished this Service Bulletin at the original issue and have to do

the additional work.

**CONF 003

MATERIAL QTY PER A/C SEE NOTES

Kit 523086D03R04 1

Component COMPD04 As required (1)

Reidentified part set REIDD06 1

Reidentified part set REIDD09 As required (2)

Consumable CMLD10 As required

NOTE (1): The matset Comp 523086D04 is applicable only for operators which

have already matset Kit 523086D01R02, Kit 523086D02R02 or Kit

523086D03R02 on stock or which have already accomplished this

Service Bulletin at the original issue and have to do the additional work.

NOTE (2): The part set Reid 523086D09 is to be used only for operators which

have already matset Kit 523086D03R02 on stock or which have already

accomplished this Service Bulletin at the original issue and have to do

the additional work.

**CONF ALL

B. CONCURRENT REQUIREMENTS

None

C. REASON

(1) History

Several cases have been reported in which the potable water service panel access door

164AR has been lost during flight. In one case, on an A340 aircraft the THS leading

edge has been hit, in a second case, on an A330 aircraft the door was presumed to

have caused damage to the THS.

Investigations have shown difficulties with the latching mechanism of the potable water

service panel access door, which can lead to a potential unsafe condition. The potential

unsafe condition could cause possible injury to persons and damage to property on

ground and potential loss of the potable water service panel access door on runway.

The Inspection Service Bulletin A330-52-3077 was issued to inspect the access door

164AR, 154AR and 171AL. The Modification Service Bulletin A330-52-3076 was issued

as the final repair solution to the Inspection Service Bulletin A330-52-3077. Further

occurrences of access door 164AR lost during flight have shown that the Modification

Service Bulletin A330-52-3076 is not the definitive final repair solution for this access

door. Therefore, this mandatory Modification Service Bulletin, A330-52-3086, is issued

as the final repair solution for the access door 164AR. The loss of this door is classified

to be a potential unsafe condition.

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

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SERVICE BULLETIN

To avoid further occurrences the design of the latching mechanism of the potable water

service panel access door has to be modified to mitigate the risk.

(2) Objective/Action

This Service Bulletin mandates the operator to install a modified potable water service

panel access door with reinforced hinge screws and more robust latches, including an

additional third latch.

(3) Advantages

After accomplishment of this Service Bulletin the handling and reliability of the potable

water service panel access door is improved.

This Service Bulletin meets the safety intent by making sure that the potable water

service panel access door can be correctly latched.

(4) Operational/Maintenance Consequences

None

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

**CONF 001

Task 523086-831-848-001: Modification

(1) Modify the potable water service panel access door PN F5348614401200

(2) Remove the potable water service panel access door

(3) Remove the fittings and the anchor nuts

(4) Install the new anchor nuts

(5) Install the new hinges

(6) Install the potable water service panel access door PN F5348614401800

(7) Install the new fittings

(8) Install the bonding lead

(9) Reidentify the potable water service panel

(10) Adjust the new potable water service panel access door

(11) Restore the aircraft surface protection

(12) Install the placard

Task 523086-831-849-001: Modification - ADDITIONAL WORK for aircraft modified by the

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SERVICE BULLETIN

original issue

(1) Modify the potable water service panel access door PN F5348614401200

(2) Apply sealant to the modified areas

**CONF 002

Task 523086-831-848-001: Modification

(1) Modify the potable water service panel access door PN F5348614401400

(2) Remove the potable water service panel access door

(3) Remove the fittings and the anchor nuts

(4) Install the new anchor nuts

(5) Install the new hinges

(6) Install the potable water service panel access door PN F5348614402000

(7) Install the new fittings

(8) Install the bonding lead

(9) Reidentify the potable water service panel

(10) Adjust the new potable water service panel access door

(11) Restore the aircraft surface protection

(12) Install the placard

Task 523086-831-849-001: Modification - ADDITIONAL WORK for aircraft modified by the

original issue

(1) Modify the potable water service panel access door PN F5348614401400

(2) Apply sealant to the modified areas

**CONF 003

Task 523086-831-848-001: Modification

(1) Modify the potable water service panel access door PN F5348614401000

(2) Remove the potable water service panel access door

(3) Remove the fittings and the anchor nuts

(4) Install the new anchor nuts

(5) Install the new hinges

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SERVICE BULLETIN

(6) Install the potable water service panel access door PN F5348614401600

(7) Install the new fittings

(8) Install the bonding lead

(9) Reidentify the potable water service panel

(10) Adjust the new potable water service panel access door

(11) Restore the aircraft surface protection

(12) Install the placard

Task 523086-831-849-001: Modification - ADDITIONAL WORK for aircraft modified by the

original issue

(1) Modify the potable water service panel access door PN F5348614401000

(2) Apply sealant to the modified areas

**CONF ALL

E. COMPLIANCE

(1) Classification

MANDATORY: Service Bulletin must be accomplished.

(2) Accomplishment Timescale

This Service Bulletin must be accomplished within 48 months after original issue date of

this Service Bulletin.

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

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

to confirm this classification. It is anticipated that the AD will confirm the threshold

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

accomplishment timescale.

If original issue has been implemented on aircraft, it is recommended to perform the

additional work within 24 months from the issue date of this Service Bulletin revision 01.

F. APPROVAL

The technical content of this document is approved under the authority of Design

Organisation Approval No. EASA.21J.031.

If an aircraft listed in the effectivity has a modification or repair embodied that is not of

AIRBUS origin, and which affects the content of this Service Bulletin, the operator is

responsible for obtaining approval by its airworthiness authority for any adaptation necessary

before incorporation of the Service Bulletin.

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

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@A330

SERVICE BULLETIN

G. MANPOWER

The manpower estimates given in this Service Bulletin are based on the direct labor cost to

do the work. These estimates assume that the work will be done by experienced personnel,

and may need to be revised upwards to suit operator’s circumstances. The estimates do not

include the time to prepare, plan or inspect the work. Manufacture and procurement of parts

and tools, drying times for paints, sealants, etc., and general administration work are also not

included.

**CONF 001

Task 523086-831-848-001: Modification

Get Access 2.50

On Aircraft

Remove the potable water service panel access door 0.50

Remove the fittings and the anchor nuts 0.50

Install the new anchor nuts 1.00

Install the new hinges 0.50

Install the potable water service panel access door PN

F5348614401800

0.50

Install the new fittings 2.00

Install the bonding lead 0.25

Reidentify the potable water service panel 0.25

Adjust the new potable water service panel access

door

0.75

Restore the aircraft surface protection 0.50

Install the placard 0.25

On Bench

Modify the potable water service panel access door PN

F5348614401200

0.25

Tests 1.25

Close-Up 2.50

TOTAL MANHOURS 13.50

ELAPSED TIME (HOURS) 12.00

Task 523086-831-849-001: Modification - ADDITIONAL WORK for aircraft modified by the

original issue

Get Access 2.50

On Aircraft

Modify the potable water service panel access door PN

F5348614401200

0.25

Apply sealant to the modified areas 1.00

Tests 1.25

Close-Up 2.50

TOTAL MANHOURS 7.50

ELAPSED TIME (HOURS) 7.50

NOTE: For a breakdown of the manhours and elapsed time, refer to the Gantt Chart,

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 13

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SERVICE BULLETIN

Fig. A-GGAAA, given in Appendix 01 - Elapsed Time Assumption .

**CONF 002

Task 523086-831-848-001: Modification

Get Access 2.50

On Aircraft

Remove the potable water service panel access door 0.50

Remove the fittings and the anchor nuts 0.50

Install the new anchor nuts 1.00

Install the new hinges 0.50

Install the potable water service panel access door PN

F5348614402000

0.50

Install the new fittings 2.00

Install the bonding lead 0.25

Reidentify the potable water service panel 0.25

Adjust the new potable water service panel access

door

0.75

Restore the aircraft surface protection 0.50

Install the placard 0.25

On Bench

Modify the potable water service panel access door PN

F5348614401400

0.25

Tests 1.25

Close-Up 2.50

TOTAL MANHOURS 13.50

ELAPSED TIME (HOURS) 12.00

Task 523086-831-849-001: Modification - ADDITIONAL WORK for aircraft modified by the

original issue

Get Access 2.50

On Aircraft

Modify the potable water service panel access door PN

F5348614401400

0.25

Apply sealant to the modified areas 1.00

Tests 1.25

Close-Up 2.50

TOTAL MANHOURS 7.50

ELAPSED TIME (HOURS) 7.50

NOTE: For a breakdown of the manhours and elapsed time, refer to the Gantt Chart,

Fig. A-GGAAA, given in Appendix 01 - Elapsed Time Assumption .

**CONF 003

Task 523086-831-848-001: Modification

Get Access 2.50

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 14

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@A330

SERVICE BULLETIN

Task 523086-831-848-001: Modification

On Aircraft

Remove the potable water service panel access door 0.50

Remove the fittings and the anchor nuts 0.50

Install the new anchor nuts 1.00

Install the new hinges 0.50

Install the potable water service panel access door PN

F5348614401600

0.50

Install the new fittings 2.00

Install the bonding lead 0.25

Reidentify the potable water service panel 0.25

Adjust the new potable water service panel access

door

0.75

Restore the aircraft surface protection 0.50

Install the placard 0.25

On Bench

Modify the potable water service panel access door PN

F5348614401000

0.25

Tests 1.25

Close-Up 2.50

TOTAL MANHOURS 13.50

ELAPSED TIME (HOURS) 12.00

Task 523086-831-849-001: Modification - ADDITIONAL WORK for aircraft modified by the

original issue

Get Access 2.50

On Aircraft

Modify the potable water service panel access door PN

F5348614401000

0.25

Apply sealant to the modified areas 1.00

Tests 1.25

Close-Up 2.50

TOTAL MANHOURS 7.50

ELAPSED TIME (HOURS) 7.50

NOTE: For a breakdown of the manhours and elapsed time, refer to the Gantt Chart,

Fig. A-GGAAA, given in Appendix 01 - Elapsed Time Assumption .

**CONF ALL

H. WEIGHT AND BALANCE

The weight and balance estimates given in this Service Bulletin are based on the

Manufacturer’s Empty Weight (MEW) and do not include operator’s items. For the definition of

(MEW) and operator’s items, refer to Weight and Balance Manual (WBM) Chapter 1-00-07.

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 15

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@A330

SERVICE BULLETIN

**CONF 001

A330-200 A330-300

Manufacturers Empty Weight +0.532 KG +1.173 LB +0.532 KG +1.173 LB

Effect on Balance +26.175 KGM +189.389

LBF.FT +29.010 KGM +209.901LBF.FT

**CONF 002

A330-200

Manufacturers Empty Weight +0.719 KG +1.585 LB

Effect on Balance +35.369 KGM +255.912 LBF.FT

**CONF 003

A330-200 A330-300

Manufacturers Empty Weight +0.744 KG +1.640 LB +0.744 KG +1.640 LB

Effect on Balance +36.599 KGM +257.576

LBF.FT +40.563 KGM +293.493LBF.FT

**CONF ALL

I. ELECTRICAL LOAD DATA

Not Changed

J. REFERENCES

**CONF 001

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

06-41-52 06-41-53 11-00-00

12-34-24 20-11-00 20-28-00

24-41-00 38-10-00 53-00-00

Consumable Material List (CML)

ATA Common Support Data Dictionary (CSDD),

Chapter 2

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

Standards Manual (SM)

Structural Repair Manual (SRM) 51-23-00 51-24-00 51-40-00

51-42-00 51-43-00 51-44-00

51-46-00 51-75-12

Weight and Balance Manual (WBM) Chapter 1-00-07

**CONF 002

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

06-41-52 06-41-53 11-00-00

12-34-24 20-11-00 20-28-00

24-41-00 38-10-00 53-00-00

Consumable Material List (CML)

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 16

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SERVICE BULLETIN

ATA Common Support Data Dictionary (CSDD),

Chapter 2

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

Standards Manual (SM)

Structural Repair Manual (SRM) 51-23-00 51-24-00 51-40-00

51-42-00 51-43-00 51-44-00

51-46-00 51-75-12

Weight and Balance Manual (WBM) Chapter 1-00-07

**CONF 003

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

06-41-52 06-41-53 11-00-00

12-34-24 20-11-00 20-28-00

24-41-00 38-10-00 53-00-00

Consumable Material List (CML)

ATA Common Support Data Dictionary (CSDD),

Chapter 2

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

Standards Manual (SM)

Structural Repair Manual (SRM) 51-23-00 51-24-00 51-40-00

51-42-00 51-43-00 51-44-00

51-46-00 51-75-12

Weight and Balance Manual (WBM) Chapter 1-00-07

**CONF ALL

K. PUBLICATION AFFECTED

Aircraft Maintenance Manual (AMM) 52-42-13

Illustrated Parts Catalog (IPC) 11-21-38 52-42-04

Maintenance Planning Document (MPD) 524000-02-1

Structural Repair Manual (SRM) 52-42-11

L. INTERCHANGEABILITY/MIXABILITY

**CONF 001

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE

NOTES

Door Assy F5348614400600 F5348614401800 03 Not

Applicable

Panel F5348612320400 F5348633920000 03 Not

Applicable

Door Assy F5348614401200 F5348614401800 03 Not

Applicable

NOTE: For definitions of interchangeability codes in column INT., refer to ATA

Common Support Data Dictionary (CSDD), Chapter 2.

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 17

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SERVICE BULLETIN

**CONF 002

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE

NOTES

Door Assy F5348614400400 F5348614402000 03 Not

Applicable

Panel F5348612320400 F5348633920000 03 Not

Applicable

Door Assy F5348614401400 F5348614402000 03 Not

Applicable

NOTE: For definitions of interchangeability codes in column INT., refer to ATA

Common Support Data Dictionary (CSDD), Chapter 2.

**CONF 003

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE

NOTES

Door Assy F5348614400800 F5348614401600 03 Not

Applicable

Panel F5348612320400 F5348634020000 03 Not

Applicable

Door Assy F5348614401000 F5348614401600 03 Not

Applicable

NOTE: For definitions of interchangeability codes in column INT., refer to ATA

Common Support Data Dictionary (CSDD), Chapter 2.

**CONF ALL

M. SPARES

None

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 18

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@A330

SERVICE BULLETIN

2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

(1) Procurement Addresses

Kit 523086D01R03

Kit 523086D02R05

Kit 523086D03R04

Customers with aircraft shown in the

effectivity of this Service Bulletin should send

a purchase order to AIRBUS. Quote the

number of this Service Bulletin. The address

is:

AIRBUS Material, Logistics and Suppliers

Weg beim Jaeger 150

D-22335 Hamburg

Germany

For ordering by internet:

http://spares.airbus.com

For ordering by fax: +49 40 50 76 25 90

For ordering by E-mail: airbus.kit@airbus.com

Customers with aircraft shown in the effectivity of this Service Bulletin should send a

purchase order to AIRBUS. Quote the number of this Service Bulletin. The address is:

Component COMPD04 AIRBUS Material, Logistics and Suppliers

IFD - In Flight Desk

Weg beim Jaeger 150

D-22335 Hamburg

Germany

For ordering by internet:

http://spares.airbus.com

For ordering by fax: +49 40 50 76 40 12

For ordering by E-mail:

ifd.spares@airbus.com

(2) Price and Availability

Kit 523086D01R03

Cost 15,280.00 USD

Availability 120 calendar days from receipt of order

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

order. If items are required before this time, please include a retrofit planning schedule

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

(costs and availability) are estimated in relation to economic conditions. The latest valid

price and lead time for ordering purposes shall be obtained through the AirbusSpares

Portal or through a request for quotation to airbus.kit@airbus.com.

Kit 523086D02R05

Cost 15,280.00 USD

Availability 120 calendar days from receipt of order

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 19

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@A330

SERVICE BULLETIN

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

order. If items are required before this time, please include a retrofit planning schedule

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

(costs and availability) are estimated in relation to economic conditions. The latest valid

price and lead time for ordering purposes shall be obtained through the AirbusSpares

Portal or through a request for quotation to airbus.kit@airbus.com.

Kit 523086D03R04

Cost 15,280.00 USD

Availability 120 calendar days from receipt of order

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

order. If items are required before this time, please include a retrofit planning schedule

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

(costs and availability) are estimated in relation to economic conditions. The latest valid

price and lead time for ordering purposes shall be obtained through the AirbusSpares

Portal or through a request for quotation to airbus.kit@airbus.com.

Component COMPD04

Operator supplied AIRBUS parts required to accomplish this Service Bulletin are to be

purchased by a spares purchase order.

B. INDUSTRY SUPPORT INFORMATION

As a special policy applied to this Service Bulletin, AIRBUS will provide a 45% reduction to

the applicable kits sales prices given in the paragraph Price and Availability for orders placed

before end of Jun 30/16.

C. LIST OF COMPONENTS

Kit 523086D01R03

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

NOTES

2 F5348614401800 1 DOOR (2) F5348614400600 03

8 NAS1100-3-7 1 SCREW

12 NAS1291C3M 9 NUT

14 NAS1149C0332R 10 WASHER

16 NAS1102E3-8 8 SCREW

20 NAS1801-4-9 4 SCREW

22 NAS1149C0432R 4 WASHER

24 F5348615700600 2 HINGE

26 F5348615520400 2 SPRING

28 F5348615620400 4 SHIM (1)

30 NSA5075-5 9 COLLAR

32 DAN6-5-4 9 PIN

34 F5348614120200 2 FITTING

35 F5348614120400 1 FITTING

50 NSA5414N24-10 16 RIVET

52 NAS1474R4K 4 NUT

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 20

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@A330

SERVICE BULLETIN

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

NOTES

54 F5348615620600 2 SHIM

60 F1121009420000 1 PLACARD

NOTE: For definitions of interchangeability codes in column INT., refer to ATA

Common Support Data Dictionary (CSDD), Chapter 2.

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

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

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

to part number relationship.

NOTE (1): A maximum of 4 shims necessary only if the hinges have to be adjusted.

Kit 523086D02R05

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

NOTES

2 F5348614402000 1 DOOR (2) F5348614400400 03

8 NAS1100-3-7 1 SCREW

12 NAS1291C3M 9 NUT

14 NAS1149C0332R 10 WASHER

16 NAS1102E3-8 8 SCREW

20 NAS1801-4-9 4 SCREW

22 NAS1149C0432R 4 WASHER

24 F5348615700600 2 HINGE

26 F5348615520400 2 SPRING

28 F5348615620400 4 SHIM (1)

30 NSA5075-5 9 COLLAR

32 DAN6-5-4 9 PIN

34 F5348614120200 2 FITTING

35 F5348614120400 1 FITTING

50 NSA5414N24-10 16 RIVET

52 NAS1474R4K 4 NUT

54 F5348615620600 2 SHIM

60 F1121009420000 1 PLACARD

NOTE: For definitions of interchangeability codes in column INT., refer to ATA

Common Support Data Dictionary (CSDD), Chapter 2.

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

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

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

to part number relationship.

NOTE (1): A maximum of 4 shims necessary only if the hinges have to be adjusted.

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 21

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SERVICE BULLETIN

Kit 523086D03R04

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

NOTES

2 F5348614401600 1 DOOR (2) F5348614400800 03

8 NAS1100-3-7 1 SCREW

12 NAS1291C3M 9 NUT

14 NAS1149C0332R 10 WASHER

16 NAS1102E3-8 8 SCREW

20 NAS1801-4-9 4 SCREW

22 NAS1149C0432R 4 WASHER

24 F5348615700600 2 HINGE

26 F5348615520400 2 SPRING

28 F5348615620400 4 SHIM (1)

30 NSA5075-5 9 COLLAR

32 DAN6-5-4 9 PIN

34 F5348614120200 2 FITTING

35 F5348614120400 1 FITTING

50 NSA5414N24-10 16 RIVET

52 NAS1474R4K 4 NUT

54 F5348615620600 2 SHIM

60 F1121009420000 1 PLACARD

NOTE: For definitions of interchangeability codes in column INT., refer to ATA

Common Support Data Dictionary (CSDD), Chapter 2.

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

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

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

to part number relationship.

NOTE (1): A maximum of 4 shims necessary only if the hinges have to be adjusted.

D. LIST OF MATERIALS - OPERATOR SUPPLIED

(1) Consumable Materials

Consumable CMLD10

ITEM DESCRIPTION REFERENCE TO CML

MAT. No.

QTY PER A/C SEE

NOTES

Top Coat Polyurethane - External

Structure

04JAA3 As required

Coating - Flexible Structure 04QAB2 As required

Varnish Polyurethane-Low Voc -

External Structure

04SBA3 As required

Varnish - Electrical Bonding

Structure

04TMB2 As required

Threadlocking Adhesive - Medium

Strength

05BAE1 As required

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 22

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@A330

SERVICE BULLETIN

ITEM DESCRIPTION REFERENCE TO CML

MAT. No.

QTY PER A/C SEE

NOTES

Polysulfide Sealant-General

Purpose Brushable

06AAA1 As required

Polysulfide Sealant-General

Purpose Fillet

06AAB1 As required

Aqueous Cleaner-Aircraft Exterior

Pressure Spray

08ABC1 As required

Non Aqueous Cleaner-General 08BAA9 As required

Corrosion Preventive CompoundWater Displacing Oil12ABE2 As required

Release Agent - Liquid Wax 14DBB1 As required

Wire-Locking Dia: 0.5 Mm (0.020

Inch) Cres Nickel

14QDB1 As required

Textile-Lint Free Cotton 14SBA1 As required

(2) Components

Component COMPD04

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

NOTES

6 A9249715920200 1 STUD

NOTE: The matset Comp 523086D04 is applicable only for operators which

have already matset Kit 523086D01R02, Kit 523086D02R02 or Kit

523086D03R02 on stock or which have already accomplished this

Service Bulletin at the original issue and have to do the additional work.

NOTE: The above list of components is not an AIRBUS Kit, the required parts

shall be ordered as necessary through the given channel.

(3) Equipment

None

E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

Reidentified part set REIDD05

ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE

NOTES

F5348633920000 PANEL F5348612320400

Reidentified part set REIDD06

ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE

NOTES

F5348634020000 PANEL F5348612320400

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 23

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SERVICE BULLETIN

Reidentified part set REIDD07

ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE

NOTES

F5348614401800 DOOR F5348614401200

NOTE: The part set Reid 523086D07 is to be used only for operators which

have already matset Kit 523086D01R02 on stock or which have already

accomplished this Service Bulletin at the original issue and have to do the

additional work.

Reidentified part set REIDD08

ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE

NOTES

F5348614402000 DOOR F5348614401400

NOTE: The part set Reid 523086D08 is to be used only for operators which

have already matset Kit 523086D02R02 on stock or which have already

accomplished this Service Bulletin at the original issue and have to do the

additional work.

Reidentified part set REIDD09

ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE

NOTES

F5348614401600 DOOR F5348614401000

NOTE: The part set Reid 523086D09 is to be used only for operators which

have already matset Kit 523086D03R02 on stock or which have already

accomplished this Service Bulletin at the original issue and have to do the

additional work.

F. TOOLING

None

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 24

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SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS

Task 523086-831-848-001 - Modification

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

INCLUDED IN THE REFERENCED PROCEDURES.

CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP

ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY

AND MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENANCE

WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING,

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

THIS:

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

NECESSARY ON WIRING AND COMPONENTS.

REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND OTHER

CONTAMINATION.

THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION

AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION.

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

NOTE: The accomplishment instructions of this Service Bulletin refer to procedures

included in other AIRBUS documents. When the words ’refer to’ are used and the

operator has an accepted alternative procedure, the accepted alternative procedure

can be used. When the words ’in accordance with’ are included in the instruction,

the procedure in the AIRBUS document must be used.

NOTE: The access and close-up instructions, not comprising return to service tests, in this

Service Bulletin do not constitute or affect the technical intent of the Service

Bulletin. Operators can therefore, as deemed necessary, omit or add access and/or

close-up steps to add flexibility to their maintenance operations as long as the

technical intent of the Service Bulletin is met within the set parameters.

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

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

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

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

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

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

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

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

the aircraft can be put back into a serviceable condition.

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 25

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SERVICE BULLETIN

Task Associated Data

**CONF 001

Zone

160

Manpower

TOTAL MANHOURS 13.50

ELAPSED TIME (HOURS) 12.00

**CONF 002

Zone

160

Manpower

TOTAL MANHOURS 13.50

ELAPSED TIME (HOURS) 12.00

**CONF 003

Zone

160

Manpower

TOTAL MANHOURS 13.50

ELAPSED TIME (HOURS) 12.00

**CONF ALL

A. GENERAL

**CONF 001

(1) Subtask 523086-910-201-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

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

06-30-00, Page Block 001

06-31-53, Page Block 001

06-41-52, Page Block 001

06-41-53, Page Block 001

11-00-00, Page Block 201

Task 20-11-00-911-801

Consumable Material List (CML)

Standards Manual (SM)

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 26

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SERVICE BULLETIN

References

Structural Repair Manual (SRM) 51-23-00

51-24-00

51-40-00

51-42-00

51-43-00

51-44-00

51-46-00

(a) For the specification of the materials (Mat. No.) given in this Service Bulletin, refer

to the Consumable Materials List (CML).

(b) Refer to the AIRBUS Standards Manual (SM) if you find part numbers for the

hardware components in the related kit(s) which you cannot identify in the LIST OF

COMPONENTS of this Service Bulletin. The SM will give you the correct part

number to part number relationship.

(c) For the identification of zones, refer to AMM 06-20-00, Page Block 001.

(d) For the Frame (FR) identification, refer to AMM 06-31-53, Page Block 001.

(e) For the location of the stringers (STGR), refer to AMM 06-30-00, Page Block 001.

(f) For the identification of access doors and panels, refer to AMM 06-41-52, Page

Block 001 and AMM 06-41-53, Page Block 001.

(g) Apply sealant in accordance with SRM 51-24-00.

(h) Renew the protective finish in accordance with SRM 51-23-00.

(i) Remove and install fasteners in accordance with SRM 51-42-00.

(j) Obtain alternative and substitute fastener data in accordance with SRM 51-43-00.

(k) If the length of any fastener specified in this Service Bulletin does not meet

installation standards given in SRM Chapter 51, then a fastener of the same

specification, or an approved substitute, with a length which meets the installation

standards given in SRM Chapter 51 may be used. In addition, washers may be

installed for fastener grip length in accordance with SRM Chapter 51.

(l) If alternative and substitute fasteners have to be used, you must make sure that the

associated nut/collar are compatible in accordance with SRM 51-40-00.

(m) Obtain fastener hole diameters and drill data in accordance with SRM 51-44-00.

(n) Obtain countersink data in accordance with SRM 51-46-00.

(o) For installation of lockwire, refer to AMM Task 20-11-00-911-801.

(p) For the installation of placards, refer to AMM 11-00-00, Page Block 201.

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 27

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SERVICE BULLETIN

(2) Subtask 523086-839-201-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF 002

(1) Subtask 523086-910-201-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

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

06-30-00, Page Block 001

06-31-53, Page Block 001

06-41-52, Page Block 001

06-41-53, Page Block 001

11-00-00, Page Block 201

Task 20-11-00-911-801

Consumable Material List (CML)

Standards Manual (SM)

Structural Repair Manual (SRM) 51-23-00

51-24-00

51-40-00

51-42-00

51-43-00

51-44-00

51-46-00

(a) For the specification of the materials (Mat. No.) given in this Service Bulletin, refer

to the Consumable Materials List (CML).

(b) Refer to the AIRBUS Standards Manual (SM) if you find part numbers for the

hardware components in the related kit(s) which you cannot identify in the LIST OF

COMPONENTS of this Service Bulletin. The SM will give you the correct part

number to part number relationship.

(c) For the identification of zones, refer to AMM 06-20-00, Page Block 001.

(d) For the Frame (FR) identification, refer to AMM 06-31-53, Page Block 001.

(e) For the location of the stringers (STGR), refer to AMM 06-30-00, Page Block 001.

(f) For the identification of access doors and panels, refer to AMM 06-41-52, Page

Block 001 and AMM 06-41-53, Page Block 001.

(g) Apply sealant in accordance with SRM 51-24-00.

(h) Renew the protective finish in accordance with SRM 51-23-00.

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 28

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@A330

SERVICE BULLETIN

(i) Remove and install fasteners in accordance with SRM 51-42-00.

(j) Obtain alternative and substitute fastener data in accordance with SRM 51-43-00.

(k) If the length of any fastener specified in this Service Bulletin does not meet

installation standards given in SRM Chapter 51, then a fastener of the same

specification, or an approved substitute, with a length which meets the installation

standards given in SRM Chapter 51 may be used. In addition, washers may be

installed for fastener grip length in accordance with SRM Chapter 51.

(l) If alternative and substitute fasteners have to be used, you must make sure that the

associated nut/collar are compatible in accordance with SRM 51-40-00.

(m) Obtain fastener hole diameters and drill data in accordance with SRM 51-44-00.

(n) Obtain countersink data in accordance with SRM 51-46-00.

(o) For installation of lockwire, refer to AMM Task 20-11-00-911-801.

(p) For the installation of placards, refer to AMM 11-00-00, Page Block 201.

(2) Subtask 523086-839-201-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF 003

(1) Subtask 523086-910-201-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

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

06-30-00, Page Block 001

06-31-53, Page Block 001

06-41-52, Page Block 001

06-41-53, Page Block 001

11-00-00, Page Block 201

Task 20-11-00-911-801

Consumable Material List (CML)

Standards Manual (SM)

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 29

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@A330

SERVICE BULLETIN

References

Structural Repair Manual (SRM) 51-23-00

51-24-00

51-40-00

51-42-00

51-43-00

51-44-00

51-46-00

(a) For the specification of the materials (Mat. No.) given in this Service Bulletin, refer

to the Consumable Materials List (CML).

(b) Refer to the AIRBUS Standards Manual (SM) if you find part numbers for the

hardware components in the related kit(s) which you cannot identify in the LIST OF

COMPONENTS of this Service Bulletin. The SM will give you the correct part

number to part number relationship.

(c) For the identification of zones, refer to AMM 06-20-00, Page Block 001.

(d) For the Frame (FR) identification, refer to AMM 06-31-53, Page Block 001.

(e) For the location of the stringers (STGR), refer to AMM 06-30-00, Page Block 001.

(f) For the identification of access doors and panels, refer to AMM 06-41-52, Page

Block 001 and AMM 06-41-53, Page Block 001.

(g) Apply sealant in accordance with SRM 51-24-00.

(h) Renew the protective finish in accordance with SRM 51-23-00.

(i) Remove and install fasteners in accordance with SRM 51-42-00.

(j) Obtain alternative and substitute fastener data in accordance with SRM 51-43-00.

(k) If the length of any fastener specified in this Service Bulletin does not meet

installation standards given in SRM Chapter 51, then a fastener of the same

specification, or an approved substitute, with a length which meets the installation

standards given in SRM Chapter 51 may be used. In addition, washers may be

installed for fastener grip length in accordance with SRM Chapter 51.

(l) If alternative and substitute fasteners have to be used, you must make sure that the

associated nut/collar are compatible in accordance with SRM 51-40-00.

(m) Obtain fastener hole diameters and drill data in accordance with SRM 51-44-00.

(n) Obtain countersink data in accordance with SRM 51-46-00.

(o) For installation of lockwire, refer to AMM Task 20-11-00-911-801.

(p) For the installation of placards, refer to AMM 11-00-00, Page Block 201.

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 30

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SERVICE BULLETIN

(2) Subtask 523086-839-201-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF ALL

B. PREPARATION

**CONF 001

(1) Subtask 523086-941-201-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802

Task 24-41-00-861-801

Task 53-00-00-000-804

(a) The following items shall be considered as the basic Aircraft configuration before

you start a maintenance task:

- Aircraft on the ground resting on landing gear (the ground safety locks and the

wheel chocks are in position on the landing gear).

- Engine shut down, thrust reversers closed and locked.

- Aircraft in clean configuration.

- Parking brake applied.

- Aircraft electrical network de-energized.

- Hydraulic systems depressurized.

- Access to the cockpit and cabin is available.

- All circuit breakers are in closed position.

- All controls in NORM, AUTO or OFF position.

(b) Make sure that the aircraft is electrically grounded, refer to AMM Task

12-34-24-860-802.

(c) Energize the aircraft electrical circuits, refer to AMM Task 24-41-00-861-801.

(d) Put an access platform in position below the potable water service panel access

door 164AR.

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 31

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SERVICE BULLETIN

(e) Remove the necessary Bulk Cargo Compartment floor panels to get access

to the inner area of the potable water service panel, refer to AMM Task

53-00-00-000-804.

**CONF 002

(1) Subtask 523086-941-201-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802

Task 24-41-00-861-801

Task 53-00-00-000-804

(a) The following items shall be considered as the basic Aircraft configuration before

you start a maintenance task:

- Aircraft on the ground resting on landing gear (the ground safety locks and the

wheel chocks are in position on the landing gear).

- Engine shut down, thrust reversers closed and locked.

- Aircraft in clean configuration.

- Parking brake applied.

- Aircraft electrical network de-energized.

- Hydraulic systems depressurized.

- Access to the cockpit and cabin is available.

- All circuit breakers are in closed position.

- All controls in NORM, AUTO or OFF position.

(b) Make sure that the aircraft is electrically grounded, refer to AMM Task

12-34-24-860-802.

(c) Energize the aircraft electrical circuits, refer to AMM Task 24-41-00-861-801.

(d) Put an access platform in position below the potable water service panel access

door 164AR.

(e) Remove the necessary Bulk Cargo Compartment floor panels to get access

to the inner area of the potable water service panel, refer to AMM Task

53-00-00-000-804.

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 32

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@A330

SERVICE BULLETIN

**CONF 003

(1) Subtask 523086-941-201-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802

Task 24-41-00-861-801

Task 53-00-00-000-804

(a) The following items shall be considered as the basic Aircraft configuration before

you start a maintenance task:

- Aircraft on the ground resting on landing gear (the ground safety locks and the

wheel chocks are in position on the landing gear).

- Engine shut down, thrust reversers closed and locked.

- Aircraft in clean configuration.

- Parking brake applied.

- Aircraft electrical network de-energized.

- Hydraulic systems depressurized.

- Access to the cockpit and cabin is available.

- All circuit breakers are in closed position.

- All controls in NORM, AUTO or OFF position.

(b) Make sure that the aircraft is electrically grounded, refer to AMM Task

12-34-24-860-802.

(c) Energize the aircraft electrical circuits, refer to AMM Task 24-41-00-861-801.

(d) Put an access platform in position below the potable water service panel access

door 164AR.

(e) Remove the necessary Bulk Cargo Compartment floor panels to get access

to the inner area of the potable water service panel, refer to AMM Task

53-00-00-000-804.

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 33

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@A330

SERVICE BULLETIN

**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 523086-831-201-001 - Modify the potable water service panel access door

PN F5348614401200

Manpower Resources

Manhours 0.25

Minimum number of person 1

Subtask elapsed time 0.25

Skills NON SPECIFIC

Material necessary to do the job

Component COMPD04

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

6 A9249715920200 1 STUD

NOTE: The matset Comp 523086D04 is applicable only for operators which

have already matset Kit 523086D01R02, Kit 523086D02R02 or Kit

523086D03R02 on stock or which have already accomplished this

Service Bulletin at the original issue and have to do the additional work.

NOTE: The above list of components is not an AIRBUS Kit, the required parts

shall be ordered as necessary through the given channel.

Reidentified part set REIDD07

ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE

NOTES

F5348614401800 DOOR F5348614401200

NOTE: The part set Reid 523086D07 is to be used only for operators which

have already matset Kit 523086D01R02 on stock or which have already

accomplished this Service Bulletin at the original issue and have to do

the additional work.

References

Fig. A-GBDAA

Additional work - Modification of the

potable water service panel access door

Sheet 01

Sheet 02

Sheet 03

NOTE: All operator, which have already matset Kit 523086D01R02 on stock,

have to modify the Door Assy, delivered with the matset Kit

523086D01R02, following the subsequent worksteps.

Otherwise continue with SUBTASK 523086-020-201 001 Remove the

potable water service panel access door .

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 34

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@A330

SERVICE BULLETIN

(a) If you have the matset Kit 523086D01 with revision 02, then on bench, remove

from the Door Assy, PN F5348614401200, as shown on Fig. A-GBDAA Sheet 01,

Fig. A-GBDAA Sheet 02 and Fig. A-GBDAA Sheet 03, View C:

1 Stud-Adjusting Item (4) Discard

1 Nut Item (3) Retain

(b) Install to the Door Assy, PN F5348614401200, as shown on Fig. A-GBDAA Sheet

01, Fig. A-GBDAA Sheet 02 and Fig. A-GBDAA Sheet 03, View C:

1 Nut Item (3) Retained at

removal

1 Stud-Adjusting A9249715920200 Item 6

(c) Reidentify the potable water service panel access door:

1 Door Assy F5348614401200

becomes

1 Door Assy F5348614401800

NOTE: Mark the new P/N on the Door Assy with a permanent marker.

(2) Subtask 523086-020-201-001 - Remove the potable water service panel access

door

Work Zones and Access Panels

Zone Access/Work location

160

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills AIRFRAME

References

Fig. A-GBAAA

Removal of the potable water service

panel access door

Sheet 01

Sheet 02

Sheet 03

Sheet 04

(a) From the door, as shown on Fig. A-GBAAA Sheet 01, Fig. A-GBAAA Sheet 02 and

Fig. A-GBAAA Sheet 03, View C remove:

1 Nut Item (12) Discard

2 Washer Item (14) Discard

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 35

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SERVICE BULLETIN

1 Screw Item (8) Discard

and disconnect

1 Bonding lead Item (10) Retain

(b) Remove, as shown on Fig. A-GBAAA Sheet 01, Fig. A-GBAAA Sheet 02 and Fig.

A-GBAAA Sheet 03, View D:

8 Nut Item (12) Discard

8 Washer Item (14) Discard

8 Screw Item (16) Discard

1 Door Assy F5348614400600 Item (2) Discard

(c) Remove, as shown on Fig. A-GBAAA Sheet 01, Fig. A-GBAAA Sheet 02 and Fig.

A-GBAAA Sheet 03, View D:

4 Bolt Item (20) Discard

4 Washer Item (22) Discard

2 Hinge Item (24) Discard

2 Spring Item (26) Discard

2 Shim Item (28) Discard

(3) Subtask 523086-020-202-001 - Remove the fittings and the anchor nuts

Work Zones and Access Panels

Zone Access/Work location

160

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills AIRFRAME

References

Fig. A-GBAAA

Removal of the potable water service

panel access door

Sheet 01

Sheet 02

Sheet 03

Sheet 04

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 36

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@A330

SERVICE BULLETIN

(a) Remove, as shown on Fig. A-GBAAA Sheet 01, Fig. A-GBAAA Sheet 02 and Fig.

A-GBAAA Sheet 04, View F:

4 Collar Item (30) Discard

4 Pin Item (32) Discard

2 Fitting Item (34) Discard

(b) Remove, as shown on Fig. A-GBAAA Sheet 01, Fig. A-GBAAA Sheet 03 and Fig.

A-GBAAA Sheet 04, View E:

8 Rivet Item (50) Discard

4 Anchor nut Item (52) Discard

(4) Subtask 523086-420-201-001 - Install the new anchor nuts

Work Zones and Access Panels

Zone Access/Work location

160

Manpower Resources

Manhours 1.00

Minimum number of person 2

Subtask elapsed time 0.50

Skills AIRFRAME

Material necessary to do the job

Kit 523086D01R03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

50 NSA5414N24-10 16 RIVET

52 NAS1474R4K 4 NUT

54 F5348615620600 2 SHIM

Consumable CMLD10

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Coating - Flexible Structure 04QAB2 As required

Polysulfide Sealant-General

Purpose Brushable

06AAA1 As required

Polysulfide Sealant-General

Purpose Fillet

06AAB1 As required

Non Aqueous CleanerGeneral08BAA9 As required

Textile-Lint Free Cotton 14SBA1 As required

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 37

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SERVICE BULLETIN

References

Structural Repair Manual (SRM) 51-24-00

51-44-00

51-46-00

Fig. A-GBBAA

Installation of the potable water service

panel access door

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

(a) Put the Shims, item 54, in position as shown on Fig. A-GBBAA Sheet 01, Fig. AGBBAA Sheet 04 and Fig. A-GBBAA Sheet 05, View G.

(b) Transfer drill the existing rivet holes to the Shims, item 54, as shown on Fig. AGBBAA Sheet 01, Fig. A-GBBAA Sheet 04 and Fig. A-GBBAA Sheet 05, View G

and in accordance with SRM 51-44-00.

(c) Temporarily install the Shims, item 54, to the structure with set screws.

(d) Drill the new rivet holes using the Anchor nut, item 52, as shown on Fig. A-GBBAA

Sheet 01, Fig. A-GBBAA Sheet 04, Fig. A-GBBAA Sheet 05, View G and H and

Fig. A-GBBAA Sheet 06, View J and in accordance with SRM 51-44-00.

(e) Drill the existing holes to a diameter of 6.8 mm (0.27 in) as shown on Fig. AGBBAA Sheet 01, Fig. A-GBBAA Sheet 04 and Fig. A-GBBAA Sheet 05, section EE.

(f) Remove the Shims, item 54, and deburr all drilled holes.

(g) Countersink where necessary the rivet holes with a 100 ̊ countersink drill as shown

on Fig. A-GBBAA Sheet 05, section D-D and section E-E and in accordance with

SRM 51-46-00.

(h) Clean the installation area and the Shims, item 54, with:

Non Aqueous

Cleaner-General

08BAA9 As required

and

Textile-Lint Free

Cotton

14SBA1 As required

(i) Install, as shown on Fig. A-GBBAA Sheet 01, Fig. A-GBBAA Sheet 04 and Fig. AGBBAA Sheet 05, View G:

2 Shim F5348615620600 Item 54

and, with:

Polysulfide SealantGeneral Purpose

Fillet

06AAB1 As required

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 38

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SERVICE BULLETIN

8 Rivet NSA5414N24-10 Item 50

NOTE: Cut the rivets to the necessary length.

(j) Install, as shown on Fig. A-GBBAA Sheet 01, Fig. A-GBBAA Sheet 04 and Fig. AGBBAA Sheet 05, View H:

4 Anchor Nut NAS1474R4K Item 52

with:

8 Rivet NSA5414N24-10 Item 50

NOTE: Cut the rivets to the necessary length.

(k) Apply to the Shim, item 54, the Anchor Nut, item 52 and the rivets, item 50, as

shown on Fig. A-GBBAA Sheet 01, Fig. A-GBBAA Sheet 04 and Fig. A-GBBAA

Sheet 05, View G and H, section D-D and E-E, and in accordance with SRM

51-24-00:

Polysulfide SealantGeneral Purpose

Brushable

06AAA1 As required

(l) Let the sealant cure.

(m) Apply to the sealed areas:

Coating - Flexible

Structure

04QAB2 As required

(5) Subtask 523086-420-202-001 - Install the new hinges

Work Zones and Access Panels

Zone Access/Work location

160

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills AIRFRAME

Material necessary to do the job

Kit 523086D01R03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

20 NAS1801-4-9 4 SCREW

22 NAS1149C0432R 4 WASHER

24 F5348615700600 2 HINGE

26 F5348615520400 2 SPRING

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 39

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@A330

SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

28 F5348615620400 4 SHIM (1)

NOTE (1): A maximum of 4 shims necessary only if the hinges have to be adjusted.

Consumable CMLD10

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Non Aqueous CleanerGeneral08BAA9 As required

Textile-Lint Free Cotton 14SBA1 As required

References

Fig. A-GBBAA

Installation of the potable water service

panel access door

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

(a) Clean the area where the hinges will be installed with:

Non Aqueous

Cleaner-General

08BAA9 As required

and

Textile-Lint Free

Cotton

14SBA1 As required

(b) Install, as shown on Fig. A-GBBAA Sheet 01, Fig. A-GBBAA Sheet 02 and Fig. AGBBAA Sheet 04, View F:

2 Spring F5348615520400 Item 26

2 Hinge Assy F5348615700600 Item 24

with

4 Washer NAS1149C0432R Item 22

4 Screw NAS1801-4-9 Item 20

(c) Check the alignment of the hinges.

1 Carefully bring the hinges, item 24, in the closed position as shown on Fig. AGBBAA Sheet 01, Fig. A-GBBAA Sheet 02 and Fig. A-GBBAA Sheet 04,

section C-C.

2 Make sure that the contour of the structure and the hinges are level and there

are no steps as shown on Fig. A-GBBAA Sheet 01, Fig. A-GBBAA Sheet 02

and Fig. A-GBBAA Sheet 04, section C-C.

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

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SERVICE BULLETIN

3 To adjust the hinges install, if necessary:

4 Shim F5348615620400 Item 28

NOTE: A maximum of two shims, item 28, per hinge are allowed.

(d) Tighten the screws, item 20, with a torque value of 8.2 Nm to 10.6 Nm (72.58 lbf.in

to 93.82 lbf.in).

(6) Subtask 523086-420-206-001 - Install the potable water service panel access door

PN F5348614401800

Work Zones and Access Panels

Zone Access/Work location

160

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills AIRFRAME

Material necessary to do the job

Kit 523086D01R03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

2 F5348614401800 1 DOOR

12 NAS1291C3M 8 NUT

14 NAS1149C0332R 8 WASHER

16 NAS1102E3-8 8 SCREW

References

Fig. A-GBBAA

Installation of the potable water service

panel access door

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

Fig. A-GBCAA

Adjustment of the potable water service

panel access door

Sheet 01

Sheet 02

Sheet 03

Sheet 04

(a) Install, as shown on Fig. A-GBBAA Sheet 01, Fig. A-GBBAA Sheet 02 and Fig. AGBBAA Sheet 04, View F:

1 Door Assy F5348614401800 Item 2

with

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 41

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SERVICE BULLETIN

8 Screw NAS1102E3-8 Item 16

8 Washer NAS1149C0332R Item 14

8 Nut NAS1291C3M Item 12

(b) Close and adjust the door, item 2, to achieve a circumferential gap as shown on

Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet 02 and Fig. A-GBCAA Sheet 04,

section C-C.

(c) Tighten the screws, item 16, with a torque value of 3.7 Nm to 4.8 Nm (32.75 lbf.in

to 42.48 lbf.in).

(7) Subtask 523086-420-203-001 - Install the new fittings

Work Zones and Access Panels

Zone Access/Work location

160

Manpower Resources

Manhours 2.00

Minimum number of person 2

Subtask elapsed time 1.00

Skills AIRFRAME

Material necessary to do the job

Kit 523086D01R03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

30 NSA5075-5 9 COLLAR

32 DAN6-5-4 9 PIN

34 F5348614120200 2 FITTING

35 F5348614120400 1 FITTING

Consumable CMLD10

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Coating - Flexible Structure 04QAB2 As required

Polysulfide Sealant-General

Purpose Brushable

06AAA1 As required

Non Aqueous CleanerGeneral08BAA9 As required

Textile-Lint Free Cotton 14SBA1 As required

References

Structural Repair Manual (SRM) 51-24-00

51-44-00

51-46-00

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 42

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SERVICE BULLETIN

References

Fig. A-GBBAA

Installation of the potable water service

panel access door

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

(a) Install the fittings, item 34, using the existing rivet holes, to the structure with set

screws as shown on Fig. A-GBBAA Sheet 01, Fig. A-GBBAA Sheet 02 and Fig. AGBBAA Sheet 03, View E.

(b) Mark the position of the new rivet holes.

(c) Drill the new rivet holes in the structure through the pilot hole.

(d) Increase the hole diameter to the correct size for the given fasteners in accordance

with SRM 51-44-00.

(e) Remove the fittings, item 34.

(f) Deburr the fastener holes.

(g) Countersink the holes of the fittings, item 34, with a 100 ̊ countersink drill in

accordance with SRM 51-46-00.

(h) Clean the installation area of the fittings, item 34, with:

Non Aqueous

Cleaner-General

08BAA9 As required

and

Textile-Lint Free

Cotton

14SBA1 As required

(i) Install, as shown on Fig. A-GBBAA Sheet 01, Fig. A-GBBAA Sheet 02 and Fig. AGBBAA Sheet 03, View E:

2 Fitting F5348614120200 Item 34

with

6 Pin-Rivet DAN6-5-4 Item 32

6 Collar NSA5075-5 Item 30

(j) Mark the position of the fitting, item 35, to the structure as shown on Fig. A-GBBAA

Sheet 01, Fig. A-GBBAA Sheet 02 and Fig. A-GBBAA Sheet 03, View C, D and

section A-A.

(k) Carefully close the door, item 2, and check that the center line of the fitting, item

35, is in line with the center line of the latch.

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 43

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SERVICE BULLETIN

(l) Open the door, item 2.

(m) If necessary, correct the position of the fitting, item 35, to make sure that the latch

of the door, item 2, engages correctly.

(n) Mark the position of the rivet holes.

(o) Drill the rivet holes in the structure.

(p) Increase the hole diameter to the correct size for the given fasteners in accordance

with SRM 51-44-00.

(q) Remove the fitting, item 35.

(r) Deburr the fastener holes.

(s) Countersink the holes of the fitting, item 35, with a 100 ̊ countersink drill in

accordance with SRM 51-46-00.

(t) Clean the installation area of the fitting, item 35, with:

Non Aqueous

Cleaner-General

08BAA9 As required

and

Textile-Lint Free

Cotton

14SBA1 As required

(u) Install, as shown on Fig. A-GBBAA Sheet 01, Fig. A-GBBAA Sheet 02 and Fig. AGBBAA Sheet 03, View C, D and section A-A:

1 Fitting F5348614120400 Item 35

with

3 Pin-Rivet DAN6-5-4 Item 32

3 Collar NSA5075-5 Item 30

(v) Apply to the Fittings, item 34 and 35, the Pin-Rivet, item 32 and the Collar, item 30,

in accordance with SRM 51-24-00:

Polysulfide SealantGeneral Purpose

Brushable

06AAA1 As required

(w) Let the sealant cure.

(x) Apply to the sealed areas:

Coating - Flexible

Structure

04QAB2 As required

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 44

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SERVICE BULLETIN

(8) Subtask 523086-420-204-001 - Install the bonding lead

Work Zones and Access Panels

Zone Access/Work location

160

Manpower Resources

Manhours 0.25

Minimum number of person 1

Subtask elapsed time 0.25

Skills AIRFRAME

Material necessary to do the job

Kit 523086D01R03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

8 NAS1100-3-7 1 SCREW

12 NAS1291C3M 1 NUT

14 NAS1149C0332R 2 WASHER

Consumable CMLD10

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Varnish - Electrical Bonding

Structure

04TMB2 As required

Non Aqueous CleanerGeneral08BAA9 As required

Textile-Lint Free Cotton 14SBA1 As required

References

Aircraft Maintenance Manual (AMM) Task 20-28-00-912-802

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

Fig. A-GBBAA

Installation of the potable water service

panel access door

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

(a) Clean the bonding points, as given in AMM Task 20-28-00-912-802 and ESPM

20-51-20, with:

Non Aqueous

Cleaner-General

08BAA9 As required

and

Textile-Lint Free

Cotton

14SBA1 As required

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 45

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@A330

SERVICE BULLETIN

(b) Install, as shown on Fig. A-GBBAA Sheet 01, Fig. A-GBBAA Sheet 02 and Fig. AGBBAA Sheet 06, View K:

1 Bonding lead Item (10) Retained at

removal

with

1 Screw NAS1100-3-7 Item 8

2 Washer NAS1149C0332R Item 14

1 Nut NAS1291C3M Item 12

(c) Apply to the bonding points as given in AMM Task 20-28-00-912-802:

Varnish - Electrical

Bonding Structure

04TMB2 As required

(9) Subtask 523086-930-201-001 - Reidentify the potable water service panel

Work Zones and Access Panels

Zone Access/Work location

160

Manpower Resources

Manhours 0.25

Minimum number of person 1

Subtask elapsed time 0.25

Skills AIRFRAME

Material necessary to do the job

Reidentified part set REIDD05

ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE

NOTES

F5348633920000 PANEL F5348612320400

Reidentify the potable water service panel:

1 Panel F5348612320400

becomes

1 Panel F5348633920000

NOTE: Mark the new P/N on the panel with a permanent marker.

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 46

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SERVICE BULLETIN

(10) Subtask 523086-820-201-001 - Adjust the new potable water service panel access

door

Work Zones and Access Panels

Zone Access/Work location

160

Manpower Resources

Manhours 0.75

Minimum number of person 1

Subtask elapsed time 0.75

Skills AIRFRAME

Material necessary to do the job

Consumable CMLD10

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Threadlocking Adhesive -

Medium Strength

05BAE1 As required

Polysulfide Sealant-General

Purpose Fillet

06AAB1 As required

Non Aqueous CleanerGeneral08BAA9 As required

Release Agent - Liquid Wax 14DBB1 As required

Wire-Locking Dia: 0.5 Mm

(0.020 Inch) Cres Nickel

14QDB1 As required

Textile-Lint Free Cotton 14SBA1 As required

References

Aircraft Maintenance Manual (AMM) Task 38-10-00-820-801

Fig. A-GBCAA

Adjustment of the potable water service

panel access door

Sheet 01

Sheet 02

Sheet 03

Sheet 04

(a) Open the door, item 2, and lock all latches. Adjust all adjustment bolts to a gap of

6.5 mm (0.26 in) to the door as shown on Fig. A-GBCAA Sheet 01, Fig. A-GBCAA

Sheet 02 and Fig. A-GBCAA Sheet 03, section A-A.

(b) Close the door, item 2, and lock all latches. Check the gap between the door, item

2, and the structure. Open the door, item 2, and adjust all adjustment bolts to

achieve a gap of 0.8 mm (0.031 in) +/- 0.5mm (0.020 in), as shown on .Fig. AGBCAA Sheet 01, Fig. A-GBCAA Sheet 02 and Fig. A-GBCAA Sheet 04, section

B-B.

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 47

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SERVICE BULLETIN

(c) Open the door, item 2, and clean the area to be sealed as shown on Fig. AGBCAA Sheet 01 and Fig. A-GBCAA Sheet 02 with:

Non Aqueous

Cleaner-General

08BAA9 As required

and

Textile-Lint Free

Cotton

14SBA1 As required

(d) Apply to the door, item 2, and to the structure as shown on Fig. A-GBCAA Sheet

01 and Fig. A-GBCAA Sheet 02:

Polysulfide SealantGeneral Purpose

Fillet

06AAB1 As required

and

Release Agent -

Liquid Wax

14DBB1 As required

(e) Close the door, item 2, and lock all latches.

(f) Let the sealant cure.

(g) Remove the unwanted sealant from the door and from the fuselage skin.

(h) Clean the door and structure skin with:

Non Aqueous

Cleaner-General

08BAA9 As required

and

Textile-Lint Free

Cotton

14SBA1 As required

(i) Do the final adjustment of the door, item 2.

1 Check the gap between the door, item 2, and the structure.

2 Adjust the door, item 2, to the minimum possible gap between the door, item

2, and the structure by adjusting the adjustment bolts without putting tension

to the latches even when they are in locked position.

3 Ensure that:

- the latches snap in clearly noticeable and without delay

- the hand force necessary to lock the latches in the door closed position is

not larger as needed to lock the latches in the door open position

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 48

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SERVICE BULLETIN

(j) Safety the adjustment bolt as follows:

1 If a latch with a drilled nut at the adjustment bolt is installed, safety the

adjustment bolt as shown on Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet

02 and Fig. A-GBCAA Sheet 03, section A-A, with:

Wire-Locking Dia:

0.5 Mm (0.020

Inch) Cres Nickel

14QDB1 As required

2 If a latch with a self-locking nut at the adjustment bolt is installed, safety the

adjustment bolt as shown on Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet

02 and Fig. A-GBCAA Sheet 03, section B-B, by tightening the self-locking nut

with a torque value of 4.0 Nm to 6.0 Nm (35.40 lbf.in to 53.10 lbf.in).

(k) Adjust the door switch as given in AMM Task 38-10-00-820-801.

(l) Safety the door switch as shown on Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet

02 and Fig. A-GBCAA Sheet 04, View C, with:

Threadlocking

Adhesive - Medium

Strength

05BAE1 As required

(11) Subtask 523086-916-201-001 - Restore the aircraft surface protection

Work Zones and Access Panels

Zone Access/Work location

160

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills AIRFRAME

Material necessary to do the job

Consumable CMLD10

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Top Coat Polyurethane -

External Structure

04JAA3 As required

Aqueous Cleaner-Aircraft

Exterior Pressure Spray

08ABC1 As required

Corrosion Preventive

Compound-Water

Displacing Oil

12ABE2 As required

Textile-Lint Free Cotton 14SBA1 As required

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 49

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@A330

SERVICE BULLETIN

References

Structural Repair Manual (SRM) 51-75-12

(a) Clean the potable water service panel access door with:

Aqueous CleanerAircraft Exterior

Pressure Spray

08ABC1 As required

and

Textile-Lint Free

Cotton

14SBA1 As required

(b) Apply, in accordance with your aircraft color scheme:

Top Coat

Polyurethane -

External Structure

04JAA3 As required

to the outside area of the potable water service panel access door, refer to SRM

51-75-12.

(c) Inside the fuselage, clean the area of the potable water service panel and make

sure that the area is dirt free.

(d) Restore the surface protection of the inner fuselage skin with:

Corrosion

Preventive

Compound-Water

Displacing Oil

12ABE2 As required

(12) Subtask 523086-420-205-001 - Install the placard

Work Zones and Access Panels

Zone Access/Work location

160

Manpower Resources

Manhours 0.25

Minimum number of person 1

Subtask elapsed time 0.25

Skills AIRFRAME

Material necessary to do the job

Kit 523086D01R03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

60 F1121009420000 1 PLACARD

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 50

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SERVICE BULLETIN

Consumable CMLD10

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Varnish Polyurethane-Low

Voc - External Structure

04SBA3 As required

Non Aqueous CleanerGeneral08BAA9 As required

Textile-Lint Free Cotton 14SBA1 As required

References

Fig. A-GBBAA

Installation of the potable water service

panel access door

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

(a) Clean the installation area of the placard, item 60, with:

Non Aqueous

Cleaner-General

08BAA9 As required

and

Textile-Lint Free

Cotton

14SBA1 As required

(b) Install, as shown on Fig. A-GBBAA Sheet 01, Fig. A-GBBAA Sheet 02 and Fig. AGBBAA Sheet 06, View L:

1 Placard F1121009420000 Item 60

(c) Apply to the placard for protection:

Varnish

Polyurethane-Low

Voc - External

Structure

04SBA3 As required

**CONF 002

(1) Subtask 523086-831-201-002 - Modify the potable water service panel access door

PN F5348614401400

Manpower Resources

Manhours 0.25

Minimum number of person 1

Subtask elapsed time 0.25

Skills NON SPECIFIC

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 51

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SERVICE BULLETIN

Material necessary to do the job

Component COMPD04

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

6 A9249715920200 1 STUD

NOTE: The matset Comp 523086D04 is applicable only for operators which

have already matset Kit 523086D01R02, Kit 523086D02R02 or Kit

523086D03R02 on stock or which have already accomplished this

Service Bulletin at the original issue and have to do the additional work.

NOTE: The above list of components is not an AIRBUS Kit, the required parts

shall be ordered as necessary through the given channel.

Reidentified part set REIDD08

ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE

NOTES

F5348614402000 DOOR F5348614401400

NOTE: The part set Reid 523086D08 is to be used only for operators which

have already matset Kit 523086D02R02 on stock or which have already

accomplished this Service Bulletin at the original issue and have to do

the additional work.

References

Fig. A-GBDAA

Additional work - Modification of the

potable water service panel access door

Sheet 01

Sheet 02

Sheet 03

NOTE: All operator, which have already matset Kit 523086D02R02 on stock,

have to modify the Door Assy, delivered with the matset Kit

523086D02R02, following the subsequent worksteps.

Otherwise continue with SUBTASK 523086-020-201 002 Remove the

potable water service panel access door .

(a) If you have the matset Kit 523086D02 with revision 02, then on bench, remove

from the Door Assy, PN F5348614401400, as shown on Fig. A-GBDAA Sheet 01,

Fig. A-GBDAA Sheet 02 and Fig. A-GBDAA Sheet 03, View C:

1 Stud-Adjusting Item (4) Discard

1 Nut Item (3) Retain

(b) Install to the Door Assy, PN F5348614401400, as shown on Fig. A-GBDAA Sheet

01, Fig. A-GBDAA Sheet 02 and Fig. A-GBDAA Sheet 03, View C:

1 Nut Item (3) Retained at

removal

1 Stud-Adjusting A9249715920200 Item 6

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 52

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@A330

SERVICE BULLETIN

(c) Reidentify the potable water service panel access door:

1 Door Assy F5348614401400

becomes

1 Door Assy F5348614402000

NOTE: Mark the new P/N on the Door Assy with a permanent marker.

(2) Subtask 523086-020-201-002 - Remove the potable water service panel access

door

Work Zones and Access Panels

Zone Access/Work location

160

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills AIRFRAME

References

Fig. A-GBAAA

Removal of the potable water service

panel access door

Sheet 01

Sheet 02

Sheet 03

Sheet 04

(a) From the door, as shown on Fig. A-GBAAA Sheet 01, Fig. A-GBAAA Sheet 02 and

Fig. A-GBAAA Sheet 03, View C remove:

1 Nut Item (12) Discard

2 Washer Item (14) Discard

1 Screw Item (8) Discard

and disconnect

1 Bonding lead Item (10) Retain

(b) Remove, as shown on Fig. A-GBAAA Sheet 01, Fig. A-GBAAA Sheet 02 and Fig.

A-GBAAA Sheet 03, View D:

8 Nut Item (12) Discard

8 Washer Item (14) Discard

8 Screw Item (16) Discard

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 53

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@A330

SERVICE BULLETIN

1 Door Assy F5348614400400 Item (2) Discard

(c) Remove, as shown on Fig. A-GBAAA Sheet 01, Fig. A-GBAAA Sheet 02 and Fig.

A-GBAAA Sheet 03, View D:

4 Bolt Item (20) Discard

4 Washer Item (22) Discard

2 Hinge Item (24) Discard

2 Spring Item (26) Discard

2 Shim Item (28) Discard

(3) Subtask 523086-020-202-001 - Remove the fittings and the anchor nuts

Work Zones and Access Panels

Zone Access/Work location

160

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills AIRFRAME

References

Fig. A-GBAAA

Removal of the potable water service

panel access door

Sheet 01

Sheet 02

Sheet 03

Sheet 04

(a) Remove, as shown on Fig. A-GBAAA Sheet 01, Fig. A-GBAAA Sheet 02 and Fig.

A-GBAAA Sheet 04, View F:

4 Collar Item (30) Discard

4 Pin Item (32) Discard

2 Fitting Item (34) Discard

(b) Remove, as shown on Fig. A-GBAAA Sheet 01, Fig. A-GBAAA Sheet 03 and Fig.

A-GBAAA Sheet 04, View E:

8 Rivet Item (50) Discard

4 Anchor nut Item (52) Discard

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 54

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@A330

SERVICE BULLETIN

(4) Subtask 523086-420-201-002 - Install the new anchor nuts

Work Zones and Access Panels

Zone Access/Work location

160

Manpower Resources

Manhours 1.00

Minimum number of person 2

Subtask elapsed time 0.50

Skills AIRFRAME

Material necessary to do the job

Kit 523086D02R05

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

50 NSA5414N24-10 16 RIVET

52 NAS1474R4K 4 NUT

54 F5348615620600 2 SHIM

Consumable CMLD10

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Coating - Flexible Structure 04QAB2 As required

Polysulfide Sealant-General

Purpose Brushable

06AAA1 As required

Polysulfide Sealant-General

Purpose Fillet

06AAB1 As required

Non Aqueous CleanerGeneral08BAA9 As required

Textile-Lint Free Cotton 14SBA1 As required

References

Structural Repair Manual (SRM) 51-24-00

51-44-00

51-46-00

Fig. A-GBBAA

Installation of the potable water service

panel access door

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

(a) Put the Shims, item 54, in position as shown on Fig. A-GBBAA Sheet 01, Fig. AGBBAA Sheet 04 and Fig. A-GBBAA Sheet 05, View G.

(b) Transfer drill the existing rivet holes to the Shims, item 54, as shown on Fig. AGBBAA Sheet 01, Fig. A-GBBAA Sheet 04 and Fig. A-GBBAA Sheet 05, View G

and in accordance with SRM 51-44-00.

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 55

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SERVICE BULLETIN

(c) Temporarily install the Shims, item 54, to the structure with set screws.

(d) Drill the new rivet holes using the Anchor nut, item 52, as shown on Fig. A-GBBAA

Sheet 01, Fig. A-GBBAA Sheet 04, Fig. A-GBBAA Sheet 05, View G and H and

Fig. A-GBBAA Sheet 06, View J and in accordance with SRM 51-44-00.

(e) Drill the existing holes to a diameter of 6.8 mm (0.27 in) as shown on Fig. AGBBAA Sheet 01, Fig. A-GBBAA Sheet 04 and Fig. A-GBBAA Sheet 05, section EE.

(f) Remove the Shims, item 54, and deburr all drilled holes.

(g) Countersink where necessary the rivet holes with a 100 ̊ countersink drill as shown

on Fig. A-GBBAA Sheet 05, section D-D and section E-E and in accordance with

SRM 51-46-00.

(h) Clean the installation area and the Shims, item 54, with:

Non Aqueous

Cleaner-General

08BAA9 As required

and

Textile-Lint Free

Cotton

14SBA1 As required

(i) Install, as shown on Fig. A-GBBAA Sheet 01, Fig. A-GBBAA Sheet 04 and Fig. AGBBAA Sheet 05, View G:

2 Shim F5348615620600 Item 54

and, with:

Polysulfide SealantGeneral Purpose

Fillet

06AAB1 As required

8 Rivet NSA5414N24-10 Item 50

NOTE: Cut the rivets to the necessary length.

(j) Install, as shown on Fig. A-GBBAA Sheet 01, Fig. A-GBBAA Sheet 04 and Fig. AGBBAA Sheet 05, View H:

4 Anchor Nut NAS1474R4K Item 52

with:

8 Rivet NSA5414N24-10 Item 50

NOTE: Cut the rivets to the necessary length.

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 56

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@A330

SERVICE BULLETIN

(k) Apply to the Shim, item 54, the Anchor Nut, item 52 and the rivets, item 50, as

shown on Fig. A-GBBAA Sheet 01, Fig. A-GBBAA Sheet 04 and Fig. A-GBBAA

Sheet 05, View G and H, section D-D and E-E, and in accordance with SRM

51-24-00:

Polysulfide SealantGeneral Purpose

Brushable

06AAA1 As required

(l) Let the sealant cure.

(m) Apply to the sealed areas:

Coating - Flexible

Structure

04QAB2 As required

(5) Subtask 523086-420-202-002 - Install the new hinges

Work Zones and Access Panels

Zone Access/Work location

160

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills AIRFRAME

Material necessary to do the job

Kit 523086D02R05

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

20 NAS1801-4-9 4 SCREW

22 NAS1149C0432R 4 WASHER

24 F5348615700600 2 HINGE

26 F5348615520400 2 SPRING

28 F5348615620400 4 SHIM (1)

NOTE (1): A maximum of 4 shims necessary only if the hinges have to be adjusted.

Consumable CMLD10

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Non Aqueous CleanerGeneral08BAA9 As required

Textile-Lint Free Cotton 14SBA1 As required

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 57

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@A330

SERVICE BULLETIN

References

Fig. A-GBBAA

Installation of the potable water service

panel access door

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

(a) Clean the area where the hinges will be installed with:

Non Aqueous

Cleaner-General

08BAA9 As required

and

Textile-Lint Free

Cotton

14SBA1 As required

(b) Install, as shown on Fig. A-GBBAA Sheet 01, Fig. A-GBBAA Sheet 02 and Fig. AGBBAA Sheet 04, View F:

2 Spring F5348615520400 Item 26

2 Hinge Assy F5348615700600 Item 24

with

4 Washer NAS1149C0432R Item 22

4 Screw NAS1801-4-9 Item 20

(c) Check the alignment of the hinges.

1 Carefully bring the hinges, item 24, in the closed position as shown on Fig. AGBBAA Sheet 01, Fig. A-GBBAA Sheet 02 and Fig. A-GBBAA Sheet 04,

section C-C.

2 Make sure that the contour of the structure and the hinges are level and there

are no steps as shown on Fig. A-GBBAA Sheet 01, Fig. A-GBBAA Sheet 02

and Fig. A-GBBAA Sheet 04, section C-C.

3 To adjust the hinges install, if necessary:

4 Shim F5348615620400 Item 28

NOTE: A maximum of two shims, item 28, per hinge are allowed.

(d) Tighten the screws, item 20, with a torque value of 8.2 Nm to 10.6 Nm (72.58 lbf.in

to 93.82 lbf.in).

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 58

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SERVICE BULLETIN

(6) Subtask 523086-420-206-002 - Install the potable water service panel access door

PN F5348614402000

Work Zones and Access Panels

Zone Access/Work location

160

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills AIRFRAME

Material necessary to do the job

Kit 523086D02R05

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

2 F5348614402000 1 DOOR

12 NAS1291C3M 8 NUT

14 NAS1149C0332R 8 WASHER

16 NAS1102E3-8 8 SCREW

References

Fig. A-GBBAA

Installation of the potable water service

panel access door

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

Fig. A-GBCAA

Adjustment of the potable water service

panel access door

Sheet 01

Sheet 02

Sheet 03

Sheet 04

(a) Install, as shown on Fig. A-GBBAA Sheet 01, Fig. A-GBBAA Sheet 02 and Fig. AGBBAA Sheet 04, View F:

1 Door Assy F5348614402000 Item 2

with

8 Screw NAS1102E3-8 Item 16

8 Washer NAS1149C0332R Item 14

8 Nut NAS1291C3M Item 12

(b) Close and adjust the door, item 2, to achieve a circumferential gap as shown on

Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet 02 and Fig. A-GBCAA Sheet 04,

section C-C.

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 59

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SERVICE BULLETIN

(c) Tighten the screws, item 16, with a torque value of 3.7 Nm to 4.8 Nm (32.75 lbf.in

to 42.48 lbf.in).

(7) Subtask 523086-420-203-002 - Install the new fittings

Work Zones and Access Panels

Zone Access/Work location

160

Manpower Resources

Manhours 2.00

Minimum number of person 2

Subtask elapsed time 1.00

Skills AIRFRAME

Material necessary to do the job

Kit 523086D02R05

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

30 NSA5075-5 9 COLLAR

32 DAN6-5-4 9 PIN

34 F5348614120200 2 FITTING

35 F5348614120400 1 FITTING

Consumable CMLD10

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Coating - Flexible Structure 04QAB2 As required

Polysulfide Sealant-General

Purpose Brushable

06AAA1 As required

Non Aqueous CleanerGeneral08BAA9 As required

Textile-Lint Free Cotton 14SBA1 As required

References

Structural Repair Manual (SRM) 51-24-00

51-44-00

51-46-00

Fig. A-GBBAA

Installation of the potable water service

panel access door

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

(a) Install the fittings, item 34, using the existing rivet holes, to the structure with set

screws as shown on Fig. A-GBBAA Sheet 01, Fig. A-GBBAA Sheet 02 and Fig. AGBBAA Sheet 03, View E.

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

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SERVICE BULLETIN

(b) Mark the position of the new rivet holes.

(c) Drill the new rivet holes in the structure through the pilot hole.

(d) Increase the hole diameter to the correct size for the given fasteners in accordance

with SRM 51-44-00.

(e) Remove the fittings, item 34.

(f) Deburr the fastener holes.

(g) Countersink the holes of the fittings, item 34, with a 100 ̊ countersink drill in

accordance with SRM 51-46-00.

(h) Clean the installation area of the fittings, item 34, with:

Non Aqueous

Cleaner-General

08BAA9 As required

and

Textile-Lint Free

Cotton

14SBA1 As required

(i) Install, as shown on Fig. A-GBBAA Sheet 01, Fig. A-GBBAA Sheet 02 and Fig. AGBBAA Sheet 03, View E:

2 Fitting F5348614120200 Item 34

with

6 Pin-Rivet DAN6-5-4 Item 32

6 Collar NSA5075-5 Item 30

(j) Mark the position of the fitting, item 35, to the structure as shown on Fig. A-GBBAA

Sheet 01, Fig. A-GBBAA Sheet 02 and Fig. A-GBBAA Sheet 03, View C, D and

section A-A.

(k) Carefully close the door, item 2, and check that the center line of the fitting, item

35, is in line with the center line of the latch.

(l) Open the door, item 2.

(m) If necessary, correct the position of the fitting, item 35, to make sure that the latch

of the door, item 2, engages correctly.

(n) Mark the position of the rivet holes.

(o) Drill the rivet holes in the structure.

(p) Increase the hole diameter to the correct size for the given fasteners in accordance

with SRM 51-44-00.

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 61

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SERVICE BULLETIN

(q) Remove the fitting, item 35.

(r) Deburr the fastener holes.

(s) Countersink the holes of the fitting, item 35, with a 100 ̊ countersink drill in

accordance with SRM 51-46-00.

(t) Clean the installation area of the fitting, item 35, with:

Non Aqueous

Cleaner-General

08BAA9 As required

and

Textile-Lint Free

Cotton

14SBA1 As required

(u) Install, as shown on Fig. A-GBBAA Sheet 01, Fig. A-GBBAA Sheet 02 and Fig. AGBBAA Sheet 03, View C, D and section A-A:

1 Fitting F5348614120400 Item 35

with

3 Pin-Rivet DAN6-5-4 Item 32

3 Collar NSA5075-5 Item 30

(v) Apply to the Fittings, item 34 and 35, the Pin-Rivet, item 32 and the Collar, item 30,

in accordance with SRM 51-24-00:

Polysulfide SealantGeneral Purpose

Brushable

06AAA1 As required

(w) Let the sealant cure.

(x) Apply to the sealed areas:

Coating - Flexible

Structure

04QAB2 As required

(8) Subtask 523086-420-204-002 - Install the bonding lead

Work Zones and Access Panels

Zone Access/Work location

160

Manpower Resources

Manhours 0.25

Minimum number of person 1

Subtask elapsed time 0.25

Skills AIRFRAME

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 62

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@A330

SERVICE BULLETIN

Material necessary to do the job

Kit 523086D02R05

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

8 NAS1100-3-7 1 SCREW

12 NAS1291C3M 1 NUT

14 NAS1149C0332R 2 WASHER

Consumable CMLD10

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Varnish - Electrical Bonding

Structure

04TMB2 As required

Non Aqueous CleanerGeneral08BAA9 As required

Textile-Lint Free Cotton 14SBA1 As required

References

Aircraft Maintenance Manual (AMM) Task 20-28-00-912-802

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

Fig. A-GBBAA

Installation of the potable water service

panel access door

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

(a) Clean the bonding points, as given in AMM Task 20-28-00-912-802 and ESPM

20-51-20, with:

Non Aqueous

Cleaner-General

08BAA9 As required

and

Textile-Lint Free

Cotton

14SBA1 As required

(b) Install, as shown on Fig. A-GBBAA Sheet 01, Fig. A-GBBAA Sheet 02 and Fig. AGBBAA Sheet 06, View K:

1 Bonding lead Item (10) Retained at

removal

with

1 Screw NAS1100-3-7 Item 8

2 Washer NAS1149C0332R Item 14

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 63

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SERVICE BULLETIN

1 Nut NAS1291C3M Item 12

(c) Apply to the bonding points as given in AMM Task 20-28-00-912-802:

Varnish - Electrical

Bonding Structure

04TMB2 As required

(9) Subtask 523086-930-201-001 - Reidentify the potable water service panel

Work Zones and Access Panels

Zone Access/Work location

160

Manpower Resources

Manhours 0.25

Minimum number of person 1

Subtask elapsed time 0.25

Skills AIRFRAME

Material necessary to do the job

Reidentified part set REIDD05

ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE

NOTES

F5348633920000 PANEL F5348612320400

Reidentify the potable water service panel:

1 Panel F5348612320400

becomes

1 Panel F5348633920000

NOTE: Mark the new P/N on the panel with a permanent marker.

(10) Subtask 523086-820-201-001 - Adjust the new potable water service panel access

door

Work Zones and Access Panels

Zone Access/Work location

160

Manpower Resources

Manhours 0.75

Minimum number of person 1

Subtask elapsed time 0.75

Skills AIRFRAME

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 64

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@A330

SERVICE BULLETIN

Material necessary to do the job

Consumable CMLD10

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Threadlocking Adhesive -

Medium Strength

05BAE1 As required

Polysulfide Sealant-General

Purpose Fillet

06AAB1 As required

Non Aqueous CleanerGeneral08BAA9 As required

Release Agent - Liquid Wax 14DBB1 As required

Wire-Locking Dia: 0.5 Mm

(0.020 Inch) Cres Nickel

14QDB1 As required

Textile-Lint Free Cotton 14SBA1 As required

References

Aircraft Maintenance Manual (AMM) Task 38-10-00-820-801

Fig. A-GBCAA

Adjustment of the potable water service

panel access door

Sheet 01

Sheet 02

Sheet 03

Sheet 04

(a) Open the door, item 2, and lock all latches. Adjust all adjustment bolts to a gap of

6.5 mm (0.26 in) to the door as shown on Fig. A-GBCAA Sheet 01, Fig. A-GBCAA

Sheet 02 and Fig. A-GBCAA Sheet 03, section A-A.

(b) Close the door, item 2, and lock all latches. Check the gap between the door, item

2, and the structure. Open the door, item 2, and adjust all adjustment bolts to

achieve a gap of 0.8 mm (0.031 in) +/- 0.5mm (0.020 in), as shown on .Fig. AGBCAA Sheet 01, Fig. A-GBCAA Sheet 02 and Fig. A-GBCAA Sheet 04, section

B-B.

(c) Open the door, item 2, and clean the area to be sealed as shown on Fig. AGBCAA Sheet 01 and Fig. A-GBCAA Sheet 02 with:

Non Aqueous

Cleaner-General

08BAA9 As required

and

Textile-Lint Free

Cotton

14SBA1 As required

(d) Apply to the door, item 2, and to the structure as shown on Fig. A-GBCAA Sheet

01 and Fig. A-GBCAA Sheet 02:

Polysulfide SealantGeneral Purpose

Fillet

06AAB1 As required

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 65

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SERVICE BULLETIN

and

Release Agent -

Liquid Wax

14DBB1 As required

(e) Close the door, item 2, and lock all latches.

(f) Let the sealant cure.

(g) Remove the unwanted sealant from the door and from the fuselage skin.

(h) Clean the door and structure skin with:

Non Aqueous

Cleaner-General

08BAA9 As required

and

Textile-Lint Free

Cotton

14SBA1 As required

(i) Do the final adjustment of the door, item 2.

1 Check the gap between the door, item 2, and the structure.

2 Adjust the door, item 2, to the minimum possible gap between the door, item

2, and the structure by adjusting the adjustment bolts without putting tension

to the latches even when they are in locked position.

3 Ensure that:

- the latches snap in clearly noticeable and without delay

- the hand force necessary to lock the latches in the door closed position is

not larger as needed to lock the latches in the door open position

(j) Safety the adjustment bolt as follows:

1 If a latch with a drilled nut at the adjustment bolt is installed, safety the

adjustment bolt as shown on Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet

02 and Fig. A-GBCAA Sheet 03, section A-A, with:

Wire-Locking Dia:

0.5 Mm (0.020

Inch) Cres Nickel

14QDB1 As required

2 If a latch with a self-locking nut at the adjustment bolt is installed, safety the

adjustment bolt as shown on Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet

02 and Fig. A-GBCAA Sheet 03, section B-B, by tightening the self-locking nut

with a torque value of 4.0 Nm to 6.0 Nm (35.40 lbf.in to 53.10 lbf.in).

(k) Adjust the door switch as given in AMM Task 38-10-00-820-801.

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 66

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@A330

SERVICE BULLETIN

(l) Safety the door switch as shown on Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet

02 and Fig. A-GBCAA Sheet 04, View C, with:

Threadlocking

Adhesive - Medium

Strength

05BAE1 As required

(11) Subtask 523086-916-201-001 - Restore the aircraft surface protection

Work Zones and Access Panels

Zone Access/Work location

160

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills AIRFRAME

Material necessary to do the job

Consumable CMLD10

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Top Coat Polyurethane -

External Structure

04JAA3 As required

Aqueous Cleaner-Aircraft

Exterior Pressure Spray

08ABC1 As required

Corrosion Preventive

Compound-Water

Displacing Oil

12ABE2 As required

Textile-Lint Free Cotton 14SBA1 As required

References

Structural Repair Manual (SRM) 51-75-12

(a) Clean the potable water service panel access door with:

Aqueous CleanerAircraft Exterior

Pressure Spray

08ABC1 As required

and

Textile-Lint Free

Cotton

14SBA1 As required

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 67

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@A330

SERVICE BULLETIN

(b) Apply, in accordance with your aircraft color scheme:

Top Coat

Polyurethane -

External Structure

04JAA3 As required

to the outside area of the potable water service panel access door, refer to SRM

51-75-12.

(c) Inside the fuselage, clean the area of the potable water service panel and make

sure that the area is dirt free.

(d) Restore the surface protection of the inner fuselage skin with:

Corrosion

Preventive

Compound-Water

Displacing Oil

12ABE2 As required

(12) Subtask 523086-420-205-002 - Install the placard

Work Zones and Access Panels

Zone Access/Work location

160

Manpower Resources

Manhours 0.25

Minimum number of person 1

Subtask elapsed time 0.25

Skills AIRFRAME

Material necessary to do the job

Kit 523086D02R05

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

60 F1121009420000 1 PLACARD

Consumable CMLD10

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Varnish Polyurethane-Low

Voc - External Structure

04SBA3 As required

Non Aqueous CleanerGeneral08BAA9 As required

Textile-Lint Free Cotton 14SBA1 As required

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 68

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@A330

SERVICE BULLETIN

References

Fig. A-GBBAA

Installation of the potable water service

panel access door

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

(a) Clean the installation area of the placard, item 60, with:

Non Aqueous

Cleaner-General

08BAA9 As required

and

Textile-Lint Free

Cotton

14SBA1 As required

(b) Install, as shown on Fig. A-GBBAA Sheet 01, Fig. A-GBBAA Sheet 02 and Fig. AGBBAA Sheet 06, View L:

1 Placard F1121009420000 Item 60

(c) Apply to the placard for protection:

Varnish

Polyurethane-Low

Voc - External

Structure

04SBA3 As required

**CONF 003

(1) Subtask 523086-831-201-003 - Modify the potable water service panel access door

PN F5348614401000

Manpower Resources

Manhours 0.25

Minimum number of person 1

Subtask elapsed time 0.25

Skills NON SPECIFIC

Material necessary to do the job

Component COMPD04

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

6 A9249715920200 1 STUD

NOTE: The matset Comp 523086D04 is applicable only for operators which

have already matset Kit 523086D01R02, Kit 523086D02R02 or Kit

523086D03R02 on stock or which have already accomplished this

Service Bulletin at the original issue and have to do the additional work.

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 69

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@A330

SERVICE BULLETIN

NOTE: The above list of components is not an AIRBUS Kit, the required parts

shall be ordered as necessary through the given channel.

Reidentified part set REIDD09

ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE

NOTES

F5348614401600 DOOR F5348614401000

NOTE: The part set Reid 523086D09 is to be used only for operators which

have already matset Kit 523086D03R02 on stock or which have already

accomplished this Service Bulletin at the original issue and have to do

the additional work.

References

Fig. A-GBDAA

Additional work - Modification of the

potable water service panel access door

Sheet 01

Sheet 02

Sheet 03

NOTE: All operator, which have already matset Kit 523086D03R02 on stock,

have to modify the Door Assy, delivered with the matset Kit

523086D03R02, following the subsequent worksteps.

Otherwise continue with SUBTASK 523086-020-201 003 Remove the

potable water service panel access door .

(a) If you have the matset Kit 523086D03 with revision 02, then on bench, remove

from the Door Assy, PN F5348614401000, as shown on Fig. A-GBDAA Sheet 01,

Fig. A-GBDAA Sheet 02 and Fig. A-GBDAA Sheet 03, View C:

1 Stud-Adjusting Item (4) Discard

1 Nut Item (3) Retain

(b) Install to the Door Assy, PN F5348614401000, as shown on Fig. A-GBDAA Sheet

01, Fig. A-GBDAA Sheet 02 and Fig. A-GBDAA Sheet 03, View C:

1 Nut Item (3) Retained at

removal

1 Stud-Adjusting A9249715920200 Item 6

(c) Reidentify the potable water service panel access door:

1 Door Assy F5348614401000

becomes

1 Door Assy F5348614401600

NOTE: Mark the new P/N on the Door Assy with a permanent marker.

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 70

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SERVICE BULLETIN

(2) Subtask 523086-020-201-003 - Remove the potable water service panel access

door

Work Zones and Access Panels

Zone Access/Work location

160

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills AIRFRAME

References

Fig. A-GBAAA

Removal of the potable water service

panel access door

Sheet 01

Sheet 02

Sheet 03

Sheet 04

(a) From the door, as shown on Fig. A-GBAAA Sheet 01, Fig. A-GBAAA Sheet 02 and

Fig. A-GBAAA Sheet 03, View C remove:

1 Nut Item (12) Discard

2 Washer Item (14) Discard

1 Screw Item (8) Discard

and disconnect

1 Bonding lead Item (10) Retain

(b) Remove, as shown on Fig. A-GBAAA Sheet 01, Fig. A-GBAAA Sheet 02 and Fig.

A-GBAAA Sheet 03, View D:

8 Nut Item (12) Discard

8 Washer Item (14) Discard

8 Screw Item (16) Discard

1 Door Assy F5348614400800 Item (2) Discard

(c) Remove, as shown on Fig. A-GBAAA Sheet 01, Fig. A-GBAAA Sheet 02 and Fig.

A-GBAAA Sheet 03, View D:

4 Bolt Item (20) Discard

4 Washer Item (22) Discard

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 71

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SERVICE BULLETIN

2 Hinge Item (24) Discard

2 Spring Item (26) Discard

2 Shim Item (28) Discard

(3) Subtask 523086-020-202-001 - Remove the fittings and the anchor nuts

Work Zones and Access Panels

Zone Access/Work location

160

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills AIRFRAME

References

Fig. A-GBAAA

Removal of the potable water service

panel access door

Sheet 01

Sheet 02

Sheet 03

Sheet 04

(a) Remove, as shown on Fig. A-GBAAA Sheet 01, Fig. A-GBAAA Sheet 02 and Fig.

A-GBAAA Sheet 04, View F:

4 Collar Item (30) Discard

4 Pin Item (32) Discard

2 Fitting Item (34) Discard

(b) Remove, as shown on Fig. A-GBAAA Sheet 01, Fig. A-GBAAA Sheet 03 and Fig.

A-GBAAA Sheet 04, View E:

8 Rivet Item (50) Discard

4 Anchor nut Item (52) Discard

(4) Subtask 523086-420-201-003 - Install the new anchor nuts

Work Zones and Access Panels

Zone Access/Work location

160

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 72

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SERVICE BULLETIN

Manpower Resources

Manhours 1.00

Minimum number of person 2

Subtask elapsed time 0.50

Skills AIRFRAME

Material necessary to do the job

Kit 523086D03R04

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

50 NSA5414N24-10 16 RIVET

52 NAS1474R4K 4 NUT

54 F5348615620600 2 SHIM

Consumable CMLD10

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Coating - Flexible Structure 04QAB2 As required

Polysulfide Sealant-General

Purpose Brushable

06AAA1 As required

Polysulfide Sealant-General

Purpose Fillet

06AAB1 As required

Non Aqueous CleanerGeneral08BAA9 As required

Textile-Lint Free Cotton 14SBA1 As required

References

Structural Repair Manual (SRM) 51-24-00

51-44-00

51-46-00

Fig. A-GBBAA

Installation of the potable water service

panel access door

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

(a) Put the Shims, item 54, in position as shown on Fig. A-GBBAA Sheet 01, Fig. AGBBAA Sheet 04 and Fig. A-GBBAA Sheet 05, View G.

(b) Transfer drill the existing rivet holes to the Shims, item 54, as shown on Fig. AGBBAA Sheet 01, Fig. A-GBBAA Sheet 04 and Fig. A-GBBAA Sheet 05, View G

and in accordance with SRM 51-44-00.

(c) Temporarily install the Shims, item 54, to the structure with set screws.

(d) Drill the new rivet holes using the Anchor nut, item 52, as shown on Fig. A-GBBAA

Sheet 01, Fig. A-GBBAA Sheet 04, Fig. A-GBBAA Sheet 05, View G and H and

Fig. A-GBBAA Sheet 06, View J and in accordance with SRM 51-44-00.

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 73

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SERVICE BULLETIN

(e) Drill the existing holes to a diameter of 6.8 mm (0.27 in) as shown on Fig. AGBBAA Sheet 01, Fig. A-GBBAA Sheet 04 and Fig. A-GBBAA Sheet 05, section EE.

(f) Remove the Shims, item 54, and deburr all drilled holes.

(g) Countersink where necessary the rivet holes with a 100 ̊ countersink drill as shown

on Fig. A-GBBAA Sheet 05, section D-D and section E-E and in accordance with

SRM 51-46-00.

(h) Clean the installation area and the Shims, item 54, with:

Non Aqueous

Cleaner-General

08BAA9 As required

and

Textile-Lint Free

Cotton

14SBA1 As required

(i) Install, as shown on Fig. A-GBBAA Sheet 01, Fig. A-GBBAA Sheet 04 and Fig. AGBBAA Sheet 05, View G:

2 Shim F5348615620600 Item 54

and, with:

Polysulfide SealantGeneral Purpose

Fillet

06AAB1 As required

8 Rivet NSA5414N24-10 Item 50

NOTE: Cut the rivets to the necessary length.

(j) Install, as shown on Fig. A-GBBAA Sheet 01, Fig. A-GBBAA Sheet 04 and Fig. AGBBAA Sheet 05, View H:

4 Anchor Nut NAS1474R4K Item 52

with:

8 Rivet NSA5414N24-10 Item 50

NOTE: Cut the rivets to the necessary length.

(k) Apply to the Shim, item 54, the Anchor Nut, item 52 and the rivets, item 50, as

shown on Fig. A-GBBAA Sheet 01, Fig. A-GBBAA Sheet 04 and Fig. A-GBBAA

Sheet 05, View G and H, section D-D and E-E, and in accordance with SRM

51-24-00:

Polysulfide SealantGeneral Purpose

Brushable

06AAA1 As required

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 74

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SERVICE BULLETIN

(l) Let the sealant cure.

(m) Apply to the sealed areas:

Coating - Flexible

Structure

04QAB2 As required

(5) Subtask 523086-420-202-003 - Install the new hinges

Work Zones and Access Panels

Zone Access/Work location

160

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills AIRFRAME

Material necessary to do the job

Kit 523086D03R04

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

20 NAS1801-4-9 4 SCREW

22 NAS1149C0432R 4 WASHER

24 F5348615700600 2 HINGE

26 F5348615520400 2 SPRING

28 F5348615620400 4 SHIM (1)

NOTE (1): A maximum of 4 shims necessary only if the hinges have to be adjusted.

Consumable CMLD10

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Non Aqueous CleanerGeneral08BAA9 As required

Textile-Lint Free Cotton 14SBA1 As required

References

Fig. A-GBBAA

Installation of the potable water service

panel access door

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 75

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SERVICE BULLETIN

(a) Clean the area where the hinges will be installed with:

Non Aqueous

Cleaner-General

08BAA9 As required

and

Textile-Lint Free

Cotton

14SBA1 As required

(b) Install, as shown on Fig. A-GBBAA Sheet 01, Fig. A-GBBAA Sheet 02 and Fig. AGBBAA Sheet 04, View F:

2 Spring F5348615520400 Item 26

2 Hinge Assy F5348615700600 Item 24

with

4 Washer NAS1149C0432R Item 22

4 Screw NAS1801-4-9 Item 20

(c) Check the alignment of the hinges.

1 Carefully bring the hinges, item 24, in the closed position as shown on Fig. AGBBAA Sheet 01, Fig. A-GBBAA Sheet 02 and Fig. A-GBBAA Sheet 04,

section C-C.

2 Make sure that the contour of the structure and the hinges are level and there

are no steps as shown on Fig. A-GBBAA Sheet 01, Fig. A-GBBAA Sheet 02

and Fig. A-GBBAA Sheet 04, section C-C.

3 To adjust the hinges install, if necessary:

4 Shim F5348615620400 Item 28

NOTE: A maximum of two shims, item 28, per hinge are allowed.

(d) Tighten the screws, item 20, with a torque value of 8.2 Nm to 10.6 Nm (72.58 lbf.in

to 93.82 lbf.in).

(6) Subtask 523086-420-206-003 - Install the potable water service panel access door

PN F5348614401600

Work Zones and Access Panels

Zone Access/Work location

160

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 76

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SERVICE BULLETIN

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills AIRFRAME

Material necessary to do the job

Kit 523086D03R04

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

2 F5348614401600 1 DOOR

12 NAS1291C3M 8 NUT

14 NAS1149C0332R 8 WASHER

16 NAS1102E3-8 8 SCREW

References

Fig. A-GBBAA

Installation of the potable water service

panel access door

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

Fig. A-GBCAA

Adjustment of the potable water service

panel access door

Sheet 01

Sheet 02

Sheet 03

Sheet 04

(a) Install, as shown on Fig. A-GBBAA Sheet 01, Fig. A-GBBAA Sheet 02 and Fig. AGBBAA Sheet 04, View F:

1 Door Assy F5348614401600 Item 2

with

8 Screw NAS1102E3-8 Item 16

8 Washer NAS1149C0332R Item 14

8 Nut NAS1291C3M Item 12

(b) Close and adjust the door, item 2, to achieve a circumferential gap as shown on

Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet 02 and Fig. A-GBCAA Sheet 04,

section C-C.

(c) Tighten the screws, item 16, with a torque value of 3.7 Nm to 4.8 Nm (32.75 lbf.in

to 42.48 lbf.in).

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 77

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SERVICE BULLETIN

(7) Subtask 523086-420-203-003 - Install the new fittings

Work Zones and Access Panels

Zone Access/Work location

160

Manpower Resources

Manhours 2.00

Minimum number of person 2

Subtask elapsed time 1.00

Skills AIRFRAME

Material necessary to do the job

Kit 523086D03R04

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

30 NSA5075-5 9 COLLAR

32 DAN6-5-4 9 PIN

34 F5348614120200 2 FITTING

35 F5348614120400 1 FITTING

Consumable CMLD10

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Coating - Flexible Structure 04QAB2 As required

Polysulfide Sealant-General

Purpose Brushable

06AAA1 As required

Non Aqueous CleanerGeneral08BAA9 As required

Textile-Lint Free Cotton 14SBA1 As required

References

Structural Repair Manual (SRM) 51-24-00

51-44-00

51-46-00

Fig. A-GBBAA

Installation of the potable water service

panel access door

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

(a) Install the fittings, item 34, using the existing rivet holes, to the structure with set

screws as shown on Fig. A-GBBAA Sheet 01, Fig. A-GBBAA Sheet 02 and Fig. AGBBAA Sheet 03, View E.

(b) Mark the position of the new rivet holes.

(c) Drill the new rivet holes in the structure through the pilot hole.

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 78

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SERVICE BULLETIN

(d) Increase the hole diameter to the correct size for the given fasteners in accordance

with SRM 51-44-00.

(e) Remove the fittings, item 34.

(f) Deburr the fastener holes.

(g) Countersink the holes of the fittings, item 34, with a 100 ̊ countersink drill in

accordance with SRM 51-46-00.

(h) Clean the installation area of the fittings, item 34, with:

Non Aqueous

Cleaner-General

08BAA9 As required

and

Textile-Lint Free

Cotton

14SBA1 As required

(i) Install, as shown on Fig. A-GBBAA Sheet 01, Fig. A-GBBAA Sheet 02 and Fig. AGBBAA Sheet 03, View E:

2 Fitting F5348614120200 Item 34

with

6 Pin-Rivet DAN6-5-4 Item 32

6 Collar NSA5075-5 Item 30

(j) Mark the position of the fitting, item 35, to the structure as shown on Fig. A-GBBAA

Sheet 01, Fig. A-GBBAA Sheet 02 and Fig. A-GBBAA Sheet 03, View C, D and

section A-A.

(k) Carefully close the door, item 2, and check that the center line of the fitting, item

35, is in line with the center line of the latch.

(l) Open the door, item 2.

(m) If necessary, correct the position of the fitting, item 35, to make sure that the latch

of the door, item 2, engages correctly.

(n) Mark the position of the rivet holes.

(o) Drill the rivet holes in the structure.

(p) Increase the hole diameter to the correct size for the given fasteners in accordance

with SRM 51-44-00.

(q) Remove the fitting, item 35.

(r) Deburr the fastener holes.

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 79

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(s) Countersink the holes of the fitting, item 35, with a 100 ̊ countersink drill in

accordance with SRM 51-46-00.

(t) Clean the installation area of the fitting, item 35, with:

Non Aqueous

Cleaner-General

08BAA9 As required

and

Textile-Lint Free

Cotton

14SBA1 As required

(u) Install, as shown on Fig. A-GBBAA Sheet 01, Fig. A-GBBAA Sheet 02 and Fig. AGBBAA Sheet 03, View C, D and section A-A:

1 Fitting F5348614120400 Item 35

with

3 Pin-Rivet DAN6-5-4 Item 32

3 Collar NSA5075-5 Item 30

(v) Apply to the Fittings, item 34 and 35, the Pin-Rivet, item 32 and the Collar, item 30,

in accordance with SRM 51-24-00:

Polysulfide SealantGeneral Purpose

Brushable

06AAA1 As required

(w) Let the sealant cure.

(x) Apply to the sealed areas:

Coating - Flexible

Structure

04QAB2 As required

(8) Subtask 523086-420-204-003 - Install the bonding lead

Work Zones and Access Panels

Zone Access/Work location

160

Manpower Resources

Manhours 0.25

Minimum number of person 1

Subtask elapsed time 0.25

Skills AIRFRAME

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 80

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SERVICE BULLETIN

Material necessary to do the job

Kit 523086D03R04

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

8 NAS1100-3-7 1 SCREW

12 NAS1291C3M 1 NUT

14 NAS1149C0332R 2 WASHER

Consumable CMLD10

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Varnish - Electrical Bonding

Structure

04TMB2 As required

Non Aqueous CleanerGeneral08BAA9 As required

Textile-Lint Free Cotton 14SBA1 As required

References

Aircraft Maintenance Manual (AMM) Task 20-28-00-912-802

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

Fig. A-GBBAA

Installation of the potable water service

panel access door

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

(a) Clean the bonding points, as given in AMM Task 20-28-00-912-802 and ESPM

20-51-20, with:

Non Aqueous

Cleaner-General

08BAA9 As required

and

Textile-Lint Free

Cotton

14SBA1 As required

(b) Install, as shown on Fig. A-GBBAA Sheet 01, Fig. A-GBBAA Sheet 02 and Fig. AGBBAA Sheet 06, View K:

1 Bonding lead Item (10) Retained at

removal

with

1 Screw NAS1100-3-7 Item 8

2 Washer NAS1149C0332R Item 14

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 81

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SERVICE BULLETIN

1 Nut NAS1291C3M Item 12

(c) Apply to the bonding points as given in AMM Task 20-28-00-912-802:

Varnish - Electrical

Bonding Structure

04TMB2 As required

(9) Subtask 523086-930-201-002 - Reidentify the potable water service panel

Work Zones and Access Panels

Zone Access/Work location

160

Manpower Resources

Manhours 0.25

Minimum number of person 1

Subtask elapsed time 0.25

Skills AIRFRAME

Material necessary to do the job

Reidentified part set REIDD06

ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE

NOTES

F5348634020000 PANEL F5348612320400

Reidentify the potable water service panel:

1 Panel F5348612320400

becomes

1 Panel F5348634020000

NOTE: Mark the new P/N on the panel with a permanent marker.

(10) Subtask 523086-820-201-001 - Adjust the new potable water service panel access

door

Work Zones and Access Panels

Zone Access/Work location

160

Manpower Resources

Manhours 0.75

Minimum number of person 1

Subtask elapsed time 0.75

Skills AIRFRAME

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 82

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SERVICE BULLETIN

Material necessary to do the job

Consumable CMLD10

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Threadlocking Adhesive -

Medium Strength

05BAE1 As required

Polysulfide Sealant-General

Purpose Fillet

06AAB1 As required

Non Aqueous CleanerGeneral08BAA9 As required

Release Agent - Liquid Wax 14DBB1 As required

Wire-Locking Dia: 0.5 Mm

(0.020 Inch) Cres Nickel

14QDB1 As required

Textile-Lint Free Cotton 14SBA1 As required

References

Aircraft Maintenance Manual (AMM) Task 38-10-00-820-801

Fig. A-GBCAA

Adjustment of the potable water service

panel access door

Sheet 01

Sheet 02

Sheet 03

Sheet 04

(a) Open the door, item 2, and lock all latches. Adjust all adjustment bolts to a gap of

6.5 mm (0.26 in) to the door as shown on Fig. A-GBCAA Sheet 01, Fig. A-GBCAA

Sheet 02 and Fig. A-GBCAA Sheet 03, section A-A.

(b) Close the door, item 2, and lock all latches. Check the gap between the door, item

2, and the structure. Open the door, item 2, and adjust all adjustment bolts to

achieve a gap of 0.8 mm (0.031 in) +/- 0.5mm (0.020 in), as shown on .Fig. AGBCAA Sheet 01, Fig. A-GBCAA Sheet 02 and Fig. A-GBCAA Sheet 04, section

B-B.

(c) Open the door, item 2, and clean the area to be sealed as shown on Fig. AGBCAA Sheet 01 and Fig. A-GBCAA Sheet 02 with:

Non Aqueous

Cleaner-General

08BAA9 As required

and

Textile-Lint Free

Cotton

14SBA1 As required

(d) Apply to the door, item 2, and to the structure as shown on Fig. A-GBCAA Sheet

01 and Fig. A-GBCAA Sheet 02:

Polysulfide SealantGeneral Purpose

Fillet

06AAB1 As required

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 83

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SERVICE BULLETIN

and

Release Agent -

Liquid Wax

14DBB1 As required

(e) Close the door, item 2, and lock all latches.

(f) Let the sealant cure.

(g) Remove the unwanted sealant from the door and from the fuselage skin.

(h) Clean the door and structure skin with:

Non Aqueous

Cleaner-General

08BAA9 As required

and

Textile-Lint Free

Cotton

14SBA1 As required

(i) Do the final adjustment of the door, item 2.

1 Check the gap between the door, item 2, and the structure.

2 Adjust the door, item 2, to the minimum possible gap between the door, item

2, and the structure by adjusting the adjustment bolts without putting tension

to the latches even when they are in locked position.

3 Ensure that:

- the latches snap in clearly noticeable and without delay

- the hand force necessary to lock the latches in the door closed position is

not larger as needed to lock the latches in the door open position

(j) Safety the adjustment bolt as follows:

1 If a latch with a drilled nut at the adjustment bolt is installed, safety the

adjustment bolt as shown on Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet

02 and Fig. A-GBCAA Sheet 03, section A-A, with:

Wire-Locking Dia:

0.5 Mm (0.020

Inch) Cres Nickel

14QDB1 As required

2 If a latch with a self-locking nut at the adjustment bolt is installed, safety the

adjustment bolt as shown on Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet

02 and Fig. A-GBCAA Sheet 03, section B-B, by tightening the self-locking nut

with a torque value of 4.0 Nm to 6.0 Nm (35.40 lbf.in to 53.10 lbf.in).

(k) Adjust the door switch as given in AMM Task 38-10-00-820-801.

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 84

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SERVICE BULLETIN

(l) Safety the door switch as shown on Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet

02 and Fig. A-GBCAA Sheet 04, View C, with:

Threadlocking

Adhesive - Medium

Strength

05BAE1 As required

(11) Subtask 523086-916-201-001 - Restore the aircraft surface protection

Work Zones and Access Panels

Zone Access/Work location

160

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills AIRFRAME

Material necessary to do the job

Consumable CMLD10

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Top Coat Polyurethane -

External Structure

04JAA3 As required

Aqueous Cleaner-Aircraft

Exterior Pressure Spray

08ABC1 As required

Corrosion Preventive

Compound-Water

Displacing Oil

12ABE2 As required

Textile-Lint Free Cotton 14SBA1 As required

References

Structural Repair Manual (SRM) 51-75-12

(a) Clean the potable water service panel access door with:

Aqueous CleanerAircraft Exterior

Pressure Spray

08ABC1 As required

and

Textile-Lint Free

Cotton

14SBA1 As required

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 85

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@A330

SERVICE BULLETIN

(b) Apply, in accordance with your aircraft color scheme:

Top Coat

Polyurethane -

External Structure

04JAA3 As required

to the outside area of the potable water service panel access door, refer to SRM

51-75-12.

(c) Inside the fuselage, clean the area of the potable water service panel and make

sure that the area is dirt free.

(d) Restore the surface protection of the inner fuselage skin with:

Corrosion

Preventive

Compound-Water

Displacing Oil

12ABE2 As required

(12) Subtask 523086-420-205-003 - Install the placard

Work Zones and Access Panels

Zone Access/Work location

160

Manpower Resources

Manhours 0.25

Minimum number of person 1

Subtask elapsed time 0.25

Skills AIRFRAME

Material necessary to do the job

Kit 523086D03R04

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

60 F1121009420000 1 PLACARD

Consumable CMLD10

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Varnish Polyurethane-Low

Voc - External Structure

04SBA3 As required

Non Aqueous CleanerGeneral08BAA9 As required

Textile-Lint Free Cotton 14SBA1 As required

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 86

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@A330

SERVICE BULLETIN

References

Fig. A-GBBAA

Installation of the potable water service

panel access door

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

(a) Clean the installation area of the placard, item 60, with:

Non Aqueous

Cleaner-General

08BAA9 As required

and

Textile-Lint Free

Cotton

14SBA1 As required

(b) Install, as shown on Fig. A-GBBAA Sheet 01, Fig. A-GBBAA Sheet 02 and Fig. AGBBAA Sheet 06, View L:

1 Placard F1121009420000 Item 60

(c) Apply to the placard for protection:

Varnish

Polyurethane-Low

Voc - External

Structure

04SBA3 As required

**CONF ALL

D. TEST

**CONF 001

(1) Subtask 523086-700-201-001 - Operational

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 38-10-00-710-801

Do the operational test of the limit switches, refer to AMM Task 38-10-00-710-801.

**CONF 002

(1) Subtask 523086-700-201-001 - Operational

Manpower Resources

Skills NON SPECIFIC

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 87

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SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) Task 38-10-00-710-801

Do the operational test of the limit switches, refer to AMM Task 38-10-00-710-801.

**CONF 003

(1) Subtask 523086-700-201-001 - Operational

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 38-10-00-710-801

Do the operational test of the limit switches, refer to AMM Task 38-10-00-710-801.

**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 523086-942-201-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 24-41-00-862-801

Task 53-00-00-400-804

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

equipment.

(b) Install the removed Bulk Cargo Compartment floor panels, refer to AMM Task

53-00-00-400-804.

(c) Remove the access platform from below the potable water service panel access

door 164AR.

(d) De-energize the aircraft electrical circuits, refer to AMM Task 24-41-00-862-801.

**CONF 002

(1) Subtask 523086-942-201-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 88

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SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) Task 24-41-00-862-801

Task 53-00-00-400-804

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

equipment.

(b) Install the removed Bulk Cargo Compartment floor panels, refer to AMM Task

53-00-00-400-804.

(c) Remove the access platform from below the potable water service panel access

door 164AR.

(d) De-energize the aircraft electrical circuits, refer to AMM Task 24-41-00-862-801.

**CONF 003

(1) Subtask 523086-942-201-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 24-41-00-862-801

Task 53-00-00-400-804

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

equipment.

(b) Install the removed Bulk Cargo Compartment floor panels, refer to AMM Task

53-00-00-400-804.

(c) Remove the access platform from below the potable water service panel access

door 164AR.

(d) De-energize the aircraft electrical circuits, refer to AMM Task 24-41-00-862-801.

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 89

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@A330

SERVICE BULLETIN

This Page Intentionally Left Blank

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 90

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@A330

SERVICE BULLETIN

Task 523086-831-849-001 - Modification - ADDITIONAL WORK for aircraft modified by the

original issue

**CONF ALL

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

INCLUDED IN THE REFERENCED PROCEDURES.

CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP

ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY

AND MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENANCE

WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING,

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

THIS:

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

NECESSARY ON WIRING AND COMPONENTS.

REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND OTHER

CONTAMINATION.

THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION

AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION.

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

NOTE: The accomplishment instructions of this Service Bulletin refer to procedures

included in other AIRBUS documents. When the words ’refer to’ are used and the

operator has an accepted alternative procedure, the accepted alternative procedure

can be used. When the words ’in accordance with’ are included in the instruction,

the procedure in the AIRBUS document must be used.

NOTE: The access and close-up instructions, not comprising return to service tests, in this

Service Bulletin do not constitute or affect the technical intent of the Service

Bulletin. Operators can therefore, as deemed necessary, omit or add access and/or

close-up steps to add flexibility to their maintenance operations as long as the

technical intent of the Service Bulletin is met within the set parameters.

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

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

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

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

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

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

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

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

the aircraft can be put back into a serviceable condition.

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 91

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@A330

SERVICE BULLETIN

Task Associated Data

**CONF 001

Manpower

TOTAL MANHOURS 7.50

ELAPSED TIME (HOURS) 7.50

**CONF 002

Manpower

TOTAL MANHOURS 7.50

ELAPSED TIME (HOURS) 7.50

**CONF 003

Manpower

TOTAL MANHOURS 7.50

ELAPSED TIME (HOURS) 7.50

**CONF ALL

A. GENERAL

**CONF 001

(1) Subtask 523086-910-202-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

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

06-30-00, Page Block 001

06-31-53, Page Block 001

06-41-52, Page Block 001

06-41-53, Page Block 001

Consumable Material List (CML)

Standards Manual (SM)

(a) For the specification of the materials (Mat. No.) given in this Service Bulletin, refer

to the Consumable Materials List (CML).

(b) Refer to the AIRBUS Standards Manual (SM) if you find part numbers for the

hardware components in the related kit(s) which you cannot identify in the LIST OF

COMPONENTS of this Service Bulletin. The SM will give you the correct part

number to part number relationship.

(c) For the identification of zones, refer to AMM 06-20-00, Page Block 001.

(d) For the Frame (FR) identification, refer to AMM 06-31-53, Page Block 001.

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 92

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@A330

SERVICE BULLETIN

(e) For the location of the stringers (STGR), refer to AMM 06-30-00, Page Block 001.

(f) For the identification of access doors and panels, refer to AMM 06-41-52, Page

Block 001 and AMM 06-41-53, Page Block 001.

(2) Subtask 523086-839-202-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF 002

(1) Subtask 523086-910-202-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

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

06-30-00, Page Block 001

06-31-53, Page Block 001

06-41-52, Page Block 001

06-41-53, Page Block 001

Consumable Material List (CML)

Standards Manual (SM)

(a) For the specification of the materials (Mat. No.) given in this Service Bulletin, refer

to the Consumable Materials List (CML).

(b) Refer to the AIRBUS Standards Manual (SM) if you find part numbers for the

hardware components in the related kit(s) which you cannot identify in the LIST OF

COMPONENTS of this Service Bulletin. The SM will give you the correct part

number to part number relationship.

(c) For the identification of zones, refer to AMM 06-20-00, Page Block 001.

(d) For the Frame (FR) identification, refer to AMM 06-31-53, Page Block 001.

(e) For the location of the stringers (STGR), refer to AMM 06-30-00, Page Block 001.

(f) For the identification of access doors and panels, refer to AMM 06-41-52, Page

Block 001 and AMM 06-41-53, Page Block 001.

(2) Subtask 523086-839-202-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 93

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@A330

SERVICE BULLETIN

**CONF 003

(1) Subtask 523086-910-202-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

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

06-30-00, Page Block 001

06-31-53, Page Block 001

06-41-52, Page Block 001

06-41-53, Page Block 001

Consumable Material List (CML)

Standards Manual (SM)

(a) For the specification of the materials (Mat. No.) given in this Service Bulletin, refer

to the Consumable Materials List (CML).

(b) Refer to the AIRBUS Standards Manual (SM) if you find part numbers for the

hardware components in the related kit(s) which you cannot identify in the LIST OF

COMPONENTS of this Service Bulletin. The SM will give you the correct part

number to part number relationship.

(c) For the identification of zones, refer to AMM 06-20-00, Page Block 001.

(d) For the Frame (FR) identification, refer to AMM 06-31-53, Page Block 001.

(e) For the location of the stringers (STGR), refer to AMM 06-30-00, Page Block 001.

(f) For the identification of access doors and panels, refer to AMM 06-41-52, Page

Block 001 and AMM 06-41-53, Page Block 001.

(2) Subtask 523086-839-202-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF ALL

B. PREPARATION

**CONF 001

(1) Subtask 523086-941-202-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 94

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@A330

SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802

Task 24-41-00-861-801

Task 53-00-00-000-804

(a) The following items shall be considered as the basic Aircraft configuration before

you start a maintenance task:

- Aircraft on the ground resting on landing gear (the ground safety locks and the

wheel chocks are in position on the landing gear).

- Engine shut down, thrust reversers closed and locked.

- Aircraft in clean configuration.

- Parking brake applied.

- Aircraft electrical network de-energized.

- Hydraulic systems depressurized.

- Access to the cockpit and cabin is available.

- All circuit breakers are in closed position.

- All controls in NORM, AUTO or OFF position.

(b) Make sure that the aircraft is electrically grounded, refer to AMM Task

12-34-24-860-802.

(c) Energize the aircraft electrical circuits, refer to AMM Task 24-41-00-861-801.

(d) Put an access platform in position below the potable water service panel access

door 164AR.

(e) Remove the necessary Bulk Cargo Compartment floor panels to get access

to the inner area of the potable water service panel, refer to AMM Task

53-00-00-000-804.

**CONF 002

(1) Subtask 523086-941-202-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802

Task 24-41-00-861-801

Task 53-00-00-000-804

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 95

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@A330

SERVICE BULLETIN

(a) The following items shall be considered as the basic Aircraft configuration before

you start a maintenance task:

- Aircraft on the ground resting on landing gear (the ground safety locks and the

wheel chocks are in position on the landing gear).

- Engine shut down, thrust reversers closed and locked.

- Aircraft in clean configuration.

- Parking brake applied.

- Aircraft electrical network de-energized.

- Hydraulic systems depressurized.

- Access to the cockpit and cabin is available.

- All circuit breakers are in closed position.

- All controls in NORM, AUTO or OFF position.

(b) Make sure that the aircraft is electrically grounded, refer to AMM Task

12-34-24-860-802.

(c) Energize the aircraft electrical circuits, refer to AMM Task 24-41-00-861-801.

(d) Put an access platform in position below the potable water service panel access

door 164AR.

(e) Remove the necessary Bulk Cargo Compartment floor panels to get access

to the inner area of the potable water service panel, refer to AMM Task

53-00-00-000-804.

**CONF 003

(1) Subtask 523086-941-202-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802

Task 24-41-00-861-801

Task 53-00-00-000-804

(a) The following items shall be considered as the basic Aircraft configuration before

you start a maintenance task:

- Aircraft on the ground resting on landing gear (the ground safety locks and the

wheel chocks are in position on the landing gear).

- Engine shut down, thrust reversers closed and locked.

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 96

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@A330

SERVICE BULLETIN

- Aircraft in clean configuration.

- Parking brake applied.

- Aircraft electrical network de-energized.

- Hydraulic systems depressurized.

- Access to the cockpit and cabin is available.

- All circuit breakers are in closed position.

- All controls in NORM, AUTO or OFF position.

(b) Make sure that the aircraft is electrically grounded, refer to AMM Task

12-34-24-860-802.

(c) Energize the aircraft electrical circuits, refer to AMM Task 24-41-00-861-801.

(d) Put an access platform in position below the potable water service panel access

door 164AR.

(e) Remove the necessary Bulk Cargo Compartment floor panels to get access

to the inner area of the potable water service panel, refer to AMM Task

53-00-00-000-804.

**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 523086-831-202-001 - Modify the potable water service panel access door

PN F5348614401200

Manpower Resources

Manhours 0.25

Minimum number of person 1

Subtask elapsed time 0.25

Skills NON SPECIFIC

Material necessary to do the job

Component COMPD04

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

6 A9249715920200 1 STUD

NOTE: The matset Comp 523086D04 is applicable only for operators which

have already matset Kit 523086D01R02, Kit 523086D02R02 or Kit

523086D03R02 on stock or which have already accomplished this

Service Bulletin at the original issue and have to do the additional work.

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 97

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@A330

SERVICE BULLETIN

NOTE: The above list of components is not an AIRBUS Kit, the required parts

shall be ordered as necessary through the given channel.

Reidentified part set REIDD07

ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE

NOTES

F5348614401800 DOOR F5348614401200

NOTE: The part set Reid 523086D07 is to be used only for operators which

have already matset Kit 523086D01R02 on stock or which have already

accomplished this Service Bulletin at the original issue and have to do

the additional work.

Consumable CMLD10

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Threadlocking Adhesive -

Medium Strength

05BAE1 As required

References

Aircraft Maintenance Manual (AMM) Task 38-10-00-820-801

Fig. A-GBCAA

Adjustment of the potable water service

panel access door

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Fig. A-GBDAA

Additional work - Modification of the

potable water service panel access door

Sheet 01

Sheet 02

Sheet 03

(a) Open the potable water service panel access door.

(b) Check the PN of the Stud-Adjusting:

1 If the PN is A9249715920200 continue with step (e).

2 If the PN is NAS563C25 continue with step (c).

(c) Remove from the Door Assy, PN F5348614401200, as shown on Fig. A-GBDAA

Sheet 01, Fig. A-GBDAA Sheet 02 and Fig. A-GBDAA Sheet 03, View C:

1 Stud-Adjusting Item (4) Discard

1 Nut Item (3) Retain

(d) Install to the Door Assy, PN F5348614401200, as shown on Fig. A-GBDAA Sheet

01, Fig. A-GBDAA Sheet 02 and Fig. A-GBDAA Sheet 03, View D:

1 Nut Item (3) Retained at

removal

1 Stud-Adjusting A9249715920200 Item 6

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 98

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@A330

SERVICE BULLETIN

(e) Reidentify the potable water service panel access door:

1 Door Assy F5348614401200

becomes

1 Door Assy F5348614401800

NOTE: Mark the new P/N on the Door Assy with a permanent marker.

(f) Adjust the door switch as given in AMM Task 38-10-00-820-801.

(g) Safety the door switch as shown on Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet

02 and Fig. A-GBCAA Sheet 04, View C, with:

Threadlocking

Adhesive - Medium

Strength

05BAE1 As required

(2) Subtask 523086-831-203-001 - Apply sealant to the modified areas

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Consumable CMLD10

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Coating - Flexible Structure 04QAB2 As required

Polysulfide Sealant-General

Purpose Brushable

06AAA1 As required

Non Aqueous CleanerGeneral08BAA9 As required

Textile-Lint Free Cotton 14SBA1 As required

References

Structural Repair Manual (SRM) 51-24-00

Fig. A-GBEAA

Additional work - Application of the

sealant

Sheet 01

Sheet 02

Sheet 03

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 99

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@A330

SERVICE BULLETIN

(a) Apply sealant to the modified areas, as shown on Fig. A-GBEAA Sheet 01, Fig. AGBEAA Sheet 02 and Fig. A-GBEAA Sheet 03, view C, section A-A, B-B and C-C.

1 Clean the installation area of the Shim and the Anchor nut, with:

Non Aqueous

Cleaner-General

08BAA9 As required

and

Textile-Lint Free

Cotton

14SBA1 As required

2 Apply to the Shim, the Anchor Nut and the rivets, in accordance with SRM

51-24-00:

Polysulfide SealantGeneral Purpose

Brushable

06AAA1 As required

3 Clean the installation area of the fitting, with:

Non Aqueous

Cleaner-General

08BAA9 As required

and

Textile-Lint Free

Cotton

14SBA1 As required

4 Apply to the Fittings, the Pin-Rivet and the Collar, in accordance with SRM

51-24-00:

Polysulfide SealantGeneral Purpose

Brushable

06AAA1 As required

(b) Let the sealant cure.

(c) Apply to the sealed areas:

Coating - Flexible

Structure

04QAB2 As required

**CONF 002

(1) Subtask 523086-831-202-002 - Modify the potable water service panel access door

PN F5348614401400

Manpower Resources

Manhours 0.25

Minimum number of person 1

Subtask elapsed time 0.25

Skills NON SPECIFIC

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 100

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@A330

SERVICE BULLETIN

Material necessary to do the job

Component COMPD04

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

6 A9249715920200 1 STUD

NOTE: The matset Comp 523086D04 is applicable only for operators which

have already matset Kit 523086D01R02, Kit 523086D02R02 or Kit

523086D03R02 on stock or which have already accomplished this

Service Bulletin at the original issue and have to do the additional work.

NOTE: The above list of components is not an AIRBUS Kit, the required parts

shall be ordered as necessary through the given channel.

Reidentified part set REIDD08

ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE

NOTES

F5348614402000 DOOR F5348614401400

NOTE: The part set Reid 523086D08 is to be used only for operators which

have already matset Kit 523086D02R02 on stock or which have already

accomplished this Service Bulletin at the original issue and have to do

the additional work.

Consumable CMLD10

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Threadlocking Adhesive -

Medium Strength

05BAE1 As required

References

Aircraft Maintenance Manual (AMM) Task 38-10-00-820-801

Fig. A-GBCAA

Adjustment of the potable water service

panel access door

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Fig. A-GBDAA

Additional work - Modification of the

potable water service panel access door

Sheet 01

Sheet 02

Sheet 03

(a) Open the potable water service panel access door.

(b) Check the PN of the Stud-Adjusting:

1 If the PN is A9249715920200 continue with step (e).

2 If the PN is NAS563C25 continue with step (c).

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 101

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@A330

SERVICE BULLETIN

(c) Remove from the Door Assy, PN F5348614401400, as shown on Fig. A-GBDAA

Sheet 01, Fig. A-GBDAA Sheet 02 and Fig. A-GBDAA Sheet 03, View C:

1 Stud-Adjusting Item (4) Discard

1 Nut Item (3) Retain

(d) Install to the Door Assy, PN F5348614401400, as shown on Fig. A-GBDAA Sheet

01, Fig. A-GBDAA Sheet 02 and Fig. A-GBDAA Sheet 03, View D:

1 Nut Item (3) Retained at

removal

1 Stud-Adjusting A9249715920200 Item 6

(e) Reidentify the potable water service panel access door:

1 Door Assy F5348614401400

becomes

1 Door Assy F5348614402000

NOTE: Mark the new P/N on the Door Assy with a permanent marker.

(f) Adjust the door switch as given in AMM Task 38-10-00-820-801.

(g) Safety the door switch as shown on Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet

02 and Fig. A-GBCAA Sheet 04, View C, with:

Threadlocking

Adhesive - Medium

Strength

05BAE1 As required

(2) Subtask 523086-831-203-001 - Apply sealant to the modified areas

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Consumable CMLD10

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Coating - Flexible Structure 04QAB2 As required

Polysulfide Sealant-General

Purpose Brushable

06AAA1 As required

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 102

6

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@A330

SERVICE BULLETIN

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Non Aqueous CleanerGeneral08BAA9 As required

Textile-Lint Free Cotton 14SBA1 As required

References

Structural Repair Manual (SRM) 51-24-00

Fig. A-GBEAA

Additional work - Application of the

sealant

Sheet 01

Sheet 02

Sheet 03

(a) Apply sealant to the modified areas, as shown on Fig. A-GBEAA Sheet 01, Fig. AGBEAA Sheet 02 and Fig. A-GBEAA Sheet 03, view C, section A-A, B-B and C-C.

1 Clean the installation area of the Shim and the Anchor nut, with:

Non Aqueous

Cleaner-General

08BAA9 As required

and

Textile-Lint Free

Cotton

14SBA1 As required

2 Apply to the Shim, the Anchor Nut and the rivets, in accordance with SRM

51-24-00:

Polysulfide SealantGeneral Purpose

Brushable

06AAA1 As required

3 Clean the installation area of the fitting, with:

Non Aqueous

Cleaner-General

08BAA9 As required

and

Textile-Lint Free

Cotton

14SBA1 As required

4 Apply to the Fittings, the Pin-Rivet and the Collar, in accordance with SRM

51-24-00:

Polysulfide SealantGeneral Purpose

Brushable

06AAA1 As required

(b) Let the sealant cure.

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 103

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@A330

SERVICE BULLETIN

(c) Apply to the sealed areas:

Coating - Flexible

Structure

04QAB2 As required

**CONF 003

(1) Subtask 523086-831-202-003 - Modify the potable water service panel access door

PN F5348614401000

Manpower Resources

Manhours 0.25

Minimum number of person 1

Subtask elapsed time 0.25

Skills NON SPECIFIC

Material necessary to do the job

Component COMPD04

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

6 A9249715920200 1 STUD

NOTE: The matset Comp 523086D04 is applicable only for operators which

have already matset Kit 523086D01R02, Kit 523086D02R02 or Kit

523086D03R02 on stock or which have already accomplished this

Service Bulletin at the original issue and have to do the additional work.

NOTE: The above list of components is not an AIRBUS Kit, the required parts

shall be ordered as necessary through the given channel.

Reidentified part set REIDD09

ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE

NOTES

F5348614401600 DOOR F5348614401000

NOTE: The part set Reid 523086D09 is to be used only for operators which

have already matset Kit 523086D03R02 on stock or which have already

accomplished this Service Bulletin at the original issue and have to do

the additional work.

Consumable CMLD10

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Threadlocking Adhesive -

Medium Strength

05BAE1 As required

References

Aircraft Maintenance Manual (AMM) Task 38-10-00-820-801

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 104

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@A330

SERVICE BULLETIN

References

Fig. A-GBCAA

Adjustment of the potable water service

panel access door

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Fig. A-GBDAA

Additional work - Modification of the

potable water service panel access door

Sheet 01

Sheet 02

Sheet 03

(a) Open the potable water service panel access door.

(b) Check the PN of the Stud-Adjusting:

1 If the PN is A9249715920200 continue with step (e).

2 If the PN is NAS563C25 continue with step (c).

(c) Remove from the Door Assy, PN F5348614401000, as shown on Fig. A-GBDAA

Sheet 01, Fig. A-GBDAA Sheet 02 and Fig. A-GBDAA Sheet 03, View C:

1 Stud-Adjusting Item (4) Discard

1 Nut Item (3) Retain

(d) Install to the Door Assy, PN F5348614401000, as shown on Fig. A-GBDAA Sheet

01, Fig. A-GBDAA Sheet 02 and Fig. A-GBDAA Sheet 03, View D:

1 Nut Item (3) Retained at

removal

1 Stud-Adjusting A9249715920200 Item 6

(e) Reidentify the potable water service panel access door:

1 Door Assy F5348614401000

becomes

1 Door Assy F5348614401600

NOTE: Mark the new P/N on the Door Assy with a permanent marker.

(f) Adjust the door switch as given in AMM Task 38-10-00-820-801.

(g) Safety the door switch as shown on Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet

02 and Fig. A-GBCAA Sheet 04, View C, with:

Threadlocking

Adhesive - Medium

Strength

05BAE1 As required

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 105

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@A330

SERVICE BULLETIN

(2) Subtask 523086-831-203-001 - Apply sealant to the modified areas

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Consumable CMLD10

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Coating - Flexible Structure 04QAB2 As required

Polysulfide Sealant-General

Purpose Brushable

06AAA1 As required

Non Aqueous CleanerGeneral08BAA9 As required

Textile-Lint Free Cotton 14SBA1 As required

References

Structural Repair Manual (SRM) 51-24-00

Fig. A-GBEAA

Additional work - Application of the

sealant

Sheet 01

Sheet 02

Sheet 03

(a) Apply sealant to the modified areas, as shown on Fig. A-GBEAA Sheet 01, Fig. AGBEAA Sheet 02 and Fig. A-GBEAA Sheet 03, view C, section A-A, B-B and C-C.

1 Clean the installation area of the Shim and the Anchor nut, with:

Non Aqueous

Cleaner-General

08BAA9 As required

and

Textile-Lint Free

Cotton

14SBA1 As required

2 Apply to the Shim, the Anchor Nut and the rivets, in accordance with SRM

51-24-00:

Polysulfide SealantGeneral Purpose

Brushable

06AAA1 As required

3 Clean the installation area of the fitting, with:

Non Aqueous

Cleaner-General

08BAA9 As required

and

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 106

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SERVICE BULLETIN

Textile-Lint Free

Cotton

14SBA1 As required

4 Apply to the Fittings, the Pin-Rivet and the Collar, in accordance with SRM

51-24-00:

Polysulfide SealantGeneral Purpose

Brushable

06AAA1 As required

(b) Let the sealant cure.

(c) Apply to the sealed areas:

Coating - Flexible

Structure

04QAB2 As required

**CONF ALL

D. TEST

**CONF 001

(1) Subtask 523086-700-202-001 - Testing

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 38-10-00-710-801

Do the operational test of the limit switches, refer to AMM Task 38-10-00-710-801.

**CONF 002

(1) Subtask 523086-700-202-001 - Testing

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 38-10-00-710-801

Do the operational test of the limit switches, refer to AMM Task 38-10-00-710-801.

**CONF 003

(1) Subtask 523086-700-202-001 - Testing

Manpower Resources

Skills NON SPECIFIC

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 107

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SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) Task 38-10-00-710-801

Do the operational test of the limit switches, refer to AMM Task 38-10-00-710-801.

**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 523086-942-202-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 24-41-00-862-801

Task 53-00-00-400-804

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

equipment.

(b) Install the removed Bulk Cargo Compartment floor panels, refer to AMM Task

53-00-00-400-804.

(c) Remove the access platform from below the potable water service panel access

door 164AR.

(d) De-energize the aircraft electrical circuits, refer to AMM Task 24-41-00-862-801.

**CONF 002

(1) Subtask 523086-942-202-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 24-41-00-862-801

Task 53-00-00-400-804

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

equipment.

(b) Install the removed Bulk Cargo Compartment floor panels, refer to AMM Task

53-00-00-400-804.

(c) Remove the access platform from below the potable water service panel access

door 164AR.

(d) De-energize the aircraft electrical circuits, refer to AMM Task 24-41-00-862-801.

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 108

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@A330

SERVICE BULLETIN

**CONF 003

(1) Subtask 523086-942-202-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 24-41-00-862-801

Task 53-00-00-400-804

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

equipment.

(b) Install the removed Bulk Cargo Compartment floor panels, refer to AMM Task

53-00-00-400-804.

(c) Remove the access platform from below the potable water service panel access

door 164AR.

(d) De-energize the aircraft electrical circuits, refer to AMM Task 24-41-00-862-801.

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 109

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@A330

SERVICE BULLETIN

**CONF ALL

G_SB_523086_6_BAAA_01_00

FR70

FR69

164AR

Z160

A

B

A

Figure A-GBAAA - Sheet 01

Removal of the potable water service panel access door

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 110

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@A330

SERVICE BULLETIN

**CONF ALL

(2)

POTABLE WATER

FR69

FR70

STGR50RH

B

SERVICE DOOR

164AR

F

F

C

D

D

G_SB_523086_6_BAAA_02_01

Figure A-GBAAA - Sheet 02

Removal of the potable water service panel access door

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 111

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@A330

SERVICE BULLETIN

**CONF ALL

(12)

(14)

(10)

(14)

(8)

(2)

C

D

(2)

(26)

(28)

(22)

(20)

(24)

(4 POS)

(4 POS)

(4 POS)

(16)

(14)

(12)

E

G_SB_523086_6_BAAA_03_00

Figure A-GBAAA - Sheet 03

Removal of the potable water service panel access door

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 112

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@A330

SERVICE BULLETIN

**CONF ALL

(34)

(30)

(32)

(52)

E (50)

F

G_SB_523086_6_BAAA_04_00

Figure A-GBAAA - Sheet 04

Removal of the potable water service panel access door

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 113

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@A330

SERVICE BULLETIN

**CONF ALL

FR70

FR69

164AR

Z160

A

B

A

G_SB_523086_6_BBAA_01_00

Figure A-GBBAA - Sheet 01

Installation of the potable water service panel access door

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 114

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@A330

SERVICE BULLETIN

**CONF ALL

2

NEW 

POTABLE WATER

FR69

FR70

STGR50RH

B

SERVICE DOOR

164AR

C

E

F E

F

L

K

NOTE:

01 OPTIONAL SOLUTION NOT SHOWN

01

TYPICAL

G_SB_523086_6_BBAA_02_02

Figure A-GBBAA - Sheet 02

Installation of the potable water service panel access door

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 115

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@A330

SERVICE BULLETIN

**CONF ALL

226.0 mm

(8.90 in)

D

35

32

30

D

FWD 3.5 mm 

(0.14 in)

35

C

34

32

30

E

02

NOTE:

02 USE EXISTING RIVET HOLES

03 04 03 04

03 APPLY SEALANT (MAT.NO.06AAA1)

04 APPLY COATING (MAT.NO.04QAB2)

FWD

34

03 04 03 04

B

B

B B

A A

A

A

G_SB_523086_6_BBAA_03_04

Figure A-GBBAA - Sheet 03

Installation of the potable water service panel access door

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 116

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@A330

SERVICE BULLETIN

**CONF ALL

2

26

28

22

20

24

F

G

07

07 USE IF NECESSARY FOR ADJUSTMENT

08

08 TORQUE VALUE = 8.2 Nm TO 10.6 Nm

(72.58 lbf.in TO 93.82 lbf.in)

(4 POS)

(4 POS)

(4 POS)

16

14

12

09

09 TORQUE VALUE = 3.7 Nm TO 4.8 Nm

(32.75 lbf.in TO 42.48 lbf.in)

24

06 HINGE SHOWN IN CLOSED POSITION

05

NOTE:

05 MAKE SURE THAT THE CONTOUR OF THE STRUCTURE

06

AND THE HINGES ARE LEVEL AND THERE ARE NO STEPS.

C

C

C C

G_SB_523086_6_BBAA_04_02

Figure A-GBBAA - Sheet 04

Installation of the potable water service panel access door

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 117

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@A330

SERVICE BULLETIN

**CONF ALL

NOTE:

50

52

50

54

54

G 10

H

H

J

6.8 mm DIA

(0.27 in)

54

50

54

50

50

52

03 04

03 APPLY SEALANT (MAT.NO.06AAA1)

04 APPLY COATING (MAT.NO.04QAB2)

03 04 03 04

D D

E E

D D

E E

10 APPLY SEALANT (MAT.NO.06AAB1)

G_SB_523086_6_BBAA_05_04

Figure A-GBBAA - Sheet 05

Installation of the potable water service panel access door

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 118

6

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@A330

SERVICE BULLETIN

**CONF ALL

54

52 52

J FWD

39° 39°

12

14

(10)

14

8

2

K

2 60

L FWD OUTSIDE PANEL DOOR

= =

= =

G_SB_523086_6_BBAA_06_01

Figure A-GBBAA - Sheet 06

Installation of the potable water service panel access door

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 119

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@A330

SERVICE BULLETIN

**CONF ALL

FR70

FR69

164AR

Z160

A

B

A

G_SB_523086_6_BCAA_01_00

Figure A-GBCAA - Sheet 01

Adjustment of the potable water service panel access door

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 120

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@A330

SERVICE BULLETIN

**CONF ALL

FR69

FR70

STGR50RH

B

02

03

02

03

NOTE:

01 OPTIONAL SOLUTION NOT SHOWN

01

TYPICAL

A

A

A

A

B

B

B

B

C

C

APPLY RELEASE AGENT (MAT.NO. 14DBB1) 

APPLY SEALANT (MAT.NO. 06AAB1)

B

B A

A

C

G_SB_523086_6_BCAA_02_02

Figure A-GBCAA - Sheet 02

Adjustment of the potable water service panel access door

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 121

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@A330

SERVICE BULLETIN

**CONF ALL

6.5 mm

(0.26 in)

04

2

A A

6.5 mm

(0.26 in)

2

SECURE WITH LOCK WIRE (MAT. NO.14QDB1)

NOTE:

04

B B

05

05 TORQUE VALUE = 4.0 Nm TO 6.0 Nm (35.40 lbf.in TO 53.10 lbf.in)

164AR

164AR

G_SB_523086_6_BCAA_03_04

Figure A-GBCAA - Sheet 03

Adjustment of the potable water service panel access door

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 122

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SERVICE BULLETIN

**CONF ALL

NOTE:

07 ADJUST THE POTABLE WATER SERVICE DOOR, SO THAT A CIRCUMFERENTIAL GAP IS ACHIEVED

2

08 ADJUST ON INSTALLATION

2

0.8 mm +/− 0.5 mm

(0.031 in +/− 0.020 in) 06

07

C

06 ADJUST THE POTABLE WATER SERVICE DOOR AS NECESSARY

164AR

164AR

08

C C

09

09 SECURE WITH THREADLOCKING ADHESIVE (MAT.NO.05BAE1)

G_SB_523086_6_BCAA_04_00

Figure A-GBCAA - Sheet 04

Adjustment of the potable water service panel access door

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 123

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SERVICE BULLETIN

**CONF ALL

FR70

FR69

164AR

Z160

A

B

A

G_SB_523086_6_BDAA_01_00

Figure A-GBDAA - Sheet 01

Additional work - Modification of the potable water service panel access door

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 124

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@A330

SERVICE BULLETIN

**CONF ALL

(2)

POTABLE WATER

FR69

FR70

STGR50RH

B

SERVICE DOOR

164AR

C D

G_SB_523086_6_BDAA_02_00

Figure A-GBDAA - Sheet 02

Additional work - Modification of the potable water service panel access door

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 125

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SERVICE BULLETIN

**CONF ALL

C

D

BEFORE

AFTER

(4)

(3)

6

(3)

G_SB_523086_6_BDAA_03_00

Figure A-GBDAA - Sheet 03

Additional work - Modification of the potable water service panel access door

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 126

6

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SERVICE BULLETIN

**CONF ALL

FR70

FR69

164AR

Z160

A

B

A

G_SB_523086_6_BEAA_01_00

Figure A-GBEAA - Sheet 01

Additional work - Application of the sealant

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 127

6

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SERVICE BULLETIN

**CONF ALL

FR69

FR70

STGR50RH

B

TYPICAL

C

C

A

A

A

A A

A

G_SB_523086_6_BEAA_02_00

Figure A-GBEAA - Sheet 02

Additional work - Application of the sealant

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 128

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SERVICE BULLETIN

**CONF ALL

NOTE:

01 APPLY SEALANT (MAT.NO.06AAA1)

02 APPLY COATING (MAT.NO.04QAB2)

01 02 01 02

A A

01 02 01 02

C

C

B B

C

C C B B

01 02

01 02 01 02

01 02

G_SB_523086_6_BEAA_03_00

Figure A-GBEAA - Sheet 03

Additional work - Application of the sealant

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 129

6

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SERVICE BULLETIN

This Page Intentionally Left Blank

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 130

6

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@A330

SERVICE BULLETIN

Appendix 01 - Elapsed Time Assumption

**CONF ALL

ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A330−52−3086

MH

ET/S:

PER

MANHOURS

ELAPSED TIME PER STEP

NUMBER OF PERSONS

01

02

THIS CHART IS ONLY A PROPOSAL.

OPERATORS MAY DETERMINE THAT ANOTHER WAY

TO DO THE WORK IS MORE SUITABLE FOR THEM.

: 02 : IF A VSB IS INVOLVED, THE ASSOCIATED MANHOURS

ARE NOT REFLECTED IN THIS GANTT CHART.

SB ELAPSED TIME

(HOURS)

MH ET/S

TOTAL MANHOURS

SB ELAPSED TIME

13.50

12.00

STEPS

0.50 0.50

0 1 5 10

REIDENTIFY THE POTABLE WATER SERVICE PANEL

RESTORE THE AIRCRAFT SURFACE PROTECTION

TEST

PER

1

234 6789 11

GET ACCESS

REMOVE THE POTABLE WATER SERVICE DOOR

REMOVE THE FITTINGS AND THE ANCHOR NUTS

INSTALL THE BONDING LEAD

ADJUST THE NEW POTABLE WATER SERVICE DOOR

CLOSE−UP

INSTALL THE PLACARD

INSTALL THE NEW ANCHOR NUTS

INSTALL THE NEW POTABLE WATER 

INSTALL THE NEW FITTING

2.50 2.50 1

0.50 0.50 1

1.00 0.50 2

0.50 0.50 1

2.00 1.00 2

0.25 0.25 1

0.25 0.25 1

0.75 0.75 1

0.50 0.50 1

0.25 0.25 1

1.25 1.25 1

2.50 2.50 1

INSTALL THE NEW HINGES 0.50 0.50 1

SERVICE PANEL ACCESS DOOR

12

01

NOTES:

0.25 0.25 1

MODIFY THE NEW POTABLE WATER 

SERVICE PANEL ACCESS DOOR

G_SB_523086_6_GAAA_01_03

Figure A-GGAAA - Sheet 01

Gantt chart

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 1

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SERVICE BULLETIN

Appendix 01 - Elapsed Time Assumption

This Page Intentionally Left Blank

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 2

6

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@A330

SERVICE BULLETIN

Appendix 02 - Status of the aircraft after accomplishment of the Service Bulletin A330-52-3086

**CONF ALL

MOD Config.001 Config.002 Config.003

201938D50379 X - -

201939D59871 X - -

201939D59870 - X -

201938D50416 - - X

203344D50725 X X X

203563D50740 X X X

NOTE: X is used for the modifications embodied on aircraft after accomplishment of the Service

Bulletin A330-52-3086.

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 1

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@A330

SERVICE BULLETIN

REPORTING SHEET

TITLE: DOORS-SERVICE DOORS-MODIFICATION OF LATCHING MECHANISM

OF POTABLE WATER SERVICE PANEL

MODIFICATION No.: 201938D50416 201938D50379 201939D59871 201939D59870 203344D50725

203563D50740

Please complete the appropriate item (A or B):

A - SB WILL BE embodied YES/NO (if NO please comment)

If YES, aircraft concerned (as per SB effectivity by default) and planned dates (month/year) of

embodiment:

B - SB HAS BEEN embodied on aircraft:

Operator comments:

From Airline:

Name/Title:

Signature: Date:

If operational documentation is affected (see Paragraph 1.K of this SB): If information is needed prior to

next normal revision or prior to SB embodiment, please indicate required service(s):

Either: Modification Operational Impact (MOI), if available YES/NO

Or : Intermediate revision YES/NO

Important Information: This SB will only be incorporated in your maintenance and operational

documentation if this sheet is returned to Airbus and signed by a duly authorised representative. With

the next feasible revision, this will result in

- Updating of maintenance documentation to show pre and post SB data.

- Updating of maintenance and operational documentation to show post SB data after embodiment.

If this SB requires previous or simultaneous accomplishment of other SBs, Airbus shall automatically

include them in the manual revisions. Refer to SIL 00-037 for detailed information.

Please return this completed sheet to:

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX FRANCE

Attn: SDC32 Technical Data and Documentation Services

FAX: (+33) 5 61 93 28 06

e-mail: sb.reporting@airbus.com

or via your Resident Customer Support Office.

Alternatively, SB lists via letters or fax are also accepted.

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 1

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@A330

SERVICE BULLETIN

QUALITY PERCEPTION FORM

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

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

improve the quality of our Service Bulletins.

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

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

- Quality rating of this SB 4321

- Quality rating of the Accomplishment Instructions 4321

- Quality rating of the Illustrations 4321

- Is this SB easy to understand ? Y/N

If you have had difficulties in the accomplishment of this SB please quote below the area(s) and give a

short description of the issue.

Planning Material Instructions

X Effectivity X Kit content X Preparation

X Reason X List of Materials Operator Supplied X Mod/Inspection

X Manpower X Industry support X Test

X References X Re-identification X Close-Up

X Publication X Tooling X Illustrations

Comments:

Operator: Date:

Name/Title:

Please return this form to:

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX FRANCE

Attn : SEM4 Service Bulletins Management

FAX : (33) 5 61 93 42 51

Or via your Resident Customer Support Office.

DATE: Apr 27/12 SERVICE BULLETIN No.: A330-52-3086

REVISION No.: 01 - Apr 25/14 Page: 1

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