@A300-600

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: ELECTRIC AND ELECTRONIC COMMON INSTALLATIONS - IMPROVE

WING WIRING INSTALLATION

MODIFICATION No.: 13397S22766 13399S22768 13516H5723

This page transmits Revision No.03 of Service Bulletin No.A300-24-6103

ADDITIONAL WORK

**CONF ALL

Additional work is required by this revision for aircraft modified by any previous issue.

Additional work between Revision No. 00 and No. 03 consists in modifying the routing of routes 1P, 2P,

1E,1G, 2E and 2G.

Additional work between Revision No. 01 and No. 03 consists in modifying the routing of routes 1P, 2P,

1E,1G, 2E and 2G.

Additional work between Revision No. 02 and No. 03 consist in modifying the installation of clamps in

LH and RH wings.

REASON

Revision No. 03 issued to update the installation of clamps in LH and RH wings and on the passage

way to the shroud box at LH and RH sides.

CHANGES

The main changes of this revision are:

- create a config. 003 for aircraft post modification No. 06127S6951,

- modify the substask for config. 001 and config. 002 for the passage way to the shroud box at LH

and RH sides,

- create the substask for config. 003 for the passage way to the shroud box at LH and RH sides,

- create the KIT A04 and KIT A05 for config. 003,

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 1

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

- modify the substask for config. 001 and config. 002 for the installation of clamps in LH and RH

wings,

- update Material effectivity and Material price,

- update the procedure paragraph,

- update the CML,

- add a task ADDITIONAL WORK for the installation of clamp in LH and RH wings.

FRONT MATTER

ELECTRIC AND ELECTRONIC COMMON

INSTALLATIONS - IMPROVE WING

WIRING INSTALLATION

CONFIGURATION UPDATED R

SUMMARY

REASON/DESCRIPTION/OPERATIONAL

CONSEQUENCES

REASON UPDATED R

GENERAL EVALUATION GENERAL EVALUATION TABLE UPDATED R

MATERIAL PRICE INFORMATION MATERIAL PRICE INFORMATION TABLE

UPDATED

R

MATERIAL PRICE INFORMATION TABLE

UPDATED

R

MATERIAL PRICE INFORMATION TABLE ADDED N

EFFECTIVITY OPERATOR LIST UPDATED R

REFERENCES / REPERCUSSIONS REFERENCES/REPERCUSSIONS TABLE

UPDATED

R

MANPOWER MANPOWER UPDATED R

MANPOWER UPDATED R

MANPOWER ADDED N

APPENDICES APPENDICES UPDATED R

PLANNING INFORMATION

EFFECTIVITY EFFECTIVITY RELATED INFORMATION

UPDATED

R

Configuration definition CONFIGURATION LIST UPDATED R

CONF 001 CONFIGURATION DEFINITION UPDATED

CONFIGURATION DESCRIPTION UPDATED

R

CONF 002 CONFIGURATION DEFINITION UPDATED

CONFIGURATION DESCRIPTION UPDATED

R

CONF 003 CONFIGURATION ADDED N

Material Effectivity MATERIAL EFFECTIVITY UPDATED

MATERIAL SET UPDATED

MATERIAL SET QUANTITY UPDATED

R

MATERIAL EFFECTIVITY UPDATED

MATERIAL SET UPDATED

MATERIAL SET QUANTITY UPDATED

R

MATERIAL EFFECTIVITY ADDED N

REASON

History HISTORY UPDATED R

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 2

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

DESCRIPTION DESCRIPTION UPDATED R

COMPLIANCE

Accomplishment Timescale ACCOMPLISHMENT TIMESCALE UPDATED R

MANPOWER MANPOWER UPDATED

CONFIGURATION UPDATED

R

MANPOWER UPDATED

CONFIGURATION UPDATED

R

MANPOWER ADDED N

REFERENCES REFERENCED DOCUMENTATION UPDATED R

REFERENCED DOCUMENTATION UPDATED R

REFERENCED DOCUMENTATION ADDED N

MATERIAL INFORMATION

MATERIAL - PRICE AND AVAILABILITY

Procurement Addresses PROCUREMENT ADDRESSES UPDATED

MATERIAL SET UPDATED

R

Price and Availability PRICE AND AVAILABILITY UPDATED

MATERIAL AVAILABILITY UPDATED

MATERIAL PRICE UPDATED

MATERIAL SET UPDATED

R

LIST OF COMPONENTS LIST OF COMPONENTS UPDATED R

Kit 246103A01R14 PART MATERIAL SET UPDATED

MATERIAL SET LABEL UPDATED

QUANTITY UPDATED

ITEM NUMBER UPDATED

PART NUMBER UPDATED

KEYWORD UPDATED

R

Kit 246103A02R12 PART MATERIAL SET UPDATED

MATERIAL SET LABEL UPDATED

QUANTITY UPDATED

ITEM NUMBER UPDATED

PART NUMBER UPDATED

KEYWORD UPDATED

R

Kit 246103A03R04 PART MATERIAL SET UPDATED

QUANTITY UPDATED

MATERIAL SET LABEL UPDATED

ITEM NUMBER UPDATED

PART NUMBER UPDATED

KEYWORD UPDATED

R

Kit 246103A04R00 PART MATERIAL SET ADDED N

Kit 246103A05R00 PART MATERIAL SET ADDED N

Supplementary Kit 246103A01S11 PART MATERIAL SET ADDED N

Supplementary Kit 246103A01S12 PART MATERIAL SET ADDED N

Supplementary Kit 246103A01S13 PART MATERIAL SET ADDED N

Supplementary Kit 246103A02S10 PART MATERIAL SET ADDED N

Supplementary Kit 246103A02S11 PART MATERIAL SET ADDED N

Supplementary Kit 246103A03S01 PART MATERIAL SET ADDED N

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 3

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Kit 246103B02R02 PART MATERIAL SET UPDATED

MATERIAL SET LABEL UPDATED

QUANTITY UPDATED

R

LIST OF MATERIALS - OPERATOR

SUPPLIED

Consumable Materials

Consumable CMLA01 CONSUMABLE MATERIAL SET UPDATED

CONSUMABLE UPDATED

QUANTITY UPDATED

R

Consumable CMLB01 CONSUMABLE MATERIAL SET UPDATED

CONSUMABLE UPDATED

R

Components COMPONENTS UPDATED R

Component COMPB01 PART MATERIAL SET ADDED N

ACCOMPLISHMENT INSTRUCTIONS

TASK 246103- 831-801-001-Modification TASK SOLUTION UPDATED

NOTE UPDATED

CAUTION UPDATED

R

Task associated data - 001 ZONE UPDATED

PANEL UPDATED

MAN HOURS UPDATED

R

Task associated data - 002 ZONE UPDATED

PANEL UPDATED

MAN HOURS UPDATED

R

Task associated data - 003 TASK ASSOCIATED DATA ADDED N

Subtask 246103-839-401-001 SUBTASK SOLUTION ADDED N

Subtask 246103-910-001-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

Subtask 246103-910-401-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

Subtask 246103-839-401-001 SUBTASK SOLUTION ADDED N

Subtask 246103-910-001-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

Subtask 246103-910-401-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

Subtask 246103-839-001-001 SUBTASK SOLUTION ADDED N

Subtask 246103-839-401-001 SUBTASK SOLUTION ADDED N

Subtask 246103-910-001-001 SUBTASK SOLUTION ADDED N

Subtask 246103-910-401-001 SUBTASK SOLUTION ADDED N

Subtask 246103-941-001-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

NOTE UPDATED

REFERENCES UPDATED

R

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 4

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Subtask 246103-941-401-001 SUBTASK SOLUTION UPDATED

MANPOWER RESSOURCE UPDATED

LOCATION UPDATED

ZONE UPDATED

REFERENCES UPDATED

PANEL UPDATED

REFERENCED DOCUMENTATION UPDATED

NOTE UPDATED

CIRCUIT BREAKER UPDATED

R

Subtask 246103-941-001-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

NOTE UPDATED

REFERENCES UPDATED

R

Subtask 246103-941-401-001 SUBTASK SOLUTION UPDATED

MANPOWER RESSOURCE UPDATED

LOCATION UPDATED

ZONE UPDATED

REFERENCES UPDATED

PANEL UPDATED

REFERENCED DOCUMENTATION UPDATED

NOTE UPDATED

CIRCUIT BREAKER UPDATED

R

Subtask 246103-941-001-001 SUBTASK SOLUTION ADDED N

Subtask 246103-941-401-001 SUBTASK SOLUTION ADDED N

Subtask 246103-831-001-001 SUBTASK SOLUTION UPDATED R

Subtask 246103-831-019-001 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

ITEM NUMBER UPDATED

PART NUMBER UPDATED

KEYWORD UPDATED

PART NUMBER DESCRIPTION UPDATED

MATERIAL LIST UPDATED

NOTE UPDATED

R

Subtask 246103-420-001-001 SUBTASK SOLUTION UPDATED

MATERIAL LIST UPDATED

R

Subtask 246103-831-003-001 SUBTASK SOLUTION UPDATED

MATERIAL LIST UPDATED

R

Subtask 246103-831-006-001 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

ITEM NUMBER UPDATED

PART NUMBER UPDATED

KEYWORD UPDATED

CONSUMABLE UPDATED

REFERENCED DOCUMENTATION UPDATED

CONFIGURATION UPDATED

FIGURE REFERENCE UPDATED

PART NUMBER DESCRIPTION UPDATED

NOTE UPDATED

MATERIAL LIST UPDATED

REFERENCES UPDATED

R

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 5

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Subtask 246103-831-010-001 SUBTASK SOLUTION UPDATED

MATERIAL LIST UPDATED

R

Subtask 246103-831-011-001 SUBTASK SOLUTION UPDATED

CONSUMABLE UPDATED

QUANTITY UPDATED

NOTE UPDATED

MATERIAL LIST UPDATED

R

Subtask 246103-831-012-001 SUBTASK SOLUTION UPDATED

MATERIAL LIST UPDATED

R

Subtask 246103-020-002-001 SUBTASK SOLUTION UPDATED R

Subtask 246103-831-005-001 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

ITEM NUMBER UPDATED

PART NUMBER UPDATED

KEYWORD UPDATED

PART NUMBER DESCRIPTION UPDATED

MATERIAL LIST UPDATED

NOTE UPDATED

R

Subtask 246103-420-002-001 SUBTASK SOLUTION UPDATED

MATERIAL LIST UPDATED

R

Subtask 246103-831-004-001 SUBTASK SOLUTION UPDATED

MATERIAL LIST UPDATED

R

Subtask 246103-831-007-001 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

ITEM NUMBER UPDATED

PART NUMBER UPDATED

KEYWORD UPDATED

CONSUMABLE UPDATED

REFERENCED DOCUMENTATION UPDATED

CONFIGURATION UPDATED

FIGURE REFERENCE UPDATED

PART NUMBER DESCRIPTION UPDATED

NOTE UPDATED

MATERIAL LIST UPDATED

REFERENCES UPDATED

R

Subtask 246103-831-013-001 SUBTASK SOLUTION UPDATED

MATERIAL LIST UPDATED

R

Subtask 246103-020-003-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

ITEM NUMBER UPDATED

FIGURE REFERENCE UPDATED

R

Subtask 246103-831-016-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

ITEM NUMBER UPDATED

FIGURE REFERENCE UPDATED

R

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 6

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Subtask 246103-831-401-001 SUBTASK SOLUTION UPDATED

ZONE UPDATED

QUANTITY UPDATED

ITEM NUMBER UPDATED

PART NUMBER UPDATED

KEYWORD UPDATED

CONSUMABLE UPDATED

CONFIGURATION UPDATED

NOTE UPDATED

PART NUMBER DESCRIPTION UPDATED

LOCATION UPDATED

MANPOWER RESSOURCE UPDATED

MATERIAL LIST UPDATED

FIGURE REFERENCE UPDATED

R

Subtask 246103-831-008-001 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

ITEM NUMBER UPDATED

PART NUMBER UPDATED

KEYWORD UPDATED

PART NUMBER DESCRIPTION UPDATED

MATERIAL LIST UPDATED

R

Subtask 246103-831-009-001 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

ITEM NUMBER UPDATED

PART NUMBER UPDATED

KEYWORD UPDATED

PART NUMBER DESCRIPTION UPDATED

MATERIAL LIST UPDATED

R

Subtask 246103-831-017-001 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

PART NUMBER UPDATED

ITEM NUMBER UPDATED

KEYWORD UPDATED

CONFIGURATION UPDATED

PART NUMBER DESCRIPTION UPDATED

MATERIAL LIST UPDATED

FIGURE REFERENCE UPDATED

R

Subtask 246103-831-018-001 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

PART NUMBER UPDATED

ITEM NUMBER UPDATED

KEYWORD UPDATED

CONFIGURATION UPDATED

PART NUMBER DESCRIPTION UPDATED

MATERIAL LIST UPDATED

FIGURE REFERENCE UPDATED

R

Subtask 246103-831-402-001 SUBTASK SOLUTION UPDATED

ZONE UPDATED

CONFIGURATION UPDATED

LOCATION UPDATED

FIGURE REFERENCE UPDATED

R

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 7

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Subtask 246103-831-403-001 SUBTASK SOLUTION UPDATED

ZONE UPDATED

CONFIGURATION UPDATED

LOCATION UPDATED

FIGURE REFERENCE UPDATED

R

Subtask 246103-831-405-001 SUBTASK SOLUTION ADDED N

Subtask 246103-831-406-001 SUBTASK SOLUTION ADDED N

Subtask 246103-831-407-001 SUBTASK SOLUTION ADDED N

Subtask 246103-831-001-001 SUBTASK SOLUTION UPDATED R

Subtask 246103-831-019-001 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

ITEM NUMBER UPDATED

PART NUMBER UPDATED

KEYWORD UPDATED

PART NUMBER DESCRIPTION UPDATED

MATERIAL LIST UPDATED

NOTE UPDATED

R

Subtask 246103-420-001-001 SUBTASK SOLUTION UPDATED

MATERIAL LIST UPDATED

R

Subtask 246103-831-003-001 SUBTASK SOLUTION UPDATED

MATERIAL LIST UPDATED

R

Subtask 246103-831-006-001 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

ITEM NUMBER UPDATED

PART NUMBER UPDATED

KEYWORD UPDATED

CONSUMABLE UPDATED

REFERENCED DOCUMENTATION UPDATED

CONFIGURATION UPDATED

FIGURE REFERENCE UPDATED

PART NUMBER DESCRIPTION UPDATED

NOTE UPDATED

MATERIAL LIST UPDATED

REFERENCES UPDATED

R

Subtask 246103-831-010-001 SUBTASK SOLUTION UPDATED

MATERIAL LIST UPDATED

R

Subtask 246103-831-011-001 SUBTASK SOLUTION UPDATED

CONSUMABLE UPDATED

QUANTITY UPDATED

NOTE UPDATED

MATERIAL LIST UPDATED

R

Subtask 246103-831-012-001 SUBTASK SOLUTION UPDATED

MATERIAL LIST UPDATED

R

Subtask 246103-020-002-001 SUBTASK SOLUTION UPDATED R

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 8

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REVISION TRANSMITTAL SHEET

Subtask 246103-831-005-001 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

ITEM NUMBER UPDATED

PART NUMBER UPDATED

KEYWORD UPDATED

PART NUMBER DESCRIPTION UPDATED

MATERIAL LIST UPDATED

NOTE UPDATED

R

Subtask 246103-420-002-001 SUBTASK SOLUTION UPDATED

MATERIAL LIST UPDATED

R

Subtask 246103-831-004-001 SUBTASK SOLUTION UPDATED

MATERIAL LIST UPDATED

R

Subtask 246103-831-007-001 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

ITEM NUMBER UPDATED

PART NUMBER UPDATED

KEYWORD UPDATED

CONSUMABLE UPDATED

REFERENCED DOCUMENTATION UPDATED

CONFIGURATION UPDATED

FIGURE REFERENCE UPDATED

PART NUMBER DESCRIPTION UPDATED

NOTE UPDATED

MATERIAL LIST UPDATED

REFERENCES UPDATED

R

Subtask 246103-831-013-001 SUBTASK SOLUTION UPDATED

MATERIAL LIST UPDATED

R

Subtask 246103-020-003-002 SUBTASK SOLUTION UPDATED

ITEM NUMBER UPDATED

R

Subtask 246103-831-016-003 SUBTASK SOLUTION UPDATED

ITEM NUMBER UPDATED

R

Subtask 246103-831-401-002 SUBTASK SOLUTION UPDATED

ZONE UPDATED

QUANTITY UPDATED

CONSUMABLE UPDATED

FIGURE REFERENCE UPDATED

CONFIGURATION UPDATED

ITEM NUMBER UPDATED

PART NUMBER UPDATED

PART NUMBER DESCRIPTION UPDATED

LOCATION UPDATED

MANPOWER RESSOURCE UPDATED

MATERIAL LIST UPDATED

REFERENCES UPDATED

R

Subtask 246103-831-008-001 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

ITEM NUMBER UPDATED

PART NUMBER UPDATED

KEYWORD UPDATED

PART NUMBER DESCRIPTION UPDATED

MATERIAL LIST UPDATED

R

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 9

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Subtask 246103-831-009-001 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

ITEM NUMBER UPDATED

PART NUMBER UPDATED

KEYWORD UPDATED

PART NUMBER DESCRIPTION UPDATED

MATERIAL LIST UPDATED

R

Subtask 246103-831-017-003 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

ITEM NUMBER UPDATED

PART NUMBER UPDATED

KEYWORD UPDATED

PART NUMBER DESCRIPTION UPDATED

MATERIAL LIST UPDATED

R

Subtask 246103-831-018-003 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

ITEM NUMBER UPDATED

PART NUMBER UPDATED

KEYWORD UPDATED

PART NUMBER DESCRIPTION UPDATED

MATERIAL LIST UPDATED

R

Subtask 246103-831-402-003 SUBTASK SOLUTION UPDATED

ZONE UPDATED

LOCATION UPDATED

R

Subtask 246103-831-403-005 SUBTASK SOLUTION UPDATED

ZONE UPDATED

LOCATION UPDATED

R

Subtask 246103-831-405-002 SUBTASK SOLUTION ADDED N

Subtask 246103-831-406-002 SUBTASK SOLUTION ADDED N

Subtask 246103-831-407-002 SUBTASK SOLUTION ADDED N

Subtask 246103-831-001-001 SUBTASK SOLUTION ADDED N

Subtask 246103-831-019-001 SUBTASK SOLUTION ADDED N

Subtask 246103-420-001-001 SUBTASK SOLUTION ADDED N

Subtask 246103-831-003-001 SUBTASK SOLUTION ADDED N

Subtask 246103-831-006-002 SUBTASK SOLUTION ADDED N

Subtask 246103-831-010-001 SUBTASK SOLUTION ADDED N

Subtask 246103-831-011-001 SUBTASK SOLUTION ADDED N

Subtask 246103-831-012-001 SUBTASK SOLUTION ADDED N

Subtask 246103-020-002-001 SUBTASK SOLUTION ADDED N

Subtask 246103-831-005-001 SUBTASK SOLUTION ADDED N

Subtask 246103-420-002-001 SUBTASK SOLUTION ADDED N

Subtask 246103-831-004-001 SUBTASK SOLUTION ADDED N

Subtask 246103-831-007-002 SUBTASK SOLUTION ADDED N

Subtask 246103-831-013-001 SUBTASK SOLUTION ADDED N

Subtask 246103-020-003-001 SUBTASK SOLUTION ADDED N

Subtask 246103-831-016-001 SUBTASK SOLUTION ADDED N

Subtask 246103-831-401-001 SUBTASK SOLUTION ADDED N

Subtask 246103-831-008-001 SUBTASK SOLUTION ADDED N

Subtask 246103-831-009-001 SUBTASK SOLUTION ADDED N

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 10

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REVISION TRANSMITTAL SHEET

Subtask 246103-831-017-001 SUBTASK SOLUTION ADDED N

Subtask 246103-831-018-001 SUBTASK SOLUTION ADDED N

Subtask 246103-831-402-001 SUBTASK SOLUTION ADDED N

Subtask 246103-831-403-001 SUBTASK SOLUTION ADDED N

Subtask 246103-831-405-001 SUBTASK SOLUTION ADDED N

Subtask 246103-831-406-001 SUBTASK SOLUTION ADDED N

Subtask 246103-831-407-001 SUBTASK SOLUTION ADDED N

Subtask 246103-700-001-001 SUBTASK SOLUTION ADDED N

Subtask 246103-942-001-001 SUBTASK SOLUTION UPDATED R

Subtask 246103-942-401-001 SUBTASK SOLUTION UPDATED

LOCATION UPDATED

PANEL UPDATED

ZONE UPDATED

R

Subtask 246103-942-001-001 SUBTASK SOLUTION UPDATED R

Subtask 246103-942-401-001 SUBTASK SOLUTION UPDATED

LOCATION UPDATED

PANEL UPDATED

ZONE UPDATED

R

Subtask 246103-942-001-001 SUBTASK SOLUTION ADDED N

Subtask 246103-942-401-001 SUBTASK SOLUTION ADDED N

TASK 246103- 831-802-001-Modification -

ADDITIONAL WORK between Revision

No. 00 and Revision No. 03

TASK SOLUTION UPDATED

TASK TITLE UPDATED

NOTE UPDATED

CAUTION UPDATED

R

Task associated data - 003 TASK ASSOCIATED DATA ADDED N

Subtask 246103-910-002-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

Subtask 246103-910-002-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

Subtask 246103-839-002-001 SUBTASK SOLUTION ADDED N

Subtask 246103-910-002-001 SUBTASK SOLUTION ADDED N

Subtask 246103-941-002-001 SUBTASK SOLUTION UPDATED

NOTE UPDATED

R

Subtask 246103-941-002-001 SUBTASK SOLUTION UPDATED

NOTE UPDATED

R

Subtask 246103-941-002-001 SUBTASK SOLUTION ADDED N

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 11

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Subtask 246103-831-028-001 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

ITEM NUMBER UPDATED

PART NUMBER UPDATED

KEYWORD UPDATED

CONSUMABLE UPDATED

REFERENCED DOCUMENTATION UPDATED

CONFIGURATION UPDATED

PART NUMBER DESCRIPTION UPDATED

FIGURE REFERENCE UPDATED

NOTE UPDATED

MATERIAL LIST UPDATED

REFERENCES UPDATED

R

Subtask 246103-831-020-001 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

ITEM NUMBER UPDATED

PART NUMBER UPDATED

KEYWORD UPDATED

CONSUMABLE UPDATED

REFERENCED DOCUMENTATION UPDATED

CONFIGURATION UPDATED

PART NUMBER DESCRIPTION UPDATED

FIGURE REFERENCE UPDATED

NOTE UPDATED

MATERIAL LIST UPDATED

REFERENCES UPDATED

R

Subtask 246103-831-021-001 SUBTASK SOLUTION UPDATED R

Subtask 246103-831-024-001 SUBTASK SOLUTION UPDATED R

Subtask 246103-831-025-001 SUBTASK SOLUTION UPDATED R

Subtask 246103-400-001-001 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

PART NUMBER UPDATED

KEYWORD UPDATED

ITEM NUMBER UPDATED

CONSUMABLE UPDATED

NOTE UPDATED

PART NUMBER DESCRIPTION UPDATED

MATERIAL LIST UPDATED

R

Subtask 246103-400-002-001 SUBTASK SOLUTION UPDATED R

Subtask 246103-400-003-001 SUBTASK SOLUTION UPDATED R

Subtask 246103-020-004-001 SUBTASK SOLUTION UPDATED R

Subtask 246103-831-026-001 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

R

Subtask 246103-831-029-001 SUBTASK SOLUTION UPDATED R

Subtask 246103-420-005-001 SUBTASK SOLUTION UPDATED R

Subtask 246103-420-003-001 SUBTASK SOLUTION UPDATED R

Subtask 246103-020-005-001 SUBTASK SOLUTION UPDATED R

Subtask 246103-831-027-001 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

R

Subtask 246103-831-030-001 SUBTASK SOLUTION UPDATED R

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 12

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Subtask 246103-420-006-001 SUBTASK SOLUTION UPDATED R

Subtask 246103-420-004-001 SUBTASK SOLUTION UPDATED R

Subtask 246103-831-028-001 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

ITEM NUMBER UPDATED

PART NUMBER UPDATED

KEYWORD UPDATED

CONSUMABLE UPDATED

REFERENCED DOCUMENTATION UPDATED

CONFIGURATION UPDATED

PART NUMBER DESCRIPTION UPDATED

FIGURE REFERENCE UPDATED

NOTE UPDATED

MATERIAL LIST UPDATED

REFERENCES UPDATED

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Subtask 246103-831-020-001 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

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KEYWORD UPDATED

CONSUMABLE UPDATED

REFERENCED DOCUMENTATION UPDATED

CONFIGURATION UPDATED

PART NUMBER DESCRIPTION UPDATED

FIGURE REFERENCE UPDATED

NOTE UPDATED

MATERIAL LIST UPDATED

REFERENCES UPDATED

R

Subtask 246103-831-021-001 SUBTASK SOLUTION UPDATED R

Subtask 246103-831-024-001 SUBTASK SOLUTION UPDATED R

Subtask 246103-831-025-001 SUBTASK SOLUTION UPDATED R

Subtask 246103-400-001-001 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

PART NUMBER UPDATED

KEYWORD UPDATED

ITEM NUMBER UPDATED

CONSUMABLE UPDATED

NOTE UPDATED

PART NUMBER DESCRIPTION UPDATED

MATERIAL LIST UPDATED

R

Subtask 246103-400-002-001 SUBTASK SOLUTION UPDATED R

Subtask 246103-400-003-001 SUBTASK SOLUTION UPDATED R

Subtask 246103-020-004-001 SUBTASK SOLUTION UPDATED R

Subtask 246103-831-026-001 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

R

Subtask 246103-831-029-001 SUBTASK SOLUTION UPDATED R

Subtask 246103-420-005-001 SUBTASK SOLUTION UPDATED R

Subtask 246103-420-003-001 SUBTASK SOLUTION UPDATED R

Subtask 246103-020-005-001 SUBTASK SOLUTION UPDATED R

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 13

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Subtask 246103-831-027-001 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

R

Subtask 246103-831-030-001 SUBTASK SOLUTION UPDATED R

Subtask 246103-420-006-001 SUBTASK SOLUTION UPDATED R

Subtask 246103-420-004-001 SUBTASK SOLUTION UPDATED R

Subtask 246103-831-028-002 SUBTASK SOLUTION ADDED N

Subtask 246103-831-020-002 SUBTASK SOLUTION ADDED N

Subtask 246103-831-021-001 SUBTASK SOLUTION ADDED N

Subtask 246103-831-024-001 SUBTASK SOLUTION ADDED N

Subtask 246103-831-025-001 SUBTASK SOLUTION ADDED N

Subtask 246103-400-001-001 SUBTASK SOLUTION ADDED N

Subtask 246103-400-002-001 SUBTASK SOLUTION ADDED N

Subtask 246103-400-003-001 SUBTASK SOLUTION ADDED N

Subtask 246103-020-004-001 SUBTASK SOLUTION ADDED N

Subtask 246103-831-026-001 SUBTASK SOLUTION ADDED N

Subtask 246103-831-029-001 SUBTASK SOLUTION ADDED N

Subtask 246103-420-005-001 SUBTASK SOLUTION ADDED N

Subtask 246103-420-003-001 SUBTASK SOLUTION ADDED N

Subtask 246103-020-005-001 SUBTASK SOLUTION ADDED N

Subtask 246103-831-027-001 SUBTASK SOLUTION ADDED N

Subtask 246103-831-030-001 SUBTASK SOLUTION ADDED N

Subtask 246103-420-006-001 SUBTASK SOLUTION ADDED N

Subtask 246103-420-004-001 SUBTASK SOLUTION ADDED N

Subtask 246103-700-002-001 SUBTASK SOLUTION ADDED N

Subtask 246103-942-002-001 SUBTASK SOLUTION UPDATED R

Subtask 246103-942-002-001 SUBTASK SOLUTION UPDATED R

Subtask 246103-942-002-001 SUBTASK SOLUTION ADDED N

TASK 246103- 831-804-001-Modification -

ADDITIONAL WORK between Revision

No. 01 and Revision No. 03

TASK SOLUTION UPDATED

TASK TITLE UPDATED

NOTE UPDATED

CAUTION UPDATED

R

Task associated data - 002 ZONE UPDATED R

Task associated data - 003 TASK ASSOCIATED DATA ADDED N

Subtask 246103-910-003-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

Subtask 246103-910-003-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

Subtask 246103-839-003-001 SUBTASK SOLUTION ADDED N

Subtask 246103-910-003-001 SUBTASK SOLUTION ADDED N

Subtask 246103-941-003-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

NOTE UPDATED

REFERENCES UPDATED

R

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REFERENCED DOCUMENTATION UPDATED

NOTE UPDATED

REFERENCES UPDATED

R

Subtask 246103-941-003-001 SUBTASK SOLUTION ADDED N

Subtask 246103-020-006-001 SUBTASK SOLUTION UPDATED R

Subtask 246103-831-031-001 SUBTASK SOLUTION UPDATED R

Subtask 246103-420-007-001 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

MATERIAL LIST UPDATED

R

Subtask 246103-420-009-001 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

R

Subtask 246103-831-033-001 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

ITEM NUMBER UPDATED

PART NUMBER UPDATED

KEYWORD UPDATED

CONSUMABLE UPDATED

FIGURE REFERENCE UPDATED

REFERENCED DOCUMENTATION UPDATED

CONFIGURATION UPDATED

PART NUMBER DESCRIPTION UPDATED

NOTE UPDATED

MATERIAL LIST UPDATED

REFERENCES UPDATED

R

Subtask 246103-831-034-001 SUBTASK SOLUTION UPDATED R

Subtask 246103-420-011-001 SUBTASK SOLUTION UPDATED

CONSUMABLE UPDATED

MATERIAL LIST UPDATED

R

Subtask 246103-831-035-001 SUBTASK SOLUTION UPDATED R

Subtask 246103-020-007-001 SUBTASK SOLUTION UPDATED R

Subtask 246103-831-032-001 SUBTASK SOLUTION UPDATED R

Subtask 246103-420-008-001 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

MATERIAL LIST UPDATED

R

Subtask 246103-420-010-001 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

R

Subtask 246103-831-050-001 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

ITEM NUMBER UPDATED

PART NUMBER UPDATED

KEYWORD UPDATED

CONSUMABLE UPDATED

FIGURE REFERENCE UPDATED

REFERENCED DOCUMENTATION UPDATED

CONFIGURATION UPDATED

PART NUMBER DESCRIPTION UPDATED

NOTE UPDATED

MATERIAL LIST UPDATED

REFERENCES UPDATED

R

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Subtask 246103-831-036-001 SUBTASK SOLUTION UPDATED R

Subtask 246103-020-008-001 SUBTASK SOLUTION UPDATED

FIGURE REFERENCE UPDATED

CONFIGURATION UPDATED

ITEM NUMBER UPDATED

QUANTITY UPDATED

PART NUMBER DESCRIPTION UPDATED

NOTE UPDATED

REFERENCES UPDATED

R

Subtask 246103-020-009-001 SUBTASK SOLUTION UPDATED

FIGURE REFERENCE UPDATED

CONFIGURATION UPDATED

ITEM NUMBER UPDATED

QUANTITY UPDATED

PART NUMBER DESCRIPTION UPDATED

NOTE UPDATED

REFERENCES UPDATED

R

Subtask 246103-831-048-001 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

ITEM NUMBER UPDATED

PART NUMBER UPDATED

KEYWORD UPDATED

FIGURE REFERENCE UPDATED

CONFIGURATION UPDATED

PART NUMBER DESCRIPTION UPDATED

MATERIAL LIST UPDATED

R

Subtask 246103-831-049-001 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

ITEM NUMBER UPDATED

PART NUMBER UPDATED

KEYWORD UPDATED

FIGURE REFERENCE UPDATED

CONFIGURATION UPDATED

PART NUMBER DESCRIPTION UPDATED

MATERIAL LIST UPDATED

R

Subtask 246103-831-045-001 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

ITEM NUMBER UPDATED

PART NUMBER UPDATED

KEYWORD UPDATED

FIGURE REFERENCE UPDATED

CONFIGURATION UPDATED

PART NUMBER DESCRIPTION UPDATED

MATERIAL LIST UPDATED

REFERENCES UPDATED

NOTE UPDATED

R

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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Subtask 246103-831-047-001 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

ITEM NUMBER UPDATED

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KEYWORD UPDATED

FIGURE REFERENCE UPDATED

CONFIGURATION UPDATED

PART NUMBER DESCRIPTION UPDATED

NOTE UPDATED

MATERIAL LIST UPDATED

REFERENCES UPDATED

R

Subtask 246103-020-006-001 SUBTASK SOLUTION UPDATED R

Subtask 246103-831-031-001 SUBTASK SOLUTION UPDATED R

Subtask 246103-420-007-001 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

MATERIAL LIST UPDATED

R

Subtask 246103-420-009-001 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

R

Subtask 246103-831-033-001 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

ITEM NUMBER UPDATED

PART NUMBER UPDATED

KEYWORD UPDATED

CONSUMABLE UPDATED

FIGURE REFERENCE UPDATED

REFERENCED DOCUMENTATION UPDATED

CONFIGURATION UPDATED

PART NUMBER DESCRIPTION UPDATED

NOTE UPDATED

MATERIAL LIST UPDATED

REFERENCES UPDATED

R

Subtask 246103-831-034-001 SUBTASK SOLUTION UPDATED R

Subtask 246103-420-011-001 SUBTASK SOLUTION UPDATED

CONSUMABLE UPDATED

MATERIAL LIST UPDATED

R

Subtask 246103-831-035-001 SUBTASK SOLUTION UPDATED R

Subtask 246103-020-007-001 SUBTASK SOLUTION UPDATED R

Subtask 246103-831-032-001 SUBTASK SOLUTION UPDATED R

Subtask 246103-420-008-001 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

MATERIAL LIST UPDATED

R

Subtask 246103-420-010-001 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

R

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 17

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Subtask 246103-831-050-001 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

ITEM NUMBER UPDATED

PART NUMBER UPDATED

KEYWORD UPDATED

CONSUMABLE UPDATED

FIGURE REFERENCE UPDATED

REFERENCED DOCUMENTATION UPDATED

CONFIGURATION UPDATED

PART NUMBER DESCRIPTION UPDATED

NOTE UPDATED

MATERIAL LIST UPDATED

REFERENCES UPDATED

R

Subtask 246103-831-036-001 SUBTASK SOLUTION UPDATED R

Subtask 246103-020-008-002 SUBTASK SOLUTION ADDED N

Subtask 246103-020-009-002 SUBTASK SOLUTION ADDED N

Subtask 246103-020-008-001 SUBTASK SOLUTION DELETED FOR

APPLICABLE MSN

D

Subtask 246103-020-009-001 SUBTASK SOLUTION DELETED FOR

APPLICABLE MSN

D

Subtask 246103-831-048-001 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

ITEM NUMBER UPDATED

PART NUMBER UPDATED

KEYWORD UPDATED

FIGURE REFERENCE UPDATED

CONFIGURATION UPDATED

PART NUMBER DESCRIPTION UPDATED

MATERIAL LIST UPDATED

R

Subtask 246103-831-049-001 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

ITEM NUMBER UPDATED

PART NUMBER UPDATED

KEYWORD UPDATED

FIGURE REFERENCE UPDATED

CONFIGURATION UPDATED

PART NUMBER DESCRIPTION UPDATED

MATERIAL LIST UPDATED

R

Subtask 246103-831-045-002 SUBTASK SOLUTION ADDED N

Subtask 246103-831-047-002 SUBTASK SOLUTION ADDED N

Subtask 246103-831-045-001 SUBTASK SOLUTION DELETED FOR

APPLICABLE MSN

D

Subtask 246103-831-047-001 SUBTASK SOLUTION DELETED FOR

APPLICABLE MSN

D

Subtask 246103-020-006-001 SUBTASK SOLUTION ADDED N

Subtask 246103-831-031-001 SUBTASK SOLUTION ADDED N

Subtask 246103-420-007-001 SUBTASK SOLUTION ADDED N

Subtask 246103-420-009-001 SUBTASK SOLUTION ADDED N

Subtask 246103-831-033-002 SUBTASK SOLUTION ADDED N

Subtask 246103-831-034-001 SUBTASK SOLUTION ADDED N

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 18

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REVISION TRANSMITTAL SHEET

Subtask 246103-420-011-001 SUBTASK SOLUTION ADDED N

Subtask 246103-831-035-001 SUBTASK SOLUTION ADDED N

Subtask 246103-020-007-001 SUBTASK SOLUTION ADDED N

Subtask 246103-831-032-001 SUBTASK SOLUTION ADDED N

Subtask 246103-420-008-001 SUBTASK SOLUTION ADDED N

Subtask 246103-420-010-001 SUBTASK SOLUTION ADDED N

Subtask 246103-831-050-002 SUBTASK SOLUTION ADDED N

Subtask 246103-831-036-001 SUBTASK SOLUTION ADDED N

Subtask 246103-020-008-001 SUBTASK SOLUTION ADDED N

Subtask 246103-020-009-001 SUBTASK SOLUTION ADDED N

Subtask 246103-831-048-001 SUBTASK SOLUTION ADDED N

Subtask 246103-831-049-001 SUBTASK SOLUTION ADDED N

Subtask 246103-831-045-001 SUBTASK SOLUTION ADDED N

Subtask 246103-831-047-001 SUBTASK SOLUTION ADDED N

Subtask 246103-700-003-001 SUBTASK SOLUTION ADDED N

Subtask 246103-942-003-001 SUBTASK SOLUTION UPDATED R

Subtask 246103-942-003-001 SUBTASK SOLUTION UPDATED R

Subtask 246103-942-003-001 SUBTASK SOLUTION ADDED N

TASK 246103- 831-805-001-Modification -

ADDITIONAL WORK between Revision

No. 02 and Revision No. 03

TASK SOLUTION ADDED N

Task associated data - 001 TASK ASSOCIATED DATA ADDED N

Task associated data - 002 TASK ASSOCIATED DATA ADDED N

Task associated data - 003 TASK ASSOCIATED DATA ADDED N

Subtask 246103-910-005-001 SUBTASK SOLUTION ADDED N

Subtask 246103-839-005-001 SUBTASK SOLUTION ADDED N

Subtask 246103-910-005-001 SUBTASK SOLUTION ADDED N

Subtask 246103-839-005-001 SUBTASK SOLUTION ADDED N

Subtask 246103-910-005-001 SUBTASK SOLUTION ADDED N

Subtask 246103-839-005-001 SUBTASK SOLUTION ADDED N

Subtask 246103-941-006-001 SUBTASK SOLUTION ADDED N

Subtask 246103-941-006-001 SUBTASK SOLUTION ADDED N

Subtask 246103-941-006-001 SUBTASK SOLUTION ADDED N

Subtask 246103-831-051-001 SUBTASK SOLUTION ADDED N

Subtask 246103-831-052-001 SUBTASK SOLUTION ADDED N

Subtask 246103-831-056-001 SUBTASK SOLUTION ADDED N

Subtask 246103-831-057-001 SUBTASK SOLUTION ADDED N

Subtask 246103-831-053-001 SUBTASK SOLUTION ADDED N

Subtask 246103-831-054-001 SUBTASK SOLUTION ADDED N

Subtask 246103-831-051-002 SUBTASK SOLUTION ADDED N

Subtask 246103-831-052-002 SUBTASK SOLUTION ADDED N

Subtask 246103-831-056-001 SUBTASK SOLUTION ADDED N

Subtask 246103-831-057-001 SUBTASK SOLUTION ADDED N

Subtask 246103-831-053-002 SUBTASK SOLUTION ADDED N

Subtask 246103-831-054-002 SUBTASK SOLUTION ADDED N

Subtask 246103-831-037-001 SUBTASK SOLUTION ADDED N

Subtask 246103-831-038-001 SUBTASK SOLUTION ADDED N

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 19

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REVISION TRANSMITTAL SHEET

Subtask 246103-831-051-001 SUBTASK SOLUTION ADDED N

Subtask 246103-831-052-001 SUBTASK SOLUTION ADDED N

Subtask 246103-831-056-001 SUBTASK SOLUTION ADDED N

Subtask 246103-831-057-001 SUBTASK SOLUTION ADDED N

Subtask 246103-831-053-001 SUBTASK SOLUTION ADDED N

Subtask 246103-831-054-001 SUBTASK SOLUTION ADDED N

Subtask 246103-700-005-001 SUBTASK SOLUTION ADDED N

Subtask 246103-700-005-001 SUBTASK SOLUTION ADDED N

Subtask 246103-700-005-001 SUBTASK SOLUTION ADDED N

Subtask 246103-942-005-001 SUBTASK SOLUTION ADDED N

Subtask 246103-942-005-001 SUBTASK SOLUTION ADDED N

Subtask 246103-942-005-001 SUBTASK SOLUTION ADDED N

Fig. A-FBCAA FIGURE SOLUTION UPDATED

CONFIGURATION UPDATED

R

Fig. A-FBCAA Sheet 02 SHEET UPDATED R

Fig. A-FBCAB FIGURE SOLUTION ADDED N

Fig. A-FBCAB Sheet 01 SHEET ADDED N

Fig. A-FBCAB Sheet 02 SHEET ADDED N

Fig. A-FBCAB Sheet 03 SHEET ADDED N

Fig. A-FBCAB Sheet 04 SHEET ADDED N

Fig. A-FBCAB Sheet 05 SHEET ADDED N

Fig. A-FBDAA FIGURE SOLUTION UPDATED

CONFIGURATION UPDATED

R

Fig. A-FBDAA Sheet 03 SHEET UPDATED R

Fig. A-FBDAB FIGURE SOLUTION ADDED N

Fig. A-FBDAB Sheet 01 SHEET ADDED N

Fig. A-FBDAB Sheet 02 SHEET ADDED N

Fig. A-FBHAA

Fig. A-FBHAA Sheet 02 SHEET UPDATED R

Fig. A-FBKAA FIGURE SOLUTION UPDATED

CONFIGURATION UPDATED

R

Fig. A-FBKAA Sheet 02 SHEET UPDATED R

Fig. A-FBKAA Sheet 03 SHEET UPDATED R

Fig. A-FBKAA Sheet 04 SHEET UPDATED R

Fig. A-FBKAA Sheet 05 SHEET UPDATED R

Fig. A-FBLAA

Fig. A-FBLAA Sheet 02 SHEET UPDATED R

Fig. A-FBLAA Sheet 03 SHEET UPDATED R

Fig. A-FBLAA Sheet 04 SHEET UPDATED R

Fig. A-FBYAA

Fig. A-FBYAA Sheet 02 SHEET UPDATED R

Fig. A-FBWAA

Fig. A-FBWAA Sheet 01 SHEET UPDATED R

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 20

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REVISION TRANSMITTAL SHEET

Fig. A-FBMAA FIGURE SOLUTION UPDATED

CONFIGURATION UPDATED

R

Fig. A-FBMAA Sheet 02 SHEET UPDATED R

Fig. A-FBMAA Sheet 03 SHEET UPDATED R

Fig. A-FBMAA Sheet 04 SHEET UPDATED R

Fig. A-FBMAB FIGURE SOLUTION ADDED N

Fig. A-FBMAB Sheet 01 SHEET ADDED N

Fig. A-FBMAB Sheet 02 SHEET ADDED N

Fig. A-FBMAB Sheet 03 SHEET ADDED N

Fig. A-FBMAB Sheet 04 SHEET ADDED N

Fig. A-FBMAB Sheet 05 SHEET ADDED N

Fig. A-FBMAB Sheet 06 SHEET ADDED N

Fig. A-FBOAA FIGURE SOLUTION ADDED N

Fig. A-FBOAA Sheet 01 SHEET ADDED N

Fig. A-FBOAA Sheet 02 SHEET ADDED N

Fig. A-FBOAA Sheet 03 SHEET ADDED N

Fig. A-FBOAA Sheet 04 SHEET ADDED N

Fig. A-FBOAA Sheet 05 SHEET ADDED N

Fig. A-FBRAA

Fig. A-FBRAA Sheet 01 SHEET UPDATED R

Fig. A-FBRAA Sheet 02 SHEET UPDATED R

Fig. A-FBRAA Sheet 03 SHEET UPDATED R

Fig. A-FBTAA

Fig. A-FBTAA Sheet 01 SHEET UPDATED R

Fig. A-FBVAA

Fig. A-FBVAA Sheet 01 SHEET UPDATED R

Fig. A-FCCAA FIGURE SOLUTION UPDATED

CONFIGURATION UPDATED

R

Fig. A-FCCAA Sheet 02 SHEET UPDATED R

Fig. A-FCCAA Sheet 03 SHEET UPDATED R

Fig. A-FCCAA Sheet 04 SHEET UPDATED R

Fig. A-FCCAB FIGURE SOLUTION ADDED N

Fig. A-FCCAB Sheet 01 SHEET ADDED N

Fig. A-FCCAB Sheet 02 SHEET ADDED N

Fig. A-FCCAB Sheet 03 SHEET ADDED N

Fig. A-FCCAB Sheet 04 SHEET ADDED N

Fig. A-FCCAB Sheet 05 SHEET ADDED N

Fig. A-FCCAB Sheet 06 SHEET ADDED N

Fig. A-FCL FIGURE DELETED FOR APPLICABLE MSN D

Fig. A-FCMAA

Fig. A-FCMAA Sheet 02 SHEET UPDATED R

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 21

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REVISION TRANSMITTAL SHEET

Fig. A-UAAAA FIGURE SOLUTION UPDATED

CONFIGURATION UPDATED

R

Fig. A-UAAAA Sheet 04 SHEET UPDATED R

Fig. A-UBAAA FIGURE SOLUTION ADDED N

Fig. A-UBAAA Sheet 01 SHEET ADDED N

Fig. A-UBAAA Sheet 02 SHEET ADDED N

Fig. A-UBAAA Sheet 03 SHEET ADDED N

Fig. A-FCOAA FIGURE SOLUTION ADDED N

Fig. A-FCOAA Sheet 01 SHEET ADDED N

Fig. A-FCOAA Sheet 02 SHEET ADDED N

Fig. A-FCOAA Sheet 03 SHEET ADDED N

Fig. A-FCOAA Sheet 04 SHEET ADDED N

Fig. A-FCPAA FIGURE SOLUTION ADDED N

Fig. A-FCPAA Sheet 01 SHEET ADDED N

Fig. A-FCPAA Sheet 02 SHEET ADDED N

Fig. A-FCPAA Sheet 03 SHEET ADDED N

Fig. A-FCPAA Sheet 04 SHEET ADDED N

Fig. A-FCPAA Sheet 05 SHEET ADDED N

Appendix 01 - Elapsed Time Assumption

APPENDIX CONTENT APPENDIX CONTENT UPDATED R

Fig. A-FAAAA FIGURE SOLUTION UPDATED

CONFIGURATION UPDATED

R

Appendix 02 - Elapsed Time Assumption - ADDITIONAL WORK BETWEEN REVISION No. 00

AND REVISION No. 03

APPENDIX CONTENT APPENDIX CONTENT ADDED N

Fig. A-FACAA FIGURE SOLUTION ADDED N

Fig. A-FACAA Sheet 01 SHEET ADDED N

Appendix 03 - Elapsed Time Assumption - ADDITIONAL WORK BETWEEN REVISION No. 01

AND REVISION No. 03

APPENDIX CONTENT APPENDIX CONTENT ADDED N

Fig. A-FADAA FIGURE SOLUTION ADDED N

Fig. A-FADAA Sheet 01 SHEET ADDED N

Appendix 04 - Elapsed Time Assumption - ADDITIONAL WORK BETWEEN REVISION No. 02

AND REVISION No. 03

APPENDIX CONTENT APPENDIX CONTENT ADDED N

Fig. A-FAFAA FIGURE SOLUTION ADDED N

Fig. A-FAFAA Sheet 01 SHEET ADDED N

Fig. A-FAFAB FIGURE SOLUTION ADDED N

Fig. A-FAFAB 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.

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 22

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

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

HISTORY OF PREVIOUS REVISIONS

Revision No. 01 issued to :

review all technical definition,

add illustrations,

improve major changes.

Revision No. 02 issued to :

review the technical definition,

add illustrations,

improve major changes.

REVISION SEQUENCE

ORIGINAL: Jun 17/10

REVISION No. : 01 - Feb 21/12

REVISION No. : 02 - Feb 07/13

REVISION No. : 03 - Jul 03/15

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 23

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REVISION TRANSMITTAL SHEET

This Page Intentionally Left Blank

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 24

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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: ELECTRIC AND ELECTRONIC COMMON INSTALLATIONS - IMPROVE

WING WIRING INSTALLATION

**CONF ALL

MODIFICATIONS

MODIFICATION CLASSIFICATION

MAJOR 13397S22766 13399S22768 13516H5723

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

The A300-600 aircraft operator’s feedback further to the accomplishment of the mandatory Inspection

Service Bulletin No. A300-24-6092 and a review of the wing electrical installation at the AIRBUS final

assembly line have shown that the wing electrical installation doesn’t comply with the minimum distance

inspection criteria to the surrounding structure in a few wing locations.

This Service Bulletin requires:

- The installation of new bracket assemblies to improve the electrical harnesses installation and

secure the clearance to the structure in identified locations,

- The installation of protective split sleeve as mechanical protection to the electrical harnesses in

areas where the minimum distance to the structure cannot be achieved.

Accomplishment of this modification Service Bulletin will improve the wing electrical installation in the

identified areas and prevent possible chafing and subsequent damage to the electrical harnesses and

surrounding structure.

GENERAL EVALUATION

EVALUATION TABLE

COMPLIANCE MANDATORY (1) CANCELS INSPECTION SB NO

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 1

5

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@A300-600

SERVICE BULLETIN

SUMMARY

EVALUATION TABLE

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

VALIDATION ON AIRCRAFT YES BOOKLET AVAILABLE YES

NOTE (1): Service Bulletin must be accomplished.

NOTE: This Service Bulletin has been validated at Revision No. 00 on A300 aircraft with

Manufacturer Serial Number (MSN) 0284.

NOTE: A booklet including photographs taken during the validation of this Service Bulletin is

available on AIRBUS|World - Maintenance and Engineering - AirN@v engineering (in

the concerned SB file).

MATERIAL PRICE INFORMATION

**CONF 001

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 246103A01R14 1 3,600.00 Seal fitting, support, conduit, spacer

Kit 246103A02R12 1 3,400.00 Conduit, spacer

Kit 246103A03R04 2 110.00 Guide, screw

Supplementary kit

246103A01S03

1 2,850.00 Bracket

Supplementary kit

246103A01S08

1 4,300.00 Bracket

Supplementary kit

246103A01S11

1 90.00 Clamps

Supplementary kit

246103A01S12

1 130.00 Clamps

Supplementary kit

246103A01S13

1 25.00 Rivets

Supplementary kit

246103A02S03

1 2,150.00 Bracket

Supplementary kit

246103A02S07

1 2,960.00 Bracket

Supplementary kit

246103A02S10

1 120.00 Clamps

Supplementary kit

246103A02S11

1 240.00 Clamps

Supplementary kit

246103A03S01

1 55.00 Screw, Nut

Kit 246103B01R03 2 6,200.00 Bracket Assy

TOTAL 26,230.00

Component COMPB01 1 See SB

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 2

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

SUMMARY

**CONF 002

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 246103A01R14 1 3,600.00 Seal fitting, support, conduit, spacer

Kit 246103A02R12 1 3,400.00 Conduit, spacer

Supplementary kit

246103A01S03

1 2,850.00 Bracket

Supplementary kit

246103A01S08

1 4,300.00 Bracket

Supplementary kit

246103A01S11

1 90.00 Clamps

Supplementary kit

246103A01S12

1 130.00 Clamps

Supplementary kit

246103A01S13

1 25.00 Rivets

Supplementary kit

246103A02S03

1 2,150.00 Bracket

Supplementary kit

246103A02S07

1 2,960.00 Bracket

Supplementary kit

246103A02S10

1 120.00 Clamps

Supplementary kit

246103A02S11

1 240.00 Clamps

Kit 246103B02R02 2 1,142.00 Bracket Assy

TOTAL 21,007.00

**CONF 003

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 246103A01R14 1 3,600.00 Seal fitting, support, conduit, spacer

Kit 246103A02R12 1 3,400.00 Conduit, spacer

Kit 246103A03R04 2 110.00 Guide, screw

Kit 246103A04R00 1 710.00 Clamps

Kit 246103A05R00 1 710.00 Clamps

Supplementary kit

246103A01S03

1 2,850.00 Bracket

Supplementary kit

246103A01S08

1 4,300.00 Bracket

Supplementary kit

246103A01S11

1 90.00 Clamps

Supplementary kit

246103A01S12

1 130.00 Clamps

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 3

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

SUMMARY

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Supplementary kit

246103A01S13

1 25.00 Rivets

Supplementary kit

246103A02S03

1 2,150.00 Bracket

Supplementary kit

246103A02S07

1 2,960.00 Bracket

Supplementary kit

246103A02S10

1 120.00 Clamps

Supplementary kit

246103A02S11

1 240.00 Clamps

Supplementary kit

246103A03S01

1 55.00 Screw, Nut

Kit 246103B01R03 2 6,200.00 Bracket Assy

TOTAL 27,650.00

Component COMPB01 1 See SB

EFFECTIVITY

**CONF ALL

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

06P 67Q ABR AHK BCS F2I FDX IRA IRM KAC MNB MRJ MSR

OHY SUD TAR THA UPS UQA URS UTP UZB

CONCURRENT REQUIREMENTS

None

REFERENCES / REPERCUSSIONS

TFU None

OEB None

AOT None

SIL None

ISI None

LINE MAINTENANCE AFFECTED No

LIFE LIMIT None

OTHER None

NATURE OF THE WORK

AIRCRAFT YES

EQUIPMENT NO

HARD NO

SOFT NO

OBRM NO

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 4

5

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@A300-600

SERVICE BULLETIN

SUMMARY

MANPOWER

**CONF 001

Task 246103-831-801-001: Modification

TOTAL MANHOURS 38.00

ELAPSED TIME (HOURS) 22.50

Task 246103-831-802-001: Modification - ADDITIONAL WORK between Revision No. 00 and

Revision No. 03

TOTAL MANHOURS 24.50

ELAPSED TIME (HOURS) 16.50

Task 246103-831-804-001: Modification - ADDITIONAL WORK between Revision No. 01 and

Revision No. 03

TOTAL MANHOURS 30.50

ELAPSED TIME (HOURS) 16.50

Task 246103-831-805-001: Modification - ADDITIONAL WORK between Revision No. 02 and

Revision No. 03

TOTAL MANHOURS 16.50

ELAPSED TIME (HOURS) 8.50

**CONF 002

Task 246103-831-801-001: Modification

TOTAL MANHOURS 36.00

ELAPSED TIME (HOURS) 20.75

Task 246103-831-802-001: Modification - ADDITIONAL WORK between Revision No. 00 and

Revision No. 03

TOTAL MANHOURS 24.50

ELAPSED TIME (HOURS) 16.50

Task 246103-831-804-001: Modification - ADDITIONAL WORK between Revision No. 01 and

Revision No. 03

TOTAL MANHOURS 30.50

ELAPSED TIME (HOURS) 16.50

Task 246103-831-805-001: Modification - ADDITIONAL WORK between Revision No. 02 and

Revision No. 03

TOTAL MANHOURS 16.50

ELAPSED TIME (HOURS) 8.50

**CONF 003

Task 246103-831-801-001: Modification

TOTAL MANHOURS 38.00

ELAPSED TIME (HOURS) 22.50

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 5

5

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@A300-600

SERVICE BULLETIN

SUMMARY

Task 246103-831-802-001: Modification - ADDITIONAL WORK between Revision No. 00 and

Revision No. 03

TOTAL MANHOURS 24.50

ELAPSED TIME (HOURS) 16.50

Task 246103-831-804-001: Modification - ADDITIONAL WORK between Revision No. 01 and

Revision No. 03

TOTAL MANHOURS 30.50

ELAPSED TIME (HOURS) 16.50

Task 246103-831-805-001: Modification - ADDITIONAL WORK between Revision No. 02 and

Revision No. 03

TOTAL MANHOURS 18.50

ELAPSED TIME (HOURS) 9.50

APPENDICES

**CONF ALL

Appendix 01 - Elapsed Time Assumption

Appendix 02 - Elapsed Time Assumption - ADDITIONAL WORK BETWEEN REVISION No. 00 AND

REVISION No. 03

Appendix 03 - Elapsed Time Assumption - ADDITIONAL WORK BETWEEN REVISION No. 01 AND

REVISION No. 03

Appendix 04 - Elapsed Time Assumption - ADDITIONAL WORK BETWEEN REVISION No. 02 AND

REVISION No. 03

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 6

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@A300-600

SERVICE BULLETIN

SUMMARY

**CONF ALL

Z572

Z571 Z513

Z613

Z672

Z147 Z148 −

D_SB_246103_5_SAAA_01_01

ZONES WITH ROUTING TO MODIFY

Figure A-FSAAA - Sheet 01

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 7

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

SUMMARY

This Page Intentionally Left Blank

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 8

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

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: ELECTRIC AND ELECTRONIC COMMON INSTALLATIONS - IMPROVE

WING WIRING INSTALLATION

MODIFICATION No.: 13397S22766 13399S22768 13516H5723

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

B4-603 B4-605R B4-620 B4-622 B4-622R C4-605R/FC4-620 F4-605R

F4-622R

(2) Effectivity by MSN

0294 0344 0358 0361 0365 0380 0388 0401 0405 0408 0411 0414 0417 0477 0479

0505 0521 0525 0529-0530 0532 0536 0543 0546 0553 0555 0557-0559 0561 0563

0572 0575 0579 0581 0584 0602-0603 0607-0608 0611 0613 0617-0618 0621 0623

0625-0626 0629-0630 0632-0633 0637 0641 0643 0657 0659 0664 0666 0668 0670

0673 0677 0679 0683 0688 0694 0696 0699 0701 0703 0707 0709 0711 0713 0715

0717 0719 0721-0730 0732-0750 0752-0764 0766 0768-0775 0777-0794 0797

0799-0840 0845-0878

(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: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 1

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@A300-600

SERVICE BULLETIN

OPERATOR MSN

06P 0788

67Q 0584 0603 0744 0749 0764

ABR 0677 0743

AHK 0683 0770 0855 0856 0857 0858 0859 0860 0870 0871

BCS 0529 0557 0602 0617 0621 0637 0641 0670 0679 0703 0711 0724

0729 0730 0737 0740 0753 0783 0797 0836 0837 0872

F2I 0294

FDX 0358 0361 0365 0388 0417 0477 0479 0530 0536 0543 0555 0559

0572 0575 0579 0581 0611 0613 0625 0630 0633 0657 0659 0664

0668 0688 0709 0713 0715 0726 0728 0735 0736 0738 0742 0745

0748 0752 0757 0759 0760 0761 0766 0768 0769 0771 0772 0774

0777 0778 0779 0780 0781 0789 0790 0791 0792 0793 0794 0799

0800 0801 0802 0803 0804 0873 0874 0875 0876 0877 0878

IRA 0632 0696 0723 0727

IRM 0380 0401 0405 0408 0411 0414 0546 0553 0608 0618 0623 0701

0773 0838

KAC 0344 0673 0694 0699 0719 0721

MNB 0521 0525 0532 0734 0739 0755 0756 0758

MRJ 0750 0762

MSR 0561 0607

OHY 0747

SUD 0666 0775

TAR 0505 0558 0563

THA 0629 0782 0784 0785 0786 0787

UPS 0805 0806 0807 0808 0809 0810 0811 0812 0813 0814 0815 0816

0817 0818 0819 0820 0821 0822 0823 0824 0825 0826 0827 0828

0829 0830 0831 0832 0833 0834 0835 0839 0840 0845 0846 0847

0848 0849 0850 0851 0852 0853 0854 0861 0862 0863 0864 0865

0866 0867 0868 0869

UQA 0626 0643

URS 0733

UTP 0707 0725 0732 0741 0746 0754 0763

UZB 0717 0722

(4) Configuration by MSN

MSN CONFIGURATION

0294 0344 0380 0401 0405 0408 0411 0414 0505 0521 0525

0532 0546 0553 0558 0563 0584 0603 0608 0618 0623 0626

0632 0643 0673 0694 0696 0699 0701 0707 0709 0713 0715

0719 0721 0725 0732 0741 0744 0746 0747 0749 0754 0755

0758 0763 0764 0773

001

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 2

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@A300-600

SERVICE BULLETIN

MSN CONFIGURATION

0358 0361 0365 0388 0417 0477 0479 0529 0530 0536 0543

0555 0557 0559 0561 0572 0575 0579 0581 0602 0607 0611

0613 0617 0621 0625 0629 0630 0633 0637 0641 0657 0659

0664 0666 0668 0670 0677 0679 0683 0688 0703 0711 0717

0722 0724 0729 0730 0733 0734 0737 0739 0740 0743 0750

0753 0756 0762 0770 0775 0782 0783 0784 0785 0786 0787

0788 0797 0805 0806 0807 0808 0809 0810 0811 0812 0813

0814 0815 0816 0817 0818 0819 0820 0821 0822 0823 0824

0825 0826 0827 0828 0829 0830 0831 0832 0833 0834 0835

0836 0837 0838 0839 0840 0845 0846 0847 0848 0849 0850

0851 0852 0853 0854 0861 0862 0863 0864 0865 0866 0867

0868 0869 0872

003

0723 0726 0727 0728 0735 0736 0738 0742 0745 0748 0752

0757 0759 0760 0761 0766 0768 0769 0771 0772 0774 0777

0778 0779 0780 0781 0789 0790 0791 0792 0793 0794 0799

0800 0801 0802 0803 0804 0855 0856 0857 0858 0859 0860

0870 0871 0873 0874 0875 0876 0877 0878

002

(5) Configuration definition

**CONF 001

Config. 001 is valid for aircraft on which Mod. No 06127S6951 (Service Bulletin

No.A300-72-6006) and Mod. No. 08966S20263 are not embodied.

**CONF 002

Config. 002 is valid for aircraft on which Mod. No 06127S6951 (Service Bulletin

No.A300-72-6006) is not embodied and Mod. No. 08966S20263 is embodied.

**CONF 003

Config. 003 is valid for aircraft on which Mod. No 06127S6951 (Service Bulletin

No.A300-72-6006) is embodied and Mod. No. 08966S20263 is not embodied.

(6) Material Effectivity

**CONF 001

MATERIAL QTY PER A/C SEE NOTES

Kit 246103A01R14 1 (1)

Kit 246103A02R12 1 (2)

Kit 246103A03R04 2 (3)

Supplementary kit 246103A01S03 1

Supplementary kit 246103A01S08 1

Supplementary kit 246103A01S11 1

Supplementary kit 246103A01S12 1

Supplementary kit 246103A01S13 1

Supplementary kit 246103A02S03 1

Supplementary kit 246103A02S07 1

Supplementary kit 246103A02S10 1

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 3

5

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@A300-600

SERVICE BULLETIN

MATERIAL QTY PER A/C SEE NOTES

Supplementary kit 246103A02S11 1

Supplementary kit 246103A03S01 1

Kit 246103B01R03 2 (4)

Consumable CMLB01 As required

Consumable CMLA01 As required

Component COMPB01 1

NOTE (1): Kit A01 concerns the work to be done on LH side of the aircraft.

NOTE (2): Kit A02 concerns the work to be done on RH side of the aircraft.

NOTE (3): Kit A03 concerns the installation of the guide in LH and RH wings.

NOTE (4): Kit B01 concerns the modification of the brackets in the outer shroud

box.

**CONF 002

MATERIAL QTY PER A/C SEE NOTES

Kit 246103A01R14 1 (1)

Kit 246103A02R12 1 (2)

Supplementary kit 246103A01S03 1

Supplementary kit 246103A01S08 1

Supplementary kit 246103A01S11 1

Supplementary kit 246103A01S12 1

Supplementary kit 246103A01S13 1

Supplementary kit 246103A02S03 1

Supplementary kit 246103A02S07 1

Supplementary kit 246103A02S10 1

Supplementary kit 246103A02S11 1

Kit 246103B02R02 2 (3)

Consumable CMLA01 As required

Consumable CMLB01 As required

NOTE (1): Kit A01 concerns the work to be done on LH side of the aircraft.

NOTE (2): Kit A02 concerns the work to be done on RH side of the aircraft.

NOTE (3): Kit B02 concerns the modification of the brackets in the outer shroud

box.

**CONF 003

MATERIAL QTY PER A/C SEE NOTES

Kit 246103A01R14 1 (1)

Kit 246103A02R12 1 (2)

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 4

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@A300-600

SERVICE BULLETIN

MATERIAL QTY PER A/C SEE NOTES

Kit 246103A03R04 2 (3)

Kit 246103A04R00 1 (4)

Kit 246103A05R00 1 (5)

Supplementary kit 246103A01S03 1

Supplementary kit 246103A01S08 1

Supplementary kit 246103A01S11 1

Supplementary kit 246103A01S12 1

Supplementary kit 246103A01S13 1

Supplementary kit 246103A02S03 1

Supplementary kit 246103A02S07 1

Supplementary kit 246103A02S10 1

Supplementary kit 246103A02S11 1

Supplementary kit 246103A03S01 1

Kit 246103B01R03 2 (6)

Consumable CMLB01 As required

Consumable CMLA01 As required

Component COMPB01 1

NOTE (1): Kit A01 concerns the work to be done on LH side of the aircraft.

NOTE (2): Kit A02 concerns the work to be done on RH side of the aircraft.

NOTE (3): Kit A03 concerns the installation of the guide in LH and RH wings.

NOTE (4): Kit A04 concerns the installation of the clamps on the Passage Way to

the Shroud box in LH side.

NOTE (5): Kit A05 concerns the installation of the clamps on the Passage Way to

the Shroud box in RH side.

NOTE (6): Kit B01 concerns the modification of the brackets in the outer shroud

box.

**CONF ALL

B. CONCURRENT REQUIREMENTS

None

C. REASON

(1) History

The A300-600 aircraft operator’s feedback further to the accomplishment of the

mandatory Inspection Service Bulletin No. A300-24-6092 and a review of the wing

electrical installation at the AIRBUS final assembly line have shown that the wing

electrical installation doesn’t comply with the minimum distance inspection criteria to the

surrounding structure in a few wing locations.

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 5

5

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@A300-600

SERVICE BULLETIN

(2) Objective/Action

This Service Bulletin requires:

- The installation of new bracket assemblies to improve the electrical harnesses

installation and secure the clearance to the structure in identified locations,

- The installation of protective split sleeve as mechanical protection to the electrical

harnesses in areas where the minimum distance to the structure cannot be

achieved.

(3) Advantages

Accomplishment of this modification Service Bulletin will improve the wing electrical

installation in the identified areas and prevent possible chafing and subsequent damage

to the electrical harnesses and surrounding structure.

(4) Operational/Maintenance Consequences

None

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

**CONF 001

Task 246103-831-801-001: Modification

(1) Remove the clamps between FR50 and FR52 at LH side

(2) Modify the Routing between FR50 and FR52 and between STGR 33 and 30 at LH

side

(3) Install the clamps between FR50 and FR52 at LH side

(4) Install a bracket on the shroud box blanking plate at LH side

(5) Modify the routing on rib 1 on the passage way to the shroud box at LH side

(6) Modify the routing of routes 1P and 2P in the hydraulic shroud box at LH side

(7) Install a support on the support of the BLUE hydraulic reservoir at LH wing

(8) Modify the routing of routes 1E and 1G in the leading edge at LH wing

(9) Remove the clamps between FR50 and FR52 at RH side

(10) Modify the Routing between FR50 and FR52 and between STGR 33 and 30 at RH

side

(11) Install the clamps between FR50 and FR52 at RH side

(12) Install a bracket on the shroud box blanking plate at RH side

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 6

5

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@A300-600

SERVICE BULLETIN

(13) Modify the routing on rib 1 on the passage way to the shroud box at RH side

(14) Modify the routing of routes 2E and 2G in the leading edge at RH wing

(15) Remove the clamps from LH wing

(16) Remove the clamps from RH wing

(17) Modify the Electrical Support Brackets in the Outer Shroud Box, LH Wing

(18) Modify the routing of routes 1P and 2P at LH wing

(19) Modify the routing of routes 1P and 2P at RH wing

(20) Install the clamps in LH wing

(21) Install the clamps in RH wing

(22) Modify the P-CLIPS at Location WOFX-204.5, LH Wing

(23) Modify the Backshell of the Connector and the Structure at Location ABX 36.5, LH

Wing

(24) Modify the Electrical Support Brackets in the Outer Shroud Box, RH Wing

(25) Modify the P-CLIPS at Location WOFX-204.5, RH Wing

(26) Modify the Backshell of the Connector and the Structure at Location ABX 36.5, RH

Wing

Task 246103-831-802-001: Modification - ADDITIONAL WORK between Revision No. 00 and

Revision No. 03

(1) Modify the routing on rib 1 on the passage way to the shroud box at LH side,

ADDITIONAL WORK

(2) Modify the routing on rib 1 on the passage way to the shroud box at RH side,

ADDITIONAL WORK

(3) Modify the routing of routes 1P and 2P in the shroud box at LH side, ADDITIONAL

WORK

(4) Modify the routing of the routes 1E and 1G in the leading edge at LH wing,

ADDITIONAL WORK

(5) Modify the routing of the routes 2E and 2G in the leading edge at RH wing,

ADDITIONAL WORK

(6) Install a support on the support of the BLUE hydraulic reservoir at LH wing,

ADDITIONAL WORK

(7) Install a bracket on the shroud box blanking plate at LH side, ADDITIONAL WORK

(8) Install a bracket on the shroud box blanking plate at RH side, ADDITIONAL WORK

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 7

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@A300-600

SERVICE BULLETIN

(9) Remove the clamps between FR50 and FR51 at STRG 32 at LH side, ADDITIONAL

WORK

(10) Remove the clamps of the Passage Way at FR52 (LH side) - ADDITIONAL WORK

(11) Modify the Routing between FR50 and FR52 and between STGR 33 and 30 at LH

side - ADDITIONAL WORK

(12) Install the clamps between FR50 and FR51 at STRG 32 at LH side, ADDITIONAL

WORK

(13) Install the clamps of the Passage Way at FR52 (LH side) - ADDITIONAL WORK

(14) Remove the clamps between FR50 and FR51 at STGR 32 at RH side,

ADDITIONAL WORK

(15) Remove the clamps of the Passage Way at FR52 (RH side) - ADDITIONAL WORK

(16) Modify the Routing between FR50 and FR52 and between STGR 33 and 30 at RH

side - ADDITIONAL WORK

(17) Install the clamps between FR50 and FR51 at STGR 32 at RH side, ADDITIONAL

WORK

(18) Install the clamps of the Passage Way at FR52 (RH side) - ADDITIONAL WORK

Task 246103-831-804-001: Modification - ADDITIONAL WORK between Revision No. 01 and

Revision No. 03

(1) Remove the clamps between FR50 and FR52 at LH side, ADDITIONAL WORK

(2) Modify the routing between FR50 and FR52 and between STGR 33 and 30 at LH

side, ADDITIONAL WORK

(3) Install the clamps between FR50 and FR52 at LH side, ADDITIONAL WORK

(4) Install a bracket on the shroud box blanking plate at LH side, ADDITIONAL WORK

(5) Modify the routing on rib 1 on the passage way to the shroud box at LH side,

ADDITIONAL WORK

(6) Modify the routing of routes 1P and 2P in the shroud box at LH side, ADDITIONAL

WORK

(7) Install a support on the support of the BLUE hydraulic reservoir at LH wing -

ADDITIONAL WORK

(8) Modify the routing of the routes 1E and 1G in the leading edge at LH wing,

ADDITIONAL WORK

(9) Remove the clamps between FR50 and FR52 at RH side, ADDITIONAL WORK

(10) Modify the routing between FR50 and FR52 and between STGR 33 and 30 at RH

side, ADDITIONAL WORK

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 8

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@A300-600

SERVICE BULLETIN

(11) Install the clamps between FR50 and FR52 at RH side, ADDITIONAL WORK

(12) Install a bracket on the shroud box blanking plate at RH side, ADDITIONAL WORK

(13) Modify the routing on Rib 1 on the passage way to the shroud box at RH side,

ADDITIONAL WORK

(14) Modify the routing of the routes 2E and 2G in the leading edge at RH wing,

ADDITIONAL WORK

(15) Remove the clamps from LH wings, ADDITIONAL WORK

(16) Remove the clamps from RH wings, ADDITIONAL WORK

(17) Modify the routing of routes 1P and 2P at LH wing, ADDITIONAL WORK

(18) Modify the routing of routes 1P and 2P at RH wing, ADDITIONAL WORK

(19) Install the clamps in LH wing, ADDITIONAL WORK

(20) Install the clamps in RH wing, ADDITIONAL WORK

Task 246103-831-805-001: Modification - ADDITIONAL WORK between Revision No. 02 and

Revision No. 03

(1) Remove the clamps from LH wing, ADDITIONAL WORK

(2) Remove the clamps from RH wing, ADDITIONAL WORK

(3) Modify the routing of routes 1P and 2P at LH wing

(4) Modify the routing of routes 1P and 2P at RH wing

(5) Install the clamps in LH wing, ADDITIONAL WORK

(6) Install the clamps in RH wing, ADDITIONAL WORK

**CONF 002

Task 246103-831-801-001: Modification

(1) Remove the clamps between FR50 and FR52 at LH side

(2) Modify the Routing between FR50 and FR52 and between STGR 33 and 30 at LH

side

(3) Install the clamps between FR50 and FR52 at LH side

(4) Install a bracket on the shroud box blanking plate at LH side

(5) Modify the routing on rib 1 on the passage way to the shroud box at LH side

(6) Modify the routing of routes 1P and 2P in the hydraulic shroud box at LH side

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 9

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@A300-600

SERVICE BULLETIN

(7) Install a support on the support of the BLUE hydraulic reservoir at LH wing

(8) Modify the routing of routes 1E and 1G in the leading edge at LH wing

(9) Remove the clamps between FR50 and FR52 at RH side

(10) Modify the Routing between FR50 and FR52 and between STGR 33 and 30 at RH

side

(11) Install the clamps between FR50 and FR52 at RH side

(12) Install a bracket on the shroud box blanking plate at RH side

(13) Modify the routing on rib 1 on the passage way to the shroud box at RH side

(14) Modify the routing of routes 2E and 2G in the leading edge at RH wing

(15) Remove the clamps from LH wing.

(16) Remove the clamps from RH wing.

(17) Modify the Electrical Support Brackets in the Outer Shroud Box, LH Wing

(18) Modify the routing of routes 1P and 2P at LH wing

(19) Modify the routing of routes 1P and 2P at RH wing

(20) Install the clamps in LH wing.

(21) Install the clamps in RH wing.

(22) Modify the P-CLIPS at Location WOFX-204.5, LH Wing

(23) Modify the Backshell of the Connector and the Structure at Location ABX 36.5, LH

Wing

(24) Modify the Electrical Support Brackets in the Outer Shroud Box, RH Wing

(25) Modify the P-CLIPS at Location WOFX-204.5, RH Wing

(26) Modify the Backshell of the Connector and the Structure at Location ABX 36.5, RH

Wing

Task 246103-831-802-001: Modification - ADDITIONAL WORK between Revision No. 00 and

Revision No. 03

(1) Modify the routing on rib 1 on the passage way to the shroud box at LH side,

ADDITIONAL WORK

(2) Modify the routing on rib 1 on the passage way to the shroud box at RH side,

ADDITIONAL WORK

(3) Modify the routing of routes 1P and 2P in the shroud box at LH side, ADDITIONAL

WORK

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 10

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@A300-600

SERVICE BULLETIN

(4) Modify the routing of the routes 1E and 1G in the leading edge at LH wing,

ADDITIONAL WORK

(5) Modify the routing of the routes 2E and 2G in the leading edge at RH wing,

ADDITIONAL WORK

(6) Install a support on the support of the BLUE hydraulic reservoir at LH wing,

ADDITIONAL WORK

(7) Install a bracket on the shroud box blanking plate at LH side, ADDITIONAL WORK

(8) Install a bracket on the shroud box blanking plate at RH side, ADDITIONAL WORK

(9) Remove the clamps between FR50 and FR51 at STRG 32 at LH side, ADDITIONAL

WORK

(10) Remove the clamps of the Passage Way at FR52 (LH side) - ADDITIONAL WORK

(11) Modify the Routing between FR50 and FR52 and between STGR 33 and 30 at LH

side - ADDITIONAL WORK

(12) Install the clamps between FR50 and FR51 at STRG 32 at LH side, ADDITIONAL

WORK

(13) Install the clamps of the Passage Way at FR52 (LH side) - ADDITIONAL WORK

(14) Remove the clamps between FR50 and FR51 at STGR 32 at RH side,

ADDITIONAL WORK

(15) Remove the clamps of the Passage Way at FR52 (RH side) - ADDITIONAL WORK

(16) Modify the Routing between FR50 and FR52 and between STGR 33 and 30 at RH

side - ADDITIONAL WORK

(17) Install the clamps between FR50 and FR51 at STGR 32 at RH side, ADDITIONAL

WORK

(18) Install the clamps of the Passage Way at FR52 (RH side) - ADDITIONAL WORK

Task 246103-831-804-001: Modification - ADDITIONAL WORK between Revision No. 01 and

Revision No. 03

(1) Remove the clamps between FR50 and FR52 at LH side, ADDITIONAL WORK

(2) Modify the routing between FR50 and FR52 and between STGR 33 and 30 at LH

side, ADDITIONAL WORK

(3) Install the clamps between FR50 and FR52 at LH side, ADDITIONAL WORK

(4) Install a bracket on the shroud box blanking plate at LH side, ADDITIONAL WORK

(5) Modify the routing on rib 1 on the passage way to the shroud box at LH side,

ADDITIONAL WORK

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 11

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@A300-600

SERVICE BULLETIN

(6) Modify the routing of routes 1P and 2P in the shroud box at LH side, ADDITIONAL

WORK

(7) Install a support on the support of the BLUE hydraulic reservoir at LH wing -

ADDITIONAL WORK

(8) Modify the routing of the routes 1E and 1G in the leading edge at LH wing,

ADDITIONAL WORK

(9) Remove the clamps between FR50 and FR52 at RH side, ADDITIONAL WORK

(10) Modify the routing between FR50 and FR52 and between STGR 33 and 30 at RH

side, ADDITIONAL WORK

(11) Install the clamps between FR50 and FR52 at RH side, ADDITIONAL WORK

(12) Install a bracket on the shroud box blanking plate at RH side, ADDITIONAL WORK

(13) Modify the routing on Rib 1 on the passage way to the shroud box at RH side,

ADDITIONAL WORK

(14) Modify the routing of the routes 2E and 2G in the leading edge at RH wing,

ADDITIONAL WORK

(15) Remove the clamps from LH wings, ADDITIONAL WORK

(16) Remove the clamps from RH wings, ADDITIONAL WORK

(17) Modify the routing of routes 1P and 2P at LH wing, ADDITIONAL WORK

(18) Modify the routing of routes 1P and 2P at RH wing, ADDITIONAL WORK

(19) Install the clamps in LH wing, ADDITIONAL WORK

(20) Install the clamps in RH wing, ADDITIONAL WORK

Task 246103-831-805-001: Modification - ADDITIONAL WORK between Revision No. 02 and

Revision No. 03

(1) Remove the clamps from LH wing, ADDITIONAL WORK

(2) Remove the clamps from RH wing, ADDITIONAL WORK

(3) Modify the routing of routes 1P and 2P at LH wing

(4) Modify the routing of routes 1P and 2P at RH wing

(5) Install the clamps in LH wing, ADDITIONAL WORK

(6) Install the clamps in RH wing, ADDITIONAL WORK

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 12

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@A300-600

SERVICE BULLETIN

**CONF 003

Task 246103-831-801-001: Modification

(1) Remove the clamps between FR50 and FR52 at LH side

(2) Modify the Routing between FR50 and FR52 and between STGR 33 and 30 at LH

side

(3) Install the clamps between FR50 and FR52 at LH side

(4) Install a bracket on the shroud box blanking plate at LH side

(5) Modify the routing on rib 1 on the passage way to the shroud box at LH side

(6) Modify the routing of routes 1P and 2P in the hydraulic shroud box at LH side

(7) Install a support on the support of the BLUE hydraulic reservoir at LH wing

(8) Modify the routing of routes 1E and 1G in the leading edge at LH wing

(9) Remove the clamps between FR50 and FR52 at RH side

(10) Modify the Routing between FR50 and FR52 and between STGR 33 and 30 at RH

side

(11) Install the clamps between FR50 and FR52 at RH side

(12) Install a bracket on the shroud box blanking plate at RH side

(13) Modify the routing on rib 1 on the passage way to the shroud box at RH side

(14) Modify the routing of routes 2E and 2G in the leading edge at RH wing

(15) Remove the clamps from LH wing

(16) Remove the clamps from RH wing

(17) Modify the Electrical Support Brackets in the Outer Shroud Box, LH Wing

(18) Modify the routing of routes 1P and 2P at LH wing

(19) Modify the routing of routes 1P and 2P at RH wing

(20) Install the clamps in LH wing

(21) Install the clamps in RH wing

(22) Modify the P-CLIPS at Location WOFX-204.5, LH Wing

(23) Modify the Backshell of the Connector and the Structure at Location ABX 36.5, LH

Wing

(24) Modify the Electrical Support Brackets in the Outer Shroud Box, RH Wing

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 13

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@A300-600

SERVICE BULLETIN

(25) Modify the P-CLIPS at Location WOFX-204.5, RH Wing

(26) Modify the Backshell of the Connector and the Structure at Location ABX 36.5, RH

Wing

Task 246103-831-802-001: Modification - ADDITIONAL WORK between Revision No. 00 and

Revision No. 03

(1) Modify the routing on rib 1 on the passage way to the shroud box at LH side,

ADDITIONAL WORK

(2) Modify the routing on rib 1 on the passage way to the shroud box at RH side,

ADDITIONAL WORK

(3) Modify the routing of routes 1P and 2P in the shroud box at LH side, ADDITIONAL

WORK

(4) Modify the routing of the routes 1E and 1G in the leading edge at LH wing,

ADDITIONAL WORK

(5) Modify the routing of the routes 2E and 2G in the leading edge at RH wing,

ADDITIONAL WORK

(6) Install a support on the support of the BLUE hydraulic reservoir at LH wing,

ADDITIONAL WORK

(7) Install a bracket on the shroud box blanking plate at LH side, ADDITIONAL WORK

(8) Install a bracket on the shroud box blanking plate at RH side, ADDITIONAL WORK

(9) Remove the clamps between FR50 and FR51 at STRG 32 at LH side, ADDITIONAL

WORK

(10) Remove the clamps of the Passage Way at FR52 (LH side) - ADDITIONAL WORK

(11) Modify the Routing between FR50 and FR52 and between STGR 33 and 30 at LH

side - ADDITIONAL WORK

(12) Install the clamps between FR50 and FR51 at STRG 32 at LH side, ADDITIONAL

WORK

(13) Install the clamps of the Passage Way at FR52 (LH side) - ADDITIONAL WORK

(14) Remove the clamps between FR50 and FR51 at STGR 32 at RH side,

ADDITIONAL WORK

(15) Remove the clamps of the Passage Way at FR52 (RH side) - ADDITIONAL WORK

(16) Modify the Routing between FR50 and FR52 and between STGR 33 and 30 at RH

side - ADDITIONAL WORK

(17) Install the clamps between FR50 and FR51 at STGR 32 at RH side, ADDITIONAL

WORK

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 14

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@A300-600

SERVICE BULLETIN

(18) Install the clamps of the Passage Way at FR52 (RH side) - ADDITIONAL WORK

Task 246103-831-804-001: Modification - ADDITIONAL WORK between Revision No. 01 and

Revision No. 03

(1) Remove the clamps between FR50 and FR52 at LH side, ADDITIONAL WORK

(2) Modify the routing between FR50 and FR52 and between STGR 33 and 30 at LH

side, ADDITIONAL WORK

(3) Install the clamps between FR50 and FR52 at LH side, ADDITIONAL WORK

(4) Install a bracket on the shroud box blanking plate at LH side, ADDITIONAL WORK

(5) Modify the routing on rib 1 on the passage way to the shroud box at LH side,

ADDITIONAL WORK

(6) Modify the routing of routes 1P and 2P in the shroud box at LH side, ADDITIONAL

WORK

(7) Install a support on the support of the BLUE hydraulic reservoir at LH wing -

ADDITIONAL WORK

(8) Modify the routing of the routes 1E and 1G in the leading edge at LH wing,

ADDITIONAL WORK

(9) Remove the clamps between FR50 and FR52 at RH side, ADDITIONAL WORK

(10) Modify the routing between FR50 and FR52 and between STGR 33 and 30 at RH

side, ADDITIONAL WORK

(11) Install the clamps between FR50 and FR52 at RH side, ADDITIONAL WORK

(12) Install a bracket on the shroud box blanking plate at RH side, ADDITIONAL WORK

(13) Modify the routing on Rib 1 on the passage way to the shroud box at RH side,

ADDITIONAL WORK

(14) Modify the routing of the routes 2E and 2G in the leading edge at RH wing,

ADDITIONAL WORK

(15) Remove the clamps from LH wings, ADDITIONAL WORK

(16) Remove the clamps from RH wings, ADDITIONAL WORK

(17) Modify the routing of routes 1P and 2P at LH wing, ADDITIONAL WORK

(18) Modify the routing of routes 1P and 2P at RH wing, ADDITIONAL WORK

(19) Install the clamps in LH wing, ADDITIONAL WORK

(20) Install the clamps in RH wing, ADDITIONAL WORK

Task 246103-831-805-001: Modification - ADDITIONAL WORK between Revision No. 02 and

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 15

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@A300-600

SERVICE BULLETIN

Revision No. 03

(1) Modify the routing on Rib 1 on the passage way to the shroud box at LH side,

ADDITIONAL WORK

(2) Modify the routing on Rib 1 on the passage way to the shroud box at RH side,

ADDITIONAL WORK

(3) Remove the clamps from LH wing, ADDITIONAL WORK

(4) Remove the clamps from RH wing, ADDITIONAL WORK

(5) Modify the routing of routes 1P and 2P at LH wing

(6) Modify the routing of routes 1P and 2P at RH wing

(7) Install the clamps in LH wing, ADDITIONAL WORK

(8) Install the clamps in RH wing, ADDITIONAL WORK

**CONF ALL

E. COMPLIANCE

(1) Classification

MANDATORY: Service Bulletin must be accomplished.

(2) Accomplishment Timescale

Accomplishment of this Service Bulletin is recommended to be embodied within 30

months from SB revision 2 issuance. This Service Bulletin has been classified

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

Aviation Safety Agency (EASA). The AD must be used as the reference document for

the mandated accomplishment timescale.

F. APPROVAL

The technical content of this document is 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.

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 16

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@A300-600

SERVICE BULLETIN

**CONF 001

Task 246103-831-801-001: Modification

Get Access 4.00

On Aircraft

Remove the clamps between FR50 and FR52 at LH

side

1.50

Modify the Routing between FR50 and FR52 and

between STGR 33 and 30 at LH side

1.00

Install the clamps between FR50 and FR52 at LH side 2.00

Install a bracket on the shroud box blanking plate at

LH side

1.00

Modify the routing on rib 1 on the passage way to the

shroud box at LH side

1.00

Modify the routing of routes 1P and 2P in the hydraulic

shroud box at LH side

1.00

Install a support on the support of the BLUE hydraulic

reservoir at LH wing

1.00

Modify the routing of routes 1E and 1G in the leading

edge at LH wing

0.50

Remove the clamps between FR50 and FR52 at RH

side

1.00

Modify the Routing between FR50 and FR52 and

between STGR 33 and 30 at RH side

1.00

Install the clamps between FR50 and FR52 at RH side 1.00

Install a bracket on the shroud box blanking plate at

RH side

1.00

Modify the routing on rib 1 on the passage way to the

shroud box at RH side

1.00

Modify the routing of routes 2E and 2G in the leading

edge at RH wing

0.50

Remove the clamps from LH wing 1.00

Remove the clamps from RH wing 1.00

Modify the Electrical Support Brackets in the Outer

Shroud Box, LH Wing

2.50

Modify the routing of routes 1P and 2P at LH wing 1.50

Modify the routing of routes 1P and 2P at RH wing 1.50

Install the clamps in LH wing 1.00

Install the clamps in RH wing 1.00

Modify the P-CLIPS at Location WOFX-204.5, LH Wing 0.50

Modify the Backshell of the Connector and the

Structure at Location ABX 36.5, LH Wing

0.50

Modify the Electrical Support Brackets in the Outer

Shroud Box, RH Wing

2.50

Modify the P-CLIPS at Location WOFX-204.5, RH

Wing

0.50

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 17

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@A300-600

SERVICE BULLETIN

Task 246103-831-801-001: Modification

Modify the Backshell of the Connector and the

Structure at Location ABX 36.5, RH Wing

0.50

Tests 0.50

Close-Up 5.00

TOTAL MANHOURS 38.00

ELAPSED TIME (HOURS) 22.50

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

Chart, Fig. A-FAAAA given in Appendix 01 - Elapsed Time Assumption

Task 246103-831-802-001: Modification - ADDITIONAL WORK between Revision No. 00 and

Revision No. 03

Get Access 4.00

On Aircraft

Modify the routing on rib 1 on the passage way to the

shroud box at LH side, ADDITIONAL WORK

1.00

Modify the routing on rib 1 on the passage way to the

shroud box at RH side, ADDITIONAL WORK

1.00

Modify the routing of routes 1P and 2P in the shroud

box at LH side, ADDITIONAL WORK

1.00

Modify the routing of the routes 1E and 1G in the

leading edge at LH wing, ADDITIONAL WORK

1.00

Modify the routing of the routes 2E and 2G in the

leading edge at RH wing, ADDITIONAL WORK

1.00

Install a support on the support of the BLUE hydraulic

reservoir at LH wing, ADDITIONAL WORK

2.00

Install a bracket on the shroud box blanking plate at

LH side, ADDITIONAL WORK

1.00

Install a bracket on the shroud box blanking plate at

RH side, ADDITIONAL WORK

1.00

Remove the clamps between FR50 and FR51 at STRG

32 at LH side, ADDITIONAL WORK

0.50

Remove the clamps of the Passage Way at FR52 (LH

side) - ADDITIONAL WORK

0.50

Modify the Routing between FR50 and FR52 and

between STGR 33 and 30 at LH side - ADDITIONAL

WORK

1.00

Install the clamps between FR50 and FR51 at STRG

32 at LH side, ADDITIONAL WORK

0.50

Install the clamps of the Passage Way at FR52 (LH

side) - ADDITIONAL WORK

0.50

Remove the clamps between FR50 and FR51 at STGR

32 at RH side, ADDITIONAL WORK

0.50

Remove the clamps of the Passage Way at FR52 (RH

side) - ADDITIONAL WORK

0.50

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 18

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SERVICE BULLETIN

Task 246103-831-802-001: Modification - ADDITIONAL WORK between Revision No. 00 and

Revision No. 03

Modify the Routing between FR50 and FR52 and

between STGR 33 and 30 at RH side - ADDITIONAL

WORK

1.00

Install the clamps between FR50 and FR51 at STGR

32 at RH side, ADDITIONAL WORK

0.50

Install the clamps of the Passage Way at FR52 (RH

side) - ADDITIONAL WORK

0.50

Tests 0.50

Close-Up 5.00

TOTAL MANHOURS 24.50

ELAPSED TIME (HOURS) 16.50

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

Chart, Fig. A-FACAA given in Appendix 02 - Elapsed Time Assumption -

ADDITIONAL WORK BETWEEN REVISION No. 00 AND REVISION No. 03

Task 246103-831-804-001: Modification - ADDITIONAL WORK between Revision No. 01 and

Revision No. 03

Get Access 4.00

On Aircraft

Remove the clamps between FR50 and FR52 at LH

side, ADDITIONAL WORK

1.00

Modify the routing between FR50 and FR52 and

between STGR 33 and 30 at LH side, ADDITIONAL

WORK

1.00

Install the clamps between FR50 and FR52 at LH side,

ADDITIONAL WORK

1.00

Install a bracket on the shroud box blanking plate at

LH side, ADDITIONAL WORK

1.00

Modify the routing on rib 1 on the passage way to the

shroud box at LH side, ADDITIONAL WORK

1.00

Modify the routing of routes 1P and 2P in the shroud

box at LH side, ADDITIONAL WORK

1.00

Install a support on the support of the BLUE hydraulic

reservoir at LH wing - ADDITIONAL WORK

2.00

Modify the routing of the routes 1E and 1G in the

leading edge at LH wing, ADDITIONAL WORK

0.50

Remove the clamps between FR50 and FR52 at RH

side, ADDITIONAL WORK

1.00

Modify the routing between FR50 and FR52 and

between STGR 33 and 30 at RH side, ADDITIONAL

WORK

1.00

Install the clamps between FR50 and FR52 at RH side,

ADDITIONAL WORK

1.00

Install a bracket on the shroud box blanking plate at

RH side, ADDITIONAL WORK

1.00

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 19

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@A300-600

SERVICE BULLETIN

Task 246103-831-804-001: Modification - ADDITIONAL WORK between Revision No. 01 and

Revision No. 03

Modify the routing on Rib 1 on the passage way to the

shroud box at RH side, ADDITIONAL WORK

1.00

Modify the routing of the routes 2E and 2G in the

leading edge at RH wing, ADDITIONAL WORK

0.50

Remove the clamps from LH wings, ADDITIONAL

WORK

1.00

Remove the clamps from RH wings, ADDITIONAL

WORK

1.00

Modify the routing of routes 1P and 2P at LH wing,

ADDITIONAL WORK

1.50

Modify the routing of routes 1P and 2P at RH wing,

ADDITIONAL WORK

1.50

Install the clamps in LH wing, ADDITIONAL WORK 1.00

Install the clamps in RH wing, ADDITIONAL WORK 1.00

Tests 0.50

Close-Up 5.00

TOTAL MANHOURS 30.50

ELAPSED TIME (HOURS) 16.50

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

Chart,Fig. A-FADAA given in Appendix 03 - Elapsed Time Assumption -

ADDITIONAL WORK BETWEEN REVISION No. 01 AND REVISION No. 03

Task 246103-831-805-001: Modification - ADDITIONAL WORK between Revision No. 02 and

Revision No. 03

Get Access 4.00

On Aircraft

Remove the clamps from LH wing, ADDITIONAL

WORK

1.00

Remove the clamps from RH wing, ADDITIONAL

WORK

1.00

Modify the routing of routes 1P and 2P at LH wing 1.50

Modify the routing of routes 1P and 2P at RH wing 1.50

Install the clamps in LH wing, ADDITIONAL WORK 1.00

Install the clamps in RH wing, ADDITIONAL WORK 1.00

Tests 0.50

Close-Up 5.00

TOTAL MANHOURS 16.50

ELAPSED TIME (HOURS) 8.50

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

Chart, Fig. A-FAFAA given in Appendix 04 - Elapsed Time Assumption -

ADDITIONAL WORK BETWEEN REVISION No. 02 AND REVISION No. 03

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 20

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@A300-600

SERVICE BULLETIN

**CONF 002

Task 246103-831-801-001: Modification

Get Access 4.00

On Aircraft

Remove the clamps between FR50 and FR52 at LH

side

1.50

Modify the Routing between FR50 and FR52 and

between STGR 33 and 30 at LH side

1.00

Install the clamps between FR50 and FR52 at LH side 2.00

Install a bracket on the shroud box blanking plate at

LH side

1.00

Modify the routing on rib 1 on the passage way to the

shroud box at LH side

1.00

Modify the routing of routes 1P and 2P in the hydraulic

shroud box at LH side

1.00

Install a support on the support of the BLUE hydraulic

reservoir at LH wing

1.00

Modify the routing of routes 1E and 1G in the leading

edge at LH wing

0.50

Remove the clamps between FR50 and FR52 at RH

side

1.00

Modify the Routing between FR50 and FR52 and

between STGR 33 and 30 at RH side

1.00

Install the clamps between FR50 and FR52 at RH side 1.00

Install a bracket on the shroud box blanking plate at

RH side

1.00

Modify the routing on rib 1 on the passage way to the

shroud box at RH side

1.00

Modify the routing of routes 2E and 2G in the leading

edge at RH wing

0.50

Remove the clamps from LH wing. 1.00

Remove the clamps from RH wing. 1.00

Modify the Electrical Support Brackets in the Outer

Shroud Box, LH Wing

1.50

Modify the routing of routes 1P and 2P at LH wing 1.50

Modify the routing of routes 1P and 2P at RH wing 1.50

Install the clamps in LH wing. 1.00

Install the clamps in RH wing. 1.00

Modify the P-CLIPS at Location WOFX-204.5, LH Wing 0.50

Modify the Backshell of the Connector and the

Structure at Location ABX 36.5, LH Wing

0.50

Modify the Electrical Support Brackets in the Outer

Shroud Box, RH Wing

1.50

Modify the P-CLIPS at Location WOFX-204.5, RH

Wing

0.50

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 21

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

Task 246103-831-801-001: Modification

Modify the Backshell of the Connector and the

Structure at Location ABX 36.5, RH Wing

0.50

Tests 0.50

Close-Up 5.00

TOTAL MANHOURS 36.00

ELAPSED TIME (HOURS) 20.75

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

Chart, Fig. A-FABAA given in Appendix 01 - Elapsed Time Assumption

Task 246103-831-802-001: Modification - ADDITIONAL WORK between Revision No. 00 and

Revision No. 03

Get Access 4.00

On Aircraft

Modify the routing on rib 1 on the passage way to the

shroud box at LH side, ADDITIONAL WORK

1.00

Modify the routing on rib 1 on the passage way to the

shroud box at RH side, ADDITIONAL WORK

1.00

Modify the routing of routes 1P and 2P in the shroud

box at LH side, ADDITIONAL WORK

1.00

Modify the routing of the routes 1E and 1G in the

leading edge at LH wing, ADDITIONAL WORK

1.00

Modify the routing of the routes 2E and 2G in the

leading edge at RH wing, ADDITIONAL WORK

1.00

Install a support on the support of the BLUE hydraulic

reservoir at LH wing, ADDITIONAL WORK

2.00

Install a bracket on the shroud box blanking plate at

LH side, ADDITIONAL WORK

1.00

Install a bracket on the shroud box blanking plate at

RH side, ADDITIONAL WORK

1.00

Remove the clamps between FR50 and FR51 at STRG

32 at LH side, ADDITIONAL WORK

0.50

Remove the clamps of the Passage Way at FR52 (LH

side) - ADDITIONAL WORK

0.50

Modify the Routing between FR50 and FR52 and

between STGR 33 and 30 at LH side - ADDITIONAL

WORK

1.00

Install the clamps between FR50 and FR51 at STRG

32 at LH side, ADDITIONAL WORK

0.50

Install the clamps of the Passage Way at FR52 (LH

side) - ADDITIONAL WORK

0.50

Remove the clamps between FR50 and FR51 at STGR

32 at RH side, ADDITIONAL WORK

0.50

Remove the clamps of the Passage Way at FR52 (RH

side) - ADDITIONAL WORK

0.50

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 22

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

Task 246103-831-802-001: Modification - ADDITIONAL WORK between Revision No. 00 and

Revision No. 03

Modify the Routing between FR50 and FR52 and

between STGR 33 and 30 at RH side - ADDITIONAL

WORK

1.00

Install the clamps between FR50 and FR51 at STGR

32 at RH side, ADDITIONAL WORK

0.50

Install the clamps of the Passage Way at FR52 (RH

side) - ADDITIONAL WORK

0.50

Tests 0.50

Close-Up 5.00

TOTAL MANHOURS 24.50

ELAPSED TIME (HOURS) 16.50

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

Chart, Fig. A-FACAA given in Appendix 02 - Elapsed Time Assumption -

ADDITIONAL WORK BETWEEN REVISION No. 00 AND REVISION No. 03

Task 246103-831-804-001: Modification - ADDITIONAL WORK between Revision No. 01 and

Revision No. 03

Get Access 4.00

On Aircraft

Remove the clamps between FR50 and FR52 at LH

side, ADDITIONAL WORK

1.00

Modify the routing between FR50 and FR52 and

between STGR 33 and 30 at LH side, ADDITIONAL

WORK

1.00

Install the clamps between FR50 and FR52 at LH side,

ADDITIONAL WORK

1.00

Install a bracket on the shroud box blanking plate at

LH side, ADDITIONAL WORK

1.00

Modify the routing on rib 1 on the passage way to the

shroud box at LH side, ADDITIONAL WORK

1.00

Modify the routing of routes 1P and 2P in the shroud

box at LH side, ADDITIONAL WORK

1.00

Install a support on the support of the BLUE hydraulic

reservoir at LH wing - ADDITIONAL WORK

2.00

Modify the routing of the routes 1E and 1G in the

leading edge at LH wing, ADDITIONAL WORK

0.50

Remove the clamps between FR50 and FR52 at RH

side, ADDITIONAL WORK

1.00

Modify the routing between FR50 and FR52 and

between STGR 33 and 30 at RH side, ADDITIONAL

WORK

1.00

Install the clamps between FR50 and FR52 at RH side,

ADDITIONAL WORK

1.00

Install a bracket on the shroud box blanking plate at

RH side, ADDITIONAL WORK

1.00

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 23

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

Task 246103-831-804-001: Modification - ADDITIONAL WORK between Revision No. 01 and

Revision No. 03

Modify the routing on Rib 1 on the passage way to the

shroud box at RH side, ADDITIONAL WORK

1.00

Modify the routing of the routes 2E and 2G in the

leading edge at RH wing, ADDITIONAL WORK

0.50

Remove the clamps from LH wings, ADDITIONAL

WORK

1.00

Remove the clamps from RH wings, ADDITIONAL

WORK

1.00

Modify the routing of routes 1P and 2P at LH wing,

ADDITIONAL WORK

1.50

Modify the routing of routes 1P and 2P at RH wing,

ADDITIONAL WORK

1.50

Install the clamps in LH wing, ADDITIONAL WORK 1.00

Install the clamps in RH wing, ADDITIONAL WORK 1.00

Tests 0.50

Close-Up 5.00

TOTAL MANHOURS 30.50

ELAPSED TIME (HOURS) 16.50

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

Chart,Fig. A-FADAA given in Appendix 03 - Elapsed Time Assumption -

ADDITIONAL WORK BETWEEN REVISION No. 01 AND REVISION No. 03

Task 246103-831-805-001: Modification - ADDITIONAL WORK between Revision No. 02 and

Revision No. 03

Get Access 4.00

On Aircraft

Remove the clamps from LH wing, ADDITIONAL

WORK

1.00

Remove the clamps from RH wing, ADDITIONAL

WORK

1.00

Modify the routing of routes 1P and 2P at LH wing 1.50

Modify the routing of routes 1P and 2P at RH wing 1.50

Install the clamps in LH wing, ADDITIONAL WORK 1.00

Install the clamps in RH wing, ADDITIONAL WORK 1.00

Tests 0.50

Close-Up 5.00

TOTAL MANHOURS 16.50

ELAPSED TIME (HOURS) 8.50

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

Chart,Fig. A-FAFAA given in Appendix 04 - Elapsed Time Assumption -

ADDITIONAL WORK BETWEEN REVISION No. 02 AND REVISION No. 03

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 24

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF 003

Task 246103-831-801-001: Modification

Get Access 4.00

On Aircraft

Remove the clamps between FR50 and FR52 at LH

side

1.50

Modify the Routing between FR50 and FR52 and

between STGR 33 and 30 at LH side

1.00

Install the clamps between FR50 and FR52 at LH side 2.00

Install a bracket on the shroud box blanking plate at

LH side

1.00

Modify the routing on rib 1 on the passage way to the

shroud box at LH side

1.00

Modify the routing of routes 1P and 2P in the hydraulic

shroud box at LH side

1.00

Install a support on the support of the BLUE hydraulic

reservoir at LH wing

1.00

Modify the routing of routes 1E and 1G in the leading

edge at LH wing

0.50

Remove the clamps between FR50 and FR52 at RH

side

1.00

Modify the Routing between FR50 and FR52 and

between STGR 33 and 30 at RH side

1.00

Install the clamps between FR50 and FR52 at RH side 1.00

Install a bracket on the shroud box blanking plate at

RH side

1.00

Modify the routing on rib 1 on the passage way to the

shroud box at RH side

1.00

Modify the routing of routes 2E and 2G in the leading

edge at RH wing

0.50

Remove the clamps from LH wing 1.00

Remove the clamps from RH wing 1.00

Modify the Electrical Support Brackets in the Outer

Shroud Box, LH Wing

2.50

Modify the routing of routes 1P and 2P at LH wing 1.50

Modify the routing of routes 1P and 2P at RH wing 1.50

Install the clamps in LH wing 1.00

Install the clamps in RH wing 1.00

Modify the P-CLIPS at Location WOFX-204.5, LH Wing 0.50

Modify the Backshell of the Connector and the

Structure at Location ABX 36.5, LH Wing

0.50

Modify the Electrical Support Brackets in the Outer

Shroud Box, RH Wing

2.50

Modify the P-CLIPS at Location WOFX-204.5, RH

Wing

0.50

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 25

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

Task 246103-831-801-001: Modification

Modify the Backshell of the Connector and the

Structure at Location ABX 36.5, RH Wing

0.50

Tests 0.50

Close-Up 5.00

TOTAL MANHOURS 38.00

ELAPSED TIME (HOURS) 22.50

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

Chart, Fig. A-FAAAA given in Appendix 01 - Elapsed Time Assumption

Task 246103-831-802-001: Modification - ADDITIONAL WORK between Revision No. 00 and

Revision No. 03

Get Access 4.00

On Aircraft

Modify the routing on rib 1 on the passage way to the

shroud box at LH side, ADDITIONAL WORK

1.00

Modify the routing on rib 1 on the passage way to the

shroud box at RH side, ADDITIONAL WORK

1.00

Modify the routing of routes 1P and 2P in the shroud

box at LH side, ADDITIONAL WORK

1.00

Modify the routing of the routes 1E and 1G in the

leading edge at LH wing, ADDITIONAL WORK

1.00

Modify the routing of the routes 2E and 2G in the

leading edge at RH wing, ADDITIONAL WORK

1.00

Install a support on the support of the BLUE hydraulic

reservoir at LH wing, ADDITIONAL WORK

2.00

Install a bracket on the shroud box blanking plate at

LH side, ADDITIONAL WORK

1.00

Install a bracket on the shroud box blanking plate at

RH side, ADDITIONAL WORK

1.00

Remove the clamps between FR50 and FR51 at STRG

32 at LH side, ADDITIONAL WORK

0.50

Remove the clamps of the Passage Way at FR52 (LH

side) - ADDITIONAL WORK

0.50

Modify the Routing between FR50 and FR52 and

between STGR 33 and 30 at LH side - ADDITIONAL

WORK

1.00

Install the clamps between FR50 and FR51 at STRG

32 at LH side, ADDITIONAL WORK

0.50

Install the clamps of the Passage Way at FR52 (LH

side) - ADDITIONAL WORK

0.50

Remove the clamps between FR50 and FR51 at STGR

32 at RH side, ADDITIONAL WORK

0.50

Remove the clamps of the Passage Way at FR52 (RH

side) - ADDITIONAL WORK

0.50

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 26

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

Task 246103-831-802-001: Modification - ADDITIONAL WORK between Revision No. 00 and

Revision No. 03

Modify the Routing between FR50 and FR52 and

between STGR 33 and 30 at RH side - ADDITIONAL

WORK

1.00

Install the clamps between FR50 and FR51 at STGR

32 at RH side, ADDITIONAL WORK

0.50

Install the clamps of the Passage Way at FR52 (RH

side) - ADDITIONAL WORK

0.50

Tests 0.50

Close-Up 5.00

TOTAL MANHOURS 24.50

ELAPSED TIME (HOURS) 16.50

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

Chart, Fig. A-FACAA given in Appendix 02 - Elapsed Time Assumption -

ADDITIONAL WORK BETWEEN REVISION No. 00 AND REVISION No. 03

Task 246103-831-804-001: Modification - ADDITIONAL WORK between Revision No. 01 and

Revision No. 03

Get Access 4.00

On Aircraft

Remove the clamps between FR50 and FR52 at LH

side, ADDITIONAL WORK

1.00

Modify the routing between FR50 and FR52 and

between STGR 33 and 30 at LH side, ADDITIONAL

WORK

1.00

Install the clamps between FR50 and FR52 at LH side,

ADDITIONAL WORK

1.00

Install a bracket on the shroud box blanking plate at

LH side, ADDITIONAL WORK

1.00

Modify the routing on rib 1 on the passage way to the

shroud box at LH side, ADDITIONAL WORK

1.00

Modify the routing of routes 1P and 2P in the shroud

box at LH side, ADDITIONAL WORK

1.00

Install a support on the support of the BLUE hydraulic

reservoir at LH wing - ADDITIONAL WORK

2.00

Modify the routing of the routes 1E and 1G in the

leading edge at LH wing, ADDITIONAL WORK

0.50

Remove the clamps between FR50 and FR52 at RH

side, ADDITIONAL WORK

1.00

Modify the routing between FR50 and FR52 and

between STGR 33 and 30 at RH side, ADDITIONAL

WORK

1.00

Install the clamps between FR50 and FR52 at RH side,

ADDITIONAL WORK

1.00

Install a bracket on the shroud box blanking plate at

RH side, ADDITIONAL WORK

1.00

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 27

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

Task 246103-831-804-001: Modification - ADDITIONAL WORK between Revision No. 01 and

Revision No. 03

Modify the routing on Rib 1 on the passage way to the

shroud box at RH side, ADDITIONAL WORK

1.00

Modify the routing of the routes 2E and 2G in the

leading edge at RH wing, ADDITIONAL WORK

0.50

Remove the clamps from LH wings, ADDITIONAL

WORK

1.00

Remove the clamps from RH wings, ADDITIONAL

WORK

1.00

Modify the routing of routes 1P and 2P at LH wing,

ADDITIONAL WORK

1.50

Modify the routing of routes 1P and 2P at RH wing,

ADDITIONAL WORK

1.50

Install the clamps in LH wing, ADDITIONAL WORK 1.00

Install the clamps in RH wing, ADDITIONAL WORK 1.00

Tests 0.50

Close-Up 5.00

TOTAL MANHOURS 30.50

ELAPSED TIME (HOURS) 16.50

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

Chart,Fig. A-FADAA given in Appendix 03 - Elapsed Time Assumption -

ADDITIONAL WORK BETWEEN REVISION No. 01 AND REVISION No. 03

Task 246103-831-805-001: Modification - ADDITIONAL WORK between Revision No. 02 and

Revision No. 03

Get Access 4.00

On Aircraft

Modify the routing on Rib 1 on the passage way to the

shroud box at LH side, ADDITIONAL WORK

1.00

Modify the routing on Rib 1 on the passage way to the

shroud box at RH side, ADDITIONAL WORK

1.00

Remove the clamps from LH wing, ADDITIONAL

WORK

1.00

Remove the clamps from RH wing, ADDITIONAL

WORK

1.00

Modify the routing of routes 1P and 2P at LH wing 1.50

Modify the routing of routes 1P and 2P at RH wing 1.50

Install the clamps in LH wing, ADDITIONAL WORK 1.00

Install the clamps in RH wing, ADDITIONAL WORK 1.00

Tests 0.50

Close-Up 5.00

TOTAL MANHOURS 18.50

ELAPSED TIME (HOURS) 9.50

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

Chart, Fig. A-FAFAB given in Appendix 04 - Elapsed Time Assumption -

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 28

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

ADDITIONAL WORK BETWEEN REVISION No. 02 AND REVISION No. 03

**CONF ALL

H. WEIGHT AND BALANCE

Not Changed

I. ELECTRICAL LOAD DATA

Not Changed

J. REFERENCES

**CONF 001

Aircraft Maintenance Manual (AMM) 06-21-00 06-31-53 06-41-57

20-21-12 24-00-00 27-50-00

27-54-41 29-10-00 29-12-46

32-12-11 51-23-10 53-15-63

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-25-51 20-33-00 20-33-11

20-33-30 20-33-41 20-33-42

20-33-44 20-33-45 20-55-00

Process and Material Specification (PMS) Process and Material Specification

(PMS) 01-01-28 Process E

Standards Manual (SM)

Structural Repair Manual (SRM) 51-21-00 51-21-10 51-23-10

51-40-00 51-40-20 51-40-30

51-40-40 51-40-50 51-75-10

**CONF 002

Aircraft Maintenance Manual (AMM) 06-21-00 06-31-53 06-41-57

20-21-12 24-00-00 27-50-00

27-54-41 29-10-00 29-12-46

32-12-11 51-23-10 53-15-63

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-25-51 20-33-00 20-33-11

20-33-30 20-33-41 20-33-42

20-33-44 20-33-45 20-55-00

Process and Material Specification (PMS) Process and Material Specification

(PMS) 01-01-28 Process E

Standards Manual (SM)

Structural Repair Manual (SRM) 51-21-00 51-21-10 51-23-10

51-40-00 51-40-20 51-40-30

51-40-40 51-40-50 51-75-10

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 29

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF 003

Aircraft Maintenance Manual (AMM) 06-21-00 06-31-53 06-41-57

20-21-12 24-00-00 27-50-00

27-54-41 29-10-00 29-12-46

32-12-11 51-23-10 53-15-63

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-25-51 20-33-00 20-33-11

20-33-30 20-33-41 20-33-42

20-33-44 20-33-45 20-55-00

Process and Material Specification (PMS) Process and Material Specification

(PMS) 01-01-28 Process E

Standards Manual (SM)

Structural Repair Manual (SRM) 51-21-00 51-21-10 51-23-10

51-40-00 51-40-20 51-40-30

51-40-40 51-40-50 51-75-10

**CONF ALL

K. PUBLICATION AFFECTED

Illustrated Parts Catalog (IPC) 24-92-03

L. INTERCHANGEABILITY/MIXABILITY

Not Applicable

M. SPARES

None

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 30

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

(1) Procurement Addresses

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 :

Kit 246103A01R14

Kit 246103A02R12

Kit 246103A03R04

Kit 246103A04R00

Kit 246103A05R00

Supplementary kit 246103A01S03

Supplementary kit 246103A01S08

Supplementary kit 246103A01S11

Supplementary kit 246103A01S12

Supplementary kit 246103A01S13

Supplementary kit 246103A02S03

Supplementary kit 246103A02S07

Supplementary kit 246103A02S10

Supplementary kit 246103A02S11

Supplementary kit 246103A03S01

AIRBUS Material, Logistics and Suppliers

ATP II B,

Hein-Sass-Weg 24

21129 HAMBURG

GERMANY

For ordering by internet:

http://spares.airbus.com

For ordering by E-mail: airbus.kit@airbus.com

Telephone Hotlines:

A350/A380: +49 40 743 51775

A330/340, A300/310: +49 40 743 51616

A318/319/320/321: +49 40 743 51660

Kit 246103B01R03

Kit 246103B02R02

AIRBUS Material, Logistics and Suppliers

ATP II B,

Hein-Sass-Weg 24

21129 HAMBURG

GERMANY

For ordering by internet:

http://spares.airbus.com

For ordering by E-mail: airbus.kit@airbus.com

Telephone Hotlines:

A350/A380: +49 40 743 51775

A330/340, A300/310: +49 40 743 51616

A318/319/320/321: +49 40 743 51660

(2) Price and Availability

Kit 246103A01R14

Cost 3,600.00 USD

Availability 120 calendar days from receipt of order

The availability given above is the standard lead time from the date of your purchase

order. If items are required before this time, please include a retrofit planning schedule

with your order so that we can try to comply with your requirements.

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 31

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

The sales terms (costs and availability) are estimated in relation to economic conditions.

The latest valid price and lead time for ordering purposes shall be obtained through the

AirbusSpares portal or through a request for quotation to airbus.kit@airbus.com.

Supplementary kit 246103A01S03

Cost 2,850.00 USD

Availability 90 calendar days from receipt of order

The availability given above is the standard lead time from the date of your purchase

order. If items are required before this time, please include a retrofit planning schedule

with your order so that we can try to comply with your requirements.

The sales terms (costs and availability) are estimated in relation to economic conditions.

The latest valid price and lead time for ordering purposes shall be obtained through the

AirbusSpares portal or through a request for quotation to airbus.kit@airbus.com.

Supplementary kit 246103A01S08

Cost 4,300.00 USD

Availability 90 calendar days from receipt of order

The availability given above is the standard lead time from the date of your purchase

order. If items are required before this time, please include a retrofit planning schedule

with your order so that we can try to comply with your requirements.

The sales terms (costs and availability) are estimated in relation to economic conditions.

The latest valid price and lead time for ordering purposes shall be obtained through the

AirbusSpares portal or through a request for quotation to airbus.kit@airbus.com.

Supplementary kit 246103A01S11

Cost 90.00 USD

Availability 90 calendar days from receipt of order

The availability given above is the standard lead time from the date of your purchase

order. If items are required before this time, please include a retrofit planning schedule

with your order so that we can try to comply with your requirements.

The sales terms (costs and availability) are estimated in relation to economic conditions.

The latest valid price and lead time for ordering purposes shall be obtained through the

AirbusSpares portal or through a request for quotation to airbus.kit@airbus.com.

Supplementary kit 246103A01S12

Cost 130.00 USD

Availability 60 calendar days from receipt of order

The availability given above is the standard lead time from the date of your purchase

order. If items are required before this time, please include a retrofit planning schedule

with your order so that we can try to comply with your requirements.

The sales terms (costs and availability) are estimated in relation to economic conditions.

The latest valid price and lead time for ordering purposes shall be obtained through the

AirbusSpares portal or through a request for quotation to airbus.kit@airbus.com.

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 32

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

Supplementary kit 246103A01S13

Cost 25.00 USD

Availability 60 calendar days from receipt of order

The availability given above is the standard lead time from the date of your purchase

order. If items are required before this time, please include a retrofit planning schedule

with your order so that we can try to comply with your requirements.

The sales terms (costs and availability) are estimated in relation to economic conditions.

The latest valid price and lead time for ordering purposes shall be obtained through the

AirbusSpares portal or through a request for quotation to airbus.kit@airbus.com.

Kit 246103A02R12

Cost 3,400.00 USD

Availability 90 calendar days from receipt of order

The availability given above is the standard lead time from the date of your purchase

order. If items are required before this time, please include a retrofit planning schedule

with your order so that we can try to comply with your requirements.

The sales terms (costs and availability) are estimated in relation to economic conditions.

The latest valid price and lead time for ordering purposes shall be obtained through the

AirbusSpares portal or through a request for quotation to airbus.kit@airbus.com.

Supplementary kit 246103A02S03

Cost 2,150.00 USD

Availability 90 calendar days from receipt of order

The availability given above is the standard lead time from the date of your purchase

order. If items are required before this time, please include a retrofit planning schedule

with your order so that we can try to comply with your requirements.

The sales terms (costs and availability) are estimated in relation to economic conditions.

The latest valid price and lead time for ordering purposes shall be obtained through the

AirbusSpares portal or through a request for quotation to airbus.kit@airbus.com.

Supplementary kit 246103A02S07

Cost 2,960.00 USD

Availability 90 calendar days from receipt of order

The availability given above is the standard lead time from the date of your purchase

order. If items are required before this time, please include a retrofit planning schedule

with your order so that we can try to comply with your requirements.

The sales terms (costs and availability) are estimated in relation to economic conditions.

The latest valid price and lead time for ordering purposes shall be obtained through the

AirbusSpares portal or through a request for quotation to airbus.kit@airbus.com.

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 33

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@A300-600

SERVICE BULLETIN

Supplementary kit 246103A02S10

Cost 120.00 USD

Availability 90 calendar days from receipt of order

The availability given above is the standard lead time from the date of your purchase

order. If items are required before this time, please include a retrofit planning schedule

with your order so that we can try to comply with your requirements.

The sales terms (costs and availability) are estimated in relation to economic conditions.

The latest valid price and lead time for ordering purposes shall be obtained through the

AirbusSpares portal or through a request for quotation to airbus.kit@airbus.com.

Supplementary kit 246103A02S11

Cost 240.00 USD

Availability 60 calendar days from receipt of order

The availability given above is the standard lead time from the date of your purchase

order. If items are required before this time, please include a retrofit planning schedule

with your order so that we can try to comply with your requirements.

The sales terms (costs and availability) are estimated in relation to economic conditions.

The latest valid price and lead time for ordering purposes shall be obtained through the

AirbusSpares portal or through a request for quotation to airbus.kit@airbus.com.

Kit 246103A03R04

Cost 55.00 USD

Availability 60 calendar days from receipt of order

The availability given above is the standard lead time from the date of your purchase

order. If items are required before this time, please include a retrofit planning schedule

with your order so that we can try to comply with your requirements.

The sales terms (costs and availability) are estimated in relation to economic conditions.

The latest valid price and lead time for ordering purposes shall be obtained through the

AirbusSpares portal or through a request for quotation to airbus.kit@airbus.com.

Supplementary kit 246103A03S01

Cost 55.00 USD

Availability 60 calendar days from receipt of order

The availability given above is the standard lead time from the date of your purchase

order. If items are required before this time, please include a retrofit planning schedule

with your order so that we can try to comply with your requirements.

The sales terms (costs and availability) are estimated in relation to economic conditions.

The latest valid price and lead time for ordering purposes shall be obtained through the

AirbusSpares portal or through a request for quotation to airbus.kit@airbus.com.

Kit 246103A04R00

Cost 710.00 USD

Availability 90 calendar days from receipt of order

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 34

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@A300-600

SERVICE BULLETIN

The availability given above is the standard lead time from the date of your purchase

order. If items are required before this time, please include a retrofit planning schedule

with your order so that we can try to comply with your requirements.

The sales terms (costs and availability) are estimated in relation to economic conditions.

The latest valid price and lead time for ordering purposes shall be obtained through the

AirbusSpares portal or through a request for quotation to airbus.kit@airbus.com.

Kit 246103A05R00

Cost 710.00 USD

Availability 90 calendar days from receipt of order

The availability given above is the standard lead time from the date of your purchase

order. If items are required before this time, please include a retrofit planning schedule

with your order so that we can try to comply with your requirements.

The sales terms (costs and availability) are estimated in relation to economic conditions.

The latest valid price and lead time for ordering purposes shall be obtained through the

AirbusSpares portal or through a request for quotation to airbus.kit@airbus.com.

Kit 246103B01R03

Cost 3,100.00 USD

Availability 120 calendar days from receipt of order

10% commission rate valid until 31.12.2015.

The availability given above is the standard lead time from the date of your purchase

order. If items are required before this time, please include a retrofit planning schedule

with your order so that we can try to comply with your requirements.

Kit 246103B02R02

Cost 571.00 USD

Availability 120 calendar days from receipt of order

10% commission rate valid until 31.12.2015.

The availability given above is the standard lead time from the date of your purchase

order. If items are required before this time, please include a retrofit planning schedule

with your order so that we can try to comply with your requirements.

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 31/15.

C. LIST OF COMPONENTS

NOTE: This table shows the supplemental kits (S kits) needed to update the kits

already held in your stock to the latest status.

Kit held by operator Supplementary kit required Latest status of kit

246103A01R01 246103A01S03 246103A01R05

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 35

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@A300-600

SERVICE BULLETIN

246103A01R01 246103A01S08 246103A01R11

246103A01R01 246103A01S11 246103A01R14

246103A01R11 246103A01S12 246103A01R14

246103A01R14 NONE 246103A01R14

NOTE: This table shows the supplemental kits (S kits) needed to update the kits

already held in your stock to the latest status.

Kit held by operator Supplementary kit required Latest status of kit

246103A02R00 246103A02S03 246103A02R04

246103A02R00 246103A02S07 246103A02R09

246103A02R00 246103A02S10 246103A02R12

246103A02R09 246103A02S11 246103A02R12

246103A02R12 NONE 246103A02R12

NOTE: This table shows the supplemental kits (S kits) needed to update the kits

already held in your stock to the latest status.

Kit held by operator Supplementary kit required Latest status of kit

246103A03R00 246103A01S03 246103A03R04

246103A03R04 None 246103A03R04

Kit 246103A01R14

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

NOTES

10 NAS1801-3-17 1 SCREW

12 NSA5527-03-01 10 SPACER

13 NSA5527-03-03 1 SPACER

14 NSA5527-03-02 5 SPACER

19 NSA935807-09 2 CLAMP

20 NSA935808-01 9 WASHER

21 NSA5050-3 4 NUT

22 NAS1801-3-24 1 SCREW

23 NSA935401-05 1 TIE

24 NSA939510BN 1 (M) STRIP

26 NSA935401-04 12 TIE

28 A0041113420000 1 BRACKET

30 NAS1801-3-8 2 SCREW

31 NAS1801-3-11 1 SCREW

33 NAS1801-3-25 1 SCREW

34 NSA5527-03-08 8 SPACER

37 NAS1801-3-9 4 SCREW

38 ABS0731A01 1 SUPPORT

39 A9222505750000 2 SPACER

41 A0041095620000 1 SEAL

42 A0041095400000 1 BRACKET

43 NSA5067-3-1 4 NUT

46 NAS1149F0332P 19 WASHER

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 36

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@A300-600

SERVICE BULLETIN

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

NOTES

47 NAS1801-3-7 4 SCREW

48 MS21042-3 1 NUT

50 NAS1801-3-13 1 SCREW

52 NSA5516-08ND 8 CLAMP

55 NAS1801-3-16 2 SCREW

63 NSA5516-13ND 14 CLAMP

64 NSA5516-31ND 14 CLAMP

66 NSA935401-13 5 TIE

67 A0041113300000 1 BRACKET

68 ASNA2050DXJ4828 2 RIVET

69 NSA935807-06 1 CLAMP

70 A0041113500000 1 CLAMP

71 NAS1801-3-12 3 SCREW

75 A0041113500200 1 CLAMP

76 A0041113500400 1 CLAMP

77 EN6049-007-19-5 7.5 (M) SLEEVE

78 EN6049-007-13-5 7.5 (M) SLEEVE

79 NAS1801-3-18 1 SCREW

81 NAS1801-3-20 6 SCREW

84 NSA5527-03-06 1 SPACER

85 ASNA51072503 2 (M) TAPE

86 EN6049-007-08-5 5 (M) SLEEVE

87 NSA360002 1 (M) EXTRUSIN

ASNA2528-3 2 NUT

EN6115V3-4 2 BOLT

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 246103A02R12

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

NOTES

12 NSA5527-03-01 5 SPACER

13 NSA5527-03-03 1 SPACER

14 NSA5527-03-02 5 SPACER

19 NSA935807-09 2 CLAMP

20 NSA935808-01 1 WASHER

21 NSA5050-3 4 NUT

22 NAS1801-3-24 1 SCREW

24 NSA939510BN 1 (M) STRIP

26 NSA935401-04 12 TIE

29 A0041113420100 1 BRACKET

30 NAS1801-3-8 2 SCREW

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 37

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SERVICE BULLETIN

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

NOTES

33 NAS1801-3-25 1 SCREW

34 NSA5527-03-08 2 SPACER

37 NAS1801-3-9 4 SCREW

39 A9222505750000 2 SPACER

43 NSA5067-3-1 2 NUT

46 NAS1149F0332P 14 WASHER

50 NAS1801-3-13 2 SCREW

52 NSA5516-08ND 8 CLAMP

55 NAS1801-3-16 2 SCREW

63 NSA5516-13ND 14 CLAMP

64 NSA5516-31ND 14 CLAMP

66 NSA935401-13 5 TIE

70 A0041113500000 1 CLAMP

71 NAS1801-3-12 2 SCREW

75 A0041113500200 1 CLAMP

76 A0041113500400 1 CLAMP

77 EN6049-007-19-5 7.5 (M) SLEEVE

78 EN6049-007-13-5 7.5 (M) SLEEVE

79 NAS1801-3-18 1 SCREW

86 EN6049-007-08-5 5 (M) SLEEVE

87 NSA360002 1 (M) EXTRUSIN

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 246103A03R04

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

NOTES

21 NSA5050-3 2 NUT

22 NAS1801-3-24 2 SCREW

90 NAS1149D0316H 2 WASHER

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 246103A04R00

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

NOTES

12 NSA5527-03-01 1 SPACER

13 NSA5527-03-03 1 SPACER

14 NSA5527-03-02 3 SPACER

21 NSA5050-3 4 NUT

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 38

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@A300-600

SERVICE BULLETIN

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

NOTES

23 NSA935401-05 2 TIE

24 NSA939510BN 3 (M) STRIP

26 NSA935401-04 2 TIE

33 NAS1801-3-25 1 SCREW

46 NAS1149F0332P 5 WASHER

51 NSA5516-12ND 15 CLAMP

52 NSA5516-08ND 15 CLAMP

62 NAS1801-3-22 1 SCREW

63 NSA5516-13ND 15 CLAMP

64 NSA5516-31ND 15 CLAMP

66 NSA935401-13 2 TIE

84 NSA5527-03-06 1 SPACER

87 NSA360002 1 (M) EXTRUSIN

91 NSA5527-03-15 2 SPACER

92 NSA5527-03-12 1 SPACER

94 NSA5159-35 1 STUD

95 NSA5527-03-18 1 SPACER

96 NSA5527-03-09 1 SPACER

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 246103A05R00

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

NOTES

12 NSA5527-03-01 5 SPACER

13 NSA5527-03-03 1 SPACER

14 NSA5527-03-02 3 SPACER

21 NSA5050-3 4 NUT

23 NSA935401-05 2 TIE

24 NSA939510BN 1 (M) STRIP

26 NSA935401-04 2 TIE

33 NAS1801-3-25 1 SCREW

46 NAS1149F0332P 5 WASHER

51 NSA5516-12ND 15 CLAMP

52 NSA5516-08ND 15 CLAMP

62 NAS1801-3-22 1 SCREW

63 NSA5516-13ND 15 CLAMP

64 NSA5516-31ND 15 CLAMP

66 NSA935401-13 2 TIE

84 NSA5527-03-06 1 SPACER

87 NSA360002 1 (M) EXTRUSIN

91 NSA5527-03-15 2 SPACER

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 39

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@A300-600

SERVICE BULLETIN

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

NOTES

92 NSA5527-03-12 1 SPACER

94 NSA5159-35 1 STUD

95 NSA5527-03-18 1 SPACER

96 NSA5527-03-09 1 SPACER

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.

Supplementary kit 246103A01S03

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

NOTES

12 NSA5527-03-01 5 SPACER

14 NSA5527-03-02 2 SPACER

19 NSA935807-09 14 CLAMP

20 NSA935808-01 8 WASHER

21 NSA5050-3 3 NUT

24 NSA939510BN 1 (M) STRIP (24) MS35489-6

28 A0041113420000 1 BRACKET

30 NAS1801-3-8 2 SCREW

31 NAS1801-3-11 1 SCREW

33 NAS1801-3-25 2 SCREW

34 NSA5527-03-08 7 SPACER

37 NAS1801-3-9 1 SCREW

43 NSA5067-3-1 2 NUT

46 NAS1149F0332P 4 WASHER

62 NAS1801-3-22 14 SCREW

63 NSA5516-13ND 12 CLAMP

64 NSA5516-31ND 12 CLAMP

66 NSA935401-08 2 TIE

67 A0041113300000 1 BRACKET

68 ASNA2050DXJ4828 2 RIVET

69 NSA935807-06 1 CLAMP

70 A0041113500000 1 CLAMP

71 NAS1801-3-12 2 SCREW

75 A0041113500200 1 CLAMP

76 A0041113500400 1 CLAMP

77 EN6049-007-19-5 7.5 (M) SLEEVE

78 EN6049-007-13-5 7.5 (M) SLEEVE

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.

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 40

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SERVICE BULLETIN

Supplementary kit 246103A01S08

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

NOTES

12 NSA5527-03-01 5 SPACER

14 NSA5527-03-02 5 SPACER

19 NSA935807-09 10 CLAMP

20 NSA935808-01 8 WASHER

21 NSA5050-3 3 NUT

24 NSA939510BN 1 (M) STRIP

25 ABS0596S005 2 INSULATR

26 NSA935401-04 12 TIE

28 A0041113420000 1 BRACKET

30 NAS1801-3-8 2 SCREW

31 NAS1801-3-11 1 SCREW

33 NAS1801-3-25 1 SCREW

34 NSA5527-03-08 4 SPACER

37 NAS1801-3-9 3 SCREW

41 A0041095620000 1 SEAL

42 A0041095400000 1 BRACKET

43 NSA5067-3-1 4 NUT

46 NAS1149F0332P 12 WASHER

51 NSA5516-12ND 6 CLAMP

63 NSA5516-13ND 14 CLAMP

64 NSA5516-31ND 14 CLAMP

66 NSA935401-13 5 TIE

67 A0041113300000 1 BRACKET

68 ASNA2050DXJ4828 2 RIVET

69 NSA935807-06 1 CLAMP

70 A0041113500000 1 CLAMP

71 NAS1801-3-12 4 SCREW

75 A0041113500200 1 CLAMP

76 A0041113500400 1 CLAMP

77 EN6049-007-19-5 7.5 (M) SLEEVE

78 EN6049-007-13-5 7.5 (M) SLEEVE

79 NAS1801-3-18 1 SCREW

81 NAS1801-3-20 6 SCREW

82 ASNA2397KD10L 2 WASHER

84 NSA5527-03-06 1 SPACER

85 ASNA51072503 2 (M) TAPE

ASNA2528-3 2 NUT

EN6115V3-4 2 BOLT

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.

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 41

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SERVICE BULLETIN

Supplementary kit 246103A01S11

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

NOTES

12 NSA5527-03-01 1 SPACER

37 NAS1801-3-9 2 SCREW

46 NAS1149F0332P 6 WASHER

52 NSA5516-08ND 8 CLAMP

55 NAS1801-3-16 1 SCREW

85 ASNA51072503 1 (M) TAPE

86 EN6049-007-08-5 5 (M) SLEEVE

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.

Supplementary kit 246103A01S12

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

NOTES

12 NSA5527-03-01 1 SPACER

14 NSA5527-03-02 3 SPACER

26 NSA935401-04 12 TIE

37 NAS1801-3-9 3 SCREW

46 NAS1149F0332P 4 WASHER

52 NSA5516-08ND 8 CLAMP

55 NAS1801-3-16 2 SCREW

66 NSA935401-13 3 TIE

86 EN6049-007-08-5 7.5 (M) SLEEVE

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.

Supplementary kit 246103A01S13

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

NOTES

100 ASNA2050DXJ5613 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.

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 42

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@A300-600

SERVICE BULLETIN

Supplementary kit 246103A02S03

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

NOTES

12 NSA5527-03-01 5 SPACER

14 NSA5527-03-02 2 SPACER

21 NSA5050-3 3 NUT

24 NSA939510BN 1 (M) STRIP (24) MS35489-6

29 A0041113420100 1 BRACKET

30 NAS1801-3-8 2 SCREW

33 NAS1801-3-25 2 SCREW

37 NAS1801-3-9 1 SCREW

43 NSA5067-3-1 2 NUT

46 NAS1149F0332P 12 WASHER

63 NSA5516-13ND 12 CLAMP

64 NSA5516-31ND 12 CLAMP

66 NSA935401-08 2 TIE

70 A0041113500000 1 CLAMP

71 NAS1801-3-12 2 SCREW

75 A0041113500200 1 CLAMP

76 A0041113500400 1 CLAMP

77 EN6049-007-19-5 7.5 (M) SLEEVE

78 EN6049-007-13-5 7.5 (M) SLEEVE

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.

Supplementary kit 246103A02S07

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

NOTES

12 NSA5527-03-01 5 SPACER

14 NSA5527-03-02 5 SPACER

21 NSA5050-3 3 NUT

24 NSA939510BN 1 (M) STRIP

25 ABS0596S005 2 INSULATR

26 NSA935401-04 12 TIE

29 A0041113420100 1 BRACKET

30 NAS1801-3-8 2 SCREW

33 NAS1801-3-25 1 SCREW

37 NAS1801-3-9 3 SCREW

43 NSA5067-3-1 2 NUT

46 NAS1149F0332P 10 WASHER

51 NSA5516-12ND 6 CLAMP

63 NSA5516-13ND 14 CLAMP

64 NSA5516-31ND 14 CLAMP

66 NSA935401-13 5 TIE

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 43

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@A300-600

SERVICE BULLETIN

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

NOTES

70 A0041113500000 1 CLAMP

71 NAS1801-3-12 3 SCREW

75 A0041113500200 1 CLAMP

76 A0041113500400 1 CLAMP

77 EN6049-007-19-5 7.5 (M) SLEEVE

78 EN6049-007-13-5 7.5 (M) SLEEVE

79 NAS1801-3-18 1 SCREW

82 ASNA2397KD10L 2 WASHER

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.

Supplementary kit 246103A02S10

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

NOTES

12 NSA5527-03-01 1 SPACER

37 NAS1801-3-9 2 SCREW

46 NAS1149F0332P 6 WASHER

52 NSA5516-08ND 8 CLAMP

55 NAS1801-3-16 1 SCREW

85 ASNA51072503 1 (M) TAPE

86 EN6049-007-08-5 2.5 (M) SLEEVE

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.

Supplementary kit 246103A02S11

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

NOTES

12 NSA5527-03-01 1 SPACER

14 NSA5527-03-02 3 SPACER

26 NSA935401-04 12 TIE

37 NAS1801-3-9 3 SCREW

46 NAS1149F0332P 4 WASHER

52 NSA5516-08ND 8 CLAMP

55 NAS1801-3-16 2 SCREW

66 NSA935401-13 3 TIE

85 ASNA51072503 1 (M) TAPE

86 EN6049-007-08-5 7.5 (M) SLEEVE

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 44

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@A300-600

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.

Supplementary kit 246103A03S01

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

NOTES

21 NSA5050-3 2 NUT

22 NAS1801-3-24 2 SCREW

90 NAS1149D0316H 2 WASHER

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 246103B01R03

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

NOTES

1 A9245005500000 1 BRACKET (1) A9244012400000

2 MS20470AD4-10 4 RIVET

3 A9245005600000 1 BRACKET (3) A5724091525800

8 DAN7-5-6 3 PIN

9 HL70-6 3 COLLAR

60 A9245000200000 2 GUIDE

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 246103B02R02

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

NOTES

1 A9245005500000 1 BRACKET (1) A9244012400000

2 MS20470AD4-10 2 RIVET

3 A9245005600000 1 BRACKET (3) A5724091525800

8 DAN7-5-6 3 PIN

9 HL70-6 3 COLLAR

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.

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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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

Primer Epoxy Paint - Tsa Anodizing

Corrosion Inhibi

04DEB2 As required

Primer Polyurethane Paint -

Corrosion Inhibiting

04EAC2 As required

Top Coat Polyurethane - Grey

Internal Structure

04JME4 As required

Epoxy Adhesive-Metal To Metal -

Legacy

05EJL9 As required

Epoxy Adhesive - Legacy 3 05EML7 As required

Contact Adhesive-Rubber & Plastic

Bonding Neopren

05JBC9 As required

Polysulfide Sealant - General

Purpose Interfay

06AAC1 As required

Polysulfide Sealant-Fuel Tank Fillet 06ABB1 As required

Non Aqueous Cleaner - General 08BAA9 As required

Non Aqueous Cleaner - Isopropyl

Alcohol

08BBD1 As required

Corrosion Preventive CompoundWater Displacing12ADB1 As required

Consumable CMLB01

ITEM DESCRIPTION REFERENCE TO CML

MAT. No.

QTY PER A/C SEE

NOTES

Primer Polyurethane Paint -

Corrosion Inhibiting

04EAC2 As required

Top Coat Polyurethane - Grey

Internal Structure

04JME4 As required

Polysulfide Sealant - General

Purpose Interfay

06AAC1 As required

Non Aqueous Cleaner - General 08BAA9 As required

Surface Pretreatment - Light Alloys

Chemical Conver

10ABC1 As required

Textile - Lint Free Cotton 14SBA1 As required

(2) Components

Component COMPB01

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

NOTES

8 DAN7-5-6 3 PIN

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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SERVICE BULLETIN

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

NOTES

9 HL70-6 3 COLLAR

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.

(3) Equipment

None

E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

None

F. TOOLING

None

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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This Page Intentionally Left Blank

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS

Task 246103-831-801-001 - 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.

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

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

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

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

authority he belongs to, the accepted alternative procedure can be used. When the

words "in accordance with" are used then the given procedure must be followed.

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

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

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

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

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

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

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

NOTE: This Service Bulletin is classified mandatory or expected to be classified mandatory

by an Airworthiness Directive (AD). The paragraphs 3.C. and 3.D. in these

accomplishment instructions are Required for Compliance (RC) and must be done

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

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

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

the aircraft can be put back into a serviceable condition.

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

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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Task Associated Data

**CONF 001

Zone

147 148 512 513 570 571 572 575 612 613 670 672 675

From 147 to 148

From 513 to 613

From 570 to 670

From 572 to 672

Manpower

TOTAL MANHOURS 38.00

ELAPSED TIME (HOURS) 22.50

**CONF 002

Zone

147 148 512 513 570 571 572 575 612 613 670 672 675

From 147 to 148

From 513 to 613

From 570 to 670

From 572 to 672

Manpower

TOTAL MANHOURS 36.00

ELAPSED TIME (HOURS) 20.75

**CONF 003

Zone

147 148 512 513 570 571 572 575 612 613 670 672 675

From 147 to 148

From 513 to 613

From 570 to 670

From 572 to 672

Manpower

TOTAL MANHOURS 38.00

ELAPSED TIME (HOURS) 22.50

**CONF ALL

A. GENERAL

**CONF 001

(1) Subtask 246103-839-001-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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(2) Subtask 246103-839-401-001 - Administrative

Manpower Resources

Skills UTILITY

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

Service Bulletin.

(3) Subtask 246103-910-001-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

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

06-31-53, Page Block 001

20-21-12, Page Block 001

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-25-51

20-33-00

20-33-30

20-33-41

20-33-42

20-33-44

Structural Repair Manual (SRM) 51-40-00

51-40-20

51-40-30

51-40-40

51-75-10

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

the Consumable Materials List (CML).

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

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

(d) For the identification of access panels, refer to AMM 06-21-00, Page Block 001.

(e) Tag all the parts you must remove and retain to make the subsequent installation

easier.

(f) Put all the retained hardware in identified plastic bags and attach the bags to the

related unit.

(g) Obtain fastener hole diameters and drill data in accordance with SRM 51-40-40.

(h) For the installation of the protective electrical conduits, refer to ESPM 20-33-30.

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

Block 001.

(j) Obtain alternative and substitute fastener data in accordance with SRM 51-40-30.

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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(k) If alternative and substitute fasteners have to be used, you must make sure that the

associated nut/collar are compatible in accordance with SRM 51-40-00 "Mating

Part" column.

(l) If the length of any fastener specified in this Service Bulletin does not meet

installation standards given in SRM Chapter 51, then a fastener of the same

specification, or an approved substitute, with a length which meets the installation

standards given in SRM Chapter 51 may be used. In addition, washers may be

installed for fastener grip length in accordance with SRM Chapter 51.

(m) Remove and install fasteners in accordance with SRM 51-40-20.

(n) For the cable tie application and tooling, refer to ESPM 20-33-44 and ESPM

20-25-51.

(o) Adapt the clamp size as necessary, refer to ESPM 20-33-42.

(p) For the general installation of electrical wire harnesses, refer to ESPM 20-33-00.

(q) Renew the protective finish in accordance with SRM 51-75-10.

(4) Subtask 246103-910-401-001 - Standard Practices

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) 51-23-10, Page Block 001

Elec. Std. Practices Manual (ESPM) 20-33-00

20-33-45

Structural Repair Manual (SRM) 51-21-10

51-40-20

51-40-40

51-75-10

(a) Remove and install fasteners in accordance with SRM 51-40-20.

(b) Obtain fastener hole diameters and drill data in accordance with SRM 51-40-40.

(c) Do the repair of the paint coatings in accordance with SRM 51-75-10 and refer to

AMM 51-23-10, Page Block 001.

(d) Do the application of protective treatments to metal parts in accordance with SRM

51-21-10.

(e) For the general installation of electrical wire harnesses, refer to ESPM 20-33-00.

(f) For Backshell, End Piece and Conduit Fitting, refer to ESPM 20-33-45.

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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**CONF 002

(1) Subtask 246103-839-001-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

(2) Subtask 246103-839-401-001 - Administrative

Manpower Resources

Skills UTILITY

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

Service Bulletin.

(3) Subtask 246103-910-001-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

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

06-31-53, Page Block 001

20-21-12, Page Block 001

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-25-51

20-33-00

20-33-30

20-33-41

20-33-42

20-33-44

Structural Repair Manual (SRM) 51-40-00

51-40-20

51-40-30

51-40-40

51-75-10

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

the Consumable Materials List (CML).

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

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

(d) For the identification of access panels, refer to AMM 06-21-00, Page Block 001.

(e) Tag all the parts you must remove and retain to make the subsequent installation

easier.

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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(f) Put all the retained hardware in identified plastic bags and attach the bags to the

related unit.

(g) Obtain fastener hole diameters and drill data in accordance with SRM 51-40-40.

(h) For the installation of the protective electrical conduits, refer to ESPM 20-33-30.

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

Block 001.

(j) Obtain alternative and substitute fastener data in accordance with SRM 51-40-30.

(k) If alternative and substitute fasteners have to be used, you must make sure that the

associated nut/collar are compatible in accordance with SRM 51-40-00 "Mating

Part" column.

(l) If the length of any fastener specified in this Service Bulletin does not meet

installation standards given in SRM Chapter 51, then a fastener of the same

specification, or an approved substitute, with a length which meets the installation

standards given in SRM Chapter 51 may be used. In addition, washers may be

installed for fastener grip length in accordance with SRM Chapter 51.

(m) Remove and install fasteners in accordance with SRM 51-40-20.

(n) For the cable tie application and tooling, refer to ESPM 20-33-44 and ESPM

20-25-51.

(o) Adapt the clamp size as necessary, refer to ESPM 20-33-42.

(p) For the general installation of electrical wire harnesses, refer to ESPM 20-33-00.

(q) Renew the protective finish in accordance with SRM 51-75-10.

(4) Subtask 246103-910-401-001 - Standard Practices

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) 51-23-10, Page Block 001

Elec. Std. Practices Manual (ESPM) 20-33-00

20-33-45

Structural Repair Manual (SRM) 51-21-10

51-40-20

51-40-40

51-75-10

(a) Remove and install fasteners in accordance with SRM 51-40-20.

(b) Obtain fastener hole diameters and drill data in accordance with SRM 51-40-40.

(c) Do the repair of the paint coatings in accordance with SRM 51-75-10 and refer to

AMM 51-23-10, Page Block 001.

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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(d) Do the application of protective treatments to metal parts in accordance with SRM

51-21-10.

(e) For the general installation of electrical wire harnesses, refer to ESPM 20-33-00.

(f) For Backshell, End Piece and Conduit Fitting, refer to ESPM 20-33-45.

**CONF 003

(1) Subtask 246103-839-001-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

(2) Subtask 246103-839-401-001 - Administrative

Manpower Resources

Skills UTILITY

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

Service Bulletin.

(3) Subtask 246103-910-001-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

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

06-31-53, Page Block 001

20-21-12, Page Block 001

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-25-51

20-33-00

20-33-30

20-33-41

20-33-42

20-33-44

Structural Repair Manual (SRM) 51-40-00

51-40-20

51-40-30

51-40-40

51-75-10

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

the Consumable Materials List (CML).

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

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

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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(d) For the identification of access panels, refer to AMM 06-21-00, Page Block 001.

(e) Tag all the parts you must remove and retain to make the subsequent installation

easier.

(f) Put all the retained hardware in identified plastic bags and attach the bags to the

related unit.

(g) Obtain fastener hole diameters and drill data in accordance with SRM 51-40-40.

(h) For the installation of the protective electrical conduits, refer to ESPM 20-33-30.

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

Block 001.

(j) Obtain alternative and substitute fastener data in accordance with SRM 51-40-30.

(k) If alternative and substitute fasteners have to be used, you must make sure that the

associated nut/collar are compatible in accordance with SRM 51-40-00 "Mating

Part" column.

(l) If the length of any fastener specified in this Service Bulletin does not meet

installation standards given in SRM Chapter 51, then a fastener of the same

specification, or an approved substitute, with a length which meets the installation

standards given in SRM Chapter 51 may be used. In addition, washers may be

installed for fastener grip length in accordance with SRM Chapter 51.

(m) Remove and install fasteners in accordance with SRM 51-40-20.

(n) For the cable tie application and tooling, refer to ESPM 20-33-44 and ESPM

20-25-51.

(o) Adapt the clamp size as necessary, refer to ESPM 20-33-42.

(p) For the general installation of electrical wire harnesses, refer to ESPM 20-33-00.

(q) Renew the protective finish in accordance with SRM 51-75-10.

(4) Subtask 246103-910-401-001 - Standard Practices

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) 51-23-10, Page Block 001

Elec. Std. Practices Manual (ESPM) 20-33-00

20-33-45

Structural Repair Manual (SRM) 51-21-10

51-40-20

51-40-40

51-75-10

(a) Remove and install fasteners in accordance with SRM 51-40-20.

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(b) Obtain fastener hole diameters and drill data in accordance with SRM 51-40-40.

(c) Do the repair of the paint coatings in accordance with SRM 51-75-10 and refer to

AMM 51-23-10, Page Block 001.

(d) Do the application of protective treatments to metal parts in accordance with SRM

51-21-10.

(e) For the general installation of electrical wire harnesses, refer to ESPM 20-33-00.

(f) For Backshell, End Piece and Conduit Fitting, refer to ESPM 20-33-45.

**CONF ALL

B. PREPARATION

**CONF 001

(1) Subtask 246103-941-001-001 - Job Set-up

Work Zones and Access Panels

Zone Access/Work location

From 513

To 613

From 570

To 670

571

From 572

To 672

From 147

To 148

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001

24-00-00, Page Block 301

27-54-41, Page Block 401

32-12-11, Page Block 301

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

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- 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 24-00-00, Page

Block 301.

(b) Put an access platform in position at Zone(s) 513(613), 570(670), 571 , 572(672)

and 147(148).

(c) Open the Main Landing Gear (MLG) doors, refer to AMM 32-12-11, Page Block

301.

(d) Remove the access panels 512AB(612AB), 512BB(612BB), 512CB(612CB),

512DB(612DB), refer to AMM 06-41-57, Page Block 001.

(e) Remove the access panels 571BB, 571DB, refer to AMM 06-41-57, Page Block

001.

(f) Open all the necessary inner deflectors between Rib. 1 and Rib. 6, refer to AMM

27-54-41, Page Block 401.

(2) Subtask 246103-941-401-001 - Job Set-up

Manpower Resources

Skills AIRFRAME

References

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

27-50-00, Page Block 301

29-10-00, Page Block 301

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

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- 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 24-00-00, Page

Block 301.

(b) Fully extend the flaps, refer to AMM 27-50-00, Page Block 301.

(c) Depressurize the hydraulic system, refer to AMM 29-10-00, Page Block 301.

(d) Put an access platform in position at Zone(s) 512(612), 572(672) and 575(675).

(e) Open, safety and tag these circuit breakers:

PANEL DESIGNATION FIN LOCATION SEE

NOTES

133VU FLT CTL/FLAPS/SYS

1/26VAC

1CV 335/R61

133VU FLT CTL/FLAPS/SYS

2/26VAC

2CV 334/S62

133VU SLATS/26VAC/SYS 1 3CV 335/R65

133VU SLATS/26VAC/SYS 2 4CV 335/R64

133VU FLT CTL/SFCC/NORM

SUPPLY/FLAPS/SYS 1

5CV 332/U61

133VU FLT CTL/SFCC/NORM

SUPPLY/FLAPS/SYS 2

6CV 331/V61

133VU SFCC/NORM

SUPPLY/SLATS/SYS 1

7CV 333/T63

133VU SFCC/NORM

SUPPLY/SLATS/SYS 2

8CV 333/T64

(f) In the cockpit, put warning notices in position to tell persons not to operate the

flaps/slats.

(g) Get access to the outer shroud box LH and RH wing.

(h) Lower the hinged access door 581DB(681DB) and remove the access panels

582AT(682AT) and 512CB(612CB).

**CONF 002

(1) Subtask 246103-941-001-001 - Job Set-up

Work Zones and Access Panels

Zone Access/Work location

From 513

To 613

From 570

To 670

571

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From 572

To 672

From 147

To 148

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001

24-00-00, Page Block 301

27-54-41, Page Block 401

32-12-11, Page Block 301

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 24-00-00, Page

Block 301.

(b) Put an access platform in position at Zone(s) 513(613), 570(670), 571 , 572(672)

and 147(148).

(c) Open the Main Landing Gear (MLG) doors, refer to AMM 32-12-11, Page Block

301.

(d) Remove the access panels 512AB(612AB), 512BB(612BB), 512CB(612CB),

512DB(612DB), refer to AMM 06-41-57, Page Block 001.

(e) Remove the access panels 571BB, 571DB, refer to AMM 06-41-57, Page Block

001.

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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SERVICE BULLETIN

(f) Open all the necessary inner deflectors between Rib. 1 and Rib. 6, refer to AMM

27-54-41, Page Block 401.

(2) Subtask 246103-941-401-001 - Job Set-up

Manpower Resources

Skills AIRFRAME

References

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

27-50-00, Page Block 301

29-10-00, Page Block 301

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 24-00-00, Page

Block 301.

(b) Fully extend the flaps, refer to AMM 27-50-00, Page Block 301.

(c) Depressurize the hydraulic system, refer to AMM 29-10-00, Page Block 301.

(d) Put an access platform in position at Zone(s) 512(612), 572(672) and 575(675).

(e) Open, safety and tag these circuit breakers:

PANEL DESIGNATION FIN LOCATION SEE

NOTES

133VU FLT CTL/FLAPS/SYS

1/26VAC

1CV 335/R61

133VU FLT CTL/FLAPS/SYS

2/26VAC

2CV 334/S62

133VU SLATS/26VAC/SYS 1 3CV 335/R65

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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@A300-600

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PANEL DESIGNATION FIN LOCATION SEE

NOTES

133VU SLATS/26VAC/SYS 2 4CV 335/R64

133VU FLT CTL/SFCC/NORM

SUPPLY/FLAPS/SYS 1

5CV 332/U61

133VU FLT CTL/SFCC/NORM

SUPPLY/FLAPS/SYS 2

6CV 331/V61

133VU SFCC/NORM

SUPPLY/SLATS/SYS 1

7CV 333/T63

133VU SFCC/NORM

SUPPLY/SLATS/SYS 2

8CV 333/T64

(f) In the cockpit, put warning notices in position to tell persons not to operate the

flaps/slats.

(g) Get access to the outer shroud box LH and RH wing.

(h) Lower the hinged access door 581DB(681DB) and remove the access panels

582AT(682AT) and 512CB(612CB).

**CONF 003

(1) Subtask 246103-941-001-001 - Job Set-up

Work Zones and Access Panels

Zone Access/Work location

From 513

To 613

From 570

To 670

571

From 572

To 672

From 147

To 148

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001

24-00-00, Page Block 301

27-54-41, Page Block 401

32-12-11, Page Block 301

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

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 62

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@A300-600

SERVICE BULLETIN

- Aircraft in clean configuration

- Parking brake applied

- Aircraft electrical network de-energized

- Hydraulic systems depressurized

- Access to the cockpit and cabin is available

- All circuit breakers are in closed position

- All controls in NORM, AUTO or OFF position

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

Block 301.

(b) Put an access platform in position at Zone(s) 513(613), 570(670), 571 , 572(672)

and 147(148).

(c) Open the Main Landing Gear (MLG) doors, refer to AMM 32-12-11, Page Block

301.

(d) Remove the access panels 512AB(612AB), 512BB(612BB), 512CB(612CB),

512DB(612DB), refer to AMM 06-41-57, Page Block 001.

(e) Remove the access panels 571BB, 571DB, refer to AMM 06-41-57, Page Block

001.

(f) Open all the necessary inner deflectors between Rib. 1 and Rib. 6, refer to AMM

27-54-41, Page Block 401.

(2) Subtask 246103-941-401-001 - Job Set-up

Manpower Resources

Skills AIRFRAME

References

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

27-50-00, Page Block 301

29-10-00, Page Block 301

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

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 63

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@A300-600

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- 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 24-00-00, Page

Block 301.

(b) Fully extend the flaps, refer to AMM 27-50-00, Page Block 301.

(c) Depressurize the hydraulic system, refer to AMM 29-10-00, Page Block 301.

(d) Put an access platform in position at Zone(s) 512(612), 572(672) and 575(675).

(e) Open, safety and tag these circuit breakers:

PANEL DESIGNATION FIN LOCATION SEE

NOTES

133VU FLT CTL/FLAPS/SYS

1/26VAC

1CV 335/R61

133VU FLT CTL/FLAPS/SYS

2/26VAC

2CV 334/S62

133VU SLATS/26VAC/SYS 1 3CV 335/R65

133VU SLATS/26VAC/SYS 2 4CV 335/R64

133VU FLT CTL/SFCC/NORM

SUPPLY/FLAPS/SYS 1

5CV 332/U61

133VU FLT CTL/SFCC/NORM

SUPPLY/FLAPS/SYS 2

6CV 331/V61

133VU SFCC/NORM

SUPPLY/SLATS/SYS 1

7CV 333/T63

133VU SFCC/NORM

SUPPLY/SLATS/SYS 2

8CV 333/T64

(f) In the cockpit, put warning notices in position to tell persons not to operate the

flaps/slats.

(g) Get access to the outer shroud box LH and RH wing.

(h) Lower the hinged access door 581DB(681DB) and remove the access panels

582AT(682AT) and 512CB(612CB).

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 64

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@A300-600

SERVICE BULLETIN

**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 246103-831-001-001 - Remove the clamps between FR50 and FR52 at LH

side

Work Zones and Access Panels

Zone Access/Work location

147 Work location from Frame 50 to Frame 52

from Stringer 32 to Stringer 33

Manpower Resources

Manhours 1.50

Minimum number of person 1

Subtask elapsed time 1.50

Skills NON SPECIFIC

References

Fig. A-FBAAA

Removal of the Old Brackets of the

Passage Way at FR52 (LH side)

Sheet 01

Sheet 02

Sheet 03

Fig. A-FBFAA

Modification of the Routing Between

FR50 and FR51 at STGR 32 (LH and

RH side)

Sheet 01

Sheet 02

(a) On the panel, remove :

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

2 Screw Item (47) Discard

2 Washer Item (46) Discard

2 Clip nut Item (43) Discard

1 Clamp Item (44) Retain

1 Clamp Item (45) Retain

(b) On the bracket (if installed), remove :

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

1 Nut Item (48) Discard

1 Washer Item (49) Discard

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 65

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SERVICE BULLETIN

1 Screw Item (10) Discard

1 Clamp Item (11) Retain

(c) Remove :

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

2 Screw Item (47) Discard

2 Washer Item (46) Discard

1 Seal fitting Item (41) Discard

1 Bracket assy Item (42) Discard

(d) Remove :

Refer to Fig. A-FBAAA Sheet 01 and Fig. A-FBAAA Sheet 03

4 Clamp Item (72) Discard

2 Screw Item (74) Retain

2 Washer Item (73) Discard

1 Clamp Item (44) Discard

1 Clamp Item (45) Discard

2 Washer Item (46) Discard

2 Screw Item (47) Retain

(e) Depending on the stacking, remove :

Refer to Fig. A-FBFAA Sheet 01

4 Clamp Item (16) Discard

2 Clamp Item (32) Discard

2 Spacer Item (14) Discard

2 Clip nut Item (43) Discard

2 Washer Item (20) Discard

2 Screw Item (33) Discard

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 66

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Or remove :

Refer to Fig. A-FBFAA Sheet 01

4 Clamp Item (16) Discard

2 Spacer Item (14) Discard

2 Clip nut Item (43) Discard

2 Washer Item (20) Discard

2 Screw Item (33) Discard

(2) Subtask 246103-831-019-001 - Modify the Routing between FR50 and FR52 and

between STGR 33 and 30 at LH side

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 246103A01R14

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

77 EN6049-007-19-5 7.5 (M) SLEEVE

78 EN6049-007-13-5 7.5 (M) SLEEVE

86 EN6049-007-08-5 7.5 (M) SLEEVE

References

Fig. A-FBWAA

Modification of the Routing between

FR50 and FR52 (LH and RH side)

Sheet 01

(a) Remove :

Refer to Fig. A-FBWAA Sheet 01

5 (M) Conduit Item (77) Discard

NOTE: A third conduit may be installed. If installed, remove it.

(b) Install :

Refer to Fig. A-FBWAA Sheet 01

5 (M) Sleeve EN6049-007-13-5 Item 78

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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SERVICE BULLETIN

or

5 (M) Sleeve EN6049-007-19-5 Item 77

or

5 (M) Sleeve-Protective EN6049-007-08-5 Item 86

NOTE: Install the sleeve Item 77 or 78 or 86 according to the harness

diameter.

NOTE: If a third conduit was installed, install :

2.5 (M) Sleeve EN6049-007-13-5 Item 78

or

2.5 (M) Sleeve EN6049-007-19-5 Item 77

or

2.5 (M) Sleeve-Protective EN6049-007-08-5 Item 86

NOTE: Install the sleeve Item 77 or 78 or 86 according to the harness

diameter.

(3) Subtask 246103-420-001-001 - Install the clamps between FR50 and FR52 at LH

side

Work Zones and Access Panels

Zone Access/Work location

147 Work location from Frame 50 to Frame 52

from Stringer 31 to Stringer 32

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 246103A01R14

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

10 NAS1801-3-17 1 SCREW

12 NSA5527-03-01 2 SPACER

14 NSA5527-03-02 2 SPACER

23 NSA935401-05 1 TIE

33 NAS1801-3-25 1 SCREW

38 ABS0731A01 1 SUPPORT

41 A0041095620000 1 SEAL

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 68

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@A300-600

SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

42 A0041095400000 1 BRACKET

43 NSA5067-3-1 4 NUT

46 NAS1149F0332P 11 WASHER

47 NAS1801-3-7 4 SCREW

48 MS21042-3 1 NUT

63 NSA5516-13ND 12 CLAMP

64 NSA5516-31ND 12 CLAMP

79 NAS1801-3-18 1 SCREW

References

Fig. A-FBFAA

Modification of the Routing Between

FR50 and FR51 at STGR 32 (LH and

RH side)

Sheet 01

Sheet 02

Fig. A-FBBAA

Installation of the New Brackets of the

Passage Way at FR52 (LH side)

Sheet 01

Sheet 02

(a) Depending on the staking, install :

Refer to Fig. A-FBFAA Sheet 01 and Fig. A-FBFAA Sheet 02 view C

3 Clamp NSA5516-13ND Item 63

or

3 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

1 Spacer NSA5527-03-01 Item 12

1 Spacer NSA5527-03-02 Item 14

1 Screw NAS1801-3-25 Item 33

1 Washer NAS1149F0332P Item 46

1 Clip nut NSA5067-3-1 Item 43

Or install :

Refer to Fig. A-FBFAA Sheet 01 and Fig. A-FBFAA Sheet 02 view C

2 Clamp NSA5516-13ND Item 63

or

2 Clamp NSA5516-31ND Item 64

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 69

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SERVICE BULLETIN

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

1 Spacer NSA5527-03-01 Item 12

1 Spacer NSA5527-03-02 Item 14

1 Screw NAS1801-3-25 Item 33

1 Washer NAS1149F0332P Item 46

1 Clip nut NSA5067-3-1 Item 43

(b) Depending on the stacking, install :

Refer to Fig. A-FBFAA Sheet 01 and Fig. A-FBFAA Sheet 02 view D

3 Clamp NSA5516-13ND Item 63

or

3 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

1 Spacer NSA5527-03-02 Item 14

1 Screw NAS1801-3-18 Item 79

1 Clip nut NSA5067-3-1 Item 43

1 Washer NAS1149F0332P Item 46

Or install :

Refer to Fig. A-FBFAA Sheet 01 and Fig. A-FBFAA Sheet 02 view D

2 Clamp NSA5516-13ND Item 63

or

2 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

1 Spacer NSA5527-03-02 Item 14

1 Screw NAS1801-3-18 Item 79

1 Washer NAS1149F0332P Item 46

1 Clip nut NSA5067-3-1 Item 43

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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SERVICE BULLETIN

(c) Install :

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

1 Seal Fitting A0041095620000 Item 41

1 Bracket assy A0041095400000 Item 42

2 Screw NAS1801-3-7 Item 47

2 Washer NAS1149F0332P Item 46

(d) On the bracket (if installed), install :

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

1 Clamp Item (11) Retained at

removal

1 Spacer NSA5527-03-01 Item 12

1 Screw NAS1801-3-17 Item 10

1 Washer NAS1149F0332P Item 46

1 Nut MS21042-3 Item 48

(e) On the panel, install :

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

1 Clamp Item (44) Retained at

removal

1 Clamp Item (45) Retained at

removal

2 Screw NAS1801-3-7 Item 47

2 Washer NAS1149F0332P Item 46

2 Clip nut NSA5067-3-1 Item 43

(f) Install :

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

6 Clamp NSA5516-13ND Item 63

or

6 Clamp NSA5516-31ND Item 64

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 71

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NOTE: Install the clamp Item 63 or 64 according to the bundle diameter.

4 Washer NAS1149F0332P Item 46

2 Screw Item (47) Retained at

removal

2 Screw Item (74) Retained at

removal

(g) Between the routes, install :

Refer to Fig. A-FBBAA Sheet 01

1 Support-Cable ABS0731A01 Item 38

1 Tie-Cable NSA935401-05 Item 23

(4) Subtask 246103-831-003-001 - Install a bracket on the shroud box blanking plate at

LH side

Work Zones and Access Panels

Zone Access/Work location

147 Work location Frame 51

from Stringer 31 to Stringer 33

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 246103A01R14

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

21 NSA5050-3 3 NUT

28 A0041113420000 1 BRACKET

30 NAS1801-3-8 2 SCREW

37 NAS1801-3-9 1 SCREW

46 NAS1149F0332P 2 WASHER

63 NSA5516-13ND 2 CLAMP

64 NSA5516-31ND 2 CLAMP

70 A0041113500000 1 CLAMP

71 NAS1801-3-12 2 SCREW

75 A0041113500200 1 CLAMP

76 A0041113500400 1 CLAMP

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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SERVICE BULLETIN

References

Fig. A-FBEAA

Installation of a Conduit on the Shroud

Box Bracket (LH and RH side)

Sheet 01

Sheet 02

Sheet 03

(a) Remove :

Refer to Fig. A-FBEAA Sheet 01

2 Screw Item (27) Discard

2 Washer Item (46) Discard

(b) Install the bracket :

Refer to Fig. A-FBEAA Sheet 01, Fig. A-FBEAA Sheet 02 and Fig. A-FBEAA Sheet

03

1 Bracket A0041113420000 Item 28

attach with :

2 Screw NAS1801-3-12 Item 71

2 Washer NAS1149F0332P Item 46

(c) Attach the bundles on the shroud box bracket :

Refer to Fig. A-FBEAA Sheet 01, Fig. A-FBEAA Sheet 02 and Fig. A-FBEAA Sheet

03

1 Attach the bundles with :

2 Clamp NSA5516-13ND Item 63

or

2 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

NOTE: Two or three bundles may be installed.

1 Nut NSA5050-3 Item 21

and

1 Screw NAS1801-3-9 Item 37

2 Or attach the bundles with :

2 Clamp NSA5516-13ND Item 63

or

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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2 Clamp NSA5516-31ND Item 64

and

1 Clamp A0041113500000 Item 70

or

1 Clamp A0041113500200 Item 75

or

1 Clamp A0041113500400 Item 76

NOTE: Install clamp Item 70 or 75 or 76 according to the bundle

diameters.

NOTE: Two or three bundles may be installed.

2 Nut NSA5050-3 Item 21

2 Screw NAS1801-3-8 Item 30

(5) Subtask 246103-831-006-001 - Modify the routing on rib 1 on the passage way to

the shroud box at LH side

Work Zones and Access Panels

Zone Access/Work location

570 Work location Rib 1

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 246103A01R14

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

12 NSA5527-03-01 6 SPACER

19 NSA935807-09 2 CLAMP

20 NSA935808-01 1 WASHER

21 NSA5050-3 1 NUT

22 NAS1801-3-24 1 SCREW

87 NSA360002 1 (M) EXTRUSIN

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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SERVICE BULLETIN

Kit 246103A04R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

24 NSA939510BN 1 (M) STRIP

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Epoxy Adhesive-Metal To

Metal - Legacy

05EJL9 As required

Epoxy Adhesive - Legacy 3 05EML7 As required

Contact Adhesive-Rubber &

Plastic Bonding Neopren

05JBC9 As required

Non Aqueous Cleaner -

Isopropyl Alcohol

08BBD1 As required

References

Elec. Std. Practices Manual (ESPM) 20-33-11

Process and Material Specification

(PMS)

Process and Material Specification (PMS)

01-01-28 Process E

Fig. A-FBCAA

Removal of the Clamps on the Passage

Way to the Shroud Box (LH and RH

side)

Sheet 01

Sheet 02

Sheet 03

Fig. A-FBDAA

Installation of the Clamps on the

Passage Way to the Shroud Box (LH

and RH side)

Sheet 01

Sheet 02

Sheet 03

(a) Remove :

Refer to Fig. A-FBCAA Sheet 01 and Fig. A-FBCAA Sheet 03

2 Clamp Item (19) Discard

1 Spacer Item (12) Discard

1 Screw Item (22) Discard

1 Washer Item (20) Discard

1 Nut Item (21) Discard

(b) Install :

Refer to Fig. A-FBDAA Sheet 01, Fig. A-FBDAA Sheet 02 and Fig. A-FBDAA Sheet

03

2 Clamp NSA935807-09 Item 19

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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2 Spacer NSA5527-03-01 Item 12

1 Screw NAS1801-3-24 Item 22

1 Washer NSA935808-01 Item 20

1 Nut NSA5050-3 Item 21

(c) Refer to Fig. A-FBDAA Sheet 01 and Fig. A-FBDAA Sheet 03

1 (M) Extrusion NSA360002 Item 87

with:

Contact AdhesiveRubber & Plastic

Bonding Neopren

05JBC9 As required

(d) Measure the gap between the clamp and the structure, refer to Fig. A-FBCAA

Sheet 01 and Fig. A-FBCAA Sheet 02:

1 If the gap between the structure and the clamp is less than 6.35 mm (0.25 in.),

install, refer to Fig. A-FBDAA Sheet 02:

4 Spacer NSA5527-03-01 Item 12

2 If the gap between the structure and the clamp is more than 130 mm (5.118

in.), CONTACT AIRBUS, refer to Fig. A-FBCAA Sheet 02:

NOTE: For operators that have the gap between the structure and the

clamp is more than 130 mm (5.118 in) contact Airbus at:

AIRBUS CUSTOMER SERVICES ENGINEERING - SEEA5

ELECTRICAL POWER GENERATION DISTRIBUTION &

LIGHTING SYSTEMS

1 ROND POINT MAURICE BELLONTE

31707 BLAGNAC CEDEX FRANCE

FAX +33 561 934 425

(e) Install a protection on the structure to protect the routes :

Refer to Fig. A-FBDAA Sheet 01, Fig. A-FBDAA Sheet 02 and Fig. A-FBDAA Sheet

03

Refer to ESPM 20-33-11

Refer to Process and Material Specification (PMS) 01-01-28 Process E

1 (M) Strip-Protective NSA939510BN Item 24

NOTE: Install the Strip-Protective Item 24 with:

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 76

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Epoxy AdhesiveMetal To Metal -

Legacy

05EJL9 As required

NOTE: Do the abrading and cleaning of the contact zones of StripProtective Item 24, on the structure with:

Non Aqueous

Cleaner - Isopropyl

Alcohol

08BBD1 As required

Epoxy Adhesive -

Legacy 3

05EML7 As required

(6) Subtask 246103-831-010-001 - Modify the routing of routes 1P and 2P in the

hydraulic shroud box at LH side

Work Zones and Access Panels

Zone Access/Work location

571

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 246103A01R14

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

20 NSA935808-01 7 WASHER

34 NSA5527-03-08 6 SPACER

71 NAS1801-3-12 1 SCREW

81 NAS1801-3-20 6 SCREW

84 NSA5527-03-06 1 SPACER

References

Fig. A-FBGAA

Modification of the Routing of Routes 1P

and 2P in the Shroud Box (LH side)

Sheet 01

Sheet 02

Sheet 03

(a) For Section A-A and C-C, remove :

Refer to Fig. A-FBGAA Sheet 01, Fig. A-FBGAA Sheet 02 and Fig. A-FBGAA

Sheet 03

7 Screw Item (22) Discard

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 77

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@A300-600

SERVICE BULLETIN

7 Washer Item (20) Discard

14 Clamp Item (19) Retain

(b) For Section B-B, install :

Refer to Fig. A-FBGAA Sheet 01, Fig. A-FBGAA Sheet 02 and Fig. A-FBGAA

Sheet 03

6 Spacer NSA5527-03-08 Item 34

12 Clamp Item (19) Retained at

removal

6 Washer NSA935808-01 Item 20

6 Screw NAS1801-3-20 Item 81

(c) For Section D-D, install :

Refer to Fig. A-FBGAA Sheet 01, Fig. A-FBGAA Sheet 02 and Fig. A-FBGAA

Sheet 03

1 Spacer NSA5527-03-06 Item 84

2 Clamp Item (19) Retained at

removal

1 Washer NSA935808-01 Item 20

1 Screw NAS1801-3-12 Item 71

(7) Subtask 246103-831-011-001 - Install a support on the support of the BLUE

hydraulic reservoir at LH wing

Work Zones and Access Panels

Zone Access/Work location

571 Work location from Frame 47 to Frame 48

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 246103A01R14

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

20 NSA935808-01 1 WASHER

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 78

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@A300-600

SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

31 NAS1801-3-11 1 SCREW

67 A0041113300000 1 BRACKET

68 ASNA2050DXJ4828 2 RIVET

69 NSA935807-06 1 CLAMP

ASNA2528-3 2 NUT

EN6115V3-4 2 BOLT

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Primer Polyurethane Paint -

Corrosion Inhibiting

04EAC2

Top Coat Polyurethane -

Grey Internal Structure

04JME4

Polysulfide Sealant -

General Purpose Interfay

06AAC1

Polysulfide Sealant-Fuel

Tank Fillet

06ABB1

Non Aqueous Cleaner -

General

08BAA9

Corrosion Preventive

Compound-Water

Displacing

12ADB1 As required

References

Fig. A-FBHAA

Installation of a Support on the Support

of the BLUE Hydraulic Reservoir (LH

wing)

Sheet 01

Sheet 02

(a) Remove :

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

2 Rivet Item (68) Discard

NOTE: Clean the area with :

Non Aqueous

Cleaner - General

08BAA9 As required

(b) Install the bracket Item 67.

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

1 Put the bracket Item 67 in position.

2 Drill two holes on the bracket Item 67 to a diameter comprised between 4.85

mm (0.191 in.) and 4.95 mm (0.195 in.) to match the holes of the structure.

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 79

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@A300-600

SERVICE BULLETIN

3 Wet install :

1 Bracket A0041113300000 Item 67

2 Rivet ASNA2050DXJ4828 Item 68

NOTE: If the installation of bracket Item 67 with the rivets is not

possible, attach with:

2 Bolt EN6115V3-4

2 Nut ASNA2528-3

NOTE: Between the bracket Item 67 and the structure, apply :

Polysulfide SealantFuel Tank Fillet

06ABB1 As required

NOTE: Wet install the rivets with :

Polysulfide Sealant

- General Purpose

Interfay

06AAC1 As required

NOTE: Apply on the head of the rivets :

Primer

Polyurethane Paint

- Corrosion

Inhibiting

04EAC2 As required

Top Coat

Polyurethane - Grey

Internal Structure

04JME4 As required

Corrosion

Preventive

Compound-Water

Displacing

12ADB1 As required

NOTE: On the modified area, apply :

(c) Attach the conduit to the support with :

1 Clamp NSA935807-06 Item 69

1 Screw NAS1801-3-11 Item 31

1 Washer NSA935808-01 Item 20

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 80

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SERVICE BULLETIN

(8) Subtask 246103-831-012-001 - Modify the routing of routes 1E and 1G in the

leading edge at LH wing

Work Zones and Access Panels

Zone Access/Work location

513

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills NON SPECIFIC

Material necessary to do the job

Kit 246103A01R14

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

34 NSA5527-03-08 2 SPACER

39 A9222505750000 2 SPACER

66 NSA935401-13 2 TIE

References

Fig. A-FBJAA

Modification of the Routing in the

Leading Edge (LH and RH side)

Sheet 01

(a) Install :

Refer to Fig. A-FBJAA Sheet 01

2 Spacer-Feeder A9222505750000 Item 39

2 Spacer NSA5527-03-08 Item 34

2 Tie-Cable NSA935401-13 Item 66

(9) Subtask 246103-020-002-001 - Remove the clamps between FR50 and FR52 at RH

side

Work Zones and Access Panels

Zone Access/Work location

148 Work location from Frame 50 to Frame 52

from Stringer 32 to Stringer 33

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 81

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@A300-600

SERVICE BULLETIN

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

References

Fig. A-FBFAA

Modification of the Routing Between

FR50 and FR51 at STGR 32 (LH and

RH side)

Sheet 01

Sheet 02

Fig. A-FBUAA

Modification of the Routing of the

Passage Way at FR52 (RH side)

Sheet 01

Sheet 02

(a) Depending on the stacking, remove :

Refer to Fig. A-FBFAA Sheet 01

4 Clamp Item (16) Discard

2 Clamp Item (32) Discard

2 Spacer Item (14) Discard

2 Clip nut Item (43) Discard

2 Washer Item (20) Discard

2 Screw Item (33) Discard

Or remove :

Refer to Fig. A-FBFAA Sheet 01

4 Clamp Item (16) Discard

2 Spacer Item (14) Discard

2 Clip nut Item (43) Discard

2 Washer Item (20) Discard

2 Screw Item (33) Discard

(b) Remove :

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

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 82

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@A300-600

SERVICE BULLETIN

4 Clamp Item (72) Discard

2 Washer Item (73) Discard

2 Screw Item (74) Retain

1 Clamp Item (44) Discard

1 Clamp Item (45) Discard

2 Washer Item (46) Discard

2 Screw Item (47) Retain

(10) Subtask 246103-831-005-001 - Modify the Routing between FR50 and FR52 and

between STGR 33 and 30 at RH side

Work Zones and Access Panels

Zone Access/Work location

148 Work location from Frame 50 to Frame 51

Stringer 32

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 246103A02R12

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

77 EN6049-007-19-5 7.5 (M) SLEEVE

78 EN6049-007-13-5 7.5 (M) SLEEVE

86 EN6049-007-08-5 7.5 (M) SLEEVE

References

Fig. A-FBWAA

Modification of the Routing between

FR50 and FR52 (LH and RH side)

Sheet 01

(a) Remove :

Refer to Fig. A-FBWAA Sheet 01

5 (M) Conduit Item (77) Discard

NOTE: A third conduit may be installed. If installed, remove it.

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 83

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@A300-600

SERVICE BULLETIN

(b) Install :

Refer to Fig. A-FBWAA Sheet 01

5 (M) Sleeve EN6049-007-13-5 Item 78

or

5 (M) Sleeve EN6049-007-19-5 Item 77

or

5 (M) Sleeve-Protective EN6049-007-08-5 Item 86

NOTE: Install sleeve Item 77 or 78 or 86 according to the harness

diameter.

NOTE: If a third conduit was installed, install :

2.5 (M) Sleeve EN6049-007-13-5 Item 78

or

2.5 (M) Sleeve EN6049-007-19-5 Item 77

or

2.5 (M) Sleeve-Protective EN6049-007-08-5 Item 86

NOTE: Install the sleeve Item 77 or 78 or 86 according to the harness

diameter.

(11) Subtask 246103-420-002-001 - Install the clamps between FR50 and FR52 at RH

side

Work Zones and Access Panels

Zone Access/Work location

148 Work location from Frame 50 to Frame 52

from Stringer 32 to Stringer 33

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 246103A02R12

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

12 NSA5527-03-01 1 SPACER

14 NSA5527-03-02 2 SPACER

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 84

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@A300-600

SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

33 NAS1801-3-25 1 SCREW

43 NSA5067-3-1 2 NUT

46 NAS1149F0332P 6 WASHER

63 NSA5516-13ND 12 CLAMP

64 NSA5516-31ND 12 CLAMP

79 NAS1801-3-18 1 SCREW

References

Fig. A-FBFAA

Modification of the Routing Between

FR50 and FR51 at STGR 32 (LH and

RH side)

Sheet 01

Sheet 02

Fig. A-FBUAA

Modification of the Routing of the

Passage Way at FR52 (RH side)

Sheet 01

Sheet 02

(a) Depending on the stacking, install :

Refer to Fig. A-FBFAA Sheet 02 view C

3 Clamp NSA5516-13ND Item 63

or

3 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

1 Spacer NSA5527-03-01 Item 12

1 Spacer NSA5527-03-02 Item 14

1 Screw NAS1801-3-25 Item 33

1 Washer NAS1149F0332P Item 46

1 Clip nut NSA5067-3-1 Item 43

Or install :

Refer to Fig. A-FBFAA Sheet 02 view C

2 Clamp NSA5516-13ND Item 63

or

2 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 85

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@A300-600

SERVICE BULLETIN

1 Spacer NSA5527-03-01 Item 12

1 Spacer NSA5527-03-02 Item 14

1 Screw NAS1801-3-25 Item 33

1 Washer NAS1149F0332P Item 46

1 Clip nut NSA5067-3-1 Item 43

(b) Depending on the stacking, install :

Refer to Fig. A-FBFAA Sheet 02 view D

3 Clamp NSA5516-13ND Item 63

or

3 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

1 Spacer NSA5527-03-02 Item 14

1 Clip nut NSA5067-3-1 Item 43

1 Screw NAS1801-3-18 Item 79

1 Washer NAS1149F0332P Item 46

Or install :

Refer to Fig. A-FBFAA Sheet 02 view D

2 Clamp NSA5516-13ND Item 63

or

2 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

1 Spacer NSA5527-03-02 Item 14

1 Clip nut NSA5067-3-1 Item 43

1 Screw NAS1801-3-18 Item 79

1 Washer NAS1149F0332P Item 46

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 86

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@A300-600

SERVICE BULLETIN

(c) Install :

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

6 Clamp NSA5516-13ND Item 63

or

6 Clamp NSA5516-31ND Item 64

NOTE: Install the clamp Item 63 or 64 according to the bundle diameter.

4 Washer NAS1149F0332P Item 46

2 Screw Item (47) Retained at

removal

2 Screw Item (74) Retained at

removal

(12) Subtask 246103-831-004-001 - Install a bracket on the shroud box blanking plate at

RH side

Work Zones and Access Panels

Zone Access/Work location

148 Work location Frame 51

from Stringer 31 to Stringer 33

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 246103A02R12

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

21 NSA5050-3 3 NUT

29 A0041113420100 1 BRACKET

30 NAS1801-3-8 2 SCREW

37 NAS1801-3-9 1 SCREW

46 NAS1149F0332P 2 WASHER

63 NSA5516-13ND 2 CLAMP

64 NSA5516-31ND 2 CLAMP

70 A0041113500000 1 CLAMP

71 NAS1801-3-12 2 SCREW

75 A0041113500200 1 CLAMP

76 A0041113500400 1 CLAMP

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 87

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@A300-600

SERVICE BULLETIN

References

Fig. A-FBEAA

Installation of a Conduit on the Shroud

Box Bracket (LH and RH side)

Sheet 01

Sheet 02

Sheet 03

(a) Remove :

Refer to Fig. A-FBEAA Sheet 01

2 Screw Item (27) Discard

2 Washer Item (46) Discard

(b) Install the bracket :

Refer to Fig. A-FBEAA Sheet 01, Fig. A-FBEAA Sheet 02 and Fig. A-FBEAA Sheet

03

1 Bracket A0041113420100 Item 29

2 Screw NAS1801-3-12 Item 71

2 Washer NAS1149F0332P Item 46

(c) Attach the bundles on the shroud box bracket :

Refer to Fig. A-FBEAA Sheet 01, Fig. A-FBEAA Sheet 02 and Fig. A-FBEAA Sheet

03

1 Attach the bundles with :

2 Clamp NSA5516-13ND Item 63

or

2 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

NOTE: Two or three bundles may be installed.

1 Nut NSA5050-3 Item 21

and

1 Screw NAS1801-3-9 Item 37

2 Or attach the bundles with :

1 Clamp NSA5516-13ND Item 63

or

1 Clamp NSA5516-31ND Item 64

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 88

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@A300-600

SERVICE BULLETIN

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

NOTE: Two or three bundles may be installed.

and

1 Clamp A0041113500000 Item 70

or

1 Clamp A0041113500200 Item 75

or

1 Clamp A0041113500400 Item 76

NOTE: Install clamp Item 70 or 75 or 76 according to the bundle

diameters.

2 Nut NSA5050-3 Item 21

2 Screw NAS1801-3-8 Item 30

(13) Subtask 246103-831-007-001 - Modify the routing on rib 1 on the passage way to

the shroud box at RH side

Work Zones and Access Panels

Zone Access/Work location

670 Work location Rib 1

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 246103A01R14

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

12 NSA5527-03-01 4 SPACER

Kit 246103A02R12

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

12 NSA5527-03-01 2 SPACER

19 NSA935807-09 2 CLAMP

20 NSA935808-01 1 WASHER

21 NSA5050-3 1 NUT

22 NAS1801-3-24 1 SCREW

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 89

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@A300-600

SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

87 NSA360002 1 (M) EXTRUSIN

Kit 246103A04R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

24 NSA939510BN 1 (M) STRIP

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Epoxy Adhesive-Metal To

Metal - Legacy

05EJL9 As required

Epoxy Adhesive - Legacy 3 05EML7 As required

Contact Adhesive-Rubber &

Plastic Bonding Neopren

05JBC9 As required

Non Aqueous Cleaner -

Isopropyl Alcohol

08BBD1 As required

References

Elec. Std. Practices Manual (ESPM) 20-33-11

Process and Material Specification

(PMS)

Process and Material Specification (PMS)

01-01-28 Process E

Fig. A-FBCAA

Removal of the Clamps on the Passage

Way to the Shroud Box (LH and RH

side)

Sheet 01

Sheet 02

Sheet 03

Fig. A-FBDAA

Installation of the Clamps on the

Passage Way to the Shroud Box (LH

and RH side)

Sheet 01

Sheet 02

Sheet 03

(a) Remove :

Refer to Fig. A-FBCAA Sheet 01, Fig. A-FBCAA Sheet 02 and Fig. A-FBCAA Sheet

03

2 Clamp Item (19) Discard

1 Spacer Item (12) Discard

1 Screw Item (22) Discard

1 Washer Item (20) Discard

1 Nut Item (21) Discard

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 90

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@A300-600

SERVICE BULLETIN

(b) Install :

Refer to Fig. A-FBDAA Sheet 01, Fig. A-FBDAA Sheet 02 and Fig. A-FBDAA Sheet

03

2 Clamp NSA935807-09 Item 19

2 Spacer NSA5527-03-01 Item 12

1 Screw NAS1801-3-24 Item 22

1 Washer NSA935808-01 Item 20

1 Nut NSA5050-3 Item 21

(c) Refer to Fig. A-FBDAA Sheet 01 and Fig. A-FBDAA Sheet 03

1 (M) Extrusion NSA360002 Item 87

with:

Contact AdhesiveRubber & Plastic

Bonding Neopren

05JBC9 As required

(d) Measure the gap between the clamp and the structure, refer to Fig. A-FBCAA

Sheet 01 and Fig. A-FBCAA Sheet 02:

1 If the gap between the structure and the clamp is less than 6.35 mm (0.25 in.),

install, refer to Fig. A-FBDAA Sheet 02:

4 Spacer NSA5527-03-01 Item 12

2 If the gap between the structure and the clamp is more than 130 mm (5.118

in), contact AIRBUS, refer to Fig. A-FBCAA Sheet 02

NOTE: For operators that have the gap between the structure and the

clamp is more than 130 mm (5.118 in) contact Airbus at:

AIRBUS CUSTOMER SERVICES ENGINEERING - SEEA5

ELECTRICAL POWER GENERATION DISTRIBUTION &

LIGHTING SYSTEMS

1 ROND POINT MAURICE BELLONTE

31707 BLAGNAC CEDEX FRANCE

FAX +33 561 934 425

(e) Install a protection on the structure to protect the routes :

Refer to Fig. A-FBDAA Sheet 01, Fig. A-FBDAA Sheet 02 and Fig. A-FBDAA Sheet

03

Refer to ESPM 20-33-11

Refer to Process and Material Specification (PMS) 01-01-28 Process E

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 91

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@A300-600

SERVICE BULLETIN

1 (M) Strip-Protective NSA939510BN Item 24

NOTE: Install the Strip-Protective Item 24 with:

Epoxy AdhesiveMetal To Metal -

Legacy

05EJL9 As required

NOTE: Do the abrading and cleaning of the contact zones of StripProtective Item 24, on the structure with:

Non Aqueous

Cleaner - Isopropyl

Alcohol

08BBD1 As required

Epoxy Adhesive -

Legacy 3

05EML7 As required

(14) Subtask 246103-831-013-001 - Modify the routing of routes 2E and 2G in the

leading edge at RH wing

Work Zones and Access Panels

Zone Access/Work location

613

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills NON SPECIFIC

Material necessary to do the job

Kit 246103A02R12

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

34 NSA5527-03-08 2 SPACER

39 A9222505750000 2 SPACER

66 NSA935401-13 2 TIE

References

Fig. A-FBJAA

Modification of the Routing in the

Leading Edge (LH and RH side)

Sheet 01

(a) Install :

Refer to Fig. A-FBJAA Sheet 01

2 Spacer-Feeder A9222505750000 Item 39

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 92

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SERVICE BULLETIN

2 Spacer NSA5527-03-08 Item 34

2 Tie-Cable NSA935401-13 Item 66

(15) Subtask 246103-020-003-001 - Remove the clamps from LH wing

Work Zones and Access Panels

Zone Access/Work location

572

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

References

Fig. A-FBKAA

Removal/Installation of the Clamps in LH

and RH Wings

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

(a) Remove the clamps from LH wing at Rib location WIAX-27.96

Refer to Fig. A-FBKAA Sheet 01 and Fig. A-FBKAA Sheet 05 view J

1 Remove:

2 Clamps Item (51) Discard

1 Screw Item (37) Discard

1 Washer Item (46) Discard

(b) Remove the clamps from LH wing at Rib location WIAX-35.12.

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

1 Remove :

1 Screw Item (50) Discard

1 Washer Item (46) Discard

2 Clamp Item (51) Discard

1 Spacer Item (13) Discard

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 93

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@A300-600

SERVICE BULLETIN

(c) Remove the clamps from LH wing at Rib location WIAX-40.53.

Refer to Fig. A-FBKAA Sheet 01 and Fig. A-FBKAA Sheet 03

1 Remove :

2 Screw Item (50) Discard

2 Washer Item (46) Discard

2 Clamp Item (51) Discard

2 Spacer Item (13) Discard

(d) Remove the clamps from LH wing at Rib location WIAX-48.25

Refer to Fig. A-FBKAA Sheet 01 and Fig. A-FBKAA Sheet 05 view L

1 Remove:

2 Clamp Item (51) Discard

1 Screw Item (37) Retain

1 Washer Item (46) Discard

(e) Remove the clamps from LH wing at Rib location WIAX-74.08.

Refer to Fig. A-FBKAA Sheet 01 and Fig. A-FBKAA Sheet 04

1 Remove :

2 Screw Item (50) Discard

2 Washer Item (46) Discard

1 Clamp Item (51) Discard

1 Clamp Item (52) Discard

2 Clamp Item (53) Discard

1 Clamp Item (54) Discard

3 Spacer Item (13) Discard

(16) Subtask 246103-831-016-001 - Remove the clamps from RH wing

Work Zones and Access Panels

Zone Access/Work location

672

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 94

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@A300-600

SERVICE BULLETIN

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

References

Fig. A-FBKAA

Removal/Installation of the Clamps in LH

and RH Wings

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

(a) Remove the clamps from RH wing at Rib location WIAX-27.96.

Refer to Fig. A-FBKAA Sheet 01 and Fig. A-FBKAA Sheet 05 view J

1 Remove:

2 Clamps Item (51) Discard

1 Screw Item (37) Discard

1 Washer Item (46) Discard

(b) Remove the clamps from RH wing at Rib location WIAX-35.12.

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

1 Remove :

1 Screw Item (50) Discard

1 Washer Item (46) Discard

2 Clamp Item (51) Discard

1 Spacer Item (13) Discard

(c) Remove the clamps from RH wing at Rib location WIAX-40.53.

Refer to Fig. A-FBKAA Sheet 01 and Fig. A-FBKAA Sheet 03

1 Remove :

2 Screw Item (50) Discard

2 Washer Item (46) Discard

2 Clamp Item (51) Discard

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 95

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@A300-600

SERVICE BULLETIN

2 Spacer Item (13) Discard

(d) Remove the clamps from RH wing at Rib location WIAX-48.25.

Refer to Fig. A-FBKAA Sheet 01 and Fig. A-FBKAA Sheet 05 view L

1 Remove:

2 Clamp Item (51) Discard

1 Screw Item (37) Retain

1 Washer Item (46) Discard

(e) Remove the clamps from RH wing at Rib location WIAX-74.08.

Refer to Fig. A-FBKAA Sheet 01 and Fig. A-FBKAA Sheet 04

1 Remove :

2 Screw Item (50) Discard

2 Washer Item (46) Discard

1 Clamp Item (51) Discard

1 Clamp Item (52) Discard

2 Clamp Item (53) Discard

1 Clamp Item (54) Discard

3 Spacer Item (13) Discard

(17) Subtask 246103-831-401-001 - Modify the Electrical Support Brackets in the Outer

Shroud Box, LH Wing

Work Zones and Access Panels

Zone Access/Work location

572

Manpower Resources

Manhours 2.50

Minimum number of person 2

Subtask elapsed time 1.25

Skills AIRFRAME

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 96

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

Material necessary to do the job

Kit 246103B01R03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 A9245005500000 1 BRACKET

2 MS20470AD4-10 4 RIVET

3 A9245005600000 1 BRACKET

8 DAN7-5-6 3 PIN

9 HL70-6 3 COLLAR

Component COMPB01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

8 DAN7-5-6 3 PIN

9 HL70-6 3 COLLAR

Consumable CMLB01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Primer Polyurethane Paint -

Corrosion Inhibiting

04EAC2 As required

Top Coat Polyurethane -

Grey Internal Structure

04JME4 As required

Polysulfide Sealant -

General Purpose Interfay

06AAC1 As required

Non Aqueous Cleaner -

General

08BAA9 As required

Surface Pretreatment - Light

Alloys Chemical Conver

10ABC1 As required

Textile - Lint Free Cotton 14SBA1 As required

References

Fig. A-UAAAA

Modification of the Support Brackets in

the Outer Shroud Box

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Refer to Fig. A-UAAAA Sheet 01, Fig. A-UAAAA Sheet 02, Fig. A-UAAAA Sheet 03 and

Fig. A-UAAAA Sheet 04

(a) Modify the LH Support Bracket Assembly at Rib Location WIAX-35.12

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

1 Carefully drill out and remove the items that follow:

2 Rivet Item (2) Discard

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 97

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@A300-600

SERVICE BULLETIN

2 Remove from the structure the item that follows:

1 Bracket Assy-Cable

Support

A9244012400000 Item (1) Discard

3 Clean the area with a:

Textile - Lint Free

Cotton

14SBA1 As required

made moist with:

Non Aqueous

Cleaner - General

08BAA9 As required

4 Use:

Polysulfide Sealant

- General Purpose

Interfay

06AAC1 As required

and wet assemble to the structure the item that follows:

1 Bracket Assy-Cable

Support

A9245005500000 Item 1

with:

2 Rivet MS20470AD4-10 Item 2

5 Apply

Primer

Polyurethane Paint

- Corrosion

Inhibiting

04EAC2 As required

and

Top Coat

Polyurethane - Grey

Internal Structure

04JME4 As required

to the heads and tails of the rivets.

(b) Modify the LH Support Bracket Assembly at Rib Location WIAX-40.53

Refer to Fig. A-UAAAA Sheet 01 and Fig. A-UAAAA Sheet 03

1 Carefully drill out and remove the items that follow:

3 Rivet Item (2) Discard

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 98

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

2 Remove from the structure the item that follows:

1 Angle-Attachment A5724091525800 Item (3) Discard

3 Clean the area with a:

Textile - Lint Free

Cotton

14SBA1 As required

made moist with:

Non Aqueous

Cleaner - General

08BAA9 As required

4 Use:

Polysulfide Sealant

- General Purpose

Interfay

06AAC1 As required

and wet assemble to the structure the item that follows:

1 Bracket Assy-Cable

Support

A9245005600000 Item 3

with:

For operators with KITB01R03:

3 Pin-Rivet DAN7-5-6 Item 8

3 Collar HL70-6 Item 9

For operators with KITB01R02, get this item from COMPB01:

3 Pin-Rivet DAN7-5-6 Item 8

3 Collar HL70-6 Item 9

5 Apply:

Primer

Polyurethane Paint

- Corrosion

Inhibiting

04EAC2 As required

and

Top Coat

Polyurethane - Grey

Internal Structure

04JME4 As required

to the heads and tails of the fasteners.

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 99

5

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@A300-600

SERVICE BULLETIN

(c) Modify the LH Support Bracket Assembly at Rib Location WIAX-74.08

Refer to Fig. A-UAAAA Sheet 01 and Fig. A-UAAAA Sheet 04

1 Carefully drill out and remove the items that follow:

4 Rivet Item (2) Discard

2 Remove from the structure the item that follows:

2 Bracket Assy-Cable

Support

A9244012400000 Item (1) Discard

3 Clean the area with a:

Textile - Lint Free

Cotton

14SBA1 As required

made moist with:

Non Aqueous

Cleaner - General

08BAA9 As required

4 At the locations indicated, increase the two holes to 4.90mm (0.193in.), refer

to Fig. A-UAAAA Sheet 04.

5 Deburr the holes.

6 Clean the area with a:

Textile - Lint Free

Cotton

14SBA1 As required

made moist with:

Non Aqueous

Cleaner - General

08BAA9 As required

7 Apply:

Surface

Pretreatment - Light

Alloys Chemical

Conver

10ABC1 As required

to the cut surfaces of the holes.

8 At the two top holes (which are not used for the new bracket installation) wet

install these items to plug the open holes:

2 Rivet MS20470AD4-10 Item 2

use

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 100

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

Polysulfide Sealant

- General Purpose

Interfay

06AAC1 As required

(18) Subtask 246103-831-008-001 - Modify the routing of routes 1P and 2P at LH wing

Work Zones and Access Panels

Zone Access/Work location

570 Work location from Rib 1 to Rib 6

Manpower Resources

Manhours 1.50

Minimum number of person 1

Subtask elapsed time 1.50

Skills NON SPECIFIC

Material necessary to do the job

Kit 246103A01R14

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

14 NSA5527-03-02 3 SPACER

26 NSA935401-04 12 TIE

66 NSA935401-13 3 TIE

86 EN6049-007-08-5 5 (M) SLEEVE

References

Fig. A-FBYAA

Modification of the Routing in LH and

RH Wings

Sheet 01

Sheet 02

(a) Between rib 5 and rib 6, install :

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

5 (M) Sleeve-Protective EN6049-007-08-5 Item 86

12 Tie-Cable NSA935401-04 Item 26

and

3 Spacer NSA5527-03-02 Item 14

attached with :

3 Tie-Cable NSA935401-13 Item 66

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 101

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Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

(19) Subtask 246103-831-009-001 - Modify the routing of routes 1P and 2P at RH wing

Work Zones and Access Panels

Zone Access/Work location

670 Work location from Rib 1 to Rib 6

Manpower Resources

Manhours 1.50

Minimum number of person 1

Subtask elapsed time 1.50

Skills NON SPECIFIC

Material necessary to do the job

Kit 246103A02R12

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

14 NSA5527-03-02 3 SPACER

26 NSA935401-04 12 TIE

66 NSA935401-13 3 TIE

86 EN6049-007-08-5 5 (M) SLEEVE

References

Fig. A-FBYAA

Modification of the Routing in LH and

RH Wings

Sheet 01

Sheet 02

(a) Between rib 5 and rib 6, install :

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

5 (M) Sleeve-Protective EN6049-007-08-5 Item 86

12 Tie-Cable NSA935401-04 Item 26

and

3 Spacer NSA5527-03-02 Item 14

attached with :

3 Tie-Cable NSA935401-13 Item 66

(20) Subtask 246103-831-017-001 - Install the clamps in LH wing

Work Zones and Access Panels

Zone Access/Work location

572

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 102

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

Manpower Resources

Manhours 1.00

Minimum number of person 2

Subtask elapsed time 0.50

Skills NON SPECIFIC

Material necessary to do the job

Kit 246103A01R14

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

12 NSA5527-03-01 1 SPACER

13 NSA5527-03-03 1 SPACER

37 NAS1801-3-9 3 SCREW

46 NAS1149F0332P 6 WASHER

50 NAS1801-3-13 1 SCREW

52 NSA5516-08ND 8 CLAMP

55 NAS1801-3-16 1 SCREW

85 ASNA51072503 1 (M) TAPE

86 EN6049-007-08-5 2.5 (M) SLEEVE

Kit 246103A03R04

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

21 NSA5050-3 2 NUT

22 NAS1801-3-24 2 SCREW

90 NAS1149D0316H 2 WASHER

Kit 246103B01R03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

60 A9245000200000 1 GUIDE

References

Fig. A-FBKAA

Removal/Installation of the Clamps in LH

and RH Wings

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

(a) Install the clamps in LH wing at Rib location WIAX-27.96.

Refer to Fig. A-FBKAA Sheet 01 and Fig. A-FBKAA Sheet 05 view K

1 Install:

2 Clamp NSA5516-08ND Item 52

1 Screw NAS1801-3-9 Item 37

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 103

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Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

1 Washer NAS1149F0332P Item 46

(b) Install the clamps in LH wing at Rib location WIAX-35.12.

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

1 Install :

1 Spacer NSA5527-03-01 Item 12

1 Spacer NSA5527-03-03 Item 13

2 Clamp NSA5516-08ND Item 52

2 Washer NAS1149F0332P Item 46

1 Screw NAS1801-3-13 Item 50

1 Screw NAS1801-3-16 Item 55

(c) Install the clamps in LH wing at Rib location WIAX-40.53.

Refer to Fig. A-FBKAA Sheet 01 and Fig. A-FBKAA Sheet 03

1 Install :

2 Clamp NSA5516-08ND Item 52

2 Washer NAS1149F0332P Item 46

2 Screw NAS1801-3-9 Item 37

(d) Install the clamps at LH wing at Rib location WIAX-48.25.

Refer to Fig. A-FBKAA Sheet 01 and Fig. A-FBKAA Sheet 05 view M

1 Install:

2 Clamp NSA5516-08ND Item 52

1 Washer NAS1149F0332P Item 46

1 Screw Item (37) Retained at

removal

(e) Install the guide in LH wing at Rib location WIAX-74.08.

Refer to Fig. A-FBKAA Sheet 01 and Fig. A-FBKAA Sheet 04

1 Install :

1 Guide Assy-Conduit A9245000200000 Item 60

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 104

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@A300-600

SERVICE BULLETIN

2 Screw NAS1801-3-24 Item 22

2 Washer NAS1149D0316H Item 90

2 Nut NSA5050-3 Item 21

NOTE: If necessary, to make the diameters of the bundles match with

the diameter of the holes of the guide Item 60, use:

2.5 (M) Sleeve-Protective EN6049-007-08-5 Item 86

1 (M) Tape-Reinforced

Silicone

ASNA51072503 Item 85

(21) Subtask 246103-831-018-001 - Install the clamps in RH wing

Work Zones and Access Panels

Zone Access/Work location

672

Manpower Resources

Manhours 1.00

Minimum number of person 2

Subtask elapsed time 0.50

Skills NON SPECIFIC

Material necessary to do the job

Kit 246103A01R14

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

85 ASNA51072503 1 (M) TAPE

Kit 246103A02R12

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

12 NSA5527-03-01 1 SPACER

13 NSA5527-03-03 1 SPACER

37 NAS1801-3-9 3 SCREW

46 NAS1149F0332P 6 WASHER

50 NAS1801-3-13 1 SCREW

52 NSA5516-08ND 8 CLAMP

55 NAS1801-3-16 1 SCREW

86 EN6049-007-08-5 2.5 (M) SLEEVE

Kit 246103A03R04

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

21 NSA5050-3 2 NUT

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 105

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

22 NAS1801-3-24 2 SCREW

90 NAS1149D0316H 2 WASHER

Kit 246103B01R03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

60 A9245000200000 1 GUIDE

References

Fig. A-FBKAA

Removal/Installation of the Clamps in LH

and RH Wings

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

(a) Install the clamps in RH wing at Rib location WIAX-27.96.

Refer to Fig. A-FBKAA Sheet 01 and Fig. A-FBKAA Sheet 05 view K

1 Install:

2 Clamp NSA5516-08ND Item 52

1 Washer NAS1149F0332P Item 46

1 Screw NAS1801-3-9 Item 37

(b) Install the clamps in RH wing at Rib location WIAX-35.12.

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

1 Install :

1 Spacer NSA5527-03-01 Item 12

1 Spacer NSA5527-03-03 Item 13

2 Clamp NSA5516-08ND Item 52

2 Washer NAS1149F0332P Item 46

1 Screw NAS1801-3-13 Item 50

1 Screw NAS1801-3-16 Item 55

(c) Install the clamps in RH wing at Rib location WIAX-40.53.

Refer to Fig. A-FBKAA Sheet 01 and Fig. A-FBKAA Sheet 03

2 Clamp NSA5516-08ND Item 52

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 106

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@A300-600

SERVICE BULLETIN

2 Washer NAS1149F0332P Item 46

2 Screw NAS1801-3-9 Item 37

(d) Install the clamps at RH wing at Rib location WIAX-48.25.

Refer to Fig. A-FBKAA Sheet 01 and Fig. A-FBKAA Sheet 05 view M

1 Install:

2 Clamp NSA5516-08ND Item 52

1 Washer NAS1149F0332P Item 46

1 Screw Item (37) Retained at

removal

(e) Install the guide in RH wing at Rib location WIAX-74.08.

Refer to Fig. A-FBKAA Sheet 01 and Fig. A-FBKAA Sheet 04

1 Install :

1 Guide Assy-Conduit A9245000200000 Item 60

2 Screw NAS1801-3-24 Item 22

2 Washer NAS1149D0316H Item 90

2 Nut NSA5050-3 Item 21

NOTE: If necessary, to make the diameters of the bundles match with

the diameter of the holes of the guide Item 60, use:

2.5 (M) Sleeve-Protective EN6049-007-08-5 Item 86

1 (M) Tape-Reinforced

Silicone

ASNA51072503 Item 85

(22) Subtask 246103-831-402-001 - Modify the P-CLIPS at Location WOFX-204.5, LH

Wing

Work Zones and Access Panels

Zone Access/Work location

512

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills ELECTRICAL

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 107

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

References

Fig. A-UACAA

Modification of the Aircraft Clipping

Sheet 01

Sheet 02

(a) Remove from the support bracket and the harness, Item (5), refer to Fig. A-UACAA

Sheet 01:

2 Bolt Item (6) Retain

2 P-clip Item (7) Retain

(b) Rotate the two P-clips 180 degrees.

(c) Install to the harness, Item (5) and the support brackets, refer to Fig. A-UACAA

Sheet 01:

2 Bolt Item (6) Retained at

removal

2 P-clip Item (7) Retained at

removal

(23) Subtask 246103-831-403-001 - Modify the Backshell of the Connector and the

Structure at Location ABX 36.5, LH Wing

Work Zones and Access Panels

Zone Access/Work location

575

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills ELECTRICAL

References

Fig. A-UACAA

Modification of the Aircraft Clipping

Sheet 01

Sheet 02

CAUTION: DO NOT ROTATE THE BACKSHELL AT THIS WORKSTEP.

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

(a) Loosen the backshell locknut enough so that the backshell can be rotated.

CAUTION: DO NOT ROTATE THE BACKSHELL MORE THAN 45

DEGREES.

CAUTION: DO NOT STRESS THE WIRING INSIDE THE BACKSHELL.

(b) Gently rotate the backshell to get a 10mm (0.394in.) minimum clearance between

the electrical conduit and the support structure.

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 108

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@A300-600

SERVICE BULLETIN

(c) Tighten the backshell.

(d) Check to make sure that there is a minimum clearance of 10mm (0.394in.) between

the electrical conduit and the support structure.

(24) Subtask 246103-831-405-001 - Modify the Electrical Support Brackets in the Outer

Shroud Box, RH Wing

Work Zones and Access Panels

Zone Access/Work location

672

Manpower Resources

Manhours 2.50

Minimum number of person 2

Subtask elapsed time 1.25

Skills AIRFRAME

Material necessary to do the job

Kit 246103B01R03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 A9245005500000 BRACKET

2 MS20470AD4-10 RIVET

3 A9245005600000 BRACKET

8 DAN7-5-6 PIN

9 HL70-6 COLLAR

Component COMPB01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

8 DAN7-5-6 PIN

9 HL70-6 COLLAR

Consumable CMLB01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Primer Polyurethane Paint -

Corrosion Inhibiting

04EAC2 As required

Top Coat Polyurethane -

Grey Internal Structure

04JME4 As required

Polysulfide Sealant -

General Purpose Interfay

06AAC1 As required

Non Aqueous Cleaner -

General

08BAA9 As required

Surface Pretreatment - Light

Alloys Chemical Conver

10ABC1 As required

Textile - Lint Free Cotton 14SBA1 As required

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 109

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

References

Fig. A-UAAAA

Modification of the Support Brackets in

the Outer Shroud Box

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Refer to Fig. A-UAAAA Sheet 01, Fig. A-UAAAA Sheet 02, Fig. A-UAAAA Sheet 03 and

Fig. A-UAAAA Sheet 04

(a) Modify the RH Support Bracket Assembly at Rib Location WIAX-35.12

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

1 Carefully drill out and remove the items that follow:

2 Rivet Item (2) Discard

2 Remove from the structure the item that follows:

1 Bracket Assy-Cable

Support

A9244012400000 Item (1) Discard

3 Clean the area with a:

Textile - Lint Free

Cotton

14SBA1 As required

made moist with:

Non Aqueous

Cleaner - General

08BAA9 As required

4 Use:

Polysulfide Sealant

- General Purpose

Interfay

06AAC1 As required

and wet assemble to the structure the item that follows:

1 Bracket Assy-Cable

Support

A9245005500000 Item 1

with:

2 Rivet MS20470AD4-10 Item 2

5 Apply

Primer

Polyurethane Paint

- Corrosion

Inhibiting

04EAC2 As required

and

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 110

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Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

Top Coat

Polyurethane - Grey

Internal Structure

04JME4 As required

to the heads and tails of the rivets.

(b) Modify the RH Support Bracket Assembly at Rib Location WIAX-40.53

Refer to Fig. A-UAAAA Sheet 01 and Fig. A-UAAAA Sheet 03

1 Carefully drill out and remove the items that follow:

3 Rivet Item (2) Discard

2 Remove from the structure the item that follows:

1 Angle-Attachment A5724091525800 Item (3) Discard

3 Clean the area with a:

Textile - Lint Free

Cotton

14SBA1 As required

made moist with:

Non Aqueous

Cleaner - General

08BAA9 As required

4 Use:

Polysulfide Sealant

- General Purpose

Interfay

06AAC1 As required

and wet assemble to the structure the item that follows:

1 Bracket Assy-Cable

Support

A9245005600000 Item 3

with:

For operators with KITB01R03:

3 Pin-Rivet DAN7-5-6 Item 8

3 Collar HL70-6 Item 9

For operators with KITB01R02, get this item from COMPB01:

3 Pin-Rivet DAN7-5-6 Item 8

3 Collar HL70-6 Item 9

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 111

5

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@A300-600

SERVICE BULLETIN

5 Apply:

Primer

Polyurethane Paint

- Corrosion

Inhibiting

04EAC2 As required

and

Top Coat

Polyurethane - Grey

Internal Structure

04JME4 As required

to the heads and tails of the fasteners.

(c) Modify the RH Support Bracket Assembly at Rib Location WIAX-74.08

Refer to Fig. A-UAAAA Sheet 01 and Fig. A-UAAAA Sheet 04

1 Carefully drill out and remove the items that follow:

4 Rivet Item (2) Discard

2 Remove from the structure the item that follows:

2 Bracket Assy-Cable

Support

A9244012400000 Item (1) Discard

3 Clean the area with a:

Textile - Lint Free

Cotton

14SBA1 As required

made moist with:

Non Aqueous

Cleaner - General

08BAA9 As required

4 At the locations indicated, increase the two holes to 4.90mm (0.193in.), refer

to Fig. A-UAAAA Sheet 04.

5 Deburr the holes.

6 Clean the area with a:

Textile - Lint Free

Cotton

14SBA1 As required

made moist with:

Non Aqueous

Cleaner - General

08BAA9 As required

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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7 Apply:

Surface

Pretreatment - Light

Alloys Chemical

Conver

10ABC1 As required

to the cut surfaces of the holes.

8 At the two top holes (which are not used for the new bracket installation) wet

install these items to plug the open holes:

2 Rivet MS20470AD4-10 Item 2

use

Polysulfide Sealant

- General Purpose

Interfay

06AAC1 As required

(25) Subtask 246103-831-406-001 - Modify the P-CLIPS at Location WOFX-204.5, RH

Wing

Work Zones and Access Panels

Zone Access/Work location

612

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills ELECTRICAL

References

Fig. A-UACAA

Modification of the Aircraft Clipping

Sheet 01

Sheet 02

(a) Remove from the support bracket and the harness, Item (5), refer to Fig. A-UACAA

Sheet 01:

2 Bolt Item (6) Retain

2 P-clip Item (7) Retain

(b) Rotate the two P-clips 180 degrees.

(c) Install to the harness, Item (5) and the support brackets, refer to Fig. A-UACAA

Sheet 01:

2 Bolt Item (6) Retained at

removal

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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SERVICE BULLETIN

2 P-clip Item (7) Retained at

removal

(26) Subtask 246103-831-407-001 - Modify the Backshell of the Connector and the

Structure at Location ABX 36.5, RH Wing

Work Zones and Access Panels

Zone Access/Work location

675

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills ELECTRICAL

References

Fig. A-UACAA

Modification of the Aircraft Clipping

Sheet 01

Sheet 02

CAUTION: DO NOT ROTATE THE BACKSHELL AT THIS WORKSTEP.

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

(a) Loosen the backshell locknut enough so that the backshell can be rotated.

CAUTION: DO NOT ROTATE THE BACKSHELL MORE THAN 45

DEGREES.

CAUTION: DO NOT STRESS THE WIRING INSIDE THE BACKSHELL.

(b) Gently rotate the backshell to get a 10mm (0.394in.) minimum clearance between

the electrical conduit and the support structure.

(c) Tighten the backshell.

(d) Check to make sure that there is a minimum clearance of 10mm (0.394in.) between

the electrical conduit and the support structure.

**CONF 002

(1) Subtask 246103-831-001-001 - Remove the clamps between FR50 and FR52 at LH

side

Work Zones and Access Panels

Zone Access/Work location

147 Work location from Frame 50 to Frame 52

from Stringer 32 to Stringer 33

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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Manpower Resources

Manhours 1.50

Minimum number of person 1

Subtask elapsed time 1.50

Skills NON SPECIFIC

References

Fig. A-FBAAA

Removal of the Old Brackets of the

Passage Way at FR52 (LH side)

Sheet 01

Sheet 02

Sheet 03

Fig. A-FBFAA

Modification of the Routing Between

FR50 and FR51 at STGR 32 (LH and

RH side)

Sheet 01

Sheet 02

(a) On the panel, remove :

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

2 Screw Item (47) Discard

2 Washer Item (46) Discard

2 Clip nut Item (43) Discard

1 Clamp Item (44) Retain

1 Clamp Item (45) Retain

(b) On the bracket (if installed), remove :

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

1 Nut Item (48) Discard

1 Washer Item (49) Discard

1 Screw Item (10) Discard

1 Clamp Item (11) Retain

(c) Remove :

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

2 Screw Item (47) Discard

2 Washer Item (46) Discard

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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1 Seal fitting Item (41) Discard

1 Bracket assy Item (42) Discard

(d) Remove :

Refer to Fig. A-FBAAA Sheet 01 and Fig. A-FBAAA Sheet 03

4 Clamp Item (72) Discard

2 Screw Item (74) Retain

2 Washer Item (73) Discard

1 Clamp Item (44) Discard

1 Clamp Item (45) Discard

2 Washer Item (46) Discard

2 Screw Item (47) Retain

(e) Depending on the stacking, remove :

Refer to Fig. A-FBFAA Sheet 01

4 Clamp Item (16) Discard

2 Clamp Item (32) Discard

2 Spacer Item (14) Discard

2 Clip nut Item (43) Discard

2 Washer Item (20) Discard

2 Screw Item (33) Discard

Or remove :

Refer to Fig. A-FBFAA Sheet 01

4 Clamp Item (16) Discard

2 Spacer Item (14) Discard

2 Clip nut Item (43) Discard

2 Washer Item (20) Discard

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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2 Screw Item (33) Discard

(2) Subtask 246103-831-019-001 - Modify the Routing between FR50 and FR52 and

between STGR 33 and 30 at LH side

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 246103A01R14

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

77 EN6049-007-19-5 7.5 (M) SLEEVE

78 EN6049-007-13-5 7.5 (M) SLEEVE

86 EN6049-007-08-5 7.5 (M) SLEEVE

References

Fig. A-FBWAA

Modification of the Routing between

FR50 and FR52 (LH and RH side)

Sheet 01

(a) Remove :

Refer to Fig. A-FBWAA Sheet 01

5 (M) Conduit Item (77) Discard

NOTE: A third conduit may be installed. If installed, remove it.

(b) Install :

Refer to Fig. A-FBWAA Sheet 01

5 (M) Sleeve EN6049-007-13-5 Item 78

or

5 (M) Sleeve EN6049-007-19-5 Item 77

or

5 (M) Sleeve-Protective EN6049-007-08-5 Item 86

NOTE: Install the sleeve Item 77 or 78 or 86 according to the harness

diameter.

NOTE: If a third conduit was installed, install :

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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2.5 (M) Sleeve EN6049-007-13-5 Item 78

or

2.5 (M) Sleeve EN6049-007-19-5 Item 77

or

2.5 (M) Sleeve-Protective EN6049-007-08-5 Item 86

NOTE: Install the sleeve Item 77 or 78 or 86 according to the harness

diameter.

(3) Subtask 246103-420-001-001 - Install the clamps between FR50 and FR52 at LH

side

Work Zones and Access Panels

Zone Access/Work location

147 Work location from Frame 50 to Frame 52

from Stringer 31 to Stringer 32

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 246103A01R14

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

10 NAS1801-3-17 1 SCREW

12 NSA5527-03-01 2 SPACER

14 NSA5527-03-02 2 SPACER

23 NSA935401-05 1 TIE

33 NAS1801-3-25 1 SCREW

38 ABS0731A01 1 SUPPORT

41 A0041095620000 1 SEAL

42 A0041095400000 1 BRACKET

43 NSA5067-3-1 4 NUT

46 NAS1149F0332P 11 WASHER

47 NAS1801-3-7 4 SCREW

48 MS21042-3 1 NUT

63 NSA5516-13ND 12 CLAMP

64 NSA5516-31ND 12 CLAMP

79 NAS1801-3-18 1 SCREW

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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References

Fig. A-FBFAA

Modification of the Routing Between

FR50 and FR51 at STGR 32 (LH and

RH side)

Sheet 01

Sheet 02

Fig. A-FBBAA

Installation of the New Brackets of the

Passage Way at FR52 (LH side)

Sheet 01

Sheet 02

(a) Depending on the staking, install :

Refer to Fig. A-FBFAA Sheet 01 and Fig. A-FBFAA Sheet 02 view C

3 Clamp NSA5516-13ND Item 63

or

3 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

1 Spacer NSA5527-03-01 Item 12

1 Spacer NSA5527-03-02 Item 14

1 Screw NAS1801-3-25 Item 33

1 Washer NAS1149F0332P Item 46

1 Clip nut NSA5067-3-1 Item 43

Or install :

Refer to Fig. A-FBFAA Sheet 01 and Fig. A-FBFAA Sheet 02 view C

2 Clamp NSA5516-13ND Item 63

or

2 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

1 Spacer NSA5527-03-01 Item 12

1 Spacer NSA5527-03-02 Item 14

1 Screw NAS1801-3-25 Item 33

1 Washer NAS1149F0332P Item 46

1 Clip nut NSA5067-3-1 Item 43

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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(b) Depending on the stacking, install :

Refer to Fig. A-FBFAA Sheet 01 and Fig. A-FBFAA Sheet 02 view D

3 Clamp NSA5516-13ND Item 63

or

3 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

1 Spacer NSA5527-03-02 Item 14

1 Screw NAS1801-3-18 Item 79

1 Clip nut NSA5067-3-1 Item 43

1 Washer NAS1149F0332P Item 46

Or install :

Refer to Fig. A-FBFAA Sheet 01 and Fig. A-FBFAA Sheet 02 view D

2 Clamp NSA5516-13ND Item 63

or

2 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

1 Spacer NSA5527-03-02 Item 14

1 Screw NAS1801-3-18 Item 79

1 Washer NAS1149F0332P Item 46

1 Clip nut NSA5067-3-1 Item 43

(c) Install :

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

1 Seal Fitting A0041095620000 Item 41

1 Bracket assy A0041095400000 Item 42

2 Screw NAS1801-3-7 Item 47

2 Washer NAS1149F0332P Item 46

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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(d) On the bracket (if installed), install :

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

1 Clamp Item (11) Retained at

removal

1 Spacer NSA5527-03-01 Item 12

1 Screw NAS1801-3-17 Item 10

1 Washer NAS1149F0332P Item 46

1 Nut MS21042-3 Item 48

(e) On the panel, install :

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

1 Clamp Item (44) Retained at

removal

1 Clamp Item (45) Retained at

removal

2 Screw NAS1801-3-7 Item 47

2 Washer NAS1149F0332P Item 46

2 Clip nut NSA5067-3-1 Item 43

(f) Install :

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

6 Clamp NSA5516-13ND Item 63

or

6 Clamp NSA5516-31ND Item 64

NOTE: Install the clamp Item 63 or 64 according to the bundle diameter.

4 Washer NAS1149F0332P Item 46

2 Screw Item (47) Retained at

removal

2 Screw Item (74) Retained at

removal

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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(g) Between the routes, install :

Refer to Fig. A-FBBAA Sheet 01

1 Support-Cable ABS0731A01 Item 38

1 Tie-Cable NSA935401-05 Item 23

(4) Subtask 246103-831-003-001 - Install a bracket on the shroud box blanking plate at

LH side

Work Zones and Access Panels

Zone Access/Work location

147 Work location Frame 51

from Stringer 31 to Stringer 33

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 246103A01R14

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

21 NSA5050-3 3 NUT

28 A0041113420000 1 BRACKET

30 NAS1801-3-8 2 SCREW

37 NAS1801-3-9 1 SCREW

46 NAS1149F0332P 2 WASHER

63 NSA5516-13ND 2 CLAMP

64 NSA5516-31ND 2 CLAMP

70 A0041113500000 1 CLAMP

71 NAS1801-3-12 2 SCREW

75 A0041113500200 1 CLAMP

76 A0041113500400 1 CLAMP

References

Fig. A-FBEAA

Installation of a Conduit on the Shroud

Box Bracket (LH and RH side)

Sheet 01

Sheet 02

Sheet 03

(a) Remove :

Refer to Fig. A-FBEAA Sheet 01

2 Screw Item (27) Discard

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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2 Washer Item (46) Discard

(b) Install the bracket :

Refer to Fig. A-FBEAA Sheet 01, Fig. A-FBEAA Sheet 02 and Fig. A-FBEAA Sheet

03

1 Bracket A0041113420000 Item 28

attach with :

2 Screw NAS1801-3-12 Item 71

2 Washer NAS1149F0332P Item 46

(c) Attach the bundles on the shroud box bracket :

Refer to Fig. A-FBEAA Sheet 01, Fig. A-FBEAA Sheet 02 and Fig. A-FBEAA Sheet

03

1 Attach the bundles with :

2 Clamp NSA5516-13ND Item 63

or

2 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

NOTE: Two or three bundles may be installed.

1 Nut NSA5050-3 Item 21

and

1 Screw NAS1801-3-9 Item 37

2 Or attach the bundles with :

2 Clamp NSA5516-13ND Item 63

or

2 Clamp NSA5516-31ND Item 64

and

1 Clamp A0041113500000 Item 70

or

1 Clamp A0041113500200 Item 75

or

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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1 Clamp A0041113500400 Item 76

NOTE: Install clamp Item 70 or 75 or 76 according to the bundle

diameters.

NOTE: Two or three bundles may be installed.

2 Nut NSA5050-3 Item 21

2 Screw NAS1801-3-8 Item 30

(5) Subtask 246103-831-006-001 - Modify the routing on rib 1 on the passage way to

the shroud box at LH side

Work Zones and Access Panels

Zone Access/Work location

570 Work location Rib 1

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 246103A01R14

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

12 NSA5527-03-01 6 SPACER

19 NSA935807-09 2 CLAMP

20 NSA935808-01 1 WASHER

21 NSA5050-3 1 NUT

22 NAS1801-3-24 1 SCREW

87 NSA360002 1 (M) EXTRUSIN

Kit 246103A04R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

24 NSA939510BN 1 (M) STRIP

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Epoxy Adhesive-Metal To

Metal - Legacy

05EJL9 As required

Epoxy Adhesive - Legacy 3 05EML7 As required

Contact Adhesive-Rubber &

Plastic Bonding Neopren

05JBC9 As required

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Non Aqueous Cleaner -

Isopropyl Alcohol

08BBD1 As required

References

Elec. Std. Practices Manual (ESPM) 20-33-11

Process and Material Specification

(PMS)

Process and Material Specification (PMS)

01-01-28 Process E

Fig. A-FBCAA

Removal of the Clamps on the Passage

Way to the Shroud Box (LH and RH

side)

Sheet 01

Sheet 02

Sheet 03

Fig. A-FBDAA

Installation of the Clamps on the

Passage Way to the Shroud Box (LH

and RH side)

Sheet 01

Sheet 02

Sheet 03

(a) Remove :

Refer to Fig. A-FBCAA Sheet 01 and Fig. A-FBCAA Sheet 03

2 Clamp Item (19) Discard

1 Spacer Item (12) Discard

1 Screw Item (22) Discard

1 Washer Item (20) Discard

1 Nut Item (21) Discard

(b) Install :

Refer to Fig. A-FBDAA Sheet 01, Fig. A-FBDAA Sheet 02 and Fig. A-FBDAA Sheet

03

2 Clamp NSA935807-09 Item 19

2 Spacer NSA5527-03-01 Item 12

1 Screw NAS1801-3-24 Item 22

1 Washer NSA935808-01 Item 20

1 Nut NSA5050-3 Item 21

(c) Refer to Fig. A-FBDAA Sheet 01 and Fig. A-FBDAA Sheet 03

1 (M) Extrusion NSA360002 Item 87

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with:

Contact AdhesiveRubber & Plastic

Bonding Neopren

05JBC9 As required

(d) Measure the gap between the clamp and the structure, refer to Fig. A-FBCAA

Sheet 01 and Fig. A-FBCAA Sheet 02:

1 If the gap between the structure and the clamp is less than 6.35 mm (0.25 in.),

install, refer to Fig. A-FBDAA Sheet 02:

4 Spacer NSA5527-03-01 Item 12

2 If the gap between the structure and the clamp is more than 130 mm (5.118

in.), CONTACT AIRBUS, refer to Fig. A-FBCAA Sheet 02:

NOTE: For operators that have the gap between the structure and the

clamp is more than 130 mm (5.118 in) contact Airbus at:

AIRBUS CUSTOMER SERVICES ENGINEERING - SEEA5

ELECTRICAL POWER GENERATION DISTRIBUTION &

LIGHTING SYSTEMS

1 ROND POINT MAURICE BELLONTE

31707 BLAGNAC CEDEX FRANCE

FAX +33 561 934 425

(e) Install a protection on the structure to protect the routes :

Refer to Fig. A-FBDAA Sheet 01, Fig. A-FBDAA Sheet 02 and Fig. A-FBDAA Sheet

03

Refer to ESPM 20-33-11

Refer to Process and Material Specification (PMS) 01-01-28 Process E

1 (M) Strip-Protective NSA939510BN Item 24

NOTE: Install the Strip-Protective Item 24 with:

Epoxy AdhesiveMetal To Metal -

Legacy

05EJL9 As required

NOTE: Do the abrading and cleaning of the contact zones of StripProtective Item 24, on the structure with:

Non Aqueous

Cleaner - Isopropyl

Alcohol

08BBD1 As required

Epoxy Adhesive -

Legacy 3

05EML7 As required

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 126

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(6) Subtask 246103-831-010-001 - Modify the routing of routes 1P and 2P in the

hydraulic shroud box at LH side

Work Zones and Access Panels

Zone Access/Work location

571

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 246103A01R14

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

20 NSA935808-01 7 WASHER

34 NSA5527-03-08 6 SPACER

71 NAS1801-3-12 1 SCREW

81 NAS1801-3-20 6 SCREW

84 NSA5527-03-06 1 SPACER

References

Fig. A-FBGAA

Modification of the Routing of Routes 1P

and 2P in the Shroud Box (LH side)

Sheet 01

Sheet 02

Sheet 03

(a) For Section A-A and C-C, remove :

Refer to Fig. A-FBGAA Sheet 01, Fig. A-FBGAA Sheet 02 and Fig. A-FBGAA

Sheet 03

7 Screw Item (22) Discard

7 Washer Item (20) Discard

14 Clamp Item (19) Retain

(b) For Section B-B, install :

Refer to Fig. A-FBGAA Sheet 01, Fig. A-FBGAA Sheet 02 and Fig. A-FBGAA

Sheet 03

6 Spacer NSA5527-03-08 Item 34

12 Clamp Item (19) Retained at

removal

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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6 Washer NSA935808-01 Item 20

6 Screw NAS1801-3-20 Item 81

(c) For Section D-D, install :

Refer to Fig. A-FBGAA Sheet 01, Fig. A-FBGAA Sheet 02 and Fig. A-FBGAA

Sheet 03

1 Spacer NSA5527-03-06 Item 84

2 Clamp Item (19) Retained at

removal

1 Washer NSA935808-01 Item 20

1 Screw NAS1801-3-12 Item 71

(7) Subtask 246103-831-011-001 - Install a support on the support of the BLUE

hydraulic reservoir at LH wing

Work Zones and Access Panels

Zone Access/Work location

571 Work location from Frame 47 to Frame 48

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 246103A01R14

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

20 NSA935808-01 1 WASHER

31 NAS1801-3-11 1 SCREW

67 A0041113300000 1 BRACKET

68 ASNA2050DXJ4828 2 RIVET

69 NSA935807-06 1 CLAMP

ASNA2528-3 2 NUT

EN6115V3-4 2 BOLT

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Primer Polyurethane Paint -

Corrosion Inhibiting

04EAC2

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Top Coat Polyurethane -

Grey Internal Structure

04JME4

Polysulfide Sealant -

General Purpose Interfay

06AAC1

Polysulfide Sealant-Fuel

Tank Fillet

06ABB1

Non Aqueous Cleaner -

General

08BAA9

Corrosion Preventive

Compound-Water

Displacing

12ADB1 As required

References

Fig. A-FBHAA

Installation of a Support on the Support

of the BLUE Hydraulic Reservoir (LH

wing)

Sheet 01

Sheet 02

(a) Remove :

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

2 Rivet Item (68) Discard

NOTE: Clean the area with :

Non Aqueous

Cleaner - General

08BAA9 As required

(b) Install the bracket Item 67.

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

1 Put the bracket Item 67 in position.

2 Drill two holes on the bracket Item 67 to a diameter comprised between 4.85

mm (0.191 in.) and 4.95 mm (0.195 in.) to match the holes of the structure.

3 Wet install :

1 Bracket A0041113300000 Item 67

2 Rivet ASNA2050DXJ4828 Item 68

NOTE: If the installation of bracket Item 67 with the rivets is not

possible, attach with:

2 Bolt EN6115V3-4

2 Nut ASNA2528-3

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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SERVICE BULLETIN

NOTE: Between the bracket Item 67 and the structure, apply :

Polysulfide SealantFuel Tank Fillet

06ABB1 As required

NOTE: Wet install the rivets with :

Polysulfide Sealant

- General Purpose

Interfay

06AAC1 As required

NOTE: Apply on the head of the rivets :

Primer

Polyurethane Paint

- Corrosion

Inhibiting

04EAC2 As required

Top Coat

Polyurethane - Grey

Internal Structure

04JME4 As required

Corrosion

Preventive

Compound-Water

Displacing

12ADB1 As required

NOTE: On the modified area, apply :

(c) Attach the conduit to the support with :

1 Clamp NSA935807-06 Item 69

1 Screw NAS1801-3-11 Item 31

1 Washer NSA935808-01 Item 20

(8) Subtask 246103-831-012-001 - Modify the routing of routes 1E and 1G in the

leading edge at LH wing

Work Zones and Access Panels

Zone Access/Work location

513

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills NON SPECIFIC

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 130

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Material necessary to do the job

Kit 246103A01R14

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

34 NSA5527-03-08 2 SPACER

39 A9222505750000 2 SPACER

66 NSA935401-13 2 TIE

References

Fig. A-FBJAA

Modification of the Routing in the

Leading Edge (LH and RH side)

Sheet 01

(a) Install :

Refer to Fig. A-FBJAA Sheet 01

2 Spacer-Feeder A9222505750000 Item 39

2 Spacer NSA5527-03-08 Item 34

2 Tie-Cable NSA935401-13 Item 66

(9) Subtask 246103-020-002-001 - Remove the clamps between FR50 and FR52 at RH

side

Work Zones and Access Panels

Zone Access/Work location

148 Work location from Frame 50 to Frame 52

from Stringer 32 to Stringer 33

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

References

Fig. A-FBFAA

Modification of the Routing Between

FR50 and FR51 at STGR 32 (LH and

RH side)

Sheet 01

Sheet 02

Fig. A-FBUAA

Modification of the Routing of the

Passage Way at FR52 (RH side)

Sheet 01

Sheet 02

(a) Depending on the stacking, remove :

Refer to Fig. A-FBFAA Sheet 01

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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SERVICE BULLETIN

4 Clamp Item (16) Discard

2 Clamp Item (32) Discard

2 Spacer Item (14) Discard

2 Clip nut Item (43) Discard

2 Washer Item (20) Discard

2 Screw Item (33) Discard

Or remove :

Refer to Fig. A-FBFAA Sheet 01

4 Clamp Item (16) Discard

2 Spacer Item (14) Discard

2 Clip nut Item (43) Discard

2 Washer Item (20) Discard

2 Screw Item (33) Discard

(b) Remove :

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

4 Clamp Item (72) Discard

2 Washer Item (73) Discard

2 Screw Item (74) Retain

1 Clamp Item (44) Discard

1 Clamp Item (45) Discard

2 Washer Item (46) Discard

2 Screw Item (47) Retain

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 132

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SERVICE BULLETIN

(10) Subtask 246103-831-005-001 - Modify the Routing between FR50 and FR52 and

between STGR 33 and 30 at RH side

Work Zones and Access Panels

Zone Access/Work location

148 Work location from Frame 50 to Frame 51

Stringer 32

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 246103A02R12

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

77 EN6049-007-19-5 7.5 (M) SLEEVE

78 EN6049-007-13-5 7.5 (M) SLEEVE

86 EN6049-007-08-5 7.5 (M) SLEEVE

References

Fig. A-FBWAA

Modification of the Routing between

FR50 and FR52 (LH and RH side)

Sheet 01

(a) Remove :

Refer to Fig. A-FBWAA Sheet 01

5 (M) Conduit Item (77) Discard

NOTE: A third conduit may be installed. If installed, remove it.

(b) Install :

Refer to Fig. A-FBWAA Sheet 01

5 (M) Sleeve EN6049-007-13-5 Item 78

or

5 (M) Sleeve EN6049-007-19-5 Item 77

or

5 (M) Sleeve-Protective EN6049-007-08-5 Item 86

NOTE: Install sleeve Item 77 or 78 or 86 according to the harness

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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SERVICE BULLETIN

diameter.

NOTE: If a third conduit was installed, install :

2.5 (M) Sleeve EN6049-007-13-5 Item 78

or

2.5 (M) Sleeve EN6049-007-19-5 Item 77

or

2.5 (M) Sleeve-Protective EN6049-007-08-5 Item 86

NOTE: Install the sleeve Item 77 or 78 or 86 according to the harness

diameter.

(11) Subtask 246103-420-002-001 - Install the clamps between FR50 and FR52 at RH

side

Work Zones and Access Panels

Zone Access/Work location

148 Work location from Frame 50 to Frame 52

from Stringer 32 to Stringer 33

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 246103A02R12

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

12 NSA5527-03-01 1 SPACER

14 NSA5527-03-02 2 SPACER

33 NAS1801-3-25 1 SCREW

43 NSA5067-3-1 2 NUT

46 NAS1149F0332P 6 WASHER

63 NSA5516-13ND 12 CLAMP

64 NSA5516-31ND 12 CLAMP

79 NAS1801-3-18 1 SCREW

References

Fig. A-FBFAA

Modification of the Routing Between

FR50 and FR51 at STGR 32 (LH and

RH side)

Sheet 01

Sheet 02

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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References

Fig. A-FBUAA

Modification of the Routing of the

Passage Way at FR52 (RH side)

Sheet 01

Sheet 02

(a) Depending on the stacking, install :

Refer to Fig. A-FBFAA Sheet 02 view C

3 Clamp NSA5516-13ND Item 63

or

3 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

1 Spacer NSA5527-03-01 Item 12

1 Spacer NSA5527-03-02 Item 14

1 Screw NAS1801-3-25 Item 33

1 Washer NAS1149F0332P Item 46

1 Clip nut NSA5067-3-1 Item 43

Or install :

Refer to Fig. A-FBFAA Sheet 02 view C

2 Clamp NSA5516-13ND Item 63

or

2 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

1 Spacer NSA5527-03-01 Item 12

1 Spacer NSA5527-03-02 Item 14

1 Screw NAS1801-3-25 Item 33

1 Washer NAS1149F0332P Item 46

1 Clip nut NSA5067-3-1 Item 43

(b) Depending on the stacking, install :

Refer to Fig. A-FBFAA Sheet 02 view D

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 135

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3 Clamp NSA5516-13ND Item 63

or

3 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

1 Spacer NSA5527-03-02 Item 14

1 Clip nut NSA5067-3-1 Item 43

1 Screw NAS1801-3-18 Item 79

1 Washer NAS1149F0332P Item 46

Or install :

Refer to Fig. A-FBFAA Sheet 02 view D

2 Clamp NSA5516-13ND Item 63

or

2 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

1 Spacer NSA5527-03-02 Item 14

1 Clip nut NSA5067-3-1 Item 43

1 Screw NAS1801-3-18 Item 79

1 Washer NAS1149F0332P Item 46

(c) Install :

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

6 Clamp NSA5516-13ND Item 63

or

6 Clamp NSA5516-31ND Item 64

NOTE: Install the clamp Item 63 or 64 according to the bundle diameter.

4 Washer NAS1149F0332P Item 46

2 Screw Item (47) Retained at

removal

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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SERVICE BULLETIN

2 Screw Item (74) Retained at

removal

(12) Subtask 246103-831-004-001 - Install a bracket on the shroud box blanking plate at

RH side

Work Zones and Access Panels

Zone Access/Work location

148 Work location Frame 51

from Stringer 31 to Stringer 33

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 246103A02R12

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

21 NSA5050-3 3 NUT

29 A0041113420100 1 BRACKET

30 NAS1801-3-8 2 SCREW

37 NAS1801-3-9 1 SCREW

46 NAS1149F0332P 2 WASHER

63 NSA5516-13ND 2 CLAMP

64 NSA5516-31ND 2 CLAMP

70 A0041113500000 1 CLAMP

71 NAS1801-3-12 2 SCREW

75 A0041113500200 1 CLAMP

76 A0041113500400 1 CLAMP

References

Fig. A-FBEAA

Installation of a Conduit on the Shroud

Box Bracket (LH and RH side)

Sheet 01

Sheet 02

Sheet 03

(a) Remove :

Refer to Fig. A-FBEAA Sheet 01

2 Screw Item (27) Discard

2 Washer Item (46) Discard

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 137

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(b) Install the bracket :

Refer to Fig. A-FBEAA Sheet 01, Fig. A-FBEAA Sheet 02 and Fig. A-FBEAA Sheet

03

1 Bracket A0041113420100 Item 29

2 Screw NAS1801-3-12 Item 71

2 Washer NAS1149F0332P Item 46

(c) Attach the bundles on the shroud box bracket :

Refer to Fig. A-FBEAA Sheet 01, Fig. A-FBEAA Sheet 02 and Fig. A-FBEAA Sheet

03

1 Attach the bundles with :

2 Clamp NSA5516-13ND Item 63

or

2 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

NOTE: Two or three bundles may be installed.

1 Nut NSA5050-3 Item 21

and

1 Screw NAS1801-3-9 Item 37

2 Or attach the bundles with :

1 Clamp NSA5516-13ND Item 63

or

1 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

NOTE: Two or three bundles may be installed.

and

1 Clamp A0041113500000 Item 70

or

1 Clamp A0041113500200 Item 75

or

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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1 Clamp A0041113500400 Item 76

NOTE: Install clamp Item 70 or 75 or 76 according to the bundle

diameters.

2 Nut NSA5050-3 Item 21

2 Screw NAS1801-3-8 Item 30

(13) Subtask 246103-831-007-001 - Modify the routing on rib 1 on the passage way to

the shroud box at RH side

Work Zones and Access Panels

Zone Access/Work location

670 Work location Rib 1

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 246103A01R14

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

12 NSA5527-03-01 4 SPACER

Kit 246103A02R12

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

12 NSA5527-03-01 2 SPACER

19 NSA935807-09 2 CLAMP

20 NSA935808-01 1 WASHER

21 NSA5050-3 1 NUT

22 NAS1801-3-24 1 SCREW

87 NSA360002 1 (M) EXTRUSIN

Kit 246103A04R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

24 NSA939510BN 1 (M) STRIP

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Epoxy Adhesive-Metal To

Metal - Legacy

05EJL9 As required

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 139

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ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Epoxy Adhesive - Legacy 3 05EML7 As required

Contact Adhesive-Rubber &

Plastic Bonding Neopren

05JBC9 As required

Non Aqueous Cleaner -

Isopropyl Alcohol

08BBD1 As required

References

Elec. Std. Practices Manual (ESPM) 20-33-11

Process and Material Specification

(PMS)

Process and Material Specification (PMS)

01-01-28 Process E

Fig. A-FBCAA

Removal of the Clamps on the Passage

Way to the Shroud Box (LH and RH

side)

Sheet 01

Sheet 02

Sheet 03

Fig. A-FBDAA

Installation of the Clamps on the

Passage Way to the Shroud Box (LH

and RH side)

Sheet 01

Sheet 02

Sheet 03

(a) Remove :

Refer to Fig. A-FBCAA Sheet 01, Fig. A-FBCAA Sheet 02 and Fig. A-FBCAA Sheet

03

2 Clamp Item (19) Discard

1 Spacer Item (12) Discard

1 Screw Item (22) Discard

1 Washer Item (20) Discard

1 Nut Item (21) Discard

(b) Install :

Refer to Fig. A-FBDAA Sheet 01, Fig. A-FBDAA Sheet 02 and Fig. A-FBDAA Sheet

03

2 Clamp NSA935807-09 Item 19

2 Spacer NSA5527-03-01 Item 12

1 Screw NAS1801-3-24 Item 22

1 Washer NSA935808-01 Item 20

1 Nut NSA5050-3 Item 21

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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(c) Refer to Fig. A-FBDAA Sheet 01 and Fig. A-FBDAA Sheet 03

1 (M) Extrusion NSA360002 Item 87

with:

Contact AdhesiveRubber & Plastic

Bonding Neopren

05JBC9 As required

(d) Measure the gap between the clamp and the structure, refer to Fig. A-FBCAA

Sheet 01 and Fig. A-FBCAA Sheet 02:

1 If the gap between the structure and the clamp is less than 6.35 mm (0.25 in.),

install, refer to Fig. A-FBDAA Sheet 02:

4 Spacer NSA5527-03-01 Item 12

2 If the gap between the structure and the clamp is more than 130 mm (5.118

in), contact AIRBUS, refer to Fig. A-FBCAA Sheet 02

NOTE: For operators that have the gap between the structure and the

clamp is more than 130 mm (5.118 in) contact Airbus at:

AIRBUS CUSTOMER SERVICES ENGINEERING - SEEA5

ELECTRICAL POWER GENERATION DISTRIBUTION &

LIGHTING SYSTEMS

1 ROND POINT MAURICE BELLONTE

31707 BLAGNAC CEDEX FRANCE

FAX +33 561 934 425

(e) Install a protection on the structure to protect the routes :

Refer to Fig. A-FBDAA Sheet 01, Fig. A-FBDAA Sheet 02 and Fig. A-FBDAA Sheet

03

Refer to ESPM 20-33-11

Refer to Process and Material Specification (PMS) 01-01-28 Process E

1 (M) Strip-Protective NSA939510BN Item 24

NOTE: Install the Strip-Protective Item 24 with:

Epoxy AdhesiveMetal To Metal -

Legacy

05EJL9 As required

NOTE: Do the abrading and cleaning of the contact zones of StripProtective Item 24, on the structure with:

Non Aqueous

Cleaner - Isopropyl

Alcohol

08BBD1 As required

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 141

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SERVICE BULLETIN

Epoxy Adhesive -

Legacy 3

05EML7 As required

(14) Subtask 246103-831-013-001 - Modify the routing of routes 2E and 2G in the

leading edge at RH wing

Work Zones and Access Panels

Zone Access/Work location

613

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills NON SPECIFIC

Material necessary to do the job

Kit 246103A02R12

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

34 NSA5527-03-08 2 SPACER

39 A9222505750000 2 SPACER

66 NSA935401-13 2 TIE

References

Fig. A-FBJAA

Modification of the Routing in the

Leading Edge (LH and RH side)

Sheet 01

(a) Install :

Refer to Fig. A-FBJAA Sheet 01

2 Spacer-Feeder A9222505750000 Item 39

2 Spacer NSA5527-03-08 Item 34

2 Tie-Cable NSA935401-13 Item 66

(15) Subtask 246103-020-003-002 - Remove the clamps from LH wing.

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 142

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SERVICE BULLETIN

References

Fig. A-FBLAA

Removal/Installation of the Clamps in LH

and RH Wings

Sheet 01

Sheet 02

Sheet 03

Sheet 04

(a) Remove the clamps from LH wing at Rib location WIAX-27.96.

Refer to Fig. A-FBLAA Sheet 01 and Fig. A-FBLAA Sheet 04 view G

1 Remove:

2 Clamps Item (51) Discard

1 Screw Item (37) Discard

1 Washer Item (46) Discard

(b) Remove the clamps from LH wing at Rib location WIAX-35.12.

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

1 Remove :

1 Screw Item (50) Discard

1 Washer Item (46) Discard

2 Clamp Item (51) Discard

1 Spacer Item (13) Discard

(c) Remove the clamps from LH wing at Rib location WIAX-40.53.

Refer to Fig. A-FBLAA Sheet 01 and Fig. A-FBLAA Sheet 03

1 Remove :

2 Screw Item (50) Discard

2 Washer Item (46) Discard

2 Clamp Item (51) Discard

2 Spacer Item (13) Discard

(d) Remove the clamps from LH wing at Rib location WIAX-48.25

Refer to Fig. A-FBLAA Sheet 01 and Fig. A-FBLAA Sheet 04 view J

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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1 Remove:

2 Clamp Item (51) Discard

1 Screw Item (37) Retain

1 Washer Item (46) Discard

(16) Subtask 246103-831-016-003 - Remove the clamps from RH wing.

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

References

Fig. A-FBLAA

Removal/Installation of the Clamps in LH

and RH Wings

Sheet 01

Sheet 02

Sheet 03

Sheet 04

(a) Remove the clamps from RH wing at Rib location WIAX-27.96.

Refer to Fig. A-FBLAA Sheet 01 and Fig. A-FBLAA Sheet 04 view G

1 Remove:

2 Clamps Item (51) Discard

1 Screw Item (37) Discard

1 Washer Item (46) Discard

(b) Remove the clamps from RH wing at Rib location WIAX-35.12.

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

1 Remove :

1 Screw Item (50) Discard

1 Washer Item (46) Discard

2 Clamp Item (51) Discard

1 Spacer Item (13) Discard

(c) Remove the clamps from RH wing at Rib location WIAX-40.53.

Refer to Fig. A-FBLAA Sheet 01 and Fig. A-FBLAA Sheet 03

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 144

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SERVICE BULLETIN

1 Remove :

2 Screw Item (50) Discard

2 Washer Item (46) Discard

2 Clamp Item (51) Discard

2 Spacer Item (13) Discard

(d) Remove the clamps from RH wing at Rib location WIAX-48.25.

Refer to Fig. A-FBLAA Sheet 01 and Fig. A-FBLAA Sheet 04 view J

1 Remove:

2 Clamp Item (51) Discard

1 Screw Item (37) Retain

1 Washer Item (46) Discard

(17) Subtask 246103-831-401-002 - Modify the Electrical Support Brackets in the Outer

Shroud Box, LH Wing

Work Zones and Access Panels

Zone Access/Work location

572

Manpower Resources

Manhours 1.50

Minimum number of person 2

Subtask elapsed time 0.75

Skills AIRFRAME

Material necessary to do the job

Kit 246103B02R02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 A9245005500000 1 BRACKET

2 MS20470AD4-10 2 RIVET

3 A9245005600000 1 BRACKET

8 DAN7-5-6 3 PIN

9 HL70-6 3 COLLAR

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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Consumable CMLB01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Primer Polyurethane Paint -

Corrosion Inhibiting

04EAC2 As required

Top Coat Polyurethane -

Grey Internal Structure

04JME4 As required

Polysulfide Sealant -

General Purpose Interfay

06AAC1 As required

Non Aqueous Cleaner -

General

08BAA9 As required

Textile - Lint Free Cotton 14SBA1 As required

References

Fig. A-UBAAA

Modification of the Support Brackets in

the Outer Shroud Box

Sheet 01

Sheet 02

Sheet 03

(a) Modify the LH Support Bracket Assembly at Rib Location WIAX-35.12

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

1 Carefully drill out and remove the items that follow:

2 Rivet Item (2) Discard

2 Remove from the structure the item that follows:

1 Bracket Assy-Cable

Support

A9244012400000 Item (1) Discard

3 Clean the area with a:

Textile - Lint Free

Cotton

14SBA1 As required

made moist with:

Non Aqueous

Cleaner - General

08BAA9 As required

4 Use:

Polysulfide Sealant

- General Purpose

Interfay

06AAC1 As required

and wet assemble to the structure the item that follows:

1 Bracket Assy-Cable

Support

A9245005500000 Item 1

with:

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 146

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SERVICE BULLETIN

2 Rivet MS20470AD4-10 Item 2

5 Apply

Primer

Polyurethane Paint

- Corrosion

Inhibiting

04EAC2 As required

and

Top Coat

Polyurethane - Grey

Internal Structure

04JME4 As required

to the heads and tails of the rivets.

(b) Modify the LH Support Bracket Assembly at Rib Location WIAX-40.53

Refer to Fig. A-UBAAA Sheet 01 and Fig. A-UBAAA Sheet 03

1 Carefully drill out and remove the items that follow:

3 Rivet Item (2) Discard

2 Remove from the structure the item that follows:

1 Angle-Attachment A5724091525800 Item (3) Discard

3 Clean the area with a:

Textile - Lint Free

Cotton

14SBA1 As required

made moist with:

Non Aqueous

Cleaner - General

08BAA9 As required

4 Use:

Polysulfide Sealant

- General Purpose

Interfay

06AAC1 As required

and wet assemble to the structure the item that follows:

1 Bracket Assy-Cable

Support

A9245005600000 Item 3

with:

3 Pin-Rivet DAN7-5-6 Item 8

3 Collar HL70-6 Item 9

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 147

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@A300-600

SERVICE BULLETIN

5 Apply

Primer

Polyurethane Paint

- Corrosion

Inhibiting

04EAC2 As required

and

Top Coat

Polyurethane - Grey

Internal Structure

04JME4 As required

to the heads and tails of the fasteners.

(18) Subtask 246103-831-008-001 - Modify the routing of routes 1P and 2P at LH wing

Work Zones and Access Panels

Zone Access/Work location

570 Work location from Rib 1 to Rib 6

Manpower Resources

Manhours 1.50

Minimum number of person 1

Subtask elapsed time 1.50

Skills NON SPECIFIC

Material necessary to do the job

Kit 246103A01R14

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

14 NSA5527-03-02 3 SPACER

26 NSA935401-04 12 TIE

66 NSA935401-13 3 TIE

86 EN6049-007-08-5 5 (M) SLEEVE

References

Fig. A-FBYAA

Modification of the Routing in LH and

RH Wings

Sheet 01

Sheet 02

(a) Between rib 5 and rib 6, install :

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

5 (M) Sleeve-Protective EN6049-007-08-5 Item 86

12 Tie-Cable NSA935401-04 Item 26

and

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 148

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SERVICE BULLETIN

3 Spacer NSA5527-03-02 Item 14

attached with :

3 Tie-Cable NSA935401-13 Item 66

(19) Subtask 246103-831-009-001 - Modify the routing of routes 1P and 2P at RH wing

Work Zones and Access Panels

Zone Access/Work location

670 Work location from Rib 1 to Rib 6

Manpower Resources

Manhours 1.50

Minimum number of person 1

Subtask elapsed time 1.50

Skills NON SPECIFIC

Material necessary to do the job

Kit 246103A02R12

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

14 NSA5527-03-02 3 SPACER

26 NSA935401-04 12 TIE

66 NSA935401-13 3 TIE

86 EN6049-007-08-5 5 (M) SLEEVE

References

Fig. A-FBYAA

Modification of the Routing in LH and

RH Wings

Sheet 01

Sheet 02

(a) Between rib 5 and rib 6, install :

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

5 (M) Sleeve-Protective EN6049-007-08-5 Item 86

12 Tie-Cable NSA935401-04 Item 26

and

3 Spacer NSA5527-03-02 Item 14

attached with :

3 Tie-Cable NSA935401-13 Item 66

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 149

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SERVICE BULLETIN

(20) Subtask 246103-831-017-003 - Install the clamps in LH wing.

Manpower Resources

Manhours 1.00

Minimum number of person 2

Subtask elapsed time 0.50

Skills NON SPECIFIC

Material necessary to do the job

Kit 246103A01R14

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

12 NSA5527-03-01 1 SPACER

13 NSA5527-03-03 1 SPACER

37 NAS1801-3-9 3 SCREW

46 NAS1149F0332P 6 WASHER

50 NAS1801-3-13 1 SCREW

52 NSA5516-08ND 8 CLAMP

55 NAS1801-3-16 1 SCREW

References

Fig. A-FBLAA

Removal/Installation of the Clamps in LH

and RH Wings

Sheet 01

Sheet 02

Sheet 03

Sheet 04

(a) Install the clamps in LH wing at Rib location WIAX-27.96.

Refer to Fig. A-FBLAA Sheet 01 and Fig. A-FBLAA Sheet 04 view H

1 Install:

2 Clamp NSA5516-08ND Item 52

1 Screw NAS1801-3-9 Item 37

1 Washer NAS1149F0332P Item 46

(b) Install the clamps in LH wing at Rib location WIAX-35.12.

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

1 Install :

1 Spacer NSA5527-03-01 Item 12

1 Spacer NSA5527-03-03 Item 13

2 Clamp NSA5516-08ND Item 52

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 150

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SERVICE BULLETIN

2 Washer NAS1149F0332P Item 46

1 Screw NAS1801-3-13 Item 50

1 Screw NAS1801-3-16 Item 55

(c) Install the clamps in LH wing at Rib location WIAX-40.53.

Refer to Fig. A-FBLAA Sheet 01 and Fig. A-FBLAA Sheet 03

1 Install :

2 Clamp NSA5516-08ND Item 52

2 Washer NAS1149F0332P Item 46

2 Screw NAS1801-3-9 Item 37

(d) Install the clamps at LH wing at Rib location WIAX-48.25.

Refer to Fig. A-FBLAA Sheet 01 and Fig. A-FBLAA Sheet 04 view K

1 Install:

1 Screw Item (37) Retained at

removal

1 Washer NAS1149F0332P Item 46

2 Clamp NSA5516-08ND Item 52

(21) Subtask 246103-831-018-003 - Install the clamps in RH wing.

Manpower Resources

Manhours 1.00

Minimum number of person 2

Subtask elapsed time 0.50

Skills NON SPECIFIC

Material necessary to do the job

Kit 246103A02R12

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

12 NSA5527-03-01 1 SPACER

13 NSA5527-03-03 1 SPACER

37 NAS1801-3-9 3 SCREW

46 NAS1149F0332P 6 WASHER

50 NAS1801-3-13 1 SCREW

52 NSA5516-08ND 8 CLAMP

55 NAS1801-3-16 1 SCREW

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 151

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SERVICE BULLETIN

References

Fig. A-FBLAA

Removal/Installation of the Clamps in LH

and RH Wings

Sheet 01

Sheet 02

Sheet 03

Sheet 04

(a) Install the clamps in RH wing at Rib location WIAX-27.96.

Refer to Fig. A-FBLAA Sheet 01 and Fig. A-FBLAA Sheet 04 view H

1 Install:

2 Clamp NSA5516-08ND Item 52

1 Screw NAS1801-3-9 Item 37

1 Washer NAS1149F0332P Item 46

(b) Install the clamps in RH wing at Rib location WIAX-35.12.

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

1 Install :

1 Spacer NSA5527-03-01 Item 12

1 Spacer NSA5527-03-03 Item 13

2 Clamp NSA5516-08ND Item 52

2 Washer NAS1149F0332P Item 46

1 Screw NAS1801-3-13 Item 50

1 Screw NAS1801-3-16 Item 55

(c) Install the clamps in RH wing at Rib location WIAX-40.53.

Refer to Fig. A-FBLAA Sheet 01 and Fig. A-FBLAA Sheet 03

2 Clamp NSA5516-08ND Item 52

2 Washer NAS1149F0332P Item 46

2 Screw NAS1801-3-9 Item 37

(d) Install the clamps at RH wing at Rib location WIAX-48.25.

Refer to Fig. A-FBLAA Sheet 01 and Fig. A-FBLAA Sheet 04 view K

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 152

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@A300-600

SERVICE BULLETIN

1 Install:

1 Screw Item (37) Retained at

removal

1 Washer NAS1149F0332P Item 46

2 Clamp NSA5516-08ND Item 52

(22) Subtask 246103-831-402-003 - Modify the P-CLIPS at Location WOFX-204.5, LH

Wing

Work Zones and Access Panels

Zone Access/Work location

512

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills ELECTRICAL

References

Fig. A-UACAA

Modification of the Aircraft Clipping

Sheet 01

Sheet 02

(a) Remove from the support bracket and the harness, Item (5), refer to Fig. A-UACAA

Sheet 01:

2 Bolt Item (6) Retain

2 P-clip Item (7) Retain

(b) Rotate the two P-clips 180 degrees.

(c) Install to the harness, Item (5) and the support brackets, refer to Fig. A-UACAA

Sheet 01:

2 Bolt Item (6) Retained at

removal

2 P-clip Item (7) Retained at

removal

(23) Subtask 246103-831-403-005 - Modify the Backshell of the Connector and the

Structure at Location ABX 36.5, LH Wing

Work Zones and Access Panels

Zone Access/Work location

575

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 153

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@A300-600

SERVICE BULLETIN

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills ELECTRICAL

References

Fig. A-UACAA

Modification of the Aircraft Clipping

Sheet 01

Sheet 02

CAUTION: DO NOT ROTATE THE BACKSHELL AT THIS WORKSTEP.

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

(a) Loosen the backshell locknut enough so that the backshell can be rotated.

CAUTION: DO NOT ROTATE THE BACKSHELL MORE THAN 45

DEGREES.

CAUTION: DO NOT STRESS THE WIRES INSIDE THE BACKSHELL.

(b) Gently rotate the backshell to get a 10mm (0.394in.) minimum clearance between

the electrical conduit and the support structure.

(c) Tighten the backshell.

(d) Check to make sure that there is a minimum clearance of 10.0mm (0.394in.)

between the electrical conduit and the support structure.

(24) Subtask 246103-831-405-002 - Modify the Electrical Support Brackets in the Outer

Shroud Box, RH Wing

Work Zones and Access Panels

Zone Access/Work location

672

Manpower Resources

Manhours 1.50

Minimum number of person 2

Subtask elapsed time 0.75

Skills AIRFRAME

Material necessary to do the job

Kit 246103B02R02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 A9245005500000 BRACKET

2 MS20470AD4-10 RIVET

3 A9245005600000 BRACKET

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 154

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SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

8 DAN7-5-6 PIN

9 HL70-6 COLLAR

Consumable CMLB01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Primer Polyurethane Paint -

Corrosion Inhibiting

04EAC2 As required

Top Coat Polyurethane -

Grey Internal Structure

04JME4 As required

Polysulfide Sealant -

General Purpose Interfay

06AAC1 As required

Non Aqueous Cleaner -

General

08BAA9 As required

Textile - Lint Free Cotton 14SBA1 As required

References

Fig. A-UBAAA

Modification of the Support Brackets in

the Outer Shroud Box

Sheet 01

Sheet 02

Sheet 03

(a) Modify the RH Support Bracket Assembly at Rib Location WIAX-35.12

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

1 Carefully drill out and remove the items that follow:

2 Rivet Item (2) Discard

2 Remove from the structure the item that follows:

1 Bracket Assy-Cable

Support

A9244012400000 Item (1) Discard

3 Clean the area with a:

Textile - Lint Free

Cotton

14SBA1 As required

made moist with:

Non Aqueous

Cleaner - General

08BAA9 As required

4 Use:

Polysulfide Sealant

- General Purpose

Interfay

06AAC1 As required

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 155

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SERVICE BULLETIN

and wet assemble to the structure the item that follows:

1 Bracket Assy-Cable

Support

A9245005500000 Item 1

with:

2 Rivet MS20470AD4-10 Item 2

5 Apply

Primer

Polyurethane Paint

- Corrosion

Inhibiting

04EAC2 As required

and

Top Coat

Polyurethane - Grey

Internal Structure

04JME4 As required

to the heads and tails of the rivets.

(b) Modify the RH Support Bracket Assembly at Rib Location WIAX-40.53

Refer to Fig. A-UBAAA Sheet 01 and Fig. A-UBAAA Sheet 03

1 Carefully drill out and remove the items that follow:

3 Rivet Item (2) Discard

2 Remove from the structure the item that follows:

1 Angle-Attachment A5724091525800 Item (3) Discard

3 Clean the area with a:

Textile - Lint Free

Cotton

14SBA1 As required

made moist with:

Non Aqueous

Cleaner - General

08BAA9 As required

4 Use:

Polysulfide Sealant

- General Purpose

Interfay

06AAC1 As required

and wet assemble to the structure the item that follows:

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 156

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@A300-600

SERVICE BULLETIN

1 Bracket Assy-Cable

Support

A9245005600000 Item 3

with:

3 Pin-Rivet DAN7-5-6 Item 8

3 Collar HL70-6 Item 9

5 Apply

Primer

Polyurethane Paint

- Corrosion

Inhibiting

04EAC2 As required

and

Top Coat

Polyurethane - Grey

Internal Structure

04JME4 As required

to the heads and tails of the fasteners.

(25) Subtask 246103-831-406-002 - Modify the P-CLIPS at Location WOFX-204.5, RH

Wing

Work Zones and Access Panels

Zone Access/Work location

612

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills ELECTRICAL

References

Fig. A-UACAA

Modification of the Aircraft Clipping

Sheet 01

Sheet 02

(a) Remove from the support bracket and the harness, Item (5), refer to Fig. A-UACAA

Sheet 01:

2 Bolt Item (6) Retain

2 P-clip Item (7) Retain

(b) Rotate the two P-clips 180 degrees.

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 157

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@A300-600

SERVICE BULLETIN

(c) Install to the harness, Item (5) and the support brackets, refer to Fig. A-UACAA

Sheet 01:

2 Bolt Item (6) Retained at

removal

2 P-clip Item (7) Retained at

removal

(26) Subtask 246103-831-407-002 - Modify the Backshell of the Connector and the

Structure at Location ABX 36.5, RH Wing

Work Zones and Access Panels

Zone Access/Work location

675

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills ELECTRICAL

References

Fig. A-UACAA

Modification of the Aircraft Clipping

Sheet 01

Sheet 02

CAUTION: DO NOT ROTATE THE BACKSHELL AT THIS WORKSTEP.

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

(a) Loosen the backshell locknut enough so that the backshell can be rotated.

CAUTION: DO NOT ROTATE THE BACKSHELL MORE THAN 45

DEGREES.

CAUTION: DO NOT STRESS THE WIRES INSIDE THE BACKSHELL.

(b) Gently rotate the backshell to get a 10mm (0.394in.) minimum clearance between

the electrical conduit and the support structure.

(c) Tighten the backshell.

(d) Check to make sure that there is a minimum clearance of 10.0mm (0.394in.)

between the electrical conduit and the support structure.

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 158

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SERVICE BULLETIN

**CONF 003

(1) Subtask 246103-831-001-001 - Remove the clamps between FR50 and FR52 at LH

side

Work Zones and Access Panels

Zone Access/Work location

147 Work location from Frame 50 to Frame 52

from Stringer 32 to Stringer 33

Manpower Resources

Manhours 1.50

Minimum number of person 1

Subtask elapsed time 1.50

Skills NON SPECIFIC

References

Fig. A-FBAAA

Removal of the Old Brackets of the

Passage Way at FR52 (LH side)

Sheet 01

Sheet 02

Sheet 03

Fig. A-FBFAA

Modification of the Routing Between

FR50 and FR51 at STGR 32 (LH and

RH side)

Sheet 01

Sheet 02

(a) On the panel, remove :

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

2 Screw Item (47) Discard

2 Washer Item (46) Discard

2 Clip nut Item (43) Discard

1 Clamp Item (44) Retain

1 Clamp Item (45) Retain

(b) On the bracket (if installed), remove :

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

1 Nut Item (48) Discard

1 Washer Item (49) Discard

1 Screw Item (10) Discard

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 159

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SERVICE BULLETIN

1 Clamp Item (11) Retain

(c) Remove :

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

2 Screw Item (47) Discard

2 Washer Item (46) Discard

1 Seal fitting Item (41) Discard

1 Bracket assy Item (42) Discard

(d) Remove :

Refer to Fig. A-FBAAA Sheet 01 and Fig. A-FBAAA Sheet 03

4 Clamp Item (72) Discard

2 Screw Item (74) Retain

2 Washer Item (73) Discard

1 Clamp Item (44) Discard

1 Clamp Item (45) Discard

2 Washer Item (46) Discard

2 Screw Item (47) Retain

(e) Depending on the stacking, remove :

Refer to Fig. A-FBFAA Sheet 01

4 Clamp Item (16) Discard

2 Clamp Item (32) Discard

2 Spacer Item (14) Discard

2 Clip nut Item (43) Discard

2 Washer Item (20) Discard

2 Screw Item (33) Discard

Or remove :

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 160

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SERVICE BULLETIN

Refer to Fig. A-FBFAA Sheet 01

4 Clamp Item (16) Discard

2 Spacer Item (14) Discard

2 Clip nut Item (43) Discard

2 Washer Item (20) Discard

2 Screw Item (33) Discard

(2) Subtask 246103-831-019-001 - Modify the Routing between FR50 and FR52 and

between STGR 33 and 30 at LH side

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 246103A01R14

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

77 EN6049-007-19-5 7.5 (M) SLEEVE

78 EN6049-007-13-5 7.5 (M) SLEEVE

86 EN6049-007-08-5 7.5 (M) SLEEVE

References

Fig. A-FBWAA

Modification of the Routing between

FR50 and FR52 (LH and RH side)

Sheet 01

(a) Remove :

Refer to Fig. A-FBWAA Sheet 01

5 (M) Conduit Item (77) Discard

NOTE: A third conduit may be installed. If installed, remove it.

(b) Install :

Refer to Fig. A-FBWAA Sheet 01

5 (M) Sleeve EN6049-007-13-5 Item 78

or

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 161

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SERVICE BULLETIN

5 (M) Sleeve EN6049-007-19-5 Item 77

or

5 (M) Sleeve-Protective EN6049-007-08-5 Item 86

NOTE: Install the sleeve Item 77 or 78 or 86 according to the harness

diameter.

NOTE: If a third conduit was installed, install :

2.5 (M) Sleeve EN6049-007-13-5 Item 78

or

2.5 (M) Sleeve EN6049-007-19-5 Item 77

or

2.5 (M) Sleeve-Protective EN6049-007-08-5 Item 86

NOTE: Install the sleeve Item 77 or 78 or 86 according to the harness

diameter.

(3) Subtask 246103-420-001-001 - Install the clamps between FR50 and FR52 at LH

side

Work Zones and Access Panels

Zone Access/Work location

147 Work location from Frame 50 to Frame 52

from Stringer 31 to Stringer 32

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 246103A01R14

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

10 NAS1801-3-17 1 SCREW

12 NSA5527-03-01 2 SPACER

14 NSA5527-03-02 2 SPACER

23 NSA935401-05 1 TIE

33 NAS1801-3-25 1 SCREW

38 ABS0731A01 1 SUPPORT

41 A0041095620000 1 SEAL

42 A0041095400000 1 BRACKET

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 162

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SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

43 NSA5067-3-1 4 NUT

46 NAS1149F0332P 11 WASHER

47 NAS1801-3-7 4 SCREW

48 MS21042-3 1 NUT

63 NSA5516-13ND 12 CLAMP

64 NSA5516-31ND 12 CLAMP

79 NAS1801-3-18 1 SCREW

References

Fig. A-FBFAA

Modification of the Routing Between

FR50 and FR51 at STGR 32 (LH and

RH side)

Sheet 01

Sheet 02

Fig. A-FBBAA

Installation of the New Brackets of the

Passage Way at FR52 (LH side)

Sheet 01

Sheet 02

(a) Depending on the staking, install :

Refer to Fig. A-FBFAA Sheet 01 and Fig. A-FBFAA Sheet 02 view C

3 Clamp NSA5516-13ND Item 63

or

3 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

1 Spacer NSA5527-03-01 Item 12

1 Spacer NSA5527-03-02 Item 14

1 Screw NAS1801-3-25 Item 33

1 Washer NAS1149F0332P Item 46

1 Clip nut NSA5067-3-1 Item 43

Or install :

Refer to Fig. A-FBFAA Sheet 01 and Fig. A-FBFAA Sheet 02 view C

2 Clamp NSA5516-13ND Item 63

or

2 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 163

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SERVICE BULLETIN

1 Spacer NSA5527-03-01 Item 12

1 Spacer NSA5527-03-02 Item 14

1 Screw NAS1801-3-25 Item 33

1 Washer NAS1149F0332P Item 46

1 Clip nut NSA5067-3-1 Item 43

(b) Depending on the stacking, install :

Refer to Fig. A-FBFAA Sheet 01 and Fig. A-FBFAA Sheet 02 view D

3 Clamp NSA5516-13ND Item 63

or

3 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

1 Spacer NSA5527-03-02 Item 14

1 Screw NAS1801-3-18 Item 79

1 Clip nut NSA5067-3-1 Item 43

1 Washer NAS1149F0332P Item 46

Or install :

Refer to Fig. A-FBFAA Sheet 01 and Fig. A-FBFAA Sheet 02 view D

2 Clamp NSA5516-13ND Item 63

or

2 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

1 Spacer NSA5527-03-02 Item 14

1 Screw NAS1801-3-18 Item 79

1 Washer NAS1149F0332P Item 46

1 Clip nut NSA5067-3-1 Item 43

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 164

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@A300-600

SERVICE BULLETIN

(c) Install :

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

1 Seal Fitting A0041095620000 Item 41

1 Bracket assy A0041095400000 Item 42

2 Screw NAS1801-3-7 Item 47

2 Washer NAS1149F0332P Item 46

(d) On the bracket (if installed), install :

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

1 Clamp Item (11) Retained at

removal

1 Spacer NSA5527-03-01 Item 12

1 Screw NAS1801-3-17 Item 10

1 Washer NAS1149F0332P Item 46

1 Nut MS21042-3 Item 48

(e) On the panel, install :

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

1 Clamp Item (44) Retained at

removal

1 Clamp Item (45) Retained at

removal

2 Screw NAS1801-3-7 Item 47

2 Washer NAS1149F0332P Item 46

2 Clip nut NSA5067-3-1 Item 43

(f) Install :

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

6 Clamp NSA5516-13ND Item 63

or

6 Clamp NSA5516-31ND Item 64

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SERVICE BULLETIN

NOTE: Install the clamp Item 63 or 64 according to the bundle diameter.

4 Washer NAS1149F0332P Item 46

2 Screw Item (47) Retained at

removal

2 Screw Item (74) Retained at

removal

(g) Between the routes, install :

Refer to Fig. A-FBBAA Sheet 01

1 Support-Cable ABS0731A01 Item 38

1 Tie-Cable NSA935401-05 Item 23

(4) Subtask 246103-831-003-001 - Install a bracket on the shroud box blanking plate at

LH side

Work Zones and Access Panels

Zone Access/Work location

147 Work location Frame 51

from Stringer 31 to Stringer 33

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 246103A01R14

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

21 NSA5050-3 3 NUT

28 A0041113420000 1 BRACKET

30 NAS1801-3-8 2 SCREW

37 NAS1801-3-9 1 SCREW

46 NAS1149F0332P 2 WASHER

63 NSA5516-13ND 2 CLAMP

64 NSA5516-31ND 2 CLAMP

70 A0041113500000 1 CLAMP

71 NAS1801-3-12 2 SCREW

75 A0041113500200 1 CLAMP

76 A0041113500400 1 CLAMP

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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References

Fig. A-FBEAA

Installation of a Conduit on the Shroud

Box Bracket (LH and RH side)

Sheet 01

Sheet 02

Sheet 03

(a) Remove :

Refer to Fig. A-FBEAA Sheet 01

2 Screw Item (27) Discard

2 Washer Item (46) Discard

(b) Install the bracket :

Refer to Fig. A-FBEAA Sheet 01, Fig. A-FBEAA Sheet 02 and Fig. A-FBEAA Sheet

03

1 Bracket A0041113420000 Item 28

attach with :

2 Screw NAS1801-3-12 Item 71

2 Washer NAS1149F0332P Item 46

(c) Attach the bundles on the shroud box bracket :

Refer to Fig. A-FBEAA Sheet 01, Fig. A-FBEAA Sheet 02 and Fig. A-FBEAA Sheet

03

1 Attach the bundles with :

2 Clamp NSA5516-13ND Item 63

or

2 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

NOTE: Two or three bundles may be installed.

1 Nut NSA5050-3 Item 21

and

1 Screw NAS1801-3-9 Item 37

2 Or attach the bundles with :

2 Clamp NSA5516-13ND Item 63

or

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SERVICE BULLETIN

2 Clamp NSA5516-31ND Item 64

and

1 Clamp A0041113500000 Item 70

or

1 Clamp A0041113500200 Item 75

or

1 Clamp A0041113500400 Item 76

NOTE: Install clamp Item 70 or 75 or 76 according to the bundle

diameters.

NOTE: Two or three bundles may be installed.

2 Nut NSA5050-3 Item 21

2 Screw NAS1801-3-8 Item 30

(5) Subtask 246103-831-006-002 - Modify the routing on rib 1 on the passage way to

the shroud box at LH side

Work Zones and Access Panels

Zone Access/Work location

570 Work location Rib 1

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 246103A01R14

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

12 NSA5527-03-01 2 SPACER

19 NSA935807-09 2 CLAMP

20 NSA935808-01 1 WASHER

21 NSA5050-3 1 NUT

22 NAS1801-3-24 1 SCREW

Kit 246103A04R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

12 NSA5527-03-01 1 SPACER

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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@A300-600

SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

13 NSA5527-03-03 1 SPACER

14 NSA5527-03-02 3 SPACER

21 NSA5050-3 4 NUT

23 NSA935401-05 2 TIE

24 NSA939510BN 1 (M) STRIP

26 NSA935401-04 2 TIE

33 NAS1801-3-25 1 SCREW

46 NAS1149F0332P 5 WASHER

51 NSA5516-12ND 15 CLAMP

52 NSA5516-08ND 15 CLAMP

62 NAS1801-3-22 1 SCREW

63 NSA5516-13ND 15 CLAMP

64 NSA5516-31ND 15 CLAMP

66 NSA935401-13 2 TIE

84 NSA5527-03-06 1 SPACER

87 NSA360002 1 (M) EXTRUSIN

91 NSA5527-03-15 2 SPACER

92 NSA5527-03-12 1 SPACER

94 NSA5159-35 1 STUD

95 NSA5527-03-18 1 SPACER

96 NSA5527-03-09 1 SPACER

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Epoxy Adhesive-Metal To

Metal - Legacy

05EJL9 As required

Epoxy Adhesive - Legacy 3 05EML7 As required

Contact Adhesive-Rubber &

Plastic Bonding Neopren

05JBC9 As required

Non Aqueous Cleaner -

Isopropyl Alcohol

08BBD1 As required

References

Elec. Std. Practices Manual (ESPM) 20-33-11

Process and Material Specification

(PMS)

Process and Material Specification (PMS)

01-01-28 Process E

Fig. A-FBCAB

Removal of the Clamps on the Passage

Way to the Shroud Box (LH and RH

side)

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Fig. A-FBDAB

Installation of the Clamps on the

Passage Way to the Shroud Box (LH

and RH side)

Sheet 01

Sheet 02

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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(a) Remove :

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

2 Clamp Item (19) Discard

1 Spacer Item (12) Discard

1 Screw Item (22) Discard

1 Washer Item (20) Discard

1 Nut Item (21) Discard

(b) Install :

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

2 Clamp NSA935807-09 Item 19

2 Spacer NSA5527-03-01 Item 12

1 Screw NAS1801-3-24 Item 22

1 Washer NSA935808-01 Item 20

1 Nut NSA5050-3 Item 21

(c) Install:

Refer to Fig. A-FBCAB Sheet 01 and Fig. A-FBCAB Sheet 03

1 (M) Extrusion NSA360002 Item 87

with:

Contact AdhesiveRubber & Plastic

Bonding Neopren

05JBC9 As required

(d) Install:

Refer to Fig. A-FBCAB Sheet 01 and Fig. A-FBCAB Sheet 03 view A-A

1 Stud NSA5159-35 Item 94

1 Nut NSA5050-3 Item 21

3 Clamp NSA5516-12ND Item 51

or

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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3 Clamp NSA5516-08ND Item 52

or

3 Clamp NSA5516-13ND Item 63

or

3 Clamp NSA5516-31ND Item 64

1 Spacer NSA5527-03-15 Item 91

1 Spacer NSA5527-03-12 Item 92

1 Spacer NSA5527-03-03 Item 13

1 Nut NSA5050-3 Item 21

2 Washer NAS1149F0332P Item 46

(e) Install:

Refer to Fig. A-FBCAB Sheet 01 and Fig. A-FBCAB Sheet 03 view B-B

1 Nut NSA5050-3 Item 21

2 Clamp NSA5516-08ND Item 52

or

2 Clamp NSA5516-12ND Item 51

or

2 Clamp NSA5516-13ND Item 63

or

2 Clamp NSA5516-31ND Item 64

2 Spacer NSA5527-03-02 Item 14

1 Washer NAS1149F0332P Item 46

(f) Install:

Refer to Fig. A-FBCAB Sheet 01 and Fig. A-FBCAB Sheet 04 view C-C

1 Nut NSA5050-3 Item 21

5 Clamp NSA5516-08ND Item 52

or

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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5 Clamp NSA5516-12ND Item 51

or

5 Clamp NSA5516-13ND Item 63

or

5 Clamp NSA5516-31ND Item 64

1 Spacer NSA5527-03-02 Item 14

1 Spacer NSA5527-03-15 Item 91

1 Spacer NSA5527-03-06 Item 84

(g) Install:

Refer to Fig. A-FBCAB Sheet 01 and Fig. A-FBCAB Sheet 04 view D-D

1 Screw NAS1801-3-22 Item 62

1 Washer NAS1149F0332P Item 46

3 Clamp NSA5516-08ND Item 52

or

3 Clamp NSA5516-12ND Item 51

or

3 Clamp NSA5516-13ND Item 63

or

3 Clamp NSA5516-31ND Item 64

1 Spacer NSA5527-03-09 Item 96

(h) Install:

Refer to Fig. A-FBCAB Sheet 01 and Fig. A-FBCAB Sheet 04 view E-E

1 Screw NAS1801-3-25 Item 33

1 Washer NAS1149F0332P Item 46

2 Clamp NSA5516-08ND Item 52

or

2 Clamp NSA5516-12ND Item 51

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or

2 Clamp NSA5516-13ND Item 63

or

2 Clamp NSA5516-31ND Item 64

1 Spacer NSA5527-03-18 Item 95

(i) Install:

Refer to Fig. A-FBCAB Sheet 01 and Fig. A-FBCAB Sheet 04 view F-F

2 Tie-Cable NSA935401-13 Item 66

or

2 Tie-Cable NSA935401-04 Item 26

or

2 Tie-Cable NSA935401-05 Item 23

1 Spacer NSA5527-03-01 Item 12

(j) Install a protection on the structure to protect the routes:

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

Refer to ESPM 20-33-11

Refer to Process and Material Specification (PMS) 01-01-28 Process E

1 (M) Strip-Protective NSA939510BN Item 24

NOTE: Install the Strip-Protective Item 24 with:

Epoxy AdhesiveMetal To Metal -

Legacy

05EJL9 As required

NOTE: Do the abrading and cleaning of the contact zones of StripProtective Item 24, on the structure with:

Non Aqueous

Cleaner - Isopropyl

Alcohol

08BBD1 As required

Epoxy Adhesive -

Legacy 3

05EML7 As required

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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SERVICE BULLETIN

(6) Subtask 246103-831-010-001 - Modify the routing of routes 1P and 2P in the

hydraulic shroud box at LH side

Work Zones and Access Panels

Zone Access/Work location

571

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 246103A01R14

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

20 NSA935808-01 7 WASHER

34 NSA5527-03-08 6 SPACER

71 NAS1801-3-12 1 SCREW

81 NAS1801-3-20 6 SCREW

84 NSA5527-03-06 1 SPACER

References

Fig. A-FBGAA

Modification of the Routing of Routes 1P

and 2P in the Shroud Box (LH side)

Sheet 01

Sheet 02

Sheet 03

(a) For Section A-A and C-C, remove :

Refer to Fig. A-FBGAA Sheet 01, Fig. A-FBGAA Sheet 02 and Fig. A-FBGAA

Sheet 03

7 Screw Item (22) Discard

7 Washer Item (20) Discard

14 Clamp Item (19) Retain

(b) For Section B-B, install :

Refer to Fig. A-FBGAA Sheet 01, Fig. A-FBGAA Sheet 02 and Fig. A-FBGAA

Sheet 03

6 Spacer NSA5527-03-08 Item 34

12 Clamp Item (19) Retained at

removal

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 174

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6 Washer NSA935808-01 Item 20

6 Screw NAS1801-3-20 Item 81

(c) For Section D-D, install :

Refer to Fig. A-FBGAA Sheet 01, Fig. A-FBGAA Sheet 02 and Fig. A-FBGAA

Sheet 03

1 Spacer NSA5527-03-06 Item 84

2 Clamp Item (19) Retained at

removal

1 Washer NSA935808-01 Item 20

1 Screw NAS1801-3-12 Item 71

(7) Subtask 246103-831-011-001 - Install a support on the support of the BLUE

hydraulic reservoir at LH wing

Work Zones and Access Panels

Zone Access/Work location

571 Work location from Frame 47 to Frame 48

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 246103A01R14

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

20 NSA935808-01 1 WASHER

31 NAS1801-3-11 1 SCREW

67 A0041113300000 1 BRACKET

68 ASNA2050DXJ4828 2 RIVET

69 NSA935807-06 1 CLAMP

ASNA2528-3 2 NUT

EN6115V3-4 2 BOLT

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Primer Polyurethane Paint -

Corrosion Inhibiting

04EAC2

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Top Coat Polyurethane -

Grey Internal Structure

04JME4

Polysulfide Sealant -

General Purpose Interfay

06AAC1

Polysulfide Sealant-Fuel

Tank Fillet

06ABB1

Non Aqueous Cleaner -

General

08BAA9

Corrosion Preventive

Compound-Water

Displacing

12ADB1 As required

References

Fig. A-FBHAA

Installation of a Support on the Support

of the BLUE Hydraulic Reservoir (LH

wing)

Sheet 01

Sheet 02

(a) Remove :

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

2 Rivet Item (68) Discard

NOTE: Clean the area with :

Non Aqueous

Cleaner - General

08BAA9 As required

(b) Install the bracket Item 67.

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

1 Put the bracket Item 67 in position.

2 Drill two holes on the bracket Item 67 to a diameter comprised between 4.85

mm (0.191 in.) and 4.95 mm (0.195 in.) to match the holes of the structure.

3 Wet install :

1 Bracket A0041113300000 Item 67

2 Rivet ASNA2050DXJ4828 Item 68

NOTE: If the installation of bracket Item 67 with the rivets is not

possible, attach with:

2 Bolt EN6115V3-4

2 Nut ASNA2528-3

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 176

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NOTE: Between the bracket Item 67 and the structure, apply :

Polysulfide SealantFuel Tank Fillet06ABB1 As required

NOTE: Wet install the rivets with :

Polysulfide Sealant

- General Purpose

Interfay

06AAC1 As required

NOTE: Apply on the head of the rivets :

Primer

Polyurethane Paint

- Corrosion

Inhibiting

04EAC2 As required

Top Coat

Polyurethane - Grey

Internal Structure

04JME4 As required

Corrosion

Preventive

Compound-Water

Displacing

12ADB1 As required

NOTE: On the modified area, apply :

(c) Attach the conduit to the support with :

1 Clamp NSA935807-06 Item 69

1 Screw NAS1801-3-11 Item 31

1 Washer NSA935808-01 Item 20

(8) Subtask 246103-831-012-001 - Modify the routing of routes 1E and 1G in the

leading edge at LH wing

Work Zones and Access Panels

Zone Access/Work location

513

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills NON SPECIFIC

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 177

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SERVICE BULLETIN

Material necessary to do the job

Kit 246103A01R14

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

34 NSA5527-03-08 2 SPACER

39 A9222505750000 2 SPACER

66 NSA935401-13 2 TIE

References

Fig. A-FBJAA

Modification of the Routing in the

Leading Edge (LH and RH side)

Sheet 01

(a) Install :

Refer to Fig. A-FBJAA Sheet 01

2 Spacer-Feeder A9222505750000 Item 39

2 Spacer NSA5527-03-08 Item 34

2 Tie-Cable NSA935401-13 Item 66

(9) Subtask 246103-020-002-001 - Remove the clamps between FR50 and FR52 at RH

side

Work Zones and Access Panels

Zone Access/Work location

148 Work location from Frame 50 to Frame 52

from Stringer 32 to Stringer 33

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

References

Fig. A-FBFAA

Modification of the Routing Between

FR50 and FR51 at STGR 32 (LH and

RH side)

Sheet 01

Sheet 02

Fig. A-FBUAA

Modification of the Routing of the

Passage Way at FR52 (RH side)

Sheet 01

Sheet 02

(a) Depending on the stacking, remove :

Refer to Fig. A-FBFAA Sheet 01

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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SERVICE BULLETIN

4 Clamp Item (16) Discard

2 Clamp Item (32) Discard

2 Spacer Item (14) Discard

2 Clip nut Item (43) Discard

2 Washer Item (20) Discard

2 Screw Item (33) Discard

Or remove :

Refer to Fig. A-FBFAA Sheet 01

4 Clamp Item (16) Discard

2 Spacer Item (14) Discard

2 Clip nut Item (43) Discard

2 Washer Item (20) Discard

2 Screw Item (33) Discard

(b) Remove :

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

4 Clamp Item (72) Discard

2 Washer Item (73) Discard

2 Screw Item (74) Retain

1 Clamp Item (44) Discard

1 Clamp Item (45) Discard

2 Washer Item (46) Discard

2 Screw Item (47) Retain

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 179

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SERVICE BULLETIN

(10) Subtask 246103-831-005-001 - Modify the Routing between FR50 and FR52 and

between STGR 33 and 30 at RH side

Work Zones and Access Panels

Zone Access/Work location

148 Work location from Frame 50 to Frame 51

Stringer 32

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 246103A02R12

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

77 EN6049-007-19-5 7.5 (M) SLEEVE

78 EN6049-007-13-5 7.5 (M) SLEEVE

86 EN6049-007-08-5 7.5 (M) SLEEVE

References

Fig. A-FBWAA

Modification of the Routing between

FR50 and FR52 (LH and RH side)

Sheet 01

(a) Remove :

Refer to Fig. A-FBWAA Sheet 01

5 (M) Conduit Item (77) Discard

NOTE: A third conduit may be installed. If installed, remove it.

(b) Install :

Refer to Fig. A-FBWAA Sheet 01

5 (M) Sleeve EN6049-007-13-5 Item 78

or

5 (M) Sleeve EN6049-007-19-5 Item 77

or

5 (M) Sleeve-Protective EN6049-007-08-5 Item 86

NOTE: Install sleeve Item 77 or 78 or 86 according to the harness

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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SERVICE BULLETIN

diameter.

NOTE: If a third conduit was installed, install :

2.5 (M) Sleeve EN6049-007-13-5 Item 78

or

2.5 (M) Sleeve EN6049-007-19-5 Item 77

or

2.5 (M) Sleeve-Protective EN6049-007-08-5 Item 86

NOTE: Install the sleeve Item 77 or 78 or 86 according to the harness

diameter.

(11) Subtask 246103-420-002-001 - Install the clamps between FR50 and FR52 at RH

side

Work Zones and Access Panels

Zone Access/Work location

148 Work location from Frame 50 to Frame 52

from Stringer 32 to Stringer 33

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 246103A02R12

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

12 NSA5527-03-01 1 SPACER

14 NSA5527-03-02 2 SPACER

33 NAS1801-3-25 1 SCREW

43 NSA5067-3-1 2 NUT

46 NAS1149F0332P 6 WASHER

63 NSA5516-13ND 12 CLAMP

64 NSA5516-31ND 12 CLAMP

79 NAS1801-3-18 1 SCREW

References

Fig. A-FBFAA

Modification of the Routing Between

FR50 and FR51 at STGR 32 (LH and

RH side)

Sheet 01

Sheet 02

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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References

Fig. A-FBUAA

Modification of the Routing of the

Passage Way at FR52 (RH side)

Sheet 01

Sheet 02

(a) Depending on the stacking, install :

Refer to Fig. A-FBFAA Sheet 02 view C

3 Clamp NSA5516-13ND Item 63

or

3 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

1 Spacer NSA5527-03-01 Item 12

1 Spacer NSA5527-03-02 Item 14

1 Screw NAS1801-3-25 Item 33

1 Washer NAS1149F0332P Item 46

1 Clip nut NSA5067-3-1 Item 43

Or install :

Refer to Fig. A-FBFAA Sheet 02 view C

2 Clamp NSA5516-13ND Item 63

or

2 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

1 Spacer NSA5527-03-01 Item 12

1 Spacer NSA5527-03-02 Item 14

1 Screw NAS1801-3-25 Item 33

1 Washer NAS1149F0332P Item 46

1 Clip nut NSA5067-3-1 Item 43

(b) Depending on the stacking, install :

Refer to Fig. A-FBFAA Sheet 02 view D

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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SERVICE BULLETIN

3 Clamp NSA5516-13ND Item 63

or

3 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

1 Spacer NSA5527-03-02 Item 14

1 Clip nut NSA5067-3-1 Item 43

1 Screw NAS1801-3-18 Item 79

1 Washer NAS1149F0332P Item 46

Or install :

Refer to Fig. A-FBFAA Sheet 02 view D

2 Clamp NSA5516-13ND Item 63

or

2 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

1 Spacer NSA5527-03-02 Item 14

1 Clip nut NSA5067-3-1 Item 43

1 Screw NAS1801-3-18 Item 79

1 Washer NAS1149F0332P Item 46

(c) Install :

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

6 Clamp NSA5516-13ND Item 63

or

6 Clamp NSA5516-31ND Item 64

NOTE: Install the clamp Item 63 or 64 according to the bundle diameter.

4 Washer NAS1149F0332P Item 46

2 Screw Item (47) Retained at

removal

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 183

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SERVICE BULLETIN

2 Screw Item (74) Retained at

removal

(12) Subtask 246103-831-004-001 - Install a bracket on the shroud box blanking plate at

RH side

Work Zones and Access Panels

Zone Access/Work location

148 Work location Frame 51

from Stringer 31 to Stringer 33

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 246103A02R12

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

21 NSA5050-3 3 NUT

29 A0041113420100 1 BRACKET

30 NAS1801-3-8 2 SCREW

37 NAS1801-3-9 1 SCREW

46 NAS1149F0332P 2 WASHER

63 NSA5516-13ND 2 CLAMP

64 NSA5516-31ND 2 CLAMP

70 A0041113500000 1 CLAMP

71 NAS1801-3-12 2 SCREW

75 A0041113500200 1 CLAMP

76 A0041113500400 1 CLAMP

References

Fig. A-FBEAA

Installation of a Conduit on the Shroud

Box Bracket (LH and RH side)

Sheet 01

Sheet 02

Sheet 03

(a) Remove :

Refer to Fig. A-FBEAA Sheet 01

2 Screw Item (27) Discard

2 Washer Item (46) Discard

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 184

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@A300-600

SERVICE BULLETIN

(b) Install the bracket :

Refer to Fig. A-FBEAA Sheet 01, Fig. A-FBEAA Sheet 02 and Fig. A-FBEAA Sheet

03

1 Bracket A0041113420100 Item 29

2 Screw NAS1801-3-12 Item 71

2 Washer NAS1149F0332P Item 46

(c) Attach the bundles on the shroud box bracket :

Refer to Fig. A-FBEAA Sheet 01, Fig. A-FBEAA Sheet 02 and Fig. A-FBEAA Sheet

03

1 Attach the bundles with :

2 Clamp NSA5516-13ND Item 63

or

2 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

NOTE: Two or three bundles may be installed.

1 Nut NSA5050-3 Item 21

and

1 Screw NAS1801-3-9 Item 37

2 Or attach the bundles with :

1 Clamp NSA5516-13ND Item 63

or

1 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

NOTE: Two or three bundles may be installed.

and

1 Clamp A0041113500000 Item 70

or

1 Clamp A0041113500200 Item 75

or

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 185

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@A300-600

SERVICE BULLETIN

1 Clamp A0041113500400 Item 76

NOTE: Install clamp Item 70 or 75 or 76 according to the bundle

diameters.

2 Nut NSA5050-3 Item 21

2 Screw NAS1801-3-8 Item 30

(13) Subtask 246103-831-007-002 - Modify the routing on rib 1 on the passage way to

the shroud box at RH side

Work Zones and Access Panels

Zone Access/Work location

670 Work location Rib 1

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 246103A02R12

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

12 NSA5527-03-01 2 SPACER

19 NSA935807-09 2 CLAMP

20 NSA935808-01 1 WASHER

21 NSA5050-3 1 NUT

22 NAS1801-3-24 1 SCREW

Kit 246103A04R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

24 NSA939510BN 1 (M) STRIP

Kit 246103A05R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

12 NSA5527-03-01 1 SPACER

13 NSA5527-03-03 1 SPACER

14 NSA5527-03-02 3 SPACER

21 NSA5050-3 4 NUT

23 NSA935401-05 2 TIE

26 NSA935401-04 2 TIE

33 NAS1801-3-25 1 SCREW

46 NAS1149F0332P 5 WASHER

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 186

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@A300-600

SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

51 NSA5516-12ND 15 CLAMP

52 NSA5516-08ND 15 CLAMP

62 NAS1801-3-22 1 SCREW

63 NSA5516-13ND 15 CLAMP

64 NSA5516-31ND 15 CLAMP

66 NSA935401-13 2 TIE

84 NSA5527-03-06 1 SPACER

87 NSA360002 1 (M) EXTRUSIN

91 NSA5527-03-15 2 SPACER

92 NSA5527-03-12 1 SPACER

94 NSA5159-35 1 STUD

95 NSA5527-03-18 1 SPACER

96 NSA5527-03-09 1 SPACER

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Epoxy Adhesive-Metal To

Metal - Legacy

05EJL9 As required

Epoxy Adhesive - Legacy 3 05EML7 As required

Contact Adhesive-Rubber &

Plastic Bonding Neopren

05JBC9 As required

Non Aqueous Cleaner -

Isopropyl Alcohol

08BBD1 As required

References

Elec. Std. Practices Manual (ESPM) 20-33-11

Process and Material Specification

(PMS)

Process and Material Specification (PMS)

01-01-28 Process E

Fig. A-FBCAB

Removal of the Clamps on the Passage

Way to the Shroud Box (LH and RH

side)

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Fig. A-FBDAB

Installation of the Clamps on the

Passage Way to the Shroud Box (LH

and RH side)

Sheet 01

Sheet 02

(a) Remove :

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

2 Clamp Item (19) Discard

1 Spacer Item (12) Discard

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 187

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@A300-600

SERVICE BULLETIN

1 Screw Item (22) Discard

1 Washer Item (20) Discard

1 Nut Item (21) Discard

(b) Install :

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

2 Clamp NSA935807-09 Item 19

2 Spacer NSA5527-03-01 Item 12

1 Screw NAS1801-3-24 Item 22

1 Washer NSA935808-01 Item 20

1 Nut NSA5050-3 Item 21

(c) Install:

Refer to Fig. A-FBCAB Sheet 01 and Fig. A-FBCAB Sheet 03

1 (M) Extrusion NSA360002 Item 87

with:

Contact AdhesiveRubber & Plastic

Bonding Neopren

05JBC9 As required

(d) Install:

Refer to Fig. A-FBCAB Sheet 01 and Fig. A-FBCAB Sheet 03 view A-A

1 Stud NSA5159-35 Item 94

1 Nut NSA5050-3 Item 21

3 Clamp NSA5516-12ND Item 51

or

3 Clamp NSA5516-08ND Item 52

or

3 Clamp NSA5516-13ND Item 63

or

3 Clamp NSA5516-31ND Item 64

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 188

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SERVICE BULLETIN

1 Spacer NSA5527-03-15 Item 91

1 Spacer NSA5527-03-12 Item 92

1 Spacer NSA5527-03-03 Item 13

1 Nut NSA5050-3 Item 21

2 Washer NAS1149F0332P Item 46

(e) Install:

Refer to Fig. A-FBCAB Sheet 01 and Fig. A-FBCAB Sheet 03 view B-B

1 Nut NSA5050-3 Item 21

2 Clamp NSA5516-08ND Item 52

or

2 Clamp NSA5516-12ND Item 51

or

2 Clamp NSA5516-13ND Item 63

or

2 Clamp NSA5516-31ND Item 64

2 Spacer NSA5527-03-02 Item 14

1 Washer NAS1149F0332P Item 46

(f) Install:

Refer to Fig. A-FBCAB Sheet 01 and Fig. A-FBCAB Sheet 04 view C-C

1 Nut NSA5050-3 Item 21

5 Clamp NSA5516-08ND Item 52

or

5 Clamp NSA5516-12ND Item 51

or

5 Clamp NSA5516-13ND Item 63

or

5 Clamp NSA5516-31ND Item 64

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 189

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@A300-600

SERVICE BULLETIN

1 Spacer NSA5527-03-02 Item 14

1 Spacer NSA5527-03-15 Item 91

1 Spacer NSA5527-03-06 Item 84

(g) Install:

Refer to Fig. A-FBCAB Sheet 01 and Fig. A-FBCAB Sheet 04 view D-D

1 Screw NAS1801-3-22 Item 62

1 Washer NAS1149F0332P Item 46

3 Clamp NSA5516-08ND Item 52

or

3 Clamp NSA5516-12ND Item 51

or

3 Clamp NSA5516-13ND Item 63

or

3 Clamp NSA5516-31ND Item 64

1 Spacer NSA5527-03-09 Item 96

(h) Install:

Refer to Fig. A-FBCAB Sheet 01 and Fig. A-FBCAB Sheet 04 view E-E

1 Screw NAS1801-3-25 Item 33

1 Washer NAS1149F0332P Item 46

2 Clamp NSA5516-08ND Item 52

or

2 Clamp NSA5516-12ND Item 51

or

2 Clamp NSA5516-13ND Item 63

or

2 Clamp NSA5516-31ND Item 64

1 Spacer NSA5527-03-18 Item 95

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 190

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@A300-600

SERVICE BULLETIN

(i) Install:

Refer to Fig. A-FBCAB Sheet 01 and Fig. A-FBCAB Sheet 04 view F-F

2 Tie-Cable NSA935401-13 Item 66

or

2 Tie-Cable NSA935401-04 Item 26

or

2 Tie-Cable NSA935401-05 Item 23

1 Spacer NSA5527-03-01 Item 12

(j) Install a protection on the structure to protect the routes:

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

Refer to ESPM 20-33-11

Refer to Process and Material Specification (PMS) 01-01-28 Process E

1 (M) Strip-Protective NSA939510BN Item 24

NOTE: Install the Strip-Protective Item 24 with:

Epoxy AdhesiveMetal To Metal -

Legacy

05EJL9 As required

NOTE: Do the abrading and cleaning of the contact zones of StripProtective Item 24, on the structure with:

Non Aqueous

Cleaner - Isopropyl

Alcohol

08BBD1 As required

Epoxy Adhesive -

Legacy 3

05EML7 As required

(14) Subtask 246103-831-013-001 - Modify the routing of routes 2E and 2G in the

leading edge at RH wing

Work Zones and Access Panels

Zone Access/Work location

613

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 191

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@A300-600

SERVICE BULLETIN

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills NON SPECIFIC

Material necessary to do the job

Kit 246103A02R12

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

34 NSA5527-03-08 2 SPACER

39 A9222505750000 2 SPACER

66 NSA935401-13 2 TIE

References

Fig. A-FBJAA

Modification of the Routing in the

Leading Edge (LH and RH side)

Sheet 01

(a) Install :

Refer to Fig. A-FBJAA Sheet 01

2 Spacer-Feeder A9222505750000 Item 39

2 Spacer NSA5527-03-08 Item 34

2 Tie-Cable NSA935401-13 Item 66

(15) Subtask 246103-020-003-001 - Remove the clamps from LH wing

Work Zones and Access Panels

Zone Access/Work location

572

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

References

Fig. A-FBKAA

Removal/Installation of the Clamps in LH

and RH Wings

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 192

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@A300-600

SERVICE BULLETIN

(a) Remove the clamps from LH wing at Rib location WIAX-27.96

Refer to Fig. A-FBKAA Sheet 01 and Fig. A-FBKAA Sheet 05 view J

1 Remove:

2 Clamps Item (51) Discard

1 Screw Item (37) Discard

1 Washer Item (46) Discard

(b) Remove the clamps from LH wing at Rib location WIAX-35.12.

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

1 Remove :

1 Screw Item (50) Discard

1 Washer Item (46) Discard

2 Clamp Item (51) Discard

1 Spacer Item (13) Discard

(c) Remove the clamps from LH wing at Rib location WIAX-40.53.

Refer to Fig. A-FBKAA Sheet 01 and Fig. A-FBKAA Sheet 03

1 Remove :

2 Screw Item (50) Discard

2 Washer Item (46) Discard

2 Clamp Item (51) Discard

2 Spacer Item (13) Discard

(d) Remove the clamps from LH wing at Rib location WIAX-48.25

Refer to Fig. A-FBKAA Sheet 01 and Fig. A-FBKAA Sheet 05 view L

1 Remove:

2 Clamp Item (51) Discard

1 Screw Item (37) Retain

1 Washer Item (46) Discard

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 193

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SERVICE BULLETIN

(e) Remove the clamps from LH wing at Rib location WIAX-74.08.

Refer to Fig. A-FBKAA Sheet 01 and Fig. A-FBKAA Sheet 04

1 Remove :

2 Screw Item (50) Discard

2 Washer Item (46) Discard

1 Clamp Item (51) Discard

1 Clamp Item (52) Discard

2 Clamp Item (53) Discard

1 Clamp Item (54) Discard

3 Spacer Item (13) Discard

(16) Subtask 246103-831-016-001 - Remove the clamps from RH wing

Work Zones and Access Panels

Zone Access/Work location

672

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

References

Fig. A-FBKAA

Removal/Installation of the Clamps in LH

and RH Wings

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

(a) Remove the clamps from RH wing at Rib location WIAX-27.96.

Refer to Fig. A-FBKAA Sheet 01 and Fig. A-FBKAA Sheet 05 view J

1 Remove:

2 Clamps Item (51) Discard

1 Screw Item (37) Discard

1 Washer Item (46) Discard

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 194

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@A300-600

SERVICE BULLETIN

(b) Remove the clamps from RH wing at Rib location WIAX-35.12.

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

1 Remove :

1 Screw Item (50) Discard

1 Washer Item (46) Discard

2 Clamp Item (51) Discard

1 Spacer Item (13) Discard

(c) Remove the clamps from RH wing at Rib location WIAX-40.53.

Refer to Fig. A-FBKAA Sheet 01 and Fig. A-FBKAA Sheet 03

1 Remove :

2 Screw Item (50) Discard

2 Washer Item (46) Discard

2 Clamp Item (51) Discard

2 Spacer Item (13) Discard

(d) Remove the clamps from RH wing at Rib location WIAX-48.25.

Refer to Fig. A-FBKAA Sheet 01 and Fig. A-FBKAA Sheet 05 view L

1 Remove:

2 Clamp Item (51) Discard

1 Screw Item (37) Retain

1 Washer Item (46) Discard

(e) Remove the clamps from RH wing at Rib location WIAX-74.08.

Refer to Fig. A-FBKAA Sheet 01 and Fig. A-FBKAA Sheet 04

1 Remove :

2 Screw Item (50) Discard

2 Washer Item (46) Discard

1 Clamp Item (51) Discard

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 195

5

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@A300-600

SERVICE BULLETIN

1 Clamp Item (52) Discard

2 Clamp Item (53) Discard

1 Clamp Item (54) Discard

3 Spacer Item (13) Discard

(17) Subtask 246103-831-401-001 - Modify the Electrical Support Brackets in the Outer

Shroud Box, LH Wing

Work Zones and Access Panels

Zone Access/Work location

572

Manpower Resources

Manhours 2.50

Minimum number of person 2

Subtask elapsed time 1.25

Skills AIRFRAME

Material necessary to do the job

Kit 246103B01R03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 A9245005500000 1 BRACKET

2 MS20470AD4-10 4 RIVET

3 A9245005600000 1 BRACKET

8 DAN7-5-6 3 PIN

9 HL70-6 3 COLLAR

Component COMPB01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

8 DAN7-5-6 3 PIN

9 HL70-6 3 COLLAR

Consumable CMLB01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Primer Polyurethane Paint -

Corrosion Inhibiting

04EAC2 As required

Top Coat Polyurethane -

Grey Internal Structure

04JME4 As required

Polysulfide Sealant -

General Purpose Interfay

06AAC1 As required

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 196

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@A300-600

SERVICE BULLETIN

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Non Aqueous Cleaner -

General

08BAA9 As required

Surface Pretreatment - Light

Alloys Chemical Conver

10ABC1 As required

Textile - Lint Free Cotton 14SBA1 As required

References

Fig. A-UAAAA

Modification of the Support Brackets in

the Outer Shroud Box

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Refer to Fig. A-UAAAA Sheet 01, Fig. A-UAAAA Sheet 02, Fig. A-UAAAA Sheet 03 and

Fig. A-UAAAA Sheet 04

(a) Modify the LH Support Bracket Assembly at Rib Location WIAX-35.12

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

1 Carefully drill out and remove the items that follow:

2 Rivet Item (2) Discard

2 Remove from the structure the item that follows:

1 Bracket Assy-Cable

Support

A9244012400000 Item (1) Discard

3 Clean the area with a:

Textile - Lint Free

Cotton

14SBA1 As required

made moist with:

Non Aqueous

Cleaner - General

08BAA9 As required

4 Use:

Polysulfide Sealant

- General Purpose

Interfay

06AAC1 As required

and wet assemble to the structure the item that follows:

1 Bracket Assy-Cable

Support

A9245005500000 Item 1

with:

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 197

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@A300-600

SERVICE BULLETIN

2 Rivet MS20470AD4-10 Item 2

5 Apply

Primer

Polyurethane Paint

- Corrosion

Inhibiting

04EAC2 As required

and

Top Coat

Polyurethane - Grey

Internal Structure

04JME4 As required

to the heads and tails of the rivets.

(b) Modify the LH Support Bracket Assembly at Rib Location WIAX-40.53

Refer to Fig. A-UAAAA Sheet 01 and Fig. A-UAAAA Sheet 03

1 Carefully drill out and remove the items that follow:

3 Rivet Item (2) Discard

2 Remove from the structure the item that follows:

1 Angle-Attachment A5724091525800 Item (3) Discard

3 Clean the area with a:

Textile - Lint Free

Cotton

14SBA1 As required

made moist with:

Non Aqueous

Cleaner - General

08BAA9 As required

4 Use:

Polysulfide Sealant

- General Purpose

Interfay

06AAC1 As required

and wet assemble to the structure the item that follows:

1 Bracket Assy-Cable

Support

A9245005600000 Item 3

with:

For operators with KITB01R03:

3 Pin-Rivet DAN7-5-6 Item 8

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 198

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@A300-600

SERVICE BULLETIN

3 Collar HL70-6 Item 9

For operators with KITB01R02, get this item from COMPB01:

3 Pin-Rivet DAN7-5-6 Item 8

3 Collar HL70-6 Item 9

5 Apply:

Primer

Polyurethane Paint

- Corrosion

Inhibiting

04EAC2 As required

and

Top Coat

Polyurethane - Grey

Internal Structure

04JME4 As required

to the heads and tails of the fasteners.

(c) Modify the LH Support Bracket Assembly at Rib Location WIAX-74.08

Refer to Fig. A-UAAAA Sheet 01 and Fig. A-UAAAA Sheet 04

1 Carefully drill out and remove the items that follow:

4 Rivet Item (2) Discard

2 Remove from the structure the item that follows:

2 Bracket Assy-Cable

Support

A9244012400000 Item (1) Discard

3 Clean the area with a:

Textile - Lint Free

Cotton

14SBA1 As required

made moist with:

Non Aqueous

Cleaner - General

08BAA9 As required

4 At the locations indicated, increase the two holes to 4.90mm (0.193in.), refer

to Fig. A-UAAAA Sheet 04.

5 Deburr the holes.

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 199

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SERVICE BULLETIN

6 Clean the area with a:

Textile - Lint Free

Cotton

14SBA1 As required

made moist with:

Non Aqueous

Cleaner - General

08BAA9 As required

7 Apply:

Surface

Pretreatment - Light

Alloys Chemical

Conver

10ABC1 As required

to the cut surfaces of the holes.

8 At the two top holes (which are not used for the new bracket installation) wet

install these items to plug the open holes:

2 Rivet MS20470AD4-10 Item 2

use

Polysulfide Sealant

- General Purpose

Interfay

06AAC1 As required

(18) Subtask 246103-831-008-001 - Modify the routing of routes 1P and 2P at LH wing

Work Zones and Access Panels

Zone Access/Work location

570 Work location from Rib 1 to Rib 6

Manpower Resources

Manhours 1.50

Minimum number of person 1

Subtask elapsed time 1.50

Skills NON SPECIFIC

Material necessary to do the job

Kit 246103A01R14

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

14 NSA5527-03-02 3 SPACER

26 NSA935401-04 12 TIE

66 NSA935401-13 3 TIE

86 EN6049-007-08-5 5 (M) SLEEVE

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 200

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SERVICE BULLETIN

References

Fig. A-FBYAA

Modification of the Routing in LH and

RH Wings

Sheet 01

Sheet 02

(a) Between rib 5 and rib 6, install :

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

5 (M) Sleeve-Protective EN6049-007-08-5 Item 86

12 Tie-Cable NSA935401-04 Item 26

and

3 Spacer NSA5527-03-02 Item 14

attached with :

3 Tie-Cable NSA935401-13 Item 66

(19) Subtask 246103-831-009-001 - Modify the routing of routes 1P and 2P at RH wing

Work Zones and Access Panels

Zone Access/Work location

670 Work location from Rib 1 to Rib 6

Manpower Resources

Manhours 1.50

Minimum number of person 1

Subtask elapsed time 1.50

Skills NON SPECIFIC

Material necessary to do the job

Kit 246103A02R12

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

14 NSA5527-03-02 3 SPACER

26 NSA935401-04 12 TIE

66 NSA935401-13 3 TIE

86 EN6049-007-08-5 5 (M) SLEEVE

References

Fig. A-FBYAA

Modification of the Routing in LH and

RH Wings

Sheet 01

Sheet 02

(a) Between rib 5 and rib 6, install :

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

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 201

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5 (M) Sleeve-Protective EN6049-007-08-5 Item 86

12 Tie-Cable NSA935401-04 Item 26

and

3 Spacer NSA5527-03-02 Item 14

attached with :

3 Tie-Cable NSA935401-13 Item 66

(20) Subtask 246103-831-017-001 - Install the clamps in LH wing

Work Zones and Access Panels

Zone Access/Work location

572

Manpower Resources

Manhours 1.00

Minimum number of person 2

Subtask elapsed time 0.50

Skills NON SPECIFIC

Material necessary to do the job

Kit 246103A01R14

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

12 NSA5527-03-01 1 SPACER

13 NSA5527-03-03 1 SPACER

37 NAS1801-3-9 3 SCREW

46 NAS1149F0332P 6 WASHER

50 NAS1801-3-13 1 SCREW

52 NSA5516-08ND 8 CLAMP

55 NAS1801-3-16 1 SCREW

85 ASNA51072503 1 (M) TAPE

86 EN6049-007-08-5 2.5 (M) SLEEVE

Kit 246103A03R04

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

21 NSA5050-3 2 NUT

22 NAS1801-3-24 2 SCREW

90 NAS1149D0316H 2 WASHER

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 202

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Kit 246103B01R03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

60 A9245000200000 1 GUIDE

References

Fig. A-FBKAA

Removal/Installation of the Clamps in LH

and RH Wings

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

(a) Install the clamps in LH wing at Rib location WIAX-27.96.

Refer to Fig. A-FBKAA Sheet 01 and Fig. A-FBKAA Sheet 05 view K

1 Install:

2 Clamp NSA5516-08ND Item 52

1 Screw NAS1801-3-9 Item 37

1 Washer NAS1149F0332P Item 46

(b) Install the clamps in LH wing at Rib location WIAX-35.12.

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

1 Install :

1 Spacer NSA5527-03-01 Item 12

1 Spacer NSA5527-03-03 Item 13

2 Clamp NSA5516-08ND Item 52

2 Washer NAS1149F0332P Item 46

1 Screw NAS1801-3-13 Item 50

1 Screw NAS1801-3-16 Item 55

(c) Install the clamps in LH wing at Rib location WIAX-40.53.

Refer to Fig. A-FBKAA Sheet 01 and Fig. A-FBKAA Sheet 03

1 Install :

2 Clamp NSA5516-08ND Item 52

2 Washer NAS1149F0332P Item 46

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 203

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2 Screw NAS1801-3-9 Item 37

(d) Install the clamps at LH wing at Rib location WIAX-48.25.

Refer to Fig. A-FBKAA Sheet 01 and Fig. A-FBKAA Sheet 05 view M

1 Install:

2 Clamp NSA5516-08ND Item 52

1 Washer NAS1149F0332P Item 46

1 Screw Item (37) Retained at

removal

(e) Install the guide in LH wing at Rib location WIAX-74.08.

Refer to Fig. A-FBKAA Sheet 01 and Fig. A-FBKAA Sheet 04

1 Install :

1 Guide Assy-Conduit A9245000200000 Item 60

2 Screw NAS1801-3-24 Item 22

2 Washer NAS1149D0316H Item 90

2 Nut NSA5050-3 Item 21

NOTE: If necessary, to make the diameters of the bundles match with

the diameter of the holes of the guide Item 60, use:

2.5 (M) Sleeve-Protective EN6049-007-08-5 Item 86

1 (M) Tape-Reinforced

Silicone

ASNA51072503 Item 85

(21) Subtask 246103-831-018-001 - Install the clamps in RH wing

Work Zones and Access Panels

Zone Access/Work location

672

Manpower Resources

Manhours 1.00

Minimum number of person 2

Subtask elapsed time 0.50

Skills NON SPECIFIC

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 204

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Material necessary to do the job

Kit 246103A01R14

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

85 ASNA51072503 1 (M) TAPE

Kit 246103A02R12

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

12 NSA5527-03-01 1 SPACER

13 NSA5527-03-03 1 SPACER

37 NAS1801-3-9 3 SCREW

46 NAS1149F0332P 6 WASHER

50 NAS1801-3-13 1 SCREW

52 NSA5516-08ND 8 CLAMP

55 NAS1801-3-16 1 SCREW

86 EN6049-007-08-5 2.5 (M) SLEEVE

Kit 246103A03R04

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

21 NSA5050-3 2 NUT

22 NAS1801-3-24 2 SCREW

90 NAS1149D0316H 2 WASHER

Kit 246103B01R03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

60 A9245000200000 1 GUIDE

References

Fig. A-FBKAA

Removal/Installation of the Clamps in LH

and RH Wings

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

(a) Install the clamps in RH wing at Rib location WIAX-27.96.

Refer to Fig. A-FBKAA Sheet 01 and Fig. A-FBKAA Sheet 05 view K

1 Install:

2 Clamp NSA5516-08ND Item 52

1 Washer NAS1149F0332P Item 46

1 Screw NAS1801-3-9 Item 37

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 205

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(b) Install the clamps in RH wing at Rib location WIAX-35.12.

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

1 Install :

1 Spacer NSA5527-03-01 Item 12

1 Spacer NSA5527-03-03 Item 13

2 Clamp NSA5516-08ND Item 52

2 Washer NAS1149F0332P Item 46

1 Screw NAS1801-3-13 Item 50

1 Screw NAS1801-3-16 Item 55

(c) Install the clamps in RH wing at Rib location WIAX-40.53.

Refer to Fig. A-FBKAA Sheet 01 and Fig. A-FBKAA Sheet 03

2 Clamp NSA5516-08ND Item 52

2 Washer NAS1149F0332P Item 46

2 Screw NAS1801-3-9 Item 37

(d) Install the clamps at RH wing at Rib location WIAX-48.25.

Refer to Fig. A-FBKAA Sheet 01 and Fig. A-FBKAA Sheet 05 view M

1 Install:

2 Clamp NSA5516-08ND Item 52

1 Washer NAS1149F0332P Item 46

1 Screw Item (37) Retained at

removal

(e) Install the guide in RH wing at Rib location WIAX-74.08.

Refer to Fig. A-FBKAA Sheet 01 and Fig. A-FBKAA Sheet 04

1 Install :

1 Guide Assy-Conduit A9245000200000 Item 60

2 Screw NAS1801-3-24 Item 22

2 Washer NAS1149D0316H Item 90

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 206

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2 Nut NSA5050-3 Item 21

NOTE: If necessary, to make the diameters of the bundles match with

the diameter of the holes of the guide Item 60, use:

2.5 (M) Sleeve-Protective EN6049-007-08-5 Item 86

1 (M) Tape-Reinforced

Silicone

ASNA51072503 Item 85

(22) Subtask 246103-831-402-001 - Modify the P-CLIPS at Location WOFX-204.5, LH

Wing

Work Zones and Access Panels

Zone Access/Work location

512

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills ELECTRICAL

References

Fig. A-UACAA

Modification of the Aircraft Clipping

Sheet 01

Sheet 02

(a) Remove from the support bracket and the harness, Item (5), refer to Fig. A-UACAA

Sheet 01:

2 Bolt Item (6) Retain

2 P-clip Item (7) Retain

(b) Rotate the two P-clips 180 degrees.

(c) Install to the harness, Item (5) and the support brackets, refer to Fig. A-UACAA

Sheet 01:

2 Bolt Item (6) Retained at

removal

2 P-clip Item (7) Retained at

removal

(23) Subtask 246103-831-403-001 - Modify the Backshell of the Connector and the

Structure at Location ABX 36.5, LH Wing

Work Zones and Access Panels

Zone Access/Work location

575

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 207

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Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills ELECTRICAL

References

Fig. A-UACAA

Modification of the Aircraft Clipping

Sheet 01

Sheet 02

CAUTION: DO NOT ROTATE THE BACKSHELL AT THIS WORKSTEP.

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

(a) Loosen the backshell locknut enough so that the backshell can be rotated.

CAUTION: DO NOT ROTATE THE BACKSHELL MORE THAN 45

DEGREES.

CAUTION: DO NOT STRESS THE WIRING INSIDE THE BACKSHELL.

(b) Gently rotate the backshell to get a 10mm (0.394in.) minimum clearance between

the electrical conduit and the support structure.

(c) Tighten the backshell.

(d) Check to make sure that there is a minimum clearance of 10mm (0.394in.) between

the electrical conduit and the support structure.

(24) Subtask 246103-831-405-001 - Modify the Electrical Support Brackets in the Outer

Shroud Box, RH Wing

Work Zones and Access Panels

Zone Access/Work location

672

Manpower Resources

Manhours 2.50

Minimum number of person 2

Subtask elapsed time 1.25

Skills AIRFRAME

Material necessary to do the job

Kit 246103B01R03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 A9245005500000 BRACKET

2 MS20470AD4-10 RIVET

3 A9245005600000 BRACKET

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 208

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ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

8 DAN7-5-6 PIN

9 HL70-6 COLLAR

Component COMPB01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

8 DAN7-5-6 PIN

9 HL70-6 COLLAR

Consumable CMLB01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Primer Polyurethane Paint -

Corrosion Inhibiting

04EAC2 As required

Top Coat Polyurethane -

Grey Internal Structure

04JME4 As required

Polysulfide Sealant -

General Purpose Interfay

06AAC1 As required

Non Aqueous Cleaner -

General

08BAA9 As required

Surface Pretreatment - Light

Alloys Chemical Conver

10ABC1 As required

Textile - Lint Free Cotton 14SBA1 As required

References

Fig. A-UAAAA

Modification of the Support Brackets in

the Outer Shroud Box

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Refer to Fig. A-UAAAA Sheet 01, Fig. A-UAAAA Sheet 02, Fig. A-UAAAA Sheet 03 and

Fig. A-UAAAA Sheet 04

(a) Modify the RH Support Bracket Assembly at Rib Location WIAX-35.12

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

1 Carefully drill out and remove the items that follow:

2 Rivet Item (2) Discard

2 Remove from the structure the item that follows:

1 Bracket Assy-Cable

Support

A9244012400000 Item (1) Discard

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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3 Clean the area with a:

Textile - Lint Free

Cotton

14SBA1 As required

made moist with:

Non Aqueous

Cleaner - General

08BAA9 As required

4 Use:

Polysulfide Sealant

- General Purpose

Interfay

06AAC1 As required

and wet assemble to the structure the item that follows:

1 Bracket Assy-Cable

Support

A9245005500000 Item 1

with:

2 Rivet MS20470AD4-10 Item 2

5 Apply

Primer

Polyurethane Paint

- Corrosion

Inhibiting

04EAC2 As required

and

Top Coat

Polyurethane - Grey

Internal Structure

04JME4 As required

to the heads and tails of the rivets.

(b) Modify the RH Support Bracket Assembly at Rib Location WIAX-40.53

Refer to Fig. A-UAAAA Sheet 01 and Fig. A-UAAAA Sheet 03

1 Carefully drill out and remove the items that follow:

3 Rivet Item (2) Discard

2 Remove from the structure the item that follows:

1 Angle-Attachment A5724091525800 Item (3) Discard

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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3 Clean the area with a:

Textile - Lint Free

Cotton

14SBA1 As required

made moist with:

Non Aqueous

Cleaner - General

08BAA9 As required

4 Use:

Polysulfide Sealant

- General Purpose

Interfay

06AAC1 As required

and wet assemble to the structure the item that follows:

1 Bracket Assy-Cable

Support

A9245005600000 Item 3

with:

For operators with KITB01R03:

3 Pin-Rivet DAN7-5-6 Item 8

3 Collar HL70-6 Item 9

For operators with KITB01R02, get this item from COMPB01:

3 Pin-Rivet DAN7-5-6 Item 8

3 Collar HL70-6 Item 9

5 Apply:

Primer

Polyurethane Paint

- Corrosion

Inhibiting

04EAC2 As required

and

Top Coat

Polyurethane - Grey

Internal Structure

04JME4 As required

to the heads and tails of the fasteners.

(c) Modify the RH Support Bracket Assembly at Rib Location WIAX-74.08

Refer to Fig. A-UAAAA Sheet 01 and Fig. A-UAAAA Sheet 04

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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1 Carefully drill out and remove the items that follow:

4 Rivet Item (2) Discard

2 Remove from the structure the item that follows:

2 Bracket Assy-Cable

Support

A9244012400000 Item (1) Discard

3 Clean the area with a:

Textile - Lint Free

Cotton

14SBA1 As required

made moist with:

Non Aqueous

Cleaner - General

08BAA9 As required

4 At the locations indicated, increase the two holes to 4.90mm (0.193in.), refer

to Fig. A-UAAAA Sheet 04.

5 Deburr the holes.

6 Clean the area with a:

Textile - Lint Free

Cotton

14SBA1 As required

made moist with:

Non Aqueous

Cleaner - General

08BAA9 As required

7 Apply:

Surface

Pretreatment - Light

Alloys Chemical

Conver

10ABC1 As required

to the cut surfaces of the holes.

8 At the two top holes (which are not used for the new bracket installation) wet

install these items to plug the open holes:

2 Rivet MS20470AD4-10 Item 2

use

Polysulfide Sealant

- General Purpose

Interfay

06AAC1 As required

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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(25) Subtask 246103-831-406-001 - Modify the P-CLIPS at Location WOFX-204.5, RH

Wing

Work Zones and Access Panels

Zone Access/Work location

612

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills ELECTRICAL

References

Fig. A-UACAA

Modification of the Aircraft Clipping

Sheet 01

Sheet 02

(a) Remove from the support bracket and the harness, Item (5), refer to Fig. A-UACAA

Sheet 01:

2 Bolt Item (6) Retain

2 P-clip Item (7) Retain

(b) Rotate the two P-clips 180 degrees.

(c) Install to the harness, Item (5) and the support brackets, refer to Fig. A-UACAA

Sheet 01:

2 Bolt Item (6) Retained at

removal

2 P-clip Item (7) Retained at

removal

(26) Subtask 246103-831-407-001 - Modify the Backshell of the Connector and the

Structure at Location ABX 36.5, RH Wing

Work Zones and Access Panels

Zone Access/Work location

675

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills ELECTRICAL

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 213

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References

Fig. A-UACAA

Modification of the Aircraft Clipping

Sheet 01

Sheet 02

CAUTION: DO NOT ROTATE THE BACKSHELL AT THIS WORKSTEP.

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

(a) Loosen the backshell locknut enough so that the backshell can be rotated.

CAUTION: DO NOT ROTATE THE BACKSHELL MORE THAN 45

DEGREES.

CAUTION: DO NOT STRESS THE WIRING INSIDE THE BACKSHELL.

(b) Gently rotate the backshell to get a 10mm (0.394in.) minimum clearance between

the electrical conduit and the support structure.

(c) Tighten the backshell.

(d) Check to make sure that there is a minimum clearance of 10mm (0.394in.) between

the electrical conduit and the support structure.

**CONF ALL

D. TEST

**CONF 001

(1) Subtask 246103-700-001-001 - Tests

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 27-54-41, Page Block 401

29-12-46, Page Block 401

(a) Job set-up

1 Remove the safety clips and tags and close the circuit breakers as specified

after the installation of the inner flap deflectors (Refer to AMM 27-54-41, Page

Block 401).

2 Remove the safety clips and tags and close the circuit breakers as specified

after the installation of the BLUE hydraulic reservoir (Refer to AMM 29-12-46,

Page Block 401).

(b) Procedure

1 Do the test procedure as specified after the installation of the inner flap

deflectors (Refer to AMM 27-54-41, Page Block 401).

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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2 Do the test procedure as specified after the installation of the BLUE hydraulic

reservoir (Refer to AMM 29-12-46, Page Block 401).

**CONF 002

(1) Subtask 246103-700-001-001 - Tests

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 27-54-41, Page Block 401

29-12-46, Page Block 401

(a) Job set-up

1 Remove the safety clips and tags and close the circuit breakers as specified

after the installation of the inner flap deflectors (Refer to AMM 27-54-41, Page

Block 401).

2 Remove the safety clips and tags and close the circuit breakers as specified

after the installation of the BLUE hydraulic reservoir (Refer to AMM 29-12-46,

Page Block 401).

(b) Procedure

1 Do the test procedure as specified after the installation of the inner flap

deflectors (Refer to AMM 27-54-41, Page Block 401).

2 Do the test procedure as specified after the installation of the BLUE hydraulic

reservoir (Refer to AMM 29-12-46, Page Block 401).

**CONF 003

(1) Subtask 246103-700-001-001 - Tests

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 27-54-41, Page Block 401

29-12-46, Page Block 401

(a) Job set-up

1 Remove the safety clips and tags and close the circuit breakers as specified

after the installation of the inner flap deflectors (Refer to AMM 27-54-41, Page

Block 401).

2 Remove the safety clips and tags and close the circuit breakers as specified

after the installation of the BLUE hydraulic reservoir (Refer to AMM 29-12-46,

Page Block 401).

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 215

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(b) Procedure

1 Do the test procedure as specified after the installation of the inner flap

deflectors (Refer to AMM 27-54-41, Page Block 401).

2 Do the test procedure as specified after the installation of the BLUE hydraulic

reservoir (Refer to AMM 29-12-46, Page Block 401).

**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 246103-942-001-001 - Close-up

Work Zones and Access Panels

Zone Access/Work location

From 513

To 613

From 570

To 670

571

From 572

To 672

From 147

To 148

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001

27-54-41, Page Block 401

32-12-11, Page Block 301

53-15-63, Page Block 401

(a) Close the inner deflectors between Rib. 1 and Rib. 6, refer to AMM 27-54-41, Page

Block 401.

(b) Install the access panels 571BB, 571DB, refer to AMM 06-41-57, Page Block 001.

(c) Install the access panels 512AB(612AB), 512BB(612BB), 512CB(612CB),

512DB(612DB), refer to AMM 06-41-57, Page Block 001.

(d) Close the Main Landing Gear (MLG) doors, refer to AMM 32-12-11, Page Block

301.

(e) Remove the access platform(s).

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

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 216

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SERVICE BULLETIN

(2) Subtask 246103-942-401-001 - Close-up

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) 24-00-00, Page Block 201

27-50-00, Page Block 301

29-10-00, Page Block 301

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

equipment.

(b) Close the hinged access doors 581DB(681DB) and install the access panels

582AT(682AT) and 512CB(612CB).

(c) Remove the access platforms.

(d) Remove the warning notices from the cockpit.

(e) Close these circuit breakers:

PANEL DESIGNATION FIN LOCATION SEE

NOTES

133VU FLT CTL/FLAPS/SYS

1/26VAC

1CV 335/R61

133VU FLT CTL/FLAPS/SYS

2/26VAC

2CV 334/S62

133VU SLATS/26VAC/SYS 1 3CV 335/R65

133VU SLATS/26VAC/SYS 2 4CV 335/R64

133VU FLT CTL/SFCC/NORM

SUPPLY/FLAPS/SYS 1

5CV 332/U61

133VU FLT CTL/SFCC/NORM

SUPPLY/FLAPS/SYS 2

6CV 331/V61

133VU SFCC/NORM

SUPPLY/SLATS/SYS 1

7VC 333/T63

133VU SFCC/NORM

SUPPLY/SLATS/SYS 2

8CV 333/T64

(f) Fully retract the flaps, refer to AMM 27-50-00, Page Block 301.

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

**CONF 002

(1) Subtask 246103-942-001-001 - Close-up

Work Zones and Access Panels

Zone Access/Work location

From 513

To 613

From 570

To 670

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 217

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SERVICE BULLETIN

571

From 572

To 672

From 147

To 148

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001

27-54-41, Page Block 401

32-12-11, Page Block 301

53-15-63, Page Block 401

(a) Close the inner deflectors between Rib. 1 and Rib. 6, refer to AMM 27-54-41, Page

Block 401.

(b) Install the access panels 571BB, 571DB, refer to AMM 06-41-57, Page Block 001.

(c) Install the access panels 512AB(612AB), 512BB(612BB), 512CB(612CB),

512DB(612DB), refer to AMM 06-41-57, Page Block 001.

(d) Close the Main Landing Gear (MLG) doors, refer to AMM 32-12-11, Page Block

301.

(e) Remove the access platform(s).

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

(2) Subtask 246103-942-401-001 - Close-up

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) 24-00-00, Page Block 201

27-50-00, Page Block 301

29-10-00, Page Block 301

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

equipment.

(b) Close the hinged access doors 581DB(681DB) and install the access panels

582AT(682AT) and 512CB(612CB).

(c) Remove the access platforms.

(d) Remove the warning notices from the cockpit.

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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(e) Close these circuit breakers:

PANEL DESIGNATION FIN LOCATION SEE

NOTES

133VU FLT CTL/FLAPS/SYS

1/26VAC

1CV 335/R61

133VU FLT CTL/FLAPS/SYS

2/26VAC

2CV 334/S62

133VU SLATS/26VAC/SYS 1 3CV 335/R65

133VU SLATS/26VAC/SYS 2 4CV 335/R64

133VU FLT CTL/SFCC/NORM

SUPPLY/FLAPS/SYS 1

5CV 332/U61

133VU FLT CTL/SFCC/NORM

SUPPLY/FLAPS/SYS 2

6CV 331/V61

133VU SFCC/NORM

SUPPLY/SLATS/SYS 1

7VC 333/T63

133VU SFCC/NORM

SUPPLY/SLATS/SYS 2

8CV 333/T64

(f) Fully retract the flaps, refer to AMM 27-50-00, Page Block 301.

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

**CONF 003

(1) Subtask 246103-942-001-001 - Close-up

Work Zones and Access Panels

Zone Access/Work location

From 513

To 613

From 570

To 670

571

From 572

To 672

From 147

To 148

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001

27-54-41, Page Block 401

32-12-11, Page Block 301

53-15-63, Page Block 401

(a) Close the inner deflectors between Rib. 1 and Rib. 6, refer to AMM 27-54-41, Page

Block 401.

(b) Install the access panels 571BB, 571DB, refer to AMM 06-41-57, Page Block 001.

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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@A300-600

SERVICE BULLETIN

(c) Install the access panels 512AB(612AB), 512BB(612BB), 512CB(612CB),

512DB(612DB), refer to AMM 06-41-57, Page Block 001.

(d) Close the Main Landing Gear (MLG) doors, refer to AMM 32-12-11, Page Block

301.

(e) Remove the access platform(s).

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

(2) Subtask 246103-942-401-001 - Close-up

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) 24-00-00, Page Block 201

27-50-00, Page Block 301

29-10-00, Page Block 301

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

equipment.

(b) Close the hinged access doors 581DB(681DB) and install the access panels

582AT(682AT) and 512CB(612CB).

(c) Remove the access platforms.

(d) Remove the warning notices from the cockpit.

(e) Close these circuit breakers:

PANEL DESIGNATION FIN LOCATION SEE

NOTES

133VU FLT CTL/FLAPS/SYS

1/26VAC

1CV 335/R61

133VU FLT CTL/FLAPS/SYS

2/26VAC

2CV 334/S62

133VU SLATS/26VAC/SYS 1 3CV 335/R65

133VU SLATS/26VAC/SYS 2 4CV 335/R64

133VU FLT CTL/SFCC/NORM

SUPPLY/FLAPS/SYS 1

5CV 332/U61

133VU FLT CTL/SFCC/NORM

SUPPLY/FLAPS/SYS 2

6CV 331/V61

133VU SFCC/NORM

SUPPLY/SLATS/SYS 1

7VC 333/T63

133VU SFCC/NORM

SUPPLY/SLATS/SYS 2

8CV 333/T64

(f) Fully retract the flaps, refer to AMM 27-50-00, Page Block 301.

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

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 220

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@A300-600

SERVICE BULLETIN

Task 246103-831-802-001 - Modification - ADDITIONAL WORK between Revision No. 00 and

Revision No. 03

**CONF ALL

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

INCLUDED IN THE REFERENCED PROCEDURES.

CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP

ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY

AND MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENANCE

WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING,

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

THIS:

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

NECESSARY ON WIRING AND COMPONENTS.

- REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND

OTHER CONTAMINATION.

THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION

AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION.

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

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

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

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

authority he belongs to, the accepted alternative procedure can be used. When the

words "in accordance with" are used then the given procedure must be followed.

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

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

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

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

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

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

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

NOTE: This Service Bulletin is classified mandatory or expected to be classified mandatory

by an Airworthiness Directive (AD). The paragraphs 3.C. and 3.D. in these

accomplishment instructions are Required for Compliance (RC) and must be done

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

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

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

the aircraft can be put back into a serviceable condition.

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 221

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@A300-600

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Task Associated Data

**CONF 001

Zone

147 148 513 570 571 613 670

Manpower

TOTAL MANHOURS 24.50

ELAPSED TIME (HOURS) 16.50

**CONF 002

Zone

147 148 513 570 571 613 670

Manpower

TOTAL MANHOURS 24.50

ELAPSED TIME (HOURS) 16.50

**CONF 003

Zone

147 148 513 570 571 613 670

Manpower

TOTAL MANHOURS 24.50

ELAPSED TIME (HOURS) 16.50

**CONF ALL

A. GENERAL

**CONF 001

(1) Subtask 246103-839-002-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

(2) Subtask 246103-910-002-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

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

06-31-53, Page Block 001

20-21-12, Page Block 001

51-23-10

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 222

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@A300-600

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References

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-25-51

20-33-00

20-33-30

20-33-42

20-33-44

20-33-45

Standards Manual (SM)

Structural Repair Manual (SRM) 51-21-00

51-40-00

51-40-20

51-40-30

51-40-40

51-40-50

51-75-10

51-75-10

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

the Consumable Materials List (CML).

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

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

(d) For the identification of the access panels, refer to AMM 06-21-00, Page Block 001.

(e) Tag all the parts you must remove and retain to make the subsequent installation

easier.

(f) Put all the retained hardware in identified plastic bags and attach the bags to the

related unit.

(g) Obtain fastener hole diameters and drill data in accordance with SRM 51-40-40.

(h) For the installation of the protective electrical conduits, refer to ESPM 20-33-30.

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

Block 001.

(j) Obtain alternative and substitute fastener data in accordance with SRM 51-40-30.

(k) If alternative and substitute fasteners have to be used, you must make sure that the

associated nut/collar are compatible in accordance with SRM 51-40-00 "Mating

Part" column.

(l) If the length of any fastener specified in this Service Bulletin does not meet

installation standards given in SRM Chapter 51, then a fastener of the same

specification, or an approved substitute, with a length which meets the installation

standards given in SRM Chapter 51 may be used. In addition, washers may be

installed for fastener grip length in accordance with SRM Chapter 51.

(m) Remove and install fasteners in accordance with SRM 51-40-20.

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 223

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(n) For the cable tie application and tooling, refer to ESPM 20-33-44 and ESPM

20-25-51.

(o) Adapt the clamp size as necessary, refer to ESPM 20-33-42.

(p) For repair of paint coatings, refer to SRM 51-75-10 and AMM 51-23-10.

(q) For the application of protective treatments, refer to SRM 51-21-00.

(r) For the general installation of electrical wire harnesses, refer to ESPM 20-33-00.

(s) For backshell, end piece and conduit fitting, refer to ESPM 20-33-45.

(t) Renew the protective finish in accordance with SRM 51-75-10.

**CONF 002

(1) Subtask 246103-839-002-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

(2) Subtask 246103-910-002-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

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

06-31-53, Page Block 001

20-21-12, Page Block 001

51-23-10

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-25-51

20-33-00

20-33-30

20-33-42

20-33-44

20-33-45

Standards Manual (SM)

Structural Repair Manual (SRM) 51-21-00

51-40-00

51-40-20

51-40-30

51-40-40

51-40-50

51-75-10

51-75-10

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 224

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

the Consumable Materials List (CML).

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

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

(d) For the identification of the access panels, refer to AMM 06-21-00, Page Block 001.

(e) Tag all the parts you must remove and retain to make the subsequent installation

easier.

(f) Put all the retained hardware in identified plastic bags and attach the bags to the

related unit.

(g) Obtain fastener hole diameters and drill data in accordance with SRM 51-40-40.

(h) For the installation of the protective electrical conduits, refer to ESPM 20-33-30.

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

Block 001.

(j) Obtain alternative and substitute fastener data in accordance with SRM 51-40-30.

(k) If alternative and substitute fasteners have to be used, you must make sure that the

associated nut/collar are compatible in accordance with SRM 51-40-00 "Mating

Part" column.

(l) If the length of any fastener specified in this Service Bulletin does not meet

installation standards given in SRM Chapter 51, then a fastener of the same

specification, or an approved substitute, with a length which meets the installation

standards given in SRM Chapter 51 may be used. In addition, washers may be

installed for fastener grip length in accordance with SRM Chapter 51.

(m) Remove and install fasteners in accordance with SRM 51-40-20.

(n) For the cable tie application and tooling, refer to ESPM 20-33-44 and ESPM

20-25-51.

(o) Adapt the clamp size as necessary, refer to ESPM 20-33-42.

(p) For repair of paint coatings, refer to SRM 51-75-10 and AMM 51-23-10.

(q) For the application of protective treatments, refer to SRM 51-21-00.

(r) For the general installation of electrical wire harnesses, refer to ESPM 20-33-00.

(s) For backshell, end piece and conduit fitting, refer to ESPM 20-33-45.

(t) Renew the protective finish in accordance with SRM 51-75-10.

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 225

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SERVICE BULLETIN

**CONF 003

(1) Subtask 246103-839-002-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

(2) Subtask 246103-910-002-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

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

06-31-53, Page Block 001

20-21-12, Page Block 001

51-23-10

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-25-51

20-33-00

20-33-30

20-33-42

20-33-44

20-33-45

Standards Manual (SM)

Structural Repair Manual (SRM) 51-21-00

51-40-00

51-40-20

51-40-30

51-40-40

51-40-50

51-75-10

51-75-10

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

the Consumable Materials List (CML).

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

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

(d) For the identification of the access panels, refer to AMM 06-21-00, Page Block 001.

(e) Tag all the parts you must remove and retain to make the subsequent installation

easier.

(f) Put all the retained hardware in identified plastic bags and attach the bags to the

related unit.

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 226

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@A300-600

SERVICE BULLETIN

(g) Obtain fastener hole diameters and drill data in accordance with SRM 51-40-40.

(h) For the installation of the protective electrical conduits, refer to ESPM 20-33-30.

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

Block 001.

(j) Obtain alternative and substitute fastener data in accordance with SRM 51-40-30.

(k) If alternative and substitute fasteners have to be used, you must make sure that the

associated nut/collar are compatible in accordance with SRM 51-40-00 "Mating

Part" column.

(l) If the length of any fastener specified in this Service Bulletin does not meet

installation standards given in SRM Chapter 51, then a fastener of the same

specification, or an approved substitute, with a length which meets the installation

standards given in SRM Chapter 51 may be used. In addition, washers may be

installed for fastener grip length in accordance with SRM Chapter 51.

(m) Remove and install fasteners in accordance with SRM 51-40-20.

(n) For the cable tie application and tooling, refer to ESPM 20-33-44 and ESPM

20-25-51.

(o) Adapt the clamp size as necessary, refer to ESPM 20-33-42.

(p) For repair of paint coatings, refer to SRM 51-75-10 and AMM 51-23-10.

(q) For the application of protective treatments, refer to SRM 51-21-00.

(r) For the general installation of electrical wire harnesses, refer to ESPM 20-33-00.

(s) For backshell, end piece and conduit fitting, refer to ESPM 20-33-45.

(t) Renew the protective finish in accordance with SRM 51-75-10.

**CONF ALL

B. PREPARATION

**CONF 001

(1) Subtask 246103-941-002-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 227

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@A300-600

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References

Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001

24-00-00, Page Block 301

27-50-00, Page Block 301

27-54-41, Page Block 401

32-12-11, Page Block 301

53-15-63, Page Block 401

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 24-00-00, Page

Block 301.

(b) Put an access platform in position at Zone(s) 513(613), 570(670), 571 , 572(672)

and 147(148).

(c) Open the Main Landing Gear (MLG) doors, refer to AMM 32-12-11, Page Block

301.

(d) Remove the access panels 512BB and 612BB, refer to AMM 06-41-57, Page Block

001.

(e) Remove the access panels 513AT, 513BT, 571BB, 571CB, 571DB, 613AT and

613BT, refer to AMM 06-41-57, Page Block 001.

(f) If necessary, extend the flaps, refer to AMM 27-50-00, Page Block 301.

(g) If necessary, remove the fairing panels 577AB, 577BB, 577DT, 577ET, 577FT,

677AB, 677BB, 677DT, 677ET and 677FT, refer to AMM 53-15-63, Page Block

401.

(h) Remove all the necessary inner deflectors between Rib. 1 and Rib. 6, refer to AMM

27-54-41, Page Block 401.

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 228

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**CONF 002

(1) Subtask 246103-941-002-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001

24-00-00, Page Block 301

27-50-00, Page Block 301

27-54-41, Page Block 401

32-12-11, Page Block 301

53-15-63, Page Block 401

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 24-00-00, Page

Block 301.

(b) Put an access platform in position at Zone(s) 513(613), 570(670), 571 , 572(672)

and 147(148).

(c) Open the Main Landing Gear (MLG) doors, refer to AMM 32-12-11, Page Block

301.

(d) Remove the access panels 512BB and 612BB, refer to AMM 06-41-57, Page Block

001.

(e) Remove the access panels 513AT, 513BT, 571BB, 571CB, 571DB, 613AT and

613BT, refer to AMM 06-41-57, Page Block 001.

(f) If necessary, extend the flaps, refer to AMM 27-50-00, Page Block 301.

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 229

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(g) If necessary, remove the fairing panels 577AB, 577BB, 577DT, 577ET, 577FT,

677AB, 677BB, 677DT, 677ET and 677FT, refer to AMM 53-15-63, Page Block

401.

(h) Remove all the necessary inner deflectors between Rib. 1 and Rib. 6, refer to AMM

27-54-41, Page Block 401.

**CONF 003

(1) Subtask 246103-941-002-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001

24-00-00, Page Block 301

27-50-00, Page Block 301

27-54-41, Page Block 401

32-12-11, Page Block 301

53-15-63, Page Block 401

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 24-00-00, Page

Block 301.

(b) Put an access platform in position at Zone(s) 513(613), 570(670), 571 , 572(672)

and 147(148).

(c) Open the Main Landing Gear (MLG) doors, refer to AMM 32-12-11, Page Block

301.

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 230

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(d) Remove the access panels 512BB and 612BB, refer to AMM 06-41-57, Page Block

001.

(e) Remove the access panels 513AT, 513BT, 571BB, 571CB, 571DB, 613AT and

613BT, refer to AMM 06-41-57, Page Block 001.

(f) If necessary, extend the flaps, refer to AMM 27-50-00, Page Block 301.

(g) If necessary, remove the fairing panels 577AB, 577BB, 577DT, 577ET, 577FT,

677AB, 677BB, 677DT, 677ET and 677FT, refer to AMM 53-15-63, Page Block

401.

(h) Remove all the necessary inner deflectors between Rib. 1 and Rib. 6, refer to AMM

27-54-41, Page Block 401.

**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 246103-831-028-001 - Modify the routing on rib 1 on the passage way to

the shroud box at LH side, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

570 Work location Rib 1

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 246103A01R14

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

87 NSA360002 1 (M) EXTRUSIN

Supplementary kit 246103A01S03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

12 NSA5527-03-01 4 SPACER

24 NSA939510BN 1 (M) STRIP

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 231

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Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Epoxy Adhesive-Metal To

Metal - Legacy

05EJL9 As required

Epoxy Adhesive - Legacy 3 05EML7 As required

Contact Adhesive-Rubber &

Plastic Bonding Neopren

05JBC9 As required

Non Aqueous Cleaner -

Isopropyl Alcohol

08BBD1 As required

References

Process and Material Specification

(PMS)

Process and Material Specification (PMS)

01-01-28 Process E

Fig. A-FBMAA

Modification of the Clamps on the

Passage Way to the Shroud Box (LH

and RH side) - ADDITIONAL WORK

Sheet 01

Sheet 02

Sheet 03

Sheet 04

(a) Install:

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

1 (M) Extrusion NSA360002 Item 87

with:

Contact AdhesiveRubber & Plastic

Bonding Neopren

05JBC9 As required

(b) Measure the gap between the clamp and the structure, refer to Fig. A-FBMAA

Sheet 01 and Fig. A-FBMAA Sheet 02:

1 If the gap between the structure and the clamp is less than 6.35 mm (0.25 in.),

install, refer to Fig. A-FBMAA Sheet 03 :

4 Spacer NSA5527-03-01 Item 12

2 If the gap between the structure and the clamp is more than 130 mm (5.118

in), contact AIRBUS, refer to Fig. A-FBMAA Sheet 02

NOTE: For operators that have the gap between the structure and the

clamp is more than 130 mm (5.118 in) contact Airbus at:

AIRBUS CUSTOMER SERVICES ENGINEERING - SEEA5

ELECTRICAL POWER GENERATION DISTRIBUTION &

LIGHTING SYSTEMS

1 ROND POINT MAURICE BELLONTE

31707 BLAGNAC CEDEX FRANCE

FAX +33 561 934 425

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 232

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

(c) Modify the grommet installation :

Refer to Fig. A-FBMAA Sheet 01, Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03

and Fig. A-FBMAA Sheet 04

1 Remove :

1 (M) Strip-Protective Item (24) Discard

2 Install :

Refer to Process and Material Specification (PMS) 01-01-28 Process E

1 (M) Strip-Protective NSA939510BN Item 24

NOTE: Install the Strip-Protective Item 24 with:

Epoxy AdhesiveMetal To Metal -

Legacy

05EJL9 As required

NOTE: Do the abrading and cleaning of the contact zones of StripProtective Item 24, on the structure with:

Non Aqueous

Cleaner - Isopropyl

Alcohol

08BBD1 As required

Epoxy Adhesive -

Legacy 3

05EML7 As required

(2) Subtask 246103-831-020-001 - Modify the routing on rib 1 on the passage way to

the shroud box at RH side, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

670 Work location Rib 1

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 246103A02R12

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

87 NSA360002 1 (M) EXTRUSIN

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 233

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

Supplementary kit 246103A02S03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

12 NSA5527-03-01 4 SPACER

24 NSA939510BN 1 (M) STRIP

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Epoxy Adhesive-Metal To

Metal - Legacy

05EJL9 As required

Epoxy Adhesive - Legacy 3 05EML7 As required

Contact Adhesive-Rubber &

Plastic Bonding Neopren

05JBC9 As required

Non Aqueous Cleaner -

Isopropyl Alcohol

08BBD1 As required

References

Process and Material Specification

(PMS)

Process and Material Specification (PMS)

01-01-28 Process E

Fig. A-FBMAA

Modification of the Clamps on the

Passage Way to the Shroud Box (LH

and RH side) - ADDITIONAL WORK

Sheet 01

Sheet 02

Sheet 03

Sheet 04

(a) Install:

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

1 (M) Extrusion NSA360002 Item 87

with:

Contact AdhesiveRubber & Plastic

Bonding Neopren

05JBC9 As required

(b) Measure the gap between the clamp and the structure, refer to Fig. A-FBMAA

Sheet 01 and Fig. A-FBMAA Sheet 02:

1 If the gap between the structure and the clamp is less than 6.35 mm (0.25 in.),

install, refer to Fig. A-FBMAA Sheet 03:

4 Spacer NSA5527-03-01 Item 12

2 If the gap between the structure and the clamp is more than 130 mm (5.118

in), contact AIRBUS, refer to Fig. A-FBMAA Sheet 02

NOTE: For operators that have the gap between the structure and the

clamp is more than 130 mm (5.118 in) contact Airbus at:

AIRBUS CUSTOMER SERVICES ENGINEERING - SEEA5

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 234

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

ELECTRICAL POWER GENERATION DISTRIBUTION &

LIGHTING SYSTEMS

1 ROND POINT MAURICE BELLONTE

31707 BLAGNAC CEDEX FRANCE

FAX +33 561 934 425

(c) Modify the grommet installation :

Refer to Fig. A-FBMAA Sheet 01, Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03

and Fig. A-FBMAA Sheet 04

1 Remove :

1 (M) Strip-Protective Item (24) Discard

2 Install :

Refer to Process and Material Specification (PMS) 01-01-28 Process E

1 (M) Strip-Protective NSA939510BN Item 24

NOTE: Install the Strip-Protective Item 24 with:

Epoxy AdhesiveMetal To Metal -

Legacy

05EJL9 As required

NOTE: Do the abrading and cleaning of the contact zones of StripProtective Item 24, on the structure with:

Non Aqueous

Cleaner - Isopropyl

Alcohol

08BBD1 As required

Epoxy Adhesive -

Legacy 3

05EML7 As required

(3) Subtask 246103-831-021-001 - Modify the routing of routes 1P and 2P in the

shroud box at LH side, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

571

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 235

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

Material necessary to do the job

Supplementary kit 246103A01S03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

19 NSA935807-09 14 CLAMP

20 NSA935808-01 7 WASHER

34 NSA5527-03-08 7 SPACER

62 NAS1801-3-22 14 SCREW

References

Fig. A-FBNAA

Modification of the Routing of Routes 1P

and 2P in the Shroud Box (LH side) -

ADDITIONAL WORK

Sheet 01

Sheet 02

(a) Remove :

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

14 Clamp Item (19) Retain

7 Screw Item (22) Discard

7 Washer Item (20) Retain

7 Spacer Item (34) Retain

(b) Or remove :

14 Clamp Item (19) Discard

7 Screw Item (22) Discard

7 Washer Item (20) Discard

(c) Install :

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

14 Clamp Item (19) Retained at

removal

7 Screw NAS1801-3-22 Item 62

7 Washer Item (20) Retained at

removal

7 Spacer Item (34) Retained at

removal

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 236

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

(d) Or install :

14 Clamp NSA935807-09 Item 19

7 Spacer NSA5527-03-08 Item 34

7 Screw NAS1801-3-22 Item 62

7 Washer NSA935808-01 Item 20

(4) Subtask 246103-831-024-001 - Modify the routing of the routes 1E and 1G in the

leading edge at LH wing, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

513

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Supplementary kit 246103A01S03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

66 NSA935401-08 2 TIE

References

Fig. A-FBQAA

Modification of the Routing in the

Leading Edge (LH and RH side) -

ADDITIONAL WORK

Sheet 01

(a) Remove :

Refer to Fig. A-FBQAA Sheet 01

2 Tie-Cable NSA935401-05 Item (23) Discard

(b) Install :

Refer to Fig. A-FBQAA Sheet 01

2 Tie-Cable NSA935401-08 Item 66

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 237

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

(5) Subtask 246103-831-025-001 - Modify the routing of the routes 2E and 2G in the

leading edge at RH wing, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

613

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Supplementary kit 246103A02S03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

66 NSA935401-08 2 TIE

References

Fig. A-FBQAA

Modification of the Routing in the

Leading Edge (LH and RH side) -

ADDITIONAL WORK

Sheet 01

(a) Remove :

Refer to Fig. A-FBQAA Sheet 01

2 Tie-Cable NSA935401-05 Item (23) Discard

(b) Install :

Refer to Fig. A-FBQAA Sheet 01

2 Tie-Cable NSA935401-08 Item 66

(6) Subtask 246103-400-001-001 - Install a support on the support of the BLUE

hydraulic reservoir at LH wing, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

571 Work location from Frame 47 to Frame 48

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills NON SPECIFIC

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 238

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

Material necessary to do the job

Kit 246103A01R14

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2528-3 2 NUT

EN6115V3-4 2 BOLT

Supplementary kit 246103A01S03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

20 NSA935808-01 1 WASHER

31 NAS1801-3-11 1 SCREW

67 A0041113300000 1 BRACKET

68 ASNA2050DXJ4828 2 RIVET

69 NSA935807-06 1 CLAMP

Supplementary kit 246103A01S13

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

100 ASNA2050DXJ5613 2 RIVET

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Primer Epoxy Paint - TSA

Anodizing Corrosion

Inhibiting Structure

04DEB2 As required

Primer Polyurethane Paint -

Corrosion Inhibiting

04EAC2 As required

Top Coat Polyurethane -

Grey Internal Structure

04JME4 As required

Polysulfide Sealant -

General Purpose Interfay

06AAC1

Polysulfide Sealant-Fuel

Tank Fillet

06ABB1 As required

Non Aqueous Cleaner -

General

08BAA9 As required

Corrosion Preventive

Compound-Water

Displacing

12ADB1 As required

References

Fig. A-FBRAA

Installation of a Support on the Support

of the BLUE Hydraulic Reservoir (LH

wing) - ADDITIONAL WORK

Sheet 01

Sheet 02

Sheet 03

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 239

5

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@A300-600

SERVICE BULLETIN

(a) Remove :

Refer to Fig. A-FBRAA Sheet 01

1 Support Item (35) Discard

2 Screw Item (37) Discard

2 Washer Item (36) Discard

2 Nut Item (21) Discard

(b) Blank the existing holes with:

2 Rivet ASNA2050DXJ5613 Item 100

NOTE: Wet install the rivets with:

Primer Epoxy Paint

- TSA Anodizing

Corrosion Inhibiting

Structure

04DEB2 As required

(c) Install the new support :

Refer to Fig. A-FBRAA Sheet 01, Fig. A-FBRAA Sheet 02 and Fig. A-FBRAA Sheet

03

1 Remove :

2 Rivet Item (68) Discard

NOTE: Clean the area with :

Non Aqueous

Cleaner - General

08BAA9 As required

2 Install the bracket Item 67.

a Put the bracket Item 67 in position.

b Drill two holes on the bracket Item 67 to a diameter comprised between

4.85 mm (0.191 in.) and 4.95 mm (0.195 in.) to match the holes of the

structure.

c Wet install :

1 Bracket A0041113300000 Item 67

2 Rivet ASNA2050DXJ4828 Item 68

NOTE: If the installation of bracket Item 67 with the rivets is not

possible, attach with:

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 240

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

2 Bolt EN6115V3-4

2 Nut ASNA2528-3

NOTE: Between the bracket Item 67 and the structure, apply :

Polysulfide SealantFuel Tank Fillet06ABB1 As required

NOTE: Wet install the rivets with :

Polysulfide Sealant

- General Purpose

Interfay

06AAC1 As required

NOTE: Apply on the head of the rivets :

Primer

Polyurethane Paint

- Corrosion

Inhibiting

04EAC2 As required

Top Coat

Polyurethane - Grey

Internal Structure

04JME4 As required

NOTE: On the modified area, apply :

Corrosion

Preventive

Compound-Water

Displacing

12ADB1 As required

3 Attach the sleeve to the bracket with :

1 Clamp NSA935807-06 Item 69

1 Screw NAS1801-3-11 Item 31

1 Washer NSA935808-01 Item 20

(7) Subtask 246103-400-002-001 - Install a bracket on the shroud box blanking plate at

LH side, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

147 Work location Frame 51

from Stringer 31 to Stringer 33

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 241

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Supplementary kit 246103A01S03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

21 NSA5050-3 3 NUT

28 A0041113420000 1 BRACKET

30 NAS1801-3-8 2 SCREW

37 NAS1801-3-9 1 SCREW

63 NSA5516-13ND 2 CLAMP

64 NSA5516-31ND 2 CLAMP

70 A0041113500000 1 CLAMP

71 NAS1801-3-12 2 SCREW

75 A0041113500200 1 CLAMP

76 A0041113500400 1 CLAMP

Supplementary kit 246103A02S03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

46 NAS1149F0332P 2 WASHER

References

Fig. A-FBSAA

Installation of a Bracket on the Shroud

Box Blanking Plate (LH and RH side) -

ADDITIONAL WORK

Sheet 01

Sheet 02

(a) Remove :

Refer to Fig. A-FBSAA Sheet 01

2 Screw Item (27) Discard

2 Washer Item (46) Discard

(b) Install the bracket :

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

1 Bracket A0041113420000 Item 28

2 Screw NAS1801-3-12 Item 71

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 242

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

2 Washer NAS1149F0332P Item 46

(c) Attach the bundles on the shroud box bracket :

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

1 Attach the bundles with :

2 Clamp NSA5516-13ND Item 63

or

2 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

NOTE: Two or three bundles may be installed.

attach with :

1 Nut NSA5050-3 Item 21

and

1 Screw NAS1801-3-9 Item 37

2 Or attach the bundles with :

1 Clamp NSA5516-13ND Item 63

or

1 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

NOTE: Two or three bundles may be installed.

and

1 Clamp A0041113500000 Item 70

or

1 Clamp A0041113500200 Item 75

or

1 Clamp A0041113500400 Item 76

NOTE: Install clamp Item 70 or 75 or 76 according to the bundle

diameters.

attach with :

2 Nut NSA5050-3 Item 21

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 243

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

2 Screw NAS1801-3-8 Item 30

(8) Subtask 246103-400-003-001 - Install a bracket on the shroud box blanking plate at

RH side, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

148 Work location Frame 51

from Stringer 31 to Stringer 33

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Supplementary kit 246103A02S03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

21 NSA5050-3 3 NUT

29 A0041113420100 1 BRACKET

30 NAS1801-3-8 2 SCREW

37 NAS1801-3-9 1 SCREW

46 NAS1149F0332P 2 WASHER

63 NSA5516-13ND 2 CLAMP

64 NSA5516-31ND 2 CLAMP

70 A0041113500000 1 CLAMP

71 NAS1801-3-12 2 SCREW

75 A0041113500200 1 CLAMP

76 A0041113500400 1 CLAMP

References

Fig. A-FBSAA

Installation of a Bracket on the Shroud

Box Blanking Plate (LH and RH side) -

ADDITIONAL WORK

Sheet 01

Sheet 02

(a) Remove :

Refer to Fig. A-FBSAA Sheet 01

2 Screw Item (27) Discard

2 Washer Item (46) Discard

(b) Install the bracket :

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

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 244

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

1 Bracket A0041113420100 Item 29

attach with :

2 Screw NAS1801-3-12 Item 71

2 Washer NAS1149F0332P Item 46

(c) Attach the bundles on the shroud box bracket :

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

1 Attach the bundles with :

2 Clamp NSA5516-13ND Item 63

or

2 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

NOTE: Two or three bundles may be installed.

attach with :

1 Nut NSA5050-3 Item 21

1 Screw NAS1801-3-9 Item 37

2 Or attach the bundles with :

1 Clamp NSA5516-13ND Item 63

or

1 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

NOTE: Two or three bundles may be installed.

and

1 Clamp A0041113500000 Item 70

or

1 Clamp A0041113500200 Item 75

or

1 Clamp A0041113500400 Item 76

NOTE: Install clamp Item 70 or 75 or 76 according to the bundle

diameters.

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 245

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

attach with :

2 Nut NSA5050-3 Item 21

2 Screw NAS1801-3-8 Item 30

(9) Subtask 246103-020-004-001 - Remove the clamps between FR50 and FR51 at

STRG 32 at LH side, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

147 Work location from Frame 50 to Frame 51

Stringer 32

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills NON SPECIFIC

References

Fig. A-FBPAA

Modification of the Routing Between

FR50 and FR51 at STGR32 (LH and RH

side) - ADDITIONAL WORK

Sheet 01

Sheet 02

(a) Depending on the stacking, remove :

Refer to Fig. A-FBPAA Sheet 01

4 Clamp Item (16) Discard

2 Clamp Item (32) Discard

2 Spacer Item (14) Discard

2 Clip nut Item (43) Discard

2 Washer Item (20) Discard

2 Screw Item (33) Discard

Or remove :

Refer to Fig. A-FBPAA Sheet 01

4 Clamp Item (16) Discard

2 Spacer Item (14) Discard

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 246

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

2 Clip nut Item (43) Discard

2 Washer Item (20) Discard

2 Screw Item (33) Discard

(10) Subtask 246103-831-026-001 - Remove the clamps of the Passage Way at FR52 (LH

side) - ADDITIONAL WORK

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills NON SPECIFIC

References

Fig. A-FBTAA

Modification of the Routing of the

Passage Way at FR52 (LH side) -

ADDITIONAL WORK

Sheet 01

Sheet 02

(a) Remove :

Refer to Fig. A-FBTAA Sheet 01 andFig. A-FBTAA Sheet 02

4 Clamp Item (72) Discard

1 Washer Item (73) Discard

1 Screw Item (74) Retain

1 Clamp Item (44) Discard

1 Clamp Item (45) Discard

2 Washer Item (46) Discard

2 Screw Item (47) Retain

(11) Subtask 246103-831-029-001 - Modify the Routing between FR50 and FR52 and

between STGR 33 and 30 at LH side - ADDITIONAL WORK

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 247

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

Material necessary to do the job

Supplementary kit 246103A01S03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

77 EN6049-007-19-5 7.5 (M) SLEEVE

78 EN6049-007-13-5 7.5 (M) SLEEVE

References

Fig. A-FBXAA

Modification of the Routing between

FR50 and FR52 (LH and RH side) -

ADDITIONAL WORK

Sheet 01

(a) Remove :

Refer to Fig. A-FBXAA Sheet 01

5 (M) Conduit Item (77) Discard

NOTE: A third conduit may be installed. If installed, remove it.

(b) Install :

Refer to Fig. A-FBXAA Sheet 01

5 (M) Sleeve EN6049-007-13-5 Item 78

or

5 (M) Sleeve EN6049-007-19-5 Item 77

NOTE: Install the sleeve Item 77 or 78 according to the harness diameter.

NOTE: If a third conduit was installed, install :

2.5 (M) Sleeve EN6049-007-13-5 Item 78

or

2.5 (M) Sleeve EN6049-007-19-5 Item 77

NOTE: Install the sleeve Item 77 or 78 according to the harness diameter.

(12) Subtask 246103-420-005-001 - Install the clamps between FR50 and FR51 at STRG

32 at LH side, ADDITIONAL WORK

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills NON SPECIFIC

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 248

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

Material necessary to do the job

Supplementary kit 246103A01S03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

12 NSA5527-03-01 1 SPACER

14 NSA5527-03-02 2 SPACER

33 NAS1801-3-25 2 SCREW

43 NSA5067-3-1 2 NUT

46 NAS1149F0332P 4 WASHER

63 NSA5516-13ND 6 CLAMP

64 NSA5516-31ND 6 CLAMP

References

Fig. A-FBPAA

Modification of the Routing Between

FR50 and FR51 at STGR32 (LH and RH

side) - ADDITIONAL WORK

Sheet 01

Sheet 02

(a) Depending on the staking, install :

Refer to Fig. A-FBPAA Sheet 02 view C

3 Clamp NSA5516-13ND Item 63

or

3 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

1 Spacer NSA5527-03-01 Item 12

1 Spacer NSA5527-03-02 Item 14

1 Screw NAS1801-3-25 Item 33

3 Washer NAS1149F0332P Item 46

1 Clip nut NSA5067-3-1 Item 43

Or install :

Refer to Fig. A-FBPAA Sheet 02 view C

2 Clamp NSA5516-13ND Item 63

or

2 Clamp NSA5516-31ND Item 64

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 249

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@A300-600

SERVICE BULLETIN

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

1 Spacer NSA5527-03-01 Item 12

1 Spacer NSA5527-03-02 Item 14

1 Screw NAS1801-3-25 Item 33

1 Washer NAS1149F0332P Item 46

1 Clip nut NSA5067-3-1 Item 43

(b) Depending on the staking, install :

Refer to Fig. A-FBPAA Sheet 02 view D

3 Clamp NSA5516-13ND Item 63

or

3 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

1 Spacer NSA5527-03-02 Item 14

1 Screw NAS1801-3-25 Item 33

1 Washer NAS1149F0332P Item 46

1 Clip nut NSA5067-3-1 Item 43

Or install :

Refer to Fig. A-FBPAA Sheet 02 view D

2 Clamp NSA5516-13ND Item 63

or

2 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

1 Spacer NSA5527-03-02 Item 14

1 Screw NAS1801-3-25 Item 33

1 Washer NAS1149F0332P Item 46

1 Clip nut NSA5067-3-1 Item 43

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 250

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Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

(13) Subtask 246103-420-003-001 - Install the clamps of the Passage Way at FR52 (LH

side) - ADDITIONAL WORK

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills NON SPECIFIC

Material necessary to do the job

Supplementary kit 246103A01S03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

63 NSA5516-13ND 4 CLAMP

64 NSA5516-31ND 4 CLAMP

Supplementary kit 246103A02S03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

46 NAS1149F0332P 3 WASHER

References

Fig. A-FBTAA

Modification of the Routing of the

Passage Way at FR52 (LH side) -

ADDITIONAL WORK

Sheet 01

Sheet 02

(a) Install :

Refer to Fig. A-FBTAA Sheet 01 andFig. A-FBTAA Sheet 02

4 Clamp NSA5516-13ND Item 63

or

4 Clamp NSA5516-31ND Item 64

NOTE: Install the clamp Item 63 or 64 according to the bundle diameter.

3 Washer NAS1149F0332P Item 46

2 Screw Item (47) Retained at

removal

1 Screw Item (74) Retained at

removal

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 251

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Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

(14) Subtask 246103-020-005-001 - Remove the clamps between FR50 and FR51 at

STGR 32 at RH side, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

148 Work location from Frame 50 to Frame 51

Stringer 32

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills NON SPECIFIC

References

Fig. A-FBPAA

Modification of the Routing Between

FR50 and FR51 at STGR32 (LH and RH

side) - ADDITIONAL WORK

Sheet 01

Sheet 02

(a) Depending on the stacking, remove :

Refer to Fig. A-FBPAA Sheet 01

4 Clamp Item (16) Discard

2 Clamp Item (32) Discard

2 Spacer Item (14) Discard

2 Clip nut Item (43) Discard

2 Washer Item (20) Discard

2 Screw Item (33) Discard

Or remove :

Refer to Fig. A-FBPAA Sheet 01

4 Clamp Item (16) Discard

2 Spacer Item (14) Discard

2 Clip nut Item (43) Discard

2 Washer Item (20) Discard

2 Screw Item (33) Discard

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 252

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Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

(15) Subtask 246103-831-027-001 - Remove the clamps of the Passage Way at FR52

(RH side) - ADDITIONAL WORK

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills NON SPECIFIC

References

Fig. A-FBVAA

Modification of the Routing of the

Passage Way at FR52 (RH side) -

ADDITIONAL WORK

Sheet 01

Sheet 02

(a) Remove :

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

4 Clamp Item (72) Discard

1 Washer Item (73) Discard

1 Screw Item (74) Retain

1 Clamp Item (44) Discard

1 Clamp Item (45) Discard

2 Washer Item (46) Discard

2 Screw Item (47) Retain

(16) Subtask 246103-831-030-001 - Modify the Routing between FR50 and FR52 and

between STGR 33 and 30 at RH side - ADDITIONAL WORK

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Supplementary kit 246103A02S03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

77 EN6049-007-19-5 7.5 (M) SLEEVE

78 EN6049-007-13-5 7.5 (M) SLEEVE

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 253

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@A300-600

SERVICE BULLETIN

References

Fig. A-FBXAA

Modification of the Routing between

FR50 and FR52 (LH and RH side) -

ADDITIONAL WORK

Sheet 01

(a) Remove :

Refer to Fig. A-FBXAA Sheet 01

5 (M) Conduit Item (77) Discard

NOTE: A third conduit may be installed. If installed, remove it.

(b) Install :

Refer to Fig. A-FBXAA Sheet 01

5 (M) Sleeve EN6049-007-13-5 Item 78

or

5 (M) Sleeve EN6049-007-19-5 Item 77

NOTE: Install the sleeve Item 77 or 78 according to the harness diameter.

NOTE: If a third conduit was installed, install :

2.5 (M) Sleeve EN6049-007-13-5 Item 78

or

2.5 (M) Sleeve EN6049-007-19-5 Item 77

NOTE: Install the sleeve Item 77 or 78 according to the harness diameter.

(17) Subtask 246103-420-006-001 - Install the clamps between FR50 and FR51 at STGR

32 at RH side, ADDITIONAL WORK

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills NON SPECIFIC

Material necessary to do the job

Supplementary kit 246103A02S03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

12 NSA5527-03-01 1 SPACER

14 NSA5527-03-02 2 SPACER

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 254

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@A300-600

SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

33 NAS1801-3-25 2 SCREW

43 NSA5067-3-1 2 NUT

46 NAS1149F0332P 2 WASHER

63 NSA5516-13ND 6 CLAMP

64 NSA5516-31ND 6 CLAMP

References

Fig. A-FBPAA

Modification of the Routing Between

FR50 and FR51 at STGR32 (LH and RH

side) - ADDITIONAL WORK

Sheet 01

Sheet 02

(a) Depending on the staking, install :

Refer to Fig. A-FBPAA Sheet 02 view C

3 Clamp NSA5516-13ND Item 63

or

3 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

1 Spacer NSA5527-03-01 Item 12

1 Spacer NSA5527-03-02 Item 14

1 Screw NAS1801-3-25 Item 33

1 Clip nut NSA5067-3-1 Item 43

1 Washer NAS1149F0332P Item 46

Or install :

Refer to Fig. A-FBPAA Sheet 02 view C

2 Clamp NSA5516-13ND Item 63

or

2 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

1 Spacer NSA5527-03-01 Item 12

1 Spacer NSA5527-03-02 Item 14

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 255

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@A300-600

SERVICE BULLETIN

1 Screw NAS1801-3-25 Item 33

1 Clip nut NSA5067-3-1 Item 43

1 Washer NAS1149F0332P Item 46

(b) Depending on the staking, install :

Refer to Fig. A-FBPAA Sheet 02 view D

3 Clamp NSA5516-13ND Item 63

or

3 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

1 Spacer NSA5527-03-02 Item 14

1 Screw NAS1801-3-25 Item 33

1 Clip nut NSA5067-3-1 Item 43

1 Washer NAS1149F0332P Item 46

Or install :

Refer to Fig. A-FBPAA Sheet 02 view D

2 Clamp NSA5516-13ND Item 63

or

2 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

1 Spacer NSA5527-03-02 Item 14

1 Screw NAS1801-3-25 Item 33

1 Clip nut NSA5067-3-1 Item 43

1 Washer NAS1149F0332P Item 46

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 256

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Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

(18) Subtask 246103-420-004-001 - Install the clamps of the Passage Way at FR52 (RH

side) - ADDITIONAL WORK

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills NON SPECIFIC

Material necessary to do the job

Supplementary kit 246103A02S03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

46 NAS1149F0332P 3 WASHER

63 NSA5516-13ND 4 CLAMP

64 NSA5516-31ND 4 CLAMP

References

Fig. A-FBVAA

Modification of the Routing of the

Passage Way at FR52 (RH side) -

ADDITIONAL WORK

Sheet 01

Sheet 02

(a) Install :

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

4 Clamp NSA5516-13ND Item 63

or

4 Clamp NSA5516-31ND Item 64

NOTE: Install the clamp Item 63 or 64 according to the bundle diameter.

3 Washer NAS1149F0332P Item 46

2 Screw Item (47) Retained at

removal

1 Screw Item (74) Retained at

removal

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 257

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Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF 002

(1) Subtask 246103-831-028-001 - Modify the routing on rib 1 on the passage way to

the shroud box at LH side, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

570 Work location Rib 1

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 246103A01R14

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

87 NSA360002 1 (M) EXTRUSIN

Supplementary kit 246103A01S03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

12 NSA5527-03-01 4 SPACER

24 NSA939510BN 1 (M) STRIP

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Epoxy Adhesive-Metal To

Metal - Legacy

05EJL9 As required

Epoxy Adhesive - Legacy 3 05EML7 As required

Contact Adhesive-Rubber &

Plastic Bonding Neopren

05JBC9 As required

Non Aqueous Cleaner -

Isopropyl Alcohol

08BBD1 As required

References

Process and Material Specification

(PMS)

Process and Material Specification (PMS)

01-01-28 Process E

Fig. A-FBMAA

Modification of the Clamps on the

Passage Way to the Shroud Box (LH

and RH side) - ADDITIONAL WORK

Sheet 01

Sheet 02

Sheet 03

Sheet 04

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 258

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@A300-600

SERVICE BULLETIN

(a) Install:

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

1 (M) Extrusion NSA360002 Item 87

with:

Contact AdhesiveRubber & Plastic

Bonding Neopren

05JBC9 As required

(b) Measure the gap between the clamp and the structure, refer to Fig. A-FBMAA

Sheet 01 and Fig. A-FBMAA Sheet 02:

1 If the gap between the structure and the clamp is less than 6.35 mm (0.25 in.),

install, refer to Fig. A-FBMAA Sheet 03 :

4 Spacer NSA5527-03-01 Item 12

2 If the gap between the structure and the clamp is more than 130 mm (5.118

in), contact AIRBUS, refer to Fig. A-FBMAA Sheet 02

NOTE: For operators that have the gap between the structure and the

clamp is more than 130 mm (5.118 in) contact Airbus at:

AIRBUS CUSTOMER SERVICES ENGINEERING - SEEA5

ELECTRICAL POWER GENERATION DISTRIBUTION &

LIGHTING SYSTEMS

1 ROND POINT MAURICE BELLONTE

31707 BLAGNAC CEDEX FRANCE

FAX +33 561 934 425

(c) Modify the grommet installation :

Refer to Fig. A-FBMAA Sheet 01, Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03

and Fig. A-FBMAA Sheet 04

1 Remove :

1 (M) Strip-Protective Item (24) Discard

2 Install :

Refer to Process and Material Specification (PMS) 01-01-28 Process E

1 (M) Strip-Protective NSA939510BN Item 24

NOTE: Install the Strip-Protective Item 24 with:

Epoxy AdhesiveMetal To Metal -

Legacy

05EJL9 As required

NOTE: Do the abrading and cleaning of the contact zones of StripDATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 259

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@A300-600

SERVICE BULLETIN

Protective Item 24, on the structure with:

Non Aqueous

Cleaner - Isopropyl

Alcohol

08BBD1 As required

Epoxy Adhesive -

Legacy 3

05EML7 As required

(2) Subtask 246103-831-020-001 - Modify the routing on rib 1 on the passage way to

the shroud box at RH side, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

670 Work location Rib 1

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 246103A02R12

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

87 NSA360002 1 (M) EXTRUSIN

Supplementary kit 246103A02S03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

12 NSA5527-03-01 4 SPACER

24 NSA939510BN 1 (M) STRIP

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Epoxy Adhesive-Metal To

Metal - Legacy

05EJL9 As required

Epoxy Adhesive - Legacy 3 05EML7 As required

Contact Adhesive-Rubber &

Plastic Bonding Neopren

05JBC9 As required

Non Aqueous Cleaner -

Isopropyl Alcohol

08BBD1 As required

References

Process and Material Specification

(PMS)

Process and Material Specification (PMS)

01-01-28 Process E

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 260

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@A300-600

SERVICE BULLETIN

References

Fig. A-FBMAA

Modification of the Clamps on the

Passage Way to the Shroud Box (LH

and RH side) - ADDITIONAL WORK

Sheet 01

Sheet 02

Sheet 03

Sheet 04

(a) Install:

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

1 (M) Extrusion NSA360002 Item 87

with:

Contact AdhesiveRubber & Plastic

Bonding Neopren

05JBC9 As required

(b) Measure the gap between the clamp and the structure, refer to Fig. A-FBMAA

Sheet 01 and Fig. A-FBMAA Sheet 02:

1 If the gap between the structure and the clamp is less than 6.35 mm (0.25 in.),

install, refer to Fig. A-FBMAA Sheet 03:

4 Spacer NSA5527-03-01 Item 12

2 If the gap between the structure and the clamp is more than 130 mm (5.118

in), contact AIRBUS, refer to Fig. A-FBMAA Sheet 02

NOTE: For operators that have the gap between the structure and the

clamp is more than 130 mm (5.118 in) contact Airbus at:

AIRBUS CUSTOMER SERVICES ENGINEERING - SEEA5

ELECTRICAL POWER GENERATION DISTRIBUTION &

LIGHTING SYSTEMS

1 ROND POINT MAURICE BELLONTE

31707 BLAGNAC CEDEX FRANCE

FAX +33 561 934 425

(c) Modify the grommet installation :

Refer to Fig. A-FBMAA Sheet 01, Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03

and Fig. A-FBMAA Sheet 04

1 Remove :

1 (M) Strip-Protective Item (24) Discard

2 Install :

Refer to Process and Material Specification (PMS) 01-01-28 Process E

1 (M) Strip-Protective NSA939510BN Item 24

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 261

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@A300-600

SERVICE BULLETIN

NOTE: Install the Strip-Protective Item 24 with:

Epoxy AdhesiveMetal To Metal -

Legacy

05EJL9 As required

NOTE: Do the abrading and cleaning of the contact zones of StripProtective Item 24, on the structure with:

Non Aqueous

Cleaner - Isopropyl

Alcohol

08BBD1 As required

Epoxy Adhesive -

Legacy 3

05EML7 As required

(3) Subtask 246103-831-021-001 - Modify the routing of routes 1P and 2P in the

shroud box at LH side, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

571

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Supplementary kit 246103A01S03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

19 NSA935807-09 14 CLAMP

20 NSA935808-01 7 WASHER

34 NSA5527-03-08 7 SPACER

62 NAS1801-3-22 14 SCREW

References

Fig. A-FBNAA

Modification of the Routing of Routes 1P

and 2P in the Shroud Box (LH side) -

ADDITIONAL WORK

Sheet 01

Sheet 02

(a) Remove :

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

14 Clamp Item (19) Retain

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 262

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@A300-600

SERVICE BULLETIN

7 Screw Item (22) Discard

7 Washer Item (20) Retain

7 Spacer Item (34) Retain

(b) Or remove :

14 Clamp Item (19) Discard

7 Screw Item (22) Discard

7 Washer Item (20) Discard

(c) Install :

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

14 Clamp Item (19) Retained at

removal

7 Screw NAS1801-3-22 Item 62

7 Washer Item (20) Retained at

removal

7 Spacer Item (34) Retained at

removal

(d) Or install :

14 Clamp NSA935807-09 Item 19

7 Spacer NSA5527-03-08 Item 34

7 Screw NAS1801-3-22 Item 62

7 Washer NSA935808-01 Item 20

(4) Subtask 246103-831-024-001 - Modify the routing of the routes 1E and 1G in the

leading edge at LH wing, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

513

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 263

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@A300-600

SERVICE BULLETIN

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Supplementary kit 246103A01S03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

66 NSA935401-08 2 TIE

References

Fig. A-FBQAA

Modification of the Routing in the

Leading Edge (LH and RH side) -

ADDITIONAL WORK

Sheet 01

(a) Remove :

Refer to Fig. A-FBQAA Sheet 01

2 Tie-Cable NSA935401-05 Item (23) Discard

(b) Install :

Refer to Fig. A-FBQAA Sheet 01

2 Tie-Cable NSA935401-08 Item 66

(5) Subtask 246103-831-025-001 - Modify the routing of the routes 2E and 2G in the

leading edge at RH wing, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

613

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 264

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@A300-600

SERVICE BULLETIN

Material necessary to do the job

Supplementary kit 246103A02S03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

66 NSA935401-08 2 TIE

References

Fig. A-FBQAA

Modification of the Routing in the

Leading Edge (LH and RH side) -

ADDITIONAL WORK

Sheet 01

(a) Remove :

Refer to Fig. A-FBQAA Sheet 01

2 Tie-Cable NSA935401-05 Item (23) Discard

(b) Install :

Refer to Fig. A-FBQAA Sheet 01

2 Tie-Cable NSA935401-08 Item 66

(6) Subtask 246103-400-001-001 - Install a support on the support of the BLUE

hydraulic reservoir at LH wing, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

571 Work location from Frame 47 to Frame 48

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 246103A01R14

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2528-3 2 NUT

EN6115V3-4 2 BOLT

Supplementary kit 246103A01S03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

20 NSA935808-01 1 WASHER

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 265

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@A300-600

SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

31 NAS1801-3-11 1 SCREW

67 A0041113300000 1 BRACKET

68 ASNA2050DXJ4828 2 RIVET

69 NSA935807-06 1 CLAMP

Supplementary kit 246103A01S13

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

100 ASNA2050DXJ5613 2 RIVET

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Primer Epoxy Paint - TSA

Anodizing Corrosion

Inhibiting Structure

04DEB2 As required

Primer Polyurethane Paint -

Corrosion Inhibiting

04EAC2 As required

Top Coat Polyurethane -

Grey Internal Structure

04JME4 As required

Polysulfide Sealant -

General Purpose Interfay

06AAC1

Polysulfide Sealant-Fuel

Tank Fillet

06ABB1 As required

Non Aqueous Cleaner -

General

08BAA9 As required

Corrosion Preventive

Compound-Water

Displacing

12ADB1 As required

References

Fig. A-FBRAA

Installation of a Support on the Support

of the BLUE Hydraulic Reservoir (LH

wing) - ADDITIONAL WORK

Sheet 01

Sheet 02

Sheet 03

(a) Remove :

Refer to Fig. A-FBRAA Sheet 01

1 Support Item (35) Discard

2 Screw Item (37) Discard

2 Washer Item (36) Discard

2 Nut Item (21) Discard

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 266

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SERVICE BULLETIN

(b) Blank the existing holes with:

2 Rivet ASNA2050DXJ5613 Item 100

NOTE: Wet install the rivets with:

Primer Epoxy Paint

- TSA Anodizing

Corrosion Inhibiting

Structure

04DEB2 As required

(c) Install the new support :

Refer to Fig. A-FBRAA Sheet 01, Fig. A-FBRAA Sheet 02 and Fig. A-FBRAA Sheet

03

1 Remove :

2 Rivet Item (68) Discard

NOTE: Clean the area with :

Non Aqueous

Cleaner - General

08BAA9 As required

2 Install the bracket Item 67.

a Put the bracket Item 67 in position.

b Drill two holes on the bracket Item 67 to a diameter comprised between

4.85 mm (0.191 in.) and 4.95 mm (0.195 in.) to match the holes of the

structure.

c Wet install :

1 Bracket A0041113300000 Item 67

2 Rivet ASNA2050DXJ4828 Item 68

NOTE: If the installation of bracket Item 67 with the rivets is not

possible, attach with:

2 Bolt EN6115V3-4

2 Nut ASNA2528-3

NOTE: Between the bracket Item 67 and the structure, apply :

Polysulfide SealantFuel Tank Fillet

06ABB1 As required

NOTE: Wet install the rivets with :

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 267

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@A300-600

SERVICE BULLETIN

Polysulfide Sealant

- General Purpose

Interfay

06AAC1 As required

NOTE: Apply on the head of the rivets :

Primer

Polyurethane Paint

- Corrosion

Inhibiting

04EAC2 As required

Top Coat

Polyurethane - Grey

Internal Structure

04JME4 As required

NOTE: On the modified area, apply :

Corrosion

Preventive

Compound-Water

Displacing

12ADB1 As required

3 Attach the sleeve to the bracket with :

1 Clamp NSA935807-06 Item 69

1 Screw NAS1801-3-11 Item 31

1 Washer NSA935808-01 Item 20

(7) Subtask 246103-400-002-001 - Install a bracket on the shroud box blanking plate at

LH side, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

147 Work location Frame 51

from Stringer 31 to Stringer 33

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Supplementary kit 246103A01S03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

21 NSA5050-3 3 NUT

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 268

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@A300-600

SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

28 A0041113420000 1 BRACKET

30 NAS1801-3-8 2 SCREW

37 NAS1801-3-9 1 SCREW

63 NSA5516-13ND 2 CLAMP

64 NSA5516-31ND 2 CLAMP

70 A0041113500000 1 CLAMP

71 NAS1801-3-12 2 SCREW

75 A0041113500200 1 CLAMP

76 A0041113500400 1 CLAMP

Supplementary kit 246103A02S03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

46 NAS1149F0332P 2 WASHER

References

Fig. A-FBSAA

Installation of a Bracket on the Shroud

Box Blanking Plate (LH and RH side) -

ADDITIONAL WORK

Sheet 01

Sheet 02

(a) Remove :

Refer to Fig. A-FBSAA Sheet 01

2 Screw Item (27) Discard

2 Washer Item (46) Discard

(b) Install the bracket :

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

1 Bracket A0041113420000 Item 28

2 Screw NAS1801-3-12 Item 71

2 Washer NAS1149F0332P Item 46

(c) Attach the bundles on the shroud box bracket :

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

1 Attach the bundles with :

2 Clamp NSA5516-13ND Item 63

or

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 269

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@A300-600

SERVICE BULLETIN

2 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

NOTE: Two or three bundles may be installed.

attach with :

1 Nut NSA5050-3 Item 21

and

1 Screw NAS1801-3-9 Item 37

2 Or attach the bundles with :

1 Clamp NSA5516-13ND Item 63

or

1 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

NOTE: Two or three bundles may be installed.

and

1 Clamp A0041113500000 Item 70

or

1 Clamp A0041113500200 Item 75

or

1 Clamp A0041113500400 Item 76

NOTE: Install clamp Item 70 or 75 or 76 according to the bundle

diameters.

attach with :

2 Nut NSA5050-3 Item 21

2 Screw NAS1801-3-8 Item 30

(8) Subtask 246103-400-003-001 - Install a bracket on the shroud box blanking plate at

RH side, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

148 Work location Frame 51

from Stringer 31 to Stringer 33

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 270

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@A300-600

SERVICE BULLETIN

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Supplementary kit 246103A02S03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

21 NSA5050-3 3 NUT

29 A0041113420100 1 BRACKET

30 NAS1801-3-8 2 SCREW

37 NAS1801-3-9 1 SCREW

46 NAS1149F0332P 2 WASHER

63 NSA5516-13ND 2 CLAMP

64 NSA5516-31ND 2 CLAMP

70 A0041113500000 1 CLAMP

71 NAS1801-3-12 2 SCREW

75 A0041113500200 1 CLAMP

76 A0041113500400 1 CLAMP

References

Fig. A-FBSAA

Installation of a Bracket on the Shroud

Box Blanking Plate (LH and RH side) -

ADDITIONAL WORK

Sheet 01

Sheet 02

(a) Remove :

Refer to Fig. A-FBSAA Sheet 01

2 Screw Item (27) Discard

2 Washer Item (46) Discard

(b) Install the bracket :

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

1 Bracket A0041113420100 Item 29

attach with :

2 Screw NAS1801-3-12 Item 71

2 Washer NAS1149F0332P Item 46

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 271

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@A300-600

SERVICE BULLETIN

(c) Attach the bundles on the shroud box bracket :

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

1 Attach the bundles with :

2 Clamp NSA5516-13ND Item 63

or

2 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

NOTE: Two or three bundles may be installed.

attach with :

1 Nut NSA5050-3 Item 21

1 Screw NAS1801-3-9 Item 37

2 Or attach the bundles with :

1 Clamp NSA5516-13ND Item 63

or

1 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

NOTE: Two or three bundles may be installed.

and

1 Clamp A0041113500000 Item 70

or

1 Clamp A0041113500200 Item 75

or

1 Clamp A0041113500400 Item 76

NOTE: Install clamp Item 70 or 75 or 76 according to the bundle

diameters.

attach with :

2 Nut NSA5050-3 Item 21

2 Screw NAS1801-3-8 Item 30

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 272

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Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

(9) Subtask 246103-020-004-001 - Remove the clamps between FR50 and FR51 at

STRG 32 at LH side, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

147 Work location from Frame 50 to Frame 51

Stringer 32

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills NON SPECIFIC

References

Fig. A-FBPAA

Modification of the Routing Between

FR50 and FR51 at STGR32 (LH and RH

side) - ADDITIONAL WORK

Sheet 01

Sheet 02

(a) Depending on the stacking, remove :

Refer to Fig. A-FBPAA Sheet 01

4 Clamp Item (16) Discard

2 Clamp Item (32) Discard

2 Spacer Item (14) Discard

2 Clip nut Item (43) Discard

2 Washer Item (20) Discard

2 Screw Item (33) Discard

Or remove :

Refer to Fig. A-FBPAA Sheet 01

4 Clamp Item (16) Discard

2 Spacer Item (14) Discard

2 Clip nut Item (43) Discard

2 Washer Item (20) Discard

2 Screw Item (33) Discard

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 273

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Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

(10) Subtask 246103-831-026-001 - Remove the clamps of the Passage Way at FR52 (LH

side) - ADDITIONAL WORK

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills NON SPECIFIC

References

Fig. A-FBTAA

Modification of the Routing of the

Passage Way at FR52 (LH side) -

ADDITIONAL WORK

Sheet 01

Sheet 02

(a) Remove :

Refer to Fig. A-FBTAA Sheet 01 andFig. A-FBTAA Sheet 02

4 Clamp Item (72) Discard

1 Washer Item (73) Discard

1 Screw Item (74) Retain

1 Clamp Item (44) Discard

1 Clamp Item (45) Discard

2 Washer Item (46) Discard

2 Screw Item (47) Retain

(11) Subtask 246103-831-029-001 - Modify the Routing between FR50 and FR52 and

between STGR 33 and 30 at LH side - ADDITIONAL WORK

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Supplementary kit 246103A01S03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

77 EN6049-007-19-5 7.5 (M) SLEEVE

78 EN6049-007-13-5 7.5 (M) SLEEVE

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 274

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@A300-600

SERVICE BULLETIN

References

Fig. A-FBXAA

Modification of the Routing between

FR50 and FR52 (LH and RH side) -

ADDITIONAL WORK

Sheet 01

(a) Remove :

Refer to Fig. A-FBXAA Sheet 01

5 (M) Conduit Item (77) Discard

NOTE: A third conduit may be installed. If installed, remove it.

(b) Install :

Refer to Fig. A-FBXAA Sheet 01

5 (M) Sleeve EN6049-007-13-5 Item 78

or

5 (M) Sleeve EN6049-007-19-5 Item 77

NOTE: Install the sleeve Item 77 or 78 according to the harness diameter.

NOTE: If a third conduit was installed, install :

2.5 (M) Sleeve EN6049-007-13-5 Item 78

or

2.5 (M) Sleeve EN6049-007-19-5 Item 77

NOTE: Install the sleeve Item 77 or 78 according to the harness diameter.

(12) Subtask 246103-420-005-001 - Install the clamps between FR50 and FR51 at STRG

32 at LH side, ADDITIONAL WORK

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills NON SPECIFIC

Material necessary to do the job

Supplementary kit 246103A01S03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

12 NSA5527-03-01 1 SPACER

14 NSA5527-03-02 2 SPACER

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 275

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Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

33 NAS1801-3-25 2 SCREW

43 NSA5067-3-1 2 NUT

46 NAS1149F0332P 4 WASHER

63 NSA5516-13ND 6 CLAMP

64 NSA5516-31ND 6 CLAMP

References

Fig. A-FBPAA

Modification of the Routing Between

FR50 and FR51 at STGR32 (LH and RH

side) - ADDITIONAL WORK

Sheet 01

Sheet 02

(a) Depending on the staking, install :

Refer to Fig. A-FBPAA Sheet 02 view C

3 Clamp NSA5516-13ND Item 63

or

3 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

1 Spacer NSA5527-03-01 Item 12

1 Spacer NSA5527-03-02 Item 14

1 Screw NAS1801-3-25 Item 33

3 Washer NAS1149F0332P Item 46

1 Clip nut NSA5067-3-1 Item 43

Or install :

Refer to Fig. A-FBPAA Sheet 02 view C

2 Clamp NSA5516-13ND Item 63

or

2 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

1 Spacer NSA5527-03-01 Item 12

1 Spacer NSA5527-03-02 Item 14

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 276

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@A300-600

SERVICE BULLETIN

1 Screw NAS1801-3-25 Item 33

1 Washer NAS1149F0332P Item 46

1 Clip nut NSA5067-3-1 Item 43

(b) Depending on the staking, install :

Refer to Fig. A-FBPAA Sheet 02 view D

3 Clamp NSA5516-13ND Item 63

or

3 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

1 Spacer NSA5527-03-02 Item 14

1 Screw NAS1801-3-25 Item 33

1 Washer NAS1149F0332P Item 46

1 Clip nut NSA5067-3-1 Item 43

Or install :

Refer to Fig. A-FBPAA Sheet 02 view D

2 Clamp NSA5516-13ND Item 63

or

2 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

1 Spacer NSA5527-03-02 Item 14

1 Screw NAS1801-3-25 Item 33

1 Washer NAS1149F0332P Item 46

1 Clip nut NSA5067-3-1 Item 43

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 277

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Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

(13) Subtask 246103-420-003-001 - Install the clamps of the Passage Way at FR52 (LH

side) - ADDITIONAL WORK

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills NON SPECIFIC

Material necessary to do the job

Supplementary kit 246103A01S03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

63 NSA5516-13ND 4 CLAMP

64 NSA5516-31ND 4 CLAMP

Supplementary kit 246103A02S03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

46 NAS1149F0332P 3 WASHER

References

Fig. A-FBTAA

Modification of the Routing of the

Passage Way at FR52 (LH side) -

ADDITIONAL WORK

Sheet 01

Sheet 02

(a) Install :

Refer to Fig. A-FBTAA Sheet 01 andFig. A-FBTAA Sheet 02

4 Clamp NSA5516-13ND Item 63

or

4 Clamp NSA5516-31ND Item 64

NOTE: Install the clamp Item 63 or 64 according to the bundle diameter.

3 Washer NAS1149F0332P Item 46

2 Screw Item (47) Retained at

removal

1 Screw Item (74) Retained at

removal

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 278

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Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

(14) Subtask 246103-020-005-001 - Remove the clamps between FR50 and FR51 at

STGR 32 at RH side, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

148 Work location from Frame 50 to Frame 51

Stringer 32

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills NON SPECIFIC

References

Fig. A-FBPAA

Modification of the Routing Between

FR50 and FR51 at STGR32 (LH and RH

side) - ADDITIONAL WORK

Sheet 01

Sheet 02

(a) Depending on the stacking, remove :

Refer to Fig. A-FBPAA Sheet 01

4 Clamp Item (16) Discard

2 Clamp Item (32) Discard

2 Spacer Item (14) Discard

2 Clip nut Item (43) Discard

2 Washer Item (20) Discard

2 Screw Item (33) Discard

Or remove :

Refer to Fig. A-FBPAA Sheet 01

4 Clamp Item (16) Discard

2 Spacer Item (14) Discard

2 Clip nut Item (43) Discard

2 Washer Item (20) Discard

2 Screw Item (33) Discard

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 279

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Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

(15) Subtask 246103-831-027-001 - Remove the clamps of the Passage Way at FR52

(RH side) - ADDITIONAL WORK

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills NON SPECIFIC

References

Fig. A-FBVAA

Modification of the Routing of the

Passage Way at FR52 (RH side) -

ADDITIONAL WORK

Sheet 01

Sheet 02

(a) Remove :

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

4 Clamp Item (72) Discard

1 Washer Item (73) Discard

1 Screw Item (74) Retain

1 Clamp Item (44) Discard

1 Clamp Item (45) Discard

2 Washer Item (46) Discard

2 Screw Item (47) Retain

(16) Subtask 246103-831-030-001 - Modify the Routing between FR50 and FR52 and

between STGR 33 and 30 at RH side - ADDITIONAL WORK

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Supplementary kit 246103A02S03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

77 EN6049-007-19-5 7.5 (M) SLEEVE

78 EN6049-007-13-5 7.5 (M) SLEEVE

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 280

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@A300-600

SERVICE BULLETIN

References

Fig. A-FBXAA

Modification of the Routing between

FR50 and FR52 (LH and RH side) -

ADDITIONAL WORK

Sheet 01

(a) Remove :

Refer to Fig. A-FBXAA Sheet 01

5 (M) Conduit Item (77) Discard

NOTE: A third conduit may be installed. If installed, remove it.

(b) Install :

Refer to Fig. A-FBXAA Sheet 01

5 (M) Sleeve EN6049-007-13-5 Item 78

or

5 (M) Sleeve EN6049-007-19-5 Item 77

NOTE: Install the sleeve Item 77 or 78 according to the harness diameter.

NOTE: If a third conduit was installed, install :

2.5 (M) Sleeve EN6049-007-13-5 Item 78

or

2.5 (M) Sleeve EN6049-007-19-5 Item 77

NOTE: Install the sleeve Item 77 or 78 according to the harness diameter.

(17) Subtask 246103-420-006-001 - Install the clamps between FR50 and FR51 at STGR

32 at RH side, ADDITIONAL WORK

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills NON SPECIFIC

Material necessary to do the job

Supplementary kit 246103A02S03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

12 NSA5527-03-01 1 SPACER

14 NSA5527-03-02 2 SPACER

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 281

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@A300-600

SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

33 NAS1801-3-25 2 SCREW

43 NSA5067-3-1 2 NUT

46 NAS1149F0332P 2 WASHER

63 NSA5516-13ND 6 CLAMP

64 NSA5516-31ND 6 CLAMP

References

Fig. A-FBPAA

Modification of the Routing Between

FR50 and FR51 at STGR32 (LH and RH

side) - ADDITIONAL WORK

Sheet 01

Sheet 02

(a) Depending on the staking, install :

Refer to Fig. A-FBPAA Sheet 02 view C

3 Clamp NSA5516-13ND Item 63

or

3 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

1 Spacer NSA5527-03-01 Item 12

1 Spacer NSA5527-03-02 Item 14

1 Screw NAS1801-3-25 Item 33

1 Clip nut NSA5067-3-1 Item 43

1 Washer NAS1149F0332P Item 46

Or install :

Refer to Fig. A-FBPAA Sheet 02 view C

2 Clamp NSA5516-13ND Item 63

or

2 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

1 Spacer NSA5527-03-01 Item 12

1 Spacer NSA5527-03-02 Item 14

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 282

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@A300-600

SERVICE BULLETIN

1 Screw NAS1801-3-25 Item 33

1 Clip nut NSA5067-3-1 Item 43

1 Washer NAS1149F0332P Item 46

(b) Depending on the staking, install :

Refer to Fig. A-FBPAA Sheet 02 view D

3 Clamp NSA5516-13ND Item 63

or

3 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

1 Spacer NSA5527-03-02 Item 14

1 Screw NAS1801-3-25 Item 33

1 Clip nut NSA5067-3-1 Item 43

1 Washer NAS1149F0332P Item 46

Or install :

Refer to Fig. A-FBPAA Sheet 02 view D

2 Clamp NSA5516-13ND Item 63

or

2 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

1 Spacer NSA5527-03-02 Item 14

1 Screw NAS1801-3-25 Item 33

1 Clip nut NSA5067-3-1 Item 43

1 Washer NAS1149F0332P Item 46

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 283

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Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

(18) Subtask 246103-420-004-001 - Install the clamps of the Passage Way at FR52 (RH

side) - ADDITIONAL WORK

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills NON SPECIFIC

Material necessary to do the job

Supplementary kit 246103A02S03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

46 NAS1149F0332P 3 WASHER

63 NSA5516-13ND 4 CLAMP

64 NSA5516-31ND 4 CLAMP

References

Fig. A-FBVAA

Modification of the Routing of the

Passage Way at FR52 (RH side) -

ADDITIONAL WORK

Sheet 01

Sheet 02

(a) Install :

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

4 Clamp NSA5516-13ND Item 63

or

4 Clamp NSA5516-31ND Item 64

NOTE: Install the clamp Item 63 or 64 according to the bundle diameter.

3 Washer NAS1149F0332P Item 46

2 Screw Item (47) Retained at

removal

1 Screw Item (74) Retained at

removal

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 284

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@A300-600

SERVICE BULLETIN

**CONF 003

(1) Subtask 246103-831-028-002 - Modify the routing on rib 1 on the passage way to

the shroud box at LH side, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

570 Work location Rib 1

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 246103A04R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

12 NSA5527-03-01 1 SPACER

13 NSA5527-03-03 1 SPACER

14 NSA5527-03-02 3 SPACER

21 NSA5050-3 4 NUT

23 NSA935401-05 2 TIE

26 NSA935401-04 2 TIE

33 NAS1801-3-25 1 SCREW

46 NAS1149F0332P 6 WASHER

51 NSA5516-12ND 15 CLAMP

52 NSA5516-08ND 15 CLAMP

62 NAS1801-3-22 1 SCREW

63 NSA5516-13ND 15 CLAMP

64 NSA5516-31ND 15 CLAMP

66 NSA935401-13 2 TIE

84 NSA5527-03-06 1 SPACER

87 NSA360002 1 (M) EXTRUSIN

91 NSA5527-03-15 2 SPACER

92 NSA5527-03-12 1 SPACER

94 NSA5159-35 1 STUD

95 NSA5527-03-18 2 SPACER

96 NSA5527-03-09 1 SPACER

Supplementary kit 246103A01S03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

24 NSA939510BN 1 (M) STRIP

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 285

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@A300-600

SERVICE BULLETIN

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Epoxy Adhesive-Metal To

Metal - Legacy

05EJL9 As required

Epoxy Adhesive - Legacy 3 05EML7 As required

Contact Adhesive-Rubber &

Plastic Bonding Neopren

05JBC9 As required

Non Aqueous Cleaner -

Isopropyl Alcohol

08BBD1 As required

References

Process and Material Specification

(PMS)

Process and Material Specification (PMS)

01-01-28 Process E

Fig. A-FBMAB

Modification of the Clamps on the

Passage Way to the Shroud Box (LH

and RH side) - ADDITIONAL WORK

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

(a) Depending of the stacking, remove:

Refer to Fig. A-FBMAB Sheet 01 and Fig. A-FBMAB Sheet 03 view A-A

1 Nut Item (21) Discard

5 Clamp Item (51) Discard

or

5 Clamp Item (52) Discard

or

5 Clamp Item (63) Discard

or

5 Clamp Item (64) Discard

1 Spacer Item (91) Discard

1 Spacer Item (92) Discard

1 Spacer Item (93) Discard

1 Washer Item (46) Discard

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SERVICE BULLETIN

(b) Depending of the stacking, remove:

Refer to Fig. A-FBMAB Sheet 01 and Fig. A-FBMAB Sheet 03 view B-B

1 Nut Item (21) Discard

5 Clamp Item (51) Discard

or

5 Clamp Item (52) Discard

or

5 Clamp Item (63) Discard

or

5 Clamp Item (64) Discard

1 Spacer Item (14) Discard

1 Spacer Item (91) Discard

1 Spacer Item (84) Discard

1 Spacer Item (97) Discard

1 Washer Item (46) Discard

(c) Depending of the stacking, remove:

Refer to Fig. A-FBMAB Sheet 01 and Fig. A-FBMAB Sheet 04 view C-C

1 Screw Item (33) Discard

1 Screw Item (62) Discard

2 Washer Item (46) Discard

5 Clamp Item (51) Discard

or

5 Clamp Item (52) Discard

or

5 Clamp Item (63) Discard

or

5 Clamp Item (64) Discard

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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SERVICE BULLETIN

1 Spacer Item (84) Discard

2 Spacer Item (95) Discard

3 Spacer Item (93) Discard

(d) Install:

Refer to Fig. A-FBMAB Sheet 01 and Fig. A-FBMAB Sheet 05 view D-D

1 Stud NSA5159-35 Item 94

1 Nut NSA5050-3 Item 21

3 Clamp NSA5516-12ND Item 51

or

3 Clamp NSA5516-08ND Item 52

or

3 Clamp NSA5516-13ND Item 63

or

3 Clamp NSA5516-31ND Item 64

1 Spacer NSA5527-03-15 Item 91

1 Spacer NSA5527-03-12 Item 92

1 Spacer NSA5527-03-03 Item 13

1 Nut NSA5050-3 Item 21

2 Washer NAS1149F0332P Item 46

(e) Install:

Refer to Fig. A-FBMAB Sheet 01 and Fig. A-FBMAB Sheet 05 view E-E

1 Nut NSA5050-3 Item 21

2 Clamp NSA5516-08ND Item 52

or

2 Clamp NSA5516-12ND Item 51

2 Clamp NSA5516-13ND Item 63

or

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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2 Clamp NSA5516-31ND Item 64

2 Spacer NSA5527-03-02 Item 14

1 Washer NAS1149F0332P Item 46

(f) Install:

Refer to Fig. A-FBMAB Sheet 01 and Fig. A-FBMAB Sheet 06 and view F-F

1 Nut NSA5050-3 Item 21

5 Clamp NSA5516-08ND Item 52

or

5 Clamp NSA5516-12ND Item 51

or

5 Clamp NSA5516-13ND Item 63

or

5 Clamp NSA5516-31ND Item 64

1 Spacer NSA5527-03-02 Item 14

1 Spacer NSA5527-03-15 Item 91

1 Spacer NSA5527-03-06 Item 84

1 Washer NAS1149F0332P Item 46

(g) Install:

Refer to Fig. A-FBMAB Sheet 01 and Fig. A-FBMAB Sheet 06 view G-G

1 Screw NAS1801-3-22 Item 62

1 Washer NAS1149F0332P Item 46

3 Clamp NSA5516-08ND Item 52

or

3 Clamp NSA5516-12ND Item 51

or

3 Clamp NSA5516-13ND Item 63

or

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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3 Clamp NSA5516-31ND Item 64

1 Spacer NSA5527-03-09 Item 96

(h) Install:

Refer to Fig. A-FBMAB Sheet 01 and Fig. A-FBMAB Sheet 06 view H-H

1 Screw NAS1801-3-25 Item 33

1 Washer NAS1149F0332P Item 46

2 Clamp NSA5516-08ND Item 52

or

2 Clamp NSA5516-12ND Item 51

or

2 Clamp NSA5516-13ND Item 63

or

2 Clamp NSA5516-31ND Item 64

2 Spacer NSA5527-03-18 Item 95

(i) Install:

Refer to Fig. A-FBMAB Sheet 01 and Fig. A-FBMAB Sheet 06 view J-J

2 Tie-Cable NSA935401-13 Item 66

or

2 Tie-Cable NSA935401-04 Item 26

or

2 Tie-Cable NSA935401-05 Item 23

1 Spacer NSA5527-03-01 Item 12

(j) Install:

Refer to Fig. A-FBMAB Sheet 01 and Fig. A-FBMAB Sheet 05

1 (M) Extrusion NSA360002 Item 87

with:

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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SERVICE BULLETIN

Contact AdhesiveRubber & Plastic

Bonding Neopren

05JBC9 As required

(k) Modify the grommet installation :

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

1 Remove :

1 (M) Strip-Protective Item (24) Discard

2 Install :

Refer to Process and Material Specification (PMS) 01-01-28 Process E

1 (M) Strip-Protective NSA939510BN Item 24

NOTE: Install the Strip-Protective Item 24 with:

Epoxy AdhesiveMetal To Metal -

Legacy

05EJL9 As required

NOTE: Do the abrading and cleaning of the contact zones of StripProtective Item 24, on the structure with:

Non Aqueous

Cleaner - Isopropyl

Alcohol

08BBD1 As required

Epoxy Adhesive -

Legacy 3

05EML7 As required

(2) Subtask 246103-831-020-002 - Modify the routing on rib 1 on the passage way to

the shroud box at RH side, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

670 Work location Rib 1

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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Material necessary to do the job

Kit 246103A04R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

24 NSA939510BN 1 (M) STRIP

Kit 246103A05R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

12 NSA5527-03-01 1 SPACER

13 NSA5527-03-03 1 SPACER

14 NSA5527-03-02 3 SPACER

21 NSA5050-3 4 NUT

23 NSA935401-05 2 TIE

26 NSA935401-04 2 TIE

33 NAS1801-3-25 1 SCREW

46 NAS1149F0332P 6 WASHER

51 NSA5516-12ND 15 CLAMP

52 NSA5516-08ND 15 CLAMP

62 NAS1801-3-22 1 SCREW

63 NSA5516-13ND 15 CLAMP

64 NSA5516-31ND 15 CLAMP

66 NSA935401-13 2 TIE

84 NSA5527-03-06 1 SPACER

87 NSA360002 1 (M) EXTRUSIN

91 NSA5527-03-15 2 SPACER

92 NSA5527-03-12 1 SPACER

94 NSA5159-35 1 STUD

95 NSA5527-03-18 2 SPACER

96 NSA5527-03-09 1 SPACER

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Epoxy Adhesive-Metal To

Metal - Legacy

05EJL9 As required

Epoxy Adhesive - Legacy 3 05EML7 As required

Contact Adhesive-Rubber &

Plastic Bonding Neopren

05JBC9 As required

Non Aqueous Cleaner -

Isopropyl Alcohol

08BBD1 As required

References

Process and Material Specification

(PMS)

Process and Material Specification (PMS)

01-01-28 Process E

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References

Fig. A-FBMAB

Modification of the Clamps on the

Passage Way to the Shroud Box (LH

and RH side) - ADDITIONAL WORK

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

(a) Depending on the stacking, remove:

Refer to Fig. A-FBMAB Sheet 01 and Fig. A-FBMAB Sheet 03 view A-A

1 Nut Item (21) Discard

5 Clamp Item (51) Discard

or

5 Clamp Item (52) Discard

or

5 Clamp Item (63) Discard

or

5 Clamp Item (64) Discard

1 Spacer Item (91) Discard

1 Spacer Item (92) Discard

1 Spacer Item (93) Discard

1 Washer Item (46) Discard

(b) Depending on the stacking, remove:

Refer to Fig. A-FBMAB Sheet 01 and Fig. A-FBMAB Sheet 03 view B-B

1 Nut Item (21) Discard

5 Clamp Item (51) Discard

or

5 Clamp Item (52) Discard

or

5 Clamp Item (63) Discard

or

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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5 Clamp Item (64) Discard

1 Spacer Item (14) Discard

1 Spacer Item (91) Discard

1 Spacer Item (84) Discard

1 Spacer Item (97) Discard

1 Washer Item (46) Discard

(c) Depending on the stacking, remove:

Refer to Fig. A-FBMAB Sheet 01 and Fig. A-FBMAB Sheet 04 view C-C

1 Screw Item (33) Discard

1 Screw Item (62) Discard

2 Washer Item (46) Discard

5 Clamp Item (51) Discard

or

5 Clamp Item (52) Discard

or

5 Clamp Item (63) Discard

or

5 Clamp Item (64) Discard

1 Spacer Item (84) Discard

2 Spacer Item (95) Discard

3 Spacer Item (93) Discard

(d) Install:

Refer to Fig. A-FBMAB Sheet 01 and Fig. A-FBMAB Sheet 05 view D-D

1 Stud NSA5159-35 Item 94

1 Nut NSA5050-3 Item 21

3 Clamp NSA5516-12ND Item 51

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or

3 Clamp NSA5516-08ND Item 52

or

3 Clamp NSA5516-13ND Item 63

or

3 Clamp NSA5516-31ND Item 64

1 Spacer NSA5527-03-15 Item 91

1 Spacer NSA5527-03-12 Item 92

1 Spacer NSA5527-03-03 Item 13

1 Nut NSA5050-3 Item 21

2 Washer NAS1149F0332P Item 46

(e) Install:

Refer to Fig. A-FBMAB Sheet 01 and Fig. A-FBMAB Sheet 05 view E-E

1 Nut NSA5050-3 Item 21

2 Clamp NSA5516-08ND Item 52

or

2 Clamp NSA5516-12ND Item 51

or

2 Clamp NSA5516-13ND Item 63

or

2 Clamp NSA5516-31ND Item 64

2 Spacer NSA5527-03-02 Item 14

1 Washer NAS1149F0332P Item 46

(f) Install:

Refer to Fig. A-FBMAB Sheet 01 and Fig. A-FBMAB Sheet 06 view F-F

1 Nut NSA5050-3 Item 21

5 Clamp NSA5516-08ND Item 52

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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or

5 Clamp NSA5516-12ND Item 51

or

5 Clamp NSA5516-13ND Item 63

or

5 Clamp NSA5516-31ND Item 64

1 Spacer NSA5527-03-02 Item 14

1 Spacer NSA5527-03-15 Item 91

1 Spacer NSA5527-03-06 Item 84

1 Washer NAS1149F0332P Item 46

(g) Install:

Refer to Fig. A-FBMAB Sheet 01 and Fig. A-FBMAB Sheet 06 view G-G

1 Screw NAS1801-3-22 Item 62

1 Washer NAS1149F0332P Item 46

3 Clamp NSA5516-08ND Item 52

or

3 Clamp NSA5516-12ND Item 51

or

3 Clamp NSA5516-13ND Item 63

or

3 Clamp NSA5516-31ND Item 64

1 Spacer NSA5527-03-09 Item 96

(h) Install:

Refer to Fig. A-FBMAB Sheet 01 and Fig. A-FBMAB Sheet 06 view H-H

1 Screw NAS1801-3-25 Item 33

1 Washer NAS1149F0332P Item 46

2 Clamp NSA5516-08ND Item 52

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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or

2 Clamp NSA5516-12ND Item 51

or

2 Clamp NSA5516-13ND Item 63

or

2 Clamp NSA5516-31ND Item 64

2 Spacer NSA5527-03-18 Item 95

(i) Install:

Refer to Fig. A-FBMAB Sheet 01 and Fig. A-FBMAB Sheet 06 view J-J

2 Tie-Cable NSA935401-13 Item 66

or

2 Tie-Cable NSA935401-04 Item 26

or

2 Tie-Cable NSA935401-05 Item 23

1 Spacer NSA5527-03-01 Item 12

(j) Install:

Refer to Fig. A-FBMAB Sheet 01 and Fig. A-FBMAB Sheet 05

1 (M) Extrusion NSA360002 Item 87

with:

Contact AdhesiveRubber & Plastic

Bonding Neopren

05JBC9 As required

(k) Modify the grommet installation :

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

1 Remove :

1 (M) Strip-Protective Item (24) Discard

2 Install :

Refer to Process and Material Specification (PMS) 01-01-28 Process E

1 (M) Strip-Protective NSA939510BN Item 24

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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NOTE: Install the Strip-Protective Item 24 with:

Epoxy AdhesiveMetal To Metal -

Legacy

05EJL9 As required

NOTE: Do the abrading and cleaning of the contact zones of StripProtective Item 24, on the structure with:

Non Aqueous

Cleaner - Isopropyl

Alcohol

08BBD1 As required

and install the Strip-Protective Item 24 with:

Epoxy Adhesive -

Legacy 3

05EML7 As required

(3) Subtask 246103-831-021-001 - Modify the routing of routes 1P and 2P in the

shroud box at LH side, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

571

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Supplementary kit 246103A01S03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

19 NSA935807-09 14 CLAMP

20 NSA935808-01 7 WASHER

34 NSA5527-03-08 7 SPACER

62 NAS1801-3-22 14 SCREW

References

Fig. A-FBNAA

Modification of the Routing of Routes 1P

and 2P in the Shroud Box (LH side) -

ADDITIONAL WORK

Sheet 01

Sheet 02

(a) Remove :

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

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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14 Clamp Item (19) Retain

7 Screw Item (22) Discard

7 Washer Item (20) Retain

7 Spacer Item (34) Retain

(b) Or remove :

14 Clamp Item (19) Discard

7 Screw Item (22) Discard

7 Washer Item (20) Discard

(c) Install :

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

14 Clamp Item (19) Retained at

removal

7 Screw NAS1801-3-22 Item 62

7 Washer Item (20) Retained at

removal

7 Spacer Item (34) Retained at

removal

(d) Or install :

14 Clamp NSA935807-09 Item 19

7 Spacer NSA5527-03-08 Item 34

7 Screw NAS1801-3-22 Item 62

7 Washer NSA935808-01 Item 20

(4) Subtask 246103-831-024-001 - Modify the routing of the routes 1E and 1G in the

leading edge at LH wing, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

513

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Supplementary kit 246103A01S03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

66 NSA935401-08 2 TIE

References

Fig. A-FBQAA

Modification of the Routing in the

Leading Edge (LH and RH side) -

ADDITIONAL WORK

Sheet 01

(a) Remove :

Refer to Fig. A-FBQAA Sheet 01

2 Tie-Cable NSA935401-05 Item (23) Discard

(b) Install :

Refer to Fig. A-FBQAA Sheet 01

2 Tie-Cable NSA935401-08 Item 66

(5) Subtask 246103-831-025-001 - Modify the routing of the routes 2E and 2G in the

leading edge at RH wing, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

613

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 300

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SERVICE BULLETIN

Material necessary to do the job

Supplementary kit 246103A02S03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

66 NSA935401-08 2 TIE

References

Fig. A-FBQAA

Modification of the Routing in the

Leading Edge (LH and RH side) -

ADDITIONAL WORK

Sheet 01

(a) Remove :

Refer to Fig. A-FBQAA Sheet 01

2 Tie-Cable NSA935401-05 Item (23) Discard

(b) Install :

Refer to Fig. A-FBQAA Sheet 01

2 Tie-Cable NSA935401-08 Item 66

(6) Subtask 246103-400-001-001 - Install a support on the support of the BLUE

hydraulic reservoir at LH wing, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

571 Work location from Frame 47 to Frame 48

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 246103A01R14

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2528-3 2 NUT

EN6115V3-4 2 BOLT

Supplementary kit 246103A01S03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

20 NSA935808-01 1 WASHER

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SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

31 NAS1801-3-11 1 SCREW

67 A0041113300000 1 BRACKET

68 ASNA2050DXJ4828 2 RIVET

69 NSA935807-06 1 CLAMP

Supplementary kit 246103A01S13

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

100 ASNA2050DXJ5613 2 RIVET

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Primer Epoxy Paint - TSA

Anodizing Corrosion

Inhibiting Structure

04DEB2 As required

Primer Polyurethane Paint -

Corrosion Inhibiting

04EAC2 As required

Top Coat Polyurethane -

Grey Internal Structure

04JME4 As required

Polysulfide Sealant -

General Purpose Interfay

06AAC1

Polysulfide Sealant-Fuel

Tank Fillet

06ABB1 As required

Non Aqueous Cleaner -

General

08BAA9 As required

Corrosion Preventive

Compound-Water

Displacing

12ADB1 As required

References

Fig. A-FBRAA

Installation of a Support on the Support

of the BLUE Hydraulic Reservoir (LH

wing) - ADDITIONAL WORK

Sheet 01

Sheet 02

Sheet 03

(a) Remove :

Refer to Fig. A-FBRAA Sheet 01

1 Support Item (35) Discard

2 Screw Item (37) Discard

2 Washer Item (36) Discard

2 Nut Item (21) Discard

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(b) Blank the existing holes with:

2 Rivet ASNA2050DXJ5613 Item 100

NOTE: Wet install the rivets with:

Primer Epoxy Paint

- TSA Anodizing

Corrosion Inhibiting

Structure

04DEB2 As required

(c) Install the new support :

Refer to Fig. A-FBRAA Sheet 01, Fig. A-FBRAA Sheet 02 and Fig. A-FBRAA Sheet

03

1 Remove :

2 Rivet Item (68) Discard

NOTE: Clean the area with :

Non Aqueous

Cleaner - General

08BAA9 As required

2 Install the bracket Item 67.

a Put the bracket Item 67 in position.

b Drill two holes on the bracket Item 67 to a diameter comprised between

4.85 mm (0.191 in.) and 4.95 mm (0.195 in.) to match the holes of the

structure.

c Wet install :

1 Bracket A0041113300000 Item 67

2 Rivet ASNA2050DXJ4828 Item 68

NOTE: If the installation of bracket Item 67 with the rivets is not

possible, attach with:

2 Bolt EN6115V3-4

2 Nut ASNA2528-3

NOTE: Between the bracket Item 67 and the structure, apply :

Polysulfide SealantFuel Tank Fillet06ABB1 As required

NOTE: Wet install the rivets with :

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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SERVICE BULLETIN

Polysulfide Sealant

- General Purpose

Interfay

06AAC1 As required

NOTE: Apply on the head of the rivets :

Primer

Polyurethane Paint

- Corrosion

Inhibiting

04EAC2 As required

Top Coat

Polyurethane - Grey

Internal Structure

04JME4 As required

NOTE: On the modified area, apply :

Corrosion

Preventive

Compound-Water

Displacing

12ADB1 As required

3 Attach the sleeve to the bracket with :

1 Clamp NSA935807-06 Item 69

1 Screw NAS1801-3-11 Item 31

1 Washer NSA935808-01 Item 20

(7) Subtask 246103-400-002-001 - Install a bracket on the shroud box blanking plate at

LH side, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

147 Work location Frame 51

from Stringer 31 to Stringer 33

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Supplementary kit 246103A01S03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

21 NSA5050-3 3 NUT

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SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

28 A0041113420000 1 BRACKET

30 NAS1801-3-8 2 SCREW

37 NAS1801-3-9 1 SCREW

63 NSA5516-13ND 2 CLAMP

64 NSA5516-31ND 2 CLAMP

70 A0041113500000 1 CLAMP

71 NAS1801-3-12 2 SCREW

75 A0041113500200 1 CLAMP

76 A0041113500400 1 CLAMP

Supplementary kit 246103A02S03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

46 NAS1149F0332P 2 WASHER

References

Fig. A-FBSAA

Installation of a Bracket on the Shroud

Box Blanking Plate (LH and RH side) -

ADDITIONAL WORK

Sheet 01

Sheet 02

(a) Remove :

Refer to Fig. A-FBSAA Sheet 01

2 Screw Item (27) Discard

2 Washer Item (46) Discard

(b) Install the bracket :

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

1 Bracket A0041113420000 Item 28

2 Screw NAS1801-3-12 Item 71

2 Washer NAS1149F0332P Item 46

(c) Attach the bundles on the shroud box bracket :

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

1 Attach the bundles with :

2 Clamp NSA5516-13ND Item 63

or

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 305

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2 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

NOTE: Two or three bundles may be installed.

attach with :

1 Nut NSA5050-3 Item 21

and

1 Screw NAS1801-3-9 Item 37

2 Or attach the bundles with :

1 Clamp NSA5516-13ND Item 63

or

1 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

NOTE: Two or three bundles may be installed.

and

1 Clamp A0041113500000 Item 70

or

1 Clamp A0041113500200 Item 75

or

1 Clamp A0041113500400 Item 76

NOTE: Install clamp Item 70 or 75 or 76 according to the bundle

diameters.

attach with :

2 Nut NSA5050-3 Item 21

2 Screw NAS1801-3-8 Item 30

(8) Subtask 246103-400-003-001 - Install a bracket on the shroud box blanking plate at

RH side, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

148 Work location Frame 51

from Stringer 31 to Stringer 33

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Supplementary kit 246103A02S03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

21 NSA5050-3 3 NUT

29 A0041113420100 1 BRACKET

30 NAS1801-3-8 2 SCREW

37 NAS1801-3-9 1 SCREW

46 NAS1149F0332P 2 WASHER

63 NSA5516-13ND 2 CLAMP

64 NSA5516-31ND 2 CLAMP

70 A0041113500000 1 CLAMP

71 NAS1801-3-12 2 SCREW

75 A0041113500200 1 CLAMP

76 A0041113500400 1 CLAMP

References

Fig. A-FBSAA

Installation of a Bracket on the Shroud

Box Blanking Plate (LH and RH side) -

ADDITIONAL WORK

Sheet 01

Sheet 02

(a) Remove :

Refer to Fig. A-FBSAA Sheet 01

2 Screw Item (27) Discard

2 Washer Item (46) Discard

(b) Install the bracket :

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

1 Bracket A0041113420100 Item 29

attach with :

2 Screw NAS1801-3-12 Item 71

2 Washer NAS1149F0332P Item 46

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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(c) Attach the bundles on the shroud box bracket :

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

1 Attach the bundles with :

2 Clamp NSA5516-13ND Item 63

or

2 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

NOTE: Two or three bundles may be installed.

attach with :

1 Nut NSA5050-3 Item 21

1 Screw NAS1801-3-9 Item 37

2 Or attach the bundles with :

1 Clamp NSA5516-13ND Item 63

or

1 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

NOTE: Two or three bundles may be installed.

and

1 Clamp A0041113500000 Item 70

or

1 Clamp A0041113500200 Item 75

or

1 Clamp A0041113500400 Item 76

NOTE: Install clamp Item 70 or 75 or 76 according to the bundle

diameters.

attach with :

2 Nut NSA5050-3 Item 21

2 Screw NAS1801-3-8 Item 30

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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(9) Subtask 246103-020-004-001 - Remove the clamps between FR50 and FR51 at

STRG 32 at LH side, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

147 Work location from Frame 50 to Frame 51

Stringer 32

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills NON SPECIFIC

References

Fig. A-FBPAA

Modification of the Routing Between

FR50 and FR51 at STGR32 (LH and RH

side) - ADDITIONAL WORK

Sheet 01

Sheet 02

(a) Depending on the stacking, remove :

Refer to Fig. A-FBPAA Sheet 01

4 Clamp Item (16) Discard

2 Clamp Item (32) Discard

2 Spacer Item (14) Discard

2 Clip nut Item (43) Discard

2 Washer Item (20) Discard

2 Screw Item (33) Discard

Or remove :

Refer to Fig. A-FBPAA Sheet 01

4 Clamp Item (16) Discard

2 Spacer Item (14) Discard

2 Clip nut Item (43) Discard

2 Washer Item (20) Discard

2 Screw Item (33) Discard

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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(10) Subtask 246103-831-026-001 - Remove the clamps of the Passage Way at FR52 (LH

side) - ADDITIONAL WORK

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills NON SPECIFIC

References

Fig. A-FBTAA

Modification of the Routing of the

Passage Way at FR52 (LH side) -

ADDITIONAL WORK

Sheet 01

Sheet 02

(a) Remove :

Refer to Fig. A-FBTAA Sheet 01 andFig. A-FBTAA Sheet 02

4 Clamp Item (72) Discard

1 Washer Item (73) Discard

1 Screw Item (74) Retain

1 Clamp Item (44) Discard

1 Clamp Item (45) Discard

2 Washer Item (46) Discard

2 Screw Item (47) Retain

(11) Subtask 246103-831-029-001 - Modify the Routing between FR50 and FR52 and

between STGR 33 and 30 at LH side - ADDITIONAL WORK

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Supplementary kit 246103A01S03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

77 EN6049-007-19-5 7.5 (M) SLEEVE

78 EN6049-007-13-5 7.5 (M) SLEEVE

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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References

Fig. A-FBXAA

Modification of the Routing between

FR50 and FR52 (LH and RH side) -

ADDITIONAL WORK

Sheet 01

(a) Remove :

Refer to Fig. A-FBXAA Sheet 01

5 (M) Conduit Item (77) Discard

NOTE: A third conduit may be installed. If installed, remove it.

(b) Install :

Refer to Fig. A-FBXAA Sheet 01

5 (M) Sleeve EN6049-007-13-5 Item 78

or

5 (M) Sleeve EN6049-007-19-5 Item 77

NOTE: Install the sleeve Item 77 or 78 according to the harness diameter.

NOTE: If a third conduit was installed, install :

2.5 (M) Sleeve EN6049-007-13-5 Item 78

or

2.5 (M) Sleeve EN6049-007-19-5 Item 77

NOTE: Install the sleeve Item 77 or 78 according to the harness diameter.

(12) Subtask 246103-420-005-001 - Install the clamps between FR50 and FR51 at STRG

32 at LH side, ADDITIONAL WORK

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills NON SPECIFIC

Material necessary to do the job

Supplementary kit 246103A01S03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

12 NSA5527-03-01 1 SPACER

14 NSA5527-03-02 2 SPACER

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

33 NAS1801-3-25 2 SCREW

43 NSA5067-3-1 2 NUT

46 NAS1149F0332P 4 WASHER

63 NSA5516-13ND 6 CLAMP

64 NSA5516-31ND 6 CLAMP

References

Fig. A-FBPAA

Modification of the Routing Between

FR50 and FR51 at STGR32 (LH and RH

side) - ADDITIONAL WORK

Sheet 01

Sheet 02

(a) Depending on the staking, install :

Refer to Fig. A-FBPAA Sheet 02 view C

3 Clamp NSA5516-13ND Item 63

or

3 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

1 Spacer NSA5527-03-01 Item 12

1 Spacer NSA5527-03-02 Item 14

1 Screw NAS1801-3-25 Item 33

3 Washer NAS1149F0332P Item 46

1 Clip nut NSA5067-3-1 Item 43

Or install :

Refer to Fig. A-FBPAA Sheet 02 view C

2 Clamp NSA5516-13ND Item 63

or

2 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

1 Spacer NSA5527-03-01 Item 12

1 Spacer NSA5527-03-02 Item 14

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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1 Screw NAS1801-3-25 Item 33

1 Washer NAS1149F0332P Item 46

1 Clip nut NSA5067-3-1 Item 43

(b) Depending on the staking, install :

Refer to Fig. A-FBPAA Sheet 02 view D

3 Clamp NSA5516-13ND Item 63

or

3 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

1 Spacer NSA5527-03-02 Item 14

1 Screw NAS1801-3-25 Item 33

1 Washer NAS1149F0332P Item 46

1 Clip nut NSA5067-3-1 Item 43

Or install :

Refer to Fig. A-FBPAA Sheet 02 view D

2 Clamp NSA5516-13ND Item 63

or

2 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

1 Spacer NSA5527-03-02 Item 14

1 Screw NAS1801-3-25 Item 33

1 Washer NAS1149F0332P Item 46

1 Clip nut NSA5067-3-1 Item 43

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(13) Subtask 246103-420-003-001 - Install the clamps of the Passage Way at FR52 (LH

side) - ADDITIONAL WORK

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills NON SPECIFIC

Material necessary to do the job

Supplementary kit 246103A01S03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

63 NSA5516-13ND 4 CLAMP

64 NSA5516-31ND 4 CLAMP

Supplementary kit 246103A02S03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

46 NAS1149F0332P 3 WASHER

References

Fig. A-FBTAA

Modification of the Routing of the

Passage Way at FR52 (LH side) -

ADDITIONAL WORK

Sheet 01

Sheet 02

(a) Install :

Refer to Fig. A-FBTAA Sheet 01 andFig. A-FBTAA Sheet 02

4 Clamp NSA5516-13ND Item 63

or

4 Clamp NSA5516-31ND Item 64

NOTE: Install the clamp Item 63 or 64 according to the bundle diameter.

3 Washer NAS1149F0332P Item 46

2 Screw Item (47) Retained at

removal

1 Screw Item (74) Retained at

removal

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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(14) Subtask 246103-020-005-001 - Remove the clamps between FR50 and FR51 at

STGR 32 at RH side, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

148 Work location from Frame 50 to Frame 51

Stringer 32

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills NON SPECIFIC

References

Fig. A-FBPAA

Modification of the Routing Between

FR50 and FR51 at STGR32 (LH and RH

side) - ADDITIONAL WORK

Sheet 01

Sheet 02

(a) Depending on the stacking, remove :

Refer to Fig. A-FBPAA Sheet 01

4 Clamp Item (16) Discard

2 Clamp Item (32) Discard

2 Spacer Item (14) Discard

2 Clip nut Item (43) Discard

2 Washer Item (20) Discard

2 Screw Item (33) Discard

Or remove :

Refer to Fig. A-FBPAA Sheet 01

4 Clamp Item (16) Discard

2 Spacer Item (14) Discard

2 Clip nut Item (43) Discard

2 Washer Item (20) Discard

2 Screw Item (33) Discard

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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(15) Subtask 246103-831-027-001 - Remove the clamps of the Passage Way at FR52

(RH side) - ADDITIONAL WORK

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills NON SPECIFIC

References

Fig. A-FBVAA

Modification of the Routing of the

Passage Way at FR52 (RH side) -

ADDITIONAL WORK

Sheet 01

Sheet 02

(a) Remove :

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

4 Clamp Item (72) Discard

1 Washer Item (73) Discard

1 Screw Item (74) Retain

1 Clamp Item (44) Discard

1 Clamp Item (45) Discard

2 Washer Item (46) Discard

2 Screw Item (47) Retain

(16) Subtask 246103-831-030-001 - Modify the Routing between FR50 and FR52 and

between STGR 33 and 30 at RH side - ADDITIONAL WORK

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Supplementary kit 246103A02S03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

77 EN6049-007-19-5 7.5 (M) SLEEVE

78 EN6049-007-13-5 7.5 (M) SLEEVE

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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References

Fig. A-FBXAA

Modification of the Routing between

FR50 and FR52 (LH and RH side) -

ADDITIONAL WORK

Sheet 01

(a) Remove :

Refer to Fig. A-FBXAA Sheet 01

5 (M) Conduit Item (77) Discard

NOTE: A third conduit may be installed. If installed, remove it.

(b) Install :

Refer to Fig. A-FBXAA Sheet 01

5 (M) Sleeve EN6049-007-13-5 Item 78

or

5 (M) Sleeve EN6049-007-19-5 Item 77

NOTE: Install the sleeve Item 77 or 78 according to the harness diameter.

NOTE: If a third conduit was installed, install :

2.5 (M) Sleeve EN6049-007-13-5 Item 78

or

2.5 (M) Sleeve EN6049-007-19-5 Item 77

NOTE: Install the sleeve Item 77 or 78 according to the harness diameter.

(17) Subtask 246103-420-006-001 - Install the clamps between FR50 and FR51 at STGR

32 at RH side, ADDITIONAL WORK

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills NON SPECIFIC

Material necessary to do the job

Supplementary kit 246103A02S03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

12 NSA5527-03-01 1 SPACER

14 NSA5527-03-02 2 SPACER

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

33 NAS1801-3-25 2 SCREW

43 NSA5067-3-1 2 NUT

46 NAS1149F0332P 2 WASHER

63 NSA5516-13ND 6 CLAMP

64 NSA5516-31ND 6 CLAMP

References

Fig. A-FBPAA

Modification of the Routing Between

FR50 and FR51 at STGR32 (LH and RH

side) - ADDITIONAL WORK

Sheet 01

Sheet 02

(a) Depending on the staking, install :

Refer to Fig. A-FBPAA Sheet 02 view C

3 Clamp NSA5516-13ND Item 63

or

3 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

1 Spacer NSA5527-03-01 Item 12

1 Spacer NSA5527-03-02 Item 14

1 Screw NAS1801-3-25 Item 33

1 Clip nut NSA5067-3-1 Item 43

1 Washer NAS1149F0332P Item 46

Or install :

Refer to Fig. A-FBPAA Sheet 02 view C

2 Clamp NSA5516-13ND Item 63

or

2 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

1 Spacer NSA5527-03-01 Item 12

1 Spacer NSA5527-03-02 Item 14

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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1 Screw NAS1801-3-25 Item 33

1 Clip nut NSA5067-3-1 Item 43

1 Washer NAS1149F0332P Item 46

(b) Depending on the staking, install :

Refer to Fig. A-FBPAA Sheet 02 view D

3 Clamp NSA5516-13ND Item 63

or

3 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

1 Spacer NSA5527-03-02 Item 14

1 Screw NAS1801-3-25 Item 33

1 Clip nut NSA5067-3-1 Item 43

1 Washer NAS1149F0332P Item 46

Or install :

Refer to Fig. A-FBPAA Sheet 02 view D

2 Clamp NSA5516-13ND Item 63

or

2 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

1 Spacer NSA5527-03-02 Item 14

1 Screw NAS1801-3-25 Item 33

1 Clip nut NSA5067-3-1 Item 43

1 Washer NAS1149F0332P Item 46

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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(18) Subtask 246103-420-004-001 - Install the clamps of the Passage Way at FR52 (RH

side) - ADDITIONAL WORK

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills NON SPECIFIC

Material necessary to do the job

Supplementary kit 246103A02S03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

46 NAS1149F0332P 3 WASHER

63 NSA5516-13ND 4 CLAMP

64 NSA5516-31ND 4 CLAMP

References

Fig. A-FBVAA

Modification of the Routing of the

Passage Way at FR52 (RH side) -

ADDITIONAL WORK

Sheet 01

Sheet 02

(a) Install :

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

4 Clamp NSA5516-13ND Item 63

or

4 Clamp NSA5516-31ND Item 64

NOTE: Install the clamp Item 63 or 64 according to the bundle diameter.

3 Washer NAS1149F0332P Item 46

2 Screw Item (47) Retained at

removal

1 Screw Item (74) Retained at

removal

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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**CONF ALL

D. TEST

**CONF 001

(1) Subtask 246103-700-002-001 - Testing

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 27-54-41, Page Block 401

29-12-46, Page Block 401

(a) Job set-up

1 Remove the safety clips and tags and close the circuit breakers as specified

after the installation of the inner flap deflectors (Refer to AMM 27-54-41, Page

Block 401).

2 Remove the safety clips and tags and close the circuit breakers as specified

after the installation of the BLUE hydraulic reservoir (Refer to AMM 29-12-46,

Page Block 401).

(b) Procedure

1 Do the test procedure as specified after the installation of the inner flap

deflectors (Refer to AMM 27-54-41, Page Block 401).

2 Do the test procedure as specified after the installation of the BLUE hydraulic

reservoir (Refer to AMM 29-12-46, Page Block 401).

**CONF 002

(1) Subtask 246103-700-002-001 - Testing

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 27-54-41, Page Block 401

29-12-46, Page Block 401

(a) Job set-up

1 Remove the safety clips and tags and close the circuit breakers as specified

after the installation of the inner flap deflectors (Refer to AMM 27-54-41, Page

Block 401).

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2 Remove the safety clips and tags and close the circuit breakers as specified

after the installation of the BLUE hydraulic reservoir (Refer to AMM 29-12-46,

Page Block 401).

(b) Procedure

1 Do the test procedure as specified after the installation of the inner flap

deflectors (Refer to AMM 27-54-41, Page Block 401).

2 Do the test procedure as specified after the installation of the BLUE hydraulic

reservoir (Refer to AMM 29-12-46, Page Block 401).

**CONF 003

(1) Subtask 246103-700-002-001 - Testing

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 27-54-41, Page Block 401

29-12-46, Page Block 401

(a) Job set-up

1 Remove the safety clips and tags and close the circuit breakers as specified

after the installation of the inner flap deflectors (Refer to AMM 27-54-41, Page

Block 401).

2 Remove the safety clips and tags and close the circuit breakers as specified

after the installation of the BLUE hydraulic reservoir (Refer to AMM 29-12-46,

Page Block 401).

(b) Procedure

1 Do the test procedure as specified after the installation of the inner flap

deflectors (Refer to AMM 27-54-41, Page Block 401).

2 Do the test procedure as specified after the installation of the BLUE hydraulic

reservoir (Refer to AMM 29-12-46, Page Block 401).

**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 246103-942-002-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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References

Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001

27-54-41, Page Block 401

32-12-11, Page Block 301

53-15-63, Page Block 401

(a) If removed, install the inner deflectors between Rib. 1 and Rib. 6, refer to AMM

27-54-41, Page Block 401.

(b) If removed, install the fairing panels 577AB, 577BB, 577DT, 577ET, 577FT, 677AB,

677BB, 677DT, 677ET and 677FT, refer to AMM 53-15-63, Page Block 401.

(c) Install the access panels 513AT, 513BT, 571BB, 571CB, 571DB, 613AT and

613BT, refer to AMM 06-41-57, Page Block 001.

(d) Install the access panels 512BB and 612BB, refer to AMM 06-41-57, Page Block

001.

(e) Close the Main Landing Gear (MLG) doors, refer to AMM 32-12-11, Page Block

301.

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

equipment.

(g) Remove the access platform(s).

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

**CONF 002

(1) Subtask 246103-942-002-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001

27-54-41, Page Block 401

32-12-11, Page Block 301

53-15-63, Page Block 401

(a) If removed, install the inner deflectors between Rib. 1 and Rib. 6, refer to AMM

27-54-41, Page Block 401.

(b) If removed, install the fairing panels 577AB, 577BB, 577DT, 577ET, 577FT, 677AB,

677BB, 677DT, 677ET and 677FT, refer to AMM 53-15-63, Page Block 401.

(c) Install the access panels 513AT, 513BT, 571BB, 571CB, 571DB, 613AT and

613BT, refer to AMM 06-41-57, Page Block 001.

(d) Install the access panels 512BB and 612BB, refer to AMM 06-41-57, Page Block

001.

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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@A300-600

SERVICE BULLETIN

(e) Close the Main Landing Gear (MLG) doors, refer to AMM 32-12-11, Page Block

301.

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

equipment.

(g) Remove the access platform(s).

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

**CONF 003

(1) Subtask 246103-942-002-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001

27-54-41, Page Block 401

32-12-11, Page Block 301

53-15-63, Page Block 401

(a) If removed, install the inner deflectors between Rib. 1 and Rib. 6, refer to AMM

27-54-41, Page Block 401.

(b) If removed, install the fairing panels 577AB, 577BB, 577DT, 577ET, 577FT, 677AB,

677BB, 677DT, 677ET and 677FT, refer to AMM 53-15-63, Page Block 401.

(c) Install the access panels 513AT, 513BT, 571BB, 571CB, 571DB, 613AT and

613BT, refer to AMM 06-41-57, Page Block 001.

(d) Install the access panels 512BB and 612BB, refer to AMM 06-41-57, Page Block

001.

(e) Close the Main Landing Gear (MLG) doors, refer to AMM 32-12-11, Page Block

301.

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

equipment.

(g) Remove the access platform(s).

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

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 324

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@A300-600

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Task 246103-831-804-001 - Modification - ADDITIONAL WORK between Revision No. 01 and

Revision No. 03

**CONF ALL

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

INCLUDED IN THE REFERENCED PROCEDURES.

CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP

ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY

AND MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENANCE

WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING,

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

THIS:

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

NECESSARY ON WIRING AND COMPONENTS.

- REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND

OTHER CONTAMINATION.

THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION

AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION.

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

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

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

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

authority he belongs to, the accepted alternative procedure can be used. When the

words "in accordance with" are used then the given procedure must be followed.

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

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

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

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

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

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

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

NOTE: This Service Bulletin is classified mandatory or expected to be classified mandatory

by an Airworthiness Directive (AD). The paragraphs 3.C. and 3.D. in these

accomplishment instructions are Required for Compliance (RC) and must be done

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

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

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

the aircraft can be put back into a serviceable condition.

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 325

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@A300-600

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Task Associated Data

**CONF 001

Zone

147 148 513 570 571 572 613 670 672

Manpower

TOTAL MANHOURS 30.50

ELAPSED TIME (HOURS) 16.50

**CONF 002

Zone

147 148 513 570 571 613 670

Manpower

TOTAL MANHOURS 30.50

ELAPSED TIME (HOURS) 16.50

**CONF 003

Zone

147 148 513 570 571 572 613 670 672

Manpower

TOTAL MANHOURS 30.50

ELAPSED TIME (HOURS) 16.50

**CONF ALL

A. GENERAL

**CONF 001

(1) Subtask 246103-839-003-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

(2) Subtask 246103-910-003-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

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

06-31-53, Page Block 001

20-21-12, Page Block 001

51-23-10

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 326

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@A300-600

SERVICE BULLETIN

References

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-25-51

20-33-00

20-33-30

20-33-42

20-33-44

20-33-45

Standards Manual (SM)

Structural Repair Manual (SRM) 51-21-00

51-23-10

51-40-00

51-40-20

51-40-30

51-40-40

51-75-10

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

the Consumable Materials List (CML).

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

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

(d) For the identification of the access panels, refer to AMM 06-21-00, Page Block 001

(e) Tag all the parts you must remove and retain to make the subsequent installation

easier.

(f) Put all the retained hardware in identified plastic bags and attach the bags to the

related unit.

(g) Obtain fastener hole diameters and drill data in accordance with SRM 51-40-40.

(h) For the installation of the protective electrical conduits, refer to ESPM 20-33-30.

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

Block 001).

(j) For alternative and substitute fasteners, refer to SRM 51-40-30.

(k) If alternative and substitute fasteners have to be used, you must make sure that the

associated nut/collar are compatible in accordance with SRM 51-40-00 "Mating

Part" column.

(l) If the length of any fastener specified in this Service Bulletin does not meet

installation standards given in SRM Chapter 51, then a fastener of the same

specification, or an approved substitute, with a length which meets the installation

standards given in SRM Chapter 51 may be used. In addition, washers may be

installed for fastener grip length in accordance with SRM Chapter 51.

(m) Remove and install fasteners in accordance with SRM 51-40-20.

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 327

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SERVICE BULLETIN

(n) For the cable tie application and tooling, refer to ESPM 20-33-44 and ESPM

20-25-51.

(o) Adapt the clamp size as necessary,, refer to ESPM 20-33-42.

(p) For repair of paint coatings, refer to SRM 51-75-10 and AMM 51-23-10.

(q) For the application of protective treatments, refer to SRM 51-21-00.

(r) For the general installation of electrical wire harnesses, refer to ESPM 20-33-00.

(s) For backshell, end piece and conduit fitting, refer to ESPM 20-33-45.

(t) Renew the protective finish in accordance with SRM 51-75-10.

**CONF 002

(1) Subtask 246103-839-003-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

(2) Subtask 246103-910-003-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

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

06-31-53, Page Block 001

20-21-12, Page Block 001

51-23-10

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-25-51

20-33-00

20-33-30

20-33-42

20-33-44

20-33-45

Standards Manual (SM)

Structural Repair Manual (SRM) 51-21-00

51-23-10

51-40-00

51-40-20

51-40-30

51-40-40

51-75-10

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 328

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

the Consumable Materials List (CML).

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

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

(d) For the identification of the access panels, refer to AMM 06-21-00, Page Block 001

(e) Tag all the parts you must remove and retain to make the subsequent installation

easier.

(f) Put all the retained hardware in identified plastic bags and attach the bags to the

related unit.

(g) Obtain fastener hole diameters and drill data in accordance with SRM 51-40-40.

(h) For the installation of the protective electrical conduits, refer to ESPM 20-33-30.

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

Block 001).

(j) For alternative and substitute fasteners, refer to SRM 51-40-30.

(k) If alternative and substitute fasteners have to be used, you must make sure that the

associated nut/collar are compatible in accordance with SRM 51-40-00 "Mating

Part" column.

(l) If the length of any fastener specified in this Service Bulletin does not meet

installation standards given in SRM Chapter 51, then a fastener of the same

specification, or an approved substitute, with a length which meets the installation

standards given in SRM Chapter 51 may be used. In addition, washers may be

installed for fastener grip length in accordance with SRM Chapter 51.

(m) Remove and install fasteners in accordance with SRM 51-40-20.

(n) For the cable tie application and tooling, refer to ESPM 20-33-44 and ESPM

20-25-51.

(o) Adapt the clamp size as necessary,, refer to ESPM 20-33-42.

(p) For repair of paint coatings, refer to SRM 51-75-10 and AMM 51-23-10.

(q) For the application of protective treatments, refer to SRM 51-21-00.

(r) For the general installation of electrical wire harnesses, refer to ESPM 20-33-00.

(s) For backshell, end piece and conduit fitting, refer to ESPM 20-33-45.

(t) Renew the protective finish in accordance with SRM 51-75-10.

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 329

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SERVICE BULLETIN

**CONF 003

(1) Subtask 246103-839-003-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

(2) Subtask 246103-910-003-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

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

06-31-53, Page Block 001

20-21-12, Page Block 001

51-23-10

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-25-51

20-33-00

20-33-30

20-33-42

20-33-44

20-33-45

Standards Manual (SM)

Structural Repair Manual (SRM) 51-21-00

51-23-10

51-40-00

51-40-20

51-40-30

51-40-40

51-75-10

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

the Consumable Materials List (CML).

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

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

(d) For the identification of the access panels, refer to AMM 06-21-00, Page Block 001

(e) Tag all the parts you must remove and retain to make the subsequent installation

easier.

(f) Put all the retained hardware in identified plastic bags and attach the bags to the

related unit.

(g) Obtain fastener hole diameters and drill data in accordance with SRM 51-40-40.

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 330

5

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@A300-600

SERVICE BULLETIN

(h) For the installation of the protective electrical conduits, refer to ESPM 20-33-30.

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

Block 001).

(j) For alternative and substitute fasteners, refer to SRM 51-40-30.

(k) If alternative and substitute fasteners have to be used, you must make sure that the

associated nut/collar are compatible in accordance with SRM 51-40-00 "Mating

Part" column.

(l) If the length of any fastener specified in this Service Bulletin does not meet

installation standards given in SRM Chapter 51, then a fastener of the same

specification, or an approved substitute, with a length which meets the installation

standards given in SRM Chapter 51 may be used. In addition, washers may be

installed for fastener grip length in accordance with SRM Chapter 51.

(m) Remove and install fasteners in accordance with SRM 51-40-20.

(n) For the cable tie application and tooling, refer to ESPM 20-33-44 and ESPM

20-25-51.

(o) Adapt the clamp size as necessary,, refer to ESPM 20-33-42.

(p) For repair of paint coatings, refer to SRM 51-75-10 and AMM 51-23-10.

(q) For the application of protective treatments, refer to SRM 51-21-00.

(r) For the general installation of electrical wire harnesses, refer to ESPM 20-33-00.

(s) For backshell, end piece and conduit fitting, refer to ESPM 20-33-45.

(t) Renew the protective finish in accordance with SRM 51-75-10.

**CONF ALL

B. PREPARATION

**CONF 001

(1) Subtask 246103-941-003-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001

24-00-00, Page Block 301

27-54-41, Page Block 401

32-12-11, Page Block 301

NOTE: The items given in this note shall be considered as the basic Aircraft

configuration before you start a maintenance task:

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 331

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SERVICE BULLETIN

- 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 24-00-00, Page

Block 301.

(b) Put an access platform in position at Zone(s) 513(613), 570(670), 571 , 572(672)

and 147(148).

(c) Open the Main Landing Gear (MLG) doors, refer to AMM 32-12-11, Page Block

301.

(d) Remove the access panels 512AB(612AB), 512BB(612BB), 512CB(612CB),

512DB(612DB), refer to AMM 06-41-57, Page Block 001.

(e) Remove the access panels 571BB, 571DB, refer to AMM 06-41-57, Page Block

001.

(f) Open all the necessary inner deflectors between Rib. 1 and Rib. 6, refer to AMM

27-54-41, Page Block 401.

**CONF 002

(1) Subtask 246103-941-003-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001

24-00-00, Page Block 301

27-54-41, Page Block 401

32-12-11, Page Block 301

NOTE: The items given in this note shall be considered as the basic Aircraft

configuration before you start a maintenance task:

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 332

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@A300-600

SERVICE BULLETIN

- 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 24-00-00, Page

Block 301.

(b) Put an access platform in position at Zone(s) 513(613), 570(670), 571 , 572(672)

and 147(148).

(c) Open the Main Landing Gear (MLG) doors, refer to AMM 32-12-11, Page Block

301.

(d) Remove the access panels 512AB(612AB), 512BB(612BB), 512CB(612CB),

512DB(612DB), refer to AMM 06-41-57, Page Block 001.

(e) Remove the access panels 571BB, 571DB, refer to AMM 06-41-57, Page Block

001.

(f) Open all the necessary inner deflectors between Rib. 1 and Rib. 6, refer to AMM

27-54-41, Page Block 401.

**CONF 003

(1) Subtask 246103-941-003-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001

24-00-00, Page Block 301

27-54-41, Page Block 401

32-12-11, Page Block 301

NOTE: The items given in this note shall be considered as the basic Aircraft

configuration before you start a maintenance task:

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 333

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@A300-600

SERVICE BULLETIN

- 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 24-00-00, Page

Block 301.

(b) Put an access platform in position at Zone(s) 513(613), 570(670), 571 , 572(672)

and 147(148).

(c) Open the Main Landing Gear (MLG) doors, refer to AMM 32-12-11, Page Block

301.

(d) Remove the access panels 512AB(612AB), 512BB(612BB), 512CB(612CB),

512DB(612DB), refer to AMM 06-41-57, Page Block 001.

(e) Remove the access panels 571BB, 571DB, refer to AMM 06-41-57, Page Block

001.

(f) Open all the necessary inner deflectors between Rib. 1 and Rib. 6, refer to AMM

27-54-41, Page Block 401.

**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 246103-020-006-001 - Remove the clamps between FR50 and FR52 at LH

side, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

147 Work location from Frame 50 to Frame 52

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 334

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@A300-600

SERVICE BULLETIN

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

References

Fig. A-FCAAA

Modification of the Routing of the

Passage Way at FR52 (LH Side) -

ADDITIONAL WORK

Sheet 01

Sheet 02

Fig. A-FCDAA

Modification of the Routing Between

FR50 and FR51 at STGR32 (LH and RH

Side) - ADDITIONAL WORK

Sheet 01

Sheet 02

(a) Remove:

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

4 Clamp Item (72) Discard

2 Screw Item (74) Retain

2 Washer Item (73) Discard

1 Seal fitting Item (41) Discard

1 Bracket assy Item (42) Discard

2 Clip nut Item (43) Discard

2 Clamp Item (63) Retain

or

2 Clamp Item (64) Retain

4 Screw Item (47) Retain

4 Washer Item (46) Discard

(b) Depending on the stacking, remove:

Refer to Fig. A-FCDAA Sheet 01

4 Clamp Item (16) Discard

2 Clamp Item (32) Discard

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 335

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@A300-600

SERVICE BULLETIN

2 Spacer Item (14) Discard

2 Clip nut Item (43) Discard

2 Washer Item (20) Discard

2 Screw Item (33) Discard

Or remove:

Refer to Fig. A-FCDAA Sheet 01

4 Clamp Item (16) Discard

2 Spacer Item (14) Discard

2 Clip nut Item (43) Discard

2 Washer Item (20) Discard

2 Screw Item (33) Discard

(2) Subtask 246103-831-031-001 - Modify the routing between FR50 and FR52 and

between STGR 33 and 30 at LH side, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

147 Work location from Frame 50 to Frame 52

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Supplementary kit 246103A01S08

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

77 EN6049-007-19-5 7.5 (M) SLEEVE

78 EN6049-007-13-5 7.5 (M) SLEEVE

References

Fig. A-FBXAA

Modification of the Routing between

FR50 and FR52 (LH and RH side) -

ADDITIONAL WORK

Sheet 01

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 336

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SERVICE BULLETIN

(a) Remove :

Refer to Fig. A-FBXAA Sheet 01

5 (M) Conduit Item (77) Discard

NOTE: A third conduit may be installed. If installed, remove it.

(b) Install :

Refer to Fig. A-FBXAA Sheet 01

5 (M) Sleeve EN6049-007-13-5 Item 78

or

5 (M) Sleeve EN6049-007-19-5 Item 77

NOTE: Install the sleeve Item 77 or 78 according to the harness diameter.

NOTE: If a third conduit was installed, install :

2.5 (M) Sleeve EN6049-007-13-5 Item 78

or

2.5 (M) Sleeve EN6049-007-19-5 Item 77

NOTE: Install the sleeve Item 77 or 78 according to the harness diameter.

(3) Subtask 246103-420-007-001 - Install the clamps between FR50 and FR52 at LH

side, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

147 Work location from Frame 50 to Frame 52

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Supplementary kit 246103A01S08

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

12 NSA5527-03-01 2 SPACER

14 NSA5527-03-02 2 SPACER

33 NAS1801-3-25 1 SCREW

41 A0041095620000 1 SEAL

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 337

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@A300-600

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ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

42 A0041095400000 1 BRACKET

43 NSA5067-3-1 6 NUT

46 NAS1149F0332P 8 WASHER

63 NSA5516-13ND 14 CLAMP

64 NSA5516-31ND 14 CLAMP

79 NAS1801-3-18 1 SCREW

References

Fig. A-FCAAA

Modification of the Routing of the

Passage Way at FR52 (LH Side) -

ADDITIONAL WORK

Sheet 01

Sheet 02

Fig. A-FCDAA

Modification of the Routing Between

FR50 and FR51 at STGR32 (LH and RH

Side) - ADDITIONAL WORK

Sheet 01

Sheet 02

(a) Install :

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

6 Clamp NSA5516-13ND Item 63

or

6 Clamp NSA5516-31ND Item 64

NOTE: Install the clamp Item 63 or 64 according to the bundle diameter.

6 Washer NAS1149F0332P Item 46

1 Seal Fitting A0041095620000 Item 41

1 Bracket assy A0041095400000 Item 42

2 Clip nut NSA5067-3-1 Item 43

4 Screw Item (47) Retained at

removal

2 Screw Item (74) Retained at

removal

(b) Depending on the staking, install :

Refer to Fig. A-FCDAA Sheet 02 view C

3 Clamp NSA5516-13ND Item 63

or

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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@A300-600

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3 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

1 Spacer NSA5527-03-01 Item 12

1 Spacer NSA5527-03-02 Item 14

1 Screw NAS1801-3-25 Item 33

1 Washer NAS1149F0332P Item 46

1 Clip nut NSA5067-3-1 Item 43

Or install :

Refer to Fig. A-FCDAA Sheet 02 view C

2 Clamp NSA5516-13ND Item 63

or

2 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

1 Spacer NSA5527-03-01 Item 12

1 Spacer NSA5527-03-02 Item 14

1 Screw NAS1801-3-25 Item 33

1 Washer NAS1149F0332P Item 46

1 Clip nut NSA5067-3-1 Item 43

(c) Depending on the staking, install :

Refer to Fig. A-FCDAA Sheet 02 view D

3 Clamp NSA5516-13ND Item 63

or

3 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

1 Spacer NSA5527-03-02 Item 14

1 Screw NAS1801-3-18 Item 79

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 339

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@A300-600

SERVICE BULLETIN

1 Washer NAS1149F0332P Item 46

1 Clip nut NSA5067-3-1 Item 43

Or install :

Refer to Fig. A-FCDAA Sheet 02 view D

2 Clamp NSA5516-13ND Item 63

or

2 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

1 Spacer NSA5527-03-02 Item 14

1 Screw NAS1801-3-18 Item 79

1 Washer NAS1149F0332P Item 46

1 Clip nut NSA5067-3-1 Item 43

(4) Subtask 246103-420-009-001 - Install a bracket on the shroud box blanking plate at

LH side, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

147 Work location Frame 51

from Stringer 31 to Stringer 33

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills AIRFRAME

Material necessary to do the job

Supplementary kit 246103A01S08

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

21 NSA5050-3 3 NUT

28 A0041113420000 1 BRACKET

30 NAS1801-3-8 2 SCREW

37 NAS1801-3-9 1 SCREW

46 NAS1149F0332P 2 WASHER

63 NSA5516-13ND CLAMP

64 NSA5516-31ND CLAMP

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 340

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@A300-600

SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

70 A0041113500000 1 CLAMP

71 NAS1801-3-12 2 SCREW

75 A0041113500200 1 CLAMP

76 A0041113500400 1 CLAMP

References

Fig. A-FBSAA

Installation of a Bracket on the Shroud

Box Blanking Plate (LH and RH side) -

ADDITIONAL WORK

Sheet 01

Sheet 02

(a) Remove :

Refer to Fig. A-FBSAA Sheet 01

2 Screw Item (27) Discard

2 Washer Item (46) Discard

(b) Install the bracket :

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

1 Bracket A0041113420000 Item 28

2 Screw NAS1801-3-12 Item 71

2 Washer NAS1149F0332P Item 46

(c) Attach the bundles on the shroud box bracket :

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

1 Attach the bundles with :

2 Clamp NSA5516-13ND Item 63

or

2 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

NOTE: Two or three bundles may be installed.

attach with :

1 Nut NSA5050-3 Item 21

and

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 341

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@A300-600

SERVICE BULLETIN

1 Screw NAS1801-3-9 Item 37

2 Or attach the bundles with :

1 Clamp NSA5516-13ND Item 63

or

1 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

NOTE: Two or three bundles may be installed.

and

1 Clamp A0041113500000 Item 70

or

1 Clamp A0041113500200 Item 75

or

1 Clamp A0041113500400 Item 76

NOTE: Install clamp Item 70 or 75 or 76 according to the bundle

diameters.

attach with :

2 Nut NSA5050-3 Item 21

2 Screw NAS1801-3-8 Item 30

(5) Subtask 246103-831-033-001 - Modify the routing on rib 1 on the passage way to

the shroud box at LH side, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

147 Work location Frame 51

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 342

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@A300-600

SERVICE BULLETIN

Material necessary to do the job

Kit 246103A01R14

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

87 NSA360002 1 (M) EXTRUSIN

Supplementary kit 246103A01S08

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

12 NSA5527-03-01 4 SPACER

24 NSA939510BN 1 (M) STRIP

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Epoxy Adhesive-Metal To

Metal - Legacy

05EJL9 As required

Epoxy Adhesive - Legacy 3 05EML7 As required

Contact Adhesive-Rubber &

Plastic Bonding Neopren

05JBC9 As required

Non Aqueous Cleaner -

Isopropyl Alcohol

08BBD1

References

Process and Material Specification

(PMS)

Process and Material Specification (PMS)

01-01-28 Process E

Fig. A-FCCAA

Modification of the Clamps on the

Passage Way to the Shroud Box (LH

and RH Side) - ADDITIONAL WORK

Sheet 01

Sheet 02

Sheet 03

Sheet 04

(a) Install:

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

1 (M) Extrusion NSA360002 Item 87

with:

Contact AdhesiveRubber & Plastic

Bonding Neopren

05JBC9 As required

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 343

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@A300-600

SERVICE BULLETIN

(b) Measure the gap between the clamp and the structure, refer to Fig. A-FCCAA

Sheet 01, Fig. A-FCCAA Sheet 02, Fig. A-FCCAA Sheet 03 and Fig. A-FCCAA

Sheet 04:

1 If the gap between the structure and the clamp is less than 6.35 mm (0.25 in.),

install, refer to Fig. A-FCCAA Sheet 03

4 Spacer NSA5527-03-01 Item 12

2 If the gap between the structure and the clamp is more than 130 mm (5.118

in), contact AIRBUS, refer to Fig. A-FCCAA Sheet 02

NOTE: For operators that have the gap between the structure and the

clamp is more than 130 mm (5.118 in) contact Airbus at:

AIRBUS CUSTOMER SERVICES ENGINEERING - SEEA5

ELECTRICAL POWER GENERATION DISTRIBUTION &

LIGHTING SYSTEMS

1 ROND POINT MAURICE BELLONTE

31707 BLAGNAC CEDEX FRANCE

FAX +33 561 934 425

(c) Modify the grommet installation :

Refer to Fig. A-FCCAA Sheet 01, Fig. A-FCCAA Sheet 02, Fig. A-FCCAA Sheet 03

and Fig. A-FCCAA Sheet 04

1 Remove :

1 (M) Strip-Protective Item (24) Discard

2 Install :

Refer to Process and Material Specification (PMS) 01-01-28 Process E

1 (M) Strip-Protective NSA939510BN Item 24

NOTE: Install the Strip-Protective Item 24 with:

Epoxy AdhesiveMetal To Metal -

Legacy

05EJL9 As required

NOTE: Do the abrading and cleaning of the contact zones of the StripProtective Item 24, on the structure with:

Non Aqueous

Cleaner - Isopropyl

Alcohol

08BBD1 As required

Epoxy Adhesive -

Legacy 3

05EML7 As required

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 344

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Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

(6) Subtask 246103-831-034-001 - Modify the routing of routes 1P and 2P in the

shroud box at LH side, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

571

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Supplementary kit 246103A01S08

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

19 NSA935807-09 10 CLAMP

20 NSA935808-01 7 WASHER

34 NSA5527-03-08 4 SPACER

71 NAS1801-3-12 1 SCREW

81 NAS1801-3-20 6 SCREW

84 NSA5527-03-06 1 SPACER

References

Fig. A-FCEAA

Modification of the Routing of Routes 1P

and 2P in the Shroud Box (LH Side) -

ADDITIONAL WORK

Sheet 01

Sheet 02

Sheet 03

Sheet 04

(a) For Section A-A, remove :

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

4 Screw Item (22) Discard

4 Washer Item (20) Discard

8 Clamp Item (19) Discard

(b) For Section B-B, install :

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

4 Spacer NSA5527-03-08 Item 34

8 Clamp NSA935807-09 Item 19

4 Washer NSA935808-01 Item 20

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 345

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SERVICE BULLETIN

4 Screw NAS1801-3-20 Item 81

(c) For Section C-C, remove :

Refer to Fig. A-FCEAA Sheet 01 and Fig. A-FCEAA Sheet 03

2 Screw Item (22) Discard

2 Washer Item (20) Discard

4 Clamp Item (19) Retain

2 Spacer Item (34) Retain

(d) For Section D-D, install :

Refer to Fig. A-FCEAA Sheet 01 and Fig. A-FCEAA Sheet 03

2 Spacer Item (34) Retained at

removal

4 Clamp Item (19) Retained at

removal

2 Washer NSA935808-01 Item 20

2 Screw NAS1801-3-20 Item 81

(e) For Section E-E, remove :

Refer to Fig. A-FCEAA Sheet 01 and Fig. A-FCEAA Sheet 04

1 Screw Item (22) Discard

1 Washer Item (20) Discard

2 Clamp Item (19) Discard

(f) For Section F-F, install :

Refer to Fig. A-FCEAA Sheet 01 and Fig. A-FCEAA Sheet 04

1 Spacer NSA5527-03-06 Item 84

2 Clamp NSA935807-09 Item 19

1 Washer NSA935808-01 Item 20

1 Screw NAS1801-3-12 Item 71

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 346

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Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

(7) Subtask 246103-420-011-001 - Install a support on the support of the BLUE

hydraulic reservoir at LH wing - ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

571 Work location from Frame 47 to Frame 48

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills NON SPECIFIC

Material necessary to do the job

Supplementary kit 246103A01S08

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

20 NSA935808-01 1 WASHER

31 NAS1801-3-11 1 SCREW

67 A0041113300000 1 BRACKET

68 ASNA2050DXJ4828 2 RIVET

69 NSA935807-06 1 CLAMP

ASNA2528-3 2 NUT

EN6115V3-4 2 BOLT

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Primer Polyurethane Paint -

Corrosion Inhibiting

04EAC2 As required

Top Coat Polyurethane -

Grey Internal Structure

04JME4 As required

Polysulfide Sealant -

General Purpose Interfay

06AAC1 As required

Polysulfide Sealant-Fuel

Tank Fillet

06ABB1 As required

Non Aqueous Cleaner -

General

08BAA9 As required

Corrosion Preventive

Compound-Water

Displacing

12ADB1 As required

References

Fig. A-FBRAA

Installation of a Support on the Support

of the BLUE Hydraulic Reservoir (LH

wing) - ADDITIONAL WORK

Sheet 01

Sheet 02

Sheet 03

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 347

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@A300-600

SERVICE BULLETIN

(a) Remove :

Refer to Fig. A-FBRAA Sheet 01

1 Support Item (35) Discard

2 Screw Item (37) Discard

2 Washer Item (36) Discard

2 Nut Item (21) Discard

(b) Install the new support :

Refer to Fig. A-FBRAA Sheet 01, Fig. A-FBRAA Sheet 02 and Fig. A-FBRAA Sheet

03

1 Remove :

2 Rivet Item (68) Discard

NOTE: Clean the area with :

Non Aqueous

Cleaner - General

08BAA9 As required

2 Install the bracket Item 67.

a Put the bracket Item 67 in position.

b Drill two holes on the bracket Item 67 to a diameter comprised between

4.85 mm (0.191 in.) and 4.95 mm (0.195 in.) to match the holes of the

structure.

c Wet install :

1 Bracket A0041113300000 Item 67

2 Rivet ASNA2050DXJ4828 Item 68

NOTE: If the installation of bracket Item 67 with the rivets is not

possible, attach with:

2 Bolt EN6115V3-4

2 Nut ASNA2528-3

NOTE: Between the bracket Item 67 and the structure, apply :

Polysulfide SealantFuel Tank Fillet

06ABB1 As required

NOTE: Wet install the rivets with :

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 348

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@A300-600

SERVICE BULLETIN

Polysulfide Sealant

- General Purpose

Interfay

06AAC1 As required

NOTE: Apply on the head of the rivets :

Primer

Polyurethane Paint

- Corrosion

Inhibiting

04EAC2 As required

Top Coat

Polyurethane - Grey

Internal Structure

04JME4 As required

NOTE: On the modified area, apply :

Corrosion

Preventive

Compound-Water

Displacing

12ADB1 As required

3 Attach the sleeve to the bracket with :

1 Clamp NSA935807-06 Item 69

1 Screw NAS1801-3-11 Item 31

1 Washer NSA935808-01 Item 20

(8) Subtask 246103-831-035-001 - Modify the routing of the routes 1E and 1G in the

leading edge at LH wing, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

513

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills NON SPECIFIC

Material necessary to do the job

Supplementary kit 246103A01S08

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

66 NSA935401-13 2 TIE

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 349

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@A300-600

SERVICE BULLETIN

References

Fig. A-FBQAA

Modification of the Routing in the

Leading Edge (LH and RH side) -

ADDITIONAL WORK

Sheet 01

(a) Remove :

Refer to Fig. A-FBQAA Sheet 01

2 Tie-Cable NSA935401-05 Item (23) Discard

(b) Install :

Refer to Fig. A-FBQAA Sheet 01

2 Tie-Cable NSA935401-13 Item 66

(9) Subtask 246103-020-007-001 - Remove the clamps between FR50 and FR52 at RH

side, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

148 Work location from Frame 50 to Frame 52

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

References

Fig. A-FCBAA

Modification of the Routing of the

Passage Way at FR52 (RH Side) -

ADDITIONAL WORK

Sheet 01

Sheet 02

Fig. A-FCDAA

Modification of the Routing Between

FR50 and FR51 at STGR32 (LH and RH

Side) - ADDITIONAL WORK

Sheet 01

Sheet 02

(a) Remove:

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

4 Clamp Item (72) Discard

2 Screw Item (74) Retain

2 Washer Item (73) Discard

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 350

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@A300-600

SERVICE BULLETIN

1 Clamp Item (44) Discard

1 Clamp Item (45) Discard

2 Screw Item (47) Retain

2 Washer Item (46) Discard

(b) Depending on the stacking, remove:

Refer to Fig. A-FCDAA Sheet 01

4 Clamp Item (16) Discard

2 Clamp Item (32) Discard

2 Spacer Item (14) Discard

2 Clip nut Item (43) Discard

2 Washer Item (20) Discard

2 Screw Item (33) Discard

Or remove:

Refer to Fig. A-FCDAA Sheet 01

4 Clamp Item (16) Discard

2 Spacer Item (14) Discard

2 Clip nut Item (43) Discard

2 Washer Item (20) Discard

2 Screw Item (33) Discard

(10) Subtask 246103-831-032-001 - Modify the routing between FR50 and FR52 and

between STGR 33 and 30 at RH side, ADDITIONAL WORK

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 351

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@A300-600

SERVICE BULLETIN

Material necessary to do the job

Supplementary kit 246103A02S07

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

77 EN6049-007-19-5 7.5 (M) SLEEVE

78 EN6049-007-13-5 7.5 (M) SLEEVE

References

Fig. A-FBXAA

Modification of the Routing between

FR50 and FR52 (LH and RH side) -

ADDITIONAL WORK

Sheet 01

(a) Remove :

Refer to Fig. A-FBXAA Sheet 01

5 (M) Conduit Item (77) Discard

NOTE: A third conduit may be installed. If installed, remove it.

(b) Install :

Refer to Fig. A-FBXAA Sheet 01

5 (M) Sleeve EN6049-007-13-5 Item 78

or

5 (M) Sleeve EN6049-007-19-5 Item 77

NOTE: Install the sleeve Item 77 or 78 according to the harness diameter.

NOTE: If a third conduit was installed, install :

2.5 (M) Sleeve EN6049-007-13-5 Item 78

or

2.5 (M) Sleeve EN6049-007-19-5 Item 77

NOTE: Install the sleeve Item 77 or 78 according to the harness diameter.

(11) Subtask 246103-420-008-001 - Install the clamps between FR50 and FR52 at RH

side, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

148 Work location from Frame 50 to Frame 52

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 352

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@A300-600

SERVICE BULLETIN

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Supplementary kit 246103A02S07

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

12 NSA5527-03-01 1 SPACER

14 NSA5527-03-02 2 SPACER

33 NAS1801-3-25 1 SCREW

43 NSA5067-3-1 2 NUT

46 NAS1149F0332P 6 WASHER

63 NSA5516-13ND 14 CLAMP

64 NSA5516-31ND 14 CLAMP

79 NAS1801-3-18 1 SCREW

References

Fig. A-FCBAA

Modification of the Routing of the

Passage Way at FR52 (RH Side) -

ADDITIONAL WORK

Sheet 01

Sheet 02

Fig. A-FCDAA

Modification of the Routing Between

FR50 and FR51 at STGR32 (LH and RH

Side) - ADDITIONAL WORK

Sheet 01

Sheet 02

(a) Install :

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

6 Clamp NSA5516-13ND Item 63

or

6 Clamp NSA5516-31ND Item 64

NOTE: Install the clamp Item 63 or 64 according to the bundle diameter.

4 Washer NAS1149F0332P Item 46

2 Screw Item (47) Retained at

removal

1 Screw Item (74) Retained at

removal

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 353

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@A300-600

SERVICE BULLETIN

(b) Depending on the staking, install :

Refer toFig. A-FCDAA Sheet 02 view C

3 Clamp NSA5516-13ND Item 63

or

3 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

1 Spacer NSA5527-03-01 Item 12

1 Spacer NSA5527-03-02 Item 14

1 Screw NAS1801-3-25 Item 33

1 Washer NAS1149F0332P Item 46

1 Clip nut NSA5067-3-1 Item 43

Or install :

Refer to Fig. A-FCDAA Sheet 02 view C

2 Clamp NSA5516-13ND Item 63

or

2 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

1 Spacer NSA5527-03-01 Item 12

1 Spacer NSA5527-03-02 Item 14

1 Screw NAS1801-3-25 Item 33

1 Washer NAS1149F0332P Item 46

1 Clip nut NSA5067-3-1 Item 43

(c) Depending on the staking, install :

Refer to Fig. A-FCDAA Sheet 02 view D

3 Clamp NSA5516-13ND Item 63

or

3 Clamp NSA5516-31ND Item 64

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 354

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@A300-600

SERVICE BULLETIN

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

1 Spacer NSA5527-03-02 Item 14

1 Screw NAS1801-3-18 Item 79

1 Washer NAS1149F0332P Item 46

1 Clip nut NSA5067-3-1 Item 43

Or install :

Refer to Fig. A-FCDAA Sheet 02 view D

2 Clamp NSA5516-13ND Item 63

or

2 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

1 Spacer NSA5527-03-02 Item 14

1 Screw NAS1801-3-18 Item 79

1 Washer NAS1149F0332P Item 46

1 Clip nut NSA5067-3-1 Item 43

(12) Subtask 246103-420-010-001 - Install a bracket on the shroud box blanking plate at

RH side, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

148 Work location Frame 51

from Stringer 31 to Stringer 33

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills AIRFRAME

Material necessary to do the job

Supplementary kit 246103A02S07

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

21 NSA5050-3 3 NUT

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 355

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@A300-600

SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

29 A0041113420100 1 BRACKET

30 NAS1801-3-8 2 SCREW

37 NAS1801-3-9 1 SCREW

46 NAS1149F0332P 2 WASHER

63 NSA5516-13ND CLAMP

64 NSA5516-31ND CLAMP

70 A0041113500000 1 CLAMP

71 NAS1801-3-12 2 SCREW

75 A0041113500200 1 CLAMP

76 A0041113500400 1 CLAMP

References

Fig. A-FBSAA

Installation of a Bracket on the Shroud

Box Blanking Plate (LH and RH side) -

ADDITIONAL WORK

Sheet 01

Sheet 02

(a) Remove :

Refer to Fig. A-FBSAA Sheet 01

2 Screw Item (27) Discard

2 Washer Item (46) Discard

(b) Install the bracket :

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

1 Bracket A0041113420100 Item 29

attach with :

2 Screw NAS1801-3-12 Item 71

2 Washer NAS1149F0332P Item 46

(c) Attach the bundles on the shroud box bracket :

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

1 Attach the bundles with :

2 Clamp NSA5516-13ND Item 63

or

2 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 356

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@A300-600

SERVICE BULLETIN

NOTE: Two or three bundles may be installed.

attach with :

1 Nut NSA5050-3 Item 21

1 Screw NAS1801-3-9 Item 37

2 Or attach the bundles with :

1 Clamp NSA5516-13ND Item 63

or

1 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

NOTE: Two or three bundles may be installed.

and

1 Clamp A0041113500000 Item 70

or

1 Clamp A0041113500200 Item 75

or

1 Clamp A0041113500400 Item 76

NOTE: Install clamp Item 70 or 75 or 76 according to the bundle

diameters.

attach with :

2 Nut NSA5050-3 Item 21

2 Screw NAS1801-3-8 Item 30

(13) Subtask 246103-831-050-001 - Modify the routing on Rib 1 on the passage way to

the shroud box at RH side, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

147 Work location Frame 51

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 357

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@A300-600

SERVICE BULLETIN

Material necessary to do the job

Kit 246103A02R12

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

87 NSA360002 1 (M) EXTRUSIN

Supplementary kit 246103A02S07

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

12 NSA5527-03-01 4 SPACER

24 NSA939510BN 1 (M) STRIP

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Epoxy Adhesive-Metal To

Metal - Legacy

05EJL9 As required

Epoxy Adhesive - Legacy 3 05EML7 As required

Contact Adhesive-Rubber &

Plastic Bonding Neopren

05JBC9 As required

Non Aqueous Cleaner -

Isopropyl Alcohol

08BBD1 As required

References

Process and Material Specification

(PMS)

Process and Material Specification (PMS)

01-01-28 Process E

Fig. A-FCCAA

Modification of the Clamps on the

Passage Way to the Shroud Box (LH

and RH Side) - ADDITIONAL WORK

Sheet 01

Sheet 02

Sheet 03

Sheet 04

(a) Install:

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

1 (M) Extrusion NSA360002 Item 87

with:

Contact AdhesiveRubber & Plastic

Bonding Neopren

05JBC9 As required

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 358

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@A300-600

SERVICE BULLETIN

(b) Measure the gap between the clamp and the structure, refer to Fig. A-FCCAA

Sheet 01, Fig. A-FCCAA Sheet 02 and Fig. A-FCCAA Sheet 03:

1 If the gap between the structure and the clamp is less than 6.35 mm (0.25 in.),

install, refer to Fig. A-FCCAA Sheet 03:

4 Spacer NSA5527-03-01 Item 12

2 If the gap between the structure and the clamp is more than 130 mm (5.118

in), contact AIRBUS, refer to Fig. A-FCCAA Sheet 02

NOTE: For operators that have the gap between the structure and the

clamp is more than 130 mm (5.118 in) contact Airbus at:

AIRBUS CUSTOMER SERVICES ENGINEERING - SEEA5

ELECTRICAL POWER GENERATION DISTRIBUTION &

LIGHTING SYSTEMS

1 ROND POINT MAURICE BELLONTE

31707 BLAGNAC CEDEX FRANCE

FAX +33 561 934 425

(c) Modify the grommet installation :

Refer to Fig. A-FCCAA Sheet 01, Fig. A-FCCAA Sheet 02, Fig. A-FCCAA Sheet 03

and Fig. A-FCCAA Sheet 04

1 Remove :

1 (M) Strip-Protective Item (24) Discard

2 Install :

Refer to Process and Material Specification (PMS) 01-01-28 Process E

1 (M) Strip-Protective NSA939510BN Item 24

NOTE: Install the Strip-Protective Item 24 with:

Epoxy AdhesiveMetal To Metal -

Legacy

05EJL9 As required

NOTE: Do the abrading and cleaning of the contact zones of the StripProtective Item 24, on the structure with:

Non Aqueous

Cleaner - Isopropyl

Alcohol

08BBD1 As required

Epoxy Adhesive -

Legacy 3

05EML7 As required

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 359

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SERVICE BULLETIN

(14) Subtask 246103-831-036-001 - Modify the routing of the routes 2E and 2G in the

leading edge at RH wing, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

613

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills NON SPECIFIC

Material necessary to do the job

Supplementary kit 246103A02S07

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

66 NSA935401-13 2 TIE

References

Fig. A-FBQAA

Modification of the Routing in the

Leading Edge (LH and RH side) -

ADDITIONAL WORK

Sheet 01

(a) Remove :

Refer to Fig. A-FBQAA Sheet 01

2 Tie-Cable NSA935401-05 Item (23) Discard

(b) Install :

Refer to Fig. A-FBQAA Sheet 01

2 Tie-Cable NSA935401-13 Item 66

(15) Subtask 246103-020-008-001 - Remove the clamps from LH wings, ADDITIONAL

WORK

Work Zones and Access Panels

Zone Access/Work location

572

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 360

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@A300-600

SERVICE BULLETIN

References

Fig. A-FBOAA

Removal/Installation of the Clamps in LH

and RH Wings - ADDITIONAL WORK

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

(a) Remove the clamps from LH wing at Rib location WIAX-27.96.

Refer to Fig. A-FBOAA Sheet 01 and Fig. A-FBOAA Sheet 05 view J

1 Remove :

2 Clamp Item (51) Discard

1 Screw Item (71) Discard

1 Washer Item (82) Discard

(b) Remove the clamps from LH wing at Rib location WIAX-40-53.

Refer to Fig. A-FBOAA Sheet 01 and Fig. A-FBOAA Sheet 03

1 Remove:

2 Screw Item (37) Retain

2 Washer Item (46) Discard

2 Clamp Item (51) Discard

(c) Remove the clamps from LH wing at Rib location WIAX-48-25.

Refer to Fig. A-FBOAA Sheet 01 and Fig. A-FBOAA Sheet 05 view L

1 Remove:

2 Clamp Item (51) Discard

1 Screw Item (83) Discard

1 Washer Item (82) Discard

NOTE: If necessary, on LH wing at Rib location WIAX-74.08, remove:

2 (M) Tape-Reinforced

Silicone

Item (85) Discard

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 361

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SERVICE BULLETIN

(16) Subtask 246103-020-009-001 - Remove the clamps from RH wings, ADDITIONAL

WORK

Work Zones and Access Panels

Zone Access/Work location

672

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

References

Fig. A-FBOAA

Removal/Installation of the Clamps in LH

and RH Wings - ADDITIONAL WORK

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

(a) Remove the clamps from RH wing at Rib location WIAX-27.96.

Refer to Fig. A-FBOAA Sheet 01 and Fig. A-FBOAA Sheet 05 view J

1 Remove :

2 Clamp Item (51) Discard

1 Screw Item (71) Discard

1 Washer Item (82) Discard

(b) Remove the clamps from RH wing at Rib location WIAX-40-53.

Refer to Fig. A-FBOAA Sheet 01 and Fig. A-FBOAA Sheet 03

1 Remove:

2 Screw Item (37) Retain

2 Washer Item (46) Discard

2 Clamp Item (51) Discard

(c) Remove the clamps from RH wing at Rib location WIAX-48-25.

Refer to Fig. A-FBOAA Sheet 01 and Fig. A-FBOAA Sheet 05 view L

1 Remove:

2 Clamp Item (51) Discard

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 362

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@A300-600

SERVICE BULLETIN

1 Screw Item (83) Discard

1 Washer Item (82) Discard

NOTE: If necessary, on RH wing at Rib location WIAX 74.08, remove:

2 (M) Tape-Reinforced

Silicone

Item (85) Discard

(17) Subtask 246103-831-048-001 - Modify the routing of routes 1P and 2P at LH wing,

ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

570 Work location from Rib 1 to Rib 6

Manpower Resources

Manhours 1.50

Minimum number of person 1

Subtask elapsed time 1.50

Skills NON SPECIFIC

Material necessary to do the job

Supplementary kit 246103A01S08

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

14 NSA5527-03-02 3 SPACER

25 ABS0596S005 2 INSULATR

26 NSA935401-04 12 TIE

66 NSA935401-13 3 TIE

Supplementary kit 246103A01S11

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

86 EN6049-007-08-5 2.5 (M) SLEEVE

References

Fig. A-FCMAA

Modification of the Routing in LH and

RH Wings - ADDITIONAL WORK

Sheet 01

Sheet 02

(a) Between rib 5 and rib 6, remove:

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

2 Insulator Item (25) Discard

12 Tie-Cable Item (26)

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 363

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@A300-600

SERVICE BULLETIN

and

3 Spacer Item (14) Discard

attached with:

3 Tie-Cable Item (66) Discard

(b) Between rib 5 and rib 6, install:

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

2.5 (M) Sleeve-Protective EN6049-007-08-5 Item 86

12 Tie-Cable NSA935401-04 Item 26

and

3 Spacer NSA5527-03-02 Item 14

attached with :

3 Tie-Cable NSA935401-13 Item 66

(c) The following part of the Skit A01S08 must no be used anymore for LH wing:

2 Insulator ABS0596S005 Item 25

(18) Subtask 246103-831-049-001 - Modify the routing of routes 1P and 2P at RH wing,

ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

670 Work location from Rib 1 to Rib 6

Manpower Resources

Manhours 1.50

Minimum number of person 1

Subtask elapsed time 1.50

Skills NON SPECIFIC

Material necessary to do the job

Supplementary kit 246103A02S07

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

14 NSA5527-03-02 3 SPACER

25 ABS0596S005 2 INSULATR

26 NSA935401-04 12 TIE

66 NSA935401-13 3 TIE

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 364

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@A300-600

SERVICE BULLETIN

Supplementary kit 246103A02S10

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

86 EN6049-007-08-5 2.5 (M) SLEEVE

References

Fig. A-FCMAA

Modification of the Routing in LH and

RH Wings - ADDITIONAL WORK

Sheet 01

Sheet 02

(a) Between rib 5 and rib 6, remove:

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

2 Insulator Item (25) Discard

12 Tie-Cable Item (26) Discard

and

3 Spacer Item (14) Discard

attached with:

3 Tie-Cable Item (66) Discard

(b) Between rib 5 and rib 6, install:

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

2.5 (M) Sleeve-Protective EN6049-007-08-5 Item 86

12 Tie-Cable NSA935401-04 Item 26

and

3 Spacer NSA5527-03-02 Item 14

attached with :

3 Tie-Cable NSA935401-13 Item 66

(c) The following part of the Skit A02S07 must no be used anymore for RH wing:

2 Insulator ABS0596S005 Item 25

(19) Subtask 246103-831-045-001 - Install the clamps in LH wing, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

572

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 365

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@A300-600

SERVICE BULLETIN

Manpower Resources

Manhours 1.00

Minimum number of person 2

Subtask elapsed time 0.50

Skills NON SPECIFIC

Material necessary to do the job

Kit 246103B01R03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

60 A9245000200000 1 GUIDE

Supplementary kit 246103A01S08

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

51 NSA5516-12ND 6 CLAMP

82 ASNA2397KD10L 2 WASHER

85 ASNA51072503 2 (M) TAPE

Supplementary kit 246103A01S11

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

12 NSA5527-03-01 1 SPACER

37 NAS1801-3-9 2 SCREW

46 NAS1149F0332P 6 WASHER

52 NSA5516-08ND 8 CLAMP

55 NAS1801-3-16 1 SCREW

86 EN6049-007-08-5 2.5 (M) SLEEVE

Supplementary kit 246103A03S01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

21 NSA5050-3 2 NUT

22 NAS1801-3-24 2 SCREW

90 NAS1149D0316H 2 WASHER

References

Fig. A-FBOAA

Removal/Installation of the Clamps in LH

and RH Wings - ADDITIONAL WORK

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

(a) Install the clamps LH wing at Rib location WIAX-27.96

Refer to Fig. A-FBOAA Sheet 01 and Fig. A-FBOAA Sheet 05 view K

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 366

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@A300-600

SERVICE BULLETIN

1 Install:

2 Clamp NSA5516-08ND Item 52

1 Washer NAS1149F0332P Item 46

1 Screw NAS1801-3-9 Item 37

(b) Install the clamps LH wing at Rib location WIAX-35.12

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

1 Install:

1 Screw Item (50) Retained at

removal

1 Spacer Item (13) Retained at

removal

1 Spacer NSA5527-03-01 Item 12

2 Washer NAS1149F0332P Item 46

1 Screw NAS1801-3-16 Item 55

2 Clamp NSA5516-08ND Item 52

(c) Install the clamps in LH wing at Rib location WIAX-40.53.

Refer to Fig. A-FBOAA Sheet 01 and Fig. A-FBOAA Sheet 03

1 Install:

2 Screw Item (37) Retained at

removal

2 Washer NAS1149F0332P Item 46

2 Clamp NSA5516-08ND Item 52

(d) Install the clamps LH wing at Rib location WIAX-48.25

Refer to Fig. A-FBOAA Sheet 01 and Fig. A-FBOAA Sheet 05 view M

1 Install:

2 Clamp NSA5516-08ND Item 52

1 Washer NAS1149F0332P Item 46

1 Screw NAS1801-3-9 Item 37

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 367

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(e) Install the clamps at LH wing at Rib location WIAX-74.08.

Refer to Fig. A-FBOAA Sheet 01 and Fig. A-FBOAA Sheet 04

1 Install:

2 Nut NSA5050-3 Item 21

2 Screw NAS1801-3-24 Item 22

2 Washer NAS1149D0316H Item 90

1 Guide Assy-Conduit A9245000200000 Item 60

NOTE: If necessary, to make the diameters of the bundles match with

the diameter of the holes of the guide Item 60, use:

2.5 (M) Sleeve-Protective EN6049-007-08-5 Item 86

2 (M) Tape-Reinforced

Silicone

ASNA51072503 Item 85

(f) The following parts of the Skit A01S08 must not be used anymore for WIAX-27.96,

WIAX-40.53, WIAX-48.25 and WIAX-74.08:

6 Clamp NSA5516-12ND Item 51

2 Washer ASNA2397KD10L Item 82

(20) Subtask 246103-831-047-001 - Install the clamps in RH wing, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

672

Manpower Resources

Manhours 1.00

Minimum number of person 2

Subtask elapsed time 0.5

Skills NON SPECIFIC

Material necessary to do the job

Kit 246103B01R03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

60 A9245000200000 1 GUIDE

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 368

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SERVICE BULLETIN

Supplementary kit 246103A02S10

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

12 NSA5527-03-01 1 SPACER

37 NAS1801-3-9 2 SCREW

46 NAS1149F0332P 6 WASHER

52 NSA5516-08ND 8 CLAMP

55 NAS1801-3-16 1 SCREW

85 ASNA51072503 1 (M) TAPE

86 EN6049-007-08-5 2.5 (M) SLEEVE

Supplementary kit 246103A03S01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

21 NSA5050-3 2 NUT

22 NAS1801-3-24 2 SCREW

90 NAS1149D0316H 2 WASHER

References

Fig. A-FBOAA

Removal/Installation of the Clamps in LH

and RH Wings - ADDITIONAL WORK

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

(a) Install the clamps in RH wing at Rib location WIAX-27.96

Refer to Fig. A-FBOAA Sheet 01 and Fig. A-FBOAA Sheet 05 view K

1 Install:

2 Clamp NSA5516-08ND Item 52

1 Washer NAS1149F0332P Item 46

1 Screw NAS1801-3-9 Item 37

(b) Install the clamps in RH wing at Rib location WIAX-35.12.

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

1 Install:

1 Spacer Item (13) Retained at

removal

1 Screw Item (50) Retained at

removal

1 Spacer NSA5527-03-01 Item 12

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 369

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2 Washer NAS1149F0332P Item 46

1 Screw NAS1801-3-16 Item 55

2 Clamp NSA5516-08ND Item 52

(c) Install the clamps in RH wing at Rib location WIAX-40.53

Refer to Fig. A-FBOAA Sheet 01 and Fig. A-FBOAA Sheet 03

1 Install:

2 Screw Item (37) Retained at

removal

2 Washer NAS1149F0332P Item 46

2 Clamp NSA5516-08ND Item 52

(d) Install the clamps in RH wing at Rib location WIAX-48.25

Refer to Fig. A-FBOAA Sheet 01 and Fig. A-FBOAA Sheet 05 view M

1 Install:

2 Clamp NSA5516-08ND Item 52

1 Washer NAS1149F0332P Item 46

1 Screw NAS1801-3-9 Item 37

(e) Install the clamps in LH wing at Rib location WIAX-74.08.

Refer to Fig. A-FBOAA Sheet 01 and Fig. A-FBOAA Sheet 04

1 Install:

2 Nut NSA5050-3 Item 21

2 Screw NAS1801-3-24 Item 22

2 Washer NAS1149D0316H Item 90

1 Guide Assy-Conduit A9245000200000 Item 60

NOTE: If necessary, to make the diameters of the bundles match with

the diameter of the holes of the guide Item 60, use:

2.5 (M) Sleeve-Protective EN6049-007-08-5 Item 86

1 (M) Tape-Reinforced

Silicone

ASNA51072503 Item 85

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 370

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SERVICE BULLETIN

**CONF 002

(1) Subtask 246103-020-006-001 - Remove the clamps between FR50 and FR52 at LH

side, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

147 Work location from Frame 50 to Frame 52

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

References

Fig. A-FCAAA

Modification of the Routing of the

Passage Way at FR52 (LH Side) -

ADDITIONAL WORK

Sheet 01

Sheet 02

Fig. A-FCDAA

Modification of the Routing Between

FR50 and FR51 at STGR32 (LH and RH

Side) - ADDITIONAL WORK

Sheet 01

Sheet 02

(a) Remove:

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

4 Clamp Item (72) Discard

2 Screw Item (74) Retain

2 Washer Item (73) Discard

1 Seal fitting Item (41) Discard

1 Bracket assy Item (42) Discard

2 Clip nut Item (43) Discard

2 Clamp Item (63) Retain

or

2 Clamp Item (64) Retain

4 Screw Item (47) Retain

4 Washer Item (46) Discard

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 371

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@A300-600

SERVICE BULLETIN

(b) Depending on the stacking, remove:

Refer to Fig. A-FCDAA Sheet 01

4 Clamp Item (16) Discard

2 Clamp Item (32) Discard

2 Spacer Item (14) Discard

2 Clip nut Item (43) Discard

2 Washer Item (20) Discard

2 Screw Item (33) Discard

Or remove:

Refer to Fig. A-FCDAA Sheet 01

4 Clamp Item (16) Discard

2 Spacer Item (14) Discard

2 Clip nut Item (43) Discard

2 Washer Item (20) Discard

2 Screw Item (33) Discard

(2) Subtask 246103-831-031-001 - Modify the routing between FR50 and FR52 and

between STGR 33 and 30 at LH side, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

147 Work location from Frame 50 to Frame 52

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Supplementary kit 246103A01S08

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

77 EN6049-007-19-5 7.5 (M) SLEEVE

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 372

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@A300-600

SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

78 EN6049-007-13-5 7.5 (M) SLEEVE

References

Fig. A-FBXAA

Modification of the Routing between

FR50 and FR52 (LH and RH side) -

ADDITIONAL WORK

Sheet 01

(a) Remove :

Refer to Fig. A-FBXAA Sheet 01

5 (M) Conduit Item (77) Discard

NOTE: A third conduit may be installed. If installed, remove it.

(b) Install :

Refer to Fig. A-FBXAA Sheet 01

5 (M) Sleeve EN6049-007-13-5 Item 78

or

5 (M) Sleeve EN6049-007-19-5 Item 77

NOTE: Install the sleeve Item 77 or 78 according to the harness diameter.

NOTE: If a third conduit was installed, install :

2.5 (M) Sleeve EN6049-007-13-5 Item 78

or

2.5 (M) Sleeve EN6049-007-19-5 Item 77

NOTE: Install the sleeve Item 77 or 78 according to the harness diameter.

(3) Subtask 246103-420-007-001 - Install the clamps between FR50 and FR52 at LH

side, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

147 Work location from Frame 50 to Frame 52

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 373

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@A300-600

SERVICE BULLETIN

Material necessary to do the job

Supplementary kit 246103A01S08

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

12 NSA5527-03-01 2 SPACER

14 NSA5527-03-02 2 SPACER

33 NAS1801-3-25 1 SCREW

41 A0041095620000 1 SEAL

42 A0041095400000 1 BRACKET

43 NSA5067-3-1 6 NUT

46 NAS1149F0332P 8 WASHER

63 NSA5516-13ND 14 CLAMP

64 NSA5516-31ND 14 CLAMP

79 NAS1801-3-18 1 SCREW

References

Fig. A-FCAAA

Modification of the Routing of the

Passage Way at FR52 (LH Side) -

ADDITIONAL WORK

Sheet 01

Sheet 02

Fig. A-FCDAA

Modification of the Routing Between

FR50 and FR51 at STGR32 (LH and RH

Side) - ADDITIONAL WORK

Sheet 01

Sheet 02

(a) Install :

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

6 Clamp NSA5516-13ND Item 63

or

6 Clamp NSA5516-31ND Item 64

NOTE: Install the clamp Item 63 or 64 according to the bundle diameter.

6 Washer NAS1149F0332P Item 46

1 Seal Fitting A0041095620000 Item 41

1 Bracket assy A0041095400000 Item 42

2 Clip nut NSA5067-3-1 Item 43

4 Screw Item (47) Retained at

removal

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 374

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2 Screw Item (74) Retained at

removal

(b) Depending on the staking, install :

Refer to Fig. A-FCDAA Sheet 02 view C

3 Clamp NSA5516-13ND Item 63

or

3 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

1 Spacer NSA5527-03-01 Item 12

1 Spacer NSA5527-03-02 Item 14

1 Screw NAS1801-3-25 Item 33

1 Washer NAS1149F0332P Item 46

1 Clip nut NSA5067-3-1 Item 43

Or install :

Refer to Fig. A-FCDAA Sheet 02 view C

2 Clamp NSA5516-13ND Item 63

or

2 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

1 Spacer NSA5527-03-01 Item 12

1 Spacer NSA5527-03-02 Item 14

1 Screw NAS1801-3-25 Item 33

1 Washer NAS1149F0332P Item 46

1 Clip nut NSA5067-3-1 Item 43

(c) Depending on the staking, install :

Refer to Fig. A-FCDAA Sheet 02 view D

3 Clamp NSA5516-13ND Item 63

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 375

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SERVICE BULLETIN

or

3 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

1 Spacer NSA5527-03-02 Item 14

1 Screw NAS1801-3-18 Item 79

1 Washer NAS1149F0332P Item 46

1 Clip nut NSA5067-3-1 Item 43

Or install :

Refer to Fig. A-FCDAA Sheet 02 view D

2 Clamp NSA5516-13ND Item 63

or

2 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

1 Spacer NSA5527-03-02 Item 14

1 Screw NAS1801-3-18 Item 79

1 Washer NAS1149F0332P Item 46

1 Clip nut NSA5067-3-1 Item 43

(4) Subtask 246103-420-009-001 - Install a bracket on the shroud box blanking plate at

LH side, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

147 Work location Frame 51

from Stringer 31 to Stringer 33

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills AIRFRAME

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 376

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Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

Material necessary to do the job

Supplementary kit 246103A01S08

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

21 NSA5050-3 3 NUT

28 A0041113420000 1 BRACKET

30 NAS1801-3-8 2 SCREW

37 NAS1801-3-9 1 SCREW

46 NAS1149F0332P 2 WASHER

63 NSA5516-13ND CLAMP

64 NSA5516-31ND CLAMP

70 A0041113500000 1 CLAMP

71 NAS1801-3-12 2 SCREW

75 A0041113500200 1 CLAMP

76 A0041113500400 1 CLAMP

References

Fig. A-FBSAA

Installation of a Bracket on the Shroud

Box Blanking Plate (LH and RH side) -

ADDITIONAL WORK

Sheet 01

Sheet 02

(a) Remove :

Refer to Fig. A-FBSAA Sheet 01

2 Screw Item (27) Discard

2 Washer Item (46) Discard

(b) Install the bracket :

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

1 Bracket A0041113420000 Item 28

2 Screw NAS1801-3-12 Item 71

2 Washer NAS1149F0332P Item 46

(c) Attach the bundles on the shroud box bracket :

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

1 Attach the bundles with :

2 Clamp NSA5516-13ND Item 63

or

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 377

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2 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

NOTE: Two or three bundles may be installed.

attach with :

1 Nut NSA5050-3 Item 21

and

1 Screw NAS1801-3-9 Item 37

2 Or attach the bundles with :

1 Clamp NSA5516-13ND Item 63

or

1 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

NOTE: Two or three bundles may be installed.

and

1 Clamp A0041113500000 Item 70

or

1 Clamp A0041113500200 Item 75

or

1 Clamp A0041113500400 Item 76

NOTE: Install clamp Item 70 or 75 or 76 according to the bundle

diameters.

attach with :

2 Nut NSA5050-3 Item 21

2 Screw NAS1801-3-8 Item 30

(5) Subtask 246103-831-033-001 - Modify the routing on rib 1 on the passage way to

the shroud box at LH side, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

147 Work location Frame 51

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 378

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@A300-600

SERVICE BULLETIN

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 246103A01R14

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

87 NSA360002 1 (M) EXTRUSIN

Supplementary kit 246103A01S08

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

12 NSA5527-03-01 4 SPACER

24 NSA939510BN 1 (M) STRIP

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Epoxy Adhesive-Metal To

Metal - Legacy

05EJL9 As required

Epoxy Adhesive - Legacy 3 05EML7 As required

Contact Adhesive-Rubber &

Plastic Bonding Neopren

05JBC9 As required

Non Aqueous Cleaner -

Isopropyl Alcohol

08BBD1

References

Process and Material Specification

(PMS)

Process and Material Specification (PMS)

01-01-28 Process E

Fig. A-FCCAA

Modification of the Clamps on the

Passage Way to the Shroud Box (LH

and RH Side) - ADDITIONAL WORK

Sheet 01

Sheet 02

Sheet 03

Sheet 04

(a) Install:

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

1 (M) Extrusion NSA360002 Item 87

with:

Contact AdhesiveRubber & Plastic

Bonding Neopren

05JBC9 As required

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 379

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(b) Measure the gap between the clamp and the structure, refer to Fig. A-FCCAA

Sheet 01, Fig. A-FCCAA Sheet 02, Fig. A-FCCAA Sheet 03 and Fig. A-FCCAA

Sheet 04:

1 If the gap between the structure and the clamp is less than 6.35 mm (0.25 in.),

install, refer to Fig. A-FCCAA Sheet 03

4 Spacer NSA5527-03-01 Item 12

2 If the gap between the structure and the clamp is more than 130 mm (5.118

in), contact AIRBUS, refer to Fig. A-FCCAA Sheet 02

NOTE: For operators that have the gap between the structure and the

clamp is more than 130 mm (5.118 in) contact Airbus at:

AIRBUS CUSTOMER SERVICES ENGINEERING - SEEA5

ELECTRICAL POWER GENERATION DISTRIBUTION &

LIGHTING SYSTEMS

1 ROND POINT MAURICE BELLONTE

31707 BLAGNAC CEDEX FRANCE

FAX +33 561 934 425

(c) Modify the grommet installation :

Refer to Fig. A-FCCAA Sheet 01, Fig. A-FCCAA Sheet 02, Fig. A-FCCAA Sheet 03

and Fig. A-FCCAA Sheet 04

1 Remove :

1 (M) Strip-Protective Item (24) Discard

2 Install :

Refer to Process and Material Specification (PMS) 01-01-28 Process E

1 (M) Strip-Protective NSA939510BN Item 24

NOTE: Install the Strip-Protective Item 24 with:

Epoxy AdhesiveMetal To Metal -

Legacy

05EJL9 As required

NOTE: Do the abrading and cleaning of the contact zones of the StripProtective Item 24, on the structure with:

Non Aqueous

Cleaner - Isopropyl

Alcohol

08BBD1 As required

Epoxy Adhesive -

Legacy 3

05EML7 As required

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 380

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SERVICE BULLETIN

(6) Subtask 246103-831-034-001 - Modify the routing of routes 1P and 2P in the

shroud box at LH side, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

571

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Supplementary kit 246103A01S08

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

19 NSA935807-09 10 CLAMP

20 NSA935808-01 7 WASHER

34 NSA5527-03-08 4 SPACER

71 NAS1801-3-12 1 SCREW

81 NAS1801-3-20 6 SCREW

84 NSA5527-03-06 1 SPACER

References

Fig. A-FCEAA

Modification of the Routing of Routes 1P

and 2P in the Shroud Box (LH Side) -

ADDITIONAL WORK

Sheet 01

Sheet 02

Sheet 03

Sheet 04

(a) For Section A-A, remove :

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

4 Screw Item (22) Discard

4 Washer Item (20) Discard

8 Clamp Item (19) Discard

(b) For Section B-B, install :

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

4 Spacer NSA5527-03-08 Item 34

8 Clamp NSA935807-09 Item 19

4 Washer NSA935808-01 Item 20

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 381

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4 Screw NAS1801-3-20 Item 81

(c) For Section C-C, remove :

Refer to Fig. A-FCEAA Sheet 01 and Fig. A-FCEAA Sheet 03

2 Screw Item (22) Discard

2 Washer Item (20) Discard

4 Clamp Item (19) Retain

2 Spacer Item (34) Retain

(d) For Section D-D, install :

Refer to Fig. A-FCEAA Sheet 01 and Fig. A-FCEAA Sheet 03

2 Spacer Item (34) Retained at

removal

4 Clamp Item (19) Retained at

removal

2 Washer NSA935808-01 Item 20

2 Screw NAS1801-3-20 Item 81

(e) For Section E-E, remove :

Refer to Fig. A-FCEAA Sheet 01 and Fig. A-FCEAA Sheet 04

1 Screw Item (22) Discard

1 Washer Item (20) Discard

2 Clamp Item (19) Discard

(f) For Section F-F, install :

Refer to Fig. A-FCEAA Sheet 01 and Fig. A-FCEAA Sheet 04

1 Spacer NSA5527-03-06 Item 84

2 Clamp NSA935807-09 Item 19

1 Washer NSA935808-01 Item 20

1 Screw NAS1801-3-12 Item 71

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 382

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SERVICE BULLETIN

(7) Subtask 246103-420-011-001 - Install a support on the support of the BLUE

hydraulic reservoir at LH wing - ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

571 Work location from Frame 47 to Frame 48

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills NON SPECIFIC

Material necessary to do the job

Supplementary kit 246103A01S08

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

20 NSA935808-01 1 WASHER

31 NAS1801-3-11 1 SCREW

67 A0041113300000 1 BRACKET

68 ASNA2050DXJ4828 2 RIVET

69 NSA935807-06 1 CLAMP

ASNA2528-3 2 NUT

EN6115V3-4 2 BOLT

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Primer Polyurethane Paint -

Corrosion Inhibiting

04EAC2 As required

Top Coat Polyurethane -

Grey Internal Structure

04JME4 As required

Polysulfide Sealant -

General Purpose Interfay

06AAC1 As required

Polysulfide Sealant-Fuel

Tank Fillet

06ABB1 As required

Non Aqueous Cleaner -

General

08BAA9 As required

Corrosion Preventive

Compound-Water

Displacing

12ADB1 As required

References

Fig. A-FBRAA

Installation of a Support on the Support

of the BLUE Hydraulic Reservoir (LH

wing) - ADDITIONAL WORK

Sheet 01

Sheet 02

Sheet 03

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 383

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(a) Remove :

Refer to Fig. A-FBRAA Sheet 01

1 Support Item (35) Discard

2 Screw Item (37) Discard

2 Washer Item (36) Discard

2 Nut Item (21) Discard

(b) Install the new support :

Refer to Fig. A-FBRAA Sheet 01, Fig. A-FBRAA Sheet 02 and Fig. A-FBRAA Sheet

03

1 Remove :

2 Rivet Item (68) Discard

NOTE: Clean the area with :

Non Aqueous

Cleaner - General

08BAA9 As required

2 Install the bracket Item 67.

a Put the bracket Item 67 in position.

b Drill two holes on the bracket Item 67 to a diameter comprised between

4.85 mm (0.191 in.) and 4.95 mm (0.195 in.) to match the holes of the

structure.

c Wet install :

1 Bracket A0041113300000 Item 67

2 Rivet ASNA2050DXJ4828 Item 68

NOTE: If the installation of bracket Item 67 with the rivets is not

possible, attach with:

2 Bolt EN6115V3-4

2 Nut ASNA2528-3

NOTE: Between the bracket Item 67 and the structure, apply :

Polysulfide SealantFuel Tank Fillet

06ABB1 As required

NOTE: Wet install the rivets with :

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 384

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SERVICE BULLETIN

Polysulfide Sealant

- General Purpose

Interfay

06AAC1 As required

NOTE: Apply on the head of the rivets :

Primer

Polyurethane Paint

- Corrosion

Inhibiting

04EAC2 As required

Top Coat

Polyurethane - Grey

Internal Structure

04JME4 As required

NOTE: On the modified area, apply :

Corrosion

Preventive

Compound-Water

Displacing

12ADB1 As required

3 Attach the sleeve to the bracket with :

1 Clamp NSA935807-06 Item 69

1 Screw NAS1801-3-11 Item 31

1 Washer NSA935808-01 Item 20

(8) Subtask 246103-831-035-001 - Modify the routing of the routes 1E and 1G in the

leading edge at LH wing, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

513

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills NON SPECIFIC

Material necessary to do the job

Supplementary kit 246103A01S08

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

66 NSA935401-13 2 TIE

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 385

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SERVICE BULLETIN

References

Fig. A-FBQAA

Modification of the Routing in the

Leading Edge (LH and RH side) -

ADDITIONAL WORK

Sheet 01

(a) Remove :

Refer to Fig. A-FBQAA Sheet 01

2 Tie-Cable NSA935401-05 Item (23) Discard

(b) Install :

Refer to Fig. A-FBQAA Sheet 01

2 Tie-Cable NSA935401-13 Item 66

(9) Subtask 246103-020-007-001 - Remove the clamps between FR50 and FR52 at RH

side, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

148 Work location from Frame 50 to Frame 52

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

References

Fig. A-FCBAA

Modification of the Routing of the

Passage Way at FR52 (RH Side) -

ADDITIONAL WORK

Sheet 01

Sheet 02

Fig. A-FCDAA

Modification of the Routing Between

FR50 and FR51 at STGR32 (LH and RH

Side) - ADDITIONAL WORK

Sheet 01

Sheet 02

(a) Remove:

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

4 Clamp Item (72) Discard

2 Screw Item (74) Retain

2 Washer Item (73) Discard

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 386

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SERVICE BULLETIN

1 Clamp Item (44) Discard

1 Clamp Item (45) Discard

2 Screw Item (47) Retain

2 Washer Item (46) Discard

(b) Depending on the stacking, remove:

Refer to Fig. A-FCDAA Sheet 01

4 Clamp Item (16) Discard

2 Clamp Item (32) Discard

2 Spacer Item (14) Discard

2 Clip nut Item (43) Discard

2 Washer Item (20) Discard

2 Screw Item (33) Discard

Or remove:

Refer to Fig. A-FCDAA Sheet 01

4 Clamp Item (16) Discard

2 Spacer Item (14) Discard

2 Clip nut Item (43) Discard

2 Washer Item (20) Discard

2 Screw Item (33) Discard

(10) Subtask 246103-831-032-001 - Modify the routing between FR50 and FR52 and

between STGR 33 and 30 at RH side, ADDITIONAL WORK

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 387

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SERVICE BULLETIN

Material necessary to do the job

Supplementary kit 246103A02S07

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

77 EN6049-007-19-5 7.5 (M) SLEEVE

78 EN6049-007-13-5 7.5 (M) SLEEVE

References

Fig. A-FBXAA

Modification of the Routing between

FR50 and FR52 (LH and RH side) -

ADDITIONAL WORK

Sheet 01

(a) Remove :

Refer to Fig. A-FBXAA Sheet 01

5 (M) Conduit Item (77) Discard

NOTE: A third conduit may be installed. If installed, remove it.

(b) Install :

Refer to Fig. A-FBXAA Sheet 01

5 (M) Sleeve EN6049-007-13-5 Item 78

or

5 (M) Sleeve EN6049-007-19-5 Item 77

NOTE: Install the sleeve Item 77 or 78 according to the harness diameter.

NOTE: If a third conduit was installed, install :

2.5 (M) Sleeve EN6049-007-13-5 Item 78

or

2.5 (M) Sleeve EN6049-007-19-5 Item 77

NOTE: Install the sleeve Item 77 or 78 according to the harness diameter.

(11) Subtask 246103-420-008-001 - Install the clamps between FR50 and FR52 at RH

side, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

148 Work location from Frame 50 to Frame 52

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 388

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@A300-600

SERVICE BULLETIN

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Supplementary kit 246103A02S07

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

12 NSA5527-03-01 1 SPACER

14 NSA5527-03-02 2 SPACER

33 NAS1801-3-25 1 SCREW

43 NSA5067-3-1 2 NUT

46 NAS1149F0332P 6 WASHER

63 NSA5516-13ND 14 CLAMP

64 NSA5516-31ND 14 CLAMP

79 NAS1801-3-18 1 SCREW

References

Fig. A-FCBAA

Modification of the Routing of the

Passage Way at FR52 (RH Side) -

ADDITIONAL WORK

Sheet 01

Sheet 02

Fig. A-FCDAA

Modification of the Routing Between

FR50 and FR51 at STGR32 (LH and RH

Side) - ADDITIONAL WORK

Sheet 01

Sheet 02

(a) Install :

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

6 Clamp NSA5516-13ND Item 63

or

6 Clamp NSA5516-31ND Item 64

NOTE: Install the clamp Item 63 or 64 according to the bundle diameter.

4 Washer NAS1149F0332P Item 46

2 Screw Item (47) Retained at

removal

1 Screw Item (74) Retained at

removal

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 389

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SERVICE BULLETIN

(b) Depending on the staking, install :

Refer toFig. A-FCDAA Sheet 02 view C

3 Clamp NSA5516-13ND Item 63

or

3 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

1 Spacer NSA5527-03-01 Item 12

1 Spacer NSA5527-03-02 Item 14

1 Screw NAS1801-3-25 Item 33

1 Washer NAS1149F0332P Item 46

1 Clip nut NSA5067-3-1 Item 43

Or install :

Refer to Fig. A-FCDAA Sheet 02 view C

2 Clamp NSA5516-13ND Item 63

or

2 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

1 Spacer NSA5527-03-01 Item 12

1 Spacer NSA5527-03-02 Item 14

1 Screw NAS1801-3-25 Item 33

1 Washer NAS1149F0332P Item 46

1 Clip nut NSA5067-3-1 Item 43

(c) Depending on the staking, install :

Refer to Fig. A-FCDAA Sheet 02 view D

3 Clamp NSA5516-13ND Item 63

or

3 Clamp NSA5516-31ND Item 64

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 390

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@A300-600

SERVICE BULLETIN

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

1 Spacer NSA5527-03-02 Item 14

1 Screw NAS1801-3-18 Item 79

1 Washer NAS1149F0332P Item 46

1 Clip nut NSA5067-3-1 Item 43

Or install :

Refer to Fig. A-FCDAA Sheet 02 view D

2 Clamp NSA5516-13ND Item 63

or

2 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

1 Spacer NSA5527-03-02 Item 14

1 Screw NAS1801-3-18 Item 79

1 Washer NAS1149F0332P Item 46

1 Clip nut NSA5067-3-1 Item 43

(12) Subtask 246103-420-010-001 - Install a bracket on the shroud box blanking plate at

RH side, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

148 Work location Frame 51

from Stringer 31 to Stringer 33

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills AIRFRAME

Material necessary to do the job

Supplementary kit 246103A02S07

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

21 NSA5050-3 3 NUT

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 391

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@A300-600

SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

29 A0041113420100 1 BRACKET

30 NAS1801-3-8 2 SCREW

37 NAS1801-3-9 1 SCREW

46 NAS1149F0332P 2 WASHER

63 NSA5516-13ND CLAMP

64 NSA5516-31ND CLAMP

70 A0041113500000 1 CLAMP

71 NAS1801-3-12 2 SCREW

75 A0041113500200 1 CLAMP

76 A0041113500400 1 CLAMP

References

Fig. A-FBSAA

Installation of a Bracket on the Shroud

Box Blanking Plate (LH and RH side) -

ADDITIONAL WORK

Sheet 01

Sheet 02

(a) Remove :

Refer to Fig. A-FBSAA Sheet 01

2 Screw Item (27) Discard

2 Washer Item (46) Discard

(b) Install the bracket :

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

1 Bracket A0041113420100 Item 29

attach with :

2 Screw NAS1801-3-12 Item 71

2 Washer NAS1149F0332P Item 46

(c) Attach the bundles on the shroud box bracket :

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

1 Attach the bundles with :

2 Clamp NSA5516-13ND Item 63

or

2 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 392

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SERVICE BULLETIN

NOTE: Two or three bundles may be installed.

attach with :

1 Nut NSA5050-3 Item 21

1 Screw NAS1801-3-9 Item 37

2 Or attach the bundles with :

1 Clamp NSA5516-13ND Item 63

or

1 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

NOTE: Two or three bundles may be installed.

and

1 Clamp A0041113500000 Item 70

or

1 Clamp A0041113500200 Item 75

or

1 Clamp A0041113500400 Item 76

NOTE: Install clamp Item 70 or 75 or 76 according to the bundle

diameters.

attach with :

2 Nut NSA5050-3 Item 21

2 Screw NAS1801-3-8 Item 30

(13) Subtask 246103-831-050-001 - Modify the routing on Rib 1 on the passage way to

the shroud box at RH side, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

147 Work location Frame 51

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 393

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SERVICE BULLETIN

Material necessary to do the job

Kit 246103A02R12

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

87 NSA360002 1 (M) EXTRUSIN

Supplementary kit 246103A02S07

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

12 NSA5527-03-01 4 SPACER

24 NSA939510BN 1 (M) STRIP

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Epoxy Adhesive-Metal To

Metal - Legacy

05EJL9 As required

Epoxy Adhesive - Legacy 3 05EML7 As required

Contact Adhesive-Rubber &

Plastic Bonding Neopren

05JBC9 As required

Non Aqueous Cleaner -

Isopropyl Alcohol

08BBD1 As required

References

Process and Material Specification

(PMS)

Process and Material Specification (PMS)

01-01-28 Process E

Fig. A-FCCAA

Modification of the Clamps on the

Passage Way to the Shroud Box (LH

and RH Side) - ADDITIONAL WORK

Sheet 01

Sheet 02

Sheet 03

Sheet 04

(a) Install:

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

1 (M) Extrusion NSA360002 Item 87

with:

Contact AdhesiveRubber & Plastic

Bonding Neopren

05JBC9 As required

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 394

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@A300-600

SERVICE BULLETIN

(b) Measure the gap between the clamp and the structure, refer to Fig. A-FCCAA

Sheet 01, Fig. A-FCCAA Sheet 02 and Fig. A-FCCAA Sheet 03:

1 If the gap between the structure and the clamp is less than 6.35 mm (0.25 in.),

install, refer to Fig. A-FCCAA Sheet 03:

4 Spacer NSA5527-03-01 Item 12

2 If the gap between the structure and the clamp is more than 130 mm (5.118

in), contact AIRBUS, refer to Fig. A-FCCAA Sheet 02

NOTE: For operators that have the gap between the structure and the

clamp is more than 130 mm (5.118 in) contact Airbus at:

AIRBUS CUSTOMER SERVICES ENGINEERING - SEEA5

ELECTRICAL POWER GENERATION DISTRIBUTION &

LIGHTING SYSTEMS

1 ROND POINT MAURICE BELLONTE

31707 BLAGNAC CEDEX FRANCE

FAX +33 561 934 425

(c) Modify the grommet installation :

Refer to Fig. A-FCCAA Sheet 01, Fig. A-FCCAA Sheet 02, Fig. A-FCCAA Sheet 03

and Fig. A-FCCAA Sheet 04

1 Remove :

1 (M) Strip-Protective Item (24) Discard

2 Install :

Refer to Process and Material Specification (PMS) 01-01-28 Process E

1 (M) Strip-Protective NSA939510BN Item 24

NOTE: Install the Strip-Protective Item 24 with:

Epoxy AdhesiveMetal To Metal -

Legacy

05EJL9 As required

NOTE: Do the abrading and cleaning of the contact zones of the StripProtective Item 24, on the structure with:

Non Aqueous

Cleaner - Isopropyl

Alcohol

08BBD1 As required

Epoxy Adhesive -

Legacy 3

05EML7 As required

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 395

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SERVICE BULLETIN

(14) Subtask 246103-831-036-001 - Modify the routing of the routes 2E and 2G in the

leading edge at RH wing, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

613

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills NON SPECIFIC

Material necessary to do the job

Supplementary kit 246103A02S07

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

66 NSA935401-13 2 TIE

References

Fig. A-FBQAA

Modification of the Routing in the

Leading Edge (LH and RH side) -

ADDITIONAL WORK

Sheet 01

(a) Remove :

Refer to Fig. A-FBQAA Sheet 01

2 Tie-Cable NSA935401-05 Item (23) Discard

(b) Install :

Refer to Fig. A-FBQAA Sheet 01

2 Tie-Cable NSA935401-13 Item 66

(15) Subtask 246103-020-008-002 - Remove the clamps from LH wings, ADDITIONAL

WORK

Manpower Resources

Manhours 1.00

Minimum number of person 2

Subtask elapsed time 0.50

Skills NON SPECIFIC

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 396

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SERVICE BULLETIN

References

Fig. A-FCOAA

Removal/Installation of the Clamps in LH

and RH Wings - ADDITIONAL WORK

Sheet 01

Sheet 02

Sheet 03

Sheet 04

(a) Remove the clamps from RH wing at Rib location WIAX-27.96.

Refer to Fig. A-FCOAA Sheet 01 and Fig. A-FCOAA Sheet 04 view J

1 Remove:

2 Clamp Item (51) Discard

1 Screw Item (71) Discard

1 Washer Item (82) Discard

(b) Remove the clamps from LH wing at Rib location WIAX-40.53

Refer to Fig. A-FCOAA Sheet 01 and Fig. A-FCOAA Sheet 03

1 Remove:

2 Screw Item (37) Retain

2 Washer Item (46) Discard

2 Clamp Item (51) Discard

(c) Remove the clamps from LH wing at Rib location WIAX-48.25.

Refer to Fig. A-FCOAA Sheet 01 and Fig. A-FCOAA Sheet 04 view L

1 Remove:

1 Washer Item (82) Discard

1 Screw Item (83) Discard

2 Clamp Item (51) Discard

(16) Subtask 246103-020-009-002 - Remove the clamps from RH wings, ADDITIONAL

WORK

Manpower Resources

Manhours 1.00

Minimum number of person 2

Subtask elapsed time 0.50

Skills NON SPECIFIC

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 397

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@A300-600

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References

Fig. A-FCOAA

Removal/Installation of the Clamps in LH

and RH Wings - ADDITIONAL WORK

Sheet 01

Sheet 02

Sheet 03

Sheet 04

(a) Remove the clamps from RH wing at Rib location WIAX-27.96.

Fig. A-FCOAA Sheet 01 and Fig. A-FCOAA Sheet 04 view J

1 Remove:

2 Clamp Item (51) Discard

1 Screw Item (71) Discard

1 Washer Item (82) Discard

(b) Remove the clamps from RH wing at Rib location WIAX-40.53.

Refer to Fig. A-FCOAA Sheet 01 and Fig. A-FCOAA Sheet 03

1 Remove:

2 Screw Item (37) Retain

2 Washer Item (46) Discard

2 Clamp Item (51) Discard

(c) Remove the clamps from RH wing at Rib location WIAX-48.25.

Refer to Fig. A-FCOAA Sheet 01and Fig. A-FCOAA Sheet 04 view L

1 Remove:

1 Washer Item (82) Discard

1 Screw Item (83) Discard

2 Clamp Item (51) Discard

(17) Subtask 246103-831-048-001 - Modify the routing of routes 1P and 2P at LH wing,

ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

570 Work location from Rib 1 to Rib 6

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 398

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@A300-600

SERVICE BULLETIN

Manpower Resources

Manhours 1.50

Minimum number of person 1

Subtask elapsed time 1.50

Skills NON SPECIFIC

Material necessary to do the job

Supplementary kit 246103A01S08

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

14 NSA5527-03-02 3 SPACER

25 ABS0596S005 2 INSULATR

26 NSA935401-04 12 TIE

66 NSA935401-13 3 TIE

Supplementary kit 246103A01S11

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

86 EN6049-007-08-5 2.5 (M) SLEEVE

References

Fig. A-FCMAA

Modification of the Routing in LH and

RH Wings - ADDITIONAL WORK

Sheet 01

Sheet 02

(a) Between rib 5 and rib 6, remove:

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

2 Insulator Item (25) Discard

12 Tie-Cable Item (26)

and

3 Spacer Item (14) Discard

attached with:

3 Tie-Cable Item (66) Discard

(b) Between rib 5 and rib 6, install:

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

2.5 (M) Sleeve-Protective EN6049-007-08-5 Item 86

12 Tie-Cable NSA935401-04 Item 26

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 399

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SERVICE BULLETIN

and

3 Spacer NSA5527-03-02 Item 14

attached with :

3 Tie-Cable NSA935401-13 Item 66

(c) The following part of the Skit A01S08 must no be used anymore for LH wing:

2 Insulator ABS0596S005 Item 25

(18) Subtask 246103-831-049-001 - Modify the routing of routes 1P and 2P at RH wing,

ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

670 Work location from Rib 1 to Rib 6

Manpower Resources

Manhours 1.50

Minimum number of person 1

Subtask elapsed time 1.50

Skills NON SPECIFIC

Material necessary to do the job

Supplementary kit 246103A02S07

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

14 NSA5527-03-02 3 SPACER

25 ABS0596S005 2 INSULATR

26 NSA935401-04 12 TIE

66 NSA935401-13 3 TIE

Supplementary kit 246103A02S10

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

86 EN6049-007-08-5 2.5 (M) SLEEVE

References

Fig. A-FCMAA

Modification of the Routing in LH and

RH Wings - ADDITIONAL WORK

Sheet 01

Sheet 02

(a) Between rib 5 and rib 6, remove:

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

2 Insulator Item (25) Discard

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 400

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@A300-600

SERVICE BULLETIN

12 Tie-Cable Item (26) Discard

and

3 Spacer Item (14) Discard

attached with:

3 Tie-Cable Item (66) Discard

(b) Between rib 5 and rib 6, install:

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

2.5 (M) Sleeve-Protective EN6049-007-08-5 Item 86

12 Tie-Cable NSA935401-04 Item 26

and

3 Spacer NSA5527-03-02 Item 14

attached with :

3 Tie-Cable NSA935401-13 Item 66

(c) The following part of the Skit A02S07 must no be used anymore for RH wing:

2 Insulator ABS0596S005 Item 25

(19) Subtask 246103-831-045-002 - Install the clamps in LH wing, ADDITIONAL WORK

Manpower Resources

Manhours 1.00

Minimum number of person 2

Subtask elapsed time 0.50

Skills NON SPECIFIC

Material necessary to do the job

Supplementary kit 246103A01S11

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

12 NSA5527-03-01 1 SPACER

37 NAS1801-3-9 2 SCREW

46 NAS1149F0332P 6 WASHER

52 NSA5516-08ND 8 CLAMP

55 NAS1801-3-16 1 SCREW

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 401

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SERVICE BULLETIN

Supplementary kit 246103A02S07

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

51 NSA5516-12ND 6 CLAMP

82 ASNA2397KD10L 2 WASHER

References

Fig. A-FCOAA

Removal/Installation of the Clamps in LH

and RH Wings - ADDITIONAL WORK

Sheet 01

Sheet 02

Sheet 03

Sheet 04

(a) Install the clamps in LH wing at Rib location WIAX-27.96.

Refer to Fig. A-FCOAA Sheet 01 and Fig. A-FCOAA Sheet 04 view K

1 Install:

2 Clamp NSA5516-08ND Item 52

1 Washer NAS1149F0332P Item 46

1 Screw NAS1801-3-9 Item 37

(b) Install the clamps in LH wing at Rib location WIAX-35.12.

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

1 Install:

1 Screw Item (50) Retained at

removal

1 Spacer Item (13) Retained at

removal

1 Spacer NSA5527-03-01 Item 12

2 Washer NAS1149F0332P Item 46

1 Screw NAS1801-3-16 Item 55

2 Clamp NSA5516-08ND Item 52

(c) Install the clamps in LH wing at Rib location WIAX-40.53.

Refer to Fig. A-FCOAA Sheet 01 and Fig. A-FCOAA Sheet 03

1 Install:

2 Screw Item (37) Retained at

removal

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 402

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SERVICE BULLETIN

2 Washer NAS1149F0332P Item 46

2 Clamp NSA5516-08ND Item 52

(d) Install the clamps in LH wing at Rib location WIAX-48.25.

Refer to Fig. A-FCOAA Sheet 01 and Fig. A-FCOAA Sheet 04 view M

1 Install:

2 Clamp NSA5516-08ND Item 52

1 Washer NAS1149F0332P Item 46

1 Screw NAS1801-3-9 Item 37

(e) The following parts of the Skit A02S07 must not be used anymore for WIAX-27.96,

WIAX-40.53 and WIAX-48.25:

6 Clamp NSA5516-12ND Item 51

2 Washer ASNA2397KD10L Item 82

(20) Subtask 246103-831-047-002 - Install the clamps in RH wing, ADDITIONAL WORK

Manpower Resources

Manhours 1.00

Minimum number of person 2

Subtask elapsed time 0.50

Skills NON SPECIFIC

Material necessary to do the job

Supplementary kit 246103A02S10

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

12 NSA5527-03-01 1 SPACER

37 NAS1801-3-9 2 SCREW

46 NAS1149F0332P 6 WASHER

52 NSA5516-08ND 8 CLAMP

55 NAS1801-3-16 1 SCREW

References

Fig. A-FCOAA

Removal/Installation of the Clamps in LH

and RH Wings - ADDITIONAL WORK

Sheet 01

Sheet 02

Sheet 03

Sheet 04

(a) Install the clamps in RH wing at Rib location WIAX-27.96.

Refer to Fig. A-FCOAA Sheet 01 and Fig. A-FCOAA Sheet 04 view K

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 403

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@A300-600

SERVICE BULLETIN

1 Install:

2 Clamp NSA5516-08ND Item 52

1 Washer NAS1149F0332P Item 46

1 Screw NAS1801-3-9 Item 37

(b) Install the clamps in RH wing at Rib location WIAX-35.12.

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

1 Install:

1 Spacer Item (13) Retained at

removal

1 Screw Item (50) Retained at

removal

1 Spacer NSA5527-03-01 Item 12

2 Washer NAS1149F0332P Item 46

1 Screw NAS1801-3-16 Item 55

2 Clamp NSA5516-08ND Item 52

(c) Install the clamps in RH wing at Rib location WIAX-40.53.

Refer to Fig. A-FCOAA Sheet 01 and Fig. A-FCOAA Sheet 03

1 Install:

2 Screw Item (37) Retained at

removal

2 Washer NAS1149F0332P Item 46

2 Clamp NSA5516-08ND Item 52

(d) Install the clamps in RH wing at Rib location WIAX-48.25.

Refer to Fig. A-FCOAA Sheet 01 and Fig. A-FCOAA Sheet 04 view M

1 Install:

2 Clamp NSA5516-08ND Item 52

1 Washer NAS1149F0332P Item 46

1 Screw NAS1801-3-9 Item 37

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 404

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SERVICE BULLETIN

**CONF 003

(1) Subtask 246103-020-006-001 - Remove the clamps between FR50 and FR52 at LH

side, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

147 Work location from Frame 50 to Frame 52

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

References

Fig. A-FCAAA

Modification of the Routing of the

Passage Way at FR52 (LH Side) -

ADDITIONAL WORK

Sheet 01

Sheet 02

Fig. A-FCDAA

Modification of the Routing Between

FR50 and FR51 at STGR32 (LH and RH

Side) - ADDITIONAL WORK

Sheet 01

Sheet 02

(a) Remove:

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

4 Clamp Item (72) Discard

2 Screw Item (74) Retain

2 Washer Item (73) Discard

1 Seal fitting Item (41) Discard

1 Bracket assy Item (42) Discard

2 Clip nut Item (43) Discard

2 Clamp Item (63) Retain

or

2 Clamp Item (64) Retain

4 Screw Item (47) Retain

4 Washer Item (46) Discard

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 405

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SERVICE BULLETIN

(b) Depending on the stacking, remove:

Refer to Fig. A-FCDAA Sheet 01

4 Clamp Item (16) Discard

2 Clamp Item (32) Discard

2 Spacer Item (14) Discard

2 Clip nut Item (43) Discard

2 Washer Item (20) Discard

2 Screw Item (33) Discard

Or remove:

Refer to Fig. A-FCDAA Sheet 01

4 Clamp Item (16) Discard

2 Spacer Item (14) Discard

2 Clip nut Item (43) Discard

2 Washer Item (20) Discard

2 Screw Item (33) Discard

(2) Subtask 246103-831-031-001 - Modify the routing between FR50 and FR52 and

between STGR 33 and 30 at LH side, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

147 Work location from Frame 50 to Frame 52

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Supplementary kit 246103A01S08

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

77 EN6049-007-19-5 7.5 (M) SLEEVE

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 406

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@A300-600

SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

78 EN6049-007-13-5 7.5 (M) SLEEVE

References

Fig. A-FBXAA

Modification of the Routing between

FR50 and FR52 (LH and RH side) -

ADDITIONAL WORK

Sheet 01

(a) Remove :

Refer to Fig. A-FBXAA Sheet 01

5 (M) Conduit Item (77) Discard

NOTE: A third conduit may be installed. If installed, remove it.

(b) Install :

Refer to Fig. A-FBXAA Sheet 01

5 (M) Sleeve EN6049-007-13-5 Item 78

or

5 (M) Sleeve EN6049-007-19-5 Item 77

NOTE: Install the sleeve Item 77 or 78 according to the harness diameter.

NOTE: If a third conduit was installed, install :

2.5 (M) Sleeve EN6049-007-13-5 Item 78

or

2.5 (M) Sleeve EN6049-007-19-5 Item 77

NOTE: Install the sleeve Item 77 or 78 according to the harness diameter.

(3) Subtask 246103-420-007-001 - Install the clamps between FR50 and FR52 at LH

side, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

147 Work location from Frame 50 to Frame 52

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 407

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@A300-600

SERVICE BULLETIN

Material necessary to do the job

Supplementary kit 246103A01S08

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

12 NSA5527-03-01 2 SPACER

14 NSA5527-03-02 2 SPACER

33 NAS1801-3-25 1 SCREW

41 A0041095620000 1 SEAL

42 A0041095400000 1 BRACKET

43 NSA5067-3-1 6 NUT

46 NAS1149F0332P 8 WASHER

63 NSA5516-13ND 14 CLAMP

64 NSA5516-31ND 14 CLAMP

79 NAS1801-3-18 1 SCREW

References

Fig. A-FCAAA

Modification of the Routing of the

Passage Way at FR52 (LH Side) -

ADDITIONAL WORK

Sheet 01

Sheet 02

Fig. A-FCDAA

Modification of the Routing Between

FR50 and FR51 at STGR32 (LH and RH

Side) - ADDITIONAL WORK

Sheet 01

Sheet 02

(a) Install :

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

6 Clamp NSA5516-13ND Item 63

or

6 Clamp NSA5516-31ND Item 64

NOTE: Install the clamp Item 63 or 64 according to the bundle diameter.

6 Washer NAS1149F0332P Item 46

1 Seal Fitting A0041095620000 Item 41

1 Bracket assy A0041095400000 Item 42

2 Clip nut NSA5067-3-1 Item 43

4 Screw Item (47) Retained at

removal

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 408

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SERVICE BULLETIN

2 Screw Item (74) Retained at

removal

(b) Depending on the staking, install :

Refer to Fig. A-FCDAA Sheet 02 view C

3 Clamp NSA5516-13ND Item 63

or

3 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

1 Spacer NSA5527-03-01 Item 12

1 Spacer NSA5527-03-02 Item 14

1 Screw NAS1801-3-25 Item 33

1 Washer NAS1149F0332P Item 46

1 Clip nut NSA5067-3-1 Item 43

Or install :

Refer to Fig. A-FCDAA Sheet 02 view C

2 Clamp NSA5516-13ND Item 63

or

2 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

1 Spacer NSA5527-03-01 Item 12

1 Spacer NSA5527-03-02 Item 14

1 Screw NAS1801-3-25 Item 33

1 Washer NAS1149F0332P Item 46

1 Clip nut NSA5067-3-1 Item 43

(c) Depending on the staking, install :

Refer to Fig. A-FCDAA Sheet 02 view D

3 Clamp NSA5516-13ND Item 63

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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@A300-600

SERVICE BULLETIN

or

3 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

1 Spacer NSA5527-03-02 Item 14

1 Screw NAS1801-3-18 Item 79

1 Washer NAS1149F0332P Item 46

1 Clip nut NSA5067-3-1 Item 43

Or install :

Refer to Fig. A-FCDAA Sheet 02 view D

2 Clamp NSA5516-13ND Item 63

or

2 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

1 Spacer NSA5527-03-02 Item 14

1 Screw NAS1801-3-18 Item 79

1 Washer NAS1149F0332P Item 46

1 Clip nut NSA5067-3-1 Item 43

(4) Subtask 246103-420-009-001 - Install a bracket on the shroud box blanking plate at

LH side, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

147 Work location Frame 51

from Stringer 31 to Stringer 33

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills AIRFRAME

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 410

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@A300-600

SERVICE BULLETIN

Material necessary to do the job

Supplementary kit 246103A01S08

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

21 NSA5050-3 3 NUT

28 A0041113420000 1 BRACKET

30 NAS1801-3-8 2 SCREW

37 NAS1801-3-9 1 SCREW

46 NAS1149F0332P 2 WASHER

63 NSA5516-13ND CLAMP

64 NSA5516-31ND CLAMP

70 A0041113500000 1 CLAMP

71 NAS1801-3-12 2 SCREW

75 A0041113500200 1 CLAMP

76 A0041113500400 1 CLAMP

References

Fig. A-FBSAA

Installation of a Bracket on the Shroud

Box Blanking Plate (LH and RH side) -

ADDITIONAL WORK

Sheet 01

Sheet 02

(a) Remove :

Refer to Fig. A-FBSAA Sheet 01

2 Screw Item (27) Discard

2 Washer Item (46) Discard

(b) Install the bracket :

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

1 Bracket A0041113420000 Item 28

2 Screw NAS1801-3-12 Item 71

2 Washer NAS1149F0332P Item 46

(c) Attach the bundles on the shroud box bracket :

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

1 Attach the bundles with :

2 Clamp NSA5516-13ND Item 63

or

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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2 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

NOTE: Two or three bundles may be installed.

attach with :

1 Nut NSA5050-3 Item 21

and

1 Screw NAS1801-3-9 Item 37

2 Or attach the bundles with :

1 Clamp NSA5516-13ND Item 63

or

1 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

NOTE: Two or three bundles may be installed.

and

1 Clamp A0041113500000 Item 70

or

1 Clamp A0041113500200 Item 75

or

1 Clamp A0041113500400 Item 76

NOTE: Install clamp Item 70 or 75 or 76 according to the bundle

diameters.

attach with :

2 Nut NSA5050-3 Item 21

2 Screw NAS1801-3-8 Item 30

(5) Subtask 246103-831-033-002 - Modify the routing on rib 1 on the passage way to

the shroud box at LH side, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

147 Work location Frame 51

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 412

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@A300-600

SERVICE BULLETIN

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 246103A04R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

12 NSA5527-03-01 1 SPACER

13 NSA5527-03-03 1 SPACER

14 NSA5527-03-02 3 SPACER

21 NSA5050-3 5 NUT

23 NSA935401-05 2 TIE

26 NSA935401-04 2 TIE

33 NAS1801-3-25 1 SCREW

46 NAS1149F0332P 6 WASHER

51 NSA5516-12ND 15 CLAMP

52 NSA5516-08ND 15 CLAMP

62 NAS1801-3-22 1 SCREW

63 NSA5516-13ND 15 CLAMP

64 NSA5516-31ND 15 CLAMP

66 NSA935401-13 2 TIE

84 NSA5527-03-06 1 SPACER

87 NSA360002 1 (M) EXTRUSIN

91 NSA5527-03-15 2 SPACER

92 NSA5527-03-12 1 SPACER

94 NSA5159-35 1 STUD

95 NSA5527-03-18 2 SPACER

96 NSA5527-03-09 1 SPACER

Supplementary kit 246103A01S08

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

24 NSA939510BN 1 (M) STRIP

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Epoxy Adhesive-Metal To

Metal - Legacy

05EJL9 As required

Epoxy Adhesive - Legacy 3 05EML7 As required

Contact Adhesive-Rubber &

Plastic Bonding Neopren

05JBC9 As required

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 413

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@A300-600

SERVICE BULLETIN

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Non Aqueous Cleaner -

Isopropyl Alcohol

08BBD1

References

Process and Material Specification

(PMS)

Process and Material Specification (PMS)

01-01-28 Process E

Fig. A-FCCAB

Modification of the Clamps on the

Passage Way to the Shroud Box (LH

and RH Side) - ADDITIONAL WORK

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

(a) Depending on the stacking, remove:

Refer to Fig. A-FCCAB Sheet 01 and Fig. A-FCCAB Sheet 03 view A-A

1 Nut Item (21) Discard

5 Clamp Item (51) Discard

or

5 Clamp Item (52) Discard

or

5 Clamp Item (63) Discard

or

5 Clamp Item (64) Discard

1 Spacer Item (91) Discard

1 Spacer Item (92) Discard

1 Spacer Item (93) Discard

1 Washer Item (46) Discard

(b) Depending on the stacking, remove:

Refer to Fig. A-FCCAB Sheet 01 and Fig. A-FCCAB Sheet 03 view B-B

1 Nut Item (21) Discard

5 Clamp Item (51) Discard

or

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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SERVICE BULLETIN

5 Clamp Item (52) Discard

or

5 Clamp Item (63) Discard

or

5 Clamp Item (64) Discard

1 Spacer Item (14) Discard

1 Spacer Item (91) Discard

1 Spacer Item (84) Discard

1 Spacer Item (97) Discard

1 Washer Item (46) Discard

(c) Depending on the stacking, remove:

Refer to Fig. A-FCCAB Sheet 01 and Fig. A-FCCAB Sheet 04 view C-C

1 Screw Item (33) Discard

1 Screw Item (62) Discard

2 Washer Item (46) Discard

5 Clamp Item (51) Discard

or

5 Clamp Item (52) Discard

or

5 Clamp Item (63) Discard

or

5 Clamp Item (64) Discard

1 Spacer Item (84) Discard

2 Spacer Item (95) Discard

3 Spacer Item (93) Discard

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 415

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(d) Install:

Refer to Fig. A-FCCAB Sheet 01 and Fig. A-FCCAB Sheet 05 view D-D

1 Stud NSA5159-35 Item 94

1 Nut NSA5050-3 Item 21

3 Clamp NSA5516-12ND Item 51

or

3 Clamp NSA5516-08ND Item 52

or

3 Clamp NSA5516-13ND Item 63

or

3 Clamp NSA5516-31ND Item 64

1 Spacer NSA5527-03-15 Item 91

1 Spacer NSA5527-03-12 Item 92

1 Spacer NSA5527-03-03 Item 13

2 Nut NSA5050-3 Item 21

2 Washer NAS1149F0332P Item 46

(e) Install:

Refer to Fig. A-FCCAB Sheet 01 and Fig. A-FCCAB Sheet 05 view E-E

1 Nut NSA5050-3 Item 21

2 Clamp NSA5516-08ND Item 52

or

2 Clamp NSA5516-12ND Item 51

or

2 Clamp NSA5516-13ND Item 63

or

2 Clamp NSA5516-31ND Item 64

2 Spacer NSA5527-03-02 Item 14

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 416

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@A300-600

SERVICE BULLETIN

1 Washer NAS1149F0332P Item 46

(f) Install:

Refer to Fig. A-FCCAB Sheet 01 and Fig. A-FCCAB Sheet 06 and view F-F

1 Nut NSA5050-3 Item 21

5 Clamp NSA5516-08ND Item 52

or

5 Clamp NSA5516-12ND Item 51

or

5 Clamp NSA5516-13ND Item 63

or

5 Clamp NSA5516-31ND Item 64

1 Spacer NSA5527-03-02 Item 14

1 Spacer NSA5527-03-15 Item 91

1 Spacer NSA5527-03-06 Item 84

1 Washer NAS1149F0332P Item 46

(g) Install:

Refer to Fig. A-FCCAB Sheet 01 and Fig. A-FCCAB Sheet 06 view G-G

1 Screw NAS1801-3-22 Item 62

1 Washer NAS1149F0332P Item 46

3 Clamp NSA5516-08ND Item 52

or

3 Clamp NSA5516-12ND Item 51

or

3 Clamp NSA5516-13ND Item 63

or

3 Clamp NSA5516-31ND Item 64

1 Spacer NSA5527-03-09 Item 96

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

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SERVICE BULLETIN

(h) Install:

Refer to Fig. A-FCCAB Sheet 01 and Fig. A-FCCAB Sheet 06 view H-H

1 Screw NAS1801-3-25 Item 33

1 Washer NAS1149F0332P Item 46

2 Clamp NSA5516-08ND Item 52

or

2 Clamp NSA5516-12ND Item 51

or

2 Clamp NSA5516-13ND Item 63

or

2 Clamp NSA5516-31ND Item 64

2 Spacer NSA5527-03-18 Item 95

(i) Install:

Refer to Fig. A-FCCAB Sheet 01 and Fig. A-FCCAB Sheet 06 view J-J

2 Tie-Cable NSA935401-13 Item 66

or

2 Tie-Cable NSA935401-04 Item 26

or

2 Tie-Cable NSA935401-05 Item 23

1 Spacer NSA5527-03-01 Item 12

(j) Install:

Refer to Fig. A-FCCAB Sheet 01 and Fig. A-FCCAB Sheet 05

1 (M) Extrusion NSA360002 Item 87

with:

Contact AdhesiveRubber & Plastic

Bonding Neopren

05JBC9 As required

(k) Modify the grommet installation :

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

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 418

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@A300-600

SERVICE BULLETIN

1 Remove :

1 Strip-Protective Item (24) Discard

2 Install :

Refer to Process and Material Specification (PMS) 01-01-28 Process E

1 (M) Strip-Protective NSA939510BN Item 24

NOTE: Install the Strip-Protective Item 24 with:

Epoxy AdhesiveMetal To Metal -

Legacy

05EJL9 As required

NOTE: Do the abrading and cleaning of the contact zones of the StripProtective Item 24, on the structure with:

Non Aqueous

Cleaner - Isopropyl

Alcohol

08BBD1 As required

Epoxy Adhesive -

Legacy 3

05EML7 As required

(6) Subtask 246103-831-034-001 - Modify the routing of routes 1P and 2P in the

shroud box at LH side, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

571

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Supplementary kit 246103A01S08

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

19 NSA935807-09 10 CLAMP

20 NSA935808-01 7 WASHER

34 NSA5527-03-08 4 SPACER

71 NAS1801-3-12 1 SCREW

81 NAS1801-3-20 6 SCREW

84 NSA5527-03-06 1 SPACER

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 419

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@A300-600

SERVICE BULLETIN

References

Fig. A-FCEAA

Modification of the Routing of Routes 1P

and 2P in the Shroud Box (LH Side) -

ADDITIONAL WORK

Sheet 01

Sheet 02

Sheet 03

Sheet 04

(a) For Section A-A, remove :

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

4 Screw Item (22) Discard

4 Washer Item (20) Discard

8 Clamp Item (19) Discard

(b) For Section B-B, install :

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

4 Spacer NSA5527-03-08 Item 34

8 Clamp NSA935807-09 Item 19

4 Washer NSA935808-01 Item 20

4 Screw NAS1801-3-20 Item 81

(c) For Section C-C, remove :

Refer to Fig. A-FCEAA Sheet 01 and Fig. A-FCEAA Sheet 03

2 Screw Item (22) Discard

2 Washer Item (20) Discard

4 Clamp Item (19) Retain

2 Spacer Item (34) Retain

(d) For Section D-D, install :

Refer to Fig. A-FCEAA Sheet 01 and Fig. A-FCEAA Sheet 03

2 Spacer Item (34) Retained at

removal

4 Clamp Item (19) Retained at

removal

2 Washer NSA935808-01 Item 20

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 420

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SERVICE BULLETIN

2 Screw NAS1801-3-20 Item 81

(e) For Section E-E, remove :

Refer to Fig. A-FCEAA Sheet 01 and Fig. A-FCEAA Sheet 04

1 Screw Item (22) Discard

1 Washer Item (20) Discard

2 Clamp Item (19) Discard

(f) For Section F-F, install :

Refer to Fig. A-FCEAA Sheet 01 and Fig. A-FCEAA Sheet 04

1 Spacer NSA5527-03-06 Item 84

2 Clamp NSA935807-09 Item 19

1 Washer NSA935808-01 Item 20

1 Screw NAS1801-3-12 Item 71

(7) Subtask 246103-420-011-001 - Install a support on the support of the BLUE

hydraulic reservoir at LH wing - ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

571 Work location from Frame 47 to Frame 48

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills NON SPECIFIC

Material necessary to do the job

Supplementary kit 246103A01S08

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

20 NSA935808-01 1 WASHER

31 NAS1801-3-11 1 SCREW

67 A0041113300000 1 BRACKET

68 ASNA2050DXJ4828 2 RIVET

69 NSA935807-06 1 CLAMP

ASNA2528-3 2 NUT

EN6115V3-4 2 BOLT

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 421

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@A300-600

SERVICE BULLETIN

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Primer Polyurethane Paint -

Corrosion Inhibiting

04EAC2 As required

Top Coat Polyurethane -

Grey Internal Structure

04JME4 As required

Polysulfide Sealant -

General Purpose Interfay

06AAC1 As required

Polysulfide Sealant-Fuel

Tank Fillet

06ABB1 As required

Non Aqueous Cleaner -

General

08BAA9 As required

Corrosion Preventive

Compound-Water

Displacing

12ADB1 As required

References

Fig. A-FBRAA

Installation of a Support on the Support

of the BLUE Hydraulic Reservoir (LH

wing) - ADDITIONAL WORK

Sheet 01

Sheet 02

Sheet 03

(a) Remove :

Refer to Fig. A-FBRAA Sheet 01

1 Support Item (35) Discard

2 Screw Item (37) Discard

2 Washer Item (36) Discard

2 Nut Item (21) Discard

(b) Install the new support :

Refer to Fig. A-FBRAA Sheet 01, Fig. A-FBRAA Sheet 02 and Fig. A-FBRAA Sheet

03

1 Remove :

2 Rivet Item (68) Discard

NOTE: Clean the area with :

Non Aqueous

Cleaner - General

08BAA9 As required

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 422

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SERVICE BULLETIN

2 Install the bracket Item 67.

a Put the bracket Item 67 in position.

b Drill two holes on the bracket Item 67 to a diameter comprised between

4.85 mm (0.191 in.) and 4.95 mm (0.195 in.) to match the holes of the

structure.

c Wet install :

1 Bracket A0041113300000 Item 67

2 Rivet ASNA2050DXJ4828 Item 68

NOTE: If the installation of bracket Item 67 with the rivets is not

possible, attach with:

2 Bolt EN6115V3-4

2 Nut ASNA2528-3

NOTE: Between the bracket Item 67 and the structure, apply :

Polysulfide SealantFuel Tank Fillet06ABB1 As required

NOTE: Wet install the rivets with :

Polysulfide Sealant

- General Purpose

Interfay

06AAC1 As required

NOTE: Apply on the head of the rivets :

Primer

Polyurethane Paint

- Corrosion

Inhibiting

04EAC2 As required

Top Coat

Polyurethane - Grey

Internal Structure

04JME4 As required

NOTE: On the modified area, apply :

Corrosion

Preventive

Compound-Water

Displacing

12ADB1 As required

3 Attach the sleeve to the bracket with :

1 Clamp NSA935807-06 Item 69

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 423

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SERVICE BULLETIN

1 Screw NAS1801-3-11 Item 31

1 Washer NSA935808-01 Item 20

(8) Subtask 246103-831-035-001 - Modify the routing of the routes 1E and 1G in the

leading edge at LH wing, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

513

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills NON SPECIFIC

Material necessary to do the job

Supplementary kit 246103A01S08

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

66 NSA935401-13 2 TIE

References

Fig. A-FBQAA

Modification of the Routing in the

Leading Edge (LH and RH side) -

ADDITIONAL WORK

Sheet 01

(a) Remove :

Refer to Fig. A-FBQAA Sheet 01

2 Tie-Cable NSA935401-05 Item (23) Discard

(b) Install :

Refer to Fig. A-FBQAA Sheet 01

2 Tie-Cable NSA935401-13 Item 66

(9) Subtask 246103-020-007-001 - Remove the clamps between FR50 and FR52 at RH

side, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

148 Work location from Frame 50 to Frame 52

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 424

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@A300-600

SERVICE BULLETIN

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

References

Fig. A-FCBAA

Modification of the Routing of the

Passage Way at FR52 (RH Side) -

ADDITIONAL WORK

Sheet 01

Sheet 02

Fig. A-FCDAA

Modification of the Routing Between

FR50 and FR51 at STGR32 (LH and RH

Side) - ADDITIONAL WORK

Sheet 01

Sheet 02

(a) Remove:

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

4 Clamp Item (72) Discard

2 Screw Item (74) Retain

2 Washer Item (73) Discard

1 Clamp Item (44) Discard

1 Clamp Item (45) Discard

2 Screw Item (47) Retain

2 Washer Item (46) Discard

(b) Depending on the stacking, remove:

Refer to Fig. A-FCDAA Sheet 01

4 Clamp Item (16) Discard

2 Clamp Item (32) Discard

2 Spacer Item (14) Discard

2 Clip nut Item (43) Discard

2 Washer Item (20) Discard

2 Screw Item (33) Discard

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 425

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@A300-600

SERVICE BULLETIN

Or remove:

Refer to Fig. A-FCDAA Sheet 01

4 Clamp Item (16) Discard

2 Spacer Item (14) Discard

2 Clip nut Item (43) Discard

2 Washer Item (20) Discard

2 Screw Item (33) Discard

(10) Subtask 246103-831-032-001 - Modify the routing between FR50 and FR52 and

between STGR 33 and 30 at RH side, ADDITIONAL WORK

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Supplementary kit 246103A02S07

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

77 EN6049-007-19-5 7.5 (M) SLEEVE

78 EN6049-007-13-5 7.5 (M) SLEEVE

References

Fig. A-FBXAA

Modification of the Routing between

FR50 and FR52 (LH and RH side) -

ADDITIONAL WORK

Sheet 01

(a) Remove :

Refer to Fig. A-FBXAA Sheet 01

5 (M) Conduit Item (77) Discard

NOTE: A third conduit may be installed. If installed, remove it.

(b) Install :

Refer to Fig. A-FBXAA Sheet 01

5 (M) Sleeve EN6049-007-13-5 Item 78

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 426

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@A300-600

SERVICE BULLETIN

or

5 (M) Sleeve EN6049-007-19-5 Item 77

NOTE: Install the sleeve Item 77 or 78 according to the harness diameter.

NOTE: If a third conduit was installed, install :

2.5 (M) Sleeve EN6049-007-13-5 Item 78

or

2.5 (M) Sleeve EN6049-007-19-5 Item 77

NOTE: Install the sleeve Item 77 or 78 according to the harness diameter.

(11) Subtask 246103-420-008-001 - Install the clamps between FR50 and FR52 at RH

side, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

148 Work location from Frame 50 to Frame 52

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Supplementary kit 246103A02S07

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

12 NSA5527-03-01 1 SPACER

14 NSA5527-03-02 2 SPACER

33 NAS1801-3-25 1 SCREW

43 NSA5067-3-1 2 NUT

46 NAS1149F0332P 6 WASHER

63 NSA5516-13ND 14 CLAMP

64 NSA5516-31ND 14 CLAMP

79 NAS1801-3-18 1 SCREW

References

Fig. A-FCBAA

Modification of the Routing of the

Passage Way at FR52 (RH Side) -

ADDITIONAL WORK

Sheet 01

Sheet 02

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 427

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SERVICE BULLETIN

References

Fig. A-FCDAA

Modification of the Routing Between

FR50 and FR51 at STGR32 (LH and RH

Side) - ADDITIONAL WORK

Sheet 01

Sheet 02

(a) Install :

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

6 Clamp NSA5516-13ND Item 63

or

6 Clamp NSA5516-31ND Item 64

NOTE: Install the clamp Item 63 or 64 according to the bundle diameter.

4 Washer NAS1149F0332P Item 46

2 Screw Item (47) Retained at

removal

1 Screw Item (74) Retained at

removal

(b) Depending on the staking, install :

Refer toFig. A-FCDAA Sheet 02 view C

3 Clamp NSA5516-13ND Item 63

or

3 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

1 Spacer NSA5527-03-01 Item 12

1 Spacer NSA5527-03-02 Item 14

1 Screw NAS1801-3-25 Item 33

1 Washer NAS1149F0332P Item 46

1 Clip nut NSA5067-3-1 Item 43

Or install :

Refer to Fig. A-FCDAA Sheet 02 view C

2 Clamp NSA5516-13ND Item 63

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 428

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SERVICE BULLETIN

or

2 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

1 Spacer NSA5527-03-01 Item 12

1 Spacer NSA5527-03-02 Item 14

1 Screw NAS1801-3-25 Item 33

1 Washer NAS1149F0332P Item 46

1 Clip nut NSA5067-3-1 Item 43

(c) Depending on the staking, install :

Refer to Fig. A-FCDAA Sheet 02 view D

3 Clamp NSA5516-13ND Item 63

or

3 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

1 Spacer NSA5527-03-02 Item 14

1 Screw NAS1801-3-18 Item 79

1 Washer NAS1149F0332P Item 46

1 Clip nut NSA5067-3-1 Item 43

Or install :

Refer to Fig. A-FCDAA Sheet 02 view D

2 Clamp NSA5516-13ND Item 63

or

2 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

1 Spacer NSA5527-03-02 Item 14

1 Screw NAS1801-3-18 Item 79

1 Washer NAS1149F0332P Item 46

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 429

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@A300-600

SERVICE BULLETIN

1 Clip nut NSA5067-3-1 Item 43

(12) Subtask 246103-420-010-001 - Install a bracket on the shroud box blanking plate at

RH side, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

148 Work location Frame 51

from Stringer 31 to Stringer 33

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills AIRFRAME

Material necessary to do the job

Supplementary kit 246103A02S07

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

21 NSA5050-3 3 NUT

29 A0041113420100 1 BRACKET

30 NAS1801-3-8 2 SCREW

37 NAS1801-3-9 1 SCREW

46 NAS1149F0332P 2 WASHER

63 NSA5516-13ND CLAMP

64 NSA5516-31ND CLAMP

70 A0041113500000 1 CLAMP

71 NAS1801-3-12 2 SCREW

75 A0041113500200 1 CLAMP

76 A0041113500400 1 CLAMP

References

Fig. A-FBSAA

Installation of a Bracket on the Shroud

Box Blanking Plate (LH and RH side) -

ADDITIONAL WORK

Sheet 01

Sheet 02

(a) Remove :

Refer to Fig. A-FBSAA Sheet 01

2 Screw Item (27) Discard

2 Washer Item (46) Discard

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 430

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@A300-600

SERVICE BULLETIN

(b) Install the bracket :

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

1 Bracket A0041113420100 Item 29

attach with :

2 Screw NAS1801-3-12 Item 71

2 Washer NAS1149F0332P Item 46

(c) Attach the bundles on the shroud box bracket :

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

1 Attach the bundles with :

2 Clamp NSA5516-13ND Item 63

or

2 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

NOTE: Two or three bundles may be installed.

attach with :

1 Nut NSA5050-3 Item 21

1 Screw NAS1801-3-9 Item 37

2 Or attach the bundles with :

1 Clamp NSA5516-13ND Item 63

or

1 Clamp NSA5516-31ND Item 64

NOTE: Install clamp Item 63 or 64 according to the bundle diameters.

NOTE: Two or three bundles may be installed.

and

1 Clamp A0041113500000 Item 70

or

1 Clamp A0041113500200 Item 75

or

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 431

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@A300-600

SERVICE BULLETIN

1 Clamp A0041113500400 Item 76

NOTE: Install clamp Item 70 or 75 or 76 according to the bundle

diameters.

attach with :

2 Nut NSA5050-3 Item 21

2 Screw NAS1801-3-8 Item 30

(13) Subtask 246103-831-050-002 - Modify the routing on Rib 1 on the passage way to

the shroud box at RH side, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

147 Work location Frame 51

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 246103A04R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

24 NSA939510BN 1 (M) STRIP

Kit 246103A05R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

12 NSA5527-03-01 1 SPACER

13 NSA5527-03-03 3 SPACER

14 NSA5527-03-02 3 SPACER

21 NSA5050-3 4 NUT

23 NSA935401-05 2 TIE

26 NSA935401-04 2 TIE

33 NAS1801-3-25 1 SCREW

46 NAS1149F0332P 6 WASHER

51 NSA5516-12ND 15 CLAMP

52 NSA5516-08ND 15 CLAMP

62 NAS1801-3-22 1 SCREW

63 NSA5516-13ND 15 CLAMP

64 NSA5516-31ND 15 CLAMP

66 NSA935401-13 2 TIE

84 NSA5527-03-06 1 SPACER

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 432

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@A300-600

SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

87 NSA360002 1 (M) EXTRUSIN

91 NSA5527-03-15 2 SPACER

92 NSA5527-03-12 1 SPACER

94 NSA5159-35 1 STUD

95 NSA5527-03-18 2 SPACER

96 NSA5527-03-09 1 SPACER

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Epoxy Adhesive-Metal To

Metal - Legacy

05EJL9 As required

Epoxy Adhesive - Legacy 3 05EML7 As required

Contact Adhesive-Rubber &

Plastic Bonding Neopren

05JBC9 As required

Non Aqueous Cleaner -

Isopropyl Alcohol

08BBD1 As required

References

Process and Material Specification

(PMS)

Process and Material Specification (PMS)

01-01-28 Process E

Fig. A-FCCAB

Modification of the Clamps on the

Passage Way to the Shroud Box (LH

and RH Side) - ADDITIONAL WORK

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

(a) Depending on the stacking, remove:

Refer to Fig. A-FCCAB Sheet 01 and Fig. A-FCCAB Sheet 03 view A-A

1 Nut Item (21) Discard

5 Clamp Item (51) Discard

or

5 Clamp Item (52) Discard

or

5 Clamp Item (63) Discard

or

5 Clamp Item (64) Discard

1 Spacer Item (91) Discard

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 433

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@A300-600

SERVICE BULLETIN

1 Spacer Item (92) Discard

1 Spacer Item (93) Discard

1 Washer Item (46) Discard

(b) Depending on the stacking, remove:

Refer to Fig. A-FCCAB Sheet 01 and Fig. A-FCCAB Sheet 03 view B-B

1 Nut Item (21) Discard

5 Clamp Item (51) Discard

or

5 Clamp Item (52) Discard

or

5 Clamp Item (63) Discard

or

5 Clamp Item (64) Discard

1 Spacer Item (14) Discard

1 Spacer Item (91) Discard

1 Spacer Item (84) Discard

1 Spacer Item (97) Discard

1 Washer Item (46) Discard

(c) Depending on the stacking, remove:

Refer to Fig. A-FCCAB Sheet 01 and Fig. A-FCCAB Sheet 04 view C-C

1 Screw Item (33) Discard

1 Screw Item (62) Discard

2 Washer Item (46) Discard

5 Clamp Item (51) Discard

or

5 Clamp Item (52) Discard

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 434

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@A300-600

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or

5 Clamp Item (63) Discard

or

5 Clamp Item (64) Discard

1 Spacer Item (84) Discard

2 Spacer Item (95) Discard

3 Spacer Item (93) Discard

(d) Install:

Refer to Fig. A-FCCAB Sheet 01 and Fig. A-FCCAB Sheet 05view D-D

1 Stud NSA5159-35 Item 94

1 Nut NSA5050-3 Item 21

3 Clamp NSA5516-12ND Item 51

or

3 Clamp NSA5516-08ND Item 52

or

3 Clamp NSA5516-13ND Item 63

or

3 Clamp NSA5516-31ND Item 64

1 Spacer NSA5527-03-15 Item 91

1 Spacer NSA5527-03-12 Item 92

3 Spacer NSA5527-03-03 Item 13

1 Nut NSA5050-3 Item 21

2 Washer NAS1149F0332P Item 46

(e) Refer to Fig. A-FCCAB Sheet 01 and Fig. A-FCCAB Sheet 05 view E-E

1 Nut NSA5050-3 Item 21

2 Clamp NSA5516-08ND Item 52

or

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 435

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@A300-600

SERVICE BULLETIN

2 Clamp NSA5516-12ND Item 51

or

2 Clamp NSA5516-13ND Item 63

or

2 Clamp NSA5516-31ND Item 64

2 Spacer NSA5527-03-02 Item 14

1 Washer NAS1149F0332P Item 46

(f) Refer to Fig. A-FCCAB Sheet 01 and Fig. A-FCCAB Sheet 06 view F-F

1 Nut NSA5050-3 Item 21

5 Clamp NSA5516-08ND Item 52

or

5 Clamp NSA5516-12ND Item 51

or

5 Clamp NSA5516-13ND Item 63

or

5 Clamp NSA5516-31ND Item 64

1 Spacer NSA5527-03-02 Item 14

1 Spacer NSA5527-03-15 Item 91

1 Spacer NSA5527-03-06 Item 84

1 Washer NAS1149F0332P Item 46

(g) Refer to Fig. A-FCCAB Sheet 01 and Fig. A-FCCAB Sheet 06 and view G-G

1 Screw NAS1801-3-22 Item 62

1 Washer NAS1149F0332P Item 46

3 Clamp NSA5516-08ND Item 52

3 Clamp NSA5516-12ND Item 51

3 Clamp NSA5516-13ND Item 63

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 436

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3 Clamp NSA5516-31ND Item 64

1 Spacer NSA5527-03-09 Item 96

(h) Refer to Fig. A-FCCAB Sheet 01 and Fig. A-FCCAB Sheet 06 view H-H

1 Screw NAS1801-3-25 Item 33

1 Washer NAS1149F0332P Item 46

2 Clamp NSA5516-08ND Item 52

2 Clamp NSA5516-12ND Item 51

2 Clamp NSA5516-13ND Item 63

2 Clamp NSA5516-31ND Item 64

2 Spacer NSA5527-03-18 Item 95

(i) Refer to Fig. A-FCCAB Sheet 01 and Fig. A-FCCAB Sheet 06 view J-J

2 Tie-Cable NSA935401-13 Item 66

or

2 Tie-Cable NSA935401-04 Item 26

or

2 Tie-Cable NSA935401-05 Item 23

1 Spacer NSA5527-03-01 Item 12

(j) Install:

Refer to Fig. A-FCCAB Sheet 01 and Fig. A-FCCAB Sheet 05

1 (M) Extrusion NSA360002 Item 87

with:

Contact AdhesiveRubber & Plastic

Bonding Neopren

05JBC9 As required

(k) Modify the grommet installation :

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

1 Remove :

1 (M) Strip Protective Item (24) Discard

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 437

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@A300-600

SERVICE BULLETIN

2 Install :

Refer to Process and Material Specification (PMS) 01-01-28 Process E

1 (M) Strip-Protective NSA939510BN Item 24

NOTE: Install the Strip-Protective Item 24 with:

Epoxy AdhesiveMetal To Metal -

Legacy

05EJL9 As required

NOTE: Do the abrading and cleaning of the contact zones of StripProtective Item 24, on the structure with:

Non Aqueous

Cleaner - Isopropyl

Alcohol

08BBD1 As required

Epoxy Adhesive -

Legacy 3

05EML7 As required

(14) Subtask 246103-831-036-001 - Modify the routing of the routes 2E and 2G in the

leading edge at RH wing, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

613

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills NON SPECIFIC

Material necessary to do the job

Supplementary kit 246103A02S07

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

66 NSA935401-13 2 TIE

References

Fig. A-FBQAA

Modification of the Routing in the

Leading Edge (LH and RH side) -

ADDITIONAL WORK

Sheet 01

(a) Remove :

Refer to Fig. A-FBQAA Sheet 01

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 438

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SERVICE BULLETIN

2 Tie-Cable NSA935401-05 Item (23) Discard

(b) Install :

Refer to Fig. A-FBQAA Sheet 01

2 Tie-Cable NSA935401-13 Item 66

(15) Subtask 246103-020-008-001 - Remove the clamps from LH wings, ADDITIONAL

WORK

Work Zones and Access Panels

Zone Access/Work location

572

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

References

Fig. A-FBOAA

Removal/Installation of the Clamps in LH

and RH Wings - ADDITIONAL WORK

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

(a) Remove the clamps from LH wing at Rib location WIAX-27.96.

Refer to Fig. A-FBOAA Sheet 01 and Fig. A-FBOAA Sheet 05 view J

1 Remove :

2 Clamp Item (51) Discard

1 Screw Item (71) Discard

1 Washer Item (82) Discard

(b) Remove the clamps from LH wing at Rib location WIAX-40-53.

Refer to Fig. A-FBOAA Sheet 01 and Fig. A-FBOAA Sheet 03

1 Remove:

2 Screw Item (37) Retain

2 Washer Item (46) Discard

2 Clamp Item (51) Discard

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 439

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SERVICE BULLETIN

(c) Remove the clamps from LH wing at Rib location WIAX-48-25.

Refer to Fig. A-FBOAA Sheet 01 and Fig. A-FBOAA Sheet 05 view L

1 Remove:

2 Clamp Item (51) Discard

1 Screw Item (83) Discard

1 Washer Item (82) Discard

NOTE: If necessary, on LH wing at Rib location WIAX-74.08, remove:

2 (M) Tape-Reinforced

Silicone

Item (85) Discard

(16) Subtask 246103-020-009-001 - Remove the clamps from RH wings, ADDITIONAL

WORK

Work Zones and Access Panels

Zone Access/Work location

672

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

References

Fig. A-FBOAA

Removal/Installation of the Clamps in LH

and RH Wings - ADDITIONAL WORK

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

(a) Remove the clamps from RH wing at Rib location WIAX-27.96.

Refer to Fig. A-FBOAA Sheet 01 and Fig. A-FBOAA Sheet 05 view J

1 Remove :

2 Clamp Item (51) Discard

1 Screw Item (71) Discard

1 Washer Item (82) Discard

(b) Remove the clamps from RH wing at Rib location WIAX-40-53.

Refer to Fig. A-FBOAA Sheet 01 and Fig. A-FBOAA Sheet 03

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 440

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@A300-600

SERVICE BULLETIN

1 Remove:

2 Screw Item (37) Retain

2 Washer Item (46) Discard

2 Clamp Item (51) Discard

(c) Remove the clamps from RH wing at Rib location WIAX-48-25.

Refer to Fig. A-FBOAA Sheet 01 and Fig. A-FBOAA Sheet 05 view L

1 Remove:

2 Clamp Item (51) Discard

1 Screw Item (83) Discard

1 Washer Item (82) Discard

NOTE: If necessary, on RH wing at Rib location WIAX 74.08, remove:

2 (M) Tape-Reinforced

Silicone

Item (85) Discard

(17) Subtask 246103-831-048-001 - Modify the routing of routes 1P and 2P at LH wing,

ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

570 Work location from Rib 1 to Rib 6

Manpower Resources

Manhours 1.50

Minimum number of person 1

Subtask elapsed time 1.50

Skills NON SPECIFIC

Material necessary to do the job

Supplementary kit 246103A01S08

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

14 NSA5527-03-02 3 SPACER

25 ABS0596S005 2 INSULATR

26 NSA935401-04 12 TIE

66 NSA935401-13 3 TIE

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 441

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@A300-600

SERVICE BULLETIN

Supplementary kit 246103A01S11

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

86 EN6049-007-08-5 2.5 (M) SLEEVE

References

Fig. A-FCMAA

Modification of the Routing in LH and

RH Wings - ADDITIONAL WORK

Sheet 01

Sheet 02

(a) Between rib 5 and rib 6, remove:

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

2 Insulator Item (25) Discard

12 Tie-Cable Item (26)

and

3 Spacer Item (14) Discard

attached with:

3 Tie-Cable Item (66) Discard

(b) Between rib 5 and rib 6, install:

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

2.5 (M) Sleeve-Protective EN6049-007-08-5 Item 86

12 Tie-Cable NSA935401-04 Item 26

and

3 Spacer NSA5527-03-02 Item 14

attached with :

3 Tie-Cable NSA935401-13 Item 66

(c) The following part of the Skit A01S08 must no be used anymore for LH wing:

2 Insulator ABS0596S005 Item 25

(18) Subtask 246103-831-049-001 - Modify the routing of routes 1P and 2P at RH wing,

ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

670 Work location from Rib 1 to Rib 6

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 442

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@A300-600

SERVICE BULLETIN

Manpower Resources

Manhours 1.50

Minimum number of person 1

Subtask elapsed time 1.50

Skills NON SPECIFIC

Material necessary to do the job

Supplementary kit 246103A02S07

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

14 NSA5527-03-02 3 SPACER

25 ABS0596S005 2 INSULATR

26 NSA935401-04 12 TIE

66 NSA935401-13 3 TIE

Supplementary kit 246103A02S10

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

86 EN6049-007-08-5 2.5 (M) SLEEVE

References

Fig. A-FCMAA

Modification of the Routing in LH and

RH Wings - ADDITIONAL WORK

Sheet 01

Sheet 02

(a) Between rib 5 and rib 6, remove:

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

2 Insulator Item (25) Discard

12 Tie-Cable Item (26) Discard

and

3 Spacer Item (14) Discard

attached with:

3 Tie-Cable Item (66) Discard

(b) Between rib 5 and rib 6, install:

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

2.5 (M) Sleeve-Protective EN6049-007-08-5 Item 86

12 Tie-Cable NSA935401-04 Item 26

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 443

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SERVICE BULLETIN

and

3 Spacer NSA5527-03-02 Item 14

attached with :

3 Tie-Cable NSA935401-13 Item 66

(c) The following part of the Skit A02S07 must no be used anymore for RH wing:

2 Insulator ABS0596S005 Item 25

(19) Subtask 246103-831-045-001 - Install the clamps in LH wing, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

572

Manpower Resources

Manhours 1.00

Minimum number of person 2

Subtask elapsed time 0.50

Skills NON SPECIFIC

Material necessary to do the job

Kit 246103B01R03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

60 A9245000200000 1 GUIDE

Supplementary kit 246103A01S08

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

51 NSA5516-12ND 6 CLAMP

82 ASNA2397KD10L 2 WASHER

85 ASNA51072503 2 (M) TAPE

Supplementary kit 246103A01S11

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

12 NSA5527-03-01 1 SPACER

37 NAS1801-3-9 2 SCREW

46 NAS1149F0332P 6 WASHER

52 NSA5516-08ND 8 CLAMP

55 NAS1801-3-16 1 SCREW

86 EN6049-007-08-5 2.5 (M) SLEEVE

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 444

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@A300-600

SERVICE BULLETIN

Supplementary kit 246103A03S01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

21 NSA5050-3 2 NUT

22 NAS1801-3-24 2 SCREW

90 NAS1149D0316H 2 WASHER

References

Fig. A-FBOAA

Removal/Installation of the Clamps in LH

and RH Wings - ADDITIONAL WORK

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

(a) Install the clamps LH wing at Rib location WIAX-27.96

Refer to Fig. A-FBOAA Sheet 01 and Fig. A-FBOAA Sheet 05 view K

1 Install:

2 Clamp NSA5516-08ND Item 52

1 Washer NAS1149F0332P Item 46

1 Screw NAS1801-3-9 Item 37

(b) Install the clamps LH wing at Rib location WIAX-35.12

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

1 Install:

1 Screw Item (50) Retained at

removal

1 Spacer Item (13) Retained at

removal

1 Spacer NSA5527-03-01 Item 12

2 Washer NAS1149F0332P Item 46

1 Screw NAS1801-3-16 Item 55

2 Clamp NSA5516-08ND Item 52

(c) Install the clamps in LH wing at Rib location WIAX-40.53.

Refer to Fig. A-FBOAA Sheet 01 and Fig. A-FBOAA Sheet 03

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 445

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@A300-600

SERVICE BULLETIN

1 Install:

2 Screw Item (37) Retained at

removal

2 Washer NAS1149F0332P Item 46

2 Clamp NSA5516-08ND Item 52

(d) Install the clamps LH wing at Rib location WIAX-48.25

Refer to Fig. A-FBOAA Sheet 01 and Fig. A-FBOAA Sheet 05 view M

1 Install:

2 Clamp NSA5516-08ND Item 52

1 Washer NAS1149F0332P Item 46

1 Screw NAS1801-3-9 Item 37

(e) Install the clamps at LH wing at Rib location WIAX-74.08.

Refer to Fig. A-FBOAA Sheet 01 and Fig. A-FBOAA Sheet 04

1 Install:

2 Nut NSA5050-3 Item 21

2 Screw NAS1801-3-24 Item 22

2 Washer NAS1149D0316H Item 90

1 Guide Assy-Conduit A9245000200000 Item 60

NOTE: If necessary, to make the diameters of the bundles match with

the diameter of the holes of the guide Item 60, use:

2.5 (M) Sleeve-Protective EN6049-007-08-5 Item 86

2 (M) Tape-Reinforced

Silicone

ASNA51072503 Item 85

(f) The following parts of the Skit A01S08 must not be used anymore for WIAX-27.96,

WIAX-40.53, WIAX-48.25 and WIAX-74.08:

6 Clamp NSA5516-12ND Item 51

2 Washer ASNA2397KD10L Item 82

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 446

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SERVICE BULLETIN

(20) Subtask 246103-831-047-001 - Install the clamps in RH wing, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

672

Manpower Resources

Manhours 1.00

Minimum number of person 2

Subtask elapsed time 0.5

Skills NON SPECIFIC

Material necessary to do the job

Kit 246103B01R03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

60 A9245000200000 1 GUIDE

Supplementary kit 246103A02S10

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

12 NSA5527-03-01 1 SPACER

37 NAS1801-3-9 2 SCREW

46 NAS1149F0332P 6 WASHER

52 NSA5516-08ND 8 CLAMP

55 NAS1801-3-16 1 SCREW

85 ASNA51072503 1 (M) TAPE

86 EN6049-007-08-5 2.5 (M) SLEEVE

Supplementary kit 246103A03S01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

21 NSA5050-3 2 NUT

22 NAS1801-3-24 2 SCREW

90 NAS1149D0316H 2 WASHER

References

Fig. A-FBOAA

Removal/Installation of the Clamps in LH

and RH Wings - ADDITIONAL WORK

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

(a) Install the clamps in RH wing at Rib location WIAX-27.96

Refer to Fig. A-FBOAA Sheet 01 and Fig. A-FBOAA Sheet 05 view K

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 447

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SERVICE BULLETIN

1 Install:

2 Clamp NSA5516-08ND Item 52

1 Washer NAS1149F0332P Item 46

1 Screw NAS1801-3-9 Item 37

(b) Install the clamps in RH wing at Rib location WIAX-35.12.

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

1 Install:

1 Spacer Item (13) Retained at

removal

1 Screw Item (50) Retained at

removal

1 Spacer NSA5527-03-01 Item 12

2 Washer NAS1149F0332P Item 46

1 Screw NAS1801-3-16 Item 55

2 Clamp NSA5516-08ND Item 52

(c) Install the clamps in RH wing at Rib location WIAX-40.53

Refer to Fig. A-FBOAA Sheet 01 and Fig. A-FBOAA Sheet 03

1 Install:

2 Screw Item (37) Retained at

removal

2 Washer NAS1149F0332P Item 46

2 Clamp NSA5516-08ND Item 52

(d) Install the clamps in RH wing at Rib location WIAX-48.25

Refer to Fig. A-FBOAA Sheet 01 and Fig. A-FBOAA Sheet 05 view M

1 Install:

2 Clamp NSA5516-08ND Item 52

1 Washer NAS1149F0332P Item 46

1 Screw NAS1801-3-9 Item 37

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 448

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SERVICE BULLETIN

(e) Install the clamps in LH wing at Rib location WIAX-74.08.

Refer to Fig. A-FBOAA Sheet 01 and Fig. A-FBOAA Sheet 04

1 Install:

2 Nut NSA5050-3 Item 21

2 Screw NAS1801-3-24 Item 22

2 Washer NAS1149D0316H Item 90

1 Guide Assy-Conduit A9245000200000 Item 60

NOTE: If necessary, to make the diameters of the bundles match with

the diameter of the holes of the guide Item 60, use:

2.5 (M) Sleeve-Protective EN6049-007-08-5 Item 86

1 (M) Tape-Reinforced

Silicone

ASNA51072503 Item 85

**CONF ALL

D. TEST

**CONF 001

(1) Subtask 246103-700-003-001 - Testing

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 27-54-41, Page Block 401

29-12-46, Page Block 401

(a) Job set-up

1 Remove the safety clips and tags and close the circuit breakers as specified

after the installation of the inner flap deflectors (Refer to AMM 27-54-41, Page

Block 401).

2 Remove the safety clips and tags and close the circuit breakers as specified

after the installation of the BLUE hydraulic reservoir (Refer to AMM 29-12-46,

Page Block 401).

(b) Procedure

1 Do the test procedure as specified after the installation of the inner flap

deflectors (Refer to AMM 27-54-41, Page Block 401).

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 449

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2 Do the test procedure as specified after the installation of the BLUE hydraulic

reservoir (Refer to AMM 29-12-46, Page Block 401).

**CONF 002

(1) Subtask 246103-700-003-001 - Testing

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 27-54-41, Page Block 401

29-12-46, Page Block 401

(a) Job set-up

1 Remove the safety clips and tags and close the circuit breakers as specified

after the installation of the inner flap deflectors (Refer to AMM 27-54-41, Page

Block 401).

2 Remove the safety clips and tags and close the circuit breakers as specified

after the installation of the BLUE hydraulic reservoir (Refer to AMM 29-12-46,

Page Block 401).

(b) Procedure

1 Do the test procedure as specified after the installation of the inner flap

deflectors (Refer to AMM 27-54-41, Page Block 401).

2 Do the test procedure as specified after the installation of the BLUE hydraulic

reservoir (Refer to AMM 29-12-46, Page Block 401).

**CONF 003

(1) Subtask 246103-700-003-001 - Testing

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 27-54-41, Page Block 401

29-12-46, Page Block 401

(a) Job set-up

1 Remove the safety clips and tags and close the circuit breakers as specified

after the installation of the inner flap deflectors (Refer to AMM 27-54-41, Page

Block 401).

2 Remove the safety clips and tags and close the circuit breakers as specified

after the installation of the BLUE hydraulic reservoir (Refer to AMM 29-12-46,

Page Block 401).

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 450

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SERVICE BULLETIN

(b) Procedure

1 Do the test procedure as specified after the installation of the inner flap

deflectors (Refer to AMM 27-54-41, Page Block 401).

2 Do the test procedure as specified after the installation of the BLUE hydraulic

reservoir (Refer to AMM 29-12-46, Page Block 401).

**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 246103-942-003-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001

27-54-41, Page Block 401

32-12-11, Page Block 301

(a) Close the inner deflectors between Rib. 1 and Rib. 6, refer to AMM 27-54-41, Page

Block 401.

(b) Install the access panels 512AB(612AB), 512BB(612BB), 512CB(612CB),

512DB(612DB), refer to AMM 06-41-57, Page Block 001.

(c) Install the access panels 512BB(612BB), refer to AMM 06-41-57, Page Block 001.

(d) Close the Main Landing Gear (MLG) doors, refer to AMM 32-12-11, Page Block

301.

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

(f) Remove the access platform(s).

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

**CONF 002

(1) Subtask 246103-942-003-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001

27-54-41, Page Block 401

32-12-11, Page Block 301

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 451

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(a) Close the inner deflectors between Rib. 1 and Rib. 6, refer to AMM 27-54-41, Page

Block 401.

(b) Install the access panels 512AB(612AB), 512BB(612BB), 512CB(612CB),

512DB(612DB), refer to AMM 06-41-57, Page Block 001.

(c) Install the access panels 512BB(612BB), refer to AMM 06-41-57, Page Block 001.

(d) Close the Main Landing Gear (MLG) doors, refer to AMM 32-12-11, Page Block

301.

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

(f) Remove the access platform(s).

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

**CONF 003

(1) Subtask 246103-942-003-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001

27-54-41, Page Block 401

32-12-11, Page Block 301

(a) Close the inner deflectors between Rib. 1 and Rib. 6, refer to AMM 27-54-41, Page

Block 401.

(b) Install the access panels 512AB(612AB), 512BB(612BB), 512CB(612CB),

512DB(612DB), refer to AMM 06-41-57, Page Block 001.

(c) Install the access panels 512BB(612BB), refer to AMM 06-41-57, Page Block 001.

(d) Close the Main Landing Gear (MLG) doors, refer to AMM 32-12-11, Page Block

301.

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

(f) Remove the access platform(s).

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

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 452

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SERVICE BULLETIN

Task 246103-831-805-001 - Modification - ADDITIONAL WORK between Revision No. 02 and

Revision No. 03

**CONF ALL

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

INCLUDED IN THE REFERENCED PROCEDURES.

CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP

ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY

AND MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENANCE

WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING,

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

THIS:

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

NECESSARY ON WIRING AND COMPONENTS.

- REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND

OTHER CONTAMINATION.

THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION

AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION.

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

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

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

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

authority he belongs to, the accepted alternative procedure can be used. When the

words "in accordance with" are used then the given procedure must be followed.

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

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

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

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

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

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

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

NOTE: This Service Bulletin is classified mandatory or expected to be classified mandatory

by an Airworthiness Directive (AD). The paragraphs 3.C. and 3.D. in these

accomplishment instructions are Required for Compliance (RC) and must be done

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

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

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

the aircraft can be put back into a serviceable condition.

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 453

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Task Associated Data

**CONF 001

Zone

570 572 670 672

Manpower

TOTAL MANHOURS 16.50

ELAPSED TIME (HOURS) 8.50

**CONF 002

Zone

570 572 670 672

Manpower

TOTAL MANHOURS 16.50

ELAPSED TIME (HOURS) 8.50

**CONF 003

Zone

570 572 670 672

Manpower

TOTAL MANHOURS 18.50

ELAPSED TIME (HOURS) 9.50

**CONF ALL

A. GENERAL

**CONF 001

(1) Subtask 246103-910-005-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

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

06-31-53, Page Block 001

20-21-12, Page Block 001

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-25-51

20-33-00

20-33-30

20-33-41

20-33-42

20-33-44

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 454

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References

Structural Repair Manual (SRM) 51-40-00

51-40-20

51-40-30

51-40-40

51-75-10

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

the Consumable Material List (CML).

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

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

(d) For the identification of access panels, refer to AMM 06-21-00, Page Block 001.

(e) Tag all the parts you must remove and retain to make the subsequent installation

easier.

(f) Put all the retained hardware in identified plastic bags and attach the bags to the

related unit.

(g) Obtain fastener hole diameters and drill data in accordance with SRM 51-40-40.

(h) For the installation of the protective electrical conduits, refer to ESPM 20-33-00.

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

Block 001.

(j) Obtain alternative and substitute fastener data in accordance with SRM 51-40-30.

(k) If alternative and substitute fasteners have to be used, you must make sure that the

associated nut/collar are compatible in accordance with SRM 51-40-00 "Mating

Part" column.

(l) If the length of any fastener specified in this Service Bulletin does not meet

installation standards given in SRM Chapter 51, then a fastener of the same

specification, or an approved substitute, with a length which meets the installation

standards given in SRM Chapter 51 may be used. In addition, washers may be

installed for fastener grip length in accordance with SRM Chapter 51.

(m) Remove and install fasteners in accordance with SRM 51-40-20.

(n) For the cable tie application and tooling, refer to ESPM 20-33-44 and ESPM

20-25-51.

(o) Adapt the clamp size as necessary, refer to ESPM 20-33-42.

(p) For the general installation of electrical wire harnesses, refer to ESPM 20-33-00.

(q) Renew the protective finish in accordance with SRM 51-75-10.

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 455

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SERVICE BULLETIN

(2) Subtask 246103-839-005-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF 002

(1) Subtask 246103-910-005-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

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

06-31-53, Page Block 001

20-21-12, Page Block 001

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-25-51

20-33-00

20-33-30

20-33-41

20-33-42

20-33-44

Structural Repair Manual (SRM) 51-40-00

51-40-20

51-40-30

51-40-40

51-75-10

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

the Consumable Material List (CML).

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

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

(d) For the identification of access panels, refer to AMM 06-21-00, Page Block 001.

(e) Tag all the parts you must remove and retain to make the subsequent installation

easier.

(f) Put all the retained hardware in identified plastic bags and attach the bags to the

related unit.

(g) Obtain fastener hole diameters and drill data in accordance with SRM 51-40-40.

(h) For the installation of the protective electrical conduits, refer to ESPM 20-33-00.

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

Block 001.

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 456

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SERVICE BULLETIN

(j) Obtain alternative and substitute fastener data in accordance with SRM 51-40-30.

(k) If alternative and substitute fasteners have to be used, you must make sure that the

associated nut/collar are compatible in accordance with SRM 51-40-00 "Mating

Part" column.

(l) If the length of any fastener specified in this Service Bulletin does not meet

installation standards given in SRM Chapter 51, then a fastener of the same

specification, or an approved substitute, with a length which meets the installation

standards given in SRM Chapter 51 may be used. In addition, washers may be

installed for fastener grip length in accordance with SRM Chapter 51.

(m) Remove and install fasteners in accordance with SRM 51-40-20.

(n) For the cable tie application and tooling, refer to ESPM 20-33-44 and ESPM

20-25-51.

(o) Adapt the clamp size as necessary, refer to ESPM 20-33-42.

(p) For the general installation of electrical wire harnesses, refer to ESPM 20-33-00.

(q) Renew the protective finish in accordance with SRM 51-75-10.

(2) Subtask 246103-839-005-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF 003

(1) Subtask 246103-910-005-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

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

06-31-53, Page Block 001

20-21-12, Page Block 001

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-25-51

20-33-00

20-33-30

20-33-41

20-33-42

20-33-44

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 457

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SERVICE BULLETIN

References

Structural Repair Manual (SRM) 51-40-00

51-40-20

51-40-30

51-40-40

51-75-10

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

the Consumable Material List (CML).

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

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

(d) For the identification of access panels, refer to AMM 06-21-00, Page Block 001.

(e) Tag all the parts you must remove and retain to make the subsequent installation

easier.

(f) Put all the retained hardware in identified plastic bags and attach the bags to the

related unit.

(g) Obtain fastener hole diameters and drill data in accordance with SRM 51-40-40.

(h) For the installation of the protective electrical conduits, refer to ESPM 20-33-00.

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

Block 001.

(j) Obtain alternative and substitute fastener data in accordance with SRM 51-40-30.

(k) If alternative and substitute fasteners have to be used, you must make sure that the

associated nut/collar are compatible in accordance with SRM 51-40-00 "Mating

Part" column.

(l) If the length of any fastener specified in this Service Bulletin does not meet

installation standards given in SRM Chapter 51, then a fastener of the same

specification, or an approved substitute, with a length which meets the installation

standards given in SRM Chapter 51 may be used. In addition, washers may be

installed for fastener grip length in accordance with SRM Chapter 51.

(m) Remove and install fasteners in accordance with SRM 51-40-20.

(n) For the cable tie application and tooling, refer to ESPM 20-33-44 and ESPM

20-25-51.

(o) Adapt the clamp size as necessary, refer to ESPM 20-33-42.

(p) For the general installation of electrical wire harnesses, refer to ESPM 20-33-00.

(q) Renew the protective finish in accordance with SRM 51-75-10.

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 458

5

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@A300-600

SERVICE BULLETIN

(2) Subtask 246103-839-005-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF ALL

B. PREPARATION

**CONF 001

(1) Subtask 246103-941-006-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001

24-00-00, Page Block 301

27-54-41, Page Block 401

32-12-11, Page Block 301

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 24-00-00, Page

Block 301.

(b) Put an access platform in position at Zone(s) 513(613), 570(670), 571, 572(672)

and 147(148).

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 459

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(c) Open the Main Landing Gear (MLG) doors, refer to AMM 32-12-11, Page Block

301.

(d) Remove the access panels 512AB(612AB), 512BB(612BB), 512CB(612CB) and

512DB(612DB), refer to AMM 06-41-57, Page Block 001.

(e) Remove the access panels 571BB and 571DB, refer to AMM 06-41-57, Page Block

001.

(f) Open all the necessary inner deflectors between Rib. 1 and Rib. 6, refer to AMM

27-54-41, Page Block 401.

**CONF 002

(1) Subtask 246103-941-006-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001

24-00-00, Page Block 301

27-54-41, Page Block 401

32-12-11, Page Block 301

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 24-00-00, Page

Block 301.

(b) Put an access platform in position at Zone(s) 513(613), 570(670), 571, 572(672)

and 147(148).

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 460

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(c) Open the Main Landing Gear (MLG) doors, refer to AMM 32-12-11, Page Block

301.

(d) Remove the access panels 512AB(612AB), 512BB(612BB), 512CB(612CB) and

512DB(612DB), refer to AMM 06-41-57, Page Block 001.

(e) Remove the access panels 571BB and 571DB, refer to AMM 06-41-57, Page Block

001.

(f) Open all the necessary inner deflectors between Rib. 1 and Rib. 6, refer to AMM

27-54-41, Page Block 401.

**CONF 003

(1) Subtask 246103-941-006-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001

24-00-00, Page Block 301

27-54-41, Page Block 401

32-12-11, Page Block 301

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 24-00-00, Page

Block 301.

(b) Put an access platform in position at Zone(s) 513(613), 570(670), 571, 572(672)

and 147(148).

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 461

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@A300-600

SERVICE BULLETIN

(c) Open the Main Landing Gear (MLG) doors, refer to AMM 32-12-11, Page Block

301.

(d) Remove the access panels 512AB(612AB), 512BB(612BB), 512CB(612CB) and

512DB(612DB), refer to AMM 06-41-57, Page Block 001.

(e) Remove the access panels 571BB and 571DB, refer to AMM 06-41-57, Page Block

001.

(f) Open all the necessary inner deflectors between Rib. 1 and Rib. 6, refer to AMM

27-54-41, Page Block 401.

**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 246103-831-051-001 - Remove the clamps from LH wing, ADDITIONAL

WORK

Work Zones and Access Panels

Zone Access/Work location

572

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

References

Fig. A-FBOAA

Removal/Installation of the Clamps in LH

and RH Wings - ADDITIONAL WORK

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

(a) Remove the clamps from LH wing at Rib location WIAX-27.96.

Refer to Fig. A-FBOAA Sheet 01 and Fig. A-FBOAA Sheet 05 view J

1 Remove:

2 Clamp Item (51) Discard

1 Screw Item (71) Discard

1 Washer Item (82) Discard

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 462

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@A300-600

SERVICE BULLETIN

(b) Remove the clamps from LH wing at Rib location WIAX-35.12.

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

1 Remove:

1 Screw Item (50) Retain

1 Screw Item (50) Discard

2 Washer Item (46) Discard

2 Clamp Item (51) Discard

1 Spacer Item (13) Discard

1 Spacer Item (13) Retain

(c) Remove the clamps from LH wing at Rib location WIAX-40.53.

Refer to Fig. A-FBOAA Sheet 01 and Fig. A-FBOAA Sheet 03

1 Remove:

2 Screw Item (37) Retain

2 Washer Item (46) Discard

2 Clamp Item (51) Discard

(d) Remove the clamps from LH wing at Rib location WIAX-48.25.

Refer to Fig. A-FBOAA Sheet 01 and Fig. A-FBOAA Sheet 05 view L

1 Remove:

2 Clamp Item (51) Discard

1 Screw Item (83) Discard

1 Washer Item (82) Discard

(e) Remove the clamps from LH wing at Rib location WIAX-74.08.

Refer to Fig. A-FBOAA Sheet 01 and Fig. A-FBOAA Sheet 04

1 Remove:

2 Spacer Item (12) Discard

2 Nut Item (21) Discard

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 463

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@A300-600

SERVICE BULLETIN

2 Washer Item (61) Discard

2 Screw Item (80) Discard

1 Guide Assy-Conduit Item (60) Retain

(2) Subtask 246103-831-052-001 - Remove the clamps from RH wing, ADDITIONAL

WORK

Work Zones and Access Panels

Zone Access/Work location

672

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

References

Fig. A-FBOAA

Removal/Installation of the Clamps in LH

and RH Wings - ADDITIONAL WORK

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

(a) Remove the clamps from RH wing at Rib location WIAX-27.96.

Refer to Fig. A-FBOAA Sheet 01 and Fig. A-FBOAA Sheet 05 view J

1 Remove:

2 Clamp Item (51) Discard

1 Screw Item (71) Discard

1 Washer Item (82) Discard

(b) Remove the clamps from RH wing at Rib location WIAX-35.12.

Fig. A-FBOAA Sheet 01 and Fig. A-FBOAA Sheet 02

1 Remove:

1 Screw Item (50) Discard

1 Screw Item (50) Retain

2 Washer Item (46) Discard

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 464

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@A300-600

SERVICE BULLETIN

2 Clamp Item (51) Discard

1 Spacer Item (13) Discard

1 Spacer Item (13) Retain

(c) Remove the clamps from RH wing at Rib location WIAX-40.53.

Refer to Fig. A-FBOAA Sheet 01 and Fig. A-FBOAA Sheet 03

1 Remove:

2 Screw Item (37) Retain

2 Washer Item (46) Discard

2 Clamp Item (51) Discard

(d) Remove the clamps from RH wing at Rib location WIAX-48.25.

Refer to Fig. A-FBOAA Sheet 01 and Fig. A-FBOAA Sheet 05 view L

1 Remove:

2 Clamp Item (51) Discard

1 Screw Item (83) Discard

1 Washer Item (82) Discard

(e) Remove the clamps from RH wing at Rib location WIAX-74.08.

Refer to Fig. A-FBOAA Sheet 01 and Fig. A-FBOAA Sheet 04

1 Remove:

2 Spacer Item (12) Discard

2 Nut Item (21) Retain

2 Washer Item (61) Discard

2 Screw Item (80) Discard

1 Guide Assy-Conduit Item (60) Retain

(3) Subtask 246103-831-056-001 - Modify the routing of routes 1P and 2P at LH wing

Work Zones and Access Panels

Zone Access/Work location

570 Work location from Rib 1 to Rib 6

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 465

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@A300-600

SERVICE BULLETIN

Manpower Resources

Manhours 1.50

Minimum number of person 1

Subtask elapsed time 1.50

Skills NON SPECIFIC

Material necessary to do the job

Supplementary kit 246103A01S12

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

14 NSA5527-03-02 3 SPACER

26 NSA935401-04 12 TIE

66 NSA935401-13 3 TIE

86 EN6049-007-08-5 5 (M) SLEEVE

References

Fig. A-FCMAA

Modification of the Routing in LH and

RH Wings - ADDITIONAL WORK

Sheet 01

Sheet 02

(a) Between rib 5 and rib 6, remove:

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

2 Insulator Discard

12 Tie-Cable Discard

and

3 Spacer Discard

attached with:

3 Tie-Cable Discard

(b) Between rib 5 and rib 6, install:

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

5 (M) Sleeve-Protective EN6049-007-08-5 Item 86

12 Tie-Cable NSA935401-04 Item 26

and

3 Spacer NSA5527-03-02 Item 14

attached with:

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 466

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@A300-600

SERVICE BULLETIN

3 Tie-Cable NSA935401-13 Item 66

(4) Subtask 246103-831-057-001 - Modify the routing of routes 1P and 2P at RH wing

Work Zones and Access Panels

Zone Access/Work location

670 Work location from Rib 1 to Rib 6

Manpower Resources

Manhours 1.50

Minimum number of person 1

Subtask elapsed time 1.50

Skills NON SPECIFIC

Material necessary to do the job

Supplementary kit 246103A02S11

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

14 NSA5527-03-02 3 SPACER

26 NSA935401-04 12 TIE

66 NSA935401-13 3 TIE

86 EN6049-007-08-5 5 (M) SLEEVE

References

Fig. A-FCMAA

Modification of the Routing in LH and

RH Wings - ADDITIONAL WORK

Sheet 01

Sheet 02

(a) Between rib 5 and rib 6, remove:

Refer toFig. A-FCMAA Sheet 01 and Fig. A-FCMAA Sheet 02

2 Insulator Discard

12 Tie-Cable Discard

and

3 Spacer Discard

attached with:

3 Tie-Cable Discard

(b) Between rib 5 and rib 6, install:

Refer toFig. A-FCMAA Sheet 01 and Fig. A-FCMAA Sheet 02

5 (M) Sleeve-Protective EN6049-007-08-5 Item 86

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 467

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@A300-600

SERVICE BULLETIN

12 Tie-Cable NSA935401-04 Item 26

and

3 Spacer NSA5527-03-02 Item 14

attached with:

3 Tie-Cable NSA935401-13 Item 66

(5) Subtask 246103-831-053-001 - Install the clamps in LH wing, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

572

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Supplementary kit 246103A01S11

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

85 ASNA51072503 1 (M) TAPE

Supplementary kit 246103A01S12

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

12 NSA5527-03-01 1 SPACER

37 NAS1801-3-9 2 SCREW

46 NAS1149F0332P 6 WASHER

52 NSA5516-08ND 8 CLAMP

55 NAS1801-3-16 1 SCREW

86 EN6049-007-08-5 2.5 (M) SLEEVE

Supplementary kit 246103A03S01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

21 NSA5050-3 2 NUT

22 NAS1801-3-24 2 SCREW

90 NAS1149D0316H 2 WASHER

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 468

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@A300-600

SERVICE BULLETIN

References

Fig. A-FBOAA

Removal/Installation of the Clamps in LH

and RH Wings - ADDITIONAL WORK

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

(a) Install the clamps in LH wing at Rib location WIAX-27.96.

Refer to Fig. A-FBOAA Sheet 01 and Fig. A-FBOAA Sheet 05 view K

1 Install:

2 Clamp NSA5516-08ND Item 52

1 Washer NAS1149F0332P Item 46

1 Screw NAS1801-3-9 Item 37

(b) Install the clamps in LH wing at Rib location WIAX-35.12.

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

1 Install:

1 Screw Item (50) Retained at

removal

1 Spacer Item (13) Retained at

removal

1 Spacer NSA5527-03-01 Item 12

2 Washer NAS1149F0332P Item 46

1 Screw NAS1801-3-16 Item 55

2 Clamp NSA5516-08ND Item 52

(c) Install the clamps in LH wing at Rib location WIAX-40.53.

Refer to Fig. A-FBOAA Sheet 01 and Fig. A-FBOAA Sheet 03

1 Install:

2 Screw Item (37) Retained at

removal

2 Washer NAS1149F0332P Item 46

2 Clamp NSA5516-08ND Item 52

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 469

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@A300-600

SERVICE BULLETIN

(d) Install the clamps at LH wing at Rib location WIAX-48.25.

Refer to Fig. A-FBOAA Sheet 01 and Fig. A-FBOAA Sheet 05 view M

1 Install:

2 Clamp NSA5516-08ND Item 52

1 Washer NAS1149F0332P Item 46

1 Screw NAS1801-3-9 Item 37

(e) Install the clamps at LH wing at Rib location WIAX-74.08.

Refer to Fig. A-FBOAA Sheet 01 and Fig. A-FBOAA Sheet 04

1 Install:

2 Nut NSA5050-3 Item 21

2 Screw NAS1801-3-24 Item 22

2 Washer NAS1149D0316H Item 90

1 Guide Assy-conduit Item (60) Retained at

removal

NOTE: If necessary, to make the diameters of the bundles match with

the diameter of the holes of the guide Item 60, use:

2.5 (M) Sleeve-Protective EN6049-007-08-5 Item 86

1 (M) Tape-Reinforced

Silicone

ASNA51072503 Item 85

(6) Subtask 246103-831-054-001 - Install the clamps in RH wing, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

672

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 470

5

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@A300-600

SERVICE BULLETIN

Material necessary to do the job

Supplementary kit 246103A02S11

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

12 NSA5527-03-01 1 SPACER

37 NAS1801-3-9 2 SCREW

46 NAS1149F0332P 6 WASHER

52 NSA5516-08ND 6 CLAMP

55 NAS1801-3-16 1 SCREW

85 ASNA51072503 1 (M) TAPE

86 EN6049-007-08-5 2.5 (M) SLEEVE

Supplementary kit 246103A03S01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

21 NSA5050-3 2 NUT

22 NAS1801-3-24 2 SCREW

90 NAS1149D0316H 2 WASHER

References

Fig. A-FBOAA

Removal/Installation of the Clamps in LH

and RH Wings - ADDITIONAL WORK

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

(a) Install the clamps in RH wing at Rib location WIAX-27.96.

Refer to Fig. A-FBOAA Sheet 01 and Fig. A-FBOAA Sheet 05 view K

1 Install:

2 Clamp NSA5516-08ND Item 52

1 Washer NAS1149F0332P Item 46

1 Screw NAS1801-3-9 Item 37

(b) Install the clamps in RH wing at Rib location WIAX-35.12.

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

1 Install:

1 Spacer Item (13) Retained at

removal

1 Screw Item (50) Retained at

removal

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 471

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@A300-600

SERVICE BULLETIN

1 Spacer NSA5527-03-01 Item 12

2 Washer NAS1149F0332P Item 46

1 Screw NAS1801-3-16 Item 55

2 Clamp NSA5516-08ND Item 52

(c) Install the clamps in LH wing at Rib location WIAX-40.53.

Refer to Fig. A-FBOAA Sheet 01 and Fig. A-FBOAA Sheet 03

1 Install:

2 Screw Item (37) Retained at

removal

2 Washer NAS1149F0332P Item 46

2 Clamp NSA5516-08ND Item 52

(d) Install the clamps in LH wing at Rib location WIAX-48.25.

Refer to Fig. A-FBOAA Sheet 01 and Fig. A-FBOAA Sheet 05 view M

1 Install:

2 Clamp NSA5516-08ND Item 52

1 Washer NAS1149F0332P Item 46

1 Screw NAS1801-3-9 Item 37

(e) Install the clamps in LH wing at Rib location WIAX-74.08.

Refer to Fig. A-FBOAA Sheet 01 and Fig. A-FBOAA Sheet 04

1 Install:

2 Nut NSA5050-3 Item 21

2 Screw NAS1801-3-24 Item 22

2 Washer NAS1149D0316H Item 90

1 Guide Assy conduit Item (60) Retained at

removal

NOTE: If necessary, to make the diameters of the bundles match with

the diameter of the holes of the guide Item 60, use:

2.5 (M) Sleeve-Protective EN6049-007-08-5 Item 86

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 472

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@A300-600

SERVICE BULLETIN

1 (M) Tape-Reinforced

Silicone

ASNA51072503 Item 85

**CONF 002

(1) Subtask 246103-831-051-002 - Remove the clamps from LH wing, ADDITIONAL

WORK

Work Zones and Access Panels

Zone Access/Work location

572

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

References

Fig. A-FCOAA

Removal/Installation of the Clamps in LH

and RH Wings - ADDITIONAL WORK

Sheet 01

Sheet 02

Sheet 03

Sheet 04

(a) Remove the clamps from LH wing at Rib location WIAX-27.96.

Refer to Fig. A-FCOAA Sheet 01 and Fig. A-FCOAA Sheet 04 view J

1 Remove:

2 Clamp Item (51) Discard

1 Screw Item (71) Discard

1 Washer Item (82) Discard

(b) Remove the clamps from LH wing at Rib location WIAX-35.12.

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

1 Remove:

1 Screw Item (50) Retain

1 Screw Item (50) Discard

2 Washer Item (46) Discard

2 Clamp Item (51) Discard

1 Spacer Item (13) Discard

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 473

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SERVICE BULLETIN

1 Spacer Item (13) Retain

(c) Remove the clamps from LH wing at Rib location WIAX-40.53.

Refer to Fig. A-FCOAA Sheet 01 and Fig. A-FCOAA Sheet 03

1 Remove:

2 Screw Item (37) Retain

2 Washer Item (46) Discard

2 Clamp Item (51) Discard

(d) Remove the clamps from LH wing at Rib location WIAX-48.25.

Refer to Fig. A-FCOAA Sheet 01 and Fig. A-FCOAA Sheet 04 view L

1 Remove:

1 Washer Item (82) Discard

1 Screw Item (83) Discard

2 Clamp Item (51) Discard

(2) Subtask 246103-831-052-002 - Remove the clamps from RH wing, ADDITIONAL

WORK

Work Zones and Access Panels

Zone Access/Work location

672

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

References

Fig. A-FCOAA

Removal/Installation of the Clamps in LH

and RH Wings - ADDITIONAL WORK

Sheet 01

Sheet 02

Sheet 03

Sheet 04

(a) Remove the clamps from RH wing at Rib location WIAX-27.96.

Refer to Fig. A-FCOAA Sheet 01 and Fig. A-FCOAA Sheet 04view J

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 474

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@A300-600

SERVICE BULLETIN

1 Remove:

2 Clamp Item (51) Discard

1 Screw Item (71) Discard

1 Washer Item (82) Discard

(b) Remove the clamps from RH wing at Rib location WIAX-35.12.

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

1 Remove:

1 Screw Item (50) Discard

1 Screw Item (50) Retain

2 Washer Item (46) Discard

2 Clamp Item (51) Discard

1 Spacer Item (13) Discard

1 Spacer Item (13) Retain

(c) Remove the clamps from RH wing at Rib location WIAX-40.53.

Refer to Fig. A-FCOAA Sheet 01 and Fig. A-FCOAA Sheet 03

1 Remove:

2 Screw Item (37) Retain

2 Washer Item (46) Discard

2 Clamp Item (51) Discard

(d) Remove the clamps from RH wing at Rib location WIAX-48.25.

Refer to Fig. A-FCOAA Sheet 01 and Fig. A-FCOAA Sheet 04 view L

1 Remove:

1 Washer Item (82) Discard

1 Screw Item (83) Discard

2 Clamp Item (51) Discard

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 475

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@A300-600

SERVICE BULLETIN

(3) Subtask 246103-831-056-001 - Modify the routing of routes 1P and 2P at LH wing

Work Zones and Access Panels

Zone Access/Work location

570 Work location from Rib 1 to Rib 6

Manpower Resources

Manhours 1.50

Minimum number of person 1

Subtask elapsed time 1.50

Skills NON SPECIFIC

Material necessary to do the job

Supplementary kit 246103A01S12

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

14 NSA5527-03-02 3 SPACER

26 NSA935401-04 12 TIE

66 NSA935401-13 3 TIE

86 EN6049-007-08-5 5 (M) SLEEVE

References

Fig. A-FCMAA

Modification of the Routing in LH and

RH Wings - ADDITIONAL WORK

Sheet 01

Sheet 02

(a) Between rib 5 and rib 6, remove:

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

2 Insulator Discard

12 Tie-Cable Discard

and

3 Spacer Discard

attached with:

3 Tie-Cable Discard

(b) Between rib 5 and rib 6, install:

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

5 (M) Sleeve-Protective EN6049-007-08-5 Item 86

12 Tie-Cable NSA935401-04 Item 26

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 476

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@A300-600

SERVICE BULLETIN

and

3 Spacer NSA5527-03-02 Item 14

attached with:

3 Tie-Cable NSA935401-13 Item 66

(4) Subtask 246103-831-057-001 - Modify the routing of routes 1P and 2P at RH wing

Work Zones and Access Panels

Zone Access/Work location

670 Work location from Rib 1 to Rib 6

Manpower Resources

Manhours 1.50

Minimum number of person 1

Subtask elapsed time 1.50

Skills NON SPECIFIC

Material necessary to do the job

Supplementary kit 246103A02S11

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

14 NSA5527-03-02 3 SPACER

26 NSA935401-04 12 TIE

66 NSA935401-13 3 TIE

86 EN6049-007-08-5 5 (M) SLEEVE

References

Fig. A-FCMAA

Modification of the Routing in LH and

RH Wings - ADDITIONAL WORK

Sheet 01

Sheet 02

(a) Between rib 5 and rib 6, remove:

Refer toFig. A-FCMAA Sheet 01 and Fig. A-FCMAA Sheet 02

2 Insulator Discard

12 Tie-Cable Discard

and

3 Spacer Discard

attached with:

3 Tie-Cable Discard

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 477

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@A300-600

SERVICE BULLETIN

(b) Between rib 5 and rib 6, install:

Refer toFig. A-FCMAA Sheet 01 and Fig. A-FCMAA Sheet 02

5 (M) Sleeve-Protective EN6049-007-08-5 Item 86

12 Tie-Cable NSA935401-04 Item 26

and

3 Spacer NSA5527-03-02 Item 14

attached with:

3 Tie-Cable NSA935401-13 Item 66

(5) Subtask 246103-831-053-002 - Install the clamps in LH wing, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

572

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Supplementary kit 246103A01S12

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

12 NSA5527-03-01 1 SPACER

37 NAS1801-3-9 1 SCREW

46 NAS1149F0332P 5 WASHER

52 NSA5516-08ND 6 CLAMP

55 NAS1801-3-16 1 SCREW

References

Fig. A-FCOAA

Removal/Installation of the Clamps in LH

and RH Wings - ADDITIONAL WORK

Sheet 01

Sheet 02

Sheet 03

Sheet 04

(a) Install the clamps in LH wing at Rib location WIAX-27.96.

Refer to Fig. A-FCOAA Sheet 01 and Fig. A-FCOAA Sheet 04 view K

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 478

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

1 Install:

2 Clamp NSA5516-08ND Item 52

1 Washer NAS1149F0332P Item 46

1 Screw NAS1801-3-9 Item 37

(b) Install the clamps in LH wing at Rib location WIAX-35.12.

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

1 Install:

1 Screw Item (50) Retained at

removal

1 Spacer Item (13) Retained at

removal

1 Spacer NSA5527-03-01 Item 12

2 Washer NAS1149F0332P Item 46

1 Screw NAS1801-3-16 Item 55

2 Clamp NSA5516-08ND Item 52

(c) Install the clamps in LH wing at Rib location WIAX-40.53.

Refer to Fig. A-FCOAA Sheet 01 and Fig. A-FCOAA Sheet 03

1 Install:

2 Screw Item (37) Retained at

removal

2 Washer NAS1149F0332P Item 46

2 Clamp NSA5516-08ND Item 52

(d) Install the clamps in LH wing at Rib location WIAX-48.25.

Refer to Fig. A-FCOAA Sheet 01 and Fig. A-FCOAA Sheet 04 view M

1 Install:

2 Clamp NSA5516-08ND Item 52

1 Washer NAS1149F0332P Item 46

1 Screw NAS1801-3-9 Item 37

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 479

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

(6) Subtask 246103-831-054-002 - Install the clamps in RH wing, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

672

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Supplementary kit 246103A02S11

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

12 NSA5527-03-01 1 SPACER

37 NAS1801-3-9 2 SCREW

46 NAS1149F0332P 6 WASHER

52 NSA5516-08ND 8 CLAMP

55 NAS1801-3-16 1 SCREW

References

Fig. A-FCOAA

Removal/Installation of the Clamps in LH

and RH Wings - ADDITIONAL WORK

Sheet 01

Sheet 02

Sheet 03

Sheet 04

(a) Install the clamps in RH wing at Rib location WIAX-27.96.

Refer to Fig. A-FCOAA Sheet 01 and Fig. A-FCOAA Sheet 04 view K

1 Install:

2 Clamp NSA5516-08ND Item 52

1 Washer NAS1149F0332P Item 46

1 Screw NAS1801-3-9 Item 37

(b) Install the clamps in RH wing at Rib location WIAX-35.12.

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

1 Install:

1 Spacer Item (13) Retained at

removal

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 480

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

1 Screw Item (50) Retained at

removal

1 Spacer NSA5527-03-01 Item 12

2 Washer NAS1149F0332P Item 46

1 Screw NAS1801-3-16 Item 55

2 Clamp NSA5516-08ND Item 52

(c) Install the clamps in RH wing at Rib location WIAX-40.53.

Refer to Fig. A-FCOAA Sheet 01 and Fig. A-FCOAA Sheet 03

1 Install:

2 Screw Item (37) Retained at

removal

2 Washer NAS1149F0332P Item 46

2 Clamp NSA5516-08ND Item 52

(d) Install the clamps in RH wing at Rib location WIAX-48.25.

Refer to Fig. A-FCOAA Sheet 01 and Fig. A-FCOAA Sheet 04 view M

1 Install:

2 Clamp NSA5516-08ND Item 52

1 Washer NAS1149F0332P Item 46

1 Screw NAS1801-3-9 Item 37

**CONF 003

(1) Subtask 246103-831-037-001 - Modify the routing on Rib 1 on the passage way to

the shroud box at LH side, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

570 Work location Rib 1

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 481

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

Material necessary to do the job

Kit 246103A04R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

12 NSA5527-03-01 1 SPACER

13 NSA5527-03-03 3 SPACER

14 NSA5527-03-02 3 SPACER

21 NSA5050-3 4 NUT

23 NSA935401-05 2 TIE

26 NSA935401-04 2 TIE

33 NAS1801-3-25 1 SCREW

46 NAS1149F0332P 6 WASHER

51 NSA5516-12ND 15 CLAMP

52 NSA5516-08ND 15 CLAMP

62 NAS1801-3-22 1 SCREW

63 NSA5516-13ND 15 CLAMP

64 NSA5516-31ND 15 CLAMP

66 NSA935401-13 2 TIE

84 NSA5527-03-06 1 SPACER

91 NSA5527-03-15 2 SPACER

92 NSA5527-03-12 1 SPACER

94 NSA5159-35 1 STUD

95 NSA5527-03-18 1 SPACER

96 NSA5527-03-09 1 SPACER

References

Fig. A-FCPAA

Removal and Installation of the Clamps

on the Passage Way to the Shroud Box

(LH and RH side)

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

(a) Depending on the stacking, remove:

Refer to Fig. A-FCPAA Sheet 01 and Fig. A-FCPAA Sheet 02 view A-A

1 Nut Item (21) Discard

5 Clamp Item (51) Discard

or

5 Clamp Item (52) Discard

or

5 Clamp Item (63) Discard

or

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 482

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

5 Clamp Item (64) Discard

1 Spacer Item (91) Discard

1 Spacer Item (92) Discard

1 Spacer Item (13) Discard

1 Washer Item (46) Discard

(b) Depending on the stacking, remove:

Refer to Fig. A-FCPAA Sheet 01 and Fig. A-FCPAA Sheet 02 view B-B

1 Nut Item (21) Discard

5 Clamp Item (51) Discard

or

5 Clamp Item (52) Discard

or

5 Clamp Item (63) Discard

or

5 Clamp Item (64) Discard

1 Spacer Item (14) Discard

1 Spacer Item (91) Discard

1 Spacer Item (84) Discard

1 Spacer Item (97) Discard

1 Washer Item (46) Discard

(c) Depending on the stacking, remove:

Refer to Fig. A-FCPAA Sheet 01 and Fig. A-FCPAA Sheet 03 view C-C

1 Screw Item (33) Discard

2 Washer Item (46) Discard

1 Screw Item (62) Discard

5 Clamp Item (51) Discard

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 483

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

or

5 Clamp Item (52) Discard

or

5 Clamp Item (63) Discard

or

5 Clamp Item (64) Discard

1 Spacer Item (84) Discard

2 Spacer Item (95) Discard

3 Spacer Item (13) Discard

(d) Install:

Refer to Fig. A-FCPAA Sheet 01 and Fig. A-FCPAA Sheet 04 view D-D

1 Stud NSA5159-35 Item 94

1 Nut NSA5050-3 Item 21

3 Clamp NSA5516-12ND Item 51

or

3 Clamp NSA5516-08ND Item 52

or

3 Clamp NSA5516-13ND Item 63

or

3 Clamp NSA5516-31ND Item 64

1 Spacer NSA5527-03-15 Item 91

1 Spacer NSA5527-03-12 Item 92

3 Spacer NSA5527-03-03 Item 13

1 Nut NSA5050-3 Item 21

2 Washer NAS1149F0332P Item 46

(e) Install:

Refer to Fig. A-FCPAA Sheet 01 and Fig. A-FCPAA Sheet 04 view E-E

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 484

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

1 Nut NSA5050-3 Item 21

2 Clamp NSA5516-08ND Item 52

or

2 Clamp NSA5516-12ND Item 51

or

2 Clamp NSA5516-13ND Item 63

or

2 Clamp NSA5516-31ND Item 64

2 Spacer NSA5527-03-02 Item 14

1 Washer NAS1149F0332P Item 46

(f) Install:

Refer to Fig. A-FCPAA Sheet 01 and Fig. A-FCPAA Sheet 05 and view F-F

1 Nut NSA5050-3 Item 21

5 Clamp NSA5516-08ND Item 52

or

5 Clamp NSA5516-12ND Item 51

or

5 Clamp NSA5516-13ND Item 63

or

5 Clamp NSA5516-31ND Item 64

1 Spacer NSA5527-03-02 Item 14

1 Spacer NSA5527-03-15 Item 91

1 Spacer NSA5527-03-06 Item 84

1 Washer NAS1149F0332P Item 46

(g) Install:

Refer to Fig. A-FCPAA Sheet 01 and Fig. A-FCPAA Sheet 05 and view G-G

1 Screw NAS1801-3-22 Item 62

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 485

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

1 Washer NAS1149F0332P Item 46

3 Clamp NSA5516-08ND Item 52

or

3 Clamp NSA5516-12ND Item 51

or

3 Clamp NSA5516-13ND Item 63

or

3 Clamp NSA5516-31ND Item 64

1 Spacer NSA5527-03-09 Item 96

(h) Install:

Refer to Fig. A-FCPAA Sheet 01 and Fig. A-FCPAA Sheet 05 and view H-H

1 Screw NAS1801-3-25 Item 33

1 Washer NAS1149F0332P Item 46

2 Clamp NSA5516-08ND Item 52

or

2 Clamp NSA5516-12ND Item 51

or

2 Clamp NSA5516-13ND Item 63

or

2 Clamp NSA5516-31ND Item 64

1 Spacer NSA5527-03-18 Item 95

(i) Install:

Refer to Fig. A-FCPAA Sheet 01 and Fig. A-FCPAA Sheet 05 and view J-J

2 Tie-Cable NSA935401-13 Item 66

or

2 Tie-Cable NSA935401-04 Item 26

or

2 Tie-Cable NSA935401-05 Item 23

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 486

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

1 Spacer NSA5527-03-01 Item 12

(2) Subtask 246103-831-038-001 - Modify the routing on Rib 1 on the passage way to

the shroud box at RH side, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

670 Work location Rib 1

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 246103A05R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

12 NSA5527-03-01 1 SPACER

13 NSA5527-03-03 3 SPACER

14 NSA5527-03-02 3 SPACER

21 NSA5050-3 4 NUT

23 NSA935401-05 2 TIE

26 NSA935401-04 2 TIE

33 NAS1801-3-25 1 SCREW

46 NAS1149F0332P 6 WASHER

51 NSA5516-12ND 15 CLAMP

52 NSA5516-08ND 15 CLAMP

62 NAS1801-3-22 1 SCREW

63 NSA5516-13ND 15 CLAMP

64 NSA5516-31ND 15 CLAMP

66 NSA935401-13 2 TIE

84 NSA5527-03-06 1 SPACER

91 NSA5527-03-15 2 SPACER

92 NSA5527-03-12 1 SPACER

94 NSA5159-35 1 STUD

95 NSA5527-03-18 1 SPACER

96 NSA5527-03-09 1 SPACER

References

Fig. A-FCPAA

Removal and Installation of the Clamps

on the Passage Way to the Shroud Box

(LH and RH side)

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 487

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

(a) Depending on the stacking, remove:

Refer to Fig. A-FCPAA Sheet 01 and Fig. A-FCPAA Sheet 02 view A-A

1 Nut Item (21) Discard

5 Clamp Item (51) Discard

or

5 Clamp Item (52) Discard

or

5 Clamp Item (63) Discard

or

5 Clamp Item (64) Discard

1 Spacer Item (91) Discard

1 Spacer Item (92) Discard

1 Spacer Item (13) Discard

1 Washer Item (46) Discard

(b) Depending on the stacking, remove:

Refer to Fig. A-FCPAA Sheet 01 and Fig. A-FCPAA Sheet 02 view B-B

1 Nut Item (21) Discard

5 Clamp Item (51) Discard

or

5 Clamp Item (52) Discard

or

5 Clamp Item (63) Discard

or

5 Clamp Item (64) Discard

1 Spacer Item (14) Discard

1 Spacer Item (91) Discard

1 Spacer Item (84) Discard

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 488

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

1 Spacer Item (97) Discard

1 Washer Item (46) Discard

(c) Depending on the stacking, remove:

Refer to Fig. A-FCPAA Sheet 01 and Fig. A-FCPAA Sheet 03 view C-C

1 Screw Item (33) Discard

2 Washer Item (46) Discard

1 Screw Item (62) Discard

5 Clamp Item (51) Discard

or

5 Clamp Item (52) Discard

or

5 Clamp Item (63) Discard

or

5 Clamp Item (64) Discard

1 Spacer Item (84) Discard

2 Spacer Item (95) Discard

3 Spacer Item (13) Discard

(d) Install:

Refer to Fig. A-FCPAA Sheet 01 and Fig. A-FCPAA Sheet 04 view D-D

1 Stud NSA5159-35 Item 94

1 Nut NSA5050-3 Item 21

3 Clamp NSA5516-12ND Item 51

or

3 Clamp NSA5516-08ND Item 52

or

3 Clamp NSA5516-13ND Item 63

or

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 489

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

3 Clamp NSA5516-31ND Item 64

1 Spacer NSA5527-03-15 Item 91

1 Spacer NSA5527-03-12 Item 92

3 Spacer NSA5527-03-03 Item 13

1 Nut NSA5050-3 Item 21

2 Washer NAS1149F0332P Item 46

(e) Install:

Refer to Fig. A-FCPAA Sheet 01 and Fig. A-FCPAA Sheet 04 view E-E

1 Nut NSA5050-3 Item 21

2 Clamp NSA5516-08ND Item 52

or

2 Clamp NSA5516-12ND Item 51

or

2 Clamp NSA5516-13ND Item 63

or

2 Clamp NSA5516-31ND Item 64

2 Spacer NSA5527-03-02 Item 14

1 Washer NAS1149F0332P Item 46

(f) Install:

Refer to Fig. A-FCPAA Sheet 01 and Fig. A-FCPAA Sheet 05 view F-F

1 Nut NSA5050-3 Item 21

5 Clamp NSA5516-08ND Item 52

or

5 Clamp NSA5516-12ND Item 51

or

5 Clamp NSA5516-13ND Item 63

or

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 490

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

5 Clamp NSA5516-31ND Item 64

1 Spacer NSA5527-03-02 Item 14

1 Spacer NSA5527-03-15 Item 91

1 Spacer NSA5527-03-06 Item 84

1 Washer NAS1149F0332P Item 46

(g) Install:

Refer to Fig. A-FCPAA Sheet 01 and Fig. A-FCPAA Sheet 05 view G-G

1 Screw NAS1801-3-22 Item 62

1 Washer NAS1149F0332P Item 46

3 Clamp NSA5516-08ND Item 52

or

3 Clamp NSA5516-12ND Item 51

or

3 Clamp NSA5516-13ND Item 63

or

3 Clamp NSA5516-31ND Item 64

1 Spacer NSA5527-03-09 Item 96

(h) Install:

Refer to Fig. A-FCPAA Sheet 01 and Fig. A-FCPAA Sheet 05 view H-H

1 Screw NAS1801-3-25 Item 33

1 Washer NAS1149F0332P Item 46

2 Clamp NSA5516-08ND Item 52

or

2 Clamp NSA5516-12ND Item 51

or

2 Clamp NSA5516-13ND Item 63

or

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 491

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

2 Clamp NSA5516-31ND Item 64

1 Spacer NSA5527-03-18 Item 95

(i) Install:

Refer to Fig. A-FCPAA Sheet 01 and Fig. A-FCPAA Sheet 05 view J-J

2 Tie-Cable NSA935401-13 Item 66

or

2 Tie-Cable NSA935401-04 Item 26

or

2 Tie-Cable NSA935401-05 Item 23

1 Spacer NSA5527-03-01 Item 12

(3) Subtask 246103-831-051-001 - Remove the clamps from LH wing, ADDITIONAL

WORK

Work Zones and Access Panels

Zone Access/Work location

572

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

References

Fig. A-FBOAA

Removal/Installation of the Clamps in LH

and RH Wings - ADDITIONAL WORK

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

(a) Remove the clamps from LH wing at Rib location WIAX-27.96.

Refer to Fig. A-FBOAA Sheet 01 and Fig. A-FBOAA Sheet 05 view J

1 Remove:

2 Clamp Item (51) Discard

1 Screw Item (71) Discard

1 Washer Item (82) Discard

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 492

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

(b) Remove the clamps from LH wing at Rib location WIAX-35.12.

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

1 Remove:

1 Screw Item (50) Retain

1 Screw Item (50) Discard

2 Washer Item (46) Discard

2 Clamp Item (51) Discard

1 Spacer Item (13) Discard

1 Spacer Item (13) Retain

(c) Remove the clamps from LH wing at Rib location WIAX-40.53.

Refer to Fig. A-FBOAA Sheet 01 and Fig. A-FBOAA Sheet 03

1 Remove:

2 Screw Item (37) Retain

2 Washer Item (46) Discard

2 Clamp Item (51) Discard

(d) Remove the clamps from LH wing at Rib location WIAX-48.25.

Refer to Fig. A-FBOAA Sheet 01 and Fig. A-FBOAA Sheet 05 view L

1 Remove:

2 Clamp Item (51) Discard

1 Screw Item (83) Discard

1 Washer Item (82) Discard

(e) Remove the clamps from LH wing at Rib location WIAX-74.08.

Refer to Fig. A-FBOAA Sheet 01 and Fig. A-FBOAA Sheet 04

1 Remove:

2 Spacer Item (12) Discard

2 Nut Item (21) Discard

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 493

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

2 Washer Item (61) Discard

2 Screw Item (80) Discard

1 Guide Assy-Conduit Item (60) Retain

(4) Subtask 246103-831-052-001 - Remove the clamps from RH wing, ADDITIONAL

WORK

Work Zones and Access Panels

Zone Access/Work location

672

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

References

Fig. A-FBOAA

Removal/Installation of the Clamps in LH

and RH Wings - ADDITIONAL WORK

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

(a) Remove the clamps from RH wing at Rib location WIAX-27.96.

Refer to Fig. A-FBOAA Sheet 01 and Fig. A-FBOAA Sheet 05 view J

1 Remove:

2 Clamp Item (51) Discard

1 Screw Item (71) Discard

1 Washer Item (82) Discard

(b) Remove the clamps from RH wing at Rib location WIAX-35.12.

Fig. A-FBOAA Sheet 01 and Fig. A-FBOAA Sheet 02

1 Remove:

1 Screw Item (50) Discard

1 Screw Item (50) Retain

2 Washer Item (46) Discard

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 494

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

2 Clamp Item (51) Discard

1 Spacer Item (13) Discard

1 Spacer Item (13) Retain

(c) Remove the clamps from RH wing at Rib location WIAX-40.53.

Refer to Fig. A-FBOAA Sheet 01 and Fig. A-FBOAA Sheet 03

1 Remove:

2 Screw Item (37) Retain

2 Washer Item (46) Discard

2 Clamp Item (51) Discard

(d) Remove the clamps from RH wing at Rib location WIAX-48.25.

Refer to Fig. A-FBOAA Sheet 01 and Fig. A-FBOAA Sheet 05 view L

1 Remove:

2 Clamp Item (51) Discard

1 Screw Item (83) Discard

1 Washer Item (82) Discard

(e) Remove the clamps from RH wing at Rib location WIAX-74.08.

Refer to Fig. A-FBOAA Sheet 01 and Fig. A-FBOAA Sheet 04

1 Remove:

2 Spacer Item (12) Discard

2 Nut Item (21) Retain

2 Washer Item (61) Discard

2 Screw Item (80) Discard

1 Guide Assy-Conduit Item (60) Retain

(5) Subtask 246103-831-056-001 - Modify the routing of routes 1P and 2P at LH wing

Work Zones and Access Panels

Zone Access/Work location

570 Work location from Rib 1 to Rib 6

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 495

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

Manpower Resources

Manhours 1.50

Minimum number of person 1

Subtask elapsed time 1.50

Skills NON SPECIFIC

Material necessary to do the job

Supplementary kit 246103A01S12

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

14 NSA5527-03-02 3 SPACER

26 NSA935401-04 12 TIE

66 NSA935401-13 3 TIE

86 EN6049-007-08-5 5 (M) SLEEVE

References

Fig. A-FCMAA

Modification of the Routing in LH and

RH Wings - ADDITIONAL WORK

Sheet 01

Sheet 02

(a) Between rib 5 and rib 6, remove:

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

2 Insulator Discard

12 Tie-Cable Discard

and

3 Spacer Discard

attached with:

3 Tie-Cable Discard

(b) Between rib 5 and rib 6, install:

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

5 (M) Sleeve-Protective EN6049-007-08-5 Item 86

12 Tie-Cable NSA935401-04 Item 26

and

3 Spacer NSA5527-03-02 Item 14

attached with:

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 496

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

3 Tie-Cable NSA935401-13 Item 66

(6) Subtask 246103-831-057-001 - Modify the routing of routes 1P and 2P at RH wing

Work Zones and Access Panels

Zone Access/Work location

670 Work location from Rib 1 to Rib 6

Manpower Resources

Manhours 1.50

Minimum number of person 1

Subtask elapsed time 1.50

Skills NON SPECIFIC

Material necessary to do the job

Supplementary kit 246103A02S11

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

14 NSA5527-03-02 3 SPACER

26 NSA935401-04 12 TIE

66 NSA935401-13 3 TIE

86 EN6049-007-08-5 5 (M) SLEEVE

References

Fig. A-FCMAA

Modification of the Routing in LH and

RH Wings - ADDITIONAL WORK

Sheet 01

Sheet 02

(a) Between rib 5 and rib 6, remove:

Refer toFig. A-FCMAA Sheet 01 and Fig. A-FCMAA Sheet 02

2 Insulator Discard

12 Tie-Cable Discard

and

3 Spacer Discard

attached with:

3 Tie-Cable Discard

(b) Between rib 5 and rib 6, install:

Refer toFig. A-FCMAA Sheet 01 and Fig. A-FCMAA Sheet 02

5 (M) Sleeve-Protective EN6049-007-08-5 Item 86

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 497

5

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SERVICE BULLETIN

12 Tie-Cable NSA935401-04 Item 26

and

3 Spacer NSA5527-03-02 Item 14

attached with:

3 Tie-Cable NSA935401-13 Item 66

(7) Subtask 246103-831-053-001 - Install the clamps in LH wing, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

572

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Supplementary kit 246103A01S11

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

85 ASNA51072503 1 (M) TAPE

Supplementary kit 246103A01S12

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

12 NSA5527-03-01 1 SPACER

37 NAS1801-3-9 2 SCREW

46 NAS1149F0332P 6 WASHER

52 NSA5516-08ND 8 CLAMP

55 NAS1801-3-16 1 SCREW

86 EN6049-007-08-5 2.5 (M) SLEEVE

Supplementary kit 246103A03S01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

21 NSA5050-3 2 NUT

22 NAS1801-3-24 2 SCREW

90 NAS1149D0316H 2 WASHER

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 498

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References

Fig. A-FBOAA

Removal/Installation of the Clamps in LH

and RH Wings - ADDITIONAL WORK

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

(a) Install the clamps in LH wing at Rib location WIAX-27.96.

Refer to Fig. A-FBOAA Sheet 01 and Fig. A-FBOAA Sheet 05 view K

1 Install:

2 Clamp NSA5516-08ND Item 52

1 Washer NAS1149F0332P Item 46

1 Screw NAS1801-3-9 Item 37

(b) Install the clamps in LH wing at Rib location WIAX-35.12.

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

1 Install:

1 Screw Item (50) Retained at

removal

1 Spacer Item (13) Retained at

removal

1 Spacer NSA5527-03-01 Item 12

2 Washer NAS1149F0332P Item 46

1 Screw NAS1801-3-16 Item 55

2 Clamp NSA5516-08ND Item 52

(c) Install the clamps in LH wing at Rib location WIAX-40.53.

Refer to Fig. A-FBOAA Sheet 01 and Fig. A-FBOAA Sheet 03

1 Install:

2 Screw Item (37) Retained at

removal

2 Washer NAS1149F0332P Item 46

2 Clamp NSA5516-08ND Item 52

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 499

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(d) Install the clamps at LH wing at Rib location WIAX-48.25.

Refer to Fig. A-FBOAA Sheet 01 and Fig. A-FBOAA Sheet 05 view M

1 Install:

2 Clamp NSA5516-08ND Item 52

1 Washer NAS1149F0332P Item 46

1 Screw NAS1801-3-9 Item 37

(e) Install the clamps at LH wing at Rib location WIAX-74.08.

Refer to Fig. A-FBOAA Sheet 01 and Fig. A-FBOAA Sheet 04

1 Install:

2 Nut NSA5050-3 Item 21

2 Screw NAS1801-3-24 Item 22

2 Washer NAS1149D0316H Item 90

1 Guide Assy-conduit Item (60) Retained at

removal

NOTE: If necessary, to make the diameters of the bundles match with

the diameter of the holes of the guide Item 60, use:

2.5 (M) Sleeve-Protective EN6049-007-08-5 Item 86

1 (M) Tape-Reinforced

Silicone

ASNA51072503 Item 85

(8) Subtask 246103-831-054-001 - Install the clamps in RH wing, ADDITIONAL WORK

Work Zones and Access Panels

Zone Access/Work location

672

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 500

5

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@A300-600

SERVICE BULLETIN

Material necessary to do the job

Supplementary kit 246103A02S11

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

12 NSA5527-03-01 1 SPACER

37 NAS1801-3-9 2 SCREW

46 NAS1149F0332P 6 WASHER

52 NSA5516-08ND 6 CLAMP

55 NAS1801-3-16 1 SCREW

85 ASNA51072503 1 (M) TAPE

86 EN6049-007-08-5 2.5 (M) SLEEVE

Supplementary kit 246103A03S01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

21 NSA5050-3 2 NUT

22 NAS1801-3-24 2 SCREW

90 NAS1149D0316H 2 WASHER

References

Fig. A-FBOAA

Removal/Installation of the Clamps in LH

and RH Wings - ADDITIONAL WORK

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

(a) Install the clamps in RH wing at Rib location WIAX-27.96.

Refer to Fig. A-FBOAA Sheet 01 and Fig. A-FBOAA Sheet 05 view K

1 Install:

2 Clamp NSA5516-08ND Item 52

1 Washer NAS1149F0332P Item 46

1 Screw NAS1801-3-9 Item 37

(b) Install the clamps in RH wing at Rib location WIAX-35.12.

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

1 Install:

1 Spacer Item (13) Retained at

removal

1 Screw Item (50) Retained at

removal

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 501

5

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1 Spacer NSA5527-03-01 Item 12

2 Washer NAS1149F0332P Item 46

1 Screw NAS1801-3-16 Item 55

2 Clamp NSA5516-08ND Item 52

(c) Install the clamps in LH wing at Rib location WIAX-40.53.

Refer to Fig. A-FBOAA Sheet 01 and Fig. A-FBOAA Sheet 03

1 Install:

2 Screw Item (37) Retained at

removal

2 Washer NAS1149F0332P Item 46

2 Clamp NSA5516-08ND Item 52

(d) Install the clamps in LH wing at Rib location WIAX-48.25.

Refer to Fig. A-FBOAA Sheet 01 and Fig. A-FBOAA Sheet 05 view M

1 Install:

2 Clamp NSA5516-08ND Item 52

1 Washer NAS1149F0332P Item 46

1 Screw NAS1801-3-9 Item 37

(e) Install the clamps in LH wing at Rib location WIAX-74.08.

Refer to Fig. A-FBOAA Sheet 01 and Fig. A-FBOAA Sheet 04

1 Install:

2 Nut NSA5050-3 Item 21

2 Screw NAS1801-3-24 Item 22

2 Washer NAS1149D0316H Item 90

1 Guide Assy conduit Item (60) Retained at

removal

NOTE: If necessary, to make the diameters of the bundles match with

the diameter of the holes of the guide Item 60, use:

2.5 (M) Sleeve-Protective EN6049-007-08-5 Item 86

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 502

5

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@A300-600

SERVICE BULLETIN

1 (M) Tape-Reinforced

Silicone

ASNA51072503 Item 85

**CONF ALL

D. TEST

**CONF 001

(1) Subtask 246103-700-005-001 - Tests

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 27-54-41, Page Block 401

29-12-46, Page Block 401

(a) Job set-up

1 Remove the safety clips and tags and close the circuit breakers as specified

after the installation of the inner flap deflectors, refer to AMM 27-54-41, Page

Block 401.

2 Remove the safety clips and tags and close the circuit breakers as specified

after the installation of the BLUE hydraulic reservoir, refer to AMM 29-12-46,

Page Block 401.

(b) Procedure

1 Do the test procedure as specified after the installation of the inner flap

deflectors, refer to AMM 27-54-41, Page Block 401.

2 Do the test procedure as specified after the installation of the BLUE hydraulic

reservoir, refer to AMM 29-12-46, Page Block 401.

**CONF 002

(1) Subtask 246103-700-005-001 - Tests

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 27-54-41, Page Block 401

29-12-46, Page Block 401

(a) Job set-up

1 Remove the safety clips and tags and close the circuit breakers as specified

after the installation of the inner flap deflectors, refer to AMM 27-54-41, Page

Block 401.

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 503

5

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2 Remove the safety clips and tags and close the circuit breakers as specified

after the installation of the BLUE hydraulic reservoir, refer to AMM 29-12-46,

Page Block 401.

(b) Procedure

1 Do the test procedure as specified after the installation of the inner flap

deflectors, refer to AMM 27-54-41, Page Block 401.

2 Do the test procedure as specified after the installation of the BLUE hydraulic

reservoir, refer to AMM 29-12-46, Page Block 401.

**CONF 003

(1) Subtask 246103-700-005-001 - Tests

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 27-54-41, Page Block 401

29-12-46, Page Block 401

(a) Job set-up

1 Remove the safety clips and tags and close the circuit breakers as specified

after the installation of the inner flap deflectors, refer to AMM 27-54-41, Page

Block 401.

2 Remove the safety clips and tags and close the circuit breakers as specified

after the installation of the BLUE hydraulic reservoir, refer to AMM 29-12-46,

Page Block 401.

(b) Procedure

1 Do the test procedure as specified after the installation of the inner flap

deflectors, refer to AMM 27-54-41, Page Block 401.

2 Do the test procedure as specified after the installation of the BLUE hydraulic

reservoir, refer to AMM 29-12-46, Page Block 401.

**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 246103-942-005-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 504

5

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@A300-600

SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001

27-54-41, Page Block 401

32-12-11, Page Block 301

(a) Close the inner deflectors between Rib. 1 and Rib. 6, refer to AMM 27-54-41, Page

Block 401.

(b) Install the access panels 512AB(612AB), 512BB(612BB), 512CB(612CB) and

512DB(612DB), refer to AMM 06-41-57, Page Block 001.

(c) Install the access panels 512BB(612BB), refer to AMM 06-41-57, Page Block 001.

(d) Close the Main Landing Gear (MLG) doors, refer to AMM 32-12-11, Page Block

301.

(e) Remove the access platform(s).

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

**CONF 002

(1) Subtask 246103-942-005-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001

27-54-41, Page Block 401

32-12-11, Page Block 301

(a) Close the inner deflectors between Rib. 1 and Rib. 6, refer to AMM 27-54-41, Page

Block 401.

(b) Install the access panels 512AB(612AB), 512BB(612BB), 512CB(612CB) and

512DB(612DB), refer to AMM 06-41-57, Page Block 001.

(c) Install the access panels 512BB(612BB), refer to AMM 06-41-57, Page Block 001.

(d) Close the Main Landing Gear (MLG) doors, refer to AMM 32-12-11, Page Block

301.

(e) Remove the access platform(s).

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

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 505

5

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SERVICE BULLETIN

**CONF 003

(1) Subtask 246103-942-005-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001

27-54-41, Page Block 401

32-12-11, Page Block 301

(a) Close the inner deflectors between Rib. 1 and Rib. 6, refer to AMM 27-54-41, Page

Block 401.

(b) Install the access panels 512AB(612AB), 512BB(612BB), 512CB(612CB) and

512DB(612DB), refer to AMM 06-41-57, Page Block 001.

(c) Install the access panels 512BB(612BB), refer to AMM 06-41-57, Page Block 001.

(d) Close the Main Landing Gear (MLG) doors, refer to AMM 32-12-11, Page Block

301.

(e) Remove the access platform(s).

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

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 506

5

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@A300-600

SERVICE BULLETIN

**CONF ALL

VIEW LOOKING INSIDE

FR52

FR51

FR50 B

A

FWD B

Z147

A

FR52

STGR32

A

A C

STGR33

2S−4A

1S/B−3A−3R−1V

D

PANEL

BRACKET

(74)

(73)

(72) (4 POS)

(2 POS)

D_SB_246103_5_BAAA_01_04

Figure A-FBAAA - Sheet 01

Removal of the Old Brackets of the Passage Way at FR52 (LH side)

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 507

5

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@A300-600

SERVICE BULLETIN

**CONF ALL

2S−4A

VIEW LOOKING AFT

A A

OR

C

(11)

(10)

OUTB

(41)

(42)

(43)

(44)

(45)

(46)

(47)

(46)

(47)

(42)

(43)

(41)

(44)

(45)

(46)

(47)

(46)

(47)

(47)

(46)

(49)

(48)

D_SB_246103_5_BAAA_02_02

NOTE:

01 DEPENDING ON AIRCRAFT CONFIGURATION,

THE BRAKET MAY NOT BE INSTALLED.

01

Figure A-FBAAA - Sheet 02

Removal of the Old Brackets of the Passage Way at FR52 (LH side)

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 508

5

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SERVICE BULLETIN

**CONF ALL

(44)

(46)

(47)

(45)

(46)

D

D_SB_246103_5_BAAA_03_00

Figure A-FBAAA - Sheet 03

Removal of the Old Brackets of the Passage Way at FR52 (LH side)

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 509

5

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@A300-600

SERVICE BULLETIN

**CONF ALL

VIEW LOOKING INSIDE

FR52

FR51

FR50 B

FR52

STGR32

A

A C

A

B

STGR33

2S−4A

FWD 38 23 1S/B−3A−3R−1V

46

(74)

63

64

OR (4 POS)

D

PANEL

BRACKET

(2 POS)

Z147

A

D_SB_246103_5_BBAA_01_03

Figure A-FBBAA - Sheet 01

Installation of the New Brackets of the Passage Way at FR52 (LH side)

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 510

5

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@A300-600

SERVICE BULLETIN

**CONF ALL

10

2S−4A

VIEW LOOKING AFT

C

12

(11)

A A

OUTB

46

48

41

42

43

(45)

(44)

46

47 46

47

(47)

64

46

D

OR

63

46

64

OR

63

BRACKET

NOTE:

01 IF INSTALLED

01

D_SB_246103_5_BBAA_02_05

Figure A-FBBAA - Sheet 02

Installation of the New Brackets of the Passage Way at FR52 (LH side)

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 511

5

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SERVICE BULLETIN

**CONF ALL

VIEW LOOKING AFT

A

FR46

FR47

FR48

FR49

FR50

FR51

FR52

FR53

FR54

Z147 Z148 −

LH SIDE SHOWN

RH SIDE SYMMETRICAL

A

C B

BEFORE

FUSELAGE THEORICAL

CONTOUR

B

STGR31

STGR32

STGR33

STGR31

STGR32

STGR33

FUSELAGE THEORICAL

CONTOUR

(27)

(46)

(27)

(46)

OR

D_SB_246103_5_BEAA_01_02

Figure A-FBEAA - Sheet 01

Installation of a Conduit on the Shroud Box Bracket (LH and RH side)

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 512

5

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SERVICE BULLETIN

**CONF ALL

VIEW LOOKING AFT

AFTER

1M

2M

2M

1M

2M

1M

OR

C

46

71

28

29

46

71

21

37

63

64

OR

46

71

46

71

28

29

LH SIDE

RH SIDE

LH SIDE

RH SIDE

70

21

30

21

30

63

64

OR

C

D

75

OR

76

OR

NOTE:

01 2 OR 3 BUNDLES MAY BE INSTALLED

01

01

D_SB_246103_5_BEAA_02_04

Figure A-FBEAA - Sheet 02

Installation of a Conduit on the Shroud Box Bracket (LH and RH side)

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 513

5

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@A300-600

SERVICE BULLETIN

**CONF ALL

28

29

LH SIDE

RH SIDE

28

29

LH SIDE C RH SIDE

D

D_SB_246103_5_BEAA_03_00

Figure A-FBEAA - Sheet 03

Installation of a Conduit on the Shroud Box Bracket (LH and RH side)

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 514

5

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SERVICE BULLETIN

**CONF ALL

VIEW LOOKING FORWARD

A

Z147 Z148 −

BEFORE

(16) (14) (32)

(33)

(43)

(16)

B

A

STGR32

(20)

(16) (14)

(33)

(43) (16)

STGR32

(20)

OR

B C

B D

D_SB_246103_5_BFAA_01_04

Figure A-FBFAA - Sheet 01

Modification of the Routing Between FR50 and FR51 at STGR 32 (LH and RH side)

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 515

5

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@A300-600

SERVICE BULLETIN

**CONF ALL

STGR32

VIEW LOOKING FORWARD

AFTER

33

43

12

64 14

46

OR

63

64

OR

63

STGR32

33

43

12

64 14

46

OR

63

64

OR

63

OR

STGR32

VIEW LOOKING FORWARD

79

43

64 14

46

OR

63

64

OR

63

STGR32

79

43

64 14

46

OR

63

64

OR

63

OR

NOTE:

02 IF NECESSARY, INSTALL THE SPACER ITEM

02 02

C

D

12

D_SB_246103_5_BFAA_02_03

Figure A-FBFAA - Sheet 02

Modification of the Routing Between FR50 and FR51 at STGR 32 (LH and RH side)

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 516

5

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SERVICE BULLETIN

**CONF 001 thru 002

D_SB_246103_5_BCAA_01_00

RIB6A

RIB6

B

LH SIDE SHOWN

RH SIDE SYMMETRICAL

A

A

A

Figure A-FBCAA - Sheet 01

Removal of the Clamps on the Passage Way to the Shroud Box (LH and RH side)

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 517

5

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SERVICE BULLETIN

**CONF 001 thru 002

B

B

A

A

1S/B−3A (RH)

1S−3R (LH)

1M (LH)

2M (LH) 1M/B (LH)

2S/B−4A (LH)

2S−3R (RH)

2M (RH)

1M (RH) 2M/B (RH)

A A

STGR33

LH SIDE SHOWN

RH SIDE SYMMETRICAL

B

6.35 mm

(0.25 in)

03 IF THE GAP IS LESS THAN 6.35 mm (0.25 in)

ADD A SPACER ITEM 12 BETWEEN THE SPACER

ITEM 13 AND THE STRUCTURE

(REFER TO FIG. A−FBDAA SHEET 02)

03

2S/B−4A (RH)

1S/B−3A (LH)

04

04

A

A

A

A

(13)

ONLY ONE CONFIGURATION SHOWN

THE STACKING AND NUMBER OF CLAMPS

AND SPACERS MAY DIFFER DEPENDING

ON THE POSITION AND AIRCRAFT

CONFIGURATION

130 mm

(5.118 in)

NOTE:

01 IF THE GAP IS MORE THAN 130 mm (5.118 in)

CONTACT AIRBUS

02 INSTALL THE EXTRUSION ITEM 87

AND APPLY MATERIAL No 05JBC9 IF

NEEDED PROTECTION ADDED IF MISSING

A

A

01

02

02

SHROUD BOX

FRONT SPAR

D_SB_246103_5_BCAA_02_08

Figure A-FBCAA - Sheet 02

Removal of the Clamps on the Passage Way to the Shroud Box (LH and RH side)

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 518

5

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SERVICE BULLETIN

**CONF 001 thru 002

1P 2P

C

OR

B B

(22)

(20)

(19)

(12)

(21)

C

1P 2P

C

D_SB_246103_5_BCAA_03_01

Figure A-FBCAA - Sheet 03

Removal of the Clamps on the Passage Way to the Shroud Box (LH and RH side)

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 519

5

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@A300-600

SERVICE BULLETIN

**CONF 003

RIB6A

RIB6

A

LH SHOWN

RH SYMMETRICAL

A

A

B C D

D_SB_246103_5_BCAB_01_01

Figure A-FBCAB - Sheet 01

Removal of the Clamps on the Passage Way to the Shroud Box (LH and RH side)

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 520

5

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@A300-600

SERVICE BULLETIN

**CONF 003

1P 2P

(22)

(20)

(19)

(12)

(21)

C

1P 2P

B

C C

OR

D_SB_246103_5_BCAB_02_01

Figure A-FBCAB - Sheet 02

Removal of the Clamps on the Passage Way to the Shroud Box (LH and RH side)

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 521

5

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@A300-600

SERVICE BULLETIN

**CONF 003

NOTE:

01 ADD ITEM 21, 46, 94 IF NECESSARY.

STGR33

FUSELAGE

02

02

02 INSTALL EXTRUSION ITEM 87 AND APPLY MATERIAL No 05JBC9 IF NEEDED

PROTECTION ADDED IF MISSING.

94

21

91 92 13

46 21

46

01

01

21

14 46

AFTER

51

52

63

64

OR

OR

OR

51

52

63

64

OR

OR

OR

B

B

A

A

C

C

E

E

D

F D

F

B B

D

A A

D_SB_246103_5_BCAB_03_02

Figure A-FBCAB - Sheet 03

Removal of the Clamps on the Passage Way to the Shroud Box (LH and RH side)

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 522

5

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@A300-600

SERVICE BULLETIN

**CONF 003

NOTE:

03 PRINCIPLE TO AVOID THE CONTACTS BETWEEN

ELECTRICAL HARNESSES.

12

84 91 46

14

46

62

96

33

46

95

03

21

51

52

63

64

OR

OR

OR

51

52

63

64

OR

OR

OR

51

52

63

64

OR

OR

OR

51

52

63

64

OR

OR

OR

51

52

63

64

OR

OR

OR

51

52

63

64

OR

OR

OR

23

26

66

OR

OR

C C D D

E E F F

D_SB_246103_5_BCAB_04_02

Figure A-FBCAB - Sheet 04

Removal of the Clamps on the Passage Way to the Shroud Box (LH and RH side)

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 523

5

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@A300-600

SERVICE BULLETIN

**CONF 003

NOTE:

03 PRINCIPLE TO AVOID THE CONTACTS BETWEEN

ELECTRICAL HARNESSES.

12

84 91 46

14

46

62

96

33

46

95

03

21

51

52

63

64

OR

OR

OR

51

52

63

64

OR

OR

OR

51

52

63

64

OR

OR

OR

51

52

63

64

OR

OR

OR

51

52

63

64

OR

OR

OR

51

52

63

64

OR

OR

OR

23

26

66

OR

OR

C C D D

E E F F

D_SB_246103_5_BCAB_05_00

Figure A-FBCAB - Sheet 05

Removal of the Clamps on the Passage Way to the Shroud Box (LH and RH side)

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 524

5

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@A300-600

SERVICE BULLETIN

**CONF 001 thru 002

RIB6A

RIB6

B

A

LH SIDE SHOWN

RH SIDE SYMMETRICAL

A

A

D_SB_246103_5_BDAA_01_01

Figure A-FBDAA - Sheet 01

Installation of the Clamps on the Passage Way to the Shroud Box (LH and RH side)

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 525

5

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@A300-600

SERVICE BULLETIN

**CONF 001 thru 002

A

A STGR33

C

C

B

A A

1S/B−3A (RH)

2M (LH) 1M/B (LH)

2S/B−4A (LH)

1M (RH) 2M/B (RH)

12

2S/B−4A (RH)

1S/B−3A (LH)

NOTE:

IF PREVIOUSLY INSTALLED,

01

KEEP THE OLD SPACER ON THE 

NEW STACKING

ONLY ONE CONFIGURATION SHOWN.

02

THE STACKING AND NUMBER OF CLAMPS

AND SPACERS MAY DIFFER DEPENDING

ON THE POSITION AND AIRCRAFT

CONFIGURATION.

A

A

A

A

A

A

1S−3R (LH)

1M (LH)

2S−3R (RH)

2M (RH)

01 02

LH SIDE SHOWN

RH SIDE SYMMETRICAL

D_SB_246103_5_BDAA_02_03

Figure A-FBDAA - Sheet 02

Installation of the Clamps on the Passage Way to the Shroud Box (LH and RH side)

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 526

5

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@A300-600

SERVICE BULLETIN

**CONF 001 thru 002

1P−2P

OR

22

20

19

12

19

12

21

C

C C

1P−2P

24 24

C C

01 01

FWD 02 02

NOTE:

01 APPLY MATERIAL No 05EML7 AND 08BBD1

02 INSTALL THE STRIP PROTECTIVE ITEM

WITH MATERIAL No 05EJL9

24

D_SB_246103_5_BDAA_03_07

Figure A-FBDAA - Sheet 03

Installation of the Clamps on the Passage Way to the Shroud Box (LH and RH side)

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 527

5

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@A300-600

SERVICE BULLETIN

**CONF 003

RIB6A

RIB6

A

LH SHOWN

RH SYMMETRICAL

A

A

B

D_SB_246103_5_BDAB_01_00

Figure A-FBDAB - Sheet 01

Installation of the Clamps on the Passage Way to the Shroud Box (LH and RH side)

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 528

5

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@A300-600

SERVICE BULLETIN

**CONF 003

1P−2P

22

20

19

12

19

12

21

C

1P−2P

24 24

02 INSTALL THE STRIP PROTECTIVE ITEM 24

01 01

FWD

02 02

NOTE:

01 APPLY MATERIAL No 05EML7 AND 08BBD1

WITH MATERIAL No 05EJL9

B

C C

OR

D_SB_246103_5_BDAB_02_01

Figure A-FBDAB - Sheet 02

Installation of the Clamps on the Passage Way to the Shroud Box (LH and RH side)

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 529

5

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@A300-600

SERVICE BULLETIN

**CONF ALL

Z571

A

A

FR47

A

A

A

A

A

A A

A

A

A

A

A

B

B

B

B

B

B B

B

B

B

B

B D

D

C

C

D_SB_246103_5_BGAA_01_02

Figure A-FBGAA - Sheet 01

Modification of the Routing of Routes 1P and 2P in the Shroud Box (LH side)

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 530

5

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@A300-600

SERVICE BULLETIN

**CONF ALL

TYPICAL INSTALLATION

20

81 (19) (19)

TYPICAL INSTALLATION

(19)

(20)

(22) (19)

BEFORE AFTER

A A B B

34

D_SB_246103_5_BGAA_02_04

Figure A-FBGAA - Sheet 02

Modification of the Routing of Routes 1P and 2P in the Shroud Box (LH side)

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 531

5

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@A300-600

SERVICE BULLETIN

**CONF ALL

TYPICAL INSTALLATION

20

(19) 71 (19)

TYPICAL INSTALLATION

(19)

(20)

(22) (19)

BEFORE AFTER

84

C C D D

D_SB_246103_5_BGAA_03_01

Figure A-FBGAA - Sheet 03

Modification of the Routing of Routes 1P and 2P in the Shroud Box (LH side)

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 532

5

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@A300-600

SERVICE BULLETIN

**CONF ALL

FR50

FR47

Z571 B

A

A

STGR30

STGR31

STGR32

D C

B

NOTE:

01 ROTATE THE BACKSHELL OF THE CONNECTOR 35HA TO BE ABLE TO ATTACH THE

WIRES FROM 35HA TO THE NEW BRACKET.

TAKE CARE TO HAVE A GAP OF 15 mm TO 20 mm (0.590 in TO 0.787 in) 

BETWEEN THE WIRE AND THE HYDRAULIC PIPE.

01 3GHA

D_SB_246103_5_BHAA_01_04

Figure A-FBHAA - Sheet 01

Installation of a Support on the Support of the BLUE Hydraulic Reservoir (LH wing)

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 533

5

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@A300-600

SERVICE BULLETIN

**CONF ALL

HOLE

SYMBOL ITEM PN DESCRIPTION

HOLE DIAMETER

MIN MAX

4.85 mm

(0.191 in)

4.95 mm

(0.195 in) ASNA2050DXJ4828 RIVET

NAS1801−3−11 SCREW

68

31

STGR30

STGR31

STGR32

STGR30

STGR31

STGR32

20 NSA935808−01 WASHER

N

N

N

HEAD ON VISIBLE SIDE

FASTENERS NOT AFFECTED

CONDUIT

BEFORE AFTER

VIEW LOOKING INBOARD VIEW LOOKING INBOARD

C D

NOTE:

01 APPLY MAT. No 06ABB1

67

69

01

D_SB_246103_5_BHAA_02_02

Figure A-FBHAA - Sheet 02

Installation of a Support on the Support of the BLUE Hydraulic Reservoir (LH wing)

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 534

5

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@A300-600

SERVICE BULLETIN

**CONF ALL

PRINCIPLE

LH SIDE SHOWN

RH SIDE SYMMETRICAL

39

66

A

A

A

A

1E (LH)

2E (RH)

LOWER WING SURFACE

UPPER WING SURFACE

FUSELAGE THEORICAL

CONTOUR

A

A A

34

STGR27

STGR28

STGR29

STGR30

2G (RH)

1G (LH)

A

A

Z613

Z513

D_SB_246103_5_BJAA_01_02

Figure A-FBJAA - Sheet 01

Modification of the Routing in the Leading Edge (LH and RH side)

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 535

5

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@A300-600

SERVICE BULLETIN

**CONF 001, 003

RIB WIAX − 74.08

RIB WIAX − 40.53

RIB WIAX − 35.12

B

B

Z572 (Z672)

A

A

A

C D

E F

G H

L M J K

RIB WIAX − 48.25

RIB WIAX − 27.96

LH SIDE SHOWN

RH SIDE SYMMETRICAL

D_SB_246103_5_BKAA_01_02

Figure A-FBKAA - Sheet 01

Removal/Installation of the Clamps in LH and RH Wings

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 536

5

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@A300-600

SERVICE BULLETIN

**CONF 001, 003

(51)

(46)

(50)

(13)

(51)

WY 307.40 REF

BEFORE

AFTER

FWD C

FWD D

13

12

46

55

46

50

52

WY 307.40 REF

D_SB_246103_5_BKAA_02_03

Figure A-FBKAA - Sheet 02

Removal/Installation of the Clamps in LH and RH Wings

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 537

5

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@A300-600

SERVICE BULLETIN

**CONF 001, 003

WY 307.40 REF

BEFORE

AFTER

(13)

(46)

(50)

(51)

(46)

(50)

(13)

E

F

FWD

FWD

52

46

37 46

37

WY 307.40 REF

D_SB_246103_5_BKAA_03_04

Figure A-FBKAA - Sheet 03

Removal/Installation of the Clamps in LH and RH Wings

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 538

5

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@A300-600

SERVICE BULLETIN

**CONF 001, 003

(13)

WY 290.337 REF

(46)

(50)

(51) (53) (54)

(53) (52) (13)

WY 290.337 REF

FWD

FWD

60

22

BEFORE

AFTER

G

H

90

21

NOTE:

01 OVERLAP THE BUNDLES TO MAKE THEIR DIAMETER

MATCH WITH THE DIAMETER OF THE HOLES OF THE

GUIDE ITEM 60 WITH TAPE ASNA51072503 ITEM 85 AND

EN6049−007−08−5 ITEM 86

01

D_SB_246103_5_BKAA_04_06

Figure A-FBKAA - Sheet 04

Removal/Installation of the Clamps in LH and RH Wings

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 539

5

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@A300-600

SERVICE BULLETIN

**CONF 001, 003

(37)

(46)

FWD

BEFORE

ROUTE 1P

(2 POS) (51)

ROUTE 2P

J

37

46

FWD

AFTER

(2 POS) 52

K

BEFORE

ROUTE 1P

(2 POS) (51) ROUTE 2P

(46)

(37)

W/AX −55.55

L

AFTER

ROUTE 1P

(2 POS) 52 ROUTE 2P

46

(37)

W/AX −55.55

M

D_SB_246103_5_BKAA_05_02

Figure A-FBKAA - Sheet 05

Removal/Installation of the Clamps in LH and RH Wings

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 540

5

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@A300-600

SERVICE BULLETIN

**CONF 002

RIB WIAX − 74.08

RIB WIAX − 40.53

RIB WIAX − 35.12

B

B

Z572 (Z672)

A

A

A

C D

E F

RIB WIAX − 48.25

RIB WIAX − 27.96

LH SIDE SHOWN

RH SIDE SYMMETRICAL

G H J K

D_SB_246103_5_BLAA_01_01

Figure A-FBLAA - Sheet 01

Removal/Installation of the Clamps in LH and RH Wings

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 541

5

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@A300-600

SERVICE BULLETIN

**CONF 002

(51)

(46)

(50)

(13)

(51)

WY 307.40 REF

FWD C

FWD D

BEFORE

AFTER

13

12

46

55

46

50

52

WY 307.40 REF

D_SB_246103_5_BLAA_02_03

Figure A-FBLAA - Sheet 02

Removal/Installation of the Clamps in LH and RH Wings

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 542

5

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@A300-600

SERVICE BULLETIN

**CONF 002

WY 307.40 REF

BEFORE

AFTER

(13)

(46)

(50)

(51)

(46)

(50)

(13)

E

F

FWD

FWD

52

46

37 46

37

WY 307.40 REF

D_SB_246103_5_BLAA_03_04

Figure A-FBLAA - Sheet 03

Removal/Installation of the Clamps in LH and RH Wings

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 543

5

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@A300-600

SERVICE BULLETIN

**CONF 002

(37)

(46)

FWD

BEFORE

ROUTE 1P

(2 POS) (51)

ROUTE 2P

37

46

FWD

AFTER

(2 POS) 52

BEFORE

ROUTE 1P

(2 POS) (51) ROUTE 2P

(46)

(37)

W/AX −55.55

AFTER

ROUTE 1P

(2 POS) 52 ROUTE 2P

46

W/AX −55.55

G H

J

K

(37)

D_SB_246103_5_BLAA_04_02

Figure A-FBLAA - Sheet 04

Removal/Installation of the Clamps in LH and RH Wings

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 544

5

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@A300-600

SERVICE BULLETIN

**CONF ALL

RIB6A

RIB6

A

LH SIDE SHOWN

RH SIDE SYMMETRICAL

B

A

A

D_SB_246103_5_BYAA_01_00

Figure A-FBYAA - Sheet 01

Modification of the Routing in LH and RH Wings

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 545

5

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@A300-600

SERVICE BULLETIN

**CONF ALL

TYPICAL INSTALLATION

14

66

C

C C

C

C

C

01

CLAMPS

CLAMPS

RIB6 RIB6A

86

VIEW LOOKING DOWN

NOTE:

01 INSTALL SLEEVE ITEM 86 ON ROUTES 1P AND 2P

WITH TIE−CABLES ITEM 26

C C

B

WIAX 40.53

WIAX 35.12

F

W

D

INBD

DISCARD THE VARIOUS ELECTRICAL CONDUIT FROM THE BUNDLES

WHICH WILL BE MODIFIED WITH THE NEW SLEEVE

D_SB_246103_5_BYAA_02_03

Figure A-FBYAA - Sheet 02

Modification of the Routing in LH and RH Wings

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 546

5

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@A300-600

SERVICE BULLETIN

**CONF ALL

MIN 10 mm/MAX 20mm

MIN (0.394 in)/MAX 0.787 in)

INSTALLATION PRINCIPLE

Z147 Z148 −

STGR30

STGR31

STGR32

STGR33

STGR34

FR51 FR52

TO 1776VC, 1777VC,

2043VC, 2673VC

TO 1774VC, 1775VC,

2044VC, 2674VC

(77)

77 OR 78

NOTE:

01 A THIRD CONDUIT MAY BE INSTALLED

IF INSTALLED REPLACE IT

01

LAST CLAMP FUSELAGE PLUG

A

FOR SLEEVE INSTALLATION

LAST CLAMP FUSELAGE PLUG

OR 86

A

LH SHOWN

RH SYMMETRICAL

D_SB_246103_5_BWAA_01_02

Figure A-FBWAA - Sheet 01

Modification of the Routing between FR50 and FR52 (LH and RH side)

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 547

5

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@A300-600

SERVICE BULLETIN

**CONF ALL

VIEW LOOKING INSIDE

FR50

FR51

FR52

B A

B

FR52

STGR32

C

STGR33

2S−4A

1S/B−3A−3R−1V (73)

(74)

46

63

64

OR (4 POS)

(72)

FWD

PANEL

BRACKET

A

Z148

(2 POS)

D_SB_246103_5_BUAA_01_02

Figure A-FBUAA - Sheet 01

Modification of the Routing of the Passage Way at FR52 (RH side)

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 548

5

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@A300-600

SERVICE BULLETIN

**CONF ALL

(47)

(46)

(45)

46

64

OR

63

(46)

(44)

64

46

OR

63

C

D_SB_246103_5_BUAA_02_01

Figure A-FBUAA - Sheet 02

Modification of the Routing of the Passage Way at FR52 (RH side)

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 549

5

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@A300-600

SERVICE BULLETIN

**CONF 001 thru 002

RIB6A

RIB6

B

LH SIDE SHOWN

RH SIDE SYMMETRICAL

A

A

A

D_SB_246103_5_BMAA_01_00

Figure A-FBMAA - Sheet 01

Modification of the Clamps on the Passage Way to the Shroud Box (LH and RH side) - ADDITIONAL

WORK

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 550

5

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@A300-600

SERVICE BULLETIN

**CONF 001 thru 002

A

A STGR33

B

2S/B−4A (RH)

1S/B−3A (RH)

1S−3R (LH) 1M (LH)

1M/B (LH)

1S/B−3A (LH)

2S/B−4A (LH)

2S−3R (RH) 2M (RH)

2M/B (RH)

(13)

B

B

C

C

D

D

BEFORE

A A

6.35 mm

(0.25 in)

02

2M (LH)

1M (RH)

03

A

A

B

B

A

A

B

B

A

A

B

B

02 IF THE GAP IS LESS THAN 6.35 mm (0.25 in)

ADD A SPACER ITEM 12 BETWEEN THE SPACER

ITEM 13 AND THE STRUCTURE

03 ONLY ONE CONFIGURATION SHOWN

THE STACKING AND NUMBER OF CLAMPS

AND SPACERS MAY DIFFER DEPENDING

ON THE POSITION AND AIRCRAFT

CONFIGURATION

LH SHOWN

RH SYMMETRICAL

01

01

NOTE:

01

APPLY MATERIAL No 05JBC9 IF NEEDED

PROTECTION ADDED IF MISSING

INSTALL THE EXTRUSION ITEM 87 AND

(REFER TO FIG. A−FBDAA SHEET 02)

D_SB_246103_5_BMAA_02_04

Figure A-FBMAA - Sheet 02

Modification of the Clamps on the Passage Way to the Shroud Box (LH and RH side) - ADDITIONAL

WORK

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 551

5

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@A300-600

SERVICE BULLETIN

**CONF 001 thru 002

AFTER

B B

1M (LH)

1M/B (LH)

2M (RH)

2M/B (RH)

2M (LH)

1M (RH)

04

2S/B−4A (RH)

1S/B−3A (RH)

1S/B−3A (LH)

2S/B−4A (LH)

1S−3R (LH)

2S−3R (RH)

130 mm

(5.118 in)

(13)

12 05

NOTE:

04 IF THE GAP IS MORE THAN 130 mm (5.118 in) CONTACT AIRBUS

IF PREVIOUSLY INSTALLED,

KEEP THE OLD SPACER ON THE NEW STACKING

05

SHROUD BOX

FRONT SPAR

D_SB_246103_5_BMAA_03_05

Figure A-FBMAA - Sheet 03

Modification of the Clamps on the Passage Way to the Shroud Box (LH and RH side) - ADDITIONAL

WORK

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 552

5

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@A300-600

SERVICE BULLETIN

**CONF 001 thru 002

1P−2P 1P−2P BEFORE

(24) (24)

1P−2P AFTER 1P−2P

24 24

NOTE:

06 APPLY MATERIAL No 05EML7 AND 08BBD1

C C

07 INSTALL THE STRIP PROTECTIVE ITEM 24 WITH MATERIAL No 05EJL9.

OR

OR

06

07

06

07

D D

D_SB_246103_5_BMAA_04_05

Figure A-FBMAA - Sheet 04

Modification of the Clamps on the Passage Way to the Shroud Box (LH and RH side) - ADDITIONAL

WORK

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 553

5

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@A300-600

SERVICE BULLETIN

**CONF 003

RIB6A

RIB6

A

LH SHOWN

RH SYMMETRICAL

A

A

B C D E

D_SB_246103_5_BMAB_01_01

Figure A-FBMAB - Sheet 01

Modification of the Clamps on the Passage Way to the Shroud Box (LH and RH side) - ADDITIONAL

WORK

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 554

5

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@A300-600

SERVICE BULLETIN

**CONF 003

1P−2P 1P−2P BEFORE

(24) (24)

1P−2P 1P−2P AFTER

24 24

NOTE:

01 APPLY MATERIAL No 05EML7 AND 08BBD1

01

02

02 INSTALL THE STRIP PROTECTIVE ITEM 24 WITH MATERIAL No 05EJL9.

OR

OR

01

02

B

C

D_SB_246103_5_BMAB_02_01

Figure A-FBMAB - Sheet 02

Modification of the Clamps on the Passage Way to the Shroud Box (LH and RH side) - ADDITIONAL

WORK

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 555

5

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@A300-600

SERVICE BULLETIN

**CONF 003

(21) (91)

(92)

(93)

(46)

(51)

(52)

(63)

(64)

OR

OR

OR

(51)

(52)

(63)

(64)

OR

OR

OR

(46) (91) (84)

(51)

(52)

(63)

(64)

OR

OR

OR

(21) (14)

(97)

(51)

(52)

(63)

(64)

OR

OR

OR

STGR32

STGR33

FUSELAGE

BEFORE

A A B B

A

A

B

B

C

C

D

D_SB_246103_5_BMAB_03_01

Figure A-FBMAB - Sheet 03

Modification of the Clamps on the Passage Way to the Shroud Box (LH and RH side) - ADDITIONAL

WORK

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 556

5

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@A300-600

SERVICE BULLETIN

**CONF 003

(93)

(93)

(51)

(52)

(63)

(64)

OR

OR

(84) (95)

(33)

(46)

(62)

(46)

(95)

OR

(51)

(52)

(63)

(64)

OR

OR

OR

(51)

(52)

(63)

(64)

OR

OR

OR (93)

C C

D_SB_246103_5_BMAB_04_02

Figure A-FBMAB - Sheet 04

Modification of the Clamps on the Passage Way to the Shroud Box (LH and RH side) - ADDITIONAL

WORK

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 557

5

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@A300-600

SERVICE BULLETIN

**CONF 003

NOTE:

03 ADD ITEM 21, 46, 94 IF NECESSARY.

STGR33

FUSELAGE

04

04

04 INSTALL EXTRUSION ITEM 87 AND APPLY MATERIAL No 05JBC9 IF NEEDED

PROTECTION ADDED IF MISSING.

94

21

91 92 13

46 21

46

03

03

21

14 46

AFTER

51

52

63

64

OR

OR

OR

51

52

63

64

OR

OR

OR

D D E E

D

D

E

E

F

F

G

G

H

H

J

J

E

D_SB_246103_5_BMAB_05_01

Figure A-FBMAB - Sheet 05

Modification of the Clamps on the Passage Way to the Shroud Box (LH and RH side) - ADDITIONAL

WORK

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 558

5

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@A300-600

SERVICE BULLETIN

**CONF 003

NOTE:

05 PRINCIPLE TO AVOID THE CONTACTS BETWEEN

ELECTRICAL HARNESSES.

12

84 91 46

14

46

62

96

33

46

95

05

21

51

52

63

64

OR

OR

OR

51

52

63

64

OR

OR

OR

51

52

63

64

OR

OR

OR

51

52

63

64

OR

OR

OR

51

52

63

64

OR

OR

OR

51

52

63

64

OR

OR

OR

23

26

66

OR

OR

F F G G

H H J J

D_SB_246103_5_BMAB_06_01

Figure A-FBMAB - Sheet 06

Modification of the Clamps on the Passage Way to the Shroud Box (LH and RH side) - ADDITIONAL

WORK

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 559

5

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@A300-600

SERVICE BULLETIN

**CONF ALL

Z571

A

A

FR47

A

A

A

A

A

A A

A

A

A

A

A

B

B

B

B

B

B B

B

B

B

B

B

D_SB_246103_5_BNAA_01_00

Figure A-FBNAA - Sheet 01

Modification of the Routing of Routes 1P and 2P in the Shroud Box (LH side) - ADDITIONAL

WORK

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 560

5

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@A300-600

SERVICE BULLETIN

**CONF ALL

TYPICAL INSTALLATION

(20)

(22) (19) (19)

(34)

TYPICAL INSTALLATION

BEFORE

AFTER

A A

B B

(20)

62 (19) (19)

(34)

(19)

(20)

(22) (19)

OR

OR

20

62 19 19

34

D_SB_246103_5_BNAA_02_01

Figure A-FBNAA - Sheet 02

Modification of the Routing of Routes 1P and 2P in the Shroud Box (LH side) - ADDITIONAL WORK

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 561

5

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@A300-600

SERVICE BULLETIN

**CONF 001, 003

RIB WIAX − 74.08

RIB WIAX − 40.53

RIB WIAX − 35.12

B

B

Z572 (Z672)

A

A

A

C D

E F

G H

L M J K

RIB WIAX − 48.25

RIB WIAX − 27.96

LH SIDE SHOWN

RH SIDE SYMMETRICAL

D_SB_246103_5_BOAA_01_02

Figure A-FBOAA - Sheet 01

Removal/Installation of the Clamps in LH and RH Wings - ADDITIONAL WORK

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 562

5

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@A300-600

SERVICE BULLETIN

**CONF 001, 003

BEFORE

AFTER

FWD C

(13)

12

46

55

46

(50)

52

FWD D

WY 307.40 REF

(13)

(13)

(46)

(50)

(46)

(50) (51)

WY 307.40 REF

D_SB_246103_5_BOAA_02_01

Figure A-FBOAA - Sheet 02

Removal/Installation of the Clamps in LH and RH Wings - ADDITIONAL WORK

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 563

5

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@A300-600

SERVICE BULLETIN

**CONF 001, 003

BEFORE

AFTER

52

46

(37) 46

(37)

WY 307.40 REF

E

F

FWD

FWD

(51)

(46)

(37) (46)

(37)

WY 307.40 REF

D_SB_246103_5_BOAA_03_00

Figure A-FBOAA - Sheet 03

Removal/Installation of the Clamps in LH and RH Wings - ADDITIONAL WORK

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 564

5

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@A300-600

SERVICE BULLETIN

**CONF 001, 003

WY 290.337 REF

FWD

FWD

(60)

22

BEFORE

AFTER

G

H

90

(21)

NOTE:

01 OVERLAP THE BUNDLES TO MAKE THEIR DIAMETER

MATCH WITH THE DIAMETER OF THE HOLES OF THE

GUIDE ITEM 60 WITH TAPE ASNA51072503 ITEM 85 AND

EN6049−007−08−5 ITEM 86

01

WY 290.337 REF

(60)

(12)

(21)

(61)

(80)

01

D_SB_246103_5_BOAA_04_01

Figure A-FBOAA - Sheet 04

Removal/Installation of the Clamps in LH and RH Wings - ADDITIONAL WORK

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 565

5

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@A300-600

SERVICE BULLETIN

**CONF 001, 003

(71)

(82)

FWD

BEFORE

ROUTE 1P

(2 POS) (51)

ROUTE 2P

J

37

46

FWD

AFTER

(2 POS) 52

K

BEFORE

ROUTE 1P

(2 POS) (51) ROUTE 2P

(82)

(83)

W/AX −55.55

L

AFTER

ROUTE 1P

(2 POS) 52 ROUTE 2P

46

37

W/AX −55.55

M

D_SB_246103_5_BOAA_05_00

Figure A-FBOAA - Sheet 05

Removal/Installation of the Clamps in LH and RH Wings - ADDITIONAL WORK

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 566

5

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@A300-600

SERVICE BULLETIN

**CONF ALL

VIEW LOOKING FORWARD

A

Z147 Z148 −

BEFORE

(16) (14) (32)

(33)

(43)

(16)

B

A

STGR32

(20)

(16) (14)

(33)

(43) (16)

STGR32

(20)

OR

B C

B D

D_SB_246103_5_BPAA_01_03

Figure A-FBPAA - Sheet 01

Modification of the Routing Between FR50 and FR51 at STGR32 (LH and RH side) - ADDITIONAL

WORK

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 567

5

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@A300-600

SERVICE BULLETIN

**CONF ALL

STGR32

VIEW LOOKING FORWARD

AFTER

33

43

12

64 14

46

OR

63

64

OR

63

STGR32

33

43

12

64 14

46

OR

63

64

OR

63

OR

STGR32

VIEW LOOKING FORWARD

33

43

64 14

46

OR

63

64

OR

63

STGR32

33

43

64 14

46

OR

63

64

OR

63

OR

NOTE:

02 IF NECESSARY, INSTALL THE SPACER ITEM

02 02

C

D

12

D_SB_246103_5_BPAA_02_02

Figure A-FBPAA - Sheet 02

Modification of the Routing Between FR50 and FR51 at STGR32 (LH and RH side) - ADDITIONAL

WORK

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 568

5

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@A300-600

SERVICE BULLETIN

**CONF ALL

LH SIDE SHOWN

RH SIDE SYMMETRICAL

1E (LH)

2E (RH)

LOWER WING SURFACE

UPPER WING SURFACE

FUSELAGE THEORICAL

CONTOUR

A

STGR27

STGR28

STGR29

STGR30

2G (RH)

1G (LH)

PRINCIPLE

(23)

A A

PRINCIPLE

66

BEFORE AFTER

B B

A

A

Z613

Z513

AB

AB

AB

AB

D_SB_246103_5_BQAA_01_01

Figure A-FBQAA - Sheet 01

Modification of the Routing in the Leading Edge (LH and RH side) - ADDITIONAL WORK

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 569

5

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@A300-600

SERVICE BULLETIN

**CONF ALL

FR50

FR47

Z571

A

A

(35)

HOLE

SYMBOL ITEM DESCRIPTION

NUT

WASHER

SCREW

B

(21)

(36)

(37)

BEFORE

B C

VIEW LOOKING FWD

D_SB_246103_5_BRAA_01_01

Figure A-FBRAA - Sheet 01

Installation of a Support on the Support of the BLUE Hydraulic Reservoir (LH wing) - ADDITIONAL

WORK

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 570

5

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@A300-600

SERVICE BULLETIN

**CONF ALL

STGR30

STGR31

STGR32

D E

01 3GHA

AFTER

NOTE:

01 ROTATE THE BACKSHELL OF THE CONNECTOR 35HA TO BE ABLE TO ATTACH THE

WIRES FROM 35HA TO THE NEW BRACKET

TAKE CARE TO HAVE A GAP OF 15 mm TO 20 mm (0.590 in TO 0.787 in) 

BETWEEN THE WIRE AND THE HYDRAULIC PIPE

02 INSTALL THE RIVETS ITEM 100 WITH MATERIAL No 04DEB2

HOLE

SYMBOL ITEM PN DESCRIPTION REMARK

100 ASNA2050DXJ5613 RIVET 02

C

VIEW LOOKING FWD

D_SB_246103_5_BRAA_02_03

Figure A-FBRAA - Sheet 02

Installation of a Support on the Support of the BLUE Hydraulic Reservoir (LH wing) - ADDITIONAL

WORK

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 571

5

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@A300-600

SERVICE BULLETIN

**CONF ALL

HOLE

SYMBOL ITEM PN DESCRIPTION

HOLE DIAMETER

MIN MAX

4.85 mm

(0.191 in)

4.95 mm

(0.195 in) ASNA2050DXJ4828 RIVET

NAS1801−3−11 SCREW

68

31

STGR30

STGR31

STGR32

STGR30

STGR31

STGR32

20 NSA935808−01 WASHER

N

N

N

HEAD ON VISIBLE SIDE

FASTENERS NOT AFFECTED

CONDUIT

BEFORE AFTER

VIEW LOOKING INBOARD VIEW LOOKING INBOARD

NOTE:

01 APPLY MATERIAL No 06ABB1

67

69

01

D E

D_SB_246103_5_BRAA_03_03

Figure A-FBRAA - Sheet 03

Installation of a Support on the Support of the BLUE Hydraulic Reservoir (LH wing) - ADDITIONAL

WORK

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 572

5

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@A300-600

SERVICE BULLETIN

**CONF ALL

VIEW LOOKING AFT

A

FR46

FR47

FR48

FR49

FR50

FR51

FR52

FR53

FR54

Z147 Z148 −

LH SIDE SHOWN

RH SIDE SYMMETRICAL

A

C B

BEFORE

FUSELAGE THEORICAL

CONTOUR

B

STGR31

STGR32

STGR33

STGR31

STGR32

STGR33

FUSELAGE THEORICAL

CONTOUR

(27)

(46)

(27)

(46)

OR

D_SB_246103_5_BSAA_01_00

Figure A-FBSAA - Sheet 01

Installation of a Bracket on the Shroud Box Blanking Plate (LH and RH side) - ADDITIONAL WORK

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 573

5

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@A300-600

SERVICE BULLETIN

**CONF ALL

VIEW LOOKING AFT

AFTER

1M

2M

2M

1M

2M

1M

OR

C

46

71

28

29

46

71

21

37

63

64

OR

46

71

46

71

28

29

LH SIDE

RH SIDE

LH SIDE

RH SIDE

70

21

30

21

30

63

64

OR

75

OR

76

OR

NOTE:

01 2 OR 3 BUNDLES MAY BE INSTALLED

01

01

D_SB_246103_5_BSAA_02_02

Figure A-FBSAA - Sheet 02

Installation of a Bracket on the Shroud Box Blanking Plate (LH and RH side) - ADDITIONAL WORK

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 574

5

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@A300-600

SERVICE BULLETIN

**CONF ALL

VIEW LOOKING INSIDE

FR52

FR51

FR50 B

A

FWD B

FR52

STGR32

STGR33

2S−4A

1S/B−3A−3R−1V

(74)

(73)

(72)

C D

63 OR 64

46

PANEL

BRACKET (4 POS)

Z147

A

(2 POS)

D_SB_246103_5_BTAA_01_04

Figure A-FBTAA - Sheet 01

Modification of the Routing of the Passage Way at FR52 (LH side) - ADDITIONAL WORK

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 575

5

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@A300-600

SERVICE BULLETIN

**CONF ALL

63

46

(47)

46

BEFORE

AFTER

(44)

(46)

(47)

(45)

(46)

OR

64

63

OR

64

C

D

D_SB_246103_5_BTAA_02_00

Figure A-FBTAA - Sheet 02

Modification of the Routing of the Passage Way at FR52 (LH side) - ADDITIONAL WORK

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 576

5

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@A300-600

SERVICE BULLETIN

**CONF ALL

VIEW LOOKING INSIDE

FR50

FR51

FR52

B A

B

FR52

STGR32

C

STGR33

2S−4A

1S/B−3A−3R−1V (73)

(74)

46

63

64

OR (4 POS)

(72)

FWD

PANEL

BRACKET

A

Z148

(2 POS)

D_SB_246103_5_BVAA_01_03

Figure A-FBVAA - Sheet 01

Modification of the Routing of the Passage Way at FR52 (RH side) - ADDITIONAL WORK

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 577

5

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@A300-600

SERVICE BULLETIN

**CONF ALL

(47)

(46)

(45)

46

64

OR

63

(46)

(44)

64

46

OR

63

C

D_SB_246103_5_BVAA_02_01

Figure A-FBVAA - Sheet 02

Modification of the Routing of the Passage Way at FR52 (RH side) - ADDITIONAL WORK

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 578

5

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@A300-600

SERVICE BULLETIN

**CONF ALL

MIN 10 mm/MAX 20mm

MIN (0.394 in)/MAX 0.787 in)

INSTALLATION PRINCIPLE

Z147 Z148 −

STGR30

STGR31

STGR32

STGR33

STGR34

FR51 FR52

TO 1776VC, 1777VC,

2043VC, 2673VC

TO 1774VC, 1775VC,

2044VC, 2674VC

(77)

77 OR 78

NOTE:

01 A THIRD CONDUIT MAY BE INSTALLED.

IF INSTALLED, REPLACE IT.

01

LH SIDE SHOWN

RH SIDE SYMMETRICAL

LAST CLAMP FUSELAGE PLUG

A

A

FOR SLEEVE INSTALLATION

D_SB_246103_5_BXAA_01_00

Figure A-FBXAA - Sheet 01

Modification of the Routing between FR50 and FR52 (LH and RH side) - ADDITIONAL WORK

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 579

5

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@A300-600

SERVICE BULLETIN

**CONF ALL

VIEW LOOKING INSIDE

FR52

FR51

FR50 B

A

FWD B

FR52

STGR32

STGR33

2S−4A

1S/B−3A−3R−1V

(72)

C D

63 OR 64

PANEL

BRACKET (4 POS)

Z147

A

(74)

(73) (2 POS) 46

D_SB_246103_5_CAAA_01_00

Figure A-FCAAA - Sheet 01

Modification of the Routing of the Passage Way at FR52 (LH Side) - ADDITIONAL WORK

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 580

5

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@A300-600

SERVICE BULLETIN

**CONF ALL

BEFORE

AFTER

(47)

(46)

C

D

(43)

(63)

(64)

OR

(41)

(42)

(63)

(64)

OR (47)

(46)

(47)

46

43

63

64

OR

41

42

63

64

OR (47)

46

D_SB_246103_5_CAAA_02_02

Figure A-FCAAA - Sheet 02

Modification of the Routing of the Passage Way at FR52 (LH Side) - ADDITIONAL WORK

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 581

5

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@A300-600

SERVICE BULLETIN

**CONF ALL

VIEW LOOKING INSIDE

FR50

FR51

FR52

B A

B

FR52

STGR32

C

STGR33

2S−4A

1S/B−3A−3R−1V (73)

(74)

46

63

64

OR (4 POS)

(72)

FWD

PANEL

BRACKET

A

Z148

(2 POS)

D_SB_246103_5_CBAA_01_00

Figure A-FCBAA - Sheet 01

Modification of the Routing of the Passage Way at FR52 (RH Side) - ADDITIONAL WORK

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 582

5

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@A300-600

SERVICE BULLETIN

**CONF ALL

(47)

(46)

(45)

46

64

OR

63

(46)

(44)

64

46

OR

63

C

D_SB_246103_5_CBAA_02_00

Figure A-FCBAA - Sheet 02

Modification of the Routing of the Passage Way at FR52 (RH Side) - ADDITIONAL WORK

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 583

5

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@A300-600

SERVICE BULLETIN

**CONF 001 thru 002

RIB6A

RIB6

B

A

LH SHOWN

RH SYMMETRICAL

A

A

D_SB_246103_5_CCAA_01_00

Figure A-FCCAA - Sheet 01

Modification of the Clamps on the Passage Way to the Shroud Box (LH and RH Side) - ADDITIONAL

WORK

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 584

5

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@A300-600

SERVICE BULLETIN

**CONF 001 thru 002

A

A STGR33

B

2S/B−4A (RH)

1S/B−3A (RH)

1S−3R (LH) 1M (LH)

1M/B (LH)

1S/B−3A (LH)

2S/B−4A (LH)

2S−3R (RH) 2M (RH)

2M/B (RH)

(13)

B

B

C

C

D

D

BEFORE

A A

6.35 mm

(0.25 in)

02

2M (LH)

1M (RH)

03

A

A

B

B

A

A

B

B

A

A

B

B

02 IF THE GAP IS LESS THAN 6.35 mm (0.25 in)

ADD A SPACER ITEM 12 BETWEEN THE SPACER

ITEM 13 AND THE STRUCTURE

03 ONLY ONE CONFIGURATION SHOWN

THE STACKING AND NUMBER OF CLAMPS

AND SPACERS MAY DIFFER DEPENDING

ON THE POSITION AND AIRCRAFT

CONFIGURATION

LH SHOWN

RH SYMMETRICAL

01

01

NOTE:

01

APPLY MATERIAL No 05JBC9 IF NEEDED

PROTECTION ADDED IF MISSING

INSTALL THE EXTRUSION ITEM 87 AND

(REFER TO FIG. A−FBDAA SHEET 02)

D_SB_246103_5_CCAA_02_03

Figure A-FCCAA - Sheet 02

Modification of the Clamps on the Passage Way to the Shroud Box (LH and RH Side) - ADDITIONAL

WORK

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 585

5

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@A300-600

SERVICE BULLETIN

**CONF 001 thru 002

AFTER

B B

1M (LH)

1M/B (LH)

2M (RH)

2M/B (RH)

2M (LH)

1M (RH)

04

2S/B−4A (RH)

1S/B−3A (RH)

1S/B−3A (LH)

2S/B−4A (LH)

1S−3R (LH)

2S−3R (RH)

130 mm

(5.118 in)

(13)

12 05

NOTE:

04 IF THE GAP IS MORE THAN 130 mm (5.118 in) CONTACT AIRBUS

IF PREVIOUSLY INSTALLED,

KEEP THE OLD SPACER ON THE NEW STACKING

05

SHROUD BOX

FRONT SPAR

D_SB_246103_5_CCAA_03_04

Figure A-FCCAA - Sheet 03

Modification of the Clamps on the Passage Way to the Shroud Box (LH and RH Side) - ADDITIONAL

WORK

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 586

5

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@A300-600

SERVICE BULLETIN

**CONF 001 thru 002

1P−2P 1P−2P BEFORE

(24) (24)

1P−2P AFTER 1P−2P

24 24

NOTE:

06 APPLY MATERIAL No 05EML7 AND 08BBD1

C C

D D

07 INSTALL THE STRIP PROTECTIVE ITEM 24 WITH MATERIAL No 05EJL9

OR

OR

06

07

06

07

D_SB_246103_5_CCAA_04_04

Figure A-FCCAA - Sheet 04

Modification of the Clamps on the Passage Way to the Shroud Box (LH and RH Side) - ADDITIONAL

WORK

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 587

5

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@A300-600

SERVICE BULLETIN

**CONF 003

RIB6A

RIB6

A

LH SHOWN

RH SYMMETRICAL

B C D E

A

A

D_SB_246103_5_CCAB_01_01

Figure A-FCCAB - Sheet 01

Modification of the Clamps on the Passage Way to the Shroud Box (LH and RH Side) - ADDITIONAL

WORK

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 588

5

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@A300-600

SERVICE BULLETIN

**CONF 003

1P−2P 1P−2P BEFORE

(24) (24)

1P−2P 1P−2P AFTER

24 24

NOTE:

01 APPLY MATERIAL No 05EML7 AND 08BBD1

01

02

02 INSTALL THE STRIP PROTECTIVE ITEM 24 WITH MATERIAL No 05EJL9

OR

OR

01

02

B

C

D_SB_246103_5_CCAB_02_01

Figure A-FCCAB - Sheet 02

Modification of the Clamps on the Passage Way to the Shroud Box (LH and RH Side) - ADDITIONAL

WORK

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 589

5

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@A300-600

SERVICE BULLETIN

**CONF 003

(21) (91)

(92)

(93)

(46)

(51)

(52)

(63)

(64)

OR

OR

OR

(51)

(52)

(63)

(64)

OR

OR

OR

(46) (91) (84)

(51)

(52)

(63)

(64)

OR

OR

OR

(21) (14)

(97)

(51)

(52)

(63)

(64)

OR

OR

OR

STGR32

STGR33

FUSELAGE

BEFORE

A A B B

C

C

B

B

A

A

D

D_SB_246103_5_CCAB_03_01

Figure A-FCCAB - Sheet 03

Modification of the Clamps on the Passage Way to the Shroud Box (LH and RH Side) - ADDITIONAL

WORK

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 590

5

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@A300-600

SERVICE BULLETIN

**CONF 003

(93)

(93)

(51)

(52)

(63)

(64)

OR

OR

(84) (95)

(33)

(46)

(62)

(46)

(95)

OR

(51)

(52)

(63)

(64)

OR

OR

OR

(51)

(52)

(63)

(64)

OR

OR

OR (93)

C C

D_SB_246103_5_CCAB_04_02

Figure A-FCCAB - Sheet 04

Modification of the Clamps on the Passage Way to the Shroud Box (LH and RH Side) - ADDITIONAL

WORK

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 591

5

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@A300-600

SERVICE BULLETIN

**CONF 003

NOTE:

03 ADD ITEM 21, 46, 94 IF NECESSARY

STGR33

FUSELAGE

04

04

04 INSTALL EXTRUSION ITEM 87 AND APPLY MATERIAL No 05JBC9 IF NEEDED

PROTECTION ADDED IF MISSING

94

21

91 92 13

46 21

46

03

03

21

14 46

AFTER

51

52

63

64

OR

OR

OR

51

52

63

64

OR

OR

OR

D D E E

J

J

H

H

G

G

F

F D

D

E

E

E

D_SB_246103_5_CCAB_05_01

Figure A-FCCAB - Sheet 05

Modification of the Clamps on the Passage Way to the Shroud Box (LH and RH Side) - ADDITIONAL

WORK

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 592

5

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@A300-600

SERVICE BULLETIN

**CONF 003

NOTE:

05 PRINCIPLE TO AVOID THE CONTACTS BETWEEN

ELECTRICAL HARNESSES.

12

84 91 46

14

46

62

96

33

46

95

05

21

51

52

63

64

OR

OR

OR

51

52

63

64

OR

OR

OR

51

52

63

64

OR

OR

OR

51

52

63

64

OR

OR

OR

51

52

63

64

OR

OR

OR

51

52

63

64

OR

OR

OR

23

26

66

OR

OR

F F G G

H H J J

D_SB_246103_5_CCAB_06_01

Figure A-FCCAB - Sheet 06

Modification of the Clamps on the Passage Way to the Shroud Box (LH and RH Side) - ADDITIONAL

WORK

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 593

5

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@A300-600

SERVICE BULLETIN

**CONF ALL

VIEW LOOKING FORWARD

BEFORE

(16) (14) (32)

(33)

(43) (16)

B

STGR32

(20)

(16) (14)

(33)

(43) (16)

STGR32

(20)

OR

Z147 Z148 − A

B C

B D

A

D_SB_246103_5_CDAA_01_00

Figure A-FCDAA - Sheet 01

Modification of the Routing Between FR50 and FR51 at STGR32 (LH and RH Side) - ADDITIONAL

WORK

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 594

5

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@A300-600

SERVICE BULLETIN

**CONF ALL

STGR32

VIEW LOOKING FORWARD

AFTER

33

43

12

64 14

46

OR

63

64

OR

63

STGR32

33

43

12

64 14

46

OR

63

64

OR

63

OR

STGR32

VIEW LOOKING FORWARD

79

43

64 14

46

OR

63

64

OR

63

STGR32

79

43

64 14

46

OR

63

64

OR

63

OR

NOTE:

02 IF NECESSARY, INSTALL THE SPACER ITEM

02 02

C

D

12

D_SB_246103_5_CDAA_02_01

Figure A-FCDAA - Sheet 02

Modification of the Routing Between FR50 and FR51 at STGR32 (LH and RH Side) - ADDITIONAL

WORK

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 595

5

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@A300-600

SERVICE BULLETIN

**CONF ALL

A

FR47

A

A

A

A

A

A

A

A

B

B

B

B

B

B

B

B

Z571

A

D

D

C

C

C

C

D

D

F

F

E

E

D_SB_246103_5_CEAA_01_01

Figure A-FCEAA - Sheet 01

Modification of the Routing of Routes 1P and 2P in the Shroud Box (LH Side) - ADDITIONAL

WORK

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 596

5

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@A300-600

SERVICE BULLETIN

**CONF ALL

TYPICAL INSTALLATION

20

81 19 19

TYPICAL INSTALLATION

(19)

(20)

(22) (19)

BEFORE AFTER

A A B B

34

D_SB_246103_5_CEAA_02_02

Figure A-FCEAA - Sheet 02

Modification of the Routing of Routes 1P and 2P in the Shroud Box (LH Side) - ADDITIONAL WORK

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 597

5

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@A300-600

SERVICE BULLETIN

**CONF ALL

TYPICAL INSTALLATION

20

81 (19) (19)

TYPICAL INSTALLATION

BEFORE AFTER

(34)

(20)

(22) (19) (19)

(34)

C C D D

D_SB_246103_5_CEAA_03_01

Figure A-FCEAA - Sheet 03

Modification of the Routing of Routes 1P and 2P in the Shroud Box (LH Side) - ADDITIONAL WORK

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 598

5

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@A300-600

SERVICE BULLETIN

**CONF ALL

TYPICAL INSTALLATION

20

71 19 19

TYPICAL INSTALLATION

(19)

(20)

(22) (19)

BEFORE AFTER

84

E E F F

D_SB_246103_5_CEAA_04_00

Figure A-FCEAA - Sheet 04

Modification of the Routing of Routes 1P and 2P in the Shroud Box (LH Side) - ADDITIONAL WORK

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 599

5

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@A300-600

SERVICE BULLETIN

**CONF ALL

RIB6A

RIB6

A

LH SIDE SHOWN

RH SIDE SYMMETRICAL

B

A

A

D_SB_246103_5_CMAA_01_00

Figure A-FCMAA - Sheet 01

Modification of the Routing in LH and RH Wings - ADDITIONAL WORK

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 600

5

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@A300-600

SERVICE BULLETIN

**CONF ALL

C

C C

C

C

C

CLAMPS CLAMPS 01

RIB6 RIB6A

VIEW LOOKING DOWN

B

F

W

D

INBD

AFTER

WIAX 40.53

WIAX 35.12

NOTE:

01 INSTALL SLEEVE ITEM 86 ON ROUTES 1P AND 2P

WITH TIE−CABLES ITEM 26

DISCARD THE VARIOUS ELECTRICAL CONDUIT FROM THE BUNDLES

WHICH WILL BE MODIFIED WITH THE NEW SLEEVE

BEFORE

TYPICAL INSTALLATION

(14)

(66)

14

66

(25) 86

C C

D_SB_246103_5_CMAA_02_01

Figure A-FCMAA - Sheet 02

Modification of the Routing in LH and RH Wings - ADDITIONAL WORK

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 601

5

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@A300-600

SERVICE BULLETIN

**CONF 001, 003

RIB WIAX − 74.08

RIB WIAX − 40.53

RIB WIAX − 35.12

B

B

Z572 (Z672)

A

A

A

C D

E F

G H

D_SB_246103_7_AAAA_01_03

LH SHOWN

RH SIMILAR

Figure A-UAAAA - Sheet 01

Modification of the Support Brackets in the Outer Shroud Box

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 602

5

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@A300-600

SERVICE BULLETIN

**CONF 001, 003

D_SB_246103_7_AAAA_02_02

WY 307.40 REF

BEFORE

AFTER

FWD C

FWD D

WY 307.40 REF

(1)

(2)

1

2

Figure A-UAAAA - Sheet 02

Modification of the Support Brackets in the Outer Shroud Box

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 603

5

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@A300-600

SERVICE BULLETIN

**CONF 001, 003

D_SB_246103_7_AAAA_03_02

WY 307.40 REF

BEFORE

AFTER

WY 307.40 REF

E

F

FWD

FWD

(3)

(2)

3

8

9

Figure A-UAAAA - Sheet 03

Modification of the Support Brackets in the Outer Shroud Box

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 604

5

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@A300-600

SERVICE BULLETIN

**CONF 001, 003

WY 290.337 REF

WY 290.337 REF

FWD

FWD

BEFORE

AFTER

HOLES TO BE

INCREASED TO

4.90MM (0.193IN.)

G

H

(2)

(1)

(2)

2

NOTE:

01 PLUG RIVETS.

01

D_SB_246103_7_AAAA_04_05

Figure A-UAAAA - Sheet 04

Modification of the Support Brackets in the Outer Shroud Box

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 605

5

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@A300-600

SERVICE BULLETIN

**CONF 002

A

A

RIB WIAX − 74.08

RIB WIAX − 40.53

RIB WIAX − 35.12

B

Z572 (Z672)

A

LH SHOWN

RH SIMILAR

B

E F

C D

D_SB_246103_7_BAAA_01_00

Figure A-UBAAA - Sheet 01

Modification of the Support Brackets in the Outer Shroud Box

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 606

5

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@A300-600

SERVICE BULLETIN

**CONF 002

WY 307.40 REF

BEFORE

AFTER

FWD C

FWD D

WY 307.40 REF

(1)

(2)

1

2

D_SB_246103_7_BAAA_02_00

Figure A-UBAAA - Sheet 02

Modification of the Support Brackets in the Outer Shroud Box

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 607

5

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@A300-600

SERVICE BULLETIN

**CONF 002

WY 307.40 REF

BEFORE

AFTER

WY 307.40 REF

E

F

FWD

FWD

(3)

(2)

3

8

9

D_SB_246103_7_BAAA_03_00

Figure A-UBAAA - Sheet 03

Modification of the Support Brackets in the Outer Shroud Box

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 608

5

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@A300-600

SERVICE BULLETIN

**CONF ALL

D_SB_246103_7_ACAA_01_03

VIEW LOOKING AFT ON

FRONT SPAR PRE MOD

JACK No 1

DATUM

FRONT SPAR ROTATE CLIP

THRU 180°

FRONT SPAR

A

D

Z575 (Z675)

Z512 (Z612)

B C B C

(5)

A

(6)

(7)

(7)

(6)

B C

LH SHOWN

RH SIMILAR

Figure A-UACAA - Sheet 01

Modification of the Aircraft Clipping

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 609

5

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@A300-600

SERVICE BULLETIN

**CONF ALL

D_SB_246103_7_ACAA_02_02

REAR SPAR

FLAP TRACK 3 SPOILER HINGE

ABX 47.80 ABX 36.05 WDRX 59.74 ABX 16.30

ROTATE THE BACKSHELL IF

NECESSARY UP TO A MAXIMUM OF

45° TO MAKE SURE THERE IS

A MINIMUM GAP OF 10mm (0.394in.)

BETWEEN THE ELECTRCAL CONDUIT

AND ADJACENT STRUCTURE

VIEW LOOKING INBOARD ON ABX 36.5

WZ 0

E

D

E

Figure A-UACAA - Sheet 02

Modification of the Aircraft Clipping

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 610

5

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@A300-600

SERVICE BULLETIN

**CONF 002

RIB WIAX − 40.53

RIB WIAX − 35.12

B

B

Z572 (Z672)

A

A

A

C D

E F

L M J K

RIB WIAX − 48.25

RIB WIAX − 27.96

LH SIDE SHOWN

RH SIDE SYMMETRICAL

D_SB_246103_5_COAA_01_01

Figure A-FCOAA - Sheet 01

Removal/Installation of the Clamps in LH and RH Wings - ADDITIONAL WORK

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 611

5

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@A300-600

SERVICE BULLETIN

**CONF 002

BEFORE

AFTER

FWD C

(13)

12

46

55

46

(50)

52

FWD D

WY 307.40 REF

(13)

(13)

(46)

(50)

(46)

(50)

(51)

WY 307.40 REF

D_SB_246103_5_COAA_02_00

Figure A-FCOAA - Sheet 02

Removal/Installation of the Clamps in LH and RH Wings - ADDITIONAL WORK

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 612

5

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@A300-600

SERVICE BULLETIN

**CONF 002

BEFORE

AFTER

52

46

(37) 46

(37)

WY 307.40 REF

E

F

FWD

FWD

(51)

(46)

(37) (46)

(37)

WY 307.40 REF

D_SB_246103_5_COAA_03_00

Figure A-FCOAA - Sheet 03

Removal/Installation of the Clamps in LH and RH Wings - ADDITIONAL WORK

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 613

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF 002

(71)

(82)

FWD

BEFORE

ROUTE 1P

(2 POS) (51)

ROUTE 2P

J

37

46

FWD

AFTER

(2 POS) 52

K

BEFORE

ROUTE 1P

(2 POS) (51) ROUTE 2P

(82)

(83)

W/AX −55.55

L

AFTER

ROUTE 1P

(2 POS) 52 ROUTE 2P

46

37

W/AX −55.55

M

D_SB_246103_5_COAA_04_00

Figure A-FCOAA - Sheet 04

Removal/Installation of the Clamps in LH and RH Wings - ADDITIONAL WORK

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 614

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF 003

RIB6A

RIB6

A

LH SHOWN

RH SYMMETRICAL

A

A

B C

D_SB_246103_5_CPAA_01_00

Figure A-FCPAA - Sheet 01

Removal and Installation of the Clamps on the Passage Way to the Shroud Box (LH and RH side)

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 615

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF 003

(21) (91)

(92)

(13)

(46)

(51)

(52)

(63)

(64)

OR

OR

OR

(51)

(52)

(63)

(64)

OR

OR

OR

A A

(46) (91) (84)

(51)

(52)

(63)

(64)

OR

OR

OR

(21) (14)

(97)

(51)

(52)

(63)

(64)

OR

OR

OR

B B

STGR32

STGR33

FUSELAGE

B

B

B

C

C

A

A

BEFORE

D_SB_246103_5_CPAA_02_00

Figure A-FCPAA - Sheet 02

Removal and Installation of the Clamps on the Passage Way to the Shroud Box (LH and RH side)

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 616

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF 003

(13)

(13)

(51)

(52)

(63)

(64)

OR

OR

(84) (95)

(33)

(46)

(62)

(46)

(95)

OR

(51)

(52)

(63)

(64)

OR

OR

OR

(51)

(52)

(63)

(64)

OR

OR

OR

C C

(13)

D_SB_246103_5_CPAA_03_00

Figure A-FCPAA - Sheet 03

Removal and Installation of the Clamps on the Passage Way to the Shroud Box (LH and RH side)

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 617

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF 003

NOTE:

01 ADD ITEM 21, 46, 94 IF NECESSARY.

STGR33

FUSELAGE

02

02

02 INSTALL EXTRUSION ITEM 87 AND APPLY MATERIAL No 05JBC9 IF NEEDED

PROTECTION ADDED IF MISSING.

94

21

91 92 13

46 21

46

01

01

21

14 46

AFTER

C

51

52

63

64

OR

OR

OR

51

52

63

64

OR

OR

OR

D D E E

D

D

E

E

F

F

H

H

G

G

J

J

D_SB_246103_5_CPAA_04_00

Figure A-FCPAA - Sheet 04

Removal and Installation of the Clamps on the Passage Way to the Shroud Box (LH and RH side)

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 618

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF 003

NOTE:

03 PRINCIPLE TO AVOID THE CONTACTS BETWEEN

ELECTRICAL HARNESSES.

12

84 91 46

14

46

62

96

33

46

95

03

21

51

52

63

64

OR

OR

OR

51

52

63

64

OR

OR

OR

51

52

63

64

OR

OR

OR

51

52

63

64

OR

OR

OR

51

52

63

64

OR

OR

OR

51

52

63

64

OR

OR

OR

23

26

66

OR

OR

F F G G

H H J J

D_SB_246103_5_CPAA_05_00

Figure A-FCPAA - Sheet 05

Removal and Installation of the Clamps on the Passage Way to the Shroud Box (LH and RH side)

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 619

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

This Page Intentionally Left Blank

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103

REVISION No.: 03 - Jul 03/15 Page: 620

5

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