@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 - GREEN AUXILIARY HYDRAULIC POWER (RAM

AIR TURBINE) - INTRODUCE NEW SHIMMING PROCEDURE OF RAT

DEPLOY SOLENOIDS

**CONF ALL

MODIFICATIONS

MODIFICATION CLASSIFICATION

MAJOR 204067D50787

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

An A330 operator experienced that a Ram Air Turbine (RAT) did not deploy when tested. An

investigation, conducted by HAMILTON SUNDSTRAND and ARKWIN INDUSTRIES, has found that the

RAT did not deploy because there was not sufficient stroke inside one of the actuator deploy solenoids

due to insufficient shimming. The actuators will be modified by HAMILTON SUNDSTRAND to make

sure they are correctly shimmed with the correct stroke length.

This Service Bulletin is published to advise all operators of A340 aircraft of the issue of HAMILTON

SUNDSTRAND Service Bulletin No. ERPS06M-29-21.

HAMILTON SUNDSTRAND Service Bulletin No. ERPS06M-29-21 describes the procedure to identify

the part number of the RAT actuator and modify the shimming procedure of the RAT actuator.

The accomplishment of this Service Bulletin will contribute to ensure the correct function of the RAT.

GENERAL EVALUATION

EVALUATION TABLE

COMPLIANCE MANDATORY (1) CANCELS INSPECTION SB NO

POTENTIAL AD YES A/C OPERATION AFFECTED NO

DATE: Jun 12/14 SERVICE BULLETIN No.: A340-29-4097

REVISION No.: 00 - Jun 12/14 Page: 1

6

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

SERVICE BULLETIN

SUMMARY

EVALUATION TABLE

RELIABILITY AFFECTED YES PAX COMFORT AFFECTED NO

COST SAVING NO LROPS AFFECTED NO

STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED YES

NOTE (1): Service Bulletin must be accomplished.

MATERIAL PRICE INFORMATION

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Equipment BFEZ01 1 See SB Actuator

EFFECTIVITY

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

06Y 15R 15T 31V 36V 38W 58X 74W 98X ABD AFR AIB ALK

ARG BOE CAL CCA CPA DGA DLH FIN G8E GAF HFY I2L IBE

IRC IRM KAC LAN M3R MAU MDG MSR NMB OAL PAL PUE QAF

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

VIR XAX

CONCURRENT REQUIREMENTS

Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishment of the

following Service Bulletins as per effectivity specified in these Service Bulletins:

Service Bulletin No. A340-29-4093

NOTE: A340-29-4093 HYDRAULIC POWER - GREEN AUXILIARY HYDRAULIC POWER

(RAM AIR TURBINE) - RAT PUMP HEX SHAFT MODIFICATION - applies Modification

No. 202537D50553.

REFERENCES / REPERCUSSIONS

TFU None

OEB None

AOT None

SIL None

LINE MAINTENANCE AFFECTED No

LIFE LIMIT None

OTHER None

NATURE OF THE WORK

AIRCRAFT NO

EQUIPMENT YES

HARD NO

SOFT NO

OBRM NO

DATE: Jun 12/14 SERVICE BULLETIN No.: A340-29-4097

REVISION No.: 00 - Jun 12/14 Page: 2

6

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

SERVICE BULLETIN

SUMMARY

MANPOWER

Task 294097-831-848-001: MODIFICATION

TOTAL MANHOURS 14.00

ELAPSED TIME (HOURS) 14.00

APPENDICES

None

DATE: Jun 12/14 SERVICE BULLETIN No.: A340-29-4097

REVISION No.: 00 - Jun 12/14 Page: 3

6

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

SERVICE BULLETIN

SUMMARY

**CONF ALL

Z633

A

A

ACTUATOR

11JR

RAM AIR TURBINE (RAT)

F_SB_294097_6_SAAA_01_01

Figure A-GSAAA - Sheet 01

DATE: Jun 12/14 SERVICE BULLETIN No.: A340-29-4097

REVISION No.: 00 - Jun 12/14 Page: 4

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 - GREEN AUXILIARY HYDRAULIC POWER (RAM

AIR TURBINE) - INTRODUCE NEW SHIMMING PROCEDURE OF RAT

DEPLOY SOLENOIDS

MODIFICATION No.: 204067D50787

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

(1) Models

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

(2) Effectivity by MSN

0002 0004 0006 0009 0014 0020 0022-0026 0029 0031-0035 0038 0041 0043-0044

0046-0049 0051-0053 0056-0058 0061 0063 0074-0076 0078-0081 0084-0085

0088-0091 0093-0094 0101 0104 0114-0115 0117 0123 0125-0126 0128 0131

0134-0137 0139 0141-0142 0145-0147 0149-0152 0154 0156-0161 0163-0164

0166-0170 0173-0176 0178-0180 0182 0185-0187 0190 0192-0194 0196-0197 0199

0201-0202 0204 0207-0208 0210 0212-0218 0220-0221 0225 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 0359 0363 0367 0373-0374 0377-0379 0381

0385 0387 0390 0395 0399 0402 0406 0411 0413-0415 0424 0429-0430 0433-0435

0438 0442 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

DATE: Jun 12/14 SERVICE BULLETIN No.: A340-29-4097

REVISION No.: 00 - Jun 12/14 Page: 1

6

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

SERVICE BULLETIN

(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

15T 0009

31V 0048 0088 0257

36V 0024 0052

38W 0282

58X 0004

74W 0047

98X 0429

ABD 0210

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

0399

AIB 0131 0141 0161 0182

ALK 0032 0033 0034 0367 0374 0381

ARG 0063 0074 0080 0085 0093 0094 0123 0126 0128 0170 0193 0373

BOE 0554

CAL 0402 0406 0411 0415 0433 0541

CCA 0192 0199 0201 0242 0243 0264

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

DGA 0075 0081

DLH 0035 0053 0135 0158 0213 0233 0252 0297 0304 0321 0325 0327

0335 0347 0352 0354 0379 0390 0434 0447

FIN 0058 0168 0174 0835 0844 0921 0938

G8E 0414

GAF 0274 0355

HFY 0117 0190 0202

I2L 0216

IBE 0125 0134 0145 0146 0217 0221 0329 0474 0483

IRC 0002

IRM 0020 0056

KAC 0089 0090 0101 0104

LAN 0359 0363 0442

M3R 0061

MAU 0076 0152 0194 0268 0793 0800

MDG 0319

MSR 0156 0159 0178

NMB 0051

OAL 0280 0292

PAL 0173 0176 0187 0196 0302 0318 0332 0387 0459

PUE 0212 0215

DATE: Jun 12/14 SERVICE BULLETIN No.: A340-29-4097

REVISION No.: 00 - Jun 12/14 Page: 2

6

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

SERVICE BULLETIN

OPERATOR MSN

QAF 0026 0528

RJA 0014 0022 0038 0043

S3R 0204

SAA 0006 0197 0378 0544 0582 0590 0643 0646 0651

SAS 0167 0413 0424 0430 0435 0450 0467 0470

SFB 0046

SLM 0049

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

VIR 0114 0164 0214 0225

XAX 0273 0278

(4) Configuration by MSN

MSN CONFIGURATION

0002 0004 0006 0009 0014 0020 0022 0023 0024 0025 0026

0029 0031 0032 0033 0034 0035 0038 0041 0043 0044 0046

0047 0048 0049 0051 0052 0053 0056 0057 0058 0061 0063

0074 0075 0076 0078 0079 0080 0081 0084 0085 0088 0089

0090 0091 0093 0094 0101 0104 0114 0115 0117 0123 0125

0126 0128 0131 0134 0135 0136 0137 0139 0141 0142 0145

0146 0147 0149 0150 0151 0152 0154 0156 0157 0158 0159

0160 0161 0163 0164 0166 0167 0168 0169 0170 0173 0174

0175 0176 0178 0179 0180 0182 0185 0186 0187 0190 0192

0193 0194 0196 0197 0199 0201 0202 0204 0207 0208 0210

0212 0213 0214 0215 0216 0217 0218 0220 0221 0225 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 0359 0363 0367 0373 0374

0377 0378 0379 0381 0385 0387 0390 0395 0399 0402 0406

0411 0413 0414 0415 0424 0429 0430 0433 0434 0435 0438

0442 0446 0447 0450 0459 0467 0470 0474 0483 0528 0538

0541 0544 0545 0546 0554 0556 0559 0561 0562 0582 0585

0590 0598 0643 0646 0651 0668 0793 0800 0835 0844 0921

0938 0955

001

(5) Configuration definition

**CONF 001

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

standard configuration.

DATE: Jun 12/14 SERVICE BULLETIN No.: A340-29-4097

REVISION No.: 00 - Jun 12/14 Page: 3

6

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

SERVICE BULLETIN

(6) Material Effectivity

MATERIAL QTY PER A/C SEE NOTES

Equipment BFEZ01 1

Reidentified part set REIDD01 1

Consumable CMLD01 As required

B. CONCURRENT REQUIREMENTS

Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishment of

the following Service Bulletins as per effectivity specified in these Service Bulletins:

Service Bulletin No. A340-29-4093

NOTE: A340-29-4093 HYDRAULIC POWER - GREEN AUXILIARY HYDRAULIC

POWER (RAM AIR TURBINE) - RAT PUMP HEX SHAFT MODIFICATION -

applies Modification No. 202537D50553.

C. REASON

(1) History

An A330 operator experienced that a Ram Air Turbine (RAT) did not deploy when

tested. An investigation, conducted by HAMILTON SUNDSTRAND and ARKWIN

INDUSTRIES, has found that the RAT did not deploy because there was not sufficient

stroke inside one of the actuator deploy solenoids due to insufficient shimming. The

actuators will be modified by HAMILTON SUNDSTRAND to make sure they are correctly

shimmed with the correct stroke length.

(2) Objective/Action

This Service Bulletin is published to advise all operators of A340 aircraft of the issue of

HAMILTON SUNDSTRAND Service Bulletin No. ERPS06M-29-21.

HAMILTON SUNDSTRAND Service Bulletin No. ERPS06M-29-21 describes the

procedure to identify the part number of the RAT actuator and modify the shimming

procedure of the RAT actuator.

(3) Advantages

The accomplishment of this Service Bulletin will contribute to ensure the correct function

of the RAT.

(4) Operational/Maintenance Consequences

None

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

DATE: Jun 12/14 SERVICE BULLETIN No.: A340-29-4097

REVISION No.: 00 - Jun 12/14 Page: 4

6

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

SERVICE BULLETIN

Task 294097-831-848-001: MODIFICATION

(1) Identify the Part and Serial Number of the RAT Actuator

(2) Modify the RAT Actuator

E. COMPLIANCE

(1) Classification

MANDATORY: Service Bulletin must be accomplished.

(2) Accomplishment Timescale

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 of 36

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

accomplishment timescale.

F. APPROVAL

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

Organisation Approval No. EASA.21J.031.

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

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

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

before incorporation of the Service Bulletin.

G. MANPOWER

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

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

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

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

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

included.

Task 294097-831-848-001: MODIFICATION

Get Access 1.00

On Aircraft

Identify the Part and Serial Number of the RAT

Actuator

1.00

Modify the RAT Actuator 9.00

Tests 2.00

Close-Up 1.00

TOTAL MANHOURS 14.00

ELAPSED TIME (HOURS) 14.00

DATE: Jun 12/14 SERVICE BULLETIN No.: A340-29-4097

REVISION No.: 00 - Jun 12/14 Page: 5

6

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

SERVICE BULLETIN

H. WEIGHT AND BALANCE

Not Changed

I. ELECTRICAL LOAD DATA

Not Changed

J. REFERENCES

Aircraft Maintenance Manual (AMM) 06-20-00 12-34-34 20-16-00

29-24-00 29-24-56

Consumable Material List (CML)

ATA Common Support Data Dictionary (CSDD),

Chapter 2

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

Vendor Service Bulletin (VSB) HAMILTON SUNDSTRAND

ERPS06M-29-21

K. PUBLICATION AFFECTED

Aircraft Maintenance Manual (AMM) 29-24-56

Illustrated Parts Catalog (IPC) 29-24-05 29-24-52 29-24-56

L. INTERCHANGEABILITY/MIXABILITY

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE

NOTES

Actuator 5915768 5917109-1 01 Not

Applicable

Actuator 5912958 5917109-2 01 Not

Applicable

Actuator 5915768 5917109-2 01 Not

Applicable

Ram Air Turbine 1702934D 1702934E 01 Not

Applicable

Ram Air Turbine 1702934C 1702934E 01 Not

Applicable

Ram Air Turbine 766351A 766351B 01 Not

Applicable

Ram Air Turbine 768084A 768084B 01 Not

Applicable

Ram Air Turbine 770379A 770379B 01 Not

Applicable

Ram Air Turbine 770952C 770952F 01 Not

Applicable

Ram Air Turbine 770952D 770952F 01 Not

Applicable

Ram Air Turbine 770952E 770952F 01 Not

Applicable

DATE: Jun 12/14 SERVICE BULLETIN No.: A340-29-4097

REVISION No.: 00 - Jun 12/14 Page: 6

6

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

SERVICE BULLETIN

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

Common Support Data Dictionary (CSDD), Chapter 2.

M. SPARES

Ram Air Turbine 1702934C

Ram Air Turbine 1702934D

Actuator 5912958

Actuator 5915768

Ram Air Turbine 766351A

Ram Air Turbine 768084A

Ram Air Turbine 770379A

Ram Air Turbine 770952C

Ram Air Turbine 770952D

Ram Air Turbine 770952E

DATE: Jun 12/14 SERVICE BULLETIN No.: A340-29-4097

REVISION No.: 00 - Jun 12/14 Page: 7

6

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

SERVICE BULLETIN

This Page Intentionally Left Blank

DATE: Jun 12/14 SERVICE BULLETIN No.: A340-29-4097

REVISION No.: 00 - Jun 12/14 Page: 8

6

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

SERVICE BULLETIN

2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

(1) Procurement Addresses

Modification of removed equipment should be negotiated directly with HAMILTON

SUNDSTRAND as per instructions given in Vendor Service Bulletin No.

ERPS06M-29-21.

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

(2) Price and Availability

No AIRBUS kit will be provided.

Refer to the Vendor Service Bulletin No. ERPS06M-29-21 for the equipment modification

sales terms.

B. INDUSTRY SUPPORT INFORMATION

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

Tel : (33) 5 67 19 06 22

Fax : (33) 5 61 93 27 45

Refer to the HAMILTON SUNDSTRAND Vendor Service Bulletin No. ERPS06M-29-21 for the

industry support terms.

C. LIST OF COMPONENTS

No Kit

D. LIST OF MATERIALS - OPERATOR SUPPLIED

(1) Consumable Materials

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO CML

MAT. No.

QTY PER A/C SEE

NOTES

Clear Polyurethane Coating 04MDA3 As required

Non Aqueous Cleaner 08BAA9 As required

DATE: Jun 12/14 SERVICE BULLETIN No.: A340-29-4097

REVISION No.: 00 - Jun 12/14 Page: 9

6

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

SERVICE BULLETIN

ITEM DESCRIPTION REFERENCE TO CML

MAT. No.

QTY PER A/C SEE

NOTES

Textile-Lint Free Cotton 14SBA1 As required

(2) Components

None

(3) Equipment

Equipment BFEZ01

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

NOTES

1 5917109-1 1 ACTUATOR (1) 5915768 01 (1)

1 5917109-2 1 ACTUATOR (1) 5912958 01 (1)

(1) 5915768 01

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

Common Support Data Dictionary (CSDD), Chapter 2.

NOTE (1): 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

Parts are re-identified in accordance with the HAMILTON SUNDSTRAND Service Bulletin No.

ERPS06M-29-21.

Reidentified part set REIDD01

ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE

NOTES

1702934E RAT 1702934C

1702934D

766351B RAT 766351A

768084B RAT 768084A

770379B RAT 770379A

770952F RAT 770952C

770952D

770952E

F. TOOLING

None

DATE: Jun 12/14 SERVICE BULLETIN No.: A340-29-4097

REVISION No.: 00 - Jun 12/14 Page: 10

6

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

SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS

Task 294097-831-848-001 - MODIFICATION

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

INCLUDED IN THE REFERENCED PROCEDURES

WARNING: OBEY THE HYDRAULIC SAFETY PROCEDURES. WORK ON THE HYDRAULIC

SYSTEMS CAN BE DANGEROUS.

WARNING: MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS

ARE CLEAR. MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO

PERSONS AND/OR DAMAGE.

WARNING: MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE

IN POSITION BEFORE YOU START A TASK ON OR NEAR:

- THE FLIGHT CONTROLS

- THE FLIGHT CONTROL SURFACES

- THE LANDING GEAR AND THE RELATED DOORS

- COMPONENTS THAT MOVE.

MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS.

WARNING: SUPPORT THE UNIT/ASSEMBLY CAREFULLY TO PREVENT INJURY TO

PERSONS AND DAMAGE. THE UNIT/ASSEMBLY IS HEAVY.

CAUTION: DO NOT LIFT THE RAT BY THE TURBINE BLADES. YOU CAN CAUSE

DAMAGE TO THE TURBINE BLADES IF YOU USE THEM TO LIFT THE RAT.

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 ELECTRICAL 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

DATE: Jun 12/14 SERVICE BULLETIN No.: A340-29-4097

REVISION No.: 00 - Jun 12/14 Page: 11

6

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

SERVICE BULLETIN

’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.

Task Associated Data

Zone

633

Manpower

TOTAL MANHOURS 14.00

ELAPSED TIME (HOURS) 14.00

A. GENERAL

(1) Subtask 294097-910-201-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

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

Task 20-16-00-912-801

Consumable Material List (CML)

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

the Consumable Materials List (CML).

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

(c) For circuit breaker safety precautions, refer to AMM Task 20-16-00-912-801.

(d) Put blanking caps on the disconnected electrical connectors and hydraulic

connections.

DATE: Jun 12/14 SERVICE BULLETIN No.: A340-29-4097

REVISION No.: 00 - Jun 12/14 Page: 12

6

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

SERVICE BULLETIN

(2) Subtask 294097-839-201-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

B. PREPARATION

(1) Subtask 294097-941-201-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

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

Task 29-24-00-869-801

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 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

12-34-34-860-802.

(b) Extend the RAT, refer to AMM Task 29-24-00-869-801.

(c) Open, safety/lock and tag this (these) circuit breaker(s):

PANEL DESIGNATION FIN LOCATION SEE

NOTES

721VU HSMU B + PART G 6JG U10

722VU HSMU Y + PART G 7JG X46

742VU RAT STOW CTL 1JR D77

DATE: Jun 12/14 SERVICE BULLETIN No.: A340-29-4097

REVISION No.: 00 - Jun 12/14 Page: 13

6

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

SERVICE BULLETIN

PANEL DESIGNATION FIN LOCATION SEE

NOTES

742VU HYD RAT EXT SOL 2 5JR D76

742VU RAT MAN ON 2JR K74

(d) Put the warning notices on panel 114VU to tell persons not to operate the flap/slat

controls.

(e) Put the warning notices in position on the Yellow ground service-panel to tell

persons not to retract the RAT.

(f) Put an access platform in position below the flap track fairing No. 4, RH.

C. PROCEDURE

(1) Subtask 294097-831-201-001 - Identify the Part and Serial Number of the RAT

Actuator

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills AIRFRAME

Material necessary to do the job

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Clear Polyurethane Coating 04MDA3 As required

Non Aqueous Cleaner 08BAA9 As required

Textile-Lint Free Cotton 14SBA1 As required

References

Vendor Service Bulletin (VSB) HAMILTON SUNDSTRAND

ERPS06M-29-21

Fig. A-GBAAA

Removal / Installation of the RAT

Actuator

Sheet 01

Fig. A-GCAAA

Identification of the RAT Actuator

Sheet 01

Sheet 02

(a) Identify the RAT actuator in accordance with HAMILTON SUNDSTRAND Service

Bulletin No. ERPS06M-29-21.

Refer to Fig. A-GCAAA Sheet 01 and Fig. A-GCAAA Sheet 02.

DATE: Jun 12/14 SERVICE BULLETIN No.: A340-29-4097

REVISION No.: 00 - Jun 12/14 Page: 14

6

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

SERVICE BULLETIN

1 If the installed actuator is from the supplier ARKWIN, as shown on Fig. AGCAAA Sheet 02:

a Identify the part number and the serial number of the installed actuator

in accordance with HAMILTON SUNDSTRAND Service Bulletin No.

ERPS06M-29-21.

<1> If the installed actuator has the part number / serial number as

affected in the HAMILTON SUNDSTRAND Service Bulletin No.

ERPS06M-29-21:

<a> Continue with SUBTASK 294097-831-202 001 Modify the RAT

Actuator .

<2> If the installed actuator has the part number / serial number

listed with modification already incorporated but not re-identified in

accordance with the HAMILTON SUNDSTRAND Service Bulletin

No. ERPS06M-29-21:

<a> Re-identify the actuator and the RAT in accordance

with HAMILTON SUNDSTRAND Service Bulletin No.

ERPS06M-29-21, clean the surface of the actuator with:

Non Aqueous

Cleaner

08BAA9 As required

with

Textile-Lint Free

Cotton

14SBA1 As required

<b> Protect the identification plate with:

Clear Polyurethane

Coating

04MDA3 As required

<c> No further action is required in accordance with this Service

Bulletin.

<3> If the actuator name plate is missing or the serial number is not

listed:

<a> Continue with SUBTASK 294097-831-202 001 Modify the RAT

Actuator .

2 If the installed actuator is from the supplier LIEBHERR, as shown on Fig. AGCAAA Sheet 02, refer to HAMILTON SUNDSTRAND Service Bulletin No.

ERPS06M-29-21.

(2) Subtask 294097-831-202-001 - Modify the RAT Actuator

Work Zones and Access Panels

Zone Access/Work location

633

DATE: Jun 12/14 SERVICE BULLETIN No.: A340-29-4097

REVISION No.: 00 - Jun 12/14 Page: 15

6

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

SERVICE BULLETIN

Manpower Resources

Manhours 9.00

Minimum number of person 1

Subtask elapsed time 9.00

Skills AIRFRAME

Material necessary to do the job

Equipment BFEZ01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 5917109-1 1 ACTUATOR (1)

1 5917109-2 1 ACTUATOR (1)

NOTE (1): The above list of components is not an AIRBUS Kit, the required parts

shall be ordered as necessary through the given channel.

Reidentified part set REIDD01

ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE

NOTES

1702934E RAT 1702934C

1702934D

766351B RAT 766351A

768084B RAT 768084A

770379B RAT 770379A

770952F RAT 770952C

770952D

770952E

References

Aircraft Maintenance Manual (AMM) Task 29-24-56-000-801

Task 29-24-56-400-801

Vendor Service Bulletin (VSB) HAMILTON SUNDSTRAND

ERPS06M-29-21

Fig. A-GBAAA

Removal / Installation of the RAT

Actuator

Sheet 01

(a) Modify the actuator of the RAT.

1 Remove the actuator from the RAT, refer to AMM Task 29-24-56-000-801.

a As shown in Fig. A-GBAAA Sheet 01, remove:

1 Actuator 5912958 Item (1) Retain

or

1 Actuator 5915768 Item (1) Retain

DATE: Jun 12/14 SERVICE BULLETIN No.: A340-29-4097

REVISION No.: 00 - Jun 12/14 Page: 16

6

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

SERVICE BULLETIN

2 For the accomplishment of HAMILTON SUNDSTRAND Service Bulletin

No. ERPS06M-29-21, send the removed actuator, Item (1), to HAMILTON

SUNDSTRAND.

3 Install the modified actuator on the RAT, refer to AMM Task

29-24-56-400-801.

a As shown in Fig. A-GBAAA Sheet 01, install:

1 Actuator 5917109-1 Item 1

or

1 Actuator 5917109-2 Item 1

(b) After modification:

1 Ram Air Turbine 1702934D

becomes:

1 Ram Air Turbine 1702934E

or

1 Ram Air Turbine 1702934C

becomes:

1 Ram Air Turbine 1702934E

or

1 Ram Air Turbine 766351A

becomes:

1 Ram Air Turbine 766351B

or

1 Ram Air Turbine 768084A

becomes:

1 Ram Air Turbine 768084B

or

1 Ram Air Turbine 770379A

becomes:

1 Ram Air Turbine 770379B

or

1 Ram Air Turbine 770952C

DATE: Jun 12/14 SERVICE BULLETIN No.: A340-29-4097

REVISION No.: 00 - Jun 12/14 Page: 17

6

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

SERVICE BULLETIN

becomes:

1 Ram Air Turbine 770952F

or

1 Ram Air Turbine 770952D

becomes:

1 Ram Air Turbine 770952F

or

1 Ram Air Turbine 770952E

becomes:

1 Ram Air Turbine 770952F

D. TEST

(1) Subtask 294097-710-201-001 - Test

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 29-24-00-710-803

Task 29-24-00-710-806

Task 29-24-00-820-803

Task 29-24-56-400-801

(a) Preparation

1 Remove the safety clip(s) and/or tag(s) and close/unlock this (these) circuit

breakers:

PANEL DESIGNATION FIN LOCATION SEE

NOTES

721VU HSMU B + PART G 6JG U10

722VU HSMU Y + PART G 7JG X46

742VU RAT STOW CTL 1JR D77

742VU HYD RAT EXT SOL 2 5JR D76

742VU RAT MAN ON 2JR K74

2 Do the preparation procedure for the test of the actuator, refer to AMM Task

29-24-56-400-801.

(b) Procedure

1 Do the adjustment of the RAT, refer to AMM Task 29-24-00-820-803.

2 Do the operational test of the RAT extension and retraction, refer to AMM

Task 29-24-00-710-803.

DATE: Jun 12/14 SERVICE BULLETIN No.: A340-29-4097

REVISION No.: 00 - Jun 12/14 Page: 18

6

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

SERVICE BULLETIN

3 Examine the hydraulic connections of the RAT for leaks.

NOTE: Leaks are not permitted.

4 Do the operational test of the automatic RAT deployment, refer to AMM Task

29-24-00-710-806.

E. CLOSE-UP

(1) Subtask 294097-942-201-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

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

equipment.

(b) Remove the warning notices.

(c) Remove the access platform(s).

DATE: Jun 12/14 SERVICE BULLETIN No.: A340-29-4097

REVISION No.: 00 - Jun 12/14 Page: 19

6

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

SERVICE BULLETIN

**CONF ALL

A

B C

Z633

A

F_SB_294097_6_CAAA_01_00

Figure A-GCAAA - Sheet 01

Identification of the RAT Actuator

DATE: Jun 12/14 SERVICE BULLETIN No.: A340-29-4097

REVISION No.: 00 - Jun 12/14 Page: 20

6

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

SERVICE BULLETIN

**CONF ALL

B

C

RAT ACTUATOR FROM

RAT ACTUATOR FROM

 THE SUPPLIER LIEBHERR

 THE SUPPLIER ARKWIN

LOCATION OF

EXISTING NAMEPLATE

LOCATION OF

NAMEPLATE

F_SB_294097_6_CAAA_02_00

Figure A-GCAAA - Sheet 02

Identification of the RAT Actuator

DATE: Jun 12/14 SERVICE BULLETIN No.: A340-29-4097

REVISION No.: 00 - Jun 12/14 Page: 21

6

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

SERVICE BULLETIN

**CONF ALL

Z633

A

A

11JR

RAM AIR TURBINE (RAT)

(1)

1

IDENTIFICATION

PLATE

F_SB_294097_6_BAAA_01_00

Figure A-GBAAA - Sheet 01

Removal / Installation of the RAT Actuator

DATE: Jun 12/14 SERVICE BULLETIN No.: A340-29-4097

REVISION No.: 00 - Jun 12/14 Page: 22

6

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

SERVICE BULLETIN

REPORTING SHEET

TITLE: HYDRAULIC POWER - GREEN AUXILIARY HYDRAULIC POWER (RAM

AIR TURBINE) - INTRODUCE NEW SHIMMING PROCEDURE OF RAT

DEPLOY SOLENOIDS

MODIFICATION No.: 204067D50787

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: Jun 12/14 SERVICE BULLETIN No.: A340-29-4097

REVISION No.: 00 - Jun 12/14 Page: 1

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@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: Jun 12/14 SERVICE BULLETIN No.: A340-29-4097

REVISION No.: 00 - Jun 12/14 Page: 1

6

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