@A300

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: 24

TITLE: ELECTRICAL POWER-INSPECTION OF SHUT-OFF VALVE BONDING

LEAD

MODIFICATION No.: None

This page transmits Revision No.01 of Service Bulletin No.A300-24-0106

ADDITIONAL WORK

**CONF ALL

ADDITIONAL WORK is required by this revision for aircraft inspected by the original issue of this

Service Bulletin.

The ADDITIONAL WORK for this Service Bulletin is issued to ensure that the correct bonding leads

(one on RH and one on LH) are inspected. At original issue, the description of the bonding leads (two

on RH and two on LH) to be inspected was misleading and some operators could have inspected other

bonding leads than the one to be checked.

REASON

Revision 01 issued to clarify the bonding leads (RH and LH) to be inspected, to replace PN

E0088-10-80 by PN E0088-10-80NN (as per Standards Manual evolution) and to update the effectivity.

CHANGES

The main changes of revision 01 are:

- To modify figure A-FBAAA to correct the bonding lead to be inspected.

- To modify the Inspection Report (figure A-FRAAA) in accordance with the correct bonding leads

(RH and LH) to be inspected.

- To modify the COMPA01:

. Bonding lead PN E0088-10-80 replaced by PN E0088-10-80NN in accordance with Standards

Manual.

. Bonding leads quantity changed from 4 to 2.

. Nuts (PN NSA5050-3) quantity changed from 8 to 4.

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-0106

REVISION No.: 01 - Mar 26/13 Page: 1

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

- To add a NOTE to align the clamps.

- To update the effectivity.

SUMMARY

REASON/DESCRIPTION/OPERATIONAL

CONSEQUENCES

REASON UPDATED R

EFFECTIVITY OPERATOR LIST UPDATED R

MANPOWER MANPOWER UPDATED R

APPENDICES APPENDICES UPDATED R

PLANNING INFORMATION

EFFECTIVITY EFFECTIVITY RELATED INFORMATION

UPDATED

R

Configuration definition

CONF 001 CONFIGURATION DEFINITION UPDATED R

Material Effectivity MATERIAL EFFECTIVITY UPDATED

MATERIAL SET QUANTITY UPDATED

MATERIAL SET UPDATED

R

REASON

History HISTORY UPDATED R

Objective/Action OBJECTIVE/ACTION UPDATED R

COMPLIANCE

Accomplishment Timescale ACCOMPLISHMENT TIMESCALE UPDATED

CONFIGURATION UPDATED

R

APPROVAL APPROVAL UPDATED R

MANPOWER MANPOWER UPDATED R

REFERENCES REFERENCED DOCUMENTATION UPDATED R

MATERIAL INFORMATION

MATERIAL - PRICE AND AVAILABILITY

Procurement Addresses PROCUREMENT ADDRESSES UPDATED

MATERIAL SET UPDATED

R

Price and Availability PRICE AND AVAILABILITY UPDATED R

LIST OF MATERIALS - OPERATOR

SUPPLIED

Consumable Materials CONSUMABLE MATERIALS UPDATED R

Consumable CMLA01 CONSUMABLE MATERIAL SET ADDED N

Components

Component COMPA01 PART MATERIAL SET UPDATED

QUANTITY UPDATED

PART NUMBER UPDATED

R

ACCOMPLISHMENT INSTRUCTIONS

TASK 240106- 832-801-001-Inspection

Subtask 240106-910-001-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

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REVISION No.: 01 - Mar 26/13 Page: 2

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Subtask 240106-832-001-001 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

PART NUMBER UPDATED

CONSUMABLE UPDATED

FIGURE REFERENCE UPDATED

NOTE UPDATED

MATERIAL LIST UPDATED

REFERENCES UPDATED

R

Subtask 240106-832-002-001 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

PART NUMBER UPDATED

CONSUMABLE UPDATED

FIGURE REFERENCE UPDATED

NOTE UPDATED

MATERIAL LIST UPDATED

REFERENCES UPDATED

R

TASK 240106- 832-802-001-Inspection -

ADDITIONAL WORK

TASK SOLUTION ADDED N

Task associated data - 001 TASK ASSOCIATED DATA ADDED N

Subtask 240106-910-002-001 SUBTASK SOLUTION ADDED N

Subtask 240106-839-002-001 SUBTASK SOLUTION ADDED N

Subtask 240106-941-002-001 SUBTASK SOLUTION ADDED N

Subtask 240106-865-003-001 SUBTASK SOLUTION ADDED N

Subtask 240106-010-003-001 SUBTASK SOLUTION ADDED N

Subtask 240106-010-004-001 SUBTASK SOLUTION ADDED N

Subtask 240106-832-003-001 SUBTASK SOLUTION ADDED N

Subtask 240106-832-004-001 SUBTASK SOLUTION ADDED N

Subtask 240106-865-004-001 SUBTASK SOLUTION ADDED N

Subtask 240106-700-002-001 SUBTASK SOLUTION ADDED N

Subtask 240106-410-003-001 SUBTASK SOLUTION ADDED N

Subtask 240106-410-004-001 SUBTASK SOLUTION ADDED N

Subtask 240106-942-002-001 SUBTASK SOLUTION ADDED N

Fig. A-FBAAA

Fig. A-FBAAA Sheet 01 SHEET UPDATED R

Fig. A-FFAAA FIGURE SOLUTION ADDED N

Fig. A-FFAAA Sheet 01 SHEET ADDED N

Fig. A-FBCAA FIGURE SOLUTION ADDED N

Fig. A-FBCAA Sheet 01 SHEET ADDED N

Fig. A-FFBAA FIGURE SOLUTION ADDED N

Fig. A-FFBAA Sheet 01 SHEET ADDED N

Fig. A-FBB FIGURE DELETED FOR APPLICABLE MSN D

Appendix 01 - Inspection Report

Fig. A-FRAAA FIGURE SOLUTION ADDED N

Fig. A-FRAAA Sheet 01 SHEET ADDED N

Fig. A-FAA FIGURE DELETED FOR APPLICABLE MSN D

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-0106

REVISION No.: 01 - Mar 26/13 Page: 3

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Appendix 03 - Inspection Report (Additional Work)

APPENDIX CONTENT APPENDIX CONTENT ADDED N

Fig. A-FRBAA FIGURE SOLUTION ADDED N

Fig. A-FRBAA Sheet 01 SHEET ADDED N

Appendix 04 - Gantt Chart (Additional Work)

APPENDIX CONTENT APPENDIX CONTENT ADDED N

Fig. A-FADAA FIGURE SOLUTION ADDED N

Fig. A-FADAA Sheet 01 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

No previous revision

REVISION SEQUENCE

ORIGINAL: Jul 09/10

REVISION No. : 01 - Mar 26/13

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-0106

REVISION No.: 01 - Mar 26/13 Page: 4

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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: 24

TITLE: ELECTRICAL POWER-INSPECTION OF SHUT-OFF VALVE BONDING

LEAD

**CONF ALL

MODIFICATIONS

None

REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES

During maintenance an operator has reported an inoperative GREEN hydraulic Fire Shut-Off Valve

(FSOV).

Troubleshooting evidenced some damages :

- A wire located between Engine 2 hydraulic FSOV and wing rear spar (zones 575/675) has been

found cut

- A bonding lead (E0088-10-80NN) located between Rib 7A and Rib 8 below Hydraulic Pressure

Lines has been found cut.

Investigations on different aircraft have shown that some aircraft are fitted with bonding leads of

(120mm (4.72in) length instead of 80mm (3.15in)).

This overlength can lead to contact and chafing between the harness and the bonding lead, which can

lead to the findings. It can also entail damages in case of lightning strike.

This Inspection Service Bulletin requires inspection and repair (when necessary) of the :

- Wires located between Engines hydraulic FSOV and wing rear spar (zones 575/675)

- Two bonding leads (RH and LH) (E0088-10-80NN) located between Rib 7A and Rib 8 below

Hydraulic Pressure Lines.

Accomplishment of this Inspection Service Bulletin will avoid such a case of inoperative hydraulic FSOV

due to wiring damaged by a bonding lead and restore the aircraft system reliability.

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-0106

REVISION No.: 01 - Mar 26/13 Page: 1

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@A300

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

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Component COMPA01 1 See SB Bonding leads, Nuts.

EFFECTIVITY

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

001 50W 69X 72U ABR AFG DHL F2I FLM GST IAW IRA IRM

KYE KZU MNB MNG MSR NTR P2A RUN SOP TIW TNO TSY

CONCURRENT REQUIREMENTS

None

REFERENCES / REPERCUSSIONS

TFU None

OEB None

AOT None

SIL None

LINE MAINTENANCE AFFECTED No

LIFE LIMIT None

OTHER None

NATURE OF THE WORK

AIRCRAFT YES

EQUIPMENT NO

HARD NO

SOFT NO

OBRM NO

MANPOWER

Task 240106-832-801-001: Inspection

TOTAL MANHOURS 8.00

ELAPSED TIME (HOURS) 4.50

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-0106

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SERVICE BULLETIN

SUMMARY

Task 240106-832-802-001: Inspection - ADDITIONAL WORK

TOTAL MANHOURS 8.00

ELAPSED TIME (HOURS) 4.50

APPENDICES

Appendix 01 - Inspection Report

Appendix 02 - Gantt Chart

Appendix 03 - Inspection Report (Additional Work)

Appendix 04 - Gantt Chart (Additional Work)

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-0106

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SERVICE BULLETIN

SUMMARY

**CONF ALL

AREA TO BE INSPECTED

A

Z575 (Z675)

RIB5

RIB8

REAR SPAR

A

LH SIDE SHOWN

RH SIDE SYMMETRICAL

RIB7A

A_SB_240106_5_SAAA_01_01

Figure A-FSAAA - Sheet 01

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-0106

REVISION No.: 01 - Mar 26/13 Page: 4

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@A300

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: 24

TITLE: ELECTRICAL POWER-INSPECTION OF SHUT-OFF VALVE BONDING

LEAD

MODIFICATION No.: None

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

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

F4-203

(2) Effectivity by MSN

0003 0041 0045 0047 0053 0055 0075 0079-0080 0082-0085 0090 0094-0095 0101

0105 0107 0116-0117 0123-0126 0128-0129 0133 0135-0137 0139 0141 0149-0152

0154-0157 0160 0170 0173 0175-0176 0180 0183-0185 0187 0189 0199-0200

0203-0204 0210-0212 0218-0220 0226-0227 0234-0236 0239 0243-0244 0247

0249-0250 0255-0256 0259 0261 0265 0274 0277 0289 0292 0299 0302 0304

(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.

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-0106

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@A300

SERVICE BULLETIN

OPERATOR MSN

001 0125 0157 0203 0218

50W 0003

69X 0095

72U 0079

ABR 0152 0184 0189 0199 0219 0220 0234 0236 0250 0259 0274 0289

AFG 0180

DHL 0084 0085 0141 0149 0249 0265

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

FLM 0082 0176

GST 0277 0292

IAW 0239

IRA 0080 0139 0151 0173 0185 0187 0226 0256 0299 0302

IRM 0055 0090 0160 0175 0204 0244

KYE 0053 0211

KZU 0041 0101 0117

MNB 0123 0212 0304

MNG 0047

MSR 0200 0255

NTR 0124 0155

P2A 0116 0150

RUN 0075 0105 0107 0154 0183

SOP 0126

TIW 0261

TNO 0045 0210 0227 0247

TSY 0129

(4) Configuration by MSN

MSN CONFIGURATION

0003 0041 0045 0047 0053 0055 0075 0079 0080 0082 0083

0084 0085 0090 0094 0095 0101 0105 0107 0116 0117 0123

0124 0125 0126 0128 0129 0133 0135 0136 0137 0139 0141

0149 0150 0151 0152 0154 0155 0156 0157 0160 0170 0173

0175 0176 0180 0183 0184 0185 0187 0189 0199 0200 0203

0204 0210 0211 0212 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

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.

(6) Material Effectivity

MATERIAL QTY PER A/C SEE NOTES

Component COMPA01 1

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-0106

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SERVICE BULLETIN

MATERIAL QTY PER A/C SEE NOTES

Consumable CMLA01 1

B. CONCURRENT REQUIREMENTS

None

C. REASON

(1) History

During maintenance an operator has reported an inoperative GREEN hydraulic Fire

Shut-Off Valve (FSOV).

Troubleshooting evidenced some damages :

- A wire located between Engine 2 hydraulic FSOV and wing rear spar (zones

575/675) has been found cut

- A bonding lead (E0088-10-80NN) located between Rib 7A and Rib 8 below

Hydraulic Pressure Lines has been found cut.

Investigations on different aircraft have shown that some aircraft are fitted with bonding

leads of (120mm (4.72in) length instead of 80mm (3.15in)).

This overlength can lead to contact and chafing between the harness and the bonding

lead, which can lead to the findings. It can also entail damages in case of lightning

strike.

(2) Objective/Action

This Inspection Service Bulletin requires inspection and repair (when necessary) of the :

- Wires located between Engines hydraulic FSOV and wing rear spar (zones 575/675)

- Two bonding leads (RH and LH) (E0088-10-80NN) located between Rib 7A and Rib

8 below Hydraulic Pressure Lines.

(3) Advantages

Accomplishment of this Inspection Service Bulletin will avoid such a case of inoperative

hydraulic FSOV due to wiring damaged by a bonding lead and restore the aircraft

system reliability.

(4) Operational/Maintenance Consequences

None

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-0106

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@A300

SERVICE BULLETIN

Task 240106-832-801-001: Inspection

(1) Do a Detailed Inspection of the FSOV Bonding Lead and of the Wires Located on

Wing Rear Spar (RH side).

(2) Do a Detailed Inspection of the FSOV Bonding Lead and of the Wires Located on

Wing Rear Spar (LH side).

Task 240106-832-802-001: Inspection - ADDITIONAL WORK

(1) Do a Detailed Inspection of the FSOV Bonding Lead and of the Wires Located on

Wing Rear Spar (RH side).

(2) Do a Detailed Inspection of the FSOV Bonding Lead and of the Wires Located on

Wing Rear Spar (LH side).

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 thresholds given

in Table 1 but reference should be made to the AD for confirmation of the mandated

accomplishment timescale.

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-0106

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@A300

SERVICE BULLETIN

Table 1, Config. 001: Detailed inspection of the FSOV bonding leads and of the wires located on wing

rear spar (zones 575-675)

COMPLIANCE TIME (Whichever occurs

later)

CONDITION ACTION

THRESHOLD GRACE PERIOD

REPETITIVE

INTERVAL

Aircraft on which

original issue of

this ISB has not

been accomplished

Inspect in

accordance with

SUBTASK

240106-832-001

001 Do a Detailed

Inspection of the

FSOV Bonding

Lead and of the

Wires Located on

Wing Rear Spar

(RH side). and

SUBTASK

240106-832-002

001 Do a Detailed

Inspection of the

FSOV Bonding

Lead and of the

Wires Located on

Wing Rear Spar

(LH side).

Within 4,500 Flight

Hours (FH) or 30

months after the

reception of the

Service Bulletin at

original issue

whichever occurs

first.

None None

Aircraft on which

original issue of

this ISB has been

accomplished

Inspect in

accordance with

SUBTASK

240106-832-003

001 Do a Detailed

Inspection of the

FSOV Bonding

Lead and of the

Wires Located on

Wing Rear Spar

(RH side). and

SUBTASK

240106-832-004

001 Do a Detailed

Inspection of the

FSOV Bonding

Lead and of the

Wires Located on

Wing Rear Spar

(LH side).

Within 4,500 Flight

Hours (FH) or 30

months after the

reception of the

Service Bulletin at

Revision No. 01

whichever occurs

first.

None None

F. APPROVAL

Approved under EASA Design Organization Approval No. EASA 21J.031.

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SERVICE BULLETIN

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 240106-832-801-001: Inspection

Get Access 2.00

On Aircraft

Do a Detailed Inspection of the FSOV Bonding Lead

and of the Wires Located on Wing Rear Spar (RH

side).

1.50

Do a Detailed Inspection of the FSOV Bonding Lead

and of the Wires Located on Wing Rear Spar (LH

side).

1.50

Tests 1.00

Close-Up 2.00

TOTAL MANHOURS 8.00

ELAPSED TIME (HOURS) 4.50

NOTE: For an explanation of the manhours and elapsed time, refer to the Gantt

Chart given in Appendix 02 - Gantt Chart .

Task 240106-832-802-001: Inspection - ADDITIONAL WORK

Get Access 2.00

On Aircraft

Do a Detailed Inspection of the FSOV Bonding Lead

and of the Wires Located on Wing Rear Spar (RH

side).

1.50

Do a Detailed Inspection of the FSOV Bonding Lead

and of the Wires Located on Wing Rear Spar (LH

side).

1.50

Tests 1.00

Close-Up 2.00

TOTAL MANHOURS 8.00

ELAPSED TIME (HOURS) 4.50

NOTE: For an explanation of the manhours and elapsed time, refer to the Gantt

Chart given in Appendix 04 - Gantt Chart (Additional Work) .

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-0106

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SERVICE BULLETIN

H. WEIGHT AND BALANCE

Not Changed

I. ELECTRICAL LOAD DATA

Not Changed

J. REFERENCES

Aircraft Maintenance Manual (AMM) 06-21-00 06-21-57 20-21-12

20-28-11 24-00-00 24-50-20

24-50-40 29-10-00 52-10-00

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-51-20 20-53-21 20-55-00

Standards Manual (SM)

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

K. PUBLICATION AFFECTED

None

L. INTERCHANGEABILITY/MIXABILITY

Not Applicable

M. SPARES

None

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-0106

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SERVICE BULLETIN

This Page Intentionally Left Blank

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-0106

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SERVICE BULLETIN

2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

(1) Procurement Addresses

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

multiple suppliers ensure access to minimum prices. AIRBUS recommends Customers

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

B/E Aerospace. The address is:

Component COMPA01 B/E AEROSPACE INC

CONSUMABLES MANAGEMENT

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_CMG@beaerospace.com

Internet: http://www.beconsumables.com

or, alternatively any other source on the open

market.

(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

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

C. LIST OF COMPONENTS

No Kit

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-0106

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SERVICE BULLETIN

D. LIST OF MATERIALS - OPERATOR SUPPLIED

(1) Consumable Materials

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO CML

MAT. No.

QTY PER A/C SEE

NOTES

Fuel Tank Sealant Polysulfid 09-002 As required

(2) Components

Component COMPA01

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

NOTES

2 NSA5050-3 4 NUT (1)

3 E0088-10-80NN 2 LEAD (1)

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.

NOTE (1): The quantity depends on the result of the inspection.

(3) Equipment

None

E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

None

F. TOOLING

None

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-0106

REVISION No.: 01 - Mar 26/13 Page: 10

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3. ACCOMPLISHMENT INSTRUCTIONS

Task 240106-832-801-001 - Inspection

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

INCLUDED IN THE REFERENCED PROCEDURES.

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.

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

Zone

575 675

Access

Panel 575CB 575DB 575FB 675CB 675DB 675FB

Manpower

TOTAL MANHOURS 8.00

ELAPSED TIME (HOURS) 4.50

A. GENERAL

(1) Subtask 240106-910-001-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-0106

REVISION No.: 01 - Mar 26/13 Page: 11

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SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) 06-21-00, Page Block 001

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

(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 06-21-00, Page Block 001).

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

(d) For alternative and substitute fasteners, (Refer to SRM 51-30-31).

(e) Do the electrical bonding, (Refer to AMM 20-28-11, Page Block 001 and to ESPM

20-51-20).

(f) To torque tighten the standard thread fasteners, (Refer to AMM 20-21-12, Page

Block 001).

(2) Subtask 240106-839-001-001 - 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 240106-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

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

52-10-00, Page Block 001

(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 passenger/crew door 831 (Refer to AMM 52-10-00, Page Block 001).

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-0106

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SERVICE BULLETIN

(2) Subtask 240106-865-001-001 - C/B Opening

Manpower Resources

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) 24-50-20, Page Block 001

24-50-40, Page Block 001

(a) If the wire(s) must be repaired, open, safety tag these circuit breakers :

PANEL DESIGNATION FIN LOCATION SEE

NOTES

120VU PWR TRANSF/G/Y 6GL (1)

120VU RAM AIR/TEST/ and ELEC

PUMPS

1GK (1)

120VU HYD SHUT OFF

VALVES/WARN/IND

3GJ (1)

120VU HYD SHUT OFF

VALVES/CONTRL/ENG 2

4GJ (1)

NOTE (1): Refer to AMM 24-50-20, Page Block 001 for the C/B location.

or open, safety tag these circuit breakers :

PANEL DESIGNATION FIN LOCATION SEE

NOTES

120VU PTU/CTL/G/Y 6GL (1)

120VU FIRE VALVES/ENG 2 4GJ (1)

101VU ELEC PUMPS (19GK) 63GK (1)

101VU ELEC PUMPS (20GK) 64GK (1)

129VU COCKPIT LTS/MAINT/PNL/MI

and/ANN LTS

1WB (1)

NOTE (1): Refer to AMM 24-50-20, Page Block 001 or to AMM 24-50-40, Page

Block 001 for the C/B location.

(3) Subtask 240106-010-001-001 - Open for Access on RH Side

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-21-57, Page Block 001

(a) Open the access panels 675DB and/or 675CB and/or 675FB (Refer to AMM

06-21-57, Page Block 001).

(4) Subtask 240106-010-002-001 - Open for Access on LH Side

Manpower Resources

Skills NON SPECIFIC

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-0106

REVISION No.: 01 - Mar 26/13 Page: 13

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SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) 06-21-57, Page Block 001

(a) Open the access panels 575DB and/or 575CB and/or 575FB (Refer to AMM

06-21-57, Page Block 001).

C. PROCEDURE

(1) Subtask 240106-832-001-001 - Do a Detailed Inspection of the FSOV Bonding Lead

and of the Wires Located on Wing Rear Spar (RH side).

Work Zones and Access Panels

Zone Access/Work location

675 Access Panel 675DB, Panel 675CB, Panel 675FB

Work location from Rib 7A to Rib 8

Manpower Resources

Manhours 1.50

Minimum number of person 1

Subtask elapsed time 1.50

Skills ELECTRICAL

Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

2 NSA5050-3 2 NUT (1)

3 E0088-10-80NN 1 LEAD (1)

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

shall be ordered as necessary through the given channel.

NOTE (1): The quantity depends on the result of the inspection.

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Fuel Tank Sealant

Polysulfid

09-002 As required

References

Elec. Std. Practices Manual (ESPM) 20-53-21

Fig. A-FBAAA

Area to be inspected

Sheet 01

Fig. A-FFAAA

Flow Chart

Sheet 01

(a) For the inspection area, Refer to Fig. A-FBAAA

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-0106

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(b) Do a detailed inspection of the length of the bonding lead, Refer to Fig. A-FFAAA

1 Depending on the inspection result :

a Remove :

1 lead-Bonding Item (3)

attached with :

2 Bolt Item (1) Retain

2 Nut Item (2) Discard

b Install :

1 Lead-Bonding E0088-10-80NN Item 3

with :

2 Bolt Item (1) Retained at

removal

and with :

2 Nut NSA5050-3 Item 2

NOTE: Do the alignment of the two clamps and seal them with:

Fuel Tank Sealant

Polysulfid

09-002 As required

(c) Do a detailed inspection of the wires, Refer to Fig. A-FFAAA.

1 If there is no contact and no chafing, no further action is required.

2 If there is chafing, repair the wire(s) (Refer to ESPM 20-53-21).

(d) For the inspection report, Refer to Appendix 01 - Inspection Report .

(2) Subtask 240106-832-002-001 - Do a Detailed Inspection of the FSOV Bonding Lead

and of the Wires Located on Wing Rear Spar (LH side).

Work Zones and Access Panels

Zone Access/Work location

575 Access Panel 575DB, Panel 575CB, Panel 575FB

Work location from Rib 7A to Rib 8

Manpower Resources

Manhours 1.50

Minimum number of person 1

Subtask elapsed time 1.50

Skills ELECTRICAL

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-0106

REVISION No.: 01 - Mar 26/13 Page: 15

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SERVICE BULLETIN

Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

2 NSA5050-3 2 NUT (1)

3 E0088-10-80NN 1 LEAD (1)

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

shall be ordered as necessary through the given channel.

NOTE (1): The quantity depends on the result of the inspection.

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Fuel Tank Sealant

Polysulfid

09-002 As required

References

Elec. Std. Practices Manual (ESPM) 20-53-21

Fig. A-FBAAA

Area to be inspected

Sheet 01

Fig. A-FFAAA

Flow Chart

Sheet 01

(a) For the inspection area, Refer to Fig. A-FBAAA

(b) Do a detailed inspection of the length of the bonding lead, Refer to Fig. A-FFAAA

1 Depending on the inspection result :

a Remove :

1 lead-Bonding Item (3)

attached with :

2 Bolt Item (1) Retain

2 Nut Item (2) Discard

b Install :

1 Lead-Bonding E0088-10-80NN Item 3

with :

2 Bolt Item (1) Retained at

removal

and with :

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-0106

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SERVICE BULLETIN

2 Nut NSA5050-3 Item 2

NOTE: Do the alignment of the two clamps and seal them with:

Fuel Tank Sealant

Polysulfid

09-002 As required

(c) Do a detailed inspection of the wires, Refer to Fig. A-FFAAA.

1 If there is no contact and no chafing, no further action is required.

2 If there is chafing, repair the wire(s) (Refer to ESPM 20-53-21).

(d) For the inspection report, Refer to Appendix 01 - Inspection Report .

D. TEST

(1) Subtask 240106-865-002-001 - C/B Closing

Manpower Resources

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) 24-50-20, Page Block 001

24-50-40, Page Block 001

(a) If a wire has been repaired, remove the safety clips and tags and close the

following circuit breakers :

PANEL DESIGNATION FIN LOCATION SEE

NOTES

120VU PWR TRANSF/G/Y 6GL (1)

120VU RAM AIR/TEST/ and ELEC

PUMPS

1GK (1)

120VU HYD SHUT OFF

VALVES/WARN/IND

3GJ (1)

120VU HYD SHUT OFF

VALVES/CONTRL/ENG 2

4GJ (1)

NOTE (1): Refer to AMM 24-50-20, Page Block 001 for the C/B location.

or remove the safety clips and tags and close the following circuit breakers :

PANEL DESIGNATION FIN LOCATION SEE

NOTES

120VU PTU/CTL/G/Y 6GL (1)

120VU FIRE VALVES/ENG 2 4GJ (1)

101VU ELEC PUMPS (19GK) 63GK (1)

101VU ELEC PUMPS (20GK) 64GK (1)

129VU COCKPIT LTS/MAINT/PNL/MI

and/ANN LTS

1WB (1)

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-0106

REVISION No.: 01 - Mar 26/13 Page: 17

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SERVICE BULLETIN

NOTE (1): Refer to AMM 24-50-20, Page Block 001 or to AMM 24-50-40, Page

Block 001 for the C/B location.

(2) Subtask 240106-700-001-001 - Testing

Manpower Resources

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) 20-28-11, Page Block 001

29-10-00, Page Block 501

(a) If a bonding lead has been replaced, do the check of the electrical bonding (Refer

to AMM 20-28-11, Page Block 001).

NOTE: For the maximum Permissible Resistance Values, (Refer to the

Table AMM 20-28-11, Page Block 001).

(b) If a wire has been repaired, do a functional test of fire valves (Refer to AMM

29-10-00, Page Block 501).

E. CLOSE-UP

(1) Subtask 240106-410-001-001 - Close the access panels on RH Side

Work Zones and Access Panels

Zone Access/Work location

675

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-21-57, Page Block 001

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

equipment.

(b) Close the access panels 675DB and/or 675CB and/or 675FB (Refer to AMM

06-21-57, Page Block 001).

(2) Subtask 240106-410-002-001 - Close the access panels on LH Side

Work Zones and Access Panels

Zone Access/Work location

575

Manpower Resources

Skills NON SPECIFIC

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-0106

REVISION No.: 01 - Mar 26/13 Page: 18

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SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) 06-21-57, Page Block 001

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

equipment.

(b) Close the access panels 575DB and/or 575CB and/or 575FB (Refer to AMM

06-21-57, Page Block 001).

(3) Subtask 240106-942-001-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 52-10-00, Page Block 001

(a) Close the passenger/crew door 831 (Refer to AMM 52-10-00, Page Block 001).

(b) Remove the access platform(s).

(c) Restore the system and the aircraft to the normal operating condition.

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-0106

REVISION No.: 01 - Mar 26/13 Page: 19

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This Page Intentionally Left Blank

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-0106

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SERVICE BULLETIN

Task 240106-832-802-001 - Inspection - ADDITIONAL WORK

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

INCLUDED IN THE REFERENCED PROCEDURES.

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.

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

Zone

575 675

Access

Panel 575CB 575DB 575FB 675CB 675DB 675FB

Manpower

TOTAL MANHOURS 8.00

ELAPSED TIME (HOURS) 4.50

A. GENERAL

(1) Subtask 240106-910-002-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-0106

REVISION No.: 01 - Mar 26/13 Page: 21

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SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) 06-21-00, Page Block 001

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

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

Consumable Material List (CML).

(b) For the identification of zones, refer to AMM 06-21-00, Page Block 001.

(c) Remove and install fasteners in accordance with SRM 51-30-29.

(d) Obtain alternative and substitute fasteners data, in accordance with SRM 51-30-31.

(e) For the electrical bonding, refer to ESPM 20-51-20 and AMM 20-28-11, Page Block

001.

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

Block 001.

(2) Subtask 240106-839-002-001 - 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 240106-941-002-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

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

52-10-00, Page Block 001

(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 passenger/crew door 831, refer to AMM 52-10-00, Page Block 001.

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-0106

REVISION No.: 01 - Mar 26/13 Page: 22

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SERVICE BULLETIN

(2) Subtask 240106-865-003-001 - C/B Opening

Manpower Resources

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) 24-50-20, Page Block 001

24-50-40, Page Block 001

(a) If the wire(s) must be repaired, open, safety/lock and tag these circuit breakers:

PANEL DESIGNATION FIN LOCATION SEE

NOTES

120VU PWR TRANSF/G/Y 6GL (1)

120VU RAM AIR/TEST/ and ELEC

PUMPS

1GK (1)

120VU HYD SHUT OFF

VALVES/WARN/IND

3GJ (1)

120VU HYD SHUT OFF

VALVES/CONTRL/ENG 2

4GJ (1)

NOTE (1): Refer to AMM 24-50-20, Page Block 001 for the C/B location.

or open, safety/lock and tag these circuit breakers:

PANEL DESIGNATION FIN LOCATION SEE

NOTES

120VU PTU/CTL/G/Y 6GL (1)

120VU FIRE VALVES/ENG 2 4GJ (1)

101VU ELEC PUMPS (19GK) 63GK (1)

101VU ELEC PUMPS (20GK) 64GK (1)

129VU COCKPIT LTS/MAINT/PNL/MI

and/ANN LTS

1WB (1)

NOTE (1): Refer to AMM 24-50-20, Page Block 001 or to AMM 24-50-40, Page

Block 001 for the C/B location.

(3) Subtask 240106-010-003-001 - Open for Access on RH Side

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-21-57, Page Block 001

(a) Open the access panels 675DB and/or 675CB and/or 675FB, refer to AMM

06-21-57, Page Block 001.

(4) Subtask 240106-010-004-001 - Open for Access on LH Side

Manpower Resources

Skills NON SPECIFIC

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-0106

REVISION No.: 01 - Mar 26/13 Page: 23

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SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) 06-21-57, Page Block 001

(a) Open the access panels 575DB and/or 575CB and/or 575FB, refer to AMM

06-21-57, Page Block 001.

C. PROCEDURE

(1) Subtask 240106-832-003-001 - Do a Detailed Inspection of the FSOV Bonding Lead

and of the Wires Located on Wing Rear Spar (RH side).

Work Zones and Access Panels

Zone Access/Work location

675 Access Panel 675DB, Panel 675CB, Panel 675FB

Work location from Rib 7A to Rib 8

Manpower Resources

Manhours 1.50

Minimum number of person 1

Subtask elapsed time 1.50

Skills ELECTRICAL

Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

2 NSA5050-3 2 NUT (1)

3 E0088-10-80NN 1 LEAD (1)

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

shall be ordered as necessary through the given channel.

NOTE (1): The quantity depends on the result of the inspection.

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Fuel Tank Sealant

Polysulfid

09-002 As required

References

Elec. Std. Practices Manual (ESPM) 20-53-21

Fig. A-FBCAA

Area to be inspected (Additional Work)

Sheet 01

Fig. A-FFBAA

Flow Chart (Additional Work)

Sheet 01

(a) For the inspection area, refer to Fig. A-FBCAA.

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(b) Do a detailed inspection of the length of the bonding lead, refer to Fig. A-FFBAA.

1 Depending on the inspection result:

a Remove:

1 Lead-Bonding Item (3)

attached with:

2 Bolt Item (1) Retain

2 Nut Item (2) Discard

b Install:

1 Lead-Bonding E0088-10-80NN Item 3

with:

2 Bolt Item (1) Retained at

removal

and with:

2 Nut NSA5050-3 Item 2

NOTE: Do the alignment of the two clamps and seal them with:

Fuel Tank Sealant

Polysulfid

09-002 As required

(c) Do a detailed inspection of the wires, refer to Fig. A-FFBAA.

1 If there is no contact and no chafing, no further action is required.

2 If there is chafing, repair the wire(s), refer to ESPM 20-53-21.

(d) For the inspection report, refer to Appendix 03 - Inspection Report (Additional

Work) .

(2) Subtask 240106-832-004-001 - Do a Detailed Inspection of the FSOV Bonding Lead

and of the Wires Located on Wing Rear Spar (LH side).

Work Zones and Access Panels

Zone Access/Work location

575 Access Panel 575DB, Panel 575CB, Panel 575FB

Work location from Rib 7A to Rib 8

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-0106

REVISION No.: 01 - Mar 26/13 Page: 25

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SERVICE BULLETIN

Manpower Resources

Manhours 1.50

Minimum number of person 1

Subtask elapsed time 1.50

Skills ELECTRICAL

Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

2 NSA5050-3 2 NUT (1)

3 E0088-10-80NN 1 LEAD (1)

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

shall be ordered as necessary through the given channel.

NOTE (1): The quantity depends on the result of the inspection.

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Fuel Tank Sealant

Polysulfid

09-002 As required

References

Elec. Std. Practices Manual (ESPM) 20-53-21

Fig. A-FBCAA

Area to be inspected (Additional Work)

Sheet 01

Fig. A-FFBAA

Flow Chart (Additional Work)

Sheet 01

(a) For the inspection area, refer to Fig. A-FBCAA.

(b) Do a detailed inspection of the length of the bonding lead, refer to Fig. A-FFBAA.

1 Depending on the inspection result:

a Remove:

1 Lead-Bonding Item (3)

attached with:

2 Bolt Item (1) Retain

2 Nut Item (2) Discard

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b Install:

1 Lead-Bonding E0088-10-80NN Item 3

with:

2 Bolt Item (1) Retained at

removal

and with:

2 Nut NSA5050-3 Item 2

NOTE: Do the alignment of the two clamps and seal them with:

Fuel Tank Sealant

Polysulfid

09-002 As required

(c) Do a detailed inspection of the wires, refer to Fig. A-FFBAA.

1 If there is no contact and no chafing, no further action is required.

2 If there is chafing, repair the wire(s), refer to ESPM 20-53-21.

(d) For the inspection report, refer to Appendix 03 - Inspection Report (Additional

Work) .

D. TEST

(1) Subtask 240106-865-004-001 - C/B Closing

Manpower Resources

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) 24-50-20, Page Block 001

24-50-40, Page Block 001

(a) If a wire has been repaired, remove the safety clips and/or tags and close/unlock

the following circuit breakers:

PANEL DESIGNATION FIN LOCATION SEE

NOTES

120VU PWR TRANSF/G/Y 6GL (1)

120VU RAM AIR/TEST/ and ELEC

PUMPS

1GK (1)

120VU HYD SHUT OFF

VALVES/WARN/IND

3GJ (1)

120VU HYD SHUT OFF

VALVES/CONTRL/ENG 2

4GJ (1)

NOTE (1): Refer to AMM 24-50-20, Page Block 001 for the C/B location.

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-0106

REVISION No.: 01 - Mar 26/13 Page: 27

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SERVICE BULLETIN

or remove the safety clips and/or tags and close/unlock the following circuit

breakers:

PANEL DESIGNATION FIN LOCATION SEE

NOTES

120VU PTU/CTL/G/Y 6GL (1)

120VU FIRE VALVES/ENG 2 4GJ (1)

101VU ELEC PUMPS (19GK) 63GK (1)

101VU ELEC PUMPS (20GK) 64GK (1)

129VU COCKPIT LTS/MAINT/PNL/MI

and/ANN LTS

1WB (1)

NOTE (1): Refer to AMM 24-50-20, Page Block 001 or to AMM 24-50-40, Page

Block 001 for the C/B location.

(2) Subtask 240106-700-002-001 - Testing

Manpower Resources

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) 20-28-11, Page Block 001

29-10-00, Page Block 501

(a) If a bonding lead has been replaced, do the check of the electrical bonding, refer to

AMM 20-28-11, Page Block 001.

NOTE: For the maximum Permissible Resistance Values, refer to the Table

AMM 20-28-11, Page Block 001.

(b) If a wire has been repaired, do a functional test of fire valves, refer to AMM

29-10-00, Page Block 501.

E. CLOSE-UP

(1) Subtask 240106-410-003-001 - Close the access panels on RH Side

Work Zones and Access Panels

Zone Access/Work location

675

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-21-57, Page Block 001

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

equipment.

(b) Close the access panels 675DB and/or 675CB and/or 675FB, refer to AMM

06-21-57, Page Block 001.

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-0106

REVISION No.: 01 - Mar 26/13 Page: 28

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(2) Subtask 240106-410-004-001 - Close the access panels on LH Side

Work Zones and Access Panels

Zone Access/Work location

575

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-21-57, Page Block 001

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

equipment.

(b) Close the access panels 575DB3 and/or 575CB and/or 575FB, refer to AMM

06-21-57, Page Block 001.

(3) Subtask 240106-942-002-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 52-10-00, Page Block 001

(a) Close the passenger/crew door 831, refer to AMM 52-10-00, Page Block 001.

(b) Remove the access platform(s).

(c) Restore the systems and the aircraft to normal operating condition.

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-0106

REVISION No.: 01 - Mar 26/13 Page: 29

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SERVICE BULLETIN

**CONF ALL

Z575 (Z675)

LH SIDE SHOWN

RH SIDE SYMMETRICAL

RIB8

RIB5

WIRES TO BE

RIB7A

AREA TO BE INSPECTED

NOTE:

BONDING

 LEAD TO BE

ELECTRICAL BONDING

REAR SPAR

INSPECTED

(1)

(2)

2 (3)

3

A

B

A

B

C

C

BONDING LEAD

TO BE INSPECTED

(2)

(1)

INSPECTED

2

A_SB_240106_5_BAAA_01_05

Figure A-FBAAA - Sheet 01

Area to be inspected

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-0106

REVISION No.: 01 - Mar 26/13 Page: 30

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SERVICE BULLETIN

**CONF ALL

QUESTION

ACTION

FINDING

AT THE THRESHOLD GIVEN IN THE PLANNING

INFORMATION PARAGRAPH E.(2).

NO BONDING LEAD (RH AND LH) IS YES

DO A DETAILED INSPECTION OF THE

LENGTH OF THE BONDING LEAD (RH AND LH)

DO A DETAILED INSPECTION OF THE FSOV BONDING LEAD (RH AND LH)

AND OF THE WIRES (RH AND LH) LOCATED ON WING REAR SPAR

REPLACE THE BONDING LEAD (RH AND LH)

NO CONTACT/CHAFING YES

REPAIR THE WIRE(S) (RH AND LH)

LENGTH OF THE

80 mm (3.15 in)

WITH THE LENGTH = 80 mm (3.15 in)

DO A DETAILED INSPECTION

OF THE WIRES (RH AND LH)

SEND TO AIRBUS THE INSPECTION

REPORT REFER TO APPENDIX 1

NO FURTHER ACTION

REFER TO ACCOMPLISHMENT INSTRUCTIONS

PARAGRAPH INSPECTION

(SUBTASK 240106−832−001−001 AND

240106−832−002−001)

PARAGRAPH INSPECTION

(SUBTASK 240106−832−001−001 AND

240106−832−002−001)

REFER TO ACCOMPLISHMENT INSTRUCTIONS

A_SB_240106_5_FAAA_01_01

Figure A-FFAAA - Sheet 01

Flow Chart

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-0106

REVISION No.: 01 - Mar 26/13 Page: 31

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SERVICE BULLETIN

**CONF ALL

Z575 (Z675)

LH SIDE SHOWN

RH SIDE SYMMETRICAL

RIB8

RIB5

WIRES TO BE

RIB7A

AREA TO BE INSPECTED

NOTE:

BONDING

 LEAD TO BE

ELECTRICAL BONDING

REAR SPAR

INSPECTED

(1)

(2)

2 (3)

3

A

B

A

B

C

C

BONDING LEAD

TO BE INSPECTED

(2)

(1)

INSPECTED

2

A_SB_240106_5_BCAA_01_01

Figure A-FBCAA - Sheet 01

Area to be inspected (Additional Work)

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-0106

REVISION No.: 01 - Mar 26/13 Page: 32

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SERVICE BULLETIN

**CONF ALL

QUESTION

ACTION

FINDING

AT THE THRESHOLD GIVEN IN THE PLANNING

INFORMATION PARAGRAPH E.(2).

NO BONDING LEAD (RH AND LH) IS YES

DO A DETAILED INSPECTION OF THE

LENGTH OF THE BONDING LEAD (RH AND LH)

DO A DETAILED INSPECTION OF THE FSOV BONDING LEAD (RH AND LH)

AND OF THE WIRES (RH AND LH) LOCATED ON WING REAR SPAR

REPLACE THE BONDING LEAD (RH AND LH)

NO CONTACT/CHAFING YES

REPAIR THE WIRE(S) (RH AND LH)

LENGTH OF THE

80 mm (3.15 in)

WITH THE LENGTH = 80 mm (3.15 in)

DO A DETAILED INSPECTION

OF THE WIRES (RH AND LH)

SEND TO AIRBUS THE INSPECTION

REPORT REFER TO APPENDIX 3

NO FURTHER ACTION

REFER TO ACCOMPLISHMENT INSTRUCTIONS

PARAGRAPH INSPECTION

(SUBTASK 240106−832−003−001 AND

240106−832−004−001)

PARAGRAPH INSPECTION

(SUBTASK 240106−832−003−001 AND

240106−832−004−001)

REFER TO ACCOMPLISHMENT INSTRUCTIONS

A_SB_240106_5_FBAA_01_01

Figure A-FFBAA - Sheet 01

Flow Chart (Additional Work)

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-0106

REVISION No.: 01 - Mar 26/13 Page: 33

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This Page Intentionally Left Blank

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-0106

REVISION No.: 01 - Mar 26/13 Page: 34

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SERVICE BULLETIN

Appendix 01 - Inspection Report

**CONF ALL

The results of the inspection, including no findings, replacement or action to be done, must be

forwarded to AIRBUS department SEEA6, on the attached inspection report sheet.

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-0106

REVISION No.: 01 - Mar 26/13 Page: 1

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SERVICE BULLETIN

Appendix 01 - Inspection Report

**CONF ALL

INSPECTION REPORT

SERVICE BULLETIN No. :

A/C MSN :

FLIGHT CYCLES :

FLIGHT HOURS :

A300−24−0106

DATE OF INSPECTION :

RETURN TO :

AIRBUS

CUSTOMER SERVICES ENGINEERING − SEEA6

ELECTRICAL INSTALLATION & ELECTRICAL

INSPECTION METHOD : DETAILED INSPECTION

STANDARD ITEMS

1 ROND POINT MAURICE BELLONTE

31707 BLAGNAC CEDEX

FRANCE

FAX +33 (0)5 61 93 44 25

LENGTH 80 mm (3.15 in)

BONDING LEAD

CONTACT/CHAFING

YES

NO

BONDING LEAD

WIRE(S) REPAIRED

REPLACED

WIRE(S)

YES

NO

YES

NO

N/A

YES

NO

N/A

N/A

N/A

LH SIDE

LENGTH 80 mm (3.15 in)

BONDING LEAD

CONTACT/CHAFING

YES

NO

BONDING LEAD

WIRE(S) REPAIRED

REPLACED

WIRE(S)

YES

NO

YES

NO

N/A

YES

NO

N/A

N/A

N/A

RH SIDE

A_SB_240106_5_RAAA_01_00

Figure A-FRAAA - Sheet 01

Inspection Report

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-0106

REVISION No.: 01 - Mar 26/13 Page: 2

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SERVICE BULLETIN

Appendix 02 - Gantt Chart

**CONF ALL

(1) For detail concerning the elapsed time assumption of the modification, refer to the Gantt chart

shown in the next page :

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-0106

REVISION No.: 01 - Mar 26/13 Page: 1

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SERVICE BULLETIN

Appendix 02 - Gantt Chart

**CONF ALL

ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A300−24−0106

ELAPSED TIME

(HOURS)

NOTE: THIS CHART IS ONLY A PROPOSAL.

OPERATORS MAY DETERMINE THAT ANOTHER WAY

TO DO THE WORK IS MORE SUITABLE FOR THEM.

MH ET PER

MH:

ET:

PER:

MANHOURS

ELAPSED TIME

NUMBER OF PERSONS

TOTAL MANHOURS (MH)

ELAPSED TIME (ET)

8.00

4.50

STEPS

0 1

GET ACCESS 2.00 1.00 2

1.50 1.50 1

CLOSE−UP 2.00 1.00 2

OF THE SHUT−OFF VALVE

DO A DETAILED INSPECTION

BONDING LEAD AND WIRE

TEST 1.00 1.00 1

2345

(LH SIDE)

1.50 1.50 1 OF THE SHUT−OFF VALVE

DO A DETAILED INSPECTION

BONDING LEAD AND WIRE

(RH SIDE)

A_SB_240106_5_ABAA_01_02

Figure A-FABAA - Sheet 01

Gantt Chart

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-0106

REVISION No.: 01 - Mar 26/13 Page: 2

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SERVICE BULLETIN

Appendix 03 - Inspection Report (Additional Work)

**CONF ALL

(1) The results of the inspection, including no findings, replacement or action to be done, must be

forwarded to AIRBUS department SEEA6, on the attached inspection report sheet.

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-0106

REVISION No.: 01 - Mar 26/13 Page: 1

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SERVICE BULLETIN

Appendix 03 - Inspection Report (Additional Work)

**CONF ALL

INSPECTION REPORT

SERVICE BULLETIN No. :

A/C MSN :

FLIGHT CYCLES :

FLIGHT HOURS :

A300−24−0106

DATE OF INSPECTION :

RETURN TO :

AIRBUS

CUSTOMER SERVICES ENGINEERING − SEEA6

ELECTRICAL INSTALLATION & ELECTRICAL

INSPECTION METHOD : DETAILED INSPECTION

STANDARD ITEMS

1 ROND POINT MAURICE BELLONTE

31707 BLAGNAC CEDEX

FRANCE

FAX +33 (0)5 61 93 44 25

LENGTH 80 mm (3.15 in)

BONDING LEAD

CONTACT/CHAFING

YES

NO

BONDING LEAD

WIRE(S) REPAIRED

REPLACED

WIRE(S)

YES

NO

YES

NO

N/A

YES

NO

N/A

N/A

N/A

LH SIDE

LENGTH 80 mm (3.15 in)

BONDING LEAD

CONTACT/CHAFING

YES

NO

BONDING LEAD

WIRE(S) REPAIRED

REPLACED

WIRE(S)

YES

NO

YES

NO

N/A

YES

NO

N/A

N/A

N/A

RH SIDE

A_SB_240106_5_RBAA_01_00

Figure A-FRBAA - Sheet 01

Inspection Report (Additional Work)

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-0106

REVISION No.: 01 - Mar 26/13 Page: 2

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SERVICE BULLETIN

Appendix 04 - Gantt Chart (Additional Work)

**CONF ALL

(1) The following Gantt Chart is only a proposal. Operators may determine that another way to do the

work is more suitable for them.

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-0106

REVISION No.: 01 - Mar 26/13 Page: 1

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SERVICE BULLETIN

Appendix 04 - Gantt Chart (Additional Work)

**CONF ALL

ELAPSED TIME ASSUMPTION SERVICE BULLETIN No A300−24−0106

MH ET/S

TOTAL MANHOURS

SB ELAPSED TIME

8.00

4.50

STEPS

2.00 1.00

0 5

1.50 1.50

1.50 1.50

2.00 1.00

MH

ET/S:

PER

MANHOURS

ELAPSED TIME PER STEP

NUMBER OF PERSONS

01

02

THIS CHART IS ONLY A PROPOSAL.

OPERATORS MAY DETERMINE THAT ANOTHER WAY

TO DO THE WORK IS MORE SUITABLE FOR THEM.

01

02

NOTE:

PER

2

1

1

2

1.00 1.00 1

:

:

SB ELAPSED TIME

(HOURS)

1 2 3 4

IF A VSB IS INVOLVED, THE ASSOCIATED MANHOURS

ARE NOT REFLECTED IN THIS GANTT CHART.

GET ACCESS

CLOSE−UP

OF THE SHUT−OFF VALVE

DO A DETAILED INSPECTION

BONDING LEAD AND WIRE

TEST

(LH SIDE)

OF THE SHUT−OFF VALVE

DO A DETAILED INSPECTION

BONDING LEAD AND WIRE

(RH SIDE)

A_SB_240106_5_ADAA_01_00

Figure A-FADAA - Sheet 01

Gantt Chart (Additional Work)

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-0106

REVISION No.: 01 - Mar 26/13 Page: 2

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SERVICE BULLETIN

REPORTING SHEET

TITLE: ELECTRICAL POWER-INSPECTION OF SHUT-OFF VALVE BONDING

LEAD

MODIFICATION No.: None

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: Jul 09/10 SERVICE BULLETIN No.: A300-24-0106

REVISION No.: 01 - Mar 26/13 Page: 1

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SERVICE BULLETIN

QUALITY PERCEPTION FORM

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

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

improve the quality of our Service Bulletins.

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

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

- Quality rating of this SB 4321

- Quality rating of the Accomplishment Instructions 4321

- Quality rating of the Illustrations 4321

- Is this SB easy to understand ? Y/N

If you have had difficulties in the accomplishment of this SB please quote below the area(s) and give a

short description of the issue.

Planning Material Instructions

X Effectivity X Kit content X Preparation

X Reason X List of Materials Operator Supplied X Mod/Inspection

X Manpower X Industry support X Test

X References X Re-identification X Close-Up

X Publication X Tooling X Illustrations

Comments:

Operator: Date:

Name/Title:

Please return this form to:

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX FRANCE

Attn : SEM4 Service Bulletins Management

FAX : (33) 5 61 93 42 51

Or via your Resident Customer Support Office.

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-0106

REVISION No.: 01 - Mar 26/13 Page: 1

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