@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: 29

TITLE: HYDRAULIC POWER - MAIN HYDRAULIC POWER - REPLACE CHECK

VALVE PN CAR401 WITH IMPROVED CHECK VALVE PN CAR402

MODIFICATION No.: 203972D50812

This page transmits Revision No.03 of Service Bulletin No.A330-29-3125

ADDITIONAL WORK

**CONF ALL

No additional work is required by this revision for aircraft modified by any previous issue.

REASON

Revision No. 03 issued to incorporate a note related to the way of working on the hydraulic systems.

CHANGES

The main changes of this revision are:

- Add note related to work on hydraulic circuits.

- In para DESCRIPTION, ’on aircraft’ between quotation marks replaced by ’on aircraft’ between

apostrophes to avoid computing issues.

- In para DESCRIPTION, ’on bench’ between quotation marks replaced by ’on bench’ between

apostrophes to avoid computing issues.

- In para MATERIAL - PRICE AND AVAILABILITY, sentence deleted for the procurement terms.

- In para INDUSTRY SUPPORT INFORMATION, one sentence deleted and one sentence modified

for the industry supports terms.

- In para STANDARD PRACTICES one sentence added for the removal/installation of the O-rings

seal.

- In all SUBTASKS for the modification of the green, blue or yellow HP manifolds, note for the

storage seals replaced by a workstep.

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 1

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@A330

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

- In SUBTASK 293125-930-208-001 Reidentify the Green HP Manifold, note added in case the old

PN is written in the hidden face of the green HP manifold.

- In SUBTASK 293125-930-209-001 Reidentify the Blue Manifold (FIN 6103JM), paragraph (a).2.,

reference to view updated.

- Title updated in SUBTASK 293125-730-208-001 Test of the Green HP Manifold (FIN 5102JM).

- In all Test subtasks, sentences added to ensure there are no leaks from the unions on the manifold

and from the pipe connections.

- In para INDUSTRY SUPPORT INFORMATION, tel and fax numbers deleted for AIRBUS

CUSTOMER SERVICES DIRECTORATE contact.

SUMMARY

EFFECTIVITY OPERATOR LIST UPDATED R

REFERENCES / REPERCUSSIONS REFERENCES/REPERCUSSIONS TABLE

UPDATED

R

PLANNING INFORMATION

EFFECTIVITY EFFECTIVITY RELATED INFORMATION

UPDATED

R

Configuration definition

CONF 001 CONFIGURATION DEFINITION UPDATED R

CONF 002 CONFIGURATION DEFINITION UPDATED R

DESCRIPTION DESCRIPTION UPDATED R

INTERCHANGEABILITY/MIXABILITY INTERCHANGEABILITY/MIXABILITY UPDATED R

INTERCHANGEABILITY/MIXABILITY UPDATED R

SPARES SPARES UPDATED R

MATERIAL INFORMATION

MATERIAL - PRICE AND AVAILABILITY

Procurement Addresses PROCUREMENT ADDRESSES UPDATED R

Price and Availability PRICE AND AVAILABILITY UPDATED R

INDUSTRY SUPPORT INFORMATION INDUSTRY SUPPORT INFORMATION UPDATED R

ACCOMPLISHMENT INSTRUCTIONS

TASK 293125- 831-854-001-Modify the

Green HP Hydraulic Manifold on Aircraft

TASK SOLUTION UPDATED

NOTE UPDATED

R

Subtask 293125-910-207-002 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

Subtask 293125-831-209-001 SUBTASK SOLUTION UPDATED

NOTE UPDATED

R

Subtask 293125-930-208-001 SUBTASK SOLUTION UPDATED

NOTE UPDATED

R

Subtask 293125-730-208-001 SUBTASK SOLUTION UPDATED R

TASK 293125- 831-855-001-Modify the

Blue HP Hydraulic Manifold on Aircraft

TASK SOLUTION UPDATED

NOTE UPDATED

R

Subtask 293125-910-208-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 2

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@A330

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Subtask 293125-831-210-001 SUBTASK SOLUTION UPDATED

NOTE UPDATED

R

Subtask 293125-930-209-001 SUBTASK SOLUTION UPDATED

NOTE UPDATED

R

Subtask 293125-730-209-001 SUBTASK SOLUTION UPDATED R

TASK 293125- 831-856-001-Modify the

Yellow HP Hydraulic Manifold on Aircraft

TASK SOLUTION UPDATED

NOTE UPDATED

R

Subtask 293125-910-209-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

Subtask 293125-831-211-001 SUBTASK SOLUTION UPDATED

NOTE UPDATED

R

Subtask 293125-730-210-001 SUBTASK SOLUTION UPDATED R

TASK 293125- 831-848-001-Modify the

Green HP Hydraulic Manifold on Aircraft

TASK SOLUTION UPDATED

NOTE UPDATED

R

Subtask 293125-910-201-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

Subtask 293125-831-201-001 SUBTASK SOLUTION UPDATED

NOTE UPDATED

R

Subtask 293125-730-211-001 SUBTASK SOLUTION UPDATED R

TASK 293125- 831-849-001-Modify the

Green HP Hydraulic Manifold on Bench

TASK SOLUTION UPDATED

NOTE UPDATED

R

Subtask 293125-910-202-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

Subtask 293125-831-204-001 SUBTASK SOLUTION UPDATED

NOTE UPDATED

R

Subtask 293125-730-204-001 SUBTASK SOLUTION UPDATED R

TASK 293125- 831-850-001-Modify the

Blue HP Hydraulic Manifold on Aircraft

TASK SOLUTION UPDATED

NOTE UPDATED

R

Subtask 293125-910-203-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

Subtask 293125-831-205-001 SUBTASK SOLUTION UPDATED

NOTE UPDATED

R

Subtask 293125-730-205-001 SUBTASK SOLUTION UPDATED R

TASK 293125- 831-851-001-Modify the

Blue HP Hydraulic Manifold on Bench

TASK SOLUTION UPDATED

NOTE UPDATED

R

Subtask 293125-910-204-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

Subtask 293125-831-206-004 SUBTASK SOLUTION UPDATED

NOTE UPDATED

R

Subtask 293125-730-206-001 SUBTASK SOLUTION UPDATED R

TASK 293125- 831-852-001-Modify the

Yellow HP Hydraulic Manifold on Aircraft

TASK SOLUTION UPDATED

NOTE UPDATED

R

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 3

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

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Subtask 293125-910-205-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

Subtask 293125-831-207-001 SUBTASK SOLUTION UPDATED

NOTE UPDATED

R

Subtask 293125-730-207-001 SUBTASK SOLUTION UPDATED R

TASK 293125- 831-853-001-Modify the

Yellow HP Hydraulic Manifold on Bench

TASK SOLUTION UPDATED

NOTE UPDATED

R

Subtask 293125-910-206-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

Subtask 293125-831-208-001 SUBTASK SOLUTION UPDATED

NOTE UPDATED

R

Subtask 293125-730-212-001 SUBTASK SOLUTION UPDATED R

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

Revision No.01 issued to:

update the effectivity

clarify the accomplishment instructions following operator requests after the accomplishment of this

Service Bulletin at original issue

update the illustrations.

Revision No. 02 issued to:

add reference to SBIT 15-0088 to the REFERENCES/REPERCUSSIONS table

update Paragraph 1.C.(4) Operational/Maintenance Consequences

add MPD task No. 291000-19-3 to Paragraph 1.K. PUBLICATION AFFECTED

correct the torque values given in Subtask 293125-730-209-001 Table 2

clarify the accomplishment instructions for modification of the Yellow HP Manifold ’On Bench’

correct AMM Task in Subtask ’293125-730-209-001 - Test the Blue HP Manifold’

update the Service Bulletin effectivity

add illustrations showing the location of the existing storage seal, lower O-ring and back-up ring.

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 4

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@A330

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

REVISION SEQUENCE

ORIGINAL: Aug 08/14

REVISION No. : 01 - Jul 30/15

REVISION No. : 02 - Jan 21/16

REVISION No. : 03 - Apr 08/16

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 5

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@A330

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

This Page Intentionally Left Blank

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 6

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: 29

TITLE: HYDRAULIC POWER - MAIN HYDRAULIC POWER - REPLACE CHECK

VALVE PN CAR401 WITH IMPROVED CHECK VALVE PN CAR402

**CONF ALL

MODIFICATIONS

MODIFICATION CLASSIFICATION

MAJOR 203972D50812

MINOR None

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

Due to in service leakage problems with the Hydraulic Check Valve (CV) PN CAR401 a repetitive

inspection has been mandated by an Airworthiness Directive (AD) to address the problem.

CV PN CAR401, can be installed on:

- 5316JM101, at the Green High Pressure (HP) manifold, (FIN 5102JM)

- 5316JM102, at the Green High Pressure (HP) manifold, (FIN 5102JM)

- 5316JM201, at the Blue High Pressure (HP) manifold, (FIN 6103JM)

- 5316JM301, at the Yellow High Pressure (HP) manifold, (FIN 7103JM).

CV PN CAR402 will be introduced for production and for mandatory replacement on in-service aircraft

as the successor of CV PN CAR401.

This Service Bulletin introduces an improved CV PN CAR402 for A330 aircraft. Where CV PN CAR401

is installed it can be replaced on the aircraft by CV PN CAR402. Where CV PN CAR401 is installed

and torqued to a value higher than 250Nm, the manifold must be removed and the CV replaced on

the bench by CV PN CAR402. Modification No. 201384D50293 (Service Bulletin No. A330-29-3119)

introduced a torque value of 400Nm for CV PN CAR401.

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 1

6

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

SERVICE BULLETIN

SUMMARY

Accomplishment of this Service Bulletin cancels the requirements of Service Bulletin No. A330-29-3111

and AOT 29L001-12.

The maintenance consequence of this Service Bulletin are the visual leak check of the CVs in

accordance with new Maintenance Planning Document (MPD) task 291000-19-3. This new task is for a

visual check of the CVs every 24 months.

GENERAL EVALUATION

EVALUATION TABLE

COMPLIANCE MANDATORY (1) CANCELS INSPECTION SB YES

POTENTIAL AD YES A/C OPERATION AFFECTED NO

RELIABILITY AFFECTED YES 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

Component COMPD01 1 See SB Packing

Equipment BFEZ01 1 See SB Check Valve

**CONF 002

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Standard tool TOOLD01 1 1,660.00 Installation Tooling

Component COMPD01 1 See SB Packing

Equipment BFEZ01 1 See SB Check Valve

EFFECTIVITY

**CONF ALL

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

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 2

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@A330

SERVICE BULLETIN

SUMMARY

18P 34Z 38W 43P 87Z AAR AAW ABD ACA ACI AEA AFL AFR

AIB ALK ARA ARG ASY AVA AZA AZU BEC BEL BER BGH CAL

CBJ CCA CEB CES CHH CPA CRK CRL CSA CSC CSN DAH DAL

DGA DLH EDW EIN ETD EVA EVE EZX F2I FIN FJI FWI G8E

GAP GFA GIA GRL HAL HDA HFY HVN IAW IBE JAI KAL KLM

LAA MAS MAU MEA MLM MNB MON MSR NMB OBS OHY OMA ONE

PAL QAF QFA QTR RJA RSF RSY RZO SAA SAI SAS SEY SIA

SVA SWR SXD TAE TAM TAP TCX THA THY TNA TOW TPA TSC

UAE UAF USA VIR VKG VOZ WRC XAX XLF

CONCURRENT REQUIREMENTS

None

REFERENCES / REPERCUSSIONS

TFU 29.10.00.034

OEB None

AOT A29L001-12

SIL None

ISI 00.00.00135

00.00.00198

LINE MAINTENANCE AFFECTED No

LIFE LIMIT None

OTHER SBIT 15-0088

NATURE OF THE WORK

AIRCRAFT YES

EQUIPMENT YES

HARD NO

SOFT NO

OBRM NO

MANPOWER

**CONF 001

Task 293125-831-854-001: Modify the Green HP Hydraulic Manifold on Aircraft

TOTAL MANHOURS 7.50

ELAPSED TIME (HOURS) 7.50

Task 293125-831-855-001: Modify the Blue HP Hydraulic Manifold on Aircraft

TOTAL MANHOURS 7.50

ELAPSED TIME (HOURS) 7.50

Task 293125-831-856-001: Modify the Yellow HP Hydraulic Manifold on Aircraft

TOTAL MANHOURS 7.50

ELAPSED TIME (HOURS) 7.50

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 3

6

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@A330

SERVICE BULLETIN

SUMMARY

Task 293125-831-848-001: Modify the Green HP Hydraulic Manifold on Aircraft

TOTAL MANHOURS 0.00

Task 293125-831-849-001: Modify the Green HP Hydraulic Manifold on Bench

TOTAL MANHOURS 0.00

Task 293125-831-850-001: Modify the Blue HP Hydraulic Manifold on Aircraft

TOTAL MANHOURS 0.00

Task 293125-831-851-001: Modify the Blue HP Hydraulic Manifold on Bench

TOTAL MANHOURS 0.00

Task 293125-831-852-001: Modify the Yellow HP Hydraulic Manifold on Aircraft

TOTAL MANHOURS 0.00

Task 293125-831-853-001: Modify the Yellow HP Hydraulic Manifold on Bench

TOTAL MANHOURS 0.00

**CONF 002

Task 293125-831-854-001: Modify the Green HP Hydraulic Manifold on Aircraft

TOTAL MANHOURS 0.00

Task 293125-831-855-001: Modify the Blue HP Hydraulic Manifold on Aircraft

TOTAL MANHOURS 0.00

Task 293125-831-856-001: Modify the Yellow HP Hydraulic Manifold on Aircraft

TOTAL MANHOURS 0.00

Task 293125-831-848-001: Modify the Green HP Hydraulic Manifold on Aircraft

TOTAL MANHOURS 7.50

ELAPSED TIME (HOURS) 7.50

Task 293125-831-849-001: Modify the Green HP Hydraulic Manifold on Bench

TOTAL MANHOURS 10.50

ELAPSED TIME (HOURS) 10.50

Task 293125-831-850-001: Modify the Blue HP Hydraulic Manifold on Aircraft

TOTAL MANHOURS 7.50

ELAPSED TIME (HOURS) 7.50

Task 293125-831-851-001: Modify the Blue HP Hydraulic Manifold on Bench

TOTAL MANHOURS 10.50

ELAPSED TIME (HOURS) 10.50

Task 293125-831-852-001: Modify the Yellow HP Hydraulic Manifold on Aircraft

TOTAL MANHOURS 7.50

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 4

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

SERVICE BULLETIN

SUMMARY

Task 293125-831-852-001: Modify the Yellow HP Hydraulic Manifold on Aircraft

ELAPSED TIME (HOURS) 7.50

Task 293125-831-853-001: Modify the Yellow HP Hydraulic Manifold on Bench

TOTAL MANHOURS 10.50

ELAPSED TIME (HOURS) 10.50

APPENDICES

**CONF ALL

Appendix 01: PN Evolution of the Green, Blue and Yellow System HP Hydraulic Manifolds

Appendix 02: Local Manufacture of Tooling

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 5

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@A330

SERVICE BULLETIN

SUMMARY

**CONF ALL

FR53.2

FR53.1

5102JM

FR46

FR47

7103JM

6103JM

Z190

A

B

A

B

MANIFOLD

MANIFOLD

MANIFOLD

G_SB_293125_6_SAAA_01_00

Figure A-GSAAA - Sheet 01

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 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: 29

TITLE: HYDRAULIC POWER - MAIN HYDRAULIC POWER - REPLACE CHECK

VALVE PN CAR401 WITH IMPROVED CHECK VALVE PN CAR402

MODIFICATION No.: 203972D50812

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

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

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

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

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

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

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

AIRBUS prior written consent.

1. PLANNING INFORMATION

**CONF ALL

A. EFFECTIVITY

NOTE: This modification is embodied before delivery on aircraft with Manufacturer

Serial Number (MSN) 1537 and subsequent.

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

54491S18191 is embodied or Service Bulletin No. A330-29-3101 has been

accomplished.

NOTE: This Service Bulletin is not applicable to aircraft on which Mod No.

203796D50774 has been embodied or Service Bulletin No. A330-29-3124 has

been accomplished.

(1) Models

330-202 330-203 330-223 330-223F 330-243 330-243F 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 0064-0065 0070-0072

0082-0083 0086-0087 0095-0096 0098-0099 0102 0106 0109 0111-0113 0116 0118

0120-0122 0127 0132 0138 0140 0143-0144 0148 0153 0155 0162 0165 0171-0172

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 1

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@A330

SERVICE BULLETIN

0177 0181 0195 0200 0206 0209 0211 0219 0222-0224 0226 0229-0232 0234 0238

0240-0241 0244 0247-0251 0253-0256 0258-0259 0261-0262 0265-0267 0269

0271-0272 0275-0277 0279 0281 0283-0288 0290-0291 0293-0296 0299-0301 0303

0305-0306 0308-0309 0311-0317 0320 0322-0324 0326 0328 0330 0333-0334

0337-0340 0342-0346 0348-0351 0353 0356-0358 0361-0362 0364-0366 0368-0370

0372 0375 0380 0382 0384 0386 0388-0389 0392-0393 0396-0398 0400-0401

0403-0405 0407-0409 0412 0418-0423 0425 0427-0428 0432 0437 0439 0441

0443-0444 0448 0451-0452 0454-0456 0458 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

0925-0928 0930-0932 0934-0937 0939-0952 0954 0956-0959 0961-0971 0973-0980

0982-0986 0988-0992 0994-0998 1000-1004 1006-1016 1018-1023 1025-1026

1028-1029 1031-1039 1041-1049 1051-1055 1057-1063 1065-1067 1069-1078

1080-1082 1084-1090 1092-1101 1103-1108 1110 1112 1114-1116 1118 1120

1123-1124 1126-1127 1129-1133 1135-1138 1141 1143 1145-1151 1153 1155-1157

1159-1161 1163-1165 1167-1175 1177-1178 1180-1181 1183-1184 1186-1193

1195-1196 1198-1206 1208-1241 1243-1252 1254-1256 1258-1272 1274-1536

(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

18P 1321

34Z 1483 1491

38W 0401

43P 1053

87Z 0535

AAR 0640 0676 0708 0772 0803 0845 1001 1055 1151 1211 1326 1340

1435 1464 1518

AAW 1043 1472 1535

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

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 2

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@A330

SERVICE BULLETIN

OPERATOR MSN

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

1264 1270 1284 1299 1301 1323 1328 1345 1356 1371

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

0567 0584 0657

AIB 0437 0871

ALK 0303 0306 0311 0313 0404 0456 0627

ARA 0891 0927

ARG 0290 0300 0358 0364

ASY 0747 0892 0898 0951 0969 1036 1183

AVA 0967 1009 1016 1073 1208 1224 1279 1342 1400 1508

AZA 0272 0339 0825 0831 1123 1135 1218 1225 1252 1283 1308 1313

1327 1354

AZU 0365 0372 0462 0494 0527 0529 0532

BEC 0863

BEL 0030 0037 0045 0082 0095 0229 0249 0324 1085

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

0828 0911

BGH 0255

CAL 0602 0607 0641 0671 0675 0691 0699 0707 0714 0725 0752 0769

0805 0823 0838 0861 0920 1177 1272 1278 1346 1367 1450

CBJ 1020 1052

CCA 0750 0756 0759 0780 0785 0797 0810 0815 0839 0860 0867 0873

0884 0890 0903 0909 0930 0941 0944 0957 1087 1110 1130 1187

1199 1216 1237 1260 1282 1304 1330 1333 1353 1373 1383 1396

1413 1434 1444 1459 1471 1493 1509 1525

CEB 1420 1445 1495 1527

CES 0713 0720 0728 0732 0735 0773 0777 0781 0782 0791 0821 0830

0836 0851 0862 0866 0916 0928 0936 0942 1262 1267 1280 1291

1303 1324 1331 1372 1375 1402 1421 1429 1440 1461 1468 1479

1484 1500 1520

CHH 0875 0881 0906 0919 0982 1159 1168 1178 1190 1255 1325 1438

1532

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 1317 1343 1349 1362 1366 1387 1409 1436 1443 1503

1523

CRK 1031 1034 1039 1042 1051 1054 1059 1062 1115 1175 1277 1286

1320 1322 1358 1369 1384 1398

CRL 0285 0320 1359 1376

CSA 0425

CSC 1082 1138 1241 1397 1432 1528

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

0958 0964 1096 1116 1129 1202 1220 1233 1244 1297 1309 1335

1392 1425 1430 1494 1519 1536

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

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SERVICE BULLETIN

OPERATOR MSN

DGA 0240

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

0913 0922 0989 1292 1305 1314 1497

EDW 0291 1193

EIN 0269 0330 0397 0841 0847 0985 1025 1106

ETD 0658 0688 0717 0724 0729 0730 0737 0788 0807 0809 0824 0832

0852 0854 0868 0885 0975 0991 1032 1070 1071 1081 1167 1205

1226 1245 1414 1486 1521 1524

EVA 0555 0573 0587 0634 0655 0661 0678 0693 0755 1254 1268 1274

EVE 0802

EZX 0261

F2I 0200

FIN 0994 1007 1013 1023 1067 1078 1088 1173

FJI 1394 1416 1465

FWI 0253 0758 0965 1021 1265

G8E 0294 0299

GAP 1463

GFA 0276 0281 0286 0287 0334 0340

GIA 0138 0140 0144 0148 0153 0165 0988 1028 1184 1214 1261 1288

1364 1410 1446 1474

GRL 0230

HAL 1104 1114 1171 1217 1259 1295 1302 1310 1316 1389 1399 1404

1422 1469 1488 1496 1511 1530

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

0479 0512 0581 0669 0673 1457

HFY 0096 0127 0211 0262 1008

HVN 0275 0366 0943 0946 0962 1019 1256 1266

IAW 1339

IBE 1377 1385 1405 1426 1437 1490 1507 1515

JAI 0888 0923 0947 0956 1351 1361 1370 1391

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

0351 0368 0428 0484 0490 0550 1133 1155 1200 1203 1393

KLM 0682 0686 0703 0738 0770 0801 0811 0819 0834 0900 0925 1161

1287 1294 1300 1381

LAA 1412 1424 1505

MAS 0116 1136 1148 1164 1180 1209 1219 1229 1234 1243 1281 1318

1336 1337 1347 1388 1395 1431 1470 1489

MAU 0883 1057

MEA 0926 0984 0995 0998

MLM 0451

MNB 1332

MON 0265

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

NMB 1451 1466

OBS 0833

OHY 0072 0087 0098 0143 0316 0345 0353 0362 0625 0632

OMA 1038 1044 1049 1063 1093 1120 1227

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SERVICE BULLETIN

OPERATOR MSN

ONE 1492 1506

PAL 1449 1456 1460 1467 1475 1482 1504 1510 1531

QAF 0487 0605

QFA 0506 0508 0513 0522 0553 0558 0564 0574 0593 0595 0603 0695

0705 0712 0842 0853 0887 0940 0945 0976 1061 1094 1169 1174

1198 1251 1258 1365

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

0680 0711 0721 0734 0743 0746 0760 0789 0792 0813 0820 0826

0849 0893 0907 0918 1350 1386 1406

RJA 0979 1002

RSF 0980 0996 1235 1379 1478 1516

RSY 0120 0171

RZO 0970

SAA 1191 1210 1223 1236 1249 1271

SAI 0055 0070 0086

SAS 0496 0497 0515 0568

SEY 0751

SIA 0978 0983 0986 0997 1006 1010 1012 1015 1098 1099 1105 1107

1124 1132 1149 1156 1382 1401 1427 1447 1453 1477 1485 1517

SVA 1108 1127 1137 1141 1147 1153 1189 1192 1454 1462 1473 1513

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

1355 1403

SXD 0530 0684

TAE 0348

TAM 0232 0238 0247 0259 0361 0466 0472 0700 0968 1112

TAP 0181 0195 0223 0305 0308 0312 0317 0477 0486 0877 0899 0904

0914 0934

TCX 0254 0266 0301 0398 0948

THA 0050 0060 0062 0064 0065 0112 0122 0209 0224 0231 0346 0990

1003 1035 1037 1060 1074 1086 1090 1263 1269 1289 1338 1348

1374 1408

THY 0463 0504 0697 0704 0742 0754 0774 0869 0874 0876 0882 0901

0932 0939 0949 0961 0977 1004 1092 1118 1150 1160 1170 1172

1204 1212 1213 1221 1228 1240 1298 1307 1311 1344 1418 1442

1458 1476 1487 1499 1501 1514 1522 1529

TNA 1146 1157 1357 1378

TOW 1033 1046 1248 1275 1312 1334 1363 1390 1419 1439 1498

TPA 1368 1380 1428 1448 1534

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

UAE 0248 0251 0283 0293 0295 0314 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 1415 1417 1441 1455 1480 1502 1512 1526

VIR 1195 1201 1206 1215 1231 1296 1315 1329 1341 1352

VKG 0309 0349 0356 0357

VOZ 1293 1306 1319 1407 1452

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SERVICE BULLETIN

OPERATOR MSN

WRC 0296

XAX 0054 0654 0662 0692 0716 0741 0786 0952 0974 1048 1066 1075

1126 1131 1165 1411 1423 1433 1481 1533

XLF 0501 0635 1360

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SERVICE BULLETIN

(4) Configuration by MSN

MSN CONFIGURATION

0012 0017 0030 0037 0045 0050 0054 0055 0060 0062 0064

0065 0070 0071 0072 0082 0083 0086 0087 0096 0099 0102

0106 0109 0111 0112 0113 0116 0118 0121 0122 0132 0138

0140 0143 0144 0148 0153 0155 0162 0165 0171 0172 0177

0181 0195 0200 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 0276 0277 0279 0281 0283

0284 0285 0286 0287 0288 0290 0295 0296 0300 0301 0303

0305 0306 0308 0309 0311 0312 0313 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

0357 0358 0361 0362 0364 0365 0368 0369 0370 0372 0375

0380 0382 0384 0386 0388 0389 0392 0393 0396 0397 0398

0400 0401 0403 0404 0405 0407 0408 0409 0412 0418 0419

0420 0421 0422 0423 0425 0427 0428 0432 0437 0439 0441

0443 0444 0448 0451 0452 0454 0455 0456 0458 0461 0462

0463 0465 0466 0469 0472 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 0512

0513 0515 0516 0518 0519 0522 0524 0525 0526 0527 0529

0532 0533 0536 0539 0542 0548 0549 0550 0551 0552 0553

0558 0564 0565 0567 0568 0570 0574 0576 0578 0579 0581

0584 0588 0591 0593 0595 0597 0600 0602 0603 0607 0609

0610 0614 0616 0618 0620 0621 0625 0627 0629 0631 0632

0633 0635 0636 0640 0641 0642 0644 0645 0647 0648 0650

0653 0654 0657 0659 0662 0663 0665 0666 0667 0669 0670

0671 0673 0674 0675 0676 0679 0680 0682 0683 0684 0686

0687 0690 0691 0692 0693 0695 0696 0697 0699 0700 0701

0703 0704 0705 0707 0708 0709 0711 0712 0713 0714 0716

0718 0720 0721 0722 0725 0726 0728 0732 0733 0735 0738

0739 0741 0742 0743 0745 0747 0749 0750 0751 0752 0754

0756 0758 0759 0769 0770 0772 0773 0774 0776 0777 0778

0780 0781 0782 0784 0785 0786 0789 0791 0795 0796 0797

0799 0801 0803 0805 0806 0807 0810 0811 0814 0815 0817

0819 0820 0821 0822 0823 0825 0827 0828 0830 0831 0833

0834 0836 0838 0839 0841 0842 0843 0845 0847 0850 0851

0853 0855 0857 0858 0859 0860 0861 0862 0863 0865 0866

0867 0869 0871 0873 0874 0875 0876 0877 0881 0883 0884

0887 0890 0891 0892 0895 0896 0898 0899 0900 0903 0904

0905 0906 0907 0909 0911 0913 0914 0915 0916 0918 0919

0920 0922 0926 0927 0928 0930 0931 0932 0934 0936 0939

0940 0941 0942 0944 0945 0946 0947 0948 0949 0950 0951

0957 0959 0961 0963 0965 0966 0967 0968 0969 0970 0971

0973 0976 0977 0979 0980 0982 0985 0988 0989 0990 0992

0996 1001 1002 1003 1004 1008 1011 1014 1020 1021 1022

1025 1028 1031 1033 1034 1035 1036 1037 1038 1039 1041

1042 1043 1044 1045 1046 1047 1049 1051 1052 1053 1054

1055 1057 1058 1059 1060 1061 1062 1063 1065 1069 1073

001 002

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SERVICE BULLETIN

MSN CONFIGURATION

1074 1076 1077 1080 1082 1086 1087 1090 1093 1094 1095

1097 1100 1103 1104 1106 1108 1110 1112 1114 1118 1120

1123 1127 1130 1133 1135 1137 1138 1141 1147 1150 1151

1153 1155 1159 1160 1161 1163 1168 1169 1170 1171 1172

1174 1177 1178 1183 1184 1186 1187 1189 1190 1191 1192

1195 1196 1198 1199 1200 1201 1203 1204 1206 1209 1210

1211 1212 1213 1214 1215 1216 1217 1218 1219

001 002

0095 0098 0120 0127 0275 0291 0293 0294 0299 0314 0356

0366 0473 0511 0521 0530 0535 0555 0571 0573 0587 0605

0612 0623 0634 0637 0638 0649 0652 0655 0656 0658 0661

0664 0678 0688 0717 0724 0729 0730 0734 0737 0746 0755

0760 0788 0792 0802 0809 0813 0818 0824 0826 0832 0840

0849 0852 0854 0868 0879 0882 0885 0888 0889 0893 0901

0908 0923 0925 0935 0937 0943 0952 0954 0956 0958 0962

0964 0974 0975 0978 0983 0984 0986 0991 0994 0995 0997

0998 1000 1006 1007 1009 1010 1012 1013 1015 1016 1018

1019 1023 1026 1029 1032 1048 1066 1067 1070 1071 1072

1075 1078 1081 1084 1085 1088 1089 1092 1096 1098 1099

1101 1105 1107 1115 1116 1124 1126 1129 1131 1132 1136

1143 1145 1146 1148 1149 1156 1157 1164 1165 1167 1173

1175 1180 1181 1188 1193 1202 1205 1208 1220 1221 1222

1223 1224 1225 1226 1227 1228 1229 1230 1231 1232 1233

1234 1235 1236 1237 1238 1239 1240 1241 1243 1244 1245

1246 1247 1248 1249 1250 1251 1252 1254 1255 1256 1258

1259 1260 1261 1262 1263 1264 1265 1266 1267 1268 1269

1270 1271 1272 1274 1275 1276 1277 1278 1279 1280 1281

1282 1283 1284 1285 1286 1287 1288 1289 1290 1291 1292

1293 1294 1295 1296 1297 1298 1299 1300 1301 1302 1303

1304 1305 1306 1307 1308 1309 1310 1311 1312 1313 1314

1315 1316 1317 1318 1319 1320 1321 1322 1323 1324 1325

1326 1327 1328 1329 1330 1331 1332 1333 1334 1335 1336

1337 1338 1339 1340 1341 1342 1343 1344 1345 1346 1347

1348 1349 1350 1351 1352 1353 1354 1355 1356 1357 1358

1359 1360 1361 1362 1363 1364 1365 1366 1367 1368 1369

1370 1371 1372 1373 1374 1375 1376 1377 1378 1379 1380

1381 1382 1383 1384 1385 1386 1387 1388 1389 1390 1391

1392 1393 1394 1395 1396 1397 1398 1399 1400 1401 1402

1403 1404 1405 1406 1407 1408 1409 1410 1411 1412 1413

1414 1415 1416 1417 1418 1419 1420 1421 1422 1423 1424

1425 1426 1427 1428 1429 1430 1431 1432 1433 1434 1435

1436 1437 1438 1439 1440 1441 1442 1443 1444 1445 1446

1447 1448 1449 1450 1451 1452 1453 1454 1455 1456 1457

1458 1459 1460 1461 1462 1463 1464 1465 1466 1467 1468

1469 1470 1471 1472 1473 1474 1475 1476 1477 1478 1479

1480 1481 1482 1483 1484 1485 1486 1487 1488 1489 1490

1491 1492 1493 1494 1495 1496 1497 1498 1499 1500 1501

1502 1503 1504 1505 1506 1507 1508 1509 1510 1511 1512

1513 1514 1515 1516 1517 1518 1519 1520 1521 1522 1523

1524 1525 1526 1527 1528 1529 1530 1531 1532 1533 1534

1535 1536

002

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

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SERVICE BULLETIN

(5) Configuration definition

**CONF 001

Config. 001 is valid for all the aircraft given in the effectivity of this Service Bulletin that

have not embodied Modification No. 201384D50293 or not accomplished Service

Bulletin A330-29-3119.

**CONF 002

Config. 002 is valid for all the aircraft given in the effectivity of this Service Bulletin that

have embodied Modification No. 201384D50293, or have accomplished Service Bulletin

No. A330-29-3119 and may also have accomplished AOT 29L001-12.

(6) Material Effectivity

**CONF 001

MATERIAL QTY PER A/C SEE NOTES

Consumable CMLD01 1

Component COMPD01 1

Equipment BFEZ01 1

**CONF 002

MATERIAL QTY PER A/C SEE NOTES

Consumable CMLD01 1

Component COMPD01 1

Equipment BFEZ01 1

Standard tool TOOLD01 1

**CONF ALL

B. CONCURRENT REQUIREMENTS

None

C. REASON

(1) History

Due to in service leakage problems with the Hydraulic Check Valve (CV) PN CAR401 a

repetitive inspection has been mandated by an Airworthiness Directive (AD) to address

the problem.

CV PN CAR401, can be installed on:

- 5316JM101, at the Green High Pressure (HP) manifold, (FIN 5102JM)

- 5316JM102, at the Green High Pressure (HP) manifold, (FIN 5102JM)

- 5316JM201, at the Blue High Pressure (HP) manifold, (FIN 6103JM)

- 5316JM301, at the Yellow High Pressure (HP) manifold, (FIN 7103JM).

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

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SERVICE BULLETIN

CV PN CAR402 will be introduced for production and for mandatory replacement on inservice aircraft as the successor of CV PN CAR401.

(2) Objective/Action

This Service Bulletin introduces an improved CV PN CAR402 for A330 aircraft. Where

CV PN CAR401 is installed it can be replaced on the aircraft by CV PN CAR402. Where

CV PN CAR401 is installed and torqued to a value higher than 250Nm, the manifold

must be removed and the CV replaced on the bench by CV PN CAR402. Modification

No. 201384D50293 (Service Bulletin No. A330-29-3119) introduced a torque value of

400Nm for CV PN CAR401.

(3) Advantages

Accomplishment of this Service Bulletin cancels the requirements of Service Bulletin No.

A330-29-3111 and AOT 29L001-12.

(4) Operational/Maintenance Consequences

The maintenance consequence of this Service Bulletin are the visual leak check of the

CVs in accordance with new Maintenance Planning Document (MPD) task 291000-19-3.

This new task is for a visual check of the CVs every 24 months.

D. DESCRIPTION

NOTE: To accomplish this Service Bulletin, two possibilities are available for aircraft

in Config. 002 for each HP Hydraulic Manifold:

- either modify the HP manifold ’on aircraft’ for aircraft on which the CVs

have been re-torqued in accordance with AOT 29-L001-12

or

- modify the HP manifold ’on bench’ for aircraft on which the CVs have not

been re-torqued in accordance with AOT 29-L001-12.

To accomplish this Service Bulletin it is necessary to :

**CONF 001

Task 293125-831-854-001: Modify the Green HP Hydraulic Manifold on Aircraft

(1) Modify the Green HP Manifold (FIN 5102JM)

(2) Reidentify the Green HP Manifold (FIN 5102JM)

Task 293125-831-855-001: Modify the Blue HP Hydraulic Manifold on Aircraft

(1) Modify the Blue HP Manifold (FIN 6103JM)

(2) Reidentify the Blue Manifold (FIN 6103JM)

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

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SERVICE BULLETIN

Task 293125-831-856-001: Modify the Yellow HP Hydraulic Manifold on Aircraft

(1) Modify the Yellow HP Manifold (FIN 7103JM)

(2) Reidentify the Yellow HP Manifold (FIN 7103JM)

**CONF 002

Task 293125-831-848-001: Modify the Green HP Hydraulic Manifold on Aircraft

(1) Modify the Green HP Manifold (FIN 5102JM)

(2) Reidentify the Green HP Manifold (FIN 5102JM)

Task 293125-831-849-001: Modify the Green HP Hydraulic Manifold on Bench

(1) Remove the Green HP Manifold (FIN 5102JM)

(2) Modify the Green HP Manifold (FIN 5102JM)

(3) Reidentify the Green HP Manifold (FIN 5102JM)

(4) Install the Green HP Manifold (FIN 5102JM)

Task 293125-831-850-001: Modify the Blue HP Hydraulic Manifold on Aircraft

(1) Modify the Blue HP Manifold (FIN 6103JM)

(2) Reidentify the Blue HP Manifold (FIN 6103JM)

Task 293125-831-851-001: Modify the Blue HP Hydraulic Manifold on Bench

(1) Remove the Blue HP Manifold (FIN 6103JM)

(2) Modify the Blue HP Manifold (FIN 6103JM)

(3) Reidentify the Blue HP Manifold (FIN 6103JM)

(4) Install the Blue HP Manifold (FIN 6103JM)

Task 293125-831-852-001: Modify the Yellow HP Hydraulic Manifold on Aircraft

(1) Modify the Yellow HP Manifold (FIN 7103JM)

(2) Reidentify the Yellow HP Manifold (FIN 7103JM)

Task 293125-831-853-001: Modify the Yellow HP Hydraulic Manifold on Bench

(1) Remove the Yellow HP Manifold (FIN 7103JM)

(2) Modify the Yellow HP Manifold (FIN 7103JM)

(3) Reidentify the Yellow HP Manifold (FIN 7103JM)

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SERVICE BULLETIN

(4) Install the Yellow HP Manifold (FIN 7103JM)

**CONF ALL

E. COMPLIANCE

(1) Classification

MANDATORY: Service Bulletin must be accomplished.

(2) Accomplishment Timescale

**CONF 001

This Service Bulletin has been classified Mandatory by the issue of an Airworthiness

Directive (AD) published by the European Aviation Safety Agency (EASA). The AD must

be used as the reference document for the mandated accomplishment timescale.

Manifold to be modified Threshold Action

Green HP Hydraulic

Manifold

36 months from Issue of

this Service Bulletin

Do TASK 293125-831-854 001 Modify the

Green HP Hydraulic Manifold on Aircraft

Blue HP Hydraulic

Manifold

36 months from Issue of

this Service Bulletin

Do TASK 293125-831-855 001 Modify the Blue

HP Hydraulic Manifold on Aircraft

Yellow HP Hydraulic

Manifold

36 months from Issue of

this Service Bulletin

Do TASK 293125-831-856 001 Modify the

Yellow HP Hydraulic Manifold on Aircraft

**CONF 002

This Service Bulletin has been classified Mandatory by the issue of an Airworthiness

Directive (AD) published by the European Aviation Safety Agency (EASA). The AD must

be used as the reference document for the mandated accomplishment timescale.

Manifold to be modified Threshold Action

Green Manifold where

CV have been re-torqued

in accordance with AOT

29-L001-12

36 months from Issue of

this Service Bulletin

Do TASK 293125-831-848 001 Modify the

Green HP Hydraulic Manifold on Aircraft

Green Manifold where

CV have not been retorqued in accordance

with AOT 29-L001-12

36 months from Issue of

this Service Bulletin

Do TASK 293125-831-849 001 Modify the

Green HP Hydraulic Manifold on Bench

Blue Manifold where CV

have been re-torqued in

accordance with AOT 29-

L001-12

36 months from Issue of

this Service Bulletin

Do TASK 293125-831-850 001 Modify the Blue

HP Hydraulic Manifold on Aircraft

Blue Manifold where CV

have not been re-torqued

in accordance with AOT

29-L001-12

36 months from Issue of

this Service Bulletin

Do TASK 293125-831-851 001 Modify the Blue

HP Hydraulic Manifold on Bench

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SERVICE BULLETIN

Manifold to be modified Threshold Action

Yellow Manifold where

CV have been re-torqued

in accordance with AOT

29-L001-12

36 months from Issue of

this Service Bulletin

Do TASK 293125-831-852 001 Modify the

Yellow HP Hydraulic Manifold on Aircraft

Yellow Manifold where

CV have not been retorqued in accordance

with AOT 29-L001-12

36 months from Issue of

this Service Bulletin

Do TASK 293125-831-853 001 Modify the

Yellow HP Hydraulic Manifold on Bench

**CONF ALL

F. APPROVAL

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

Organisation Approval No. EASA.21J.031.

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

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

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

before incorporation of the Service Bulletin.

G. MANPOWER

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

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

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

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

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

included.

**CONF 001

Task 293125-831-854-001: Modify the Green HP Hydraulic Manifold on Aircraft

Get Access 1.00

On Aircraft

Modify the Green HP Manifold (FIN 5102JM) 2.00

Reidentify the Green HP Manifold (FIN 5102JM) 0.50

Tests 3.00

Close-Up 1.00

TOTAL MANHOURS 7.50

ELAPSED TIME (HOURS) 7.50

Task 293125-831-855-001: Modify the Blue HP Hydraulic Manifold on Aircraft

Get Access 1.00

On Aircraft

Modify the Blue HP Manifold (FIN 6103JM) 2.00

Reidentify the Blue Manifold (FIN 6103JM) 0.50

Tests 3.00

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

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Task 293125-831-855-001: Modify the Blue HP Hydraulic Manifold on Aircraft

Close-Up 1.00

TOTAL MANHOURS 7.50

ELAPSED TIME (HOURS) 7.50

Task 293125-831-856-001: Modify the Yellow HP Hydraulic Manifold on Aircraft

Get Access 1.00

On Aircraft

Modify the Yellow HP Manifold (FIN 7103JM) 2.00

Reidentify the Yellow HP Manifold (FIN 7103JM) 0.50

Tests 3.00

Close-Up 1.00

TOTAL MANHOURS 7.50

ELAPSED TIME (HOURS) 7.50

Task 293125-831-848-001: Modify the Green HP Hydraulic Manifold on Aircraft

On Aircraft

TOTAL MANHOURS 0.00

Task 293125-831-849-001: Modify the Green HP Hydraulic Manifold on Bench

On Aircraft

On Bench

TOTAL MANHOURS 0.00

Task 293125-831-850-001: Modify the Blue HP Hydraulic Manifold on Aircraft

On Aircraft

TOTAL MANHOURS 0.00

Task 293125-831-851-001: Modify the Blue HP Hydraulic Manifold on Bench

On Aircraft

On Bench

TOTAL MANHOURS 0.00

Task 293125-831-852-001: Modify the Yellow HP Hydraulic Manifold on Aircraft

On Aircraft

TOTAL MANHOURS 0.00

Task 293125-831-853-001: Modify the Yellow HP Hydraulic Manifold on Bench

On Aircraft

On Bench

TOTAL MANHOURS 0.00

**CONF 002

Task 293125-831-854-001: Modify the Green HP Hydraulic Manifold on Aircraft

On Aircraft

TOTAL MANHOURS 0.00

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SERVICE BULLETIN

Task 293125-831-855-001: Modify the Blue HP Hydraulic Manifold on Aircraft

On Aircraft

TOTAL MANHOURS 0.00

Task 293125-831-856-001: Modify the Yellow HP Hydraulic Manifold on Aircraft

On Aircraft

TOTAL MANHOURS 0.00

Task 293125-831-848-001: Modify the Green HP Hydraulic Manifold on Aircraft

Get Access 1.00

On Aircraft

Modify the Green HP Manifold (FIN 5102JM) 2.00

Reidentify the Green HP Manifold (FIN 5102JM) 0.50

Tests 3.00

Close-Up 1.00

TOTAL MANHOURS 7.50

ELAPSED TIME (HOURS) 7.50

Task 293125-831-849-001: Modify the Green HP Hydraulic Manifold on Bench

Get Access 1.50

On Aircraft

Install the Green HP Manifold (FIN 5102JM) 1.00

On Bench

Remove the Green HP Manifold (FIN 5102JM) 1.00

Modify the Green HP Manifold (FIN 5102JM) 2.00

Reidentify the Green HP Manifold (FIN 5102JM) 0.50

Tests 3.00

Close-Up 1.50

TOTAL MANHOURS 10.50

ELAPSED TIME (HOURS) 10.50

Task 293125-831-850-001: Modify the Blue HP Hydraulic Manifold on Aircraft

Get Access 1.00

On Aircraft

Modify the Blue HP Manifold (FIN 6103JM) 2.00

Reidentify the Blue HP Manifold (FIN 6103JM) 0.50

Tests 3.00

Close-Up 1.00

TOTAL MANHOURS 7.50

ELAPSED TIME (HOURS) 7.50

Task 293125-831-851-001: Modify the Blue HP Hydraulic Manifold on Bench

Get Access 1.50

On Aircraft

Remove the Blue HP Manifold (FIN 6103JM) 1.00

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SERVICE BULLETIN

Task 293125-831-851-001: Modify the Blue HP Hydraulic Manifold on Bench

Install the Blue HP Manifold (FIN 6103JM) 1.00

On Bench

Modify the Blue HP Manifold (FIN 6103JM) 2.00

Reidentify the Blue HP Manifold (FIN 6103JM) 0.50

Tests 3.00

Close-Up 1.50

TOTAL MANHOURS 10.50

ELAPSED TIME (HOURS) 10.50

Task 293125-831-852-001: Modify the Yellow HP Hydraulic Manifold on Aircraft

Get Access 1.00

On Aircraft

Modify the Yellow HP Manifold (FIN 7103JM) 2.00

Reidentify the Yellow HP Manifold (FIN 7103JM) 0.50

Tests 3.00

Close-Up 1.00

TOTAL MANHOURS 7.50

ELAPSED TIME (HOURS) 7.50

Task 293125-831-853-001: Modify the Yellow HP Hydraulic Manifold on Bench

Get Access 1.50

On Aircraft

Remove the Yellow HP Manifold (FIN 7103JM) 1.00

Install the Yellow HP Manifold (FIN 7103JM) 1.00

On Bench

Modify the Yellow HP Manifold (FIN 7103JM) 2.00

Reidentify the Yellow HP Manifold (FIN 7103JM) 0.50

Tests 3.00

Close-Up 1.50

TOTAL MANHOURS 10.50

ELAPSED TIME (HOURS) 10.50

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

Weight (kg) Weight (lb) Balance (kgm) Balance (lb.ft)

A330-200 -1.752 -3.863 -59.177 -428.024

A330-300 -1.752 -3.863 -65.299 -472.3

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SERVICE BULLETIN

I. ELECTRICAL LOAD DATA

Not Changed

J. REFERENCES

**CONF 001

Aircraft Maintenance Manual (AMM) 06-20-00 06-31-53 06-41-53

12-34-24 20-11-11 20-23-11

20-23-22 20-29-00 29-00-00

29-11-53 29-12-53 29-13-53

Consumable Material List (CML)

ATA Common Support Data Dictionary (CSDD),

Chapter 2

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

Process and Material Specification (PMS) Process and Material Specification

(PMS) 01-06-12

Standards Manual (SM)

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

**CONF 002

Aircraft Maintenance Manual (AMM) 06-20-00 06-31-53 06-41-53

12-34-24 20-11-11 20-23-11

20-23-22 20-29-00 29-00-00

29-11-53 29-12-53 29-13-53

Consumable Material List (CML)

ATA Common Support Data Dictionary (CSDD),

Chapter 2

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

Process and Material Specification (PMS) Process and Material Specification

(PMS) 01-06-12

Standards Manual (SM)

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

**CONF ALL

K. PUBLICATION AFFECTED

Aircraft Maintenance Manual (AMM) 29-11-53 29-12-53 29-13-53

29-10-00

Illustrated Parts Catalog (IPC) 29-11-53 29-12-53 29-13-53

29-11-03 29-12-03 29-13-03

Maintenance Planning Document (MPD) 29-10-00-19-1

29-10-00-19-2

29-10-00-19-3

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

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SERVICE BULLETIN

L. INTERCHANGEABILITY/MIXABILITY

**CONF 001

The interchangeability/mixability possibilities are for new or modified parts introduced by the

accomplishment of this Service Bulletin.

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE

NOTES

Seal Assy 818114 NAS1612-24 03 Not

Applicable

(1) (2)

Valve-check CAR401 CAR402 03 NO (2)

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

Common Support Data Dictionary (CSDD), Chapter 2.

NOTE: Only the mixability configuration(s) and condition(s) stated in this Service

Bulletin are approved.

NOTE (1): The Seal and Check Valve are not interchangeable, but are one way

interchangeable when changed together.

NOTE (2): Manifold assembly equipped with PN CAR402 is not interchangeable with

Manifold assembly equipped with PN CAR401.

**CONF 002

The interchangeability/mixability possibilities are for new or modified parts introduced by the

accomplishment of this Service Bulletin.

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE

NOTES

Seal Assy 818114 NAS1612-24 03 Not

Applicable

(1) (2)

Valve-check CAR401 CAR402 03 NO (2)

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

Common Support Data Dictionary (CSDD), Chapter 2.

NOTE: Only the mixability configuration(s) and condition(s) stated in this Service

Bulletin are approved.

NOTE (1): The Seal and Check Valve are not interchangeable, but are one way

interchangeable when changed together.

NOTE (2): Manifold assembly equipped with PN CAR402 is not interchangeable with

Manifold assembly equipped with PN CAR401.

**CONF ALL

M. SPARES

Valve-check CAR401

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

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The parts listed here must not be installed anymore on aircraft which have accomplished this

Service Bulletin or which have the equivalent production modification embodied.

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

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This Page Intentionally Left Blank

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SERVICE BULLETIN

2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

(1) Procurement Addresses

AIRBUS Material, Logistics and Suppliers do not stock standard hardware as competitive

multiple suppliers ensure access to minimum prices. AIRBUS recommends Customers

with aircraft shown in the effectivity of this Service Bulletin to send a purchase order to

KLX Aerospace Solutions. The address is:

Component COMPD01 KLX Aerospace Solutions.

10000 NW 15th Terrace Miami

FL 33172

USA

Tel EMEA: +49 (0) 40 822 285 31500

Tel US: +1 305 925 2600

Tel ASIA: +1 310 900 1300

Fax EMEA: +49 (0) 40 822 285 31010

Fax US: +1 305 507 7191

Fax ASIA: +1 310 819 1200

SITA: MIAMMCR

E-Mail: AOGdesk@klx.com

internet: http://www.KLXaerospace.com

or, alternatively any other source on the open

market.

Vendor parts are to be procured from

Equipment BFEZ01 UTC AEROSPACE SYSTEMS (UTAS)

13 AVENUE DE L’EGUILLETTE

95310 SAINT OUEN L’AUMONE

FRANCE

For ordering by fax: +33 (0)1 34 32 63 10

For ordering by phone: +33 (0)1 34 32 63 00

(2) Price and Availability

No AIRBUS kit will be provided.

Operator supplied standard hardware parts required to accomplish this Service Bulletin

are to be supplied from the Operator’s stock.

B. INDUSTRY SUPPORT INFORMATION

This Service Bulletin is the subject of an AIRBUS monitored retrofit campaign.

For the organisation of this retrofit, you are kindly requested to contact AIRBUS retrofit

management department.

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

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SERVICE BULLETIN

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

E-mail: monitored.retrofit@airbus.com

AIRBUS will credit the man hours indicated in this Service Bulletin at the agreed in-house

warranty labour rate for claims received not later than 90 days after completion of the last

affected aircraft of your fleet, for the accomplishment of this Service Bulletin before Jul 30/17.

C. LIST OF COMPONENTS

No Kit

D. LIST OF MATERIALS - OPERATOR SUPPLIED

(1) Consumable Materials

To accomplish this Service Bulletin it is necessary to use the expendable parts listed in

the subsequent referenced tasks: AMM Task 20-23-22-910-801.

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO CML

MAT. No.

QTY PER A/C SEE

NOTES

Phosphate Ester Hydraulic FluidGeneral Power02ABA1 As required

Varnish Polyurethane-- Marking

Structure

04SAB2 As required

Varnish Polyurethane-Low Voc

External Structure

04SBA3 As required

Non Aqueous Cleaner - General 08BAA9 As required

Non Aqueous Cleaner Petroleum

Based

08BBB1 As required

Wire-Locking Dia: 1 Mm (0.041

Inch) Cres

14QGC1 As required

Textile - Lint Free Cotton 14SBA1 As required

(2) Components

Component COMPD01

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

NOTES

2 NAS1612-24 4 PACKING (2) 818114 03

4 NAS1612-8 2 PACKING

8 NAS1612-16 8 PACKING

14 NAS1612-10 3 PACKING

15 NAS1612-12 3 PACKING

21 NAS1612-4 1 PACKING

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

shall be ordered as necessary through the given channel.

(3) Equipment

Equipment BFEZ01

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

NOTES

3 CAR402 4 VALVE (3) CAR401 03

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

Common Support Data Dictionary (CSDD), Chapter 2.

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

shall be ordered as necessary through the given channel.

E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

For the table to identify the PN evolution of the Green, Blue and Yellow system HP Hydraulic

Manifolds, refer to Fig. A-GABAA given in Appendix 01: PN Evolution of the Green, Blue and

Yellow System HP Hydraulic Manifolds .

F. TOOLING

(1) Tooling - Price and Availability

(a) Procurement Addresses

NOTE: Tooling that follows must be requested for aircraft in CONF 002

only.

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:

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SERVICE BULLETIN

Standard tool TOOLD01 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

As an alternative, the operators can

manufacture the tool kit locally at their

workshop, refer to Appendix 02: Local

Manufacture of Tooling .

(b) Price and Availability

Standard tool TOOLD01

Cost 1,660.00 USD

Availability 60 calendar days from receipt of order

(2) Tools

Standard tool TOOLD01

ITEM TOOL N ̊ TOOL NAME QTY SEE

NOTES

54 97F29108805000 Kit-Instl, CAR401 VLV 1

(3) Special Tools

None

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3. ACCOMPLISHMENT INSTRUCTIONS

Task 293125-831-854-001 - Modify the Green HP Hydraulic Manifold on Aircraft

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

INCLUDED IN THE REFERENCED PROCEDURES.

CAUTION: DO NOT WORK ON ALL THREE HYDRAULIC SYSTEMS DURING THE SAME

MAINTENANCE INPUT WITH THE SAME MAINTENANCE PERSONNEL. THIS

IS TO MAKE SURE THAT A POSSIBLE MAINTENANCE ERROR ON ONE

SYSTEM IS NOT DONE AGAIN ON A DIFFERENT SYSTEM. A MAINTENANCE

ERROR ON MORE THAN ONE HYDRAULIC SYSTEM CAN CAUSE SYSTEM

FAILURE ON MULTIPLE SYSTEMS. IF MAINTENANCE IS NECESSARY ON

MORE THAN ONE SYSTEM AT THE SAME TIME AND INVOLVES LINES /

COMPONENTS DISCONNECTION, DIFFERENT MAINTENANCE PERSONNEL

MUST BE USED FOR EACH SYSTEM.

CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP

ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY

AND MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENANCE

WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING,

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

THIS:

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

NECESSARY ON WIRING AND COMPONENTS.

- REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND

OTHER CONTAMINATION.

THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION

AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION.

IF THERE IS CONTAMINATION, REFER TO ESPM 20-55-00.

NOTE: The accomplishment instructions of this Service Bulletin include procedures given

in other documents or in other sections of the Service Bulletin. When the words

’refer to’ are used and the operator has a procedure accepted by the local authority

he belongs to, the accepted alternative procedure can be used. When the words ’in

accordance with’ are used then the given procedure must be followed.

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

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

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

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

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

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

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

NOTE: 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

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SERVICE BULLETIN

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

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

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

the aircraft can be put back into a serviceable condition.

NOTE: AIRBUS generally recommends not to open the three hydraulic systems during

the same maintenance input. Therefore it is recommended to apply this Service

Bulletin during two different maintenance inputs, for instance the Yellow and Blue

hydraulic system first and the Green hydraulic system at a later opportunity.

NOTE: Discarded parts must be managed at the operator’s discretion.

NOTE: This Service Bulletin contains the instructions for the on-aircraft maintenance

necessary to ensure the continued airworthiness of the aircraft.

For any deviations to the instructions contained herein, contact Airbus for further

instructions and approval.

Task Associated Data

**CONF 001

Zone

147 190

Modified FIN

5102JM 5316JM101 5316JM102

Access

Door 197CB 811

Manpower

TOTAL MANHOURS 7.50

ELAPSED TIME (HOURS) 7.50

**CONF 002

Manpower

TOTAL MANHOURS 0.00

**CONF ALL

A. GENERAL

**CONF 001

(1) Subtask 293125-910-207-002 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

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SERVICE BULLETIN

References

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

06-31-53, Page Block 001

06-41-53, Page Block 001

Task 20-11-11-911-803

Task 20-29-00-911-801

Task 29-00-00-910-805

Consumable Material List (CML)

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

Consumable Materials List (CML).

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

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

(d) For the identification of access panels, refer to AMM 06-41-53, Page Block 001.

(e) For the safety procedures of the hydraulic systems, refer to AMM Task

29-00-00-910-805.

(f) For the removal/installation of O-ring seals, refer to AMM Task 20-29-00-911-801.

(g) Put a blanking plug on an open manifold port.

(h) For wirelocking safety procedures and warnings, refer to AMM Task

20-11-11-911-803.

(2) Subtask 293125-839-207-001 - 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

None

**CONF ALL

B. PREPARATION

**CONF 001

(1) Subtask 293125-941-208-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

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References

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

Task 20-23-22-910-801

Task 29-11-53-000-806

NOTE: The items given in this note 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 are 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.

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

12-34-24-860-802.

(b) Do the Job Set-up procedure for the removal of the CV FIN 5316JM101 and FIN

5316JM102, refer to AMM Task 29-11-53-000-806.

(c) Inspect the red marking on all the manifold unions. Apply red marking on the

unions where it is not visible, refer to AMM Task 20-23-22-910-801.

**CONF 002

None

**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 293125-831-209-001 - Modify the Green HP Manifold (FIN 5102JM)

Work Zones and Access Panels

Zone Access/Work location

147 Access Door 811, Door 197CB

Work location from Frame 53.1 to Frame 53.2

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Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills AIRFRAME

Material necessary to do the job

Component COMPD01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

2 NAS1612-24 2 PACKING

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

shall be ordered as necessary through the given channel.

Equipment BFEZ01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

3 CAR402 2 VALVE

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

shall be ordered as necessary through the given channel.

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Phosphate Ester Hydraulic

Fluid-General Power

02ABA1 As required

Varnish Polyurethane--

Marking Structure

04SAB2 As required

Non Aqueous Cleaner -

General

08BAA9 As required

Wire-Locking Dia: 1 Mm

(0.041 Inch) Cres

14QGC1 As required

Textile - Lint Free Cotton 14SBA1 As required

References

Aircraft Maintenance Manual (AMM) Task 20-23-22-910-801

Task 29-11-53-000-806

Fig. A-GBAAA

Removal and Installation of the CVs and

Re-identification on the Green Hydraulic

System HP Manifold

Sheet 01

Sheet 02

Sheet 03

(a) Remove the CVs from the Green HP manifold (FIN 5102JM), refer to AMM Task

29-11-53-000-806.

1

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SERVICE BULLETIN

CAUTION: DO NOT USE POINTED, SHARP OR METAL TOOLS TO

REMOVE THE O-RING OR SQUARE SEAL OR BACK-UP

RINGS. SHARP EDGES CAN CAUSE DAMAGE TO THE

BOBBINS (GROOVES OR SEAL CONTACT SURFACES).

As shown in Fig. A-GBAAA Sheet 01, View B, cut and discard the lockwire

then remove:

FIN 5316JM101

1 Valve-check CAR401 Item (3) Discard

FIN 5316JM101

1 Seal Assy 818114 Item (2) Discard

and

FIN 5316JM102

1 Valve-check CAR401 Item (3) Discard

FIN 5316JM102

1 Seal Assy 818114 Item (2) Discard

(b) Install the CVs on the Green HP manifold (FIN 5102JM).

1 Clean the related components and work areas with:

Non Aqueous

Cleaner - General

08BAA9 As required

and

Textile - Lint Free

Cotton

14SBA1 As required

2

CAUTION: ONLY USE THE SPECIFIED LUBRICANT TO LUBRICATE

THE FITTING THREADS.

Apply to the threads of the CV:

Phosphate Ester

Hydraulic FluidGeneral Power

02ABA1 As required

3 Discard the storage seals from the new CVs.

4 As shown in Fig. A-GBAAA Sheet 01, View B and Fig. A-GBAAA Sheet 03,

install:

FIN 5316JM101

1 Valve-check CAR402 Item 3

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FIN 5316JM101

1 Packing NAS1612-24 Item 2

and

FIN 5316JM102

1 Valve-check CAR402 Item 3

FIN 5316JM102

1 Packing NAS1612-24 Item 2

a Before installation, make sure that the back-up ring is flush with the

groove in the CVs, Item 3.

(c) Torque the CVs, Item 3, two times:

1 Torque the CV between 230 and 250 Nm (169.64-184.39 lbf.ft).

2 Undo the CV by a 1/8th turn.

3 Torque the CV between 230 and 250 Nm (169.64-184.39 lbf.ft).

(d) Make a red mark on the CV and the manifold, refer to AMM Task

20-23-22-910-801.

1 Use:

Varnish

Polyurethane--

Marking Structure

04SAB2 As required

(e) As shown in Fig. A-GBAAA Sheet 01, View B, safety the two CVs, Item 3, with:

Wire-Locking Dia: 1

Mm (0.041 Inch)

Cres

14QGC1 As required

(2) Subtask 293125-930-208-001 - Reidentify the Green HP Manifold (FIN 5102JM)

Work Zones and Access Panels

Zone Access/Work location

147 Access Door 811, Door 197CB

Work location from Frame 53.1 to Frame 53.2

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills AIRFRAME

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Material necessary to do the job

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Varnish Polyurethane-Low

Voc External Structure

04SBA3 As required

Non Aqueous Cleaner

Petroleum Based

08BBB1 As required

Textile - Lint Free Cotton 14SBA1 As required

References

Process and Material Specification

(PMS)

Process and Material Specification (PMS)

01-06-12

Fig. A-GBAAA

Removal and Installation of the CVs and

Re-identification on the Green Hydraulic

System HP Manifold

Sheet 01

Sheet 02

Sheet 03

Fig. A-GABAA

PN Evolution of the Green, Blue and

Yellow System HP Hydraulic Manifolds

Sheet 01

(a) Re-identify the Green HP Manifold (FIN 5102JM), refer to Process and Material

Specification (PMS) 01-06-12, Fig. A-GBAAA Sheet 01 and Fig. A-GBAAA Sheet

02, Views C and D for information and the table given in Appendix 01: PN

Evolution of the Green, Blue and Yellow System HP Hydraulic Manifolds , refer to

Fig. A-GABAA Sheet 01.

1 Clean the Manifold identification PN located on the body of the Green HP

Manifold (FIN 5102JM), use:

Textile - Lint Free

Cotton

14SBA1 As required

made moist with

Non Aqueous

Cleaner Petroleum

Based

08BBB1 As required

2 Use an indelible ink pen to re-identify the Green HP Manifold with the new

PN,Fig. A-GABAA Sheet 01 refer to the table given in Appendix 01: PN

Evolution of the Green, Blue and Yellow System HP Hydraulic Manifolds ,

refer to Fig. A-GABAA Sheet 01.

NOTE: If the old HP manifold PN cannot be found at the location

shown in Fig. A-GBAAA Sheet 02, Views C and D, the IPC

body manifold PN should be used to find the new HP manifold

PN, refer to the table given in Appendix 01: PN Evolution of

the Green, Blue and Yellow System HP Hydraulic Manifolds ,

refer to Fig. A-GABAA Sheet 01.

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SERVICE BULLETIN

NOTE: In case the old PN is written in the hidden face of the Green

HP Manifold, cross the old PN and reidentify the manifold on a

visible face.

3 Apply varnish to the new identification PN, use:

Varnish

Polyurethane-Low

Voc External

Structure

04SBA3 As required

**CONF 002

None

**CONF ALL

D. TEST

**CONF 001

(1) Subtask 293125-730-208-001 - Test of the Green Hydraulic Manifold (FIN 5102JM)

Work Zones and Access Panels

Zone Access/Work location

147 Access Door 811, Door 197CB

Work location from Frame 53.1 to Frame 53.2

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 20-23-11-400-801

Task 20-23-11-917-801

Task 20-23-11-917-802

Task 20-23-22-910-801

Task 20-29-00-911-801

Task 29-00-00-210-801

Task 29-00-00-863-801

Task 29-00-00-864-801

Task 29-11-53-400-806

Fig. A-GCAAA

Torque Check of the Hydraulic Unions

on the Green Hydraulic System HP

Manifold

Sheet 01

(a) Inspect the red marking on all the plug-in unions on the manifold.

1 If any red marking is not aligned:

a Disconnect the pipe from the plug-in union.

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b Remove the plug-in union from the manifold.

c Replace the packing of the plug-in union with a new one, refer to AMM

Task 20-29-00-911-801.

d As shown in Fig. A-GCAAA Sheet 01, View B, install and tighten

all removed plug-in unions on the manifold, refer to AMM Task

20-29-00-911-801 and Table 1, below.

e As shown in Fig. A-GCAAA Sheet 01, View B, install and tighten the pipe

to the plug-in union and manifold, refer to AMM Task 20-23-11-917-802

and Table 1, below.

Item No. Pipe Torque Value (Nm) Item No. Union Torque Value

(Nm)

(26) 54-59 (5) 34.7-35.8

(25) 85-95 (9) 116.4-118.6

Table 1

(b) Tighten all connections of the pipes connected to the manifold on both sides

which have been not already tightened during previous step, refer to AMM Task

20-23-11-400-801, AMM Task 20-23-11-917-801 and Table 1, above.

(c) Make a new red mark on any of the unions where the red mark is no longer aligned

or not clearly visible, refer to AMM Task 20-23-22-910-801.

(d) Remove the safety clip(s) and/or tag(s) and close/unlock the circuit breaker(s) as

specified in the Job Set-up in the Installation of the Check-Valves, refer to AMM

Task 29-11-53-400-806.

(e) Pressurize the Green hydraulic system with the electric pump, refer to AMM Task

29-00-00-863-801.

(f) Make sure there are no leaks from the unions on the manifold.

(g) Make sure there are no leaks from the connections of the CVs.

(h) Make sure there are no leaks from the pipe connections.

(i) Check for air in the Green hydraulic system, refer to AMM Task 29-00-00-210-801.

(j) Depressurize the Green hydraulic system, refer to AMM Task 29-00-00-864-801.

**CONF 002

None

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

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**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 293125-942-207-001 - Close-up

Work Zones and Access Panels

Zone Access/Work location

190

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 29-11-53-400-806

(a) Make sure that the work areas are clean and clear of tools and other items of

equipment.

(b) Do the Job Close-up procedure for the installation of the CV FIN 5316JM101 and

FIN 5316JM102, refer to AMM Task 29-11-53-400-806.

(c) Put the aircraft back to its initial configuration.

**CONF 002

None

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

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This Page Intentionally Left Blank

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SERVICE BULLETIN

Task 293125-831-855-001 - Modify the Blue HP Hydraulic Manifold on Aircraft

**CONF ALL

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

INCLUDED IN THE REFERENCED PROCEDURES.

CAUTION: DO NOT WORK ON ALL THREE HYDRAULIC SYSTEMS DURING THE SAME

MAINTENANCE INPUT WITH THE SAME MAINTENANCE PERSONNEL. THIS

IS TO MAKE SURE THAT A POSSIBLE MAINTENANCE ERROR ON ONE

SYSTEM IS NOT DONE AGAIN ON A DIFFERENT SYSTEM. A MAINTENANCE

ERROR ON MORE THAN ONE HYDRAULIC SYSTEM CAN CAUSE SYSTEM

FAILURE ON MULTIPLE SYSTEMS. IF MAINTENANCE IS NECESSARY ON

MORE THAN ONE SYSTEM AT THE SAME TIME AND INVOLVES LINES /

COMPONENTS DISCONNECTION, DIFFERENT MAINTENANCE PERSONNEL

MUST BE USED FOR EACH SYSTEM.

CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP

ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY

AND MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENANCE

WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING,

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

THIS:

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

NECESSARY ON WIRING AND COMPONENTS.

- REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND

OTHER CONTAMINATION.

THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION

AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION.

IF THERE IS CONTAMINATION, REFER TO ESPM 20-55-00.

NOTE: The accomplishment instructions of this Service Bulletin include procedures given

in other documents or in other sections of the Service Bulletin. When the words

’refer to’ are used and the operator has a procedure accepted by the local authority

he belongs to, the accepted alternative procedure can be used. When the words ’in

accordance with’ are used then the given procedure must be followed.

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

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

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

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

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

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

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

NOTE: 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

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

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SERVICE BULLETIN

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

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

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

the aircraft can be put back into a serviceable condition.

NOTE: AIRBUS generally recommends not to open the three hydraulic systems during

the same maintenance input. Therefore it is recommended to apply this Service

Bulletin during two different maintenance inputs, for instance the Yellow and Blue

hydraulic system first and the Green hydraulic system at a later opportunity.

NOTE: Discarded parts must be managed at the operator’s discretion.

NOTE: This Service Bulletin contains the instructions for the on-aircraft maintenance

necessary to ensure the continued airworthiness of the aircraft.

For any deviations to the instructions contained herein, contact Airbus for further

instructions and approval.

Task Associated Data

**CONF 001

Zone

190 195

Modified FIN

5316JM201 6103JM

Access

Door 195BB 811

Manpower

TOTAL MANHOURS 7.50

ELAPSED TIME (HOURS) 7.50

**CONF 002

Manpower

TOTAL MANHOURS 0.00

**CONF ALL

A. GENERAL

**CONF 001

(1) Subtask 293125-910-208-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

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SERVICE BULLETIN

References

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

06-31-53, Page Block 001

06-41-53, Page Block 001

Task 20-11-11-911-803

Task 20-29-00-911-801

Task 29-00-00-910-805

Consumable Material List (CML)

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

Consumable Materials List (CML).

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

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

(d) For the identification of access panels, refer to AMM 06-41-53, Page Block 001.

(e) For the safety procedures of the hydraulic systems, refer to AMM Task

29-00-00-910-805.

(f) For the removal/installation of O-ring seals, refer to AMM Task 20-29-00-911-801.

(g) Put a blanking plug on an open manifold port.

(h) For wirelocking safety procedures and warnings, refer to AMM Task

20-11-11-911-803.

(2) Subtask 293125-839-208-001 - 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

None

**CONF ALL

B. PREPARATION

**CONF 001

(1) Subtask 293125-941-209-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

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References

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

Task 20-23-22-910-801

Task 29-12-53-000-806

NOTE: The items given in this note 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 are 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.

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

12-34-24-860-802.

(b) Do the Job Set-up procedure for the removal of the CV FIN 5316JM201, refer to

AMM Task 29-12-53-000-806.

(c) Inspect the red marking on all the manifold unions. Apply red marking on the

unions where it is not visible, refer to AMM Task 20-23-22-910-801.

**CONF 002

None

**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 293125-831-210-001 - Modify the Blue HP Manifold (FIN 6103JM)

Work Zones and Access Panels

Zone Access/Work location

195 Access Door 811, Door 195BB

Work location from Frame 45 to Frame 46

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

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Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills AIRFRAME

Material necessary to do the job

Component COMPD01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

2 NAS1612-24 1 PACKING

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

shall be ordered as necessary through the given channel.

Equipment BFEZ01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

3 CAR402 1 VALVE

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

shall be ordered as necessary through the given channel.

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Phosphate Ester Hydraulic

Fluid-General Power

02ABA1 As required

Varnish Polyurethane--

Marking Structure

04SAB2 As required

Non Aqueous Cleaner -

General

08BAA9 As required

Wire-Locking Dia: 1 Mm

(0.041 Inch) Cres

14QGC1 As required

Textile - Lint Free Cotton 14SBA1 As required

References

Aircraft Maintenance Manual (AMM) Task 20-23-22-910-801

Task 29-12-53-000-806

Fig. A-GBBAA

Removal and Installation of the CVs and

Re-identification of the Blue Hydraulic

System HP Manifold

Sheet 01

Sheet 02

Sheet 03

(a) Remove the CV from the Blue HP manifold (FIN 6103JM), refer to AMM Task

29-12-53-000-806.

1

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CAUTION: DO NOT USE POINTED, SHARP OR METAL TOOLS TO

REMOVE THE O-RING OR SQUARE SEAL OR BACK-UP

RINGS. SHARP EDGES CAN CAUSE DAMAGE TO THE

BOBBINS (GROOVES OR SEAL CONTACT SURFACES).

As shown in Fig. A-GBBAA Sheet 01, View B, cut and discard the lockwire

then remove:

FIN 5316JM201

1 Valve-check CAR401 Item (3) Discard

FIN 5316JM201

1 Seal Assy 818114 Item (2) Discard

(b) Install the CV on the Blue HP manifold (FIN 6103JM).

1 Clean the related components and work areas with:

Non Aqueous

Cleaner - General

08BAA9 As required

and

Textile - Lint Free

Cotton

14SBA1 As required

2

CAUTION: ONLY USE THE SPECIFIED LUBRICANT TO LUBRICATE

THE FITTING THREADS.

Apply to the threads of the CV:

Phosphate Ester

Hydraulic FluidGeneral Power

02ABA1 As required

3 Discard the storage seals from the new CVs.

4 As shown in Fig. A-GBBAA Sheet 01, View B and Fig. A-GBBAA Sheet 03,

install:

FIN 5316JM201

1 Valve-check CAR402 Item 3

FIN 5316JM201

1 Packing NAS1612-24 Item 2

a Before installation, make sure that the back-up ring is flush with the

groove in the CVs, Item 3.

(c) Torque the CV, Item 3, two times:

1 Torque the CV between 230 and 250 Nm (169.64-184.39 lbf.ft).

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2 Undo the CV by a 1/8th turn.

3 Torque the CV between 230 and 250 Nm (169.64-184.39 lbf.ft).

(d) Make a red mark on the CV and the manifold, refer to AMM Task

20-23-22-910-801.

1 Use:

Varnish

Polyurethane--

Marking Structure

04SAB2 As required

(e) As shown in Fig. A-GBBAA Sheet 01, View B, safety the CV, Item 3, with:

Wire-Locking Dia: 1

Mm (0.041 Inch)

Cres

14QGC1 As required

(2) Subtask 293125-930-209-001 - Reidentify the Blue Manifold (FIN 6103JM)

Work Zones and Access Panels

Zone Access/Work location

195 Access Door 811, Door 195BB

Work location from Frame 45 to Frame 46

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills AIRFRAME

Material necessary to do the job

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Varnish Polyurethane-Low

Voc External Structure

04SBA3 As required

Non Aqueous Cleaner

Petroleum Based

08BBB1 As required

Textile - Lint Free Cotton 14SBA1 As required

References

Process and Material Specification

(PMS)

Process and Material Specification (PMS)

01-06-12

Fig. A-GBBAA

Removal and Installation of the CVs and

Re-identification of the Blue Hydraulic

System HP Manifold

Sheet 01

Sheet 02

Sheet 03

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References

Fig. A-GABAA

PN Evolution of the Green, Blue and

Yellow System HP Hydraulic Manifolds

Sheet 01

(a) Re-identify the Blue HP Manifold (FIN 6103JM), refer to Process and Material

Specification (PMS) 01-06-12, Fig. A-GBBAA Sheet 01 and Fig. A-GBBAA Sheet

02, View C for information and the table given in Appendix 01: PN Evolution of the

Green, Blue and Yellow System HP Hydraulic Manifolds , refer to Fig. A-GABAA

Sheet 01.

1 Clean the Manifold identification PN located on the body of the Blue HP

Manifold (FIN 6103JM) use:

Textile - Lint Free

Cotton

14SBA1 As required

made moist with

Non Aqueous

Cleaner Petroleum

Based

08BBB1 As required

2 Use an indelible ink pen to re-identify the Blue HP Manifold with the new PN,

refer to the table given in Appendix 01: PN Evolution of the Green, Blue and

Yellow System HP Hydraulic Manifolds , refer to Fig. A-GABAA Sheet 01.

NOTE: If the old HP manifold PN cannot be found at the location

shown in Fig. A-GBBAA Sheet 02, View C, the IPC body

manifold PN should be used to find the new HP manifold PN,

refer to the table given in Appendix 01: PN Evolution of the

Green, Blue and Yellow System HP Hydraulic Manifolds , refer

to Fig. A-GABAA Sheet 01.

3 Apply varnish to the new identification PN, use:

Varnish

Polyurethane-Low

Voc External

Structure

04SBA3 As required

**CONF 002

None

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

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**CONF ALL

D. TEST

**CONF 001

(1) Subtask 293125-730-209-001 - Test the Blue HP Manifold

Work Zones and Access Panels

Zone Access/Work location

195 Access Door 811, Door 195BB

Work location from Frame 45 to Frame 46

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 20-23-11-400-801

Task 20-23-11-917-801

Task 20-23-11-917-802

Task 20-23-22-910-801

Task 20-29-00-911-801

Task 29-00-00-210-801

Task 29-00-00-863-802

Task 29-00-00-864-802

Task 29-12-53-400-805

Fig. A-GBBAA

Removal and Installation of the CVs and

Re-identification of the Blue Hydraulic

System HP Manifold

Sheet 01

Sheet 02

Sheet 03

Fig. A-GDAAA

Torque Check of the Hydraulic Unions

on the Blue Hydraulic System HP

Manifold

Sheet 01

(a) Inspect the red marking on all the plug-in unions on the manifold.

1 If any red marking is not aligned:

a Disconnect the pipe from the plug-in union.

b Remove the plug-in union from the manifold.

c Replace the packing of the plug-in union with a new one, refer to AMM

Task 20-29-00-911-801.

d As shown in Fig. A-GDAAA Sheet 01, View B, install and tighten

all removed plug-in unions on the manifold, refer to AMM Task

20-29-00-911-801 and Table 2, below.

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e As shown in Fig. A-GDAAA Sheet 01, View B, install and tighten the pipe

to the plug-in union and manifold, refer to AMM Task 20-23-11-917-802

and Table 2, below.

Item No. Pipe Torque Value (Nm) Item No. Union Torque Value

(Nm)

(29) 85-95 (9) 116.4-118.6

(30) 85-95 (16) 72.9-74

(31) 54-59 (17) 34.7-35.8

(32) 81-89 (12) 116.4-118.6

(33) 75-83 (13) 50.3-51.4

(34) 85-95 (16) 116.4-118.6

(35) 75-83 (13) 50.3-51.4

Table 2

(b) Tighten all connections of the pipes connected to the manifold on both sides

which have been not already tightened during previous step, refer to AMM Task

20-23-11-400-801, AMM Task 20-23-11-917-801 and Table 2, above.

(c) Make a new red mark on all the unions where the red mark is not aligned or no

longer visible, refer to AMM Task 20-23-22-910-801.

(d) Remove the safety clip(s) and/or tag(s) and close/unlock the circuit breaker(s) as

specified in the Job Set-up in the Installation of the Blue HP Manifold-Supply

Check-Valves, refer to AMM Task 29-12-53-400-805.

(e) Pressurize the Blue hydraulic system with the electric pump, refer to AMM Task

29-00-00-863-802.

(f) Make sure there are no leaks from the unions on the manifold.

(g) Make sure there are no leaks from the connections of the CV.

(h) Make sure there are no leaks from the pipe connections.

(i) Check for air in the Blue hydraulic system, refer to AMM Task 29-00-00-210-801.

(j) Depressurize the Blue hydraulic system, refer to AMM Task 29-00-00-864-802.

**CONF 002

None

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 46

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SERVICE BULLETIN

**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 293125-942-208-001 - Close-up

Work Zones and Access Panels

Zone Access/Work location

190

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 29-12-53-400-806

(a) Make sure that the work areas are clean and clear of tools and other items of

equipment.

(b) Do the Job Close-up procedure for the installation of the CV FIN 5316JM201, refer

to AMM Task 29-12-53-400-806.

(c) Put the aircraft back to its initial configuration.

**CONF 002

None

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 47

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This Page Intentionally Left Blank

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REVISION No.: 03 - Apr 08/16 Page: 48

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SERVICE BULLETIN

Task 293125-831-856-001 - Modify the Yellow HP Hydraulic Manifold on Aircraft

**CONF ALL

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

INCLUDED IN THE REFERENCED PROCEDURES.

CAUTION: DO NOT WORK ON ALL THREE HYDRAULIC SYSTEMS DURING THE SAME

MAINTENANCE INPUT WITH THE SAME MAINTENANCE PERSONNEL. THIS

IS TO MAKE SURE THAT A POSSIBLE MAINTENANCE ERROR ON ONE

SYSTEM IS NOT DONE AGAIN ON A DIFFERENT SYSTEM. A MAINTENANCE

ERROR ON MORE THAN ONE HYDRAULIC SYSTEM CAN CAUSE SYSTEM

FAILURE ON MULTIPLE SYSTEMS. IF MAINTENANCE IS NECESSARY ON

MORE THAN ONE SYSTEM AT THE SAME TIME AND INVOLVES LINES /

COMPONENTS DISCONNECTION, DIFFERENT MAINTENANCE PERSONNEL

MUST BE USED FOR EACH SYSTEM.

CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP

ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY

AND MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENANCE

WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING,

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

THIS:

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

NECESSARY ON WIRING AND COMPONENTS.

- REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND

OTHER CONTAMINATION.

THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION

AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION.

IF THERE IS CONTAMINATION, REFER TO ESPM 20-55-00.

NOTE: The accomplishment instructions of this Service Bulletin include procedures given

in other documents or in other sections of the Service Bulletin. When the words

’refer to’ are used and the operator has a procedure accepted by the local authority

he belongs to, the accepted alternative procedure can be used. When the words ’in

accordance with’ are used then the given procedure must be followed.

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

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

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

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

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

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

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

NOTE: 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

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 49

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SERVICE BULLETIN

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

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

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

the aircraft can be put back into a serviceable condition.

NOTE: AIRBUS generally recommends not to open the three hydraulic systems during

the same maintenance input. Therefore it is recommended to apply this Service

Bulletin during two different maintenance inputs, for instance the Yellow and Blue

hydraulic system first and the Green hydraulic system at a later opportunity.

NOTE: Discarded parts must be managed at the operator’s discretion.

NOTE: This Service Bulletin contains the instructions for the on-aircraft maintenance

necessary to ensure the continued airworthiness of the aircraft.

For any deviations to the instructions contained herein, contact Airbus for further

instructions and approval.

Task Associated Data

**CONF 001

Zone

195 196

Modified FIN

5316JM301 7103JM

Access

Door 195BB 196BB 811

Manpower

TOTAL MANHOURS 7.50

ELAPSED TIME (HOURS) 7.50

**CONF 002

Manpower

TOTAL MANHOURS 0.00

**CONF ALL

A. GENERAL

**CONF 001

(1) Subtask 293125-910-209-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 50

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SERVICE BULLETIN

References

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

06-31-53, Page Block 001

06-41-53, Page Block 001

Task 20-11-11-911-803

Task 20-29-00-911-801

Task 29-00-00-910-805

Consumable Material List (CML)

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

Consumable Materials List (CML).

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

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

(d) For the identification of access panels, refer to AMM 06-41-53, Page Block 001.

(e) For the safety procedures of the hydraulic systems, refer to AMM Task

29-00-00-910-805.

(f) For the removal/installation of O-ring seals, refer to AMM Task 20-29-00-911-801.

(g) Put a blanking plug on an open manifold port.

(h) For wirelocking safety procedures and warnings, refer to AMM Task

20-11-11-911-803.

(2) Subtask 293125-839-209-001 - 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

None

**CONF ALL

B. PREPARATION

**CONF 001

(1) Subtask 293125-941-210-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 51

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SERVICE BULLETIN

References

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

Task 20-23-22-910-801

Task 29-13-53-000-804

NOTE: The items given in this note 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 are 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.

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

12-34-24-860-802.

(b) Do the Job Set-up procedure for the removal of the CV FIN 5316JM301, refer to

AMM Task 29-13-53-000-804.

(c) Inspect the red marking on all the manifold unions. Apply red marking on the

unions where it is not visible, refer to AMM Task 20-23-22-910-801.

**CONF 002

None

**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 293125-831-211-001 - Modify the Yellow HP Manifold (FIN 7103JM)

Work Zones and Access Panels

Zone Access/Work location

196 Access Door 811, Door 196BB

Work location from Frame 45 to Frame 46

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 52

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Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills AIRFRAME

Material necessary to do the job

Component COMPD01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

2 NAS1612-24 1 PACKING

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

shall be ordered as necessary through the given channel.

Equipment BFEZ01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

3 CAR402 1 VALVE

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

shall be ordered as necessary through the given channel.

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Phosphate Ester Hydraulic

Fluid-General Power

02ABA1 As required

Varnish Polyurethane--

Marking Structure

04SAB2 As required

Non Aqueous Cleaner -

General

08BAA9 As required

Wire-Locking Dia: 1 Mm

(0.041 Inch) Cres

14QGC1 As required

Textile - Lint Free Cotton 14SBA1 As required

References

Aircraft Maintenance Manual (AMM) Task 20-23-22-910-801

Task 29-13-53-000-804

Process and Material Specification

(PMS)

Process and Material Specification (PMS)

01-06-12

Fig. A-GBCAA

Removal and Installation of the CVs and

Re-identification of the Yellow Hydraulic

System HP Manifold

Sheet 01

Sheet 02

Sheet 03

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 53

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SERVICE BULLETIN

(a) Remove the CV, Item 3 from the Yellow HP manifold (FIN 7103JM), refer to AMM

Task 29-13-53-000-804.

1

CAUTION: DO NOT USE POINTED, SHARP OR METAL TOOLS TO

REMOVE THE O-RING OR SQUARE SEAL OR BACK-UP

RINGS. SHARP EDGES CAN CAUSE DAMAGE TO THE

BOBBINS (GROOVES OR SEAL CONTACT SURFACES).

As shown in Fig. A-GBCAA Sheet 01, View B, cut and discard the lockwire

then remove:

FIN 5316JM301

1 Valve-check CAR401 Item (3) Discard

FIN 5316JM301

1 Seal Assy 818114 Item (2) Discard

(b) Install the CV on the Yellow HP manifold (FIN 7103JM).

1 Clean the related components and work areas with:

Non Aqueous

Cleaner - General

08BAA9 As required

and

Textile - Lint Free

Cotton

14SBA1 As required

2

CAUTION: ONLY USE THE SPECIFIED LUBRICANT TO LUBRICATE

THE FITTING THREADS.

Apply to the threads of the CV:

Phosphate Ester

Hydraulic FluidGeneral Power

02ABA1 As required

3 Discard the storage seals from the new CVs.

4 As shown in Fig. A-GBCAA Sheet 01, View B and Fig. A-GBCAA Sheet 03,

install:

FIN 5316JM301

1 Valve-check CAR402 Item 3

FIN 5316JM301

1 Packing NAS1612-24 Item 2

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

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SERVICE BULLETIN

a Before installation, make sure that the back-up ring is flush with the

groove in the CVs, Item 3.

(c) Torque the CV, Item 3, two times:

1 Torque the CV between 230 and 250 Nm (169.64-184.39 lbf.ft).

2 Undo the CV by a 1/8th turn.

3 Torque the CV between 230 and 250 Nm (169.64-184.39 lbf.ft).

(d) Make a red mark on the CV and the manifold, refer to AMM Task

20-23-22-910-801.

1 Use:

Varnish

Polyurethane--

Marking Structure

04SAB2 As required

(e) As shown in Fig. A-GBCAA Sheet 01, View B, safety the CV, Item 3, with:

Wire-Locking Dia: 1

Mm (0.041 Inch)

Cres

14QGC1 As required

(2) Subtask 293125-930-210-001 - Reidentify the Yellow HP Manifold (FIN 7103JM)

Work Zones and Access Panels

Zone Access/Work location

195 Access Door 811, Door 195BB

Work location from Frame 45 to Frame 46

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills AIRFRAME

Material necessary to do the job

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Varnish Polyurethane-Low

Voc External Structure

04SBA3 As required

Non Aqueous Cleaner

Petroleum Based

08BBB1 As required

Textile - Lint Free Cotton 14SBA1 As required

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 55

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SERVICE BULLETIN

References

Process and Material Specification

(PMS)

Process and Material Specification (PMS)

01-06-12

Fig. A-GBCAA

Removal and Installation of the CVs and

Re-identification of the Yellow Hydraulic

System HP Manifold

Sheet 01

Sheet 02

Sheet 03

Fig. A-GABAA

PN Evolution of the Green, Blue and

Yellow System HP Hydraulic Manifolds

Sheet 01

(a) Re-identify the Yellow HP Manifold (FIN 7103JM), refer to Process and Material

Specification (PMS) 01-06-12, Fig. A-GBCAA Sheet 01 and Fig. A-GBCAA Sheet

02, Views C and D for information and the table given in Appendix 01: PN

Evolution of the Green, Blue and Yellow System HP Hydraulic Manifolds , refer to

Fig. A-GABAA Sheet 01.

1 Clean the Manifold identification PN located on the body of the Yellow HP

Manifold (FIN 7103JM), use:

Textile - Lint Free

Cotton

14SBA1 As required

made moist with

Non Aqueous

Cleaner Petroleum

Based

08BBB1 As required

2 Use an indelible ink pen to re-identify the Yellow HP Manifold with the new

PN, refer to the table given in Appendix 01: PN Evolution of the Green, Blue

and Yellow System HP Hydraulic Manifolds , refer to Fig. A-GABAA Sheet 01.

NOTE: If the old HP manifold PN cannot be found at the location

shown in Fig. A-GBCAA Sheet 02, Views C and D, the IPC

body manifold PN should be used to find the new HP manifold

PN, refer to the table given in Appendix 01: PN Evolution of

the Green, Blue and Yellow System HP Hydraulic Manifolds ,

refer to Fig. A-GABAA Sheet 01.

3 Apply varnish to the new identification PN, use:

Varnish

Polyurethane-Low

Voc External

Structure

04SBA3 As required

**CONF 002

None

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 56

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SERVICE BULLETIN

**CONF ALL

D. TEST

**CONF 001

(1) Subtask 293125-730-210-001 - Test the Yellow HP Manifold (FIN7103JM)

Work Zones and Access Panels

Zone Access/Work location

195 Access Door 811, Door 195BB

Work location from Frame 45 to Frame 46

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 20-23-11-400-801

Task 20-23-11-917-801

Task 20-23-11-917-802

Task 20-23-22-910-801

Task 20-29-00-911-801

Task 29-00-00-210-801

Task 29-00-00-863-803

Task 29-00-00-864-803

Task 29-13-53-400-804

Fig. A-GEAAA

Torque Check of the Hydraulic Unions

on the Yellow Hydraulic System HP

Manifold

Sheet 01

(a) Inspect the red marking on all the plug-in unions on the manifold.

1 If any red marking is not aligned:

a Disconnect the pipe from the plug-in union.

b Remove the plug-in union from the manifold.

c Replace the packing of the plug-in union with a new one, refer to AMM

Task 20-29-00-911-801.

d As shown in Fig. A-GEAAA Sheet 01, View B, install and tighten

all removed plug-in unions on the manifold, refer to AMM Task

20-29-00-911-801 and Table 3, below.

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

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SERVICE BULLETIN

e As shown in Fig. A-GEAAA Sheet 01, View B, install and tighten the pipe

to the plug-in union and manifold, refer to AMM Task 20-23-11-917-802

and Table 3, below.

Item No. Pipe Torque Value (Nm) Item No. Union Torque Value

(Nm)

(36) 15-17 (22) 12.1-13.2

(37) 85-95 (16) 72.9-74

(38) 81-89 (12) 116.4-118.6

(39) 85-95 (9) 116.4-118.6

(41) 75-83 (13) 50.3-51.4

(40) 85-95 (9) 116.4-118.6

Table 3

(b) Tighten all connections of the pipes connected to the manifold on both sides

which have been not already tightened during previous step, refer to AMM Task

20-23-11-400-801, AMM Task 20-23-11-917-801 and Table 3, above.

(c) Make a new red mark on all the unions where the red mark is not aligned or not

clearly visible, refer to AMM Task 20-23-22-910-801.

(d) Remove the safety clip(s) and/or tag(s) and close/unlock the circuit breaker(s) as

specified in the Job Set-up in the Installation of the Yellow HP Manifold-Supply

Check-Valves, refer to AMM Task 29-13-53-400-804.

(e) Pressurize the Yellow hydraulic system with the electric pump, refer to AMM Task

29-00-00-863-803.

(f) Make sure there are no leaks from the unions on the manifold.

(g) Make sure there are no leaks from the connections of the CV.

(h) Make sure there are no leaks from the pipe connections.

(i) Check for air in the Yellow hydraulic system, refer to AMM Task 29-00-00-210-801.

(j) Depressurize the Yellow hydraulic system, refer to AMM Task 29-00-00-864-803.

**CONF 002

None

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 58

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SERVICE BULLETIN

**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 293125-942-209-001 - Close-up

Work Zones and Access Panels

Zone Access/Work location

195

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 29-13-53-400-804

(a) Make sure that the work areas are clean and clear of tools and other items of

equipment.

(b) Do the Job Close-up procedure for the installation of the CV FIN 5316JM301, refer

to AMM Task 29-13-53-400-804.

(c) Put the aircraft back to its initial configuration.

**CONF 002

None

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 59

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This Page Intentionally Left Blank

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 60

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SERVICE BULLETIN

Task 293125-831-848-001 - Modify the Green HP Hydraulic Manifold on Aircraft

**CONF ALL

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

INCLUDED IN THE REFERENCED PROCEDURES.

CAUTION: DO NOT WORK ON ALL THREE HYDRAULIC SYSTEMS DURING THE SAME

MAINTENANCE INPUT WITH THE SAME MAINTENANCE PERSONNEL. THIS

IS TO MAKE SURE THAT A POSSIBLE MAINTENANCE ERROR ON ONE

SYSTEM IS NOT DONE AGAIN ON A DIFFERENT SYSTEM. A MAINTENANCE

ERROR ON MORE THAN ONE HYDRAULIC SYSTEM CAN CAUSE SYSTEM

FAILURE ON MULTIPLE SYSTEMS. IF MAINTENANCE IS NECESSARY ON

MORE THAN ONE SYSTEM AT THE SAME TIME AND INVOLVES LINES /

COMPONENTS DISCONNECTION, DIFFERENT MAINTENANCE PERSONNEL

MUST BE USED FOR EACH SYSTEM.

CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP

ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY

AND MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENANCE

WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING,

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

THIS:

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

NECESSARY ON WIRING AND COMPONENTS.

- REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND

OTHER CONTAMINATION.

THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION

AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION.

IF THERE IS CONTAMINATION, REFER TO ESPM 20-55-00.

NOTE: The accomplishment instructions of this Service Bulletin include procedures given

in other documents or in other sections of the Service Bulletin. When the words

’refer to’ are used and the operator has a procedure accepted by the local authority

he belongs to, the accepted alternative procedure can be used. When the words ’in

accordance with’ are used then the given procedure must be followed.

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

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

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

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

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

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

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

NOTE: 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

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 61

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SERVICE BULLETIN

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

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

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

the aircraft can be put back into a serviceable condition.

NOTE: AIRBUS generally recommends not to open the three hydraulic systems during

the same maintenance input. Therefore it is recommended to apply this Service

Bulletin during two different maintenance inputs, for instance the Yellow and Blue

hydraulic system first and the Green hydraulic system at a later opportunity.

NOTE: Discarded parts must be managed at the operator’s discretion.

NOTE: This Service Bulletin contains the instructions for the on-aircraft maintenance

necessary to ensure the continued airworthiness of the aircraft.

For any deviations to the instructions contained herein, contact Airbus for further

instructions and approval.

Task Associated Data

**CONF 001

Manpower

TOTAL MANHOURS 0.00

**CONF 002

Zone

147 190

Modified FIN

5102JM 5316JM101 5316JM102

Access

Door 197CB 811

Manpower

TOTAL MANHOURS 7.50

ELAPSED TIME (HOURS) 7.50

**CONF ALL

A. GENERAL

**CONF 001

None

**CONF 002

(1) Subtask 293125-910-201-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 62

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SERVICE BULLETIN

References

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

06-31-53, Page Block 001

06-41-53, Page Block 001

Task 20-11-11-911-803

Task 20-29-00-911-801

Task 29-00-00-910-805

Consumable Material List (CML)

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

Consumable Materials List (CML).

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

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

(d) For the identification of access panels, refer to AMM 06-41-53, Page Block 001.

(e) For the safety procedures of the hydraulic systems, refer to AMM Task

29-00-00-910-805.

(f) For the removal/installation of O-ring seals, refer to AMM Task 20-29-00-911-801.

(g) Put a blanking plug on an open manifold port.

(h) For wirelocking safety procedures and warnings, refer to AMM Task

20-11-11-911-803.

(2) Subtask 293125-839-201-001 - 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

None

**CONF 002

(1) Subtask 293125-941-201-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 63

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@A330

SERVICE BULLETIN

References

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

Task 20-23-22-910-801

Task 29-11-53-000-806

NOTE: The items given in this note 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 are 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.

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

12-34-24-860-802.

(b) Do the Job Set-up procedure for the removal of the CV FIN 5316JM101 and FIN

5316JM102, refer to AMM Task 29-11-53-000-806.

(c) Inspect the red marking on all the manifold unions. Apply red marking on the

unions where it is not visible, refer to AMM Task 20-23-22-910-801.

**CONF ALL

C. PROCEDURE

**CONF 001

None

**CONF 002

(1) Subtask 293125-831-201-001 - Modify the Green HP Manifold (FIN 5102JM)

Work Zones and Access Panels

Zone Access/Work location

147 Access Door 811, Door 197CB

Work location from Frame 53.1 to Frame 53.2

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 64

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SERVICE BULLETIN

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills AIRFRAME

Material necessary to do the job

Component COMPD01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

2 NAS1612-24 2 PACKING

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

shall be ordered as necessary through the given channel.

Equipment BFEZ01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

3 CAR402 2 VALVE

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

shall be ordered as necessary through the given channel.

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Phosphate Ester Hydraulic

Fluid-General Power

02ABA1 As required

Varnish Polyurethane--

Marking Structure

04SAB2 As required

Non Aqueous Cleaner -

General

08BAA9 As required

Wire-Locking Dia: 1 Mm

(0.041 Inch) Cres

14QGC1 As required

Textile - Lint Free Cotton 14SBA1 As required

References

Aircraft Maintenance Manual (AMM) Task 20-23-22-910-801

Task 29-11-53-000-806

Fig. A-GBAAA

Removal and Installation of the CVs and

Re-identification on the Green Hydraulic

System HP Manifold

Sheet 01

Sheet 02

Sheet 03

(a) Remove the CVs from the Green HP manifold (FIN 5102JM), refer to AMM Task

29-11-53-000-806.

1

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 65

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SERVICE BULLETIN

CAUTION: DO NOT USE POINTED, SHARP OR METAL TOOLS TO

REMOVE THE O-RING OR SQUARE SEAL OR BACK-UP

RINGS. SHARP EDGES CAN CAUSE DAMAGE TO THE

BOBBINS (GROOVES OR SEAL CONTACT SURFACES).

As shown in Fig. A-GBAAA Sheet 01, View B, cut and discard the lockwire

then remove:

FIN 5316JM101

1 Valve-check CAR401 Item (3) Discard

FIN 5316JM101

1 Seal Assy 818114 Item (2) Discard

and

FIN 5316JM102

1 Valve-check CAR401 Item (3) Discard

FIN 5316JM102

1 Seal Assy 818114 Item (2) Discard

(b) Install the CVs on the Green HP manifold (FIN 5102JM).

1 Clean the related components and work areas with:

Non Aqueous

Cleaner - General

08BAA9 As required

and

Textile - Lint Free

Cotton

14SBA1 As required

2

CAUTION: ONLY USE THE SPECIFIED LUBRICANT TO LUBRICATE

THE FITTING THREADS.

Apply to the threads of the CVs:

Phosphate Ester

Hydraulic FluidGeneral Power

02ABA1 As required

3 Discard the storage seals from the new CVs.

4 As shown in Fig. A-GBAAA Sheet 01, View B and Fig. A-GBAAA Sheet 03,

install:

FIN 5316JM101

1 Valve-check CAR402 Item 3

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 66

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SERVICE BULLETIN

FIN 5316JM101

1 Packing NAS1612-24 Item 2

and

FIN 5316JM102

1 Valve-check CAR402 Item 3

FIN 5316JM102

1 Packing NAS1612-24 Item 2

a Before installation, make sure that the back-up ring is flush with the

groove in the CVs, Item 3.

(c) Torque the CVs, Item 3, two times:

1 Torque the CVs between 230 and 250 Nm (169.64-184.39 lbf.ft).

2 Undo the CVs by a 1/8th turn.

3 Torque the CVs between 230 and 250 Nm (169.64-184.39 lbf.ft).

(d) Make a red mark on the CVs and the manifold, refer to AMM Task

20-23-22-910-801.

1 Use:

Varnish

Polyurethane--

Marking Structure

04SAB2 As required

(e) As shown in Fig. A-GBAAA Sheet 01, View B, safety the two CVs, Item 3, with:

Wire-Locking Dia: 1

Mm (0.041 Inch)

Cres

14QGC1 As required

(2) Subtask 293125-930-211-001 - Reidentify the Green HP Manifold (FIN 5102JM)

Work Zones and Access Panels

Zone Access/Work location

147 Access Door 811, Door 197CB

Work location from Frame 53.1 to Frame 53.2

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills AIRFRAME

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 67

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SERVICE BULLETIN

Material necessary to do the job

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Varnish Polyurethane-Low

Voc External Structure

04SBA3 As required

Non Aqueous Cleaner

Petroleum Based

08BBB1 As required

Textile - Lint Free Cotton 14SBA1 As required

References

Process and Material Specification

(PMS)

Process and Material Specification (PMS)

01-06-12

Fig. A-GBDAA

Removal and Installation of the CVs and

Re-identification of the Green Hydraulic

System HP Manifold

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Fig. A-GABAA

PN Evolution of the Green, Blue and

Yellow System HP Hydraulic Manifolds

Sheet 01

(a) Re-identify the Green HP Manifold (FIN 5102JM), refer to Process and Material

Specification (PMS) 01-06-12, Fig. A-GBDAA Sheet 03, View D, Fig. A-GBDAA

Sheet 04, Views E and F for information and the table given in Appendix 01: PN

Evolution of the Green, Blue and Yellow System HP Hydraulic Manifolds , refer to

Fig. A-GABAA Sheet 01.

1 Clean the Manifold identification PN located on the body of the Green HP

Manifold (FIN 5102JM), use:

Textile - Lint Free

Cotton

14SBA1 As required

made moist with

Non Aqueous

Cleaner Petroleum

Based

08BBB1 As required

2 Use an indelible ink pen to re-identify the Green HP Manifold with the new PN,

refer to the table given in Appendix 01: PN Evolution of the Green, Blue and

Yellow System HP Hydraulic Manifolds , refer to Fig. A-GABAA Sheet 01.

NOTE: If the old HP manifold PN cannot be found at the location

shown in Fig. A-GBDAA Sheet 04, Views E and F, the IPC

body manifold PN should be used to find the new HP manifold

PN, refer to the table given in Appendix 01: PN Evolution of

the Green, Blue and Yellow System HP Hydraulic Manifolds ,

refer to Fig. A-GABAA Sheet 01.

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

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SERVICE BULLETIN

3 Apply varnish to the new identification PN, use:

Varnish

Polyurethane-Low

Voc External

Structure

04SBA3 As required

**CONF ALL

D. TEST

**CONF 001

None

**CONF 002

(1) Subtask 293125-730-211-001 - Test of the Green Hydraulic System HP Manifold

Work Zones and Access Panels

Zone Access/Work location

147 Access Door 811, Door 197CB

Work location from Frame 53.1 to Frame 53.2

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 20-23-11-917-802

Task 20-23-22-910-801

Task 20-29-00-911-801

Task 29-00-00-210-801

Task 29-00-00-863-801

Task 29-00-00-864-801

Task 29-11-53-400-806

Fig. A-GCAAA

Torque Check of the Hydraulic Unions

on the Green Hydraulic System HP

Manifold

Sheet 01

(a) Inspect the red marking on all the plug-in unions on the manifold.

1 If any red marking is not aligned:

a Disconnect the pipe from the plug-in union.

b Remove the plug-in union from the manifold.

c Replace the packing of the plug-in union with a new one, refer to AMM

Task 20-29-00-911-801.

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 69

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d As shown in Fig. A-GCAAA Sheet 01, View B, install and tighten

all removed plug-in unions on the manifold, refer to AMM Task

20-29-00-911-801 and Table 1, below.

e As shown in Fig. A-GCAAA Sheet 01, View B, install and tighten the pipe

to the plug-in union and manifold, refer to AMM Task 20-23-11-917-802

and Table 1, below.

Item No. Pipe Torque Value (Nm) Item No. Union Torque Value

(Nm)

(26) 54-59 (5) 34.7-35.8

(25) 85-95 (9) 116.4-118.6

Table 1

(b) Make a new red mark on any of the unions where the red mark is no longer aligned

or not clearly visible, refer to AMM Task 20-23-22-910-801.

(c) Remove the safety clip(s) and/or tag(s) and close/unlock the circuit breaker(s) as

specified in the Job Set-up in the Installation of the Check-Valves, refer to AMM

Task 29-11-53-400-806.

(d) Pressurize the Green hydraulic system with the electric pump, refer to AMM Task

29-00-00-863-801.

(e) Make sure there are no leaks from the unions on the manifold.

(f) Make sure there are no leaks from the connections of the CVs.

(g) Make sure there are no leaks from the pipe connections.

(h) Check for air in the Green hydraulic system, refer to AMM Task 29-00-00-210-801.

(i) Depressurize the Green hydraulic system, refer to AMM Task 29-00-00-864-801.

**CONF ALL

E. CLOSE-UP

**CONF 001

None

**CONF 002

(1) Subtask 293125-942-201-001 - Close-up

Work Zones and Access Panels

Zone Access/Work location

190

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 70

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SERVICE BULLETIN

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 29-11-53-400-806

(a) Make sure that the work areas are clean and clear of tools and other items of

equipment.

(b) Do the Job Close-up procedure for the installation of the CV FIN 5316JM101 and

FIN 5316JM102, refer to AMM Task 29-11-53-400-806.

(c) Put the aircraft back to its initial configuration.

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

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This Page Intentionally Left Blank

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 72

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SERVICE BULLETIN

Task 293125-831-849-001 - Modify the Green HP Hydraulic Manifold on Bench

**CONF ALL

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

INCLUDED IN THE REFERENCED PROCEDURES.

CAUTION: DO NOT WORK ON ALL THREE HYDRAULIC SYSTEMS DURING THE SAME

MAINTENANCE INPUT WITH THE SAME MAINTENANCE PERSONNEL. THIS

IS TO MAKE SURE THAT A POSSIBLE MAINTENANCE ERROR ON ONE

SYSTEM IS NOT DONE AGAIN ON A DIFFERENT SYSTEM. A MAINTENANCE

ERROR ON MORE THAN ONE HYDRAULIC SYSTEM CAN CAUSE SYSTEM

FAILURE ON MULTIPLE SYSTEMS. IF MAINTENANCE IS NECESSARY ON

MORE THAN ONE SYSTEM AT THE SAME TIME AND INVOLVES LINES /

COMPONENTS DISCONNECTION, DIFFERENT MAINTENANCE PERSONNEL

MUST BE USED FOR EACH SYSTEM.

CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP

ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY

AND MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENANCE

WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING,

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

THIS:

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

NECESSARY ON WIRING AND COMPONENTS.

- REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND

OTHER CONTAMINATION.

THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION

AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION.

IF THERE IS CONTAMINATION, REFER TO ESPM 20-55-00.

NOTE: The accomplishment instructions of this Service Bulletin include procedures given

in other documents or in other sections of the Service Bulletin. When the words

’refer to’ are used and the operator has a procedure accepted by the local authority

he belongs to, the accepted alternative procedure can be used. When the words ’in

accordance with’ are used then the given procedure must be followed.

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

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

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

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

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

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

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

NOTE: 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

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 73

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SERVICE BULLETIN

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

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

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

the aircraft can be put back into a serviceable condition.

NOTE: AIRBUS generally recommends not to open the three hydraulic systems during

the same maintenance input. Therefore it is recommended to apply this Service

Bulletin during two different maintenance inputs, for instance the Yellow and Blue

hydraulic system first and the Green hydraulic system at a later opportunity.

NOTE: Discarded parts must be managed at the operator’s discretion.

NOTE: This Service Bulletin contains the instructions for the on-aircraft maintenance

necessary to ensure the continued airworthiness of the aircraft.

For any deviations to the instructions contained herein, contact Airbus for further

instructions and approval.

Task Associated Data

**CONF 001

Manpower

TOTAL MANHOURS 0.00

**CONF 002

Zone

147 190

Modified FIN

5102JM 5316JM101 5316JM102

Access

Door 197CB 811

Manpower

TOTAL MANHOURS 10.50

ELAPSED TIME (HOURS) 10.50

**CONF ALL

A. GENERAL

**CONF 001

None

**CONF 002

(1) Subtask 293125-910-202-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 74

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References

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

06-31-53, Page Block 001

06-41-53, Page Block 001

Task 20-11-11-911-803

Task 20-29-00-911-801

Task 29-00-00-910-805

Consumable Material List (CML)

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

Consumable Materials List (CML).

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

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

(d) For the identification of access panels, refer to AMM 06-41-53, Page Block 001.

(e) For the safety procedures of the hydraulic systems, refer to AMM Task

29-00-00-910-805.

(f) For the removal/installation of O-ring seals, refer to AMM Task 20-29-00-911-801.

(g) Put a blanking plug on an open manifold port.

(h) For wirelocking safety procedures and warnings, refer to AMM Task

20-11-11-911-803.

(2) Subtask 293125-839-202-001 - 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

None

**CONF 002

(1) Subtask 293125-941-203-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 75

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SERVICE BULLETIN

References

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

Task 20-23-22-910-801

Task 29-11-53-000-805

NOTE: The items given in this note 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 are 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.

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

12-34-24-860-802.

(b) Do the Job Set-up procedure for the removal of the HP manifold FIN 5102JM, refer

to AMM Task 29-11-53-000-805.

**CONF ALL

C. PROCEDURE

**CONF 001

None

**CONF 002

(1) Subtask 293125-020-208-001 - Remove the Green HP Manifold (FIN 5102JM)

Work Zones and Access Panels

Zone Access/Work location

147 Access Door 811, Door 197CB

Work location from Frame 53.1 to Frame 53.2

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 76

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SERVICE BULLETIN

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 20-29-00-911-801

Task 29-11-53-000-805

Fig. A-GBDAA

Removal and Installation of the CVs and

Re-identification of the Green Hydraulic

System HP Manifold

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

(a) As shown in Fig. A-GBDAA Sheet 01, View B, disconnect:

3 Pipe Item (25) Retain

1 Pipe Item (26) Retain

(b) As shown in Fig. A-GBDAA Sheet 01, View B, refer to AMM Task

29-11-53-000-805 and AMM Task 20-29-00-911-801, remove:

FIN 5102JM

1 HP manifold assembly Item (1) Retain

with

1 Bolt NAS6604-32 Item (10) Retain

1 Bolt NAS6604-34 Item (11) Retain

2 Bolt NAS6604-6 Item (7) Retain

4 Washer ASNA2397-416L Item (6) Retain

3 Plug-in Union Item (9) Retain

3 Packing NAS1612-16 Item (8) Discard

1 Plug-in Union Item (5) Retain

1 Packing NAS1612-8 Item (4) Discard

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 77

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(2) Subtask 293125-831-204-001 - Modify the Green HP Manifold (FIN 5102JM)

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills AIRFRAME

Material necessary to do the job

Component COMPD01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

2 NAS1612-24 2 PACKING

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

shall be ordered as necessary through the given channel.

Equipment BFEZ01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

3 CAR402 2 VALVE

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

shall be ordered as necessary through the given channel.

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Phosphate Ester Hydraulic

Fluid-General Power

02ABA1 As required

Varnish Polyurethane--

Marking Structure

04SAB2 As required

Non Aqueous Cleaner -

General

08BAA9 As required

Wire-Locking Dia: 1 Mm

(0.041 Inch) Cres

14QGC1 As required

Textile - Lint Free Cotton 14SBA1 As required

Standard tool TOOLD01

ITEM TOOL N ̊ TOOL NAME QTY SEE

NOTES

54 97F29108805000 Kit-Instl, CAR401 VLV 1

References

Aircraft Maintenance Manual (AMM) Task 20-23-22-910-801

Task 20-29-00-911-801

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 78

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References

Fig. A-GBDAA

Removal and Installation of the CVs and

Re-identification of the Green Hydraulic

System HP Manifold

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Fig. A-GCAAA

Torque Check of the Hydraulic Unions

on the Green Hydraulic System HP

Manifold

Sheet 01

(a) On the bench, install the Green HP manifold (FIN 5102JM), Item (1) onto the

Installation Tool for CAR401, Item 54.

1 As shown in Fig. A-GBDAA Sheet 02, View C, install on vice:

Item 54 97F29108805000 Kit-Instl, CAR401

VLV

1

2 Install the HP manifold on the Installation Tool for CAR401.

NOTE: To install the Green HP Manifold (FIN 5102JM), Item (1),

correctly, use the G marks on the Installation Tool for CAR401,

Item 54.

3 As shown in Fig. A-GBDAA Sheet 02, View C, install the items that follow from

the Installation Kit:

4 Screw Item 50

8 Washer Item 51

4 Nut Item 53

1 Support Item 34

NOTE: The Support, Item 34, can be hexagonal or spherical.

NOTE: The items listed above are part of Standard tool TOOLD01.

(b) Remove the CVs, Items (3), from the Green HP manifold (FIN 5102JM).

1

CAUTION: DO NOT USE POINTED, SHARP OR METAL TOOLS TO

REMOVE THE O-RING OR SQUARE SEAL OR BACK-UP

RINGS. SHARP EDGES CAN CAUSE DAMAGE TO THE

BOBBINS (GROOVES OR SEAL CONTACT SURFACES).

As shown in Fig. A-GBDAA Sheet 01, View B and Fig. A-GBDAA Sheet 02,

View C, cut and discard the lockwire then remove:

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

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FIN 5316JM101

1 Valve-check CAR401 Item (3) Discard

FIN 5316JM101

1 Seal Assy 818114 Item (2) Discard

and

FIN 5316JM102

1 Valve-check CAR401 Item (3) Discard

FIN 5316JM102

1 Seal Assy 818114 Item (2) Discard

(c) Remove from the Green HP manifold (FIN 5102JM), refer to Fig. A-GBDAA Sheet

02, View C:

1 Installation Placard Item (45) Discard

(d) Clean the related components and work areas with:

Non Aqueous

Cleaner - General

08BAA9 As required

and

Textile - Lint Free

Cotton

14SBA1 As required

(e) Install the CVs on the Green HP manifold (FIN 5102JM).

1 Clean the related components and work areas with:

Non Aqueous

Cleaner - General

08BAA9 As required

and

Textile - Lint Free

Cotton

14SBA1 As required

2

CAUTION: ONLY USE THE SPECIFIED LUBRICANT TO LUBRICATE

THE FITTING THREADS.

Apply to the threads of the CVs:

Phosphate Ester

Hydraulic FluidGeneral Power

02ABA1 As required

3 Discard the storage seals from the new CVs.

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 80

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4 As shown in Fig. A-GBDAA Sheet 03, View D Fig. A-GBDAA Sheet 05, install:

FIN 5316JM101

1 Valve-check CAR402 Item 3

FIN 5316JM101

1 Packing NAS1612-24 Item 2

and

FIN 5316JM102

1 Valve-check CAR402 Item 3

FIN 5316JM102

1 Packing NAS1612-24 Item 2

a Before installation, make sure that the back-up ring is flush with the

groove in the CVs, Item 3.

(f) Torque the CVs, Item 3, two times:

1 Torque the CVs between 230 and 250 Nm (169.64-184.39 lbf.ft).

2 Undo the CVs by a 1/8th turn.

3 Torque the CVs between 230 and 250 Nm (169.64-184.39 lbf.ft).

(g) Make a red mark on the CVs and the manifold, refer to AMM Task

20-23-22-910-801.

1 Use:

Varnish

Polyurethane--

Marking Structure

04SAB2 As required

(h) As shown in Fig. A-GBDAA Sheet 03, View D, safety the two CVs, Item 3, with:

Wire-Locking Dia: 1

Mm (0.041 Inch)

Cres

14QGC1 As required

(3) Subtask 293125-930-204-001 - Reidentify the Green HP Manifold (FIN 5102JM)

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills AIRFRAME

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

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Material necessary to do the job

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Varnish Polyurethane-Low

Voc External Structure

04SBA3 As required

Non Aqueous Cleaner

Petroleum Based

08BBB1 As required

Textile - Lint Free Cotton 14SBA1 As required

References

Process and Material Specification

(PMS)

Process and Material Specification (PMS)

01-06-12

Fig. A-GBDAA

Removal and Installation of the CVs and

Re-identification of the Green Hydraulic

System HP Manifold

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Fig. A-GABAA

PN Evolution of the Green, Blue and

Yellow System HP Hydraulic Manifolds

Sheet 01

(a) Re-identify the Green HP Manifold (FIN 5102JM), refer to Process and Material

Specification (PMS) 01-06-12, Fig. A-GBDAA Sheet 03, View E, Fig. A-GBDAA

Sheet 04, View E and F for information and the table given in Appendix 01: PN

Evolution of the Green, Blue and Yellow System HP Hydraulic Manifolds , refer to

Fig. A-GABAA Sheet 01.

1 Manifold identification PN located on the body of the Green HP Manifold (FIN

5102JM), use:

Textile - Lint Free

Cotton

14SBA1 As required

made moist with

Non Aqueous

Cleaner Petroleum

Based

08BBB1 As required

2 Use an indelible ink pen to re-identify the Green HP Manifold with the new PN,

refer to the table given in Appendix 01: PN Evolution of the Green, Blue and

Yellow System HP Hydraulic Manifolds , refer to Fig. A-GABAA Sheet 01.

NOTE: If the old HP manifold PN cannot be found at the location

shown in Fig. A-GBDAA Sheet 04, Views E and F, the IPC

body manifold PN should be used to find the new HP manifold

PN, refer to the table given in Appendix 01: PN Evolution of

the Green, Blue and Yellow System HP Hydraulic Manifolds ,

refer to Fig. A-GABAA Sheet 01.

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

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3 Apply varnish to the new identification PN, use:

Varnish

Polyurethane-Low

Voc External

Structure

04SBA3 As required

(4) Subtask 293125-420-208-001 - Install the Green HP Manifold (FIN 5102JM)

Work Zones and Access Panels

Zone Access/Work location

147 Access Door 811, Door 197CB

Work location from Frame 53.1 to Frame 53.2

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills AIRFRAME

Material necessary to do the job

Component COMPD01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

4 NAS1612-8 1 PACKING

8 NAS1612-16 3 PACKING

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

shall be ordered as necessary through the given channel.

References

Aircraft Maintenance Manual (AMM) Task 20-23-11-917-802

Task 20-23-22-910-801

Task 20-29-00-911-801

Task 29-11-53-400-805

Fig. A-GBDAA

Removal and Installation of the CVs and

Re-identification of the Green Hydraulic

System HP Manifold

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Fig. A-GCAAA

Torque Check of the Hydraulic Unions

on the Green Hydraulic System HP

Manifold

Sheet 01

(a) As shown in Fig. A-GBDAA Sheet 02, View C, remove the Green HP Manifold (FIN

5102JM), Item (1) from the Installation Tool for CAR401, Item 54.

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

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(b) Install the Green hydraulic system HP manifold (FIN 5102JM), refer to AMM Task

29-11-53-400-805 and AMM Task 20-29-00-911-801.

1 As shown in Fig. A-GBDAA Sheet 01, View B, install:

FIN 5102JM

1 HP manifold assembly Item (1) Retained at

removal

with

1 Bolt NAS6604-32 Item (10) Retained at

removal

1 Bolt NAS6604-34 Item (11) Retained at

removal

2 Bolt NAS6604-6 Item (7) Retained at

removal

4 Washer ASNA2397-416L Item (6) Retained at

removal

3 Packing NAS1612-16 Item 8

3 Plug-in Union Item (9) Retained at

removal

1 Packing NAS1612-8 Item 4

1 Plug-in Union Item (5) Retained at

removal

and reconnect:

3 Pipe Item (25) Retained at

removal

1 Pipe Item (26) Retained at

removal

(c) Tighten the plug-in unions and pipes.

1 As shown in Fig. A-GCAAA Sheet 01, View B, tighten all removed plug-in

unions, refer to AMM Task 20-29-00-911-801 and Table 1, below.

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

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2 As shown in Fig. A-GCAAA Sheet 01, View B, tighten the pipes at both ends

to the plug-in union and manifold, refer to AMM Task 20-23-11-917-802, AMM

Task 20-29-00-911-801 and Table 1, below.

Item No. Pipe Torque Value (Nm) Item No. Union Torque Value

(Nm)

(26) 54-59 (5) 34.7-35.8

(25) 85-95 (9) 116.4-118.6

Table 1

(d) Make a new red mark on any of the unions where the red mark is no longer aligned

or not clearly visible, refer to AMM Task 20-23-22-910-801.

**CONF ALL

D. TEST

**CONF 001

None

**CONF 002

(1) Subtask 293125-730-204-001 - Test the Green HP Manifold (FIN 5102JM)

Work Zones and Access Panels

Zone Access/Work location

147 Access Door 811, Door 197CB

Work location from Frame 53.1 to Frame 53.2

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 29-00-00-210-801

Task 29-00-00-863-801

Task 29-00-00-864-801

Task 29-11-53-400-806

Fig. A-GCAAA

Torque Check of the Hydraulic Unions

on the Green Hydraulic System HP

Manifold

Sheet 01

(a) Remove the safety clip(s) and/or tag(s) and close/unlock the circuit breaker(s) as

specified in the Job Set-up in the Installation of the Check-Valves, refer to AMM

Task 29-11-53-400-806.

(b) Pressurize the Green hydraulic system with the electric pump, refer to AMM Task

29-00-00-863-801.

(c) Make sure there are no leaks from all the unions on the manifold.

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

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(d) Make sure there are no leaks from the connections of the CVs.

(e) Make sure there are no leaks from the pipe connections.

(f) Check for air in the Green hydraulic system, refer to AMM Task 29-00-00-210-801.

(g) Depressurize the Green hydraulic system, refer to AMM Task 29-00-00-864-801.

**CONF ALL

E. CLOSE-UP

**CONF 001

None

**CONF 002

(1) Subtask 293125-942-202-001 - Close-up

Work Zones and Access Panels

Zone Access/Work location

190

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 29-11-53-400-805

(a) Make sure that the work areas are clean and clear of tools and other items of

equipment.

(b) Do the Job Close-up procedure for the installation of the Green Hydraulic Manifold

FIN 5102JM, refer to AMM Task 29-11-53-400-805.

(c) Put the aircraft back to its initial configuration.

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

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Task 293125-831-850-001 - Modify the Blue HP Hydraulic Manifold on Aircraft

**CONF ALL

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

INCLUDED IN THE REFERENCED PROCEDURES.

CAUTION: DO NOT WORK ON ALL THREE HYDRAULIC SYSTEMS DURING THE SAME

MAINTENANCE INPUT WITH THE SAME MAINTENANCE PERSONNEL. THIS

IS TO MAKE SURE THAT A POSSIBLE MAINTENANCE ERROR ON ONE

SYSTEM IS NOT DONE AGAIN ON A DIFFERENT SYSTEM. A MAINTENANCE

ERROR ON MORE THAN ONE HYDRAULIC SYSTEM CAN CAUSE SYSTEM

FAILURE ON MULTIPLE SYSTEMS. IF MAINTENANCE IS NECESSARY ON

MORE THAN ONE SYSTEM AT THE SAME TIME AND INVOLVES LINES /

COMPONENTS DISCONNECTION, DIFFERENT MAINTENANCE PERSONNEL

MUST BE USED FOR EACH SYSTEM.

CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP

ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY

AND MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENANCE

WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING,

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

THIS:

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

NECESSARY ON WIRING AND COMPONENTS.

- REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND

OTHER CONTAMINATION.

THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION

AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION.

IF THERE IS CONTAMINATION, REFER TO ESPM 20-55-00.

NOTE: The accomplishment instructions of this Service Bulletin include procedures given

in other documents or in other sections of the Service Bulletin. When the words

’refer to’ are used and the operator has a procedure accepted by the local authority

he belongs to, the accepted alternative procedure can be used. When the words ’in

accordance with’ are used then the given procedure must be followed.

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

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

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

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

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

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

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

NOTE: 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

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

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SERVICE BULLETIN

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

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

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

the aircraft can be put back into a serviceable condition.

NOTE: AIRBUS generally recommends not to open the three hydraulic systems during

the same maintenance input. Therefore it is recommended to apply this Service

Bulletin during two different maintenance inputs, for instance the Yellow and Blue

hydraulic system first and the Green hydraulic system at a later opportunity.

NOTE: Discarded parts must be managed at the operator’s discretion.

NOTE: This Service Bulletin contains the instructions for the on-aircraft maintenance

necessary to ensure the continued airworthiness of the aircraft.

For any deviations to the instructions contained herein, contact Airbus for further

instructions and approval.

Task Associated Data

**CONF 001

Manpower

TOTAL MANHOURS 0.00

**CONF 002

Zone

190 195

Modified FIN

5316JM201 6103JM

Access

Door 195BB 811

Manpower

TOTAL MANHOURS 7.50

ELAPSED TIME (HOURS) 7.50

**CONF ALL

A. GENERAL

**CONF 001

None

**CONF 002

(1) Subtask 293125-910-203-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

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References

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

06-31-53, Page Block 001

06-41-53, Page Block 001

Task 20-11-11-911-803

Task 20-29-00-911-801

Task 29-00-00-910-805

Consumable Material List (CML)

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

Consumable Materials List (CML).

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

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

(d) For the identification of access panels, refer to AMM 06-41-53, Page Block 001.

(e) For the safety procedures of the hydraulic systems, refer to AMM Task

29-00-00-910-805.

(f) For the removal/installation of O-ring seals, refer to AMM Task 20-29-00-911-801.

(g) Put a blanking plug on an open manifold port.

(h) For wirelocking safety procedures and warnings, refer to AMM Task

20-11-11-911-803.

(2) Subtask 293125-839-203-001 - 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

None

**CONF 002

(1) Subtask 293125-941-204-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

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References

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

Task 20-23-22-910-801

Task 29-12-53-000-806

NOTE: The items given in this note 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 are 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.

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

12-34-24-860-802.

(b) Do the Job Set-up procedure for the removal of the CV FIN 5316JM201, refer to

AMM Task 29-12-53-000-806.

(c) Inspect the red marking on all the manifold unions. Apply red marking on the

unions where it is not visible, refer to AMM Task 20-23-22-910-801.

**CONF ALL

C. PROCEDURE

**CONF 001

None

**CONF 002

(1) Subtask 293125-831-205-001 - Modify the Blue HP Manifold (FIN 6103JM)

Work Zones and Access Panels

Zone Access/Work location

195 Access Door 811, Door 195BB

Work location from Frame 45 to Frame 46

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

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Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills AIRFRAME

Material necessary to do the job

Component COMPD01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

2 NAS1612-24 1 PACKING

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

shall be ordered as necessary through the given channel.

Equipment BFEZ01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

3 CAR402 1 VALVE

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

shall be ordered as necessary through the given channel.

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Phosphate Ester Hydraulic

Fluid-General Power

02ABA1 As required

Varnish Polyurethane--

Marking Structure

04SAB2 As required

Non Aqueous Cleaner -

General

08BAA9 As required

Wire-Locking Dia: 1 Mm

(0.041 Inch) Cres

14QGC1 As required

Textile - Lint Free Cotton 14SBA1 As required

References

Aircraft Maintenance Manual (AMM) Task 20-23-22-910-801

Task 29-12-53-000-806

Process and Material Specification

(PMS)

Process and Material Specification (PMS)

01-06-12

Fig. A-GBBAA

Removal and Installation of the CVs and

Re-identification of the Blue Hydraulic

System HP Manifold

Sheet 01

Sheet 02

Sheet 03

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(a) Remove the CV from the Blue HP manifold (FIN 6103JM), refer to AMM Task

29-12-53-000-806.

1

CAUTION: DO NOT USE POINTED, SHARP OR METAL TOOLS TO

REMOVE THE O-RING OR SQUARE SEAL OR BACK-UP

RINGS. SHARP EDGES CAN CAUSE DAMAGE TO THE

BOBBINS (GROOVES OR SEAL CONTACT SURFACES).

As shown in Fig. A-GBBAA Sheet 01, View B, cut and discard the lockwire

then remove:

FIN 5316JM201

1 Valve-check CAR401 Item (3) Discard

FIN 5316JM201

1 Seal Assy 818114 Item (2) Discard

(b) Install the CV on the Blue HP manifold (FIN 6103JM).

1 Clean the related components and work areas with:

Non Aqueous

Cleaner - General

08BAA9 As required

and

Textile - Lint Free

Cotton

14SBA1 As required

2

CAUTION: ONLY USE THE SPECIFIED LUBRICANT TO LUBRICATE

THE FITTING THREADS.

Apply to the threads of the CV:

Phosphate Ester

Hydraulic FluidGeneral Power

02ABA1 As required

3 Discard the storage seals from the new CVs.

4 As shown in Fig. A-GBBAA Sheet 01, View B and Fig. A-GBBAA Sheet 03,

install:

FIN 5316JM201

1 Valve-check CAR402 Item 3

FIN 5316JM201

1 Packing NAS1612-24 Item 2

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a Before installation, make sure that the back-up ring is flush with the

groove in the CVs, Item 3.

(c) Torque the CV, Item 3, two times:

1 Torque the CV between 230 and 250 Nm (169.64-184.39 lbf.ft).

2 Undo the CV by a 1/8th turn.

3 Torque the CV between 230 and 250 Nm (169.64-184.39 lbf.ft).

(d) Make a red mark on the CV and the manifold, refer to AMM Task

20-23-22-910-801.

1 Use:

Varnish

Polyurethane--

Marking Structure

04SAB2 As required

(e) As shown in Fig. A-GBBAA Sheet 01, View B, safety the CV, Item 3, with:

Wire-Locking Dia: 1

Mm (0.041 Inch)

Cres

14QGC1 As required

(2) Subtask 293125-930-205-001 - Reidentify the Blue HP Manifold (FIN 6103JM)

Work Zones and Access Panels

Zone Access/Work location

195 Access Door 811, Door 195BB

Work location from Frame 45 to Frame 46

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills AIRFRAME

Material necessary to do the job

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Varnish Polyurethane-Low

Voc External Structure

04SBA3 As required

Non Aqueous Cleaner

Petroleum Based

08BBB1 As required

Textile - Lint Free Cotton 14SBA1 As required

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 93

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References

Process and Material Specification

(PMS)

Process and Material Specification (PMS)

01-06-12

Fig. A-GBEAA

Removal and Installation of the CVs and

Re-identification of the Blue Hydraulic

System HP Manifold

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Fig. A-GABAA

PN Evolution of the Green, Blue and

Yellow System HP Hydraulic Manifolds

Sheet 01

(a) Re-identify the Blue HP Manifold (FIN 6103JM), refer to Process and Material

Specification (PMS) 01-06-12, Fig. A-GBEAA Sheet 03, View D, Fig. A-GBEAA

Sheet 04, View E for information and the table given in Appendix 01: PN Evolution

of the Green, Blue and Yellow System HP Hydraulic Manifolds , refer to Fig. AGABAA Sheet 01.

1 Clean the Manifold identification PN located on the body of the Blue HP

Manifold (FIN 6103JM), use:

Textile - Lint Free

Cotton

14SBA1 As required

made moist with

Non Aqueous

Cleaner Petroleum

Based

08BBB1 As required

2 Use an indelible ink pen to re-identify the Blue HP Manifold with the new PN,

refer to the table given in Appendix 01: PN Evolution of the Green, Blue and

Yellow System HP Hydraulic Manifolds , refer to Fig. A-GABAA Sheet 01.

NOTE: If the old HP manifold PN cannot be found at the location

shown in Fig. A-GBEAA Sheet 04, View E , the IPC body

manifold PN should be used to find the new HP manifold PN,

refer to the table given in Appendix 01: PN Evolution of the

Green, Blue and Yellow System HP Hydraulic Manifolds , refer

to Fig. A-GABAA Sheet 01.

3 Apply varnish to the new identification PN, use:

Varnish

Polyurethane-Low

Voc External

Structure

04SBA3 As required

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

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**CONF ALL

D. TEST

**CONF 001

None

**CONF 002

(1) Subtask 293125-730-205-001 - Test the Blue HP Manifold (FIN 6103JM)

Work Zones and Access Panels

Zone Access/Work location

195 Access Door 811, Door 195BB

Work location from Frame 45 to Frame 46

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 20-23-11-917-802

Task 20-23-22-910-801

Task 20-29-00-911-801

Task 29-00-00-210-801

Task 29-00-00-863-802

Task 29-00-00-864-802

Task 29-12-53-400-805

Fig. A-GDAAA

Torque Check of the Hydraulic Unions

on the Blue Hydraulic System HP

Manifold

Sheet 01

(a) Inspect the red marking on all the plug-in unions on the manifold.

1 If any red marking is not aligned:

a Disconnect the pipe from the plug-in union.

b Remove the plug-in union from the manifold.

c Replace the packing of the plug-in union with a new one, refer to AMM

Task 20-29-00-911-801.

d As shown in Fig. A-GDAAA Sheet 01, View B, install and tighten

all removed plug-in unions on the manifold, refer to AMM Task

20-29-00-911-801 and Table 2, below.

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e As shown in Fig. A-GDAAA Sheet 01, View B, install and tighten the pipe

to the plug-in union and manifold, refer to AMM Task 20-23-11-917-802

and Table 2, below.

Item No. Pipe Torque Value (Nm) Item No. Union Torque Value

(Nm)

(29) 85-95 (9) 116.4-118.6

(30) 85-95 (16) 72.9-74

(31) 54-59 (17) 34.7-35.8

(32) 81-89 (12) 116.4-118.6

(33) 75-83 (13) 50.3-51.4

(34) 85-95 (16) 116.4-118.6

(35) 75-83 (13) 50.3-51.4

Table 2

(b) Make a new red mark on all the unions where the red mark is not aligned or no

longer visible, refer to AMM Task 20-23-22-910-801.

(c) Remove the safety clip(s) and/or tag(s) and close/unlock the circuit breaker(s) as

specified in the Job Set-up in the Installation of the Blue HP Manifold-Supply

Check-Valves, refer to AMM Task 29-12-53-400-805.

(d) Pressurize the Blue hydraulic system with the electric pump, refer to AMM Task

29-00-00-863-802.

(e) Make sure there are no leaks from the unions on the manifold.

(f) Make sure there are no leaks from the connections of the CV.

(g) Make sure there are no leaks from the pipe connections.

(h) Check for air in the Blue hydraulic system, refer to AMM Task 29-00-00-210-801.

(i) Depressurize the Blue hydraulic system, refer to AMM Task 29-00-00-864-802.

**CONF ALL

E. CLOSE-UP

**CONF 001

None

**CONF 002

(1) Subtask 293125-942-203-001 - Close-up

Work Zones and Access Panels

Zone Access/Work location

190

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

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Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 29-12-53-400-806

(a) Make sure that the work areas are clean and clear of tools and other items of

equipment.

(b) Do the Job Close-up procedure for the installation of the CV FIN 5316JM201, refer

to AMM Task 29-12-53-400-806.

(c) Put the aircraft back to its initial configuration.

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 97

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This Page Intentionally Left Blank

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

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SERVICE BULLETIN

Task 293125-831-851-001 - Modify the Blue HP Hydraulic Manifold on Bench

**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.

IF THERE IS CONTAMINATION, REFER TO ESPM 20-55-00.

NOTE: The accomplishment instructions of this Service Bulletin include procedures given

in other documents or in other sections of the Service Bulletin. When the words

’refer to’ are used and the operator has a procedure accepted by the local authority

he belongs to, the accepted alternative procedure can be used. When the words ’in

accordance with’ are used then the given procedure must be followed.

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

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

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

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

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

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

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

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

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

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

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

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

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

the aircraft can be put back into a serviceable condition.

NOTE: AIRBUS generally recommends not to open the three hydraulic systems during

the same maintenance input. Therefore it is recommended to apply this Service

Bulletin during two different maintenance inputs, for instance the Yellow and Blue

hydraulic system first and the Green hydraulic system at a later opportunity.

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 99

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SERVICE BULLETIN

NOTE: Discarded parts must be managed at the operator’s discretion.

NOTE: This Service Bulletin contains the instructions for the on-aircraft maintenance

necessary to ensure the continued airworthiness of the aircraft.

For any deviations to the instructions contained herein, contact Airbus for further

instructions and approval.

Task Associated Data

**CONF 001

Manpower

TOTAL MANHOURS 0.00

**CONF 002

Zone

190 195

Modified FIN

5316JM201 6103JM

Access

Door 195BB 811

Manpower

TOTAL MANHOURS 10.50

ELAPSED TIME (HOURS) 10.50

**CONF ALL

A. GENERAL

**CONF 001

None

**CONF 002

(1) Subtask 293125-910-204-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

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

06-31-53, Page Block 001

06-41-53, Page Block 001

Task 20-11-11-911-803

Task 20-29-00-911-801

Task 29-00-00-910-805

Consumable Material List (CML)

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

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SERVICE BULLETIN

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

Consumable Materials List (CML).

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

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

(d) For the identification of access panels, refer to AMM 06-41-53, Page Block 001.

(e) For the safety procedures of the hydraulic systems, refer to AMM Task

29-00-00-910-805.

(f) For the removal/installation of O-ring seals, refer to AMM Task 20-29-00-911-801.

(g) Put a blanking plug on an open manifold port.

(h) For wirelocking safety procedures and warnings, refer to AMM Task

20-11-11-911-803.

(2) Subtask 293125-839-204-001 - 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

None

**CONF 002

(1) Subtask 293125-941-205-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

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

Task 20-23-22-910-801

Task 29-12-53-000-805

NOTE: The items given in this note 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)

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 101

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- Engine shut down, thrust reversers are 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.

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

12-34-24-860-802.

(b) Do the Job Set-up procedure for the removal of the Blue HP manifold FIN 6103JM,

refer to AMM Task 29-12-53-000-805.

**CONF ALL

C. PROCEDURE

**CONF 001

None

**CONF 002

(1) Subtask 293125-020-209-001 - Remove the Blue HP Manifold (FIN 6103JM)

Work Zones and Access Panels

Zone Access/Work location

195 Access Door 811, Door 195BB

Work location from Frame 45 to Frame 46

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 20-29-00-911-801

Task 29-12-53-000-805

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

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SERVICE BULLETIN

References

Fig. A-GBEAA

Removal and Installation of the CVs and

Re-identification of the Blue Hydraulic

System HP Manifold

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

(a) As shown in Fig. A-GBEAA Sheet 01, View B, disconnect:

1 Pipe Item (29) Retain

1 Pipe Item (30) Retain

1 Pipe Item (31) Retain

1 Pipe Item (32) Retain

1 Pipe Item (33) Retain

1 Pipe Item (34) Retain

1 Pipe Item (35) Retain

(b) As shown in Fig. A-GBEAA Sheet 01, View B, refer to AMM Task

29-12-53-000-805 and AMM Task 20-29-00-911-801, remove:

FIN 6103JM

1 HP Manifold Assembly Item (20) Retain

with

4 Bolt NAS6604-32 Item (10) Retain

4 Washer ASNA2397-416L Item (6) Retain

1 Plug and Bleeder AN814-6L Item (17) Retain

1 Plug-in Union Item (9) Retain

1 Plug-in Union Item (12) Retain

2 Packing NAS1612-16 Item (8) Discard

1 Packing NAS1612-8 Item (4) Discard

2 Plug-in Union Item (13) Retain

2 Packing NAS1612-10 Item (14) Discard

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

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SERVICE BULLETIN

2 Plug-in Union Item (16) Retain

2 Packing NAS1612-12 Item (15) Discard

(2) Subtask 293125-831-206-004 - Modify the Blue HP Manifold (FIN 6103JM)

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills AIRFRAME

Material necessary to do the job

Component COMPD01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

2 NAS1612-24 1 PACKING

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

shall be ordered as necessary through the given channel.

Equipment BFEZ01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

3 CAR402 1 VALVE

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

shall be ordered as necessary through the given channel.

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Phosphate Ester Hydraulic

Fluid-General Power

02ABA1 As required

Varnish Polyurethane--

Marking Structure

04SAB2 As required

Non Aqueous Cleaner -

General

08BAA9 As required

Wire-Locking Dia: 1 Mm

(0.041 Inch) Cres

14QGC1 As required

Textile - Lint Free Cotton 14SBA1 As required

Standard tool TOOLD01

ITEM TOOL N ̊ TOOL NAME QTY SEE

NOTES

54 97F29108805000 Kit-Instl, CAR401 VLV 1

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

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SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) Task 20-23-22-910-801

Task 20-29-00-911-801

Fig. A-GBEAA

Removal and Installation of the CVs and

Re-identification of the Blue Hydraulic

System HP Manifold

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Fig. A-GDAAA

Torque Check of the Hydraulic Unions

on the Blue Hydraulic System HP

Manifold

Sheet 01

(a) On the bench, install the Blue HP manifold (FIN 6103JM), Item (20) onto the

Installation Tool for CAR401, Item 54.

1 As shown in Fig. A-GBEAA Sheet 02, View C, install on vice:

Item 54 97F29108805000 Kit-Instl, CAR401

VLV

1

2 Install the Blue HP Manifold (FIN 6103JM), Item (20), on the Installation Tool

for CAR401, Item 54.

NOTE: To install the HP manifold (FIN 6103JM), Item (20), correctly,

use the B marks on the Installation Tool for CAR401, Item 54.

3 As shown in Fig. A-GBEAA Sheet 02, View C, install the items that follow from

the Installation Kit:

4 Screw Item 50

8 Washer Item 51

4 Nut Item 53

1 Support Item 34

NOTE: The Support, Item 34, can be hexagonal or spherical.

NOTE: The items listed above are part of Standard tool TOOLD01.

(b) Remove the CV Item 3, from the Blue HP manifold (FIN 6103JM).

1

CAUTION: DO NOT USE POINTED, SHARP OR METAL TOOLS TO

REMOVE THE O-RING OR SQUARE SEAL OR BACK-UP

RINGS. SHARP EDGES CAN CAUSE DAMAGE TO THE

BOBBINS (GROOVES OR SEAL CONTACT SURFACES).

As shown in Fig. A-GBEAA Sheet 01, View B and Fig. A-GBEAA Sheet 02,

View C, cut and discard the lockwire then remove:

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

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SERVICE BULLETIN

FIN 5316JM201

1 Valve-check CAR401 Item (3) Discard

FIN 5316JM201

1 Seal Assy 818114 Item (2) Discard

(c) Remove the Installation Placard, Item (45), from the Blue HP manifold (FIN

6103JM).

1 As shown in Fig. A-GBEAA Sheet 02, View C, remove with a scraper:

1 Installation Placard Item (45) Discard

(d) Clean the related components and work areas with:

Non Aqueous

Cleaner - General

08BAA9 As required

and

Textile - Lint Free

Cotton

14SBA1 As required

(e) Install the CVs on the Blue HP manifold (FIN 6103JM).

1 Clean the related components and work areas with:

Non Aqueous

Cleaner - General

08BAA9 As required

and

Textile - Lint Free

Cotton

14SBA1 As required

2

CAUTION: ONLY USE THE SPECIFIED LUBRICANT TO LUBRICATE

THE FITTING THREADS.

Apply to the threads of the CV:

Phosphate Ester

Hydraulic FluidGeneral Power

02ABA1 As required

3 Discard the storage seals from the new CVs.

4 As shown in Fig. A-GBEAA Sheet 03, View D and Fig. A-GBEAA Sheet 05,

install:

FIN 5316JM201

1 Valve-check CAR402 Item 3

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

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SERVICE BULLETIN

FIN 5316JM201

1 Packing NAS1612-24 Item 2

a Before installation, make sure that the back-up ring is flush with the

groove in the CVs, Item 3.

(f) Torque the CV, Item 3, two times:

1 Torque the CV between 230 and 250 Nm (169.64-184.39 lbf.ft).

2 Undo the CV by a 1/8th turn.

3 Torque the CV between 230 and 250 Nm (169.64-184.39 lbf.ft).

(g) Make a red mark on the CV and the manifold, refer to AMM Task

20-23-22-910-801.

1 Use:

Varnish

Polyurethane--

Marking Structure

04SAB2 As required

(h) As shown in Fig. A-GBEAA Sheet 03, View D, safety the CV, Item 3, with:

Wire-Locking Dia: 1

Mm (0.041 Inch)

Cres

14QGC1 As required

(3) Subtask 293125-930-206-001 - Reidentify the Blue HP Manifold (FIN 6103JM)

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills AIRFRAME

Material necessary to do the job

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Varnish Polyurethane-Low

Voc External Structure

04SBA3 As required

Non Aqueous Cleaner

Petroleum Based

08BBB1 As required

Textile - Lint Free Cotton 14SBA1 As required

References

Process and Material Specification

(PMS)

Process and Material Specification (PMS)

01-06-12

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

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References

Fig. A-GBEAA

Removal and Installation of the CVs and

Re-identification of the Blue Hydraulic

System HP Manifold

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Fig. A-GABAA

PN Evolution of the Green, Blue and

Yellow System HP Hydraulic Manifolds

Sheet 01

(a) Re-identify the Blue HP Manifold (FIN 6103JM), refer to Process and Material

Specification (PMS) 01-06-12, Fig. A-GBEAA Sheet 03, Views D and E, Fig. AGBEAA Sheet 04, View E for information and the table given in Appendix 01: PN

Evolution of the Green, Blue and Yellow System HP Hydraulic Manifolds , refer to

Fig. A-GABAA Sheet 01.

1 Clean the Manifold identification PN located on the body of the Blue HP

Manifold (FIN 6103JM), use:

Textile - Lint Free

Cotton

14SBA1 As required

made moist with

Non Aqueous

Cleaner Petroleum

Based

08BBB1 As required

2 Use an indelible ink pen to re-identify the Blue HP Manifold with the new PN,

refer to the table given in Appendix 01: PN Evolution of the Green, Blue and

Yellow System HP Hydraulic Manifolds , refer to Fig. A-GABAA Sheet 01.

NOTE: If the old HP manifold PN cannot be found at the location

shown in Fig. A-GBEAA Sheet 04, View E, the IPC body

manifold PN should be used to find the new HP manifold PN,

refer to the table given in Appendix 01: PN Evolution of the

Green, Blue and Yellow System HP Hydraulic Manifolds , refer

to Fig. A-GABAA Sheet 01.

3 Apply varnish to the new identification PN, use:

Varnish

Polyurethane-Low

Voc External

Structure

04SBA3 As required

(4) Subtask 293125-420-210-001 - Install the Blue HP Manifold (FIN 6103JM)

Work Zones and Access Panels

Zone Access/Work location

195 Access Door 811, Door 195BB

Work location from Frame 45 to Frame 46

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 108

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SERVICE BULLETIN

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills AIRFRAME

Material necessary to do the job

Component COMPD01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

4 NAS1612-8 1 PACKING

8 NAS1612-16 2 PACKING

14 NAS1612-10 2 PACKING

15 NAS1612-12 2 PACKING

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

shall be ordered as necessary through the given channel.

References

Aircraft Maintenance Manual (AMM) Task 20-23-11-917-802

Task 20-23-22-910-801

Task 20-29-00-911-801

Task 29-12-53-400-805

Fig. A-GBEAA

Removal and Installation of the CVs and

Re-identification of the Blue Hydraulic

System HP Manifold

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Fig. A-GDAAA

Torque Check of the Hydraulic Unions

on the Blue Hydraulic System HP

Manifold

Sheet 01

(a) As shown in Fig. A-GBEAA Sheet 02, View C, remove the Blue HP Manifold (FIN

6103JM), Item (20) from the Installation Tool for CAR401, Item 54.

(b) Install the Blue hydraulic system HP manifold (FIN 6103JM), refer to AMM Task

29-12-53-400-805 and AMM Task 20-29-00-911-801.

1 As shown in Fig. A-GBEAA Sheet 01, View B, install:

FIN 6103JM

1 HP Manifold Assembly Item (20) Retained at

removal

with

1 Bolt NAS6604-32 Item (10) Retained at

removal

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

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4 Washer ASNA2397-416L Item (6) Retained at

removal

1 Plug and Bleeder AN814-6L Item (17) Retained at

removal

2 Packing NAS1612-16 Item 8

1 Plug-in Union Item (9) Retained at

removal

1 Plug-in Union Item (12) Retained at

removal

1 Packing NAS1612-8 Item 4

2 Packing NAS1612-10 Item 14

2 Plug-in Union Item (13) Retained at

removal

2 Packing NAS1612-12 Item 15

2 Plug-in Union Item (16) Retained at

removal

and reconnect:

1 Pipe Item (29) Retained at

removal

1 Pipe Item (30) Retained at

removal

1 Pipe Item (31) Retained at

removal

1 Pipe Item (32) Retained at

removal

1 Pipe Item (33) Retained at

removal

1 Pipe Item (34) Retained at

removal

1 Pipe Item (35) Retained at

removal

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

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SERVICE BULLETIN

(c) Tighten the plug-in unions and pipes.

1 As shown in Fig. A-GDAAA Sheet 01, View B, tighten all removed plug-in

unions, refer to AMM Task 20-29-00-911-801 and Table 2, below.

2 As shown in Fig. A-GDAAA Sheet 01, View B, tighten the pipes at both ends

to the plug-in union and manifold, refer to AMM Task 20-23-11-917-802, AMM

Task 20-29-00-911-801 and Table 2, below.

Item No. Pipe Torque Value (Nm) Item No. Union Torque Value

(Nm)

(29) 85-95 (9) 116.4-118.6

(30) 85-95 (16) 72.9-74

(31) 54-59 (17) 34.7-35.8

(32) 81-89 (12) 116.4-118.6

(33) 75-83 (13) 50.3-51.4

(34) 85-95 (16) 116.4-118.6

(35) 75-83 (13) 50.3-51.4

Table 2

(d) Make a new red mark on all the unions where the red mark is not aligned or no

longer visible, refer to AMM Task 20-23-22-910-801.

**CONF ALL

D. TEST

**CONF 001

None

**CONF 002

(1) Subtask 293125-730-206-001 - Test of the Blue HP Manifold (FIN 6103JM)

Work Zones and Access Panels

Zone Access/Work location

195 Access Door 811, Door 195BB

Work location from Frame 45 to Frame 46

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 29-00-00-210-801

Task 29-00-00-863-802

Task 29-00-00-864-802

Task 29-12-53-400-805

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 111

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SERVICE BULLETIN

References

Fig. A-GDAAA

Torque Check of the Hydraulic Unions

on the Blue Hydraulic System HP

Manifold

Sheet 01

(a) Remove the safety clip(s) and/or tag(s) and close/unlock the circuit breaker(s) as

specified in the Job Set-up in the Installation of the Blue HP Manifold-Supply

Check-Valves, refer to AMM Task 29-12-53-400-805.

(b) Pressurize the Blue hydraulic system with the electric pump, refer to AMM Task

29-00-00-863-802.

(c) Make sure there are no leaks from all the unions on the manifold.

(d) Make sure there are no leaks from the connections of the CV.

(e) Make sure there are no leaks from the pipe connections.

(f) Check for air in the Blue hydraulic system, refer to AMM Task 29-00-00-210-801.

(g) Depressurize the Blue hydraulic system, refer to AMM Task 29-00-00-864-802.

**CONF ALL

E. CLOSE-UP

**CONF 001

None

**CONF 002

(1) Subtask 293125-942-204-001 - Close-up

Work Zones and Access Panels

Zone Access/Work location

190

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 29-12-53-400-805

(a) Make sure that the work areas are clean and clear of tools and other items of

equipment.

(b) Do the Job Close-up procedure for the installation of the Blue Hydraulic Manifold

FIN 6103JM, refer to AMM Task 29-12-53-400-805.

(c) Put the aircraft back to its initial configuration.

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 112

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SERVICE BULLETIN

Task 293125-831-852-001 - Modify the Yellow HP Hydraulic Manifold on Aircraft

**CONF ALL

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

INCLUDED IN THE REFERENCED PROCEDURES.

CAUTION: DO NOT WORK ON ALL THREE HYDRAULIC SYSTEMS DURING THE SAME

MAINTENANCE INPUT WITH THE SAME MAINTENANCE PERSONNEL. THIS

IS TO MAKE SURE THAT A POSSIBLE MAINTENANCE ERROR ON ONE

SYSTEM IS NOT DONE AGAIN ON A DIFFERENT SYSTEM. A MAINTENANCE

ERROR ON MORE THAN ONE HYDRAULIC SYSTEM CAN CAUSE SYSTEM

FAILURE ON MULTIPLE SYSTEMS. IF MAINTENANCE IS NECESSARY ON

MORE THAN ONE SYSTEM AT THE SAME TIME AND INVOLVES LINES /

COMPONENTS DISCONNECTION, DIFFERENT MAINTENANCE PERSONNEL

MUST BE USED FOR EACH SYSTEM.

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 ModifyS, ALWAYS KEEP ELECTRICAL WIRING, COMPONENTS

AND THE WORK AREA AS CLEAN AS POSSIBLE. TO DO THIS:

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

NECESSARY ON WIRING AND COMPONENTS.

- REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND

OTHER CONTAMINATION.

THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION

AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION.

IF THERE IS CONTAMINATION, REFER TO ESPM 20-55-00.

NOTE: The accomplishment instructions of this Service Bulletin include procedures given

in other documents or in other sections of the Service Bulletin. When the words

’refer to’ are used and the operator has a procedure accepted by the local authority

he belongs to, the accepted alternative procedure can be used. When the words ’in

accordance with’ are used then the given procedure must be followed.

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

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

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

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

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

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

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

NOTE: 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

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 113

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@A330

SERVICE BULLETIN

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

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

the aircraft can be put back into a serviceable condition.

NOTE: AIRBUS generally recommends not to open the three hydraulic systems during

the same maintenance input. Therefore it is recommended to apply this Service

Bulletin during two different maintenance inputs, for instance the Yellow and Blue

hydraulic system first and the Green hydraulic system at a later opportunity.

NOTE: Discarded parts must be managed at the operator’s discretion.

NOTE: This Service Bulletin contains the instructions for the on-aircraft maintenance

necessary to ensure the continued airworthiness of the aircraft.

For any deviations to the instructions contained herein, contact Airbus for further

instructions and approval.

Task Associated Data

**CONF 001

Manpower

TOTAL MANHOURS 0.00

**CONF 002

Zone

190 196

Modified FIN

5316JM301 7103JM

Access

Door 196BB 811

Manpower

TOTAL MANHOURS 7.50

ELAPSED TIME (HOURS) 7.50

**CONF ALL

A. GENERAL

**CONF 001

None

**CONF 002

(1) Subtask 293125-910-205-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 114

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@A330

SERVICE BULLETIN

References

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

06-31-53, Page Block 001

06-41-53, Page Block 001

Task 20-11-11-911-803

Task 20-29-00-911-801

Task 29-00-00-910-805

Consumable Material List (CML)

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

Consumable Materials List (CML).

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

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

(d) For the identification of access panels, refer to AMM 06-41-53, Page Block 001.

(e) For the safety procedures of the hydraulic systems, refer to AMM Task

29-00-00-910-805.

(f) For the removal/installation of O-ring seals, refer to AMM Task 20-29-00-911-801.

(g) Put a blanking plug on an open manifold port.

(h) For wirelocking safety procedures and warnings, refer to AMM Task

20-11-11-911-803.

(2) Subtask 293125-839-205-001 - 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

None

**CONF 002

(1) Subtask 293125-941-206-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 115

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@A330

SERVICE BULLETIN

References

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

Task 20-23-22-910-801

Task 29-13-53-000-804

NOTE: The items given in this note 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 are 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.

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

12-34-24-860-802.

(b) Do the Job Set-up procedure for the removal of the CV FIN 5316JM301, refer to

AMM Task 29-13-53-000-804.

(c) Inspect the red marking on all the manifold unions. Apply red marking on the

unions where it is not visible, refer to AMM Task 20-23-22-910-801.

**CONF ALL

C. PROCEDURE

**CONF 001

None

**CONF 002

(1) Subtask 293125-831-207-001 - Modify the Yellow HP Manifold (FIN 7103JM)

Work Zones and Access Panels

Zone Access/Work location

196 Access Door 811, Door 196BB

Work location from Frame 45 to Frame 46

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 116

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SERVICE BULLETIN

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills AIRFRAME

Material necessary to do the job

Component COMPD01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

2 NAS1612-24 1 PACKING

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

shall be ordered as necessary through the given channel.

Equipment BFEZ01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

3 CAR402 1 VALVE

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

shall be ordered as necessary through the given channel.

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Phosphate Ester Hydraulic

Fluid-General Power

02ABA1 As required

Varnish Polyurethane--

Marking Structure

04SAB2 As required

Non Aqueous Cleaner -

General

08BAA9 As required

Wire-Locking Dia: 1 Mm

(0.041 Inch) Cres

14QGC1 As required

Textile - Lint Free Cotton 14SBA1 As required

References

Aircraft Maintenance Manual (AMM) Task 20-23-22-910-801

Task 29-13-53-000-804

Process and Material Specification

(PMS)

Process and Material Specification (PMS)

01-06-12

Fig. A-GBCAA

Removal and Installation of the CVs and

Re-identification of the Yellow Hydraulic

System HP Manifold

Sheet 01

Sheet 02

Sheet 03

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 117

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SERVICE BULLETIN

(a) Remove the CV, Item 3 from the HP manifold (FIN 7103JM), refer to AMM Task

29-13-53-000-804.

1

CAUTION: DO NOT USE POINTED, SHARP OR METAL TOOLS TO

REMOVE THE O-RING OR SQUARE SEAL OR BACK-UP

RINGS. SHARP EDGES CAN CAUSE DAMAGE TO THE

BOBBINS (GROOVES OR SEAL CONTACT SURFACES).

As shown in Fig. A-GBCAA Sheet 01, View B, cut and discard the lockwire

then remove:

FIN 5316JM301

1 Valve-check CAR401 Item (3) Discard

FIN 5316JM301

1 Seal Assy 818114 Item (2) Discard

(b) Install the CV on the Yellow HP manifold (FIN 7103JM).

1 Clean the related components and work areas with:

Non Aqueous

Cleaner - General

08BAA9 As required

and

Textile - Lint Free

Cotton

14SBA1 As required

2

CAUTION: ONLY USE THE SPECIFIED LUBRICANT TO LUBRICATE

THE FITTING THREADS.

Apply to the threads of the CV:

Phosphate Ester

Hydraulic FluidGeneral Power

02ABA1 As required

3 Discard the storage seals from the new CVs.

4 As shown in Fig. A-GBCAA Sheet 01, View B and Fig. A-GBCAA Sheet 03,

install:

FIN 5316JM301

1 Valve-check CAR402 Item 3

FIN 5316JM301

1 Packing NAS1612-24 Item 2

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 118

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SERVICE BULLETIN

a Before installation, make sure that the back-up ring is flush with the

groove in the CVs, Item 3.

(c) Torque the CV, Item 3, two times:

1 Torque the CV between 230 and 250 Nm (169.64-184.39 lbf.ft).

2 Undo the CV by a 1/8th turn.

3 Torque the CV between 230 and 250 Nm (169.64-184.39 lbf.ft).

(d) Make a red mark on the CV and the manifold, refer to AMM Task

20-23-22-910-801.

1 Use:

Varnish

Polyurethane--

Marking Structure

04SAB2 As required

(e) As shown in Fig. A-GBCAA Sheet 01, View B, safety the CV, Item 3, with:

Wire-Locking Dia: 1

Mm (0.041 Inch)

Cres

14QGC1 As required

(2) Subtask 293125-930-212-001 - Reidentify the Yellow HP Manifold (FIN 7103JM)

Work Zones and Access Panels

Zone Access/Work location

196 Access Door 811, Door 196BB

Work location from Frame 45 to Frame 46

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills AIRFRAME

Material necessary to do the job

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Varnish Polyurethane-Low

Voc External Structure

04SBA3 As required

Non Aqueous Cleaner

Petroleum Based

08BBB1 As required

Textile - Lint Free Cotton 14SBA1 As required

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 119

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SERVICE BULLETIN

References

Process and Material Specification

(PMS)

Process and Material Specification (PMS)

01-06-12

Fig. A-GBFAA

Removal and Installation of the CVs and

Re-identification of the Yellow Hydraulic

System HP Manifold

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Fig. A-GABAA

PN Evolution of the Green, Blue and

Yellow System HP Hydraulic Manifolds

Sheet 01

(a) Re-identify the Yellow HP Manifold (FIN 7103JM), refer to Process and Material

Specification (PMS) 01-06-12, Fig. A-GBFAA Sheet 03, View D, Fig. A-GBFAA

Sheet 04, Views E and F for information and the table given in Appendix 01: PN

Evolution of the Green, Blue and Yellow System HP Hydraulic Manifolds , refer to

Fig. A-GABAA Sheet 01.

1 Clean the Manifold identification PN located on the body of the Yellow HP

Manifold (FIN 7103JM), use:

Textile - Lint Free

Cotton

14SBA1 As required

made moist with

Non Aqueous

Cleaner Petroleum

Based

08BBB1 As required

2 Use an indelible ink pen to re-identify the Yellow HP Manifold with the new

PN, refer to the table given in Appendix 01: PN Evolution of the Green, Blue

and Yellow System HP Hydraulic Manifolds , refer to Fig. A-GABAA Sheet 01.

NOTE: If the old HP manifold PN cannot be found at the location

shown in Fig. A-GBFAA Sheet 04, Views E and F, the IPC

body manifold PN should be used to find the new HP manifold

PN, refer to the table given in Appendix 01: PN Evolution of

the Green, Blue and Yellow System HP Hydraulic Manifolds ,

refer to Fig. A-GABAA Sheet 01.

3 Apply varnish to the new identification PN, use:

Varnish

Polyurethane-Low

Voc External

Structure

04SBA3 As required

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 120

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@A330

SERVICE BULLETIN

**CONF ALL

D. TEST

**CONF 001

None

**CONF 002

(1) Subtask 293125-730-207-001 - Test the Yellow HP Manifold (FIN 7103JM)

Work Zones and Access Panels

Zone Access/Work location

196 Access Door 811, Door 196BB

Work location from Frame 45 to Frame 46

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 20-23-11-917-802

Task 20-23-22-910-801

Task 20-29-00-911-801

Task 29-00-00-210-801

Task 29-00-00-863-803

Task 29-00-00-864-803

Task 29-13-53-400-804

Fig. A-GEAAA

Torque Check of the Hydraulic Unions

on the Yellow Hydraulic System HP

Manifold

Sheet 01

(a) Inspect the red marking on all the plug-in unions on the manifold.

1 If any red marking is not aligned:

a Disconnect the pipe from the plug-in union.

b Remove the plug-in union from the manifold.

c Replace the packing of the plug-in union with a new one, refer to AMM

Task 20-29-00-911-801.

d As shown in Fig. A-GEAAA Sheet 01, View B, install and tighten

all removed plug-in unions on the manifold, refer to AMM Task

20-29-00-911-801 and Table 3, below.

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 121

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@A330

SERVICE BULLETIN

e As shown in Fig. A-GEAAA Sheet 01, View B, install and tighten the pipe

to the plug-in union and manifold, refer to AMM Task 20-23-11-917-802

and Table 3, below.

Item No. Pipe Torque Value (Nm) Item No. Union Torque Value

(Nm)

(36) 15-17 (22) 12.1-13.2

(37) 85-95 (16) 72.9-74

(38) 81-89 (12) 116.4-118.6

(39) 85-95 (9) 116.4-118.6

(41) 75-83 (13) 50.3-51.4

(40) 85-95 (9) 116.4-118.6

Table 3

(b) Make a new red mark on all the unions where the red mark is not aligned or not

clearly visible, refer to AMM Task 20-23-22-910-801.

(c) Remove the safety clip(s) and/or tag(s) and close/unlock the circuit breaker(s) as

specified in the Job Set-up in the Installation of the Yellow HP Manifold-Supply

Check-Valves, refer to AMM Task 29-13-53-400-804.

(d) Pressurize the Yellow hydraulic system with the electric pump, refer to AMM Task

29-00-00-863-803.

(e) Make sure there are no leaks from the unions on the manifold.

(f) Make sure there are no leaks from the connections of the CV.

(g) Make sure there are no leaks from the pipe connections.

(h) Check for air in the Yellow hydraulic system, refer to AMM Task 29-00-00-210-801.

(i) Depressurize the Yellow hydraulic system, refer to AMM Task 29-00-00-864-803.

**CONF ALL

E. CLOSE-UP

**CONF 001

None

**CONF 002

(1) Subtask 293125-942-205-001 - Close-up

Work Zones and Access Panels

Zone Access/Work location

190

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 122

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@A330

SERVICE BULLETIN

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 29-11-53-400-806

Task 29-13-53-400-804

(a) Make sure that the work areas are clean and clear of tools and other items of

equipment.

(b) Do the Job Close-up procedure for the installation of the CV FIN 5316JM301, refer

to AMM Task 29-13-53-400-804.

(c) Put the aircraft back to its initial configuration.

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 123

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@A330

SERVICE BULLETIN

This Page Intentionally Left Blank

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 124

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SERVICE BULLETIN

Task 293125-831-853-001 - Modify the Yellow HP Hydraulic Manifold on Bench

**CONF ALL

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

INCLUDED IN THE REFERENCED PROCEDURES.

CAUTION: DO NOT WORK ON ALL THREE HYDRAULIC SYSTEMS DURING THE SAME

MAINTENANCE INPUT WITH THE SAME MAINTENANCE PERSONNEL. THIS

IS TO MAKE SURE THAT A POSSIBLE MAINTENANCE ERROR ON ONE

SYSTEM IS NOT DONE AGAIN ON A DIFFERENT SYSTEM. A MAINTENANCE

ERROR ON MORE THAN ONE HYDRAULIC SYSTEM CAN CAUSE SYSTEM

FAILURE ON MULTIPLE SYSTEMS. IF MAINTENANCE IS NECESSARY ON

MORE THAN ONE SYSTEM AT THE SAME TIME AND INVOLVES LINES /

COMPONENTS DISCONNECTION, DIFFERENT MAINTENANCE PERSONNEL

MUST BE USED FOR EACH SYSTEM.

CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP

ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY

AND MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENANCE

WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING,

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

THIS:

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

NECESSARY ON WIRING AND COMPONENTS.

- REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND

OTHER CONTAMINATION.

THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION

AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION.

IF THERE IS CONTAMINATION, REFER TO ESPM 20-55-00.

NOTE: The accomplishment instructions of this Service Bulletin include procedures given

in other documents or in other sections of the Service Bulletin. When the words

’refer to’ are used and the operator has a procedure accepted by the local authority

he belongs to, the accepted alternative procedure can be used. When the words ’in

accordance with’ are used then the given procedure must be followed.

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

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

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

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

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

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

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

NOTE: 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

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 125

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@A330

SERVICE BULLETIN

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

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

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

the aircraft can be put back into a serviceable condition.

NOTE: AIRBUS generally recommends not to open the three hydraulic systems during

the same maintenance input. Therefore it is recommended to apply this Service

Bulletin during two different maintenance inputs, for instance the Yellow and Blue

hydraulic system first and the Green hydraulic system at a later opportunity.

NOTE: Discarded parts must be managed at the operator’s discretion.

NOTE: This Service Bulletin contains the instructions for the on-aircraft maintenance

necessary to ensure the continued airworthiness of the aircraft.

For any deviations to the instructions contained herein, contact Airbus for further

instructions and approval.

Task Associated Data

**CONF 001

Manpower

TOTAL MANHOURS 0.00

**CONF 002

Zone

190 196

Modified FIN

5316JM301 7103JM

Access

Door 196BB 811

Manpower

TOTAL MANHOURS 10.50

ELAPSED TIME (HOURS) 10.50

**CONF ALL

A. GENERAL

**CONF 001

None

**CONF 002

(1) Subtask 293125-910-206-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 126

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@A330

SERVICE BULLETIN

References

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

06-31-53, Page Block 001

06-41-53, Page Block 001

Task 20-11-11-911-803

Task 20-29-00-911-801

Task 29-00-00-910-805

Consumable Material List (CML)

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

Consumable Materials List (CML).

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

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

(d) For the identification of access panels, refer to AMM 06-41-53, Page Block 001.

(e) For the safety procedures of the hydraulic systems, refer to AMM Task

29-00-00-910-805.

(f) For the removal/installation of O-ring seals, refer to AMM Task 20-29-00-911-801.

(g) Put a blanking plug on an open manifold port.

(h) For wirelocking safety procedures and warnings, refer to AMM Task

20-11-11-911-803.

(2) Subtask 293125-839-206-001 - 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

None

**CONF 002

(1) Subtask 293125-941-207-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 127

6

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@A330

SERVICE BULLETIN

References

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

Task 29-13-53-000-803

NOTE: The items given in this note 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 are 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.

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

12-34-24-860-802.

(b) Do the Job Set-up procedure for the removal of the HP manifold FIN 7103JM, refer

to AMM Task 29-13-53-000-803.

**CONF ALL

C. PROCEDURE

**CONF 001

None

**CONF 002

(1) Subtask 293125-020-210-001 - Remove the Yellow HP Manifold (FIN 7103JM)

Work Zones and Access Panels

Zone Access/Work location

196 Access Door 811, Door 196BB

Work location from Frame 45 to Frame 46

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 128

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@A330

SERVICE BULLETIN

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 20-29-00-911-801

Task 29-13-53-000-804

Fig. A-GBFAA

Removal and Installation of the CVs and

Re-identification of the Yellow Hydraulic

System HP Manifold

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

(a) As shown in Fig. A-GBFAA Sheet 01, View B, disconnect:

1 Pipe Item (36) Retain

1 Pipe Item (37) Retain

1 Pipe Item (38) Retain

1 Pipe Item (39) Retain

1 Pipe Item (40) Retain

1 Pipe Item (41) Retain

(b) As shown in Fig. A-GBFAA Sheet 01, View B, refer to AMM Task

29-13-53-000-804 and AMM Task 20-29-00-911-801, remove:

FIN 7103JM

1 HP Manifold Assembly Item (24) Retain

with

3 Bolt-Hexagon Head NAS6605-5 Item (23) Retain

3 Washer ASNA2397-516L Item (18) Retain

2 Plug-in Union Item (9) Retain

1 Plug-in Union Item (12) Retain

3 Packing NAS1612-16 Item (8) Discard

1 Plug-in Union Item (13) Retain

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 129

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@A330

SERVICE BULLETIN

1 Packing NAS1612-10 Item (14) Discard

1 Plug-in Union Item (16) Retain

1 Packing NAS1612-12 Item (15) Discard

1 Plug-in Union Item (22) Retain

1 Packing NAS1612-4 Item (21) Discard

(2) Subtask 293125-831-208-001 - Modify the Yellow HP Manifold (FIN 7103JM)

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills AIRFRAME

Material necessary to do the job

Component COMPD01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

2 NAS1612-24 1 PACKING

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

shall be ordered as necessary through the given channel.

Equipment BFEZ01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

3 CAR402 1 VALVE

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

shall be ordered as necessary through the given channel.

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Phosphate Ester Hydraulic

Fluid-General Power

02ABA1 As required

Varnish Polyurethane--

Marking Structure

04SAB2 As required

Non Aqueous Cleaner -

General

08BAA9 As required

Wire-Locking Dia: 1 Mm

(0.041 Inch) Cres

14QGC1 As required

Textile - Lint Free Cotton 14SBA1 As required

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 130

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@A330

SERVICE BULLETIN

Standard tool TOOLD01

ITEM TOOL N ̊ TOOL NAME QTY SEE

NOTES

54 97F29108805000 Kit-Instl, CAR401 VLV 1

References

Aircraft Maintenance Manual (AMM) Task 20-23-22-910-801

Task 20-29-00-911-801

Fig. A-GBFAA

Removal and Installation of the CVs and

Re-identification of the Yellow Hydraulic

System HP Manifold

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Fig. A-GEAAA

Torque Check of the Hydraulic Unions

on the Yellow Hydraulic System HP

Manifold

Sheet 01

(a) On the bench, install the Yellow HP manifold (FIN 7103JM), Item (24) onto the

Installation Tool for CAR401, Item 54.

1 As shown in Fig. A-GBFAA Sheet 02, View C, install in vice:

Item 54 97F29108805000 Kit-Instl, CAR401

VLV

1

2 Install the HP Manifold (FIN 7103JM), Item (24), on the Installation Tool for

CAR401, Item 54.

NOTE: To install the HP manifold (FIN 7103JM), Item (24), correctly,

use the Y marks on the installation tool for CAR401, Item 54.

3 As shown in Fig. A-GBFAA Sheet 02, View C, install the items that follow from

the Installation Kit:

3 Screw Item 50

6 Washer Item 51

3 Nut Item 53

1 Support Item 34

NOTE: The Support, Item 34, can be hexagonal or spherical.

NOTE: The items listed above are part of Standard tool TOOLD01.

(b) Remove the CV Item (3), from the Yellow HP manifold (FIN 7103JM).

1

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 131

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@A330

SERVICE BULLETIN

CAUTION: DO NOT USE POINTED, SHARP OR METAL TOOLS TO

REMOVE THE O-RING OR SQUARE SEAL OR BACK-UP

RINGS. SHARP EDGES CAN CAUSE DAMAGE TO THE

BOBBINS (GROOVES OR SEAL CONTACT SURFACES).

As shown in Fig. A-GBFAA Sheet 02, View C, cut and discard the lockwire

then remove:

FIN 5316JM301

1 Valve-check CAR401 Item (3) Discard

FIN 5316JM301

1 Seal Assy 818114 Item (2) Discard

(c) Remove the Installation Placard, Item (45), from the Yellow HP manifold (FIN

7103JM).

1 As shown in Fig. A-GBFAA Sheet 02, View C, remove with a scraper:

1 Installation Placard Item (45) Discard

(d) Clean the related components and work areas with:

Non Aqueous

Cleaner - General

08BAA9 As required

and

Textile - Lint Free

Cotton

14SBA1 As required

(e) Install the CV on the Yellow HP manifold (FIN 7103JM).

1 Clean the related components and work areas with:

Non Aqueous

Cleaner - General

08BAA9 As required

and

Textile - Lint Free

Cotton

14SBA1 As required

2

CAUTION: ONLY USE THE SPECIFIED LUBRICANT TO LUBRICATE

THE FITTING THREADS.

Apply to the threads of the CV:

Phosphate Ester

Hydraulic FluidGeneral Power

02ABA1 As required

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 132

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@A330

SERVICE BULLETIN

3 Discard the storage seals from the new CVs.

4 As shown in Fig. A-GBFAA Sheet 03, View D and Fig. A-GBFAA Sheet 05,

install:

FIN 5316JM301

1 Valve-check CAR402 Item 3

FIN 5316JM301

1 Packing NAS1612-24 Item 2

a Before installation, make sure that the back-up ring is flush with the

groove in the CVs, Item 3.

(f) Torque the CV, Item 3, two times:

1 Torque the CV between 230 and 250 Nm (169.64-184.39 lbf.ft).

2 Undo the CV by a 1/8th turn.

3 Torque the CV between 230 and 250 Nm (169.64-184.39 lbf.ft).

(g) Make a red mark on the CV and the manifold, refer to AMM Task

20-23-22-910-801.

1 Use:

Varnish

Polyurethane--

Marking Structure

04SAB2 As required

(h) As shown in Fig. A-GBFAA Sheet 03, View D, safety the CV, Item 3, with:

Wire-Locking Dia: 1

Mm (0.041 Inch)

Cres

14QGC1 As required

(3) Subtask 293125-930-207-001 - Reidentify the Yellow HP Manifold (FIN 7103JM)

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills AIRFRAME

Material necessary to do the job

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Varnish Polyurethane-Low

Voc External Structure

04SBA3 As required

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 133

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@A330

SERVICE BULLETIN

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Non Aqueous Cleaner

Petroleum Based

08BBB1 As required

Textile - Lint Free Cotton 14SBA1 As required

References

Process and Material Specification

(PMS)

Process and Material Specification (PMS)

01-06-12

Fig. A-GBFAA

Removal and Installation of the CVs and

Re-identification of the Yellow Hydraulic

System HP Manifold

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Fig. A-GABAA

PN Evolution of the Green, Blue and

Yellow System HP Hydraulic Manifolds

Sheet 01

(a) Re-identify the Yellow HP Manifold (FIN 7103JM), refer to Process and Material

Specification (PMS) 01-06-12, Fig. A-GBFAA Sheet 03, View D, Fig. A-GBFAA

Sheet 04, Views E and F for information and the table given in Appendix 01: PN

Evolution of the Green, Blue and Yellow System HP Hydraulic Manifolds , refer to

Fig. A-GABAA Sheet 01.

1 Clean the Manifold identification PN located on the body of the Yellow HP

Manifold (FIN 7103JM), use:

Textile - Lint Free

Cotton

14SBA1 As required

made moist with

Non Aqueous

Cleaner Petroleum

Based

08BBB1 As required

2 Use an indelible ink pen to re-identify the Yellow HP Manifold with the new

PN, refer to the table given in Appendix 01: PN Evolution of the Green, Blue

and Yellow System HP Hydraulic Manifolds , refer to Fig. A-GABAA Sheet 01.

NOTE: If the old HP manifold PN cannot be found at the location

shown in Fig. A-GBFAA Sheet 04, Views E and F, the IPC

body manifold PN should be used to find the new HP manifold

PN, refer to the table given in Appendix 01: PN Evolution of

the Green, Blue and Yellow System HP Hydraulic Manifolds ,

refer to Fig. A-GABAA Sheet 01.

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 134

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@A330

SERVICE BULLETIN

3 Apply varnish to the new identification PN, use:

Varnish

Polyurethane-Low

Voc External

Structure

04SBA3 As required

(4) Subtask 293125-420-211-001 - Install the Yellow HP Manifold (FIN 7103JM)

Work Zones and Access Panels

Zone Access/Work location

196 Access Door 811, Door 196BB

Work location from Frame 45 to Frame 46

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills AIRFRAME

Material necessary to do the job

Component COMPD01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

8 NAS1612-16 3 PACKING

14 NAS1612-10 1 PACKING

15 NAS1612-12 1 PACKING

21 NAS1612-4 1 PACKING

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

shall be ordered as necessary through the given channel.

References

Aircraft Maintenance Manual (AMM) Task 20-23-11-917-802

Task 20-23-22-910-801

Task 20-29-00-911-801

Task 29-13-53-400-803

Fig. A-GBFAA

Removal and Installation of the CVs and

Re-identification of the Yellow Hydraulic

System HP Manifold

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Fig. A-GEAAA

Torque Check of the Hydraulic Unions

on the Yellow Hydraulic System HP

Manifold

Sheet 01

(a) As shown in Fig. A-GBFAA Sheet 02, View C, remove the Yellow HP Manifold (FIN

7103JM), Item (24) from the Installation Tool for CAR401, Item 54.

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 135

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SERVICE BULLETIN

(b) Install the Yellow hydraulic system HP manifold (FIN 7103JM), refer to AMM Task

29-13-53-400-803 and AMM Task 20-29-00-911-801.

1 As shown in Fig. A-GBFAA Sheet 01, View B, install:

FIN 7103JM

1 HP manifold assembly Item (24) Retained at

removal

with

3 Bolt-Hexagon Head NAS6605-5 Item (23) Retained at

removal

3 Washer ASNA2397-516L Item (18) Retained at

removal

3 Packing NAS1612-16 Item 8

2 Plug-in Union Item (9) Retained at

removal

1 Plug-in Union Item (12) Retained at

removal

1 Packing NAS1612-10 Item 14

1 Plug-in Union Item (13) Retained at

removal

1 Packing NAS1612-12 Item 15

1 Plug-in Union Item (16) Retained at

removal

1 Packing NAS1612-4 Item 21

1 Plug-in Union Item (22) Retained at

removal

and reconnect:

1 Pipe Item (36) Retained at

removal

1 Pipe Item (37) Retained at

removal

1 Pipe Item (38) Retained at

removal

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 136

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@A330

SERVICE BULLETIN

1 Pipe Item (39) Retained at

removal

1 Pipe Item (40) Retained at

removal

1 Pipe Item (41) Retained at

removal

(c) Tighten the plug-in unions and pipes.

1 As shown in Fig. A-GEAAA Sheet 01, View B, tighten all removed plug-in

unions, refer to AMM Task 20-23-22-910-801 and Table 3, below.

2 As shown in Fig. A-GEAAA Sheet 01, View B, tighten the pipes at both ends

to the plug-in union and manifold, refer to AMM Task 20-23-11-917-802, AMM

Task 20-29-00-911-801 and Table 3, below.

Item No. Pipe Torque Value (Nm) Item No. Union Torque Value

(Nm)

(36) 15-17 (22) 12.1-13.2

(37) 85-95 (16) 72.9-74

(38) 81-89 (12) 116.4-118.6

(39) 85-95 (9) 116.4-118.6

(41) 75-83 (13) 50.3-51.4

(40) 85-95 (9) 116.4-118.6

Table 3

(d) Make a new red mark on all the unions where the red mark is not aligned or not

clearly visible, refer to AMM Task 20-23-22-910-801.

**CONF ALL

D. TEST

**CONF 001

None

**CONF 002

(1) Subtask 293125-730-212-001 - Test of the Yellow HP Manifold (7103JM)

Work Zones and Access Panels

Zone Access/Work location

196 Access Door 811, Door 196BB

Work location from Frame 45 to Frame 46

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 137

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SERVICE BULLETIN

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 29-00-00-210-801

Task 29-00-00-863-803

Task 29-00-00-864-803

Task 29-13-53-400-804

Fig. A-GEAAA

Torque Check of the Hydraulic Unions

on the Yellow Hydraulic System HP

Manifold

Sheet 01

(a) Remove the safety clip(s) and/or tag(s) and close/unlock the circuit breaker(s) as

specified in the Job Set-up in the Installation of the Yellow HP Manifold-Supply

Check-Valves, refer to AMM Task 29-13-53-400-804.

(b) Pressurize the Yellow hydraulic system with the electric pump, refer to AMM Task

29-00-00-863-803.

(c) Make sure there are no leaks from all the unions on the manifold.

(d) Make sure there are no leaks from the connections of the CV.

(e) Make sure there are no leaks from the pipe connections.

(f) Check for air in the Yellow hydraulic system, refer to AMM Task 29-00-00-210-801.

(g) Depressurize the Yellow hydraulic system, refer to AMM Task 29-00-00-864-803.

**CONF ALL

E. CLOSE-UP

**CONF 001

None

**CONF 002

(1) Subtask 293125-942-206-001 - Close-up

Work Zones and Access Panels

Zone Access/Work location

190

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 29-11-53-400-803

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 138

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@A330

SERVICE BULLETIN

(a) Make sure that the work areas are clean and clear of tools and other items of

equipment.

(b) Do the Job Close-up procedure for the installation of the Yellow Hydraulic Manifold

FIN 7103JM, refer to AMM Task 29-11-53-400-803.

(c) Put the aircraft back to its initial configuration.

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 139

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@A330

SERVICE BULLETIN

**CONF ALL

FR53.1

FR53.2

Z147

(3) 3

(3) 3

HP MANIFOLD

5102JM

5316JM102

5316JM101

A

A

B

B

(2) 2

(2) 2

01 MAKE SAFE WITH LOCKWIRE.

NOTE:

01

C

E

G_SB_293125_6_BAAA_01_04

Figure A-GBAAA - Sheet 01

Removal and Installation of the CVs and Re-identification on the Green Hydraulic System HP Manifold

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 140

6

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@A330

SERVICE BULLETIN

**CONF ALL

AREA OF VIEW LOOKING FWD

RE−IDENTIFICATION

C

D

D

THE LOCATION OF THE OLD PN OF THE

GREEN HP MANIFOLD IS GIVEN FOR INFORMATION

02

NOTE: 02

G_SB_293125_6_BAAA_02_06

Figure A-GBAAA - Sheet 02

Removal and Installation of the CVs and Re-identification on the Green Hydraulic System HP Manifold

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 141

6

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@A330

SERVICE BULLETIN

**CONF ALL

03 BEFORE INSTALLATION, MAKE SURE THAT THE BACK−UP

NOTE:

2

03

RING IS FLUSH TO THE GROOVE AND THE LOWER O−RING .

BACK−UP RING

O−RING

04

04 REMOVE STORAGE SEAL AND DISCARD, BEFORE INSTALLING

NEW PACKING SEAL, ITEM 2.

E

G_SB_293125_6_BAAA_03_01

Figure A-GBAAA - Sheet 03

Removal and Installation of the CVs and Re-identification on the Green Hydraulic System HP Manifold

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 142

6

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@A330

SERVICE BULLETIN

**CONF 002

FR53.1

FR53.2

Z147

A

A

B

(6)

(11)

(1)

(6)

(7)

(6)

(10)

(5)

(4)4

(9)

(8) 8 (9)

(8) 8

(8) 8

(9)

5102JM

C

(26)

(25)

(25)

(25)

B D

G_SB_293125_6_BDAA_01_00

Figure A-GBDAA - Sheet 01

Removal and Installation of the CVs and Re-identification of the Green Hydraulic System HP Manifold

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 143

6

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@A330

SERVICE BULLETIN

**CONF 002

50

51

50

51 (1)

54

51

51

51

53

53

53

(45)

IDENTIFICATION

PLACARD

(3)

(3)

5316JM102

5316JM101 (2)

(2)

C

CAR 401 400 N.M OFF A/C

34

STANDARD

WRENCH

G_SB_293125_6_BDAA_02_03

Figure A-GBDAA - Sheet 02

Removal and Installation of the CVs and Re-identification of the Green Hydraulic System HP Manifold

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 144

6

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@A330

SERVICE BULLETIN

**CONF 002

3

3

HP MANIFOLD

5102JM

5316JM102

5316JM101

2

2

01 MAKE SAFE WITH LOCKWIRE.

NOTE:

01

D

E

G

G_SB_293125_6_BDAA_03_02

Figure A-GBDAA - Sheet 03

Removal and Installation of the CVs and Re-identification of the Green Hydraulic System HP Manifold

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 145

6

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@A330

SERVICE BULLETIN

**CONF 002

VIEW LOOKING FWD

E

F

F

AREA OF

RE−IDENTIFICATION

THE LOCATION OF THE OLD PN OF THE

GREEN HP MANIFOLD IS GIVEN FOR INFORMATION

02

NOTE: 02

G_SB_293125_6_BDAA_04_03

Figure A-GBDAA - Sheet 04

Removal and Installation of the CVs and Re-identification of the Green Hydraulic System HP Manifold

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 146

6

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@A330

SERVICE BULLETIN

**CONF 002

03 BEFORE INSTALLATION, MAKE SURE THAT THE BACK−UP

NOTE:

2

03

RING IS FLUSH TO THE GROOVE AND THE LOWER O−RING .

BACK−UP RING

O−RING

G

04

04 REMOVE STORAGE SEAL AND DISCARD, BEFORE INSTALLING

NEW PACKING SEAL, ITEM 2.

G_SB_293125_6_BDAA_05_01

Figure A-GBDAA - Sheet 05

Removal and Installation of the CVs and Re-identification of the Green Hydraulic System HP Manifold

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 147

6

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@A330

SERVICE BULLETIN

**CONF ALL

A

FR47

FR46

HP MANIFOLD

(3) 3

6103JM

5316JM201

Z195

A

B

(2) 2

01 MAKE SAFE WITH LOCKWIRE.

NOTE:

01

C

B

D

G_SB_293125_6_BBAA_01_05

Figure A-GBBAA - Sheet 01

Removal and Installation of the CVs and Re-identification of the Blue Hydraulic System HP Manifold

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 148

6

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@A330

SERVICE BULLETIN

**CONF ALL

VIEW LOOKING FWD

AREA OF

RE−IDENTIFICATION

C

THE LOCATION OF THE OLD PN OF THE

BLUE HP MANIFOLD IS GIVEN FOR INFORMATION

02

NOTE:

02

G_SB_293125_6_BBAA_02_05

Figure A-GBBAA - Sheet 02

Removal and Installation of the CVs and Re-identification of the Blue Hydraulic System HP Manifold

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 149

6

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@A330

SERVICE BULLETIN

**CONF ALL

03 BEFORE INSTALLATION, MAKE SURE THAT THE BACK−UP

NOTE:

2

03

RING IS FLUSH TO THE GROOVE AND THE LOWER O−RING .

BACK−UP RING

O−RING

04

04 REMOVE STORAGE SEAL AND DISCARD, BEFORE INSTALLING

NEW PACKING SEAL, ITEM 2.

D

G_SB_293125_6_BBAA_03_01

Figure A-GBBAA - Sheet 03

Removal and Installation of the CVs and Re-identification of the Blue Hydraulic System HP Manifold

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 150

6

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@A330

SERVICE BULLETIN

**CONF 002

A

FR47

FR46

6103JM

Z195

A

B

(20)

(10)

(6)

(12)

(8)8

(17) (4)4

(14)14

(13) (16)

(15)15

(13)

(14)14

(8)8

(9) (15)15

(16)

C

(31)

(32)

(33)

(34)

(35)

(29)

(30)

B D

G_SB_293125_6_BEAA_01_00

Figure A-GBEAA - Sheet 01

Removal and Installation of the CVs and Re-identification of the Blue Hydraulic System HP Manifold

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 151

6

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@A330

SERVICE BULLETIN

**CONF 002

(20)

54

50

51

50

51

51

51

51

53

53

53

50

51

(45)

IDENTIFICATION

PLACARD

5316JM201 (3)

(2)

C

CAR 401 400 N.M OFF A/C

34

STANDARD 

WRENCH

G_SB_293125_6_BEAA_02_03

Figure A-GBEAA - Sheet 02

Removal and Installation of the CVs and Re-identification of the Blue Hydraulic System HP Manifold

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 152

6

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@A330

SERVICE BULLETIN

**CONF 002

HP MANIFOLD

3

6103JM

5316JM201 2

01 MAKE SAFE WITH LOCKWIRE.

NOTE:

01

D

E

F

G_SB_293125_6_BEAA_03_02

Figure A-GBEAA - Sheet 03

Removal and Installation of the CVs and Re-identification of the Blue Hydraulic System HP Manifold

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 153

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@A330

SERVICE BULLETIN

**CONF 002

VIEW LOOKING FWD

E

AREA OF

RE−IDENTIFICATION

THE LOCATION OF THE OLD PN OF THE

BLUE HP MANIFOLD IS GIVEN FOR INFORMATION

02

NOTE:

02

G_SB_293125_6_BEAA_04_04

Figure A-GBEAA - Sheet 04

Removal and Installation of the CVs and Re-identification of the Blue Hydraulic System HP Manifold

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 154

6

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@A330

SERVICE BULLETIN

**CONF 002

03 BEFORE INSTALLATION, MAKE SURE THAT THE BACK−UP

NOTE:

2

03

RING IS FLUSH TO THE GROOVE AND THE LOWER O−RING .

BACK−UP RING

O−RING

04

04 REMOVE STORAGE SEAL AND DISCARD, BEFORE INSTALLING

NEW PACKING SEAL, ITEM 2.

F

G_SB_293125_6_BEAA_05_01

Figure A-GBEAA - Sheet 05

Removal and Installation of the CVs and Re-identification of the Blue Hydraulic System HP Manifold

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 155

6

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@A330

SERVICE BULLETIN

**CONF ALL

FR47

FR46

(3) 3

7103JM

HP MANIFOLD

5316JM301

A

Z196

A

B

(2) 2

01 MAKE SAFE WITH LOCKWIRE.

NOTE:

01

C

B

E

G_SB_293125_6_BCAA_01_04

Figure A-GBCAA - Sheet 01

Removal and Installation of the CVs and Re-identification of the Yellow Hydraulic System HP Manifold

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 156

6

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@A330

SERVICE BULLETIN

**CONF ALL

VIEW LOOKING FWD

AREA OF

RE−IDENTIFICATION

D

C

D

THE LOCATION OF THE OLD PN OF THE

YELLOW HP MANIFOLD IS GIVEN FOR INFORMATION

02

NOTE:

02

G_SB_293125_6_BCAA_02_04

Figure A-GBCAA - Sheet 02

Removal and Installation of the CVs and Re-identification of the Yellow Hydraulic System HP Manifold

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 157

6

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@A330

SERVICE BULLETIN

**CONF ALL

03 BEFORE INSTALLATION, MAKE SURE THAT THE BACK−UP

NOTE:

2

03

RING IS FLUSH TO THE GROOVE AND THE LOWER O−RING .

BACK−UP RING

O−RING

04

04 REMOVE STORAGE SEAL AND DISCARD, BEFORE INSTALLING

NEW PACKING SEAL, ITEM 2.

E

G_SB_293125_6_BCAA_03_01

Figure A-GBCAA - Sheet 03

Removal and Installation of the CVs and Re-identification of the Yellow Hydraulic System HP Manifold

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 158

6

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@A330

SERVICE BULLETIN

**CONF 002

FR47

FR46

7103JM

A

Z196

A

B

(24)

(18)

(23)

(23)

(18)

(16)

(15)15 (12)

(8)8

(9)

(8)8

(13)

(14)14

(9)

(8)8

(21)21

(22)

C

(36)

(37)

(38) (39)

(40)

(41)

B D

G_SB_293125_6_BFAA_01_00

Figure A-GBFAA - Sheet 01

Removal and Installation of the CVs and Re-identification of the Yellow Hydraulic System HP Manifold

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 159

6

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@A330

SERVICE BULLETIN

**CONF 002

(24)

51

53

54

50

51

53

51

(45)

50

51

IDENTIFICATION

PLACARD

(3) 5316JM301

(2)

C

CAR 401 400 N.M OFF A/C

34

STANDARD

WRENCH

G_SB_293125_6_BFAA_02_03

Figure A-GBFAA - Sheet 02

Removal and Installation of the CVs and Re-identification of the Yellow Hydraulic System HP Manifold

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 160

6

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@A330

SERVICE BULLETIN

**CONF 002

3

7103JM

HP MANIFOLD

5316JM301

2

01 MAKE SAFE WITH LOCKWIRE.

NOTE:

01

D

E

G

G_SB_293125_6_BFAA_03_02

Figure A-GBFAA - Sheet 03

Removal and Installation of the CVs and Re-identification of the Yellow Hydraulic System HP Manifold

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 161

6

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

SERVICE BULLETIN

**CONF 002

VIEW LOOKING FWD

E

F

F

AREA OF

RE−IDENTIFICATION

THE LOCATION OF THE OLD PN OF THE

YELLOW HP MANIFOLD IS GIVEN FOR INFORMATION

01

NOTE:

01

G_SB_293125_6_BFAA_04_02

Figure A-GBFAA - Sheet 04

Removal and Installation of the CVs and Re-identification of the Yellow Hydraulic System HP Manifold

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 162

6

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

SERVICE BULLETIN

**CONF 002

03 BEFORE INSTALLATION, MAKE SURE THAT THE BACK−UP

NOTE:

2

03

RING IS FLUSH TO THE GROOVE AND THE LOWER O−RING .

BACK−UP RING

O−RING

G

04

04 REMOVE STORAGE SEAL AND DISCARD, BEFORE INSTALLING

NEW PACKING SEAL, ITEM 2.

G_SB_293125_6_BFAA_05_01

Figure A-GBFAA - Sheet 05

Removal and Installation of the CVs and Re-identification of the Yellow Hydraulic System HP Manifold

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 163

6

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

SERVICE BULLETIN

**CONF ALL

FR53.1

FR53.2

Z147

A

A

B

B

(1)

(5)

(9)

(9)

(9)

5102JM

(26)

(25)

(25)

(25)

01 PIPES AND UNIONS SHOWN EXPLODED FOR CLARITY.

NOTE:

01

G_SB_293125_6_CAAA_01_00

Figure A-GCAAA - Sheet 01

Torque Check of the Hydraulic Unions on the Green Hydraulic System HP Manifold

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 164

6

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@A330

SERVICE BULLETIN

**CONF ALL

A

FR47

FR46

6103JM

Z195

A

B

B

(20)

(12)

(17)

(13) (16)

(13)

(9) (16)

(31)

(32) (33) (34)

(35)

(29)

(30)

01 PIPES AND UNIONS SHOWN EXPLODED FOR CLARITY.

NOTE:

01

G_SB_293125_6_DAAA_01_00

Figure A-GDAAA - Sheet 01

Torque Check of the Hydraulic Unions on the Blue Hydraulic System HP Manifold

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 165

6

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@A330

SERVICE BULLETIN

**CONF ALL

FR47

FR46

7103JM

A

Z196

A

B

B

(24)

(16)

(12) (9)

(13) (9)

(22)

(36)

(37)

(38) (39)

(40) (41)

01

01 PIPES AND UNIONS SHOWN EXPLODED FOR CLARITY.

NOTE:

G_SB_293125_6_EAAA_01_00

Figure A-GEAAA - Sheet 01

Torque Check of the Hydraulic Unions on the Yellow Hydraulic System HP Manifold

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 166

6

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@A330

SERVICE BULLETIN

Appendix 01: PN Evolution of the Green, Blue and Yellow System HP Hydraulic Manifolds

**CONF ALL

F2911086603400

(1) THE EVOLUTION TABLE THAT FOLLOWS IS TO BE USED TO IDENTIFY THE IPC PART NUMBER.

F2911086603600

F2911086602400

F2911086603200

F2911086603000

F2911086602800

F2911086603600

F2911086602400

F2911086602600

F2911086603400

F2911086603200

F2911086603000

F2911086602400

F2911086602600

F2911086602800

F2911086302200

F2911086303200

F2911086303000

F2911086302400

F2911086302600

F2911086302800

F2911086302200

F2911086303200

F2911086303000

F2911086302400

F2911086302600

F2911086302800

F2911086302200

F2911037601800

F2911037602600

F2911037602000

F2911037602200

F2911037602400

F2911037601800

F2911037602600

F2911037602400

F2911037601800

F2911037602000

F2911037602200

NEW PN HP MANIFOLD

F2911086601800

F2911086602000

F2911086602200

F2911086601600

F2911086601400

F2911086601200

F2911086600000

F2911086600800

F2911086601000

F2911086600100

F2911086600200

F2911086600300

F2911086600600

F2911086600500

F2911086600400

F2911086302000

F2911086301800

F2911086301600

F2911086301000

F2911086301200

F2911086301400

F2911086300800

F2911086300000

F2911086300100

F2911086300500

F2911086300400

F2911086300200

F2911086300600

F2911037601600

F2911037601400

F2911037600800

F2911037601000

F2911037601200

F2911037600600

F2911037600000

F2911037600100

F2911037600400

F2911037600300

F2911037600200

OLD PN HP MANIFOLD

F2911183300000

F2911085700000

F2911188500000

F2911183300000

F2911183300100

F2911186800000

F2911085700000

F2911188500000

F2911187500000

F2911183300000

F2911183300000

F2911183300100

F2911188500000

F2911187500000

F2911186800000

F2911189400000

F2911185800000

F2911183400000

F2911187600000

F2911186900000

F2911183400000

F2911189400000

F2911185800000

F2911183400000

F2911187600000

F2911186900000

F2911183400000

F2911189400000

F2911048900000

F2911044400000

F2911047200000

F2911044400100

F2911044400000

F2911048900000

F2911034000000

F2911044400000

F2911048900000

F2911047200000

F2911044400100

IPC PN BODY MANIFOLD

GREEN

HYDRAULIC SYSTEM

BLUE

YELLOW

NOTE: THE LAST TWO DIGITS OF THE PNs LISTED ARE NOT APPLICABLE

FOR RE−IDENTIFICATION. G_SB_293125_6_ABAA_01_02

Figure A-GABAA - Sheet 01

PN Evolution of the Green, Blue and Yellow System HP Hydraulic Manifolds

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 1

6

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@A330

SERVICE BULLETIN

Appendix 01: PN Evolution of the Green, Blue and Yellow System HP Hydraulic Manifolds

This Page Intentionally Left Blank

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 2

6

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@A330

SERVICE BULLETIN

Appendix 02: Local Manufacture of Tooling

**CONF 002

G_SB_293125_6_ACAA_01_00

Figure A-GACAA - Sheet 01

Local Manufacture of Tooling

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 1

6

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@A330

SERVICE BULLETIN

Appendix 02: Local Manufacture of Tooling

**CONF 002

G_SB_293125_6_ACAA_02_00

Figure A-GACAA - Sheet 02

Local Manufacture of Tooling

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 2

6

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SERVICE BULLETIN

Appendix 02: Local Manufacture of Tooling

**CONF 002

G_SB_293125_6_ACAA_03_00

Figure A-GACAA - Sheet 03

Local Manufacture of Tooling

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 3

6

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SERVICE BULLETIN

REPORTING SHEET

TITLE: HYDRAULIC POWER - MAIN HYDRAULIC POWER - REPLACE CHECK

VALVE PN CAR401 WITH IMPROVED CHECK VALVE PN CAR402

MODIFICATION No.: 203972D50812

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: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 1

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SERVICE BULLETIN

QUALITY PERCEPTION FORM

Use this form to tell us what is your perception of the quality of this Service Bulletin. The reported data

that you provide us will be used to analyse areas of difficulties and to take corrective action to further

improve the quality of our Service Bulletins.

We thank you for the time you have taken in completing this form.

(Please rate on a scale of 1 to 4, with 4 being the highest score)

- Quality rating of this SB 4321

- Quality rating of the Accomplishment Instructions 4321

- Quality rating of the Illustrations 4321

- Is this SB easy to understand ? Y/N

If you have had difficulties in the accomplishment of this SB please quote below the area(s) and give a

short description of the issue.

Planning Material Instructions

X Effectivity X Kit content X Preparation

X Reason X List of Materials Operator Supplied X Mod/Inspection

X Manpower X Industry support X Test

X References X Re-identification X Close-Up

X Publication X Tooling X Illustrations

Comments:

Operator: Date:

Name/Title:

Please return this form to:

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX FRANCE

Attn : SEM4 Service Bulletins Management

FAX : (33) 5 61 93 42 51

Or via your Resident Customer Support Office.

DATE: Aug 08/14 SERVICE BULLETIN No.: A330-29-3125

REVISION No.: 03 - Apr 08/16 Page: 1

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