# @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



# MANDATORYMANDATORYMANDATORY 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 5

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# @A300-600 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 5

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# @A300-600 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 5

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# @A300-600 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 5

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# @A300-600 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 5

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# @A300-600 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 5

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# @A300-600 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 5

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# @A300-600 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 5

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# @A300-600 SERVICE BULLETIN 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 5

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# @A300-600 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 5

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# @A300-600 SERVICE BULLETIN 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 5

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# @A300-600 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 5

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# @A300-600 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 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

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103 REVISION No.: 03 - Jul 03/15 Page: 13 5

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# @A300-600 SERVICE BULLETIN REVISION TRANSMITTAL SHEET 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

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103 REVISION No.: 03 - Jul 03/15 Page: 14 5

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# @A300-600 SERVICE BULLETIN REVISION TRANSMITTAL SHEET Subtask 246103-941-003-001 SUBTASK SOLUTION UPDATED 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

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103 REVISION No.: 03 - Jul 03/15 Page: 15 5

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# @A300-600 SERVICE BULLETIN REVISION TRANSMITTAL SHEET 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 REVISION No.: 03 - Jul 03/15 Page: 16 5

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# @A300-600 SERVICE BULLETIN REVISION TRANSMITTAL SHEET Subtask 246103-831-047-001 SUBTASK SOLUTION UPDATED QUANTITY UPDATED ITEM NUMBER UPDATED PART NUMBER UPDATED 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 5

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# @A300-600 SERVICE BULLETIN REVISION TRANSMITTAL SHEET 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 5

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# @A300-600 SERVICE BULLETIN 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 5

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# @A300-600 SERVICE BULLETIN 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 5

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# @A300-600 SERVICE BULLETIN 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 5

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# @A300-600 SERVICE BULLETIN 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 5

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# @A300-600 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 5

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# @A300-600 SERVICE BULLETIN 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 5

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# @A300-600 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. 

# MANDATORYMANDATORYMANDATORY 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 Kit246103A01R14 1 3,600.00 Seal fitting, support, conduit, spacer Kit246103A02R12 1 3,400.00 Conduit, spacer Kit246103A03R04 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

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# @A300-600 SERVICE BULLETIN SUMMARY **CONF 002 MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Kit246103A01R14 1 3,600.00 Seal fitting, support, conduit, spacer Kit246103A02R12 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 Kit246103B02R02 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 Kit246103A01R14 1 3,600.00 Seal fitting, support, conduit, spacer Kit246103A02R12 1 3,400.00 Conduit, spacer Kit246103A03R04 2 110.00 Guide, screw Kit246103A04R00 1 710.00 Clamps Kit246103A05R00 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

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# @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 Kit246103B01R03 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 5

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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

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# @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

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# @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



# MANDATORYMANDATORYMANDATORY 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 5

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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 5

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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 Kit246103A01R14 1 (1) Kit246103A02R12 1 (2) Kit246103A03R04 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 Kit246103A01R14 1 (1) Kit246103A02R12 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 Kit246103B02R02 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 Kit246103A01R14 1 (1) Kit246103A02R12 1 (2) 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
MATERIAL QTY PER A/C SEE NOTES Kit246103A03R04 2 (3) Kit246103A04R00 1 (4) Kit246103A05R00 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 Kit246103B01R03 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 5

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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 5

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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 5

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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 5

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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 5

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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 5

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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 5

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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 5

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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 5

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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 5

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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 5

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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-FAAAAgiven 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 5

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# @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: 19 5

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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 5

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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

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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 36.00 ELAPSED TIME (HOURS) 20.75 NOTE: For an explanation of the manhours and elapsed time, refer to the Gantt Chart, Fig. A-FABAAgiven 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

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# @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

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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: 24 5

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# @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

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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-FAAAAgiven 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

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# @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

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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 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

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# @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

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# @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

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# @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 : Kit246103A01R14 Kit246103A02R12 Kit246103A03R04 Kit246103A04R00 Kit246103A05R00 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 Kit246103B02R02 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

Kit246103A01R14 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

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# @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

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# @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. Kit246103A02R12 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 5

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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. Kit246103A03R04 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. Kit246103A04R00 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 5

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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. Kit246103A05R00 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. Kit246103B02R02 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 5

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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 5

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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 5

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# @A300-600 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 5

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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 5

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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 5

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# @A300-600 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 5

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# @A300-600 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 5

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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 5

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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 5

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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 REVISION No.: 03 - Jul 03/15 Page: 45 5

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# @A300-600 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 requiredCorrosion Preventive CompoundWater Displacing 12ADB1 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 REVISION No.: 03 - Jul 03/15 Page: 46 5

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# @A300-600 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 REVISION No.: 03 - Jul 03/15 Page: 47 5

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# @A300-600 SERVICE BULLETIN

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DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103 REVISION No.: 03 - Jul 03/15 Page: 48 5

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# @A300-600 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 REVISION No.: 03 - Jul 03/15 Page: 49 5

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# @A300-600 SERVICE BULLETIN
Task Associated Data **CONF 001 Zone 147 148 512 513 570 571 572 575 612 613 670 672 675 From 147to 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 147to 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 147to 148 From 513to 613 From 570to 670 From 572to 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 REVISION No.: 03 - Jul 03/15 Page: 50 5

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# @A300-600 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 toAMM 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 REVISION No.: 03 - Jul 03/15 Page: 51 5

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# @A300-600 SERVICE BULLETIN (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 REVISION No.: 03 - Jul 03/15 Page: 52 5

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# @A300-600 SERVICE BULLETIN
**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 toAMM 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 REVISION No.: 03 - Jul 03/15 Page: 53 5

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# @A300-600 SERVICE BULLETIN (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 REVISION No.: 03 - Jul 03/15 Page: 54 5

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# @A300-600 SERVICE BULLETIN (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 REVISION No.: 03 - Jul 03/15 Page: 55 5

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# @A300-600 SERVICE BULLETIN (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. DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103 REVISION No.: 03 - Jul 03/15 Page: 56 5

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# @A300-600 SERVICE BULLETIN (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 DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103 REVISION No.: 03 - Jul 03/15 Page: 57 5

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# @A300-600 SERVICE BULLETIN - 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 toAMM 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 DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103 REVISION No.: 03 - Jul 03/15 Page: 58 5

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# @A300-600 SERVICE BULLETIN - 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 toAMM 27-50-00, Page Block 301. (c) Depressurize the hydraulic system, refer toAMM 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 DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103 REVISION No.: 03 - Jul 03/15 Page: 59 5

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# @A300-600 SERVICE BULLETIN
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 toAMM 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 REVISION No.: 03 - Jul 03/15 Page: 60 5

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# @A300-600 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 toAMM 27-50-00, Page Block 301. (c) Depressurize the hydraulic system, refer toAMM 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 REVISION No.: 03 - Jul 03/15 Page: 61 5

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# @A300-600 SERVICE BULLETIN
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 5

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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 5

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# @A300-600 SERVICE BULLETIN - 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 5

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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 5

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# @A300-600 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 5

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# @A300-600 SERVICE BULLETIN
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 REVISION No.: 03 - Jul 03/15 Page: 67 5

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# @A300-600 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 5

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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 5

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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 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: 70 5

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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 DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103 REVISION No.: 03 - Jul 03/15 Page: 71 5

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# @A300-600 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 REVISION No.: 03 - Jul 03/15 Page: 72 5

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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 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 REVISION No.: 03 - Jul 03/15 Page: 73 5

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# @A300-600 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 246103-831-006-001 - 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 REVISION No.: 03 - Jul 03/15 Page: 74 5

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# @A300-600 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 REVISION No.: 03 - Jul 03/15 Page: 75 5

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# @A300-600 SERVICE BULLETIN 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 5

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# @A300-600 SERVICE BULLETINEpoxy 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 5

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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 5

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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 5

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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 5

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# @A300-600 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 5

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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 5

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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 5

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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 5

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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 5

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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 5

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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 5

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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 5

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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 5

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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 5

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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 5

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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 5

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# @A300-600 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 05view 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 5

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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 05view 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 5

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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 05view 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 5

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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 05view 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 5

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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 5

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 05view 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 5

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 05view 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 5

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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

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# @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 05view 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 5

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

# @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 05view 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

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# @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 sothat 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 5

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

# @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 5

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

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

# @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 REVISION No.: 03 - Jul 03/15 Page: 112 5

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# @A300-600 SERVICE BULLETIN
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 REVISION No.: 03 - Jul 03/15 Page: 113 5

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# @A300-600 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 sothat 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 REVISION No.: 03 - Jul 03/15 Page: 114 5

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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 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 REVISION No.: 03 - Jul 03/15 Page: 115 5

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# @A300-600 SERVICE BULLETIN 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 REVISION No.: 03 - Jul 03/15 Page: 116 5

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# @A300-600 SERVICE BULLETIN 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 REVISION No.: 03 - Jul 03/15 Page: 117 5

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# @A300-600 SERVICE BULLETIN 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 REVISION No.: 03 - Jul 03/15 Page: 118 5

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# @A300-600 SERVICE BULLETIN
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 REVISION No.: 03 - Jul 03/15 Page: 119 5

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# @A300-600 SERVICE BULLETIN (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 REVISION No.: 03 - Jul 03/15 Page: 120 5

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# @A300-600 SERVICE BULLETIN (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 REVISION No.: 03 - Jul 03/15 Page: 121 5

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# @A300-600 SERVICE BULLETIN (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 REVISION No.: 03 - Jul 03/15 Page: 122 5

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# @A300-600 SERVICE BULLETIN 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 REVISION No.: 03 - Jul 03/15 Page: 123 5

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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. 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 REVISION No.: 03 - Jul 03/15 Page: 124 5

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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 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 DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103 REVISION No.: 03 - Jul 03/15 Page: 125 5

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# @A300-600 SERVICE BULLETIN
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 5

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# @A300-600 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: 127 5

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# @A300-600 SERVICE BULLETIN
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 REVISION No.: 03 - Jul 03/15 Page: 128 5

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# @A300-600 SERVICE BULLETIN
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: 129 5

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# @A300-600 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 5

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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 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 REVISION No.: 03 - Jul 03/15 Page: 131 5

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# @A300-600 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 5

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# @A300-600 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 REVISION No.: 03 - Jul 03/15 Page: 133 5

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# @A300-600 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 REVISION No.: 03 - Jul 03/15 Page: 134 5

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# @A300-600 SERVICE BULLETIN
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 5

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# @A300-600 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: 136 5

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

# @A300-600 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 5

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

# @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: 138 5

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

# @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 246103-831-007-001 - 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 5

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

# @A300-600 SERVICE BULLETIN
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 REVISION No.: 03 - Jul 03/15 Page: 140 5

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

# @A300-600 SERVICE BULLETIN (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 5

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

# @A300-600 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 5

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

# @A300-600 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 04view 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 04view J

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103 REVISION No.: 03 - Jul 03/15 Page: 143 5

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

# @A300-600 SERVICE BULLETIN
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 04view 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 5

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

# @A300-600 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 04view 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 REVISION No.: 03 - Jul 03/15 Page: 145 5

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

# @A300-600 SERVICE BULLETIN
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 5

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

# @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-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 5

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

# @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 5

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

# @A300-600 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 5

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

# @A300-600 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 04view 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 5

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

# @A300-600 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 04view 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 5

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# @A300-600 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 04view 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 04view K

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103 REVISION No.: 03 - Jul 03/15 Page: 152 5

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

# @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 5

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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 sothat 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 5

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# @A300-600 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 5

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# @A300-600 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 5

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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 5

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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 sothat 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 5

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# @A300-600 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 5

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# @A300-600 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 5

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# @A300-600 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 5

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# @A300-600 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 5

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# @A300-600 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 5

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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 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 5

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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 DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103 REVISION No.: 03 - Jul 03/15 Page: 165 5

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# @A300-600 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 REVISION No.: 03 - Jul 03/15 Page: 166 5

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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 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 REVISION No.: 03 - Jul 03/15 Page: 167 5

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# @A300-600 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 REVISION No.: 03 - Jul 03/15 Page: 168 5

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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 REVISION No.: 03 - Jul 03/15 Page: 169 5

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# @A300-600 SERVICE BULLETIN (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 03view 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 REVISION No.: 03 - Jul 03/15 Page: 170 5

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# @A300-600 SERVICE BULLETIN
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 03view 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 04view 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 REVISION No.: 03 - Jul 03/15 Page: 171 5

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# @A300-600 SERVICE BULLETIN
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 04view 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 04view 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
DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103 REVISION No.: 03 - Jul 03/15 Page: 172 5

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# @A300-600 SERVICE BULLETIN

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 04view 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 REVISION No.: 03 - Jul 03/15 Page: 173 5

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# @A300-600 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 5

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# @A300-600 SERVICE BULLETIN
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 REVISION No.: 03 - Jul 03/15 Page: 175 5

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# @A300-600 SERVICE BULLETIN
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 5

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# @A300-600 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: 177 5

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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 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 REVISION No.: 03 - Jul 03/15 Page: 178 5

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# @A300-600 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 5

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# @A300-600 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 REVISION No.: 03 - Jul 03/15 Page: 180 5

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# @A300-600 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 REVISION No.: 03 - Jul 03/15 Page: 181 5

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# @A300-600 SERVICE BULLETIN
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: 182 5

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# @A300-600 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 5

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# @A300-600 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 5

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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 5

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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 5

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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 5

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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 03view 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 5

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# @A300-600 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 03view 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 04view 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 5

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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 04view 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 04view 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 5

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# @A300-600 SERVICE BULLETIN (i) Install: Refer to Fig. A-FBCAB Sheet 01 and Fig. A-FBCAB Sheet 04view 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 5

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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 5

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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 05view 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 05view 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 5

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# @A300-600 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 05view 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 5

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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 05view 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 5

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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 5

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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 5

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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 5

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# @A300-600 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 5

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# @A300-600 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 5

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# @A300-600 SERVICE BULLETIN
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 5

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# @A300-600 SERVICE BULLETIN
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 05view 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 5

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# @A300-600 SERVICE BULLETIN
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 05view 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 5

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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 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 05view 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 5

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# @A300-600 SERVICE BULLETIN (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 05view 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 5

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# @A300-600 SERVICE BULLETIN
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 5

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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 sothat 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 5

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# @A300-600 SERVICE BULLETIN
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 REVISION No.: 03 - Jul 03/15 Page: 209 5

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# @A300-600 SERVICE BULLETIN
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 REVISION No.: 03 - Jul 03/15 Page: 210 5

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# @A300-600 SERVICE BULLETIN
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 REVISION No.: 03 - Jul 03/15 Page: 211 5

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# @A300-600 SERVICE BULLETIN
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 REVISION No.: 03 - Jul 03/15 Page: 212 5

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# @A300-600 SERVICE BULLETIN (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 5

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# @A300-600 SERVICE BULLETIN
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 sothat 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 REVISION No.: 03 - Jul 03/15 Page: 214 5

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# @A300-600 SERVICE BULLETIN
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 5

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# @A300-600 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 246103-942-001-001 - 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 toAMM 06-41-57, Page Block 001. (c) Install the access panels 512AB(612AB), 512BB(612BB), 512CB(612CB), 512DB(612DB), refer toAMM 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 5

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# @A300-600 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 toAMM 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 5

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# @A300-600 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 toAMM 06-41-57, Page Block 001. (c) Install the access panels 512AB(612AB), 512BB(612BB), 512CB(612CB), 512DB(612DB), refer toAMM 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 REVISION No.: 03 - Jul 03/15 Page: 218 5

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# @A300-600 SERVICE BULLETIN (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 toAMM 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 REVISION No.: 03 - Jul 03/15 Page: 219 5

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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 5

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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 5

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# @A300-600 SERVICE BULLETIN
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 5

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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 51-40-00 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 toAMM 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 5

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# @A300-600 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 246103-839-002-001 - 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 5

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# @A300-600 SERVICE BULLETIN (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 toAMM 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 5

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# @A300-600 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 5

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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 5

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# @A300-600 SERVICE BULLETIN
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 toAMM 06-41-57, Page Block 001. (f) If necessary, extend the flaps, refer toAMM 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 5

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# @A300-600 SERVICE BULLETIN
**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 toAMM 06-41-57, Page Block 001. (f) If necessary, extend the flaps, refer toAMM 27-50-00, Page Block 301. DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103 REVISION No.: 03 - Jul 03/15 Page: 229 5

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# @A300-600 SERVICE BULLETIN (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 5

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# @A300-600 SERVICE BULLETIN (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 5

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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-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

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# @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

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# @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

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# @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

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# @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

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# @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

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# @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

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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 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

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# @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 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
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

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# @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

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# @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

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# @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

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# @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

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# @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

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# @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 02view 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 02view 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 5

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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 02view 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 02view 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 5

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 5

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# @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 5

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# @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 5

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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 5

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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 02view 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 02view 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 5

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

# @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 02view 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 02view 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 5

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# @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 5

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# @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 5

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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 5

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

# @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 5

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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 5

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

# @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 5

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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 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 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 5

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

# @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 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 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 5

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

# @A300-600 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 5

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

# @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 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 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 5

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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 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 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 5

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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 5

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 5

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 5

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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 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 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 02view 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 02view 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 5

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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 02view 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 02view 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 5

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# @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 5

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# @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 5

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# @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 5

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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 5

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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 02view 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 02view 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 5

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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 02view 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 02view 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 5

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# @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 5

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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 5

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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

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103 REVISION No.: 03 - Jul 03/15 Page: 286 5

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# @A300-600 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 04view 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 REVISION No.: 03 - Jul 03/15 Page: 287 5

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# @A300-600 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 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 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 05view 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 REVISION No.: 03 - Jul 03/15 Page: 288 5

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# @A300-600 SERVICE BULLETIN
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 06view 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 REVISION No.: 03 - Jul 03/15 Page: 289 5

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# @A300-600 SERVICE BULLETIN
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 06view 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 06view 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 REVISION No.: 03 - Jul 03/15 Page: 290 5

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# @A300-600 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 REVISION No.: 03 - Jul 03/15 Page: 291 5

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# @A300-600 SERVICE BULLETIN 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

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103 REVISION No.: 03 - Jul 03/15 Page: 292 5

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# @A300-600 SERVICE BULLETIN
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 REVISION No.: 03 - Jul 03/15 Page: 293 5

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# @A300-600 SERVICE BULLETIN
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 04view 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 05view D-D 1 Stud NSA5159-35 Item 94 1 Nut NSA5050-3 Item 21 3 Clamp NSA5516-12ND Item 51 DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103 REVISION No.: 03 - Jul 03/15 Page: 294 5

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# @A300-600 SERVICE BULLETIN

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 05view 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 06view F-F 1 Nut NSA5050-3 Item 21 5 Clamp NSA5516-08ND Item 52
DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103 REVISION No.: 03 - Jul 03/15 Page: 295 5

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# @A300-600 SERVICE BULLETIN

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 06view 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 06view 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 REVISION No.: 03 - Jul 03/15 Page: 296 5

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# @A300-600 SERVICE BULLETIN

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 06view 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 REVISION No.: 03 - Jul 03/15 Page: 297 5

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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
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 REVISION No.: 03 - Jul 03/15 Page: 298 5

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# @A300-600 SERVICE BULLETIN
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 REVISION No.: 03 - Jul 03/15 Page: 299 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 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 5

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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: 301 5

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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: 302 5

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# @A300-600 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: 303 5

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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: 304 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 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 5

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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: 306 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 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: 307 5

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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: 308 5

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: 309 5

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# @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: 310 5

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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: 311 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 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 02view 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 02view 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: 312 5

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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 02view 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 02view 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: 313 5

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: 314 5

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: 315 5

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# @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: 316 5

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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: 317 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 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 02view 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 02view 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: 318 5

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

# @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 02view 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 02view 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: 319 5

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# @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: 320 5

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# @A300-600 SERVICE BULLETIN
**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).

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103 REVISION No.: 03 - Jul 03/15 Page: 321 5

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# @A300-600 SERVICE BULLETIN
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 REVISION No.: 03 - Jul 03/15 Page: 322 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 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 toAMM 53-15-63, Page Block 401. (c) Install the access panels 513AT, 513BT, 571BB, 571CB, 571DB, 613AT and 613BT, refer toAMM 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 toAMM 53-15-63, Page Block 401. (c) Install the access panels 513AT, 513BT, 571BB, 571CB, 571DB, 613AT and 613BT, refer toAMM 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 REVISION No.: 03 - Jul 03/15 Page: 323 5

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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 5

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# @A300-600 SERVICE BULLETIN
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 5

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# @A300-600 SERVICE BULLETIN
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 5

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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 toAMM 06-31-53, Page Block 001. (c) For the identification of zones, refer toAMM 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 5

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# @A300-600 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 5

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# @A300-600 SERVICE BULLETIN (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 toAMM 06-31-53, Page Block 001. (c) For the identification of zones, refer toAMM 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 5

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# @A300-600 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 5

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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 toAMM 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 5

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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 toAMM 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 5

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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 5

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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 5

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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 5

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# @A300-600 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 5

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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 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 REVISION No.: 03 - Jul 03/15 Page: 338 5

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

# @A300-600 SERVICE BULLETIN 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 5

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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 5

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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 5

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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 5

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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 5

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

# @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 5

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 5

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

# @A300-600 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 5

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# @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 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) 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 5

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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 5

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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 5

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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 5

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

# @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 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 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 5

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

# @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 5

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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 5

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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 5

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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 5

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

# @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 5

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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 5

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# @A300-600 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 5

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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 05view 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 05view 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 5

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# @A300-600 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 05view 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 05view 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 5

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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 5

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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 5

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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 5

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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 05view K

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103 REVISION No.: 03 - Jul 03/15 Page: 366 5

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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 05view 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 5

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# @A300-600 SERVICE BULLETIN (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 5

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# @A300-600 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 05view 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 5

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# @A300-600 SERVICE BULLETIN
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 05view 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 5

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# @A300-600 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 5

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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 5

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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 5

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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 5

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# @A300-600 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 REVISION No.: 03 - Jul 03/15 Page: 375 5

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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: 376 5

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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 REVISION No.: 03 - Jul 03/15 Page: 377 5

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

# @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

(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 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 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 5

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

# @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: 380 5

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: 381 5

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

# @A300-600 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: 382 5

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: 383 5

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

# @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: 384 5

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

# @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: 385 5

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

# @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: 386 5

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

# @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: 387 5

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

# @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: 388 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 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 5

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

# @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: 390 5

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

# @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 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 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 5

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

# @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: 393 5

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

# @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: 394 5

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

# @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 5

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

# @A300-600 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 5

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

# @A300-600 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 04view 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 04view 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 5

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

# @A300-600 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. Fig. A-FCOAA Sheet 01 and Fig. A-FCOAA Sheet 04view 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 04view 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 5

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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 5

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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 (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 5

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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 5

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# @A300-600 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 04view 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 5

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# @A300-600 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 04view 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 04view K DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103 REVISION No.: 03 - Jul 03/15 Page: 403 5

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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 04view 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 5

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# @A300-600 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 5

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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: 406 5

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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 5

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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 5

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# @A300-600 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 REVISION No.: 03 - Jul 03/15 Page: 409 5

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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 5

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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 REVISION No.: 03 - Jul 03/15 Page: 411 5

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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

(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 5

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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 5

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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 REVISION No.: 03 - Jul 03/15 Page: 414 5

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# @A300-600 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 04view 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 5

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# @A300-600 SERVICE BULLETIN (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 5

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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 REVISION No.: 03 - Jul 03/15 Page: 417 5

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# @A300-600 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 5

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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 5

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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 5

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# @A300-600 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 5

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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 5

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# @A300-600 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 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

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 5

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# @A300-600 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 5

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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 5

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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 5

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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 5

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# @A300-600 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 5

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# @A300-600 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 5

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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 5

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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 5

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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 5

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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 5

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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 04view 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 5

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# @A300-600 SERVICE BULLETIN

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 5

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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 5

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# @A300-600 SERVICE BULLETIN
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 5

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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 5

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# @A300-600 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 05view 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 5

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# @A300-600 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 05view 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 05view 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 5

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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 05view 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 5

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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 5

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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 5

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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 (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 5

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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 05view 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 5

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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 05view 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 5

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# @A300-600 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 05view K

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103 REVISION No.: 03 - Jul 03/15 Page: 447 5

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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-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 05view 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 5

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# @A300-600 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 5

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# @A300-600 SERVICE BULLETIN
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 5

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# @A300-600 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 toAMM 06-41-57, Page Block 001. (c) Install the access panels 512BB(612BB), refer toAMM 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 5

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# @A300-600 SERVICE BULLETIN (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 toAMM 06-41-57, Page Block 001. (c) Install the access panels 512BB(612BB), refer toAMM 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 5

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# @A300-600 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 5

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# @A300-600 SERVICE BULLETIN
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 **CONFALL 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 5

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# @A300-600 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: 455 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 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 5

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# @A300-600 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 5

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# @A300-600 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. **CONFALL 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 5

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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 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 5

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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 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 5

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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. **CONFALL 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 05view 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 5

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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 05view 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 5

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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 05view 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 5

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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 05view 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 5

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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 5

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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 5

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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 5

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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 05view 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 5

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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 05view 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 05view 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 5

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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 05view 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 5

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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 04view 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 5

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# @A300-600 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 04view 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 5

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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 04view 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 5

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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 5

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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 5

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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 04view K

DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103 REVISION No.: 03 - Jul 03/15 Page: 478 5

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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 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 04view 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

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# @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 04view 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

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# @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 04view 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

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# @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 02view 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

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# @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 02view 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 03view 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

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# @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 04view 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 04view E-E DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103 REVISION No.: 03 - Jul 03/15 Page: 484 5

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# @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

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# @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

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# @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

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# @A300-600 SERVICE BULLETIN (a) Depending on the stacking, remove: Refer to Fig. A-FCPAA Sheet 01 and Fig. A-FCPAA Sheet 02view 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 02view 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

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# @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 03view 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 04view 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

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# @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 04view 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 05view 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

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# @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 05view 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 05view 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

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# @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 05view 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 05view 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

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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 05view 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

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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

(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 05view 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

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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 05view 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

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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: 496 5

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# @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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# @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

(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 5

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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 05view 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 5

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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 05view 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

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

# @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 05view 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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# @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 05view 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 **CONFALL 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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# @A300-600 SERVICE BULLETIN
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. **CONFALL 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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# @A300-600 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

B FWD 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: DEPENDING ON AIRCRAFT CONFIGURATION, 01 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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# @A300-600 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 1S/B

−3A

−3R

−1V 23 38 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: IF INSTALLED 01 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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# @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_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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# @A300-600 SERVICE BULLETIN

**CONF ALL

VIEW LOOKING AFT 

## AFTER

1M2M2M

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: 2 OR 3 BUNDLES MAY BE INSTALLED 01 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 29LH SIDE RH SIDE

28 29LH SIDE RH SIDE 

## C

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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# @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) 

## ORB 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 14 64

46 OR 63

64 OR 63 STGR32

33 43 12

14 64

46 OR 63

64 OR 63 

## OR

STGR32

VIEW LOOKING FORWARD 79 43 14 64

46 OR 63

64 OR 63 STGR32

79 4314 64

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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# @A300-600 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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# @A300-600 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)

IF THE GAP IS LESS THAN 6.35 mm (0.25 in) 03 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: IF THE GAP IS MORE THAN 130 mm (5.118 in) 01 CONTACT AIRBUS INSTALL THE EXTRUSION ITEM 87 02 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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# @A300-600 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: ADD ITEM 21, 46, 94 IF NECESSARY. 01 STGR33 FUSELAGE

02 02

INSTALL EXTRUSION ITEM 87 AND APPLY MATERIAL No 05JBC9 IF NEEDED 02 PROTECTION ADDED IF MISSING. 94 21 91 92 1346 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 DD F 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: PRINCIPLE TO AVOID THE CONTACTS BETWEEN 03 ELECTRICAL HARNESSES. 12 84 46 91
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: PRINCIPLE TO AVOID THE CONTACTS BETWEEN 03 ELECTRICAL HARNESSES. 12 84 46 91
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

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

# @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

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

# @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) 02 01 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: APPLY MATERIAL No 05EML7 AND 08BBD1 01 INSTALL THE STRIP PROTECTIVE ITEM 02 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

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

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

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

# @A300-600 SERVICE BULLETIN

**CONF 003 1P

−2P

22

20 19
12
19 12

21 

## C 1P

−2P

24 24

INSTALL THE STRIP PROTECTIVE ITEM 24 02 01 01 FWD 02 02

NOTE: APPLY MATERIAL No 05EML7 AND 08BBD1 01 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

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

# @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

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

# @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 71 (19) (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

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

# @A300-600 SERVICE BULLETIN

**CONF ALL FR50
FR47



### B Z571 

### A



## A STGR30

STGR31

STGR32 

### D C



## B NOTE: ROTATE THE BACKSHELL OF THE CONNECTOR 35HA TO BE ABLE TO ATTACH THE 01 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

NSA935808

−01 WASHER 20 N
N N HEAD ON VISIBLE SIDE FASTENERS NOT AFFECTED CONDUIT 

## BEFORE AFTER

VIEW LOOKING INBOARD VIEW LOOKING INBOARD 

## C D

NOTE: APPLY MAT. No 06ABB1 01 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

J K L M 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

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

# @A300-600 SERVICE BULLETIN
**CONF 001, 003

(51)

(46) (50) (13)

(51) WY 307.40 REF 

## BEFORE

AFTER C FWD

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

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

# @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

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

# @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: OVERLAP THE BUNDLES TO MAKE THEIR DIAMETER 01 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

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

# @A300-600 SERVICE BULLETIN
**CONF 001, 003

(37) (46)

FWD 

## BEFORE ROUTE 1P (51) (2 POS)

ROUTE 2P 

## J 37 46

FWD 

## AFTER

52 (2 POS)



## K


## BEFORE ROUTE 1P

ROUTE 2P (51) (2 POS) (46) (37)W/AX−55.55



## L


## AFTER ROUTE 1P

ROUTE 2P 52 (2 POS) 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

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

# @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

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

# @A300-600 SERVICE BULLETIN

**CONF 002

(51)

(46) (50) (13)

(51) WY 307.40 REF


## C FWD

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

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

# @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

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

# @A300-600 SERVICE BULLETIN

**CONF 002

(37) (46)

FWD 

## BEFORE ROUTE 1P (51) (2 POS)

ROUTE 2P 37 46

FWD 

## AFTER

52 (2 POS)



## BEFORE ROUTE 1P

ROUTE 2P (51) (2 POS) (46) (37)W/AX−55.55



## AFTER ROUTE 1P

ROUTE 2P 52 (2 POS) 46W/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

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

# @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:
INSTALL SLEEVE ITEM 86 ON ROUTES 1P AND 2P 01 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

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

# @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) 77OR 78 NOTE: 01 A THIRD CONDUIT MAY BE INSTALLED IF INSTALLED REPLACE IT01

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

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

# @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

IF THE GAP IS LESS THAN 6.35 mm (0.25 in) 02 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: IF THE GAP IS MORE THAN 130 mm (5.118 in) CONTACT AIRBUS 04 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 1P

−2P 

## AFTER

24 24
NOTE: APPLY MATERIAL No 05EML7 AND 08BBD1 06 

## 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

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

# @A300-600 SERVICE BULLETIN

**CONF 003 1P

−2P 1P

−2P 

## BEFORE

(24) (24)

1P

−2P 1P

−2P 

## AFTER

24 24
NOTE: APPLY MATERIAL No 05EML7 AND 08BBD1 01 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

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

# @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) (84) (91) (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

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

# @A300-600 SERVICE BULLETIN

**CONF 003

(93)

(93) (51) (52) (63) (64) OR
OR (95) (84)

(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

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

# @A300-600 SERVICE BULLETIN

**CONF 003

NOTE: ADD ITEM 21, 46, 94 IF NECESSARY. 03 STGR33 FUSELAGE

04 04

INSTALL EXTRUSION ITEM 87 AND APPLY MATERIAL No 05JBC9 IF NEEDED 04 PROTECTION ADDED IF MISSING. 94 21 91 92 1346 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 GG 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

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

# @A300-600 SERVICE BULLETIN

**CONF 003

NOTE: PRINCIPLE TO AVOID THE CONTACTS BETWEEN 05 ELECTRICAL HARNESSES. 12 84 46 91
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

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

# @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

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

# @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

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

# @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

J K L M 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

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

# @A300-600 SERVICE BULLETIN
**CONF 001, 003 

## BEFORE

AFTER C FWD

(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

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

# @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

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

# @A300-600 SERVICE BULLETIN
**CONF 001, 003

WY 290.337 REF

FWD FWD

(60) 22 

## BEFORE

AFTER G

H 90 (21)

NOTE: OVERLAP THE BUNDLES TO MAKE THEIR DIAMETER 01 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

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

# @A300-600 SERVICE BULLETIN
**CONF 001, 003

(71) (82)

FWD 

## BEFORE ROUTE 1P (51) (2 POS)

ROUTE 2P 

## J 37 46

FWD 

## AFTER

52 (2 POS)



## K


## BEFORE ROUTE 1P

ROUTE 2P (51) (2 POS) (82) (83)W/AX−55.55



## L


## AFTER ROUTE 1P

ROUTE 2P 52 (2 POS) 46 37W/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

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

# @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) 

## ORB 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

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

# @A300-600 SERVICE BULLETIN

**CONF ALL

STGR32

VIEW LOOKING FORWARD 

## AFTER

33 43 12 14 64

46 OR 63

64 OR 63 STGR32

33 43 12

14 64

46 OR 63

64 OR 63 

## OR

STGR32

VIEW LOOKING FORWARD 33 43 14 64

46 OR 63

64 OR 63 STGR32

33 4314 64

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: ROTATE THE BACKSHELL OF THE CONNECTOR 35HA TO BE ABLE TO ATTACH THE 01 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 INSTALL THE RIVETS ITEM 100 WITH MATERIAL No 04DEB2 02

HOLE SYMBOL ITEM PN DESCRIPTION REMARK
ASNA2050DXJ5613 RIVET 100 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

NSA935808

−01 WASHER 20 N
N N HEAD ON VISIBLE SIDE FASTENERS NOT AFFECTED CONDUIT 

## BEFORE AFTER

VIEW LOOKING INBOARD VIEW LOOKING INBOARD

NOTE:

APPLY MATERIAL No 06ABB1 01 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

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

# @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

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

# @A300-600 SERVICE BULLETIN

**CONF ALL

VIEW LOOKING AFT 

## AFTER

1M2M2M

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: 2 OR 3 BUNDLES MAY BE INSTALLED 01 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

B FWD FR52
STGR32

STGR33 2S

−4A

1S/B

−3A

−3R

−1V (74) (73)

(72) 

### C D

63OR64 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) 77OR 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

B FWD FR52
STGR32

STGR33 2S

−4A

1S/B

−3A

−3R

−1V (72) 

### C D

63OR64 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) 4643

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

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

# @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

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

# @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

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

# @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

IF THE GAP IS LESS THAN 6.35 mm (0.25 in) 02 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: IF THE GAP IS MORE THAN 130 mm (5.118 in) CONTACT AIRBUS 04 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 1P

−2P 

## AFTER

24 24
NOTE: APPLY MATERIAL No 05EML7 AND 08BBD1 06 

## 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: APPLY MATERIAL No 05EML7 AND 08BBD1 01 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

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

# @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) (84) (91) (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

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

# @A300-600 SERVICE BULLETIN

**CONF 003

(93)

(93) (51) (52) (63) (64) OR
OR (95) (84)

(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

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

# @A300-600 SERVICE BULLETIN

**CONF 003

NOTE: ADD ITEM 21, 46, 94 IF NECESSARY 03 STGR33 FUSELAGE

04 04

INSTALL EXTRUSION ITEM 87 AND APPLY MATERIAL No 05JBC9 IF NEEDED 04 PROTECTION ADDED IF MISSING 94 21 91 92 1346 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: PRINCIPLE TO AVOID THE CONTACTS BETWEEN 05 ELECTRICAL HARNESSES. 12 84 46 91
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 14 64

46 OR 63

64 OR 63 STGR32

33 43 12

14 64

46 OR 63

64 OR 63 

## OR

STGR32

VIEW LOOKING FORWARD 79 43 14 64

46 OR 63

64 OR 63 STGR32

79 4314 64

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

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

# @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 01 CLAMPS CLAMPS

RIB6 RIB6A

VIEW LOOKING DOWN 

## B F W D INBD



## AFTER WIAX 40.53 WIAX 35.12

NOTE:
INSTALL SLEEVE ITEM 86 ON ROUTES 1P AND 2P 01 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

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

# @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

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

# @A300-600 SERVICE BULLETIN
**CONF 001, 003

D_SB_246103_7_AAAA_02_02 WY 307.40 REF 

## BEFORE

AFTER C FWD

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

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

# @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: PLUG RIVETS. 01 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

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

# @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

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

# @A300-600 SERVICE BULLETIN

**CONF 002

WY 307.40 REF 

## BEFORE

AFTER C FWD

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

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

# @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

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

# @A300-600 SERVICE BULLETIN

**CONF ALL

D_SB_246103_7_ACAA_02_02 REAR SPAR

SPOILER HINGE FLAP TRACK 3 ABX 16.30 WDRX 59.74 ABX 36.05 ABX 47.80

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

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

# @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

J K L M 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

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

# @A300-600 SERVICE BULLETIN

**CONF 002 

## BEFORE

AFTER C FWD

(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

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

# @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 (51) (2 POS)

ROUTE 2P 

## J 37 46

FWD 

## AFTER

52 (2 POS)



## K


## BEFORE ROUTE 1P

ROUTE 2P (51) (2 POS) (82) (83)W/AX−55.55



## L


## AFTER ROUTE 1P

ROUTE 2P 52 (2 POS) 46 37W/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) (84) (91) (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

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# @A300-600 SERVICE BULLETIN

**CONF 003

(13)

(13) (51) (52) (63) (64) OR
OR (95) (84)

(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

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# @A300-600 SERVICE BULLETIN

**CONF 003

NOTE: ADD ITEM 21, 46, 94 IF NECESSARY. 01 STGR33 FUSELAGE

02 02

INSTALL EXTRUSION ITEM 87 AND APPLY MATERIAL No 05JBC9 IF NEEDED 02 PROTECTION ADDED IF MISSING. 94 21 91 92 1346 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: PRINCIPLE TO AVOID THE CONTACTS BETWEEN 03 ELECTRICAL HARNESSES. 12 84 46 91
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

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# @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.