# Airbus Service Bulletin A300-24-6103

Copy: Revision 05 ("A300-24-6103R5"), 709 pages: PDF https://openairdocs.org/files/sha256/d5/f0/d5f0ffe7345d25b14b41ca5a51d93023039175f5a66f37e06a1bb427801f5a6d; text https://openairdocs.org/service-documents/airbus/a300-24-6103/file/d5f0ffe7345d.md. Rights: © Airbus S.A.S. Filed by the FAA in regulations.gov docket FAA-2019-0253, the docket of AD 2019-14-08. Not covered by OpenAirDocs’ CC0 dedication.

## Details

- Manufacturer: [Airbus](https://openairdocs.org/service-documents/airbus.md)
- Type: Service bulletin (Service Bulletin)
- Number: A300-24-6103
- Latest revision known: A300-24-6103, Revision 03, dated July 3, 2015 (OpenAirDocs)
- Page: https://openairdocs.org/service-documents/airbus/a300-24-6103

## ADs that cite it (2) (OpenAirDocs)

Newest first, with the revision each names, as OpenAirDocs read it from the AD's text.

- [AD 2019-14-08](https://openairdocs.org/ad/2019-14-08.md), effective Oct 2, 2019: Revision 03
- [AD 2016-07-22](https://openairdocs.org/ad/2016-07-22.md), effective May 16, 2016: Revisions 02 and 03

Also cited in [2 proposed ADs](https://openairdocs.org/service-documents/airbus/a300-24-6103/proposed.md).

## Text (709 pages)

Rights: © Airbus S.A.S. Filed by the FAA in regulations.gov docket FAA-2019-0253, the docket of AD 2019-14-08. Not covered by OpenAirDocs’ CC0 dedication. Each page's text from the PDF; open the PDF at a page with #page=N.

### Page 1

@A300-600
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET
AIRBUS
CUSTOMER SERVICES DIRECTORATE
1 Rond Point Maurice Bellonte
31707 BLAGNAC CEDEX
FRANCE
T e l:( 3 3 )56 19 33 33 3
Telex : AIRBU 530526F
F a x:( 3 3 )56 19 34 25 1
MANDATORY
 MANDATORY
 MANDATORY
ATA SYSTEM: 24
TITLE: ELECTRIC AND ELECTRONIC COMMON INSTALLATIONS - IMPROVE
WING WIRING INSTALLATION
MODIFICATION No.: 13397S22766 13399S22768 13516H5723
This page transmits Revision No.05 of Service Bulletin No.A300-24-6103
ADDITIONAL WORK
**CONF ALL
No additional work is required for aircraft which have embodied this Service Bulletin (SB) for the first
time at Revision No. 04.
Additional work is required by this revision for aircraft in CONF 001 and CONF 003 which have
embodied this Service Bulletin at Revision No. 03.
This additional work describes:
- Installation of Spacers to the Guide Assembly - Conduit in the LH and RH Wings for aircraft in
CONF 001 and CONF 003 (installation of two spacers were removed at Revision No. 03 of this SB)
- Modification of the Clamp on the routing on Rib 1 on the passage way to the shroud box LH and
RH sides for aircraft in CONF 003 (Revision No. 04 asked to contact AIRBUS for the clamps
installation, Revision No. 05 describes this additional work).
Additional work is required by this revision for aircraft in CONF 001 and CONF 003 which have
embodied this Service Bulletin successively at Revision No. 03 and at Revision No. 04.
This additional work describes:
- Installation of Spacers to the Guide Assembly - Conduit in the LH and RH Wings for aircraft in
CONF 001 and CONF 003 (installation of two spacers were removed at Revision No. 03 of this
SB).
Unless otherwise stated by an Airworthiness Directive, AIRBUS recommends the additional work to be
accomplished within one year after the issue of this revision.
If all additional work required with Service Bulletin Revision No. 04 has not been embodied, the
following additional work is required:
DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103
REVISION No.: 05 - Aug 20/18 Page: 1
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 2

@A300-600
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET
- Additional work between Revision No. 00 and No. 05 consists in modifying the routing of routes 1P,
2P, 1E, 1G, 2E and 2G
- Additional work between Revision No. 01 and No. 05 consists in modifying the routing of routes 1P,
2P, 1E, 1G, 2E and 2G
- Additional work between Revision No. 02 and No. 05 consists in modifying the installation of
clamps in the LH and RH wings.
REASON
Revision No. 05 issued to incorporate:
- For aircraft in CONF 003, the additional work introduced in SB 24-6103 at Revision No. 04 (but
which only stated "contact Airbus" in Revision No. 04)
- For aircraft in CONF 001 and CONF 003 that have accomplished SB 24-6103 at Revision No. 03,
the additional work related to the guide assy installation (reference SBIT 15-0078, no additional
work was introduced at SB 24-6103 at Revision No. 04)
- For aircraft in CONF 001 and CONF 003 which have accomplished SB 24-6103 successively at
Revision No. 03 and at Revision No. 04, the additional work related to the guide assy installation
- Update quantity of spacers PN NSA5527-03-01 from 10 to 13 in Kit 246103A01R14
- Update quantity of spacers PN NSA5527-03-01 from 5 to 4 in Kit 246103A02R12
- Update quantity of sleeve PN EN6049-007-08-5 from 10 meters to 15 meters in Kit 246103A01R14
- Update quantity of sleeve PN EN6049-007-08-5 from 10 meters to 15 meters in Kit 246103A02R12
- Update Subtask 246103-831-001-001 step (1) (d) to add (if installed)
- Update Subtask 246103-831-001-001 step (1) (e) to add (if installed)
- Add NOTE to Subtask 246103-831-006-001 step (5) (e) stating if necessary, the strip-protective,
Item 24, can be cut to help installation
- Add NOTE to Subtask 246103-831-006-002 step (5) (j) stating if necessary, the strip-protective,
Item 24, can be cut to help installation
- Add NOTE to Subtask 246103-831-007-001 step (13) (e) stating if necessary, the strip-protective,
Item 24, can be cut to help installation
- Add NOTE to Subtask 246103-831-007-002 step (13) (j) stating if necessary, the strip-protective,
Item 24, can be cut to help installation
- Add NOTE to Subtask 246103-831-020-001 step (2) (c) stating if necessary, the strip-protective,
Item 24, can be cut to help installation
- Add NOTE to Subtask 246103-831-020-002 step (2) (k) stating if necessary, the strip-protective,
Item 24, can be cut to help installation
DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103
REVISION No.: 05 - Aug 20/18 Page: 2
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 3

@A300-600
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET
- Add NOTE to Subtask 246103-831-028-001 step (1) (c) stating if necessary, the strip-protective,
Item 24, can be cut to help installation
- Add NOTE to Subtask 246103-831-028-002 step (1) (k) stating if necessary, the strip-protective,
Item 24, can be cut to help installation
- Add NOTE to Subtask 246103-831-033-001 step (5) (c) stating if necessary, the strip-protective,
Item 24, can be cut to help installation
- Add NOTE to Subtask 246103-831-033-002 step (5) (k) stating if necessary, the strip-protective,
Item 24, can be cut to help installation
- Add NOTE to Subtask 246103-831-050-001 step (13) (c) stating if necessary, the strip-protective,
Item 24, can be cut to help installation
- Add NOTE to Subtask 246103-831-050-002 step (13) (k) stating if necessary, the strip-protective,
Item 24, can be cut to help installation
- Update Subtask 246103-400-001-001 step (6) (a) to add (if installed) and step (b) add If necessary
- Update Subtask 246103-420-001-001 step (3) (a) and (b) to add (if removed previously)
- Update Subtask 246103-420-001-001 step (3) (f) to add (if removed)
- Update Subtask 246103-020-002-001 step (9) (a) and (b) to add (if installed)
- Update Subtask 246103-420-002-001 step (11) (a) and (b) to add (if removed previously)
- Update Subtask 246103-420-002-001 step (11) (c) to add (if removed)
- ADDITIONAL WORK TASK No. 246103-831-806-001 added.
- ADDITIONAL WORK TASK No. 246103-831-807-001 added.
NOTE
: This revision satisfies the requirements of the subsequent Technical Adaptation(s) (TA)
issued for Subtask 246103-831-006-002 (LH) and Subtask 246103-831-007-002 (RH)
for the related Manufacturer Serial Number (MSN)s:
TA
 MSN
80205706/003/2016
 0805, 0806, 0807, 0808, 0809, 0810, 0811,
0812, 0813, 0814, 0815, 0816, 0817, 0818,
0819, 0820, 0821, 0822, 0823, 0824, 0825,
0826, 0827, 0828, 0829, 0830, 0831, 0832,
0833, 0834, 0835, 0839, 0840, 0840, 0845,
0846, 0847, 0948, 0849, 0850, 0851, 0852,
0853, 0854, 0861, 0862, 0863, 0864, 0865,
0866, 0867, 0868 and 0869
NOTE
: This revision satisfies the requirements of the subsequent Technical Adaptation(s) (TA)
issued for Subtasks 246103-831-037-001 (LH) and 246103-831-038-001 (RH) referring
to Fig. A-FCPAA Sheet 05 "Section F-F" for the related MSN’s:
TA
 MSN
DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103
REVISION No.: 05 - Aug 20/18 Page: 3
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 4

@A300-600
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET
80199484/013/2018
 0872
80199484/026/2018
 0557 and 0729
CHANGES
The main changes of this revision are:
- SBIT 16-0030 and SBIT 16-0051 added
- TA 80199484/013/2018, TA 80199484/026/2018 and TA 80205706/003/2016 added
- Kit 246103A01 and Kit 246103A02 revised
- Kit 246103A06R00 and Kit 246103A07R00 created
- Subtasks 246103-910-401-001, 246103-941-401-001 and 246103-942-401-001 removed
- Subtasks 246103-910-001-001, 246103-941-001-001 and 246103-942-001-001 updated
- APPENDIX 05 - Elapsed Time Assumption ADDITIONAL WORK between Revision No. 03 and
Revision No. 05 created
- APPENDIX 06 - Elapsed Time Assumption ADDITIONAL WORK between Revision No. 04 and
Revision No. 05 created and only if Revision No. 03 was also Embodied
- Figure ref’s A-FBAAA, A-FBBAA, A-FBDAA, A-FBDAB, A-FFAAA, A-FBMAA, A-FBMAB, A-FBRAA,
A-FBUAA, A-FCCAA and A-FCCAB updated
- Figure ref’s A-FCQAA, A-FCRAA, A-FAGAA, A-FAGAB created
- NOTE added to Kit COMPB01
- NOTE added to Kit 246103A03R06
- NOTE added to Kit 246103B01R03
- NOTE added to Subtask 246103-831-028-001 step (1) (c) stating if necessary, the strip-protective,
Item 24, can be cut to help installation
- NOTE added to Subtask 246103-831-020-001 step (2) (c) stating if necessary, the strip-protective,
Item 24, can be cut to help installation
- NOTE added to Subtask 246103-831-028-002 step (1) (k) stating if necessary, the strip-protective,
Item 24, can be cut to help installation
- NOTE added to Subtask 246103-831-020-002 step (2) (k) stating if necessary, the strip-protective,
Item 24, can be cut to help installation
- NOTE added to Subtask 246103-831-033-001 step (5) (c) stating if necessary, the strip-protective,
Item 24, can be cut to help installation
- NOTE added to Subtask 246103-831-050-001 step (13) (c) stating if necessary, the strip-protective,
Item 24, can be cut to help installation
DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103
REVISION No.: 05 - Aug 20/18 Page: 4
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 5

@A300-600
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET
- NOTE added to Subtask 246103-831-033-002 step (5) (k) stating if necessary, the strip-protective,
Item 24, can be cut to help installation
- NOTE added to Subtask 246103-831-050-002 step (13) (k) stating if necessary, the strip-protective,
Item 24, can be cut to help installation
- Service Bulletin Effectivity updated.
SUMMARY
MATERIAL PRICE INFORMATION
 MATERIAL PRICE INFORMATION TABLE
UPDATED
R
MATERIAL PRICE INFORMATION TABLE
UPDATED
R
MATERIAL PRICE INFORMATION TABLE
UPDATED
R
EFFECTIVITY
 OPERATOR LIST UPDATED
 R
REFERENCES / REPERCUSSIONS
 REFERENCES/REPERCUSSIONS TABLE
UPDATED
R
MANPOWER
 MANPOWER UPDATED
 R
MANPOWER UPDATED
 R
MANPOWER UPDATED
 R
APPENDICES
 APPENDICES UPDATED
 R
PLANNING INFORMATION
EFFECTIVITY
 EFFECTIVITY RELATED INFORMATION
UPDATED
R
Configuration definition
CONF 001
 CONFIGURATION DEFINITION UPDATED
 R
Material Effectivity
 MATERIAL EFFECTIVITY UPDATED
MATERIAL SET UPDATED
MATERIAL SET QUANTITY UPDATED
R
MATERIAL EFFECTIVITY UPDATED
MATERIAL SET UPDATED
MATERIAL SET QUANTITY UPDATED
R
MATERIAL EFFECTIVITY UPDATED
MATERIAL SET UPDATED
MATERIAL SET QUANTITY UPDATED
R
MANPOWER
 MANPOWER UPDATED
CONFIGURATION UPDATED
R
MANPOWER UPDATED
 R
MANPOWER UPDATED
CONFIGURATION UPDATED
R
REFERENCES
 REFERENCED DOCUMENTATION UPDATED
 R
REFERENCED DOCUMENTATION UPDATED
 R
REFERENCED DOCUMENTATION UPDATED
 R
MATERIAL INFORMATION
MATERIAL - PRICE AND AVAILABILITY
Procurement Addresses
 PROCUREMENT ADDRESSES UPDATED
MATERIAL SET UPDATED
R
DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103
REVISION No.: 05 - Aug 20/18 Page: 5
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 6

@A300-600
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET
Price and Availability
 PRICE AND AVAILABILITY UPDATED
MATERIAL AVAILABILITY UPDATED
MATERIAL SET UPDATED
MATERIAL PRICE UPDATED
R
LIST OF COMPONENTS
 LIST OF COMPONENTS UPDATED
 R
Kit 246103A01R15
 PART MATERIAL SET UPDATED
MATERIAL SET LABEL UPDATED
QUANTITY UPDATED
R
Kit 246103A02R13
 PART MATERIAL SET UPDATED
MATERIAL SET LABEL UPDATED
QUANTITY UPDATED
R
Kit 246103A06R00
 PART MATERIAL SET ADDED
 N
Kit 246103A07R00
 PART MATERIAL SET ADDED
 N
Supplementary Kit 246103A01S13
 PART MATERIAL SET UPDATED
 R
Kit 246103B01R03
 PART MATERIAL SET UPDATED
 R
Kit 246103B02R02
 PART MATERIAL SET UPDATED
 R
LIST OF MATERIALS - OPERATOR
SUPPLIED
Components
Component COMPB01
 PART MATERIAL SET UPDATED
 R
ACCOMPLISHMENT INSTRUCTIONS
TASK 246103- 831-801-001-Modification
 TASK SOLUTION UPDATED
NOTE UPDATED
R
Task associated data - 001
 ELAPSED TIME UPDATED
 R
Task associated data - 002
 ELAPSED TIME UPDATED
 R
Task associated data - 003
 ELAPSED TIME UPDATED
 R
Subtask 246103-839-401-001
 SUBTASK SOLUTION DELETED FOR
APPLICABLE MSN
D
Subtask 246103-910-001-001
 SUBTASK SOLUTION UPDATED
REFERENCED DOCUMENTATION UPDATED
REFERENCES UPDATED
R
Subtask 246103-910-401-001
 SUBTASK SOLUTION DELETED FOR
APPLICABLE MSN
D
Subtask 246103-839-401-001
 SUBTASK SOLUTION DELETED FOR
APPLICABLE MSN
D
Subtask 246103-910-001-001
 SUBTASK SOLUTION UPDATED
REFERENCED DOCUMENTATION UPDATED
REFERENCES UPDATED
R
Subtask 246103-910-401-001
 SUBTASK SOLUTION DELETED FOR
APPLICABLE MSN
D
Subtask 246103-839-401-001
 SUBTASK SOLUTION DELETED FOR
APPLICABLE MSN
D
Subtask 246103-910-001-001
 SUBTASK SOLUTION UPDATED
REFERENCED DOCUMENTATION UPDATED
REFERENCES UPDATED
R
Subtask 246103-910-401-001
 SUBTASK SOLUTION DELETED FOR
APPLICABLE MSN
D
DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103
REVISION No.: 05 - Aug 20/18 Page: 6
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 7

@A300-600
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET
Subtask 246103-941-001-001
 SUBTASK SOLUTION UPDATED
REFERENCED DOCUMENTATION UPDATED
CIRCUIT BREAKER UPDATED
PANEL UPDATED
REFERENCES UPDATED
R
Subtask 246103-941-401-001
 SUBTASK SOLUTION DELETED FOR
APPLICABLE MSN
D
Subtask 246103-941-001-001
 SUBTASK SOLUTION UPDATED
REFERENCED DOCUMENTATION UPDATED
CIRCUIT BREAKER UPDATED
PANEL UPDATED
REFERENCES UPDATED
R
Subtask 246103-941-401-001
 SUBTASK SOLUTION DELETED FOR
APPLICABLE MSN
D
Subtask 246103-941-001-001
 SUBTASK SOLUTION UPDATED
REFERENCED DOCUMENTATION UPDATED
CIRCUIT BREAKER UPDATED
PANEL UPDATED
REFERENCES UPDATED
R
Subtask 246103-941-401-001
 SUBTASK SOLUTION DELETED FOR
APPLICABLE MSN
D
Subtask 246103-831-001-001
 SUBTASK SOLUTION UPDATED
 R
Subtask 246103-831-019-001
 SUBTASK SOLUTION UPDATED
MATERIAL LIST UPDATED
R
Subtask 246103-420-001-001
 SUBTASK SOLUTION UPDATED
MATERIAL LIST UPDATED
R
Subtask 246103-831-003-001
 SUBTASK SOLUTION UPDATED
MATERIAL LIST UPDATED
R
Subtask 246103-831-006-001
 SUBTASK SOLUTION UPDATED
NOTE UPDATED
MATERIAL LIST UPDATED
R
Subtask 246103-831-010-001
 SUBTASK SOLUTION UPDATED
MATERIAL LIST UPDATED
R
Subtask 246103-831-011-001
 SUBTASK SOLUTION UPDATED
QUANTITY UPDATED
MATERIAL LIST UPDATED
R
Subtask 246103-831-012-001
 SUBTASK SOLUTION UPDATED
MATERIAL LIST UPDATED
R
Subtask 246103-020-002-001
 SUBTASK SOLUTION UPDATED
 R
Subtask 246103-831-005-001
 SUBTASK SOLUTION UPDATED
MATERIAL LIST UPDATED
R
Subtask 246103-420-002-001
 SUBTASK SOLUTION UPDATED
MATERIAL LIST UPDATED
R
Subtask 246103-831-004-001
 SUBTASK SOLUTION UPDATED
MATERIAL LIST UPDATED
R
Subtask 246103-831-007-001
 SUBTASK SOLUTION UPDATED
NOTE UPDATED
MATERIAL LIST UPDATED
R
DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103
REVISION No.: 05 - Aug 20/18 Page: 7
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 8

@A300-600
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET
Subtask 246103-831-013-001
 SUBTASK SOLUTION UPDATED
MATERIAL LIST UPDATED
R
Subtask 246103-831-401-001
 SUBTASK SOLUTION UPDATED
MATERIAL LIST UPDATED
R
Subtask 246103-831-008-001
 SUBTASK SOLUTION UPDATED
MATERIAL LIST UPDATED
R
Subtask 246103-831-009-001
 SUBTASK SOLUTION UPDATED
MATERIAL LIST UPDATED
R
Subtask 246103-831-017-001
 SUBTASK SOLUTION UPDATED
MATERIAL LIST UPDATED
R
Subtask 246103-831-018-001
 SUBTASK SOLUTION UPDATED
MATERIAL LIST UPDATED
R
Subtask 246103-831-405-001
 SUBTASK SOLUTION UPDATED
QUANTITY UPDATED
MATERIAL LIST UPDATED
R
Subtask 246103-831-001-001
 SUBTASK SOLUTION UPDATED
 R
Subtask 246103-831-019-001
 SUBTASK SOLUTION UPDATED
MATERIAL LIST UPDATED
R
Subtask 246103-420-001-001
 SUBTASK SOLUTION UPDATED
MATERIAL LIST UPDATED
R
Subtask 246103-831-003-001
 SUBTASK SOLUTION UPDATED
MATERIAL LIST UPDATED
R
Subtask 246103-831-006-001
 SUBTASK SOLUTION UPDATED
NOTE UPDATED
MATERIAL LIST UPDATED
R
Subtask 246103-831-010-001
 SUBTASK SOLUTION UPDATED
MATERIAL LIST UPDATED
R
Subtask 246103-831-011-001
 SUBTASK SOLUTION UPDATED
QUANTITY UPDATED
MATERIAL LIST UPDATED
R
Subtask 246103-831-012-001
 SUBTASK SOLUTION UPDATED
MATERIAL LIST UPDATED
R
Subtask 246103-020-002-001
 SUBTASK SOLUTION UPDATED
 R
Subtask 246103-831-005-001
 SUBTASK SOLUTION UPDATED
MATERIAL LIST UPDATED
R
Subtask 246103-420-002-001
 SUBTASK SOLUTION UPDATED
MATERIAL LIST UPDATED
R
Subtask 246103-831-004-001
 SUBTASK SOLUTION UPDATED
MATERIAL LIST UPDATED
R
Subtask 246103-831-007-001
 SUBTASK SOLUTION UPDATED
NOTE UPDATED
MATERIAL LIST UPDATED
R
Subtask 246103-831-013-001
 SUBTASK SOLUTION UPDATED
MATERIAL LIST UPDATED
R
Subtask 246103-831-401-002
 SUBTASK SOLUTION UPDATED
MATERIAL LIST UPDATED
R
Subtask 246103-831-008-001
 SUBTASK SOLUTION UPDATED
MATERIAL LIST UPDATED
R
DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103
REVISION No.: 05 - Aug 20/18 Page: 8
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 9

@A300-600
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET
Subtask 246103-831-009-001
 SUBTASK SOLUTION UPDATED
MATERIAL LIST UPDATED
R
Subtask 246103-831-017-003
 SUBTASK SOLUTION UPDATED
MATERIAL LIST UPDATED
R
Subtask 246103-831-018-003
 SUBTASK SOLUTION UPDATED
MATERIAL LIST UPDATED
R
Subtask 246103-831-405-002
 SUBTASK SOLUTION UPDATED
QUANTITY UPDATED
MATERIAL LIST UPDATED
R
Subtask 246103-831-001-001
 SUBTASK SOLUTION UPDATED
 R
Subtask 246103-831-019-001
 SUBTASK SOLUTION UPDATED
MATERIAL LIST UPDATED
R
Subtask 246103-420-001-001
 SUBTASK SOLUTION UPDATED
MATERIAL LIST UPDATED
R
Subtask 246103-831-003-001
 SUBTASK SOLUTION UPDATED
MATERIAL LIST UPDATED
R
Subtask 246103-831-006-002
 SUBTASK SOLUTION UPDATED
NOTE UPDATED
MATERIAL LIST UPDATED
R
Subtask 246103-831-010-001
 SUBTASK SOLUTION UPDATED
MATERIAL LIST UPDATED
R
Subtask 246103-831-011-001
 SUBTASK SOLUTION UPDATED
QUANTITY UPDATED
MATERIAL LIST UPDATED
R
Subtask 246103-831-012-001
 SUBTASK SOLUTION UPDATED
MATERIAL LIST UPDATED
R
Subtask 246103-020-002-001
 SUBTASK SOLUTION UPDATED
 R
Subtask 246103-831-005-001
 SUBTASK SOLUTION UPDATED
MATERIAL LIST UPDATED
R
Subtask 246103-420-002-001
 SUBTASK SOLUTION UPDATED
MATERIAL LIST UPDATED
R
Subtask 246103-831-004-001
 SUBTASK SOLUTION UPDATED
MATERIAL LIST UPDATED
R
Subtask 246103-831-007-002
 SUBTASK SOLUTION UPDATED
NOTE UPDATED
MATERIAL LIST UPDATED
R
Subtask 246103-831-013-001
 SUBTASK SOLUTION UPDATED
MATERIAL LIST UPDATED
R
Subtask 246103-831-401-001
 SUBTASK SOLUTION UPDATED
MATERIAL LIST UPDATED
R
Subtask 246103-831-008-001
 SUBTASK SOLUTION UPDATED
MATERIAL LIST UPDATED
R
Subtask 246103-831-009-001
 SUBTASK SOLUTION UPDATED
MATERIAL LIST UPDATED
R
Subtask 246103-831-017-001
 SUBTASK SOLUTION UPDATED
MATERIAL LIST UPDATED
R
Subtask 246103-831-018-001
 SUBTASK SOLUTION UPDATED
MATERIAL LIST UPDATED
R
DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103
REVISION No.: 05 - Aug 20/18 Page: 9
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 10

@A300-600
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET
Subtask 246103-831-405-001
 SUBTASK SOLUTION UPDATED
QUANTITY UPDATED
MATERIAL LIST UPDATED
R
Subtask 246103-942-001-001
 SUBTASK SOLUTION UPDATED
REFERENCED DOCUMENTATION UPDATED
PANEL UPDATED
CIRCUIT BREAKER UPDATED
REFERENCES UPDATED
R
Subtask 246103-942-401-001
 SUBTASK SOLUTION DELETED FOR
APPLICABLE MSN
D
Subtask 246103-942-001-001
 SUBTASK SOLUTION UPDATED
REFERENCED DOCUMENTATION UPDATED
PANEL UPDATED
CIRCUIT BREAKER UPDATED
REFERENCES UPDATED
R
Subtask 246103-942-401-001
 SUBTASK SOLUTION DELETED FOR
APPLICABLE MSN
D
Subtask 246103-942-001-001
 SUBTASK SOLUTION UPDATED
REFERENCED DOCUMENTATION UPDATED
PANEL UPDATED
CIRCUIT BREAKER UPDATED
REFERENCES UPDATED
R
Subtask 246103-942-401-001
 SUBTASK SOLUTION DELETED FOR
APPLICABLE MSN
D
TASK 246103- 831-802-001-Modification -
ADDITIONAL WORK between Revision
No. 00 and Revision No. 05
TASK SOLUTION UPDATED
TASK TITLE UPDATED
NOTE UPDATED
R
Subtask 246103-910-002-001
 SUBTASK SOLUTION UPDATED
REFERENCED DOCUMENTATION UPDATED
REFERENCES UPDATED
R
Subtask 246103-910-002-001
 SUBTASK SOLUTION UPDATED
REFERENCED DOCUMENTATION UPDATED
REFERENCES UPDATED
R
Subtask 246103-910-002-001
 SUBTASK SOLUTION UPDATED
REFERENCED DOCUMENTATION UPDATED
REFERENCES UPDATED
R
Subtask 246103-831-028-001
 SUBTASK SOLUTION UPDATED
NOTE UPDATED
MATERIAL LIST UPDATED
R
Subtask 246103-831-020-001
 SUBTASK SOLUTION UPDATED
NOTE UPDATED
MATERIAL LIST UPDATED
R
Subtask 246103-400-001-001
 SUBTASK SOLUTION UPDATED
QUANTITY UPDATED
MATERIAL LIST UPDATED
R
Subtask 246103-420-005-001
 SUBTASK SOLUTION UPDATED
 R
Subtask 246103-420-006-001
 SUBTASK SOLUTION UPDATED
 R
Subtask 246103-831-028-001
 SUBTASK SOLUTION UPDATED
NOTE UPDATED
MATERIAL LIST UPDATED
R
DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103
REVISION No.: 05 - Aug 20/18 Page: 10
5
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### Page 11

@A300-600
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET
Subtask 246103-831-020-001
 SUBTASK SOLUTION UPDATED
NOTE UPDATED
MATERIAL LIST UPDATED
R
Subtask 246103-400-001-001
 SUBTASK SOLUTION UPDATED
QUANTITY UPDATED
MATERIAL LIST UPDATED
R
Subtask 246103-420-005-001
 SUBTASK SOLUTION UPDATED
 R
Subtask 246103-420-006-001
 SUBTASK SOLUTION UPDATED
 R
Subtask 246103-831-028-002
 SUBTASK SOLUTION UPDATED
NOTE UPDATED
R
Subtask 246103-831-020-002
 SUBTASK SOLUTION UPDATED
NOTE UPDATED
R
Subtask 246103-400-001-001
 SUBTASK SOLUTION UPDATED
QUANTITY UPDATED
MATERIAL LIST UPDATED
R
Subtask 246103-420-005-001
 SUBTASK SOLUTION UPDATED
 R
Subtask 246103-420-006-001
 SUBTASK SOLUTION UPDATED
 R
TASK 246103- 831-804-001-Modification -
ADDITIONAL WORK between Revision
No. 01 and Revision No. 05
TASK SOLUTION UPDATED
TASK TITLE UPDATED
NOTE UPDATED
R
Subtask 246103-910-003-001
 SUBTASK SOLUTION UPDATED
REFERENCED DOCUMENTATION UPDATED
REFERENCES UPDATED
R
Subtask 246103-910-003-001
 SUBTASK SOLUTION UPDATED
REFERENCED DOCUMENTATION UPDATED
REFERENCES UPDATED
R
Subtask 246103-910-003-001
 SUBTASK SOLUTION UPDATED
REFERENCED DOCUMENTATION UPDATED
REFERENCES UPDATED
R
Subtask 246103-420-007-001
 SUBTASK SOLUTION UPDATED
 R
Subtask 246103-420-009-001
 SUBTASK SOLUTION UPDATED
QUANTITY UPDATED
MATERIAL LIST UPDATED
R
Subtask 246103-831-033-001
 SUBTASK SOLUTION UPDATED
QUANTITY UPDATED
NOTE UPDATED
MATERIAL LIST UPDATED
R
Subtask 246103-420-008-001
 SUBTASK SOLUTION UPDATED
 R
Subtask 246103-420-010-001
 SUBTASK SOLUTION UPDATED
QUANTITY UPDATED
MATERIAL LIST UPDATED
R
Subtask 246103-831-050-001
 SUBTASK SOLUTION UPDATED
NOTE UPDATED
R
Subtask 246103-420-007-001
 SUBTASK SOLUTION UPDATED
 R
Subtask 246103-420-009-001
 SUBTASK SOLUTION UPDATED
QUANTITY UPDATED
MATERIAL LIST UPDATED
R
DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103
REVISION No.: 05 - Aug 20/18 Page: 11
5
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### Page 12

@A300-600
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET
Subtask 246103-831-033-001
 SUBTASK SOLUTION UPDATED
QUANTITY UPDATED
NOTE UPDATED
MATERIAL LIST UPDATED
R
Subtask 246103-420-008-001
 SUBTASK SOLUTION UPDATED
 R
Subtask 246103-420-010-001
 SUBTASK SOLUTION UPDATED
QUANTITY UPDATED
MATERIAL LIST UPDATED
R
Subtask 246103-831-050-001
 SUBTASK SOLUTION UPDATED
NOTE UPDATED
R
Subtask 246103-420-007-001
 SUBTASK SOLUTION UPDATED
 R
Subtask 246103-420-009-001
 SUBTASK SOLUTION UPDATED
QUANTITY UPDATED
MATERIAL LIST UPDATED
R
Subtask 246103-831-033-002
 SUBTASK SOLUTION UPDATED
QUANTITY UPDATED
NOTE UPDATED
MATERIAL LIST UPDATED
R
Subtask 246103-420-008-001
 SUBTASK SOLUTION UPDATED
 R
Subtask 246103-420-010-001
 SUBTASK SOLUTION UPDATED
QUANTITY UPDATED
MATERIAL LIST UPDATED
R
Subtask 246103-831-050-002
 SUBTASK SOLUTION UPDATED
NOTE UPDATED
R
TASK 246103- 831-805-001-Modification -
ADDITIONAL WORK between Revision
No. 02 and Revision No. 05
TASK SOLUTION UPDATED
TASK TITLE UPDATED
NOTE UPDATED
R
Task associated data - 001
 ELAPSED TIME UPDATED
 R
Task associated data - 002
 ELAPSED TIME UPDATED
 R
Subtask 246103-910-005-001
 SUBTASK SOLUTION UPDATED
REFERENCED DOCUMENTATION UPDATED
REFERENCES UPDATED
R
Subtask 246103-910-005-001
 SUBTASK SOLUTION UPDATED
REFERENCED DOCUMENTATION UPDATED
REFERENCES UPDATED
R
Subtask 246103-910-005-001
 SUBTASK SOLUTION UPDATED
REFERENCED DOCUMENTATION UPDATED
REFERENCES UPDATED
R
TASK 246103- 831-806-001-Modification -
ADDITIONAL WORK between Revision
No. 03 and Revision No. 05
TASK SOLUTION ADDED
 N
Task associated data - 001
 TASK ASSOCIATED DATA ADDED
 N
Task associated data - 002
 TASK ASSOCIATED DATA ADDED
 N
Task associated data - 003
 TASK ASSOCIATED DATA ADDED
 N
Subtask 246103-910-007-001
 SUBTASK SOLUTION ADDED
 N
Subtask 246103-839-007-001
 SUBTASK SOLUTION ADDED
 N
Subtask 246103-910-007-001
 SUBTASK SOLUTION ADDED
 N
Subtask 246103-839-007-001
 SUBTASK SOLUTION ADDED
 N
Subtask 246103-941-008-001
 SUBTASK SOLUTION ADDED
 N
DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103
REVISION No.: 05 - Aug 20/18 Page: 12
5
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### Page 13

@A300-600
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET
Subtask 246103-941-008-001
 SUBTASK SOLUTION ADDED
 N
Subtask 246103-420-014-001
 SUBTASK SOLUTION ADDED
 N
Subtask 246103-420-015-001
 SUBTASK SOLUTION ADDED
 N
Subtask 246103-831-055-001
 SUBTASK SOLUTION ADDED
 N
Subtask 246103-831-046-001
 SUBTASK SOLUTION ADDED
 N
Subtask 246103-420-014-001
 SUBTASK SOLUTION ADDED
 N
Subtask 246103-420-015-001
 SUBTASK SOLUTION ADDED
 N
Subtask 246103-700-007-001
 SUBTASK SOLUTION ADDED
 N
Subtask 246103-700-007-001
 SUBTASK SOLUTION ADDED
 N
Subtask 246103-942-007-001
 SUBTASK SOLUTION ADDED
 N
Subtask 246103-942-007-001
 SUBTASK SOLUTION ADDED
 N
TASK 246103- 831-807-001-Modification -
ADDITIONAL WORK between Revision
No. 04 and Revision No. 05 and only if
Revision No. 03 is also Embodied
TASK SOLUTION ADDED
 N
Task associated data - 001
 TASK ASSOCIATED DATA ADDED
 N
Task associated data - 002
 TASK ASSOCIATED DATA ADDED
 N
Task associated data - 003
 TASK ASSOCIATED DATA ADDED
 N
Subtask 246103-910-008-001
 SUBTASK SOLUTION ADDED
 N
Subtask 246103-839-008-001
 SUBTASK SOLUTION ADDED
 N
Subtask 246103-910-008-001
 SUBTASK SOLUTION ADDED
 N
Subtask 246103-839-008-001
 SUBTASK SOLUTION ADDED
 N
Subtask 246103-941-009-001
 SUBTASK SOLUTION ADDED
 N
Subtask 246103-941-009-001
 SUBTASK SOLUTION ADDED
 N
Subtask 246103-420-016-001
 SUBTASK SOLUTION ADDED
 N
Subtask 246103-420-017-001
 SUBTASK SOLUTION ADDED
 N
Subtask 246103-420-016-001
 SUBTASK SOLUTION ADDED
 N
Subtask 246103-420-017-001
 SUBTASK SOLUTION ADDED
 N
Subtask 246103-700-008-001
 SUBTASK SOLUTION ADDED
 N
Subtask 246103-700-008-001
 SUBTASK SOLUTION ADDED
 N
Subtask 246103-942-008-001
 SUBTASK SOLUTION ADDED
 N
Subtask 246103-942-008-001
 SUBTASK SOLUTION ADDED
 N
Fig. A-FBAAA
Fig. A-FBAAA Sheet 01
 SHEET UPDATED
 R
Fig. A-FBAAA Sheet 03
 SHEET UPDATED
 R
Fig. A-FBBAA
Fig. A-FBBAA Sheet 01
 SHEET UPDATED
 R
Fig. A-FBBAA Sheet 02
 SHEET UPDATED
 R
Fig. A-FBFAA
Fig. A-FBFAA Sheet 01
 SHEET UPDATED
 R
Fig. A-FBFAA Sheet 02
 SHEET UPDATED
 R
Fig. A-FBDAA
Fig. A-FBDAA Sheet 03
 SHEET UPDATED
 R
Fig. A-FBDAB
Fig. A-FBDAB Sheet 02
 SHEET UPDATED
 R
DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103
REVISION No.: 05 - Aug 20/18 Page: 13
5
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### Page 14

@A300-600
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET
Fig. A-FBUAA
Fig. A-FBUAA Sheet 01
 SHEET UPDATED
 R
Fig. A-FBUAA Sheet 02
 SHEET UPDATED
 R
Fig. A-FBMAA
Fig. A-FBMAA Sheet 04
 SHEET UPDATED
 R
Fig. A-FBMAB
Fig. A-FBMAB Sheet 02
 SHEET UPDATED
 R
Fig. A-FBRAA
Fig. A-FBRAA Sheet 01
 SHEET UPDATED
 R
Fig. A-FBRAA Sheet 02
 SHEET UPDATED
 R
Fig. A-FBRAA Sheet 03
 SHEET UPDATED
 R
Fig. A-FCCAA
Fig. A-FCCAA Sheet 04
 SHEET UPDATED
 R
Fig. A-FCCAB
Fig. A-FCCAB Sheet 02
 SHEET UPDATED
 R
Fig. A-FCQAA
 FIGURE SOLUTION ADDED
 N
Fig. A-FCQAA Sheet 01
 SHEET ADDED
 N
Fig. A-FCQAA Sheet 02
 SHEET ADDED
 N
Fig. A-FCRAA
 FIGURE SOLUTION ADDED
 N
Fig. A-FCRAA Sheet 01
 SHEET ADDED
 N
Fig. A-FCRAA Sheet 02
 SHEET ADDED
 N
Fig. A-FCRAA Sheet 03
 SHEET ADDED
 N
Appendix 01 - Elapsed Time Assumption
APPENDIX CONTENT
 APPENDIX CONTENT UPDATED
 R
Fig. A-FAAAA
 FIGURE SOLUTION UPDATED
 R
Fig. A-FAAAA Sheet 01
 SHEET UPDATED
 R
Fig. A-FAAAA Sheet 02
 SHEET ADDED
 N
Fig. A-FABAA
 FIGURE SOLUTION UPDATED
 R
Fig. A-FABAA Sheet 01
 SHEET UPDATED
 R
Fig. A-FABAA Sheet 02
 SHEET ADDED
 N
Appendix 02 - Elapsed Time Assumption - ADDITIONAL WORK between Revision No. 00 and
Revision No. 05
APPENDIX CONTENT
 APPENDIX CONTENT UPDATED
 R
Fig. A-FACAA
 FIGURE SOLUTION UPDATED
 R
Fig. A-FACAA Sheet 01
 SHEET UPDATED
 R
Fig. A-FACAA Sheet 02
 SHEET ADDED
 N
Appendix 03 - Elapsed Time Assumption - ADDITIONAL WORK between Revision No. 01 and
Revision No. 05
APPENDIX CONTENT
 APPENDIX CONTENT UPDATED
 R
Fig. A-FADAA
 FIGURE SOLUTION UPDATED
 R
DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103
REVISION No.: 05 - Aug 20/18 Page: 14
5
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### Page 15

@A300-600
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET
Appendix 04 - Elapsed Time Assumption - ADDITIONAL WORK between Revision No. 02 and
Revision No. 05
APPENDIX CONTENT
 APPENDIX CONTENT UPDATED
 R
Fig. A-FAFAA
 FIGURE SOLUTION UPDATED
 R
Fig. A-FAFAB
 FIGURE SOLUTION UPDATED
 R
Appendix 05 - Elapsed Time Assumption - ADDITIONAL WORK between Revision No. 03 and
Revision No. 05
APPENDIX CONTENT
 APPENDIX CONTENT ADDED
 N
Fig. A-FAGAA
 FIGURE SOLUTION ADDED
 N
Fig. A-FAGAA Sheet 01
 SHEET ADDED
 N
Fig. A-FAGAB
 FIGURE SOLUTION ADDED
 N
Fig. A-FAGAB Sheet 01
 SHEET ADDED
 N
Appendix 06 - Elapsed Time Assumption - ADDITIONAL WORK between Revision No. 04 and
Revision No. 05 and only if Revision No. 03 was also Embodied
APPENDIX CONTENT
 APPENDIX CONTENT ADDED
 N
Fig. A-FAHAA
 FIGURE SOLUTION ADDED
 N
Fig. A-FAHAA Sheet 01
 SHEET ADDED
 N
FILING 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 issued to :
review all technical definition,
add illustrations,
improve major changes.
Revision No. 02 issued to :
review the technical definition,
add illustrations,
improve major changes.
Revision No. 03 issued to update the installation of clamps in LH and RH wings and on the passage
way to the shroud box at LH and RH sides.
Revision No. 04 issued to:
modify quantity of the Guide PN A9245000200000, value 1 instead of 2 in Kit 246103B01R03,
DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103
REVISION No.: 05 - Aug 20/18 Page: 15
5
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### Page 16

@A300-600
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET
modify kit reference in Subtasks 246103-931-006-001 and 246103-831-007-001,
add note for Kit 246103A01S13 and for Kit 246103A03R06,
review the installation of the Item 60,
replace LH wing by RH wing in Subtask 246103-831-054-001,
modify the routing on Rib 1 on the passage way to the shroud box at LH and RH side updated in
Config. 003,
add the PN NSA360002 Item 87, in Kits 246103A01S14, 246103A01S15, 246103A02S12 and
246103A02S13.
REVISION SEQUENCE
ORIGINAL: Jun 17/10
REVISION No. : 01 - Feb 21/12
REVISION No. : 02 - Feb 07/13
REVISION No. : 03 - Jul 03/15
REVISION No. : 04 - Feb 10/16
REVISION No. : 05 - Aug 20/18
DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103
REVISION No.: 05 - Aug 20/18 Page: 16
5
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### Page 17

@A300-600
SERVICE BULLETIN
SUMMARY
AIRBUS
CUSTOMER SERVICES DIRECTORATE
1 Rond Point Maurice Bellonte
31707 BLAGNAC CEDEX
FRANCE
T e l:( 3 3 )56 19 33 33 3
Telex : AIRBU 530526F
F a x:( 3 3 )56 19 34 25 1
This summary is for information only and is not approved for modification of the aircraft.
MANDATORY
 MANDATORY
 MANDATORY
ATA SYSTEM: 24
TITLE: ELECTRIC AND ELECTRONIC COMMON INSTALLATIONS - IMPROVE
WING WIRING INSTALLATION
**CONF ALL
MODIFICATIONS
MODIFICATION CLASSIFICATION
MAJOR
 13397S22766
 13399S22768
 13516H5723
MINOR
 None
NOTE
: As per EASA IR 21, a minor change is one that has no appreciable effect on the
mass, balance, structural strength, reliability, operational characteristics affecting the
airworthiness of the product. All other changes are major changes.
REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES
The A300-600 aircraft operator’s feedback further to the accomplishment of the mandatory Inspection
Service Bulletin No. A300-24-6092 and a review of the wing electrical installation at the AIRBUS final
assembly line have shown that the wing electrical installation doesn’t comply with the minimum distance
inspection criteria to the surrounding structure in a few wing locations.
This Service Bulletin requires:
- The installation of new bracket assemblies to improve the electrical harnesses installation and
secure the clearance to the structure in identified locations,
- The installation of protective split sleeve as mechanical protection to the electrical harnesses in
areas where the minimum distance to the structure cannot be achieved.
Accomplishment of this modification Service Bulletin will improve the wing electrical installation in the
identified areas and prevent possible chafing and subsequent damage to the electrical harnesses and
surrounding structure.
GENERAL EVALUATION
EVALUATION TABLE
COMPLIANCE
 MANDATORY (1)
 CANCELS INSPECTION SB
 NO
DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103
REVISION No.: 05 - Aug 20/18 Page: 1
5
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### Page 18

@A300-600
SERVICE BULLETIN
SUMMARY
EVALUATION TABLE
POTENTIAL AD
 YES
 A/C OPERATION AFFECTED
 NO
RELIABILITY AFFECTED
 NO
 PAX COMFORT AFFECTED
 NO
COST SAVING
 NO
 ETOPS AFFECTED
 NO
STRUCTURAL LIFE EXTN
 NO
 VENDOR SB INVOLVED
 NO
VALIDATION ON AIRCRAFT
 YES
 BOOKLET AVAILABLE
 YES
NOTE
 (1)
: Service Bulletin must be accomplished.
NOTE
: This Service Bulletin has been validated at Revision No. 00 on A300 aircraft with
Manufacturer Serial Number (MSN) 0284.
NOTE
: A booklet including photographs taken during the validation of this Service Bulletin is
available on AIRBUS|World - Maintenance and Engineering - AirN@v engineering (in
the concerned SB file).
MATERIAL PRICE INFORMATION
**CONF 001
MATERIAL PRICE INFORMATION TABLE
MATERIAL SET
 QTY PER
A/C
PRICE PER
A/C (USD)
MAIN PARTS
Kit
 246103A01R15
 1
 5,530.00
 Seal fitting, support, conduit, spacer
Kit
 246103A02R13
 1
 4,130.00
 Conduit, spacer
Kit 246103A03R06
 2
 110.00
 Spacer, screw
Kit
 246103A06R00
 2
 100.00
 Screws, washers, nuts
Supplementary kit
246103A01S03
1
 3,090.00
 Bracket
Supplementary kit
246103A01S08
1
 4,670.00
 Bracket
Supplementary kit
246103A01S14
1
 196.00
 Clamps
Supplementary kit
246103A01S15
1
 227.00
 Clamps
Supplementary kit
246103A01S13
1
 55.00
 Rivets
Supplementary kit
246103A02S03
1
 2,330.00
 Bracket
Supplementary kit
246103A02S07
1
 3,210.00
 Bracket
Supplementary kit
246103A02S12
1
 196.00
 Clamps
Supplementary kit
246103A02S13
1
 227.00
 Clamps
Kit 246103B01R03
 2
 4,020.00
 Bracket assemblies and guide
TOTAL
 28,091.00
Component COMPB01
 1
 See SB
DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103
REVISION No.: 05 - Aug 20/18 Page: 2
5
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### Page 19

@A300-600
SERVICE BULLETIN
SUMMARY
**CONF 002
MATERIAL PRICE INFORMATION TABLE
MATERIAL SET
 QTY PER
A/C
PRICE PER
A/C (USD)
MAIN PARTS
Kit
 246103A01R15
 1
 5,530.00
 Seal fitting, support, conduit, spacer
Kit
 246103A02R13
 1
 4,130.00
 Conduit, spacer
Supplementary kit
246103A01S03
1
 3,090.00
 Bracket
Supplementary kit
246103A01S08
1
 4,670.00
 Bracket
Supplementary kit
246103A01S14
1
 196.00
 Clamps
Supplementary kit
246103A01S15
1
 227.00
 Clamps
Supplementary kit
246103A01S13
1
 55.00
 Rivets
Supplementary kit
246103A02S03
1
 2,330.00
 Bracket
Supplementary kit
246103A02S07
1
 3,210.00
 Bracket
Supplementary kit
246103A02S12
1
 196.00
 Clamps
Supplementary kit
246103A02S13
1
 227.00
 Clamps
Kit 246103B02R02
 2
 1,820.00
 Bracket assemblies
TOTAL
 25,681.00
**CONF 003
MATERIAL PRICE INFORMATION TABLE
MATERIAL SET
 QTY PER
A/C
PRICE PER
A/C (USD)
MAIN PARTS
Kit
 246103A01R15
 1
 5,530.00
 Seal fitting, support, conduit, spacer
Kit
 246103A02R13
 1
 4,130.00
 Conduit, spacer
Kit 246103A03R06
 2
 110.00
 Spacer, screw
Kit 246103A04R01
 1
 678.00
 Clamps
Kit 246103A05R01
 1
 678.00
 Clamps
Kit
 246103A06R00
 2
 100.00
 Screws, washers, nuts
Kit
 246103A07R00
 2
 100.00
 Screw, spacers, washer, nut
Supplementary kit
246103A01S03
1
 3,090.00
 Bracket
Supplementary kit
246103A01S08
1
 4,670.00
 Bracket
Supplementary kit
246103A01S14
1
 196.00
 Clamps
DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103
REVISION No.: 05 - Aug 20/18 Page: 3
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 20

@A300-600
SERVICE BULLETIN
SUMMARY
MATERIAL PRICE INFORMATION TABLE
MATERIAL SET
 QTY PER
A/C
PRICE PER
A/C (USD)
MAIN PARTS
Supplementary kit
246103A01S15
1
 227.00
 Clamps
Supplementary kit
246103A01S13
1
 55.00
 Rivets
Supplementary kit
246103A02S03
1
 2,330.00
 Bracket
Supplementary kit
246103A02S07
1
 3,210.00
 Bracket
Supplementary kit
246103A02S12
1
 196.00
 Clamps
Supplementary kit
246103A02S13
1
 227.00
 Clamps
Kit 246103B01R03
 2
 4,020.00
 Bracket assemblies and guide
TOTAL
 29,547.00
Component COMPB01
 1
 See SB
EFFECTIVITY
**CONF ALL
This Service Bulletin is applicable to this (these) operator(s) :
14S
 AAW
 ABR AHK BCS EFX
 FDX IRA IRM KAC MNB MRJ MSR
QSM
 SOP SUD TAR THA TNO
 UPS URS UTP
CONCURRENT REQUIREMENTS
None
REFERENCES / REPERCUSSIONS
TFU
 None
OEB
 None
AOT
 None
SIL
 None
ISI
 None
LINE MAINTENANCE AFFECTED
 No
LIFE LIMIT
 None
OTHER
 SBIT 16-0030 SBIT 16-0051
OTHER
 TA 80199484/013/2018 TA 80199484/026/2018 TA
80205706/003/2016
NATURE OF THE WORK
AIRCRAFT
 YES
EQUIPMENT
 NO
HARD
 NO
DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103
REVISION No.: 05 - Aug 20/18 Page: 4
5
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### Page 21

@A300-600
SERVICE BULLETIN
SUMMARY
SOFT
 NO
OBRM
 NO
MANPOWER
**CONF 001
Task 246103-831-801-001: Modification
TOTAL MANHOURS
 38.00
ELAPSED TIME (HOURS)
 21.75
Task 246103-831-802-001: Modification - ADDITIONAL WORK between Revision No. 00 and
Revision No. 05
TOTAL MANHOURS
 24.50
ELAPSED TIME (HOURS)
 16.50
Task 246103-831-804-001: Modification - ADDITIONAL WORK between Revision No. 01 and
Revision No. 05
TOTAL MANHOURS
 30.50
ELAPSED TIME (HOURS)
 16.50
Task 246103-831-805-001: Modification - ADDITIONAL WORK between Revision No. 02 and
Revision No. 05
TOTAL MANHOURS
 17.50
ELAPSED TIME (HOURS)
 9.00
Task 246103-831-806-001: Modification - ADDITIONAL WORK between Revision No. 03 and
Revision No. 05
TOTAL MANHOURS
 10.00
ELAPSED TIME (HOURS)
 5.25
Task 246103-831-807-001: Modification - ADDITIONAL WORK between Revision No. 04 and
Revision No. 05 and only if Revision No. 03 is also Embodied
TOTAL MANHOURS
 10.00
ELAPSED TIME (HOURS)
 5.25
**CONF 002
Task 246103-831-801-001: Modification
TOTAL MANHOURS
 36.00
ELAPSED TIME (HOURS)
 21.25
Task 246103-831-802-001: Modification - ADDITIONAL WORK between Revision No. 00 and
Revision No. 05
TOTAL MANHOURS
 24.50
ELAPSED TIME (HOURS)
 16.50
DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103
REVISION No.: 05 - Aug 20/18 Page: 5
5
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@A300-600
SERVICE BULLETIN
SUMMARY
Task 246103-831-804-001: Modification - ADDITIONAL WORK between Revision No. 01 and
Revision No. 05
TOTAL MANHOURS
 30.50
ELAPSED TIME (HOURS)
 16.50
Task 246103-831-805-001: Modification - ADDITIONAL WORK between Revision No. 02 and
Revision No. 05
TOTAL MANHOURS
 17.50
ELAPSED TIME (HOURS)
 9.00
**CONF 003
Task 246103-831-801-001: Modification
TOTAL MANHOURS
 38.00
ELAPSED TIME (HOURS)
 21.75
Task 246103-831-802-001: Modification - ADDITIONAL WORK between Revision No. 00 and
Revision No. 05
TOTAL MANHOURS
 24.50
ELAPSED TIME (HOURS)
 16.50
Task 246103-831-804-001: Modification - ADDITIONAL WORK between Revision No. 01 and
Revision No. 05
TOTAL MANHOURS
 30.50
ELAPSED TIME (HOURS)
 16.50
Task 246103-831-805-001: Modification - ADDITIONAL WORK between Revision No. 02 and
Revision No. 05
TOTAL MANHOURS
 18.50
ELAPSED TIME (HOURS)
 9.50
Task 246103-831-806-001: Modification - ADDITIONAL WORK between Revision No. 03 and
Revision No. 05
TOTAL MANHOURS
 11.00
ELAPSED TIME (HOURS)
 5.75
Task 246103-831-807-001: Modification - ADDITIONAL WORK between Revision No. 04 and
Revision No. 05 and only if Revision No. 03 is also Embodied
TOTAL MANHOURS
 10.00
ELAPSED TIME (HOURS)
 5.25
APPENDICES
**CONF ALL
Appendix 01 - Elapsed Time Assumption
Appendix 02 - Elapsed Time Assumption - ADDITIONAL WORK between Revision No. 00 and Revision
No. 05
DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103
REVISION No.: 05 - Aug 20/18 Page: 6
5
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@A300-600
SERVICE BULLETIN
SUMMARY
Appendix 03 - Elapsed Time Assumption - ADDITIONAL WORK between Revision No. 01 and Revision
No. 05
Appendix 04 - Elapsed Time Assumption - ADDITIONAL WORK between Revision No. 02 and Revision
No. 05
Appendix 05 - Elapsed Time Assumption - ADDITIONAL WORK between Revision No. 03 and Revision
No. 05
Appendix 06 - Elapsed Time Assumption - ADDITIONAL WORK between Revision No. 04 and Revision
No. 05 and only if Revision No. 03 was also Embodied
DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103
REVISION No.: 05 - Aug 20/18 Page: 7
5
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@A300-600
SERVICE BULLETIN
SUMMARY
**CONF ALL
Z572
Z571Z513
Z613
Z672
 − Z147 Z148
D_SB_246103_5_SAAA_01_01
ZONES WITH ROUTING TO MODIFY
Figure A-FSAAA - Sheet 01
DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103
REVISION No.: 05 - Aug 20/18 Page: 8
5
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### Page 25

@A300-600
SERVICE BULLETIN
AIRBUS
CUSTOMER SERVICES DIRECTORATE
1 Rond Point Maurice Bellonte
31707 BLAGNAC CEDEX
FRANCE
T e l:( 3 3 )56 19 33 33 3
Telex : AIRBU 530526F
F a x:( 3 3 )56 19 34 25 1
MANDATORY
 MANDATORY
 MANDATORY
ATA SYSTEM: 24
TITLE: ELECTRIC AND ELECTRONIC COMMON INSTALLATIONS - IMPROVE
WING WIRING INSTALLATION
MODIFICATION No.: 13397S22766 13399S22768 13516H5723
This document contains AIRBUS PROPRIETARY INFORMATION and shall at all times remain the
property of AIRBUS; no intellectual property right or licence is granted by AIRBUS in connection with
any information contained in it. It is delivered on the express condition that said document and the
information contained in it shall be treated as confidential, shall not be used for any purpose other than
that for which it is hereby delivered. It shall not be disclosed in whole or in part to third parties and shall
not be duplicated in any manner (except for the purposes of performing the tasks described hereunder
and provided that any recipient of such document shall comply with the conditions herein), without
AIRBUS prior written consent.
1. PLANNING INFORMATION
**CONF ALL
A. EFFECTIVITY
(1) Models
B4-603 B4-605R B4-622 B4-622R C4-605R/FC4-620 F4-605R F4-622R
(2) Effectivity by MSN
0344 0358 0361 0365 0380 0388 0401 0405 0408 0411 0414 0417 0477 0479 0505
0521 0525 0530 0532 0536 0543 0546 0553 0555 0557-0559 0561 0563 0572 0575
0579 0581 0584 0602-0603 0607-0608 0611 0613 0617-0618 0621 0623 0625-0626
0629-0630 0632-0633 0637 0641 0643 0657 0659 0664 0666 0668 0670 0677 0679
0683 0688 0694 0696 0699 0701 0703 0707 0709 0711 0713 0715 0717 0719
0721-0730 0732-0746 0748-0750 0752-0764 0766 0768-0775 0777-0794 0797
0799-0840 0845-0878
(3) Effectivity by Operator
The Operator/MSN relationship is provided for information only and is correct at the time
of issue in accordance with the information available to AIRBUS. Any future changes
resulting from transfer of an aircraft from one operator to another will not be reflected in
this list unless the Service Bulletin is revised for another reason.
DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103
REVISION No.: 05 - Aug 20/18 Page: 1
5
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@A300-600
SERVICE BULLETIN
OPERATOR
 MSN
14S
 0694
 0699
 0719
 0721
 0782
 0784
 0785
 0786
 0787
AAW
 0788
ABR
 0557 0677
 0717 0722
AHK
 0683 0770 0855 0856 0857 0858 0859 0860 0870 0871
BCS
 0602 0617 0621 0637 0641 0670 0679 0703 0711 0724 0729 0730
0737 0740 0743 0753 0783 0797 0836 0837 0872
EFX
 0755
FDX
 0358 0361 0365 0388 0417 0477 0479 0530 0536 0543 0555 0559
0572 0575 0579 0581 0611 0613 0625 0630 0633 0657 0659 0664
0668 0688 0709 0713 0715 0726 0728 0735 0736 0738 0742 0745
0748 0752 0757 0759 0760 0761 0766 0768 0769 0771 0772 0774
0777 0778 0779 0780 0781 0789 0790 0791 0792 0793 0794 0799
0800 0801 0802 0803 0804 0873 0874 0875 0876 0877 0878
IRA
 0632 0696 0723 0727
IRM
 0380 0401 0405 0408 0411 0414 0546 0553 0608 0618 0623 0701
0773 0838
KAC
 0344
MNB
 0521 0525 0734 0739 0756 0758
MRJ
 0750 0762
MSR
 0561 0607
QSM
 0584
 0603
 0744
 0749
 0764
SOP
 0532
SUD
 0666 0775
TAR
 0505 0558 0563
THA
 0629
TNO
 0626
 0643
UPS
 0805 0806 0807 0808 0809 0810 0811 0812 0813 0814 0815 0816
0817 0818 0819 0820 0821 0822 0823 0824 0825 0826 0827 0828
0829 0830 0831 0832 0833 0834 0835 0839 0840 0845 0846 0847
0848 0849 0850 0851 0852 0853 0854 0861 0862 0863 0864 0865
0866 0867 0868 0869
URS
 0733
UTP
 0707 0725 0732 0741 0746 0754 0763
(4) Configuration by MSN
MSN
 CONFIGURATION
0344 0380 0401 0405 0408 0411 0414 0505 0521 0525 0532
0546 0553 0558 0563 0584 0603 0608 0618 0623 0626 0632
0643 0694 0696 0699 0701 0707 0709 0713 0715 0719 0721
0725 0732 0741 0744 0746 0749 0754 0755 0758 0763 0764
0773
001
DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103
REVISION No.: 05 - Aug 20/18 Page: 2
5
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### Page 27

@A300-600
SERVICE BULLETIN
MSN
 CONFIGURATION
0358 0361 0365 0388 0417 0477 0479 0530 0536 0543 0555
0557 0559 0561 0572 0575 0579 0581 0602 0607 0611 0613
0617 0621 0625 0629 0630 0633 0637 0641 0657 0659 0664
0666 0668 0670 0677 0679 0683 0688 0703 0711 0717 0722
0724 0729 0730 0733 0734 0737 0739 0740 0743 0750 0753
0756 0762 0770 0775 0782 0783 0784 0785 0786 0787 0788
0797 0805 0806 0807 0808 0809 0810 0811 0812 0813 0814
0815 0816 0817 0818 0819 0820 0821 0822 0823 0824 0825
0826 0827 0828 0829 0830 0831 0832 0833 0834 0835 0836
0837 0838 0839 0840 0845 0846 0847 0848 0849 0850 0851
0852 0853 0854 0861 0862 0863 0864 0865 0866 0867 0868
0869 0872
003
0723 0726 0727 0728 0735 0736 0738 0742 0745 0748 0752
0757 0759 0760 0761 0766 0768 0769 0771 0772 0774 0777
0778 0779 0780 0781 0789 0790 0791 0792 0793 0794 0799
0800 0801 0802 0803 0804 0855 0856 0857 0858 0859 0860
0870 0871 0873 0874 0875 0876 0877 0878
002
(5) Configuration definition
**CONF 001
Config. 001 is valid for aircraft on which MOD No. 06127S6951 (Service Bulletin No.
A300-72-6006) and MOD No. 08966S20263 are not embodied.
**CONF 002
Config. 002 is valid for aircraft on which MOD No. 06127S6951 (Service Bulletin No.
A300-72-6006) is not embodied and MOD No. 08966S20263 is embodied.
**CONF 003
Config. 003 is valid for aircraft on which MOD No. 06127S6951 (Service Bulletin No.
A300-72-6006) is embodied and MOD No. 08966S20263 is not embodied.
(6) Material Effectivity
**CONF 001
MATERIAL
 QTY PER A/C
 SEE NOTES
Kit
 246103A01R15
 1
 (1)
Kit
 246103A02R13
 1
 (2)
Kit 246103A03R06
 2
 (3)
Kit
 246103A06R00
 2
 (4
)
Supplementary kit 246103A01S03
 1
Supplementary kit 246103A01S08
 1
Supplementary kit 246103A01S14
 1
Supplementary kit 246103A01S15
 1
Supplementary kit 246103A01S13
 1
Supplementary kit 246103A02S03
 1
Supplementary kit 246103A02S07
 1
DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103
REVISION No.: 05 - Aug 20/18 Page: 3
5
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@A300-600
SERVICE BULLETIN
MATERIAL
 QTY PER A/C
 SEE NOTES
Supplementary kit 246103A02S12
 1
Supplementary kit 246103A02S13
 1
Kit 246103B01R03
 2
 (5
)
Consumable CMLB01
 1
Consumable CMLA01
 1
Component COMPB01
 1
NOTE
 (1)
: Kit A01 concerns the work to be done on LH side of the aircraft.
NOTE
 (2)
: Kit A02 concerns the work to be done on RH side of the aircraft.
NOTE
 (3)
: Kit A03 concerns the installation of the guide in LH and RH wings.
NOTE
 (4)
: Kit A06 concerns the installation of the guide assembly in LH and RH
wings ADDITIONAL WORK.
NOTE
 (5)
: Kit B01 concerns the modification of the brackets in the outer shroud
box.
**CONF 002
MATERIAL
 QTY PER A/C
 SEE NOTES
Kit
 246103A01R15
 1
 (1)
Kit
 246103A02R13
 1
 (2)
Supplementary kit 246103A01S03
 1
Supplementary kit 246103A01S08
 1
Supplementary kit 246103A01S14
 1
Supplementary kit 246103A01S15
 1
Supplementary kit 246103A01S13
 1
Supplementary kit 246103A02S03
 1
Supplementary kit 246103A02S07
 1
Supplementary kit 246103A02S12
 1
Supplementary kit 246103A02S13
 1
Kit 246103B02R02
 2
 (3)
Consumable CMLA01
 1
Consumable CMLB01
 1
NOTE
 (1)
: Kit A01 concerns the work to be done on LH side of the aircraft.
NOTE
 (2)
: Kit A02 concerns the work to be done on RH side of the aircraft.
NOTE
 (3)
: Kit B02 concerns the modification of the brackets in the outer shroud
box.
DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103
REVISION No.: 05 - Aug 20/18 Page: 4
5
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@A300-600
SERVICE BULLETIN
**CONF 003
MATERIAL
 QTY PER A/C
 SEE NOTES
Kit
 246103A01R15
 1
 (1)
Kit
 246103A02R13
 1
 (2)
Kit 246103A03R06
 2
 (3)
Kit 246103A04R01
 1
 (4)
Kit 246103A05R01
 1
 (5)
Kit
 246103A06R00
 2
 (6
)
Kit
 246103A07R00
 2
 (7
)
Supplementary kit 246103A01S03
 1
Supplementary kit 246103A01S08
 1
Supplementary kit 246103A01S14
 1
Supplementary kit 246103A01S15
 1
Supplementary kit 246103A01S13
 1
Supplementary kit 246103A02S03
 1
Supplementary kit 246103A02S07
 1
Supplementary kit 246103A02S12
 1
Supplementary kit 246103A02S13
 1
Kit 246103B01R03
 2
 (8
)
Consumable CMLB01
 1
Consumable CMLA01
 1
Component COMPB01
 1
NOTE
 (1)
: Kit A01 concerns the work to be done on LH side of the aircraft.
NOTE
 (2)
: Kit A02 concerns the work to be done on RH side of the aircraft.
NOTE
 (3)
: Kit A03 concerns the installation of the guide in LH and RH wings.
NOTE
 (4)
: Kit A04 concerns the installation of the clamps on the Passage Way to
the Shroud box in LH side.
NOTE
 (5)
: Kit A05 concerns the installation of the clamps on the Passage Way to
the Shroud box in RH side.
NOTE
 (6)
: Kit A06 concerns the installation of the guide assembly in LH and RH
wings ADDITIONAL WORK.
NOTE
 (7)
: Kit A07 concerns the modification of the clamp on the routing at Rib 1
on the passageway to the shroud box at the in LH and RH wings
ADDITIONAL WORK.
NOTE
 (8)
: Kit B01 concerns the modification of the brackets in the outer shroud
box.
DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103
REVISION No.: 05 - Aug 20/18 Page: 5
5
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### Page 30

@A300-600
SERVICE BULLETIN
**CONF ALL
B. CONCURRENT REQUIREMENTS
None
C. REASON
(1) History
The A300-600 aircraft operator’s feedback further to the accomplishment of the
mandatory Inspection Service Bulletin No. A300-24-6092 and a review of the wing
electrical installation at the AIRBUS final assembly line have shown that the wing
electrical installation doesn’t comply with the minimum distance inspection criteria to the
surrounding structure in a few wing locations.
(2) Objective/Action
This Service Bulletin requires:
- The installation of new bracket assemblies to improve the electrical harnesses
installation and secure the clearance to the structure in identified locations,
- The installation of protective split sleeve as mechanical protection to the electrical
harnesses in areas where the minimum distance to the structure cannot be
achieved.
(3) Advantages
Accomplishment of this modification Service Bulletin will improve the wing electrical
installation in the identified areas and prevent possible chafing and subsequent damage
to the electrical harnesses and surrounding structure.
(4) Operational/Maintenance Consequences
None
D. DESCRIPTION
To accomplish this Service Bulletin it is necessary to :
**CONF 001
Task 246103-831-801-001: Modification
(1) Remove the clamps between FR50 and FR52 at LH side
(2) Modify the Routing between FR50 and FR52 and between STGR 33 and 30 at LH
side
(3) Install the clamps between FR50 and FR52 at LH side
(4) Install a bracket on the shroud box blanking plate at LH side
DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103
REVISION No.: 05 - Aug 20/18 Page: 6
5
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SERVICE BULLETIN
(5) Modify the routing on rib 1 on the passage way to the shroud box at LH side
(6) Modify the routing of routes 1P and 2P in the hydraulic shroud box at LH side
(7) Install a support on the support of the BLUE hydraulic reservoir at LH wing
(8) Modify the routing of routes 1E and 1G in the leading edge at LH wing
(9) Remove the clamps between FR50 and FR52 at RH side
(10) Modify the Routing between FR50 and FR52 and between STGR 33 and 30 at RH
side
(11) Install the clamps between FR50 and FR52 at RH side
(12) Install a bracket on the shroud box blanking plate at RH side
(13) Modify the routing on rib 1 on the passage way to the shroud box at RH side
(14) Modify the routing of routes 2E and 2G in the leading edge at RH wing
(15) Remove the clamps from LH wing
(16) Remove the clamps from RH wing
(17) Modify the Electrical Support Brackets in the Outer Shroud Box, LH Wing
(18) Modify the routing of routes 1P and 2P at LH wing
(19) Modify the routing of routes 1P and 2P at RH wing
(20) Install the clamps in LH wing
(21) Install the clamps in RH wing
(22) Modify the P-CLIPS at Location WOFX-204.5, LH Wing
(23) Modify the Backshell of the Connector and the Structure at Location ABX 36.5, LH
Wing
(24) Modify the Electrical Support Brackets in the Outer Shroud Box, RH Wing
(25) Modify the P-CLIPS at Location WOFX-204.5, RH Wing
(26) Modify the Backshell of the Connector and the Structure at Location ABX 36.5, RH
Wing
Task 246103-831-802-001: Modification - ADDITIONAL WORK between Revision No. 00 and
Revision No. 05
(1) Modify the routing on rib 1 on the passage way to the shroud box at LH side,
ADDITIONAL WORK
(2) Modify the routing on rib 1 on the passage way to the shroud box at RH side,
DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103
REVISION No.: 05 - Aug 20/18 Page: 7
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@A300-600
SERVICE BULLETIN
ADDITIONAL WORK
(3) Modify the routing of routes 1P and 2P in the shroud box at LH side, ADDITIONAL
WORK
(4) Modify the routing of the routes 1E and 1G in the leading edge at LH wing,
ADDITIONAL WORK
(5) Modify the routing of the routes 2E and 2G in the leading edge at RH wing,
ADDITIONAL WORK
(6) Install a support on the support of the BLUE hydraulic reservoir at LH wing,
ADDITIONAL WORK
(7) Install a bracket on the shroud box blanking plate at LH side, ADDITIONAL WORK
(8) Install a bracket on the shroud box blanking plate at RH side, ADDITIONAL WORK
(9) Remove the clamps between FR50 and FR51 at STRG 32 at LH side, ADDITIONAL
WORK
(10) Remove the clamps of the Passage Way at FR52 (LH side) - ADDITIONAL WORK
(11) Modify the Routing between FR50 and FR52 and between STGR 33 and 30 at LH
side - ADDITIONAL WORK
(12) Install the clamps between FR50 and FR51 at STRG 32 at LH side, ADDITIONAL
WORK
(13) Install the clamps of the Passage Way at FR52 (LH side) - ADDITIONAL WORK
(14) Remove the clamps between FR50 and FR51 at STGR 32 at RH side,
ADDITIONAL WORK
(15) Remove the clamps of the Passage Way at FR52 (RH side) - ADDITIONAL WORK
(16) Modify the Routing between FR50 and FR52 and between STGR 33 and 30 at RH
side - ADDITIONAL WORK
(17) Install the clamps between FR50 and FR51 at STGR 32 at RH side, ADDITIONAL
WORK
(18) Install the clamps of the Passage Way at FR52 (RH side) - ADDITIONAL WORK
Task 246103-831-804-001: Modification - ADDITIONAL WORK between Revision No. 01 and
Revision No. 05
(1) Remove the clamps between FR50 and FR52 at LH side, ADDITIONAL WORK
(2) Modify the routing between FR50 and FR52 and between STGR 33 and 30 at LH
side, ADDITIONAL WORK
(3) Install the clamps between FR50 and FR52 at LH side, ADDITIONAL WORK
DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103
REVISION No.: 05 - Aug 20/18 Page: 8
5
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### Page 33

@A300-600
SERVICE BULLETIN
(4) Install a bracket on the shroud box blanking plate at LH side, ADDITIONAL WORK
(5) Modify the routing on rib 1 on the passage way to the shroud box at LH side,
ADDITIONAL WORK
(6) Modify the routing of routes 1P and 2P in the shroud box at LH side, ADDITIONAL
WORK
(7) Install a support on the support of the BLUE hydraulic reservoir at LH wing -
ADDITIONAL WORK
(8) Modify the routing of the routes 1E and 1G in the leading edge at LH wing,
ADDITIONAL WORK
(9) Remove the clamps between FR50 and FR52 at RH side, ADDITIONAL WORK
(10) Modify the routing between FR50 and FR52 and between STGR 33 and 30 at RH
side, ADDITIONAL WORK
(11) Install the clamps between FR50 and FR52 at RH side, ADDITIONAL WORK
(12) Install a bracket on the shroud box bl anking plate at RH side, ADDITIONAL WORK
(13) Modify the routing on Rib 1 on the passage way to the shroud box at RH side,
ADDITIONAL WORK
(14) Modify the routing of the routes 2E and 2G in the leading edge at RH wing,
ADDITIONAL WORK
(15) Remove the clamps from LH wings, ADDITIONAL WORK
(16) Remove the clamps from RH wings, ADDITIONAL WORK
(17) Modify the routing of routes 1P and 2P at LH wing, ADDITIONAL WORK
(18) Modify the routing of routes 1P and 2P at RH wing, ADDITIONAL WORK
(19) Install the clamps in LH wing, ADDITIONAL WORK
(20) Install the clamps in RH wing, ADDITIONAL WORK
Task 246103-831-805-001: Modification - ADDITIONAL WORK between Revision No. 02 and
Revision No. 05
(1) Modify the routing on Rib 1 on the passage way to the shroud box at LH side,
ADDITIONAL WORK
(2) Modify the routing on Rib 1 on the passage way to the shroud box at RH side,
ADDITIONAL WORK
(3) Remove the clamps from LH wing, ADDITIONAL WORK
(4) Remove the clamps from RH wing, ADDITIONAL WORK
DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103
REVISION No.: 05 - Aug 20/18 Page: 9
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@A300-600
SERVICE BULLETIN
(5) Modify the routing of routes 1P and 2P at LH wing, ADDITIONAL WORK
(6) Modify the routing of routes 1P and 2P at RH wing, ADDITIONAL WORK
(7) Install the clamps in LH wing, ADDITIONAL WORK
(8) Install the clamps in RH wing, ADDITIONAL WORK
Task 246103-831-806-001: Modification - ADDITIONAL WORK between Revision No. 03 and
Revision No. 05
(1) Install the Spacers to the Guide Assembly - Conduit in the LH Wing - ADDITIONAL
WORK
(2) Install the Spacers to the Guide Assembly - Conduit in the RH Wing - ADDITIONAL
WORK
Task 246103-831-807-001: Modification - ADDITIONAL WORK between Revision No. 04 and
Revision No. 05 and only if Revision No. 03 is also Embodied
(1) Install the Spacers to the Guide Assembly - Conduit in the LH Wing - ADDITIONAL
WORK
(2) Install the Spacers to the Guide Assembly - Conduit in the RH Wing - ADDITIONAL
WORK
**CONF 002
Task 246103-831-801-001: Modification
(1) Remove the clamps between FR50 and FR52 at LH side
(2) Modify the Routing between FR50 and FR52 and between STGR 33 and 30 at LH
side
(3) Install the clamps between FR50 and FR52 at LH side
(4) Install a bracket on the shroud box blanking plate at LH side
(5) Modify the routing on rib 1 on the passage way to the shroud box at LH side
(6) Modify the routing of routes 1P and 2P in the hydraulic shroud box at LH side
(7) Install a support on the support of the BLUE hydraulic reservoir at LH wing
(8) Modify the routing of routes 1E and 1G in the leading edge at LH wing
(9) Remove the clamps between FR50 and FR52 at RH side
(10) Modify the Routing between FR50 and FR52 and between STGR 33 and 30 at RH
side
(11) Install the clamps between FR50 and FR52 at RH side
DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103
REVISION No.: 05 - Aug 20/18 Page: 10
5
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@A300-600
SERVICE BULLETIN
(12) Install a bracket on the shroud box blanking plate at RH side
(13) Modify the routing on rib 1 on the passage way to the shroud box at RH side
(14) Modify the routing of routes 2E and 2G in the leading edge at RH wing
(15) Remove the clamps from LH wing.
(16) Remove the clamps from RH wing.
(17) Modify the Electrical Support Brackets in the Outer Shroud Box, LH Wing
(18) Modify the routing of routes 1P and 2P at LH wing
(19) Modify the routing of routes 1P and 2P at RH wing
(20) Install the clamps in LH wing.
(21) Install the clamps in RH wing.
(22) Modify the P-CLIPS at Location WOFX-204.5, LH Wing
(23) Modify the Backshell of the Connector and the Structure at Location ABX 36.5, LH
Wing
(24) Modify the Electrical Support Brackets in the Outer Shroud Box, RH Wing
(25) Modify the P-CLIPS at Location WOFX-204.5, RH Wing
(26) Modify the Backshell of the Connector and the Structure at Location ABX 36.5, RH
Wing
Task 246103-831-802-001: Modification - ADDITIONAL WORK between Revision No. 00 and
Revision No. 05
(1) Modify the routing on rib 1 on the passage way to the shroud box at LH side,
ADDITIONAL WORK
(2) Modify the routing on rib 1 on the passage way to the shroud box at RH side,
ADDITIONAL WORK
(3) Modify the routing of routes 1P and 2P in the shroud box at LH side, ADDITIONAL
WORK
(4) Modify the routing of the routes 1E and 1G in the leading edge at LH wing,
ADDITIONAL WORK
(5) Modify the routing of the routes 2E and 2G in the leading edge at RH wing,
ADDITIONAL WORK
(6) Install a support on the support of the BLUE hydraulic reservoir at LH wing,
ADDITIONAL WORK
(7) Install a bracket on the shroud box blanking plate at LH side, ADDITIONAL WORK
DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103
REVISION No.: 05 - Aug 20/18 Page: 11
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SERVICE BULLETIN
(8) Install a bracket on the shroud box blanking plate at RH side, ADDITIONAL WORK
(9) Remove the clamps between FR50 and FR51 at STRG 32 at LH side, ADDITIONAL
WORK
(10) Remove the clamps of the Passage Way at FR52 (LH side) - ADDITIONAL WORK
(11) Modify the Routing between FR50 and FR52 and between STGR 33 and 30 at LH
side - ADDITIONAL WORK
(12) Install the clamps between FR50 and FR51 at STRG 32 at LH side, ADDITIONAL
WORK
(13) Install the clamps of the Passage Way at FR52 (LH side) - ADDITIONAL WORK
(14) Remove the clamps between FR50 and FR51 at STGR 32 at RH side,
ADDITIONAL WORK
(15) Remove the clamps of the Passage Way at FR52 (RH side) - ADDITIONAL WORK
(16) Modify the Routing between FR50 and FR52 and between STGR 33 and 30 at RH
side - ADDITIONAL WORK
(17) Install the clamps between FR50 and FR51 at STGR 32 at RH side, ADDITIONAL
WORK
(18) Install the clamps of the Passage Way at FR52 (RH side) - ADDITIONAL WORK
Task 246103-831-804-001: Modification - ADDITIONAL WORK between Revision No. 01 and
Revision No. 05
(1) Remove the clamps between FR50 and FR52 at LH side, ADDITIONAL WORK
(2) Modify the routing between FR50 and FR52 and between STGR 33 and 30 at LH
side, ADDITIONAL WORK
(3) Install the clamps between FR50 and FR52 at LH side, ADDITIONAL WORK
(4) Install a bracket on the shroud box blanking plate at LH side, ADDITIONAL WORK
(5) Modify the routing on rib 1 on the passage way to the shroud box at LH side,
ADDITIONAL WORK
(6) Modify the routing of routes 1P and 2P in the shroud box at LH side, ADDITIONAL
WORK
(7) Install a support on the support of the BLUE hydraulic reservoir at LH wing -
ADDITIONAL WORK
(8) Modify the routing of the routes 1E and 1G in the leading edge at LH wing,
ADDITIONAL WORK
(9) Remove the clamps between FR50 and FR52 at RH side, ADDITIONAL WORK
DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103
REVISION No.: 05 - Aug 20/18 Page: 12
5
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@A300-600
SERVICE BULLETIN
(10) Modify the routing between FR50 and FR52 and between STGR 33 and 30 at RH
side, ADDITIONAL WORK
(11) Install the clamps between FR50 and FR52 at RH side, ADDITIONAL WORK
(12) Install a bracket on the shroud box bl anking plate at RH side, ADDITIONAL WORK
(13) Modify the routing on Rib 1 on the passage way to the shroud box at RH side,
ADDITIONAL WORK
(14) Modify the routing of the routes 2E and 2G in the leading edge at RH wing,
ADDITIONAL WORK
(15) Remove the clamps from LH wings, ADDITIONAL WORK
(16) Remove the clamps from RH wings, ADDITIONAL WORK
(17) Modify the routing of routes 1P and 2P at LH wing, ADDITIONAL WORK
(18) Modify the routing of routes 1P and 2P at RH wing, ADDITIONAL WORK
(19) Install the clamps in LH wing, ADDITIONAL WORK
(20) Install the clamps in RH wing, ADDITIONAL WORK
Task 246103-831-805-001: Modification - ADDITIONAL WORK between Revision No. 02 and
Revision No. 05
(1) Modify the routing on Rib 1 on the passage way to the shroud box at LH side,
ADDITIONAL WORK
(2) Modify the routing on Rib 1 on the passage way to the shroud box at RH side,
ADDITIONAL WORK
(3) Remove the clamps from LH wing, ADDITIONAL WORK
(4) Remove the clamps from RH wing, ADDITIONAL WORK
(5) Modify the routing of routes 1P and 2P at LH wing, ADDITIONAL WORK
(6) Modify the routing of routes 1P and 2P at RH wing, ADDITIONAL WORK
(7) Install the clamps in LH wing, ADDITIONAL WORK
(8) Install the clamps in RH wing, ADDITIONAL WORK
**CONF 003
Task 246103-831-801-001: Modification
(1) Remove the clamps between FR50 and FR52 at LH side
(2) Modify the Routing between FR50 and FR52 and between STGR 33 and 30 at LH
side
DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103
REVISION No.: 05 - Aug 20/18 Page: 13
5
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@A300-600
SERVICE BULLETIN
(3) Install the clamps between FR50 and FR52 at LH side
(4) Install a bracket on the shroud box blanking plate at LH side
(5) Modify the routing on rib 1 on the passage way to the shroud box at LH side
(6) Modify the routing of routes 1P and 2P in the hydraulic shroud box at LH side
(7) Install a support on the support of the BLUE hydraulic reservoir at LH wing
(8) Modify the routing of routes 1E and 1G in the leading edge at LH wing
(9) Remove the clamps between FR50 and FR52 at RH side
(10) Modify the Routing between FR50 and FR52 and between STGR 33 and 30 at RH
side
(11) Install the clamps between FR50 and FR52 at RH side
(12) Install a bracket on the shroud box blanking plate at RH side
(13) Modify the routing on rib 1 on the passage way to the shroud box at RH side
(14) Modify the routing of routes 2E and 2G in the leading edge at RH wing
(15) Remove the clamps from LH wing
(16) Remove the clamps from RH wing
(17) Modify the Electrical Support Brackets in the Outer Shroud Box, LH Wing
(18) Modify the routing of routes 1P and 2P at LH wing
(19) Modify the routing of routes 1P and 2P at RH wing
(20) Install the clamps in LH wing
(21) Install the clamps in RH wing
(22) Modify the P-CLIPS at Location WOFX-204.5, LH Wing
(23) Modify the Backshell of the Connector and the Structure at Location ABX 36.5, LH
Wing
(24) Modify the Electrical Support Brackets in the Outer Shroud Box, RH Wing
(25) Modify the P-CLIPS at Location WOFX-204.5, RH Wing
(26) Modify the Backshell of the Connector and the Structure at Location ABX 36.5, RH
Wing
Task 246103-831-802-001: Modification - ADDITIONAL WORK between Revision No. 00 and
DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103
REVISION No.: 05 - Aug 20/18 Page: 14
5
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@A300-600
SERVICE BULLETIN
Revision No. 05
(1) Modify the routing on rib 1 on the passage way to the shroud box at LH side,
ADDITIONAL WORK
(2) Modify the routing on rib 1 on the passage way to the shroud box at RH side,
ADDITIONAL WORK
(3) Modify the routing of routes 1P and 2P in the shroud box at LH side, ADDITIONAL
WORK
(4) Modify the routing of the routes 1E and 1G in the leading edge at LH wing,
ADDITIONAL WORK
(5) Modify the routing of the routes 2E and 2G in the leading edge at RH wing,
ADDITIONAL WORK
(6) Install a support on the support of the BLUE hydraulic reservoir at LH wing,
ADDITIONAL WORK
(7) Install a bracket on the shroud box blanking plate at LH side, ADDITIONAL WORK
(8) Install a bracket on the shroud box blanking plate at RH side, ADDITIONAL WORK
(9) Remove the clamps between FR50 and FR51 at STRG 32 at LH side, ADDITIONAL
WORK
(10) Remove the clamps of the Passage Way at FR52 (LH side) - ADDITIONAL WORK
(11) Modify the Routing between FR50 and FR52 and between STGR 33 and 30 at LH
side - ADDITIONAL WORK
(12) Install the clamps between FR50 and FR51 at STRG 32 at LH side, ADDITIONAL
WORK
(13) Install the clamps of the Passage Way at FR52 (LH side) - ADDITIONAL WORK
(14) Remove the clamps between FR50 and FR51 at STGR 32 at RH side,
ADDITIONAL WORK
(15) Remove the clamps of the Passage Way at FR52 (RH side) - ADDITIONAL WORK
(16) Modify the Routing between FR50 and FR52 and between STGR 33 and 30 at RH
side - ADDITIONAL WORK
(17) Install the clamps between FR50 and FR51 at STGR 32 at RH side, ADDITIONAL
WORK
(18) Install the clamps of the Passage Way at FR52 (RH side) - ADDITIONAL WORK
Task 246103-831-804-001: Modification - ADDITIONAL WORK between Revision No. 01 and
Revision No. 05
(1) Remove the clamps between FR50 and FR52 at LH side, ADDITIONAL WORK
DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103
REVISION No.: 05 - Aug 20/18 Page: 15
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@A300-600
SERVICE BULLETIN
(2) Modify the routing between FR50 and FR52 and between STGR 33 and 30 at LH
side, ADDITIONAL WORK
(3) Install the clamps between FR50 and FR52 at LH side, ADDITIONAL WORK
(4) Install a bracket on the shroud box blanking plate at LH side, ADDITIONAL WORK
(5) Modify the routing on rib 1 on the passage way to the shroud box at LH side,
ADDITIONAL WORK
(6) Modify the routing of routes 1P and 2P in the shroud box at LH side, ADDITIONAL
WORK
(7) Install a support on the support of the BLUE hydraulic reservoir at LH wing -
ADDITIONAL WORK
(8) Modify the routing of the routes 1E and 1G in the leading edge at LH wing,
ADDITIONAL WORK
(9) Remove the clamps between FR50 and FR52 at RH side, ADDITIONAL WORK
(10) Modify the routing between FR50 and FR52 and between STGR 33 and 30 at RH
side, ADDITIONAL WORK
(11) Install the clamps between FR50 and FR52 at RH side, ADDITIONAL WORK
(12) Install a bracket on the shroud box bl anking plate at RH side, ADDITIONAL WORK
(13) Modify the routing on Rib 1 on the passage way to the shroud box at RH side,
ADDITIONAL WORK
(14) Modify the routing of the routes 2E and 2G in the leading edge at RH wing,
ADDITIONAL WORK
(15) Remove the clamps from LH wings, ADDITIONAL WORK
(16) Remove the clamps from RH wings, ADDITIONAL WORK
(17) Modify the routing of routes 1P and 2P at LH wing, ADDITIONAL WORK
(18) Modify the routing of routes 1P and 2P at RH wing, ADDITIONAL WORK
(19) Install the clamps in LH wing, ADDITIONAL WORK
(20) Install the clamps in RH wing, ADDITIONAL WORK
Task 246103-831-805-001: Modification - ADDITIONAL WORK between Revision No. 02 and
Revision No. 05
(1) Modify the routing on Rib 1 on the passage way to the shroud box at LH side,
ADDITIONAL WORK
(2) Modify the routing on Rib 1 on the passage way to the shroud box at RH side,
ADDITIONAL WORK
DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103
REVISION No.: 05 - Aug 20/18 Page: 16
5
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### Page 41

@A300-600
SERVICE BULLETIN
(3) Remove the clamps from LH wing, ADDITIONAL WORK
(4) Remove the clamps from RH wing, ADDITIONAL WORK
(5) Modify the routing of routes 1P and 2P at LH wing, ADDITIONAL WORK
(6) Modify the routing of routes 1P and 2P at RH wing, ADDITIONAL WORK
(7) Install the clamps in LH wing, ADDITIONAL WORK
(8) Install the clamps in RH wing, ADDITIONAL WORK
Task 246103-831-806-001: Modification - ADDITIONAL WORK between Revision No. 03 and
Revision No. 05
(1) Modify the Clamp on the routing on Rib 1 on the passage way to the shroud box LH
side, ADDITIONAL WORK
(2) Modify the Clamp on the routing on Rib 1 on the passage way to the shroud box RH
side, ADDITIONAL WORK
(3) Install the Spacers to the Guide Assembly - Conduit in the LH Wing - ADDITIONAL
WORK
(4) Install the Spacers to the Guide Assembly - Conduit in the RH Wing - ADDITIONAL
WORK
Task 246103-831-807-001: Modification - ADDITIONAL WORK between Revision No. 04 and
Revision No. 05 and only if Revision No. 03 is also Embodied
(1) Install the Spacers to the Guide Assembly - Conduit in the LH Wing - ADDITIONAL
WORK
(2) Install the Spacers to the Guide Assembly - Conduit in the RH Wing - ADDITIONAL
WORK
**CONF ALL
E. COMPLIANCE
(1) Classification
MANDATORY: Service Bulletin must be accomplished.
(2) Accomplishment Timescale
Accomplishment of this Service Bulletin is recommended to be embodied within 30
months from SB revision 2 issuance. This Service Bulletin has been classified
Mandatory by the issue of an Airworthiness Directive (AD) published by the European
Aviation Safety A gency ( EASA). The AD must be used as the refer ence document for
the mandated accomplishment timescale.
DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103
REVISION No.: 05 - Aug 20/18 Page: 17
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@A300-600
SERVICE BULLETIN
F. APPROVAL
The technical content of this document is approved under EASA Design Or ganisation
Approval No. EASA 21J.031.
If an aircraft listed in the effectivity has a modification or repair embodied that is not of
AIRBUS origin, and which affects the content of this Service Bulletin, the operator is
responsible for obtaining approval by its airworthiness authority for any adaptation necessary
before incorporation of the Service Bulletin.
G. MANPOWER
The manpower estimates given in this Service Bulletin are based on the direct labor cost to
do the work. These estimates assume that the work will be done by experienced personnel,
and may need to be revised upwards to suit operator’s circumstances. The estimates do not
include the time to prepare, plan or inspect the work. Manufacture and procurement of parts
and tools, drying times for paints, sealants, etc., and general administration work are also not
included.
**CONF 001
Task 246103-831-801-001: Modification
Get Access
 4.00
On Aircraft
Remove the clamps between FR50 and FR52 at LH
side
1.50
Modify the Routing between FR50 and FR52 and
between STGR 33 and 30 at LH side
1.00
Install the clamps between FR50 and FR52 at LH side
 2.00
Install a bracket on the shroud box blanking plate at
LH side
1.00
Modify the routing on rib 1 on the passage way to the
shroud box at LH side
1.00
Modify the routing of routes 1P and 2P in the hydraulic
shroud box at LH side
1.00
Install a support on the support of the BLUE hydraulic
reservoir at LH wing
1.00
Modify the routing of routes 1E and 1G in the leading
edge at LH wing
0.50
Remove the clamps between FR50 and FR52 at RH
side
1.00
Modify the Routing between FR50 and FR52 and
between STGR 33 and 30 at RH side
1.00
Install the clamps between FR50 and FR52 at RH side
 1.00
Install a bracket on the shroud box blanking plate at
RH side
1.00
Modify the routing on rib 1 on the passage way to the
shroud box at RH side
1.00
Modify the routing of routes 2E and 2G in the leading
edge at RH wing
0.50
DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103
REVISION No.: 05 - Aug 20/18 Page: 18
5
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### Page 43

@A300-600
SERVICE BULLETIN
Task 246103-831-801-001: Modification
Remove the clamps from LH wing
 1.00
Remove the clamps from RH wing
 1.00
Modify the Electrical Support Brackets in the Outer
Shroud Box, LH Wing
2.50
Modify the routing of routes 1P and 2P at LH wing
 1.50
Modify the routing of routes 1P and 2P at RH wing
 1.50
Install the clamps in LH wing
 1.00
Install the clamps in RH wing
 1.00
Modify the P-CLIPS at Location WOFX-204.5, LH Wing
 0.50
Modify the Backshell of the Connector and the
Structure at Location ABX 36.5, LH Wing
0.50
Modify the Electrical Support Brackets in the Outer
Shroud Box, RH Wing
2.50
Modify the P-CLIPS at Location WOFX-204.5, RH
Wing
0.50
Modify the Backshell of the Connector and the
Structure at Location ABX 36.5, RH Wing
0.50
Tests
 0.50
Close-Up
 5.00
TOTAL MANHOURS
 38.00
ELAPSED TIME (HOURS)
 21.75
NOTE
: For an explanation of the manhours and elapsed time, refer to the Gantt
Chart, Fig. A-FAAAA
 given in Appendix 01 - Elapsed Time Assumption
Task 246103-831-802-001: Modification - ADDITIONAL WORK between Revision No. 00 and
Revision No. 05
Get Access
 4.00
On Aircraft
Modify the routing on rib 1 on the passage way to the
shroud box at LH side, ADDITIONAL WORK
1.00
Modify the routing on rib 1 on the passage way to the
shroud box at RH side, ADDITIONAL WORK
1.00
Modify the routing of routes 1P and 2P in the shroud
box at LH side, ADDITIONAL WORK
1.00
Modify the routing of the routes 1E and 1G in the
leading edge at LH wing, ADDITIONAL WORK
1.00
Modify the routing of the routes 2E and 2G in the
leading edge at RH wing, ADDITIONAL WORK
1.00
Install a support on the support of the BLUE hydraulic
reservoir at LH wing, ADDITIONAL WORK
2.00
Install a bracket on the shroud box blanking plate at
LH side, ADDITIONAL WORK
1.00
Install a bracket on the shroud box blanking plate at
RH side, ADDITIONAL WORK
1.00
DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103
REVISION No.: 05 - Aug 20/18 Page: 19
5
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### Page 44

@A300-600
SERVICE BULLETIN
Task 246103-831-802-001: Modification - ADDITIONAL WORK between Revision No. 00 and
Revision No. 05
Remove the clamps between FR50 and FR51 at STRG
32 at LH side, ADDITIONAL WORK
0.50
Remove the clamps of the Passage Way at FR52 (LH
side) - ADDITIONAL WORK
0.50
Modify the Routing between FR50 and FR52 and
between STGR 33 and 30 at LH side - ADDITIONAL
WORK
1.00
Install the clamps between FR50 and FR51 at STRG
32 at LH side, ADDITIONAL WORK
0.50
Install the clamps of the Passage Way at FR52 (LH
side) - ADDITIONAL WORK
0.50
Remove the clamps between FR50 and FR51 at STGR
32 at RH side, ADDITIONAL WORK
0.50
Remove the clamps of the Passage Way at FR52 (RH
side) - ADDITIONAL WORK
0.50
Modify the Routing between FR50 and FR52 and
between STGR 33 and 30 at RH side - ADDITIONAL
WORK
1.00
Install the clamps between FR50 and FR51 at STGR
32 at RH side, ADDITIONAL WORK
0.50
Install the clamps of the Passage Way at FR52 (RH
side) - ADDITIONAL WORK
0.50
Tests
 0.50
Close-Up
 5.00
TOTAL MANHOURS
 24.50
ELAPSED TIME (HOURS)
 16.50
NOTE
: For an explanation of the manhours and elapsed time, refer to the Gantt
Chart, Fig. A-FACAA
 given in Appendix 02 - Elapsed Time Assumption -
ADDITIONAL WORK between Revision No. 00 and Revision No. 05
Task 246103-831-804-001: Modification - ADDITIONAL WORK between Revision No. 01 and
Revision No. 05
Get Access
 4.00
On Aircraft
Remove the clamps between FR50 and FR52 at LH
side, ADDITIONAL WORK
1.00
Modify the routing between FR50 and FR52 and
between STGR 33 and 30 at LH side, ADDITIONAL
WORK
1.00
Install the clamps between FR50 and FR52 at LH side,
ADDITIONAL WORK
1.00
Install a bracket on the shroud box blanking plate at
LH side, ADDITIONAL WORK
1.00
Modify the routing on rib 1 on the passage way to the
shroud box at LH side, ADDITIONAL WORK
1.00
DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103
REVISION No.: 05 - Aug 20/18 Page: 20
5
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### Page 45

@A300-600
SERVICE BULLETIN
Task 246103-831-804-001: Modification - ADDITIONAL WORK between Revision No. 01 and
Revision No. 05
Modify the routing of routes 1P and 2P in the shroud
box at LH side, ADDITIONAL WORK
1.00
Install a support on the support of the BLUE hydraulic
reservoir at LH wing - ADDITIONAL WORK
2.00
Modify the routing of the routes 1E and 1G in the
leading edge at LH wing, ADDITIONAL WORK
0.50
Remove the clamps between FR50 and FR52 at RH
side, ADDITIONAL WORK
1.00
Modify the routing between FR50 and FR52 and
between STGR 33 and 30 at RH side, ADDITIONAL
WORK
1.00
Install the clamps between FR50 and FR52 at RH side,
ADDITIONAL WORK
1.00
Install a bracket on the shroud box blanking plate at
RH side, ADDITIONAL WORK
1.00
Modify the routing on Rib 1 on the passage way to the
shroud box at RH side, ADDITIONAL WORK
1.00
Modify the routing of the routes 2E and 2G in the
leading edge at RH wing, ADDITIONAL WORK
0.50
Remove the clamps from LH wings, ADDITIONAL
WORK
1.00
Remove the clamps from RH wings, ADDITIONAL
WORK
1.00
Modify the routing of routes 1P and 2P at LH wing,
ADDITIONAL WORK
1.50
Modify the routing of routes 1P and 2P at RH wing,
ADDITIONAL WORK
1.50
Install the clamps in LH wing, ADDITIONAL WORK
 1.00
Install the clamps in RH wing, ADDITIONAL WORK
 1.00
Tests
 0.50
Close-Up
 5.00
TOTAL MANHOURS
 30.50
ELAPSED TIME (HOURS)
 16.50
NOTE
: For an explanation of the manhours and elapsed time, refer to the Gantt
Chart,
 Fig. A-FADAA
 given in Appendix 03 - Elapsed Time Assumption -
ADDITIONAL WORK between Revision No. 01 and Revision No. 05
Task 246103-831-805-001: Modification - ADDITIONAL WORK between Revision No. 02 and
Revision No. 05
Get Access
 4.00
On Aircraft
Modify the routing on Rib 1 on the passage way to the
shroud box at LH side, ADDITIONAL WORK
0.50
Modify the routing on Rib 1 on the passage way to the
shroud box at RH side, ADDITIONAL WORK
0.50
DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103
REVISION No.: 05 - Aug 20/18 Page: 21
5
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### Page 46

@A300-600
SERVICE BULLETIN
Task 246103-831-805-001: Modification - ADDITIONAL WORK between Revision No. 02 and
Revision No. 05
Remove the clamps from LH wing, ADDITIONAL
WORK
1.00
Remove the clamps from RH wing, ADDITIONAL
WORK
1.00
Modify the routing of routes 1P and 2P at LH wing,
ADDITIONAL WORK
1.50
Modify the routing of routes 1P and 2P at RH wing,
ADDITIONAL WORK
1.50
Install the clamps in LH wing, ADDITIONAL WORK
 1.00
Install the clamps in RH wing, ADDITIONAL WORK
 1.00
Tests
 0.50
Close-Up
 5.00
TOTAL MANHOURS
 17.50
ELAPSED TIME (HOURS)
 9.00
NOTE
: For an explanation of the manhours and elapsed time, refer to the Gantt
Chart, Fig. A-FAFAA
 given in Appendix 04 - Elapsed Time Assumption -
ADDITIONAL WORK between Revision No. 02 and Revision No. 05
Task 246103-831-806-001: Modification - ADDITIONAL WORK between Revision No. 03 and
Revision No. 05
Get Access
 4.00
On Aircraft
Install the Spacers to the Guide Assembly - Conduit in
the LH Wing - ADDITIONAL WORK
0.25
Install the Spacers to the Guide Assembly - Conduit in
the RH Wing - ADDITIONAL WORK
0.25
Tests
 0.50
Close-Up
 5.00
TOTAL MANHOURS
 10.00
ELAPSED TIME (HOURS)
 5.25
NOTE
: For an explanation of the manhours and elapsed time, refer to the Gantt
Chart, Fig. A-FAGAA
 given in Appendix 05 - Elapsed Time Assumption -
ADDITIONAL WORK between Revision No. 03 and Revision No. 05
Task 246103-831-807-001: Modification - ADDITIONAL WORK between Revision No. 04 and
Revision No. 05 and only if Revision No. 03 is also Embodied
Get Access
 4.00
On Aircraft
Install the Spacers to the Guide Assembly - Conduit in
the LH Wing - ADDITIONAL WORK
0.25
Install the Spacers to the Guide Assembly - Conduit in
the RH Wing - ADDITIONAL WORK
0.25
Tests
 0.50
Close-Up
 5.00
DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103
REVISION No.: 05 - Aug 20/18 Page: 22
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### Page 47

@A300-600
SERVICE BULLETIN
Task 246103-831-807-001: Modification - ADDITIONAL WORK between Revision No. 04 and
Revision No. 05 and only if Revision No. 03 is also Embodied
TOTAL MANHOURS
 10.00
ELAPSED TIME (HOURS)
 5.25
NOTE
: For an explanation of the manhours and elapsed time, refer to the Gantt
Chart, Fig. A-FAHAA
 given in Appendix 06 - Elapsed Time Assumption -
ADDITIONAL WORK between Revision No. 04 and Revision No. 05 and only
if Revision No. 03 was also Embodied
**CONF 002
Task 246103-831-801-001: Modification
Get Access
 4.00
On Aircraft
Remove the clamps between FR50 and FR52 at LH
side
1.50
Modify the Routing between FR50 and FR52 and
between STGR 33 and 30 at LH side
1.00
Install the clamps between FR50 and FR52 at LH side
 2.00
Install a bracket on the shroud box blanking plate at
LH side
1.00
Modify the routing on rib 1 on the passage way to the
shroud box at LH side
1.00
Modify the routing of routes 1P and 2P in the hydraulic
shroud box at LH side
1.00
Install a support on the support of the BLUE hydraulic
reservoir at LH wing
1.00
Modify the routing of routes 1E and 1G in the leading
edge at LH wing
0.50
Remove the clamps between FR50 and FR52 at RH
side
1.00
Modify the Routing between FR50 and FR52 and
between STGR 33 and 30 at RH side
1.00
Install the clamps between FR50 and FR52 at RH side
 1.00
Install a bracket on the shroud box blanking plate at
RH side
1.00
Modify the routing on rib 1 on the passage way to the
shroud box at RH side
1.00
Modify the routing of routes 2E and 2G in the leading
edge at RH wing
0.50
Remove the clamps from LH wing.
 1.00
Remove the clamps from RH wing.
 1.00
Modify the Electrical Support Brackets in the Outer
Shroud Box, LH Wing
1.50
Modify the routing of routes 1P and 2P at LH wing
 1.50
Modify the routing of routes 1P and 2P at RH wing
 1.50
Install the clamps in LH wing.
 1.00
DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103
REVISION No.: 05 - Aug 20/18 Page: 23
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 48

@A300-600
SERVICE BULLETIN
Task 246103-831-801-001: Modification
Install the clamps in RH wing.
 1.00
Modify the P-CLIPS at Location WOFX-204.5, LH Wing
 0.50
Modify the Backshell of the Connector and the
Structure at Location ABX 36.5, LH Wing
0.50
Modify the Electrical Support Brackets in the Outer
Shroud Box, RH Wing
1.50
Modify the P-CLIPS at Location WOFX-204.5, RH
Wing
0.50
Modify the Backshell of the Connector and the
Structure at Location ABX 36.5, RH Wing
0.50
Tests
 0.50
Close-Up
 5.00
TOTAL MANHOURS
 36.00
ELAPSED TIME (HOURS)
 21.25
NOTE
: For an explanation of the manhours and elapsed time, refer to the Gantt
Chart, Fig. A-FABAA
 given in Appendix 01 - Elapsed Time Assumption
Task 246103-831-802-001: Modification - ADDITIONAL WORK between Revision No. 00 and
Revision No. 05
Get Access
 4.00
On Aircraft
Modify the routing on rib 1 on the passage way to the
shroud box at LH side, ADDITIONAL WORK
1.00
Modify the routing on rib 1 on the passage way to the
shroud box at RH side, ADDITIONAL WORK
1.00
Modify the routing of routes 1P and 2P in the shroud
box at LH side, ADDITIONAL WORK
1.00
Modify the routing of the routes 1E and 1G in the
leading edge at LH wing, ADDITIONAL WORK
1.00
Modify the routing of the routes 2E and 2G in the
leading edge at RH wing, ADDITIONAL WORK
1.00
Install a support on the support of the BLUE hydraulic
reservoir at LH wing, ADDITIONAL WORK
2.00
Install a bracket on the shroud box blanking plate at
LH side, ADDITIONAL WORK
1.00
Install a bracket on the shroud box blanking plate at
RH side, ADDITIONAL WORK
1.00
Remove the clamps between FR50 and FR51 at STRG
32 at LH side, ADDITIONAL WORK
0.50
Remove the clamps of the Passage Way at FR52 (LH
side) - ADDITIONAL WORK
0.50
Modify the Routing between FR50 and FR52 and
between STGR 33 and 30 at LH side - ADDITIONAL
WORK
1.00
DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103
REVISION No.: 05 - Aug 20/18 Page: 24
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 49

@A300-600
SERVICE BULLETIN
Task 246103-831-802-001: Modification - ADDITIONAL WORK between Revision No. 00 and
Revision No. 05
Install the clamps between FR50 and FR51 at STRG
32 at LH side, ADDITIONAL WORK
0.50
Install the clamps of the Passage Way at FR52 (LH
side) - ADDITIONAL WORK
0.50
Remove the clamps between FR50 and FR51 at STGR
32 at RH side, ADDITIONAL WORK
0.50
Remove the clamps of the Passage Way at FR52 (RH
side) - ADDITIONAL WORK
0.50
Modify the Routing between FR50 and FR52 and
between STGR 33 and 30 at RH side - ADDITIONAL
WORK
1.00
Install the clamps between FR50 and FR51 at STGR
32 at RH side, ADDITIONAL WORK
0.50
Install the clamps of the Passage Way at FR52 (RH
side) - ADDITIONAL WORK
0.50
Tests
 0.50
Close-Up
 5.00
TOTAL MANHOURS
 24.50
ELAPSED TIME (HOURS)
 16.50
NOTE
: For an explanation of the manhours and elapsed time, refer to the Gantt
Chart, Fig. A-FACAA
 given in Appendix 02 - Elapsed Time Assumption -
ADDITIONAL WORK between Revision No. 00 and Revision No. 05
Task 246103-831-804-001: Modification - ADDITIONAL WORK between Revision No. 01 and
Revision No. 05
Get Access
 4.00
On Aircraft
Remove the clamps between FR50 and FR52 at LH
side, ADDITIONAL WORK
1.00
Modify the routing between FR50 and FR52 and
between STGR 33 and 30 at LH side, ADDITIONAL
WORK
1.00
Install the clamps between FR50 and FR52 at LH side,
ADDITIONAL WORK
1.00
Install a bracket on the shroud box blanking plate at
LH side, ADDITIONAL WORK
1.00
Modify the routing on rib 1 on the passage way to the
shroud box at LH side, ADDITIONAL WORK
1.00
Modify the routing of routes 1P and 2P in the shroud
box at LH side, ADDITIONAL WORK
1.00
Install a support on the support of the BLUE hydraulic
reservoir at LH wing - ADDITIONAL WORK
2.00
Modify the routing of the routes 1E and 1G in the
leading edge at LH wing, ADDITIONAL WORK
0.50
DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103
REVISION No.: 05 - Aug 20/18 Page: 25
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 50

@A300-600
SERVICE BULLETIN
Task 246103-831-804-001: Modification - ADDITIONAL WORK between Revision No. 01 and
Revision No. 05
Remove the clamps between FR50 and FR52 at RH
side, ADDITIONAL WORK
1.00
Modify the routing between FR50 and FR52 and
between STGR 33 and 30 at RH side, ADDITIONAL
WORK
1.00
Install the clamps between FR50 and FR52 at RH side,
ADDITIONAL WORK
1.00
Install a bracket on the shroud box blanking plate at
RH side, ADDITIONAL WORK
1.00
Modify the routing on Rib 1 on the passage way to the
shroud box at RH side, ADDITIONAL WORK
1.00
Modify the routing of the routes 2E and 2G in the
leading edge at RH wing, ADDITIONAL WORK
0.50
Remove the clamps from LH wings, ADDITIONAL
WORK
1.00
Remove the clamps from RH wings, ADDITIONAL
WORK
1.00
Modify the routing of routes 1P and 2P at LH wing,
ADDITIONAL WORK
1.50
Modify the routing of routes 1P and 2P at RH wing,
ADDITIONAL WORK
1.50
Install the clamps in LH wing, ADDITIONAL WORK
 1.00
Install the clamps in RH wing, ADDITIONAL WORK
 1.00
Tests
 0.50
Close-Up
 5.00
TOTAL MANHOURS
 30.50
ELAPSED TIME (HOURS)
 16.50
NOTE
: For an explanation of the manhours and elapsed time, refer to the Gantt
Chart,
 Fig. A-FADAA
 given in Appendix 03 - Elapsed Time Assumption -
ADDITIONAL WORK between Revision No. 01 and Revision No. 05
Task 246103-831-805-001: Modification - ADDITIONAL WORK between Revision No. 02 and
Revision No. 05
Get Access
 4.00
On Aircraft
Modify the routing on Rib 1 on the passage way to the
shroud box at LH side, ADDITIONAL WORK
0.50
Modify the routing on Rib 1 on the passage way to the
shroud box at RH side, ADDITIONAL WORK
0.50
Remove the clamps from LH wing, ADDITIONAL
WORK
1.00
Remove the clamps from RH wing, ADDITIONAL
WORK
1.00
Modify the routing of routes 1P and 2P at LH wing,
ADDITIONAL WORK
1.50
DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103
REVISION No.: 05 - Aug 20/18 Page: 26
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 51

@A300-600
SERVICE BULLETIN
Task 246103-831-805-001: Modification - ADDITIONAL WORK between Revision No. 02 and
Revision No. 05
Modify the routing of routes 1P and 2P at RH wing,
ADDITIONAL WORK
1.50
Install the clamps in LH wing, ADDITIONAL WORK
 1.00
Install the clamps in RH wing, ADDITIONAL WORK
 1.00
Tests
 0.50
Close-Up
 5.00
TOTAL MANHOURS
 17.50
ELAPSED TIME (HOURS)
 9.00
NOTE
: For an explanation of the manhours and elapsed time, refer to the Gantt
Chart,
 Fig. A-FAFAA
 given in Appendix 04 - Elapsed Time Assumption -
ADDITIONAL WORK between Revision No. 02 and Revision No. 05
**CONF 003
Task 246103-831-801-001: Modification
Get Access
 4.00
On Aircraft
Remove the clamps between FR50 and FR52 at LH
side
1.50
Modify the Routing between FR50 and FR52 and
between STGR 33 and 30 at LH side
1.00
Install the clamps between FR50 and FR52 at LH side
 2.00
Install a bracket on the shroud box blanking plate at
LH side
1.00
Modify the routing on rib 1 on the passage way to the
shroud box at LH side
1.00
Modify the routing of routes 1P and 2P in the hydraulic
shroud box at LH side
1.00
Install a support on the support of the BLUE hydraulic
reservoir at LH wing
1.00
Modify the routing of routes 1E and 1G in the leading
edge at LH wing
0.50
Remove the clamps between FR50 and FR52 at RH
side
1.00
Modify the Routing between FR50 and FR52 and
between STGR 33 and 30 at RH side
1.00
Install the clamps between FR50 and FR52 at RH side
 1.00
Install a bracket on the shroud box blanking plate at
RH side
1.00
Modify the routing on rib 1 on the passage way to the
shroud box at RH side
1.00
Modify the routing of routes 2E and 2G in the leading
edge at RH wing
0.50
Remove the clamps from LH wing
 1.00
Remove the clamps from RH wing
 1.00
DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103
REVISION No.: 05 - Aug 20/18 Page: 27
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 52

@A300-600
SERVICE BULLETIN
Task 246103-831-801-001: Modification
Modify the Electrical Support Brackets in the Outer
Shroud Box, LH Wing
2.50
Modify the routing of routes 1P and 2P at LH wing
 1.50
Modify the routing of routes 1P and 2P at RH wing
 1.50
Install the clamps in LH wing
 1.00
Install the clamps in RH wing
 1.00
Modify the P-CLIPS at Location WOFX-204.5, LH Wing
 0.50
Modify the Backshell of the Connector and the
Structure at Location ABX 36.5, LH Wing
0.50
Modify the Electrical Support Brackets in the Outer
Shroud Box, RH Wing
2.50
Modify the P-CLIPS at Location WOFX-204.5, RH
Wing
0.50
Modify the Backshell of the Connector and the
Structure at Location ABX 36.5, RH Wing
0.50
Tests
 0.50
Close-Up
 5.00
TOTAL MANHOURS
 38.00
ELAPSED TIME (HOURS)
 21.75
NOTE
: For an explanation of the manhours and elapsed time, refer to the Gantt
Chart, Fig. A-FAAAA
 given in Appendix 01 - Elapsed Time Assumption
Task 246103-831-802-001: Modification - ADDITIONAL WORK between Revision No. 00 and
Revision No. 05
Get Access
 4.00
On Aircraft
Modify the routing on rib 1 on the passage way to the
shroud box at LH side, ADDITIONAL WORK
1.00
Modify the routing on rib 1 on the passage way to the
shroud box at RH side, ADDITIONAL WORK
1.00
Modify the routing of routes 1P and 2P in the shroud
box at LH side, ADDITIONAL WORK
1.00
Modify the routing of the routes 1E and 1G in the
leading edge at LH wing, ADDITIONAL WORK
1.00
Modify the routing of the routes 2E and 2G in the
leading edge at RH wing, ADDITIONAL WORK
1.00
Install a support on the support of the BLUE hydraulic
reservoir at LH wing, ADDITIONAL WORK
2.00
Install a bracket on the shroud box blanking plate at
LH side, ADDITIONAL WORK
1.00
Install a bracket on the shroud box blanking plate at
RH side, ADDITIONAL WORK
1.00
Remove the clamps between FR50 and FR51 at STRG
32 at LH side, ADDITIONAL WORK
0.50
DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103
REVISION No.: 05 - Aug 20/18 Page: 28
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 53

@A300-600
SERVICE BULLETIN
Task 246103-831-802-001: Modification - ADDITIONAL WORK between Revision No. 00 and
Revision No. 05
Remove the clamps of the Passage Way at FR52 (LH
side) - ADDITIONAL WORK
0.50
Modify the Routing between FR50 and FR52 and
between STGR 33 and 30 at LH side - ADDITIONAL
WORK
1.00
Install the clamps between FR50 and FR51 at STRG
32 at LH side, ADDITIONAL WORK
0.50
Install the clamps of the Passage Way at FR52 (LH
side) - ADDITIONAL WORK
0.50
Remove the clamps between FR50 and FR51 at STGR
32 at RH side, ADDITIONAL WORK
0.50
Remove the clamps of the Passage Way at FR52 (RH
side) - ADDITIONAL WORK
0.50
Modify the Routing between FR50 and FR52 and
between STGR 33 and 30 at RH side - ADDITIONAL
WORK
1.00
Install the clamps between FR50 and FR51 at STGR
32 at RH side, ADDITIONAL WORK
0.50
Install the clamps of the Passage Way at FR52 (RH
side) - ADDITIONAL WORK
0.50
Tests
 0.50
Close-Up
 5.00
TOTAL MANHOURS
 24.50
ELAPSED TIME (HOURS)
 16.50
NOTE
: For an explanation of the manhours and elapsed time, refer to the Gantt
Chart, Fig. A-FACAA
 given in Appendix 02 - Elapsed Time Assumption -
ADDITIONAL WORK between Revision No. 00 and Revision No. 05
Task 246103-831-804-001: Modification - ADDITIONAL WORK between Revision No. 01 and
Revision No. 05
Get Access
 4.00
On Aircraft
Remove the clamps between FR50 and FR52 at LH
side, ADDITIONAL WORK
1.00
Modify the routing between FR50 and FR52 and
between STGR 33 and 30 at LH side, ADDITIONAL
WORK
1.00
Install the clamps between FR50 and FR52 at LH side,
ADDITIONAL WORK
1.00
Install a bracket on the shroud box blanking plate at
LH side, ADDITIONAL WORK
1.00
Modify the routing on rib 1 on the passage way to the
shroud box at LH side, ADDITIONAL WORK
1.00
Modify the routing of routes 1P and 2P in the shroud
box at LH side, ADDITIONAL WORK
1.00
DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103
REVISION No.: 05 - Aug 20/18 Page: 29
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 54

@A300-600
SERVICE BULLETIN
Task 246103-831-804-001: Modification - ADDITIONAL WORK between Revision No. 01 and
Revision No. 05
Install a support on the support of the BLUE hydraulic
reservoir at LH wing - ADDITIONAL WORK
2.00
Modify the routing of the routes 1E and 1G in the
leading edge at LH wing, ADDITIONAL WORK
0.50
Remove the clamps between FR50 and FR52 at RH
side, ADDITIONAL WORK
1.00
Modify the routing between FR50 and FR52 and
between STGR 33 and 30 at RH side, ADDITIONAL
WORK
1.00
Install the clamps between FR50 and FR52 at RH side,
ADDITIONAL WORK
1.00
Install a bracket on the shroud box blanking plate at
RH side, ADDITIONAL WORK
1.00
Modify the routing on Rib 1 on the passage way to the
shroud box at RH side, ADDITIONAL WORK
1.00
Modify the routing of the routes 2E and 2G in the
leading edge at RH wing, ADDITIONAL WORK
0.50
Remove the clamps from LH wings, ADDITIONAL
WORK
1.00
Remove the clamps from RH wings, ADDITIONAL
WORK
1.00
Modify the routing of routes 1P and 2P at LH wing,
ADDITIONAL WORK
1.50
Modify the routing of routes 1P and 2P at RH wing,
ADDITIONAL WORK
1.50
Install the clamps in LH wing, ADDITIONAL WORK
 1.00
Install the clamps in RH wing, ADDITIONAL WORK
 1.00
Tests
 0.50
Close-Up
 5.00
TOTAL MANHOURS
 30.50
ELAPSED TIME (HOURS)
 16.50
NOTE
: For an explanation of the manhours and elapsed time, refer to the Gantt
Chart,
 Fig. A-FADAA
 given in Appendix 03 - Elapsed Time Assumption -
ADDITIONAL WORK between Revision No. 01 and Revision No. 05
Task 246103-831-805-001: Modification - ADDITIONAL WORK between Revision No. 02 and
Revision No. 05
Get Access
 4.00
On Aircraft
Modify the routing on Rib 1 on the passage way to the
shroud box at LH side, ADDITIONAL WORK
1.00
Modify the routing on Rib 1 on the passage way to the
shroud box at RH side, ADDITIONAL WORK
1.00
Remove the clamps from LH wing, ADDITIONAL
WORK
1.00
DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103
REVISION No.: 05 - Aug 20/18 Page: 30
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 55

@A300-600
SERVICE BULLETIN
Task 246103-831-805-001: Modification - ADDITIONAL WORK between Revision No. 02 and
Revision No. 05
Remove the clamps from RH wing, ADDITIONAL
WORK
1.00
Modify the routing of routes 1P and 2P at LH wing,
ADDITIONAL WORK
1.50
Modify the routing of routes 1P and 2P at RH wing,
ADDITIONAL WORK
1.50
Install the clamps in LH wing, ADDITIONAL WORK
 1.00
Install the clamps in RH wing, ADDITIONAL WORK
 1.00
Tests
 0.50
Close-Up
 5.00
TOTAL MANHOURS
 18.50
ELAPSED TIME (HOURS)
 9.50
NOTE
: For an explanation of the manhours and elapsed time, refer to the Gantt
Chart, Fig. A-FAFAB
 given in Appendix 04 - Elapsed Time Assumption -
ADDITIONAL WORK between Revision No. 02 and Revision No. 05
Task 246103-831-806-001: Modification - ADDITIONAL WORK between Revision No. 03 and
Revision No. 05
Get Access
 4.00
On Aircraft
Modify the Clamp on the routing on Rib 1 on the
passage way to the shroud box LH side, ADDITIONAL
WORK
0.50
Modify the Clamp on the routing on Rib 1 on the
passage way to the shroud box RH side, ADDITIONAL
WORK
0.50
Install the Spacers to the Guide Assembly - Conduit in
the LH Wing - ADDITIONAL WORK
0.25
Install the Spacers to the Guide Assembly - Conduit in
the RH Wing - ADDITIONAL WORK
0.25
Tests
 0.50
Close-Up
 5.00
TOTAL MANHOURS
 11.00
ELAPSED TIME (HOURS)
 5.75
NOTE
: For an explanation of the manhours and elapsed time, refer to the Gantt
Chart, Fig. A-FAGAB
 given in Appendix 05 - Elapsed Time Assumption -
ADDITIONAL WORK between Revision No. 03 and Revision No. 05
 .
Task 246103-831-807-001: Modification - ADDITIONAL WORK between Revision No. 04 and
Revision No. 05 and only if Revision No. 03 is also Embodied
Get Access
 4.00
On Aircraft
Install the Spacers to the Guide Assembly - Conduit in
the LH Wing - ADDITIONAL WORK
0.25
DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103
REVISION No.: 05 - Aug 20/18 Page: 31
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 56

@A300-600
SERVICE BULLETIN
Task 246103-831-807-001: Modification - ADDITIONAL WORK between Revision No. 04 and
Revision No. 05 and only if Revision No. 03 is also Embodied
Install the Spacers to the Guide Assembly - Conduit in
the RH Wing - ADDITIONAL WORK
0.25
Tests
 0.50
Close-Up
 5.00
TOTAL MANHOURS
 10.00
ELAPSED TIME (HOURS)
 5.25
NOTE
: For an explanation of the manhours and elapsed time, refer to the Gantt
Chart, Fig. A-FAHAA
 given in Appendix 06 - Elapsed Time Assumption -
ADDITIONAL WORK between Revision No. 04 and Revision No. 05 and only
if Revision No. 03 was also Embodied
 .
**CONF ALL
H. WEIGHT AND BALANCE
Not Changed
I. ELECTRICAL LOAD DATA
Not Changed
J. REFERENCES
**CONF 001
Aircraft Maintenance Manual (AMM)
 06-21-00 06-31-53 06-41-00
06-41-57 20-21-12 24-00-00
27-50-00 27-54-41 29-10-00
29-12-46 32-12-11 51-23-10
53-15-63
Consumable Material List (CML)
Elec. Std. Practices Manual (ESPM)
 20-33-00 20-33-11 20-33-30
20-33-41 20-33-42 20-33-44
20-33-45 20-55-00 20-56-51
Process and Material Specification (PMS)
 Process and Material Specification
(PMS) 01-01-28 Process E
Service Bulletin (SB)
 A300-24-6103
Standards Manual (SM)
Structural Repair Manual (SRM)
 51-21-00 51-21-10 51-23-10
51-40-00 51-40-20 51-40-30
51-40-40 51-40-50 51-75-10
**CONF 002
Aircraft Maintenance Manual (AMM)
 06-21-00 06-31-53 06-41-00
06-41-57 20-21-12 24-00-00
27-50-00 27-54-41 29-10-00
29-12-46 32-12-11 51-23-10
53-15-63
DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103
REVISION No.: 05 - Aug 20/18 Page: 32
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 57

@A300-600
SERVICE BULLETIN
Consumable Material List (CML)
Elec. Std. Practices Manual (ESPM)
 20-33-00 20-33-11 20-33-30
20-33-41 20-33-42 20-33-44
20-33-45 20-55-00 20-56-51
Process and Material Specification (PMS)
 Process and Material Specification
(PMS) 01-01-28 Process E
Standards Manual (SM)
Structural Repair Manual (SRM)
 51-21-00 51-21-10 51-23-10
51-40-00 51-40-20 51-40-30
51-40-40 51-40-50 51-75-10
**CONF 003
Aircraft Maintenance Manual (AMM)
 06-21-00 06-31-53 06-41-00
06-41-57 20-21-12 24-00-00
27-50-00 27-54-41 29-10-00
29-12-46 32-12-11 51-23-10
53-15-63
Consumable Material List (CML)
Elec. Std. Practices Manual (ESPM)
 20-33-00 20-33-11 20-33-30
20-33-41 20-33-42 20-33-44
20-33-45 20-55-00 20-56-51
Process and Material Specification (PMS)
 Process and Material Specification
(PMS) 01-01-28 Process E
Service Bulletin (SB)
 A300-24-6103
Standards Manual (SM)
Structural Repair Manual (SRM)
 51-21-00 51-21-10 51-23-10
51-40-00 51-40-20 51-40-30
51-40-40 51-40-50 51-75-10
**CONF ALL
K. PUBLICATION AFFECTED
Illustrated Parts Catalog (IPC)
 24-92-03
L. INTERCHANGEABILITY/MIXABILITY
Not Applicable
M. SPARES
None
DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103
REVISION No.: 05 - Aug 20/18 Page: 33
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 58

@A300-600
SERVICE BULLETIN
This Page Intentionally Left Blank
DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103
REVISION No.: 05 - Aug 20/18 Page: 34
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 59

@A300-600
SERVICE BULLETIN
2. MATERIAL INFORMATION
**CONF ALL
A. MATERIAL - PRICE AND AVAILABILITY
(1) Procurement Addresses
Customers with aircraft shown in the effectivity of this Service Bulletin should send a
purchase order to AIRBUS. Quote the number of this Service Bulletin. The address is :
Kit
 246103A01R15
Kit
 246103A02R13
Kit 246103A03R06
Kit 246103A04R01
Kit 246103A05R01
Kit
 246103A06R00
Kit
 246103A07R00
Supplementary kit 246103A01S03
Supplementary kit 246103A01S08
Supplementary kit 246103A01S14
Supplementary kit 246103A01S15
Supplementary kit 246103A01S13
Supplementary kit 246103A02S03
Supplementary kit 246103A02S07
Supplementary kit 246103A02S12
Supplementary kit 246103A02S13
Kit 246103B01R03
Kit 246103B02R02
AIRBUS Material, Logistics and Suppliers
ATP II B,
Hein-Sass-Weg 24
21129 HAMBURG
GERMANY
For ordering by internet:
http://spares.airbus.com
For ordering by E-mail: airbus.kit@airbus.com
Telephone Hotlines:
+49 40 743 51616
For standard hardware the purchase order shall be addressed to AIRBUS. Quote the
number of this Service Bulletin, the MSN and, if applicable the Retrofit Information Letter
(RIL) reference. Please send your request to:
Component
 COMPB01
 AIRBUS Material, Logistics and Suppliers
Standard Parts
For ordering by internet:
http://spares.airbus.com or vi a SPEC2000
For ordering by E-mail:
ifd.spares@airbus.com
Phone: +49 (0) 40 50 76 40 03
(2) Price and Availability
Kit
 246103A01R15
Cost
 5,530.00
 USD
Availability
 360 calendar days from receipt of order
The availability given above is the standard lead time from the date of your purchase
order. If items are required before this time, please include a retrofit planning schedule
with your order so that we can try to comply with your requirements.
DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103
REVISION No.: 05 - Aug 20/18 Page: 35
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 60

@A300-600
SERVICE BULLETIN
The sales terms (costs and availability) are estimated in relation to economic conditions.
The latest valid price and lead time for ordering purposes shall be obtained through the
AIRBUS Spares portal or through a request for quotation to airbus.kit@airbus.com.
Supplementary kit 246103A01S03
Cost
 3,090.00
 USD
Availability
 360 calendar days from receipt of order
The availability given above is the standard lead time from the date of your purchase
order. If items are required before this time, please include a retrofit planning schedule
with your order so that we can try to comply with your requirements.
The sales terms (costs and availability) are estimated in relation to economic conditions.
The latest valid price and lead time for ordering purposes shall be obtained through the
AIRBUS Spares portal or through a request for quotation to airbus.kit@airbus.com.
Supplementary kit 246103A01S08
Cost
 4,670.00
 USD
Availability
 360 calendar days from receipt of order
The availability given above is the standard lead time from the date of your purchase
order. If items are required before this time, please include a retrofit planning schedule
with your order so that we can try to comply with your requirements.
The sales terms (costs and availability) are estimated in relation to economic conditions.
The latest valid price and lead time for ordering purposes shall be obtained through the
AIRBUS Spares portal or through a request for quotation to airbus.kit@airbus.com.
Supplementary kit 246103A01S13
Cost
 55.00
 USD
Availability
 160 calendar days from receipt of order
The availability given above is the standard lead time from the date of your purchase
order. If items are required before this time, please include a retrofit planning schedule
with your order so that we can try to comply with your requirements.
The sales terms (costs and availability) are estimated in relation to economic conditions.
The latest valid price and lead time for ordering purposes shall be obtained through the
AIRBUS Spares portal or through a request for quotation to airbus.kit@airbus.com.
Supplementary kit 246103A01S14
Cost
 196.00
 USD
Availability
 340 calendar days from receipt of order
The availability given above is the standard lead time from the date of your purchase
order. If items are required before this time, please include a retrofit planning schedule
with your order so that we can try to comply with your requirements.
The sales terms (costs and availability) are estimated in relation to economic conditions.
The latest valid price and lead time for ordering purposes shall be obtained through the
AIRBUS Spares portal or through a request for quotation to airbus.kit@airbus.com.
DATE: Jun 17/10 SERVICE BULLETIN No.: A300-24-6103
REVISION No.: 05 - Aug 20/18 Page: 36
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

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