# @A310 SERVICE BULLETIN REVISION TRANSMITTAL SHEET AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Tel : (33) 5 61 93 33 33 Telex : AIRBU 530526F Fax : (33) 5 61 93 42 51



# MANDATORY MANDATORY MANDATORY
ATA SYSTEM: 28 

### TITLE: ELECTRIC/ELECTRONIC COMMON INSTALLATION - WING - IMPROVE THE 2S-ROUTE IN THE RH-WING MODIFICATION No.: 12427D21883 12435S22116 13478D23233 This page transmits Revision No.06 of Service Bulletin No.A310-28-2148 ADDITIONAL WORK **CONF ALL Additional work 3 is required on configurations 003, 004, 007 and 008 by this revision for aircraft modified at revision 00, 01, 02 and 03 and without Service Bulletin A310-36-2015 (Modification No. 7633S7885) embodied. ADDITIONAL WORK 1: applicable to Configuration 001, 002, 005 and 006 is required for aircraft that have been modified by accomplishment of this Service Bulletin from the original issue up to revision 01. The work which follows is required: - segregation of the route 2S in RH pylon area - installation of an additional protection sleeve in the outer wing area near the cadensicon sensor 10QT. ADDITIONAL WORK 2: applicable to Configuration 001, 002, 005 and 006 is required for aircraft that have been modified by accomplishment of this Service Bulletin from the original issue up to revision 02. The work which follows is required: - installation of an modified bracket on the RH wing. ADDITIONAL WORK 3: applicable to Configuration 003, 004, 007 and 008 is required for aircraft that have been modified by accomplishment of this Service Bulletin from the original issue up to revision 03. The work which follows is required: - improvement of the 2S route in the RH wing pylon area.

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 1 6

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# @A310 SERVICE BULLETIN REVISION TRANSMITTAL SHEET REASON Revision No. 06 issued to update the additional work statement to add ADDITIONAL WORK 3. The opportunity is taken to produce this Service Bulletin in the latest format. Layout changes due to computerization of this revision are not identified. CHANGES SUMMARY MODIFICATIONS Minor editorial or document structure change N REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES Minor editorial or document structure change N GENERAL EVALUATION Minor editorial or document structure change N MATERIAL PRICE INFORMATION Minor editorial or document structure change N Minor editorial or document structure change N Minor editorial or document structure change N Minor editorial or document structure change N Minor editorial or document structure change N Minor editorial or document structure change N Minor editorial or document structure change N Minor editorial or document structure change N EFFECTIVITY Minor editorial or document structure change N CONCURRENT REQUIREMENTS Minor editorial or document structure change N REFERENCES / REPERCUSSIONS Minor editorial or document structure change N NATURE OF THE WORK Minor editorial or document structure change N MANPOWER Minor editorial or document structure change N Minor editorial or document structure change N Minor editorial or document structure change N Minor editorial or document structure change N Minor editorial or document structure change N Minor editorial or document structure change N Minor editorial or document structure change N Minor editorial or document structure change N APPENDICES Minor editorial or document structure change N Fig. A-GSAAA Minor editorial or document structure change N Fig. A-GSAAA Sheet 01 Minor editorial or document structure change N Fig. A-GSAAA Sheet 02 Minor editorial or document structure change N Fig. A-GSAAA Sheet 03 Minor editorial or document structure change N Fig. A-GSAAA Sheet 04 Minor editorial or document structure change N PLANNING INFORMATION EFFECTIVITY Minor editorial or document structure change N Configuration definition Minor editorial or document structure change N
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 2 6

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# @A310 SERVICE BULLETIN REVISION TRANSMITTAL SHEET
CONF 001 Minor editorial or document structure change N CONF 002 Minor editorial or document structure change N CONF 003 Minor editorial or document structure change N CONF 004 Minor editorial or document structure change N CONF 005 Minor editorial or document structure change N CONF 006 Minor editorial or document structure change N CONF 007 Minor editorial or document structure change N CONF 008 Minor editorial or document structure change N Material Effectivity Minor editorial or document structure change N Minor editorial or document structure change N Minor editorial or document structure change N Minor editorial or document structure change N Minor editorial or document structure change N CONCURRENT REQUIREMENTS Minor editorial or document structure change N REASON Minor editorial or document structure change N History Minor editorial or document structure change N Objective/Action Minor editorial or document structure change N Advantages Minor editorial or document structure change N Operational/Maintenance Consequences Minor editorial or document structure change N DESCRIPTION Minor editorial or document structure change N COMPLIANCE Minor editorial or document structure change N Classification Minor editorial or document structure change N Accomplishment Timescale Minor editorial or document structure change N APPROVAL Minor editorial or document structure change N Minor editorial or document structure change N MANPOWER Minor editorial or document structure change N Minor editorial or document structure change N Minor editorial or document structure change N Minor editorial or document structure change N Minor editorial or document structure change N Minor editorial or document structure change N Minor editorial or document structure change N Minor editorial or document structure change N Minor editorial or document structure change N WEIGHT AND BALANCE Minor editorial or document structure change N Minor editorial or document structure change N Minor editorial or document structure change N Minor editorial or document structure change N Minor editorial or document structure change N ELECTRICAL LOAD DATA Minor editorial or document structure change N
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 3 6

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# @A310 SERVICE BULLETIN REVISION TRANSMITTAL SHEET
REFERENCES Minor editorial or document structure change N Minor editorial or document structure change N Minor editorial or document structure change N Minor editorial or document structure change N Minor editorial or document structure change N Minor editorial or document structure change N Minor editorial or document structure change N Minor editorial or document structure change N Minor editorial or document structure change N PUBLICATION AFFECTED Minor editorial or document structure change N Minor editorial or document structure change N INTERCHANGEABILITY/MIXABILITY Minor editorial or document structure change N SPARES Minor editorial or document structure change N MATERIAL INFORMATION MATERIAL - PRICE AND AVAILABILITY Minor editorial or document structure change N Procurement Addresses Minor editorial or document structure change N Price and Availability Minor editorial or document structure change N INDUSTRY SUPPORT INFORMATION Minor editorial or document structure change N LIST OF COMPONENTS Minor editorial or document structure change N Kit 282148A01R00 Minor editorial or document structure change N Kit 282148D01R00 Minor editorial or document structure change N Kit 282148D02R01 Minor editorial or document structure change N Kit 282148D03R01 Minor editorial or document structure change N Kit 282148D05R01 Minor editorial or document structure change N Kit 282148D06R01 Minor editorial or document structure change N Kit 282148D07R00 Minor editorial or document structure change N Kit 282148D08R00 Minor editorial or document structure change N Kit 282148B01R00 Minor editorial or document structure change N LIST OF MATERIALS - OPERATOR SUPPLIED Minor editorial or document structure change N Consumable Materials Minor editorial or document structure change N Consumable CMLD01 Minor editorial or document structure change N Consumable CMLB01 Minor editorial or document structure change N Components Minor editorial or document structure change N Equipment Minor editorial or document structure change N PARTS TO BE RE-IDENTIFIED BY OPERATOR Minor editorial or document structure change N TOOLING Minor editorial or document structure change N ACCOMPLISHMENT INSTRUCTIONS TASK 282148- 831-848-001- MODIFICATION Minor editorial or document structure change N Task associated data - 001 Minor editorial or document structure change N
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 4 6

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# @A310 SERVICE BULLETIN REVISION TRANSMITTAL SHEET
Task associated data - 002 Minor editorial or document structure change N Task associated data - 003 Minor editorial or document structure change N Task associated data - 004 Minor editorial or document structure change N Task associated data - 005 Minor editorial or document structure change N Task associated data - 006 Minor editorial or document structure change N Task associated data - 007 Minor editorial or document structure change N Task associated data - 008 Minor editorial or document structure change N Subtask 282148-910-401-001 Minor editorial or document structure change N Subtask 282148-910-204-001 Minor editorial or document structure change N Subtask 282148-900-202-001 Minor editorial or document structure change N Subtask 282148-910-401-001 Minor editorial or document structure change N Subtask 282148-910-204-001 Minor editorial or document structure change N Subtask 282148-900-202-001 Minor editorial or document structure change N Subtask 282148-910-401-001 Minor editorial or document structure change N Subtask 282148-910-204-001 Minor editorial or document structure change N Subtask 282148-900-202-001 Minor editorial or document structure change N Subtask 282148-910-401-001 Minor editorial or document structure change N Subtask 282148-910-204-001 Minor editorial or document structure change N Subtask 282148-900-202-001 Minor editorial or document structure change N Subtask 282148-910-401-001 Minor editorial or document structure change N Subtask 282148-910-204-001 Minor editorial or document structure change N Subtask 282148-900-202-001 Minor editorial or document structure change N Subtask 282148-910-401-001 Minor editorial or document structure change N Subtask 282148-910-204-001 Minor editorial or document structure change N Subtask 282148-900-202-001 Minor editorial or document structure change N Subtask 282148-910-401-001 Minor editorial or document structure change N Subtask 282148-910-204-001 Minor editorial or document structure change N Subtask 282148-900-202-001 Minor editorial or document structure change N Subtask 282148-910-401-001 Minor editorial or document structure change N Subtask 282148-910-204-001 Minor editorial or document structure change N Subtask 282148-900-202-001 Minor editorial or document structure change N Subtask 282148-941-001-001 Minor editorial or document structure change N Subtask 282148-862-001-001 Minor editorial or document structure change N Subtask 282148-941-001-001 Minor editorial or document structure change N Subtask 282148-862-001-001 Minor editorial or document structure change N Subtask 282148-941-001-001 Minor editorial or document structure change N Subtask 282148-862-001-001 Minor editorial or document structure change N Subtask 282148-941-001-001 Minor editorial or document structure change N Subtask 282148-862-001-001 Minor editorial or document structure change N Subtask 282148-941-001-001 Minor editorial or document structure change N Subtask 282148-862-001-001 Minor editorial or document structure change N
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 5 6

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# @A310 SERVICE BULLETIN REVISION TRANSMITTAL SHEET
Subtask 282148-941-001-001 Minor editorial or document structure change N Subtask 282148-862-001-001 Minor editorial or document structure change N Subtask 282148-941-001-001 Minor editorial or document structure change N Subtask 282148-862-001-001 Minor editorial or document structure change N Subtask 282148-941-001-001 Minor editorial or document structure change N Subtask 282148-862-001-001 Minor editorial or document structure change N Subtask 282148-831-405-001 Minor editorial or document structure change N Subtask 282148-831-004-001 Minor editorial or document structure change N Subtask 282148-831-005-001 Minor editorial or document structure change N Subtask 282148-831-006-001 Minor editorial or document structure change N Subtask 282148-831-208-001 Minor editorial or document structure change N Subtask 282148-831-209-001 Minor editorial or document structure change N Subtask 282148-831-210-001 Minor editorial or document structure change N Subtask 282148-831-211-001 Minor editorial or document structure change N Subtask 282148-831-405-001 Minor editorial or document structure change N Subtask 282148-831-004-001 Minor editorial or document structure change N Subtask 282148-831-005-001 Minor editorial or document structure change N Subtask 282148-831-006-001 Minor editorial or document structure change N Subtask 282148-831-208-002 Minor editorial or document structure change N Subtask 282148-831-209-002 Minor editorial or document structure change N Subtask 282148-831-210-002 Minor editorial or document structure change N Subtask 282148-831-211-002 Minor editorial or document structure change N Subtask 282148-831-405-001 Minor editorial or document structure change N Subtask 282148-831-004-001 Minor editorial or document structure change N Subtask 282148-831-005-001 Minor editorial or document structure change N Subtask 282148-831-006-001 Minor editorial or document structure change N Subtask 282148-831-208-003 Minor editorial or document structure change N Subtask 282148-831-209-003 Minor editorial or document structure change N Subtask 282148-831-210-003 Minor editorial or document structure change N Subtask 282148-831-211-003 Minor editorial or document structure change N Subtask 282148-831-405-001 Minor editorial or document structure change N Subtask 282148-831-004-001 Minor editorial or document structure change N Subtask 282148-831-005-001 Minor editorial or document structure change N Subtask 282148-831-006-001 Minor editorial or document structure change N Subtask 282148-831-208-004 Minor editorial or document structure change N Subtask 282148-831-209-004 Minor editorial or document structure change N Subtask 282148-831-210-004 Minor editorial or document structure change N Subtask 282148-831-211-004 Minor editorial or document structure change N Subtask 282148-831-405-001 Minor editorial or document structure change N Subtask 282148-831-004-001 Minor editorial or document structure change N Subtask 282148-831-005-001 Minor editorial or document structure change N
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 6 6

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# @A310 SERVICE BULLETIN REVISION TRANSMITTAL SHEET
Subtask 282148-831-006-002 Minor editorial or document structure change N Subtask 282148-831-208-001 Minor editorial or document structure change N Subtask 282148-831-209-001 Minor editorial or document structure change N Subtask 282148-831-210-001 Minor editorial or document structure change N Subtask 282148-831-211-001 Minor editorial or document structure change N Subtask 282148-831-405-001 Minor editorial or document structure change N Subtask 282148-831-004-001 Minor editorial or document structure change N Subtask 282148-831-005-001 Minor editorial or document structure change N Subtask 282148-831-006-002 Minor editorial or document structure change N Subtask 282148-831-208-002 Minor editorial or document structure change N Subtask 282148-831-209-002 Minor editorial or document structure change N Subtask 282148-831-210-002 Minor editorial or document structure change N Subtask 282148-831-211-002 Minor editorial or document structure change N Subtask 282148-831-405-001 Minor editorial or document structure change N Subtask 282148-831-004-001 Minor editorial or document structure change N Subtask 282148-831-005-001 Minor editorial or document structure change N Subtask 282148-831-006-002 Minor editorial or document structure change N Subtask 282148-831-208-003 Minor editorial or document structure change N Subtask 282148-831-209-003 Minor editorial or document structure change N Subtask 282148-831-210-003 Minor editorial or document structure change N Subtask 282148-831-211-003 Minor editorial or document structure change N Subtask 282148-831-405-001 Minor editorial or document structure change N Subtask 282148-831-004-001 Minor editorial or document structure change N Subtask 282148-831-005-001 Minor editorial or document structure change N Subtask 282148-831-006-002 Minor editorial or document structure change N Subtask 282148-831-208-004 Minor editorial or document structure change N Subtask 282148-831-209-004 Minor editorial or document structure change N Subtask 282148-831-210-004 Minor editorial or document structure change N Subtask 282148-831-211-004 Minor editorial or document structure change N Subtask 282148-710-201-001 Minor editorial or document structure change N Subtask 282148-710-201-001 Minor editorial or document structure change N Subtask 282148-710-201-001 Minor editorial or document structure change N Subtask 282148-710-201-001 Minor editorial or document structure change N Subtask 282148-710-201-001 Minor editorial or document structure change N Subtask 282148-710-201-001 Minor editorial or document structure change N Subtask 282148-710-201-001 Minor editorial or document structure change N Subtask 282148-710-201-001 Minor editorial or document structure change N Subtask 282148-861-002-001 Minor editorial or document structure change N Subtask 282148-942-009-001 Minor editorial or document structure change N Subtask 282148-861-002-001 Minor editorial or document structure change N Subtask 282148-942-009-001 Minor editorial or document structure change N
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 7 6

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# @A310 SERVICE BULLETIN REVISION TRANSMITTAL SHEET
Subtask 282148-861-002-001 Minor editorial or document structure change N Subtask 282148-942-009-001 Minor editorial or document structure change N Subtask 282148-861-002-001 Minor editorial or document structure change N Subtask 282148-942-009-001 Minor editorial or document structure change N Subtask 282148-861-002-001 Minor editorial or document structure change N Subtask 282148-942-009-001 Minor editorial or document structure change N Subtask 282148-861-002-001 Minor editorial or document structure change N Subtask 282148-942-009-001 Minor editorial or document structure change N Subtask 282148-861-002-001 Minor editorial or document structure change N Subtask 282148-942-009-001 Minor editorial or document structure change N Subtask 282148-861-002-001 Minor editorial or document structure change N Subtask 282148-942-009-001 Minor editorial or document structure change N TASK 282148- 831-853-001-Modification - ADDITIONAL WORK 1 (Introduced at Rev 02) Minor editorial or document structure change N

Task associated data - 001 Minor editorial or document structure change N Task associated data - 002 Minor editorial or document structure change N Task associated data - 003 Minor editorial or document structure change N Task associated data - 004 Minor editorial or document structure change N Task associated data - 005 Minor editorial or document structure change N Task associated data - 006 Minor editorial or document structure change N Task associated data - 007 Minor editorial or document structure change N Task associated data - 008 Minor editorial or document structure change N Subtask 282148-910-205-001 Minor editorial or document structure change N Subtask 282148-839-203-001 Minor editorial or document structure change N Subtask 282148-910-205-001 Minor editorial or document structure change N Subtask 282148-839-203-001 Minor editorial or document structure change N Subtask 282148-910-205-001 Minor editorial or document structure change N Subtask 282148-839-203-001 Minor editorial or document structure change N Subtask 282148-910-205-001 Minor editorial or document structure change N Subtask 282148-839-203-001 Minor editorial or document structure change N Subtask 282148-941-205-001 Minor editorial or document structure change N Subtask 282148-941-205-001 Minor editorial or document structure change N Subtask 282148-941-205-001 Minor editorial or document structure change N Subtask 282148-941-205-001 Minor editorial or document structure change N Subtask 282148-831-256-001 Minor editorial or document structure change N Subtask 282148-831-256-002 Minor editorial or document structure change N Subtask 282148-831-256-001 Minor editorial or document structure change N Subtask 282148-831-256-002 Minor editorial or document structure change N Subtask 282148-700-202-001 Minor editorial or document structure change N Subtask 282148-700-202-001 Minor editorial or document structure change N
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 8 6

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# @A310 SERVICE BULLETIN REVISION TRANSMITTAL SHEET
Subtask 282148-700-202-001 Minor editorial or document structure change N Subtask 282148-700-202-001 Minor editorial or document structure change N Subtask 282148-942-204-001 Minor editorial or document structure change N Subtask 282148-942-204-001 Minor editorial or document structure change N Subtask 282148-942-204-001 Minor editorial or document structure change N Subtask 282148-942-204-001 Minor editorial or document structure change N TASK 282148- 831-849-001-Modification - ADDITIONAL WORK 2 (Introduced at Rev 03) Minor editorial or document structure change N

Task associated data - 001 Minor editorial or document structure change N Task associated data - 002 Minor editorial or document structure change N Task associated data - 003 Minor editorial or document structure change N Task associated data - 004 Minor editorial or document structure change N Task associated data - 005 Minor editorial or document structure change N Task associated data - 006 Minor editorial or document structure change N Task associated data - 007 Minor editorial or document structure change N Task associated data - 008 Minor editorial or document structure change N Subtask 282148-839-401-001 Minor editorial or document structure change N Subtask 282148-910-206-001 Minor editorial or document structure change N Subtask 282148-839-401-001 Minor editorial or document structure change N Subtask 282148-910-206-001 Minor editorial or document structure change N Subtask 282148-839-401-001 Minor editorial or document structure change N Subtask 282148-839-401-001 Minor editorial or document structure change N Subtask 282148-839-401-001 Minor editorial or document structure change N Subtask 282148-910-206-001 Minor editorial or document structure change N Subtask 282148-839-401-001 Minor editorial or document structure change N Subtask 282148-910-206-001 Minor editorial or document structure change N Subtask 282148-839-401-001 Minor editorial or document structure change N Subtask 282148-839-401-001 Minor editorial or document structure change N Subtask 282148-941-402-001 Minor editorial or document structure change N Subtask 282148-941-402-001 Minor editorial or document structure change N Subtask 282148-941-402-001 Minor editorial or document structure change N Subtask 282148-941-402-001 Minor editorial or document structure change N Subtask 282148-831-402-001 Minor editorial or document structure change N Subtask 282148-831-402-001 Minor editorial or document structure change N Subtask 282148-831-402-001 Minor editorial or document structure change N Subtask 282148-831-402-001 Minor editorial or document structure change N Subtask 282148-942-402-001 Minor editorial or document structure change N Subtask 282148-942-402-001 Minor editorial or document structure change N Subtask 282148-942-402-001 Minor editorial or document structure change N Subtask 282148-942-402-001 Minor editorial or document structure change N
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 9 6

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# @A310 SERVICE BULLETIN REVISION TRANSMITTAL SHEET
TASK 282148- 831-850-001-Modification - ADDITIONAL WORK 3 (Introduced at Rev 06) Minor editorial or document structure change N

Task associated data - 001 Minor editorial or document structure change N Task associated data - 002 Minor editorial or document structure change N Task associated data - 003 Minor editorial or document structure change N Task associated data - 004 Minor editorial or document structure change N Task associated data - 005 Minor editorial or document structure change N Task associated data - 006 Minor editorial or document structure change N Task associated data - 007 Minor editorial or document structure change N Task associated data - 008 Minor editorial or document structure change N Subtask 282148-910-203-001 Minor editorial or document structure change N Subtask 282148-839-201-001 Minor editorial or document structure change N Subtask 282148-910-203-001 Minor editorial or document structure change N Subtask 282148-839-201-001 Minor editorial or document structure change N Subtask 282148-910-203-001 Minor editorial or document structure change N Subtask 282148-839-201-001 Minor editorial or document structure change N Subtask 282148-910-203-001 Minor editorial or document structure change N Subtask 282148-839-201-001 Minor editorial or document structure change N Subtask 282148-941-203-001 Minor editorial or document structure change N Subtask 282148-941-203-001 Minor editorial or document structure change N Subtask 282148-941-203-001 Minor editorial or document structure change N Subtask 282148-941-203-001 Minor editorial or document structure change N Subtask 282148-831-253-001 Minor editorial or document structure change N Subtask 282148-831-253-003 Minor editorial or document structure change N Subtask 282148-831-253-001 Minor editorial or document structure change N Subtask 282148-831-253-003 Minor editorial or document structure change N Subtask 282148-942-202-001 Minor editorial or document structure change N Subtask 282148-942-202-001 Minor editorial or document structure change N Subtask 282148-942-202-001 Minor editorial or document structure change N Subtask 282148-942-202-001 Minor editorial or document structure change N Fig. A-GBEAA Minor editorial or document structure change N Fig. A-GBEAA Sheet 01 Minor editorial or document structure change N Fig. A-GBEAA Sheet 02 Minor editorial or document structure change N Fig. A-GBEAA Sheet 03 Minor editorial or document structure change N Fig. A-GBEAA Sheet 04 Minor editorial or document structure change N Fig. A-GBEAA Sheet 05 Minor editorial or document structure change N Fig. A-GBEAA Sheet 06 Minor editorial or document structure change N Fig. A-GBEAA Sheet 07 Minor editorial or document structure change N Fig. A-GBEAA Sheet 08 Minor editorial or document structure change N Fig. A-GBFAA Minor editorial or document structure change N
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 10 6

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# @A310 SERVICE BULLETIN REVISION TRANSMITTAL SHEET Fig. A-GBFAA Sheet 01 Minor editorial or document structure change N Fig. A-GBFAA Sheet 02 Minor editorial or document structure change N Fig. A-GBFAA Sheet 03 Minor editorial or document structure change N Fig. A-GBFAA Sheet 04 Minor editorial or document structure change N Fig. A-GBFAA Sheet 05 Minor editorial or document structure change N Fig. A-GBFAA Sheet 06 Minor editorial or document structure change N Fig. A-GBFAA Sheet 07 Minor editorial or document structure change N Fig. A-GBFAA Sheet 08 Minor editorial or document structure change N Fig. A-GBFAA Sheet 09 Minor editorial or document structure change N Fig. A-GBFAA Sheet 10 Minor editorial or document structure change N Fig. A-GBGAA Minor editorial or document structure change N Fig. A-GBGAA Sheet 01 Minor editorial or document structure change N Fig. A-GBGAA Sheet 02 Minor editorial or document structure change N Fig. A-GBGAA Sheet 03 Minor editorial or document structure change N Fig. A-GBGAA Sheet 04 Minor editorial or document structure change N Fig. A-GBGAA Sheet 05 Minor editorial or document structure change N Fig. A-GBGAA Sheet 06 Minor editorial or document structure change N Fig. A-GBGAA Sheet 07 Minor editorial or document structure change N Fig. A-GBGAA Sheet 08 Minor editorial or document structure change N Fig. A-GBHAA Minor editorial or document structure change N Fig. A-GBHAA Sheet 01 Minor editorial or document structure change N Fig. A-GBHAA Sheet 02 Minor editorial or document structure change N Fig. A-GBHAA Sheet 03 Minor editorial or document structure change N Fig. A-GBHAA Sheet 04 Minor editorial or document structure change N Fig. A-GBHAA Sheet 05 Minor editorial or document structure change N Fig. A-GBHAA Sheet 06 Minor editorial or document structure change N Fig. A-GBHAA Sheet 07 Minor editorial or document structure change N Fig. A-GBHAA Sheet 08 Minor editorial or document structure change N Fig. A-GBJAA Minor editorial or document structure change N Fig. A-GBJAA Sheet 01 Minor editorial or document structure change N Fig. A-GBJAA Sheet 02 Minor editorial or document structure change N Fig. A-GBJAA Sheet 03 Minor editorial or document structure change N Fig. A-GBJAA Sheet 04 Minor editorial or document structure change N Fig. A-GBJAA Sheet 05 Minor editorial or document structure change N Fig. A-GBJAA Sheet 06 Minor editorial or document structure change N Fig. A-GBJAA Sheet 07 Minor editorial or document structure change N Fig. A-GBJAA Sheet 08 Minor editorial or document structure change N Fig. A-GBJAA Sheet 09 Minor editorial or document structure change N Fig. A-GBKAA Minor editorial or document structure change N Fig. A-GBKAA Sheet 01 Minor editorial or document structure change N Fig. A-GBKAA Sheet 02 Minor editorial or document structure change N
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 11 6

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# @A310 SERVICE BULLETIN REVISION TRANSMITTAL SHEET Fig. A-GBKAA Sheet 03 Minor editorial or document structure change N Fig. A-GBKAA Sheet 04 Minor editorial or document structure change N Fig. A-GBKAA Sheet 05 Minor editorial or document structure change N Fig. A-GBKAA Sheet 06 Minor editorial or document structure change N Fig. A-GBKAA Sheet 07 Minor editorial or document structure change N Fig. A-GBKAA Sheet 08 Minor editorial or document structure change N Fig. A-GBKAA Sheet 09 Minor editorial or document structure change N Fig. A-GHAAA Minor editorial or document structure change N Fig. A-GHAAA Sheet 01 Minor editorial or document structure change N Fig. A-GHBAA Minor editorial or document structure change N Fig. A-GHBAA Sheet 01 Minor editorial or document structure change N Fig. A-FCAAA Minor editorial or document structure change N Fig. A-FCAAA Sheet 01 Minor editorial or document structure change N Fig. A-FCBAA Minor editorial or document structure change N Fig. A-FCBAA Sheet 01 Minor editorial or document structure change N Fig. A-FCCAA Minor editorial or document structure change N Fig. A-FCCAA Sheet 01 Minor editorial or document structure change N Fig. A-FCCAB Minor editorial or document structure change N Fig. A-FCCAB Sheet 01 Minor editorial or document structure change N Fig. A-FWAAA Minor editorial or document structure change N Fig. A-FWAAA Sheet 01 Minor editorial or document structure change N Fig. A-UBAAA Minor editorial or document structure change N Fig. A-UBAAA Sheet 01 Minor editorial or document structure change N Fig. A-GBLAA Minor editorial or document structure change N Fig. A-GBLAA Sheet 01 Minor editorial or document structure change N Fig. A-GBLAA Sheet 02 Minor editorial or document structure change N Fig. A-GBLAA Sheet 03 Minor editorial or document structure change N Fig. A-GBMAA Minor editorial or document structure change N Fig. A-GBMAA Sheet 01 Minor editorial or document structure change N Fig. A-GBMAA Sheet 02 Minor editorial or document structure change N Fig. A-GBMAA Sheet 03 Minor editorial or document structure change N Fig. A-GBMAA Sheet 04 Minor editorial or document structure change N Fig. A-GBMAA Sheet 05 Minor editorial or document structure change N Fig. A-GBMAA Sheet 06 Minor editorial or document structure change N Fig. A-GBMAA Sheet 07 Minor editorial or document structure change N Fig. A-GBMAA Sheet 08 Minor editorial or document structure change N Fig. A-UBCAA Minor editorial or document structure change N Fig. A-UBCAA Sheet 01 Minor editorial or document structure change N Fig. A-GBNAA Minor editorial or document structure change N Fig. A-GBNAA Sheet 01 Minor editorial or document structure change N Fig. A-GBNAA Sheet 02 Minor editorial or document structure change N
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 12 6

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# @A310 SERVICE BULLETIN REVISION TRANSMITTAL SHEET Fig. A-GBNAA Sheet 03 Minor editorial or document structure change N Fig. A-GBNAA Sheet 04 Minor editorial or document structure change N Fig. A-GBNAA Sheet 05 Minor editorial or document structure change N Fig. A-GBNAA Sheet 06 Minor editorial or document structure change N Fig. A-GBNAA Sheet 07 Minor editorial or document structure change N Fig. A-GBNAA Sheet 08 Minor editorial or document structure change N Fig. A-GBPAA Minor editorial or document structure change N Fig. A-GBPAA Sheet 01 Minor editorial or document structure change N Fig. A-GBPAB Minor editorial or document structure change N Fig. A-GBPAB Sheet 01 Minor editorial or document structure change N FILLING INSTRUCTIONS This Service Bulletin has been generated electronically and is reissued as a complete document. Replace the complete document. Put this Revision Transmittal Sheet in front of the Service Bulletin. HISTORY OF PREVIOUS REVISIONS Revision No. 01 was issued to extend the effectivity and to add the applicable Kit A01 at the end of the MSN list. Revision No. 02 was issued to add the route 2S segregation in the RH pylon area and at the cadensicon sensor 10QT, add Config. 01 for aircraft having Service Bulletin No. A310-28-2140 accomplished, add Config. 02 for aircraft having Service Bulletin No. A310-28-2140 not accomplished, add ADDITIONAL WORK for Config. 01 and Config. 02, revise the manhours and to remove aircraft MSN 0276, 0285, 0295, 0306, 0311, 0340, 0347, 0350, 0352, 0363, 0404, 0409, 0412, 0432, 0433, 0435, 0440, 0442, 0443, 0493, 0504 and 0570 from the effectivity. This Revision 03 was issued to add Mod 13478D23233, add Kit B01, add Workstep for ADDITIONAL WORK 2, remove aircraft MSNs 0172, 0300, 0451, 0453, 0501, 0540, 0548, 0589, 0598, 0634, 0690 and 0695 from the effectivity and update the operators, add figure 4 and revise figures 5 thru 13 to the new standard and to introduce minor changes. This Revision 04 was issued to incorporate the pre and post Service Bulletin A310-36-2015 (MOD. No. 7633S7885) configuration with Config. 03 and 04, and to delete the aircraft MSN 0254, 0273, 0397 and 400 from the effectivity. Revision No. 05 was issued to remove MSN 0349 from the effectivity and add MSN’s 0254, 0273, 0397 and 0400 to the effectivity. REVISION SEQUENCE ORIGINAL: Jan 23/02 REVISION No.: 02 - Mar 09/07 REVISION No.: 03 - Jun 02/09
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 13 6

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# @A310 SERVICE BULLETIN REVISION TRANSMITTAL SHEET REVISION No.: 04 - Apr 14/10 REVISION No.: 05 - Aug 03/10 REVISION No. : 06 - Aug 31/11

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 14 6

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# @A310 SERVICE BULLETIN SUMMARY AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Tel : (33) 5 61 93 33 33 Telex : AIRBU 530526F Fax : (33) 5 61 93 42 51 This summary is for information only and is not approved for modification of the aircraft. 

# MANDATORY MANDATORY MANDATORY
ATA SYSTEM: 28 

### TITLE: ELECTRIC/ELECTRONIC COMMON INSTALLATION - WING - IMPROVE THE 2S-ROUTE IN THE RH-WING **CONF ALL MODIFICATIONS MODIFICATION CLASSIFICATION MAJOR 13478D23233 MINOR 12427D21883 12435S22116 NOTE: As per EASA IR 21, a minor change is one that has no appreciable effect on the mass, balance, structural strength, reliability, operational characteristics affecting the airworthiness of the product. All other changes are major changes. REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES An analysis of the wire routing under the fuel system safety program has shown that the route 2S of circuit QT in the RH-wing has to be modified to allow a better segregation between fuel quantity indication wires and the 115V wires of the route 2S. This Service Bulletin details the procedure to segregate the wires in the RH-wing by installation of sleeves for the complete route 2S in the RH electronics rack 90VU, the FWD cargo compartment, the RH forward wing root and krueger flap and in zones 612 and 623 of the wing. The accomplishment of this modification will ensure the proper segregation of the fuel quantity indication wires and the 115V wires in order to avoid interaction in the case of wire damage. GENERAL EVALUATION EVALUATION TABLE COMPLIANCE MANDATORY (1) CANCELS INSPECTION SB NO POTENTIAL AD YES A/C OPERATION AFFECTED NO RELIABILITY AFFECTED NO PAX COMFORT AFFECTED NO COST SAVING NO ETOPS AFFECTED NO STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED NO KIT PRICE (USD) See SB
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 1 6

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# @A310 SERVICE BULLETIN SUMMARY NOTE (1) : Service Bulletin must be accomplished. MATERIAL PRICE INFORMATION **CONF 001 MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Kit 282148A01R00 1 1,100.00 Sleeve, Tie Kit 282148B01R00 1 90.00 Bracket, Rivet Kit 282148D01R00 1 2,210.00 Clamp, Washer, Insulator, Screw, Spacer, Cord , Tie Kit 282148D02R01 1 1,580.00 Clamp, Washer, Insulator, Screw, Spacer, Cord , Tie TOTAL 4,980.00 **CONF 002 MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Kit 282148A01R00 1 1,100.00 Sleeve, Tie Kit 282148B01R00 1 90.00 Bracket, Rivet Kit 282148D01R00 1 2,210.00 Clamp, Washer, Insulator, Screw, Spacer, Cord , Tie Kit 282148D03R01 1 1,530.00 Clamp, Washer, Insulator, Screw, Spacer, Cord , Tie TOTAL 4,930.00 **CONF 003 MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Kit 282148A01R00 1 1,100.00 Sleeve, Tie Kit 282148B01R00 1 90.00 Bracket, Rivet Kit 282148D01R00 1 2,210.00 Clamp, Washer, Insulator, Screw, Spacer, Cord , Tie Kit 282148D05R01 1 570.00 Clamp, Washer, Screw, Spacer Kit 282148D07R00 1 32.50 Clamp, Washer, Screw, Spacer TOTAL 4,002.50

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 2 6

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# @A310 SERVICE BULLETIN SUMMARY **CONF 004 MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Kit 282148A01R00 1 1,100.00 Sleeve, Tie Kit 282148B01R00 1 90.00 Bracket, Rivet Kit 282148D01R00 1 2,210.00 Clamp, Washer, Insulator, Screw, Spacer, Cord , Tie Kit 282148D06R01 1 560.00 Clamp, Washer, Screw, Spacer Kit 282148D08R00 1 33.20 Clamp, Washer, Screw, Spacer TOTAL 3,993.20 **CONF 005 MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Kit 282148A01R00 1 1,100.00 Sleeve, Tie Kit 282148B01R00 1 90.00 Bracket, Rivet Kit 282148D01R00 1 2,210.00 Clamp, Washer, Insulator, Screw, Spacer, Cord , Tie Kit 282148D02R01 1 1,580.00 Clamp, Washer, Insulator, Screw, Spacer, Cord , Tie TOTAL 4,980.00 **CONF 006 MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Kit 282148A01R00 1 1,100.00 Sleeve, Tie Kit 282148B01R00 1 90.00 Bracket, Rivet Kit 282148D01R00 1 2,210.00 Clamp, Washer, Insulator, Screw, Spacer, Cord , Tie Kit 282148D03R01 1 1,530.00 Clamp, Washer, Insulator, Screw, Spacer, Cord , Tie TOTAL 4,930.00 **CONF 007 MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Kit 282148A01R00 1 1,100.00 Sleeve, Tie Kit 282148B01R00 1 90.00 Bracket, Rivet
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 3 6

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

# @A310 SERVICE BULLETIN SUMMARY MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Kit 282148D01R00 1 2,210.00 Clamp, Washer, Insulator, Screw, Spacer, Cord , Tie Kit 282148D05R01 1 570.00 Clamp, Washer, Screw, Spacer Kit 282148D07R00 1 32.50 Clamp, Washer, Screw, Spacer TOTAL 4,002.50 **CONF 008 MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Kit 282148A01R00 1 1,100.00 Sleeve, Tie Kit 282148B01R00 1 90.00 Bracket, Rivet Kit 282148D01R00 1 2,210.00 Clamp, Washer, Insulator, Screw, Spacer, Cord , Tie Kit 282148D06R01 1 560.00 Clamp, Washer, Screw, Spacer Kit 282148D08R00 1 33.20 Clamp, Washer, Screw, Spacer TOTAL 3,993.20 EFFECTIVITY **CONF ALL This Service Bulletin is applicable to this (these) operator(s) :

18T 19U 46T 52X 58X 82Z 83V 85Z 98W 99Y AFG AIB AIC BAF BBC CFC DAH DEC DGA F2I FDX G8E GAF HFY IRA IRM IYE JAB JAV K1P KAC KZU MGL MWA PIA QAF R1T RJA ROT RZO SBI SGX SUD THY TSC UBD UZB WHT WTJ CONCURRENT REQUIREMENTS None REFERENCES / REPERCUSSIONS TFU None OEB None AOT None SIL None LINE MAINTENANCE AFFECTED No LIFE LIMIT None OTHER SBIT 11-0012 dated 15 March 2011

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 4 6

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# @A310 SERVICE BULLETIN SUMMARY NATURE OF THE WORK AIRCRAFT YES EQUIPMENT NO HARD NO SOFT NO OBRM NO MANPOWER **CONF 001 Task 282148-831-848-001: MODIFICATION TOTAL MANHOURS 40.00 ELAPSED TIME (HOURS) 14.00 Task 282148-831-853-001: Modification - ADDITIONAL WORK 1 (Introduced at Rev 02) TOTAL MANHOURS 23.00 ELAPSED TIME (HOURS) 13.00 Task 282148-831-849-001: Modification - ADDITIONAL WORK 2 (Introduced at Rev 03) TOTAL MANHOURS 3.00 ELAPSED TIME (HOURS) 3.00 Task 282148-831-850-001: Modification - ADDITIONAL WORK 3 (Introduced at Rev 06) TOTAL MANHOURS 0.00 ELAPSED TIME (HOURS) 0.00 **CONF 002 Task 282148-831-848-001: MODIFICATION TOTAL MANHOURS 32.00 ELAPSED TIME (HOURS) 14.00 Task 282148-831-853-001: Modification - ADDITIONAL WORK 1 (Introduced at Rev 02) TOTAL MANHOURS 23.00 ELAPSED TIME (HOURS) 13.00 Task 282148-831-849-001: Modification - ADDITIONAL WORK 2 (Introduced at Rev 03) TOTAL MANHOURS 3.00 ELAPSED TIME (HOURS) 3.00 Task 282148-831-850-001: Modification - ADDITIONAL WORK 3 (Introduced at Rev 06) TOTAL MANHOURS 0.00 ELAPSED TIME (HOURS) 0.00

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 5 6

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# @A310 SERVICE BULLETIN SUMMARY **CONF 003 Task 282148-831-848-001: MODIFICATION TOTAL MANHOURS 32.00 ELAPSED TIME (HOURS) 14.00 Task 282148-831-853-001: Modification - ADDITIONAL WORK 1 (Introduced at Rev 02) TOTAL MANHOURS 0.00 ELAPSED TIME (HOURS) 0.00 Task 282148-831-849-001: Modification - ADDITIONAL WORK 2 (Introduced at Rev 03) TOTAL MANHOURS 0.00 ELAPSED TIME (HOURS) 0.00 Task 282148-831-850-001: Modification - ADDITIONAL WORK 3 (Introduced at Rev 06) TOTAL MANHOURS 3.00 ELAPSED TIME (HOURS) 3.00 **CONF 004 Task 282148-831-848-001: MODIFICATION TOTAL MANHOURS 32.00 ELAPSED TIME (HOURS) 14.00 Task 282148-831-853-001: Modification - ADDITIONAL WORK 1 (Introduced at Rev 02) TOTAL MANHOURS 0.00 ELAPSED TIME (HOURS) 0.00 Task 282148-831-849-001: Modification - ADDITIONAL WORK 2 (Introduced at Rev 03) TOTAL MANHOURS 0.00 ELAPSED TIME (HOURS) 0.00 Task 282148-831-850-001: Modification - ADDITIONAL WORK 3 (Introduced at Rev 06) TOTAL MANHOURS 3.00 ELAPSED TIME (HOURS) 3.00 **CONF 005 Task 282148-831-848-001: MODIFICATION TOTAL MANHOURS 40.00 ELAPSED TIME (HOURS) 14.00 Task 282148-831-853-001: Modification - ADDITIONAL WORK 1 (Introduced at Rev 02) TOTAL MANHOURS 23.00 ELAPSED TIME (HOURS) 13.00

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 6 6

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# @A310 SERVICE BULLETIN SUMMARY Task 282148-831-849-001: Modification - ADDITIONAL WORK 2 (Introduced at Rev 03) TOTAL MANHOURS 3.00 ELAPSED TIME (HOURS) 3.00 Task 282148-831-850-001: Modification - ADDITIONAL WORK 3 (Introduced at Rev 06) TOTAL MANHOURS 0.00 ELAPSED TIME (HOURS) 0.00 **CONF 006 Task 282148-831-848-001: MODIFICATION TOTAL MANHOURS 32.00 ELAPSED TIME (HOURS) 14.00 Task 282148-831-853-001: Modification - ADDITIONAL WORK 1 (Introduced at Rev 02) TOTAL MANHOURS 23.00 ELAPSED TIME (HOURS) 13.00 Task 282148-831-849-001: Modification - ADDITIONAL WORK 2 (Introduced at Rev 03) TOTAL MANHOURS 3.00 ELAPSED TIME (HOURS) 3.00 Task 282148-831-850-001: Modification - ADDITIONAL WORK 3 (Introduced at Rev 06) TOTAL MANHOURS 0.00 ELAPSED TIME (HOURS) 0.00 **CONF 007 Task 282148-831-848-001: MODIFICATION TOTAL MANHOURS 32.00 ELAPSED TIME (HOURS) 14.00 Task 282148-831-853-001: Modification - ADDITIONAL WORK 1 (Introduced at Rev 02) TOTAL MANHOURS 0.00 ELAPSED TIME (HOURS) 0.00 Task 282148-831-849-001: Modification - ADDITIONAL WORK 2 (Introduced at Rev 03) TOTAL MANHOURS 0.00 ELAPSED TIME (HOURS) 0.00 Task 282148-831-850-001: Modification - ADDITIONAL WORK 3 (Introduced at Rev 06) TOTAL MANHOURS 3.00 ELAPSED TIME (HOURS) 3.00

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 7 6

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# @A310 SERVICE BULLETIN SUMMARY **CONF 008 Task 282148-831-848-001: MODIFICATION TOTAL MANHOURS 32.00 ELAPSED TIME (HOURS) 14.00 Task 282148-831-853-001: Modification - ADDITIONAL WORK 1 (Introduced at Rev 02) TOTAL MANHOURS 0.00 ELAPSED TIME (HOURS) 0.00 Task 282148-831-849-001: Modification - ADDITIONAL WORK 2 (Introduced at Rev 03) TOTAL MANHOURS 0.00 ELAPSED TIME (HOURS) 0.00 Task 282148-831-850-001: Modification - ADDITIONAL WORK 3 (Introduced at Rev 06) TOTAL MANHOURS 3.00 ELAPSED TIME (HOURS) 3.00 APPENDICES **CONF ALL None

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 8 6

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# @A310 SERVICE BULLETIN SUMMARY

**CONF ALL

TO

2S

2S

INSTALLATION OF CABLE SLEEVES IN THE INSTALLATION OF CABLE SLEEVES IN THE INSTALLATION OF CABLE SLEEVES IN THE RH ELECTRONICS RACK 90VU (KIT A01)

RH FORWARD WING ROOT AND KRUEGER FLAP (KIT A01) FWD CARGO COMPARTMENT (KIT A01) **NOTE:** FR39 FR40 FR38.1 FR38.2 FR39 FR40 15QTB 2354VC Z140

Z120 Z612 Z623 

### B

**C A**  **F D**  **E** FR20



## A

**B C** 

B_SB_282148_6_SAAA_01_00 

### G

Figure A-GSAAA - Sheet 01

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 9 6

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# @A310 SERVICE BULLETIN SUMMARY

**CONF ALL

PYLON

FRONT SPAR 3R/1S TRACK 1 SCREW JACK 1

SCREW JACK 2 TRACK 3

INSTALLATION OF CABLE SLEEVES IN THE RH−WING FORWARD OF THE FRONT SPAR (KIT D01) PYLON SCREW JACK 3

1M

1S MASTER TRACK 5

B_SB_282148_6_SAAA_02_00

RIB8 RIB7 RIB4 RIB3 RIB2

/2S 624VB 624VB /2S 624VB/2S

/2S 636VB 636VB/2M RIB9 RIB10 RIB11
RIB12 TRACK 4

**NOTE:** FRONT SPAR



## D

**E** 3R/1S

Figure A-GSAAA - Sheet 02

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 10 6

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# @A310 SERVICE BULLETIN SUMMARY

**CONF ALL



## F 40VC 5006VC

2S (QT) 2S 636VB

52VP 44VP

B_SB_282148_6_SAAA_03_00 52VP 5006VC 2S (QT) 2S

636VB 40VC

Figure A-GSAAA - Sheet 03

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 11 6

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# @A310 SERVICE BULLETIN SUMMARY

**CONF ALL

CENTERLINE PYLON D NOSE

SUB SPAR VIEW LOOKING FWD WOFZ 0.0 WDFX −53.0

WOFZ 0.0 WDFX −53.0 RIB8 RIB9



## AFTER **BEFORE**

SUB SPAR VIEW LOOKING FWD 

## G **H**

**J** RETRO−FIT BRACKET

ORIGINAL BRACKET



### H **J**

B_SB_282148_6_SAAA_04_00 Figure A-GSAAA - Sheet 04

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 12 6

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# @A310 SERVICE BULLETIN
AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Tel : (33) 5 61 93 33 33 Telex : AIRBU 530526F Fax : (33) 5 61 93 42 51



# MANDATORY MANDATORY MANDATORY
ATA SYSTEM: 28 

### TITLE: ELECTRIC/ELECTRONIC COMMON INSTALLATION - WING - IMPROVE THE 2S-ROUTE IN THE RH-WING MODIFICATION No.: 12427D21883 12435S22116 13478D23233 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 ADDITIONAL WORK 1: applicable to Configuration 001, 002, 005 and 006 is required for aircraft that have been modified by accomplishment of this Service Bulletin from the original issue up to revision 01. The work which follows is required: - segregation of the route 2S in RH pylon area - installation of an additional protection sleeve in the outer wing area near the cadensicon sensor 10QT. ADDITIONAL WORK 2: applicable to Configuration 001, 002, 005 and 006 is required for aircraft that have been modified by accomplishment of this Service Bulletin from the original issue up to revision 02. The work which follows is required: - installation of an modified bracket on the RH wing.

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 1 6

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# @A310 SERVICE BULLETIN ADDITIONAL WORK 3: applicable to Configuration 003, 004, 007 and 008 is required for aircraft that have been modified by accomplishment of this Service Bulletin from the original issue up to revision 03. The work which follows is required: - improvement of the 2S route in the RH wing pylon area. (1) Models 310-203 310-204 310-221 310-222 310-304 310-308 310-322 310-324 310-325 (2) Effectivity by MSN 0162 0191 0201 0217 0224 0230 0233 0237 0241 0245 0248 0251 0254 0257 0260 0264 0267 0273 0278 0281 0283 0288 0291 0293 0297 0303 0309 0313 0316 0318 0320 0326 0331 0333 0335 0338-0339 0342-0343 0345-0346 0353 0355-0357 0359-0360 0362 0364 0367 0369-0370 0372 0375 0378-0379 0389-0390 0392 0394 0397 0399-0400 0406-0407 0410 0413 0416 0418-0419 0421-0422 0425 0427-0429 0431 0434 0436-0437 0439 0441 0444-0449 0452 0454 0456-0458 0467 0472-0473 0475-0476 0478 0480-0485 0487-0492 0494-0500 0502-0503 0519-0520 0522-0524 0526-0527 0531 0534 0537-0539 0541-0542 0544-0545 0547 0549-0552 0562 0564-0565 0567-0568 0571 0573-0574 0576 0585-0588 0590-0595 0597 0599-0600 0620 0622 0624 0636 0638 0642 0644 0646-0654 0656 0658 0660-0661 0663 0665 0667 0669 0671-0672 0674 0676 0678 0680 0682 0684 0686-0687 0689 0691 0693 0697 0700 0702 0704 0706 (3) Effectivity by Operator The Operator/MSN relationship is provided for information only and is correct at the time of issue in accordance with the information available to AIRBUS. Any future changes resulting from transfer of an aircraft from one operator to another will not be reflected in this list unless the Service Bulletin is revised for another reason. OPERATOR MSN 18T 0473 19U 0399 46T 0413 52X 0410 58X 0431 82Z 0550 0551 83V 0427 85Z 0547 98W 0416 99Y 0489 AFG 0496 0497 AIB 0650 0674 0686 AIC 0392 0406 0407 0428 0429 0538 0544 0654 0665 0669 0680 BAF 0367 0372 BBC 0594 0642 0700
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 2 6

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# @A310 SERVICE BULLETIN

OPERATOR MSN CFC 0425 0441 0444 0446 0482 DAH 0291 0293 DEC 0684 0693 0697 DGA 0418 0421 0422 F2I 0309 0419 0487 FDX 0162 0191 0201 0217 0224 0230 0233 0237 0241 0245 0248 0251 0254 0257 0260 0264 0267 0273 0278 0281 0283 0288 0297 0303 0313 0316 0318 0326 0331 0333 0335 0339 0342 0343 0345 0346 0353 0355 0356 0359 0360 0362 0364 0369 0378 0394 0397 0400 0439 0449 0452 0454 0456 0457 0458 0467 0492 0500 0534 0539 0542 0549 0552 0593 0638 G8E 0475 GAF 0434 0484 0498 0499 0503 0522 0523 HFY 0495 0565 IRA 0338 0370 0375 0379 0389 0390 0436 0671 IRM 0488 0524 0537 0564 0567 0586 0595 0620 IYE 0568 0702 0704 JAB 0320 JAV 0357 0481 K1P 0648 KAC 0647 0649 0663 KZU 0592 0622 0646 MGL 0526 MWA 0652 PIA 0585 0587 0590 0653 0656 0660 0676 0678 0682 0687 0689 0691 QAF 0667 R1T 0591 RJA 0445 0490 0491 0531 ROT 0636 0644 RZO 0571 0624 0651 0661 SBI 0520 SGX 0519 0562 SUD 0437 THY 0476 0478 0480 0502 TSC 0447 0472 0483 0485 0527 0541 0545 0588 0597 0599 0600 0658 UBD 0672 UZB 0574 0576 0706 WHT 0448 0573 WTJ 0494 (4) Configuration by MSN MSN CONFIGURATION 0162 0191 0201 0217 0224 0241 0245 0248 0260 0267 0273 0278 0303 0309 0313 0318 0326 0331 0335 0353 0355 0356 0357 0362 0364 0369 0394 0399 0410 0437 0439 002 004

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 3 6

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# @A310 SERVICE BULLETIN

MSN CONFIGURATION 0230 0237 0254 0257 0288 0291 0293 0339 0342 0343 0345 0346 0359 0360 0379 0390 0397 0400 0419 001 002 003 004 0233 0320 0333 0338 0370 0375 0389 0392 0406 0407 0413 0416 0418 0421 0422 0425 0427 0428 0429 0441 003 004 0251 0264 0281 0283 0297 0316 0367 0372 0378 0431 0434 0436 004 0444 0445 0446 0447 0448 0472 0475 0476 0480 0481 0482 0487 0490 0491 0496 0497 0519 0520 0526 0531 0537 0538 0544 007 008
0449 0452 0457 0458 0473 0483 0484 0485 0488 0494 0495 0498 0499 0500 0502 0503 0522 0523 0527 0541 0545 0547 0550 0551 0562 0564 0565 0567 0568 0571 0573 0574 0576 0585 0586 0587 0588 0590 0592 0593 0595 0597 0599 0600 0620 0622 0624 0636 0638 0644 0646 0647 0648 0649 0651 0653 0654 0656 0658 0660 0661 0663 0665 0667 0671 0672 0674 0676 0678 0682 0684 0687 0689 0691 0693 0697 0700 0702 0704 0706 008

0454 0456 0467 0489 0492 0524 0534 0549 0552 0591 0594 0642 0650 0652 0669 0680 0686 006 008 0478 0539 0542 005 006 007 008 (5) Configuration definition **CONF 001 Config. 001 is valid for aircraft up to MSN 0442 and having Service Bulletin Nos. A310-28-2140 and A310-36-2015 accomplished or MOD. No. 7633S7885 embodied. **CONF 002 Config. 002 is valid for aircraft up to MSN 0442 and not having Service Bulletin No. A310-28-2140 accomplished but having Service Bulletin No. A310-36-2015 accomplished or MOD. No. 7633S7885 embodied. **CONF 003 Config. 003 is valid for aircraft up to MSN 0442 and having Service Bulletin A310-28-2140 accomplished but not having Service Bulletin No. A310-36-2015 accomplished or MOD. No. 7633S7885 not embodied. **CONF 004 Config. 004 is valid for aircraft up to MSN 0442 and not having Service Bulletin Nos. A310-28-2140 and A310-36-2015 accomplished or MOD. No. 7633S7885 not embodied. **CONF 005 Config. 005 is valid for aircraft MSN 0442 and subsequent and having Service Bulletin Nos. A310-28-2140 and A310-36-2015 accomplished or MOD. No. 7633S7885 embodied. **CONF 006 Config. 006 is valid for aircraft MSN 0442 and subsequent and not having Service Bulletin No. A310-28-2140 accomplished but having Service Bulletin No. A310-36-2015 accomplished or MOD. No. 7633S7885 embodied.

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 4 6

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# @A310 SERVICE BULLETIN
**CONF 007 Config. 007 is valid for aircraft MSN 0442 and subsequent and having Service Bulletin A310-28-2140 accomplished but not having Service Bulletin No. A310-36-2015 accomplished or MOD. No. 7633S7885 not embodied. **CONF 008 Config. 008 is valid for aircraft MSN 0442 and subsequent and not having Service Bulletin Nos. A310-28-2140 and A310-36-2015 accomplished or MOD. No. 7633S7885 not embodied. (6) Material Effectivity **CONF 001, 005 MATERIAL QTY PER A/C SEE NOTES Kit 282148A01R00 1 Consumable CMLB01 1 Consumable CMLD01 As required Kit 282148B01R00 1 Kit 282148D01R00 1 Kit 282148D02R01 1 **CONF 002, 006 MATERIAL QTY PER A/C SEE NOTES Kit 282148A01R00 1 Consumable CMLB01 1 Consumable CMLD01 As required Kit 282148B01R00 1 Kit 282148D01R00 1 Kit 282148D03R01 1 **CONF 003, 007 MATERIAL QTY PER A/C SEE NOTES Kit 282148A01R00 1 Consumable CMLB01 1 Consumable CMLD01 As required Kit 282148B01R00 1 Kit 282148D01R00 1 Kit 282148D05R01 1 Kit 282148D07R00 1 **CONF 004, 008 MATERIAL QTY PER A/C SEE NOTES Kit 282148A01R00 1 Consumable CMLB01 1 Consumable CMLD01 As required

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 5 6

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# @A310 SERVICE BULLETIN

MATERIAL QTY PER A/C SEE NOTES Kit 282148B01R00 1 Kit 282148D01R00 1 Kit 282148D06R01 1 Kit 282148D08R00 1 **CONF ALL B. CONCURRENT REQUIREMENTS None C. REASON (1) History An analysis of the wire routing under the fuel system safety program has shown that the route 2S of circuit QT in the RH-wing has to be modified to allow a better segregation between fuel quantity indication wires and the 115V wires of the route 2S. (2) Objective/Action This Service Bulletin details the procedure to segregate the wires in the RH-wing by installation of sleeves for the complete route 2S in the RH electronics rack 90VU, the FWD cargo compartment, the RH forward wing root and krueger flap and in zones 612 and 623 of the wing. (3) Advantages The accomplishment of this modification will ensure the proper segregation of the fuel quantity indication wires and the 115V wires in order to avoid interaction in the case of wire damage. (4) Operational/Maintenance Consequences None D. DESCRIPTION To accomplish this Service Bulletin it is necessary to : **CONF 001 Task 282148-831-848-001: MODIFICATION (1) Install a New Bracket on the Sub Spar Behind the Front Spar Between RIB 8 and RIB 9 on the RH Wing (2) Install cable sleeves in the RH Electronics Rack 90VU. (3) Install cable sleeves between FR38.2 and FR39, in the forward cargo compartment. (4) Install cable sleeves in the RH forward wing root and krueger flap. DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 6 6

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# @A310 SERVICE BULLETIN (5) Install the cable sleeves in the RH-wing forward of the front spar between rib 2 and rib 3 in zone 612. (6) Install the cable sleeves in the RH-wing forward of the front spar between rib 7 and rib 8 in zone 612. (7) Install the cable sleeves in the RH-wing forward of the front spar between rib 8 and rib 9 (pylon area) in zone 612. (8) Install the cable sleeves in the RH-wing forward of the front spar between rib 9 and rib 12 in zone 623. Task 282148-831-853-001: Modification - ADDITIONAL WORK 1 (Introduced at Rev 02) (1) Modification Task 282148-831-849-001: Modification - ADDITIONAL WORK 2 (Introduced at Rev 03) (1) Introduce a New Bracket on the Sub Spar Behind the Front Spar Between RIB 8 and RIB 9 on the RH Wing **CONF 002 Task 282148-831-848-001: MODIFICATION (1) Install a New Bracket on the Sub Spar Behind the Front Spar Between RIB 8 and RIB 9 on the RH Wing (2) Install cable sleeves in the RH Electronics Rack 90VU. (3) Install cable sleeves between FR38.2 and FR39, in the forward cargo compartment. (4) Install cable sleeves in the RH forward wing root and krueger flap. (5) Install the cable sleeves in the RH-wing forward of the front spar between rib 2 and rib 3 in zone 612. (6) Install the cable sleeves in the RH-wing forward of the front spar between rib 7 and rib 8 in zone 612. (7) Install the cable sleeves in the RH-wing forward of the front spar between rib 8 and rib 9 (pylon area) in zone 612. (8) Install the cable sleeves in the RH-wing forward of the front spar between rib 9 and rib 12 in zone 623. Task 282148-831-853-001: Modification - ADDITIONAL WORK 1 (Introduced at Rev 02) (1) Modification Task 282148-831-849-001: Modification - ADDITIONAL WORK 2 (Introduced at Rev 03) (1) Introduce a New Bracket on the Sub Spar Behind the Front Spar Between RIB 8 and RIB 9 on the RH Wing DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 7 6

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# @A310 SERVICE BULLETIN
**CONF 003 Task 282148-831-848-001: MODIFICATION (1) Install a New Bracket on the Sub Spar Behind the Front Spar Between RIB 8 and RIB 9 on the RH Wing (2) Install cable sleeves in the RH Electronics Rack 90VU. (3) Install cable sleeves between FR38.2 and FR39, in the forward cargo compartment. (4) Install cable sleeves in the RH forward wing root and krueger flap. (5) Install the cable sleeves in the RH-wing forward of the front spar between rib 2 and rib 3 in zone 612. (6) Install the cable sleeves in the RH-wing forward of the front spar between rib 7 and rib 8 in zone 612. (7) Install the cable sleeves in the RH-wing forward of the front spar between rib 8 and rib 9 (pylon area) in zone 612. (8) Install the cable sleeves in the RH-wing forward of the front spar between rib 9 and rib 12 in zone 623. Task 282148-831-850-001: Modification - ADDITIONAL WORK 3 (Introduced at Rev 06) (1) Modification **CONF 004 Task 282148-831-848-001: MODIFICATION (1) Install a New Bracket on the Sub Spar Behind the Front Spar Between RIB 8 and RIB 9 on the RH Wing (2) Install cable sleeves in the RH Electronics Rack 90VU. (3) Install cable sleeves between FR38.2 and FR39, in the forward cargo compartment. (4) Install cable sleeves in the RH forward wing root and krueger flap. (5) Install the cable sleeves in the RH-wing forward of the front spar between rib 2 and rib 3 in zone 612. (6) Install the cable sleeves in the RH-wing forward of the front spar between rib 7 and rib 8 in zone 612. (7) Install the cable sleeves in the RH-wing forward of the front spar between rib 8 and rib 9 (pylon area) in zone 612. (8) Install the cable sleeves in the RH-wing forward of the front spar between rib 9 and rib 12 in zone 623.
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 8 6

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# @A310 SERVICE BULLETIN Task 282148-831-850-001: Modification - ADDITIONAL WORK 3 (Introduced at Rev 06) (1) Modification **CONF 005 Task 282148-831-848-001: MODIFICATION (1) Install a New Bracket on the Sub Spar Behind the Front Spar Between RIB 8 and RIB 9 on the RH Wing (2) Install cable sleeves in the RH Electronics Rack 90VU. (3) Install cable sleeves between FR38.2 and FR39, in the forward cargo compartment. (4) Install cable sleeves in the RH forward wing root and krueger flap. (5) Install the cable sleeves in the RH-wing forward of the front spar between rib 2 and rib 3 in zone 612. (6) Install the cable sleeves in the RH-wing forward of the front spar between rib 7 and rib 8 in zone 612. (7) Install the cable sleeves in the RH-wing forward of the front spar between rib 8 and rib 9 (pylon area) in zone 612. (8) Install the cable sleeves in the RH-wing forward of the front spar between rib 9 and rib 12 in zone 623. Task 282148-831-853-001: Modification - ADDITIONAL WORK 1 (Introduced at Rev 02) (1) Modification Task 282148-831-849-001: Modification - ADDITIONAL WORK 2 (Introduced at Rev 03) (1) Introduce a New Bracket on the Sub Spar Behind the Front Spar Between RIB 8 and RIB 9 on the RH Wing **CONF 006 Task 282148-831-848-001: MODIFICATION (1) Install a New Bracket on the Sub Spar Behind the Front Spar Between RIB 8 and RIB 9 on the RH Wing (2) Install cable sleeves in the RH Electronics Rack 90VU. (3) Install cable sleeves between FR38.2 and FR39, in the forward cargo compartment. (4) Install cable sleeves in the RH forward wing root and krueger flap. (5) Install the cable sleeves in the RH-wing forward of the front spar between rib 2 and rib 3 in zone 612.

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 9 6

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# @A310 SERVICE BULLETIN (6) Install the cable sleeves in the RH-wing forward of the front spar between rib 7 and rib 8 in zone 612. (7) Install the cable sleeves in the RH-wing forward of the front spar between rib 8 and rib 9 (pylon area) in zone 612. (8) Install the cable sleeves in the RH-wing forward of the front spar between rib 9 and rib 12 in zone 623. Task 282148-831-853-001: Modification - ADDITIONAL WORK 1 (Introduced at Rev 02) (1) Modification Task 282148-831-849-001: Modification - ADDITIONAL WORK 2 (Introduced at Rev 03) (1) Introduce a New Bracket on the Sub Spar Behind the Front Spar Between RIB 8 and RIB 9 on the RH Wing **CONF 007 Task 282148-831-848-001: MODIFICATION (1) Install a New Bracket on the Sub Spar Behind the Front Spar Between RIB 8 and RIB 9 on the RH Wing (2) Install cable sleeves in the RH Electronics Rack 90VU. (3) Install cable sleeves between FR38.2 and FR39, in the forward cargo compartment. (4) Install cable sleeves in the RH forward wing root and krueger flap. (5) Install the cable sleeves in the RH-wing forward of the front spar between rib 2 and rib 3 in zone 612. (6) Install the cable sleeves in the RH-wing forward of the front spar between rib 7 and rib 8 in zone 612. (7) Install the cable sleeves in the RH-wing forward of the front spar between rib 8 and rib 9 (pylon area) in zone 612. (8) Install the cable sleeves in the RH-wing forward of the front spar between rib 9 and rib 12 in zone 623. Task 282148-831-850-001: Modification - ADDITIONAL WORK 3 (Introduced at Rev 06) (1) Modification **CONF 008 Task 282148-831-848-001: MODIFICATION (1) Install a New Bracket on the Sub Spar Behind the Front Spar Between RIB 8 and RIB 9 on the RH Wing
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 10 6

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# @A310 SERVICE BULLETIN (2) Install cable sleeves in the RH Electronics Rack 90VU. (3) Install cable sleeves between FR38.2 and FR39, in the forward cargo compartment. (4) Install cable sleeves in the RH forward wing root and krueger flap. (5) Install the cable sleeves in the RH-wing forward of the front spar between rib 2 and rib 3 in zone 612. (6) Install the cable sleeves in the RH-wing forward of the front spar between rib 7 and rib 8 in zone 612. (7) Install the cable sleeves in the RH-wing forward of the front spar between rib 8 and rib 9 (pylon area) in zone 612. (8) Install the cable sleeves in the RH-wing forward of the front spar between rib 9 and rib 12 in zone 623. Task 282148-831-850-001: Modification - ADDITIONAL WORK 3 (Introduced at Rev 06) (1) Modification **CONF ALL E. COMPLIANCE (1) Classification MANDATORY: Service Bulletin must be accomplished. (2) Accomplishment Timescale 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 the authority of the 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: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 11 6

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# @A310 SERVICE BULLETIN
**CONF 001 Task 282148-831-848-001: MODIFICATION Get Access 11.00 On Aircraft Install a New Bracket on the Sub Spar Behind the Front Spar Between RIB 8 and RIB 9 on the RH Wing 1.00 Install cable sleeves in the RH Electronics Rack 90VU. 6.00 Install cable sleeves between FR38.2 and FR39, in the forward cargo compartment. 1.00 Install cable sleeves in the RH forward wing root and krueger flap. 2.00 Install the cable sleeves in the RH-wing forward of the front spar between rib 2 and rib 3 in zone 612. 2.00 Install the cable sleeves in the RH-wing forward of the front spar between rib 7 and rib 8 in zone 612. 2.00 Install the cable sleeves in the RH-wing forward of the front spar between rib 8 and rib 9 (pylon area) in zone 612. 4.00 Install the cable sleeves in the RH-wing forward of the front spar between rib 9 and rib 12 in zone 623. 4.00 Tests 3.00 Close-Up 4.00 TOTAL MANHOURS 40.00 ELAPSED TIME (HOURS) 14.00

Task 282148-831-853-001: Modification - ADDITIONAL WORK 1 (Introduced at Rev 02) Get Access 3.00 On Aircraft Modification 14.00 Tests 3.00 Close-Up 3.00 TOTAL MANHOURS 23.00 ELAPSED TIME (HOURS) 13.00

Task 282148-831-849-001: Modification - ADDITIONAL WORK 2 (Introduced at Rev 03) Get Access 1.00 On Aircraft Introduce a New Bracket on the Sub Spar Behind the Front Spar Between RIB 8 and RIB 9 on the RH Wing 1.00 Tests 0.00 Close-Up 1.00 TOTAL MANHOURS 3.00 ELAPSED TIME (HOURS) 3.00

Task 282148-831-850-001: Modification - ADDITIONAL WORK 3 (Introduced at Rev 06) Get Access 0.00 DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 12 6

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# @A310 SERVICE BULLETIN
Task 282148-831-850-001: Modification - ADDITIONAL WORK 3 (Introduced at Rev 06) On Aircraft Tests 0.00 Close-Up 0.00 TOTAL MANHOURS 0.00 ELAPSED TIME (HOURS) 0.00 **CONF 002 Task 282148-831-848-001: MODIFICATION Get Access 11.00 On Aircraft Install a New Bracket on the Sub Spar Behind the Front Spar Between RIB 8 and RIB 9 on the RH Wing 1.00 Install cable sleeves in the RH Electronics Rack 90VU. 6.00 Install cable sleeves between FR38.2 and FR39, in the forward cargo compartment. 1.00 Install cable sleeves in the RH forward wing root and krueger flap. 2.00 Install the cable sleeves in the RH-wing forward of the front spar between rib 2 and rib 3 in zone 612. 1.00 Install the cable sleeves in the RH-wing forward of the front spar between rib 7 and rib 8 in zone 612. 1.00 Install the cable sleeves in the RH-wing forward of the front spar between rib 8 and rib 9 (pylon area) in zone 612. 1.00 Install the cable sleeves in the RH-wing forward of the front spar between rib 9 and rib 12 in zone 623. 1.00 Tests 3.00 Close-Up 4.00 TOTAL MANHOURS 32.00 ELAPSED TIME (HOURS) 14.00

Task 282148-831-853-001: Modification - ADDITIONAL WORK 1 (Introduced at Rev 02) Get Access 3.00 On Aircraft Modification 14.00 Tests 3.00 Close-Up 3.00 TOTAL MANHOURS 23.00 ELAPSED TIME (HOURS) 13.00

Task 282148-831-849-001: Modification - ADDITIONAL WORK 2 (Introduced at Rev 03) Get Access 1.00 On Aircraft Introduce a New Bracket on the Sub Spar Behind the Front Spar Between RIB 8 and RIB 9 on the RH Wing 1.00

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 13 6

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# @A310 SERVICE BULLETIN
Task 282148-831-849-001: Modification - ADDITIONAL WORK 2 (Introduced at Rev 03) Tests 0.00 Close-Up 1.00 TOTAL MANHOURS 3.00 ELAPSED TIME (HOURS) 3.00

Task 282148-831-850-001: Modification - ADDITIONAL WORK 3 (Introduced at Rev 06) Get Access 0.00 On Aircraft Tests 0.00 Close-Up 0.00 TOTAL MANHOURS 0.00 ELAPSED TIME (HOURS) 0.00 **CONF 003 Task 282148-831-848-001: MODIFICATION Get Access 11.00 On Aircraft Install a New Bracket on the Sub Spar Behind the Front Spar Between RIB 8 and RIB 9 on the RH Wing 1.00 Install cable sleeves in the RH Electronics Rack 90VU. 6.00 Install cable sleeves between FR38.2 and FR39, in the forward cargo compartment. 1.00 Install cable sleeves in the RH forward wing root and krueger flap. 2.00 Install the cable sleeves in the RH-wing forward of the front spar between rib 2 and rib 3 in zone 612. 1.00 Install the cable sleeves in the RH-wing forward of the front spar between rib 7 and rib 8 in zone 612. 1.00 Install the cable sleeves in the RH-wing forward of the front spar between rib 8 and rib 9 (pylon area) in zone 612. 1.00 Install the cable sleeves in the RH-wing forward of the front spar between rib 9 and rib 12 in zone 623. 1.00 Tests 3.00 Close-Up 4.00 TOTAL MANHOURS 32.00 ELAPSED TIME (HOURS) 14.00

Task 282148-831-853-001: Modification - ADDITIONAL WORK 1 (Introduced at Rev 02) Get Access 0.00 On Aircraft Tests 0.00 Close-Up 0.00 TOTAL MANHOURS 0.00
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 14 6

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# @A310 SERVICE BULLETIN
Task 282148-831-853-001: Modification - ADDITIONAL WORK 1 (Introduced at Rev 02) ELAPSED TIME (HOURS) 0.00

Task 282148-831-849-001: Modification - ADDITIONAL WORK 2 (Introduced at Rev 03) Get Access 0.00 On Aircraft Tests 0.00 Close-Up 0.00 TOTAL MANHOURS 0.00 ELAPSED TIME (HOURS) 0.00

Task 282148-831-850-001: Modification - ADDITIONAL WORK 3 (Introduced at Rev 06) Get Access 1.00 On Aircraft Modification 1.00 Tests 0.00 Close-Up 1.00 TOTAL MANHOURS 3.00 ELAPSED TIME (HOURS) 3.00 **CONF 004 Task 282148-831-848-001: MODIFICATION Get Access 11.00 On Aircraft Install a New Bracket on the Sub Spar Behind the Front Spar Between RIB 8 and RIB 9 on the RH Wing 1.00 Install cable sleeves in the RH Electronics Rack 90VU. 6.00 Install cable sleeves between FR38.2 and FR39, in the forward cargo compartment. 1.00 Install cable sleeves in the RH forward wing root and krueger flap. 2.00 Install the cable sleeves in the RH-wing forward of the front spar between rib 2 and rib 3 in zone 612. 1.00 Install the cable sleeves in the RH-wing forward of the front spar between rib 7 and rib 8 in zone 612. 1.00 Install the cable sleeves in the RH-wing forward of the front spar between rib 8 and rib 9 (pylon area) in zone 612. 1.00 Install the cable sleeves in the RH-wing forward of the front spar between rib 9 and rib 12 in zone 623. 1.00 Tests 3.00 Close-Up 4.00 TOTAL MANHOURS 32.00 ELAPSED TIME (HOURS) 14.00

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 15 6

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# @A310 SERVICE BULLETIN
Task 282148-831-853-001: Modification - ADDITIONAL WORK 1 (Introduced at Rev 02) Get Access 0.00 On Aircraft Tests 0.00 Close-Up 0.00 TOTAL MANHOURS 0.00 ELAPSED TIME (HOURS) 0.00

Task 282148-831-849-001: Modification - ADDITIONAL WORK 2 (Introduced at Rev 03) Get Access 0.00 On Aircraft Tests 0.00 Close-Up 0.00 TOTAL MANHOURS 0.00 ELAPSED TIME (HOURS) 0.00

Task 282148-831-850-001: Modification - ADDITIONAL WORK 3 (Introduced at Rev 06) Get Access 1.00 On Aircraft Modification 1.00 Tests 0.00 Close-Up 1.00 TOTAL MANHOURS 3.00 ELAPSED TIME (HOURS) 3.00 **CONF 005 Task 282148-831-848-001: MODIFICATION Get Access 11.00 On Aircraft Install a New Bracket on the Sub Spar Behind the Front Spar Between RIB 8 and RIB 9 on the RH Wing 1.00 Install cable sleeves in the RH Electronics Rack 90VU. 6.00 Install cable sleeves between FR38.2 and FR39, in the forward cargo compartment. 1.00 Install cable sleeves in the RH forward wing root and krueger flap. 2.00 Install the cable sleeves in the RH-wing forward of the front spar between rib 2 and rib 3 in zone 612. 2.00 Install the cable sleeves in the RH-wing forward of the front spar between rib 7 and rib 8 in zone 612. 2.00 Install the cable sleeves in the RH-wing forward of the front spar between rib 8 and rib 9 (pylon area) in zone 612. 4.00 Install the cable sleeves in the RH-wing forward of the front spar between rib 9 and rib 12 in zone 623. 4.00 Tests 3.00 DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 16 6

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# @A310 SERVICE BULLETIN

Task 282148-831-848-001: MODIFICATION Close-Up 4.00 TOTAL MANHOURS 40.00 ELAPSED TIME (HOURS) 14.00

Task 282148-831-853-001: Modification - ADDITIONAL WORK 1 (Introduced at Rev 02) Get Access 3.00 On Aircraft Modification 14.00 Tests 3.00 Close-Up 3.00 TOTAL MANHOURS 23.00 ELAPSED TIME (HOURS) 13.00

Task 282148-831-849-001: Modification - ADDITIONAL WORK 2 (Introduced at Rev 03) Get Access 1.00 On Aircraft Introduce a New Bracket on the Sub Spar Behind the Front Spar Between RIB 8 and RIB 9 on the RH Wing 1.00 Tests 0.00 Close-Up 1.00 TOTAL MANHOURS 3.00 ELAPSED TIME (HOURS) 3.00

Task 282148-831-850-001: Modification - ADDITIONAL WORK 3 (Introduced at Rev 06) Get Access 0.00 On Aircraft Tests 0.00 Close-Up 0.00 TOTAL MANHOURS 0.00 ELAPSED TIME (HOURS) 0.00 **CONF 006 Task 282148-831-848-001: MODIFICATION Get Access 11.00 On Aircraft Install a New Bracket on the Sub Spar Behind the Front Spar Between RIB 8 and RIB 9 on the RH Wing 1.00 Install cable sleeves in the RH Electronics Rack 90VU. 6.00 Install cable sleeves between FR38.2 and FR39, in the forward cargo compartment. 1.00 Install cable sleeves in the RH forward wing root and krueger flap. 2.00 Install the cable sleeves in the RH-wing forward of the front spar between rib 2 and rib 3 in zone 612. 1.00

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 17 6

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# @A310 SERVICE BULLETIN

Task 282148-831-848-001: MODIFICATION Install the cable sleeves in the RH-wing forward of the front spar between rib 7 and rib 8 in zone 612. 1.00 Install the cable sleeves in the RH-wing forward of the front spar between rib 8 and rib 9 (pylon area) in zone 612. 1.00 Install the cable sleeves in the RH-wing forward of the front spar between rib 9 and rib 12 in zone 623. 1.00 Tests 3.00 Close-Up 4.00 TOTAL MANHOURS 32.00 ELAPSED TIME (HOURS) 14.00

Task 282148-831-853-001: Modification - ADDITIONAL WORK 1 (Introduced at Rev 02) Get Access 3.00 On Aircraft Modification 14.00 Tests 3.00 Close-Up 3.00 TOTAL MANHOURS 23.00 ELAPSED TIME (HOURS) 13.00

Task 282148-831-849-001: Modification - ADDITIONAL WORK 2 (Introduced at Rev 03) Get Access 1.00 On Aircraft Introduce a New Bracket on the Sub Spar Behind the Front Spar Between RIB 8 and RIB 9 on the RH Wing 1.00 Tests 0.00 Close-Up 1.00 TOTAL MANHOURS 3.00 ELAPSED TIME (HOURS) 3.00

Task 282148-831-850-001: Modification - ADDITIONAL WORK 3 (Introduced at Rev 06) Get Access 0.00 On Aircraft Tests 0.00 Close-Up 0.00 TOTAL MANHOURS 0.00 ELAPSED TIME (HOURS) 0.00 **CONF 007 Task 282148-831-848-001: MODIFICATION Get Access 11.00 On Aircraft Install a New Bracket on the Sub Spar Behind the Front Spar Between RIB 8 and RIB 9 on the RH Wing 1.00

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 18 6

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# @A310 SERVICE BULLETIN

Task 282148-831-848-001: MODIFICATION Install cable sleeves in the RH Electronics Rack 90VU. 6.00 Install cable sleeves between FR38.2 and FR39, in the forward cargo compartment. 1.00 Install cable sleeves in the RH forward wing root and krueger flap. 2.00 Install the cable sleeves in the RH-wing forward of the front spar between rib 2 and rib 3 in zone 612. 1.00 Install the cable sleeves in the RH-wing forward of the front spar between rib 7 and rib 8 in zone 612. 1.00 Install the cable sleeves in the RH-wing forward of the front spar between rib 8 and rib 9 (pylon area) in zone 612. 1.00 Install the cable sleeves in the RH-wing forward of the front spar between rib 9 and rib 12 in zone 623. 1.00 Tests 3.00 Close-Up 4.00 TOTAL MANHOURS 32.00 ELAPSED TIME (HOURS) 14.00

Task 282148-831-853-001: Modification - ADDITIONAL WORK 1 (Introduced at Rev 02) Get Access 0.00 On Aircraft Tests 0.00 Close-Up 0.00 TOTAL MANHOURS 0.00 ELAPSED TIME (HOURS) 0.00

Task 282148-831-849-001: Modification - ADDITIONAL WORK 2 (Introduced at Rev 03) Get Access 0.00 On Aircraft Tests 0.00 Close-Up 0.00 TOTAL MANHOURS 0.00 ELAPSED TIME (HOURS) 0.00

Task 282148-831-850-001: Modification - ADDITIONAL WORK 3 (Introduced at Rev 06) Get Access 1.00 On Aircraft Modification 1.00 Tests 0.00 Close-Up 1.00 TOTAL MANHOURS 3.00 ELAPSED TIME (HOURS) 3.00

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 19 6

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# @A310 SERVICE BULLETIN
**CONF 008 Task 282148-831-848-001: MODIFICATION Get Access 11.00 On Aircraft Install a New Bracket on the Sub Spar Behind the Front Spar Between RIB 8 and RIB 9 on the RH Wing 1.00 Install cable sleeves in the RH Electronics Rack 90VU. 6.00 Install cable sleeves between FR38.2 and FR39, in the forward cargo compartment. 1.00 Install cable sleeves in the RH forward wing root and krueger flap. 2.00 Install the cable sleeves in the RH-wing forward of the front spar between rib 2 and rib 3 in zone 612. 1.00 Install the cable sleeves in the RH-wing forward of the front spar between rib 7 and rib 8 in zone 612. 1.00 Install the cable sleeves in the RH-wing forward of the front spar between rib 8 and rib 9 (pylon area) in zone 612. 1.00 Install the cable sleeves in the RH-wing forward of the front spar between rib 9 and rib 12 in zone 623. 1.00 Tests 3.00 Close-Up 4.00 TOTAL MANHOURS 32.00 ELAPSED TIME (HOURS) 14.00

Task 282148-831-853-001: Modification - ADDITIONAL WORK 1 (Introduced at Rev 02) Get Access 0.00 On Aircraft Close-Up 0.00 TOTAL MANHOURS 0.00 ELAPSED TIME (HOURS) 0.00

Task 282148-831-849-001: Modification - ADDITIONAL WORK 2 (Introduced at Rev 03) Get Access 0.00 On Aircraft Tests 0.00 Close-Up 0.00 TOTAL MANHOURS 0.00 ELAPSED TIME (HOURS) 0.00

Task 282148-831-850-001: Modification - ADDITIONAL WORK 3 (Introduced at Rev 06) Get Access 1.00 On Aircraft Modification 1.00 Tests 0.00

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 20 6

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# @A310 SERVICE BULLETIN
Task 282148-831-850-001: Modification - ADDITIONAL WORK 3 (Introduced at Rev 06) Close-Up 1.00 TOTAL MANHOURS 3.00 ELAPSED TIME (HOURS) 3.00 **CONF ALL H. WEIGHT AND BALANCE **CONF 001, 005 The weight and balance estimates given in this Service Bulletin are based on the Manufacturer’s Empty Weight (MEW) and do not include operator item’s. For the definition of MEW and operator’s items, refer to the 01-00-07 Manufacturers Empty Weight +1.856 KG (+4.0917 LB) Effect on Balance +41.89 KGM (+297.196 LB.FT) ADDITIONAL WORK 1 Manufacturers Empty Weight +0.336 KG (+0.7407 LB) Effect on Balance +9.186 KGM (+66.442 LB.FT) ADDITIONAL WORK 2 Manufacturers Empty Weight +0.437 KG (+0.9634 LB) Effect on Balance +11.948 KGM (+86.419 LB.FT) **CONF 002, 006 The weight and balance estimates given in this Service Bulletin are based on the Manufacturer’s Empty Weight (MEW) and do not include operator item’s. For the definition of MEW and operator’s items, refer to the 01-00-07 Manufacturers Empty Weight +1.883 KG (+4.1512 LB) Effect on Balance +41.705 KGM (+301.652 LB.FT) ADDITIONAL WORK 1 Manufacturers Empty Weight +0.437 KG (+0.9634 LB) Effect on Balance +11.948 KGM (+86.419 LB.FT) ADDITIONAL WORK 2 Not Changed **CONF 003, 007 The weight and balance estimates given in this Service Bulletin are based on the Manufacturer’s Empty Weight (MEW) and do not include operator item’s. For the definition of MEW and operator’s items, refer to the 01-00-07 Manufacturers Empty Weight +2.492 KG (+5.4938 LB) Effect on Balance +55.177 KGM (+399.095 LB.FT) ADDITIONAL WORK 3 Not Changed DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 21 6

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# @A310 SERVICE BULLETIN
**CONF 004, 008 The weight and balance estimates given in this Service Bulletin are based on the Manufacturer’s Empty Weight (MEW) and do not include operator item’s. For the definition of MEW and operator’s items, refer to the 01-00-07 Manufacturers Empty Weight +2.569 KG (+5.6636 LB) Effect on Balance +56.889 KGM (+411.478 LB.FT) ADDITIONAL WORK 3 Not Changed **CONF ALL I. ELECTRICAL LOAD DATA Not Changed J. REFERENCES **CONF 001 Aircraft Maintenance Manual (AMM) 06-41-53 06-41-57 24-00-00 24-31-11 24-41-00 25-54-10 27-28-00 27-80-00 27-84-00 28-42-44 30-11-00 36-11-00 52-10-00 52-30-00 53-10-55 Consumable Material List (CML) Elec. Std. Practices Manual (ESPM) 20-25-21 20-33-00 20-52-00 20-52-21 20-55-00 Standards Manual (SM) Structural Repair Manual (SRM) 51-23-10 51-23-11 51-40-21 51-40-44 51-42-11 Weight and Balance Manual (WBM) 01-00-07 **CONF 002 Aircraft Maintenance Manual (AMM) 06-41-53 06-41-57 24-00-00 24-31-11 24-41-00 25-54-10 27-28-00 27-80-00 27-84-00 28-42-44 30-11-00 36-11-00 52-10-00 52-30-00 53-10-55 Consumable Material List (CML) Elec. Std. Practices Manual (ESPM) 20-25-21 20-33-00 20-52-00 20-52-21 20-55-00 Standards Manual (SM) Structural Repair Manual (SRM) 51-23-10 51-23-11 51-40-21 51-40-44 51-42-11 Weight and Balance Manual (WBM) 01-00-07

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 22 6

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# @A310 SERVICE BULLETIN
**CONF 003 Aircraft Maintenance Manual (AMM) 06-41-53 06-41-57 24-00-00 24-31-11 24-41-00 25-54-10 27-84-00 28-42-44 30-11-00 36-11-00 52-10-00 52-30-00 53-10-55 Consumable Material List (CML) Elec. Std. Practices Manual (ESPM) 20-25-21 20-33-00 20-55-00 Standards Manual (SM) Structural Repair Manual (SRM) 51-23-10 51-23-11 51-40-21 51-40-44 51-42-11 Weight and Balance Manual (WBM) 01-00-07 **CONF 004 Aircraft Maintenance Manual (AMM) 06-41-53 06-41-57 24-00-00 24-31-11 24-41-00 25-54-10 27-84-00 28-42-44 30-11-00 36-11-00 52-10-00 52-30-00 53-10-55 Consumable Material List (CML) Elec. Std. Practices Manual (ESPM) 20-25-21 20-33-00 20-55-00 Standards Manual (SM) Structural Repair Manual (SRM) 51-23-10 51-23-11 51-40-21 51-40-44 51-42-11 Weight and Balance Manual (WBM) 01-00-07 **CONF 005 Aircraft Maintenance Manual (AMM) 06-41-53 06-41-57 24-00-00 24-31-11 24-41-00 25-54-10 27-28-00 27-80-00 27-84-00 28-42-44 30-11-00 36-11-00 52-10-00 52-30-00 53-10-55 Consumable Material List (CML) Elec. Std. Practices Manual (ESPM) 20-25-21 20-33-00 20-52-00 20-52-21 20-55-00 Standards Manual (SM) Structural Repair Manual (SRM) 51-23-10 51-23-11 51-40-21 51-40-44 51-42-11 Weight and Balance Manual (WBM) 01-00-07 **CONF 006 Aircraft Maintenance Manual (AMM) 06-41-53 06-41-57 24-00-00 24-31-11 24-41-00 25-54-10 27-28-00 27-80-00 27-84-00 28-42-44 30-11-00 36-11-00 52-10-00 52-30-00 53-10-55

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 23 6

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# @A310 SERVICE BULLETIN
Consumable Material List (CML) Elec. Std. Practices Manual (ESPM) 20-25-21 20-33-00 20-52-00 20-52-21 20-55-00 Standards Manual (SM) Structural Repair Manual (SRM) 51-23-10 51-23-11 51-40-21 51-40-44 51-42-11 Weight and Balance Manual (WBM) 01-00-07 **CONF 007 Aircraft Maintenance Manual (AMM) 06-41-53 06-41-57 24-00-00 24-31-11 24-41-00 25-54-10 27-84-00 28-42-44 30-11-00 36-11-00 52-10-00 52-30-00 53-10-55 Consumable Material List (CML) Elec. Std. Practices Manual (ESPM) 20-25-21 20-33-00 20-55-00 Standards Manual (SM) Structural Repair Manual (SRM) 51-23-10 51-23-11 51-40-21 51-40-44 51-42-11 Weight and Balance Manual (WBM) 01-00-07 **CONF 008 Aircraft Maintenance Manual (AMM) 06-41-53 06-41-57 24-00-00 24-31-11 24-41-00 25-54-10 27-84-00 28-42-44 30-11-00 36-11-00 52-10-00 52-30-00 53-10-55 Consumable Material List (CML) Elec. Std. Practices Manual (ESPM) 20-25-21 20-33-00 20-55-00 Standards Manual (SM) Structural Repair Manual (SRM) 51-23-10 51-23-11 51-40-21 51-40-44 51-42-11 Weight and Balance Manual (WBM) 01-00-07 **CONF ALL K. PUBLICATION AFFECTED

Aircraft Wiring Manual (AWM) 28-42-07 Illustrated Parts Catalog (IPC) 24-92-03 L. INTERCHANGEABILITY/MIXABILITY Not Applicable M. SPARES None

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 24 6

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# @A310 SERVICE BULLETIN
2. MATERIAL INFORMATION **CONF ALL A. MATERIAL - PRICE AND AVAILABILITY (1) Procurement Addresses Customers with aircraft shown in the effectivity of this Service Bulletin should send a purchase order to AIRBUS. Quote the number of this Service Bulletin. The address is: Kit 282148A01R00 Kit 282148B01R00 Kit 282148D01R00 Kit 282148D02R01 Kit 282148D03R01 Kit 282148D05R01 Kit 282148D06R01 Kit 282148D07R00 Kit 282148D08R00 AIRBUS MATERIAL LOGISTICS AND SUPPLIERS Weg beim Jaeger 150 D-22335 HAMBURG GERMANY For ordering by internet: http://spares.airbus.com For ordering modification kits by fax: +49 40 50 76 25 90 For ordering of single spares by fax: +49 40 50 76 40 12 For ordering by E-mail: airbus.kit@airbus.com (2) Price and Availability

Kit 282148A01R00 Cost 1,100.00 USD Availability 30 calendar days from receipt of order The Kit availability given above is the standard lead time from the date of your purchase order. If you require Kits 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 at the issue date of the Service Bulletin. Kit 282148B01R00 Cost 90.00 USD Availability 90 calendar days from receipt of order The Kit availability given above is the standard lead time from the date of your purchase order. If you require the Kit(s) before this time, please include a retrofit planning schedule with your order so that we can try to comply with your requirements. Kit 282148D01R00 Cost 2,210.00 USD Availability 90 calendar days from receipt of order The Kit availability given above is the standard lead time from the date of your purchase order. If you require the Kit(s) before this time, please include a retrofit planning schedule with your order so that we can try to comply with your requirements.
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 25 6

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# @A310 SERVICE BULLETIN The sales terms (costs and availability) are estimated in relation to the economic conditions at the issue date of the Service Bulletin. Kit 282148D02R01 Cost 1,580.00 USD Availability 90 calendar days from receipt of order The Kit availability given above is the standard lead time from the date of your purchase order. If you require the Kit(s) 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 the economic conditions at the issue date of the Service Bulletin. Kit 282148D03R01 Cost 1,530.00 USD Availability 90 calendar days from receipt of order The Kit availability given above is the standard lead time from the date of your purchase order. If you require the Kit(s) 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 the economic conditions at the issue date of the Service Bulletin. Kit 282148D05R01 Cost 570.00 USD Availability 90 calendar days from receipt of order The Kit availability given above is the standard lead time from the date of your purchase order. If you require the Kit(s) 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 the economic conditions at the issue date of the Service Bulletin. Kit 282148D06R01 Cost 560.00 USD Availability 90 calendar days from receipt of order The Kit availability given above is the standard lead time from the date of your purchase order. If you require the Kit(s) 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 the economic conditions at the issue date of the Service Bulletin. Kit 282148D07R00 Cost 32.50 USD Availability 90 calendar days from receipt of order

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 26 6

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# @A310 SERVICE BULLETIN The Kit availability given above is the standard lead time from the date of your purchase order. If you require the Kit(s) 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 the economic conditions at the issue date of the Service Bulletin. Kit 282148D08R00 Cost 33.20 USD Availability 90 calendar days from receipt of order The Kit availability given above is the standard lead time from the date of your purchase order. If you require the Kit(s) 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 the economic conditions at the issue date of the Service Bulletin. B. INDUSTRY SUPPORT INFORMATION AIRBUS will not provide industry support for accomplishment of this Service Bulletin. C. LIST OF COMPONENTS Kit 282148A01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 1 ABS0596S004 2000 SLEEVE 2 ABS0596S006 2000 (mm) SLEEVE NSA935401-04 50 TIE NSA935401-05 100 TIE 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 282148D01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 1 ABS0596S004 12 SLEEVE 10 MS21919WCH9 8 CLAMP 11 MS21919WCH13 2 CLAMP 12 MS21919WCH14 2 CLAMP 14 NAS1096-3-19 2 SCREW 15 NSA5527-03-03 3 SPACER 16 NSA8420-2 0.5 (ME) CORD 149 NSA935401-03 31 TIE 150 NSA935401-04 47 TIE DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 27 6

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# @A310 SERVICE BULLETIN
NOTE: If you find part numbers of hardware components in the related kit(s) which you cannot identify in the LIST OF COMPONENTS of this Service Bulletin, refer to Standards Manual (SM). The SM will give you the correct part number to part number relationship. Kit 282148D02R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 1 ABS0596S004 3 SLEEVE 10 MS21919WCH9 1 CLAMP 30 NSA5527-03-01D 2 SPACER 31 NSA5527-03-02D 1 SPACER 109 NSA935805-09 3 (ME) CONDUIT 117 NSA935807C09 12 CLAMP 121 NAS1096-3-40 1 SCREW 125 B9299071900200 1 EQUIPMNT 126 NSA938184PV1601 15 PIN 149 NSA935401-03 30 TIE 150 NSA935401-04 30 TIE 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 282148D03R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 1 ABS0596S004 3 SLEEVE 10 MS21919WCH9 1 CLAMP 31 NSA5527-03-02D 3 SPACER 109 NSA935805-09 CONDUIT 117 NSA935807C09 7 CLAMP 121 NAS1096-3-40 1 SCREW 123 NAS1801-3-31 3 SCREW 126 NSA938184PV1601 7 PIN 130 NSA5527-03-08D 2 SPACER 131 NSA5527-03-07D 2 SPACER 132 B9299071900600 1 EQUIPMNT 149 NSA935401-03 30 TIE 150 NSA935401-04 40 TIE 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: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 28 6

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# @A310 SERVICE BULLETIN
Kit 282148D05R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 1 ABS0596S004 3 SLEEVE 30 NSA5527-03-01D 2 SPACER 31 NSA5527-03-02D 1 SPACER 109 NSA935805-09 3 (ME) CONDUIT 117 NSA935807C09 12 CLAMP 125 B9299071900200 1 EQUIPMNT 126 NSA938184PV1601 15 PIN 135 NAS1096-3-42 1 SCREW 136 NAS1096-3-30 1 SCREW 149 NSA935401-03 30 TIE 150 NSA935401-04 30 TIE 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 282148D06R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 1 ABS0596S004 3 SLEEVE 31 NSA5527-03-02D 2 SPACER 109 NSA935805-09 1.5 (ME) CONDUIT 117 NSA935807C09 7 CLAMP 121 NAS1096-3-40 1 SCREW 123 NAS1801-3-31 2 SCREW 126 NSA938184PV1601 7 PIN 130 NSA5527-03-08D 1 SPACER 131 NSA5527-03-07D 1 SPACER 132 B9299071900600 1 EQUIPMNT 149 NSA935401-03 30 TIE 150 NSA935401-04 30 TIE 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 282148D07R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 31 NSA5527-03-02D 2 SPACER 110 NSA935807C10 1 CLAMP 112 NAS1149D0332K 1 WASHER
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 29 6

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# @A310 SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 117 NSA935807C09 3 CLAMP 120 NSA5516-04NV 1 CLAMP 130 NSA5527-03-08D 1 SPACER 135 NAS1096-3-42 1 SCREW 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 282148D08R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 30 NSA5527-03-01D 1 SPACER 31 NSA5527-03-02D 1 SPACER 111 NSA935807C16 2 CLAMP 112 NSA935808-01 1 WASHER 117 NSA935807C09 1 CLAMP 120 NSA5516-04NV 1 CLAMP 123 NAS1801-3-31 1 SCREW 130 NSA5527-03-08D 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 282148B01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 1 A5725068600000 1 Bracket 2 ASNA0078A502 2 Rivet NOTE: If you find part numbers of hardware components in the related kit(s) which you cannot identify in the LIST OF COMPONENTS of this Service Bulletin, refer to Standards Manual (SM). The SM will give you the correct part number to part number relationship. D. LIST OF MATERIALS - OPERATOR SUPPLIED (1) Consumable Materials Consumable CMLD01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Storage compound 15-008A As required

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 30 6

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# @A310 SERVICE BULLETIN
Consumable CMLB01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Corrosion Inhibiting Low Adhesion Sealant 09-018 As required Solvent General Purpose 11-026 As required Lint-Free Cotton Cloth 19-003 As required (2) Components None (3) Equipment None E. PARTS TO BE RE-IDENTIFIED BY OPERATOR None F. TOOLING None

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 31 6

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# @A310 SERVICE BULLETIN

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# @A310 SERVICE BULLETIN
3. ACCOMPLISHMENT INSTRUCTIONS Task 282148-831-848-001 - MODIFICATION WARNING: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND CAUTIONS INCLUDED IN THE REFERENCED PROCEDURES. WARNING: THIS PROCEDURE USES A FUEL SYSTEM ITEM THAT IS IN A CATEGORY KNOWN AS A CRITICAL DESIGN CONFIGURATION CONTROL LIMITATION (CDCCL) CDCCL IDENTIFIES AN ITEM THAT CAN BE THE SOURCE OF A POSSIBLE FUEL TANK IGNITION. YOU MUST KEEP ALL CDCCL ITEMS IN THE APPROVED CONFIGURATION. DAMAGE, WEAR OR CHANGES TO A CDCCL ITEM CAN CAUSE A POSSIBLE FUEL TANK EXPLOSION. 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. Task Associated Data **CONF 001 Manpower TOTAL MANHOURS 40.00 ELAPSED TIME (HOURS) 14.00 **CONF 002 Manpower TOTAL MANHOURS 32.00 ELAPSED TIME (HOURS) 14.00 **CONF 003 Manpower TOTAL MANHOURS 32.00 ELAPSED TIME (HOURS) 14.00
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# @A310 SERVICE BULLETIN
**CONF 004 Manpower TOTAL MANHOURS 32.00 ELAPSED TIME (HOURS) 14.00 **CONF 005 Manpower TOTAL MANHOURS 40.00 ELAPSED TIME (HOURS) 14.00 **CONF 006 Manpower TOTAL MANHOURS 32.00 ELAPSED TIME (HOURS) 14.00 **CONF 007 Manpower TOTAL MANHOURS 32.00 ELAPSED TIME (HOURS) 14.00 **CONF 008 Manpower TOTAL MANHOURS 32.00 ELAPSED TIME (HOURS) 14.00 **CONF ALL A. GENERAL **CONF 001 (1) Subtask 282148-910-401-001 - Standard Practices Manpower Resources Skills AIRFRAME References Structural Repair Manual (SRM) 51-23-10 51-40-21 51-40-44 (a) For material specification (Mat. No.) given in this Service Bulletin, refer to the Consumable Material List (CML). (b) For fastener hole and drill data (Refer to SRM 51-40-44). DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 34 6

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# @A310 SERVICE BULLETIN (c) For paint coatings (Refer to SRM 51-23-10). (d) Installation of fasteners (Refer to SRM 51-40-21). (2) Subtask 282148-910-204-001 - Standard Practices Manpower Resources Skills NON SPECIFIC Material necessary to do the job Consumable CMLD01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Storage compound 15-008A As required References Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001 Consumable Material List (CML) Elec. Std. Practices Manual (ESPM) 20-33-00 (a) For panel location (Refer to AMM 06-41-53, Page Block 001). (b) Obey the instructions for the wiring installation (Refer to ESPM 20-33-00). (c) Apply: Storage compound 15-008A As required to the screws after assembly. (3) Subtask 282148-900-202-001 - 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 282148-910-401-001 - Standard Practices Manpower Resources Skills AIRFRAME References Structural Repair Manual (SRM) 51-23-10 51-40-21 51-40-44

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 35 6

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# @A310 SERVICE BULLETIN (a) For material specification (Mat. No.) given in this Service Bulletin, refer to the Consumable Material List (CML). (b) For fastener hole and drill data (Refer to SRM 51-40-44). (c) For paint coatings (Refer to SRM 51-23-10). (d) Installation of fasteners (Refer to SRM 51-40-21). (2) Subtask 282148-910-204-001 - Standard Practices Manpower Resources Skills NON SPECIFIC Material necessary to do the job Consumable CMLD01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Storage compound 15-008A As required References Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001 Consumable Material List (CML) Elec. Std. Practices Manual (ESPM) 20-33-00 (a) For panel location (Refer to AMM 06-41-53, Page Block 001). (b) Obey the instructions for the wiring installation (Refer to ESPM 20-33-00). (c) Apply: Storage compound 15-008A As required to the screws after assembly. (3) Subtask 282148-900-202-001 - 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 282148-910-401-001 - Standard Practices Manpower Resources Skills AIRFRAME

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 36 6

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# @A310 SERVICE BULLETIN

References Structural Repair Manual (SRM) 51-23-10 51-40-21 51-40-44 (a) For material specification (Mat. No.) given in this Service Bulletin, refer to the Consumable Material List (CML). (b) For fastener hole and drill data (Refer to SRM 51-40-44). (c) For paint coatings (Refer to SRM 51-23-10). (d) Installation of fasteners (Refer to SRM 51-40-21). (2) Subtask 282148-910-204-001 - Standard Practices Manpower Resources Skills NON SPECIFIC Material necessary to do the job Consumable CMLD01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Storage compound 15-008A As required References Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001 Consumable Material List (CML) Elec. Std. Practices Manual (ESPM) 20-33-00 (a) For panel location (Refer to AMM 06-41-53, Page Block 001). (b) Obey the instructions for the wiring installation (Refer to ESPM 20-33-00). (c) Apply: Storage compound 15-008A As required to the screws after assembly. (3) Subtask 282148-900-202-001 - 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: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 37 6

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# @A310 SERVICE BULLETIN
**CONF 004 (1) Subtask 282148-910-401-001 - Standard Practices Manpower Resources Skills AIRFRAME References Structural Repair Manual (SRM) 51-23-10 51-40-21 51-40-44 (a) For material specification (Mat. No.) given in this Service Bulletin, refer to the Consumable Material List (CML). (b) For fastener hole and drill data (Refer to SRM 51-40-44). (c) For paint coatings (Refer to SRM 51-23-10). (d) Installation of fasteners (Refer to SRM 51-40-21). (2) Subtask 282148-910-204-001 - Standard Practices Manpower Resources Skills NON SPECIFIC Material necessary to do the job Consumable CMLD01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Storage compound 15-008A As required References Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001 Consumable Material List (CML) Elec. Std. Practices Manual (ESPM) 20-33-00 (a) For panel location (Refer to AMM 06-41-53, Page Block 001). (b) Obey the instructions for the wiring installation (Refer to ESPM 20-33-00). (c) Apply: Storage compound 15-008A As required to the screws after assembly.

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 38 6

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

# @A310 SERVICE BULLETIN (3) Subtask 282148-900-202-001 - 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 005 (1) Subtask 282148-910-401-001 - Standard Practices Manpower Resources Skills AIRFRAME References Structural Repair Manual (SRM) 51-23-10 51-40-21 51-40-44 (a) For material specification (Mat. No.) given in this Service Bulletin, refer to the Consumable Material List (CML). (b) For fastener hole and drill data (Refer to SRM 51-40-44). (c) For paint coatings (Refer to SRM 51-23-10). (d) Installation of fasteners (Refer to SRM 51-40-21). (2) Subtask 282148-910-204-001 - Standard Practices Manpower Resources Skills NON SPECIFIC Material necessary to do the job Consumable CMLD01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Storage compound 15-008A As required References Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001 Consumable Material List (CML) Elec. Std. Practices Manual (ESPM) 20-33-00 (a) For panel location (Refer to AMM 06-41-53, Page Block 001). (b) Obey the instructions for the wiring installation (Refer to ESPM 20-33-00).

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 39 6

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# @A310 SERVICE BULLETIN (c) Apply: Storage compound 15-008A As required to the screws after assembly. (3) Subtask 282148-900-202-001 - 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 006 (1) Subtask 282148-910-401-001 - Standard Practices Manpower Resources Skills AIRFRAME References Structural Repair Manual (SRM) 51-23-10 51-40-21 51-40-44 (a) For material specification (Mat. No.) given in this Service Bulletin, refer to the Consumable Material List (CML). (b) For fastener hole and drill data (Refer to SRM 51-40-44). (c) For paint coatings (Refer to SRM 51-23-10). (d) Installation of fasteners (Refer to SRM 51-40-21). (2) Subtask 282148-910-204-001 - Standard Practices Manpower Resources Skills NON SPECIFIC Material necessary to do the job Consumable CMLD01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Storage compound 15-008A As required References Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001 Consumable Material List (CML) Elec. Std. Practices Manual (ESPM) 20-33-00
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 40 6

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

# @A310 SERVICE BULLETIN (a) For panel location (Refer to AMM 06-41-53, Page Block 001). (b) Obey the instructions for the wiring installation (Refer to ESPM 20-33-00). (c) Apply: Storage compound 15-008A As required to the screws after assembly. (3) Subtask 282148-900-202-001 - 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 007 (1) Subtask 282148-910-401-001 - Standard Practices Manpower Resources Skills AIRFRAME References Structural Repair Manual (SRM) 51-23-10 51-40-21 51-40-44 (a) For material specification (Mat. No.) given in this Service Bulletin, refer to the Consumable Material List (CML). (b) For fastener hole and drill data (Refer to SRM 51-40-44). (c) For paint coatings (Refer to SRM 51-23-10). (d) Installation of fasteners (Refer to SRM 51-40-21). (2) Subtask 282148-910-204-001 - Standard Practices Manpower Resources Skills NON SPECIFIC Material necessary to do the job Consumable CMLD01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Storage compound 15-008A As required

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 41 6

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# @A310 SERVICE BULLETIN

References Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001 Consumable Material List (CML) Elec. Std. Practices Manual (ESPM) 20-33-00 (a) For panel location (Refer to AMM 06-41-53, Page Block 001). (b) Obey the instructions for the wiring installation (Refer to ESPM 20-33-00). (c) Apply: Storage compound 15-008A As required to the screws after assembly. (3) Subtask 282148-900-202-001 - 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 008 (1) Subtask 282148-910-401-001 - Standard Practices Manpower Resources Skills AIRFRAME References Structural Repair Manual (SRM) 51-23-10 51-40-21 51-40-44 (a) For material specification (Mat. No.) given in this Service Bulletin, refer to the Consumable Material List (CML). (b) For fastener hole and drill data (Refer to SRM 51-40-44). (c) For paint coatings (Refer to SRM 51-23-10). (d) Installation of fasteners (Refer to SRM 51-40-21). (2) Subtask 282148-910-204-001 - Standard Practices Manpower Resources Skills NON SPECIFIC

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 42 6

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# @A310 SERVICE BULLETIN
Material necessary to do the job Consumable CMLD01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Storage compound 15-008A As required References Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001 Consumable Material List (CML) Elec. Std. Practices Manual (ESPM) 20-33-00 (a) For panel location (Refer to AMM 06-41-53, Page Block 001). (b) Obey the instructions for the wiring installation (Refer to ESPM 20-33-00). (c) Apply: Storage compound 15-008A As required to the screws after assembly. (3) Subtask 282148-900-202-001 - Administrative Manpower Resources Skills NON SPECIFIC Write in the applicable aircraft records that you have done all the work given in this Service Bulletin. **CONF ALL B. PREPARATION **CONF 001 (1) Subtask 282148-941-001-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001 06-41-57, Page Block 001 24-00-00, Page Block 301 25-54-10, Page Block 201 52-10-00, Page Block 001 52-30-00, Page Block 001 53-10-55, Page Block 401 (a) Make sure that the aircraft is grounded (Refer to AMM 24-00-00, Page Block 301).
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 43 6

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# @A310 SERVICE BULLETIN (b) Put the access platform(s) in position. (c) Open the forward cargo compartment door 811 (Refer to AMM 52-30-00, Page Block 001). (d) Open the passenger/crew door 831 (Refer to AMM 52-10-00, Page Block 001). (e) In the forward cargo compartment, at FR38.2, remove the partition panel 132SW (Refer to AMM 06-41-53, Page Block 001 and AMM 53-10-55, Page Block 401). (f) In the forward cargo compartment, remove the sidewall panel 132QW (Refer to AMM 06-41-53, Page Block 001 and AMM 25-54-10, Page Block 201). (g) From the RH wing, remove the access panel 613RR (Refer to AMM 06-41-57, Page Block 001). (2) Subtask 282148-862-001-001 - De-energize Electrical Network (Safety Precautions) Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 24-31-11, Page Block 401 (a) Make sure that the external connector(s) is (are) not connected to the aircraft receptacle(s) EXT PW. (b) Make sure that there is (are) warning notice(s) on external power receptacle to tell persons not to connect an external power source. (c) Make sure that the EMER EXIT LT pushbutton switch on 436VU is on DISARM position. (d) In the cockpit, on the overhead panel 424VU release BAT pushbutton switches. (e) Put a warning notice on panel 424VU to tell persons not to operate the batteries. (f) Put a warning notice on the refuel/defuel panel 110VU to tell persons not to operate the NORMAL BATTERY switch. (g) Put a warning notice in the cockpit to tell persons not to start the APU. (h) Put a warning notice in the cockpit to tell persons not to start the ENG1,2. (i) Battery disconnection : - For job set-up, refer to removal/installation of the batteries (Refer to AMM 24-31-11, Page Block 401), - Turn the knurled nut a quarter turn, - Disconnect the connectors,

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 44 6

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# @A310 SERVICE BULLETIN - Put blanking caps on the disconnected electrical connectors. **CONF 002 (1) Subtask 282148-941-001-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001 06-41-57, Page Block 001 24-00-00, Page Block 301 25-54-10, Page Block 201 52-10-00, Page Block 001 52-30-00, Page Block 001 53-10-55, Page Block 401 (a) Make sure that the aircraft is grounded (Refer to AMM 24-00-00, Page Block 301). (b) Put the access platform(s) in position. (c) Open the forward cargo compartment door 811 (Refer to AMM 52-30-00, Page Block 001). (d) Open the passenger/crew door 831 (Refer to AMM 52-10-00, Page Block 001). (e) In the forward cargo compartment, at FR38.2, remove the partition panel 132SW (Refer to AMM 06-41-53, Page Block 001 and AMM 53-10-55, Page Block 401). (f) In the forward cargo compartment, remove the sidewall panel 132QW (Refer to AMM 06-41-53, Page Block 001 and AMM 25-54-10, Page Block 201). (g) From the RH wing, remove the access panel 613RR (Refer to AMM 06-41-57, Page Block 001). (2) Subtask 282148-862-001-001 - De-energize Electrical Network (Safety Precautions) Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 24-31-11, Page Block 401 (a) Make sure that the external connector(s) is (are) not connected to the aircraft receptacle(s) EXT PW. (b) Make sure that there is (are) warning notice(s) on external power receptacle to tell persons not to connect an external power source. (c) Make sure that the EMER EXIT LT pushbutton switch on 436VU is on DISARM position.
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 45 6

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# @A310 SERVICE BULLETIN (d) In the cockpit, on the overhead panel 424VU release BAT pushbutton switches. (e) Put a warning notice on panel 424VU to tell persons not to operate the batteries. (f) Put a warning notice on the refuel/defuel panel 110VU to tell persons not to operate the NORMAL BATTERY switch. (g) Put a warning notice in the cockpit to tell persons not to start the APU. (h) Put a warning notice in the cockpit to tell persons not to start the ENG1,2. (i) Battery disconnection : - For job set-up, refer to removal/installation of the batteries (Refer to AMM 24-31-11, Page Block 401), - Turn the knurled nut a quarter turn, - Disconnect the connectors, - Put blanking caps on the disconnected electrical connectors. **CONF 003 (1) Subtask 282148-941-001-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001 06-41-57, Page Block 001 24-00-00, Page Block 301 25-54-10, Page Block 201 52-10-00, Page Block 001 52-30-00, Page Block 001 53-10-55, Page Block 401 (a) Make sure that the aircraft is grounded (Refer to AMM 24-00-00, Page Block 301). (b) Put the access platform(s) in position. (c) Open the forward cargo compartment door 811 (Refer to AMM 52-30-00, Page Block 001). (d) Open the passenger/crew door 831 (Refer to AMM 52-10-00, Page Block 001). (e) In the forward cargo compartment, at FR38.2, remove the partition panel 132SW (Refer to AMM 06-41-53, Page Block 001 and AMM 53-10-55, Page Block 401). (f) In the forward cargo compartment, remove the sidewall panel 132QW (Refer to AMM 06-41-53, Page Block 001 and AMM 25-54-10, Page Block 201).

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 46 6

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# @A310 SERVICE BULLETIN (g) From the RH wing, remove the access panel 613RR (Refer to AMM 06-41-57, Page Block 001). (2) Subtask 282148-862-001-001 - De-energize Electrical Network (Safety Precautions) Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 24-31-11, Page Block 401 (a) Make sure that the external connector(s) is (are) not connected to the aircraft receptacle(s) EXT PW. (b) Make sure that there is (are) warning notice(s) on external power receptacle to tell persons not to connect an external power source. (c) Make sure that the EMER EXIT LT pushbutton switch on 436VU is on DISARM position. (d) In the cockpit, on the overhead panel 424VU release BAT pushbutton switches. (e) Put a warning notice on panel 424VU to tell persons not to operate the batteries. (f) Put a warning notice on the refuel/defuel panel 110VU to tell persons not to operate the NORMAL BATTERY switch. (g) Put a warning notice in the cockpit to tell persons not to start the APU. (h) Put a warning notice in the cockpit to tell persons not to start the ENG1,2. (i) Battery disconnection : - For job set-up, refer to removal/installation of the batteries (Refer to AMM 24-31-11, Page Block 401), - Turn the knurled nut a quarter turn, - Disconnect the connectors, - Put blanking caps on the disconnected electrical connectors. **CONF 004 (1) Subtask 282148-941-001-001 - Job Set-up Manpower Resources Skills NON SPECIFIC

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 47 6

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# @A310 SERVICE BULLETIN

References Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001 06-41-57, Page Block 001 24-00-00, Page Block 301 25-54-10, Page Block 201 52-10-00, Page Block 001 52-30-00, Page Block 001 53-10-55, Page Block 401 (a) Make sure that the aircraft is grounded (Refer to AMM 24-00-00, Page Block 301). (b) Put the access platform(s) in position. (c) Open the forward cargo compartment door 811 (Refer to AMM 52-30-00, Page Block 001). (d) Open the passenger/crew door 831 (Refer to AMM 52-10-00, Page Block 001). (e) In the forward cargo compartment, at FR38.2, remove the partition panel 132SW (Refer to AMM 06-41-53, Page Block 001 and AMM 53-10-55, Page Block 401). (f) In the forward cargo compartment, remove the sidewall panel 132QW (Refer to AMM 06-41-53, Page Block 001 and AMM 25-54-10, Page Block 201). (g) From the RH wing, remove the access panel 613RR (Refer to AMM 06-41-57, Page Block 001). (2) Subtask 282148-862-001-001 - De-energize Electrical Network (Safety Precautions) Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 24-31-11, Page Block 401 (a) Make sure that the external connector(s) is (are) not connected to the aircraft receptacle(s) EXT PW. (b) Make sure that there is (are) warning notice(s) on external power receptacle to tell persons not to connect an external power source. (c) Make sure that the EMER EXIT LT pushbutton switch on 436VU is on DISARM position. (d) In the cockpit, on the overhead panel 424VU release BAT pushbutton switches. (e) Put a warning notice on panel 424VU to tell persons not to operate the batteries. (f) Put a warning notice on the refuel/defuel panel 110VU to tell persons not to operate the NORMAL BATTERY switch. (g) Put a warning notice in the cockpit to tell persons not to start the APU.
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 48 6

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# @A310 SERVICE BULLETIN (h) Put a warning notice in the cockpit to tell persons not to start the ENG1,2. (i) Battery disconnection : - For job set-up, refer to removal/installation of the batteries (Refer to AMM 24-31-11, Page Block 401), - Turn the knurled nut a quarter turn, - Disconnect the connectors, - Put blanking caps on the disconnected electrical connectors. **CONF 005 (1) Subtask 282148-941-001-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001 06-41-57, Page Block 001 24-00-00, Page Block 301 25-54-10, Page Block 201 52-10-00, Page Block 001 52-30-00, Page Block 001 53-10-55, Page Block 401 (a) Make sure that the aircraft is grounded (Refer to AMM 24-00-00, Page Block 301). (b) Put the access platform(s) in position. (c) Open the forward cargo compartment door 811 (Refer to AMM 52-30-00, Page Block 001). (d) Open the passenger/crew door 831 (Refer to AMM 52-10-00, Page Block 001). (e) In the forward cargo compartment, at FR38.2, remove the partition panel 132SW (Refer to AMM 06-41-53, Page Block 001 and AMM 53-10-55, Page Block 401). (f) In the forward cargo compartment, remove the sidewall panel 132QW (Refer to AMM 06-41-53, Page Block 001 and AMM 25-54-10, Page Block 201). (g) From the RH wing, remove the access panel 613RR (Refer to AMM 06-41-57, Page Block 001). (2) Subtask 282148-862-001-001 - De-energize Electrical Network (Safety Precautions) Manpower Resources Skills NON SPECIFIC

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 49 6

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# @A310 SERVICE BULLETIN

References Aircraft Maintenance Manual (AMM) 24-31-11, Page Block 401 (a) Make sure that the external connector(s) is (are) not connected to the aircraft receptacle(s) EXT PW. (b) Make sure that there is (are) warning notice(s) on external power receptacle to tell persons not to connect an external power source. (c) Make sure that the EMER EXIT LT pushbutton switch on 436VU is on DISARM position. (d) In the cockpit, on the overhead panel 424VU release BAT pushbutton switches. (e) Put a warning notice on panel 424VU to tell persons not to operate the batteries. (f) Put a warning notice on the refuel/defuel panel 110VU to tell persons not to operate the NORMAL BATTERY switch. (g) Put a warning notice in the cockpit to tell persons not to start the APU. (h) Put a warning notice in the cockpit to tell persons not to start the ENG1,2. (i) Battery disconnection : - For job set-up, refer to removal/installation of the batteries (Refer to AMM 24-31-11, Page Block 401), - Turn the knurled nut a quarter turn, - Disconnect the connectors, - Put blanking caps on the disconnected electrical connectors. **CONF 006 (1) Subtask 282148-941-001-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001 06-41-57, Page Block 001 24-00-00, Page Block 301 25-54-10, Page Block 201 52-10-00, Page Block 001 52-30-00, Page Block 001 53-10-55, Page Block 401 (a) Make sure that the aircraft is grounded (Refer to AMM 24-00-00, Page Block 301). (b) Put the access platform(s) in position. DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 50 6

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# @A310 SERVICE BULLETIN (c) Open the forward cargo compartment door 811 (Refer to AMM 52-30-00, Page Block 001). (d) Open the passenger/crew door 831 (Refer to AMM 52-10-00, Page Block 001). (e) In the forward cargo compartment, at FR38.2, remove the partition panel 132SW (Refer to AMM 06-41-53, Page Block 001 and AMM 53-10-55, Page Block 401). (f) In the forward cargo compartment, remove the sidewall panel 132QW (Refer to AMM 06-41-53, Page Block 001 and AMM 25-54-10, Page Block 201). (g) From the RH wing, remove the access panel 613RR (Refer to AMM 06-41-57, Page Block 001). (2) Subtask 282148-862-001-001 - De-energize Electrical Network (Safety Precautions) Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 24-31-11, Page Block 401 (a) Make sure that the external connector(s) is (are) not connected to the aircraft receptacle(s) EXT PW. (b) Make sure that there is (are) warning notice(s) on external power receptacle to tell persons not to connect an external power source. (c) Make sure that the EMER EXIT LT pushbutton switch on 436VU is on DISARM position. (d) In the cockpit, on the overhead panel 424VU release BAT pushbutton switches. (e) Put a warning notice on panel 424VU to tell persons not to operate the batteries. (f) Put a warning notice on the refuel/defuel panel 110VU to tell persons not to operate the NORMAL BATTERY switch. (g) Put a warning notice in the cockpit to tell persons not to start the APU. (h) Put a warning notice in the cockpit to tell persons not to start the ENG1,2. (i) Battery disconnection : - For job set-up, refer to removal/installation of the batteries (Refer to AMM 24-31-11, Page Block 401), - Turn the knurled nut a quarter turn, - Disconnect the connectors, - Put blanking caps on the disconnected electrical connectors.

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 51 6

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# @A310 SERVICE BULLETIN
**CONF 007 (1) Subtask 282148-941-001-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001 06-41-57, Page Block 001 24-00-00, Page Block 301 25-54-10, Page Block 201 52-10-00, Page Block 001 52-30-00, Page Block 001 53-10-55, Page Block 401 (a) Make sure that the aircraft is grounded (Refer to AMM 24-00-00, Page Block 301). (b) Put the access platform(s) in position. (c) Open the forward cargo compartment door 811 (Refer to AMM 52-30-00, Page Block 001). (d) Open the passenger/crew door 831 (Refer to AMM 52-10-00, Page Block 001). (e) In the forward cargo compartment, at FR38.2, remove the partition panel 132SW (Refer to AMM 06-41-53, Page Block 001 and AMM 53-10-55, Page Block 401). (f) In the forward cargo compartment, remove the sidewall panel 132QW (Refer to AMM 06-41-53, Page Block 001 and AMM 25-54-10, Page Block 201). (g) From the RH wing, remove the access panel 613RR (Refer to AMM 06-41-57, Page Block 001). (2) Subtask 282148-862-001-001 - De-energize Electrical Network (Safety Precautions) Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 24-31-11, Page Block 401 (a) Make sure that the external connector(s) is (are) not connected to the aircraft receptacle(s) EXT PW. (b) Make sure that there is (are) warning notice(s) on external power receptacle to tell persons not to connect an external power source. (c) Make sure that the EMER EXIT LT pushbutton switch on 436VU is on DISARM position. (d) In the cockpit, on the overhead panel 424VU release BAT pushbutton switches.
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 52 6

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# @A310 SERVICE BULLETIN (e) Put a warning notice on panel 424VU to tell persons not to operate the batteries. (f) Put a warning notice on the refuel/defuel panel 110VU to tell persons not to operate the NORMAL BATTERY switch. (g) Put a warning notice in the cockpit to tell persons not to start the APU. (h) Put a warning notice in the cockpit to tell persons not to start the ENG1,2. (i) Battery disconnection : - For job set-up, refer to removal/installation of the batteries (Refer to AMM 24-31-11, Page Block 401), - Turn the knurled nut a quarter turn, - Disconnect the connectors, - Put blanking caps on the disconnected electrical connectors. **CONF 008 (1) Subtask 282148-941-001-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001 06-41-57, Page Block 001 24-00-00, Page Block 301 25-54-10, Page Block 201 52-10-00, Page Block 001 52-30-00, Page Block 001 53-10-55, Page Block 401 (a) Make sure that the aircraft is grounded (Refer to AMM 24-00-00, Page Block 301). (b) Put the access platform(s) in position. (c) Open the forward cargo compartment door 811 (Refer to AMM 52-30-00, Page Block 001). (d) Open the passenger/crew door 831 (Refer to AMM 52-10-00, Page Block 001). (e) In the forward cargo compartment, at FR38.2, remove the partition panel 132SW (Refer to AMM 06-41-53, Page Block 001 and AMM 53-10-55, Page Block 401). (f) In the forward cargo compartment, remove the sidewall panel 132QW (Refer to AMM 06-41-53, Page Block 001 and AMM 25-54-10, Page Block 201). (g) From the RH wing, remove the access panel 613RR (Refer to AMM 06-41-57, Page Block 001).
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 53 6

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# @A310 SERVICE BULLETIN (2) Subtask 282148-862-001-001 - De-energize Electrical Network (Safety Precautions) Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 24-31-11, Page Block 401 (a) Make sure that the external connector(s) is (are) not connected to the aircraft receptacle(s) EXT PW. (b) Make sure that there is (are) warning notice(s) on external power receptacle to tell persons not to connect an external power source. (c) Make sure that the EMER EXIT LT pushbutton switch on 436VU is on DISARM position. (d) In the cockpit, on the overhead panel 424VU release BAT pushbutton switches. (e) Put a warning notice on panel 424VU to tell persons not to operate the batteries. (f) Put a warning notice on the refuel/defuel panel 110VU to tell persons not to operate the NORMAL BATTERY switch. (g) Put a warning notice in the cockpit to tell persons not to start the APU. (h) Put a warning notice in the cockpit to tell persons not to start the ENG1,2. (i) Battery disconnection : - For job set-up, refer to removal/installation of the batteries (Refer to AMM 24-31-11, Page Block 401), - Turn the knurled nut a quarter turn, - Disconnect the connectors, - Put blanking caps on the disconnected electrical connectors.

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 54 6

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# @A310 SERVICE BULLETIN
**CONF ALL C. PROCEDURE **CONF 001 (1) Subtask 282148-831-405-001 - Install a New Bracket on the Sub Spar Behind the Front Spar Between RIB 8 and RIB 9 on the RH Wing Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills AIRFRAME Material necessary to do the job Kit 282148B01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 A5725068600000 1 Bracket 2 ASNA0078A502 2 Rivet Consumable CMLB01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Corrosion Inhibiting Low Adhesion Sealant 09-018 As required Solvent General Purpose 11-026 As required Lint-Free Cotton Cloth 19-003 As required References Fig. A-UBAAA Location of Bracket on the Sub Spar Behind the Front Spar Between RIB 8 and RIB 9 (RH Wing) Sheet 01

Refer to Fig. A-UBAAA Sheet 01 (a) Remove from the sub spar behind the front spar between RIB 8 and RIB 9 on the RH wing, the items that follow: 2 Rivet NSA54213510DCA Item (2) Discard 1 Bracket A5724630400000 Item (1) Discard (b) Clean the mating surfaces use Lint-Free Cotton Cloth 19-003 As required

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 55 6

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# @A310 SERVICE BULLETIN
made moist with Solvent General Purpose 11-026 As required (c) Put the 1 Bracket A5725068600000 Item 1 in position on the sub spar behind the front spar between RIB 8 and RIB 9 on the RH wing (Refer to Fig. A-UBAAA Sheet 01 ). (d) Copy drill the two holes from the sub spar through the Bracket, Item 1 to a dimension of between 4.060 and 4.160 mm (0.160 and 0.164 in.). (e) Deburr the holes that have been worked. (f) Use Corrosion Inhibiting Low Adhesion Sealant 09-018 As required

and wet install the 1 Bracket A5725068600000 Item 1 with the 2 Rivet, Blind ASNA0078A502 Item 2 on the sub spar behind the front spar between RIB 8 and RIB 9 on the RH wing. (2) Subtask 282148-831-004-001 - Install cable sleeves in the RH Electronics Rack 90VU. Manpower Resources Manhours 6.00 Minimum number of person 1 Subtask elapsed time 6.00 Skills NON SPECIFIC Material necessary to do the job Kit 282148A01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 ABS0596S004 2000 (mm) SLEEVE NSA935401-04 50 TIE

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 56 6

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# @A310 SERVICE BULLETIN

References Fig. A-FCAAA Installation of Cable Sleeves in the RH Electronics Rack 90VU. Sheet 01 Fig. A-FWAAA Installation of Cable Sleeves in the RH Electronics Rack 90VU. Sheet 01

NOTE: The sleeves ABS0596S004 and ABS0596S006 are supplied in pieces of 1000 mm (39.370 inches), cut or assemble these pieces to get the correct length. NOTE: The lengths of the sleeves given in this Service Bulletin are approximate lengths. Adapt the lengths of the sleeves in relation to the aircraft configuration. NOTE: Before you install a sleeve, cut and discard the cable ties around the cable bundle to install the sleeve correctly around the cable bundle. (a) On the Shelf 92VU, only around the wires identified in figure Fig. A-FWAAA Sheet 01 , from the equipment 15QT-B to the connector 2354VC, install: 1600 (mm) Sleeve ABS0596S004 Item 1 (b) Around the cable bundle of the connector 2354VC-A, install: 400 (mm) Sleeve ABS0596S004 Item 1 (c) Attach the sleeves with: 50 Tie-Cable NSA935401-04

(3) Subtask 282148-831-005-001 - Install cable sleeves between FR38.2 and FR39, in the forward cargo compartment. 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 282148A01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 2 ABS0596S006 1000 (mm) SLEEVE NSA935401-05 50 TIE

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 57 6

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# @A310 SERVICE BULLETIN

References Fig. A-FCBAA Installation of Cable Sleeves in the Forward Cargo Compartment. Sheet 01

NOTE: The sleeves ABS0596S004 and ABS0596S006 are supplied in pieces of 1000 mm (39.370 inches), cut or assemble these pieces to get the correct length. NOTE: The lengths of the sleeves given in this Service Bulletin are approximate lengths. Adapt the lengths of the sleeves in relation to the aircraft configuration. NOTE: Before you install a sleeve, cut and discard the cable ties around the cable bundle to install the sleeve correctly around the cable bundle. (a) Around the cable bundle of the pressure seal 20VP, install: 1000 (mm) Sleeve ABS0596S006 Item 2 (b) Attach the sleeves with: 50 Tie-Cable NSA935401-05

(4) Subtask 282148-831-006-001 - Install cable sleeves in the RH forward wing root and krueger flap. 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 282148A01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 2 ABS0596S006 1000 (mm) SLEEVE NSA935401-05 50 TIE References Fig. A-FCCAA Installation of Cable Sleeves in the RH forward wing root and krueger flap. Sheet 01
(a) Around the cable bundle of the pressure seal 20VP, install: 1000 (mm) Sleeve ABS0596S006 Item 2

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 58 6

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# @A310 SERVICE BULLETIN (b) Attach the sleeves with: 50 Tie-Cable NSA935401-05

(5) Subtask 282148-831-208-001 - Install the cable sleeves in the RH-wing forward of the front spar between rib 2 and rib 3 in zone 612. Manpower Resources Manhours 2.00 Minimum number of person 1 Subtask elapsed time 2.00 Skills ELECTRICAL Material necessary to do the job Kit 282148D01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 ABS0596S004 1 SLEEVE 11 MS21919WCH13 2 CLAMP 149 NSA935401-03 1 TIE 150 NSA935401-04 1 TIE References Fig. A-GBEAAImprovement of the 2S-Route in the RHWing in Zone 612 (Kit D01) Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Sheet 08 NOTE (1): The sleeve ABS0596S004 is supplied in pieces of 1000 mm. Cut or assemble these pieces to get the correct length. NOTE (2): The lengths of the sleeves given in this Service Bulletin are approximate lengths. Adapt the lengths of the sleeves in relation to the aircraft configuration. NOTE (3): Before you install a sleeve, cut and discard the cable ties around the cable bundle to install the sleeve correctly around the cable bundle. NOTE (4): Adapt the number of cable ties to the required quantity. Install the cable sleeves in the RH-wing forward of the front spar between rib 2 and rib 3 in zone 612. Refer to Fig. A-GBEAA Sheet 01 , Fig. A-GBEAA Sheet 02, Fig. A-GBEAA Sheet 03, Fig. A-GBEAA Sheet 04, Fig. A-GBEAA Sheet 05, Fig. A-GBEAA Sheet 06, Fig. A-GBEAA Sheet 07 and Fig. A-GBEAA Sheet 08
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 59 6

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# @A310 SERVICE BULLETIN (a) Remove these items from the bracket of the rib 2 and cable bundle 2S/624VB, as shown in Details A and B: 1 Clamp MS21919WCH4 Item (22) Retain 1 Clamp MS21919WCH3 Item (23) Retain 1 Spacer NSA5527-03-02D Item (31) Retain 1 Washer NAS1149D0332K Item (40) Retain 1 Screw NAS1096-3-21 Item (50) Retain 1 Clamp MS21919WCH10 Item (100) Retain 1 Clamp Item (100) Discard (b) Remove these items from the riblet and cable bundle 2S/624VB, as shown in Details A and D: 1 Clamp MS21919WCH4 Item (22) Retain 3 Spacer NSA5527-03-02D Item (31) Retain 1 Washer NAS1149D0332K Item (40) Retain 1 Screw NAS1096-3-38 Item (54) Retain 1 Clamp Item (100) Discard (c) Install this cable sleeve around these identified wires from the cable bundle 2S/624VB, as shown in Details A, C, E and F: Wire number 2842-5052 Wire number 2842-5053 Wire number 2842-5054 Wire number 2842-5055 Wire number 2842-5056 Wire number 2842-5070 1 Sleeve ABS0596S004 Item 1 and attach the cable sleeve with: 1 Tie NSA935401-03 Item 149 1 Tie-Cable NSA935401-04 Item 150 DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 60 6

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# @A310 SERVICE BULLETIN
as necessary. (d) Install these items to the bracket of the rib 2, cable bundle 2S/624VB and cable sleeve, Item 1, as shown in Details A and C: 1 Clamp MS21919WCH4 Item (22) Retained at removal 1 Clamp MS21919WCH3 Item (23) Retained at removal 1 Spacer NSA5527-03-02D Item (31) Retained at removal 1 Washer NAS1149D0332K Item (40) Retained at removal 1 Screw NAS1096-3-21 Item (50) Retained at removal 1 Clamp MS21919WCH10 Item (100) Retained at removal 1 Clamp MS21919WCH13 Item 11 (e) Install these items to the riblet, cable bundle 2S/624VB and cable sleeve, Item 1, as shown in Details A and E: 1 Clamp MS21919WCH4 Item (22) Retained at removal 3 Spacer NSA5527-03-02D Item (31) Retained at removal 1 Washer NAS1149D0332K Item (40) Retained at removal 1 Screw NAS1096-3-38 Item (54) Retained at removal 1 Clamp MS21919WCH13 Item 11

(6) Subtask 282148-831-209-001 - Install the cable sleeves in the RH-wing forward of the front spar between rib 7 and rib 8 in zone 612. Manpower Resources Manhours 2.00 Minimum number of person 1 Subtask elapsed time 2.00 Skills ELECTRICAL

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 61 6

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# @A310 SERVICE BULLETIN
Material necessary to do the job Kit 282148D01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 ABS0596S004 2 SLEEVE 12 MS21919WCH14 2 CLAMP 149 NSA935401-03 2 TIE 150 NSA935401-04 2 TIE References Fig. A-GBEAAImprovement of the 2S-Route in the RHWing in Zone 612 (Kit D01) Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Sheet 08 NOTE (1): The sleeves ABS0596S004 is supplied in pieces of 1000 mm. Cut or assemble these pieces to get the correct length. NOTE (2): The lengths of the sleeves given in this Service Bulletin are approximate lengths. Adapt the lengths of the sleeves in relation to the aircraft configuration. NOTE (3): Before you install a sleeve, cut and discard the cable ties around the cable bundle to install the sleeve correctly around the cable bundle. NOTE (4): Adapt the number of cable ties to the required quantity. Refer to Fig. A-GBEAA Sheet 01 , Fig. A-GBEAA Sheet 02, Fig. A-GBEAA Sheet 03, Fig. A-GBEAA Sheet 04, Fig. A-GBEAA Sheet 05, Fig. A-GBEAA Sheet 06, Fig. A-GBEAA Sheet 07 and Fig. A-GBEAA Sheet 08 (a) Remove these items from the two brackets of the riblets and cable bundle 2S/624VB, as shown in Details A, H and K: 2 Clamp MS21919WCH4 Item (22) Retain 2 Washer NAS1149D0332K Item (40) Retain 2 Screw NAS1096-3-8 Item (55) Retain 2 Clamp Item (100) Discard (b) Install this cable sleeve around these identified wires from the cable bundle 2S/624VB, as shown in Details A, J, K, L, M and N: Wire number 2842-5052
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 62 6

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# @A310 SERVICE BULLETIN
Wire number 2842-5053 Wire number 2842-5054 Wire number 2842-5055 Wire number 2842-5056 1 Sleeve ABS0596S004 Item 1 and attach the cable sleeves with: 1 Tie NSA935401-03 Item 149 1 Tie-Cable NSA935401-04 Item 150 (c) Install this cable sleeve around this identified wire from the cable bundle 2S/624VB, as shown in Details A, J, K, L, M and N: Wire number 2842-5070 1 Sleeve ABS0596S004 Item 1 and attach the cable sleeves with: 1 Tie NSA935401-03 Item 149 1 Tie-Cable NSA935401-04 Item 150 (d) Install these items to the two brackets of the riblets, cable bundle 2S/624VB and cable sleeves, Item 1, as shown in Detail A, J and L: 2 Clamp MS21919WCH4 Item (22) Retained at removal 2 Washer NAS1149D0332K Item (40) Retained at removal 2 Screw NAS1096-3-8 Item (55) Retained at removal 2 Clamp MS21919WCH14 Item 12

(7) Subtask 282148-831-210-001 - Install the cable sleeves in the RH-wing forward of the front spar between rib 8 and rib 9 (pylon area) in zone 612. Manpower Resources Manhours 4.00 Minimum number of person 1 Subtask elapsed time 4.00 Skills ELECTRICAL

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 63 6

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# @A310 SERVICE BULLETIN
Material necessary to do the job Kit 282148D02R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 ABS0596S004 2 SLEEVE 30 NSA5527-03-01D 2 SPACER 109 NSA935805-09 3 (ME) CONDUIT 117 NSA935807C09 13 CLAMP 125 B9299071900200 1 EQUIPMNT 126 NSA938184PV1601 15 PIN 149 NSA935401-03 20 TIE 150 NSA935401-04 20 TIE References Fig. A-GBGAAImprovement of the 2S-Route in the RHWing Pylon Area (Kit D02) Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Sheet 08 Fig. A-GHAAA Hook-up Chart Sheet 01 Fig. A-GHBAA Hook-up Chart Sheet 01
NOTE (1): The sleeves ABS0596S004 is supplied in pieces of 1000 mm. Cut or assemble these pieces to get the correct length. NOTE (2): The lengths of the sleeves given in this Service Bulletin are approximate lengths. Adapt the lengths of the sleeves in relation to the aircraft configuration. NOTE (3): Before you install a sleeve, cut and discard the cable ties around the cable bundle to install the sleeve correctly around the cable bundle. NOTE (4): Adapt the number of cable ties to the required quantity. Refer to Fig. A-GBGAA Sheet 01 , Fig. A-GBGAA Sheet 02, Fig. A-GBGAA Sheet 03, Fig. A-GBGAA Sheet 04, Fig. A-GBGAA Sheet 05, Fig. A-GBGAA Sheet 06, Fig. AGBGAA Sheet 07 and Fig. A-GBGAA Sheet 08 Refer to Fig. A-GHAAA Sheet 01 and Fig. A-GHBAA Sheet 01 (a) Disconnect these wires of route 2S from the receptacles 40VC and 5006VC in accordance with the Hook-up Chart 1, Lines 1 thru 14, END 1, Fig. A-GHAAA Sheet 01 and the Hook-up Chart 2, Lines 2 thru 8, END 1, Fig. A-GHBAA Sheet 01

.
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 64 6

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# @A310 SERVICE BULLETIN (b) Remove, refer to Fig. A-GBGAA Sheet 03, Detail D, BEFORE: 1 Spacer NSA5527-03-02D Item (31) Discard 1 Clamp NSA935807C10 Item (110) Discard 1 Clamp NSA935807C16 Item (111) Retain 1 Washer NSA935808-01 Item (112) Retain 1 Screw NAS1096-3-23 Item (113) Retain 1 Spacer NSA5527-03-05D Item (114) Discard 1 Washer NSA1149D0332K Item (115) Retain 1 Nut NAS1291C3M Item (116) Retain 1 Clamp NSA935807C09 Item (117) Retain (c) Remove, refer to Fig. A-GBGAA Sheet 04, Detail F, BEFORE: 2 Spacer NSA5527-03-01D Item (30) Retain 1 Spacer NSA5527-03-02D Item (31) Retain 1 Clamp NSA935807C10 Item (110) Retain 1 Clamp NSA935807C10 Item (110) Discard 1 Clamp NSA935807C16 Item (111) Retain 1 Washer NSA935808-01 Item (112) Retain 1 Clamp NSA935807C09 Item (117) Retain 1 Screw NAS1096-3-33 Item (118) Retain (d) Remove, refer to Fig. A-GBGAA Sheet 05, Detail H, BEFORE: 2 Spacer NSA5527-03-01D Item (30) Retain 2 Spacer NSA5527-03-02D Item (31) Retain 2 Clamp NSA935807C10 Item (110) Discard 2 Clamp NSA935807C16 Item (111) Retain

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 65 6

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# @A310 SERVICE BULLETIN
2 Spacer NSA5527-03-05D Item (114) Retain 2 Washer NSA1149D0332K Item (115) Retain 2 Clamp NSA935807C09 Item (117) Retain 2 Screw NAS1096-3-33 Item (118) Retain (e) Remove, refer to Fig. A-GBGAA Sheet 06, Detail K, BEFORE: 1 Spacer NSA5527-03-01D Item (30) Retain 1 Spacer NSA5527-03-02D Item (31) Retain 1 Clamp NSA935807C10 Item (110) Discard 1 Clamp NSA935807C16 Item (111) Retain 1 Spacer NSA5527-03-05D Item (114) Retain 1 Washer NSA1149D0332K Item (115) Retain 1 Clamp NSA935807C09 Item (117) Retain 1 Screw NAS1096-3-33 Item (118) Retain (f) Remove, refer to Fig. A-GBGAA Sheet 07, Detail M, BEFORE: 1 Spacer NSA5527-03-01D Item (30) Retain 1 Spacer NSA5527-03-02D Item (31) Retain 1 Clamp NSA935807C10 Item (110) Discard 1 Clamp NSA935807C16 Item (111) Retain 1 Washer NSA935808-01 Item (112) Retain 1 Spacer NSA5527-03-05D Item (114) Retain 1 Clamp NSA935807C09 Item (117) Retain 1 Screw NAS1096-3-33 Item (118) Retain (g) Remove, refer to Fig. A-GBGAA Sheet 08, Detail P, BEFORE: 1 Spacer NSA5527-03-02D Item (31) Retain

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 66 6

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# @A310 SERVICE BULLETIN
1 Clamp NSA935807C10 Item (110) Discard 1 Clamp NSA935807C16 Item (111) Retain 1 Washer NSA935808-01 Item (112) Retain 1 Spacer NSA5527-03-05D Item (114) Retain 1 Clamp NSA935807C09 Item (117) Retain 1 Screw NAS1096-3-25 Item (119) Retain (h) Remove the identification sleeves from the cable harnesses near the receptacles 40VC and 5006VC as shown Fig. A-GBGAA Sheet 01 , Detail A As required placard Item (125) Discard (i) Remove the protection sleeve from the cable harness as shown Fig. A-GBGAA Sheet 01 , Fig. A-GBGAA Sheet 02, Fig. A-GBGAA Sheet 03, Fig. A-GBGAA Sheet 04, Fig. A-GBGAA Sheet 05, Fig. A-GBGAA Sheet 06, Fig. A-GBGAA Sheet 07 and Fig. A-GBGAA Sheet 08, Details D, F, H, K, M and P: 1 Sleeve NSA935805-10 Item (109) Discard (j) Cut the conduit to the required length and install as shown Fig. A-GBGAA Sheet 01 , Fig. A-GBGAA Sheet 02, Fig. A-GBGAA Sheet 03, Fig. A-GBGAA Sheet 04, Fig. A-GBGAA Sheet 05, Fig. A-GBGAA Sheet 06, Fig. A-GBGAA Sheet 07 and Fig. A-GBGAA Sheet 08, Details E, G, J, L, N and Q: 3 (ME) Conduit NSA935805-09 Item 109 1 One part 1500.0 mm (59.06 in.) to the electrical wires for 10QT-A and 10QT-B of route 2S/636VB, refer to the Hook-up Chart 2, Fig. A-GHBAA Sheet 01 2 Three parts, one 520 mm (20.47 in.) and two 240.0 mm (9.45 in.) to the remaining electrical wires of route 2S/636VB, refer to Fig. A-GHAAA Sheet 01 (k) Connect the electrical wires of route 2S to the receptacles 40VC and 5006VC in accordance with the Hook-up Chart 1, Lines 1 thru 14, END 1, Fig. A-GHAAA Sheet 01 and the Hook-up Chart 2, lines 2 thru 8, END 1, Fig. A-GHBAA Sheet 01

. Use the contact pins if required: 15 Pin NSA938184PV1601 Item 126 (l) Install, refer to Fig. A-GBGAA Sheet 08, Detail Q, AFTER: 1 Spacer NSA5527-03-02D Item (31) Retained at removal 1 Clamp NSA935807C16 Item (111) Retained at removal DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 67 6

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# @A310 SERVICE BULLETIN
1 Washer NSA935808-01 Item (112) Retained at removal 1 Spacer NSA5527-03-05D Item (114) Retained at removal 2 Clamp NSA935807C09 Item (117) Retained at removal 1 Screw NAS1096-3-25 Item (119) Retained at removal 1 Clamp NSA935807C09 Item 117 (m) Install, refer to Fig. A-GBGAA Sheet 07, Detail N, AFTER: 1 Spacer NSA5527-03-01D Item (30) Retained at removal 1 Spacer NSA5527-03-02D Item (31) Retained at removal 1 Clamp NSA935807C16 Item (111) Retained at removal 1 Washer NSA935808-01 Item (112) Retained at removal 1 Spacer NSA5527-03-05D Item (114) Retained at removal 1 Clamp NSA935807C09 Item (117) Retained at removal 1 Screw NAS1096-3-33 Item (118) Retained at removal 2 Clamp NSA935807C09 Item 117 (n) Install, refer to Fig. A-GBGAA Sheet 06, Detail L, AFTER: 1 Spacer NSA5527-03-01D Item (30) Retained at removal 1 Spacer NSA5527-03-02D Item (31) Retained at removal 1 Clamp NSA935807C16 Item (111) Retained at removal 1 Spacer NSA5527-03-05D Item (114) Retained at removal DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 68 6

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# @A310 SERVICE BULLETIN
1 Washer NSA1149D0332K Item (115) Retained at removal 1 Clamp NSA935807C09 Item (117) Retained at removal 1 Screw NAS1096-3-33 Item (118) Retained at removal 2 Clamp NSA935807C09 Item 117 (o) Install, refer to Fig. A-GBGAA Sheet 05, Detail J, AFTER: 2 Spacer NSA5527-03-01D Item (30) Retained at removal 2 Spacer NSA5527-03-02D Item (31) Retained at removal 2 Clamp NSA935807C16 Item (111) Retained at removal 2 Spacer NSA5527-03-05D Item (114) Retained at removal 2 Washer NSA1149D0332K Item (115) Retained at removal 2 Clamp NSA935807C09 Item (117) Retained at removal 2 Screw NAS1096-3-33 Item (118) Retained at removal 4 Clamp NSA935807C09 Item 117 (p) Install, refer to Fig. A-GBGAA Sheet 04, Detail G, AFTER: 2 Spacer NSA5527-03-01D Item (30) Retained at removal 1 Spacer NSA5527-03-02D Item (31) Retained at removal 1 Clamp NSA935807C10 Item (110) Retained at removal 1 Clamp NSA935807C16 Item (111) Retained at removal 1 Washer NSA935808-01 Item (112) Retained at removal DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 69 6

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# @A310 SERVICE BULLETIN
1 Clamp NSA935807C09 Item (117) Retained at removal 1 Screw NAS1096-3-33 Item (118) Retained at removal 2 Clamp NSA935807C09 Item 117 (q) Install, refer to Fig. A-GBGAA Sheet 03, Detail E, AFTER: 2 Spacer NSA5527-03-01D Item 30 1 Clamp NSA935807C16 Item (111) Retained at removal 1 Washer NSA935808-01 Item (112) Retained at removal 1 Screw NAS1096-3-23 Item (113) Retained at removal 1 Washer NSA1149D0332K Item (115) Retained at removal 1 Nut NAS1291C3M Item (116) Retained at removal 1 Clamp NSA935807C09 Item (117) Retained at removal 2 Clamp NSA935807C09 Item 117 (r) Protect the electrical wires for 10QT-A and 10QT-B of route 2S/636VB, refer to the Hook-up Chart 2, Fig. A-GHBAA Sheet 01 with: 2 Sleeve ABS0596S004 Item 1 and 20 Tie NSA935401-03 Item 149 20 Tie-Cable NSA935401-04 Item 150 (s) Install the identification placards: 1 Placard set B9299071900200 Item 125

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 70 6

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# @A310 SERVICE BULLETIN (8) Subtask 282148-831-211-001 - Install the cable sleeves in the RH-wing forward of the front spar between rib 9 and rib 12 in zone 623. Manpower Resources Manhours 4.00 Minimum number of person 1 Subtask elapsed time 4.00 Skills ELECTRICAL Material necessary to do the job Kit 282148D01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 ABS0596S004 3 SLEEVE 10 MS21919WCH9 8 CLAMP 14 NAS1096-3-19 2 SCREW 15 NSA5527-03-03 3 SPACER 16 NSA8420-2 0.5 (ME) CORD 149 NSA935401-03 1 TIE 150 NSA935401-04 1 TIE Kit 282148D02R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 31 NSA5527-03-02D 2 SPACER 121 NAS1096-3-40 1 SCREW References Fig. A-GBFAAImprovement of the 2S-Route in the RHWing in Zone 623 (Kit D01) Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Sheet 08 Sheet 09 Sheet 10 NOTE (1): The sleeves ABS0596S004 is supplied in pieces of 1000 mm. Cut or assemble these pieces to get the correct length. NOTE (2): The lengths of the sleeves given in this Service Bulletin are approximate lengths. Adapt the lengths of the sleeves in relation to the aircraft configuration. NOTE (3): Before you install a sleeve, cut and discard the cable ties around the cable bundle to install the sleeve correctly around the cable bundle.

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 71 6

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# @A310 SERVICE BULLETIN
NOTE (4): Adapt the number of cable ties to the required quantity. Refer to Fig. A-GBFAA Sheet 01 , Fig. A-GBFAA Sheet 02, Fig. A-GBFAA Sheet 03, Fig. A-GBFAA Sheet 04, Fig. A-GBFAA Sheet 05, Fig. A-GBFAA Sheet 06, Fig. A-GBFAA Sheet 07, Fig. A-GBFAA Sheet 08, Fig. A-GBFAA Sheet 09 and Fig. A-GBFAA Sheet 10 (a) At one position, remove these items from the bracket between rib 11 and rib 12 and cable bundle 2S/636VB, as shown in Details A and D: 2 Clamp MS21919WCH4 Item (22) Retain 1 Clamp MS21919WCH4 Item (22) Discard 1 Clamp MS21919WCH3 Item (23) Retain 1 Spacer NSA5527-03-01D Item (30) Retain 1 Spacer NSA5527-03-02D Item (31) Retain 1 Washer NSA935808-01 Item (112) Retain 1 Screw NAS1096-3-30 Item (121) Discard 1 Clamp NSA935807-06 Item (122) Retain (b) At two positions, remove these items from the brackets between rib 10 and rib 11 and between rib 11 and rib 12 and cable bundle 2S/636VB, as shown in Details A and F: 2 Clamp Item (22) Discard 6 Clamp MS21919WCH4 Item (22) Retain 4 Spacer NSA5527-03-01D Item (30) Retain 2 Washer NAS1149D0332K Item (40) Retain 2 Screw NAS1096-3-27 Item (52) Retain (c) At two positions, remove these items from the brackets of the rib 11 and cable bundle 2S/636VB, as shown in Details A and H: 2 Clamp MS21919WCH4 Item (22) Retain 1 Clamp Item (23) Discard 1 Spacer NSA5527-03-01D Item (30) Retain 1 Spacer NSA5527-03-04D Item (32) Retain

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 72 6

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# @A310 SERVICE BULLETIN
1 Washer NAS1149D0332K Item (40) Retain 1 Screw NAS1096-3-22 Item (51) Retain (d) At two positions, remove these items from the brackets of the rib 10 and cable bundle 2S/636VB, as shown in Details A and K: 2 Clamp Item (22) Discard 2 Clamp MS21919WCH4 Item (22) Retain 2 Spacer NSA5527-03-01D Item (30) Retain 2 Spacer Item (32) Discard 2 Washer NAS1149D0332K Item (40) Retain 2 Screw Item (51) Discard (e) Remove these items from the bracket between rib 9 and rib 10 and cable bundle 2S/636VB, as shown in Details A and M: 3 Clamp MS21919WCH4 Item (22) Retain 1 Clamp Item (23) Discard 1 Spacer NSA5527-03-01D Item (30) Retain 1 Spacer NSA5527-03-04D Item (32) Retain 1 Washer NAS1149D0332K Item (40) Retain 1 Screw NAS1096-3-22 Item (51) Retain (f) Remove these items from the bracket of the rib 9 and cable bundle 2S/636VB, as shown in Details A and T: 1 Clamp Item (21) Discard 1 Clamp MS21919WCH5 Item (21) Retain 1 Spacer NSA5527-03-02D Item (31) Retain 1 Spacer NSA5527-03-04D Item (32) Retain 1 Washer NAS1149D0332K Item (40) Retain 1 Screw NAS1096-3-27 Item (52) Retain

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 73 6

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# @A310 SERVICE BULLETIN (g) Install this cable sleeve around these identified wires from the cable bundle 2S/636VB, as shown in Details A, C, E, G, J, L, N, A and R: Wire number 2842-5061 Wire number 2842-5062 Wire number 2842-5063 Wire number 2842-5064 Wire number 2842-5065 Wire number 2842-5071 3 Sleeve ABS0596S004 Item 1 and attach the cable sleeves with: 3 Spacer NSA5527-03-03 Item 15 0.5 (ME) Cord NSA8420-2 Item 16 1 Tie NSA935401-03 Item 149 1 Tie-Cable NSA935401-04 Item 150 (h) At one positions, install these items to the brackets between rib 10 and rib 11 and between rib 11 and rib 12, cable sleeves, Item 1 and cable bundle 2S/636VB, as shown in Details A and E: 2 Clamp MS21919WCH4 Item (22) Retained at removal 1 Clamp MS21919WCH3 Item (23) Retained at removal 1 Spacer NSA5527-03-01D Item (30) Retained at removal 1 Spacer NSA5527-03-02D Item (31) Retained at removal 1 Washer NSA935808-01 Item (112) Retained at removal 1 Clamp NSA935807-06 Item (122) Retained at removal 1 Clamp MS21919WCH9 Item 10 2 Spacer NSA5527-03-02D Item 31
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 74 6

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# @A310 SERVICE BULLETIN

1 Screw NAS1096-3-40 Item 121 (i) At two positions, install these items to the brackets between rib 10 and rib 11 and between rib 11 and rib 12, cable sleeves, Item 1 and cable bundle 2S/636VB, as shown in Details A and G: 6 Clamp MS21919WCH4 Item (22) Retained at removal 4 Spacer NSA5527-03-01D Item (30) Retained at removal 2 Washer NAS1149D0332K Item (40) Retained at removal 2 Screw NAS1096-3-27 Item (52) Retained at removal 2 Clamp MS21919WCH9 Item 10 (j) At two positions, install these items to the brackets of the rib 11, cable sleeves, Item 1 and cable bundle 2S/636VB, as shown in Details A and J: 2 Clamp MS21919WCH4 Item (22) Retained at removal 1 Spacer NSA5527-03-01D Item (30) Retained at removal 1 Spacer NSA5527-03-04D Item (32) Retained at removal 1 Washer NAS1149D0332K Item (40) Retained at removal 1 Screw NAS1096-3-22 Item (51) Retained at removal 1 Clamp MS21919WCH9 Item 10 (k) At two positions, install these items to the brackets of the rib 10, cable sleeves, Item 1 and cable bundle 2S/636VB, as shown in Details A and L: 2 Clamp MS21919WCH4 Item (22) Retained at removal 2 Spacer NSA5527-03-01D Item (30) Retained at removal 2 Washer NAS1149D0332K Item (40) Retained at removal

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 75 6

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# @A310 SERVICE BULLETIN
2 Clamp MS21919WCH9 Item 10 2 Screw NAS1096-3-19 Item 14 (l) Install these items to the bracket between rib 9 and rib 10, cable sleeves, Item 1 and cable bundle 2S/636VB, as shown in Details A and N: 3 Clamp MS21919WCH4 Item (22) Retained at removal 1 Spacer NSA5527-03-01D Item (30) Retained at removal 1 Spacer NSA5527-03-04D Item (32) Retained at removal 1 Washer NAS1149D0332K Item (40) Retained at removal 1 Screw NAS1096-3-22 Item (51) Retained at removal 1 Clamp MS21919WCH9 Item 10 (m) Install these items to the bracket of the rib 9, cable sleeves, Item 1 and cable bundle 2S/636VB, as shown in Details A and Q: 1 Clamp MS21919WCH5 Item (21) Retained at removal 1 Spacer NSA5527-03-02D Item (31) Retained at removal 1 Spacer NSA5527-03-04D Item (32) Retained at removal 1 Washer NAS1149D0332K Item (40) Retained at removal 1 Screw NAS1096-3-27 Item (52) Retained at removal 1 Clamp MS21919WCH9 Item 10

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 76 6

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# @A310 SERVICE BULLETIN
**CONF 002 (1) Subtask 282148-831-405-001 - Install a New Bracket on the Sub Spar Behind the Front Spar Between RIB 8 and RIB 9 on the RH Wing Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills AIRFRAME Material necessary to do the job Kit 282148B01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 A5725068600000 1 Bracket 2 ASNA0078A502 2 Rivet Consumable CMLB01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Corrosion Inhibiting Low Adhesion Sealant 09-018 As required Solvent General Purpose 11-026 As required Lint-Free Cotton Cloth 19-003 As required References Fig. A-UBAAA Location of Bracket on the Sub Spar Behind the Front Spar Between RIB 8 and RIB 9 (RH Wing) Sheet 01

Refer to Fig. A-UBAAA Sheet 01 (a) Remove from the sub spar behind the front spar between RIB 8 and RIB 9 on the RH wing, the items that follow: 2 Rivet NSA54213510DCA Item (2) Discard 1 Bracket A5724630400000 Item (1) Discard (b) Clean the mating surfaces use Lint-Free Cotton Cloth 19-003 As required

made moist with

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 77 6

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# @A310 SERVICE BULLETIN

Solvent General Purpose 11-026 As required (c) Put the 1 Bracket A5725068600000 Item 1 in position on the sub spar behind the front spar between RIB 8 and RIB 9 on the RH wing (Refer to Fig. A-UBAAA Sheet 01 ). (d) Copy drill the two holes from the sub spar through the Bracket, Item 1 to a dimension of between 4.060 and 4.160 mm (0.160 and 0.164 in.). (e) Deburr the holes that have been worked. (f) Use Corrosion Inhibiting Low Adhesion Sealant 09-018 As required

and wet install the 1 Bracket A5725068600000 Item 1 with the 2 Rivet, Blind ASNA0078A502 Item 2 on the sub spar behind the front spar between RIB 8 and RIB 9 on the RH wing. (2) Subtask 282148-831-004-001 - Install cable sleeves in the RH Electronics Rack 90VU. Manpower Resources Manhours 6.00 Minimum number of person 1 Subtask elapsed time 6.00 Skills NON SPECIFIC Material necessary to do the job Kit 282148A01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 ABS0596S004 2000 (mm) SLEEVE NSA935401-04 50 TIE References Fig. A-FCAAA Installation of Cable Sleeves in the RH Electronics Rack 90VU. Sheet 01

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 78 6

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# @A310 SERVICE BULLETIN

References Fig. A-FWAAA Installation of Cable Sleeves in the RH Electronics Rack 90VU. Sheet 01

NOTE: The sleeves ABS0596S004 and ABS0596S006 are supplied in pieces of 1000 mm (39.370 inches), cut or assemble these pieces to get the correct length. NOTE: The lengths of the sleeves given in this Service Bulletin are approximate lengths. Adapt the lengths of the sleeves in relation to the aircraft configuration. NOTE: Before you install a sleeve, cut and discard the cable ties around the cable bundle to install the sleeve correctly around the cable bundle. (a) On the Shelf 92VU, only around the wires identified in figure Fig. A-FWAAA Sheet 01 , from the equipment 15QT-B to the connector 2354VC, install: 1600 (mm) Sleeve ABS0596S004 Item 1 (b) Around the cable bundle of the connector 2354VC-A, install: 400 (mm) Sleeve ABS0596S004 Item 1 (c) Attach the sleeves with: 50 Tie-Cable NSA935401-04

(3) Subtask 282148-831-005-001 - Install cable sleeves between FR38.2 and FR39, in the forward cargo compartment. 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 282148A01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 2 ABS0596S006 1000 (mm) SLEEVE NSA935401-05 50 TIE References Fig. A-FCBAA Installation of Cable Sleeves in the Forward Cargo Compartment. Sheet 01

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 79 6

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# @A310 SERVICE BULLETIN
NOTE: The sleeves ABS0596S004 and ABS0596S006 are supplied in pieces of 1000 mm (39.370 inches), cut or assemble these pieces to get the correct length. NOTE: The lengths of the sleeves given in this Service Bulletin are approximate lengths. Adapt the lengths of the sleeves in relation to the aircraft configuration. NOTE: Before you install a sleeve, cut and discard the cable ties around the cable bundle to install the sleeve correctly around the cable bundle. (a) Around the cable bundle of the pressure seal 20VP, install: 1000 (mm) Sleeve ABS0596S006 Item 2 (b) Attach the sleeves with: 50 Tie-Cable NSA935401-05

(4) Subtask 282148-831-006-001 - Install cable sleeves in the RH forward wing root and krueger flap. 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 282148A01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 2 ABS0596S006 1000 (mm) SLEEVE NSA935401-05 50 TIE References Fig. A-FCCAA Installation of Cable Sleeves in the RH forward wing root and krueger flap. Sheet 01
(a) Around the cable bundle of the pressure seal 20VP, install: 1000 (mm) Sleeve ABS0596S006 Item 2 (b) Attach the sleeves with: 50 Tie-Cable NSA935401-05

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 80 6

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# @A310 SERVICE BULLETIN (5) Subtask 282148-831-208-002 - Install the cable sleeves in the RH-wing forward of the front spar between rib 2 and rib 3 in zone 612. Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills ELECTRICAL Material necessary to do the job Kit 282148D01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 ABS0596S004 1 SLEEVE 11 MS21919WCH13 CLAMP 149 NSA935401-03 1 TIE 150 NSA935401-04 1 TIE References Fig. A-GBEAAImprovement of the 2S-Route in the RHWing in Zone 612 (Kit D01) Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Sheet 08 NOTE (1): The sleeves ABS0596S004 is supplied in pieces of 1000 mm. Cut or assemble these pieces to get the correct length. NOTE (2): The lengths of the sleeves given in this Service Bulletin are approximate lengths. Adapt the lengths of the sleeves in relation to the aircraft configuration. NOTE (3): Before you install a sleeve, cut and discard the cable ties around the cable bundle to install the sleeve correctly around the cable bundle. NOTE (4): Adapt the number of cable ties to the required quantity. Refer to Fig. A-GBEAA Sheet 01 , Fig. A-GBEAA Sheet 02, Fig. A-GBEAA Sheet 03, Fig. A-GBEAA Sheet 04, Fig. A-GBEAA Sheet 05, Fig. A-GBEAA Sheet 06, Fig. A-GBEAA Sheet 07 and Fig. A-GBEAA Sheet 08 (a) Remove these items from the bracket of the rib 2 and cable bundle 2S/624VB, as shown in Details A and B: 1 Clamp MS21919WCH4 Item (22) Retain 1 Clamp MS21919WCH3 Item (23) Retain
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 81 6

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# @A310 SERVICE BULLETIN
1 Spacer NSA5527-03-02D Item (31) Retain 1 Washer NAS1149D0332K Item (40) Retain 1 Screw NAS1096-3-21 Item (50) Retain 1 Clamp MS21919WCH10 Item (100) Retain 1 Clamp Item (100) Discard (b) Remove these items from the riblet and cable bundle 2S/624VB, as shown in Details A and D: 1 Clamp MS21919WCH4 Item (22) Retain 3 Spacer NSA5527-03-02D Item (31) Retain 1 Washer NAS1149D0332K Item (40) Retain 1 Screw NAS1096-3-38 Item (54) Retain 1 Clamp Item (100) Discard (c) Install this cable sleeve around these identified wires from the cable bundle 2S/624VB, as shown in Details A, C, E and F: Wire number 2842-5052 Wire number 2842-5053 Wire number 2842-5054 Wire number 2842-5055 Wire number 2842-5056 Wire number 2842-5070 Install this cable sleeve around these identified wires from the cable bundle 2S/624VB, as shown in Details A, C, E and F: Wire number 2842-5052 Wire number 2842-5053 Wire number 2842-5054 Wire number 2842-5055 Wire number 2842-5056 Wire number 2842-5070 DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 82 6

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# @A310 SERVICE BULLETIN

1 Sleeve ABS0596S004 Item 1 and attach the cable sleeve with: 1 Tie NSA935401-03 Item 149 1 Tie-Cable NSA935401-04 Item 150 (d) Install these items to the bracket of the rib 2, cable bundle 2S/624VB and cable sleeve, Item 1, as shown in Details A and C: 1 Clamp MS21919WCH4 Item (22) Retained at removal 1 Clamp MS21919WCH3 Item (23) Retained at removal 1 Spacer NSA5527-03-02D Item (31) Retained at removal 1 Washer NAS1149D0332K Item (40) Retained at removal 1 Screw NAS1096-3-21 Item (50) Retained at removal 1 Clamp MS21919WCH10 Item (100) Retained at removal 1 Clamp MS21919WCH13 Item 11 (e) Install these items to the riblet, cable bundle 2S/624VB and cable sleeve, Item 1, as shown in Details A and E: 1 Clamp MS21919WCH4 Item (22) Retained at removal 3 Spacer NSA5527-03-02D Item (31) Retained at removal 1 Washer NAS1149D0332K Item (40) Retained at removal 1 Screw NAS1096-3-38 Item (54) Retained at removal 1 Clamp MS21919WCH13 Item 11

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 83 6

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# @A310 SERVICE BULLETIN (6) Subtask 282148-831-209-002 - Install the cable sleeves in the RH-wing forward of the front spar between rib 7 and rib 8 in zone 612. Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills ELECTRICAL Material necessary to do the job Kit 282148D01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 ABS0596S004 2 SLEEVE 12 MS21919WCH14 CLAMP 149 NSA935401-03 2 TIE 150 NSA935401-04 2 TIE References Fig. A-GBEAAImprovement of the 2S-Route in the RHWing in Zone 612 (Kit D01) Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Sheet 08 NOTE (1): The sleeves ABS0596S004 is are supplied in pieces of 1000 mm. Cut or assemble these pieces to get the correct length. NOTE (2): The lengths of the sleeves given in this Service Bulletin are approximate lengths. Adapt the lengths of the sleeves in relation to the aircraft configuration. NOTE (3): Before you install a sleeve, cut and discard the cable ties around the cable bundle to install the sleeve correctly around the cable bundle. NOTE (4): Adapt the number of cable ties to the required quantity. Refer to Fig. A-GBEAA Sheet 01 , Fig. A-GBEAA Sheet 02, Fig. A-GBEAA Sheet 03, Fig. A-GBEAA Sheet 04, Fig. A-GBEAA Sheet 05, Fig. A-GBEAA Sheet 06, Fig. A-GBEAA Sheet 07 and Fig. A-GBEAA Sheet 08 (a) Remove these items from the two brackets of the riblets and cable bundle 2S/624VB, as shown in Details A, H and K: 2 Clamp MS21919WCH4 Item (22) Retain 2 Washer NAS1149D0332K Item (40) Retain DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 84 6

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# @A310 SERVICE BULLETIN
2 Screw NAS1096-3-8 Item (55) Retain 2 Clamp Item (100) Discard (b) Install this cable sleeve around these identified wires from the cable bundle 2S/624VB, as shown in Details A, J, K, L, M and N: Wire number 2842-5052 Wire number 2842-5053 Wire number 2842-5054 Wire number 2842-5055 Wire number 2842-5056 1 Sleeve ABS0596S004 Item 1 and attach the cable sleeves with: 1 Tie NSA935401-03 Item 149 1 Tie-Cable NSA935401-04 Item 150 (c) Install this cable sleeve around this identified wire from the cable bundle 2S/624VB, as shown in Details A, J, K, L, M and N: Wire number 2842-5070 1 Sleeve ABS0596S004 Item 1 and attach the cable sleeves with: 1 Tie NSA935401-03 Item 149 1 Tie-Cable NSA935401-04 Item 150 (d) Install these items to the two brackets of the riblets, cable bundle 2S/624VB and cable sleeves, Item 1, as shown in Detail A, J and L: 2 Clamp MS21919WCH4 Item (22) Retained at removal 2 Washer NAS1149D0332K Item (40) Retained at removal 2 Screw NAS1096-3-8 Item (55) Retained at removal 2 Clamp MS21919WCH14 Item 12

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 85 6

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# @A310 SERVICE BULLETIN (7) Subtask 282148-831-210-002 - Install the cable sleeves in the RH-wing forward of the front spar between rib 8 and rib 9 (pylon area) in zone 612. Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills ELECTRICAL Material necessary to do the job Kit 282148D02R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 109 NSA935805-09 CONDUIT Kit 282148D03R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 ABS0596S004 3 SLEEVE 31 NSA5527-03-02D 1 SPACER 117 NSA935807C09 7 CLAMP 123 NAS1801-3-31 3 SCREW 126 NSA938184PV1601 7 PIN 130 NSA5527-03-08D 1 SPACER 131 NSA5527-03-07D 1 SPACER 132 B9299071900600 1 EQUIPMNT 149 NSA935401-03 20 TIE 150 NSA935401-04 20 TIE References Fig. A-GBHAAImprovement of the 2S-Route in the RHWing Pylon Area (Kit D03) Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Sheet 08 Fig. A-GHBAA Hook-up Chart Sheet 01
NOTE (1): The sleeves ABS0596S004 is supplied in pieces of 1000 mm. Cut or assemble these pieces to get the correct length. NOTE (2): The lengths of the sleeves given in this Service Bulletin are approximate lengths. Adapt the lengths of the sleeves in relation to the aircraft configuration.

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 86 6

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# @A310 SERVICE BULLETIN
NOTE (3): Before you install a sleeve, cut and discard the cable ties around the cable bundle to install the sleeve correctly around the cable bundle. NOTE (4): Adapt the number of cable ties to the required quantity. Refer to Fig. A-GBHAA Sheet 01 , Fig. A-GBHAA Sheet 02, Fig. A-GBHAA Sheet 03, Fig. A-GBHAA Sheet 04, Fig. A-GBHAA Sheet 05, Fig. A-GBHAA Sheet 06, Fig. AGBHAA Sheet 07 and Fig. A-GBHAA Sheet 08 (a) Disconnect the wires of route 2S from the receptacles 40VC and 5006VC in accordance with the Hook-up Chart 2, Lines 2 thru 8, END 1, Fig. A-GHBAA Sheet 01

. (b) Remove, refer to Fig. A-GBHAA Sheet 03, Detail D, BEFORE: 1 Spacer NSA5527-03-02D Item (31) Retain 2 Clamp NSA935807C16 Item (111) Retain 1 Washer NSA935808-01 Item (112) Retain 1 Screw NAS1096-3-23 Item (113) Retain 1 Spacer NSA5527-03-05D Item (114) Retain 1 Nut NAS1291C3M Item (116) Retain 1 Washer AN960KD10l Item (124) Retain (c) Remove, refer to Fig. A-GBHAA Sheet 04, Detail F, BEFORE: 1 Spacer NSA5527-03-02D Item (31) Retain 2 Clamp NSA935807C16 Item (111) Retain 1 Washer NSA935808-01 Item (112) Retain 1 Screw NAS1096-3-23 Item (113) Retain 1 Spacer NSA5527-03-05D Item (114) Retain (d) Remove, refer to Fig. A-GBHAA Sheet 05, Detail H, BEFORE: 2 Spacer NSA5527-03-02D Item (31) Retain 4 Clamp NSA935807C16 Item (111) Retain 2 Washer NSA935808-01 Item (112) Retain 2 Screw NAS1096-3-23 Item (113) Retain DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 87 6

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# @A310 SERVICE BULLETIN
2 Spacer NSA5527-03-05D Item (114) Retain (e) Remove, refer to Fig. A-GBHAA Sheet 06, Detail K, BEFORE: 1 Spacer NSA5527-03-02D Item (31) Retain 2 Clamp NSA935807C16 Item (111) Retain 1 Washer NSA935808-01 Item (112) Retain 1 Screw NAS1096-3-23 Item (113) Discard 1 Clamp NSA5516-04NV Item (120) Retain (f) Remove, refer to Fig. A-GBHAA Sheet 07, Detail M, BEFORE: 1 Spacer NSA5527-03-02D Item (31) Retain 2 Clamp NSA935807C16 Item (111) Retain 1 Washer NSA935808-01 Item (112) Retain 1 Screw NAS1096-3-23 Item (113) Discard 1 Spacer NSA5527-03-05D Item (114) Retain (g) Remove, refer to Fig. A-GBHAA Sheet 08, Detail P, BEFORE: 1 Spacer NSA5527-03-02D Item (31) Retain 2 Clamp NSA935807C16 Item (111) Retain 1 Washer NSA935808-01 Item (112) Retain 1 Screw NAS1096-3-23 Item (113) Discard 1 Spacer NSA5527-03-05D Item (114) Retain (h) Remove the identification placards from the cable harnesses near the receptacles 52VC and 5006VC as shown Fig. A-GBHAA Sheet 02, Detail A As required placard Item (132) Discard (i) Remove the disconnected electrical wires from the protection sleeve. (j) Install to the electrical wires for 10QT-A and 10QT-B of route 2S/636VB, refer to the Hook-up Chart 2, Lines 2 thru 8, Fig. A-GHBAA Sheet 01 : 1 (ME) Conduit NSA935805-09 Item 109 DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 88 6

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# @A310 SERVICE BULLETIN (k) Connect the electrical wires of route 2S to the receptacles 40VC and 5006VC in accordance with the Hook-up Chart 2, Lines 2 thru 8, END 1, Fig. A-GHBAA Sheet 01 . Use the contact pins if required: 7 Pin NSA938184PV1601 Item 126 (l) Install, refer to Fig. A-GBHAA Sheet 08, Detail Q, AFTER: 1 Spacer NSA5527-03-02D Item (31) Retained at removal 1 Spacer NSA5527-03-02D Item 31 2 Clamp NSA935807C16 Item (111) Retained at removal 1 Washer NSA935808-01 Item (112) Retained at removal 1 Spacer NSA5527-03-05D Item (114) Retained at removal 1 Clamp NSA935807C09 Item 117 1 Screw NAS1801-3-31 Item 123 1 Spacer NSA5527-03-07D Item 131 (m) Install, refer to Fig. A-GBHAA Sheet 07, Detail N, AFTER: 1 Spacer NSA5527-03-02D Item (31) Retained at removal 2 Clamp NSA935807C16 Item (111) Retained at removal 1 Washer NSA935808-01 Item (112) Retained at removal 1 Spacer NSA5527-03-05D Item (114) Retained at removal 1 Clamp NSA935807C09 Item 117 1 Screw NAS1801-3-31 Item 123 1 Spacer NSA5527-03-08D Item 130 (n) Install, refer to Fig. A-GBHAA Sheet 06, Detail L, AFTER: 2 Spacer NSA5527-03-02D Item (31) Retained at removal DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 89 6

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# @A310 SERVICE BULLETIN
2 Clamp NSA935807C16 Item (111) Retained at removal 1 Washer NSA935808-01 Item (112) Retained at removal 1 Clamp NSA5516-04NV Item (120) Retained at removal 1 Clamp NSA935807C09 Item 117 2 Screw NAS1801-3-31 Item 123 (o) Install, refer to Fig. A-GBHAA Sheet 05, Detail J, AFTER: 2 Spacer NSA5527-03-02D Item (31) Retained at removal 4 Clamp NSA935807C16 Item (111) Retained at removal 2 Washer NSA935808-01 Item (112) Retained at removal 2 Screw NAS1096-3-23 Item (113) Retained at removal 2 Spacer NSA5527-03-05D Item (114) Retained at removal 2 Clamp NSA935807C09 Item 117 (p) Install, refer to Fig. A-GBHAA Sheet 04, Detail G, AFTER: 1 Spacer NSA5527-03-02D Item (31) Retained at removal 2 Clamp NSA935807C16 Item (111) Retained at removal 1 Washer NSA935808-01 Item (112) Retained at removal 1 Screw NAS1096-3-23 Item (113) Retained at removal 1 Spacer NSA5527-03-05D Item (114) Retained at removal 1 Clamp NSA935807C09 Item 117

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 90 6

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# @A310 SERVICE BULLETIN (q) Install, refer to Fig. A-GBHAA Sheet 03, Detail E, AFTER: 1 Spacer NSA5527-03-02D Item (31) Retained at removal 2 Clamp NSA935807C16 Item (111) Retained at removal 1 Washer NSA935808-01 Item (112) Retained at removal 1 Screw NAS1096-3-23 Item (113) Retained at removal 1 Spacer NSA5527-03-05D Item (114) Retained at removal 1 Nut NAS1291C3M Item (116) Retained at removal 1 Washer AN960KD10l Item (124) Retained at removal 1 Clamp NSA935807C09 Item 117 (r) Protect the electrical wires for 10QT-A and 10QT-B of route 2S/636VB, refer to the Hook-up Chart 2, Fig. A-GHBAA Sheet 01 with: 3 Sleeve ABS0596S004 Item 1 and 20 Tie NSA935401-03 Item 149 20 Tie-Cable NSA935401-04 Item 150 (s) Install the identification placards, refer to Fig. A-GBHAA Sheet 02: 1 Placard Set B9299071900600 Item 132

(8) Subtask 282148-831-211-002 - Install the cable sleeves in the RH-wing forward of the front spar between rib 9 and rib 12 in zone 623. Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills ELECTRICAL

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 91 6

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# @A310 SERVICE BULLETIN
Material necessary to do the job Kit 282148D01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 ABS0596S004 3 SLEEVE 10 MS21919WCH9 CLAMP 14 NAS1096-3-19 2 SCREW 15 NSA5527-03-03 3 SPACER 16 NSA8420-2 1 (ME) CORD 149 NSA935401-03 10 TIE 150 NSA935401-04 20 TIE Kit 282148D03R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 31 NSA5527-03-02D 1 SPACER 121 NAS1096-3-40 1 SCREW References Fig. A-GBFAAImprovement of the 2S-Route in the RHWing in Zone 623 (Kit D01) Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Sheet 08 Sheet 09 Sheet 10 NOTE (1): The sleeve ABS0596S004 is supplied in pieces of 1000 mm. Cut or assemble these pieces to get the correct length. NOTE (2): The lengths of the sleeves given in this Service Bulletin are approximate lengths. Adapt the lengths of the sleeves in relation to the aircraft configuration. NOTE (3): Before you install a sleeve, cut and discard the cable ties around the cable bundle to install the sleeve correctly around the cable bundle. NOTE (4): Adapt the number of cable ties to the required quantity. Refer to Fig. A-GBFAA Sheet 01 , Fig. A-GBFAA Sheet 02, Fig. A-GBFAA Sheet 03, Fig. A-GBFAA Sheet 04, Fig. A-GBFAA Sheet 05, Fig. A-GBFAA Sheet 06, Fig. A-GBFAA Sheet 07, Fig. A-GBFAA Sheet 08, Fig. A-GBFAA Sheet 09 and Fig. A-GBFAA Sheet 10 (a) At one position, remove these items from the bracket between rib 11 and rib 12 and cable bundle 2S/636VB, as shown in Details A and D: 2 Clamp MS21919WCH4 Item (22) Retain
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 92 6

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# @A310 SERVICE BULLETIN
1 Clamp MS21919WCH4 Item (22) Discard 1 Clamp MS21919WCH3 Item (23) Retain 1 Spacer NSA5527-03-01D Item (30) Retain 1 Spacer NSA5527-03-02D Item (31) Retain 2 Washer NSA935808-01 Item (112) Retain 2 Screw NAS1096-3-30 Item (121) Discard 1 Clamp NSA935807-06 Item (122) Retain (b) At two positions, remove these items from the brackets between rib 10 and rib 11 and between rib 11 and rib 12 and cable bundle 2S/636VB, as shown in Details A and F: 2 Clamp Item (22) Discard 6 Clamp MS21919WCH4 Item (22) Retain 4 Spacer NSA5527-03-01D Item (30) Retain 2 Washer NAS1149D0332K Item (40) Retain 2 Screw NAS1096-3-27 Item (52) Retain (c) At two positions, remove these items from the brackets of the rib 11 and cable bundle 2S/636VB, as shown in Details A and H: 6 Clamp MS21919WCH4 Item (22) Retain 2 Clamp Item (23) Discard 2 Spacer NSA5527-03-01D Item (30) Retain 2 Spacer NSA5527-03-04D Item (32) Retain 2 Washer NAS1149D0332K Item (40) Retain 2 Screw NAS1096-3-22 Item (51) Retain (d) At two positions, remove these items from the brackets of the rib 10 and cable bundle 2S/636VB, as shown in Details A and K: 2 Clamp Item (22) Discard 2 Clamp MS21919WCH4 Item (22) Retain
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 93 6

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# @A310 SERVICE BULLETIN
2 Spacer NSA5527-03-01D Item (30) Retain 2 Spacer Item (32) Discard 2 Washer NAS1149D0332K Item (40) Retain 2 Screw Item (51) Discard (e) Remove these items from the bracket between rib 9 and rib 10 and cable bundle 2S/636VB, as shown in Details A and M: 3 Clamp MS21919WCH4 Item (22) Retain 1 Clamp Item (23) Discard 1 Spacer NSA5527-03-01D Item (30) Retain 1 Spacer NSA5527-03-04D Item (32) Retain 1 Washer NAS1149D0332K Item (40) Retain 1 Screw NAS1096-3-22 Item (51) Retain (f) Remove these items from the bracket of the rib 9 and cable bundle 2S/636VB, as shown in Details A and T: 1 Clamp Item (21) Discard 1 Clamp MS21919WCH5 Item (21) Retain 1 Spacer NSA5527-03-02D Item (31) Retain 1 Spacer NSA5527-03-04D Item (32) Retain 1 Washer NAS1149D0332K Item (40) Retain 1 Screw NAS1096-3-27 Item (52) Retain (g) Install this cable sleeve around these identified wires from the cable bundle 2S/636VB, as shown in Details A, C, E, G, J, L, N, Q, R, S and T: Wire number 2842-5061 Wire number 2842-5062 Wire number 2842-5063 Wire number 2842-5064 Wire number 2842-5065 DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 94 6

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# @A310 SERVICE BULLETIN
Wire number 2842-5071 3 Sleeve ABS0596S004 Item 1 and attach the cable sleeves with: 3 Spacer NSA5527-03-03 Item 15 1 (ME) Cord NSA8420-2 Item 16 10 Tie NSA935401-03 Item 149 20 Tie-Cable NSA935401-04 Item 150 (h) At one positions, install these items to the brackets between rib 10 and rib 11 and between rib 11 and rib 12, cable sleeves, Item 1 and cable bundle 2S/636VB, as shown in Details A and E: 2 Clamp MS21919WCH4 Item (22) Retained at removal 1 Clamp MS21919WCH3 Item (23) Retained at removal 1 Spacer NSA5527-03-01D Item (30) Retained at removal 1 Spacer NSA5527-03-02D Item (31) Retained at removal 1 Washer NSA935808-01 Item (112) Retained at removal 1 Clamp NSA935807-06 Item (122) Retained at removal 1 Clamp MS21919WCH9 Item 10 1 Spacer NSA5527-03-02D Item 31 1 Screw NAS1096-3-40 Item 121 (i) At two positions, install these items to the brackets between rib 10 and rib 11 and between rib 11 and rib 12, cable sleeves, Item 1 and cable bundle 2S/636VB, as shown in Details A and G: 6 Clamp MS21919WCH4 Item (22) Retained at removal 4 Spacer NSA5527-03-01D Item (30) Retained at removal

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 95 6

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# @A310 SERVICE BULLETIN
2 Washer NAS1149D0332K Item (40) Retained at removal 2 Screw NAS1096-3-27 Item (52) Retained at removal 2 Clamp MS21919WCH9 Item 10 (j) At two positions, install these items to the brackets of the rib 11, cable sleeves, Item 1 and cable bundle 2S/636VB, as shown in Details A and J: 6 Clamp MS21919WCH4 Item (22) Retained at removal 2 Spacer NSA5527-03-01D Item (30) Retained at removal 2 Spacer NSA5527-03-04D Item (32) Retained at removal 2 Washer NAS1149D0332K Item (40) Retained at removal 2 Screw NAS1096-3-22 Item (51) Retained at removal 2 Clamp MS21919WCH9 Item 10 (k) At two positions, install these items to the brackets of the rib 10, cable sleeves, Item 1 and cable bundle 2S/636VB, as shown in Details A and L: 2 Clamp MS21919WCH4 Item (22) Retained at removal 2 Spacer NSA5527-03-01D Item (30) Retained at removal 2 Washer NAS1149D0332K Item (40) Retained at removal 2 Clamp MS21919WCH9 Item 10 2 Screw NAS1096-3-19 Item 14 (l) Install these items to the bracket between rib 9 and rib 10, cable sleeves, Item 1 and cable bundle 2S/636VB, as shown in Details A and Q: 3 Clamp MS21919WCH4 Item (22) Retained at removal 1 Spacer NSA5527-03-01D Item (30) Retained at removal DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 96 6

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# @A310 SERVICE BULLETIN
1 Spacer NSA5527-03-04D Item (32) Retained at removal 1 Washer NAS1149D0332K Item (40) Retained at removal 1 Screw NAS1096-3-22 Item (51) Retained at removal 1 Clamp MS21919WCH9 Item 10 (m) Install these items to the bracket of the rib 9, cable sleeves, Item 1 and cable bundle 2S/636VB, as shown in Details A and Q: 1 Clamp MS21919WCH5 Item (21) Retained at removal 1 Spacer NSA5527-03-02D Item (31) Retained at removal 1 Spacer NSA5527-03-04D Item (32) Retained at removal 1 Washer NAS1149D0332K Item (40) Retained at removal 1 Screw NAS1096-3-27 Item (52) Retained at removal 1 Clamp MS21919WCH9 Item 10 **CONF 003 (1) Subtask 282148-831-405-001 - Install a New Bracket on the Sub Spar Behind the Front Spar Between RIB 8 and RIB 9 on the RH Wing Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills AIRFRAME Material necessary to do the job Kit 282148B01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 A5725068600000 1 Bracket 2 ASNA0078A502 2 Rivet

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 97 6

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# @A310 SERVICE BULLETIN

Consumable CMLB01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Corrosion Inhibiting Low Adhesion Sealant 09-018 As required Solvent General Purpose 11-026 As required Lint-Free Cotton Cloth 19-003 As required References Fig. A-UBAAA Location of Bracket on the Sub Spar Behind the Front Spar Between RIB 8 and RIB 9 (RH Wing) Sheet 01

Refer to Fig. A-UBAAA Sheet 01 (a) Remove from the sub spar behind the front spar between RIB 8 and RIB 9 on the RH wing, the items that follow: 2 Rivet NSA54213510DCA Item (2) Discard 1 Bracket A5724630400000 Item (1) Discard (b) Clean the mating surfaces use Lint-Free Cotton Cloth 19-003 As required

made moist with Solvent General Purpose 11-026 As required (c) Put the 1 Bracket A5725068600000 Item 1 in position on the sub spar behind the front spar between RIB 8 and RIB 9 on the RH wing (Refer to Fig. A-UBAAA Sheet 01 ). (d) Copy drill the two holes from the sub spar through the Bracket, Item 1 to a dimension of between 4.060 and 4.160 mm (0.160 and 0.164 in.). (e) Deburr the holes that have been worked. (f) Use Corrosion Inhibiting Low Adhesion Sealant 09-018 As required

and wet install the
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 98 6

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# @A310 SERVICE BULLETIN

1 Bracket A5725068600000 Item 1 with the 2 Rivet, Blind ASNA0078A502 Item 2 on the sub spar behind the front spar between RIB 8 and RIB 9 on the RH wing. (2) Subtask 282148-831-004-001 - Install cable sleeves in the RH Electronics Rack 90VU. Manpower Resources Manhours 6.00 Minimum number of person 1 Subtask elapsed time 6.00 Skills NON SPECIFIC Material necessary to do the job Kit 282148A01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 ABS0596S004 2000 (mm) SLEEVE NSA935401-04 50 TIE References Fig. A-FCAAA Installation of Cable Sleeves in the RH Electronics Rack 90VU. Sheet 01 Fig. A-FWAAA Installation of Cable Sleeves in the RH Electronics Rack 90VU. Sheet 01

NOTE: The sleeves ABS0596S004 and ABS0596S006 are supplied in pieces of 1000 mm (39.370 inches), cut or assemble these pieces to get the correct length. NOTE: The lengths of the sleeves given in this Service Bulletin are approximate lengths. Adapt the lengths of the sleeves in relation to the aircraft configuration. NOTE: Before you install a sleeve, cut and discard the cable ties around the cable bundle to install the sleeve correctly around the cable bundle. (a) On the Shelf 92VU, only around the wires identified in figure Fig. A-FWAAA Sheet 01 , from the equipment 15QT-B to the connector 2354VC, install: 1600 (mm) Sleeve ABS0596S004 Item 1

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 99 6

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# @A310 SERVICE BULLETIN (b) Around the cable bundle of the connector 2354VC-A, install: 400 (mm) Sleeve ABS0596S004 Item 1 (c) Attach the sleeves with: 50 Tie-Cable NSA935401-04

(3) Subtask 282148-831-005-001 - Install cable sleeves between FR38.2 and FR39, in the forward cargo compartment. 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 282148A01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 2 ABS0596S006 1000 (mm) SLEEVE NSA935401-05 50 TIE References Fig. A-FCBAA Installation of Cable Sleeves in the Forward Cargo Compartment. Sheet 01

NOTE: The sleeves ABS0596S004 and ABS0596S006 are supplied in pieces of 1000 mm (39.370 inches), cut or assemble these pieces to get the correct length. NOTE: The lengths of the sleeves given in this Service Bulletin are approximate lengths. Adapt the lengths of the sleeves in relation to the aircraft configuration. NOTE: Before you install a sleeve, cut and discard the cable ties around the cable bundle to install the sleeve correctly around the cable bundle. (a) Around the cable bundle of the pressure seal 20VP, install: 1000 (mm) Sleeve ABS0596S006 Item 2 (b) Attach the sleeves with: 50 Tie-Cable NSA935401-05

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 100 6

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# @A310 SERVICE BULLETIN (4) Subtask 282148-831-006-001 - Install cable sleeves in the RH forward wing root and krueger flap. 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 282148A01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 2 ABS0596S006 1000 (mm) SLEEVE NSA935401-05 50 TIE References Fig. A-FCCAA Installation of Cable Sleeves in the RH forward wing root and krueger flap. Sheet 01
(a) Around the cable bundle of the pressure seal 20VP, install: 1000 (mm) Sleeve ABS0596S006 Item 2 (b) Attach the sleeves with: 50 Tie-Cable NSA935401-05

(5) Subtask 282148-831-208-003 - Install the cable sleeves in the RH-wing forward of the front spar between rib 2 and rib 3 in zone 612. Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills ELECTRICAL Material necessary to do the job Kit 282148D01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 ABS0596S004 1 SLEEVE 11 MS21919WCH13 CLAMP 149 NSA935401-03 1 TIE 150 NSA935401-04 1 TIE

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 101 6

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# @A310 SERVICE BULLETIN

Kit 282148D05R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 125 B9299071900200 1 EQUIPMNT References Fig. A-GBEAAImprovement of the 2S-Route in the RHWing in Zone 612 (Kit D01) Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Sheet 08 NOTE (1): The sleeves ABS0596S004 is supplied in pieces of 1000 mm. Cut or assemble these pieces to get the correct length. NOTE (2): The lengths of the sleeves given in this Service Bulletin are approximate lengths. Adapt the lengths of the sleeves in relation to the aircraft configuration. NOTE (3): Before you install a sleeve, cut and discard the cable ties around the cable bundle to install the sleeve correctly around the cable bundle. NOTE (4): Adapt the number of cable ties to the required quantity. Refer to Fig. A-GBEAA Sheet 01 , Fig. A-GBEAA Sheet 02, Fig. A-GBEAA Sheet 03, Fig. A-GBEAA Sheet 04, Fig. A-GBEAA Sheet 05, Fig. A-GBEAA Sheet 06, Fig. A-GBEAA Sheet 07 and Fig. A-GBEAA Sheet 08 (a) Remove these items from the bracket of the rib 2 and cable bundle 2S/624VB, as shown in Details A and B: 1 Clamp MS21919WCH4 Item (22) Retain 1 Clamp MS21919WCH3 Item (23) Retain 1 Spacer NSA5527-03-02D Item (31) Retain 1 Washer NAS1149D0332K Item (40) Retain 1 Screw NAS1096-3-21 Item (50) Retain 1 Clamp MS21919WCH10 Item (100) Retain 1 Clamp Item (100) Discard

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 102 6

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# @A310 SERVICE BULLETIN (b) Remove these items from the riblet and cable bundle 2S/624VB, as shown in Details A and D: 1 Clamp MS21919WCH4 Item (22) Retain 3 Spacer NSA5527-03-02D Item (31) Retain 1 Washer NAS1149D0332K Item (40) Retain 1 Screw NAS1096-3-38 Item (54) Retain 1 Clamp Item (100) Discard (c) Install this cable sleeve around these identified wires from the cable bundle 2S/624VB, as shown in Details A, C and F: Wire number 2842-5052 Wire number 2842-5053 Wire number 2842-5054 Wire number 2842-5055 Wire number 2842-5056 Wire number 2842-5070 1 Sleeve ABS0596S004 Item 1 and attach the cable sleeve with: 1 Tie NSA935401-03 Item 149 1 Tie-Cable NSA935401-04 Item 150 and 1 Placard set B9299071900200 Item 125 as necessary. (d) Install these items to the bracket of the rib 2, cable bundle 2S/624VB and cable sleeve, Item 1, as shown in Details A and C: 1 Clamp MS21919WCH4 Item (22) Retained at removal 1 Clamp MS21919WCH3 Item (23) Retained at removal 1 Spacer NSA5527-03-02D Item (31) Retained at removal
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 103 6

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# @A310 SERVICE BULLETIN
1 Washer NAS1149D0332K Item (40) Retained at removal 1 Screw NAS1096-3-21 Item (50) Retained at removal 1 Clamp MS21919WCH10 Item (100) Retained at removal 1 Clamp MS21919WCH13 Item 11 (e) Install these items to the riblet, cable bundle 2S/624VB and cable sleeve, Item 1, as shown in Details A and E: 1 Clamp MS21919WCH4 Item (22) Retained at removal 3 Spacer NSA5527-03-02D Item (31) Retained at removal 1 Washer NAS1149D0332K Item (40) Retained at removal 1 Screw NAS1096-3-38 Item (54) Retained at removal 1 Clamp MS21919WCH13 Item 11

(6) Subtask 282148-831-209-003 - Install the cable sleeves in the RH-wing forward of the front spar between rib 7 and rib 8 in zone 612. Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills ELECTRICAL Material necessary to do the job Kit 282148D01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 ABS0596S004 2 SLEEVE 12 MS21919WCH14 CLAMP 149 NSA935401-03 2 TIE 150 NSA935401-04 2 TIE

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 104 6

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# @A310 SERVICE BULLETIN

References Fig. A-GBEAAImprovement of the 2S-Route in the RHWing in Zone 612 (Kit D01) Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Sheet 08 NOTE (1): The sleeves ABS0596S004 is supplied in pieces of 1000 mm. Cut or assemble these pieces to get the correct length. NOTE (2): The lengths of the sleeves given in this Service Bulletin are approximate lengths. Adapt the lengths of the sleeves in relation to the aircraft configuration. NOTE (3): Before you install a sleeve, cut and discard the cable ties around the cable bundle to install the sleeve correctly around the cable bundle. NOTE (4): Adapt the number of cable ties to the required quantity. Refer to Fig. A-GBEAA Sheet 01 , Fig. A-GBEAA Sheet 02, Fig. A-GBEAA Sheet 03, Fig. A-GBEAA Sheet 04, Fig. A-GBEAA Sheet 05, Fig. A-GBEAA Sheet 06, Fig. A-GBEAA Sheet 07 and Fig. A-GBEAA Sheet 08 (a) Remove these items from the two brackets of the riblets and cable bundle 2S/624VB, as shown in Details A, H and K: 2 Clamp MS21919WCH4 Item (22) Retain 2 Washer NAS1149D0332K Item (40) Retain 2 Screw NAS1096-3-8 Item (55) Retain 2 Clamp Item (100) Discard (b) Install this cable sleeve around these identified wires from the cable bundle 2S/624VB, as shown in Details A, J, K, L, M and N: Wire number 2842-5052 Wire number 2842-5053 Wire number 2842-5054 Wire number 2842-5055 Wire number 2842-5056 1 Sleeve ABS0596S004 Item 1 and attach the cable sleeves with: DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 105 6

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# @A310 SERVICE BULLETIN

1 Tie NSA935401-03 Item 149 1 Tie-Cable NSA935401-04 Item 150 (c) Install this cable sleeve around this identified wire from the cable bundle 2S/624VB, as shown in Details A, J, K, L, M and N: Wire number 2842-5070 1 Sleeve ABS0596S004 Item 1 and attach the cable sleeves with: 1 Tie NSA935401-03 Item 149 1 Tie-Cable NSA935401-04 Item 150 (d) Install these items to the two brackets of the riblets, cable bundle 2S/624VB and cable sleeves, Item 1, as shown in Detail A, J and L: 2 Clamp MS21919WCH4 Item (22) Retained at removal 2 Washer NAS1149D0332K Item (40) Retained at removal 2 Screw NAS1096-3-8 Item (55) Retained at removal 2 Clamp MS21919WCH14 Item 12

(7) Subtask 282148-831-210-003 - Install the cable sleeves in the RH-wing forward of the front spar between rib 8 and rib 9 (pylon area) in zone 612. Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills ELECTRICAL Material necessary to do the job Kit 282148D05R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 ABS0596S004 3 SLEEVE 30 NSA5527-03-01D 2 SPACER 31 NSA5527-03-02D 1 SPACER 109 NSA935805-09 3 (ME) CONDUIT 117 NSA935807C09 12 CLAMP 126 NSA938184PV1601 15 PIN DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 106 6

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# @A310 SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 135 NAS1096-3-42 1 SCREW 136 NAS1096-3-30 1 SCREW 149 NSA935401-03 30 TIE 150 NSA935401-04 30 TIE References Fig. A-GBJAAImprovement of the 2S-Route in the RHWing Pylon Area (Kit D05) Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Sheet 08 Sheet 09 Fig. A-GHAAA Hook-up Chart Sheet 01 Fig. A-GHBAA Hook-up Chart Sheet 01
NOTE (1): The sleeves ABS0596S004 is supplied in pieces of 1000 mm. Cut or assemble these pieces to get the correct length. NOTE (2): The lengths of the sleeves given in this Service Bulletin are approximate lengths. Adapt the lengths of the sleeves in relation to the aircraft configuration. NOTE (3): Before you install a sleeve, cut and discard the cable ties around the cable bundle to install the sleeve correctly around the cable bundle. NOTE (4): Adapt the number of cable ties to the required quantity. Refer to Fig. A-GBJAA Sheet 01 , Fig. A-GBJAA Sheet 02, Fig. A-GBJAA Sheet 03, Fig. A-GBJAA Sheet 04, Fig. A-GBJAA Sheet 05, Fig. A-GBJAA Sheet 06, Fig. A-GBJAA Sheet 07, Fig. A-GBJAA Sheet 08 and Fig. A-GBJAA Sheet 09 Refer to Fig. A-GHAAA Sheet 01 and Fig. A-GHBAA Sheet 01 (a) Disconnect these wires of route 2S from the receptacles 40VC and 5006VC in accordance with the Hook-up Chart 1, Lines 1 thru 14, END 1, Fig. A-GHAAA Sheet 01 and the Hook-up Chart 2, Lines 2 thru 8, END 1, Fig. A-GHBAA Sheet 01

. (b) Remove, refer to Fig. A-GBJAA Sheet 03, Detail C, BEFORE: 2 Spacer NSA5527-03-05D Item (30) Discard 1 Washer NSA935808-01 Item (112) Retain

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 107 6

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# @A310 SERVICE BULLETIN
1 Nut NAS1291C3M Item (116) Retain 1 Clamp NSA935807C10 Item (117) Discard 1 Screw Item (136) Discard (c) Remove, refer to Fig. A-GBJAA Sheet 04, Detail E, BEFORE: 1 Washer NSA935808-01 Item (112) Retain 1 Screw Item (113) Retain 1 Clamp NSA935807C10 Item (117) Discard (d) Remove, refer to Fig. A-GBJAA Sheet 05, Detail G, BEFORE: 2 Washer NSA935808-01 Item (112) Retain 2 Screw Item (113) Retain 2 Clamp NSA935807C10 Item (117) Discard (e) Remove, refer to Fig. A-GBJAA Sheet 06, Detail J, BEFORE: 1 Spacer NSA5527-03-05D Item (30) Discard 1 Washer NSA935808-01 Item (112) Retain 1 Clamp NSA935807C10 Item (117) Discard 1 Screw Item (135) Retain (f) Remove, refer to Fig. A-GBJAA Sheet 07, Detail L, BEFORE: 1 Washer NSA935808-01 Item (112) Retain 1 Screw Item (113) Retain 1 Clamp NSA935807C10 Item (117) Discard (g) Remove, refer to Fig. A-GBJAA Sheet 08, Detail N, BEFORE: 1 Washer NSA935808-01 Item (112) Retain 1 Screw Item (113) Retain 1 Clamp NSA935807C10 Item (117) Discard

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 108 6

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# @A310 SERVICE BULLETIN (h) Remove the protection sleeve from the cable harness as shown Fig. A-GBJAA Sheet 01 , Fig. A-GBJAA Sheet 02, Fig. A-GBJAA Sheet 03, Fig. A-GBJAA Sheet 04, Fig. A-GBJAA Sheet 05, Fig. A-GBJAA Sheet 06, Fig. A-GBJAA Sheet 07, Fig. A-GBJAA Sheet 08 and Fig. A-GBJAA Sheet 09, Details A, C, E, G, J, L and N: 1 Sleeve NSA935805-10 Item (1) Discard (i) Cut the conduit to the required length and install as shown Refer to Fig. A-GBJAA Sheet 01 , Fig. A-GBJAA Sheet 02, Fig. A-GBJAA Sheet 03, Fig. A-GBJAA Sheet 04, Fig. A-GBJAA Sheet 05, Fig. A-GBJAA Sheet 06, Fig. A-GBJAA Sheet 07, Fig. A-GBJAA Sheet 08 and Fig. A-GBJAA Sheet 09, Details B, D, F, H, K, M, P and Q: 3 Sleeve ABS0596S004 Item 1 3 (ME) Conduit NSA935805-09 Item 109 1 One part 1500.0 mm (59.06 in.) to the electrical wires for 10QT-A and 10QT-B of route 2S/636VB, refer to the Hook-up Chart 2, Fig. A-GHBAA Sheet 01 (j) Connect the electrical wires of route 2S to the receptacles 40VC and 5006VC in accordance with the Hook-up Chart 1, Lines 1 thru 14, END 1, Fig. A-GHAAA Sheet 01 and the Hook-up Chart 2, lines 2 thru 8, END 1, Fig. A-GHBAA Sheet 01

. Use the contact pins if required: 15 Pin NSA938184PV1601 Item 126 (k) Install, refer to Fig. A-GBJAA Sheet 08, Detail P, AFTER: 1 Washer NSA935808-01 Item (112) Retained at removal 1 Screw Item (113) Retained at removal 2 Clamp NSA935807C09 Item 117 (l) Install, refer to Fig. A-GBJAA Sheet 07, Detail M, AFTER: 1 Washer NSA935808-01 Item (112) Retained at removal 1 Screw Item (113) Retained at removal 2 Clamp NSA935807C09 Item 117 (m) Install, refer to Fig. A-GBJAA Sheet 06, Detail K, AFTER: 1 Spacer NSA5527-03-02D Item 31 1 Washer NSA935808-01 Item (112) Retained at removal
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 109 6

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# @A310 SERVICE BULLETIN
2 Clamp NSA935807C09 Item 117 1 Screw NAS1096-3-42 Item 135 (n) Install, refer to Fig. A-GBJAA Sheet 05, Detail H, AFTER: 2 Washer NSA935808-01 Item (112) Retained at removal 2 Screw Item (113) Retained at removal 4 Clamp NSA935807C09 Item 117 (o) Install, refer to Fig. A-GBJAA Sheet 04, Detail F, AFTER: 1 Washer NSA935808-01 Item (112) Retained at removal 1 Screw Item (113) Retained at removal 2 Clamp NSA935807C09 Item 117 (p) Install, refer to Fig. A-GBJAA Sheet 03, Detail D, AFTER: 2 Spacer NSA5527-03-01D Item 30 2 Washer NSA935808-01 Item (112) Retained at removal 2 Nut NAS1291C3M Item (116) Retained at removal 2 Clamp NSA935807C09 Item 117 1 Screw NAS1096-3-30 Item 136 (q) Protect the electrical wires for 10QT-A and 10QT-B of route 2S/636VB, refer to Fig. A-GBJAA Sheet 09, Detail Q, and the Hook-up Chart 2, Fig. A-GHBAA Sheet 01 with: 30 Tie NSA935401-03 Item 149 30 Tie-Cable NSA935401-04 Item 150

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 110 6

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# @A310 SERVICE BULLETIN (8) Subtask 282148-831-211-003 - Install the cable sleeves in the RH-wing forward of the front spar between rib 9 and rib 12 in zone 623. Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills ELECTRICAL Material necessary to do the job Kit 282148D01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 ABS0596S004 3 SLEEVE 10 MS21919WCH9 CLAMP 14 NAS1096-3-19 2 SCREW 15 NSA5527-03-03 3 SPACER 16 NSA8420-2 1 (ME) CORD 149 NSA935401-03 10 TIE 150 NSA935401-04 20 TIE Kit 282148D05R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 31 NSA5527-03-02D SPACER 135 NAS1096-3-42 SCREW References Fig. A-GBFAAImprovement of the 2S-Route in the RHWing in Zone 623 (Kit D01) Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Sheet 08 Sheet 09 Sheet 10 NOTE (1): The sleeve ABS0596S004 is supplied in pieces of 1000 mm. Cut or assemble these pieces to get the correct length. NOTE (2): The lengths of the sleeves given in this Service Bulletin are approximate lengths. Adapt the lengths of the sleeves in relation to the aircraft configuration. NOTE (3): Before you install a sleeve, cut and discard the cable ties around the cable bundle to install the sleeve correctly around the cable bundle.

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 111 6

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# @A310 SERVICE BULLETIN
NOTE (4): Adapt the number of cable ties to the required quantity. Refer to Refer to Fig. A-GBFAA Sheet 01 , Fig. A-GBFAA Sheet 02, Fig. A-GBFAA Sheet 03, Fig. A-GBFAA Sheet 04, Fig. A-GBFAA Sheet 05, Fig. A-GBFAA Sheet 06, Fig. A-GBFAA Sheet 07, Fig. A-GBFAA Sheet 08, Fig. A-GBFAA Sheet 09 and Fig. AGBFAA Sheet 10 (a) At one position, remove these items from the bracket between rib 11 and rib 12 and cable bundle 2S/636VB, as shown in Details A and D: 2 Clamp MS21919WCH4 Item (22) Retain 1 Clamp MS21919WCH4 Item (22) Discard 1 Clamp MS21919WCH3 Item (23) Retain 1 Spacer NSA5527-03-01D Item (30) Retain 1 Spacer NSA5527-03-02D Item (31) Retain 2 Washer NSA935808-01 Item (112) Retain 2 Screw NAS1096-3-30 Item (121) Discard 1 Clamp NSA935807-06 Item (122) Retain (b) At two positions, remove these items from the brackets between rib 10 and rib 11 and between rib 11 and rib 12 and cable bundle 2S/636VB, as shown in Details A and F: 2 Clamp Item (22) Discard 6 Clamp MS21919WCH4 Item (22) Retain 4 Spacer NSA5527-03-01D Item (30) Retain 2 Washer NAS1149D0332K Item (40) Retain 2 Screw NAS1096-3-27 Item (52) Retain (c) At two positions, remove these items from the brackets of the rib 11 and cable bundle 2S/636VB, as shown in Details A and H: 6 Clamp MS21919WCH4 Item (22) Retain 2 Clamp Item (23) Discard 2 Spacer NSA5527-03-01D Item (30) Retain 2 Spacer NSA5527-03-04D Item (32) Retain DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 112 6

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# @A310 SERVICE BULLETIN
2 Washer NAS1149D0332K Item (40) Retain 2 Screw NAS1096-3-22 Item (51) Retain (d) At two positions, remove these items from the brackets of the rib 10 and cable bundle 2S/636VB, as shown in Details A and K: 2 Clamp Item (22) Discard 2 Clamp MS21919WCH4 Item (22) Retain 2 Spacer NSA5527-03-01D Item (30) Retain 2 Spacer Item (32) Discard 2 Washer NAS1149D0332K Item (40) Retain 2 Screw Item (51) Discard (e) Remove these items from the bracket between rib 9 and rib 10 and cable bundle 2S/636VB, as shown in Details A and M: 3 Clamp MS21919WCH4 Item (22) Retain 1 Clamp Item (23) Discard 1 Spacer NSA5527-03-01D Item (30) Retain 1 Spacer NSA5527-03-04D Item (32) Retain 1 Washer NAS1149D0332K Item (40) Retain 1 Screw NAS1096-3-22 Item (51) Retain (f) Remove these items from the bracket of the rib 9 and cable bundle 2S/636VB, as shown in Details A and T: 1 Clamp Item (21) Discard 1 Clamp MS21919WCH5 Item (21) Retain 1 Spacer NSA5527-03-02D Item (31) Retain 1 Spacer NSA5527-03-04D Item (32) Retain 1 Washer NAS1149D0332K Item (40) Retain 1 Screw NAS1096-3-27 Item (52) Retain

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 113 6

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# @A310 SERVICE BULLETIN (g) Install this cable sleeve around these identified wires from the cable bundle 2S/636VB, as shown in Details A, C, E, G, J, L, N, Q and R: Wire number 2842-5061 Wire number 2842-5062 Wire number 2842-5063 Wire number 2842-5064 Wire number 2842-5065 Wire number 2842-5071 3 Sleeve ABS0596S004 Item 1 and attach the cable sleeves with: 3 Spacer NSA5527-03-03 Item 15 1 (ME) Cord NSA8420-2 Item 16 10 Tie NSA935401-03 Item 149 20 Tie-Cable NSA935401-04 Item 150 (h) At one positions, install these items to the brackets between rib 10 and rib 11 and between rib 11 and rib 12, cable sleeves, Item 1 and cable bundle 2S/636VB, as shown in Details A and E: 2 Clamp MS21919WCH4 Item (22) Retained at removal 1 Clamp MS21919WCH3 Item (23) Retained at removal 1 Spacer NSA5527-03-01D Item (30) Retained at removal 1 Spacer NSA5527-03-02D Item (31) Retained at removal 1 Washer NSA935808-01 Item (112) Retained at removal 1 Clamp NSA935807-06 Item (122) Retained at removal 1 Clamp MS21919WCH9 Item 10 1 Spacer NSA5527-03-02D Item 31
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 114 6

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# @A310 SERVICE BULLETIN

1 Screw NAS1096-3-42 Item 135 (i) At two positions, install these items to the brackets between rib 10 and rib 11 and between rib 11 and rib 12, cable sleeves, Item 1 and cable bundle 2S/636VB, as shown in Details A and G: 6 Clamp MS21919WCH4 Item (22) Retained at removal 4 Spacer NSA5527-03-01D Item (30) Retained at removal 2 Washer NAS1149D0332K Item (40) Retained at removal 2 Screw NAS1096-3-27 Item (52) Retained at removal 2 Clamp MS21919WCH9 Item 10 (j) At two positions, install these items to the brackets of the rib 11, cable sleeves, Item 1 and cable bundle 2S/636VB, as shown in Details A and J: 2 Clamp MS21919WCH4 Item (22) Retained at removal 1 Spacer NSA5527-03-01D Item (30) Retained at removal 1 Spacer NSA5527-03-04D Item (32) Retained at removal 1 Washer NAS1149D0332K Item (40) Retained at removal 1 Screw NAS1096-3-22 Item (51) Retained at removal 1 Clamp MS21919WCH9 Item 10 (k) At two positions, install these items to the brackets of the rib 10, cable sleeves, Item 1 and cable bundle 2S/636VB, as shown in Details A and L: 2 Clamp MS21919WCH4 Item (22) Retained at removal 2 Spacer NSA5527-03-01D Item (30) Retained at removal 2 Washer NAS1149D0332K Item (40) Retained at removal

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 115 6

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# @A310 SERVICE BULLETIN
2 Clamp MS21919WCH9 Item 10 2 Screw NAS1096-3-19 Item 14 (l) Install these items to the bracket between rib 9 and rib 10, cable sleeves, Item 1 and cable bundle 2S/636VB, as shown in Details A and N: 3 Clamp MS21919WCH4 Item (22) Retained at removal 1 Spacer NSA5527-03-01D Item (30) Retained at removal 1 Spacer NSA5527-03-04D Item (32) Retained at removal 1 Washer NAS1149D0332K Item (40) Retained at removal 1 Screw NAS1096-3-22 Item (51) Retained at removal 1 Clamp MS21919WCH9 Item 10 (m) Install these items to the bracket of the rib 9, cable sleeves, Item 1 and cable bundle 2S/636VB, as shown in Details A and Q: 1 Clamp MS21919WCH5 Item (21) Retained at removal 1 Spacer NSA5527-03-02D Item (31) Retained at removal 1 Spacer NSA5527-03-04D Item (32) Retained at removal 1 Washer NAS1149D0332K Item (40) Retained at removal 1 Screw NAS1096-3-27 Item (52) Retained at removal 1 Clamp MS21919WCH9 Item 10

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 116 6

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# @A310 SERVICE BULLETIN
**CONF 004 (1) Subtask 282148-831-405-001 - Install a New Bracket on the Sub Spar Behind the Front Spar Between RIB 8 and RIB 9 on the RH Wing Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills AIRFRAME Material necessary to do the job Kit 282148B01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 A5725068600000 1 Bracket 2 ASNA0078A502 2 Rivet Consumable CMLB01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Corrosion Inhibiting Low Adhesion Sealant 09-018 As required Solvent General Purpose 11-026 As required Lint-Free Cotton Cloth 19-003 As required References Fig. A-UBAAA Location of Bracket on the Sub Spar Behind the Front Spar Between RIB 8 and RIB 9 (RH Wing) Sheet 01

Refer to Fig. A-UBAAA Sheet 01 (a) Remove from the sub spar behind the front spar between RIB 8 and RIB 9 on the RH wing, the items that follow: 2 Rivet NSA54213510DCA Item (2) Discard 1 Bracket A5724630400000 Item (1) Discard (b) Clean the mating surfaces use Lint-Free Cotton Cloth 19-003 As required

made moist with

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 117 6

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# @A310 SERVICE BULLETIN

Solvent General Purpose 11-026 As required (c) Put the 1 Bracket A5725068600000 Item 1 in position on the sub spar behind the front spar between RIB 8 and RIB 9 on the RH wing (Refer to Fig. A-UBAAA Sheet 01 ). (d) Copy drill the two holes from the sub spar through the Bracket, Item 1 to a dimension of between 4.060 and 4.160 mm (0.160 and 0.164 in.). (e) Deburr the holes that have been worked. (f) Use Corrosion Inhibiting Low Adhesion Sealant 09-018 As required

and wet install the 1 Bracket A5725068600000 Item 1 with the 2 Rivet, Blind ASNA0078A502 Item 2 on the sub spar behind the front spar between RIB 8 and RIB 9 on the RH wing. (2) Subtask 282148-831-004-001 - Install cable sleeves in the RH Electronics Rack 90VU. Manpower Resources Manhours 6.00 Minimum number of person 1 Subtask elapsed time 6.00 Skills NON SPECIFIC Material necessary to do the job Kit 282148A01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 ABS0596S004 2000 (mm) SLEEVE NSA935401-04 50 TIE References Fig. A-FCAAA Installation of Cable Sleeves in the RH Electronics Rack 90VU. Sheet 01

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 118 6

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# @A310 SERVICE BULLETIN

References Fig. A-FWAAA Installation of Cable Sleeves in the RH Electronics Rack 90VU. Sheet 01

NOTE: The sleeves ABS0596S004 and ABS0596S006 are supplied in pieces of 1000 mm (39.370 inches), cut or assemble these pieces to get the correct length. NOTE: The lengths of the sleeves given in this Service Bulletin are approximate lengths. Adapt the lengths of the sleeves in relation to the aircraft configuration. NOTE: Before you install a sleeve, cut and discard the cable ties around the cable bundle to install the sleeve correctly around the cable bundle. (a) On the Shelf 92VU, only around the wires identified in figure Fig. A-FWAAA Sheet 01 , from the equipment 15QT-B to the connector 2354VC, install: 1600 (mm) Sleeve ABS0596S004 Item 1 (b) Around the cable bundle of the connector 2354VC-A, install: 400 (mm) Sleeve ABS0596S004 Item 1 (c) Attach the sleeves with: 50 Tie-Cable NSA935401-04

(3) Subtask 282148-831-005-001 - Install cable sleeves between FR38.2 and FR39, in the forward cargo compartment. 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 282148A01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 2 ABS0596S006 1000 (mm) SLEEVE NSA935401-05 50 TIE References Fig. A-FCBAA Installation of Cable Sleeves in the Forward Cargo Compartment. Sheet 01

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 119 6

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# @A310 SERVICE BULLETIN
NOTE: The sleeves ABS0596S004 and ABS0596S006 are supplied in pieces of 1000 mm (39.370 inches), cut or assemble these pieces to get the correct length. NOTE: The lengths of the sleeves given in this Service Bulletin are approximate lengths. Adapt the lengths of the sleeves in relation to the aircraft configuration. NOTE: Before you install a sleeve, cut and discard the cable ties around the cable bundle to install the sleeve correctly around the cable bundle. (a) Around the cable bundle of the pressure seal 20VP, install: 1000 (mm) Sleeve ABS0596S006 Item 2 (b) Attach the sleeves with: 50 Tie-Cable NSA935401-05

(4) Subtask 282148-831-006-001 - Install cable sleeves in the RH forward wing root and krueger flap. 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 282148A01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 2 ABS0596S006 1000 (mm) SLEEVE NSA935401-05 50 TIE References Fig. A-FCCAA Installation of Cable Sleeves in the RH forward wing root and krueger flap. Sheet 01
(a) Around the cable bundle of the pressure seal 20VP, install: 1000 (mm) Sleeve ABS0596S006 Item 2 (b) Attach the sleeves with: 50 Tie-Cable NSA935401-05

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 120 6

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# @A310 SERVICE BULLETIN (5) Subtask 282148-831-208-004 - Install the cable sleeves in the RH-wing forward of the front spar between rib 2 and rib 3 in zone 612. Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills ELECTRICAL Material necessary to do the job Kit 282148D01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 ABS0596S004 1 SLEEVE 11 MS21919WCH13 CLAMP 149 NSA935401-03 1 TIE 150 NSA935401-04 1 TIE Kit 282148D06R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 132 B9299071900600 1 EQUIPMNT References Fig. A-GBEAAImprovement of the 2S-Route in the RHWing in Zone 612 (Kit D01) Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Sheet 08 NOTE (1): The sleeves ABS0596S004 is supplied in pieces of 1000 mm. Cut or assemble these pieces to get the correct length. NOTE (2): The lengths of the sleeves given in this Service Bulletin are approximate lengths. Adapt the lengths of the sleeves in relation to the aircraft configuration. NOTE (3): Before you install a sleeve, cut and discard the cable ties around the cable bundle to install the sleeve correctly around the cable bundle. NOTE (4): Adapt the number of cable ties to the required quantity. Refer to Fig. A-GBEAA Sheet 01 , Fig. A-GBEAA Sheet 02, Fig. A-GBEAA Sheet 03, Fig. A-GBEAA Sheet 04, Fig. A-GBEAA Sheet 05, Fig. A-GBEAA Sheet 06, Fig. A-GBEAA Sheet 07 and Fig. A-GBEAA Sheet 08

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 121 6

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# @A310 SERVICE BULLETIN (a) Remove these items from the bracket of the rib 2 and cable bundle 2S/624VB, as shown in Details A and B: 1 Clamp MS21919WCH4 Item (22) Retain 1 Clamp MS21919WCH3 Item (23) Retain 1 Spacer NSA5527-03-02D Item (31) Retain 1 Washer NAS1149D0332K Item (40) Retain 1 Screw NAS1096-3-21 Item (50) Retain 1 Clamp MS21919WCH10 Item (100) Retain 1 Clamp Item (100) Discard (b) Remove these items from the riblet and cable bundle 2S/624VB, as shown in Details A and D: 1 Clamp MS21919WCH4 Item (22) Retain 3 Spacer NSA5527-03-02D Item (31) Retain 1 Washer NAS1149D0332K Item (40) Retain 1 Screw NAS1096-3-38 Item (54) Retain 1 Clamp Item (100) Discard (c) Install this cable sleeve around these identified wires from the cable bundle 2S/624VB, as shown in Details A, C, E and F: Wire number 2842-5052 Wire number 2842-5053 Wire number 2842-5054 Wire number 2842-5055 Wire number 2842-5056 Wire number 2842-5070 1 Sleeve ABS0596S004 Item 1 and attach the cable sleeve with: 1 Tie NSA935401-03 Item 149 1 Tie-Cable NSA935401-04 Item 150 DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 122 6

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# @A310 SERVICE BULLETIN
and 1 Placard Set B9299071900600 Item 132 as necessary. (d) Install these items to the bracket of the rib 2, cable bundle 2S/624VB and cable sleeve, Item 1, as shown in Details A and C: 1 Clamp MS21919WCH4 Item (22) Retained at removal 1 Clamp MS21919WCH3 Item (23) Retained at removal 1 Spacer NSA5527-03-02D Item (31) Retained at removal 1 Washer NAS1149D0332K Item (40) Retained at removal 1 Screw NAS1096-3-21 Item (50) Retained at removal 1 Clamp MS21919WCH10 Item (100) Retained at removal 1 Clamp MS21919WCH13 Item 11 (e) Install these items to the riblet, cable bundle 2S/624VB and cable sleeve, Item 1, as shown in Details A and E: 1 Clamp MS21919WCH4 Item (22) Retained at removal 3 Spacer NSA5527-03-02D Item (31) Retained at removal 1 Washer NAS1149D0332K Item (40) Retained at removal 1 Screw NAS1096-3-38 Item (54) Retained at removal 1 Clamp MS21919WCH13 Item 11

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 123 6

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# @A310 SERVICE BULLETIN (6) Subtask 282148-831-209-004 - Install the cable sleeves in the RH-wing forward of the front spar between rib 7 and rib 8 in zone 612. Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills ELECTRICAL Material necessary to do the job Kit 282148D01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 ABS0596S004 2 SLEEVE 12 MS21919WCH14 CLAMP 149 NSA935401-03 2 TIE 150 NSA935401-04 2 TIE References Fig. A-GBEAAImprovement of the 2S-Route in the RHWing in Zone 612 (Kit D01) Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Sheet 08 NOTE (1): The sleeves ABS0596S004 is supplied in pieces of 1000 mm. Cut or assemble these pieces to get the correct length. NOTE (2): The lengths of the sleeves given in this Service Bulletin are approximate lengths. Adapt the lengths of the sleeves in relation to the aircraft configuration. NOTE (3): Before you install a sleeve, cut and discard the cable ties around the cable bundle to install the sleeve correctly around the cable bundle. NOTE (4): Adapt the number of cable ties to the required quantity. Refer to Fig. A-GBEAA Sheet 01 , Fig. A-GBEAA Sheet 02, Fig. A-GBEAA Sheet 03, Fig. A-GBEAA Sheet 04, Fig. A-GBEAA Sheet 05, Fig. A-GBEAA Sheet 06, Fig. A-GBEAA Sheet 07 and Fig. A-GBEAA Sheet 08 (a) Remove these items from the two brackets of the riblets and cable bundle 2S/624VB, as shown in Details A, H and K: 2 Clamp MS21919WCH4 Item (22) Retain 2 Washer NAS1149D0332K Item (40) Retain DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 124 6

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# @A310 SERVICE BULLETIN
2 Screw NAS1096-3-8 Item (55) Retain 2 Clamp Item (100) Discard (b) Install this cable sleeve around these identified wires from the cable bundle 2S/624VB, as shown in Details A, J, K, L, M and N: Wire number 2842-5052 Wire number 2842-5053 Wire number 2842-5054 Wire number 2842-5055 Wire number 2842-5056 1 Sleeve ABS0596S004 Item 1 and attach the cable sleeves with: 1 Tie NSA935401-03 Item 149 1 Tie-Cable NSA935401-04 Item 150 (c) Install this cable sleeve around this identified wire from the cable bundle 2S/624VB, as shown in Details A, J, K, L, M and N: Wire number 2842-5070 1 Sleeve ABS0596S004 Item 1 and attach the cable sleeves with: 1 Tie NSA935401-03 Item 149 1 Tie-Cable NSA935401-04 Item 150 (d) Install these items to the two brackets of the riblets, cable bundle 2S/624VB and cable sleeves, Item 1, as shown in Detail A, J and L: 2 Clamp MS21919WCH4 Item (22) Retained at removal 2 Washer NAS1149D0332K Item (40) Retained at removal 2 Screw NAS1096-3-8 Item (55) Retained at removal 2 Clamp MS21919WCH14 Item 12

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 125 6

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# @A310 SERVICE BULLETIN (7) Subtask 282148-831-210-004 - Install the cable sleeves in the RH-wing forward of the front spar between rib 8 and rib 9 (pylon area) in zone 612. Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills ELECTRICAL Material necessary to do the job Kit 282148D06R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 ABS0596S004 3 SLEEVE 31 NSA5527-03-02D 2 SPACER 109 NSA935805-09 1.5 (ME) CONDUIT 117 NSA935807C09 7 CLAMP 121 NAS1096-3-40 1 SCREW 123 NAS1801-3-31 2 SCREW 126 NSA938184PV1601 7 PIN 130 NSA5527-03-08D 1 SPACER 131 NSA5527-03-07D 1 SPACER 149 NSA935401-03 30 TIE 150 NSA935401-04 30 TIE References Fig. A-GBKAAImprovement of the 2S-Route in the RHWing Pylon Area (Kit D06) Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Sheet 08 Sheet 09 Fig. A-GHBAA Hook-up Chart Sheet 01
NOTE (1): The sleeves ABS0596S004 is supplied in pieces of 1000 mm. Cut or assemble these pieces to get the correct length. NOTE (2): The lengths of the sleeves given in this Service Bulletin are approximate lengths. Adapt the lengths of the sleeves in relation to the aircraft configuration. NOTE (3): Before you install a sleeve, cut and discard the cable ties around the cable bundle to install the sleeve correctly around the cable bundle. NOTE (4): Adapt the number of cable ties to the required quantity. DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 126 6

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# @A310 SERVICE BULLETIN
Refer to Fig. A-GBKAA Sheet 01 , Fig. A-GBKAA Sheet 02, Fig. A-GBKAA Sheet 03, Fig. A-GBKAA Sheet 04, Fig. A-GBKAA Sheet 05, Fig. A-GBKAA Sheet 06, Fig. A-GBKAA Sheet 07, Fig. A-GBKAA Sheet 08 and Fig. A-GBKAA Sheet 09 Refer to Fig. A-GHBAA Sheet 01 (a) Disconnect the wires of route 2S from the receptacles 40VC and 5006VC in accordance with the Hook-up Chart 2, Lines 2 thru 8, END 1, Fig. A-GHBAA Sheet 01

. (b) Remove, refer to Fig. A-GBKAA Sheet 03, Detail C, BEFORE: 1 Washer NSA935808-01 Item (112) Retain 1 Screw NAS1096-3-23 Item (113) Retain 1 Nut NAS1291C3M Item (116) Retain 1 Washer AN960KD10l Item (124) Retain (c) Remove, refer to Fig. A-GBKAA Sheet 04, Detail E, BEFORE: 1 Washer NSA935808-01 Item (112) Retain 1 Screw NAS1096-3-23 Item (113) Retain (d) Remove, refer to Fig. A-GBKAA Sheet 05, Detail G, BEFORE: 2 Washer NSA935808-01 Item (112) Retain 2 Screw NAS1096-3-23 Item (113) Retain (e) Remove, refer to Fig. A-GBKAA Sheet 06, Detail J, BEFORE: 1 Spacer NSA5527-03-02D Item (31) Retain 1 Screw Item (121) Discard (f) Remove, refer to Fig. A-GBKAA Sheet 07, Detail L, BEFORE: 1 Screw Item (123) Discard (g) Remove, refer to Fig. A-GBKAA Sheet 08, Detail N, BEFORE: 1 Screw Item (123) Discard (h) Cut the conduit to the required length and install as shown Fig. A-GBKAA Sheet 01 , Fig. A-GBKAA Sheet 02, Fig. A-GBKAA Sheet 03, Fig. A-GBKAA Sheet 04, Fig. A-GBKAA Sheet 05, Fig. A-GBKAA Sheet 06, Fig. A-GBKAA Sheet 07, Fig. AGBKAA Sheet 08 and Fig. A-GBKAA Sheet 09, Details B and R: 3 Sleeve ABS0596S004 Item 1 DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 127 6

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# @A310 SERVICE BULLETIN
1.5 (ME) Conduit NSA935805-09 Item 109 1 One part 1500.0 mm (59.06 in.) to the electrical wires for 10QT-A and 10QT-B of route 2S/636VB, refer to the Hook-up Chart 2, Fig. A-GHBAA Sheet 01 (i) Connect the electrical wires of route 2S to the receptacles 40VC and 5006VC in accordance with the Hook-up Chart 2, Lines 2 thru 8, END 1, Fig. A-GHBAA Sheet 01 . Use the contact pins if required: 7 Pin NSA938184PV1601 Item 126 (j) Install, refer to Fig. A-GBKAA Sheet 08, Detail P, AFTER: 1 Spacer NSA5527-03-02D Item 31 1 Clamp NSA935807C09 Item 117 1 Screw NAS1801-3-31 Item 123 1 Spacer NSA5527-03-07D Item 131 (k) Install, refer to Fig. A-GBKAA Sheet 07, Detail M, AFTER: 1 Clamp NSA935807C09 Item 117 1 Screw NAS1801-3-31 Item 123 1 Spacer NSA5527-03-08D Item 130 (l) Install, refer to Fig. A-GBKAA Sheet 06, Detail K, AFTER: 1 Spacer NSA5527-03-02D Item 31 1 Clamp NSA935807C09 Item 117 1 Screw NAS1096-3-40 Item 121 (m) Install, refer to Fig. A-GBKAA Sheet 05, Detail H, AFTER: 2 Washer NSA935808-01 Item (112) Retained at removal 2 Screw NAS1096-3-23 Item (113) Retained at removal 2 Clamp NSA935807C09 Item 117 (n) Install, refer to Fig. A-GBKAA Sheet 04, Detail F, AFTER: 1 Washer NSA935808-01 Item (112) Retained at removal
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 128 6

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# @A310 SERVICE BULLETIN
1 Screw NAS1096-3-23 Item (113) Retained at removal 1 Clamp NSA935807C09 Item 117 (o) Install, refer to Fig. A-GBKAA Sheet 03, Detail D, AFTER: 1 Washer NSA935808-01 Item (112) Retained at removal 1 Screw NAS1096-3-23 Item (113) Retained at removal 1 Nut NAS1291C3M Item (116) Retained at removal 1 Washer AN960KD10l Item (124) Retained at removal 1 Clamp NSA935807C09 Item 117 (p) Protect the electrical wires for 10QT-A and 10QT-B of route 2S/636VB, refer to the Hook-up Chart 2, Fig. A-GHBAA Sheet 01 and Fig. A-GBKAA Sheet 01 , Fig. AGBKAA Sheet 02, Fig. A-GBKAA Sheet 03, Fig. A-GBKAA Sheet 04, Fig. AGBKAA Sheet 05, Fig. A-GBKAA Sheet 06, Fig. A-GBKAA Sheet 07, Fig. AGBKAA Sheet 08 and Fig. A-GBKAA Sheet 09, Detail Q with: 30 Tie NSA935401-03 Item 149 30 Tie-Cable NSA935401-04 Item 150

(8) Subtask 282148-831-211-004 - Install the cable sleeves in the RH-wing forward of the front spar between rib 9 and rib 12 in zone 623. Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills ELECTRICAL Material necessary to do the job Kit 282148D01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 ABS0596S004 3 SLEEVE 10 MS21919WCH9 CLAMP 14 NAS1096-3-19 SCREW 15 NSA5527-03-03 SPACER 16 NSA8420-2 CORD
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 129 6

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# @A310 SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 150 NSA935401-04 1 TIE Kit 282148D06R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 31 NSA5527-03-02D 2 SPACER 121 NAS1096-3-40 1 SCREW References Fig. A-GBFAAImprovement of the 2S-Route in the RHWing in Zone 623 (Kit D01) Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Sheet 08 Sheet 09 Sheet 10 NOTE (1): The sleeve ABS0596S004 is supplied in pieces of 1000 mm. Cut or assemble these pieces to get the correct length. NOTE (2): The lengths of the sleeves given in this Service Bulletin are approximate lengths. Adapt the lengths of the sleeves in relation to the aircraft configuration. NOTE (3): Before you install a sleeve, cut and discard the cable ties around the cable bundle to install the sleeve correctly around the cable bundle. NOTE (4): Adapt the number of cable ties to the required quantity. Refer to Refer to Fig. A-GBFAA Sheet 01 , Fig. A-GBFAA Sheet 02, Fig. A-GBFAA Sheet 03, Fig. A-GBFAA Sheet 04, Fig. A-GBFAA Sheet 05, Fig. A-GBFAA Sheet 06, Fig. A-GBFAA Sheet 07, Fig. A-GBFAA Sheet 08, Fig. A-GBFAA Sheet 09 and Fig. AGBFAA Sheet 10 (a) At one position, remove these items from the bracket between rib 11 and rib 12 and cable bundle 2S/636VB, as shown in Details A and D: 2 Clamp MS21919WCH4 Item (22) Retain 1 Clamp MS21919WCH4 Item (22) Discard 1 Clamp MS21919WCH3 Item (23) Retain 1 Spacer NSA5527-03-01D Item (30) Retain 1 Spacer NSA5527-03-02D Item (31) Retain
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 130 6

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# @A310 SERVICE BULLETIN
1 Washer NSA935808-01 Item (112) Retain 1 Screw NAS1096-3-30 Item (121) Discard 1 Clamp NSA935807-06 Item (122) Retain (b) At two positions, remove these items from the brackets between rib 10 and rib 11 and between rib 11 and rib 12 and cable bundle 2S/636VB, as shown in Details A and F: 2 Clamp Item (22) Discard 6 Clamp MS21919WCH4 Item (22) Retain 4 Spacer NSA5527-03-01D Item (30) Retain 2 Washer NAS1149D0332K Item (40) Retain 2 Screw NAS1096-3-27 Item (52) Retain (c) At two positions, remove these items from the brackets of the rib 11 and cable bundle 2S/636VB, as shown in Details A and H: 6 Clamp MS21919WCH4 Item (22) Retain 2 Clamp Item (23) Discard 2 Spacer NSA5527-03-01D Item (30) Retain 2 Spacer NSA5527-03-04D Item (32) Retain 2 Washer NAS1149D0332K Item (40) Retain 2 Screw NAS1096-3-22 Item (51) Retain (d) At two positions, remove these items from the brackets of the rib 10 and cable bundle 2S/636VB, as shown in Details A and K: 2 Clamp Item (22) Discard 2 Clamp MS21919WCH4 Item (22) Retain 2 Spacer NSA5527-03-01D Item (30) Retain 2 Spacer Item (32) Discard 2 Washer NAS1149D0332K Item (40) Retain 2 Screw Item (51) Discard
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 131 6

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# @A310 SERVICE BULLETIN (e) Remove these items from the bracket between rib 9 and rib 10 and cable bundle 2S/636VB, as shown in Details A and M: 3 Clamp MS21919WCH4 Item (22) Retain 1 Clamp Item (23) Discard 1 Spacer NSA5527-03-01D Item (30) Retain 1 Spacer NSA5527-03-04D Item (32) Retain 1 Washer NAS1149D0332K Item (40) Retain 1 Screw NAS1096-3-22 Item (51) Retain (f) Remove these items from the bracket of the rib 9 and cable bundle 2S/636VB, as shown in Details A and T: 1 Clamp Item (21) Discard 1 Clamp MS21919WCH5 Item (21) Retain 1 Spacer NSA5527-03-02D Item (31) Retain 1 Spacer NSA5527-03-04D Item (32) Retain 1 Washer NAS1149D0332K Item (40) Retain 1 Screw NAS1096-3-27 Item (52) Retain (g) Install this cable sleeve around these identified wires from the cable bundle 2S/636VB, as shown in Details A, C, E, G, J, L, N and R: Wire number 2842-5061 Wire number 2842-5062 Wire number 2842-5063 Wire number 2842-5064 Wire number 2842-5065 Wire number 2842-5071 3 Sleeve ABS0596S004 Item 1 and attach the cable sleeves with: 3 Spacer NSA5527-03-03 Item 15

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 132 6

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# @A310 SERVICE BULLETIN
1 (ME) Cord NSA8420-2 Item 16 1 Tie-Cable NSA935401-04 Item 150 (h) At one positions, install these items to the brackets between rib 10 and rib 11 and between rib 11 and rib 12, cable sleeves, Item 1 and cable bundle 2S/636VB, as shown in Details A and E: 2 Clamp MS21919WCH4 Item (22) Retained at removal 1 Clamp MS21919WCH3 Item (23) Retained at removal 1 Spacer NSA5527-03-01D Item (30) Retained at removal 1 Spacer NSA5527-03-02D Item (31) Retained at removal 1 Washer NSA935808-01 Item (112) Retained at removal 1 Clamp NSA935807-06 Item (122) Retained at removal 1 Clamp MS21919WCH9 Item 10 2 Spacer NSA5527-03-02D Item 31 1 Screw NAS1096-3-40 Item 121 (i) At two positions, install these items to the brackets between rib 10 and rib 11 and between rib 11 and rib 12, cable sleeves, Item 1 and cable bundle 2S/636VB, as shown in Details A and G: 6 Clamp MS21919WCH4 Item (22) Retained at removal 4 Spacer NSA5527-03-01D Item (30) Retained at removal 2 Washer NAS1149D0332K Item (40) Retained at removal 2 Screw NAS1096-3-27 Item (52) Retained at removal 2 Clamp MS21919WCH9 Item 10

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 133 6

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# @A310 SERVICE BULLETIN (j) At two positions, install these items to the brackets of the rib 11, cable sleeves, Item 1 and cable bundle 2S/636VB, as shown in Details A and J: 2 Clamp MS21919WCH4 Item (22) Retained at removal 1 Spacer NSA5527-03-01D Item (30) Retained at removal 1 Spacer NSA5527-03-04D Item (32) Retained at removal 1 Washer NAS1149D0332K Item (40) Retained at removal 1 Screw NAS1096-3-22 Item (51) Retained at removal 1 Clamp MS21919WCH9 Item 10 (k) At two positions, install these items to the brackets of the rib 10, cable sleeves, Item 1 and cable bundle 2S/636VB, as shown in Details A and L: 2 Clamp MS21919WCH4 Item (22) Retained at removal 2 Spacer NSA5527-03-01D Item (30) Retained at removal 2 Washer NAS1149D0332K Item (40) Retained at removal 2 Clamp MS21919WCH9 Item 10 2 Screw NAS1096-3-19 Item 14 (l) Install these items to the bracket between rib 9 and rib 10, cable sleeves, Item 1 and cable bundle 2S/636VB, as shown in Details A and Q: 3 Clamp MS21919WCH4 Item (22) Retained at removal 1 Spacer NSA5527-03-01D Item (30) Retained at removal 1 Spacer NSA5527-03-04D Item (32) Retained at removal 1 Washer NAS1149D0332K Item (40) Retained at removal

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 134 6

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# @A310 SERVICE BULLETIN
1 Screw NAS1096-3-22 Item (51) Retained at removal 1 Clamp MS21919WCH9 Item 10 (m) Install these items to the bracket of the rib 9, cable sleeves, Item 1 and cable bundle 2S/636VB, as shown in Details A and Q: 1 Clamp MS21919WCH5 Item (21) Retained at removal 1 Spacer NSA5527-03-02D Item (31) Retained at removal 1 Spacer NSA5527-03-04D Item (32) Retained at removal 1 Washer NAS1149D0332K Item (40) Retained at removal 1 Screw NAS1096-3-27 Item (52) Retained at removal 1 Clamp MS21919WCH9 Item 10 **CONF 005 (1) Subtask 282148-831-405-001 - Install a New Bracket on the Sub Spar Behind the Front Spar Between RIB 8 and RIB 9 on the RH Wing Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills AIRFRAME Material necessary to do the job Kit 282148B01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 A5725068600000 1 Bracket 2 ASNA0078A502 2 Rivet Consumable CMLB01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Corrosion Inhibiting Low Adhesion Sealant 09-018 As required Solvent General Purpose 11-026 As required
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 135 6

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# @A310 SERVICE BULLETIN

ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Lint-Free Cotton Cloth 19-003 As required References Fig. A-UBAAA Location of Bracket on the Sub Spar Behind the Front Spar Between RIB 8 and RIB 9 (RH Wing) Sheet 01

Refer to Fig. A-UBAAA Sheet 01 (a) Remove from the sub spar behind the front spar between RIB 8 and RIB 9 on the RH wing, the items that follow: 2 Rivet NSA54213510DCA Item (2) Discard 1 Bracket A5724630400000 Item (1) Discard (b) Clean the mating surfaces use Lint-Free Cotton Cloth 19-003 As required

made moist with Solvent General Purpose 11-026 As required (c) Put the 1 Bracket A5725068600000 Item 1 in position on the sub spar behind the front spar between RIB 8 and RIB 9 on the RH wing (Refer to Fig. A-UBAAA Sheet 01 ). (d) Copy drill the two holes from the sub spar through the Bracket, Item 1 to a dimension of between 4.060 and 4.160 mm (0.160 and 0.164 in.). (e) Deburr the holes that have been worked. (f) Use Corrosion Inhibiting Low Adhesion Sealant 09-018 As required

and wet install the 1 Bracket A5725068600000 Item 1 with the 2 Rivet, Blind ASNA0078A502 Item 2 DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 136 6

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# @A310 SERVICE BULLETIN on the sub spar behind the front spar between RIB 8 and RIB 9 on the RH wing. (2) Subtask 282148-831-004-001 - Install cable sleeves in the RH Electronics Rack 90VU. Manpower Resources Manhours 6.00 Minimum number of person 1 Subtask elapsed time 6.00 Skills NON SPECIFIC Material necessary to do the job Kit 282148A01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 ABS0596S004 2000 (mm) SLEEVE NSA935401-04 50 TIE References Fig. A-FCAAA Installation of Cable Sleeves in the RH Electronics Rack 90VU. Sheet 01 Fig. A-FWAAA Installation of Cable Sleeves in the RH Electronics Rack 90VU. Sheet 01

NOTE: The sleeves ABS0596S004 and ABS0596S006 are supplied in pieces of 1000 mm (39.370 inches), cut or assemble these pieces to get the correct length. NOTE: The lengths of the sleeves given in this Service Bulletin are approximate lengths. Adapt the lengths of the sleeves in relation to the aircraft configuration. NOTE: Before you install a sleeve, cut and discard the cable ties around the cable bundle to install the sleeve correctly around the cable bundle. (a) On the Shelf 92VU, only around the wires identified in figure Fig. A-FWAAA Sheet 01 , from the equipment 15QT-B to the connector 2354VC, install: 1600 (mm) Sleeve ABS0596S004 Item 1 (b) Around the cable bundle of the connector 2354VC-A, install: 400 (mm) Sleeve ABS0596S004 Item 1 (c) Attach the sleeves with: 50 Tie-Cable NSA935401-04

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 137 6

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# @A310 SERVICE BULLETIN (3) Subtask 282148-831-005-001 - Install cable sleeves between FR38.2 and FR39, in the forward cargo compartment. 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 282148A01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 2 ABS0596S006 1000 (mm) SLEEVE NSA935401-05 50 TIE References Fig. A-FCBAA Installation of Cable Sleeves in the Forward Cargo Compartment. Sheet 01

NOTE: The sleeves ABS0596S004 and ABS0596S006 are supplied in pieces of 1000 mm (39.370 inches), cut or assemble these pieces to get the correct length. NOTE: The lengths of the sleeves given in this Service Bulletin are approximate lengths. Adapt the lengths of the sleeves in relation to the aircraft configuration. NOTE: Before you install a sleeve, cut and discard the cable ties around the cable bundle to install the sleeve correctly around the cable bundle. (a) Around the cable bundle of the pressure seal 20VP, install: 1000 (mm) Sleeve ABS0596S006 Item 2 (b) Attach the sleeves with: 50 Tie-Cable NSA935401-05

(4) Subtask 282148-831-006-002 - Install cable sleeves in the RH forward wing root and krueger flap. Manpower Resources Manhours 2.00 Minimum number of person 1 Subtask elapsed time 2.00 Skills NON SPECIFIC

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 138 6

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# @A310 SERVICE BULLETIN
Material necessary to do the job Kit 282148A01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 2 ABS0596S006 SLEEVE NSA935401-05 TIE References Fig. A-FCCAB Installation of Cable Sleeves in the RH forward wing root and krueger flap. Sheet 01

NOTE: The sleeves ABS0596S004 and ABS0596S006 are supplied in pieces of 1000 mm (39.370 inches), cut or assemble these pieces to get the correct length. NOTE: The lengths of the sleeves given in this Service Bulletin are approximate lengths. Adapt the lengths of the sleeves in relation to the aircraft configuration. NOTE: Before you install a sleeve, cut and discard the cable ties around the cable bundle to install the sleeve correctly around the cable bundle. (a) Around the cable bundle of the pressure seal 20VP, install: 1000 (mm) Sleeve ABS0596S006 Item 2 (b) Attach the sleeves with: 50 Tie-Cable NSA935401-05

(5) Subtask 282148-831-208-001 - Install the cable sleeves in the RH-wing forward of the front spar between rib 2 and rib 3 in zone 612. Manpower Resources Manhours 2.00 Minimum number of person 1 Subtask elapsed time 2.00 Skills ELECTRICAL Material necessary to do the job Kit 282148D01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 ABS0596S004 1 SLEEVE 11 MS21919WCH13 2 CLAMP 149 NSA935401-03 1 TIE 150 NSA935401-04 1 TIE
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 139 6

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# @A310 SERVICE BULLETIN

References Fig. A-GBEAAImprovement of the 2S-Route in the RHWing in Zone 612 (Kit D01) Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Sheet 08 NOTE (1): The sleeve ABS0596S004 is supplied in pieces of 1000 mm. Cut or assemble these pieces to get the correct length. NOTE (2): The lengths of the sleeves given in this Service Bulletin are approximate lengths. Adapt the lengths of the sleeves in relation to the aircraft configuration. NOTE (3): Before you install a sleeve, cut and discard the cable ties around the cable bundle to install the sleeve correctly around the cable bundle. NOTE (4): Adapt the number of cable ties to the required quantity. Install the cable sleeves in the RH-wing forward of the front spar between rib 2 and rib 3 in zone 612. Refer to Fig. A-GBEAA Sheet 01 , Fig. A-GBEAA Sheet 02, Fig. A-GBEAA Sheet 03, Fig. A-GBEAA Sheet 04, Fig. A-GBEAA Sheet 05, Fig. A-GBEAA Sheet 06, Fig. A-GBEAA Sheet 07 and Fig. A-GBEAA Sheet 08 (a) Remove these items from the bracket of the rib 2 and cable bundle 2S/624VB, as shown in Details A and B: 1 Clamp MS21919WCH4 Item (22) Retain 1 Clamp MS21919WCH3 Item (23) Retain 1 Spacer NSA5527-03-02D Item (31) Retain 1 Washer NAS1149D0332K Item (40) Retain 1 Screw NAS1096-3-21 Item (50) Retain 1 Clamp MS21919WCH10 Item (100) Retain 1 Clamp Item (100) Discard (b) Remove these items from the riblet and cable bundle 2S/624VB, as shown in Details A and D: 1 Clamp MS21919WCH4 Item (22) Retain

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 140 6

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# @A310 SERVICE BULLETIN
3 Spacer NSA5527-03-02D Item (31) Retain 1 Washer NAS1149D0332K Item (40) Retain 1 Screw NAS1096-3-38 Item (54) Retain 1 Clamp Item (100) Discard (c) Install this cable sleeve around these identified wires from the cable bundle 2S/624VB, as shown in Details A, C, E and F: Wire number 2842-5052 Wire number 2842-5053 Wire number 2842-5054 Wire number 2842-5055 Wire number 2842-5056 Wire number 2842-5070 1 Sleeve ABS0596S004 Item 1 and attach the cable sleeve with: 1 Tie NSA935401-03 Item 149 1 Tie-Cable NSA935401-04 Item 150 as necessary. (d) Install these items to the bracket of the rib 2, cable bundle 2S/624VB and cable sleeve, Item 1, as shown in Details A and C: 1 Clamp MS21919WCH4 Item (22) Retained at removal 1 Clamp MS21919WCH3 Item (23) Retained at removal 1 Spacer NSA5527-03-02D Item (31) Retained at removal 1 Washer NAS1149D0332K Item (40) Retained at removal 1 Screw NAS1096-3-21 Item (50) Retained at removal 1 Clamp MS21919WCH10 Item (100) Retained at removal DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 141 6

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# @A310 SERVICE BULLETIN
1 Clamp MS21919WCH13 Item 11 (e) Install these items to the riblet, cable bundle 2S/624VB and cable sleeve, Item 1, as shown in Details A and E: 1 Clamp MS21919WCH4 Item (22) Retained at removal 3 Spacer NSA5527-03-02D Item (31) Retained at removal 1 Washer NAS1149D0332K Item (40) Retained at removal 1 Screw NAS1096-3-38 Item (54) Retained at removal 1 Clamp MS21919WCH13 Item 11

(6) Subtask 282148-831-209-001 - Install the cable sleeves in the RH-wing forward of the front spar between rib 7 and rib 8 in zone 612. Manpower Resources Manhours 2.00 Minimum number of person 1 Subtask elapsed time 2.00 Skills ELECTRICAL Material necessary to do the job Kit 282148D01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 ABS0596S004 2 SLEEVE 12 MS21919WCH14 2 CLAMP 149 NSA935401-03 2 TIE 150 NSA935401-04 2 TIE References Fig. A-GBEAAImprovement of the 2S-Route in the RHWing in Zone 612 (Kit D01) Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Sheet 08 NOTE (1): The sleeves ABS0596S004 is supplied in pieces of 1000 mm. Cut or assemble these pieces to get the correct length.
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 142 6

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# @A310 SERVICE BULLETIN
NOTE (2): The lengths of the sleeves given in this Service Bulletin are approximate lengths. Adapt the lengths of the sleeves in relation to the aircraft configuration. NOTE (3): Before you install a sleeve, cut and discard the cable ties around the cable bundle to install the sleeve correctly around the cable bundle. NOTE (4): Adapt the number of cable ties to the required quantity. Refer to Fig. A-GBEAA Sheet 01 , Fig. A-GBEAA Sheet 02, Fig. A-GBEAA Sheet 03, Fig. A-GBEAA Sheet 04, Fig. A-GBEAA Sheet 05, Fig. A-GBEAA Sheet 06, Fig. A-GBEAA Sheet 07 and Fig. A-GBEAA Sheet 08 (a) Remove these items from the two brackets of the riblets and cable bundle 2S/624VB, as shown in Details A, H and K: 2 Clamp MS21919WCH4 Item (22) Retain 2 Washer NAS1149D0332K Item (40) Retain 2 Screw NAS1096-3-8 Item (55) Retain 2 Clamp Item (100) Discard (b) Install this cable sleeve around these identified wires from the cable bundle 2S/624VB, as shown in Details A, J, K, L, M and N: Wire number 2842-5052 Wire number 2842-5053 Wire number 2842-5054 Wire number 2842-5055 Wire number 2842-5056 1 Sleeve ABS0596S004 Item 1 and attach the cable sleeves with: 1 Tie NSA935401-03 Item 149 1 Tie-Cable NSA935401-04 Item 150 (c) Install this cable sleeve around this identified wire from the cable bundle 2S/624VB, as shown in Details A, J, K, L, M and N: Wire number 2842-5070 1 Sleeve ABS0596S004 Item 1 and attach the cable sleeves with:
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 143 6

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# @A310 SERVICE BULLETIN

1 Tie NSA935401-03 Item 149 1 Tie-Cable NSA935401-04 Item 150 (d) Install these items to the two brackets of the riblets, cable bundle 2S/624VB and cable sleeves, Item 1, as shown in Detail A, J and L: 2 Clamp MS21919WCH4 Item (22) Retained at removal 2 Washer NAS1149D0332K Item (40) Retained at removal 2 Screw NAS1096-3-8 Item (55) Retained at removal 2 Clamp MS21919WCH14 Item 12

(7) Subtask 282148-831-210-001 - Install the cable sleeves in the RH-wing forward of the front spar between rib 8 and rib 9 (pylon area) in zone 612. Manpower Resources Manhours 4.00 Minimum number of person 1 Subtask elapsed time 4.00 Skills ELECTRICAL Material necessary to do the job Kit 282148D02R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 ABS0596S004 2 SLEEVE 30 NSA5527-03-01D 2 SPACER 109 NSA935805-09 3 (ME) CONDUIT 117 NSA935807C09 13 CLAMP 125 B9299071900200 1 EQUIPMNT 126 NSA938184PV1601 15 PIN 149 NSA935401-03 20 TIE 150 NSA935401-04 20 TIE References Fig. A-GBGAAImprovement of the 2S-Route in the RHWing Pylon Area (Kit D02) Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Sheet 08 DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 144 6

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# @A310 SERVICE BULLETIN

References Fig. A-GHAAA Hook-up Chart Sheet 01 Fig. A-GHBAA Hook-up Chart Sheet 01
NOTE (1): The sleeves ABS0596S004 is supplied in pieces of 1000 mm. Cut or assemble these pieces to get the correct length. NOTE (2): The lengths of the sleeves given in this Service Bulletin are approximate lengths. Adapt the lengths of the sleeves in relation to the aircraft configuration. NOTE (3): Before you install a sleeve, cut and discard the cable ties around the cable bundle to install the sleeve correctly around the cable bundle. NOTE (4): Adapt the number of cable ties to the required quantity. Refer to Fig. A-GBGAA Sheet 01 , Fig. A-GBGAA Sheet 02, Fig. A-GBGAA Sheet 03, Fig. A-GBGAA Sheet 04, Fig. A-GBGAA Sheet 05, Fig. A-GBGAA Sheet 06, Fig. AGBGAA Sheet 07 and Fig. A-GBGAA Sheet 08 Refer to Fig. A-GHAAA Sheet 01 and Fig. A-GHBAA Sheet 01 (a) Disconnect these wires of route 2S from the receptacles 40VC and 5006VC in accordance with the Hook-up Chart 1, Lines 1 thru 14, END 1, Fig. A-GHAAA Sheet 01 and the Hook-up Chart 2, Lines 2 thru 8, END 1, Fig. A-GHBAA Sheet 01

. (b) Remove, refer to Fig. A-GBGAA Sheet 03, Detail D, BEFORE: 1 Spacer NSA5527-03-02D Item (31) Discard 1 Clamp NSA935807C10 Item (110) Discard 1 Clamp NSA935807C16 Item (111) Retain 1 Washer NSA935808-01 Item (112) Retain 1 Screw NAS1096-3-23 Item (113) Retain 1 Spacer NSA5527-03-05D Item (114) Discard 1 Washer NSA1149D0332K Item (115) Retain 1 Nut NAS1291C3M Item (116) Retain 1 Clamp NSA935807C09 Item (117) Retain

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 145 6

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# @A310 SERVICE BULLETIN (c) Remove, refer to Fig. A-GBGAA Sheet 04, Detail F, BEFORE: 2 Spacer NSA5527-03-01D Item (30) Retain 1 Spacer NSA5527-03-02D Item (31) Retain 1 Clamp NSA935807C10 Item (110) Retain 1 Clamp NSA935807C10 Item (110) Discard 1 Clamp NSA935807C16 Item (111) Retain 1 Washer NSA935808-01 Item (112) Retain 1 Clamp NSA935807C09 Item (117) Retain 1 Screw NAS1096-3-33 Item (118) Retain (d) Remove, refer to Fig. A-GBGAA Sheet 05, Detail H, BEFORE: 2 Spacer NSA5527-03-01D Item (30) Retain 2 Spacer NSA5527-03-02D Item (31) Retain 2 Clamp NSA935807C10 Item (110) Discard 2 Clamp NSA935807C16 Item (111) Retain 2 Spacer NSA5527-03-05D Item (114) Retain 2 Washer NSA1149D0332K Item (115) Retain 2 Clamp NSA935807C09 Item (117) Retain 2 Screw NAS1096-3-33 Item (118) Retain (e) Remove, refer to Fig. A-GBGAA Sheet 06, Detail K, BEFORE: 1 Spacer NSA5527-03-01D Item (30) Retain 1 Spacer NSA5527-03-02D Item (31) Retain 1 Clamp NSA935807C10 Item (110) Discard 1 Clamp NSA935807C16 Item (111) Retain 1 Spacer NSA5527-03-05D Item (114) Retain

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 146 6

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# @A310 SERVICE BULLETIN
1 Washer NSA1149D0332K Item (115) Retain 1 Clamp NSA935807C09 Item (117) Retain 1 Screw NAS1096-3-33 Item (118) Retain (f) Remove, refer to Fig. A-GBGAA Sheet 07, Detail M, BEFORE: 1 Spacer NSA5527-03-01D Item (30) Retain 1 Spacer NSA5527-03-02D Item (31) Retain 1 Clamp NSA935807C10 Item (110) Discard 1 Clamp NSA935807C16 Item (111) Retain 1 Washer NSA935808-01 Item (112) Retain 1 Spacer NSA5527-03-05D Item (114) Retain 1 Clamp NSA935807C09 Item (117) Retain 1 Screw NAS1096-3-33 Item (118) Retain (g) Remove, refer to Fig. A-GBGAA Sheet 08, Detail P, BEFORE: 1 Spacer NSA5527-03-02D Item (31) Retain 1 Clamp NSA935807C10 Item (110) Discard 1 Clamp NSA935807C16 Item (111) Retain 1 Washer NSA935808-01 Item (112) Retain 1 Spacer NSA5527-03-05D Item (114) Retain 1 Clamp NSA935807C09 Item (117) Retain 1 Screw NAS1096-3-25 Item (119) Retain (h) Remove the identification sleeves from the cable harnesses near the receptacles 40VC and 5006VC as shown Fig. A-GBGAA Sheet 01 , Detail A As required placard Item (125) Discard

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 147 6

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# @A310 SERVICE BULLETIN (i) Remove the protection sleeve from the cable harness as shown Fig. A-GBGAA Sheet 01 , Fig. A-GBGAA Sheet 02, Fig. A-GBGAA Sheet 03, Fig. A-GBGAA Sheet 04, Fig. A-GBGAA Sheet 05, Fig. A-GBGAA Sheet 06, Fig. A-GBGAA Sheet 07 and Fig. A-GBGAA Sheet 08, Details D, F, H, K, M and P: 1 Sleeve NSA935805-10 Item (109) Discard (j) Cut the conduit to the required length and install as shown Fig. A-GBGAA Sheet 01 , Fig. A-GBGAA Sheet 02, Fig. A-GBGAA Sheet 03, Fig. A-GBGAA Sheet 04, Fig. A-GBGAA Sheet 05, Fig. A-GBGAA Sheet 06, Fig. A-GBGAA Sheet 07 and Fig. A-GBGAA Sheet 08, Details E, G, J, L, N and Q: 3 (ME) Conduit NSA935805-09 Item 109 1 One part 1500.0 mm (59.06 in.) to the electrical wires for 10QT-A and 10QT-B of route 2S/636VB, refer to the Hook-up Chart 2, Fig. A-GHBAA Sheet 01 2 Three parts, one 520 mm (20.47 in.) and two 240.0 mm (9.45 in.) to the remaining electrical wires of route 2S/636VB, refer to Fig. A-GHAAA Sheet 01 (k) Connect the electrical wires of route 2S to the receptacles 40VC and 5006VC in accordance with the Hook-up Chart 1, Lines 1 thru 14, END 1, Fig. A-GHAAA Sheet 01 and the Hook-up Chart 2, lines 2 thru 8, END 1, Fig. A-GHBAA Sheet 01

. Use the contact pins if required: 15 Pin NSA938184PV1601 Item 126 (l) Install, refer to Fig. A-GBGAA Sheet 08, Detail Q, AFTER: 1 Spacer NSA5527-03-02D Item (31) Retained at removal 1 Clamp NSA935807C16 Item (111) Retained at removal 1 Washer NSA935808-01 Item (112) Retained at removal 1 Spacer NSA5527-03-05D Item (114) Retained at removal 2 Clamp NSA935807C09 Item (117) Retained at removal 1 Screw NAS1096-3-25 Item (119) Retained at removal 1 Clamp NSA935807C09 Item 117 (m) Install, refer to Fig. A-GBGAA Sheet 07, Detail N, AFTER: 1 Spacer NSA5527-03-01D Item (30) Retained at removal DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 148 6

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# @A310 SERVICE BULLETIN
1 Spacer NSA5527-03-02D Item (31) Retained at removal 1 Clamp NSA935807C16 Item (111) Retained at removal 1 Washer NSA935808-01 Item (112) Retained at removal 1 Spacer NSA5527-03-05D Item (114) Retained at removal 1 Clamp NSA935807C09 Item (117) Retained at removal 1 Screw NAS1096-3-33 Item (118) Retained at removal 2 Clamp NSA935807C09 Item 117 (n) Install, refer to Fig. A-GBGAA Sheet 06, Detail L, AFTER: 1 Spacer NSA5527-03-01D Item (30) Retained at removal 1 Spacer NSA5527-03-02D Item (31) Retained at removal 1 Clamp NSA935807C16 Item (111) Retained at removal 1 Spacer NSA5527-03-05D Item (114) Retained at removal 1 Washer NSA1149D0332K Item (115) Retained at removal 1 Clamp NSA935807C09 Item (117) Retained at removal 1 Screw NAS1096-3-33 Item (118) Retained at removal 2 Clamp NSA935807C09 Item 117 (o) Install, refer to Fig. A-GBGAA Sheet 05, Detail J, AFTER: 2 Spacer NSA5527-03-01D Item (30) Retained at removal 2 Spacer NSA5527-03-02D Item (31) Retained at removal DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 149 6

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# @A310 SERVICE BULLETIN
2 Clamp NSA935807C16 Item (111) Retained at removal 2 Spacer NSA5527-03-05D Item (114) Retained at removal 2 Washer NSA1149D0332K Item (115) Retained at removal 2 Clamp NSA935807C09 Item (117) Retained at removal 2 Screw NAS1096-3-33 Item (118) Retained at removal 4 Clamp NSA935807C09 Item 117 (p) Install, refer to Fig. A-GBGAA Sheet 04, Detail G, AFTER: 2 Spacer NSA5527-03-01D Item (30) Retained at removal 1 Spacer NSA5527-03-02D Item (31) Retained at removal 1 Clamp NSA935807C10 Item (110) Retained at removal 1 Clamp NSA935807C16 Item (111) Retained at removal 1 Washer NSA935808-01 Item (112) Retained at removal 1 Clamp NSA935807C09 Item (117) Retained at removal 1 Screw NAS1096-3-33 Item (118) Retained at removal 2 Clamp NSA935807C09 Item 117 (q) Install, refer to Fig. A-GBGAA Sheet 03, Detail E, AFTER: 2 Spacer NSA5527-03-01D Item 30 1 Clamp NSA935807C16 Item (111) Retained at removal 1 Washer NSA935808-01 Item (112) Retained at removal
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 150 6

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# @A310 SERVICE BULLETIN
1 Screw NAS1096-3-23 Item (113) Retained at removal 1 Washer NSA1149D0332K Item (115) Retained at removal 1 Nut NAS1291C3M Item (116) Retained at removal 1 Clamp NSA935807C09 Item (117) Retained at removal 2 Clamp NSA935807C09 Item 117 (r) Protect the electrical wires for 10QT-A and 10QT-B of route 2S/636VB, refer to the Hook-up Chart 2, Fig. A-GHBAA Sheet 01 with: 2 Sleeve ABS0596S004 Item 1 and 20 Tie NSA935401-03 Item 149 20 Tie-Cable NSA935401-04 Item 150 (s) Install the identification placards: 1 Placard set B9299071900200 Item 125

(8) Subtask 282148-831-211-001 - Install the cable sleeves in the RH-wing forward of the front spar between rib 9 and rib 12 in zone 623. Manpower Resources Manhours 4.00 Minimum number of person 1 Subtask elapsed time 4.00 Skills ELECTRICAL Material necessary to do the job Kit 282148D01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 ABS0596S004 3 SLEEVE 10 MS21919WCH9 8 CLAMP 14 NAS1096-3-19 2 SCREW 15 NSA5527-03-03 3 SPACER 16 NSA8420-2 0.5 (ME) CORD 149 NSA935401-03 1 TIE 150 NSA935401-04 1 TIE
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 151 6

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# @A310 SERVICE BULLETIN

Kit 282148D02R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 31 NSA5527-03-02D 2 SPACER 121 NAS1096-3-40 1 SCREW References Fig. A-GBFAAImprovement of the 2S-Route in the RHWing in Zone 623 (Kit D01) Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Sheet 08 Sheet 09 Sheet 10 NOTE (1): The sleeves ABS0596S004 is supplied in pieces of 1000 mm. Cut or assemble these pieces to get the correct length. NOTE (2): The lengths of the sleeves given in this Service Bulletin are approximate lengths. Adapt the lengths of the sleeves in relation to the aircraft configuration. NOTE (3): Before you install a sleeve, cut and discard the cable ties around the cable bundle to install the sleeve correctly around the cable bundle. NOTE (4): Adapt the number of cable ties to the required quantity. Refer to Fig. A-GBFAA Sheet 01 , Fig. A-GBFAA Sheet 02, Fig. A-GBFAA Sheet 03, Fig. A-GBFAA Sheet 04, Fig. A-GBFAA Sheet 05, Fig. A-GBFAA Sheet 06, Fig. A-GBFAA Sheet 07, Fig. A-GBFAA Sheet 08, Fig. A-GBFAA Sheet 09 and Fig. A-GBFAA Sheet 10 (a) At one position, remove these items from the bracket between rib 11 and rib 12 and cable bundle 2S/636VB, as shown in Details A and D: 2 Clamp MS21919WCH4 Item (22) Retain 1 Clamp MS21919WCH4 Item (22) Discard 1 Clamp MS21919WCH3 Item (23) Retain 1 Spacer NSA5527-03-01D Item (30) Retain 1 Spacer NSA5527-03-02D Item (31) Retain 1 Washer NSA935808-01 Item (112) Retain 1 Screw NAS1096-3-30 Item (121) Discard

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 152 6

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# @A310 SERVICE BULLETIN
1 Clamp NSA935807-06 Item (122) Retain (b) At two positions, remove these items from the brackets between rib 10 and rib 11 and between rib 11 and rib 12 and cable bundle 2S/636VB, as shown in Details A and F: 2 Clamp Item (22) Discard 6 Clamp MS21919WCH4 Item (22) Retain 4 Spacer NSA5527-03-01D Item (30) Retain 2 Washer NAS1149D0332K Item (40) Retain 2 Screw NAS1096-3-27 Item (52) Retain (c) At two positions, remove these items from the brackets of the rib 11 and cable bundle 2S/636VB, as shown in Details A and H: 2 Clamp MS21919WCH4 Item (22) Retain 1 Clamp Item (23) Discard 1 Spacer NSA5527-03-01D Item (30) Retain 1 Spacer NSA5527-03-04D Item (32) Retain 1 Washer NAS1149D0332K Item (40) Retain 1 Screw NAS1096-3-22 Item (51) Retain (d) At two positions, remove these items from the brackets of the rib 10 and cable bundle 2S/636VB, as shown in Details A and K: 2 Clamp Item (22) Discard 2 Clamp MS21919WCH4 Item (22) Retain 2 Spacer NSA5527-03-01D Item (30) Retain 2 Spacer Item (32) Discard 2 Washer NAS1149D0332K Item (40) Retain 2 Screw Item (51) Discard (e) Remove these items from the bracket between rib 9 and rib 10 and cable bundle 2S/636VB, as shown in Details A and M: 3 Clamp MS21919WCH4 Item (22) Retain DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 153 6

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# @A310 SERVICE BULLETIN
1 Clamp Item (23) Discard 1 Spacer NSA5527-03-01D Item (30) Retain 1 Spacer NSA5527-03-04D Item (32) Retain 1 Washer NAS1149D0332K Item (40) Retain 1 Screw NAS1096-3-22 Item (51) Retain (f) Remove these items from the bracket of the rib 9 and cable bundle 2S/636VB, as shown in Details A and T: 1 Clamp Item (21) Discard 1 Clamp MS21919WCH5 Item (21) Retain 1 Spacer NSA5527-03-02D Item (31) Retain 1 Spacer NSA5527-03-04D Item (32) Retain 1 Washer NAS1149D0332K Item (40) Retain 1 Screw NAS1096-3-27 Item (52) Retain (g) Install this cable sleeve around these identified wires from the cable bundle 2S/636VB, as shown in Details A, C, E, G, J, L, N, A and R: Wire number 2842-5061 Wire number 2842-5062 Wire number 2842-5063 Wire number 2842-5064 Wire number 2842-5065 Wire number 2842-5071 3 Sleeve ABS0596S004 Item 1 and attach the cable sleeves with: 3 Spacer NSA5527-03-03 Item 15 0.5 (ME) Cord NSA8420-2 Item 16 1 Tie NSA935401-03 Item 149 1 Tie-Cable NSA935401-04 Item 150 DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 154 6

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# @A310 SERVICE BULLETIN (h) At one positions, install these items to the brackets between rib 10 and rib 11 and between rib 11 and rib 12, cable sleeves, Item 1 and cable bundle 2S/636VB, as shown in Details A and E: 2 Clamp MS21919WCH4 Item (22) Retained at removal 1 Clamp MS21919WCH3 Item (23) Retained at removal 1 Spacer NSA5527-03-01D Item (30) Retained at removal 1 Spacer NSA5527-03-02D Item (31) Retained at removal 1 Washer NSA935808-01 Item (112) Retained at removal 1 Clamp NSA935807-06 Item (122) Retained at removal 1 Clamp MS21919WCH9 Item 10 2 Spacer NSA5527-03-02D Item 31 1 Screw NAS1096-3-40 Item 121 (i) At two positions, install these items to the brackets between rib 10 and rib 11 and between rib 11 and rib 12, cable sleeves, Item 1 and cable bundle 2S/636VB, as shown in Details A and G: 6 Clamp MS21919WCH4 Item (22) Retained at removal 4 Spacer NSA5527-03-01D Item (30) Retained at removal 2 Washer NAS1149D0332K Item (40) Retained at removal 2 Screw NAS1096-3-27 Item (52) Retained at removal 2 Clamp MS21919WCH9 Item 10 (j) At two positions, install these items to the brackets of the rib 11, cable sleeves, Item 1 and cable bundle 2S/636VB, as shown in Details A and J: 2 Clamp MS21919WCH4 Item (22) Retained at removal

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 155 6

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# @A310 SERVICE BULLETIN
1 Spacer NSA5527-03-01D Item (30) Retained at removal 1 Spacer NSA5527-03-04D Item (32) Retained at removal 1 Washer NAS1149D0332K Item (40) Retained at removal 1 Screw NAS1096-3-22 Item (51) Retained at removal 1 Clamp MS21919WCH9 Item 10 (k) At two positions, install these items to the brackets of the rib 10, cable sleeves, Item 1 and cable bundle 2S/636VB, as shown in Details A and L: 2 Clamp MS21919WCH4 Item (22) Retained at removal 2 Spacer NSA5527-03-01D Item (30) Retained at removal 2 Washer NAS1149D0332K Item (40) Retained at removal 2 Clamp MS21919WCH9 Item 10 2 Screw NAS1096-3-19 Item 14 (l) Install these items to the bracket between rib 9 and rib 10, cable sleeves, Item 1 and cable bundle 2S/636VB, as shown in Details A and N: 3 Clamp MS21919WCH4 Item (22) Retained at removal 1 Spacer NSA5527-03-01D Item (30) Retained at removal 1 Spacer NSA5527-03-04D Item (32) Retained at removal 1 Washer NAS1149D0332K Item (40) Retained at removal 1 Screw NAS1096-3-22 Item (51) Retained at removal 1 Clamp MS21919WCH9 Item 10

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 156 6

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# @A310 SERVICE BULLETIN (m) Install these items to the bracket of the rib 9, cable sleeves, Item 1 and cable bundle 2S/636VB, as shown in Details A and Q: 1 Clamp MS21919WCH5 Item (21) Retained at removal 1 Spacer NSA5527-03-02D Item (31) Retained at removal 1 Spacer NSA5527-03-04D Item (32) Retained at removal 1 Washer NAS1149D0332K Item (40) Retained at removal 1 Screw NAS1096-3-27 Item (52) Retained at removal 1 Clamp MS21919WCH9 Item 10 **CONF 006 (1) Subtask 282148-831-405-001 - Install a New Bracket on the Sub Spar Behind the Front Spar Between RIB 8 and RIB 9 on the RH Wing Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills AIRFRAME Material necessary to do the job Kit 282148B01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 A5725068600000 1 Bracket 2 ASNA0078A502 2 Rivet Consumable CMLB01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Corrosion Inhibiting Low Adhesion Sealant 09-018 As required Solvent General Purpose 11-026 As required Lint-Free Cotton Cloth 19-003 As required

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 157 6

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# @A310 SERVICE BULLETIN

References Fig. A-UBAAA Location of Bracket on the Sub Spar Behind the Front Spar Between RIB 8 and RIB 9 (RH Wing) Sheet 01

Refer to Fig. A-UBAAA Sheet 01 (a) Remove from the sub spar behind the front spar between RIB 8 and RIB 9 on the RH wing, the items that follow: 2 Rivet NSA54213510DCA Item (2) Discard 1 Bracket A5724630400000 Item (1) Discard (b) Clean the mating surfaces use Lint-Free Cotton Cloth 19-003 As required

made moist with Solvent General Purpose 11-026 As required (c) Put the 1 Bracket A5725068600000 Item 1 in position on the sub spar behind the front spar between RIB 8 and RIB 9 on the RH wing (Refer to Fig. A-UBAAA Sheet 01 ). (d) Copy drill the two holes from the sub spar through the Bracket, Item 1 to a dimension of between 4.060 and 4.160 mm (0.160 and 0.164 in.). (e) Deburr the holes that have been worked. (f) Use Corrosion Inhibiting Low Adhesion Sealant 09-018 As required

and wet install the 1 Bracket A5725068600000 Item 1 with the 2 Rivet, Blind ASNA0078A502 Item 2 on the sub spar behind the front spar between RIB 8 and RIB 9 on the RH wing.

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 158 6

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# @A310 SERVICE BULLETIN (2) Subtask 282148-831-004-001 - Install cable sleeves in the RH Electronics Rack 90VU. Manpower Resources Manhours 6.00 Minimum number of person 1 Subtask elapsed time 6.00 Skills NON SPECIFIC Material necessary to do the job Kit 282148A01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 ABS0596S004 2000 (mm) SLEEVE NSA935401-04 50 TIE References Fig. A-FCAAA Installation of Cable Sleeves in the RH Electronics Rack 90VU. Sheet 01 Fig. A-FWAAA Installation of Cable Sleeves in the RH Electronics Rack 90VU. Sheet 01

NOTE: The sleeves ABS0596S004 and ABS0596S006 are supplied in pieces of 1000 mm (39.370 inches), cut or assemble these pieces to get the correct length. NOTE: The lengths of the sleeves given in this Service Bulletin are approximate lengths. Adapt the lengths of the sleeves in relation to the aircraft configuration. NOTE: Before you install a sleeve, cut and discard the cable ties around the cable bundle to install the sleeve correctly around the cable bundle. (a) On the Shelf 92VU, only around the wires identified in figure Fig. A-FWAAA Sheet 01 , from the equipment 15QT-B to the connector 2354VC, install: 1600 (mm) Sleeve ABS0596S004 Item 1 (b) Around the cable bundle of the connector 2354VC-A, install: 400 (mm) Sleeve ABS0596S004 Item 1 (c) Attach the sleeves with: 50 Tie-Cable NSA935401-04

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 159 6

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# @A310 SERVICE BULLETIN (3) Subtask 282148-831-005-001 - Install cable sleeves between FR38.2 and FR39, in the forward cargo compartment. 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 282148A01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 2 ABS0596S006 1000 (mm) SLEEVE NSA935401-05 50 TIE References Fig. A-FCBAA Installation of Cable Sleeves in the Forward Cargo Compartment. Sheet 01

NOTE: The sleeves ABS0596S004 and ABS0596S006 are supplied in pieces of 1000 mm (39.370 inches), cut or assemble these pieces to get the correct length. NOTE: The lengths of the sleeves given in this Service Bulletin are approximate lengths. Adapt the lengths of the sleeves in relation to the aircraft configuration. NOTE: Before you install a sleeve, cut and discard the cable ties around the cable bundle to install the sleeve correctly around the cable bundle. (a) Around the cable bundle of the pressure seal 20VP, install: 1000 (mm) Sleeve ABS0596S006 Item 2 (b) Attach the sleeves with: 50 Tie-Cable NSA935401-05

(4) Subtask 282148-831-006-002 - Install cable sleeves in the RH forward wing root and krueger flap. Manpower Resources Manhours 2.00 Minimum number of person 1 Subtask elapsed time 2.00 Skills NON SPECIFIC

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 160 6

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# @A310 SERVICE BULLETIN
Material necessary to do the job Kit 282148A01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 2 ABS0596S006 SLEEVE NSA935401-05 TIE References Fig. A-FCCAB Installation of Cable Sleeves in the RH forward wing root and krueger flap. Sheet 01

NOTE: The sleeves ABS0596S004 and ABS0596S006 are supplied in pieces of 1000 mm (39.370 inches), cut or assemble these pieces to get the correct length. NOTE: The lengths of the sleeves given in this Service Bulletin are approximate lengths. Adapt the lengths of the sleeves in relation to the aircraft configuration. NOTE: Before you install a sleeve, cut and discard the cable ties around the cable bundle to install the sleeve correctly around the cable bundle. (a) Around the cable bundle of the pressure seal 20VP, install: 1000 (mm) Sleeve ABS0596S006 Item 2 (b) Attach the sleeves with: 50 Tie-Cable NSA935401-05

(5) Subtask 282148-831-208-002 - Install the cable sleeves in the RH-wing forward of the front spar between rib 2 and rib 3 in zone 612. Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills ELECTRICAL Material necessary to do the job Kit 282148D01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 ABS0596S004 1 SLEEVE 11 MS21919WCH13 CLAMP 149 NSA935401-03 1 TIE 150 NSA935401-04 1 TIE
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 161 6

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# @A310 SERVICE BULLETIN

References Fig. A-GBEAAImprovement of the 2S-Route in the RHWing in Zone 612 (Kit D01) Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Sheet 08 NOTE (1): The sleeves ABS0596S004 is supplied in pieces of 1000 mm. Cut or assemble these pieces to get the correct length. NOTE (2): The lengths of the sleeves given in this Service Bulletin are approximate lengths. Adapt the lengths of the sleeves in relation to the aircraft configuration. NOTE (3): Before you install a sleeve, cut and discard the cable ties around the cable bundle to install the sleeve correctly around the cable bundle. NOTE (4): Adapt the number of cable ties to the required quantity. Refer to Fig. A-GBEAA Sheet 01 , Fig. A-GBEAA Sheet 02, Fig. A-GBEAA Sheet 03, Fig. A-GBEAA Sheet 04, Fig. A-GBEAA Sheet 05, Fig. A-GBEAA Sheet 06, Fig. A-GBEAA Sheet 07 and Fig. A-GBEAA Sheet 08 (a) Remove these items from the bracket of the rib 2 and cable bundle 2S/624VB, as shown in Details A and B: 1 Clamp MS21919WCH4 Item (22) Retain 1 Clamp MS21919WCH3 Item (23) Retain 1 Spacer NSA5527-03-02D Item (31) Retain 1 Washer NAS1149D0332K Item (40) Retain 1 Screw NAS1096-3-21 Item (50) Retain 1 Clamp MS21919WCH10 Item (100) Retain 1 Clamp Item (100) Discard (b) Remove these items from the riblet and cable bundle 2S/624VB, as shown in Details A and D: 1 Clamp MS21919WCH4 Item (22) Retain 3 Spacer NSA5527-03-02D Item (31) Retain 1 Washer NAS1149D0332K Item (40) Retain
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 162 6

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# @A310 SERVICE BULLETIN
1 Screw NAS1096-3-38 Item (54) Retain 1 Clamp Item (100) Discard (c) Install this cable sleeve around these identified wires from the cable bundle 2S/624VB, as shown in Details A, C, E and F: Wire number 2842-5052 Wire number 2842-5053 Wire number 2842-5054 Wire number 2842-5055 Wire number 2842-5056 Wire number 2842-5070 Install this cable sleeve around these identified wires from the cable bundle 2S/624VB, as shown in Details A, C, E and F: Wire number 2842-5052 Wire number 2842-5053 Wire number 2842-5054 Wire number 2842-5055 Wire number 2842-5056 Wire number 2842-5070 1 Sleeve ABS0596S004 Item 1 and attach the cable sleeve with: 1 Tie NSA935401-03 Item 149 1 Tie-Cable NSA935401-04 Item 150 (d) Install these items to the bracket of the rib 2, cable bundle 2S/624VB and cable sleeve, Item 1, as shown in Details A and C: 1 Clamp MS21919WCH4 Item (22) Retained at removal 1 Clamp MS21919WCH3 Item (23) Retained at removal 1 Spacer NSA5527-03-02D Item (31) Retained at removal
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 163 6

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# @A310 SERVICE BULLETIN
1 Washer NAS1149D0332K Item (40) Retained at removal 1 Screw NAS1096-3-21 Item (50) Retained at removal 1 Clamp MS21919WCH10 Item (100) Retained at removal 1 Clamp MS21919WCH13 Item 11 (e) Install these items to the riblet, cable bundle 2S/624VB and cable sleeve, Item 1, as shown in Details A and E: 1 Clamp MS21919WCH4 Item (22) Retained at removal 3 Spacer NSA5527-03-02D Item (31) Retained at removal 1 Washer NAS1149D0332K Item (40) Retained at removal 1 Screw NAS1096-3-38 Item (54) Retained at removal 1 Clamp MS21919WCH13 Item 11

(6) Subtask 282148-831-209-002 - Install the cable sleeves in the RH-wing forward of the front spar between rib 7 and rib 8 in zone 612. Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills ELECTRICAL Material necessary to do the job Kit 282148D01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 ABS0596S004 2 SLEEVE 12 MS21919WCH14 CLAMP 149 NSA935401-03 2 TIE 150 NSA935401-04 2 TIE

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 164 6

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# @A310 SERVICE BULLETIN

References Fig. A-GBEAAImprovement of the 2S-Route in the RHWing in Zone 612 (Kit D01) Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Sheet 08 NOTE (1): The sleeves ABS0596S004 is are supplied in pieces of 1000 mm. Cut or assemble these pieces to get the correct length. NOTE (2): The lengths of the sleeves given in this Service Bulletin are approximate lengths. Adapt the lengths of the sleeves in relation to the aircraft configuration. NOTE (3): Before you install a sleeve, cut and discard the cable ties around the cable bundle to install the sleeve correctly around the cable bundle. NOTE (4): Adapt the number of cable ties to the required quantity. Refer to Fig. A-GBEAA Sheet 01 , Fig. A-GBEAA Sheet 02, Fig. A-GBEAA Sheet 03, Fig. A-GBEAA Sheet 04, Fig. A-GBEAA Sheet 05, Fig. A-GBEAA Sheet 06, Fig. A-GBEAA Sheet 07 and Fig. A-GBEAA Sheet 08 (a) Remove these items from the two brackets of the riblets and cable bundle 2S/624VB, as shown in Details A, H and K: 2 Clamp MS21919WCH4 Item (22) Retain 2 Washer NAS1149D0332K Item (40) Retain 2 Screw NAS1096-3-8 Item (55) Retain 2 Clamp Item (100) Discard (b) Install this cable sleeve around these identified wires from the cable bundle 2S/624VB, as shown in Details A, J, K, L, M and N: Wire number 2842-5052 Wire number 2842-5053 Wire number 2842-5054 Wire number 2842-5055 Wire number 2842-5056 1 Sleeve ABS0596S004 Item 1 and attach the cable sleeves with: DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 165 6

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# @A310 SERVICE BULLETIN

1 Tie NSA935401-03 Item 149 1 Tie-Cable NSA935401-04 Item 150 (c) Install this cable sleeve around this identified wire from the cable bundle 2S/624VB, as shown in Details A, J, K, L, M and N: Wire number 2842-5070 1 Sleeve ABS0596S004 Item 1 and attach the cable sleeves with: 1 Tie NSA935401-03 Item 149 1 Tie-Cable NSA935401-04 Item 150 (d) Install these items to the two brackets of the riblets, cable bundle 2S/624VB and cable sleeves, Item 1, as shown in Detail A, J and L: 2 Clamp MS21919WCH4 Item (22) Retained at removal 2 Washer NAS1149D0332K Item (40) Retained at removal 2 Screw NAS1096-3-8 Item (55) Retained at removal 2 Clamp MS21919WCH14 Item 12

(7) Subtask 282148-831-210-002 - Install the cable sleeves in the RH-wing forward of the front spar between rib 8 and rib 9 (pylon area) in zone 612. Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills ELECTRICAL Material necessary to do the job Kit 282148D02R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 109 NSA935805-09 CONDUIT Kit 282148D03R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 ABS0596S004 3 SLEEVE
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 166 6

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# @A310 SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 31 NSA5527-03-02D 1 SPACER 117 NSA935807C09 7 CLAMP 123 NAS1801-3-31 3 SCREW 126 NSA938184PV1601 7 PIN 130 NSA5527-03-08D 1 SPACER 131 NSA5527-03-07D 1 SPACER 132 B9299071900600 1 EQUIPMNT 149 NSA935401-03 20 TIE 150 NSA935401-04 20 TIE References Fig. A-GBHAAImprovement of the 2S-Route in the RHWing Pylon Area (Kit D03) Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Sheet 08 Fig. A-GHBAA Hook-up Chart Sheet 01
NOTE (1): The sleeves ABS0596S004 is supplied in pieces of 1000 mm. Cut or assemble these pieces to get the correct length. NOTE (2): The lengths of the sleeves given in this Service Bulletin are approximate lengths. Adapt the lengths of the sleeves in relation to the aircraft configuration. NOTE (3): Before you install a sleeve, cut and discard the cable ties around the cable bundle to install the sleeve correctly around the cable bundle. NOTE (4): Adapt the number of cable ties to the required quantity. Refer to Fig. A-GBHAA Sheet 01 , Fig. A-GBHAA Sheet 02, Fig. A-GBHAA Sheet 03, Fig. A-GBHAA Sheet 04, Fig. A-GBHAA Sheet 05, Fig. A-GBHAA Sheet 06, Fig. AGBHAA Sheet 07 and Fig. A-GBHAA Sheet 08 (a) Disconnect the wires of route 2S from the receptacles 40VC and 5006VC in accordance with the Hook-up Chart 2, Lines 2 thru 8, END 1, Fig. A-GHBAA Sheet 01

. (b) Remove, refer to Fig. A-GBHAA Sheet 03, Detail D, BEFORE: 1 Spacer NSA5527-03-02D Item (31) Retain 2 Clamp NSA935807C16 Item (111) Retain 1 Washer NSA935808-01 Item (112) Retain DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 167 6

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# @A310 SERVICE BULLETIN
1 Screw NAS1096-3-23 Item (113) Retain 1 Spacer NSA5527-03-05D Item (114) Retain 1 Nut NAS1291C3M Item (116) Retain 1 Washer AN960KD10l Item (124) Retain (c) Remove, refer to Fig. A-GBHAA Sheet 04, Detail F, BEFORE: 1 Spacer NSA5527-03-02D Item (31) Retain 2 Clamp NSA935807C16 Item (111) Retain 1 Washer NSA935808-01 Item (112) Retain 1 Screw NAS1096-3-23 Item (113) Retain 1 Spacer NSA5527-03-05D Item (114) Retain (d) Remove, refer to Fig. A-GBHAA Sheet 05, Detail H, BEFORE: 2 Spacer NSA5527-03-02D Item (31) Retain 4 Clamp NSA935807C16 Item (111) Retain 2 Washer NSA935808-01 Item (112) Retain 2 Screw NAS1096-3-23 Item (113) Retain 2 Spacer NSA5527-03-05D Item (114) Retain (e) Remove, refer to Fig. A-GBHAA Sheet 06, Detail K, BEFORE: 1 Spacer NSA5527-03-02D Item (31) Retain 2 Clamp NSA935807C16 Item (111) Retain 1 Washer NSA935808-01 Item (112) Retain 1 Screw NAS1096-3-23 Item (113) Discard 1 Clamp NSA5516-04NV Item (120) Retain (f) Remove, refer to Fig. A-GBHAA Sheet 07, Detail M, BEFORE: 1 Spacer NSA5527-03-02D Item (31) Retain 2 Clamp NSA935807C16 Item (111) Retain DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 168 6

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# @A310 SERVICE BULLETIN
1 Washer NSA935808-01 Item (112) Retain 1 Screw NAS1096-3-23 Item (113) Discard 1 Spacer NSA5527-03-05D Item (114) Retain (g) Remove, refer to Fig. A-GBHAA Sheet 08, Detail P, BEFORE: 1 Spacer NSA5527-03-02D Item (31) Retain 2 Clamp NSA935807C16 Item (111) Retain 1 Washer NSA935808-01 Item (112) Retain 1 Screw NAS1096-3-23 Item (113) Discard 1 Spacer NSA5527-03-05D Item (114) Retain (h) Remove the identification placards from the cable harnesses near the receptacles 52VC and 5006VC as shown Fig. A-GBHAA Sheet 02, Detail A As required placard Item (132) Discard (i) Remove the disconnected electrical wires from the protection sleeve. (j) Install to the electrical wires for 10QT-A and 10QT-B of route 2S/636VB, refer to the Hook-up Chart 2, Lines 2 thru 8, Fig. A-GHBAA Sheet 01 : 1 (ME) Conduit NSA935805-09 Item 109 (k) Connect the electrical wires of route 2S to the receptacles 40VC and 5006VC in accordance with the Hook-up Chart 2, Lines 2 thru 8, END 1, Fig. A-GHBAA Sheet 01 . Use the contact pins if required: 7 Pin NSA938184PV1601 Item 126 (l) Install, refer to Fig. A-GBHAA Sheet 08, Detail Q, AFTER: 1 Spacer NSA5527-03-02D Item (31) Retained at removal 1 Spacer NSA5527-03-02D Item 31 2 Clamp NSA935807C16 Item (111) Retained at removal 1 Washer NSA935808-01 Item (112) Retained at removal

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 169 6

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# @A310 SERVICE BULLETIN
1 Spacer NSA5527-03-05D Item (114) Retained at removal 1 Clamp NSA935807C09 Item 117 1 Screw NAS1801-3-31 Item 123 1 Spacer NSA5527-03-07D Item 131 (m) Install, refer to Fig. A-GBHAA Sheet 07, Detail N, AFTER: 1 Spacer NSA5527-03-02D Item (31) Retained at removal 2 Clamp NSA935807C16 Item (111) Retained at removal 1 Washer NSA935808-01 Item (112) Retained at removal 1 Spacer NSA5527-03-05D Item (114) Retained at removal 1 Clamp NSA935807C09 Item 117 1 Screw NAS1801-3-31 Item 123 1 Spacer NSA5527-03-08D Item 130 (n) Install, refer to Fig. A-GBHAA Sheet 06, Detail L, AFTER: 2 Spacer NSA5527-03-02D Item (31) Retained at removal 2 Clamp NSA935807C16 Item (111) Retained at removal 1 Washer NSA935808-01 Item (112) Retained at removal 1 Clamp NSA5516-04NV Item (120) Retained at removal 1 Clamp NSA935807C09 Item 117 2 Screw NAS1801-3-31 Item 123 (o) Install, refer to Fig. A-GBHAA Sheet 05, Detail J, AFTER: 2 Spacer NSA5527-03-02D Item (31) Retained at removal
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 170 6

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# @A310 SERVICE BULLETIN
4 Clamp NSA935807C16 Item (111) Retained at removal 2 Washer NSA935808-01 Item (112) Retained at removal 2 Screw NAS1096-3-23 Item (113) Retained at removal 2 Spacer NSA5527-03-05D Item (114) Retained at removal 2 Clamp NSA935807C09 Item 117 (p) Install, refer to Fig. A-GBHAA Sheet 04, Detail G, AFTER: 1 Spacer NSA5527-03-02D Item (31) Retained at removal 2 Clamp NSA935807C16 Item (111) Retained at removal 1 Washer NSA935808-01 Item (112) Retained at removal 1 Screw NAS1096-3-23 Item (113) Retained at removal 1 Spacer NSA5527-03-05D Item (114) Retained at removal 1 Clamp NSA935807C09 Item 117 (q) Install, refer to Fig. A-GBHAA Sheet 03, Detail E, AFTER: 1 Spacer NSA5527-03-02D Item (31) Retained at removal 2 Clamp NSA935807C16 Item (111) Retained at removal 1 Washer NSA935808-01 Item (112) Retained at removal 1 Screw NAS1096-3-23 Item (113) Retained at removal 1 Spacer NSA5527-03-05D Item (114) Retained at removal 1 Nut NAS1291C3M Item (116) Retained at removal DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 171 6

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# @A310 SERVICE BULLETIN
1 Washer AN960KD10l Item (124) Retained at removal 1 Clamp NSA935807C09 Item 117 (r) Protect the electrical wires for 10QT-A and 10QT-B of route 2S/636VB, refer to the Hook-up Chart 2, Fig. A-GHBAA Sheet 01 with: 3 Sleeve ABS0596S004 Item 1 and 20 Tie NSA935401-03 Item 149 20 Tie-Cable NSA935401-04 Item 150 (s) Install the identification placards, refer to Fig. A-GBHAA Sheet 02: 1 Placard Set B9299071900600 Item 132

(8) Subtask 282148-831-211-002 - Install the cable sleeves in the RH-wing forward of the front spar between rib 9 and rib 12 in zone 623. Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills ELECTRICAL Material necessary to do the job Kit 282148D01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 ABS0596S004 3 SLEEVE 10 MS21919WCH9 CLAMP 14 NAS1096-3-19 2 SCREW 15 NSA5527-03-03 3 SPACER 16 NSA8420-2 1 (ME) CORD 149 NSA935401-03 10 TIE 150 NSA935401-04 20 TIE Kit 282148D03R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 31 NSA5527-03-02D 1 SPACER 121 NAS1096-3-40 1 SCREW

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 172 6

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# @A310 SERVICE BULLETIN

References Fig. A-GBFAAImprovement of the 2S-Route in the RHWing in Zone 623 (Kit D01) Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Sheet 08 Sheet 09 Sheet 10 NOTE (1): The sleeve ABS0596S004 is supplied in pieces of 1000 mm. Cut or assemble these pieces to get the correct length. NOTE (2): The lengths of the sleeves given in this Service Bulletin are approximate lengths. Adapt the lengths of the sleeves in relation to the aircraft configuration. NOTE (3): Before you install a sleeve, cut and discard the cable ties around the cable bundle to install the sleeve correctly around the cable bundle. NOTE (4): Adapt the number of cable ties to the required quantity. Refer to Fig. A-GBFAA Sheet 01 , Fig. A-GBFAA Sheet 02, Fig. A-GBFAA Sheet 03, Fig. A-GBFAA Sheet 04, Fig. A-GBFAA Sheet 05, Fig. A-GBFAA Sheet 06, Fig. A-GBFAA Sheet 07, Fig. A-GBFAA Sheet 08, Fig. A-GBFAA Sheet 09 and Fig. A-GBFAA Sheet 10 (a) At one position, remove these items from the bracket between rib 11 and rib 12 and cable bundle 2S/636VB, as shown in Details A and D: 2 Clamp MS21919WCH4 Item (22) Retain 1 Clamp MS21919WCH4 Item (22) Discard 1 Clamp MS21919WCH3 Item (23) Retain 1 Spacer NSA5527-03-01D Item (30) Retain 1 Spacer NSA5527-03-02D Item (31) Retain 2 Washer NSA935808-01 Item (112) Retain 2 Screw NAS1096-3-30 Item (121) Discard 1 Clamp NSA935807-06 Item (122) Retain

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 173 6

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# @A310 SERVICE BULLETIN (b) At two positions, remove these items from the brackets between rib 10 and rib 11 and between rib 11 and rib 12 and cable bundle 2S/636VB, as shown in Details A and F: 2 Clamp Item (22) Discard 6 Clamp MS21919WCH4 Item (22) Retain 4 Spacer NSA5527-03-01D Item (30) Retain 2 Washer NAS1149D0332K Item (40) Retain 2 Screw NAS1096-3-27 Item (52) Retain (c) At two positions, remove these items from the brackets of the rib 11 and cable bundle 2S/636VB, as shown in Details A and H: 6 Clamp MS21919WCH4 Item (22) Retain 2 Clamp Item (23) Discard 2 Spacer NSA5527-03-01D Item (30) Retain 2 Spacer NSA5527-03-04D Item (32) Retain 2 Washer NAS1149D0332K Item (40) Retain 2 Screw NAS1096-3-22 Item (51) Retain (d) At two positions, remove these items from the brackets of the rib 10 and cable bundle 2S/636VB, as shown in Details A and K: 2 Clamp Item (22) Discard 2 Clamp MS21919WCH4 Item (22) Retain 2 Spacer NSA5527-03-01D Item (30) Retain 2 Spacer Item (32) Discard 2 Washer NAS1149D0332K Item (40) Retain 2 Screw Item (51) Discard (e) Remove these items from the bracket between rib 9 and rib 10 and cable bundle 2S/636VB, as shown in Details A and M: 3 Clamp MS21919WCH4 Item (22) Retain

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 174 6

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# @A310 SERVICE BULLETIN
1 Clamp Item (23) Discard 1 Spacer NSA5527-03-01D Item (30) Retain 1 Spacer NSA5527-03-04D Item (32) Retain 1 Washer NAS1149D0332K Item (40) Retain 1 Screw NAS1096-3-22 Item (51) Retain (f) Remove these items from the bracket of the rib 9 and cable bundle 2S/636VB, as shown in Details A and T: 1 Clamp Item (21) Discard 1 Clamp MS21919WCH5 Item (21) Retain 1 Spacer NSA5527-03-02D Item (31) Retain 1 Spacer NSA5527-03-04D Item (32) Retain 1 Washer NAS1149D0332K Item (40) Retain 1 Screw NAS1096-3-27 Item (52) Retain (g) Install this cable sleeve around these identified wires from the cable bundle 2S/636VB, as shown in Details A, C, E, G, J, L, N, Q, R, S and T: Wire number 2842-5061 Wire number 2842-5062 Wire number 2842-5063 Wire number 2842-5064 Wire number 2842-5065 Wire number 2842-5071 3 Sleeve ABS0596S004 Item 1 and attach the cable sleeves with: 3 Spacer NSA5527-03-03 Item 15 1 (ME) Cord NSA8420-2 Item 16 10 Tie NSA935401-03 Item 149 20 Tie-Cable NSA935401-04 Item 150 DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 175 6

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# @A310 SERVICE BULLETIN (h) At one positions, install these items to the brackets between rib 10 and rib 11 and between rib 11 and rib 12, cable sleeves, Item 1 and cable bundle 2S/636VB, as shown in Details A and E: 2 Clamp MS21919WCH4 Item (22) Retained at removal 1 Clamp MS21919WCH3 Item (23) Retained at removal 1 Spacer NSA5527-03-01D Item (30) Retained at removal 1 Spacer NSA5527-03-02D Item (31) Retained at removal 1 Washer NSA935808-01 Item (112) Retained at removal 1 Clamp NSA935807-06 Item (122) Retained at removal 1 Clamp MS21919WCH9 Item 10 1 Spacer NSA5527-03-02D Item 31 1 Screw NAS1096-3-40 Item 121 (i) At two positions, install these items to the brackets between rib 10 and rib 11 and between rib 11 and rib 12, cable sleeves, Item 1 and cable bundle 2S/636VB, as shown in Details A and G: 6 Clamp MS21919WCH4 Item (22) Retained at removal 4 Spacer NSA5527-03-01D Item (30) Retained at removal 2 Washer NAS1149D0332K Item (40) Retained at removal 2 Screw NAS1096-3-27 Item (52) Retained at removal 2 Clamp MS21919WCH9 Item 10 (j) At two positions, install these items to the brackets of the rib 11, cable sleeves, Item 1 and cable bundle 2S/636VB, as shown in Details A and J: 6 Clamp MS21919WCH4 Item (22) Retained at removal

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 176 6

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# @A310 SERVICE BULLETIN
2 Spacer NSA5527-03-01D Item (30) Retained at removal 2 Spacer NSA5527-03-04D Item (32) Retained at removal 2 Washer NAS1149D0332K Item (40) Retained at removal 2 Screw NAS1096-3-22 Item (51) Retained at removal 2 Clamp MS21919WCH9 Item 10 (k) At two positions, install these items to the brackets of the rib 10, cable sleeves, Item 1 and cable bundle 2S/636VB, as shown in Details A and L: 2 Clamp MS21919WCH4 Item (22) Retained at removal 2 Spacer NSA5527-03-01D Item (30) Retained at removal 2 Washer NAS1149D0332K Item (40) Retained at removal 2 Clamp MS21919WCH9 Item 10 2 Screw NAS1096-3-19 Item 14 (l) Install these items to the bracket between rib 9 and rib 10, cable sleeves, Item 1 and cable bundle 2S/636VB, as shown in Details A and Q: 3 Clamp MS21919WCH4 Item (22) Retained at removal 1 Spacer NSA5527-03-01D Item (30) Retained at removal 1 Spacer NSA5527-03-04D Item (32) Retained at removal 1 Washer NAS1149D0332K Item (40) Retained at removal 1 Screw NAS1096-3-22 Item (51) Retained at removal 1 Clamp MS21919WCH9 Item 10

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 177 6

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# @A310 SERVICE BULLETIN (m) Install these items to the bracket of the rib 9, cable sleeves, Item 1 and cable bundle 2S/636VB, as shown in Details A and Q: 1 Clamp MS21919WCH5 Item (21) Retained at removal 1 Spacer NSA5527-03-02D Item (31) Retained at removal 1 Spacer NSA5527-03-04D Item (32) Retained at removal 1 Washer NAS1149D0332K Item (40) Retained at removal 1 Screw NAS1096-3-27 Item (52) Retained at removal 1 Clamp MS21919WCH9 Item 10 **CONF 007 (1) Subtask 282148-831-405-001 - Install a New Bracket on the Sub Spar Behind the Front Spar Between RIB 8 and RIB 9 on the RH Wing Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills AIRFRAME Material necessary to do the job Kit 282148B01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 A5725068600000 1 Bracket 2 ASNA0078A502 2 Rivet Consumable CMLB01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Corrosion Inhibiting Low Adhesion Sealant 09-018 As required Solvent General Purpose 11-026 As required Lint-Free Cotton Cloth 19-003 As required

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 178 6

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# @A310 SERVICE BULLETIN

References Fig. A-UBAAA Location of Bracket on the Sub Spar Behind the Front Spar Between RIB 8 and RIB 9 (RH Wing) Sheet 01

Refer to Fig. A-UBAAA Sheet 01 (a) Remove from the sub spar behind the front spar between RIB 8 and RIB 9 on the RH wing, the items that follow: 2 Rivet NSA54213510DCA Item (2) Discard 1 Bracket A5724630400000 Item (1) Discard (b) Clean the mating surfaces use Lint-Free Cotton Cloth 19-003 As required

made moist with Solvent General Purpose 11-026 As required (c) Put the 1 Bracket A5725068600000 Item 1 in position on the sub spar behind the front spar between RIB 8 and RIB 9 on the RH wing (Refer to Fig. A-UBAAA Sheet 01 ). (d) Copy drill the two holes from the sub spar through the Bracket, Item 1 to a dimension of between 4.060 and 4.160 mm (0.160 and 0.164 in.). (e) Deburr the holes that have been worked. (f) Use Corrosion Inhibiting Low Adhesion Sealant 09-018 As required

and wet install the 1 Bracket A5725068600000 Item 1 with the 2 Rivet, Blind ASNA0078A502 Item 2 on the sub spar behind the front spar between RIB 8 and RIB 9 on the RH wing.

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 179 6

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# @A310 SERVICE BULLETIN (2) Subtask 282148-831-004-001 - Install cable sleeves in the RH Electronics Rack 90VU. Manpower Resources Manhours 6.00 Minimum number of person 1 Subtask elapsed time 6.00 Skills NON SPECIFIC Material necessary to do the job Kit 282148A01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 ABS0596S004 2000 (mm) SLEEVE NSA935401-04 50 TIE References Fig. A-FCAAA Installation of Cable Sleeves in the RH Electronics Rack 90VU. Sheet 01 Fig. A-FWAAA Installation of Cable Sleeves in the RH Electronics Rack 90VU. Sheet 01

NOTE: The sleeves ABS0596S004 and ABS0596S006 are supplied in pieces of 1000 mm (39.370 inches), cut or assemble these pieces to get the correct length. NOTE: The lengths of the sleeves given in this Service Bulletin are approximate lengths. Adapt the lengths of the sleeves in relation to the aircraft configuration. NOTE: Before you install a sleeve, cut and discard the cable ties around the cable bundle to install the sleeve correctly around the cable bundle. (a) On the Shelf 92VU, only around the wires identified in figure Fig. A-FWAAA Sheet 01 , from the equipment 15QT-B to the connector 2354VC, install: 1600 (mm) Sleeve ABS0596S004 Item 1 (b) Around the cable bundle of the connector 2354VC-A, install: 400 (mm) Sleeve ABS0596S004 Item 1 (c) Attach the sleeves with: 50 Tie-Cable NSA935401-04

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 180 6

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# @A310 SERVICE BULLETIN (3) Subtask 282148-831-005-001 - Install cable sleeves between FR38.2 and FR39, in the forward cargo compartment. 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 282148A01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 2 ABS0596S006 1000 (mm) SLEEVE NSA935401-05 50 TIE References Fig. A-FCBAA Installation of Cable Sleeves in the Forward Cargo Compartment. Sheet 01

NOTE: The sleeves ABS0596S004 and ABS0596S006 are supplied in pieces of 1000 mm (39.370 inches), cut or assemble these pieces to get the correct length. NOTE: The lengths of the sleeves given in this Service Bulletin are approximate lengths. Adapt the lengths of the sleeves in relation to the aircraft configuration. NOTE: Before you install a sleeve, cut and discard the cable ties around the cable bundle to install the sleeve correctly around the cable bundle. (a) Around the cable bundle of the pressure seal 20VP, install: 1000 (mm) Sleeve ABS0596S006 Item 2 (b) Attach the sleeves with: 50 Tie-Cable NSA935401-05

(4) Subtask 282148-831-006-002 - Install cable sleeves in the RH forward wing root and krueger flap. Manpower Resources Manhours 2.00 Minimum number of person 1 Subtask elapsed time 2.00 Skills NON SPECIFIC

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 181 6

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# @A310 SERVICE BULLETIN
Material necessary to do the job Kit 282148A01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 2 ABS0596S006 SLEEVE NSA935401-05 TIE References Fig. A-FCCAB Installation of Cable Sleeves in the RH forward wing root and krueger flap. Sheet 01

NOTE: The sleeves ABS0596S004 and ABS0596S006 are supplied in pieces of 1000 mm (39.370 inches), cut or assemble these pieces to get the correct length. NOTE: The lengths of the sleeves given in this Service Bulletin are approximate lengths. Adapt the lengths of the sleeves in relation to the aircraft configuration. NOTE: Before you install a sleeve, cut and discard the cable ties around the cable bundle to install the sleeve correctly around the cable bundle. (a) Around the cable bundle of the pressure seal 20VP, install: 1000 (mm) Sleeve ABS0596S006 Item 2 (b) Attach the sleeves with: 50 Tie-Cable NSA935401-05

(5) Subtask 282148-831-208-003 - Install the cable sleeves in the RH-wing forward of the front spar between rib 2 and rib 3 in zone 612. Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills ELECTRICAL Material necessary to do the job Kit 282148D01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 ABS0596S004 1 SLEEVE 11 MS21919WCH13 CLAMP 149 NSA935401-03 1 TIE 150 NSA935401-04 1 TIE
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 182 6

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# @A310 SERVICE BULLETIN

Kit 282148D05R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 125 B9299071900200 1 EQUIPMNT References Fig. A-GBEAAImprovement of the 2S-Route in the RHWing in Zone 612 (Kit D01) Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Sheet 08 NOTE (1): The sleeves ABS0596S004 is supplied in pieces of 1000 mm. Cut or assemble these pieces to get the correct length. NOTE (2): The lengths of the sleeves given in this Service Bulletin are approximate lengths. Adapt the lengths of the sleeves in relation to the aircraft configuration. NOTE (3): Before you install a sleeve, cut and discard the cable ties around the cable bundle to install the sleeve correctly around the cable bundle. NOTE (4): Adapt the number of cable ties to the required quantity. Refer to Fig. A-GBEAA Sheet 01 , Fig. A-GBEAA Sheet 02, Fig. A-GBEAA Sheet 03, Fig. A-GBEAA Sheet 04, Fig. A-GBEAA Sheet 05, Fig. A-GBEAA Sheet 06, Fig. A-GBEAA Sheet 07 and Fig. A-GBEAA Sheet 08 (a) Remove these items from the bracket of the rib 2 and cable bundle 2S/624VB, as shown in Details A and B: 1 Clamp MS21919WCH4 Item (22) Retain 1 Clamp MS21919WCH3 Item (23) Retain 1 Spacer NSA5527-03-02D Item (31) Retain 1 Washer NAS1149D0332K Item (40) Retain 1 Screw NAS1096-3-21 Item (50) Retain 1 Clamp MS21919WCH10 Item (100) Retain 1 Clamp Item (100) Discard

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 183 6

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# @A310 SERVICE BULLETIN (b) Remove these items from the riblet and cable bundle 2S/624VB, as shown in Details A and D: 1 Clamp MS21919WCH4 Item (22) Retain 3 Spacer NSA5527-03-02D Item (31) Retain 1 Washer NAS1149D0332K Item (40) Retain 1 Screw NAS1096-3-38 Item (54) Retain 1 Clamp Item (100) Discard (c) Install this cable sleeve around these identified wires from the cable bundle 2S/624VB, as shown in Details A, C and F: Wire number 2842-5052 Wire number 2842-5053 Wire number 2842-5054 Wire number 2842-5055 Wire number 2842-5056 Wire number 2842-5070 1 Sleeve ABS0596S004 Item 1 and attach the cable sleeve with: 1 Tie NSA935401-03 Item 149 1 Tie-Cable NSA935401-04 Item 150 and 1 Placard set B9299071900200 Item 125 as necessary. (d) Install these items to the bracket of the rib 2, cable bundle 2S/624VB and cable sleeve, Item 1, as shown in Details A and C: 1 Clamp MS21919WCH4 Item (22) Retained at removal 1 Clamp MS21919WCH3 Item (23) Retained at removal 1 Spacer NSA5527-03-02D Item (31) Retained at removal
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 184 6

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# @A310 SERVICE BULLETIN
1 Washer NAS1149D0332K Item (40) Retained at removal 1 Screw NAS1096-3-21 Item (50) Retained at removal 1 Clamp MS21919WCH10 Item (100) Retained at removal 1 Clamp MS21919WCH13 Item 11 (e) Install these items to the riblet, cable bundle 2S/624VB and cable sleeve, Item 1, as shown in Details A and E: 1 Clamp MS21919WCH4 Item (22) Retained at removal 3 Spacer NSA5527-03-02D Item (31) Retained at removal 1 Washer NAS1149D0332K Item (40) Retained at removal 1 Screw NAS1096-3-38 Item (54) Retained at removal 1 Clamp MS21919WCH13 Item 11

(6) Subtask 282148-831-209-003 - Install the cable sleeves in the RH-wing forward of the front spar between rib 7 and rib 8 in zone 612. Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills ELECTRICAL Material necessary to do the job Kit 282148D01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 ABS0596S004 2 SLEEVE 12 MS21919WCH14 CLAMP 149 NSA935401-03 2 TIE 150 NSA935401-04 2 TIE

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 185 6

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# @A310 SERVICE BULLETIN

References Fig. A-GBEAAImprovement of the 2S-Route in the RHWing in Zone 612 (Kit D01) Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Sheet 08 NOTE (1): The sleeves ABS0596S004 is supplied in pieces of 1000 mm. Cut or assemble these pieces to get the correct length. NOTE (2): The lengths of the sleeves given in this Service Bulletin are approximate lengths. Adapt the lengths of the sleeves in relation to the aircraft configuration. NOTE (3): Before you install a sleeve, cut and discard the cable ties around the cable bundle to install the sleeve correctly around the cable bundle. NOTE (4): Adapt the number of cable ties to the required quantity. Refer to Fig. A-GBEAA Sheet 01 , Fig. A-GBEAA Sheet 02, Fig. A-GBEAA Sheet 03, Fig. A-GBEAA Sheet 04, Fig. A-GBEAA Sheet 05, Fig. A-GBEAA Sheet 06, Fig. A-GBEAA Sheet 07 and Fig. A-GBEAA Sheet 08 (a) Remove these items from the two brackets of the riblets and cable bundle 2S/624VB, as shown in Details A, H and K: 2 Clamp MS21919WCH4 Item (22) Retain 2 Washer NAS1149D0332K Item (40) Retain 2 Screw NAS1096-3-8 Item (55) Retain 2 Clamp Item (100) Discard (b) Install this cable sleeve around these identified wires from the cable bundle 2S/624VB, as shown in Details A, J, K, L, M and N: Wire number 2842-5052 Wire number 2842-5053 Wire number 2842-5054 Wire number 2842-5055 Wire number 2842-5056 1 Sleeve ABS0596S004 Item 1 and attach the cable sleeves with: DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 186 6

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# @A310 SERVICE BULLETIN

1 Tie NSA935401-03 Item 149 1 Tie-Cable NSA935401-04 Item 150 (c) Install this cable sleeve around this identified wire from the cable bundle 2S/624VB, as shown in Details A, J, K, L, M and N: Wire number 2842-5070 1 Sleeve ABS0596S004 Item 1 and attach the cable sleeves with: 1 Tie NSA935401-03 Item 149 1 Tie-Cable NSA935401-04 Item 150 (d) Install these items to the two brackets of the riblets, cable bundle 2S/624VB and cable sleeves, Item 1, as shown in Detail A, J and L: 2 Clamp MS21919WCH4 Item (22) Retained at removal 2 Washer NAS1149D0332K Item (40) Retained at removal 2 Screw NAS1096-3-8 Item (55) Retained at removal 2 Clamp MS21919WCH14 Item 12

(7) Subtask 282148-831-210-003 - Install the cable sleeves in the RH-wing forward of the front spar between rib 8 and rib 9 (pylon area) in zone 612. Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills ELECTRICAL Material necessary to do the job Kit 282148D05R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 ABS0596S004 3 SLEEVE 30 NSA5527-03-01D 2 SPACER 31 NSA5527-03-02D 1 SPACER 109 NSA935805-09 3 (ME) CONDUIT 117 NSA935807C09 12 CLAMP 126 NSA938184PV1601 15 PIN DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 187 6

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# @A310 SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 135 NAS1096-3-42 1 SCREW 136 NAS1096-3-30 1 SCREW 149 NSA935401-03 30 TIE 150 NSA935401-04 30 TIE References Fig. A-GBJAAImprovement of the 2S-Route in the RHWing Pylon Area (Kit D05) Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Sheet 08 Sheet 09 Fig. A-GHAAA Hook-up Chart Sheet 01 Fig. A-GHBAA Hook-up Chart Sheet 01
NOTE (1): The sleeves ABS0596S004 is supplied in pieces of 1000 mm. Cut or assemble these pieces to get the correct length. NOTE (2): The lengths of the sleeves given in this Service Bulletin are approximate lengths. Adapt the lengths of the sleeves in relation to the aircraft configuration. NOTE (3): Before you install a sleeve, cut and discard the cable ties around the cable bundle to install the sleeve correctly around the cable bundle. NOTE (4): Adapt the number of cable ties to the required quantity. Refer to Fig. A-GBJAA Sheet 01 , Fig. A-GBJAA Sheet 02, Fig. A-GBJAA Sheet 03, Fig. A-GBJAA Sheet 04, Fig. A-GBJAA Sheet 05, Fig. A-GBJAA Sheet 06, Fig. A-GBJAA Sheet 07, Fig. A-GBJAA Sheet 08 and Fig. A-GBJAA Sheet 09 Refer to Fig. A-GHAAA Sheet 01 and Fig. A-GHBAA Sheet 01 (a) Disconnect these wires of route 2S from the receptacles 40VC and 5006VC in accordance with the Hook-up Chart 1, Lines 1 thru 14, END 1, Fig. A-GHAAA Sheet 01 and the Hook-up Chart 2, Lines 2 thru 8, END 1, Fig. A-GHBAA Sheet 01

. (b) Remove, refer to Fig. A-GBJAA Sheet 03, Detail C, BEFORE: 2 Spacer NSA5527-03-05D Item (30) Discard 1 Washer NSA935808-01 Item (112) Retain

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 188 6

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# @A310 SERVICE BULLETIN
1 Nut NAS1291C3M Item (116) Retain 1 Clamp NSA935807C10 Item (117) Discard 1 Screw Item (136) Discard (c) Remove, refer to Fig. A-GBJAA Sheet 04, Detail E, BEFORE: 1 Washer NSA935808-01 Item (112) Retain 1 Screw Item (113) Retain 1 Clamp NSA935807C10 Item (117) Discard (d) Remove, refer to Fig. A-GBJAA Sheet 05, Detail G, BEFORE: 2 Washer NSA935808-01 Item (112) Retain 2 Screw Item (113) Retain 2 Clamp NSA935807C10 Item (117) Discard (e) Remove, refer to Fig. A-GBJAA Sheet 06, Detail J, BEFORE: 1 Spacer NSA5527-03-05D Item (30) Discard 1 Washer NSA935808-01 Item (112) Retain 1 Clamp NSA935807C10 Item (117) Discard 1 Screw Item (135) Retain (f) Remove, refer to Fig. A-GBJAA Sheet 07, Detail L, BEFORE: 1 Washer NSA935808-01 Item (112) Retain 1 Screw Item (113) Retain 1 Clamp NSA935807C10 Item (117) Discard (g) Remove, refer to Fig. A-GBJAA Sheet 08, Detail N, BEFORE: 1 Washer NSA935808-01 Item (112) Retain 1 Screw Item (113) Retain 1 Clamp NSA935807C10 Item (117) Discard

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 189 6

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# @A310 SERVICE BULLETIN (h) Remove the protection sleeve from the cable harness as shown Fig. A-GBJAA Sheet 01 , Fig. A-GBJAA Sheet 02, Fig. A-GBJAA Sheet 03, Fig. A-GBJAA Sheet 04, Fig. A-GBJAA Sheet 05, Fig. A-GBJAA Sheet 06, Fig. A-GBJAA Sheet 07, Fig. A-GBJAA Sheet 08 and Fig. A-GBJAA Sheet 09, Details A, C, E, G, J, L and N: 1 Sleeve NSA935805-10 Item (1) Discard (i) Cut the conduit to the required length and install as shown Refer to Fig. A-GBJAA Sheet 01 , Fig. A-GBJAA Sheet 02, Fig. A-GBJAA Sheet 03, Fig. A-GBJAA Sheet 04, Fig. A-GBJAA Sheet 05, Fig. A-GBJAA Sheet 06, Fig. A-GBJAA Sheet 07, Fig. A-GBJAA Sheet 08 and Fig. A-GBJAA Sheet 09, Details B, D, F, H, K, M, P and Q: 3 Sleeve ABS0596S004 Item 1 3 (ME) Conduit NSA935805-09 Item 109 1 One part 1500.0 mm (59.06 in.) to the electrical wires for 10QT-A and 10QT-B of route 2S/636VB, refer to the Hook-up Chart 2, Fig. A-GHBAA Sheet 01 (j) Connect the electrical wires of route 2S to the receptacles 40VC and 5006VC in accordance with the Hook-up Chart 1, Lines 1 thru 14, END 1, Fig. A-GHAAA Sheet 01 and the Hook-up Chart 2, lines 2 thru 8, END 1, Fig. A-GHBAA Sheet 01

. Use the contact pins if required: 15 Pin NSA938184PV1601 Item 126 (k) Install, refer to Fig. A-GBJAA Sheet 08, Detail P, AFTER: 1 Washer NSA935808-01 Item (112) Retained at removal 1 Screw Item (113) Retained at removal 2 Clamp NSA935807C09 Item 117 (l) Install, refer to Fig. A-GBJAA Sheet 07, Detail M, AFTER: 1 Washer NSA935808-01 Item (112) Retained at removal 1 Screw Item (113) Retained at removal 2 Clamp NSA935807C09 Item 117 (m) Install, refer to Fig. A-GBJAA Sheet 06, Detail K, AFTER: 1 Spacer NSA5527-03-02D Item 31 1 Washer NSA935808-01 Item (112) Retained at removal
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 190 6

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# @A310 SERVICE BULLETIN
2 Clamp NSA935807C09 Item 117 1 Screw NAS1096-3-42 Item 135 (n) Install, refer to Fig. A-GBJAA Sheet 05, Detail H, AFTER: 2 Washer NSA935808-01 Item (112) Retained at removal 2 Screw Item (113) Retained at removal 4 Clamp NSA935807C09 Item 117 (o) Install, refer to Fig. A-GBJAA Sheet 04, Detail F, AFTER: 1 Washer NSA935808-01 Item (112) Retained at removal 1 Screw Item (113) Retained at removal 2 Clamp NSA935807C09 Item 117 (p) Install, refer to Fig. A-GBJAA Sheet 03, Detail D, AFTER: 2 Spacer NSA5527-03-01D Item 30 2 Washer NSA935808-01 Item (112) Retained at removal 2 Nut NAS1291C3M Item (116) Retained at removal 2 Clamp NSA935807C09 Item 117 1 Screw NAS1096-3-30 Item 136 (q) Protect the electrical wires for 10QT-A and 10QT-B of route 2S/636VB, refer to Fig. A-GBJAA Sheet 09, Detail Q, and the Hook-up Chart 2, Fig. A-GHBAA Sheet 01 with: 30 Tie NSA935401-03 Item 149 30 Tie-Cable NSA935401-04 Item 150

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 191 6

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# @A310 SERVICE BULLETIN (8) Subtask 282148-831-211-003 - Install the cable sleeves in the RH-wing forward of the front spar between rib 9 and rib 12 in zone 623. Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills ELECTRICAL Material necessary to do the job Kit 282148D01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 ABS0596S004 3 SLEEVE 10 MS21919WCH9 CLAMP 14 NAS1096-3-19 2 SCREW 15 NSA5527-03-03 3 SPACER 16 NSA8420-2 1 (ME) CORD 149 NSA935401-03 10 TIE 150 NSA935401-04 20 TIE Kit 282148D05R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 31 NSA5527-03-02D SPACER 135 NAS1096-3-42 SCREW References Fig. A-GBFAAImprovement of the 2S-Route in the RHWing in Zone 623 (Kit D01) Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Sheet 08 Sheet 09 Sheet 10 NOTE (1): The sleeve ABS0596S004 is supplied in pieces of 1000 mm. Cut or assemble these pieces to get the correct length. NOTE (2): The lengths of the sleeves given in this Service Bulletin are approximate lengths. Adapt the lengths of the sleeves in relation to the aircraft configuration. NOTE (3): Before you install a sleeve, cut and discard the cable ties around the cable bundle to install the sleeve correctly around the cable bundle.

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 192 6

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# @A310 SERVICE BULLETIN
NOTE (4): Adapt the number of cable ties to the required quantity. Refer to Refer to Fig. A-GBFAA Sheet 01 , Fig. A-GBFAA Sheet 02, Fig. A-GBFAA Sheet 03, Fig. A-GBFAA Sheet 04, Fig. A-GBFAA Sheet 05, Fig. A-GBFAA Sheet 06, Fig. A-GBFAA Sheet 07, Fig. A-GBFAA Sheet 08, Fig. A-GBFAA Sheet 09 and Fig. AGBFAA Sheet 10 (a) At one position, remove these items from the bracket between rib 11 and rib 12 and cable bundle 2S/636VB, as shown in Details A and D: 2 Clamp MS21919WCH4 Item (22) Retain 1 Clamp MS21919WCH4 Item (22) Discard 1 Clamp MS21919WCH3 Item (23) Retain 1 Spacer NSA5527-03-01D Item (30) Retain 1 Spacer NSA5527-03-02D Item (31) Retain 2 Washer NSA935808-01 Item (112) Retain 2 Screw NAS1096-3-30 Item (121) Discard 1 Clamp NSA935807-06 Item (122) Retain (b) At two positions, remove these items from the brackets between rib 10 and rib 11 and between rib 11 and rib 12 and cable bundle 2S/636VB, as shown in Details A and F: 2 Clamp Item (22) Discard 6 Clamp MS21919WCH4 Item (22) Retain 4 Spacer NSA5527-03-01D Item (30) Retain 2 Washer NAS1149D0332K Item (40) Retain 2 Screw NAS1096-3-27 Item (52) Retain (c) At two positions, remove these items from the brackets of the rib 11 and cable bundle 2S/636VB, as shown in Details A and H: 6 Clamp MS21919WCH4 Item (22) Retain 2 Clamp Item (23) Discard 2 Spacer NSA5527-03-01D Item (30) Retain 2 Spacer NSA5527-03-04D Item (32) Retain DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 193 6

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# @A310 SERVICE BULLETIN
2 Washer NAS1149D0332K Item (40) Retain 2 Screw NAS1096-3-22 Item (51) Retain (d) At two positions, remove these items from the brackets of the rib 10 and cable bundle 2S/636VB, as shown in Details A and K: 2 Clamp Item (22) Discard 2 Clamp MS21919WCH4 Item (22) Retain 2 Spacer NSA5527-03-01D Item (30) Retain 2 Spacer Item (32) Discard 2 Washer NAS1149D0332K Item (40) Retain 2 Screw Item (51) Discard (e) Remove these items from the bracket between rib 9 and rib 10 and cable bundle 2S/636VB, as shown in Details A and M: 3 Clamp MS21919WCH4 Item (22) Retain 1 Clamp Item (23) Discard 1 Spacer NSA5527-03-01D Item (30) Retain 1 Spacer NSA5527-03-04D Item (32) Retain 1 Washer NAS1149D0332K Item (40) Retain 1 Screw NAS1096-3-22 Item (51) Retain (f) Remove these items from the bracket of the rib 9 and cable bundle 2S/636VB, as shown in Details A and T: 1 Clamp Item (21) Discard 1 Clamp MS21919WCH5 Item (21) Retain 1 Spacer NSA5527-03-02D Item (31) Retain 1 Spacer NSA5527-03-04D Item (32) Retain 1 Washer NAS1149D0332K Item (40) Retain 1 Screw NAS1096-3-27 Item (52) Retain

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 194 6

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# @A310 SERVICE BULLETIN (g) Install this cable sleeve around these identified wires from the cable bundle 2S/636VB, as shown in Details A, C, E, G, J, L, N, Q and R: Wire number 2842-5061 Wire number 2842-5062 Wire number 2842-5063 Wire number 2842-5064 Wire number 2842-5065 Wire number 2842-5071 3 Sleeve ABS0596S004 Item 1 and attach the cable sleeves with: 3 Spacer NSA5527-03-03 Item 15 1 (ME) Cord NSA8420-2 Item 16 10 Tie NSA935401-03 Item 149 20 Tie-Cable NSA935401-04 Item 150 (h) At one positions, install these items to the brackets between rib 10 and rib 11 and between rib 11 and rib 12, cable sleeves, Item 1 and cable bundle 2S/636VB, as shown in Details A and E: 2 Clamp MS21919WCH4 Item (22) Retained at removal 1 Clamp MS21919WCH3 Item (23) Retained at removal 1 Spacer NSA5527-03-01D Item (30) Retained at removal 1 Spacer NSA5527-03-02D Item (31) Retained at removal 1 Washer NSA935808-01 Item (112) Retained at removal 1 Clamp NSA935807-06 Item (122) Retained at removal 1 Clamp MS21919WCH9 Item 10 1 Spacer NSA5527-03-02D Item 31
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 195 6

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# @A310 SERVICE BULLETIN

1 Screw NAS1096-3-42 Item 135 (i) At two positions, install these items to the brackets between rib 10 and rib 11 and between rib 11 and rib 12, cable sleeves, Item 1 and cable bundle 2S/636VB, as shown in Details A and G: 6 Clamp MS21919WCH4 Item (22) Retained at removal 4 Spacer NSA5527-03-01D Item (30) Retained at removal 2 Washer NAS1149D0332K Item (40) Retained at removal 2 Screw NAS1096-3-27 Item (52) Retained at removal 2 Clamp MS21919WCH9 Item 10 (j) At two positions, install these items to the brackets of the rib 11, cable sleeves, Item 1 and cable bundle 2S/636VB, as shown in Details A and J: 2 Clamp MS21919WCH4 Item (22) Retained at removal 1 Spacer NSA5527-03-01D Item (30) Retained at removal 1 Spacer NSA5527-03-04D Item (32) Retained at removal 1 Washer NAS1149D0332K Item (40) Retained at removal 1 Screw NAS1096-3-22 Item (51) Retained at removal 1 Clamp MS21919WCH9 Item 10 (k) At two positions, install these items to the brackets of the rib 10, cable sleeves, Item 1 and cable bundle 2S/636VB, as shown in Details A and L: 2 Clamp MS21919WCH4 Item (22) Retained at removal 2 Spacer NSA5527-03-01D Item (30) Retained at removal 2 Washer NAS1149D0332K Item (40) Retained at removal

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 196 6

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# @A310 SERVICE BULLETIN
2 Clamp MS21919WCH9 Item 10 2 Screw NAS1096-3-19 Item 14 (l) Install these items to the bracket between rib 9 and rib 10, cable sleeves, Item 1 and cable bundle 2S/636VB, as shown in Details A and N: 3 Clamp MS21919WCH4 Item (22) Retained at removal 1 Spacer NSA5527-03-01D Item (30) Retained at removal 1 Spacer NSA5527-03-04D Item (32) Retained at removal 1 Washer NAS1149D0332K Item (40) Retained at removal 1 Screw NAS1096-3-22 Item (51) Retained at removal 1 Clamp MS21919WCH9 Item 10 (m) Install these items to the bracket of the rib 9, cable sleeves, Item 1 and cable bundle 2S/636VB, as shown in Details A and Q: 1 Clamp MS21919WCH5 Item (21) Retained at removal 1 Spacer NSA5527-03-02D Item (31) Retained at removal 1 Spacer NSA5527-03-04D Item (32) Retained at removal 1 Washer NAS1149D0332K Item (40) Retained at removal 1 Screw NAS1096-3-27 Item (52) Retained at removal 1 Clamp MS21919WCH9 Item 10

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 197 6

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# @A310 SERVICE BULLETIN
**CONF 008 (1) Subtask 282148-831-405-001 - Install a New Bracket on the Sub Spar Behind the Front Spar Between RIB 8 and RIB 9 on the RH Wing Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills AIRFRAME Material necessary to do the job Kit 282148B01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 A5725068600000 1 Bracket 2 ASNA0078A502 2 Rivet Consumable CMLB01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Corrosion Inhibiting Low Adhesion Sealant 09-018 As required Solvent General Purpose 11-026 As required Lint-Free Cotton Cloth 19-003 As required References Fig. A-UBAAA Location of Bracket on the Sub Spar Behind the Front Spar Between RIB 8 and RIB 9 (RH Wing) Sheet 01

Refer to Fig. A-UBAAA Sheet 01 (a) Remove from the sub spar behind the front spar between RIB 8 and RIB 9 on the RH wing, the items that follow: 2 Rivet NSA54213510DCA Item (2) Discard 1 Bracket A5724630400000 Item (1) Discard (b) Clean the mating surfaces use Lint-Free Cotton Cloth 19-003 As required

made moist with

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 198 6

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# @A310 SERVICE BULLETIN

Solvent General Purpose 11-026 As required (c) Put the 1 Bracket A5725068600000 Item 1 in position on the sub spar behind the front spar between RIB 8 and RIB 9 on the RH wing (Refer to Fig. A-UBAAA Sheet 01 ). (d) Copy drill the two holes from the sub spar through the Bracket, Item 1 to a dimension of between 4.060 and 4.160 mm (0.160 and 0.164 in.). (e) Deburr the holes that have been worked. (f) Use Corrosion Inhibiting Low Adhesion Sealant 09-018 As required

and wet install the 1 Bracket A5725068600000 Item 1 with the 2 Rivet, Blind ASNA0078A502 Item 2 on the sub spar behind the front spar between RIB 8 and RIB 9 on the RH wing. (2) Subtask 282148-831-004-001 - Install cable sleeves in the RH Electronics Rack 90VU. Manpower Resources Manhours 6.00 Minimum number of person 1 Subtask elapsed time 6.00 Skills NON SPECIFIC Material necessary to do the job Kit 282148A01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 ABS0596S004 2000 (mm) SLEEVE NSA935401-04 50 TIE References Fig. A-FCAAA Installation of Cable Sleeves in the RH Electronics Rack 90VU. Sheet 01

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 199 6

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# @A310 SERVICE BULLETIN

References Fig. A-FWAAA Installation of Cable Sleeves in the RH Electronics Rack 90VU. Sheet 01

NOTE: The sleeves ABS0596S004 and ABS0596S006 are supplied in pieces of 1000 mm (39.370 inches), cut or assemble these pieces to get the correct length. NOTE: The lengths of the sleeves given in this Service Bulletin are approximate lengths. Adapt the lengths of the sleeves in relation to the aircraft configuration. NOTE: Before you install a sleeve, cut and discard the cable ties around the cable bundle to install the sleeve correctly around the cable bundle. (a) On the Shelf 92VU, only around the wires identified in figure Fig. A-FWAAA Sheet 01 , from the equipment 15QT-B to the connector 2354VC, install: 1600 (mm) Sleeve ABS0596S004 Item 1 (b) Around the cable bundle of the connector 2354VC-A, install: 400 (mm) Sleeve ABS0596S004 Item 1 (c) Attach the sleeves with: 50 Tie-Cable NSA935401-04

(3) Subtask 282148-831-005-001 - Install cable sleeves between FR38.2 and FR39, in the forward cargo compartment. 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 282148A01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 2 ABS0596S006 1000 (mm) SLEEVE NSA935401-05 50 TIE References Fig. A-FCBAA Installation of Cable Sleeves in the Forward Cargo Compartment. Sheet 01

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 200 6

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# @A310 SERVICE BULLETIN
NOTE: The sleeves ABS0596S004 and ABS0596S006 are supplied in pieces of 1000 mm (39.370 inches), cut or assemble these pieces to get the correct length. NOTE: The lengths of the sleeves given in this Service Bulletin are approximate lengths. Adapt the lengths of the sleeves in relation to the aircraft configuration. NOTE: Before you install a sleeve, cut and discard the cable ties around the cable bundle to install the sleeve correctly around the cable bundle. (a) Around the cable bundle of the pressure seal 20VP, install: 1000 (mm) Sleeve ABS0596S006 Item 2 (b) Attach the sleeves with: 50 Tie-Cable NSA935401-05

(4) Subtask 282148-831-006-002 - Install cable sleeves in the RH forward wing root and krueger flap. 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 282148A01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 2 ABS0596S006 SLEEVE NSA935401-05 TIE References Fig. A-FCCAB Installation of Cable Sleeves in the RH forward wing root and krueger flap. Sheet 01

NOTE: The sleeves ABS0596S004 and ABS0596S006 are supplied in pieces of 1000 mm (39.370 inches), cut or assemble these pieces to get the correct length. NOTE: The lengths of the sleeves given in this Service Bulletin are approximate lengths. Adapt the lengths of the sleeves in relation to the aircraft configuration. NOTE: Before you install a sleeve, cut and discard the cable ties around the cable bundle to install the sleeve correctly around the cable bundle.
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 201 6

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# @A310 SERVICE BULLETIN (a) Around the cable bundle of the pressure seal 20VP, install: 1000 (mm) Sleeve ABS0596S006 Item 2 (b) Attach the sleeves with: 50 Tie-Cable NSA935401-05

(5) Subtask 282148-831-208-004 - Install the cable sleeves in the RH-wing forward of the front spar between rib 2 and rib 3 in zone 612. Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills ELECTRICAL Material necessary to do the job Kit 282148D01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 ABS0596S004 1 SLEEVE 11 MS21919WCH13 CLAMP 149 NSA935401-03 1 TIE 150 NSA935401-04 1 TIE Kit 282148D06R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 132 B9299071900600 1 EQUIPMNT References Fig. A-GBEAAImprovement of the 2S-Route in the RHWing in Zone 612 (Kit D01) Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Sheet 08 NOTE (1): The sleeves ABS0596S004 is supplied in pieces of 1000 mm. Cut or assemble these pieces to get the correct length. NOTE (2): The lengths of the sleeves given in this Service Bulletin are approximate lengths. Adapt the lengths of the sleeves in relation to the aircraft configuration. NOTE (3): Before you install a sleeve, cut and discard the cable ties around the cable bundle to install the sleeve correctly around the cable bundle.
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 202 6

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# @A310 SERVICE BULLETIN
NOTE (4): Adapt the number of cable ties to the required quantity. Refer to Fig. A-GBEAA Sheet 01 , Fig. A-GBEAA Sheet 02, Fig. A-GBEAA Sheet 03, Fig. A-GBEAA Sheet 04, Fig. A-GBEAA Sheet 05, Fig. A-GBEAA Sheet 06, Fig. A-GBEAA Sheet 07 and Fig. A-GBEAA Sheet 08 (a) Remove these items from the bracket of the rib 2 and cable bundle 2S/624VB, as shown in Details A and B: 1 Clamp MS21919WCH4 Item (22) Retain 1 Clamp MS21919WCH3 Item (23) Retain 1 Spacer NSA5527-03-02D Item (31) Retain 1 Washer NAS1149D0332K Item (40) Retain 1 Screw NAS1096-3-21 Item (50) Retain 1 Clamp MS21919WCH10 Item (100) Retain 1 Clamp Item (100) Discard (b) Remove these items from the riblet and cable bundle 2S/624VB, as shown in Details A and D: 1 Clamp MS21919WCH4 Item (22) Retain 3 Spacer NSA5527-03-02D Item (31) Retain 1 Washer NAS1149D0332K Item (40) Retain 1 Screw NAS1096-3-38 Item (54) Retain 1 Clamp Item (100) Discard (c) Install this cable sleeve around these identified wires from the cable bundle 2S/624VB, as shown in Details A, C, E and F: Wire number 2842-5052 Wire number 2842-5053 Wire number 2842-5054 Wire number 2842-5055 Wire number 2842-5056 Wire number 2842-5070

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 203 6

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# @A310 SERVICE BULLETIN

1 Sleeve ABS0596S004 Item 1 and attach the cable sleeve with: 1 Tie NSA935401-03 Item 149 1 Tie-Cable NSA935401-04 Item 150 and 1 Placard Set B9299071900600 Item 132 as necessary. (d) Install these items to the bracket of the rib 2, cable bundle 2S/624VB and cable sleeve, Item 1, as shown in Details A and C: 1 Clamp MS21919WCH4 Item (22) Retained at removal 1 Clamp MS21919WCH3 Item (23) Retained at removal 1 Spacer NSA5527-03-02D Item (31) Retained at removal 1 Washer NAS1149D0332K Item (40) Retained at removal 1 Screw NAS1096-3-21 Item (50) Retained at removal 1 Clamp MS21919WCH10 Item (100) Retained at removal 1 Clamp MS21919WCH13 Item 11 (e) Install these items to the riblet, cable bundle 2S/624VB and cable sleeve, Item 1, as shown in Details A and E: 1 Clamp MS21919WCH4 Item (22) Retained at removal 3 Spacer NSA5527-03-02D Item (31) Retained at removal 1 Washer NAS1149D0332K Item (40) Retained at removal 1 Screw NAS1096-3-38 Item (54) Retained at removal 1 Clamp MS21919WCH13 Item 11 DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 204 6

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# @A310 SERVICE BULLETIN (6) Subtask 282148-831-209-004 - Install the cable sleeves in the RH-wing forward of the front spar between rib 7 and rib 8 in zone 612. Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills ELECTRICAL Material necessary to do the job Kit 282148D01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 ABS0596S004 2 SLEEVE 12 MS21919WCH14 CLAMP 149 NSA935401-03 2 TIE 150 NSA935401-04 2 TIE References Fig. A-GBEAAImprovement of the 2S-Route in the RHWing in Zone 612 (Kit D01) Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Sheet 08 NOTE (1): The sleeves ABS0596S004 is supplied in pieces of 1000 mm. Cut or assemble these pieces to get the correct length. NOTE (2): The lengths of the sleeves given in this Service Bulletin are approximate lengths. Adapt the lengths of the sleeves in relation to the aircraft configuration. NOTE (3): Before you install a sleeve, cut and discard the cable ties around the cable bundle to install the sleeve correctly around the cable bundle. NOTE (4): Adapt the number of cable ties to the required quantity. Refer to Fig. A-GBEAA Sheet 01 , Fig. A-GBEAA Sheet 02, Fig. A-GBEAA Sheet 03, Fig. A-GBEAA Sheet 04, Fig. A-GBEAA Sheet 05, Fig. A-GBEAA Sheet 06, Fig. A-GBEAA Sheet 07 and Fig. A-GBEAA Sheet 08 (a) Remove these items from the two brackets of the riblets and cable bundle 2S/624VB, as shown in Details A, H and K: 2 Clamp MS21919WCH4 Item (22) Retain 2 Washer NAS1149D0332K Item (40) Retain DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 205 6

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# @A310 SERVICE BULLETIN
2 Screw NAS1096-3-8 Item (55) Retain 2 Clamp Item (100) Discard (b) Install this cable sleeve around these identified wires from the cable bundle 2S/624VB, as shown in Details A, J, K, L, M and N: Wire number 2842-5052 Wire number 2842-5053 Wire number 2842-5054 Wire number 2842-5055 Wire number 2842-5056 1 Sleeve ABS0596S004 Item 1 and attach the cable sleeves with: 1 Tie NSA935401-03 Item 149 1 Tie-Cable NSA935401-04 Item 150 (c) Install this cable sleeve around this identified wire from the cable bundle 2S/624VB, as shown in Details A, J, K, L, M and N: Wire number 2842-5070 1 Sleeve ABS0596S004 Item 1 and attach the cable sleeves with: 1 Tie NSA935401-03 Item 149 1 Tie-Cable NSA935401-04 Item 150 (d) Install these items to the two brackets of the riblets, cable bundle 2S/624VB and cable sleeves, Item 1, as shown in Detail A, J and L: 2 Clamp MS21919WCH4 Item (22) Retained at removal 2 Washer NAS1149D0332K Item (40) Retained at removal 2 Screw NAS1096-3-8 Item (55) Retained at removal 2 Clamp MS21919WCH14 Item 12

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 206 6

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# @A310 SERVICE BULLETIN (7) Subtask 282148-831-210-004 - Install the cable sleeves in the RH-wing forward of the front spar between rib 8 and rib 9 (pylon area) in zone 612. Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills ELECTRICAL Material necessary to do the job Kit 282148D06R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 ABS0596S004 3 SLEEVE 31 NSA5527-03-02D 2 SPACER 109 NSA935805-09 1.5 (ME) CONDUIT 117 NSA935807C09 7 CLAMP 121 NAS1096-3-40 1 SCREW 123 NAS1801-3-31 2 SCREW 126 NSA938184PV1601 7 PIN 130 NSA5527-03-08D 1 SPACER 131 NSA5527-03-07D 1 SPACER 149 NSA935401-03 30 TIE 150 NSA935401-04 30 TIE References Fig. A-GBKAAImprovement of the 2S-Route in the RHWing Pylon Area (Kit D06) Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Sheet 08 Sheet 09 Fig. A-GHBAA Hook-up Chart Sheet 01
NOTE (1): The sleeves ABS0596S004 is supplied in pieces of 1000 mm. Cut or assemble these pieces to get the correct length. NOTE (2): The lengths of the sleeves given in this Service Bulletin are approximate lengths. Adapt the lengths of the sleeves in relation to the aircraft configuration. NOTE (3): Before you install a sleeve, cut and discard the cable ties around the cable bundle to install the sleeve correctly around the cable bundle. NOTE (4): Adapt the number of cable ties to the required quantity. DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 207 6

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# @A310 SERVICE BULLETIN
Refer to Fig. A-GBKAA Sheet 01 , Fig. A-GBKAA Sheet 02, Fig. A-GBKAA Sheet 03, Fig. A-GBKAA Sheet 04, Fig. A-GBKAA Sheet 05, Fig. A-GBKAA Sheet 06, Fig. A-GBKAA Sheet 07, Fig. A-GBKAA Sheet 08 and Fig. A-GBKAA Sheet 09 Refer to Fig. A-GHBAA Sheet 01 (a) Disconnect the wires of route 2S from the receptacles 40VC and 5006VC in accordance with the Hook-up Chart 2, Lines 2 thru 8, END 1, Fig. A-GHBAA Sheet 01

. (b) Remove, refer to Fig. A-GBKAA Sheet 03, Detail C, BEFORE: 1 Washer NSA935808-01 Item (112) Retain 1 Screw NAS1096-3-23 Item (113) Retain 1 Nut NAS1291C3M Item (116) Retain 1 Washer AN960KD10l Item (124) Retain (c) Remove, refer to Fig. A-GBKAA Sheet 04, Detail E, BEFORE: 1 Washer NSA935808-01 Item (112) Retain 1 Screw NAS1096-3-23 Item (113) Retain (d) Remove, refer to Fig. A-GBKAA Sheet 05, Detail G, BEFORE: 2 Washer NSA935808-01 Item (112) Retain 2 Screw NAS1096-3-23 Item (113) Retain (e) Remove, refer to Fig. A-GBKAA Sheet 06, Detail J, BEFORE: 1 Spacer NSA5527-03-02D Item (31) Retain 1 Screw Item (121) Discard (f) Remove, refer to Fig. A-GBKAA Sheet 07, Detail L, BEFORE: 1 Screw Item (123) Discard (g) Remove, refer to Fig. A-GBKAA Sheet 08, Detail N, BEFORE: 1 Screw Item (123) Discard (h) Cut the conduit to the required length and install as shown Fig. A-GBKAA Sheet 01 , Fig. A-GBKAA Sheet 02, Fig. A-GBKAA Sheet 03, Fig. A-GBKAA Sheet 04, Fig. A-GBKAA Sheet 05, Fig. A-GBKAA Sheet 06, Fig. A-GBKAA Sheet 07, Fig. AGBKAA Sheet 08 and Fig. A-GBKAA Sheet 09, Details B and R: 3 Sleeve ABS0596S004 Item 1 DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 208 6

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# @A310 SERVICE BULLETIN
1.5 (ME) Conduit NSA935805-09 Item 109 1 One part 1500.0 mm (59.06 in.) to the electrical wires for 10QT-A and 10QT-B of route 2S/636VB, refer to the Hook-up Chart 2, Fig. A-GHBAA Sheet 01 (i) Connect the electrical wires of route 2S to the receptacles 40VC and 5006VC in accordance with the Hook-up Chart 2, Lines 2 thru 8, END 1, Fig. A-GHBAA Sheet 01 . Use the contact pins if required: 7 Pin NSA938184PV1601 Item 126 (j) Install, refer to Fig. A-GBKAA Sheet 08, Detail P, AFTER: 1 Spacer NSA5527-03-02D Item 31 1 Clamp NSA935807C09 Item 117 1 Screw NAS1801-3-31 Item 123 1 Spacer NSA5527-03-07D Item 131 (k) Install, refer to Fig. A-GBKAA Sheet 07, Detail M, AFTER: 1 Clamp NSA935807C09 Item 117 1 Screw NAS1801-3-31 Item 123 1 Spacer NSA5527-03-08D Item 130 (l) Install, refer to Fig. A-GBKAA Sheet 06, Detail K, AFTER: 1 Spacer NSA5527-03-02D Item 31 1 Clamp NSA935807C09 Item 117 1 Screw NAS1096-3-40 Item 121 (m) Install, refer to Fig. A-GBKAA Sheet 05, Detail H, AFTER: 2 Washer NSA935808-01 Item (112) Retained at removal 2 Screw NAS1096-3-23 Item (113) Retained at removal 2 Clamp NSA935807C09 Item 117 (n) Install, refer to Fig. A-GBKAA Sheet 04, Detail F, AFTER: 1 Washer NSA935808-01 Item (112) Retained at removal
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 209 6

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# @A310 SERVICE BULLETIN
1 Screw NAS1096-3-23 Item (113) Retained at removal 1 Clamp NSA935807C09 Item 117 (o) Install, refer to Fig. A-GBKAA Sheet 03, Detail D, AFTER: 1 Washer NSA935808-01 Item (112) Retained at removal 1 Screw NAS1096-3-23 Item (113) Retained at removal 1 Nut NAS1291C3M Item (116) Retained at removal 1 Washer AN960KD10l Item (124) Retained at removal 1 Clamp NSA935807C09 Item 117 (p) Protect the electrical wires for 10QT-A and 10QT-B of route 2S/636VB, refer to the Hook-up Chart 2, Fig. A-GHBAA Sheet 01 and Fig. A-GBKAA Sheet 01 , Fig. AGBKAA Sheet 02, Fig. A-GBKAA Sheet 03, Fig. A-GBKAA Sheet 04, Fig. AGBKAA Sheet 05, Fig. A-GBKAA Sheet 06, Fig. A-GBKAA Sheet 07, Fig. AGBKAA Sheet 08 and Fig. A-GBKAA Sheet 09, Detail Q with: 30 Tie NSA935401-03 Item 149 30 Tie-Cable NSA935401-04 Item 150

(8) Subtask 282148-831-211-004 - Install the cable sleeves in the RH-wing forward of the front spar between rib 9 and rib 12 in zone 623. Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills ELECTRICAL Material necessary to do the job Kit 282148D01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 ABS0596S004 3 SLEEVE 10 MS21919WCH9 CLAMP 14 NAS1096-3-19 SCREW 15 NSA5527-03-03 SPACER 16 NSA8420-2 CORD
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 210 6

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# @A310 SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 150 NSA935401-04 1 TIE Kit 282148D06R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 31 NSA5527-03-02D 2 SPACER 121 NAS1096-3-40 1 SCREW References Fig. A-GBFAAImprovement of the 2S-Route in the RHWing in Zone 623 (Kit D01) Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Sheet 08 Sheet 09 Sheet 10 NOTE (1): The sleeve ABS0596S004 is supplied in pieces of 1000 mm. Cut or assemble these pieces to get the correct length. NOTE (2): The lengths of the sleeves given in this Service Bulletin are approximate lengths. Adapt the lengths of the sleeves in relation to the aircraft configuration. NOTE (3): Before you install a sleeve, cut and discard the cable ties around the cable bundle to install the sleeve correctly around the cable bundle. NOTE (4): Adapt the number of cable ties to the required quantity. Refer to Refer to Fig. A-GBFAA Sheet 01 , Fig. A-GBFAA Sheet 02, Fig. A-GBFAA Sheet 03, Fig. A-GBFAA Sheet 04, Fig. A-GBFAA Sheet 05, Fig. A-GBFAA Sheet 06, Fig. A-GBFAA Sheet 07, Fig. A-GBFAA Sheet 08, Fig. A-GBFAA Sheet 09 and Fig. AGBFAA Sheet 10 (a) At one position, remove these items from the bracket between rib 11 and rib 12 and cable bundle 2S/636VB, as shown in Details A and D: 2 Clamp MS21919WCH4 Item (22) Retain 1 Clamp MS21919WCH4 Item (22) Discard 1 Clamp MS21919WCH3 Item (23) Retain 1 Spacer NSA5527-03-01D Item (30) Retain 1 Spacer NSA5527-03-02D Item (31) Retain
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 211 6

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# @A310 SERVICE BULLETIN
1 Washer NSA935808-01 Item (112) Retain 1 Screw NAS1096-3-30 Item (121) Discard 1 Clamp NSA935807-06 Item (122) Retain (b) At two positions, remove these items from the brackets between rib 10 and rib 11 and between rib 11 and rib 12 and cable bundle 2S/636VB, as shown in Details A and F: 2 Clamp Item (22) Discard 6 Clamp MS21919WCH4 Item (22) Retain 4 Spacer NSA5527-03-01D Item (30) Retain 2 Washer NAS1149D0332K Item (40) Retain 2 Screw NAS1096-3-27 Item (52) Retain (c) At two positions, remove these items from the brackets of the rib 11 and cable bundle 2S/636VB, as shown in Details A and H: 6 Clamp MS21919WCH4 Item (22) Retain 2 Clamp Item (23) Discard 2 Spacer NSA5527-03-01D Item (30) Retain 2 Spacer NSA5527-03-04D Item (32) Retain 2 Washer NAS1149D0332K Item (40) Retain 2 Screw NAS1096-3-22 Item (51) Retain (d) At two positions, remove these items from the brackets of the rib 10 and cable bundle 2S/636VB, as shown in Details A and K: 2 Clamp Item (22) Discard 2 Clamp MS21919WCH4 Item (22) Retain 2 Spacer NSA5527-03-01D Item (30) Retain 2 Spacer Item (32) Discard 2 Washer NAS1149D0332K Item (40) Retain 2 Screw Item (51) Discard
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 212 6

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# @A310 SERVICE BULLETIN (e) Remove these items from the bracket between rib 9 and rib 10 and cable bundle 2S/636VB, as shown in Details A and M: 3 Clamp MS21919WCH4 Item (22) Retain 1 Clamp Item (23) Discard 1 Spacer NSA5527-03-01D Item (30) Retain 1 Spacer NSA5527-03-04D Item (32) Retain 1 Washer NAS1149D0332K Item (40) Retain 1 Screw NAS1096-3-22 Item (51) Retain (f) Remove these items from the bracket of the rib 9 and cable bundle 2S/636VB, as shown in Details A and T: 1 Clamp Item (21) Discard 1 Clamp MS21919WCH5 Item (21) Retain 1 Spacer NSA5527-03-02D Item (31) Retain 1 Spacer NSA5527-03-04D Item (32) Retain 1 Washer NAS1149D0332K Item (40) Retain 1 Screw NAS1096-3-27 Item (52) Retain (g) Install this cable sleeve around these identified wires from the cable bundle 2S/636VB, as shown in Details A, C, E, G, J, L, N and R: Wire number 2842-5061 Wire number 2842-5062 Wire number 2842-5063 Wire number 2842-5064 Wire number 2842-5065 Wire number 2842-5071 3 Sleeve ABS0596S004 Item 1 and attach the cable sleeves with: 3 Spacer NSA5527-03-03 Item 15

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 213 6

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# @A310 SERVICE BULLETIN
1 (ME) Cord NSA8420-2 Item 16 1 Tie-Cable NSA935401-04 Item 150 (h) At one positions, install these items to the brackets between rib 10 and rib 11 and between rib 11 and rib 12, cable sleeves, Item 1 and cable bundle 2S/636VB, as shown in Details A and E: 2 Clamp MS21919WCH4 Item (22) Retained at removal 1 Clamp MS21919WCH3 Item (23) Retained at removal 1 Spacer NSA5527-03-01D Item (30) Retained at removal 1 Spacer NSA5527-03-02D Item (31) Retained at removal 1 Washer NSA935808-01 Item (112) Retained at removal 1 Clamp NSA935807-06 Item (122) Retained at removal 1 Clamp MS21919WCH9 Item 10 2 Spacer NSA5527-03-02D Item 31 1 Screw NAS1096-3-40 Item 121 (i) At two positions, install these items to the brackets between rib 10 and rib 11 and between rib 11 and rib 12, cable sleeves, Item 1 and cable bundle 2S/636VB, as shown in Details A and G: 6 Clamp MS21919WCH4 Item (22) Retained at removal 4 Spacer NSA5527-03-01D Item (30) Retained at removal 2 Washer NAS1149D0332K Item (40) Retained at removal 2 Screw NAS1096-3-27 Item (52) Retained at removal 2 Clamp MS21919WCH9 Item 10

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 214 6

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# @A310 SERVICE BULLETIN (j) At two positions, install these items to the brackets of the rib 11, cable sleeves, Item 1 and cable bundle 2S/636VB, as shown in Details A and J: 2 Clamp MS21919WCH4 Item (22) Retained at removal 1 Spacer NSA5527-03-01D Item (30) Retained at removal 1 Spacer NSA5527-03-04D Item (32) Retained at removal 1 Washer NAS1149D0332K Item (40) Retained at removal 1 Screw NAS1096-3-22 Item (51) Retained at removal 1 Clamp MS21919WCH9 Item 10 (k) At two positions, install these items to the brackets of the rib 10, cable sleeves, Item 1 and cable bundle 2S/636VB, as shown in Details A and L: 2 Clamp MS21919WCH4 Item (22) Retained at removal 2 Spacer NSA5527-03-01D Item (30) Retained at removal 2 Washer NAS1149D0332K Item (40) Retained at removal 2 Clamp MS21919WCH9 Item 10 2 Screw NAS1096-3-19 Item 14 (l) Install these items to the bracket between rib 9 and rib 10, cable sleeves, Item 1 and cable bundle 2S/636VB, as shown in Details A and Q: 3 Clamp MS21919WCH4 Item (22) Retained at removal 1 Spacer NSA5527-03-01D Item (30) Retained at removal 1 Spacer NSA5527-03-04D Item (32) Retained at removal 1 Washer NAS1149D0332K Item (40) Retained at removal

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 215 6

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# @A310 SERVICE BULLETIN
1 Screw NAS1096-3-22 Item (51) Retained at removal 1 Clamp MS21919WCH9 Item 10 (m) Install these items to the bracket of the rib 9, cable sleeves, Item 1 and cable bundle 2S/636VB, as shown in Details A and Q: 1 Clamp MS21919WCH5 Item (21) Retained at removal 1 Spacer NSA5527-03-02D Item (31) Retained at removal 1 Spacer NSA5527-03-04D Item (32) Retained at removal 1 Washer NAS1149D0332K Item (40) Retained at removal 1 Screw NAS1096-3-27 Item (52) Retained at removal 1 Clamp MS21919WCH9 Item 10 **CONF ALL D. TEST **CONF 001 (1) Subtask 282148-710-201-001 - Operational Manpower Resources Skills ELECTRICAL References Aircraft Maintenance Manual (AMM) 27-84-00, Page Block 501 28-42-44, Page Block 401 30-11-00, Page Block 501 36-11-00, Page Block 501 Elec. Std. Practices Manual (ESPM) 20-25-21 (a) Do a continuity test of disconnected wires (Refer to ESPM 20-25-21). (b) Do an operational test of the cadensicon sensor (Refer to AMM 28-42-44, Page Block 401). (c) Do the operational test (Refer to AMM 27-84-00, Page Block 501). (d) Do the operational test of the wing ice protection (Refer to AMM 30-11-00, Page Block 501). DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 216 6

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# @A310 SERVICE BULLETIN (e) Do the bite test (Refer to AMM 36-11-00, Page Block 501). **CONF 002 (1) Subtask 282148-710-201-001 - Operational Manpower Resources Skills ELECTRICAL References Aircraft Maintenance Manual (AMM) 27-84-00, Page Block 501 28-42-44, Page Block 401 30-11-00, Page Block 501 36-11-00, Page Block 501 Elec. Std. Practices Manual (ESPM) 20-25-21 (a) Do a continuity test of disconnected wires (Refer to ESPM 20-25-21). (b) Do an operational test of the cadensicon sensor (Refer to AMM 28-42-44, Page Block 401). (c) Do the operational test (Refer to AMM 27-84-00, Page Block 501). (d) Do the operational test of the wing ice protection (Refer to AMM 30-11-00, Page Block 501). (e) Do the bite test (Refer to AMM 36-11-00, Page Block 501). **CONF 003 (1) Subtask 282148-710-201-001 - Operational Manpower Resources Skills ELECTRICAL References Aircraft Maintenance Manual (AMM) 27-84-00, Page Block 501 28-42-44, Page Block 401 30-11-00, Page Block 501 36-11-00, Page Block 501 Elec. Std. Practices Manual (ESPM) 20-25-21 (a) Do a continuity test of disconnected wires (Refer to ESPM 20-25-21). (b) Do an operational test of the cadensicon sensor (Refer to AMM 28-42-44, Page Block 401). (c) Do the operational test (Refer to AMM 27-84-00, Page Block 501). (d) Do the operational test of the wing ice protection (Refer to AMM 30-11-00, Page Block 501).

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 217 6

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# @A310 SERVICE BULLETIN (e) Do the bite test (Refer to AMM 36-11-00, Page Block 501). **CONF 004 (1) Subtask 282148-710-201-001 - Operational Manpower Resources Skills ELECTRICAL References Aircraft Maintenance Manual (AMM) 27-84-00, Page Block 501 28-42-44, Page Block 401 30-11-00, Page Block 501 36-11-00, Page Block 501 Elec. Std. Practices Manual (ESPM) 20-25-21 (a) Do a continuity test of disconnected wires (Refer to ESPM 20-25-21). (b) Do an operational test of the cadensicon sensor (Refer to AMM 28-42-44, Page Block 401). (c) Do the operational test (Refer to AMM 27-84-00, Page Block 501). (d) Do the operational test of the wing ice protection (Refer to AMM 30-11-00, Page Block 501). (e) Do the bite test (Refer to AMM 36-11-00, Page Block 501). **CONF 005 (1) Subtask 282148-710-201-001 - Operational Manpower Resources Skills ELECTRICAL References Aircraft Maintenance Manual (AMM) 27-84-00, Page Block 501 28-42-44, Page Block 401 30-11-00, Page Block 501 36-11-00, Page Block 501 Elec. Std. Practices Manual (ESPM) 20-25-21 (a) Do a continuity test of disconnected wires (Refer to ESPM 20-25-21). (b) Do an operational test of the cadensicon sensor (Refer to AMM 28-42-44, Page Block 401). (c) Do the operational test (Refer to AMM 27-84-00, Page Block 501). (d) Do the operational test of the wing ice protection (Refer to AMM 30-11-00, Page Block 501).

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 218 6

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# @A310 SERVICE BULLETIN (e) Do the bite test (Refer to AMM 36-11-00, Page Block 501). **CONF 006 (1) Subtask 282148-710-201-001 - Operational Manpower Resources Skills ELECTRICAL References Aircraft Maintenance Manual (AMM) 27-84-00, Page Block 501 28-42-44, Page Block 401 30-11-00, Page Block 501 36-11-00, Page Block 501 Elec. Std. Practices Manual (ESPM) 20-25-21 (a) Do a continuity test of disconnected wires (Refer to ESPM 20-25-21). (b) Do an operational test of the cadensicon sensor (Refer to AMM 28-42-44, Page Block 401). (c) Do the operational test (Refer to AMM 27-84-00, Page Block 501). (d) Do the operational test of the wing ice protection (Refer to AMM 30-11-00, Page Block 501). (e) Do the bite test (Refer to AMM 36-11-00, Page Block 501). **CONF 007 (1) Subtask 282148-710-201-001 - Operational Manpower Resources Skills ELECTRICAL References Aircraft Maintenance Manual (AMM) 27-84-00, Page Block 501 28-42-44, Page Block 401 30-11-00, Page Block 501 36-11-00, Page Block 501 Elec. Std. Practices Manual (ESPM) 20-25-21 (a) Do a continuity test of disconnected wires (Refer to ESPM 20-25-21). (b) Do an operational test of the cadensicon sensor (Refer to AMM 28-42-44, Page Block 401). (c) Do the operational test (Refer to AMM 27-84-00, Page Block 501). (d) Do the operational test of the wing ice protection (Refer to AMM 30-11-00, Page Block 501).

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 219 6

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# @A310 SERVICE BULLETIN (e) Do the bite test (Refer to AMM 36-11-00, Page Block 501). **CONF 008 (1) Subtask 282148-710-201-001 - Operational Manpower Resources Skills ELECTRICAL References Aircraft Maintenance Manual (AMM) 27-84-00, Page Block 501 28-42-44, Page Block 401 30-11-00, Page Block 501 36-11-00, Page Block 501 Elec. Std. Practices Manual (ESPM) 20-25-21 (a) Do a continuity test of disconnected wires (Refer to ESPM 20-25-21). (b) Do an operational test of the cadensicon sensor (Refer to AMM 28-42-44, Page Block 401). (c) Do the operational test (Refer to AMM 27-84-00, Page Block 501). (d) Do the operational test of the wing ice protection (Refer to AMM 30-11-00, Page Block 501). (e) Do the bite test (Refer to AMM 36-11-00, Page Block 501). **CONF ALL E. CLOSE-UP **CONF 001 (1) Subtask 282148-861-002-001 - Energize Electrical Network Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 24-31-11, Page Block 401 (a) Battery re-connection : - For job set-up, refer to removal/installation of the batteries (Refer to AMM 24-31-11, Page Block 401), - Remove the blanking cap from the electrical connectors, - Make sure that the electrical connectors are clean and in correct condition, - Connect the connector on the battery,
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 220 6

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# @A310 SERVICE BULLETIN - Turn the knurled nut a quarter turn. (b) Remove all warning notices. (c) Restore the systems and the aircraft to normal operating condition. (2) Subtask 282148-942-009-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001 06-41-57, Page Block 001 25-54-10, Page Block 201 52-10-00, Page Block 001 52-30-00, Page Block 001 53-10-55, Page Block 401 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) On the RH wing, install the access panel 613RR (Refer to AMM 06-41-57, Page Block 001). (c) In the forward cargo compartment, install the sidewall panel 132QW (Refer to AMM 06-41-53, Page Block 001 and AMM 25-54-10, Page Block 201). (d) In the forward cargo compartment, at FR38.2, install the partition panel 132SW (Refer to AMM 06-41-53, Page Block 001 and AMM 53-10-55, Page Block 401). (e) Close the passenger/crew door 831 (Refer to AMM 52-10-00, Page Block 001). (f) Close the forward cargo compartment door 811 (Refer to AMM 52-30-00, Page Block 001). (g) Remove the access platform(s). (h) Restore the systems and the aircraft to normal operating condition. **CONF 002 (1) Subtask 282148-861-002-001 - Energize Electrical Network Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 24-31-11, Page Block 401

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 221 6

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# @A310 SERVICE BULLETIN (a) Battery re-connection : - For job set-up, refer to removal/installation of the batteries (Refer to AMM 24-31-11, Page Block 401), - Remove the blanking cap from the electrical connectors, - Make sure that the electrical connectors are clean and in correct condition, - Connect the connector on the battery, - Turn the knurled nut a quarter turn. (b) Remove all warning notices. (c) Restore the systems and the aircraft to normal operating condition. (2) Subtask 282148-942-009-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001 06-41-57, Page Block 001 25-54-10, Page Block 201 52-10-00, Page Block 001 52-30-00, Page Block 001 53-10-55, Page Block 401 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) On the RH wing, install the access panel 613RR (Refer to AMM 06-41-57, Page Block 001). (c) In the forward cargo compartment, install the sidewall panel 132QW (Refer to AMM 06-41-53, Page Block 001 and AMM 25-54-10, Page Block 201). (d) In the forward cargo compartment, at FR38.2, install the partition panel 132SW (Refer to AMM 06-41-53, Page Block 001 and AMM 53-10-55, Page Block 401). (e) Close the passenger/crew door 831 (Refer to AMM 52-10-00, Page Block 001). (f) Close the forward cargo compartment door 811 (Refer to AMM 52-30-00, Page Block 001). (g) Remove the access platform(s). (h) Restore the systems and the aircraft to normal operating condition.

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 222 6

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# @A310 SERVICE BULLETIN
**CONF 003 (1) Subtask 282148-861-002-001 - Energize Electrical Network Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 24-31-11, Page Block 401 (a) Battery re-connection : - For job set-up, refer to removal/installation of the batteries (Refer to AMM 24-31-11, Page Block 401), - Remove the blanking cap from the electrical connectors, - Make sure that the electrical connectors are clean and in correct condition, - Connect the connector on the battery, - Turn the knurled nut a quarter turn. (b) Remove all warning notices. (c) Restore the systems and the aircraft to normal operating condition. (2) Subtask 282148-942-009-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001 06-41-57, Page Block 001 25-54-10, Page Block 201 52-10-00, Page Block 001 52-30-00, Page Block 001 53-10-55, Page Block 401 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) On the RH wing, install the access panel 613RR (Refer to AMM 06-41-57, Page Block 001). (c) In the forward cargo compartment, install the sidewall panel 132QW (Refer to AMM 06-41-53, Page Block 001 and AMM 25-54-10, Page Block 201). (d) In the forward cargo compartment, at FR38.2, install the partition panel 132SW (Refer to AMM 06-41-53, Page Block 001 and AMM 53-10-55, Page Block 401). (e) Close the passenger/crew door 831 (Refer to AMM 52-10-00, Page Block 001). DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 223 6

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# @A310 SERVICE BULLETIN (f) Close the forward cargo compartment door 811 (Refer to AMM 52-30-00, Page Block 001). (g) Remove the access platform(s). (h) Restore the systems and the aircraft to normal operating condition. **CONF 004 (1) Subtask 282148-861-002-001 - Energize Electrical Network Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 24-31-11, Page Block 401 (a) Battery re-connection : - For job set-up, refer to removal/installation of the batteries (Refer to AMM 24-31-11, Page Block 401), - Remove the blanking cap from the electrical connectors, - Make sure that the electrical connectors are clean and in correct condition, - Connect the connector on the battery, - Turn the knurled nut a quarter turn. (b) Remove all warning notices. (c) Restore the systems and the aircraft to normal operating condition. (2) Subtask 282148-942-009-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001 06-41-57, Page Block 001 25-54-10, Page Block 201 52-10-00, Page Block 001 52-30-00, Page Block 001 53-10-55, Page Block 401 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) On the RH wing, install the access panel 613RR (Refer to AMM 06-41-57, Page Block 001).
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 224 6

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# @A310 SERVICE BULLETIN (c) In the forward cargo compartment, install the sidewall panel 132QW (Refer to AMM 06-41-53, Page Block 001 and AMM 25-54-10, Page Block 201). (d) In the forward cargo compartment, at FR38.2, install the partition panel 132SW (Refer to AMM 06-41-53, Page Block 001 and AMM 53-10-55, Page Block 401). (e) Close the passenger/crew door 831 (Refer to AMM 52-10-00, Page Block 001). (f) Close the forward cargo compartment door 811 (Refer to AMM 52-30-00, Page Block 001). (g) Remove the access platform(s). (h) Restore the systems and the aircraft to normal operating condition. **CONF 005 (1) Subtask 282148-861-002-001 - Energize Electrical Network Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 24-31-11, Page Block 401 (a) Battery re-connection : - For job set-up, refer to removal/installation of the batteries (Refer to AMM 24-31-11, Page Block 401), - Remove the blanking cap from the electrical connectors, - Make sure that the electrical connectors are clean and in correct condition, - Connect the connector on the battery, - Turn the knurled nut a quarter turn. (b) Remove all warning notices. (c) Restore the systems and the aircraft to normal operating condition. (2) Subtask 282148-942-009-001 - Close-up Manpower Resources Skills NON SPECIFIC

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 225 6

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# @A310 SERVICE BULLETIN

References Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001 06-41-57, Page Block 001 25-54-10, Page Block 201 52-10-00, Page Block 001 52-30-00, Page Block 001 53-10-55, Page Block 401 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) On the RH wing, install the access panel 613RR (Refer to AMM 06-41-57, Page Block 001). (c) In the forward cargo compartment, install the sidewall panel 132QW (Refer to AMM 06-41-53, Page Block 001 and AMM 25-54-10, Page Block 201). (d) In the forward cargo compartment, at FR38.2, install the partition panel 132SW (Refer to AMM 06-41-53, Page Block 001 and AMM 53-10-55, Page Block 401). (e) Close the passenger/crew door 831 (Refer to AMM 52-10-00, Page Block 001). (f) Close the forward cargo compartment door 811 (Refer to AMM 52-30-00, Page Block 001). (g) Remove the access platform(s). (h) Restore the systems and the aircraft to normal operating condition. **CONF 006 (1) Subtask 282148-861-002-001 - Energize Electrical Network Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 24-31-11, Page Block 401 (a) Battery re-connection : - For job set-up, refer to removal/installation of the batteries (Refer to AMM 24-31-11, Page Block 401), - Remove the blanking cap from the electrical connectors, - Make sure that the electrical connectors are clean and in correct condition, - Connect the connector on the battery, - Turn the knurled nut a quarter turn. (b) Remove all warning notices. DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 226 6

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# @A310 SERVICE BULLETIN (c) Restore the systems and the aircraft to normal operating condition. (2) Subtask 282148-942-009-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001 06-41-57, Page Block 001 25-54-10, Page Block 201 52-10-00, Page Block 001 52-30-00, Page Block 001 53-10-55, Page Block 401 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) On the RH wing, install the access panel 613RR (Refer to AMM 06-41-57, Page Block 001). (c) In the forward cargo compartment, install the sidewall panel 132QW (Refer to AMM 06-41-53, Page Block 001 and AMM 25-54-10, Page Block 201). (d) In the forward cargo compartment, at FR38.2, install the partition panel 132SW (Refer to AMM 06-41-53, Page Block 001 and AMM 53-10-55, Page Block 401). (e) Close the passenger/crew door 831 (Refer to AMM 52-10-00, Page Block 001). (f) Close the forward cargo compartment door 811 (Refer to AMM 52-30-00, Page Block 001). (g) Remove the access platform(s). (h) Restore the systems and the aircraft to normal operating condition. **CONF 007 (1) Subtask 282148-861-002-001 - Energize Electrical Network Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 24-31-11, Page Block 401 (a) Battery re-connection : - For job set-up, refer to removal/installation of the batteries (Refer to AMM 24-31-11, Page Block 401), - Remove the blanking cap from the electrical connectors,
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 227 6

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# @A310 SERVICE BULLETIN
- Make sure that the electrical connectors are clean and in correct condition, - Connect the connector on the battery, - Turn the knurled nut a quarter turn. (b) Remove all warning notices. (c) Restore the systems and the aircraft to normal operating condition. (2) Subtask 282148-942-009-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001 06-41-57, Page Block 001 25-54-10, Page Block 201 52-10-00, Page Block 001 52-30-00, Page Block 001 53-10-55, Page Block 401 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) On the RH wing, install the access panel 613RR (Refer to AMM 06-41-57, Page Block 001). (c) In the forward cargo compartment, install the sidewall panel 132QW (Refer to AMM 06-41-53, Page Block 001 and AMM 25-54-10, Page Block 201). (d) In the forward cargo compartment, at FR38.2, install the partition panel 132SW (Refer to AMM 06-41-53, Page Block 001 and AMM 53-10-55, Page Block 401). (e) Close the passenger/crew door 831 (Refer to AMM 52-10-00, Page Block 001). (f) Close the forward cargo compartment door 811 (Refer to AMM 52-30-00, Page Block 001). (g) Remove the access platform(s). (h) Restore the systems and the aircraft to normal operating condition. **CONF 008 (1) Subtask 282148-861-002-001 - Energize Electrical Network Manpower Resources Skills NON SPECIFIC

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 228 6

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# @A310 SERVICE BULLETIN

References Aircraft Maintenance Manual (AMM) 24-31-11, Page Block 401 (a) Battery re-connection : - For job set-up, refer to removal/installation of the batteries (Refer to AMM 24-31-11, Page Block 401), - Remove the blanking cap from the electrical connectors, - Make sure that the electrical connectors are clean and in correct condition, - Connect the connector on the battery, - Turn the knurled nut a quarter turn. (b) Remove all warning notices. (c) Restore the systems and the aircraft to normal operating condition. (2) Subtask 282148-942-009-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001 06-41-57, Page Block 001 25-54-10, Page Block 201 52-10-00, Page Block 001 52-30-00, Page Block 001 53-10-55, Page Block 401 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) On the RH wing, install the access panel 613RR (Refer to AMM 06-41-57, Page Block 001). (c) In the forward cargo compartment, install the sidewall panel 132QW (Refer to AMM 06-41-53, Page Block 001 and AMM 25-54-10, Page Block 201). (d) In the forward cargo compartment, at FR38.2, install the partition panel 132SW (Refer to AMM 06-41-53, Page Block 001 and AMM 53-10-55, Page Block 401). (e) Close the passenger/crew door 831 (Refer to AMM 52-10-00, Page Block 001). (f) Close the forward cargo compartment door 811 (Refer to AMM 52-30-00, Page Block 001). (g) Remove the access platform(s). (h) Restore the systems and the aircraft to normal operating condition. DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 229 6

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# @A310 SERVICE BULLETIN

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# @A310 SERVICE BULLETIN
Task 282148-831-853-001 - Modification - ADDITIONAL WORK 1 (Introduced at Rev 02) **CONF ALL WARNING: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND CAUTIONS INCLUDED IN THE REFERENCED PROCEDURES. WARNING: THIS PROCEDURE USES A FUEL SYSTEM ITEM THAT IS IN A CATEGORY KNOWN AS A CRITICAL DESIGN CONFIGURATION CONTROL LIMITATION (CDCCL) CDCCL IDENTIFIES AN ITEM THAT CAN BE THE SOURCE OF A POSSIBLE FUEL TANK IGNITION. YOU MUST KEEP ALL CDCCL ITEMS IN THE APPROVED CONFIGURATION. DAMAGE, WEAR OR CHANGES TO A CDCCL ITEM CAN CAUSE A POSSIBLE FUEL TANK EXPLOSION. 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. Task Associated Data **CONF 001 Manpower TOTAL MANHOURS 23.00 ELAPSED TIME (HOURS) 13.00 **CONF 002 Manpower TOTAL MANHOURS 23.00 ELAPSED TIME (HOURS) 13.00 **CONF 003 Manpower TOTAL MANHOURS 0.00 ELAPSED TIME (HOURS) 0.00
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# @A310 SERVICE BULLETIN
**CONF 004 Manpower TOTAL MANHOURS 0.00 ELAPSED TIME (HOURS) 0.00 **CONF 005 Manpower TOTAL MANHOURS 23.00 ELAPSED TIME (HOURS) 13.00 **CONF 006 Manpower TOTAL MANHOURS 23.00 ELAPSED TIME (HOURS) 13.00 **CONF 007 Manpower TOTAL MANHOURS 0.00 ELAPSED TIME (HOURS) 0.00 **CONF 008 Manpower TOTAL MANHOURS 0.00 ELAPSED TIME (HOURS) 0.00 **CONF ALL A. GENERAL **CONF 001 (1) Subtask 282148-910-205-001 - Standard Practices Manpower Resources Skills NON SPECIFIC Material necessary to do the job Consumable CMLD01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Storage compound 15-008A

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 232 6

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# @A310 SERVICE BULLETIN

References Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001 Consumable Material List (CML) Elec. Std. Practices Manual (ESPM) 20-33-00 Structural Repair Manual (SRM) 51-23-11 51-42-11 (a) For panel location (Refer to AMM 06-41-53, Page Block 001). (b) Obey the instructions for the wiring installation (Refer to ESPM 20-33-00). (c) Apply Storage compound 15-008A As required to the screws after assembly. (d) Installation of fasteners (Refer to SRM 51-42-11). (e) For paint coatings (Refer to SRM 51-23-11). (2) Subtask 282148-839-203-001 - 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 282148-910-205-001 - Standard Practices Manpower Resources Skills NON SPECIFIC Material necessary to do the job Consumable CMLD01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Storage compound 15-008A References Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001 Consumable Material List (CML) Elec. Std. Practices Manual (ESPM) 20-33-00 Structural Repair Manual (SRM) 51-23-11 51-42-11 (a) For panel location (Refer to AMM 06-41-53, Page Block 001). DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 233 6

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# @A310 SERVICE BULLETIN (b) Obey the instructions for the wiring installation (Refer to ESPM 20-33-00). (c) Apply Storage compound 15-008A As required to the screws after assembly. (d) Installation of fasteners (Refer to SRM 51-42-11). (e) For paint coatings (Refer to SRM 51-23-11). (2) Subtask 282148-839-203-001 - 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 None **CONF 004 None **CONF 005 (1) Subtask 282148-910-205-001 - Standard Practices Manpower Resources Skills NON SPECIFIC Material necessary to do the job Consumable CMLD01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Storage compound 15-008A References Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001 Consumable Material List (CML) Elec. Std. Practices Manual (ESPM) 20-33-00 Structural Repair Manual (SRM) 51-23-11 51-42-11 (a) For panel location (Refer to AMM 06-41-53, Page Block 001). (b) Obey the instructions for the wiring installation (Refer to ESPM 20-33-00). DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 234 6

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# @A310 SERVICE BULLETIN (c) Apply Storage compound 15-008A As required to the screws after assembly. (d) Installation of fasteners (Refer to SRM 51-42-11). (e) For paint coatings (Refer to SRM 51-23-11). (2) Subtask 282148-839-203-001 - 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 006 (1) Subtask 282148-910-205-001 - Standard Practices Manpower Resources Skills NON SPECIFIC Material necessary to do the job Consumable CMLD01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Storage compound 15-008A References Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001 Consumable Material List (CML) Elec. Std. Practices Manual (ESPM) 20-33-00 Structural Repair Manual (SRM) 51-23-11 51-42-11 (a) For panel location (Refer to AMM 06-41-53, Page Block 001). (b) Obey the instructions for the wiring installation (Refer to ESPM 20-33-00). (c) Apply Storage compound 15-008A As required to the screws after assembly. (d) Installation of fasteners (Refer to SRM 51-42-11). (e) For paint coatings (Refer to SRM 51-23-11). DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 235 6

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# @A310 SERVICE BULLETIN (2) Subtask 282148-839-203-001 - 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 007 None **CONF 008 None **CONF ALL B. PREPARATION **CONF 001 (1) Subtask 282148-941-205-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 24-00-00, Page Block 301 24-41-00, Page Block 301 27-80-00, Page Block 301 36-11-00, Page Block 401 ADDITIONAL WORK 1 is required by this revision for aircraft modified by issue 00 or Revision 01. (a) Make sure that the aircraft is electrically grounded (Refer to AMM 24-00-00, Page Block 301). (b) Fully extend the slats (Refer to AMM 27-80-00, Page Block 301). (c) De-energize the aircraft electrical circuits (Refer to AMM 24-41-00, Page Block 301). (d) Put the access platform(s) in position. (e) Open the access panels 612AT, 612KB, 612JB, 623AB, 623BB and 623EB. (f) Remove the bleed air duct if necessary (Refer to AMM 36-11-00, Page Block 401).

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 236 6

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# @A310 SERVICE BULLETIN
**CONF 002 (1) Subtask 282148-941-205-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 24-00-00, Page Block 301 24-41-00, Page Block 301 27-80-00, Page Block 301 36-11-00, Page Block 401 ADDITIONAL WORK 1 is required by this revision for aircraft modified by issue 00 or Revision 01. (a) Make sure that the aircraft is electrically grounded (Refer to AMM 24-00-00, Page Block 301). (b) Fully extend the slats (Refer to AMM 27-80-00, Page Block 301). (c) De-energize the aircraft electrical circuits (Refer to AMM 24-41-00, Page Block 301). (d) Put the access platform(s) in position. (e) Open the access panels 612AT, 612KB, 612JB, 623AB, 623BB and 623EB. (f) Remove the bleed air duct if necessary (Refer to AMM 36-11-00, Page Block 401). **CONF 003 None **CONF 004 None **CONF 005 (1) Subtask 282148-941-205-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 24-00-00, Page Block 301 24-41-00, Page Block 301 27-80-00, Page Block 301 36-11-00, Page Block 401 ADDITIONAL WORK 1 is required by this revision for aircraft modified by issue 00 or Revision 01. DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 237 6

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# @A310 SERVICE BULLETIN (a) Make sure that the aircraft is electrically grounded (Refer to AMM 24-00-00, Page Block 301). (b) Fully extend the slats (Refer to AMM 27-80-00, Page Block 301). (c) De-energize the aircraft electrical circuits (Refer to AMM 24-41-00, Page Block 301). (d) Put the access platform(s) in position. (e) Open the access panels 612AT, 612KB, 612JB, 623AB, 623BB and 623EB. (f) Remove the bleed air duct if necessary (Refer to AMM 36-11-00, Page Block 401). **CONF 006 (1) Subtask 282148-941-205-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 24-00-00, Page Block 301 24-41-00, Page Block 301 27-80-00, Page Block 301 36-11-00, Page Block 401 ADDITIONAL WORK 1 is required by this revision for aircraft modified by issue 00 or Revision 01. (a) Make sure that the aircraft is electrically grounded (Refer to AMM 24-00-00, Page Block 301). (b) Fully extend the slats (Refer to AMM 27-80-00, Page Block 301). (c) De-energize the aircraft electrical circuits (Refer to AMM 24-41-00, Page Block 301). (d) Put the access platform(s) in position. (e) Open the access panels 612AT, 612KB, 612JB, 623AB, 623BB and 623EB. (f) Remove the bleed air duct if necessary (Refer to AMM 36-11-00, Page Block 401). **CONF 007 None **CONF 008 None

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 238 6

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# @A310 SERVICE BULLETIN
**CONF ALL C. PROCEDURE **CONF 001 (1) Subtask 282148-831-256-001 - Modification Manpower Resources Manhours 14.00 Minimum number of person 2 Subtask elapsed time 7.00 Skills ELECTRICAL Material necessary to do the job Kit 282148D02R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 ABS0596S004 3 SLEEVE 10 MS21919WCH9 1 CLAMP 30 NSA5527-03-01D 2 SPACER 31 NSA5527-03-02D 1 SPACER 109 NSA935805-09 CONDUIT 117 NSA935807C09 12 CLAMP 121 NAS1096-3-40 1 SCREW 125 B9299071900200 1 EQUIPMNT 126 NSA938184PV1601 15 PIN 149 NSA935401-03 30 TIE 150 NSA935401-04 30 TIE References Elec. Std. Practices Manual (ESPM) 20-52-00 Fig. A-GBMAA Additional Work 1 (Introduced atRevision 02): Improvement of the 2SRoute in the RH-Wing pylon area (Kit D02) Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Sheet 08 Fig. A-GBLAA Additional Work 1 (Introduced at Revision 02): Installation of Protection Sleeve in the Area of 10QT (Kits D02 and D03) Sheet 01 Sheet 02 Sheet 03 Fig. A-GHAAA Hook-up Chart Sheet 01

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# @A310 SERVICE BULLETIN

References Fig. A-GHBAA Hook-up Chart Sheet 01 ADDITIONAL WORK 1 is required by this revision for aircraft modified by issue 00 or Revision 01. Refer to Fig. A-GBMAA Sheet 01 , Fig. A-GBMAA Sheet 02, Fig. A-GBMAA Sheet 03, Fig. A-GBMAA Sheet 04, Fig. A-GBMAA Sheet 05, Fig. A-GBMAA Sheet 06, Fig. AGBMAA Sheet 07 and Fig. A-GBMAA Sheet 08 Refer to Fig. A-GHAAA Sheet 01 Refer to Fig. A-GHBAA Sheet 01 (a) Installation of the cable sleeves in the RH-wing forward of the front spar between rib 11 and rib 12 in zone 623. Refer to Fig. A-GBLAA Sheet 01 , Fig. A-GBLAA Sheet 02 and Fig. A-GBLAA Sheet 03 1 At one position, remove these items from the bracket rib 11 and rib 12 and cable bundle 2S/636VB, as shown in Fig. A-GBLAA Sheet 01 and Sheet Fig. A-GBLAA Sheet 03 Details A and D: 2 Clamp MS21919WCH4 Item (22) Retain 1 Clamp MS21919WCH4 Item (22) Discard 1 Clamp MS21919WCH3 Item (23) Retain 1 Spacer NSA5527-03-01D Item (30) Retain 1 Spacer NSA5527-03-02D Item (31) Retain 2 Washer NSA935808-01 Item (112) Retain 2 Screw NAS1096-3-30 Item (121) Discard 1 Clamp NSA935807-06 Item (122) Retain 2 Install protection sleeve, as shown in Fig. A-GBLAA Sheet 01 thru Sheet Fig. A-GBLAA Sheet 03, Details A, B and D: 1 Sleeve ABS0596S004 Item 1 and attach the cable sleeves with: 10 Tie NSA935401-03 Item 149 or

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 240 6

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# @A310 SERVICE BULLETIN

10 Tie-Cable NSA935401-04 Item 150 3 Install, as shown in Fig. A-GBLAA Sheet 01 and Sheet Fig. A-GBLAA Sheet 03 Details A and E: 2 Clamp MS21919WCH4 Item (22) Retained at removal 1 Clamp MS21919WCH3 Item (23) Retained at removal 1 Spacer NSA5527-03-01D Item (30) Retained at removal 1 Spacer NSA5527-03-02D Item (31) Retained at removal 1 Washer NSA935808-01 Item (112) Retained at removal 1 Clamp NSA935807-06 Item (122) Retained at removal 1 Clamp MS21919WCH9 Item 10 1 Spacer NSA5527-03-02D Item 31 1 Screw NAS1096-3-40 Item 121 (b) Installation of the cable sleeves in the RH-wing forward of the front spar between rib 8 and rib 9 (pylon area) in zone 612. Refer to Fig. A-GBMAA Sheet 01 , Fig. A-GBMAA Sheet 02, Fig. A-GBMAA Sheet 03, Fig. A-GBMAA Sheet 04, Fig. A-GBMAA Sheet 05, Fig. A-GBMAA Sheet 06, Fig. A-GBMAA Sheet 07 and Fig. A-GBMAA Sheet 08 Refer to Fig. A-GHAAA Sheet 01 Refer to Fig. A-GHBAA Sheet 01 NOTE: If other wires are installed in the conduit of route 2S, disconnect them, change the conduits in accordance with this Service Bulletin, re-install the wires in the new conduit of route 2S and reconnect the wires. Do a test in accordance with ESPM 20-52-00. 1 Disconnect these wires of route 2S from the receptacles 40VC and 5006VC in accordance with the Hook-up Chart 1, Lines 1 thru 14, END 1, Fig. A-GHAAA Sheet 01 and the Hook-up Chart 2, Lines 2 thru 8, END 1, Fig. A-GHBAA Sheet 01

.

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# @A310 SERVICE BULLETIN

2 Remove, refer to Fig. A-GBMAA Sheet 03, Detail D, BEFORE: 1 Spacer NSA5527-03-02D Item (31) Discard 1 Clamp NSA935807C10 Item (110) Discard 1 Clamp NSA935807C16 Item (111) Retain 1 Washer NSA935808-01 Item (112) Retain 1 Screw NAS1096-3-23 Item (113) Retain 1 Spacer NSA5527-03-05D Item (114) Discard 1 Washer NSA1149D0332K Item (115) Retain 1 Nut NAS1291C3M Item (116) Retain 1 Clamp NSA935807C09 Item (117) Retain 3 Remove, refer to Fig. A-GBMAA Sheet 04, Detail F, BEFORE: 2 Spacer NSA5527-03-01D Item (30) Retain 1 Spacer NSA5527-03-02D Item (31) Retain 1 Clamp NSA935807C10 Item (110) Retain 1 Clamp NSA935807C10 Item (110) Discard 1 Clamp NSA935807C16 Item (111) Retain 1 Washer NSA935808-01 Item (112) Retain 1 Clamp NSA935807C09 Item (117) Retain 1 Screw NAS1096-3-33 Item (118) Retain 4 Remove, refer to Fig. A-GBMAA Sheet 05, , Detail H, BEFORE: 2 Spacer NSA5527-03-01D Item (30) Retain 2 Spacer NSA5527-03-02D Item (31) Retain 2 Clamp NSA935807C10 Item (110) Discard 2 Clamp NSA935807C16 Item (111) Retain

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# @A310 SERVICE BULLETIN
2 Spacer NSA5527-03-05D Item (114) Retain 2 Washer NSA1149D0332K Item (115) Retain 2 Clamp NSA935807C09 Item (117) Retain 2 Screw NAS1096-3-33 Item (118) Retain 5 Remove, refer to Fig. A-GBMAA Sheet 06, Detail K, BEFORE: 1 Spacer NSA5527-03-01D Item (30) Retain 1 Spacer NSA5527-03-02D Item (31) Retain 1 Clamp NSA935807C10 Item (110) Discard 1 Clamp NSA935807C16 Item (111) Retain 1 Spacer NSA5527-03-05D Item (114) Retain 1 Washer NSA1149D0332K Item (115) Retain 1 Clamp NSA935807C09 Item (117) Retain 1 Screw NAS1096-3-33 Item (118) Retain 6 Remove, refer to Fig. A-GBMAA Sheet 07, Detail M, BEFORE: 1 Spacer NSA5527-03-01D Item (30) Retain 1 Spacer NSA5527-03-02D Item (31) Retain 1 Clamp NSA935807C10 Item (110) Discard 1 Clamp NSA935807C16 Item (111) Retain 1 Washer NSA935808-01 Item (112) Retain 1 Spacer NSA5527-03-05D Item (114) Retain 1 Clamp NSA935807C09 Item (117) Retain 1 Screw NAS1096-3-33 Item (118) Retain 7 Remove, refer to Fig. A-GBMAA Sheet 08, Detail P, BEFORE: 1 Spacer NSA5527-03-02D Item (31) Retain

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# @A310 SERVICE BULLETIN
1 Clamp NSA935807C10 Item (110) Discard 1 Clamp NSA935807C16 Item (111) Retain 1 Washer NSA935808-01 Item (112) Retain 1 Spacer NSA5527-03-05D Item (114) Retain 1 Clamp NSA935807C09 Item (117) Retain 1 Screw NAS1096-3-25 Item (119) Retain 8 Remove the identification sleeves from the cable harnesses near the receptacles 40VC and 5006VC as shown Fig. A-GBMAA Sheet 01 , Detail A As required placard Item (125) Discard
9 Remove the protection sleeve from the cable harness: 1 Sleeve Item (109) Discard 10 Cut the conduit to the required length and install: 3 (ME) Conduit NSA935805-09 Item 109
a One part 1500.0 mm (59.06 in.) to the electrical wires for 10QT-A and 10QT-B of route 2S/636VB, refer to the Hook-up Chart 2, Fig. A-GHBAA Sheet 01 b Three parts, one 520.0 mm (20.47 in.) and two 240.0 mm (9.45 in.) to the remaining electrical wires of route 2S/636VB, refer to Fig. A-GHAAA Sheet 01 11 Connect the electrical wires of route 2S to the receptacles 40VC and 5006VC in accordance with the Hook-up Chart 1, Lines 1 thru 14, END 1, Fig. AGHAAA Sheet 01 and the Hook-up Chart 2, Lines 2 thru 8, END 1, Fig. AGHBAA Sheet 01 . Use the contact pins if required: 15 Pin NSA938184PV1601 Item 126 12 Install, refer to Fig. A-GBMAA Sheet 08, Detail Q, AFTER: 1 Spacer NSA5527-03-02D Item (31) Retained at removal 1 Clamp NSA935807C16 Item (111) Retained at removal 1 Washer NSA935808-01 Item (112) Retained at removal
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 244 6

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# @A310 SERVICE BULLETIN
1 Spacer NSA5527-03-05D Item (114) Retained at removal 1 Clamp NSA935807C09 Item (117) Retained at removal 1 Screw NAS1096-3-25 Item (119) Retained at removal 2 Clamp NSA935807C09 Item 117 13 Install, refer to Fig. A-GBMAA Sheet 07, Detail N, AFTER: 1 Spacer NSA5527-03-01D Item (30) Retained at removal 1 Spacer NSA5527-03-02D Item (31) Retained at removal 1 Clamp NSA935807C16 Item (111) Retained at removal 1 Washer NSA935808-01 Item (112) Retained at removal 1 Spacer NSA5527-03-05D Item (114) Retained at removal 1 Clamp NSA935807C09 Item (117) Retained at removal 1 Screw NAS1096-3-33 Item (118) Retained at removal 2 Clamp NSA935807C09 Item 117 14 Install, refer to Fig. A-GBMAA Sheet 06, Detail L, AFTER: 1 Spacer NSA5527-03-01D Item (30) Retained at removal 1 Spacer NSA5527-03-02D Item (31) Retained at removal 1 Clamp NSA935807C16 Item (111) Retained at removal 1 Spacer NSA5527-03-05D Item (114) Retained at removal 1 Washer NSA1149D0332K Item (115) Retained at removal DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 245 6

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# @A310 SERVICE BULLETIN
1 Clamp NSA935807C09 Item (117) Retained at removal 1 Screw NAS1096-3-33 Item (118) Retained at removal 2 Clamp NSA935807C09 Item 117 15 Install, refer to Fig. A-GBMAA Sheet 05, Detail J, AFTER: 2 Spacer NSA5527-03-01D Item (30) Retained at removal 2 Spacer NSA5527-03-02D Item (31) Retained at removal 2 Clamp NSA935807C16 Item (111) Retained at removal 2 Spacer NSA5527-03-05D Item (114) Retained at removal 2 Washer NSA1149D0332K Item (115) Retained at removal 2 Clamp NSA935807C09 Item (117) Retained at removal 2 Screw NAS1096-3-33 Item (118) Retained at removal 2 Clamp NSA935807C09 Item 117 16 Install, refer to Fig. A-GBMAA Sheet 04, Detail G, AFTER: 2 Spacer NSA5527-03-01D Item (30) Retained at removal 1 Spacer NSA5527-03-02D Item (31) Retained at removal 1 Clamp NSA935807C10 Item (110) Retained at removal 1 Clamp NSA935807C16 Item (111) Retained at removal 1 Washer NSA935808-01 Item (112) Retained at removal 1 Clamp NSA935807C09 Item (117) Retained at removal DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 246 6

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# @A310 SERVICE BULLETIN
1 Screw NAS1096-3-33 Item (118) Retained at removal 2 Clamp NSA935807C09 Item 117 17 Install, refer to Fig. A-GBMAA Sheet 03, Detail E, AFTER: 2 Spacer NSA5527-03-01D Item 30 1 Clamp NSA935807C16 Item (111) Retained at removal 1 Washer NSA935808-01 Item (112) Retained at removal 1 Screw NAS1096-3-23 Item (113) Retained at removal 1 Washer NSA1149D0332K Item (115) Retained at removal 1 Nut NAS1291C3M Item (116) Retained at removal 1 Clamp NSA935807C09 Item (117) Retained at removal 2 Clamp NSA935807C09 Item 117 18 Protect the electrical wires for 10QT-A and 10QT-B of route 2S/636VB, refer to the Hook-up Chart 2, Fig. A-GHBAA Sheet 01 and refer to Fig. A-GBMAA Sheet 02 and Sheet Fig. A-GBMAA Sheet 03 with: 2 Sleeve ABS0596S004 Item 1 cut the sleeve to the required length and install with: 20 Tie NSA935401-03 Item 149 20 Tie-Cable NSA935401-04 Item 150 19 Install the identification placards, refer to Fig. A-GBMAA Sheet 02, 1 Placard set B9299071900200 Item 125

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 247 6

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# @A310 SERVICE BULLETIN
**CONF 002 (1) Subtask 282148-831-256-002 - Modification Manpower Resources Manhours 14.00 Minimum number of person 2 Subtask elapsed time 7.00 Skills ELECTRICAL Material necessary to do the job Kit 282148D03R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 ABS0596S004 SLEEVE 10 MS21919WCH9 1 CLAMP 31 NSA5527-03-02D 2 SPACER 109 NSA935805-09 CONDUIT 117 NSA935807C09 CLAMP 121 NAS1096-3-40 1 SCREW 123 NAS1801-3-31 SCREW 126 NSA938184PV1601 PIN 130 NSA5527-03-08D 1 SPACER 131 NSA5527-03-07D 1 SPACER 132 B9299071900600 EQUIPMNT 149 NSA935401-03 10 TIE 150 NSA935401-04 30 TIE References Elec. Std. Practices Manual (ESPM) 20-52-00 Fig. A-GBNAA Additional Work 1 (Introduced atRevision 02): Improvement of the 2SRoute in the RH-Wing Pylon Area (Kit D03) Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Sheet 08 Fig. A-GHBAA Hook-up Chart Sheet 01 ADDITIONAL WORK 1 is required by this revision for aircraft modified by issue 00 or Revision 01.

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 248 6

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# @A310 SERVICE BULLETIN (a) Installation of the cable sleeves in the RH-wing forward of the front spar between rib 11 and rib 12 in zone 623. Refer to Fig. A-GBNAA Sheet 01 , Fig. A-GBNAA Sheet 02, Fig. A-GBNAA Sheet 03, Fig. A-GBNAA Sheet 04, Fig. A-GBNAA Sheet 05, Fig. A-GBNAA Sheet 06, Fig. A-GBNAA Sheet 07 and Fig. A-GBNAA Sheet 08 Refer to Fig. A-GHBAA Sheet 01 1 At one position, remove these items from the bracket rib 11 and rib 12 and cable bundle 2S/636VB, as shown in Fig. A-GBNAA Sheet 01 and Sheet Fig. A-GBNAA Sheet 03 Details A and D: 2 Clamp MS21919WCH4 Item (22) Retain 1 Clamp MS21919WCH4 Item (22) Discard 1 Clamp MS21919WCH3 Item (23) Retain 1 Spacer NSA5527-03-01D Item (30) Retain 1 Spacer NSA5527-03-02D Item (31) Retain 2 Washer NSA935808-01 Item (112) Retain 2 Screw NAS1096-3-30 Item (121) Discard 1 Clamp NSA935807-06 Item (122) Retain 2 Install protection sleeve, as shown in Fig. A-GBNAA Sheet 01 thru Sheet Fig. A-GBNAA Sheet 03 Details A, B and C: 1 Sleeve ABS0596S004 Item 1 and attach the cable sleeves with: 10 Tie NSA935401-03 Item 149 or 10 Tie-Cable NSA935401-04 Item 150 3 Install, as shown in Fig. A-GBNAA Sheet 01 and Sheet Fig. A-GBNAA Sheet 03 Details A and E: 2 Clamp MS21919WCH4 Item (22) Retained at removal 1 Clamp MS21919WCH3 Item (23) Retained at removal 1 Spacer NSA5527-03-01D Item (30) Retained at removal DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 249 6

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# @A310 SERVICE BULLETIN
1 Spacer NSA5527-03-02D Item (31) Retained at removal 1 Washer NSA935808-01 Item (112) Retained at removal 1 Clamp NSA935807-06 Item (122) Retained at removal 1 Clamp MS21919WCH9 Item 10 1 Spacer NSA5527-03-02D Item 31 1 Screw NAS1096-3-40 Item 121 (b) Installation of the cable sleeves in the RH-wing forward of the front spar between rib 8 and rib 9 (pylon area) in zone 612. Refer to Fig. A-GBNAA Sheet 01 Refer to Fig. A-GHBAA Sheet 01 NOTE: If other wires are installed in the conduit of route 2S, disconnect them, change the conduits in accordance with this Service Bulletin, re-install the wires in the new conduit of route 2S and reconnect the wires. Do a test in accordance with ESPM 20-52-00. 1 Disconnect these wires of route 2S from the receptacles 40VC and 5006VC in accordance with the Hook-up Chart 2, Lines 2 thru 8, END 1, Fig. A-GHBAA Sheet 01

. 2 Remove, refer to Fig. A-GBNAA Sheet 03, Detail D, BEFORE: 1 Spacer NSA5527-03-02D Item (31) Retain 2 Clamp NSA935807C16 Item (111) Retain 1 Washer NSA935808-01 Item (112) Retain 1 Screw NAS1096-3-23 Item (113) Retain 1 Spacer NSA5527-03-05D Item (114) Retain 1 Nut NAS1291C3M Item (116) Retain 1 Washer AN960KD10l Item (124) Retain 3 Remove, refer to Fig. A-GBNAA Sheet 04, Detail F, BEFORE: 1 Spacer NSA5527-03-02D Item (31) Retain

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 250 6

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# @A310 SERVICE BULLETIN
2 Clamp NSA935807C16 Item (111) Retain 1 Washer NSA935808-01 Item (112) Retain 1 Screw NAS1096-3-23 Item (113) Retain 1 Spacer NSA5527-03-05D Item (114) Retain 4 Remove, refer to Fig. A-GBNAA Sheet 05, Detail H, BEFORE: 2 Spacer NSA5527-03-02D Item (31) Retain 4 Clamp NSA935807C16 Item (111) Retain 2 Washer NSA935808-01 Item (112) Retain 2 Screw NAS1096-3-23 Item (113) Retain 2 Spacer NSA5527-03-05D Item (114) Retain 5 Remove, refer to Fig. A-GBNAA Sheet 06, Detail K, BEFORE: 1 Spacer NSA5527-03-02D Item (31) Retain 2 Clamp NSA935807C16 Item (111) Retain 1 Washer NSA935808-01 Item (112) Retain 1 Screw NAS1096-3-23 Item (113) Discard 1 Clamp NSA5516-04NV Item (120) Retain 6 Remove, refer to Fig. A-GBNAA Sheet 07, Detail M, BEFORE: 1 Spacer NSA5527-03-02D Item (31) Retain 2 Clamp NSA935807C16 Item (111) Retain 1 Washer NSA935808-01 Item (112) Retain 1 Screw NAS1096-3-23 Item (113) Discard 1 Spacer NSA5527-03-05D Item (114) Retain 7 Remove, refer to Fig. A-GBNAA Sheet 08, Detail P, BEFORE: 1 Spacer NSA5527-03-02D Item (31) Retain 2 Clamp NSA935807C16 Item (111) Retain DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 251 6

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# @A310 SERVICE BULLETIN
1 Washer NSA935808-01 Item (112) Retain 1 Screw NAS1096-3-23 Item (113) Discard 1 Spacer NSA5527-03-05D Item (114) Retain 8 Remove the identification placards from the cable harnesses near the receptacles 40VC and 5006VC as shown Fig. A-GBNAA Sheet 02, Detail A As required placard Item (132) Discard
9 Remove the disconnected electrical wires from the protection sleeve. 10 Install to the electrical wires for 10QT-A and 10QT-B of route 2S/636VB, refer to the Hook-up Chart 2, Lines 2 thru 8, Fig. A-GHBAA Sheet 01 : 1 (ME) Conduit NSA935805-09 Item 109 11 Connect the electrical wires of route 2S to the receptacles 40VC and 5006VC in accordance with the Hook-up Chart 2, Lines 2 thru 8, END 1, Fig. AGHBAA Sheet 01 . Use the contact pins if required: 7 Pin NSA938184PV1601 Item 126 12 Install, refer to Fig. A-GBNAA Sheet 08, Detail Q, AFTER: 1 Spacer NSA5527-03-02D Item (31) Retained at removal 1 Spacer NSA5527-03-02D Item 31 2 Clamp NSA935807C16 Item (111) Retained at removal 1 Washer NSA935808-01 Item (112) Retained at removal 1 Spacer NSA5527-03-05D Item (114) Retained at removal 1 Clamp NSA935807C09 Item 117 1 Screw NAS1801-3-31 Item 123 1 Spacer NSA5527-03-07D Item 131 13 Install, refer to Fig. A-GBNAA Sheet 07, Detail N, AFTER: 1 Spacer NSA5527-03-02D Item (31) Retained at removal
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 252 6

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# @A310 SERVICE BULLETIN
2 Clamp NSA935807C16 Item (111) Retained at removal 1 Washer NSA935808-01 Item (112) Retained at removal 1 Spacer NSA5527-03-05D Item (114) Retained at removal 1 Clamp NSA935807C09 Item 117 1 Screw NAS1801-3-31 Item 123 1 Spacer NSA5527-03-08D Item 130 14 Install, refer to Fig. A-GBNAA Sheet 06, Detail L, AFTER: 2 Spacer NSA5527-03-02D Item (31) Retained at removal 2 Clamp NSA935807C16 Item (111) Retained at removal 1 Washer NSA935808-01 Item (112) Retained at removal 1 Clamp NSA5516-04NV Item (120) Retained at removal 1 Clamp NSA935807C09 Item 117 1 Screw NAS1801-3-31 Item 123 15 Install, refer to Fig. A-GBNAA Sheet 05, Detail J, AFTER: 2 Spacer NSA5527-03-02D Item (31) Retained at removal 4 Clamp NSA935807C16 Item (111) Retained at removal 2 Washer NSA935808-01 Item (112) Retained at removal 2 Screw NAS1096-3-23 Item (113) Retained at removal 2 Spacer NSA5527-03-05D Item (114) Retained at removal 2 Clamp NSA935807C09 Item 117
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 253 6

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# @A310 SERVICE BULLETIN
16 Install, refer to Fig. A-GBNAA Sheet 04, Detail G, AFTER: 1 Spacer NSA5527-03-02D Item (31) Retained at removal 2 Clamp NSA935807C16 Item (111) Retained at removal 1 Washer NSA935808-01 Item (112) Retained at removal 1 Screw NAS1096-3-23 Item (113) Retained at removal 1 Spacer NSA5527-03-05D Item (114) Retained at removal 1 Clamp NSA935807C09 Item 117 17 Install, refer to Fig. A-GBNAA Sheet 03, Detail E, AFTER: 1 Spacer NSA5527-03-02D Item (31) Retained at removal 2 Clamp NSA935807C16 Item (111) Retained at removal 1 Washer NSA935808-01 Item (112) Retained at removal 1 Screw NAS1096-3-23 Item (113) Retained at removal 1 Spacer NSA5527-03-05D Item (114) Retained at removal 1 Nut NAS1291C3M Item (116) Retained at removal 1 Washer AN960KD10l Item (124) Retained at removal 1 Clamp NSA935807C09 Item 117 18 Protect the electrical wires for 10QT-A and 10QT-B of route 2S/636VB, refer to the Hook-up Chart 2, Fig. A-GHBAA Sheet 01 with: 3 Sleeve ABS0596S004 Item 1 and 20 Tie NSA935401-03 Item 149
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 254 6

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# @A310 SERVICE BULLETIN

or 20 Tie-Cable NSA935401-04 Item 150 19 Install the identification placards, refer to Fig. A-GBNAA Sheet 02 1 Placard Set B9299071900600 Item 132 **CONF 003 None **CONF 004 None **CONF 005 (1) Subtask 282148-831-256-001 - Modification Manpower Resources Manhours 14.00 Minimum number of person 2 Subtask elapsed time 7.00 Skills ELECTRICAL Material necessary to do the job Kit 282148D02R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 ABS0596S004 3 SLEEVE 10 MS21919WCH9 1 CLAMP 30 NSA5527-03-01D 2 SPACER 31 NSA5527-03-02D 1 SPACER 109 NSA935805-09 CONDUIT 117 NSA935807C09 12 CLAMP 121 NAS1096-3-40 1 SCREW 125 B9299071900200 1 EQUIPMNT 126 NSA938184PV1601 15 PIN 149 NSA935401-03 30 TIE 150 NSA935401-04 30 TIE References Elec. Std. Practices Manual (ESPM) 20-52-00

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 255 6

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# @A310 SERVICE BULLETIN

References Fig. A-GBMAA Additional Work 1 (Introduced atRevision 02): Improvement of the 2SRoute in the RH-Wing pylon area (Kit D02) Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Sheet 08 Fig. A-GBLAA Additional Work 1 (Introduced at Revision 02): Installation of Protection Sleeve in the Area of 10QT (Kits D02 and D03) Sheet 01 Sheet 02 Sheet 03 Fig. A-GHAAA Hook-up Chart Sheet 01 Fig. A-GHBAA Hook-up Chart Sheet 01 ADDITIONAL WORK 1 is required by this revision for aircraft modified by issue 00 or Revision 01. Refer to Fig. A-GBMAA Sheet 01 , Fig. A-GBMAA Sheet 02, Fig. A-GBMAA Sheet 03, Fig. A-GBMAA Sheet 04, Fig. A-GBMAA Sheet 05, Fig. A-GBMAA Sheet 06, Fig. AGBMAA Sheet 07 and Fig. A-GBMAA Sheet 08 Refer to Fig. A-GHAAA Sheet 01 Refer to Fig. A-GHBAA Sheet 01 (a) Installation of the cable sleeves in the RH-wing forward of the front spar between rib 11 and rib 12 in zone 623. Refer to Fig. A-GBLAA Sheet 01 , Fig. A-GBLAA Sheet 02 and Fig. A-GBLAA Sheet 03 1 At one position, remove these items from the bracket rib 11 and rib 12 and cable bundle 2S/636VB, as shown in Fig. A-GBLAA Sheet 01 and Sheet Fig. A-GBLAA Sheet 03 Details A and D: 2 Clamp MS21919WCH4 Item (22) Retain 1 Clamp MS21919WCH4 Item (22) Discard 1 Clamp MS21919WCH3 Item (23) Retain 1 Spacer NSA5527-03-01D Item (30) Retain 1 Spacer NSA5527-03-02D Item (31) Retain 2 Washer NSA935808-01 Item (112) Retain DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 256 6

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# @A310 SERVICE BULLETIN
2 Screw NAS1096-3-30 Item (121) Discard 1 Clamp NSA935807-06 Item (122) Retain 2 Install protection sleeve, as shown in Fig. A-GBLAA Sheet 01 thru Sheet Fig. A-GBLAA Sheet 03, Details A, B and D: 1 Sleeve ABS0596S004 Item 1 and attach the cable sleeves with: 10 Tie NSA935401-03 Item 149 or 10 Tie-Cable NSA935401-04 Item 150 3 Install, as shown in Fig. A-GBLAA Sheet 01 and Sheet Fig. A-GBLAA Sheet 03 Details A and E: 2 Clamp MS21919WCH4 Item (22) Retained at removal 1 Clamp MS21919WCH3 Item (23) Retained at removal 1 Spacer NSA5527-03-01D Item (30) Retained at removal 1 Spacer NSA5527-03-02D Item (31) Retained at removal 1 Washer NSA935808-01 Item (112) Retained at removal 1 Clamp NSA935807-06 Item (122) Retained at removal 1 Clamp MS21919WCH9 Item 10 1 Spacer NSA5527-03-02D Item 31 1 Screw NAS1096-3-40 Item 121 (b) Installation of the cable sleeves in the RH-wing forward of the front spar between rib 8 and rib 9 (pylon area) in zone 612. Refer to Fig. A-GBMAA Sheet 01 , Fig. A-GBMAA Sheet 02, Fig. A-GBMAA Sheet 03, Fig. A-GBMAA Sheet 04, Fig. A-GBMAA Sheet 05, Fig. A-GBMAA Sheet 06, Fig. A-GBMAA Sheet 07 and Fig. A-GBMAA Sheet 08 Refer to Fig. A-GHAAA Sheet 01

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 257 6

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# @A310 SERVICE BULLETIN
Refer to Fig. A-GHBAA Sheet 01 NOTE: If other wires are installed in the conduit of route 2S, disconnect them, change the conduits in accordance with this Service Bulletin, re-install the wires in the new conduit of route 2S and reconnect the wires. Do a test in accordance with ESPM 20-52-00. 1 Disconnect these wires of route 2S from the receptacles 40VC and 5006VC in accordance with the Hook-up Chart 1, Lines 1 thru 14, END 1, Fig. A-GHAAA Sheet 01 and the Hook-up Chart 2, Lines 2 thru 8, END 1, Fig. A-GHBAA Sheet 01

. 2 Remove, refer to Fig. A-GBMAA Sheet 03, Detail D, BEFORE: 1 Spacer NSA5527-03-02D Item (31) Discard 1 Clamp NSA935807C10 Item (110) Discard 1 Clamp NSA935807C16 Item (111) Retain 1 Washer NSA935808-01 Item (112) Retain 1 Screw NAS1096-3-23 Item (113) Retain 1 Spacer NSA5527-03-05D Item (114) Discard 1 Washer NSA1149D0332K Item (115) Retain 1 Nut NAS1291C3M Item (116) Retain 1 Clamp NSA935807C09 Item (117) Retain 3 Remove, refer to Fig. A-GBMAA Sheet 04, Detail F, BEFORE: 2 Spacer NSA5527-03-01D Item (30) Retain 1 Spacer NSA5527-03-02D Item (31) Retain 1 Clamp NSA935807C10 Item (110) Retain 1 Clamp NSA935807C10 Item (110) Discard 1 Clamp NSA935807C16 Item (111) Retain 1 Washer NSA935808-01 Item (112) Retain 1 Clamp NSA935807C09 Item (117) Retain 1 Screw NAS1096-3-33 Item (118) Retain
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 258 6

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# @A310 SERVICE BULLETIN

4 Remove, refer to Fig. A-GBMAA Sheet 05, , Detail H, BEFORE: 2 Spacer NSA5527-03-01D Item (30) Retain 2 Spacer NSA5527-03-02D Item (31) Retain 2 Clamp NSA935807C10 Item (110) Discard 2 Clamp NSA935807C16 Item (111) Retain 2 Spacer NSA5527-03-05D Item (114) Retain 2 Washer NSA1149D0332K Item (115) Retain 2 Clamp NSA935807C09 Item (117) Retain 2 Screw NAS1096-3-33 Item (118) Retain 5 Remove, refer to Fig. A-GBMAA Sheet 06, Detail K, BEFORE: 1 Spacer NSA5527-03-01D Item (30) Retain 1 Spacer NSA5527-03-02D Item (31) Retain 1 Clamp NSA935807C10 Item (110) Discard 1 Clamp NSA935807C16 Item (111) Retain 1 Spacer NSA5527-03-05D Item (114) Retain 1 Washer NSA1149D0332K Item (115) Retain 1 Clamp NSA935807C09 Item (117) Retain 1 Screw NAS1096-3-33 Item (118) Retain 6 Remove, refer to Fig. A-GBMAA Sheet 07, Detail M, BEFORE: 1 Spacer NSA5527-03-01D Item (30) Retain 1 Spacer NSA5527-03-02D Item (31) Retain 1 Clamp NSA935807C10 Item (110) Discard 1 Clamp NSA935807C16 Item (111) Retain 1 Washer NSA935808-01 Item (112) Retain

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 259 6

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# @A310 SERVICE BULLETIN
1 Spacer NSA5527-03-05D Item (114) Retain 1 Clamp NSA935807C09 Item (117) Retain 1 Screw NAS1096-3-33 Item (118) Retain 7 Remove, refer to Fig. A-GBMAA Sheet 08, Detail P, BEFORE: 1 Spacer NSA5527-03-02D Item (31) Retain 1 Clamp NSA935807C10 Item (110) Discard 1 Clamp NSA935807C16 Item (111) Retain 1 Washer NSA935808-01 Item (112) Retain 1 Spacer NSA5527-03-05D Item (114) Retain 1 Clamp NSA935807C09 Item (117) Retain 1 Screw NAS1096-3-25 Item (119) Retain 8 Remove the identification sleeves from the cable harnesses near the receptacles 40VC and 5006VC as shown Fig. A-GBMAA Sheet 01 , Detail A As required placard Item (125) Discard
9 Remove the protection sleeve from the cable harness: 1 Sleeve Item (109) Discard 10 Cut the conduit to the required length and install: 3 (ME) Conduit NSA935805-09 Item 109
a One part 1500.0 mm (59.06 in.) to the electrical wires for 10QT-A and 10QT-B of route 2S/636VB, refer to the Hook-up Chart 2, Fig. A-GHBAA Sheet 01 b Three parts, one 520.0 mm (20.47 in.) and two 240.0 mm (9.45 in.) to the remaining electrical wires of route 2S/636VB, refer to Fig. A-GHAAA Sheet 01 11 Connect the electrical wires of route 2S to the receptacles 40VC and 5006VC in accordance with the Hook-up Chart 1, Lines 1 thru 14, END 1, Fig. AGHAAA Sheet 01 and the Hook-up Chart 2, Lines 2 thru 8, END 1, Fig. AGHBAA Sheet 01 . Use the contact pins if required: 15 Pin NSA938184PV1601 Item 126

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 260 6

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# @A310 SERVICE BULLETIN

12 Install, refer to Fig. A-GBMAA Sheet 08, Detail Q, AFTER: 1 Spacer NSA5527-03-02D Item (31) Retained at removal 1 Clamp NSA935807C16 Item (111) Retained at removal 1 Washer NSA935808-01 Item (112) Retained at removal 1 Spacer NSA5527-03-05D Item (114) Retained at removal 1 Clamp NSA935807C09 Item (117) Retained at removal 1 Screw NAS1096-3-25 Item (119) Retained at removal 2 Clamp NSA935807C09 Item 117 13 Install, refer to Fig. A-GBMAA Sheet 07, Detail N, AFTER: 1 Spacer NSA5527-03-01D Item (30) Retained at removal 1 Spacer NSA5527-03-02D Item (31) Retained at removal 1 Clamp NSA935807C16 Item (111) Retained at removal 1 Washer NSA935808-01 Item (112) Retained at removal 1 Spacer NSA5527-03-05D Item (114) Retained at removal 1 Clamp NSA935807C09 Item (117) Retained at removal 1 Screw NAS1096-3-33 Item (118) Retained at removal 2 Clamp NSA935807C09 Item 117 14 Install, refer to Fig. A-GBMAA Sheet 06, Detail L, AFTER: 1 Spacer NSA5527-03-01D Item (30) Retained at removal

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 261 6

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# @A310 SERVICE BULLETIN
1 Spacer NSA5527-03-02D Item (31) Retained at removal 1 Clamp NSA935807C16 Item (111) Retained at removal 1 Spacer NSA5527-03-05D Item (114) Retained at removal 1 Washer NSA1149D0332K Item (115) Retained at removal 1 Clamp NSA935807C09 Item (117) Retained at removal 1 Screw NAS1096-3-33 Item (118) Retained at removal 2 Clamp NSA935807C09 Item 117 15 Install, refer to Fig. A-GBMAA Sheet 05, Detail J, AFTER: 2 Spacer NSA5527-03-01D Item (30) Retained at removal 2 Spacer NSA5527-03-02D Item (31) Retained at removal 2 Clamp NSA935807C16 Item (111) Retained at removal 2 Spacer NSA5527-03-05D Item (114) Retained at removal 2 Washer NSA1149D0332K Item (115) Retained at removal 2 Clamp NSA935807C09 Item (117) Retained at removal 2 Screw NAS1096-3-33 Item (118) Retained at removal 2 Clamp NSA935807C09 Item 117 16 Install, refer to Fig. A-GBMAA Sheet 04, Detail G, AFTER: 2 Spacer NSA5527-03-01D Item (30) Retained at removal 1 Spacer NSA5527-03-02D Item (31) Retained at removal DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 262 6

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# @A310 SERVICE BULLETIN
1 Clamp NSA935807C10 Item (110) Retained at removal 1 Clamp NSA935807C16 Item (111) Retained at removal 1 Washer NSA935808-01 Item (112) Retained at removal 1 Clamp NSA935807C09 Item (117) Retained at removal 1 Screw NAS1096-3-33 Item (118) Retained at removal 2 Clamp NSA935807C09 Item 117 17 Install, refer to Fig. A-GBMAA Sheet 03, Detail E, AFTER: 2 Spacer NSA5527-03-01D Item 30 1 Clamp NSA935807C16 Item (111) Retained at removal 1 Washer NSA935808-01 Item (112) Retained at removal 1 Screw NAS1096-3-23 Item (113) Retained at removal 1 Washer NSA1149D0332K Item (115) Retained at removal 1 Nut NAS1291C3M Item (116) Retained at removal 1 Clamp NSA935807C09 Item (117) Retained at removal 2 Clamp NSA935807C09 Item 117 18 Protect the electrical wires for 10QT-A and 10QT-B of route 2S/636VB, refer to the Hook-up Chart 2, Fig. A-GHBAA Sheet 01 and refer to Fig. A-GBMAA Sheet 02 and Sheet Fig. A-GBMAA Sheet 03 with: 2 Sleeve ABS0596S004 Item 1 cut the sleeve to the required length and install with: 20 Tie NSA935401-03 Item 149 20 Tie-Cable NSA935401-04 Item 150 DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 263 6

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# @A310 SERVICE BULLETIN
19 Install the identification placards, refer to Fig. A-GBMAA Sheet 02, 1 Placard set B9299071900200 Item 125 **CONF 006 (1) Subtask 282148-831-256-002 - Modification Manpower Resources Manhours 14.00 Minimum number of person 2 Subtask elapsed time 7.00 Skills ELECTRICAL Material necessary to do the job Kit 282148D03R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 ABS0596S004 SLEEVE 10 MS21919WCH9 1 CLAMP 31 NSA5527-03-02D 2 SPACER 109 NSA935805-09 CONDUIT 117 NSA935807C09 CLAMP 121 NAS1096-3-40 1 SCREW 123 NAS1801-3-31 SCREW 126 NSA938184PV1601 PIN 130 NSA5527-03-08D 1 SPACER 131 NSA5527-03-07D 1 SPACER 132 B9299071900600 EQUIPMNT 149 NSA935401-03 10 TIE 150 NSA935401-04 30 TIE References Elec. Std. Practices Manual (ESPM) 20-52-00 Fig. A-GBNAA Additional Work 1 (Introduced atRevision 02): Improvement of the 2SRoute in the RH-Wing Pylon Area (Kit D03) Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Sheet 08 Fig. A-GHBAA Hook-up Chart Sheet 01 ADDITIONAL WORK 1 is required by this revision for aircraft modified by issue 00 or Revision 01.

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 264 6

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# @A310 SERVICE BULLETIN (a) Installation of the cable sleeves in the RH-wing forward of the front spar between rib 11 and rib 12 in zone 623. Refer to Fig. A-GBNAA Sheet 01 , Fig. A-GBNAA Sheet 02, Fig. A-GBNAA Sheet 03, Fig. A-GBNAA Sheet 04, Fig. A-GBNAA Sheet 05, Fig. A-GBNAA Sheet 06, Fig. A-GBNAA Sheet 07 and Fig. A-GBNAA Sheet 08 Refer to Fig. A-GHBAA Sheet 01 1 At one position, remove these items from the bracket rib 11 and rib 12 and cable bundle 2S/636VB, as shown in Fig. A-GBNAA Sheet 01 and Sheet Fig. A-GBNAA Sheet 03 Details A and D: 2 Clamp MS21919WCH4 Item (22) Retain 1 Clamp MS21919WCH4 Item (22) Discard 1 Clamp MS21919WCH3 Item (23) Retain 1 Spacer NSA5527-03-01D Item (30) Retain 1 Spacer NSA5527-03-02D Item (31) Retain 2 Washer NSA935808-01 Item (112) Retain 2 Screw NAS1096-3-30 Item (121) Discard 1 Clamp NSA935807-06 Item (122) Retain 2 Install protection sleeve, as shown in Fig. A-GBNAA Sheet 01 thru Sheet Fig. A-GBNAA Sheet 03 Details A, B and C: 1 Sleeve ABS0596S004 Item 1 and attach the cable sleeves with: 10 Tie NSA935401-03 Item 149 or 10 Tie-Cable NSA935401-04 Item 150 3 Install, as shown in Fig. A-GBNAA Sheet 01 and Sheet Fig. A-GBNAA Sheet 03 Details A and E: 2 Clamp MS21919WCH4 Item (22) Retained at removal 1 Clamp MS21919WCH3 Item (23) Retained at removal 1 Spacer NSA5527-03-01D Item (30) Retained at removal DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 265 6

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# @A310 SERVICE BULLETIN
1 Spacer NSA5527-03-02D Item (31) Retained at removal 1 Washer NSA935808-01 Item (112) Retained at removal 1 Clamp NSA935807-06 Item (122) Retained at removal 1 Clamp MS21919WCH9 Item 10 1 Spacer NSA5527-03-02D Item 31 1 Screw NAS1096-3-40 Item 121 (b) Installation of the cable sleeves in the RH-wing forward of the front spar between rib 8 and rib 9 (pylon area) in zone 612. Refer to Fig. A-GBNAA Sheet 01 Refer to Fig. A-GHBAA Sheet 01 NOTE: If other wires are installed in the conduit of route 2S, disconnect them, change the conduits in accordance with this Service Bulletin, re-install the wires in the new conduit of route 2S and reconnect the wires. Do a test in accordance with ESPM 20-52-00. 1 Disconnect these wires of route 2S from the receptacles 40VC and 5006VC in accordance with the Hook-up Chart 2, Lines 2 thru 8, END 1, Fig. A-GHBAA Sheet 01

. 2 Remove, refer to Fig. A-GBNAA Sheet 03, Detail D, BEFORE: 1 Spacer NSA5527-03-02D Item (31) Retain 2 Clamp NSA935807C16 Item (111) Retain 1 Washer NSA935808-01 Item (112) Retain 1 Screw NAS1096-3-23 Item (113) Retain 1 Spacer NSA5527-03-05D Item (114) Retain 1 Nut NAS1291C3M Item (116) Retain 1 Washer AN960KD10l Item (124) Retain 3 Remove, refer to Fig. A-GBNAA Sheet 04, Detail F, BEFORE: 1 Spacer NSA5527-03-02D Item (31) Retain

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 266 6

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# @A310 SERVICE BULLETIN
2 Clamp NSA935807C16 Item (111) Retain 1 Washer NSA935808-01 Item (112) Retain 1 Screw NAS1096-3-23 Item (113) Retain 1 Spacer NSA5527-03-05D Item (114) Retain 4 Remove, refer to Fig. A-GBNAA Sheet 05, Detail H, BEFORE: 2 Spacer NSA5527-03-02D Item (31) Retain 4 Clamp NSA935807C16 Item (111) Retain 2 Washer NSA935808-01 Item (112) Retain 2 Screw NAS1096-3-23 Item (113) Retain 2 Spacer NSA5527-03-05D Item (114) Retain 5 Remove, refer to Fig. A-GBNAA Sheet 06, Detail K, BEFORE: 1 Spacer NSA5527-03-02D Item (31) Retain 2 Clamp NSA935807C16 Item (111) Retain 1 Washer NSA935808-01 Item (112) Retain 1 Screw NAS1096-3-23 Item (113) Discard 1 Clamp NSA5516-04NV Item (120) Retain 6 Remove, refer to Fig. A-GBNAA Sheet 07, Detail M, BEFORE: 1 Spacer NSA5527-03-02D Item (31) Retain 2 Clamp NSA935807C16 Item (111) Retain 1 Washer NSA935808-01 Item (112) Retain 1 Screw NAS1096-3-23 Item (113) Discard 1 Spacer NSA5527-03-05D Item (114) Retain 7 Remove, refer to Fig. A-GBNAA Sheet 08, Detail P, BEFORE: 1 Spacer NSA5527-03-02D Item (31) Retain 2 Clamp NSA935807C16 Item (111) Retain DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 267 6

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# @A310 SERVICE BULLETIN
1 Washer NSA935808-01 Item (112) Retain 1 Screw NAS1096-3-23 Item (113) Discard 1 Spacer NSA5527-03-05D Item (114) Retain 8 Remove the identification placards from the cable harnesses near the receptacles 40VC and 5006VC as shown Fig. A-GBNAA Sheet 02, Detail A As required placard Item (132) Discard
9 Remove the disconnected electrical wires from the protection sleeve. 10 Install to the electrical wires for 10QT-A and 10QT-B of route 2S/636VB, refer to the Hook-up Chart 2, Lines 2 thru 8, Fig. A-GHBAA Sheet 01 : 1 (ME) Conduit NSA935805-09 Item 109 11 Connect the electrical wires of route 2S to the receptacles 40VC and 5006VC in accordance with the Hook-up Chart 2, Lines 2 thru 8, END 1, Fig. AGHBAA Sheet 01 . Use the contact pins if required: 7 Pin NSA938184PV1601 Item 126 12 Install, refer to Fig. A-GBNAA Sheet 08, Detail Q, AFTER: 1 Spacer NSA5527-03-02D Item (31) Retained at removal 1 Spacer NSA5527-03-02D Item 31 2 Clamp NSA935807C16 Item (111) Retained at removal 1 Washer NSA935808-01 Item (112) Retained at removal 1 Spacer NSA5527-03-05D Item (114) Retained at removal 1 Clamp NSA935807C09 Item 117 1 Screw NAS1801-3-31 Item 123 1 Spacer NSA5527-03-07D Item 131 13 Install, refer to Fig. A-GBNAA Sheet 07, Detail N, AFTER: 1 Spacer NSA5527-03-02D Item (31) Retained at removal
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 268 6

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# @A310 SERVICE BULLETIN
2 Clamp NSA935807C16 Item (111) Retained at removal 1 Washer NSA935808-01 Item (112) Retained at removal 1 Spacer NSA5527-03-05D Item (114) Retained at removal 1 Clamp NSA935807C09 Item 117 1 Screw NAS1801-3-31 Item 123 1 Spacer NSA5527-03-08D Item 130 14 Install, refer to Fig. A-GBNAA Sheet 06, Detail L, AFTER: 2 Spacer NSA5527-03-02D Item (31) Retained at removal 2 Clamp NSA935807C16 Item (111) Retained at removal 1 Washer NSA935808-01 Item (112) Retained at removal 1 Clamp NSA5516-04NV Item (120) Retained at removal 1 Clamp NSA935807C09 Item 117 1 Screw NAS1801-3-31 Item 123 15 Install, refer to Fig. A-GBNAA Sheet 05, Detail J, AFTER: 2 Spacer NSA5527-03-02D Item (31) Retained at removal 4 Clamp NSA935807C16 Item (111) Retained at removal 2 Washer NSA935808-01 Item (112) Retained at removal 2 Screw NAS1096-3-23 Item (113) Retained at removal 2 Spacer NSA5527-03-05D Item (114) Retained at removal 2 Clamp NSA935807C09 Item 117
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 269 6

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# @A310 SERVICE BULLETIN
16 Install, refer to Fig. A-GBNAA Sheet 04, Detail G, AFTER: 1 Spacer NSA5527-03-02D Item (31) Retained at removal 2 Clamp NSA935807C16 Item (111) Retained at removal 1 Washer NSA935808-01 Item (112) Retained at removal 1 Screw NAS1096-3-23 Item (113) Retained at removal 1 Spacer NSA5527-03-05D Item (114) Retained at removal 1 Clamp NSA935807C09 Item 117 17 Install, refer to Fig. A-GBNAA Sheet 03, Detail E, AFTER: 1 Spacer NSA5527-03-02D Item (31) Retained at removal 2 Clamp NSA935807C16 Item (111) Retained at removal 1 Washer NSA935808-01 Item (112) Retained at removal 1 Screw NAS1096-3-23 Item (113) Retained at removal 1 Spacer NSA5527-03-05D Item (114) Retained at removal 1 Nut NAS1291C3M Item (116) Retained at removal 1 Washer AN960KD10l Item (124) Retained at removal 1 Clamp NSA935807C09 Item 117 18 Protect the electrical wires for 10QT-A and 10QT-B of route 2S/636VB, refer to the Hook-up Chart 2, Fig. A-GHBAA Sheet 01 with: 3 Sleeve ABS0596S004 Item 1 and 20 Tie NSA935401-03 Item 149
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 270 6

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# @A310 SERVICE BULLETIN

or 20 Tie-Cable NSA935401-04 Item 150 19 Install the identification placards, refer to Fig. A-GBNAA Sheet 02 1 Placard Set B9299071900600 Item 132 **CONF 007 None **CONF 008 None **CONF ALL D. TEST **CONF 001 (1) Subtask 282148-700-202-001 - Testing Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 27-84-00, Page Block 501 28-42-44, Page Block 401 30-11-00, Page Block 501 36-11-00, Page Block 501 Elec. Std. Practices Manual (ESPM) 20-52-21 ADDITIONAL WORK 1 is required by this revision for aircraft modified by issue 00 or Revision 01. (a) Do a continuity test of disconnected wires (Refer to ESPM 20-52-21). (b) Do an operational test of the cadensicon sensor (Refer to AMM 28-42-44, Page Block 401). (c) Do the operational test (Refer to AMM 27-84-00, Page Block 501). (d) Do the operational test of the wing ice protection (Refer to AMM 30-11-00, Page Block 501). (e) Do the bite test (Refer to AMM 36-11-00, Page Block 501).

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 271 6

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# @A310 SERVICE BULLETIN
**CONF 002 (1) Subtask 282148-700-202-001 - Testing Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 27-84-00, Page Block 501 28-42-44, Page Block 401 30-11-00, Page Block 501 36-11-00, Page Block 501 Elec. Std. Practices Manual (ESPM) 20-52-21 ADDITIONAL WORK 1 is required by this revision for aircraft modified by issue 00 or Revision 01. (a) Do a continuity test of disconnected wires (Refer to ESPM 20-52-21). (b) Do an operational test of the cadensicon sensor (Refer to AMM 28-42-44, Page Block 401). (c) Do the operational test (Refer to AMM 27-84-00, Page Block 501). (d) Do the operational test of the wing ice protection (Refer to AMM 30-11-00, Page Block 501). (e) Do the bite test (Refer to AMM 36-11-00, Page Block 501). **CONF 003 None **CONF 004 None **CONF 005 (1) Subtask 282148-700-202-001 - Testing Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 27-84-00, Page Block 501 28-42-44, Page Block 401 30-11-00, Page Block 501 36-11-00, Page Block 501 Elec. Std. Practices Manual (ESPM) 20-52-21

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 272 6

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# @A310 SERVICE BULLETIN ADDITIONAL WORK 1 is required by this revision for aircraft modified by issue 00 or Revision 01. (a) Do a continuity test of disconnected wires (Refer to ESPM 20-52-21). (b) Do an operational test of the cadensicon sensor (Refer to AMM 28-42-44, Page Block 401). (c) Do the operational test (Refer to AMM 27-84-00, Page Block 501). (d) Do the operational test of the wing ice protection (Refer to AMM 30-11-00, Page Block 501). (e) Do the bite test (Refer to AMM 36-11-00, Page Block 501). **CONF 006 (1) Subtask 282148-700-202-001 - Testing Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 27-84-00, Page Block 501 28-42-44, Page Block 401 30-11-00, Page Block 501 36-11-00, Page Block 501 Elec. Std. Practices Manual (ESPM) 20-52-21 ADDITIONAL WORK 1 is required by this revision for aircraft modified by issue 00 or Revision 01. (a) Do a continuity test of disconnected wires (Refer to ESPM 20-52-21). (b) Do an operational test of the cadensicon sensor (Refer to AMM 28-42-44, Page Block 401). (c) Do the operational test (Refer to AMM 27-84-00, Page Block 501). (d) Do the operational test of the wing ice protection (Refer to AMM 30-11-00, Page Block 501). (e) Do the bite test (Refer to AMM 36-11-00, Page Block 501). **CONF 007 None **CONF 008 None

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 273 6

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# @A310 SERVICE BULLETIN
**CONF ALL E. CLOSE-UP **CONF 001 (1) Subtask 282148-942-204-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 27-28-00, Page Block 301 ADDITIONAL WORK 1 is required by this revision for aircraft modified by issue 00 or Revision 01. Close up (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Fully retract the slats (Refer to AMM 27-28-00, Page Block 301). (c) Close the access panels 612AT, 612KB, 612JB, 623AB, 623BB and 623EB. (d) Remove the access platform. **CONF 002 (1) Subtask 282148-942-204-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 27-28-00, Page Block 301 ADDITIONAL WORK 1 is required by this revision for aircraft modified by issue 00 or Revision 01. Close up (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Fully retract the slats (Refer to AMM 27-28-00, Page Block 301). (c) Close the access panels 612AT, 612KB, 612JB, 623AB, 623BB and 623EB. (d) Remove the access platform.

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 274 6

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# @A310 SERVICE BULLETIN
**CONF 003 None **CONF 004 None **CONF 005 (1) Subtask 282148-942-204-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 27-28-00, Page Block 301 ADDITIONAL WORK 1 is required by this revision for aircraft modified by issue 00 or Revision 01. Close up (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Fully retract the slats (Refer to AMM 27-28-00, Page Block 301). (c) Close the access panels 612AT, 612KB, 612JB, 623AB, 623BB and 623EB. (d) Remove the access platform. **CONF 006 (1) Subtask 282148-942-204-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 27-28-00, Page Block 301 ADDITIONAL WORK 1 is required by this revision for aircraft modified by issue 00 or Revision 01. Close up (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Fully retract the slats (Refer to AMM 27-28-00, Page Block 301). (c) Close the access panels 612AT, 612KB, 612JB, 623AB, 623BB and 623EB. DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 275 6

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# @A310 SERVICE BULLETIN (d) Remove the access platform. **CONF 007 None **CONF 008 None

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 276 6

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# @A310 SERVICE BULLETIN
Task 282148-831-849-001 - Modification - ADDITIONAL WORK 2 (Introduced at Rev 03) **CONF ALL WARNING: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND CAUTIONS INCLUDED IN THE REFERENCED PROCEDURES. WARNING: THIS PROCEDURE USES A FUEL SYSTEM ITEM THAT IS IN A CATEGORY KNOWN AS A CRITICAL DESIGN CONFIGURATION CONTROL LIMITATION (CDCCL) CDCCL IDENTIFIES AN ITEM THAT CAN BE THE SOURCE OF A POSSIBLE FUEL TANK IGNITION. YOU MUST KEEP ALL CDCCL ITEMS IN THE APPROVED CONFIGURATION. DAMAGE, WEAR OR CHANGES TO A CDCCL ITEM CAN CAUSE A POSSIBLE FUEL TANK EXPLOSION. 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. Task Associated Data **CONF 001 Zone 612 623 Access Panel 612AT 623AB Manpower TOTAL MANHOURS 3.00 ELAPSED TIME (HOURS) 3.00 **CONF 002 Zone 612 623 Access Panel 612AT 623AB

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 277 6

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# @A310 SERVICE BULLETIN
Manpower TOTAL MANHOURS 3.00 ELAPSED TIME (HOURS) 3.00 **CONF 003 Manpower TOTAL MANHOURS 0.00 ELAPSED TIME (HOURS) 0.00 **CONF 004 Manpower TOTAL MANHOURS 0.00 ELAPSED TIME (HOURS) 0.00 **CONF 005 Zone 612 623 Access Panel 612AT 623AB Manpower TOTAL MANHOURS 3.00 ELAPSED TIME (HOURS) 3.00 **CONF 006 Zone 612 623 Access Panel 612AT 623AB Manpower TOTAL MANHOURS 3.00 ELAPSED TIME (HOURS) 3.00 **CONF 007 Manpower TOTAL MANHOURS 0.00 ELAPSED TIME (HOURS) 0.00 **CONF 008 Manpower TOTAL MANHOURS 0.00 ELAPSED TIME (HOURS) 0.00

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 278 6

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# @A310 SERVICE BULLETIN
**CONF ALL A. GENERAL **CONF 001 (1) Subtask 282148-839-401-001 - Administrative Manpower Resources Skills UTILITY Write in the applicable aircraft records that you have done all the work given in the Service Bulletin. (2) Subtask 282148-910-206-001 - Standard Practices Manpower Resources Skills NON SPECIFIC References Elec. Std. Practices Manual (ESPM) 20-25-21 (a) Do a continuity test of disconnected wires (Refer to ESPM 20-25-21). **CONF 002 (1) Subtask 282148-839-401-001 - Administrative Manpower Resources Skills UTILITY Write in the applicable aircraft records that you have done all the work given in the Service Bulletin. (2) Subtask 282148-910-206-001 - Standard Practices Manpower Resources Skills NON SPECIFIC References Elec. Std. Practices Manual (ESPM) 20-25-21 (a) Do a continuity test of disconnected wires (Refer to ESPM 20-25-21). **CONF 003 (1) Subtask 282148-839-401-001 - Administrative Manpower Resources Skills UTILITY Write in the applicable aircraft records that you have done all the work given in the Service Bulletin. DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 279 6

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# @A310 SERVICE BULLETIN
**CONF 004 (1) Subtask 282148-839-401-001 - Administrative Manpower Resources Skills UTILITY Write in the applicable aircraft records that you have done all the work given in the Service Bulletin. **CONF 005 (1) Subtask 282148-839-401-001 - Administrative Manpower Resources Skills UTILITY Write in the applicable aircraft records that you have done all the work given in the Service Bulletin. (2) Subtask 282148-910-206-001 - Standard Practices Manpower Resources Skills NON SPECIFIC References Elec. Std. Practices Manual (ESPM) 20-25-21 (a) Do a continuity test of disconnected wires (Refer to ESPM 20-25-21). **CONF 006 (1) Subtask 282148-839-401-001 - Administrative Manpower Resources Skills UTILITY Write in the applicable aircraft records that you have done all the work given in the Service Bulletin. (2) Subtask 282148-910-206-001 - Standard Practices Manpower Resources Skills NON SPECIFIC References Elec. Std. Practices Manual (ESPM) 20-25-21 (a) Do a continuity test of disconnected wires (Refer to ESPM 20-25-21).

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 280 6

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# @A310 SERVICE BULLETIN
**CONF 007 (1) Subtask 282148-839-401-001 - Administrative Manpower Resources Skills UTILITY Write in the applicable aircraft records that you have done all the work given in the Service Bulletin. **CONF 008 (1) Subtask 282148-839-401-001 - Administrative Manpower Resources Skills UTILITY Write in the applicable aircraft records that you have done all the work given in the Service Bulletin. **CONF ALL B. PREPARATION **CONF 001 (1) Subtask 282148-941-402-001 - Job Set-up Work Zones and Access Panels Zone Access/Work location 612 Access Panel 612AT 623 Access Panel 623AB Manpower Resources Skills AIRFRAME References Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001 24-00-00, Page Block 301 24-41-00, Page Block 301 (a) Make sure that the aircraft is electrically grounded (Refer to AMM 24-00-00, Page Block 301). (b) De-energize the aircraft electrical circuits (Refer to AMM 24-41-00, Page Block 301). (c) Put access platforms in position. (d) Remove access panel(s) 612AT and/or 623AB (RH wing) (Refer to AMM 06-41-57, Page Block 001).

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 281 6

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# @A310 SERVICE BULLETIN
**CONF 002 (1) Subtask 282148-941-402-001 - Job Set-up Work Zones and Access Panels Zone Access/Work location 612 Access Panel 612AT 623 Access Panel 623AB Manpower Resources Skills AIRFRAME References Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001 24-00-00, Page Block 301 24-41-00, Page Block 301 (a) Make sure that the aircraft is electrically grounded (Refer to AMM 24-00-00, Page Block 301). (b) De-energize the aircraft electrical circuits (Refer to AMM 24-41-00, Page Block 301). (c) Put access platforms in position. (d) Remove access panel(s) 612AT and/or 623AB (RH wing) (Refer to AMM 06-41-57, Page Block 001). **CONF 003 None **CONF 004 None **CONF 005 (1) Subtask 282148-941-402-001 - Job Set-up Work Zones and Access Panels Zone Access/Work location 612 Access Panel 612AT 623 Access Panel 623AB Manpower Resources Skills AIRFRAME

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 282 6

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# @A310 SERVICE BULLETIN

References Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001 24-00-00, Page Block 301 24-41-00, Page Block 301 (a) Make sure that the aircraft is electrically grounded (Refer to AMM 24-00-00, Page Block 301). (b) De-energize the aircraft electrical circuits (Refer to AMM 24-41-00, Page Block 301). (c) Put access platforms in position. (d) Remove access panel(s) 612AT and/or 623AB (RH wing) (Refer to AMM 06-41-57, Page Block 001). **CONF 006 (1) Subtask 282148-941-402-001 - Job Set-up Work Zones and Access Panels Zone Access/Work location 612 Access Panel 612AT 623 Access Panel 623AB Manpower Resources Skills AIRFRAME References Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001 24-00-00, Page Block 301 24-41-00, Page Block 301 (a) Make sure that the aircraft is electrically grounded (Refer to AMM 24-00-00, Page Block 301). (b) De-energize the aircraft electrical circuits (Refer to AMM 24-41-00, Page Block 301). (c) Put access platforms in position. (d) Remove access panel(s) 612AT and/or 623AB (RH wing) (Refer to AMM 06-41-57, Page Block 001). **CONF 007 None **CONF 008 None

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 283 6

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# @A310 SERVICE BULLETIN
**CONF ALL C. PROCEDURE **CONF 001 (1) Subtask 282148-831-402-001 - Introduce a New Bracket on the Sub Spar Behind the Front Spar Between RIB 8 and RIB 9 on the RH Wing Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills AIRFRAME Material necessary to do the job Kit 282148B01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 A5725068600000 1 Bracket 2 ASNA0078A502 2 Rivet Consumable CMLB01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Corrosion Inhibiting Low Adhesion Sealant 09-018 As required Solvent General Purpose 11-026 As required Lint-Free Cotton Cloth 19-003 As required References Fig. A-UBCAA Additional Work 2 (Introduced at Revision 03)- Location of Bracket on the Sub Spar Behind the Front Spar Between RIB 8 and RIB 9 (RH Wing) Sheet 01

Refer to Fig. A-UBCAA Sheet 01 (a) Remove from the sub spar behind the front spar between RIB 8 and RIB 9 on the RH wing, the items that follow: 2 Rivet NSA54213510DCA Item (2) Discard 1 Bracket A5724630400000 Item (1) Discard

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 284 6

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# @A310 SERVICE BULLETIN (b) Clean the mating surfaces use Lint-Free Cotton Cloth 19-003 As required

made moist with Solvent General Purpose 11-026 As required (c) Put the 1 Bracket A5725068600000 Item 1 in position on the sub spar behind the front spar between RIB 8 and RIB 9 on the RH wing (Refer to Fig. A-UBCAA Sheet 01 ). (d) Copy drill the two holes from the sub spar through the Bracket, Item 1 to a dimension of between 4.060 and 4.160 mm (0.160 and 0.164 in.). (e) Deburr the holes that have been worked. (f) Use Corrosion Inhibiting Low Adhesion Sealant 09-018 As required

and wet install the 1 Bracket A5725068600000 Item 1 with the 2 Rivet, Blind ASNA0078A502 Item 2 on the sub spar behind the front spar between RIB 8 and RIB 9 on the RH wing. **CONF 002 (1) Subtask 282148-831-402-001 - Introduce a New Bracket on the Sub Spar Behind the Front Spar Between RIB 8 and RIB 9 on the RH Wing Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills AIRFRAME

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 285 6

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# @A310 SERVICE BULLETIN
Material necessary to do the job Kit 282148B01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 A5725068600000 1 Bracket 2 ASNA0078A502 2 Rivet Consumable CMLB01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Corrosion Inhibiting Low Adhesion Sealant 09-018 As required Solvent General Purpose 11-026 As required Lint-Free Cotton Cloth 19-003 As required References Fig. A-UBCAA Additional Work 2 (Introduced at Revision 03)- Location of Bracket on the Sub Spar Behind the Front Spar Between RIB 8 and RIB 9 (RH Wing) Sheet 01

Refer to Fig. A-UBCAA Sheet 01 (a) Remove from the sub spar behind the front spar between RIB 8 and RIB 9 on the RH wing, the items that follow: 2 Rivet NSA54213510DCA Item (2) Discard 1 Bracket A5724630400000 Item (1) Discard (b) Clean the mating surfaces use Lint-Free Cotton Cloth 19-003 As required

made moist with Solvent General Purpose 11-026 As required (c) Put the 1 Bracket A5725068600000 Item 1 in position on the sub spar behind the front spar between RIB 8 and RIB 9 on the RH wing (Refer to Fig. A-UBCAA Sheet 01 ). (d) Copy drill the two holes from the sub spar through the Bracket, Item 1 to a dimension of between 4.060 and 4.160 mm (0.160 and 0.164 in.).
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 286 6

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# @A310 SERVICE BULLETIN (e) Deburr the holes that have been worked. (f) Use Corrosion Inhibiting Low Adhesion Sealant 09-018 As required

and wet install the 1 Bracket A5725068600000 Item 1 with the 2 Rivet, Blind ASNA0078A502 Item 2 on the sub spar behind the front spar between RIB 8 and RIB 9 on the RH wing. **CONF 003 None **CONF 004 None **CONF 005 (1) Subtask 282148-831-402-001 - Introduce a New Bracket on the Sub Spar Behind the Front Spar Between RIB 8 and RIB 9 on the RH Wing Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills AIRFRAME Material necessary to do the job Kit 282148B01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 A5725068600000 1 Bracket 2 ASNA0078A502 2 Rivet Consumable CMLB01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Corrosion Inhibiting Low Adhesion Sealant 09-018 As required Solvent General Purpose 11-026 As required Lint-Free Cotton Cloth 19-003 As required DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 287 6

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# @A310 SERVICE BULLETIN

References Fig. A-UBCAA Additional Work 2 (Introduced at Revision 03)- Location of Bracket on the Sub Spar Behind the Front Spar Between RIB 8 and RIB 9 (RH Wing) Sheet 01

Refer to Fig. A-UBCAA Sheet 01 (a) Remove from the sub spar behind the front spar between RIB 8 and RIB 9 on the RH wing, the items that follow: 2 Rivet NSA54213510DCA Item (2) Discard 1 Bracket A5724630400000 Item (1) Discard (b) Clean the mating surfaces use Lint-Free Cotton Cloth 19-003 As required

made moist with Solvent General Purpose 11-026 As required (c) Put the 1 Bracket A5725068600000 Item 1 in position on the sub spar behind the front spar between RIB 8 and RIB 9 on the RH wing (Refer to Fig. A-UBCAA Sheet 01 ). (d) Copy drill the two holes from the sub spar through the Bracket, Item 1 to a dimension of between 4.060 and 4.160 mm (0.160 and 0.164 in.). (e) Deburr the holes that have been worked. (f) Use Corrosion Inhibiting Low Adhesion Sealant 09-018 As required

and wet install the 1 Bracket A5725068600000 Item 1 with the 2 Rivet, Blind ASNA0078A502 Item 2 on the sub spar behind the front spar between RIB 8 and RIB 9 on the RH wing.

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 288 6

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# @A310 SERVICE BULLETIN
**CONF 006 (1) Subtask 282148-831-402-001 - Introduce a New Bracket on the Sub Spar Behind the Front Spar Between RIB 8 and RIB 9 on the RH Wing Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills AIRFRAME Material necessary to do the job Kit 282148B01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 A5725068600000 1 Bracket 2 ASNA0078A502 2 Rivet Consumable CMLB01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Corrosion Inhibiting Low Adhesion Sealant 09-018 As required Solvent General Purpose 11-026 As required Lint-Free Cotton Cloth 19-003 As required References Fig. A-UBCAA Additional Work 2 (Introduced at Revision 03)- Location of Bracket on the Sub Spar Behind the Front Spar Between RIB 8 and RIB 9 (RH Wing) Sheet 01

Refer to Fig. A-UBCAA Sheet 01 (a) Remove from the sub spar behind the front spar between RIB 8 and RIB 9 on the RH wing, the items that follow: 2 Rivet NSA54213510DCA Item (2) Discard 1 Bracket A5724630400000 Item (1) Discard (b) Clean the mating surfaces use Lint-Free Cotton Cloth 19-003 As required

made moist with

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 289 6

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# @A310 SERVICE BULLETIN

Solvent General Purpose 11-026 As required (c) Put the 1 Bracket A5725068600000 Item 1 in position on the sub spar behind the front spar between RIB 8 and RIB 9 on the RH wing (Refer to Fig. A-UBCAA Sheet 01 ). (d) Copy drill the two holes from the sub spar through the Bracket, Item 1 to a dimension of between 4.060 and 4.160 mm (0.160 and 0.164 in.). (e) Deburr the holes that have been worked. (f) Use Corrosion Inhibiting Low Adhesion Sealant 09-018 As required

and wet install the 1 Bracket A5725068600000 Item 1 with the 2 Rivet, Blind ASNA0078A502 Item 2 on the sub spar behind the front spar between RIB 8 and RIB 9 on the RH wing. **CONF 007 None **CONF 008 None **CONF ALL D. TEST **CONF 001 None **CONF 002 None **CONF 003 None
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 290 6

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# @A310 SERVICE BULLETIN
**CONF 004 None **CONF 005 None **CONF 006 None **CONF 007 None **CONF 008 None **CONF ALL E. CLOSE-UP **CONF 001 (1) Subtask 282148-942-402-001 - Close-up Work Zones and Access Panels Zone Access/Work location 612 Access Panel 612AT 623 Access Panel 623AB Manpower Resources Skills AIRFRAME References Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Install access panel(s) 612AT and/or 623AB (RH wing) (Refer to AMM 06-41-57, Page Block 001). **CONF 002 (1) Subtask 282148-942-402-001 - Close-up Work Zones and Access Panels Zone Access/Work location 612 Access Panel 612AT
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 291 6

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# @A310 SERVICE BULLETIN

623 Access Panel 623AB Manpower Resources Skills AIRFRAME References Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Install access panel(s) 612AT and/or 623AB (RH wing) (Refer to AMM 06-41-57, Page Block 001). **CONF 003 None **CONF 004 None **CONF 005 (1) Subtask 282148-942-402-001 - Close-up Work Zones and Access Panels Zone Access/Work location 612 Access Panel 612AT 623 Access Panel 623AB Manpower Resources Skills AIRFRAME References Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Install access panel(s) 612AT and/or 623AB (RH wing) (Refer to AMM 06-41-57, Page Block 001). **CONF 006 (1) Subtask 282148-942-402-001 - Close-up Work Zones and Access Panels Zone Access/Work location 612 Access Panel 612AT 623 Access Panel 623AB
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 292 6

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# @A310 SERVICE BULLETIN
Manpower Resources Skills AIRFRAME References Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Install access panel(s) 612AT and/or 623AB (RH wing) (Refer to AMM 06-41-57, Page Block 001). **CONF 007 None **CONF 008 None

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 293 6

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# @A310 SERVICE BULLETIN

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DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 294 6

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# @A310 SERVICE BULLETIN
Task 282148-831-850-001 - Modification - ADDITIONAL WORK 3 (Introduced at Rev 06) **CONF ALL WARNING: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONS INCLUDED IN THE REFERENCED PROCEDURES. WARNING: THIS PROCEDURE USES A FUEL SYSTEM ITEM THAT IS IN A CATEGORY KNOWN AS A CRITICAL DESIGN CONFIGURATION CONTROL LIMITATION (CDCCL) CDCCL IDENTIFIES AN ITEM THAT CAN BE THE SOURCE OF A POSSIBLE FUEL TANK IGNITION. YOU MUST KEEP ALL CDCCL ITEMS IN THE APPROVED CONFIGURATION. DAMAGE, WEAR OR CHANGES TO A CDCCL ITEM CAN CAUSE A POSSIBLE FUEL TANK EXPLOSION. 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. Task Associated Data **CONF 001 Manpower TOTAL MANHOURS 0.00 ELAPSED TIME (HOURS) 0.00 **CONF 002 Manpower TOTAL MANHOURS 0.00 ELAPSED TIME (HOURS) 0.00 **CONF 003 Manpower TOTAL MANHOURS 3.00 ELAPSED TIME (HOURS) 3.00
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 295 6

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# @A310 SERVICE BULLETIN
**CONF 004 Manpower TOTAL MANHOURS 3.00 ELAPSED TIME (HOURS) 3.00 **CONF 005 Manpower TOTAL MANHOURS 0.00 ELAPSED TIME (HOURS) 0.00 **CONF 006 Manpower TOTAL MANHOURS 0.00 ELAPSED TIME (HOURS) 0.00 **CONF 007 Manpower TOTAL MANHOURS 3.00 ELAPSED TIME (HOURS) 3.00 **CONF 008 Manpower TOTAL MANHOURS 3.00 ELAPSED TIME (HOURS) 3.00 **CONF ALL A. GENERAL **CONF 001 None **CONF 002 None **CONF 003 (1) Subtask 282148-910-203-001 - Standard Practices Manpower Resources Skills NON SPECIFIC

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 296 6

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# @A310 SERVICE BULLETIN
Material necessary to do the job Consumable CMLD01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Storage compound 15-008A As required References Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001 Consumable Material List (CML) Elec. Std. Practices Manual (ESPM) 20-25-21 20-33-00 Standards Manual (SM) Structural Repair Manual (SRM) 51-23-11 51-42-11 (a) Refer to the AIRBUS (Refer to Standards Manual (SM)) if you find part numbers for the hardware components in the related kit(s) which you can not identify in the LIST OF COMPONENTS of this Service Bulletin. The SM will give you the correct part number to part number relationship. (b) For material specification (Mat. No.) given in this Service Bulletin (Refer to Consumable Material List (CML)). (c) For panel location (Refer to AMM 06-41-53, Page Block 001). (d) Obey the instructions for the wiring installation (Refer to ESPM 20-33-00). (e) Apply Storage compound 15-008A As required to the screws after assembly. (f) Installation of fasteners (Refer to SRM 51-42-11). (g) For paint coatings (Refer to SRM 51-23-11). (h) Do a continuity test of disconnected wires (Refer to ESPM 20-25-21). (2) Subtask 282148-839-201-001 - Documentation Manpower Resources Skills NON SPECIFIC Write in the applicable aircraft records that you have done all the work given in this Service Bulletin.

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 297 6

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# @A310 SERVICE BULLETIN
**CONF 004 (1) Subtask 282148-910-203-001 - Standard Practices Manpower Resources Skills NON SPECIFIC Material necessary to do the job Consumable CMLD01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Storage compound 15-008A As required References Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001 Consumable Material List (CML) Elec. Std. Practices Manual (ESPM) 20-25-21 20-33-00 Standards Manual (SM) Structural Repair Manual (SRM) 51-23-11 51-42-11 (a) Refer to the AIRBUS (Refer to Standards Manual (SM)) if you find part numbers for the hardware components in the related kit(s) which you can not identify in the LIST OF COMPONENTS of this Service Bulletin. The SM will give you the correct part number to part number relationship. (b) For material specification (Mat. No.) given in this Service Bulletin (Refer to Consumable Material List (CML)). (c) For panel location (Refer to AMM 06-41-53, Page Block 001). (d) Obey the instructions for the wiring installation (Refer to ESPM 20-33-00). (e) Apply Storage compound 15-008A As required to the screws after assembly. (f) Installation of fasteners (Refer to SRM 51-42-11). (g) For paint coatings (Refer to SRM 51-23-11). (h) Do a continuity test of disconnected wires (Refer to ESPM 20-25-21). (2) Subtask 282148-839-201-001 - Documentation Manpower Resources Skills NON SPECIFIC
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 298 6

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# @A310 SERVICE BULLETIN Write in the applicable aircraft records that you have done all the work given in this Service Bulletin. **CONF 005 None **CONF 006 None **CONF 007 (1) Subtask 282148-910-203-001 - Standard Practices Manpower Resources Skills NON SPECIFIC Material necessary to do the job Consumable CMLD01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Storage compound 15-008A As required References Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001 Consumable Material List (CML) Elec. Std. Practices Manual (ESPM) 20-25-21 20-33-00 Standards Manual (SM) Structural Repair Manual (SRM) 51-23-11 51-42-11 (a) Refer to the AIRBUS (Refer to Standards Manual (SM)) if you find part numbers for the hardware components in the related kit(s) which you can not identify in the LIST OF COMPONENTS of this Service Bulletin. The SM will give you the correct part number to part number relationship. (b) For material specification (Mat. No.) given in this Service Bulletin (Refer to Consumable Material List (CML)). (c) For panel location (Refer to AMM 06-41-53, Page Block 001). (d) Obey the instructions for the wiring installation (Refer to ESPM 20-33-00). (e) Apply Storage compound 15-008A As required to the screws after assembly.
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 299 6

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# @A310 SERVICE BULLETIN (f) Installation of fasteners (Refer to SRM 51-42-11). (g) For paint coatings (Refer to SRM 51-23-11). (h) Do a continuity test of disconnected wires (Refer to ESPM 20-25-21). (2) Subtask 282148-839-201-001 - Documentation Manpower Resources Skills NON SPECIFIC Write in the applicable aircraft records that you have done all the work given in this Service Bulletin. **CONF 008 (1) Subtask 282148-910-203-001 - Standard Practices Manpower Resources Skills NON SPECIFIC Material necessary to do the job Consumable CMLD01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Storage compound 15-008A As required References Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001 Consumable Material List (CML) Elec. Std. Practices Manual (ESPM) 20-25-21 20-33-00 Standards Manual (SM) Structural Repair Manual (SRM) 51-23-11 51-42-11 (a) Refer to the AIRBUS (Refer to Standards Manual (SM)) if you find part numbers for the hardware components in the related kit(s) which you can not identify in the LIST OF COMPONENTS of this Service Bulletin. The SM will give you the correct part number to part number relationship. (b) For material specification (Mat. No.) given in this Service Bulletin (Refer to Consumable Material List (CML)). (c) For panel location (Refer to AMM 06-41-53, Page Block 001). (d) Obey the instructions for the wiring installation (Refer to ESPM 20-33-00).

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 300 6

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# @A310 SERVICE BULLETIN (e) Apply Storage compound 15-008A As required to the screws after assembly. (f) Installation of fasteners (Refer to SRM 51-42-11). (g) For paint coatings (Refer to SRM 51-23-11). (h) Do a continuity test of disconnected wires (Refer to ESPM 20-25-21). (2) Subtask 282148-839-201-001 - Documentation Manpower Resources Skills NON SPECIFIC Write in the applicable aircraft records that you have done all the work given in this Service Bulletin. **CONF ALL B. PREPARATION **CONF 001 None **CONF 002 None **CONF 003 (1) Subtask 282148-941-203-001 - 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 24-41-00, Page Block 301 (a) Make sure that the aircraft is electrically grounded (Refer to AMM 24-00-00, Page Block 301). (b) De-energise the aircraft electrical circuits (Refer to AMM 24-41-00, Page Block 301). (c) Put access platforms in position.

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 301 6

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# @A310 SERVICE BULLETIN (d) Remove access panels 612AT and/or 623AB (RH wing) (Refer to AMM 06-41-57, Page Block 001). **CONF 004 (1) Subtask 282148-941-203-001 - 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 24-41-00, Page Block 301 (a) Make sure that the aircraft is electrically grounded (Refer to AMM 24-00-00, Page Block 301). (b) De-energise the aircraft electrical circuits (Refer to AMM 24-41-00, Page Block 301). (c) Put access platforms in position. (d) Remove access panels 612AT and/or 623AB (RH wing) (Refer to AMM 06-41-57, Page Block 001). **CONF 005 None **CONF 006 None **CONF 007 (1) Subtask 282148-941-203-001 - 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 24-41-00, Page Block 301 (a) Make sure that the aircraft is electrically grounded (Refer to AMM 24-00-00, Page Block 301). (b) De-energise the aircraft electrical circuits (Refer to AMM 24-41-00, Page Block 301). (c) Put access platforms in position. DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 302 6

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# @A310 SERVICE BULLETIN (d) Remove access panels 612AT and/or 623AB (RH wing) (Refer to AMM 06-41-57, Page Block 001). **CONF 008 (1) Subtask 282148-941-203-001 - 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 24-41-00, Page Block 301 (a) Make sure that the aircraft is electrically grounded (Refer to AMM 24-00-00, Page Block 301). (b) De-energise the aircraft electrical circuits (Refer to AMM 24-41-00, Page Block 301). (c) Put access platforms in position. (d) Remove access panels 612AT and/or 623AB (RH wing) (Refer to AMM 06-41-57, Page Block 001). **CONF ALL C. PROCEDURE **CONF 001 None **CONF 002 None **CONF 003 (1) Subtask 282148-831-253-001 - Modification Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills ELECTRICAL

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 303 6

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# @A310 SERVICE BULLETIN
Material necessary to do the job Kit 282148D02R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 126 NSA938184PV1601 15 PIN Kit 282148D07R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 31 NSA5527-03-02D 2 SPACER 110 NSA935807C10 1 CLAMP 112 NAS1149D0332K 1 WASHER 117 NSA935807C09 3 CLAMP 120 NSA5516-04NV 1 CLAMP 130 NSA5527-03-08D 1 SPACER 135 NAS1096-3-42 1 SCREW References Fig. A-GBPAB Additional Work 3 - Improvement of the 2S-Route in the RH-Wing Pylon Area Sheet 01 Fig. A-GHAAA Hook-up Chart Sheet 01 Fig. A-GHBAA Hook-up Chart Sheet 01 (a) Disconnect these wires of route 2S from the receptacles 40VC and 5006VC in accordance with the Hook-up Chart 1, Lines 1 thru 14, END 1, Fig. A-GHAAA Sheet 01 and the Hook-up Chart 2, Lines 2 thru 8, END 1, Fig. A-GHBAA Sheet 01

. (b) Remove, refer to Fig. A-GBPAB Sheet 01 1 Spacer NSA5527-03-05D Item (114) Discard 3 Clamp NSA935807C09 Item (117) Discard 1 Spacer NSA5527-03-02D Item (31) Discard 1 Clamp NSA5516-04NV Item (120) Discard 1 Screw NAS1096-3-28 Item (151) Discard 1 Clamp NSA935807C10 Item (110) Discard 1 Spacer Item (152) Discard

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 304 6

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# @A310 SERVICE BULLETIN (c) Install, refer to Fig. A-GBPAB Sheet 01 1 Screw NAS1096-3-42 Item 135 1 Washer NAS1149D0332K Item 112 1 Clamp NSA5516-04NV Item 120 2 Spacer NSA5527-03-02D Item 31 1 Spacer NSA5527-03-08D Item 130 3 Clamp NSA935807C09 Item 117 1 Clamp NSA935807C10 Item 110 (d) Connect the electrical wires of route 2S to the receptacles 40VC and 5006VC in accordance with the Hook-up Chart 1, Lines 1 thru 14, END 1, Fig. A-GHAAA Sheet 01 and the Hook-up Chart 2, lines 2 thru 8, END 1, Fig. A-GHBAA Sheet 01

. Use the contact pins if required: 15 Pin NSA938184PV1601 Item 126 **CONF 004 (1) Subtask 282148-831-253-003 - Modification Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills ELECTRICAL Material necessary to do the job Kit 282148D02R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 126 NSA938184PV1601 15 PIN Kit 282148D08R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 30 NSA5527-03-01D 1 SPACER 31 NSA5527-03-02D 1 SPACER 111 NSA935807C16 2 CLAMP 112 NSA935808-01 1 WASHER 117 NSA935807C09 1 CLAMP 120 NSA5516-04NV 1 CLAMP 123 NAS1801-3-31 1 SCREW DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 305 6

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# @A310 SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 130 NSA5527-03-08D 1 SPACER References Fig. A-GBPAA Additional Work 3 - Improvement of the 2S-Route in the RH-Wing Pylon Area Sheet 01 Fig. A-GHBAA Hook-up Chart Sheet 01 (a) Disconnect these wires of route 2S from the receptacles 40VC and 5006VC in accordance with the Hook-up Chart 2, Lines 2 thru 8, END 1, Fig. A-GHBAA Sheet 01

. (b) Remove, refer to Fig. A-GBPAA Sheet 01 1 Spacer NSA5527-03-05D Item (114) Discard 1 Clamp NSA935807C09 Item (117) Discard 1 Spacer NSA5527-03-01D Item (30) Discard 1 Clamp NSA5516-04NV Item (120) Discard 2 Clamp NSA935807C16 Item (111) Discard 1 Spacer NSA5527-03-08D Item (130) Discard 1 Washer NSA935808-01 Item (112) Discard 1 Screw NAS1801-3-31 Discard (c) Install, refer to Fig. A-GBPAA Sheet 01 1 Screw NAS1801-3-31 Item 123 1 Clamp NSA5516-04NV Item 120 1 Spacer NSA5527-03-01D Item 30 1 Spacer NSA5527-03-02D Item 31 1 Spacer NSA5527-03-08D Item 130 1 Clamp NSA935807C09 Item 117 2 Clamp NSA935807C16 Item 111

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 306 6

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# @A310 SERVICE BULLETIN

1 Washer NSA935808-01 Item 112 (d) Connect the electrical wires of route 2S to the receptacles 40VC and 5006VC in accordance with the Hook-up Chart 2, lines 2 thru 8, END 1, Fig. A-GHBAA Sheet 01 . Use the contact pins if required: 15 Pin NSA938184PV1601 Item 126 **CONF 005 None **CONF 006 None **CONF 007 (1) Subtask 282148-831-253-001 - Modification Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills ELECTRICAL Material necessary to do the job Kit 282148D02R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 126 NSA938184PV1601 15 PIN Kit 282148D07R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 31 NSA5527-03-02D 2 SPACER 110 NSA935807C10 1 CLAMP 112 NAS1149D0332K 1 WASHER 117 NSA935807C09 3 CLAMP 120 NSA5516-04NV 1 CLAMP 130 NSA5527-03-08D 1 SPACER 135 NAS1096-3-42 1 SCREW References Fig. A-GBPAB Additional Work 3 - Improvement of the 2S-Route in the RH-Wing Pylon Area Sheet 01 Fig. A-GHAAA Hook-up Chart Sheet 01

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 307 6

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# @A310 SERVICE BULLETIN

References Fig. A-GHBAA Hook-up Chart Sheet 01 (a) Disconnect these wires of route 2S from the receptacles 40VC and 5006VC in accordance with the Hook-up Chart 1, Lines 1 thru 14, END 1, Fig. A-GHAAA Sheet 01 and the Hook-up Chart 2, Lines 2 thru 8, END 1, Fig. A-GHBAA Sheet 01

. (b) Remove, refer to Fig. A-GBPAB Sheet 01 1 Spacer NSA5527-03-05D Item (114) Discard 3 Clamp NSA935807C09 Item (117) Discard 1 Spacer NSA5527-03-02D Item (31) Discard 1 Clamp NSA5516-04NV Item (120) Discard 1 Screw NAS1096-3-28 Item (151) Discard 1 Clamp NSA935807C10 Item (110) Discard 1 Spacer Item (152) Discard (c) Install, refer to Fig. A-GBPAB Sheet 01 1 Screw NAS1096-3-42 Item 135 1 Washer NAS1149D0332K Item 112 1 Clamp NSA5516-04NV Item 120 2 Spacer NSA5527-03-02D Item 31 1 Spacer NSA5527-03-08D Item 130 3 Clamp NSA935807C09 Item 117 1 Clamp NSA935807C10 Item 110 (d) Connect the electrical wires of route 2S to the receptacles 40VC and 5006VC in accordance with the Hook-up Chart 1, Lines 1 thru 14, END 1, Fig. A-GHAAA Sheet 01 and the Hook-up Chart 2, lines 2 thru 8, END 1, Fig. A-GHBAA Sheet 01

. Use the contact pins if required: 15 Pin NSA938184PV1601 Item 126

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 308 6

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# @A310 SERVICE BULLETIN
**CONF 008 (1) Subtask 282148-831-253-003 - Modification Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills ELECTRICAL Material necessary to do the job Kit 282148D02R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 126 NSA938184PV1601 15 PIN Kit 282148D08R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 30 NSA5527-03-01D 1 SPACER 31 NSA5527-03-02D 1 SPACER 111 NSA935807C16 2 CLAMP 112 NSA935808-01 1 WASHER 117 NSA935807C09 1 CLAMP 120 NSA5516-04NV 1 CLAMP 123 NAS1801-3-31 1 SCREW 130 NSA5527-03-08D 1 SPACER References Fig. A-GBPAA Additional Work 3 - Improvement of the 2S-Route in the RH-Wing Pylon Area Sheet 01 Fig. A-GHBAA Hook-up Chart Sheet 01 (a) Disconnect these wires of route 2S from the receptacles 40VC and 5006VC in accordance with the Hook-up Chart 2, Lines 2 thru 8, END 1, Fig. A-GHBAA Sheet 01

. (b) Remove, refer to Fig. A-GBPAA Sheet 01 1 Spacer NSA5527-03-05D Item (114) Discard 1 Clamp NSA935807C09 Item (117) Discard 1 Spacer NSA5527-03-01D Item (30) Discard 1 Clamp NSA5516-04NV Item (120) Discard
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 309 6

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# @A310 SERVICE BULLETIN
2 Clamp NSA935807C16 Item (111) Discard 1 Spacer NSA5527-03-08D Item (130) Discard 1 Washer NSA935808-01 Item (112) Discard 1 Screw NAS1801-3-31 Discard (c) Install, refer to Fig. A-GBPAA Sheet 01 1 Screw NAS1801-3-31 Item 123 1 Clamp NSA5516-04NV Item 120 1 Spacer NSA5527-03-01D Item 30 1 Spacer NSA5527-03-02D Item 31 1 Spacer NSA5527-03-08D Item 130 1 Clamp NSA935807C09 Item 117 2 Clamp NSA935807C16 Item 111 1 Washer NSA935808-01 Item 112 (d) Connect the electrical wires of route 2S to the receptacles 40VC and 5006VC in accordance with the Hook-up Chart 2, lines 2 thru 8, END 1, Fig. A-GHBAA Sheet 01 . Use the contact pins if required: 15 Pin NSA938184PV1601 Item 126 **CONF ALL D. TEST **CONF 001 None **CONF 002 None **CONF 003 None **CONF 004 None
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 310 6

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# @A310 SERVICE BULLETIN
**CONF 005 None **CONF 006 None **CONF 007 None **CONF 008 None **CONF ALL E. CLOSE-UP **CONF 001 None **CONF 002 None **CONF 003 (1) Subtask 282148-942-202-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Install access panels 612AT and/or 623AB (RH wing) (Refer to AMM 06-41-57, Page Block 001). **CONF 004 (1) Subtask 282148-942-202-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001 DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 311 6

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

# @A310 SERVICE BULLETIN (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Install access panels 612AT and/or 623AB (RH wing) (Refer to AMM 06-41-57, Page Block 001). **CONF 005 None **CONF 006 None **CONF 007 (1) Subtask 282148-942-202-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Install access panels 612AT and/or 623AB (RH wing) (Refer to AMM 06-41-57, Page Block 001). **CONF 008 (1) Subtask 282148-942-202-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Install access panels 612AT and/or 623AB (RH wing) (Refer to AMM 06-41-57, Page Block 001).

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 312 6

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

# @A310 SERVICE BULLETIN

**CONF ALLPYLONFRONT SPARTRACK 1SCREW JACK 1SCREW JACK 2TRACK 3Z612**D E** **F**RIB2RIB4RIB8RIB7RIB3624VB /2S**A**3R/1S

B_SB_282148_6_BEAA_01_00**B C** **M H** **J K** **L A** 

Figure A-GBEAA - Sheet 01 Improvement of the 2S-Route in the RH-Wing in Zone 612 (Kit D01)
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 313 6

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

# @A310 SERVICE BULLETIN

**CONF ALL

RIB2

RIB2 2842−5052 TO 2842−5056 AND 2842−5070 (MAT. NO. 15−008) WIRE NUMBERS 3R/1S

3R/1S

**NOTE:** 1M

2M

1M

2M 624VB /2S (31)

(22)
(40)

(100)

(50) (23)

(100)

624VB /2S 5006VC 624VB /2S 40VC TO AND (23)

(50) (31)

(40) (22)

(100) 1

11

B_SB_282148_6_BEAA_02_00 

## AFTER **BEFORE**

**B**

**C**
Figure A-GBEAA - Sheet 02 Improvement of the 2S-Route in the RH-Wing in Zone 612 (Kit D01)
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 314 6

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

# @A310 SERVICE BULLETIN

**CONF ALL

2842−5052 TO 2842−5056 AND 2842−5070 (MAT. NO. 15−008) WIRE NUMBERS 3R/1S

3R/1S

**NOTE:** 624VB /2S (31) (22) (40)

(100)

624VB /2S

5006VC 624VB /2S 40VC TO AND (31) (40) (22)

(54)

(54) 618VB /2G

618VB /2E

618VB /2G

618VB /2E

1 11 

## AFTER **BEFORE**

B_SB_282148_6_BEAA_03_00 

## D

**E**
Figure A-GBEAA - Sheet 03 Improvement of the 2S-Route in the RH-Wing in Zone 612 (Kit D01)
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 315 6

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

# @A310 SERVICE BULLETIN

**CONF ALLmmDIMENSIONSABC(in.)1000.039.37100.03.9430.0 1.18ABCBTOTIETIE1TO 40VC AND624VB /2S5006VC624VB /2S616VB642VB**G**624VB /2S624VB /2S40VC5006VC616VB642VBAND**F G** TYPICAL INSTALLATION OF SLEEVES

B_SB_282148_6_BEAA_04_00 Figure A-GBEAA - Sheet 04 Improvement of the 2S-Route in the RH-Wing in Zone 612 (Kit D01)
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 316 6

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

# @A310 SERVICE BULLETIN

**CONF ALL

(MAT. NO. 15−008) 3R/1S

3R/1S

**NOTE:** 624VB /2S

(22) (40) (100)

624VB /2S

5006VC 624VB /2S 40VC TO

TO (40) (22) TIE

TIE

2842−5052 TO 2842−5056 WIRE NUMBER 2842−5070 WIRE NUMBERS (100) (55)
(40) (55)

(22) 12

(22) (55) 12 (40) (55)

624VB /2S

B_SB_282148_6_BEAA_05_00 

## AFTER **BEFORE**

**H**

**J**

Figure A-GBEAA - Sheet 05 Improvement of the 2S-Route in the RH-Wing in Zone 612 (Kit D01)
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 317 6

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

# @A310 SERVICE BULLETIN

**CONF ALL

3R/1S/1M 624VB /2S 624VB /2S

2S/1M

B_SB_282148_6_BEAA_06_00 

## BEFORE

**K**

Figure A-GBEAA - Sheet 06 Improvement of the 2S-Route in the RH-Wing in Zone 612 (Kit D01)
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 318 6

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

# @A310 SERVICE BULLETIN

**CONF ALL

3R/1S/1M

**NOTE:** 624VB /2S 624VB /2S

2842−5052 TO 2842−5056 WIRE NUMBER 2842−5070 WIRE NUMBERS 2S/1M 1

B_SB_282148_6_BEAA_07_00 

## AFTER

**L**

Figure A-GBEAA - Sheet 07 Improvement of the 2S-Route in the RH-Wing in Zone 612 (Kit D01)
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 319 6

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

# @A310 SERVICE BULLETIN

**CONF ALLmmDIMENSIONSABC(in.)1000.039.37100.03.9430.0 1.18ABCBTOTIETIE1TO 40VC624VB /2S5006VC624VB /2S616VB642VB624VB /2S624VB /2S40VC5006VC616VB642VBTOTYPICAL INSTALLATION OF SLEEVES624VB /2STO624VB /2S

B_SB_282148_6_BEAA_08_00**N N** **M**

Figure A-GBEAA - Sheet 08 Improvement of the 2S-Route in the RH-Wing in Zone 612 (Kit D01)
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 320 6

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

# @A310 SERVICE BULLETIN

**CONF ALLPYLONFRONT SPARTRACK 4SCREW JACK 31M1SMASTER TRACK 5RIB12RIB11RIB10RIB9636VB /2S636VB /2MZ623

B_SB_282148_6_BFAA_01_00**A B** **C D** **E F** **G H** **J F** **G R** **S K** **L K** **L M** **N P** **Q A** 

Figure A-GBFAA - Sheet 01 Improvement of the 2S-Route in the RH-Wing in Zone 623 (Kit D01)
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 321 6

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

# @A310 SERVICE BULLETIN

**CONF ALL

TO 10QT − B

636VB /2S

B_SB_282148_6_BFAA_02_00 TO 10QT − B

1 636VB /2S 636VB /2M

636VB /2S 636VB /2M 1S

1M

1S

1M 

## BEFORE

**AFTER B** 

**C**
Figure A-GBFAA - Sheet 02 Improvement of the 2S-Route in the RH-Wing in Zone 623 (Kit D01)
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 322 6

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

# @A310 SERVICE BULLETIN

**CONF ALL

30 TYPICAL

TYPICAL 1S

1M TO 10QT − A 1S

TO 10QT − A

APPLY (MAT. NO. 15−008) **NOTE:** 636VB /2S 636VB /2M

121 (22) (121)

(122) (112)

(22) (23) (31) (30)

(112)

(122)

(23) (31) (30) 1

636VB /2S 636VB /2M 10

B_SB_282148_6_BLAA_03_00 

## BEFORE

**AFTER D** 

**E** (22) (2 POS)

B_SB_282148_6_BFAA_03_00 Figure A-GBFAA - Sheet 03 Improvement of the 2S-Route in the RH-Wing in Zone 623 (Kit D01)
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 323 6

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

# @A310 SERVICE BULLETIN

**CONF ALL

APPLY (MAT. NO. 15−008) **NOTE:** 636VB /2S

636VB /2M

636VB /2S

636VB /2M 1S

1M

TYPICAL 1S

1M

TYPICAL AND TO (30) (22) (40) (52)

(22)

636VB /2S 1

10 (30) (22) (40) (52)

(22)

B_SB_282148_6_BFAA_04_00 

## AFTER **BEFORE**

**F**

**G** 10QTA 10QTB

Figure A-GBFAA - Sheet 04 Improvement of the 2S-Route in the RH-Wing in Zone 623 (Kit D01)
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 324 6

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# @A310 SERVICE BULLETIN

**CONF ALL

APPLY (MAT. NO. 15−008) **NOTE:** 636VB /2S

636VB /2M

636VB /2S

636VB /2M TYPICAL

TYPICAL 1S

1M

1S

1M TO AND 636VB /2S

10 (32) (30)

(22)

(22) (51)
(40) (32)

(22) (23) (30)

(22)

(51) (40) 

## AFTER **BEFORE**

**H** 1



## J

B_SB_282148_6_BFAA_05_00 10QTA

10QTB

Figure A-GBFAA - Sheet 05 Improvement of the 2S-Route in the RH-Wing in Zone 623 (Kit D01)
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 325 6

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

# @A310 SERVICE BULLETIN

**CONF ALL

APPLY (MAT. NO. 15−008) **NOTE:** 636VB /2S 636VB /2M

TYPICAL

TYPICAL 1M/1S

TO AND 636VB /2S 1 10

(30) (22)

(40) (32)

(30) (22) (51)

(40)

14 636VB2M /2S 1M/1S

B_SB_282148_6_BFAA_06_00 

## AFTER **BEFORE**

**K**

**L** 10QTA

10QTB

Figure A-GBFAA - Sheet 06 Improvement of the 2S-Route in the RH-Wing in Zone 623 (Kit D01)
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 326 6

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# @A310 SERVICE BULLETIN

**CONF ALL

APPLY (MAT. NO. 15−008A) **NOTE:** 636VB /2S

636VB /2M

636VB /2S

636VB /2M

1S

1M

1S

1M TO AND 636VB /2S

1

10 (32) (30) (22) (22) (51) (40) (32) (22)

(23) (30) (22) (51) (40)

B_SB_282148_6_BFAA_07_00 

## AFTER **BEFORE**

**M**

**N** 10QTA 10QTB

Figure A-GBFAA - Sheet 07 Improvement of the 2S-Route in the RH-Wing in Zone 623 (Kit D01)
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 327 6

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# @A310 SERVICE BULLETIN

**CONF ALL

636VB2M /2S 1M/1S 52VP

44VP 5002VP 2S

2M 1M/1S

1M

636VB /2M (32) (31) (40) (52)

(21) (21)

B_SB_282148_6_BFAA_08_00 

## BEFORE

**P** Figure A-GBFAA - Sheet 08 Improvement of the 2S-Route in the RH-Wing in Zone 623 (Kit D01)
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 328 6

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

# @A310 SERVICE BULLETIN

**CONF ALL

APPLY (MAT. NO. 15−008) **NOTE:** 636VB2M /2S 1M/1S 1M

636VB /2M (32) (31) (40)

(52) (21) 52VP

44VP 5002VP 2S

2M 1M/1S

1 TO AND 636VB /2S

10

B_SB_282148_6_BFAA_09_00 

## AFTER

**Q** 10QTA

10QTB

Figure A-GBFAA - Sheet 09

Improvement of the 2S-Route in the RH-Wing in Zone 623 (Kit D01)
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 329 6

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

# @A310 SERVICE BULLETIN

**CONF ALLWIRE NUMBERS 2842−5061 TO 5065 AND 2842−5071**NOTE:**mmDIMENSIONSABC(in.)1000.0 39.370100.0 3.93730.01.181ABCBTYPICAL INSTALLATION OF SLEEVESTOTIETIETYPICAL INSTALLATION OFWIRE CROSSINGTIE OR636VB /2S636VB /2S1636VB /2S636VB /2S1516

B_SB_282148_6_BFAA_10_00**S T** **T R** 10QTA 10QTBANDTOAND10QTB10QTA

Figure A-GBFAA - Sheet 10 Improvement of the 2S-Route in the RH-Wing in Zone 623 (Kit D01)
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 330 6

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

# @A310 SERVICE BULLETIN

**CONF 001, 005

AFTER SB A310−36−2015 OR MODIFICATION 7633S8497 **NOTE:** 

### P

636VB /2S

(125)

52VP 44VP 52VP 636VB /2S

636VB /2S 2212VC 38VC 5006VC 5006VC 40VC 40VC 636VB /2S
636VB2S

(125) (125)

(125) (125)

(125) Z612

B_SB_282148_6_BGAA_01_00 

## BEFORE **A B** 

**D F** 
**H H**  **K**

**M**



## A **C**

Figure A-GBGAA - Sheet 01 Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D02)
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 331 6

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

# @A310 SERVICE BULLETIN

**CONF 001, 005

AFTER SB A310−36−2015 OR MODIFICATION 7633S8497 **NOTE:** 

### N
**Q**

52VP 44VP
52VP 2212VC 5006VC 5006VC 40VC 40VC

1

125 125 125 636VB

125 125 125

125 636VB 125

109

125 2S2S / QT

2S 2S / QT 125

B_SB_282148_6_BGAA_02_00 

## AFTER

TYPICAL PLACARD

INSTALLATION 

## C 1 

### E **G J**  **J L**  **C**



## B

Figure A-GBGAA - Sheet 02 Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D02)
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 332 6

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

# @A310 SERVICE BULLETIN

**CONF 001, 005

B_SB_282148_6_BGAA_03_00 APPLY (MAT. NO. 15−008) **NOTE:** 636VB /2S

636VB /2M

636VB /2S

636VB /2M TO 10QT 636VB /2S CLAMP

CLAMP (109) (110) (111)

(113) (112) (31) (114)
(117) (115) (116)

109 117

(112) (113)

(117) (115) (116) (111) 

## AFTER **BEFORE**

**D**

**E** 30

Figure A-GBGAA - Sheet 03 Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D02)
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 333 6

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

# @A310 SERVICE BULLETIN

**CONF 001, 005

APPLY (MAT. NO. 15−008) **NOTE:** 636VB /2S

636VB /2M

636VB /2S

636VB /2M TO 636VB /2S (109) (110) (111)

(112) (31)

(117)

109 117

(117) (111)

TO PYLON

TO TO PYLON

TO 2212VC (30)

(118) (30)

(112) (118)
2212VC (110) (31) (30)

(30) 117 109

B_SB_282148_6_BGAA_04_00 

## AFTER **BEFORE**

**F**

**G** 10QT

Figure A-GBGAA - Sheet 04 Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D02)
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 334 6

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

# @A310 SERVICE BULLETIN

**CONF 001, 005

APPLY (MAT. NO. 15−008) **NOTE:** 636VB /2S 636VB /2M

636VB /2S

636VB /2M
TO 636VB /2S (109) (110) (111)

(117)

109 117 (117) (111)

TO TO 2212VC (30) (118)

(118)

2212VC (31) (30) 117 109 TYPICAL

TYPICAL AFTER SB A310−36−2015 OR MODIFICATION 7633S8497 TO PYLON

CLAMP

CLAMP TO PYLON (115)
(114) (31)

(114) (115)

B_SB_282148_6_BGAA_05_00 

## AFTER

**BEFORE**

**H**

**J** 10QT

Figure A-GBGAA - Sheet 05 Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D02)
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 335 6

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

# @A310 SERVICE BULLETIN

**CONF 001, 005

APPLY (MAT. NO. 15−008) **NOTE:** 636VB /2S 636VB /2M

636VB /2S
636VB /2M

636VB /2S (109) (110) (111)

(117)

109117

(117) (111)

TO TO 2212VC (30) (118)

(118)

2212VC (31) (30) 117 109

AFTER SB A310−36−2015 OR MODIFICATION 7633S8497 TO PYLON

CLAMP

CLAMP TO PYLON (115) (114) (31)

(114) CONDUIT CONDUIT

(115) 

## AFTER **BEFORE**

**K**

**L**

B_SB_282148_6_BGAA_06_00 TO 10QT

Figure A-GBGAA - Sheet 06 Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D02)
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 336 6

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

# @A310 SERVICE BULLETIN

**CONF 001, 005

APPLY (MAT. NO. 15−008) **NOTE:** 636VB /2S

636VB /2M

636VB /2S

636VB /2M 636VB /2S (109)

(110) (111)
(117)

109 (111) (30)

(112) (118) (31) (30)

117 109 (114) (31)

(114) 644VB1M /1S (118) (112)

644VB1M /1S

(117) 117 

## AFTER **BEFORE**

**M**

**N**

B_SB_282148_6_BGAA_07_00 TO 10QT

Figure A-GBGAA - Sheet 07 Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D02)
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 337 6

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

# @A310 SERVICE BULLETIN

**CONF 001, 005

APPLY (MAT. NO. 15−008) **NOTE:**

636VB /2S

636VB /2M

636VB /2S

636VB /2M 636VB /2S (109) (110) (111)

(117)

109 (111)

(112) (31)

117 109 (114) (31)

(114) 644VB1M /1S

(112)

644VB1M /1S

(117) (119)

(119)

(2 POS) 

## AFTER **BEFORE**

**P**

**Q**

B_SB_282148_6_BGAA_08_00 TO 10QT

Figure A-GBGAA - Sheet 08 Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D02)
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 338 6

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

# @A310 SERVICE BULLETIN

**CONF 002, 006

AFTER SB A310−36−2015 OR MODIFICATION 7633S8497 **NOTE:** 

### P

52VP 44VP 52VP 636VB /2S

(132)

(132) 5006VC 40VC

38VC 5006VC

(132) Z612



## BEFORE

**D F**  **H H**  **K M** 



## A

B_SB_282148_6_BHAA_01_00 

### A **B**

**C**

Figure A-GBHAA - Sheet 01 Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D03)
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 339 6

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

# @A310 SERVICE BULLETIN

**CONF 002, 006

AFTER SB A310−36−2015 OR MODIFICATION 7633S8497 **NOTE:** 52VP 44VP 5006VC 40VC 40VC

636VB 126

636VB

109

132 

### N

**Q** 132 132 132 132
132

1

132

132 132 132 2S2S / QT

2S 2S / QT 

## AFTER

TYPICAL PLACARD

INSTALLATION 

## C **E G**  **J J**  **L**

52VP 

### C



## B

B_SB_282148_6_BHAA_02_00 5006VC

Figure A-GBHAA - Sheet 02 Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D03)
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 340 6

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

# @A310 SERVICE BULLETIN

**CONF 002, 006

636VB /2S 636VB /2M

636VB /2S 636VB /2M (111)

(113) (31) (114) (116)

109 117 (113)

(116) (111) CLAMP

CLAMP

(112) (31) (124) (124)
(112)

(114) 

## BEFORE

**AFTER**

B_SB_282148_6_BHAA_03_00 

## D

**E**

Figure A-GBHAA - Sheet 03 Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D03)
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 341 6

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

# @A310 SERVICE BULLETIN

**CONF 002, 006

636VB /2S 636VB /2M

636VB /2S 636VB /2M (111)

(112) (31)

(111)

(112) (31)

117 109 (113) (114)

(113) (114)

B_SB_282148_6_BHAA_04_00 

## BEFORE

**AFTER F** 

**G**

Figure A-GBHAA - Sheet 04 Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D03)
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 342 6

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

# @A310 SERVICE BULLETIN

**CONF 002, 006

636VB /2S 636VB /2M

636VB /2S 636VB /2M (111)

(112) (31)

(111)

(112) (31)
117 109 (113) (114)

(113) (114)

B_SB_282148_6_BHAA_05_00 

## BEFORE

**AFTER**

**H**

**J**

Figure A-GBHAA - Sheet 05 Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D03)
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 343 6

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

# @A310 SERVICE BULLETIN

**CONF 002, 006

636VB /2S 636VB /2M

636VB /2S 636VB /2M (111)

(112) (31)

(111)

(31)

117 109 (123) (120)

123 (120)
(112) (31) 

## BEFORE

**AFTER K** 

**L**

B_SB_282148_6_BHAA_06_00 Figure A-GBHAA - Sheet 06 Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D03)
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 344 6

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

# @A310 SERVICE BULLETIN

**CONF 002, 006

636VB /2S 636VB /2M

636VB /2S

636VB /2M (111) (112) (31)

(111) (31)

117 109 123 (112) (114) (113)

(114) 130

B_SB_282148_6_BHAA_07_00 

## BEFORE

**AFTER M** 

**N**

Figure A-GBHAA - Sheet 07 Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D03)
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 345 6

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

# @A310 SERVICE BULLETIN

**CONF 002, 006

636VB /2S 636VB /2M

636VB /2S

636VB /2M (111) (112) (31)

(111) (31)

117 109 123 (112) (114) (113)

131 31 (114) 

## BEFORE

**AFTER P** 

**Q**

B_SB_282148_6_BHAA_08_00 Figure A-GBHAA - Sheet 08 Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D03)
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 346 6

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

# @A310 SERVICE BULLETIN

**CONF 003, 007



### E **G C** 

**L**

**A B** 

**J** Z612

5006VC 40VC 636VB /2S

38VC

636VB /2S

44VP 52VP (1)

B_SB_282148_6_BJAA_01_00 

## BEFORE

**A G** 

**N**

Figure A-GBJAA - Sheet 01 Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D05)
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 347 6

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

# @A310 SERVICE BULLETIN

**CONF 003, 007

ELEC. WIRES 636VB/2S THRU 40VC (2842−5061, 2842−5062, 2842−5063, 2842−5064 AND 2842−5065) **NOTE:** 

### D **F H**  **H M** 

ELEC. WIRES 636VB/2S THRU 5006VC (2842−5071) ELEC. WIRES 636VB/2S THRU 52VP (2842−5061, 2842−5062, 2842−5063, 2842−5064, 2842−5065 AND 2842−5071) (3 POS)



### K 5006VC 40VC 636VB /2S

636VB /2S

44VP

52VP 38VC 1

B_SB_282148_6_BJAA_02_00 

## AFTER

**B Q** 

**P**

Figure A-GBJAA - Sheet 02 Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D05)
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 348 6

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

# @A310 SERVICE BULLETIN

**CONF 003, 007

117 117

136

30 (112) (116) (136)

(112) (116) 644VB /1S 644VB /1M

636VB /2M

644VB /1S 644VB /1M

636VB /2M 636VB /2S

ELEC. WIRES 636VB/2S THRU 10QT (2842−5061, 2842−5062, **NOTE:** 2842−5063, 2842−5064, 2842−5065 AND 2842−5071) 636VB /2S (117)

(30)

B_SB_282148_6_BJAA_03_00 

## BEFORE

**AFTER C** 

**D**

Figure A-GBJAA - Sheet 03 Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D05)
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 349 6

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

# @A310 SERVICE BULLETIN

**CONF 003, 007

117

117 (117)

(112) (113) (112) (113) 644VB /1S 644VB /1M

2212VC

636VB /2M

644VB /1S 644VB /1M

2212VC

636VB /2M TO

ELEC. WIRES 636VB/2S THRU 10QT (2842−5061, 2842−5062, **NOTE:** 2842−5063, 2842−5064, 2842−5065 AND 2842−5071) TO

B_SB_282148_6_BJAA_04_00 

## BEFORE

**AFTER E** 

**F**

Figure A-GBJAA - Sheet 04 Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D05)
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 350 6

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

# @A310 SERVICE BULLETIN

**CONF 003, 007

ELEC. WIRES 636VB/2S THRU 10QT (2842−5061, 2842−5062, **NOTE:** 2842−5063, 2842−5064, 2842−5065 AND 2842−5071) 117

117 (117)

(112) (113) (112) (113)

644VB /1S 644VB /1M

2212VC 636VB /2M

644VB /1S 644VB /1M

2212VC 636VB /2M TO

TO 636VB /2S

636VB /2S



## BEFORE

**AFTER G** 

**H**

B_SB_282148_6_BJAA_05_00 Figure A-GBJAA - Sheet 05 Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D05)
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 351 6

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

# @A310 SERVICE BULLETIN

**CONF 003, 007

ELEC. WIRES 636VB/2S THRU 10QT (2842−5061, 2842−5062, **NOTE:** 2842−5063, 2842−5064, 2842−5065 AND 2842−5071) 117

117 (117)

(112) (112) 644VB /1S 644VB /1M

2212VC 636VB /2M

644VB /1S 644VB /1M

2212VC 636VB /2M TO

TO 636VB /2S

636VB /2S

31 (135)

135 (30) 

## BEFORE

**AFTER J** 

**K**

B_SB_282148_6_BJAA_06_00 Figure A-GBJAA - Sheet 06 Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D05)
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 352 6

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

# @A310 SERVICE BULLETIN

**CONF 003, 007

ELEC. WIRES 636VB/2S THRU 10QT (2842−5061, 2842−5062, **NOTE:** 2842−5063, 2842−5064, 2842−5065 AND 2842−5071) 117 117 (117)

(112) (113) (112) (113) 644VB /1S 644VB /1M

636VB /2M

644VB /1S 644VB /1M

636VB /2M 636VB /2S

636VB /2S

B_SB_282148_6_BJAA_07_00 

## BEFORE

**AFTER**

**M L** 

Figure A-GBJAA - Sheet 07 Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D05)
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 353 6

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

# @A310 SERVICE BULLETIN

**CONF 003, 007

117 117 (117)

(112) (113) (112) (113) 644VB /1S 644VB /1M

636VB /2M

644VB /1S 644VB /1M

636VB /2M 636VB /2S

636VB /2S

ELEC. WIRES 636VB/2S THRU 10QT (2842−5061, 2842−5062, **NOTE:** 2842−5063, 2842−5064, 2842−5065 AND 2842−5071) B_SB_282148_6_BJAA_08_00 

## BEFORE

**AFTER N** 

**P**

Figure A-GBJAA - Sheet 08 Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D05)
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 354 6

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

# @A310 SERVICE BULLETIN

**CONF 003, 007

TO 10QT−A AND 10QT−B 

### A

**A** TO 10QT−A AND 10QT−B

ALL 100.0 mm (ALL 3.94 in) 1000.0 mm (39.37 in)

THE ENDS OF THE PROTECTION SLEEVES, ITEM 1, MUST OVERLAP **NOTE:** 636VB /2S

636VB /2S 1 149

150 150

636VB /2S

636VB /2S 1

B_SB_282148_6_BJAA_09_00 

## Q

**A A** 

Figure A-GBJAA - Sheet 09 Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D05)
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 355 6

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

# @A310 SERVICE BULLETIN

**CONF 004, 008



### E **A B** 

**C**
**G G**  **J L** 



## A Z612

5006VC 40VC

38VC

44VP
52VP

B_SB_282148_6_BKAA_01_00 

## BEFORE

**N**

Figure A-GBKAA - Sheet 01 Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D06)
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 356 6

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

# @A310 SERVICE BULLETIN

**CONF 004, 008



### D **F H**  **H K** 

ELEC. WIRES 636VB/2S THRU 40VC (2842−5061, 2842−5062, 2842−5063, 2842−5064 AND 2842−5065) **NOTE:** ELEC. WIRES 636VB/2S THRU 5006VC (2842−5071) ELEC. WIRES 636VB/2S THRU 52VP (2842−5061, 2842−5062, 2842−5063, 2842−5064, 2842−5065 AND 2842−5071) (3 POS) 5006VC 40VC

44VP
52VP 38VC
1

B_SB_282148_6_BKAA_02_00 

## AFTER

**Q**

**M**
**P**



## B

Figure A-GBKAA - Sheet 02 Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D06)
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 357 6

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

# @A310 SERVICE BULLETIN

**CONF 004, 008

117 (112) (116)

(112) (116) 644VB /1S 644VB /1M 636VB /2M

644VB /1S 644VB /1M

636VB /2M 636VB /2S

ELEC. WIRES 636VB/2S THRU 10QT (2842−5061, 2842−5062, **NOTE:** 2842−5063, 2842−5064, 2842−5065 AND 2842−5071) 636VB /2S

(113) (124)

(113) (124)

B_SB_282148_6_BKAA_03_00 

## BEFORE

**AFTER C** 

**D**

Figure A-GBKAA - Sheet 03 Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D06)
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 358 6

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

# @A310 SERVICE BULLETIN

**CONF 004, 008

117 (112)

(112) 644VB /1S 644VB /1M 636VB /2M

644VB /1S 644VB /1M

636VB /2M 636VB /2S

ELEC. WIRES 636VB/2S THRU 10QT (2842−5061, 2842−5062, **NOTE:** 2842−5063, 2842−5064, 2842−5065 AND 2842−5071) 636VB /2S

(113) (113)

B_SB_282148_6_BKAA_04_00 

## BEFORE

**AFTER E** 

**F**

Figure A-GBKAA - Sheet 04 Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D06)
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 359 6

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

# @A310 SERVICE BULLETIN

**CONF 004, 008

117 (112)

(112) 644VB /1S 644VB /1M

636VB /2M

644VB /1S 644VB /1M

636VB /2M 636VB /2S

ELEC. WIRES 636VB/2S THRU 10QT (2842−5061, 2842−5062, **NOTE:** 2842−5063, 2842−5064, 2842−5065 AND 2842−5071) 636VB /2S

(113) (113)

B_SB_282148_6_BKAA_05_00 

## BEFORE

**AFTER G** 

**H**

Figure A-GBKAA - Sheet 05 Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D06)
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 360 6

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

# @A310 SERVICE BULLETIN

**CONF 004, 008

117 644VB /1S 644VB /1M
636VB /2M

644VB /1S 644VB /1M

636VB /2M 636VB /2S

ELEC. WIRES 636VB/2S THRU 10QT (2842−5061, 2842−5062, **NOTE:** 2842−5063, 2842−5064, 2842−5065 AND 2842−5071) 636VB /2S

(31)

31 (112) (120)

(120)
121 636VB /2M

(31) 

## BEFORE

**AFTER J** 

**K**

B_SB_282148_6_BKAA_06_00 Figure A-GBKAA - Sheet 06 Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D06)
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 361 6

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

# @A310 SERVICE BULLETIN

**CONF 004, 008

117 644VB /1S 644VB /1M

636VB /2M

644VB /1S 644VB /1M

636VB /2M 636VB /2S

ELEC. WIRES 636VB/2S THRU 10QT (2842−5061, 2842−5062, **NOTE:** 2842−5063, 2842−5064, 2842−5065 AND 2842−5071) 636VB /2S (123)

130 123

B_SB_282148_6_BKAA_07_00 

## BEFORE

**AFTER L** 

**M**

Figure A-GBKAA - Sheet 07 Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D06)
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 362 6

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

# @A310 SERVICE BULLETIN

**CONF 004, 008

117 644VB /1S 644VB /1M
636VB /2M

644VB /1S 644VB /1M

636VB /2M 636VB /2S

ELEC. WIRES 636VB/2S THRU 10QT (2842−5061, 2842−5062, **NOTE:** 2842−5063, 2842−5064, 2842−5065 AND 2842−5071) 636VB /2S (123)

123 131 31

B_SB_282148_6_BKAA_08_00 

## BEFORE

**AFTER N** 

**P**

Figure A-GBKAA - Sheet 08 Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D06)
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 363 6

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

# @A310 SERVICE BULLETIN

**CONF 004, 008

TO 10QT−A AND 10QT−B 

### A

**A** TO 10QT−A AND 10QT−B

ALL 100.0 mm (ALL 3.94 in) 1000.0 mm (39.37 in)

THE ENDS OF THE PROTECTION SLEEVES, ITEM 1, MUST OVERLAP **NOTE:** 636VB /2S

636VB /2S 1 149

150 150

636VB /2S

636VB /2S 1

B_SB_282148_6_BKAA_09_00 

## Q

**A A** 

Figure A-GBKAA - Sheet 09 Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D06)
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 364 6

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

# @A310 SERVICE BULLETIN

**CONF 001, 003, 005, 007

1 481 40VC W NSA938184PV1601 3155−5202 2S DE22/DK22 1400 55 481 5110VS−A 0 NSA936809RG0002 LINE ZONE OR PANEL ELEC. IDENT TERM. TERMINAL P/N WIRE IDENT INSTRUCTIONS TERMINAL P/N ELEC. IDENT TERM. ZONE OR

PANEL LENGTH MM INCH GAUGE ROUTE COL

2 481 40VC −D NSA938184PV1601 2781−5154R 2S PE22/PG22 624 32CV−B A EN3155−019F2018 52VP T 3 481 40VC −E NSA938184PV1601 2781−5155B 2S PE22/PG22 20000 787 624 32CV−B B EN3155−019F2018 52VP U 4 481 40VC Z NSA938184PV1601 3621−5014B 2S PE22/PG22 1550 61 481 B NSA938185SV1601 5 481 40VC X NSA938184PV1601 3621−5015R 2S PE22/PG22 481 5110VS−A 0 NSA936809RG0002 6 481 40VC −F NSA938184PV1601 2781−5156B 2S QE24/QG24 20000 787 624 C EN3155−019F2018 7 481 40VC −G NSA938184PV1601 2781−5157R 2S QE24/QG24 624 32CV−B D EN3155−019F2018 52VP W 8 481 40VC −H NSA938184PV1601 2781−5158Y 2S QE24/QG24 624 E EN3155−019F2018 9 481 40VC V NSA938184PV1601 3611−5071R 2S PG22 1500 60 481 2212CV 1 E0446DW2001 10 481 40VC U NSA938184PV1601 3611−5072B 2S PG22 1500 60 481 2 11 481 40VC T NSA938184PV1601 3611−5073R 2S PG22 1500 60 481 2212CV 3 12 481 40VC S NSA938184PV1601 3611−5074B 2S PG22 1500 60 481 4 13 481 40VC R NSA938184PV1601 3611−5075R 2S PG22 1500 60 481 2212CV 5 14 481 40VC −A NSA938184PV1601 3611−5076B 2S PG22 481 6 15 481 4HX−A C NSA938184PV1601 3621−5018 2S DM20 481 408VN/DC 0 NSA936501TA2004 16 17 482 54HA−A A NSA938185SV1601 3611−65B 2S PG22 481 34VC T NSA938184PV1601 18 482 54HA−A B NSA938185SV1601 3611−66R 2S PG22 481 S NSA938184PV1601 19 482 54HA−A D NSA938185SV1601 3611−67B 2S PG22 481 34VC R NSA938184PV1601 20 482 54HA−A E NSA938185SV1601 3611−68R 2S PG22 481 P NSA938184PV1601 21 22 23 24 25 4HX−A

32CV−B 52VP V

32CV−B 52VP X

2212CV

2212CV

2212CV

34VC

34VC 1500 60 1400 56

1300 52 1300 52 1300 52 1300 52 **END 1 LEAD**  **END 2**

ELT. EQUIPMENT 10 D929 97017 000 00 "A" EQUIPMENT B929−90719−000−00 SB A310−28−2148, CONVERSION ONLY AFTER MOD 07633 OR SB A310−36−2015 AND SB−A310−2B−2140 (MOD 12173) E = EXISTING WIRE (PART OF 5606VB / 10 D929 91506 000 00) E0446DW2001 E0446DW2001 E0446DW2001 E0446DW2001 E0446DW2001

B_SB_282148_6_HAAA_01_00 Figure A-GHAAA - Sheet 01 Hook-up Chart
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 365 6

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

# @A310 SERVICE BULLETIN

**CONF ALL

1 481 5006VC B NSA938184PV1601 2842−5058 2S(QT) DE22/DK22 200 8 481 5006VC 50711* LINE ZONE OR PANEL ELEC. IDENT TERM. TERMINAL P/N WIRE IDENT INSTRUCTIONS TERMINAL P/N ELEC. IDENT TERM. ZONE OR

PANEL LENGTH MM INCH GAUGE ROUTE COL

2 481 40VC −J NSA938184PV1601 2842−5061 2S(QT) DE24/DK24 623 10QT−B E EN3155−019F2018 52VP Y 3 481 40VC −K NSA938184PV1601 2842−5062 2S(QT) DE24/DK24 4500 177 623 10QT−B D EN3155−019F2018 52VP Z 4 481 40VC −M NSA938184PV1601 2842−5063 2S(QT) DE24/DK24 4500 177 623 C EN3155−019F2018 5 481 40VC −N NSA938184PV1601 2842−5064 2S(QT) DE24/DK24 623 10QT−B B EN3155−019F2018 6 481 40VC −P NSA938184PV1601 2842−5065 2S(QT) DE24/DK24 4500 177 623 A EN3155−019F2018 7 481 5006VC A NSA938184PV1601 2842−5071 2S(QT) SG24/SW24 623 10QT−A A EN3155−019F2018 52VP R 8 481 5006VC

− 2842−50711 2S(QT) SG24/SW24 623

− 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 10QT−B
10QT−B 52VP −C
10QT−A **END 1 LEAD**  **END 2**

2S(QT) ROUTE

B_SB_282148_6_HBAA_01_00 52VP −B 52VP −A 4500

4500 177

177

Figure A-GHBAA - Sheet 01 Hook-up Chart
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 366 6

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

# @A310 SERVICE BULLETIN

**CONF ALL

FR20

ELECTRONICS RACK 

### A

2354VC

92VU 15QTB 1 1

90VU 

## A

B_SB_282148_5_CAAA_01_01 Figure A-FCAAA - Sheet 01 Installation of Cable Sleeves in the RH Electronics Rack 90VU.
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 367 6

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

# @A310 SERVICE BULLETIN

**CONF ALL

2S−4A 2S 2S 

## AFTER FR38.1 FR38.2FR39FR40



### A

FR39

FR38.2 20VP

20VCA 1904VCA 

## B 2 

## A **B**

B_SB_282148_5_CBAA_01_01 Figure A-FCBAA - Sheet 01 Installation of Cable Sleeves in the Forward Cargo Compartment.
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 368 6

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

# @A310 SERVICE BULLETIN

**CONF 001 thru 004

FR39 FR40 

## A

2S 

## AFTER

TO FWD

WING 2 FR40 FR39
20VP



## B **A B** 

B_SB_282148_5_CCAA_01_03 Figure A-FCCAA - Sheet 01 Installation of Cable Sleeves in the RH forward wing root and krueger flap.
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 369 6

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

# @A310 SERVICE BULLETIN

**CONF 005 thru 008

FR39 FR40 

## A 

## AFTER

**B A** 

TO FWD WING 2S FR40 FR39

20VP 2 

### B

B_SB_282148_5_CCAB_01_01 Figure A-FCCAB - Sheet 01 Installation of Cable Sleeves in the RH forward wing root and krueger flap.
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 370 6

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

# @A310 SERVICE BULLETIN

**CONF ALL

Figure A-FWAAA - Sheet 01 Installation of Cable Sleeves in the RH Electronics Rack 90VU.
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 371 6

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

# @A310 SERVICE BULLETIN

**CONF ALL

CENTERLINE PYLON D NOSE

1 SUB SPAR VIEW LOOKING FWD WOFZ 0.0 WDFX −53.0 (1)

SUB SPAR VIEW LOOKING FWD WOFZ 0.0 WDFX −53.0 RIB8 RIB9

(0.35 in) 2 (2)



### AFTER

8.89 mm 

### A **B**



## A

**B** (0.35 in) 8.89 mm

B_SB_282148_7_BAAA_01_00 Figure A-UBAAA - Sheet 01 Location of Bracket on the Sub Spar Behind the Front Spar Between RIB 8 and RIB 9 (RH Wing)
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 372 6

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

# @A310 SERVICE BULLETIN

**CONF 001 thru 002, 005 thru 006PYLONFRONT SPARTRACK 4SCREW JACK 31M1SMASTER TRACK 5RIB12RIB11RIB10RIB9636VB /2S636VB /2MZ623

B_SB_282148_6_BLAA_01_00**B C** **D E** **A A** 

Figure A-GBLAA - Sheet 01 Additional Work 1 (Introduced at Revision 02): Installation of Protection Sleeve in the Area of 10QT (Kits D02 and D03) DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 373 6

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

# @A310 SERVICE BULLETIN

**CONF 001 thru 002, 005 thru 006

TO 10QT − B

TO 10QT − B

1 636VB /2S 636VB /2M

636VB /2S 636VB /2M 1S

1M

1S

1M

B_SB_282148_6_BLAA_02_00 

## BEFORE

**AFTER B** 

**C**
Figure A-GBLAA - Sheet 02 Additional Work 1 (Introduced at Revision 02): Installation of Protection Sleeve in the Area of 10QT (Kits D02 and D03) DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 374 6

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

# @A310 SERVICE BULLETIN

**CONF 001 thru 002, 005 thru 006

TYPICAL

TYPICAL 1S

1M TO 10QT − A 1S

TO 10QT − A

APPLY (MAT. NO. 15−008A) **NOTE:** 636VB /2S 636VB /2M

121 (22) (121)

(122) (112)

(22) (23) (31) (30)

(112)

(122)

(23) (31) (30) 1

636VB /2S 636VB /2M 10 636VB /2S

B_SB_282148_6_BLAA_03_00 

## BEFORE

**AFTER D** 

**E** (22)

Figure A-GBLAA - Sheet 03 Additional Work 1 (Introduced at Revision 02): Installation of Protection Sleeve in the Area of 10QT (Kits D02 and D03) DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 375 6

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

# @A310 SERVICE BULLETIN

**CONF 001, 005

AFTER SB A310−36−2015 OR MODIFICATION 7633S8497 **NOTE:** 

### P

636VB /2S

(125)

52VP 44VP 52VP 636VB /2S

636VB /2S 2212VC 38VC 5006VC 5006VC 40VC 40VC 636VB /2S
636VB2S

(125) (125)

(125) (125)

(125) Z612

B_SB_282148_6_BMAA_01_00 

## BEFORE **A B** 

**D F**  **K**

**H H**  **M C** 



## A

Figure A-GBMAA - Sheet 01 Additional Work 1 (Introduced at Revision 02): Improvement of the 2S-Route in the RH-Wing pylon area (Kit D02) DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 376 6

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

# @A310 SERVICE BULLETIN

**CONF 001, 005

AFTER SB A310−36−2015 OR MODIFICATION 7633S8497 **NOTE:** 

### N
**Q**

52VP 44VP
52VP 2212VC 5006VC 40VC 40VC

(125) 1

125 125 125 636VB 1 125 125 125

125 126

636VB 125

109

125 2S2S / QT

2S 2S / QT

B_SB_282148_6_BMAA_02_00 

## AFTER

TYPICAL PLACARD

INSTALLATION 

## C **C E**  **G J**  **L**

**J**



## B 5006VC

Figure A-GBMAA - Sheet 02 Additional Work 1 (Introduced at Revision 02): Improvement of the 2S-Route in the RH-Wing pylon area (Kit D02) DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 377 6

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

# @A310 SERVICE BULLETIN

**CONF 001, 005

APPLY (MAT. NO. 15−008) **NOTE:** 636VB /2S

636VB /2M

636VB /2S

636VB /2M CLAMP

CLAMP (109) (110) (111)

(113) (112) (31) (114)
(117) (115) (116)

109

(112) (113)

(117) (115) (116) (111)

B_SB_282148_6_BMAA_03_00 

## AFTER **BEFORE**

**D**

**E** 30

Figure A-GBMAA - Sheet 03 Additional Work 1 (Introduced at Revision 02): Improvement of the 2S-Route in the RH-Wing pylon area (Kit D02) DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 378 6

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

# @A310 SERVICE BULLETIN

**CONF 001, 005

APPLY (MAT. NO. 15−008) **NOTE:** 636VB /2S

636VB /2M

636VB /2S

636VB /2M 636VB /2S (109) (110) (111)

(112) (31)

(117)

109 117

(117) (111)

TO PYLON

TO

TO PYLON

TO 2212VC (30)

(118) (30)

(112) (118)
2212VC (110) (31) (30)

(30) 117 109

B_SB_282148_6_BMAA_04_00 

## AFTER **BEFORE**

**F**

**G**

Figure A-GBMAA - Sheet 04 Additional Work 1 (Introduced at Revision 02): Improvement of the 2S-Route in the RH-Wing pylon area (Kit D02) DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 379 6

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

# @A310 SERVICE BULLETIN

**CONF 001, 005

APPLY (MAT. NO. 15−008) **NOTE:** 636VB /2S 636VB /2M

636VB /2S

636VB /2M
636VB /2S (109) (110) (111)

(117)

109 117 (117) (111)

TO TO 2212VC (30) (118)

(118)

2212VC (31) (30) 117 109 TYPICAL

TYPICAL AFTER SB A310−36−2015 OR MODIFICATION 7633S8497 TO PYLON

CLAMP

CLAMP TO PYLON (115)
(114) (31)

(114) (115)

B_SB_282148_6_BMAA_05_00 

## BEFORE

**AFTER H** 

**J**

Figure A-GBMAA - Sheet 05 Additional Work 1 (Introduced at Revision 02): Improvement of the 2S-Route in the RH-Wing pylon area (Kit D02) DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 380 6

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

# @A310 SERVICE BULLETIN

**CONF 001, 005

APPLY (MAT. NO. 15−008) **NOTE:** 636VB /2S 636VB /2M

636VB /2S
636VB /2M (109) (110) (111)

(117)

109117

(117) (111)

TO TO 2212VC (30) (118)

(118)

2212VC (31) (30) 117 109

AFTER SB A310−36−2015 OR MODIFICATION 7633S8497 TO PYLON

CLAMP

CLAMP TO PYLON (115) (114) (31)

(114) CONDUIT CONDUIT

(115)

B_SB_282148_6_BMAA_06_00 

## BEFORE

**AFTER K** 

**L**

Figure A-GBMAA - Sheet 06 Additional Work 1 (Introduced at Revision 02): Improvement of the 2S-Route in the RH-Wing pylon area (Kit D02) DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 381 6

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

# @A310 SERVICE BULLETIN

**CONF 001, 005

APPLY (MAT. NO. 15−008) **NOTE:** 636VB /2S

636VB /2M

636VB /2S

636VB /2M 636VB /2S (109)

(110) (111)
(117)

109 (117)

(111) (30)

(112) (118) (31) (30)

117 109 (114) (31)

(114) 644VB1M /1S (118) (112)

644VB1M /1S

(117)

B_SB_282148_6_BMAA_07_00 

## BEFORE

**AFTER**

**M**

**N**

Figure A-GBMAA - Sheet 07 Additional Work 1 (Introduced at Revision 02): Improvement of the 2S-Route in the RH-Wing pylon area (Kit D02) DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 382 6

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

# @A310 SERVICE BULLETIN

**CONF 001, 005

APPLY (MAT. NO. 15−008) **NOTE:** 636VB /2S

636VB /2M

636VB /2S

636VB /2M TO 636VB /2S (109) (110) (111)

(117)

109 (111)

(112) (31)

117 109 (114) (31)

(114) 644VB1M /1S

(112)

644VB1M /1S

(117) (119)

(119)

B_SB_282148_6_BMAA_08_00 

## BEFORE

**AFTER**
**P**

**Q** 10QT

Figure A-GBMAA - Sheet 08 Additional Work 1 (Introduced at Revision 02): Improvement of the 2S-Route in the RH-Wing pylon area (Kit D02) DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 383 6

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

# @A310 SERVICE BULLETIN

**CONF 001 thru 002, 005 thru 006



## AFTER

TO FWD

WING

VALID FOR AIRCRAFT UP TO MSN 0442 2 FR40 FR39



## B FR39 FR40 

## A **A B**  **C**

B_SB_282148_6_BCAA_01_00 2S 20VP

8VP

Figure A-UBCAA - Sheet 01 Additional Work 2 (Introduced at Revision 03)- Location of Bracket on the Sub Spar Behind the Front Spar Between RIB 8 and RIB 9 (RH Wing) DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 384 6

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

# @A310 SERVICE BULLETIN

**CONF 002, 006

AFTER SB A310−36−2015 OR MODIFICATION 7633S8497 **NOTE:** 

### P

52VP 44VP 52VP 636VB /2S

(132)

(132) 5006VC 40VC

38VC 5006VC

(132) Z612



## BEFORE **A B** 



## A **C**

**D F**  **H H**  **K M** 

B_SB_282148_6_BNAA_01_00 Figure A-GBNAA - Sheet 01 Additional Work 1 (Introduced at Revision 02): Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D03) DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 385 6

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

# @A310 SERVICE BULLETIN

**CONF 002, 006

AFTER SB A310−36−2015 OR MODIFICATION 7633S8497 **NOTE:** 52VP 44VP 52VP 5006VC 40VC 40VC

636VB 126

636VB

109

132 

### N

**Q** 132 132 132 132
132

1

132

132
132 132

B_SB_282148_6_BNAA_02_00 

## AFTER

TYPICAL PLACARD

INSTALLATION 

## B **C E**  **G J**  **J L**  **C** 2S 2S /QT

2S 2S /QT 5006VC

Figure A-GBNAA - Sheet 02 Additional Work 1 (Introduced at Revision 02): Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D03) DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 386 6

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

# @A310 SERVICE BULLETIN

**CONF 002, 006

636VB /2S 636VB /2M

636VB /2S 636VB /2M (111)

(113) (31) (114)

(116)

109 117 (113)

(117) (116) (111) CLAMP

CLAMP

(112) (31) (124) (124)

(112)

B_SB_282148_6_BNAA_03_00 

## BEFORE

**AFTER D** 

**E**

Figure A-GBNAA - Sheet 03 Additional Work 1 (Introduced at Revision 02): Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D03) DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 387 6

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

# @A310 SERVICE BULLETIN

**CONF 002, 006

636VB /2S 636VB /2M

636VB /2S 636VB /2M (111)

(112) (31)

(111)

(112) (31)

117 109 (113) (114)

(113) (114)

B_SB_282148_6_BNAA_04_00 

## BEFORE

**AFTER F** 

**G**

Figure A-GBNAA - Sheet 04 Additional Work 1 (Introduced at Revision 02): Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D03) DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 388 6

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# @A310 SERVICE BULLETIN

**CONF 002, 006

636VB /2S 636VB /2M

636VB /2S 636VB /2M (111)

(112) (31)

(111)

(112) (31)
117 109 (113) (114)

(113) (114)

B_SB_282148_6_BNAA_05_00 

## BEFORE

**AFTER H** 

**J**

Figure A-GBNAA - Sheet 05 Additional Work 1 (Introduced at Revision 02): Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D03) DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 389 6

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

# @A310 SERVICE BULLETIN

**CONF 002, 006

636VB /2S 636VB /2M

636VB /2S 636VB /2M (111)

(112) (31)

(111)

(31)

117 109 (123) (120)

123 (120)
(112) (31)

B_SB_282148_6_BNAA_06_00 

## BEFORE

**AFTER K** 

**L**

Figure A-GBNAA - Sheet 06 Additional Work 1 (Introduced at Revision 02): Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D03) DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 390 6

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

# @A310 SERVICE BULLETIN

**CONF 002, 006

636VB /2S 636VB /2M

636VB /2S

636VB /2M (111) (112) (31)

(111) (31)

117 109 123 (112) (114) (113)

(114) 130

B_SB_282148_6_BNAA_07_00 

## BEFORE

**AFTER M** 

**N**

Figure A-GBNAA - Sheet 07 Additional Work 1 (Introduced at Revision 02): Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D03) DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 391 6

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

# @A310 SERVICE BULLETIN

**CONF 002, 006

636VB /2S 636VB /2M

636VB /2S

636VB /2M (111) (112) (31)

(111) (31)

117 109 123 (112) (114) (113)

131 31 114

B_SB_282148_6_BNAA_08_00



## BEFORE

**AFTER P** 

**Q**

Figure A-GBNAA - Sheet 08 Additional Work 1 (Introduced at Revision 02): Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D03) DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 392 6

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# @A310 SERVICE BULLETIN

**CONF 004, 008

636VB /2S (125)

52VP 44VP 52VP 636VB /2S

636VB /2S 2212VC 38VC 5006VC 5006VC 40VC 40VC 636VB /2S
636VB2S

(125) (125)

(125) (125)

(125) Z612



### A

B_SB_282148_6_BPAA_01_00 

### A
**A B**  **B** 

## AFTER **BEFORE** (111)

(123) (111) (120)

(112) (130) (117) (30) (114)

111 111 117 120

112 123 130 31

## A **A**

**B B** 

**A** (30)

Figure A-GBPAA - Sheet 01 Additional Work 3 - Improvement of the 2S-Route in the RH-Wing Pylon Area
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 393 6

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

# @A310 SERVICE BULLETIN

**CONF 003, 007

636VB /2S (125)

52VP 44VP 52VP 636VB /2S

636VB /2S 2212VC 38VC 5006VC 5006VC 40VC 40VC 636VB /2S
636VB2S

(125) (125)

(125) (125)

(125) Z612



### A

**A**
**A B**  **B** 

## AFTER **BEFORE**

**A** (110) (117)

(151)

(120) (31) (117) (114) (152)

110 117

112

120 31 130 

## A **A**

**B B** 

B_SB_282148_6_BPAB_01_01 135

Figure A-GBPAB - Sheet 01 Additional Work 3 - Improvement of the 2S-Route in the RH-Wing Pylon Area
DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 394 6

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# @A310 SERVICE BULLETIN REPORTING SHEET 

### TITLE: ELECTRIC/ELECTRONIC COMMON INSTALLATION - WING - IMPROVE THE 2S-ROUTE IN THE RH-WING MODIFICATION No.: 12427D21883 12435S22116 13478D23233 Please complete the appropriate item (A or B): A - SB WILL BE embodied YES/NO (if NO please comment) If YES, aircraft concerned (as per SB effectivity by default) and planned dates (month/year) of embodiment:

B - SB HAS BEEN embodied on aircraft: Operator comments:
From Airline: Name/Title: Signature: Date: If operational documentation is affected (see Paragraph 1.K of this SB): If information is needed prior to next normal revision or prior to SB embodiment, please indicate required service(s): Either: Modification Operational Impact (MOI), if available YES/NO Or : Intermediate revision YES/NO Important Information: This SB will only be incorporated in your maintenance and operational documentation if this sheet is returned to Airbus and signed by a duly authorised representative. With the next feasible revision, this will result in - Updating of maintenance documentation to show pre and post SB data. - Updating of maintenance and operational documentation to show post SB data after embodiment. If this SB requires previous or simultaneous accomplishment of other SBs, Airbus shall automatically include them in the manual revisions. Refer to SIL 00-037 for detailed information. Please return this completed sheet to: AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Attn: SDC32 Technical Data and Documentation Services FAX: (+33) 5 61 93 28 06 e-mail: sb.reporting@airbus.com or via your Resident Customer Support Office. Alternatively, SB lists via letters or fax are also accepted.

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 1 6

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# @A310 SERVICE BULLETIN QUALITY PERCEPTION FORM Use this form to tell us what is your perception of the quality of this Service Bulletin. The reported data that you provide us will be used to analyse areas of difficulties and to take corrective action to further improve the quality of our Service Bulletins. We thank you for the time you have taken in completing this form. (Please rate on a scale of 1 to 4, with 4 being the highest score) - Quality rating of this SB 4321 - Quality rating of the Accomplishment Instructions 4321 - Quality rating of the Illustrations 4321 - Is this SB easy to understand ? Y/N If you have had difficulties in the accomplishment of this SB please quote below the area(s) and give a short description of the issue. Planning Material Instructions X Effectivity X Kit content X Preparation X Reason X List of Materials Operator Supplied X Mod/Inspection X Manpower X Industry support X Test X References X Re-identification X Close-Up X Publication X Tooling X Illustrations Comments:

Operator: Date: Name/Title: Please return this form to: AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Attn : SEM4 Service Bulletins Management FAX : (33) 5 61 93 42 51 Or via your Resident Customer Support Office.

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148 REVISION No.: 06 - Aug 31/11 Page: 1 6

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