@A300

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 - BRACKETS AND SUPPORTS- HYDRAULIC

COMPARTMENT - INSTALL PLACARDS FOR HYDRAULIC

ACCUMULATORS

**CONF ALL

MODIFICATIONS

MODIFICATION CLASSIFICATION

MAJOR None

MINOR 13540S22823

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

Old generation of hydraulic accumulators (pre 1984) have three welds. They can cause damage on the

systems if the accumulators burst.

A modification has been developed to change the design from three welds to one weld and to install

placards to indicate areas where hydraulic accumulators of old generation are forbidden.

Installation of accumulators with only one weld (post 1984) will be allowed.

This Service Bulletin requires installing :

- A support bracket and placard adjacent to the green and blue hydraulic system accumulators for

Aircraft on which Modification No. 02447S9027 is not embodied.

- A support bracket and placard adjacent to the blue hydraulic system accumulator for Aircraft on

which Modification No. 02447S9027 is embodied.

Accomplishment of this Service Bulletin will avoid inadvertent installation of (pre 1984) accumulator.

DATE: Aug 12/10 SERVICE BULLETIN No.: A300-29-0127

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SERVICE BULLETIN

SUMMARY

GENERAL EVALUATION

EVALUATION TABLE

COMPLIANCE MANDATORY (1) CANCELS INSPECTION SB NO

POTENTIAL AD YES A/C OPERATION AFFECTED NO

RELIABILITY AFFECTED NO PAX COMFORT AFFECTED NO

COST SAVING NO ETOPS AFFECTED NO

STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED NO

NOTE (1): Service Bulletin must be accomplished.

MATERIAL PRICE INFORMATION

**CONF 001

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 290127A01R00 1 464.00 Support

**CONF 002

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 290127A02R00 1 See SB Support

EFFECTIVITY

**CONF ALL

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

50W 69X 72U ABR AFG C2A DHL F2I FLM IAW IRA IRM KZU

MIX MNB MSR NTR P2A RUN SOP TDX TNO TSY

CONCURRENT REQUIREMENTS

Accomplishment of this Service Bulletin requires the simultaneous accomplishment of the following

Service Bulletin :

A300-29-0126.

REFERENCES / REPERCUSSIONS

TFU None

OEB None

AOT None

SIL None

LINE MAINTENANCE AFFECTED No

LIFE LIMIT None

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SERVICE BULLETIN

SUMMARY

OTHER None

NATURE OF THE WORK

AIRCRAFT YES

EQUIPMENT NO

HARD NO

SOFT NO

OBRM NO

MANPOWER

**CONF 001

Task 290127-831-801-001: Modification

TOTAL MANHOURS 4.50

ELAPSED TIME (HOURS) 4.50

**CONF 002

Task 290127-831-801-001: Modification

TOTAL MANHOURS 3.00

ELAPSED TIME (HOURS) 3.00

APPENDICES

**CONF ALL

None

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SERVICE BULLETIN

SUMMARY

**CONF 001

A

Z147

FR47

FR54

FR54

A/C CL

FR53

SUPPORTS AND PLACARDS

B C

A

B C

291070

292070

A_SB_290127_5_SAAA_01_03

TO BE INSTALLED

Figure A-FSAAA - Sheet 01

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SERVICE BULLETIN

SUMMARY

**CONF 002

A

Z147

FR47

FR54

FR53

SUPPORT AND PLACARD

B

A

B

292070

A_SB_290127_5_SBAA_01_01

TO BE INSTALLED

Figure A-FSBAA - Sheet 01

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SERVICE BULLETIN

SUMMARY

This Page Intentionally Left Blank

DATE: Aug 12/10 SERVICE BULLETIN No.: A300-29-0127

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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 - BRACKETS AND SUPPORTS- HYDRAULIC

COMPARTMENT - INSTALL PLACARDS FOR HYDRAULIC

ACCUMULATORS

MODIFICATION No.: 13540S22823

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 applicable by Service Bulletin only.

(1) Models

B2-1C B2-203 B2K-3C B4-103 B4-120 B4-203 B4-2C C4-203

F4-203

(2) Effectivity by MSN

0003 0019 0041 0044-0045 0047 0053 0055 0075 0079-0080 0082-0085 0090

0094-0095 0100-0101 0105 0107 0116-0117 0121 0123-0126 0128-0129 0133-0137

0139 0141 0147-0152 0154-0157 0160 0170 0173 0175-0176 0180 0183-0185 0187

0189-0190 0196 0199-0200 0203-0204 0208 0210-0212 0216 0218-0220 0226-0227

0234-0236 0239 0243-0244 0247 0249-0250 0255-0256 0259 0261 0265 0274 0277

0289 0292 0299 0302 0304

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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

50W 0003

69X 0095

72U 0079

ABR 0148 0152 0184 0189 0199 0208 0219 0220 0234 0236 0250 0259

0274 0289

AFG 0180 0190

C2A 0211

DHL 0084 0085 0141 0149 0249 0265

F2I 0083 0094 0128 0133 0135 0136 0137 0156 0170 0235 0243

FLM 0082 0151 0176 0256

IAW 0239

IRA 0080 0139 0173 0185 0187 0226 0299 0302

IRM 0055 0090 0160 0175 0204 0244

KZU 0041 0044 0101 0117

MIX 0125 0134 0157 0196 0203 0218

MNB 0019 0047 0123 0212 0277 0292 0304

MSR 0200 0255

NTR 0124 0155 0210 0227 0247 0261

P2A 0116 0150

RUN 0075 0105 0107 0121 0147 0154 0183

SOP 0126

TDX 0053 0100 0216

TNO 0045

TSY 0129

(4) Configuration by MSN

MSN CONFIGURATION

0003 0019 0041 0044 0045 0047 0053 0055 0075 0079 0080

0082 0083 0084 0085 0090 0094 0095

001

0100 0101 0105 0107 0116 0117 0121 0123 0124 0125 0126

0128 0129 0133 0134 0135 0136 0137 0139 0141 0147 0148

0149 0150 0151 0152 0154 0155 0156 0157 0160 0170 0173

0175 0176 0180 0183 0184 0185 0187 0189 0190 0196 0199

0200 0203 0204 0208 0210 0211 0212 0216 0218 0219 0220

0226 0227 0234 0235 0236 0239 0243 0244 0247 0249 0250

0255 0256 0259 0261 0265 0274 0277 0289 0292 0299 0302

0304

002

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SERVICE BULLETIN

(5) Configuration definition

**CONF 001

Config. 001 is valid for aircraft which Modification No. 02447S9027 (HYDRAULIC

POWER - RELOCATION OF BLUE HYDRAULIC CIRCUIT IN THE MLG BAY) is not

embodied.

**CONF 002

Config. 002 is valid for aircraft which Modification No. 02447S9027 (HYDRAULIC

POWER - RELOCATION OF BLUE HYDRAULIC CIRCUIT IN THE MLG BAY) is

embodied.

(6) Material Effectivity

**CONF 001

MATERIAL QTY PER A/C SEE NOTES

Kit 290127A01R00 1

Consumable CMLA01 1

**CONF 002

MATERIAL QTY PER A/C SEE NOTES

Kit 290127A02R00 1

Consumable CMLA01 1

**CONF ALL

B. CONCURRENT REQUIREMENTS

Accomplishment of this Service Bulletin requires the simultaneous accomplishment of the

following Service Bulletin :

A300-29-0126.

C. REASON

(1) History

Old generation of hydraulic accumulators (pre 1984) have three welds. They can cause

damage on the systems if the accumulators burst.

A modification has been developed to change the design from three welds to one weld

and to install placards to indicate areas where hydraulic accumulators of old generation

are forbidden.

Installation of accumulators with only one weld (post 1984) will be allowed.

(2) Objective/Action

This Service Bulletin requires installing :

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SERVICE BULLETIN

- A support bracket and placard adjacent to the green and blue hydraulic system

accumulators for Aircraft on which Modification No. 02447S9027 is not embodied.

- A support bracket and placard adjacent to the blue hydraulic system accumulator for

Aircraft on which Modification No. 02447S9027 is embodied.

(3) Advantages

Accomplishment of this Service Bulletin will avoid inadvertent installation of (pre 1984)

accumulator.

(4) Operational/Maintenance Consequences

None

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

**CONF 001

Task 290127-831-801-001: Modification

(1) Install the Support and Placard of the Blue System Accumulator FIN 292070

(2) Replace the Support and Placard of the Green System Accumulator FIN 291070

**CONF 002

Task 290127-831-801-001: Modification

(1) Install the Support and Placard of the Blue System Accumulator FIN 292070

**CONF ALL

E. COMPLIANCE

(1) Classification

MANDATORY: Service Bulletin must be accomplished.

(2) Accomplishment Timescale

Accomplishment of this Service Bulletin is requested within 6000 Flight Hours (FH) or 30

months after the issue date of the Service Bulletin whichever occurs first.

Accomplishment of this Service Bulletin is expected to be rendered mandatory by the

issue of an Airworthiness Directive (AD) published by the European Aviation Safety

Agency (EASA). It is anticipated that the AD will confirm the (thresholds and/or intervals

and/or date) given above but reference should be made to the AD for confirmation of the

mandated accomplishment timescale.

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SERVICE BULLETIN

F. APPROVAL

Approved under EASA 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 290127-831-801-001: Modification

Get Access 1.00

On Aircraft

Install the Support and Placard of the Blue System

Accumulator FIN 292070

1.00

Replace the Support and Placard of the Green System

Accumulator FIN 291070

1.50

Close-Up 1.00

TOTAL MANHOURS 4.50

ELAPSED TIME (HOURS) 4.50

**CONF 002

Task 290127-831-801-001: Modification

Get Access 1.00

On Aircraft

Install the Support and Placard of the Blue System

Accumulator FIN 292070

1.00

Close-Up 1.00

TOTAL MANHOURS 3.00

ELAPSED TIME (HOURS) 3.00

**CONF ALL

H. WEIGHT AND BALANCE

Not Changed

I. ELECTRICAL LOAD DATA

Not Changed

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SERVICE BULLETIN

J. REFERENCES

**CONF 001

Aircraft Maintenance Manual (AMM) 20-21-12 20-28-11 24-00-00

31-12-11 32-12-11

Consumable Material List (CML)

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

Service Bulletin (SB) A300-29-0126

Standards Manual (SM)

Structural Repair Manual (SRM) 51-30-29 51-30-31 51-30-38

51-40-12 51-40-20

**CONF 002

Aircraft Maintenance Manual (AMM) 20-21-12 20-28-11 24-00-00

31-12-11 32-12-11

Consumable Material List (CML)

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

Service Bulletin (SB) A300-29-0126

Standards Manual (SM)

Structural Repair Manual (SRM) 51-30-29 51-30-31 51-30-38

51-40-12 51-40-20

**CONF ALL

K. PUBLICATION AFFECTED

Aircraft Maintenance Manual (AMM) 29-11-56

Illustrated Parts Catalog (IPC) 53-15-03

L. INTERCHANGEABILITY/MIXABILITY

Not Applicable

M. SPARES

None

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2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

(1) Procurement Addresses

Kit 290127A01R00

Kit 290127A02R00

Customers with aircraft shown in the

effectivity of this Service Bulletin should send

a purchase order to AIRBUS. Quote the

number of this Service Bulletin. The address

is :

AIRBUS Material, Logistics and Suppliers

Weg beim Jaeger 150

D-22335 Hamburg

Germany

For ordering by internet : http :

//spares.airbus.com

For ordering modification kits by fax : +49 40

50 76 25 90

For ordering of single spares by fax : +49 40

50 76 40 13

(2) Price and Availability

Kit 290127A01R00

Cost 464.00 USD

Availability 90 calendar days from receipt of order

Kit 290127A02R00

TBD

B. INDUSTRY SUPPORT INFORMATION

AIRBUS will provide a 10% reduction to the applicable sales prices given in the paragraph

’Price and Availability’ for orders placed before Dec 31/16.

AIRBUS will not provide industry support for accomplishment of this Service Bulletin.

C. LIST OF COMPONENTS

Kit 290127A01R00

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

NOTES

1 A2913202500000 1 SUPPORT

2 ASNA2050DCJ3215 2 RIVET

3 A2913202400095 1 SUPPORT

4 NAS1801-08-7 3 BOLT

5 NAS1149FN832P 3 WASHER

6 MS21042L08 3 NUT

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SERVICE BULLETIN

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.

Kit 290127A02R00

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

NOTES

1 A2913202500000 1 SUPPORT

2 ASNA2050DCJ3215 2 RIVET

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.

D. LIST OF MATERIALS - OPERATOR SUPPLIED

(1) Consumable Materials

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO CML

MAT. No.

QTY PER A/C SEE

NOTES

Interfay Sealant 09-005E As required

Solvent General Purpose 11-026 As required

(2) Components

None

(3) Equipment

None

E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

None

F. TOOLING

None

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3. ACCOMPLISHMENT INSTRUCTIONS

Task 290127-831-801-001 - Modification

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

INCLUDED IN THE REFERENCED PROCEDURES.

CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP

ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY

AND MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENANCE

WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING,

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

THIS:

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

NECESSARY ON WIRING AND COMPONENTS.

- REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND

OTHER CONTAMINATION.

THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION

AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION.

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

Task Associated Data

**CONF 001

Zone

147

Access

Door 734

Manpower

TOTAL MANHOURS 4.50

ELAPSED TIME (HOURS) 4.50

**CONF 002

Zone

147

Access

Door 734

Manpower

TOTAL MANHOURS 3.00

ELAPSED TIME (HOURS) 3.00

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**CONF ALL

A. GENERAL

**CONF 001

(1) Subtask 290127-839-001-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

(2) Subtask 290127-910-001-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

Material necessary to do the job

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Interfay Sealant 09-005E As required

Solvent General Purpose 11-026 As required

References

Aircraft Maintenance Manual (AMM) 20-21-12, Page Block 001

20-28-11, Page Block 001

Consumable Material List (CML)

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

Structural Repair Manual (SRM) 51-30-29

51-30-31

51-30-38

51-40-12

51-40-20

(a) For the specifications of the materials numbers (Mat.No), refer to the Consumable

Material List (CML).

(b) For the removal and installation of fasteners, refer to SRM 51-30-29.

(c) For alternative and substitute fasteners, refer to SRM 51-30-31.

(d) For fastener hole diameters and drill data, refer to SRM 51-30-38.

(e) To torque tighten the standard threaded fasteners, refer to AMM 20-21-12, Page

Block 001.

(f) Cut the rivets to the necessary length.

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(g) Use a non-metallic spatula to remove the sealant and clean the areas with :

Solvent General

Purpose

11-026 As required

(h) Apply :

Interfay Sealant 09-005E As required

to interfaces of structure and new parts, (Refer to SRM 51-40-20).

(i) Renew the protective finish, (Refer to SRM 51-40-12).

(j) Do the electrical bonding (Refer to ESPM 20-51-20 and AMM 20-28-11, Page Block

001).

**CONF 002

(1) Subtask 290127-839-001-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

(2) Subtask 290127-910-001-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

Material necessary to do the job

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Interfay Sealant 09-005E As required

Solvent General Purpose 11-026 As required

References

Aircraft Maintenance Manual (AMM) 20-21-12, Page Block 001

20-28-11, Page Block 001

Consumable Material List (CML)

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

Structural Repair Manual (SRM) 51-30-29

51-30-31

51-30-38

51-40-12

51-40-20

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(a) For the specifications of the materials numbers (Mat.No), refer to the Consumable

Material List (CML).

(b) For the removal and installation of fasteners, refer to SRM 51-30-29.

(c) For alternative and substitute fasteners, refer to SRM 51-30-31.

(d) For fastener hole diameters and drill data, refer to SRM 51-30-38.

(e) To torque tighten the standard threaded fasteners, refer to AMM 20-21-12, Page

Block 001.

(f) Cut the rivets to the necessary length.

(g) Use a non-metallic spatula to remove the sealant and clean the areas with :

Solvent General

Purpose

11-026 As required

(h) Apply :

Interfay Sealant 09-005E As required

to interfaces of structure and new parts, (Refer to SRM 51-40-20).

(i) Renew the protective finish, (Refer to SRM 51-40-12).

(j) Do the electrical bonding (Refer to ESPM 20-51-20 and AMM 20-28-11, Page Block

001).

**CONF ALL

B. PREPARATION

**CONF 001

(1) Subtask 290127-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 24-00-00, Page Block 301

32-12-11, Page Block 301

(a) Make sure that the aircraft is electrically grounded (Refer to AMM 24-00-00, Page

Block 301).

(b) Put access platform(s) in position.

(c) Open the LH main landing gear door 734 (Refer to AMM 32-12-11, Page Block

301).

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**CONF 002

(1) Subtask 290127-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 24-00-00, Page Block 301

32-12-11, Page Block 301

(a) Make sure that the aircraft is electrically grounded (Refer to AMM 24-00-00, Page

Block 301).

(b) Put access platform(s) in position.

(c) Open the LH main landing gear door 734 (Refer to AMM 32-12-11, Page Block

301).

**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 290127-420-001-001 - Install the Support and Placard of the Blue System

Accumulator FIN 292070

Work Zones and Access Panels

Zone Access/Work location

147 Access Door 734

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills AIRFRAME

Material necessary to do the job

Kit 290127A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 A2913202500000 1 SUPPORT

2 ASNA2050DCJ3215 2 RIVET

References

Fig. A-FBAAA

Installation of the Support and Placard

for the Blue System Accumulator FIN

292070

Sheet 01

Sheet 02

DATE: Aug 12/10 SERVICE BULLETIN No.: A300-29-0127

REVISION No.: 00 - Aug 12/10 Page: 13

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SERVICE BULLETIN

(a) Put the support and placard Item 1 in position as shown in Fig. A-FBAAA Sheet 01

and Fig. A-FBAAA Sheet 02.

(b) Drill two holes on the structure to a diameter between 3.25 mm (0.128 in.) and 3.35

mm (0.132 in.) to match the holes of the support Item 1 as shown in Fig. A-FBAAA

Sheet 02.

(c) Install :

1 Support A2913202500000 Item 1

2 Rivet ASNA2050DCJ3215 Item 2

(2) Subtask 290127-960-001-001 - Replace the Support and Placard of the Green

System Accumulator FIN 291070

Work Zones and Access Panels

Zone Access/Work location

147 Access Door 734

Manpower Resources

Manhours 1.50

Minimum number of person 1

Subtask elapsed time 1.50

Skills AIRFRAME

Material necessary to do the job

Kit 290127A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

3 A2913202400095 1 SUPPORT

4 NAS1801-08-7 3 BOLT

5 NAS1149FN832P 3 WASHER

6 MS21042L08 3 NUT

References

Fig. A-FBBAA

Replacement of the Support and Placard

for the Green System Accumulator FIN

291070

Sheet 01

Sheet 02

(a) Remove the support and placard as shown in Fig. A-FBBAA Sheet 01.

1 Remove :

1 Support Item (3) Discard

2 Bolt Item (4) Discard

DATE: Aug 12/10 SERVICE BULLETIN No.: A300-29-0127

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

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SERVICE BULLETIN

2 Washer Item (5) Discard

2 Nut Item (6) Discard

(b) Install the new support and placard Item 3 :

1 Put the new support and placard Item 3 in position as shown in Fig. A-FBBAA

Sheet 02.

2 Drill two holes on the support Item 3 to a diameter between 4.3 mm (0.169 in.)

and 4.4 mm (0.173 in.) to match the holes of the structure as shown in Fig. AFBBAA Sheet 02.

3 Drill another hole on the structure to a diameter between 4.3 mm (0.169 in.)

and 4.4 mm (0.173 in.) to match the hole of the support Item 3 as shown in

Fig. A-FBBAA Sheet 02.

4 Install :

1 Support A2913202400095 Item 3

3 Washer NAS1149FN832P Item 5

3 Bolt NAS1801-08-7 Item 4

3 Nut MS21042L08 Item 6

**CONF 002

(1) Subtask 290127-420-001-002 - Install the Support and Placard of the Blue System

Accumulator FIN 292070

Work Zones and Access Panels

Zone Access/Work location

147 Access Door 734

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills AIRFRAME

Material necessary to do the job

Kit 290127A02R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 A2913202500000 1 SUPPORT

2 ASNA2050DCJ3215 2 RIVET

DATE: Aug 12/10 SERVICE BULLETIN No.: A300-29-0127

REVISION No.: 00 - Aug 12/10 Page: 15

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SERVICE BULLETIN

References

Fig. A-FBAAA

Installation of the Support and Placard

for the Blue System Accumulator FIN

292070

Sheet 01

Sheet 02

(a) Put the support and placard Item 1 in position as shown in Fig. A-FBAAA Sheet 01

and Fig. A-FBAAA Sheet 02.

(b) Drill two holes on the structure to a diameter between 3.25 mm (0.128 in.) and 3.35

mm (0.132 in.) to match the holes of the support Item 1 as shown in Fig. A-FBAAA

Sheet 02.

(c) Install :

1 Support A2913202500000 Item 1

2 Rivet ASNA2050DCJ3215 Item 2

**CONF ALL

D. TEST

**CONF 001

None

**CONF 002

None

**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 290127-942-001-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 31-12-11, Page Block 301

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

equipment

(b) Close the LH main landing gear door 734 (Refer to AMM 31-12-11, Page Block

301).

(c) Remove the access platform(s).

DATE: Aug 12/10 SERVICE BULLETIN No.: A300-29-0127

REVISION No.: 00 - Aug 12/10 Page: 16

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SERVICE BULLETIN

(d) Restore the systems and the aircraft to normal operating conditions.

**CONF 002

(1) Subtask 290127-942-001-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 31-12-11, Page Block 301

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

equipment

(b) Close the LH main landing gear door 734 (Refer to AMM 31-12-11, Page Block

301).

(c) Remove the access platform(s).

(d) Restore the systems and the aircraft to normal operating conditions.

DATE: Aug 12/10 SERVICE BULLETIN No.: A300-29-0127

REVISION No.: 00 - Aug 12/10 Page: 17

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SERVICE BULLETIN

**CONF ALL

A

Z147

FR47

FR54

FR53

B

99 mm

(3.898 in)

C

1

B

A

292070

A_SB_290127_5_BAAA_01_02

Figure A-FBAAA - Sheet 01

Installation of the Support and Placard for the Blue System Accumulator FIN 292070

DATE: Aug 12/10 SERVICE BULLETIN No.: A300-29-0127

REVISION No.: 00 - Aug 12/10 Page: 18

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SERVICE BULLETIN

**CONF ALL

HOLE

SYMBOL ITEM PN DESCRIPTION

HOLE DIAMETER

MIN MAX

3.25 mm

(0.128 in)

3.35 mm

(0.132 in) 2 ASNA2050DCJ3215 RIVET

1

VIEW LOOKING FORWARD

N

N

HEAD ON VISIBLE FACE

A_SB_290127_5_BAAA_02_01

C

Figure A-FBAAA - Sheet 02

Installation of the Support and Placard for the Blue System Accumulator FIN 292070

DATE: Aug 12/10 SERVICE BULLETIN No.: A300-29-0127

REVISION No.: 00 - Aug 12/10 Page: 19

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SERVICE BULLETIN

**CONF 001

A

Z147

FR47

FR54

A A/C CL

FR54

BEFORE

(3)

HOLE

SYMBOL ITEM

(4)

(5)

(6)

B C

A_SB_290127_5_BBAA_01_01

291070

B

Figure A-FBBAA - Sheet 01

Replacement of the Support and Placard for the Green System Accumulator FIN 291070

DATE: Aug 12/10 SERVICE BULLETIN No.: A300-29-0127

REVISION No.: 00 - Aug 12/10 Page: 20

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@A300

SERVICE BULLETIN

**CONF 001

A/C CL

HOLE

SYMBOL ITEM PN DESCRIPTION

HOLE DIAMETER

MIN MAX

4.30 mm

(0.169 in)

4.40 mm

(0.173 in)

NAS1801−08−7 BOLT

NAS1149FN832P WASHER

MS21042L08 NUT

110 mm

(4.331 in)

AFTER

C

3

4

5

6

N

HEAD ON VISIBLE FACE

NOTE:

01 DO THE ELECTRICAL BONDING

N

ON BOTH SIDES (AS 2 POINTS).

OF DIA. 12 mm

(0.472 in)

01

FR54

FINISH TO A DIAMETER

REMOVE THE SURFACE

A_SB_290127_5_BBAA_02_03

Figure A-FBBAA - Sheet 02

Replacement of the Support and Placard for the Green System Accumulator FIN 291070

DATE: Aug 12/10 SERVICE BULLETIN No.: A300-29-0127

REVISION No.: 00 - Aug 12/10 Page: 21

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SERVICE BULLETIN

REPORTING SHEET

TITLE: HYDRAULIC POWER - BRACKETS AND SUPPORTS- HYDRAULIC

COMPARTMENT - INSTALL PLACARDS FOR HYDRAULIC

ACCUMULATORS

MODIFICATION No.: 13540S22823

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 12/10 SERVICE BULLETIN No.: A300-29-0127

REVISION No.: 00 - Aug 12/10 Page: 1

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SERVICE BULLETIN

QUALITY PERCEPTION FORM

Use this form to tell us what is your perception of the quality of this Service Bulletin. The reported data

that you provide us will be used to analyse areas of difficulties and to take corrective action to further

improve the quality of our Service Bulletins.

We thank you for the time you have taken in completing this form.

(Please rate on a scale of 1 to 4, with 4 being the highest score)

- Quality rating of this SB 4 3 2 1

- Quality rating of the Accomplishment Instructions 4 3 2 1

- Quality rating of the Illustrations 4 3 2 1

- 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 12/10 SERVICE BULLETIN No.: A300-29-0127

REVISION No.: 00 - Aug 12/10 Page: 1

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