@A340

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.02 of Service Bulletin No.A340-29-4096

ADDITIONAL WORK

**CONF ALL

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

REASON

Revision No.02 issued to:

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

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

CUSTOMER SERVICES DIRECTORATE contact.

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

- In para PRICE AND AVAILABILITY, sentence S10 deleted.

CHANGES

SUMMARY

EFFECTIVITY OPERATOR LIST UPDATED R

REFERENCES / REPERCUSSIONS REFERENCES/REPERCUSSIONS TABLE

UPDATED

R

DATE: Aug 08/14 SERVICE BULLETIN No.: A340-29-4096

REVISION No.: 02 - Apr 08/16 Page: 1

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@A340

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

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

MATERIAL INFORMATION

MATERIAL - PRICE AND AVAILABILITY

Price and Availability PRICE AND AVAILABILITY UPDATED R

INDUSTRY SUPPORT INFORMATION INDUSTRY SUPPORT INFORMATION UPDATED R

ACCOMPLISHMENT INSTRUCTIONS

TASK 294096- 831-848-001-Modify the

Green HP Hydraulic Manifold on Aircraft

TASK SOLUTION UPDATED

NOTE UPDATED

R

Subtask 294096-910-201-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

Subtask 294096-831-201-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

FIGURE REFERENCE UPDATED

NOTE UPDATED

R

Subtask 294096-930-201-001 SUBTASK SOLUTION UPDATED

NOTE UPDATED

R

Subtask 294096-730-201-001 SUBTASK SOLUTION UPDATED R

TASK 294096- 831-849-001-Modify the

Blue HP Hydraulic Manifold on Aircraft

TASK SOLUTION UPDATED

NOTE UPDATED

R

Subtask 294096-910-202-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

Subtask 294096-831-202-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

FIGURE REFERENCE UPDATED

NOTE UPDATED

R

Subtask 294096-730-202-001 SUBTASK SOLUTION UPDATED R

TASK 294096- 831-850-001-Modify the

Yellow HP Hydraulic Manifold on Aircraft

TASK SOLUTION UPDATED

NOTE UPDATED

R

Subtask 294096-910-203-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

Subtask 294096-831-203-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

FIGURE REFERENCE UPDATED

NOTE UPDATED

R

Subtask 294096-730-203-001 SUBTASK SOLUTION UPDATED R

TASK 294096- 831-851-001-Modify the

Green HP Hydraulic Manifold on Aircraft

TASK SOLUTION UPDATED

NOTE UPDATED

R

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REVISION No.: 02 - Apr 08/16 Page: 2

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@A340

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Subtask 294096-910-204-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

Subtask 294096-831-204-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

FIGURE REFERENCE UPDATED

NOTE UPDATED

R

Subtask 294096-730-204-001 SUBTASK SOLUTION UPDATED R

TASK 294096- 831-852-001-Modify the

Green HP Hydraulic Manifold on Bench

TASK SOLUTION UPDATED

NOTE UPDATED

R

Subtask 294096-910-205-002 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

Subtask 294096-831-205-002 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

FIGURE REFERENCE UPDATED

NOTE UPDATED

R

Subtask 294096-730-205-002 SUBTASK SOLUTION UPDATED R

TASK 294096- 831-853-001-Modify the

Blue HP Hydraulic Manifold on Aircraft

TASK SOLUTION UPDATED

NOTE UPDATED

R

Subtask 294096-910-206-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

Subtask 294096-831-206-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

FIGURE REFERENCE UPDATED

NOTE UPDATED

R

Subtask 294096-730-206-001 SUBTASK SOLUTION UPDATED R

TASK 294096- 831-854-001-Modify the

Blue HP Hydraulic Manifold on Bench

TASK SOLUTION UPDATED

NOTE UPDATED

R

Subtask 294096-910-207-002 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

Subtask 294096-831-207-002 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

FIGURE REFERENCE UPDATED

NOTE UPDATED

R

Subtask 294096-730-207-002 SUBTASK SOLUTION UPDATED R

TASK 294096- 831-855-001-Modify the

Yellow HP Hydraulic Manifold on Aircraft

TASK SOLUTION UPDATED

NOTE UPDATED

R

Subtask 294096-910-208-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

Subtask 294096-831-208-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

FIGURE REFERENCE UPDATED

NOTE UPDATED

R

Subtask 294096-730-208-001 SUBTASK SOLUTION UPDATED R

DATE: Aug 08/14 SERVICE BULLETIN No.: A340-29-4096

REVISION No.: 02 - Apr 08/16 Page: 3

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@A340

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

TASK 294096- 831-856-001-Modify the

Yellow HP Hydraulic Manifold on Bench

TASK SOLUTION UPDATED

NOTE UPDATED

R

Subtask 294096-910-209-002 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

Subtask 294096-831-209-002 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

FIGURE REFERENCE UPDATED

NOTE UPDATED

R

Subtask 294096-730-209-002 SUBTASK SOLUTION UPDATED R

Fig. A-GBAAA FIGURE SOLUTION UPDATED R

Fig. A-GBAAA Sheet 01 SHEET UPDATED R

Fig. A-GBAAA Sheet 02 SHEET UPDATED R

Fig. A-GBAAA Sheet 03 SHEET ADDED N

Fig. A-GBDAA FIGURE SOLUTION UPDATED R

Fig. A-GBDAA Sheet 03 SHEET UPDATED R

Fig. A-GBDAA Sheet 04 SHEET UPDATED R

Fig. A-GBDAA Sheet 05 SHEET ADDED N

Fig. A-GBBAA FIGURE SOLUTION UPDATED R

Fig. A-GBBAA Sheet 01 SHEET UPDATED R

Fig. A-GBBAA Sheet 02 SHEET UPDATED R

Fig. A-GBBAA Sheet 03 SHEET ADDED N

Fig. A-GBEAA FIGURE SOLUTION UPDATED R

Fig. A-GBEAA Sheet 03 SHEET UPDATED R

Fig. A-GBEAA Sheet 04 SHEET UPDATED R

Fig. A-GBEAA Sheet 05 SHEET ADDED N

Fig. A-GBCAA FIGURE SOLUTION UPDATED R

Fig. A-GBCAA Sheet 01 SHEET UPDATED R

Fig. A-GBCAA Sheet 02 SHEET UPDATED R

Fig. A-GBCAA Sheet 03 SHEET ADDED N

Fig. A-GBFAA FIGURE SOLUTION UPDATED R

Fig. A-GBFAA Sheet 03 SHEET UPDATED R

Fig. A-GBFAA Sheet 04 SHEET UPDATED R

Fig. A-GBFAA Sheet 05 SHEET ADDED N

FILLING INSTRUCTIONS

This Service Bulletin has been generated electronically and is reissued as a complete document.

Replace the complete document.

Put this Revision Transmittal Sheet in front of the Service Bulletin.

HISTORY OF PREVIOUS REVISIONS

Revision No.01 issued to:

DATE: Aug 08/14 SERVICE BULLETIN No.: A340-29-4096

REVISION No.: 02 - Apr 08/16 Page: 4

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@A340

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Update the effectivity.

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

Service Bulletin at original issue.

Update the illustrations.

REVISION SEQUENCE

ORIGINAL: Aug 08/14

REVISION No. : 01 - Jul 30/15

REVISION No. : 02 - Apr 08/16

DATE: Aug 08/14 SERVICE BULLETIN No.: A340-29-4096

REVISION No.: 02 - Apr 08/16 Page: 5

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@A340

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

This Page Intentionally Left Blank

DATE: Aug 08/14 SERVICE BULLETIN No.: A340-29-4096

REVISION No.: 02 - Apr 08/16 Page: 6

6

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@A340

SERVICE BULLETIN

SUMMARY

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

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

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 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 A340 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. A340-29-4091)

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

DATE: Aug 08/14 SERVICE BULLETIN No.: A340-29-4096

REVISION No.: 02 - Apr 08/16 Page: 1

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@A340

SERVICE BULLETIN

SUMMARY

Accomplishment of this Service Bulletin cancels the requirements of Service Bulletin No. A340-29-4086

and AOT 29L001-12.

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 LROPS 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) :

06Y 15R 31V 39N 41N 74W 83V 98W 98X AFR AIB ALD ALK

ARG BOE CAL CPA DGA DLH F2I FIN G8E GAF HFM HFY IBE

IRC IRM KAC LAN M3R MAU MDG MRJ O2X PAL PUE QAF ROI

S3R SAA SAS SFB SLM SVW SWR TAP THT THY UAE VCV

CONCURRENT REQUIREMENTS

None

REFERENCES / REPERCUSSIONS

TFU 29.10.00.034

DATE: Aug 08/14 SERVICE BULLETIN No.: A340-29-4096

REVISION No.: 02 - Apr 08/16 Page: 2

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@A340

SERVICE BULLETIN

SUMMARY

OEB None

AOT A29L001-12

SIL None

ISI 00.00.00135

00.00.00198

00.00.00207

LINE MAINTENANCE AFFECTED No

LIFE LIMIT None

OTHER None

NATURE OF THE WORK

AIRCRAFT YES

EQUIPMENT YES

HARD NO

SOFT NO

OBRM NO

MANPOWER

**CONF 001

Task 294096-831-848-001: Modify the Green HP Hydraulic Manifold on Aircraft

TOTAL MANHOURS 7.50

ELAPSED TIME (HOURS) 7.50

Task 294096-831-849-001: Modify the Blue HP Hydraulic Manifold on Aircraft

TOTAL MANHOURS 7.50

ELAPSED TIME (HOURS) 7.50

Task 294096-831-850-001: Modify the Yellow HP Hydraulic Manifold on Aircraft

TOTAL MANHOURS 7.50

ELAPSED TIME (HOURS) 7.50

Task 294096-831-851-001: Modify the Green HP Hydraulic Manifold on Aircraft

TOTAL MANHOURS 0.00

Task 294096-831-852-001: Modify the Green HP Hydraulic Manifold on Bench

TOTAL MANHOURS 0.00

Task 294096-831-853-001: Modify the Blue HP Hydraulic Manifold on Aircraft

TOTAL MANHOURS 0.00

Task 294096-831-854-001: Modify the Blue HP Hydraulic Manifold on Bench

TOTAL MANHOURS 0.00

Task 294096-831-855-001: Modify the Yellow HP Hydraulic Manifold on Aircraft

TOTAL MANHOURS 0.00

DATE: Aug 08/14 SERVICE BULLETIN No.: A340-29-4096

REVISION No.: 02 - Apr 08/16 Page: 3

6

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@A340

SERVICE BULLETIN

SUMMARY

Task 294096-831-856-001: Modify the Yellow HP Hydraulic Manifold on Bench

TOTAL MANHOURS 0.00

**CONF 002

Task 294096-831-848-001: Modify the Green HP Hydraulic Manifold on Aircraft

TOTAL MANHOURS 0.00

Task 294096-831-849-001: Modify the Blue HP Hydraulic Manifold on Aircraft

TOTAL MANHOURS 0.00

Task 294096-831-850-001: Modify the Yellow HP Hydraulic Manifold on Aircraft

TOTAL MANHOURS 0.00

Task 294096-831-851-001: Modify the Green HP Hydraulic Manifold on Aircraft

TOTAL MANHOURS 7.50

ELAPSED TIME (HOURS) 7.50

Task 294096-831-852-001: Modify the Green HP Hydraulic Manifold on Bench

TOTAL MANHOURS 10.50

ELAPSED TIME (HOURS) 10.50

Task 294096-831-853-001: Modify the Blue HP Hydraulic Manifold on Aircraft

TOTAL MANHOURS 7.50

ELAPSED TIME (HOURS) 7.50

Task 294096-831-854-001: Modify the Blue HP Hydraulic Manifold on Bench

TOTAL MANHOURS 10.50

ELAPSED TIME (HOURS) 10.50

Task 294096-831-855-001: Modify the Yellow HP Hydraulic Manifold on Aircraft

TOTAL MANHOURS 7.50

ELAPSED TIME (HOURS) 7.50

Task 294096-831-856-001: 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.: A340-29-4096

REVISION No.: 02 - Apr 08/16 Page: 4

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@A340

SERVICE BULLETIN

SUMMARY

**CONF ALL

B

FR53.2

FR53.1

5102JM

FR46

FR47

7103JM

6103JM

Z190

A

A

B

MANIFOLD

MANIFOLD

MANIFOLD

F_SB_294096_6_SAAA_01_00

Figure A-GSAAA - Sheet 01

DATE: Aug 08/14 SERVICE BULLETIN No.: A340-29-4096

REVISION No.: 02 - Apr 08/16 Page: 5

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SERVICE BULLETIN

SUMMARY

This Page Intentionally Left Blank

DATE: Aug 08/14 SERVICE BULLETIN No.: A340-29-4096

REVISION No.: 02 - Apr 08/16 Page: 6

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 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. A340-29-4078 has been

accomplished.

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

203796D50774 has been embodied or Service Bulletin No. A340-29-4095 has

been accomplished.

(1) Models

340-211 340-212 340-213 340-311 340-312 340-313

(2) Effectivity by MSN

0002 0004 0009 0014 0020 0022-0023 0025-0026 0029 0031 0038 0041 0043-0044

0046-0047 0049 0051 0056-0058 0061 0063 0074-0076 0078-0081 0084-0085

0089-0091 0093-0094 0101 0104 0114-0115 0117 0123 0125-0126 0128 0134-0137

0139 0142 0145-0147 0149-0152 0154 0156-0160 0163-0164 0166-0170 0174-0175

DATE: Aug 08/14 SERVICE BULLETIN No.: A340-29-4096

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@A340

SERVICE BULLETIN

0178-0180 0185-0187 0190 0192-0194 0196-0197 0199 0201-0202 0204 0207-0208

0210 0212-0215 0217-0218 0220-0221 0227-0228 0233 0236-0237 0242-0243

0245-0246 0252 0257 0260 0263-0264 0268 0270 0273-0274 0278 0280 0282 0292

0297 0302 0304 0307 0310 0318-0319 0321 0325 0327 0329 0331-0332 0335 0347

0352 0354-0355 0363 0367 0373-0374 0377-0379 0381 0385 0387 0390 0395 0399

0402 0406 0411 0413 0415 0424 0429-0430 0433-0435 0438 0446-0447 0450 0459

0467 0470 0474 0483 0528 0538 0541 0544-0546 0554 0556 0559 0561-0562 0582

0585 0590 0598 0643 0646 0651 0668 0793 0800 0835 0844 0921 0938 0955

(3) Effectivity by Operator

The Operator/MSN relationship is provided for information only and is correct at the time

of issue in accordance with the information available to AIRBUS. Any future changes

resulting from transfer of an aircraft from one operator to another will not be reflected in

this list unless the Service Bulletin is revised for another reason.

OPERATOR MSN

06Y 0139 0149

15R 0151

31V 0093 0381

39N 0168 0174

41N 0009

74W 0047 0051

83V 0280 0292

98W 0014 0022

98X 0429

AFR 0029 0078 0084 0186 0207 0237 0245 0246 0260 0307 0310 0377

0399

AIB 0192 0243 0264

ALD 0156 0159 0178

ALK 0374

ARG 0063 0074 0080 0085 0094 0123 0126 0128 0170 0193 0373

BOE 0554

CAL 0402 0406 0411 0415 0433 0541

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

DGA 0075 0081

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

0352 0354 0379 0390 0434 0447

F2I 0038 0043 0114 0214

FIN 0058 0835 0844 0921 0938

G8E 0187 0196

GAF 0274 0355

HFM 0117 0210 0367

HFY 0190 0202

IBE 0125 0134 0145 0146 0217 0221 0329 0483

IRC 0002

IRM 0020 0056 0164 0282

KAC 0089 0090 0101 0104

LAN 0363

DATE: Aug 08/14 SERVICE BULLETIN No.: A340-29-4096

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@A340

SERVICE BULLETIN

OPERATOR MSN

M3R 0061

MAU 0076 0152 0194 0268 0793 0800

MDG 0319

MRJ 0257

O2X 0273 0278

PAL 0302 0318 0332 0387 0459 0474

PUE 0212 0215

QAF 0026 0528

ROI 0199 0201

S3R 0004 0204

SAA 0197 0378 0544 0582 0590 0643 0646 0651

SAS 0167 0413 0424 0430 0435 0450 0467 0470

SFB 0046

SLM 0049 0242

SVW 0955

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

0562 0585 0598

TAP 0041 0044 0079 0091

THT 0385 0395 0438 0446 0668

THY 0023 0025 0057 0115 0180 0270 0331

UAE 0163 0166 0185 0236

VCV 0031

(4) Configuration by MSN

MSN CONFIGURATION

0002 0004 0009 0014 0020 0022 0023 0025 0029 0031 0038

0041 0043 0044 0047 0049 0051 0056 0057 0061 0063 0074

0075 0076 0078 0079 0080 0081 0084 0085 0089 0090 0091

0093 0094 0101 0104 0114 0115 0117 0123 0125 0128 0134

0135 0136 0137 0139 0142 0145 0146 0147 0149 0151 0152

0156 0157 0158 0159 0160 0163 0164 0166 0167 0170 0178

0180 0185 0186 0187 0192 0193 0194 0196 0197 0199 0201

0202 0204 0207 0208 0210 0212 0213 0214 0215 0217 0218

0220 0221 0227 0228 0233 0237 0242 0243 0245 0246 0252

0257 0260 0264 0268 0270 0273 0274 0278 0280 0282 0292

0297 0302 0304 0307 0310 0318 0319 0321 0325 0327 0329

0331 0332 0335 0347 0352 0354 0363 0367 0373 0374 0377

0378 0379 0381 0385 0387 0390 0395 0399 0402 0406 0411

0413 0415 0424 0429 0430 0433 0434 0435 0438 0446 0447

0450 0459 0467 0470 0474 0483 0528 0541 0544 0554 0582

0590 0643 0646 0651 0668 0793 0800

001 002

0026 0046 0058 0126 0150 0154 0168 0169 0174 0175 0179

0190 0236 0263 0355 0538 0545 0546 0556 0559 0561 0562

0585 0598 0835 0844 0921 0938 0955

002

DATE: Aug 08/14 SERVICE BULLETIN No.: A340-29-4096

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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 A340-29-4091.

**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. A340-29-4091 and may also have accomplished AOT 29L001-12.

(6) Material Effectivity

**CONF 001

MATERIAL QTY PER A/C SEE NOTES

Consumable CMLD01 As required

Component COMPD01 1

Equipment BFEZ01 1

**CONF 002

MATERIAL QTY PER A/C SEE NOTES

Consumable CMLD01 As required

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.: A340-29-4096

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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 A340 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. A340-29-4091) introduced a torque value of

400Nm for CV PN CAR401.

(3) Advantages

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

A340-29-4086 and AOT 29L001-12.

(4) Operational/Maintenance Consequences

None

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 294096-831-848-001: 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 294096-831-849-001: Modify the Blue HP Hydraulic Manifold on Aircraft

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

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

Task 294096-831-850-001: Modify the Yellow HP Hydraulic Manifold on Aircraft

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

DATE: Aug 08/14 SERVICE BULLETIN No.: A340-29-4096

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SERVICE BULLETIN

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

**CONF 002

Task 294096-831-851-001: 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 294096-831-852-001: 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 294096-831-853-001: 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 294096-831-854-001: 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 294096-831-855-001: 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 294096-831-856-001: 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)

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

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**CONF ALL

E. COMPLIANCE

(1) Classification

MANDATORY: Service Bulletin must be accomplished.

(2) Accomplishment Timescale

**CONF 001

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

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

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

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

accomplishment timescale.

Manifold to be modified Threshold Action

Green HP Hydraulic

Manifold

36 months from Issue of

this Service Bulletin

Do TASK 294096-831-848 001 Modify the

Green HP Hydraulic Manifold on Aircraft

Blue HP Hydraulic

Manifold

36 months from Issue of

this Service Bulletin

Do TASK 294096-831-849 001 Modify the Blue

HP Hydraulic Manifold on Aircraft

Yellow HP Hydraulic

Manifold

36 months from Issue of

this Service Bulletin

Do TASK 294096-831-850 001 Modify the

Yellow HP Hydraulic Manifold on Aircraft

**CONF 002

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

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

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

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

accomplishment timescale.

Manifold to be modified Threshold Action

Green HP Hydraulic

Manifold where CV have

been re-torqued in

accordance with AOT 29-

L001-12

36 months from Issue of

this Service Bulletin

Do TASK 294096-831-851 001 Modify the

Green HP Hydraulic Manifold on Aircraft

Green HP Hydraulic

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 294096-831-852 001 Modify the

Green HP Hydraulic Manifold on Bench

Blue HP Hydraulic

Manifold where CV have

been re-torqued in

accordance with AOT 29-

L001-12

36 months from Issue of

this Service Bulletin

Do TASK 294096-831-853 001 Modify the Blue

HP Hydraulic Manifold on Aircraft

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SERVICE BULLETIN

Manifold to be modified Threshold Action

Blue HP Hydraulic

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 294096-831-854 001 Modify the Blue

HP Hydraulic Manifold on Bench

Yellow HP Hydraulic

Manifold where CV have

been re-torqued in

accordance with AOT 29-

L001-12

36 months from Issue of

this Service Bulletin

Do TASK 294096-831-855 001 Modify the

Yellow HP Hydraulic Manifold on Aircraft

yellow HP Hydraulic

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 294096-831-856 001 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 294096-831-848-001: 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

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Task 294096-831-849-001: 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

Close-Up 1.00

TOTAL MANHOURS 7.50

ELAPSED TIME (HOURS) 7.50

Task 294096-831-850-001: 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 294096-831-851-001: Modify the Green HP Hydraulic Manifold on Aircraft

On Aircraft

TOTAL MANHOURS 0.00

Task 294096-831-852-001: Modify the Green HP Hydraulic Manifold on Bench

On Aircraft

On Bench

TOTAL MANHOURS 0.00

Task 294096-831-853-001: Modify the Blue HP Hydraulic Manifold on Aircraft

On Aircraft

TOTAL MANHOURS 0.00

Task 294096-831-854-001: Modify the Blue HP Hydraulic Manifold on Bench

On Aircraft

On Bench

TOTAL MANHOURS 0.00

Task 294096-831-855-001: Modify the Yellow HP Hydraulic Manifold on Aircraft

On Aircraft

TOTAL MANHOURS 0.00

Task 294096-831-856-001: Modify the Yellow HP Hydraulic Manifold on Bench

On Aircraft

On Bench

TOTAL MANHOURS 0.00

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SERVICE BULLETIN

**CONF 002

Task 294096-831-848-001: Modify the Green HP Hydraulic Manifold on Aircraft

On Aircraft

TOTAL MANHOURS 0.00

Task 294096-831-849-001: Modify the Blue HP Hydraulic Manifold on Aircraft

On Aircraft

TOTAL MANHOURS 0.00

Task 294096-831-850-001: Modify the Yellow HP Hydraulic Manifold on Aircraft

On Aircraft

TOTAL MANHOURS 0.00

Task 294096-831-851-001: 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 294096-831-852-001: 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 294096-831-853-001: 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

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SERVICE BULLETIN

Task 294096-831-853-001: Modify the Blue HP Hydraulic Manifold on Aircraft

ELAPSED TIME (HOURS) 7.50

Task 294096-831-854-001: Modify the Blue HP Hydraulic Manifold on Bench

Get Access 1.50

On Aircraft

Remove the Blue HP Manifold (FIN 6103JM) 1.00

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 294096-831-855-001: 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 294096-831-856-001: 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.

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SERVICE BULLETIN

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

A340-200 -1.752 -3.863 -59.177 -428.024

A340-300 -1.752 -3.863 -65.299 -472.3

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

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@A340

SERVICE BULLETIN

L. INTERCHANGEABILITY/MIXABILITY

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

accomplishment of this Service Bulletin.

**CONF 001

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

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

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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

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

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.

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SERVICE BULLETIN

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

management department.

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

E-mail: monitored.retrofit@airbus.com

For the accomplishment of this Service Bulletin before Jul 31/17, AIRBUS will credit the

manhours indicated in this Service Bulletin at the agreed in-house warranty labor rate for

claims received not later than 90 days after completion of the last affected aircraft of your

fleet.

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 consumables listed in 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

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

NOTES

14 NAS1612-10 3 PACKING

15 NAS1612-12 3 PACKING

21 NAS1612-4 1 PACKING

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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SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS

Task 294096-831-848-001 - 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

DATE: Aug 08/14 SERVICE BULLETIN No.: A340-29-4096

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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 294096-910-201-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

DATE: Aug 08/14 SERVICE BULLETIN No.: A340-29-4096

REVISION No.: 02 - Apr 08/16 Page: 20

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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 294096-839-201-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF 002

None

**CONF ALL

B. PREPARATION

**CONF 001

(1) Subtask 294096-941-201-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

DATE: Aug 08/14 SERVICE BULLETIN No.: A340-29-4096

REVISION No.: 02 - Apr 08/16 Page: 21

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@A340

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 002

None

**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 294096-831-201-001 - 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.: A340-29-4096

REVISION No.: 02 - Apr 08/16 Page: 22

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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 of 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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REVISION No.: 02 - Apr 08/16 Page: 23

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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.: A340-29-4096

REVISION No.: 02 - Apr 08/16 Page: 24

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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 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 294096-930-201-001 - 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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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-GBAAA

Removal and Installation of the CVs and

Re-identification of the Green Hydraulic

System HP Manifold

Sheet 01

Sheet 02

Sheet 03

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

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

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 .

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

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

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.

DATE: Aug 08/14 SERVICE BULLETIN No.: A340-29-4096

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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 002

None

**CONF ALL

D. TEST

**CONF 001

(1) Subtask 294096-730-201-001 - 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.

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.: A340-29-4096

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SERVICE BULLETIN

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.: A340-29-4096

REVISION No.: 02 - Apr 08/16 Page: 28

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SERVICE BULLETIN

**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 294096-942-201-001 - 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.: A340-29-4096

REVISION No.: 02 - Apr 08/16 Page: 29

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SERVICE BULLETIN

This Page Intentionally Left Blank

DATE: Aug 08/14 SERVICE BULLETIN No.: A340-29-4096

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SERVICE BULLETIN

Task 294096-831-849-001 - 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.: A340-29-4096

REVISION No.: 02 - Apr 08/16 Page: 31

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@A340

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

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 294096-910-202-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

DATE: Aug 08/14 SERVICE BULLETIN No.: A340-29-4096

REVISION No.: 02 - Apr 08/16 Page: 32

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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 294096-839-202-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF 002

None

**CONF ALL

B. PREPARATION

**CONF 001

(1) Subtask 294096-941-202-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

DATE: Aug 08/14 SERVICE BULLETIN No.: A340-29-4096

REVISION No.: 02 - Apr 08/16 Page: 33

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@A340

SERVICE BULLETIN

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 294096-831-202-001 - 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.: A340-29-4096

REVISION No.: 02 - Apr 08/16 Page: 34

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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 29-12-53-000-806

Fig. A-GBBAA

Removal and Installation of the CV 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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REVISION No.: 02 - Apr 08/16 Page: 35

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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-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).

DATE: Aug 08/14 SERVICE BULLETIN No.: A340-29-4096

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SERVICE BULLETIN

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 294096-930-202-001 - 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 CV and

Re-identification of the Blue Hydraulic

System HP Manifold

Sheet 01

Sheet 02

Sheet 03

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SERVICE BULLETIN

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

Specification (PMS) 01-06-12, Fig. A-GBBAA Sheet 01, Fig. A-GBBAA Sheet 02,

Views C (For information) and the table given in Appendix 01: PN Evolution of the

Green, Blue and Yellow System HP Hydraulic Manifolds .

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 .

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

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

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 294096-730-202-001 - 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

DATE: Aug 08/14 SERVICE BULLETIN No.: A340-29-4096

REVISION No.: 02 - Apr 08/16 Page: 38

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SERVICE BULLETIN

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 CV 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.

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 (5) 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

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SERVICE BULLETIN

(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

**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 294096-942-202-001 - Close-up

Work Zones and Access Panels

Zone Access/Work location

195

Manpower Resources

Skills NON SPECIFIC

References

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

(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.: A340-29-4096

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**CONF 002

None

DATE: Aug 08/14 SERVICE BULLETIN No.: A340-29-4096

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This Page Intentionally Left Blank

DATE: Aug 08/14 SERVICE BULLETIN No.: A340-29-4096

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SERVICE BULLETIN

Task 294096-831-850-001 - 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.: A340-29-4096

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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

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 294096-910-203-001 - 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 294096-839-203-001 - 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 002

None

**CONF ALL

B. PREPARATION

**CONF 001

(1) Subtask 294096-941-203-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

DATE: Aug 08/14 SERVICE BULLETIN No.: A340-29-4096

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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 294096-831-203-001 - 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.: A340-29-4096

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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 CV and

Re-identification the Yellow Hydraulic

System HP Manifold

Sheet 01

Sheet 02

Sheet 03

DATE: Aug 08/14 SERVICE BULLETIN No.: A340-29-4096

REVISION No.: 02 - Apr 08/16 Page: 47

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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.: A340-29-4096

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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-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 294096-930-203-001 - Reidentify the Yellow HP Manifold (FIN 7103JM)

Work Zones and Access Panels

Zone Access/Work location

196 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.: A340-29-4096

REVISION No.: 02 - Apr 08/16 Page: 49

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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 CV and

Re-identification the Yellow Hydraulic

System HP Manifold

Sheet 01

Sheet 02

Sheet 03

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

Specification (PMS) 01-06-12, Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet 02,

Views C and D (For information) and the given in Appendix 01: PN Evolution of the

Green, Blue and Yellow System HP Hydraulic Manifolds .

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 .

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

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

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.: A340-29-4096

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**CONF ALL

D. TEST

**CONF 001

(1) Subtask 294096-730-203-001 - Test the Yellow HP Manifold (FIN7103JM)

Work Zones and Access Panels

Zone Access/Work location

196 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.

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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.: A340-29-4096

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**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 294096-942-203-001 - Close-up

Work Zones and Access Panels

Zone Access/Work location

196

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.: A340-29-4096

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This Page Intentionally Left Blank

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Task 294096-831-851-001 - 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.: A340-29-4096

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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

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 294096-910-204-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

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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 294096-839-204-001 - 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 294096-941-204-001 - 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 ALL

C. PROCEDURE

**CONF 001

None

**CONF 002

(1) Subtask 294096-831-204-001 - 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.: A340-29-4096

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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 of 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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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

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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 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 294096-930-204-001 - 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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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

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

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

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

Yellow System HP Hydraulic Manifolds .

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

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

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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 294096-730-204-001 - Test of the Green Hydraulic System 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 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.

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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 294096-942-204-001 - Close-up

Work Zones and Access Panels

Zone Access/Work location

147

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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.: A340-29-4096

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This Page Intentionally Left Blank

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SERVICE BULLETIN

Task 294096-831-852-001 - 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.: A340-29-4096

REVISION No.: 02 - Apr 08/16 Page: 67

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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 294096-910-205-002 - Standard Practices

Work Zones and Access Panels

Zone Access/Work location

147

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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)

(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 294096-839-205-002 - 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

DATE: Aug 08/14 SERVICE BULLETIN No.: A340-29-4096

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**CONF 002

(1) Subtask 294096-941-205-002 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

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

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

DATE: Aug 08/14 SERVICE BULLETIN No.: A340-29-4096

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**CONF 002

(1) Subtask 294096-020-201-002 - 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

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

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 Union MS21902-16 Item (9) Retain

3 Packing NAS1612-16 Item (8) Discard

1 Union MS21902-8 Item (5) Retain

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1 Packing NAS1612-8 Item (4) Discard

(2) Subtask 294096-831-205-002 - 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

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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:

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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.

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4 As shown in Fig. A-GBDAA Sheet 03, View D and 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 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-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 294096-930-205-002 - Reidentify the Green HP Manifold (FIN 5102JM)

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

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

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 .

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

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

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3 Apply varnish to the new identification PN, use:

Varnish

Polyurethane-Low

Voc External

Structure

04SBA3 As required

(4) Subtask 294096-420-201-002 - 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.

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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 Union MS21902-16 Item (9) Retained at

removal

3 Packing NAS1612-16 Item 8

1 Union MS21902-8 Item (5) Retained at

removal

1 Packing NAS1612-8 Item 4

reconnect:

3 Pipe Item (25) Retained at

removal

1 Pipe Item (26) Retained at

removal

(c) Tighten the plug-in unions 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.

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

pipe 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 294096-730-205-002 - 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.

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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 294096-942-205-002 - 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.

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Task 294096-831-853-001 - 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

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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 294096-910-206-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

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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 294096-839-206-001 - 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 294096-941-206-001 - 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 ALL

C. PROCEDURE

**CONF 001

None

**CONF 002

(1) Subtask 294096-831-206-001 - 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

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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 CV and

Re-identification of the Blue Hydraulic

System HP Manifold

Sheet 01

Sheet 02

Sheet 03

DATE: Aug 08/14 SERVICE BULLETIN No.: A340-29-4096

REVISION No.: 02 - Apr 08/16 Page: 85

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SERVICE BULLETIN

(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

DATE: Aug 08/14 SERVICE BULLETIN No.: A340-29-4096

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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-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 294096-930-206-001 - 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.: A340-29-4096

REVISION No.: 02 - Apr 08/16 Page: 87

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SERVICE BULLETIN

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

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

Specification (PMS) 01-06-12,Fig. A-GBEAA Sheet 03, Fig. A-GBEAA Sheet 04,

Views E (For information) and the table given in Appendix 01: PN Evolution of the

Green, Blue and Yellow System HP Hydraulic Manifolds .

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 .

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

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

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

DATE: Aug 08/14 SERVICE BULLETIN No.: A340-29-4096

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SERVICE BULLETIN

**CONF 002

(1) Subtask 294096-730-206-001 - 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.

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 (5) 34.7-35.8

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

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

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SERVICE BULLETIN

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

(Nm)

(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 294096-942-206-001 - Close-up

Work Zones and Access Panels

Zone Access/Work location

190

Manpower Resources

Skills NON SPECIFIC

References

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

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

equipment.

DATE: Aug 08/14 SERVICE BULLETIN No.: A340-29-4096

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SERVICE BULLETIN

(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.: A340-29-4096

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SERVICE BULLETIN

This Page Intentionally Left Blank

DATE: Aug 08/14 SERVICE BULLETIN No.: A340-29-4096

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SERVICE BULLETIN

Task 294096-831-854-001 - 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.: A340-29-4096

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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 6013JM 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 294096-910-207-002 - 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.: A340-29-4096

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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 294096-839-207-002 - 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 294096-941-207-002 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

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

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)

- Engine shut down, thrust reversers are closed and locked

DATE: Aug 08/14 SERVICE BULLETIN No.: A340-29-4096

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SERVICE BULLETIN

- Aircraft in clean configuration

- Parking brake applied

- Aircraft electrical network de-energized

- Hydraulic systems depressurized

- Access to the cockpit and cabin is available

- All circuit breakers are in closed position

- All controls in NORM, AUTO or OFF position.

(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 294096-020-202-002 - 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

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

DATE: Aug 08/14 SERVICE BULLETIN No.: A340-29-4096

REVISION No.: 02 - Apr 08/16 Page: 96

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SERVICE BULLETIN

(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 Union MS21902-16 Item (9) Retain

1 Union MS21902D16 Item (12) Retain

2 Packing NAS1612-16 Item (8) Discard

1 Union MS21902-8 Item (5) Retain

1 Packing NAS1612-8 Item (4) Discard

2 Union MS21902-10 Item (13) Retain

2 Packing NAS1612-10 Item (14) Discard

2 Union MS21902-12 Item (16) Retain

2 Packing NAS1612-12 Item (15) Discard

DATE: Aug 08/14 SERVICE BULLETIN No.: A340-29-4096

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SERVICE BULLETIN

(2) Subtask 294096-831-207-002 - 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

References

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

Task 20-29-00-911-801

DATE: Aug 08/14 SERVICE BULLETIN No.: A340-29-4096

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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

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:

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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.: A340-29-4096

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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 294096-930-207-002 - 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.: A340-29-4096

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

Specification (PMS) 01-06-12, Fig. A-GBEAA Sheet 03, Fig. A-GBEAA Sheet 04,

Views E (For information) and the table given in Appendix 01: PN Evolution of the

Green, Blue and Yellow System HP Hydraulic Manifolds .

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 .

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

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

3 Apply varnish to the new identification PN, use:

Varnish

Polyurethane-Low

Voc External

Structure

04SBA3 As required

(4) Subtask 294096-420-202-002 - 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

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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) 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

4 Bolt NAS6604-32 Item (10) Retained at

removal

4 Washer ASNA2397-416L Item (6) Retained at

removal

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SERVICE BULLETIN

2 Packing NAS1612-16 Item 8

1 Union MS21902-16 Item (9) Retained at

removal

1 Union MS21902D16 Item (12) Retained at

removal

1 Packing NAS1612-8 Item 4

1 Union MS21902-8 Item (5) Retained at

removal

2 Packing NAS1612-10 Item 14

2 Union MS21902-10 Item (13) Retained at

removal

2 Packing NAS1612-12 Item 15

2 Union MS21902-12 Item (16) Retained at

removal

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

(b) 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.

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

pipe 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 (5) 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

(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.

**CONF ALL

D. TEST

**CONF 001

None

**CONF 002

(1) Subtask 294096-730-207-002 - 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

Fig. A-GDAAA

Torque Check of the Hydraulic Unions

on the Blue Hydraulic System HP

Manifold

Sheet 01

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(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 294096-942-207-002 - 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 6013JM, 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.: A340-29-4096

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Task 294096-831-855-001 - 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

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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 294096-910-208-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

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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 294096-839-208-001 - 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 ALL

B. PREPARATION

**CONF 001

None

**CONF 002

(1) Subtask 294096-941-208-001 - 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 29-13-53-000-804

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 294096-831-208-001 - 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.: A340-29-4096

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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 CV and

Re-identification the Yellow Hydraulic

System HP Manifold

Sheet 01

Sheet 02

Sheet 03

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(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 CVs 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

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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-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 294096-930-208-001 - 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

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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

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

Specification (PMS) 01-06-12, Fig. A-GBFAA Sheet 03, 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 .

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 .

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

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

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

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**CONF 002

(1) Subtask 294096-730-208-001 - 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.

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

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

(Nm)

(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 294096-942-208-001 - Close-up

Work Zones and Access Panels

Zone Access/Work location

190

Manpower Resources

Skills NON SPECIFIC

References

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

Task 29-13-53-400-804

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

equipment.

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(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.

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This Page Intentionally Left Blank

DATE: Aug 08/14 SERVICE BULLETIN No.: A340-29-4096

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SERVICE BULLETIN

Task 294096-831-856-001 - 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.: A340-29-4096

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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

190 196

Modified FIN

5316JM301 7013JM 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 294096-910-209-002 - 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 294096-839-209-002 - 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 294096-941-209-002 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

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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 294096-020-203-002 - 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.: A340-29-4096

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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 29-13-53-000-804

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 Union MS21902-16 Item (9) Retain

1 Union MS21902D16 Item (12) Retain

3 Packing NAS1612-16 Item (8) Discard

1 Union MS21902-10 Item (13) Retain

DATE: Aug 08/14 SERVICE BULLETIN No.: A340-29-4096

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SERVICE BULLETIN

1 Packing NAS1612-10 Item (14) Discard

1 Union MS21902-12 Item (16) Retain

1 Packing NAS1612-12 Item (15) Discard

1 Union MS21902-4 Item (22) Retain

1 Packing NAS1612-4 Item (21) Discard

(2) Subtask 294096-831-209-002 - 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.: A340-29-4096

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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

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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-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.: A340-29-4096

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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 294096-930-209-002 - 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.: A340-29-4096

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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

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

Specification (PMS) 01-06-12, Fig. A-GBFAA Sheet 03, 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 .

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 .

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

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

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.: A340-29-4096

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SERVICE BULLETIN

(4) Subtask 294096-420-203-002 - 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) 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

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SERVICE BULLETIN

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 Union MS21902-16 Item (9) Retained at

removal

1 Union MS21902D16 Item (12) Retained at

removal

1 Packing NAS1612-10 Item 14

1 Union MS21902-10 Item (13) Retained at

removal

1 Packing NAS1612-12 Item 15

1 Union MS21902-12 Item (16) Retained at

removal

1 Packing NAS1612-4 Item 21

1 Union MS21902-4 Item (22) Retained at

removal

reconnect:

1 Pipe Item (36) Retained at

removal

1 Pipe Item (37) Retained at

removal

1 Pipe Item (38) Retained at

removal

1 Pipe Item (39) Retained at

removal

1 Pipe Item (40) Retained at

removal

1 Pipe Item (41) Retained at

removal

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(b) 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 20-23-22-910-801and Table 3, below.

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

pipe 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

(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.

**CONF ALL

D. TEST

**CONF 001

None

**CONF 002

(1) Subtask 294096-730-209-002 - 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

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

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SERVICE BULLETIN

References

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 294096-942-209-002 - 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

(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 7013JM, refer to AMM Task 29-11-53-400-803.

DATE: Aug 08/14 SERVICE BULLETIN No.: A340-29-4096

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SERVICE BULLETIN

**CONF ALL

Z147

FR53.1

FR53.2

2

(3) 3

2

(3) 3

HP MANIFOLD

5102JM

5316JM102

5316JM101

A

B

B

A

(2)

(2)

01 MAKE SAFE WITH LOCKWIRE.

NOTE:

01

C

E

F_SB_294096_6_BAAA_01_04

Figure A-GBAAA - 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.: A340-29-4096

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SERVICE BULLETIN

**CONF ALL

VIEW LOOKING FWD

AREA OF RE−IDENTIFICATION

C

02 THE LOCATION OF OLD PN HP MANIFOLD IS GIVEN FOR INFORMATION

NOTE:

02

D

D

F_SB_294096_6_BAAA_02_05

Figure A-GBAAA - 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.: A340-29-4096

REVISION No.: 02 - Apr 08/16 Page: 134

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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

F_SB_294096_6_BAAA_03_00

Figure A-GBAAA - 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.: A340-29-4096

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SERVICE BULLETIN

**CONF 002

FR53.1

FR53.2

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

Z147

A

F_SB_294096_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.: A340-29-4096

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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

F_SB_294096_6_BDAA_02_01

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.: A340-29-4096

REVISION No.: 02 - Apr 08/16 Page: 137

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

**CONF 002

3

3

HP MANIFOLD

5102JM

5316JM102

5316JM101

2

2

01 MAKE SAFE WITH LOCKWIRE.

NOTE:

01

D

E

G

F_SB_294096_6_BDAA_03_03

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.: A340-29-4096

REVISION No.: 02 - Apr 08/16 Page: 138

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

**CONF 002

VIEW LOOKING FWD

E

F

F

AREA OF RE−IDENTIFICATION

02 THE LOCATION OF OLD PN HP MANIFOLD IS GIVEN FOR INFORMATION

NOTE:

02

F_SB_294096_6_BDAA_04_04

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.: A340-29-4096

REVISION No.: 02 - Apr 08/16 Page: 139

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

**CONF 002

03

NOTE:

2

BACK−UP RING 03

O−RING

G

04

04

BEFORE INSTALLATION, MAKE SURE THAT THE BACK−UP

RING IS FLUSH TO THE GROOVE AND THE LOWER O−RING

REMOVE STORAGE SEAL AND DISCARD, BEFORE INSTALLING

NEW PACKING SEAL, ITEM 2

F_SB_294096_6_BDAA_05_00

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.: A340-29-4096

REVISION No.: 02 - Apr 08/16 Page: 140

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

**CONF ALL

A

FR47

FR46

HP MANIFOLD

(3) 3

6103JM

5316JM201

A

B

Z195

(2) 2

01 MAKE SAFE WITH LOCKWIRE.

NOTE:

01

C

B

D

F_SB_294096_6_BBAA_01_05

Figure A-GBBAA - Sheet 01

Removal and Installation of the CV and Re-identification of the Blue Hydraulic System HP Manifold

DATE: Aug 08/14 SERVICE BULLETIN No.: A340-29-4096

REVISION No.: 02 - Apr 08/16 Page: 141

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

**CONF ALL

AREA OF RE−IDENTIFICATION

02 THE LOCATION OF OLD PN HP MANIFOLD IS GIVEN FOR INFORMATION

NOTE:

02

C

F_SB_294096_6_BBAA_02_05

Figure A-GBBAA - Sheet 02

Removal and Installation of the CV and Re-identification of the Blue Hydraulic System HP Manifold

DATE: Aug 08/14 SERVICE BULLETIN No.: A340-29-4096

REVISION No.: 02 - Apr 08/16 Page: 142

6

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@A340

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

F_SB_294096_6_BBAA_03_00

Figure A-GBBAA - Sheet 03

Removal and Installation of the CV and Re-identification of the Blue Hydraulic System HP Manifold

DATE: Aug 08/14 SERVICE BULLETIN No.: A340-29-4096

REVISION No.: 02 - Apr 08/16 Page: 143

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

**CONF 002

FR47

FR46

6103JM

A

B

(20)

(10)

(6)

(12)

(8)8

(5) (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

A

Z195

F_SB_294096_6_BEAA_01_01

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.: A340-29-4096

REVISION No.: 02 - Apr 08/16 Page: 144

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

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

F_SB_294096_6_BEAA_02_01

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.: A340-29-4096

REVISION No.: 02 - Apr 08/16 Page: 145

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

**CONF 002

HP MANIFOLD

3

6103JM

5316JM201 2

01 MAKE SAFE WITH LOCKWIRE

NOTE:

01

D

E

F

F_SB_294096_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.: A340-29-4096

REVISION No.: 02 - Apr 08/16 Page: 146

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

**CONF 002

E

AREA OF RE−IDENTIFICATION

02 THE LOCATION OF OLD PN HP MANIFOLD IS GIVEN FOR INFORMATION

NOTE:

02

F_SB_294096_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.: A340-29-4096

REVISION No.: 02 - Apr 08/16 Page: 147

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

**CONF 002

03

NOTE:

2

BACK−UP RING 03

O−RING

04

04

F

BEFORE INSTALLATION, MAKE SURE THAT THE BACK−UP

RING IS FLUSH TO THE GROOVE AND THE LOWER O−RING

REMOVE STORAGE SEAL AND DISCARD, BEFORE INSTALLING

NEW PACKING SEAL, ITEM 2

F_SB_294096_6_BEAA_05_00

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.: A340-29-4096

REVISION No.: 02 - Apr 08/16 Page: 148

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

**CONF ALL

FR47

FR46

(3) 3

7103JM

HP MANIFOLD

5316JM301

A

B

A

Z196

(2) 2

01 MAKE SAFE WITH LOCKWIRE.

NOTE:

01

C

B

E

F_SB_294096_6_BCAA_01_04

Figure A-GBCAA - Sheet 01

Removal and Installation of the CV and Re-identification the Yellow Hydraulic System HP Manifold

DATE: Aug 08/14 SERVICE BULLETIN No.: A340-29-4096

REVISION No.: 02 - Apr 08/16 Page: 149

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

**CONF ALL

VIEW LOOKING FWD

C

AREA OF RE−IDENTIFICATION

02 THE LOCATION OF OLD PN HP MANIFOLD IS GIVEN FOR INFORMATION

NOTE:

02

D

D

F_SB_294096_6_BCAA_02_04

Figure A-GBCAA - Sheet 02

Removal and Installation of the CV and Re-identification the Yellow Hydraulic System HP Manifold

DATE: Aug 08/14 SERVICE BULLETIN No.: A340-29-4096

REVISION No.: 02 - Apr 08/16 Page: 150

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

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 

E

2

F_SB_294096_6_BCAA_03_00

Figure A-GBCAA - Sheet 03

Removal and Installation of the CV and Re-identification the Yellow Hydraulic System HP Manifold

DATE: Aug 08/14 SERVICE BULLETIN No.: A340-29-4096

REVISION No.: 02 - Apr 08/16 Page: 151

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

**CONF 002

FR47

FR46

7103JM

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

A

Z196

F_SB_294096_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.: A340-29-4096

REVISION No.: 02 - Apr 08/16 Page: 152

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

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

F_SB_294096_6_BFAA_02_01

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.: A340-29-4096

REVISION No.: 02 - Apr 08/16 Page: 153

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

**CONF 002

3

7103JM

HP MANIFOLD

5316JM301

2

01 MAKE SAFE WITH LOCKWIRE

NOTE:

01

D

E

G

F_SB_294096_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.: A340-29-4096

REVISION No.: 02 - Apr 08/16 Page: 154

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

**CONF 002

VIEW LOOKING FWD

E

F

F

AREA OF RE−IDENTIFICATION

02 THE LOCATION OF OLD PN HP MANIFOLD IS GIVEN FOR INFORMATION

NOTE:

02

F_SB_294096_6_BFAA_04_03

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.: A340-29-4096

REVISION No.: 02 - Apr 08/16 Page: 155

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

**CONF 002

03

NOTE:

2

BACK−UP RING 03

O−RING

G

04

04

BEFORE INSTALLATION, MAKE SURE THAT THE BACK−UP

RING IS FLUSH TO THE GROOVE AND THE LOWER O−RING

REMOVE STORAGE SEAL AND DISCARD, BEFORE INSTALLING

NEW PACKING SEAL, ITEM 2

F_SB_294096_6_BFAA_05_00

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.: A340-29-4096

REVISION No.: 02 - Apr 08/16 Page: 156

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

**CONF ALL

FR53.1

FR53.2

A

B

B

(1)

(5)

(9)

(9)

(9)

5102JM

(26)

(25)

(25)

(25)

01 PIPES AND UNIONS SHOWN EXPLODED FOR CLARITY.

NOTE:

01

Z147

A

F_SB_294096_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.: A340-29-4096

REVISION No.: 02 - Apr 08/16 Page: 157

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

**CONF ALL

FR47

FR46

6103JM

A

B

B

(20)

(12)

(5)

(13) (16)

(13)

(9) (16)

(31)

(32) (33) (34)

(35)

(29)

(30)

01 PIPES AND UNIONS SHOWN EXPLODED FOR CLARITY.

NOTE:

01

A

Z195

F_SB_294096_6_DAAA_01_01

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.: A340-29-4096

REVISION No.: 02 - Apr 08/16 Page: 158

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

**CONF ALL

FR47

FR46

7103JM

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:

A

Z196

F_SB_294096_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.: A340-29-4096

REVISION No.: 02 - Apr 08/16 Page: 159

6

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@A340

SERVICE BULLETIN

This Page Intentionally Left Blank

DATE: Aug 08/14 SERVICE BULLETIN No.: A340-29-4096

REVISION No.: 02 - Apr 08/16 Page: 160

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

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 F_SB_294096_6_ABAA_01_02

Figure A-GABAA - Sheet 01

PN Evolution Table for the Green, Blue and Yellow System HP Hydraulic Manifolds

DATE: Aug 08/14 SERVICE BULLETIN No.: A340-29-4096

REVISION No.: 02 - Apr 08/16 Page: 1

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

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.: A340-29-4096

REVISION No.: 02 - Apr 08/16 Page: 2

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

Appendix 02: Local Manufacture of Tooling

**CONF 002

F_SB_294096_6_ACAA_01_00

Figure A-GACAA - Sheet 01

Local Manufacture of Tooling

DATE: Aug 08/14 SERVICE BULLETIN No.: A340-29-4096

REVISION No.: 02 - Apr 08/16 Page: 1

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

Appendix 02: Local Manufacture of Tooling

**CONF 002

F_SB_294096_6_ACAA_02_00

Figure A-GACAA - Sheet 02

Local Manufacture of Tooling

DATE: Aug 08/14 SERVICE BULLETIN No.: A340-29-4096

REVISION No.: 02 - Apr 08/16 Page: 2

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

Appendix 02: Local Manufacture of Tooling

**CONF 002

F_SB_294096_6_ACAA_03_00

Figure A-GACAA - Sheet 03

Local Manufacture of Tooling

DATE: Aug 08/14 SERVICE BULLETIN No.: A340-29-4096

REVISION No.: 02 - Apr 08/16 Page: 3

6

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@A340

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.: A340-29-4096

REVISION No.: 02 - Apr 08/16 Page: 1

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@A340

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.: A340-29-4096

REVISION No.: 02 - Apr 08/16 Page: 1

6

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