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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 28

TITLE: ELECTRIC/ELECTRONIC COMMON INSTALLATION - WING - IMPROVE

THE 2S-ROUTE IN THE RH-WING

MODIFICATION No.: 12427D21883 12435S22116 13478D23233

This page transmits Revision No.06 of Service Bulletin No.A310-28-2148

ADDITIONAL WORK

**CONF ALL

Additional work 3 is required on configurations 003, 004, 007 and 008 by this revision for aircraft

modified at revision 00, 01, 02 and 03 and without Service Bulletin A310-36-2015 (Modification No.

7633S7885) embodied.

ADDITIONAL WORK 1: applicable to Configuration 001, 002, 005 and 006 is required for aircraft that

have been modified by accomplishment of this Service Bulletin from the original issue up to revision 01.

The work which follows is required:

- segregation of the route 2S in RH pylon area

- installation of an additional protection sleeve in the outer wing area near the cadensicon sensor

10QT.

ADDITIONAL WORK 2: applicable to Configuration 001, 002, 005 and 006 is required for aircraft that

have been modified by accomplishment of this Service Bulletin from the original issue up to revision 02.

The work which follows is required:

- installation of an modified bracket on the RH wing.

ADDITIONAL WORK 3: applicable to Configuration 003, 004, 007 and 008 is required for aircraft that

have been modified by accomplishment of this Service Bulletin from the original issue up to revision 03.

The work which follows is required:

- improvement of the 2S route in the RH wing pylon area.

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

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SERVICE BULLETIN

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REASON

Revision No. 06 issued to update the additional work statement to add ADDITIONAL WORK 3.

The opportunity is taken to produce this Service Bulletin in the latest format.

Layout changes due to computerization of this revision are not identified.

CHANGES

SUMMARY

MODIFICATIONS Minor editorial or document structure change N

REASON/DESCRIPTION/OPERATIONAL

CONSEQUENCES

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GENERAL EVALUATION Minor editorial or document structure change N

MATERIAL PRICE INFORMATION Minor editorial or document structure change N

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EFFECTIVITY Minor editorial or document structure change N

CONCURRENT REQUIREMENTS Minor editorial or document structure change N

REFERENCES / REPERCUSSIONS Minor editorial or document structure change N

NATURE OF THE WORK Minor editorial or document structure change N

MANPOWER Minor editorial or document structure change N

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APPENDICES Minor editorial or document structure change N

Fig. A-GSAAA Minor editorial or document structure change N

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PLANNING INFORMATION

EFFECTIVITY Minor editorial or document structure change N

Configuration definition Minor editorial or document structure change N

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CONF 005 Minor editorial or document structure change N

CONF 006 Minor editorial or document structure change N

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CONF 008 Minor editorial or document structure change N

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CONCURRENT REQUIREMENTS Minor editorial or document structure change N

REASON Minor editorial or document structure change N

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Operational/Maintenance

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DESCRIPTION Minor editorial or document structure change N

COMPLIANCE Minor editorial or document structure change N

Classification Minor editorial or document structure change N

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APPROVAL Minor editorial or document structure change N

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WEIGHT AND BALANCE Minor editorial or document structure change N

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ELECTRICAL LOAD DATA Minor editorial or document structure change N

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PUBLICATION AFFECTED Minor editorial or document structure change N

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SPARES Minor editorial or document structure change N

MATERIAL INFORMATION

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Procurement Addresses Minor editorial or document structure change N

Price and Availability Minor editorial or document structure change N

INDUSTRY SUPPORT INFORMATION Minor editorial or document structure change N

LIST OF COMPONENTS Minor editorial or document structure change N

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LIST OF MATERIALS - OPERATOR

SUPPLIED

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PARTS TO BE RE-IDENTIFIED BY

OPERATOR

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TOOLING Minor editorial or document structure change N

ACCOMPLISHMENT INSTRUCTIONS

TASK 282148- 831-848-001-

MODIFICATION

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TASK 282148- 831-853-001-Modification -

ADDITIONAL WORK 1 (Introduced at Rev

02)

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TASK 282148- 831-849-001-Modification -

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03)

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TASK 282148- 831-850-001-Modification -

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06)

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Fig. A-GBJAA Sheet 07 Minor editorial or document structure change N

Fig. A-GBJAA Sheet 08 Minor editorial or document structure change N

Fig. A-GBJAA Sheet 09 Minor editorial or document structure change N

Fig. A-GBKAA Minor editorial or document structure change N

Fig. A-GBKAA Sheet 01 Minor editorial or document structure change N

Fig. A-GBKAA Sheet 02 Minor editorial or document structure change N

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 11

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Fig. A-GBKAA Sheet 03 Minor editorial or document structure change N

Fig. A-GBKAA Sheet 04 Minor editorial or document structure change N

Fig. A-GBKAA Sheet 05 Minor editorial or document structure change N

Fig. A-GBKAA Sheet 06 Minor editorial or document structure change N

Fig. A-GBKAA Sheet 07 Minor editorial or document structure change N

Fig. A-GBKAA Sheet 08 Minor editorial or document structure change N

Fig. A-GBKAA Sheet 09 Minor editorial or document structure change N

Fig. A-GHAAA Minor editorial or document structure change N

Fig. A-GHAAA Sheet 01 Minor editorial or document structure change N

Fig. A-GHBAA Minor editorial or document structure change N

Fig. A-GHBAA Sheet 01 Minor editorial or document structure change N

Fig. A-FCAAA Minor editorial or document structure change N

Fig. A-FCAAA Sheet 01 Minor editorial or document structure change N

Fig. A-FCBAA Minor editorial or document structure change N

Fig. A-FCBAA Sheet 01 Minor editorial or document structure change N

Fig. A-FCCAA Minor editorial or document structure change N

Fig. A-FCCAA Sheet 01 Minor editorial or document structure change N

Fig. A-FCCAB Minor editorial or document structure change N

Fig. A-FCCAB Sheet 01 Minor editorial or document structure change N

Fig. A-FWAAA Minor editorial or document structure change N

Fig. A-FWAAA Sheet 01 Minor editorial or document structure change N

Fig. A-UBAAA Minor editorial or document structure change N

Fig. A-UBAAA Sheet 01 Minor editorial or document structure change N

Fig. A-GBLAA Minor editorial or document structure change N

Fig. A-GBLAA Sheet 01 Minor editorial or document structure change N

Fig. A-GBLAA Sheet 02 Minor editorial or document structure change N

Fig. A-GBLAA Sheet 03 Minor editorial or document structure change N

Fig. A-GBMAA Minor editorial or document structure change N

Fig. A-GBMAA Sheet 01 Minor editorial or document structure change N

Fig. A-GBMAA Sheet 02 Minor editorial or document structure change N

Fig. A-GBMAA Sheet 03 Minor editorial or document structure change N

Fig. A-GBMAA Sheet 04 Minor editorial or document structure change N

Fig. A-GBMAA Sheet 05 Minor editorial or document structure change N

Fig. A-GBMAA Sheet 06 Minor editorial or document structure change N

Fig. A-GBMAA Sheet 07 Minor editorial or document structure change N

Fig. A-GBMAA Sheet 08 Minor editorial or document structure change N

Fig. A-UBCAA Minor editorial or document structure change N

Fig. A-UBCAA Sheet 01 Minor editorial or document structure change N

Fig. A-GBNAA Minor editorial or document structure change N

Fig. A-GBNAA Sheet 01 Minor editorial or document structure change N

Fig. A-GBNAA Sheet 02 Minor editorial or document structure change N

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 12

6

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@A310

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Fig. A-GBNAA Sheet 03 Minor editorial or document structure change N

Fig. A-GBNAA Sheet 04 Minor editorial or document structure change N

Fig. A-GBNAA Sheet 05 Minor editorial or document structure change N

Fig. A-GBNAA Sheet 06 Minor editorial or document structure change N

Fig. A-GBNAA Sheet 07 Minor editorial or document structure change N

Fig. A-GBNAA Sheet 08 Minor editorial or document structure change N

Fig. A-GBPAA Minor editorial or document structure change N

Fig. A-GBPAA Sheet 01 Minor editorial or document structure change N

Fig. A-GBPAB Minor editorial or document structure change N

Fig. A-GBPAB Sheet 01 Minor editorial or document structure change N

FILLING INSTRUCTIONS

This Service Bulletin has been generated electronically and is reissued as a complete document.

Replace the complete document.

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

HISTORY OF PREVIOUS REVISIONS

Revision No. 01 was issued to extend the effectivity and to add the applicable Kit A01 at the end of the

MSN list.

Revision No. 02 was issued to add the route 2S segregation in the RH pylon area and at the

cadensicon sensor 10QT, add Config. 01 for aircraft having Service Bulletin No. A310-28-2140

accomplished, add Config. 02 for aircraft having Service Bulletin No. A310-28-2140 not accomplished,

add ADDITIONAL WORK for Config. 01 and Config. 02, revise the manhours and to remove aircraft

MSN 0276, 0285, 0295, 0306, 0311, 0340, 0347, 0350, 0352, 0363, 0404, 0409, 0412, 0432, 0433,

0435, 0440, 0442, 0443, 0493, 0504 and 0570 from the effectivity.

This Revision 03 was issued to add Mod 13478D23233, add Kit B01, add Workstep for ADDITIONAL

WORK 2, remove aircraft MSNs 0172, 0300, 0451, 0453, 0501, 0540, 0548, 0589, 0598, 0634, 0690

and 0695 from the effectivity and update the operators, add figure 4 and revise figures 5 thru 13 to the

new standard and to introduce minor changes.

This Revision 04 was issued to incorporate the pre and post Service Bulletin A310-36-2015 (MOD. No.

7633S7885) configuration with Config. 03 and 04, and to delete the aircraft MSN 0254, 0273, 0397 and

400 from the effectivity.

Revision No. 05 was issued to remove MSN 0349 from the effectivity and add MSN’s 0254, 0273, 0397

and 0400 to the effectivity.

REVISION SEQUENCE

ORIGINAL: Jan 23/02

REVISION No.: 02 - Mar 09/07

REVISION No.: 03 - Jun 02/09

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 13

6

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@A310

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

REVISION No.: 04 - Apr 14/10

REVISION No.: 05 - Aug 03/10

REVISION No. : 06 - Aug 31/11

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 14

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

SUMMARY

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

This summary is for information only and is not approved for modification of the aircraft.

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 28

TITLE: ELECTRIC/ELECTRONIC COMMON INSTALLATION - WING - IMPROVE

THE 2S-ROUTE IN THE RH-WING

**CONF ALL

MODIFICATIONS

MODIFICATION CLASSIFICATION

MAJOR 13478D23233

MINOR 12427D21883 12435S22116

NOTE: As per EASA IR 21, a minor change is one that has no appreciable effect on the

mass, balance, structural strength, reliability, operational characteristics affecting the

airworthiness of the product. All other changes are major changes.

REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES

An analysis of the wire routing under the fuel system safety program has shown that the route 2S of

circuit QT in the RH-wing has to be modified to allow a better segregation between fuel quantity

indication wires and the 115V wires of the route 2S.

This Service Bulletin details the procedure to segregate the wires in the RH-wing by installation of

sleeves for the complete route 2S in the RH electronics rack 90VU, the FWD cargo compartment, the

RH forward wing root and krueger flap and in zones 612 and 623 of the wing.

The accomplishment of this modification will ensure the proper segregation of the fuel quantity

indication wires and the 115V wires in order to avoid interaction in the case of wire damage.

GENERAL EVALUATION

EVALUATION TABLE

COMPLIANCE MANDATORY (1) CANCELS INSPECTION SB NO

POTENTIAL AD YES A/C OPERATION AFFECTED NO

RELIABILITY AFFECTED NO PAX COMFORT AFFECTED NO

COST SAVING NO ETOPS AFFECTED NO

STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED NO

KIT PRICE (USD) See SB

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 1

6

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@A310

SERVICE BULLETIN

SUMMARY

NOTE (1): Service Bulletin must be accomplished.

MATERIAL PRICE INFORMATION

**CONF 001

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 282148A01R00 1 1,100.00 Sleeve, Tie

Kit 282148B01R00 1 90.00 Bracket, Rivet

Kit 282148D01R00 1 2,210.00 Clamp, Washer, Insulator, Screw,

Spacer, Cord , Tie

Kit 282148D02R01 1 1,580.00 Clamp, Washer, Insulator, Screw,

Spacer, Cord , Tie

TOTAL 4,980.00

**CONF 002

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 282148A01R00 1 1,100.00 Sleeve, Tie

Kit 282148B01R00 1 90.00 Bracket, Rivet

Kit 282148D01R00 1 2,210.00 Clamp, Washer, Insulator, Screw,

Spacer, Cord , Tie

Kit 282148D03R01 1 1,530.00 Clamp, Washer, Insulator, Screw,

Spacer, Cord , Tie

TOTAL 4,930.00

**CONF 003

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 282148A01R00 1 1,100.00 Sleeve, Tie

Kit 282148B01R00 1 90.00 Bracket, Rivet

Kit 282148D01R00 1 2,210.00 Clamp, Washer, Insulator, Screw,

Spacer, Cord , Tie

Kit 282148D05R01 1 570.00 Clamp, Washer, Screw, Spacer

Kit 282148D07R00 1 32.50 Clamp, Washer, Screw, Spacer

TOTAL 4,002.50

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 2

6

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@A310

SERVICE BULLETIN

SUMMARY

**CONF 004

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 282148A01R00 1 1,100.00 Sleeve, Tie

Kit 282148B01R00 1 90.00 Bracket, Rivet

Kit 282148D01R00 1 2,210.00 Clamp, Washer, Insulator, Screw,

Spacer, Cord , Tie

Kit 282148D06R01 1 560.00 Clamp, Washer, Screw, Spacer

Kit 282148D08R00 1 33.20 Clamp, Washer, Screw, Spacer

TOTAL 3,993.20

**CONF 005

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 282148A01R00 1 1,100.00 Sleeve, Tie

Kit 282148B01R00 1 90.00 Bracket, Rivet

Kit 282148D01R00 1 2,210.00 Clamp, Washer, Insulator, Screw,

Spacer, Cord , Tie

Kit 282148D02R01 1 1,580.00 Clamp, Washer, Insulator, Screw,

Spacer, Cord , Tie

TOTAL 4,980.00

**CONF 006

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 282148A01R00 1 1,100.00 Sleeve, Tie

Kit 282148B01R00 1 90.00 Bracket, Rivet

Kit 282148D01R00 1 2,210.00 Clamp, Washer, Insulator, Screw,

Spacer, Cord , Tie

Kit 282148D03R01 1 1,530.00 Clamp, Washer, Insulator, Screw,

Spacer, Cord , Tie

TOTAL 4,930.00

**CONF 007

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 282148A01R00 1 1,100.00 Sleeve, Tie

Kit 282148B01R00 1 90.00 Bracket, Rivet

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 3

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

SUMMARY

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 282148D01R00 1 2,210.00 Clamp, Washer, Insulator, Screw,

Spacer, Cord , Tie

Kit 282148D05R01 1 570.00 Clamp, Washer, Screw, Spacer

Kit 282148D07R00 1 32.50 Clamp, Washer, Screw, Spacer

TOTAL 4,002.50

**CONF 008

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 282148A01R00 1 1,100.00 Sleeve, Tie

Kit 282148B01R00 1 90.00 Bracket, Rivet

Kit 282148D01R00 1 2,210.00 Clamp, Washer, Insulator, Screw,

Spacer, Cord , Tie

Kit 282148D06R01 1 560.00 Clamp, Washer, Screw, Spacer

Kit 282148D08R00 1 33.20 Clamp, Washer, Screw, Spacer

TOTAL 3,993.20

EFFECTIVITY

**CONF ALL

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

18T 19U 46T 52X 58X 82Z 83V 85Z 98W 99Y AFG AIB AIC

BAF BBC CFC DAH DEC DGA F2I FDX G8E GAF HFY IRA IRM

IYE JAB JAV K1P KAC KZU MGL MWA PIA QAF R1T RJA ROT

RZO SBI SGX SUD THY TSC UBD UZB WHT WTJ

CONCURRENT REQUIREMENTS

None

REFERENCES / REPERCUSSIONS

TFU None

OEB None

AOT None

SIL None

LINE MAINTENANCE AFFECTED No

LIFE LIMIT None

OTHER SBIT 11-0012 dated 15 March 2011

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 4

6

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@A310

SERVICE BULLETIN

SUMMARY

NATURE OF THE WORK

AIRCRAFT YES

EQUIPMENT NO

HARD NO

SOFT NO

OBRM NO

MANPOWER

**CONF 001

Task 282148-831-848-001: MODIFICATION

TOTAL MANHOURS 40.00

ELAPSED TIME (HOURS) 14.00

Task 282148-831-853-001: Modification - ADDITIONAL WORK 1 (Introduced at Rev 02)

TOTAL MANHOURS 23.00

ELAPSED TIME (HOURS) 13.00

Task 282148-831-849-001: Modification - ADDITIONAL WORK 2 (Introduced at Rev 03)

TOTAL MANHOURS 3.00

ELAPSED TIME (HOURS) 3.00

Task 282148-831-850-001: Modification - ADDITIONAL WORK 3 (Introduced at Rev 06)

TOTAL MANHOURS 0.00

ELAPSED TIME (HOURS) 0.00

**CONF 002

Task 282148-831-848-001: MODIFICATION

TOTAL MANHOURS 32.00

ELAPSED TIME (HOURS) 14.00

Task 282148-831-853-001: Modification - ADDITIONAL WORK 1 (Introduced at Rev 02)

TOTAL MANHOURS 23.00

ELAPSED TIME (HOURS) 13.00

Task 282148-831-849-001: Modification - ADDITIONAL WORK 2 (Introduced at Rev 03)

TOTAL MANHOURS 3.00

ELAPSED TIME (HOURS) 3.00

Task 282148-831-850-001: Modification - ADDITIONAL WORK 3 (Introduced at Rev 06)

TOTAL MANHOURS 0.00

ELAPSED TIME (HOURS) 0.00

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 5

6

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@A310

SERVICE BULLETIN

SUMMARY

**CONF 003

Task 282148-831-848-001: MODIFICATION

TOTAL MANHOURS 32.00

ELAPSED TIME (HOURS) 14.00

Task 282148-831-853-001: Modification - ADDITIONAL WORK 1 (Introduced at Rev 02)

TOTAL MANHOURS 0.00

ELAPSED TIME (HOURS) 0.00

Task 282148-831-849-001: Modification - ADDITIONAL WORK 2 (Introduced at Rev 03)

TOTAL MANHOURS 0.00

ELAPSED TIME (HOURS) 0.00

Task 282148-831-850-001: Modification - ADDITIONAL WORK 3 (Introduced at Rev 06)

TOTAL MANHOURS 3.00

ELAPSED TIME (HOURS) 3.00

**CONF 004

Task 282148-831-848-001: MODIFICATION

TOTAL MANHOURS 32.00

ELAPSED TIME (HOURS) 14.00

Task 282148-831-853-001: Modification - ADDITIONAL WORK 1 (Introduced at Rev 02)

TOTAL MANHOURS 0.00

ELAPSED TIME (HOURS) 0.00

Task 282148-831-849-001: Modification - ADDITIONAL WORK 2 (Introduced at Rev 03)

TOTAL MANHOURS 0.00

ELAPSED TIME (HOURS) 0.00

Task 282148-831-850-001: Modification - ADDITIONAL WORK 3 (Introduced at Rev 06)

TOTAL MANHOURS 3.00

ELAPSED TIME (HOURS) 3.00

**CONF 005

Task 282148-831-848-001: MODIFICATION

TOTAL MANHOURS 40.00

ELAPSED TIME (HOURS) 14.00

Task 282148-831-853-001: Modification - ADDITIONAL WORK 1 (Introduced at Rev 02)

TOTAL MANHOURS 23.00

ELAPSED TIME (HOURS) 13.00

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 6

6

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@A310

SERVICE BULLETIN

SUMMARY

Task 282148-831-849-001: Modification - ADDITIONAL WORK 2 (Introduced at Rev 03)

TOTAL MANHOURS 3.00

ELAPSED TIME (HOURS) 3.00

Task 282148-831-850-001: Modification - ADDITIONAL WORK 3 (Introduced at Rev 06)

TOTAL MANHOURS 0.00

ELAPSED TIME (HOURS) 0.00

**CONF 006

Task 282148-831-848-001: MODIFICATION

TOTAL MANHOURS 32.00

ELAPSED TIME (HOURS) 14.00

Task 282148-831-853-001: Modification - ADDITIONAL WORK 1 (Introduced at Rev 02)

TOTAL MANHOURS 23.00

ELAPSED TIME (HOURS) 13.00

Task 282148-831-849-001: Modification - ADDITIONAL WORK 2 (Introduced at Rev 03)

TOTAL MANHOURS 3.00

ELAPSED TIME (HOURS) 3.00

Task 282148-831-850-001: Modification - ADDITIONAL WORK 3 (Introduced at Rev 06)

TOTAL MANHOURS 0.00

ELAPSED TIME (HOURS) 0.00

**CONF 007

Task 282148-831-848-001: MODIFICATION

TOTAL MANHOURS 32.00

ELAPSED TIME (HOURS) 14.00

Task 282148-831-853-001: Modification - ADDITIONAL WORK 1 (Introduced at Rev 02)

TOTAL MANHOURS 0.00

ELAPSED TIME (HOURS) 0.00

Task 282148-831-849-001: Modification - ADDITIONAL WORK 2 (Introduced at Rev 03)

TOTAL MANHOURS 0.00

ELAPSED TIME (HOURS) 0.00

Task 282148-831-850-001: Modification - ADDITIONAL WORK 3 (Introduced at Rev 06)

TOTAL MANHOURS 3.00

ELAPSED TIME (HOURS) 3.00

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 7

6

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@A310

SERVICE BULLETIN

SUMMARY

**CONF 008

Task 282148-831-848-001: MODIFICATION

TOTAL MANHOURS 32.00

ELAPSED TIME (HOURS) 14.00

Task 282148-831-853-001: Modification - ADDITIONAL WORK 1 (Introduced at Rev 02)

TOTAL MANHOURS 0.00

ELAPSED TIME (HOURS) 0.00

Task 282148-831-849-001: Modification - ADDITIONAL WORK 2 (Introduced at Rev 03)

TOTAL MANHOURS 0.00

ELAPSED TIME (HOURS) 0.00

Task 282148-831-850-001: Modification - ADDITIONAL WORK 3 (Introduced at Rev 06)

TOTAL MANHOURS 3.00

ELAPSED TIME (HOURS) 3.00

APPENDICES

**CONF ALL

None

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 8

6

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@A310

SERVICE BULLETIN

SUMMARY

**CONF ALL

TO 

2S

2S

INSTALLATION OF CABLE SLEEVES IN THE

INSTALLATION OF CABLE SLEEVES IN THE

INSTALLATION OF CABLE SLEEVES IN THE

RH ELECTRONICS RACK 90VU (KIT A01)

RH FORWARD WING ROOT AND KRUEGER FLAP (KIT A01)

FWD CARGO COMPARTMENT (KIT A01)

NOTE:

FR39

FR40

FR38.1

FR38.2

FR39

FR40

15QTB

2354VC Z140

Z120

Z612

Z623

B

C

A

F D E

FR20

A

B

C

B_SB_282148_6_SAAA_01_00

G

Figure A-GSAAA - Sheet 01

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 9

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@A310

SERVICE BULLETIN

SUMMARY

**CONF ALL

PYLON

FRONT SPAR

3R/1S

TRACK 1

SCREW JACK 1

SCREW JACK 2

TRACK 3

INSTALLATION OF CABLE SLEEVES IN THE

RH−WING FORWARD OF THE FRONT SPAR (KIT D01)

PYLON

SCREW JACK 3

1M

1S

MASTER TRACK 5

B_SB_282148_6_SAAA_02_00

RIB8

RIB7

RIB4

RIB3

RIB2

624VB /2S

624VB /2S

624VB/2S

636VB/2S

636VB/2M

RIB9

RIB10

RIB11

RIB12

TRACK 4

NOTE:

FRONT SPAR

D

E

3R/1S

Figure A-GSAAA - Sheet 02

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 10

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@A310

SERVICE BULLETIN

SUMMARY

**CONF ALL

F

5006VC 40VC

2S (QT)

2S 

636VB

52VP

44VP

B_SB_282148_6_SAAA_03_00

52VP

5006VC

2S (QT)

2S 

636VB

40VC

Figure A-GSAAA - Sheet 03

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 11

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@A310

SERVICE BULLETIN

SUMMARY

**CONF ALL

CENTERLINE

PYLON

D NOSE

SUB SPAR

VIEW LOOKING FWD

WOFZ 0.0

WDFX −53.0

WOFZ 0.0

WDFX −53.0

RIB8 RIB9

AFTER

BEFORE

SUB SPAR

VIEW LOOKING FWD

G

H

J

RETRO−FIT

BRACKET

ORIGINAL

BRACKET

H J

B_SB_282148_6_SAAA_04_00

Figure A-GSAAA - Sheet 04

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 12

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 28

TITLE: ELECTRIC/ELECTRONIC COMMON INSTALLATION - WING - IMPROVE

THE 2S-ROUTE IN THE RH-WING

MODIFICATION No.: 12427D21883 12435S22116 13478D23233

This document contains AIRBUS PROPRIETARY INFORMATION and shall at all times remain the

property of AIRBUS; no intellectual property right or licence is granted by AIRBUS in connection with

any information contained in it. It is delivered on the express condition that said document and the

information contained in it shall be treated as confidential, shall not be used for any purpose other than

that for which it is hereby delivered. It shall not be disclosed in whole or in part to third parties and shall

not be duplicated in any manner (except for the purposes of performing the tasks described hereunder

and provided that any recipient of such document shall comply with the conditions herein), without

AIRBUS prior written consent.

1. PLANNING INFORMATION

**CONF ALL

A. EFFECTIVITY

ADDITIONAL WORK 1: applicable to Configuration 001, 002, 005 and 006 is required for

aircraft that have been modified by accomplishment of this Service Bulletin from the original

issue up to revision 01.

The work which follows is required:

- segregation of the route 2S in RH pylon area

- installation of an additional protection sleeve in the outer wing area near the cadensicon

sensor 10QT.

ADDITIONAL WORK 2: applicable to Configuration 001, 002, 005 and 006 is required for

aircraft that have been modified by accomplishment of this Service Bulletin from the original

issue up to revision 02.

The work which follows is required:

- installation of an modified bracket on the RH wing.

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 1

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

ADDITIONAL WORK 3: applicable to Configuration 003, 004, 007 and 008 is required for

aircraft that have been modified by accomplishment of this Service Bulletin from the original

issue up to revision 03.

The work which follows is required:

- improvement of the 2S route in the RH wing pylon area.

(1) Models

310-203 310-204 310-221 310-222 310-304 310-308 310-322 310-324

310-325

(2) Effectivity by MSN

0162 0191 0201 0217 0224 0230 0233 0237 0241 0245 0248 0251 0254 0257 0260

0264 0267 0273 0278 0281 0283 0288 0291 0293 0297 0303 0309 0313 0316 0318

0320 0326 0331 0333 0335 0338-0339 0342-0343 0345-0346 0353 0355-0357

0359-0360 0362 0364 0367 0369-0370 0372 0375 0378-0379 0389-0390 0392 0394

0397 0399-0400 0406-0407 0410 0413 0416 0418-0419 0421-0422 0425 0427-0429

0431 0434 0436-0437 0439 0441 0444-0449 0452 0454 0456-0458 0467 0472-0473

0475-0476 0478 0480-0485 0487-0492 0494-0500 0502-0503 0519-0520 0522-0524

0526-0527 0531 0534 0537-0539 0541-0542 0544-0545 0547 0549-0552 0562

0564-0565 0567-0568 0571 0573-0574 0576 0585-0588 0590-0595 0597 0599-0600

0620 0622 0624 0636 0638 0642 0644 0646-0654 0656 0658 0660-0661 0663 0665

0667 0669 0671-0672 0674 0676 0678 0680 0682 0684 0686-0687 0689 0691 0693

0697 0700 0702 0704 0706

(3) Effectivity by Operator

The Operator/MSN relationship is provided for information only and is correct at the time

of issue in accordance with the information available to AIRBUS. Any future changes

resulting from transfer of an aircraft from one operator to another will not be reflected in

this list unless the Service Bulletin is revised for another reason.

OPERATOR MSN

18T 0473

19U 0399

46T 0413

52X 0410

58X 0431

82Z 0550 0551

83V 0427

85Z 0547

98W 0416

99Y 0489

AFG 0496 0497

AIB 0650 0674 0686

AIC 0392 0406 0407 0428 0429 0538 0544 0654 0665 0669 0680

BAF 0367 0372

BBC 0594 0642 0700

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 2

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SERVICE BULLETIN

OPERATOR MSN

CFC 0425 0441 0444 0446 0482

DAH 0291 0293

DEC 0684 0693 0697

DGA 0418 0421 0422

F2I 0309 0419 0487

FDX 0162 0191 0201 0217 0224 0230 0233 0237 0241 0245 0248 0251

0254 0257 0260 0264 0267 0273 0278 0281 0283 0288 0297 0303

0313 0316 0318 0326 0331 0333 0335 0339 0342 0343 0345 0346

0353 0355 0356 0359 0360 0362 0364 0369 0378 0394 0397 0400

0439 0449 0452 0454 0456 0457 0458 0467 0492 0500 0534 0539

0542 0549 0552 0593 0638

G8E 0475

GAF 0434 0484 0498 0499 0503 0522 0523

HFY 0495 0565

IRA 0338 0370 0375 0379 0389 0390 0436 0671

IRM 0488 0524 0537 0564 0567 0586 0595 0620

IYE 0568 0702 0704

JAB 0320

JAV 0357 0481

K1P 0648

KAC 0647 0649 0663

KZU 0592 0622 0646

MGL 0526

MWA 0652

PIA 0585 0587 0590 0653 0656 0660 0676 0678 0682 0687 0689 0691

QAF 0667

R1T 0591

RJA 0445 0490 0491 0531

ROT 0636 0644

RZO 0571 0624 0651 0661

SBI 0520

SGX 0519 0562

SUD 0437

THY 0476 0478 0480 0502

TSC 0447 0472 0483 0485 0527 0541 0545 0588 0597 0599 0600 0658

UBD 0672

UZB 0574 0576 0706

WHT 0448 0573

WTJ 0494

(4) Configuration by MSN

MSN CONFIGURATION

0162 0191 0201 0217 0224 0241 0245 0248 0260 0267 0273

0278 0303 0309 0313 0318 0326 0331 0335 0353 0355 0356

0357 0362 0364 0369 0394 0399 0410 0437 0439

002 004

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

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@A310

SERVICE BULLETIN

MSN CONFIGURATION

0230 0237 0254 0257 0288 0291 0293 0339 0342 0343 0345

0346 0359 0360 0379 0390 0397 0400 0419

001 002 003 004

0233 0320 0333 0338 0370 0375 0389 0392 0406 0407 0413

0416 0418 0421 0422 0425 0427 0428 0429 0441

003 004

0251 0264 0281 0283 0297 0316 0367 0372 0378 0431 0434

0436

004

0444 0445 0446 0447 0448 0472 0475 0476 0480 0481 0482

0487 0490 0491 0496 0497 0519 0520 0526 0531 0537 0538

0544

007 008

0449 0452 0457 0458 0473 0483 0484 0485 0488 0494 0495

0498 0499 0500 0502 0503 0522 0523 0527 0541 0545 0547

0550 0551 0562 0564 0565 0567 0568 0571 0573 0574 0576

0585 0586 0587 0588 0590 0592 0593 0595 0597 0599 0600

0620 0622 0624 0636 0638 0644 0646 0647 0648 0649 0651

0653 0654 0656 0658 0660 0661 0663 0665 0667 0671 0672

0674 0676 0678 0682 0684 0687 0689 0691 0693 0697 0700

0702 0704 0706

008

0454 0456 0467 0489 0492 0524 0534 0549 0552 0591 0594

0642 0650 0652 0669 0680 0686

006 008

0478 0539 0542 005 006 007 008

(5) Configuration definition

**CONF 001

Config. 001 is valid for aircraft up to MSN 0442 and having Service Bulletin Nos.

A310-28-2140 and A310-36-2015 accomplished or MOD. No. 7633S7885 embodied.

**CONF 002

Config. 002 is valid for aircraft up to MSN 0442 and not having Service Bulletin No.

A310-28-2140 accomplished but having Service Bulletin No. A310-36-2015

accomplished or MOD. No. 7633S7885 embodied.

**CONF 003

Config. 003 is valid for aircraft up to MSN 0442 and having Service Bulletin

A310-28-2140 accomplished but not having Service Bulletin No. A310-36-2015

accomplished or MOD. No. 7633S7885 not embodied.

**CONF 004

Config. 004 is valid for aircraft up to MSN 0442 and not having Service Bulletin Nos.

A310-28-2140 and A310-36-2015 accomplished or MOD. No. 7633S7885 not embodied.

**CONF 005

Config. 005 is valid for aircraft MSN 0442 and subsequent and having Service Bulletin

Nos. A310-28-2140 and A310-36-2015 accomplished or MOD. No. 7633S7885

embodied.

**CONF 006

Config. 006 is valid for aircraft MSN 0442 and subsequent and not having Service

Bulletin No. A310-28-2140 accomplished but having Service Bulletin No. A310-36-2015

accomplished or MOD. No. 7633S7885 embodied.

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 4

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@A310

SERVICE BULLETIN

**CONF 007

Config. 007 is valid for aircraft MSN 0442 and subsequent and having Service Bulletin

A310-28-2140 accomplished but not having Service Bulletin No. A310-36-2015

accomplished or MOD. No. 7633S7885 not embodied.

**CONF 008

Config. 008 is valid for aircraft MSN 0442 and subsequent and not having Service

Bulletin Nos. A310-28-2140 and A310-36-2015 accomplished or MOD. No. 7633S7885

not embodied.

(6) Material Effectivity

**CONF 001, 005

MATERIAL QTY PER A/C SEE NOTES

Kit 282148A01R00 1

Consumable CMLB01 1

Consumable CMLD01 As required

Kit 282148B01R00 1

Kit 282148D01R00 1

Kit 282148D02R01 1

**CONF 002, 006

MATERIAL QTY PER A/C SEE NOTES

Kit 282148A01R00 1

Consumable CMLB01 1

Consumable CMLD01 As required

Kit 282148B01R00 1

Kit 282148D01R00 1

Kit 282148D03R01 1

**CONF 003, 007

MATERIAL QTY PER A/C SEE NOTES

Kit 282148A01R00 1

Consumable CMLB01 1

Consumable CMLD01 As required

Kit 282148B01R00 1

Kit 282148D01R00 1

Kit 282148D05R01 1

Kit 282148D07R00 1

**CONF 004, 008

MATERIAL QTY PER A/C SEE NOTES

Kit 282148A01R00 1

Consumable CMLB01 1

Consumable CMLD01 As required

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 5

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@A310

SERVICE BULLETIN

MATERIAL QTY PER A/C SEE NOTES

Kit 282148B01R00 1

Kit 282148D01R00 1

Kit 282148D06R01 1

Kit 282148D08R00 1

**CONF ALL

B. CONCURRENT REQUIREMENTS

None

C. REASON

(1) History

An analysis of the wire routing under the fuel system safety program has shown that the

route 2S of circuit QT in the RH-wing has to be modified to allow a better segregation

between fuel quantity indication wires and the 115V wires of the route 2S.

(2) Objective/Action

This Service Bulletin details the procedure to segregate the wires in the RH-wing by

installation of sleeves for the complete route 2S in the RH electronics rack 90VU, the

FWD cargo compartment, the RH forward wing root and krueger flap and in zones 612

and 623 of the wing.

(3) Advantages

The accomplishment of this modification will ensure the proper segregation of the fuel

quantity indication wires and the 115V wires in order to avoid interaction in the case of

wire damage.

(4) Operational/Maintenance Consequences

None

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

**CONF 001

Task 282148-831-848-001: MODIFICATION

(1) Install a New Bracket on the Sub Spar Behind the Front Spar Between RIB 8 and

RIB 9 on the RH Wing

(2) Install cable sleeves in the RH Electronics Rack 90VU.

(3) Install cable sleeves between FR38.2 and FR39, in the forward cargo compartment.

(4) Install cable sleeves in the RH forward wing root and krueger flap.

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 6

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@A310

SERVICE BULLETIN

(5) Install the cable sleeves in the RH-wing forward of the front spar between rib 2 and

rib 3 in zone 612.

(6) Install the cable sleeves in the RH-wing forward of the front spar between rib 7 and

rib 8 in zone 612.

(7) Install the cable sleeves in the RH-wing forward of the front spar between rib 8 and

rib 9 (pylon area) in zone 612.

(8) Install the cable sleeves in the RH-wing forward of the front spar between rib 9 and

rib 12 in zone 623.

Task 282148-831-853-001: Modification - ADDITIONAL WORK 1 (Introduced at Rev 02)

(1) Modification

Task 282148-831-849-001: Modification - ADDITIONAL WORK 2 (Introduced at Rev 03)

(1) Introduce a New Bracket on the Sub Spar Behind the Front Spar Between RIB 8 and

RIB 9 on the RH Wing

**CONF 002

Task 282148-831-848-001: MODIFICATION

(1) Install a New Bracket on the Sub Spar Behind the Front Spar Between RIB 8 and

RIB 9 on the RH Wing

(2) Install cable sleeves in the RH Electronics Rack 90VU.

(3) Install cable sleeves between FR38.2 and FR39, in the forward cargo compartment.

(4) Install cable sleeves in the RH forward wing root and krueger flap.

(5) Install the cable sleeves in the RH-wing forward of the front spar between rib 2 and

rib 3 in zone 612.

(6) Install the cable sleeves in the RH-wing forward of the front spar between rib 7 and

rib 8 in zone 612.

(7) Install the cable sleeves in the RH-wing forward of the front spar between rib 8 and

rib 9 (pylon area) in zone 612.

(8) Install the cable sleeves in the RH-wing forward of the front spar between rib 9 and

rib 12 in zone 623.

Task 282148-831-853-001: Modification - ADDITIONAL WORK 1 (Introduced at Rev 02)

(1) Modification

Task 282148-831-849-001: Modification - ADDITIONAL WORK 2 (Introduced at Rev 03)

(1) Introduce a New Bracket on the Sub Spar Behind the Front Spar Between RIB 8 and

RIB 9 on the RH Wing

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 7

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SERVICE BULLETIN

**CONF 003

Task 282148-831-848-001: MODIFICATION

(1) Install a New Bracket on the Sub Spar Behind the Front Spar Between RIB 8 and

RIB 9 on the RH Wing

(2) Install cable sleeves in the RH Electronics Rack 90VU.

(3) Install cable sleeves between FR38.2 and FR39, in the forward cargo compartment.

(4) Install cable sleeves in the RH forward wing root and krueger flap.

(5) Install the cable sleeves in the RH-wing forward of the front spar between rib 2 and

rib 3 in zone 612.

(6) Install the cable sleeves in the RH-wing forward of the front spar between rib 7 and

rib 8 in zone 612.

(7) Install the cable sleeves in the RH-wing forward of the front spar between rib 8 and

rib 9 (pylon area) in zone 612.

(8) Install the cable sleeves in the RH-wing forward of the front spar between rib 9 and

rib 12 in zone 623.

Task 282148-831-850-001: Modification - ADDITIONAL WORK 3 (Introduced at Rev 06)

(1) Modification

**CONF 004

Task 282148-831-848-001: MODIFICATION

(1) Install a New Bracket on the Sub Spar Behind the Front Spar Between RIB 8 and

RIB 9 on the RH Wing

(2) Install cable sleeves in the RH Electronics Rack 90VU.

(3) Install cable sleeves between FR38.2 and FR39, in the forward cargo compartment.

(4) Install cable sleeves in the RH forward wing root and krueger flap.

(5) Install the cable sleeves in the RH-wing forward of the front spar between rib 2 and

rib 3 in zone 612.

(6) Install the cable sleeves in the RH-wing forward of the front spar between rib 7 and

rib 8 in zone 612.

(7) Install the cable sleeves in the RH-wing forward of the front spar between rib 8 and

rib 9 (pylon area) in zone 612.

(8) Install the cable sleeves in the RH-wing forward of the front spar between rib 9 and

rib 12 in zone 623.

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 8

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SERVICE BULLETIN

Task 282148-831-850-001: Modification - ADDITIONAL WORK 3 (Introduced at Rev 06)

(1) Modification

**CONF 005

Task 282148-831-848-001: MODIFICATION

(1) Install a New Bracket on the Sub Spar Behind the Front Spar Between RIB 8 and

RIB 9 on the RH Wing

(2) Install cable sleeves in the RH Electronics Rack 90VU.

(3) Install cable sleeves between FR38.2 and FR39, in the forward cargo compartment.

(4) Install cable sleeves in the RH forward wing root and krueger flap.

(5) Install the cable sleeves in the RH-wing forward of the front spar between rib 2 and

rib 3 in zone 612.

(6) Install the cable sleeves in the RH-wing forward of the front spar between rib 7 and

rib 8 in zone 612.

(7) Install the cable sleeves in the RH-wing forward of the front spar between rib 8 and

rib 9 (pylon area) in zone 612.

(8) Install the cable sleeves in the RH-wing forward of the front spar between rib 9 and

rib 12 in zone 623.

Task 282148-831-853-001: Modification - ADDITIONAL WORK 1 (Introduced at Rev 02)

(1) Modification

Task 282148-831-849-001: Modification - ADDITIONAL WORK 2 (Introduced at Rev 03)

(1) Introduce a New Bracket on the Sub Spar Behind the Front Spar Between RIB 8 and

RIB 9 on the RH Wing

**CONF 006

Task 282148-831-848-001: MODIFICATION

(1) Install a New Bracket on the Sub Spar Behind the Front Spar Between RIB 8 and

RIB 9 on the RH Wing

(2) Install cable sleeves in the RH Electronics Rack 90VU.

(3) Install cable sleeves between FR38.2 and FR39, in the forward cargo compartment.

(4) Install cable sleeves in the RH forward wing root and krueger flap.

(5) Install the cable sleeves in the RH-wing forward of the front spar between rib 2 and

rib 3 in zone 612.

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 9

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@A310

SERVICE BULLETIN

(6) Install the cable sleeves in the RH-wing forward of the front spar between rib 7 and

rib 8 in zone 612.

(7) Install the cable sleeves in the RH-wing forward of the front spar between rib 8 and

rib 9 (pylon area) in zone 612.

(8) Install the cable sleeves in the RH-wing forward of the front spar between rib 9 and

rib 12 in zone 623.

Task 282148-831-853-001: Modification - ADDITIONAL WORK 1 (Introduced at Rev 02)

(1) Modification

Task 282148-831-849-001: Modification - ADDITIONAL WORK 2 (Introduced at Rev 03)

(1) Introduce a New Bracket on the Sub Spar Behind the Front Spar Between RIB 8 and

RIB 9 on the RH Wing

**CONF 007

Task 282148-831-848-001: MODIFICATION

(1) Install a New Bracket on the Sub Spar Behind the Front Spar Between RIB 8 and

RIB 9 on the RH Wing

(2) Install cable sleeves in the RH Electronics Rack 90VU.

(3) Install cable sleeves between FR38.2 and FR39, in the forward cargo compartment.

(4) Install cable sleeves in the RH forward wing root and krueger flap.

(5) Install the cable sleeves in the RH-wing forward of the front spar between rib 2 and

rib 3 in zone 612.

(6) Install the cable sleeves in the RH-wing forward of the front spar between rib 7 and

rib 8 in zone 612.

(7) Install the cable sleeves in the RH-wing forward of the front spar between rib 8 and

rib 9 (pylon area) in zone 612.

(8) Install the cable sleeves in the RH-wing forward of the front spar between rib 9 and

rib 12 in zone 623.

Task 282148-831-850-001: Modification - ADDITIONAL WORK 3 (Introduced at Rev 06)

(1) Modification

**CONF 008

Task 282148-831-848-001: MODIFICATION

(1) Install a New Bracket on the Sub Spar Behind the Front Spar Between RIB 8 and

RIB 9 on the RH Wing

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 10

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@A310

SERVICE BULLETIN

(2) Install cable sleeves in the RH Electronics Rack 90VU.

(3) Install cable sleeves between FR38.2 and FR39, in the forward cargo compartment.

(4) Install cable sleeves in the RH forward wing root and krueger flap.

(5) Install the cable sleeves in the RH-wing forward of the front spar between rib 2 and

rib 3 in zone 612.

(6) Install the cable sleeves in the RH-wing forward of the front spar between rib 7 and

rib 8 in zone 612.

(7) Install the cable sleeves in the RH-wing forward of the front spar between rib 8 and

rib 9 (pylon area) in zone 612.

(8) Install the cable sleeves in the RH-wing forward of the front spar between rib 9 and

rib 12 in zone 623.

Task 282148-831-850-001: Modification - ADDITIONAL WORK 3 (Introduced at Rev 06)

(1) Modification

**CONF ALL

E. COMPLIANCE

(1) Classification

MANDATORY: Service Bulletin must be accomplished.

(2) Accomplishment Timescale

This Service Bulletin has been classified Mandatory by the issue of an Airworthiness

Directive (AD) published by the European Aviation Safety Agency (EASA). The AD must

be used as the reference document for the mandated accomplishment timescale.

F. APPROVAL

The technical content of this document is approved under the authority of the Design

Organisation Approval No. EASA.21J.031.

If an aircraft listed in the effectivity has a modification or repair embodied that is not of

AIRBUS origin, and which affects the content of this Service Bulletin, the operator is

responsible for obtaining approval by its airworthiness authority for any adaptation necessary

before incorporation of the Service Bulletin.

G. MANPOWER

The manpower estimates given in this Service Bulletin are based on the direct labor cost to

do the work. These estimates assume that the work will be done by experienced personnel,

and may need to be revised upwards to suit operator’s circumstances. The estimates do not

include the time to prepare, plan or inspect the work. Manufacture and procurement of parts

and tools, drying times for paints, sealants, etc., and general administration work are also not

included.

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 11

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@A310

SERVICE BULLETIN

**CONF 001

Task 282148-831-848-001: MODIFICATION

Get Access 11.00

On Aircraft

Install a New Bracket on the Sub Spar Behind the

Front Spar Between RIB 8 and RIB 9 on the RH Wing

1.00

Install cable sleeves in the RH Electronics Rack 90VU. 6.00

Install cable sleeves between FR38.2 and FR39, in the

forward cargo compartment.

1.00

Install cable sleeves in the RH forward wing root and

krueger flap.

2.00

Install the cable sleeves in the RH-wing forward of the

front spar between rib 2 and rib 3 in zone 612.

2.00

Install the cable sleeves in the RH-wing forward of the

front spar between rib 7 and rib 8 in zone 612.

2.00

Install the cable sleeves in the RH-wing forward of the

front spar between rib 8 and rib 9 (pylon area) in zone

612.

4.00

Install the cable sleeves in the RH-wing forward of the

front spar between rib 9 and rib 12 in zone 623.

4.00

Tests 3.00

Close-Up 4.00

TOTAL MANHOURS 40.00

ELAPSED TIME (HOURS) 14.00

Task 282148-831-853-001: Modification - ADDITIONAL WORK 1 (Introduced at Rev 02)

Get Access 3.00

On Aircraft

Modification 14.00

Tests 3.00

Close-Up 3.00

TOTAL MANHOURS 23.00

ELAPSED TIME (HOURS) 13.00

Task 282148-831-849-001: Modification - ADDITIONAL WORK 2 (Introduced at Rev 03)

Get Access 1.00

On Aircraft

Introduce a New Bracket on the Sub Spar Behind the

Front Spar Between RIB 8 and RIB 9 on the RH Wing

1.00

Tests 0.00

Close-Up 1.00

TOTAL MANHOURS 3.00

ELAPSED TIME (HOURS) 3.00

Task 282148-831-850-001: Modification - ADDITIONAL WORK 3 (Introduced at Rev 06)

Get Access 0.00

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 12

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@A310

SERVICE BULLETIN

Task 282148-831-850-001: Modification - ADDITIONAL WORK 3 (Introduced at Rev 06)

On Aircraft

Tests 0.00

Close-Up 0.00

TOTAL MANHOURS 0.00

ELAPSED TIME (HOURS) 0.00

**CONF 002

Task 282148-831-848-001: MODIFICATION

Get Access 11.00

On Aircraft

Install a New Bracket on the Sub Spar Behind the

Front Spar Between RIB 8 and RIB 9 on the RH Wing

1.00

Install cable sleeves in the RH Electronics Rack 90VU. 6.00

Install cable sleeves between FR38.2 and FR39, in the

forward cargo compartment.

1.00

Install cable sleeves in the RH forward wing root and

krueger flap.

2.00

Install the cable sleeves in the RH-wing forward of the

front spar between rib 2 and rib 3 in zone 612.

1.00

Install the cable sleeves in the RH-wing forward of the

front spar between rib 7 and rib 8 in zone 612.

1.00

Install the cable sleeves in the RH-wing forward of the

front spar between rib 8 and rib 9 (pylon area) in zone

612.

1.00

Install the cable sleeves in the RH-wing forward of the

front spar between rib 9 and rib 12 in zone 623.

1.00

Tests 3.00

Close-Up 4.00

TOTAL MANHOURS 32.00

ELAPSED TIME (HOURS) 14.00

Task 282148-831-853-001: Modification - ADDITIONAL WORK 1 (Introduced at Rev 02)

Get Access 3.00

On Aircraft

Modification 14.00

Tests 3.00

Close-Up 3.00

TOTAL MANHOURS 23.00

ELAPSED TIME (HOURS) 13.00

Task 282148-831-849-001: Modification - ADDITIONAL WORK 2 (Introduced at Rev 03)

Get Access 1.00

On Aircraft

Introduce a New Bracket on the Sub Spar Behind the

Front Spar Between RIB 8 and RIB 9 on the RH Wing

1.00

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 13

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@A310

SERVICE BULLETIN

Task 282148-831-849-001: Modification - ADDITIONAL WORK 2 (Introduced at Rev 03)

Tests 0.00

Close-Up 1.00

TOTAL MANHOURS 3.00

ELAPSED TIME (HOURS) 3.00

Task 282148-831-850-001: Modification - ADDITIONAL WORK 3 (Introduced at Rev 06)

Get Access 0.00

On Aircraft

Tests 0.00

Close-Up 0.00

TOTAL MANHOURS 0.00

ELAPSED TIME (HOURS) 0.00

**CONF 003

Task 282148-831-848-001: MODIFICATION

Get Access 11.00

On Aircraft

Install a New Bracket on the Sub Spar Behind the

Front Spar Between RIB 8 and RIB 9 on the RH Wing

1.00

Install cable sleeves in the RH Electronics Rack 90VU. 6.00

Install cable sleeves between FR38.2 and FR39, in the

forward cargo compartment.

1.00

Install cable sleeves in the RH forward wing root and

krueger flap.

2.00

Install the cable sleeves in the RH-wing forward of the

front spar between rib 2 and rib 3 in zone 612.

1.00

Install the cable sleeves in the RH-wing forward of the

front spar between rib 7 and rib 8 in zone 612.

1.00

Install the cable sleeves in the RH-wing forward of the

front spar between rib 8 and rib 9 (pylon area) in zone

612.

1.00

Install the cable sleeves in the RH-wing forward of the

front spar between rib 9 and rib 12 in zone 623.

1.00

Tests 3.00

Close-Up 4.00

TOTAL MANHOURS 32.00

ELAPSED TIME (HOURS) 14.00

Task 282148-831-853-001: Modification - ADDITIONAL WORK 1 (Introduced at Rev 02)

Get Access 0.00

On Aircraft

Tests 0.00

Close-Up 0.00

TOTAL MANHOURS 0.00

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 14

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

Task 282148-831-853-001: Modification - ADDITIONAL WORK 1 (Introduced at Rev 02)

ELAPSED TIME (HOURS) 0.00

Task 282148-831-849-001: Modification - ADDITIONAL WORK 2 (Introduced at Rev 03)

Get Access 0.00

On Aircraft

Tests 0.00

Close-Up 0.00

TOTAL MANHOURS 0.00

ELAPSED TIME (HOURS) 0.00

Task 282148-831-850-001: Modification - ADDITIONAL WORK 3 (Introduced at Rev 06)

Get Access 1.00

On Aircraft

Modification 1.00

Tests 0.00

Close-Up 1.00

TOTAL MANHOURS 3.00

ELAPSED TIME (HOURS) 3.00

**CONF 004

Task 282148-831-848-001: MODIFICATION

Get Access 11.00

On Aircraft

Install a New Bracket on the Sub Spar Behind the

Front Spar Between RIB 8 and RIB 9 on the RH Wing

1.00

Install cable sleeves in the RH Electronics Rack 90VU. 6.00

Install cable sleeves between FR38.2 and FR39, in the

forward cargo compartment.

1.00

Install cable sleeves in the RH forward wing root and

krueger flap.

2.00

Install the cable sleeves in the RH-wing forward of the

front spar between rib 2 and rib 3 in zone 612.

1.00

Install the cable sleeves in the RH-wing forward of the

front spar between rib 7 and rib 8 in zone 612.

1.00

Install the cable sleeves in the RH-wing forward of the

front spar between rib 8 and rib 9 (pylon area) in zone

612.

1.00

Install the cable sleeves in the RH-wing forward of the

front spar between rib 9 and rib 12 in zone 623.

1.00

Tests 3.00

Close-Up 4.00

TOTAL MANHOURS 32.00

ELAPSED TIME (HOURS) 14.00

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 15

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

Task 282148-831-853-001: Modification - ADDITIONAL WORK 1 (Introduced at Rev 02)

Get Access 0.00

On Aircraft

Tests 0.00

Close-Up 0.00

TOTAL MANHOURS 0.00

ELAPSED TIME (HOURS) 0.00

Task 282148-831-849-001: Modification - ADDITIONAL WORK 2 (Introduced at Rev 03)

Get Access 0.00

On Aircraft

Tests 0.00

Close-Up 0.00

TOTAL MANHOURS 0.00

ELAPSED TIME (HOURS) 0.00

Task 282148-831-850-001: Modification - ADDITIONAL WORK 3 (Introduced at Rev 06)

Get Access 1.00

On Aircraft

Modification 1.00

Tests 0.00

Close-Up 1.00

TOTAL MANHOURS 3.00

ELAPSED TIME (HOURS) 3.00

**CONF 005

Task 282148-831-848-001: MODIFICATION

Get Access 11.00

On Aircraft

Install a New Bracket on the Sub Spar Behind the

Front Spar Between RIB 8 and RIB 9 on the RH Wing

1.00

Install cable sleeves in the RH Electronics Rack 90VU. 6.00

Install cable sleeves between FR38.2 and FR39, in the

forward cargo compartment.

1.00

Install cable sleeves in the RH forward wing root and

krueger flap.

2.00

Install the cable sleeves in the RH-wing forward of the

front spar between rib 2 and rib 3 in zone 612.

2.00

Install the cable sleeves in the RH-wing forward of the

front spar between rib 7 and rib 8 in zone 612.

2.00

Install the cable sleeves in the RH-wing forward of the

front spar between rib 8 and rib 9 (pylon area) in zone

612.

4.00

Install the cable sleeves in the RH-wing forward of the

front spar between rib 9 and rib 12 in zone 623.

4.00

Tests 3.00

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 16

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

Task 282148-831-848-001: MODIFICATION

Close-Up 4.00

TOTAL MANHOURS 40.00

ELAPSED TIME (HOURS) 14.00

Task 282148-831-853-001: Modification - ADDITIONAL WORK 1 (Introduced at Rev 02)

Get Access 3.00

On Aircraft

Modification 14.00

Tests 3.00

Close-Up 3.00

TOTAL MANHOURS 23.00

ELAPSED TIME (HOURS) 13.00

Task 282148-831-849-001: Modification - ADDITIONAL WORK 2 (Introduced at Rev 03)

Get Access 1.00

On Aircraft

Introduce a New Bracket on the Sub Spar Behind the

Front Spar Between RIB 8 and RIB 9 on the RH Wing

1.00

Tests 0.00

Close-Up 1.00

TOTAL MANHOURS 3.00

ELAPSED TIME (HOURS) 3.00

Task 282148-831-850-001: Modification - ADDITIONAL WORK 3 (Introduced at Rev 06)

Get Access 0.00

On Aircraft

Tests 0.00

Close-Up 0.00

TOTAL MANHOURS 0.00

ELAPSED TIME (HOURS) 0.00

**CONF 006

Task 282148-831-848-001: MODIFICATION

Get Access 11.00

On Aircraft

Install a New Bracket on the Sub Spar Behind the

Front Spar Between RIB 8 and RIB 9 on the RH Wing

1.00

Install cable sleeves in the RH Electronics Rack 90VU. 6.00

Install cable sleeves between FR38.2 and FR39, in the

forward cargo compartment.

1.00

Install cable sleeves in the RH forward wing root and

krueger flap.

2.00

Install the cable sleeves in the RH-wing forward of the

front spar between rib 2 and rib 3 in zone 612.

1.00

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 17

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

Task 282148-831-848-001: MODIFICATION

Install the cable sleeves in the RH-wing forward of the

front spar between rib 7 and rib 8 in zone 612.

1.00

Install the cable sleeves in the RH-wing forward of the

front spar between rib 8 and rib 9 (pylon area) in zone

612.

1.00

Install the cable sleeves in the RH-wing forward of the

front spar between rib 9 and rib 12 in zone 623.

1.00

Tests 3.00

Close-Up 4.00

TOTAL MANHOURS 32.00

ELAPSED TIME (HOURS) 14.00

Task 282148-831-853-001: Modification - ADDITIONAL WORK 1 (Introduced at Rev 02)

Get Access 3.00

On Aircraft

Modification 14.00

Tests 3.00

Close-Up 3.00

TOTAL MANHOURS 23.00

ELAPSED TIME (HOURS) 13.00

Task 282148-831-849-001: Modification - ADDITIONAL WORK 2 (Introduced at Rev 03)

Get Access 1.00

On Aircraft

Introduce a New Bracket on the Sub Spar Behind the

Front Spar Between RIB 8 and RIB 9 on the RH Wing

1.00

Tests 0.00

Close-Up 1.00

TOTAL MANHOURS 3.00

ELAPSED TIME (HOURS) 3.00

Task 282148-831-850-001: Modification - ADDITIONAL WORK 3 (Introduced at Rev 06)

Get Access 0.00

On Aircraft

Tests 0.00

Close-Up 0.00

TOTAL MANHOURS 0.00

ELAPSED TIME (HOURS) 0.00

**CONF 007

Task 282148-831-848-001: MODIFICATION

Get Access 11.00

On Aircraft

Install a New Bracket on the Sub Spar Behind the

Front Spar Between RIB 8 and RIB 9 on the RH Wing

1.00

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 18

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

Task 282148-831-848-001: MODIFICATION

Install cable sleeves in the RH Electronics Rack 90VU. 6.00

Install cable sleeves between FR38.2 and FR39, in the

forward cargo compartment.

1.00

Install cable sleeves in the RH forward wing root and

krueger flap.

2.00

Install the cable sleeves in the RH-wing forward of the

front spar between rib 2 and rib 3 in zone 612.

1.00

Install the cable sleeves in the RH-wing forward of the

front spar between rib 7 and rib 8 in zone 612.

1.00

Install the cable sleeves in the RH-wing forward of the

front spar between rib 8 and rib 9 (pylon area) in zone

612.

1.00

Install the cable sleeves in the RH-wing forward of the

front spar between rib 9 and rib 12 in zone 623.

1.00

Tests 3.00

Close-Up 4.00

TOTAL MANHOURS 32.00

ELAPSED TIME (HOURS) 14.00

Task 282148-831-853-001: Modification - ADDITIONAL WORK 1 (Introduced at Rev 02)

Get Access 0.00

On Aircraft

Tests 0.00

Close-Up 0.00

TOTAL MANHOURS 0.00

ELAPSED TIME (HOURS) 0.00

Task 282148-831-849-001: Modification - ADDITIONAL WORK 2 (Introduced at Rev 03)

Get Access 0.00

On Aircraft

Tests 0.00

Close-Up 0.00

TOTAL MANHOURS 0.00

ELAPSED TIME (HOURS) 0.00

Task 282148-831-850-001: Modification - ADDITIONAL WORK 3 (Introduced at Rev 06)

Get Access 1.00

On Aircraft

Modification 1.00

Tests 0.00

Close-Up 1.00

TOTAL MANHOURS 3.00

ELAPSED TIME (HOURS) 3.00

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 19

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

**CONF 008

Task 282148-831-848-001: MODIFICATION

Get Access 11.00

On Aircraft

Install a New Bracket on the Sub Spar Behind the

Front Spar Between RIB 8 and RIB 9 on the RH Wing

1.00

Install cable sleeves in the RH Electronics Rack 90VU. 6.00

Install cable sleeves between FR38.2 and FR39, in the

forward cargo compartment.

1.00

Install cable sleeves in the RH forward wing root and

krueger flap.

2.00

Install the cable sleeves in the RH-wing forward of the

front spar between rib 2 and rib 3 in zone 612.

1.00

Install the cable sleeves in the RH-wing forward of the

front spar between rib 7 and rib 8 in zone 612.

1.00

Install the cable sleeves in the RH-wing forward of the

front spar between rib 8 and rib 9 (pylon area) in zone

612.

1.00

Install the cable sleeves in the RH-wing forward of the

front spar between rib 9 and rib 12 in zone 623.

1.00

Tests 3.00

Close-Up 4.00

TOTAL MANHOURS 32.00

ELAPSED TIME (HOURS) 14.00

Task 282148-831-853-001: Modification - ADDITIONAL WORK 1 (Introduced at Rev 02)

Get Access 0.00

On Aircraft

Close-Up 0.00

TOTAL MANHOURS 0.00

ELAPSED TIME (HOURS) 0.00

Task 282148-831-849-001: Modification - ADDITIONAL WORK 2 (Introduced at Rev 03)

Get Access 0.00

On Aircraft

Tests 0.00

Close-Up 0.00

TOTAL MANHOURS 0.00

ELAPSED TIME (HOURS) 0.00

Task 282148-831-850-001: Modification - ADDITIONAL WORK 3 (Introduced at Rev 06)

Get Access 1.00

On Aircraft

Modification 1.00

Tests 0.00

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 20

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

Task 282148-831-850-001: Modification - ADDITIONAL WORK 3 (Introduced at Rev 06)

Close-Up 1.00

TOTAL MANHOURS 3.00

ELAPSED TIME (HOURS) 3.00

**CONF ALL

H. WEIGHT AND BALANCE

**CONF 001, 005

The weight and balance estimates given in this Service Bulletin are based on the

Manufacturer’s Empty Weight (MEW) and do not include operator item’s. For the definition of

MEW and operator’s items, refer to the 01-00-07

Manufacturers Empty Weight +1.856 KG (+4.0917 LB)

Effect on Balance +41.89 KGM (+297.196 LB.FT)

ADDITIONAL WORK 1

Manufacturers Empty Weight +0.336 KG (+0.7407 LB)

Effect on Balance +9.186 KGM (+66.442 LB.FT)

ADDITIONAL WORK 2

Manufacturers Empty Weight +0.437 KG (+0.9634 LB)

Effect on Balance +11.948 KGM (+86.419 LB.FT)

**CONF 002, 006

The weight and balance estimates given in this Service Bulletin are based on the

Manufacturer’s Empty Weight (MEW) and do not include operator item’s. For the definition of

MEW and operator’s items, refer to the 01-00-07

Manufacturers Empty Weight +1.883 KG (+4.1512 LB)

Effect on Balance +41.705 KGM (+301.652 LB.FT)

ADDITIONAL WORK 1

Manufacturers Empty Weight +0.437 KG (+0.9634 LB)

Effect on Balance +11.948 KGM (+86.419 LB.FT)

ADDITIONAL WORK 2

Not Changed

**CONF 003, 007

The weight and balance estimates given in this Service Bulletin are based on the

Manufacturer’s Empty Weight (MEW) and do not include operator item’s. For the definition of

MEW and operator’s items, refer to the 01-00-07

Manufacturers Empty Weight +2.492 KG (+5.4938 LB)

Effect on Balance +55.177 KGM (+399.095 LB.FT)

ADDITIONAL WORK 3

Not Changed

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 21

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

**CONF 004, 008

The weight and balance estimates given in this Service Bulletin are based on the

Manufacturer’s Empty Weight (MEW) and do not include operator item’s. For the definition of

MEW and operator’s items, refer to the 01-00-07

Manufacturers Empty Weight +2.569 KG (+5.6636 LB)

Effect on Balance +56.889 KGM (+411.478 LB.FT)

ADDITIONAL WORK 3

Not Changed

**CONF ALL

I. ELECTRICAL LOAD DATA

Not Changed

J. REFERENCES

**CONF 001

Aircraft Maintenance Manual (AMM) 06-41-53 06-41-57 24-00-00

24-31-11 24-41-00 25-54-10

27-28-00 27-80-00 27-84-00

28-42-44 30-11-00 36-11-00

52-10-00 52-30-00 53-10-55

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-25-21 20-33-00 20-52-00

20-52-21 20-55-00

Standards Manual (SM)

Structural Repair Manual (SRM) 51-23-10 51-23-11 51-40-21

51-40-44 51-42-11

Weight and Balance Manual (WBM) 01-00-07

**CONF 002

Aircraft Maintenance Manual (AMM) 06-41-53 06-41-57 24-00-00

24-31-11 24-41-00 25-54-10

27-28-00 27-80-00 27-84-00

28-42-44 30-11-00 36-11-00

52-10-00 52-30-00 53-10-55

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-25-21 20-33-00 20-52-00

20-52-21 20-55-00

Standards Manual (SM)

Structural Repair Manual (SRM) 51-23-10 51-23-11 51-40-21

51-40-44 51-42-11

Weight and Balance Manual (WBM) 01-00-07

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 22

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

**CONF 003

Aircraft Maintenance Manual (AMM) 06-41-53 06-41-57 24-00-00

24-31-11 24-41-00 25-54-10

27-84-00 28-42-44 30-11-00

36-11-00 52-10-00 52-30-00

53-10-55

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-25-21 20-33-00 20-55-00

Standards Manual (SM)

Structural Repair Manual (SRM) 51-23-10 51-23-11 51-40-21

51-40-44 51-42-11

Weight and Balance Manual (WBM) 01-00-07

**CONF 004

Aircraft Maintenance Manual (AMM) 06-41-53 06-41-57 24-00-00

24-31-11 24-41-00 25-54-10

27-84-00 28-42-44 30-11-00

36-11-00 52-10-00 52-30-00

53-10-55

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-25-21 20-33-00 20-55-00

Standards Manual (SM)

Structural Repair Manual (SRM) 51-23-10 51-23-11 51-40-21

51-40-44 51-42-11

Weight and Balance Manual (WBM) 01-00-07

**CONF 005

Aircraft Maintenance Manual (AMM) 06-41-53 06-41-57 24-00-00

24-31-11 24-41-00 25-54-10

27-28-00 27-80-00 27-84-00

28-42-44 30-11-00 36-11-00

52-10-00 52-30-00 53-10-55

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-25-21 20-33-00 20-52-00

20-52-21 20-55-00

Standards Manual (SM)

Structural Repair Manual (SRM) 51-23-10 51-23-11 51-40-21

51-40-44 51-42-11

Weight and Balance Manual (WBM) 01-00-07

**CONF 006

Aircraft Maintenance Manual (AMM) 06-41-53 06-41-57 24-00-00

24-31-11 24-41-00 25-54-10

27-28-00 27-80-00 27-84-00

28-42-44 30-11-00 36-11-00

52-10-00 52-30-00 53-10-55

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 23

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-25-21 20-33-00 20-52-00

20-52-21 20-55-00

Standards Manual (SM)

Structural Repair Manual (SRM) 51-23-10 51-23-11 51-40-21

51-40-44 51-42-11

Weight and Balance Manual (WBM) 01-00-07

**CONF 007

Aircraft Maintenance Manual (AMM) 06-41-53 06-41-57 24-00-00

24-31-11 24-41-00 25-54-10

27-84-00 28-42-44 30-11-00

36-11-00 52-10-00 52-30-00

53-10-55

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-25-21 20-33-00 20-55-00

Standards Manual (SM)

Structural Repair Manual (SRM) 51-23-10 51-23-11 51-40-21

51-40-44 51-42-11

Weight and Balance Manual (WBM) 01-00-07

**CONF 008

Aircraft Maintenance Manual (AMM) 06-41-53 06-41-57 24-00-00

24-31-11 24-41-00 25-54-10

27-84-00 28-42-44 30-11-00

36-11-00 52-10-00 52-30-00

53-10-55

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-25-21 20-33-00 20-55-00

Standards Manual (SM)

Structural Repair Manual (SRM) 51-23-10 51-23-11 51-40-21

51-40-44 51-42-11

Weight and Balance Manual (WBM) 01-00-07

**CONF ALL

K. PUBLICATION AFFECTED

Aircraft Wiring Manual (AWM) 28-42-07

Illustrated Parts Catalog (IPC) 24-92-03

L. INTERCHANGEABILITY/MIXABILITY

Not Applicable

M. SPARES

None

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 24

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

(1) Procurement Addresses

Customers with aircraft shown in the effectivity of this Service Bulletin should send a

purchase order to AIRBUS. Quote the number of this Service Bulletin. The address is:

Kit 282148A01R00

Kit 282148B01R00

Kit 282148D01R00

Kit 282148D02R01

Kit 282148D03R01

Kit 282148D05R01

Kit 282148D06R01

Kit 282148D07R00

Kit 282148D08R00

AIRBUS

MATERIAL LOGISTICS AND SUPPLIERS

Weg beim Jaeger 150

D-22335 HAMBURG

GERMANY

For ordering by internet:

http://spares.airbus.com

For ordering modification kits by fax: +49 40

50 76 25 90

For ordering of single spares by fax: +49 40

50 76 40 12

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

(2) Price and Availability

Kit 282148A01R00

Cost 1,100.00 USD

Availability 30 calendar days from receipt of order

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

order. If you require Kits before this time, please include a retrofit planning schedule with

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

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

at the issue date of the Service Bulletin.

Kit 282148B01R00

Cost 90.00 USD

Availability 90 calendar days from receipt of order

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

order. If you require the Kit(s) before this time, please include a retrofit planning

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

Kit 282148D01R00

Cost 2,210.00 USD

Availability 90 calendar days from receipt of order

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

order. If you require the Kit(s) before this time, please include a retrofit planning

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

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 25

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

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

conditions at the issue date of the Service Bulletin.

Kit 282148D02R01

Cost 1,580.00 USD

Availability 90 calendar days from receipt of order

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

order. If you require the Kit(s) before this time, please include a retrofit planning

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

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

conditions at the issue date of the Service Bulletin.

Kit 282148D03R01

Cost 1,530.00 USD

Availability 90 calendar days from receipt of order

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

order. If you require the Kit(s) before this time, please include a retrofit planning

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

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

conditions at the issue date of the Service Bulletin.

Kit 282148D05R01

Cost 570.00 USD

Availability 90 calendar days from receipt of order

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

order. If you require the Kit(s) before this time, please include a retrofit planning

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

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

conditions at the issue date of the Service Bulletin.

Kit 282148D06R01

Cost 560.00 USD

Availability 90 calendar days from receipt of order

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

order. If you require the Kit(s) before this time, please include a retrofit planning

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

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

conditions at the issue date of the Service Bulletin.

Kit 282148D07R00

Cost 32.50 USD

Availability 90 calendar days from receipt of order

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 26

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

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

order. If you require the Kit(s) before this time, please include a retrofit planning

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

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

conditions at the issue date of the Service Bulletin.

Kit 282148D08R00

Cost 33.20 USD

Availability 90 calendar days from receipt of order

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

order. If you require the Kit(s) before this time, please include a retrofit planning

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

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

conditions at the issue date of the Service Bulletin.

B. INDUSTRY SUPPORT INFORMATION

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

C. LIST OF COMPONENTS

Kit 282148A01R00

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

NOTES

1 ABS0596S004 2000 SLEEVE

2 ABS0596S006 2000

(mm)

SLEEVE

NSA935401-04 50 TIE

NSA935401-05 100 TIE

NOTE: If you find part numbers of hardware components in the related kit(s) which

you cannot identify in the LIST OF COMPONENTS of this Service Bulletin,

refer to Standards Manual (SM). The SM will give you the correct part number

to part number relationship.

Kit 282148D01R00

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

NOTES

1 ABS0596S004 12 SLEEVE

10 MS21919WCH9 8 CLAMP

11 MS21919WCH13 2 CLAMP

12 MS21919WCH14 2 CLAMP

14 NAS1096-3-19 2 SCREW

15 NSA5527-03-03 3 SPACER

16 NSA8420-2 0.5 (ME) CORD

149 NSA935401-03 31 TIE

150 NSA935401-04 47 TIE

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 27

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NOTE: If you find part numbers of hardware components in the related kit(s) which

you cannot identify in the LIST OF COMPONENTS of this Service Bulletin,

refer to Standards Manual (SM). The SM will give you the correct part number

to part number relationship.

Kit 282148D02R01

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

NOTES

1 ABS0596S004 3 SLEEVE

10 MS21919WCH9 1 CLAMP

30 NSA5527-03-01D 2 SPACER

31 NSA5527-03-02D 1 SPACER

109 NSA935805-09 3 (ME) CONDUIT

117 NSA935807C09 12 CLAMP

121 NAS1096-3-40 1 SCREW

125 B9299071900200 1 EQUIPMNT

126 NSA938184PV1601 15 PIN

149 NSA935401-03 30 TIE

150 NSA935401-04 30 TIE

NOTE: If you find part numbers of hardware components in the related kit(s) which

you cannot identify in the LIST OF COMPONENTS of this Service Bulletin,

refer to Standards Manual (SM). The SM will give you the correct part number

to part number relationship.

Kit 282148D03R01

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

NOTES

1 ABS0596S004 3 SLEEVE

10 MS21919WCH9 1 CLAMP

31 NSA5527-03-02D 3 SPACER

109 NSA935805-09 CONDUIT

117 NSA935807C09 7 CLAMP

121 NAS1096-3-40 1 SCREW

123 NAS1801-3-31 3 SCREW

126 NSA938184PV1601 7 PIN

130 NSA5527-03-08D 2 SPACER

131 NSA5527-03-07D 2 SPACER

132 B9299071900600 1 EQUIPMNT

149 NSA935401-03 30 TIE

150 NSA935401-04 40 TIE

NOTE: If you find part numbers of hardware components in the related kit(s) which

you cannot identify in the LIST OF COMPONENTS of this Service Bulletin,

refer to Standards Manual (SM). The SM will give you the correct part number

to part number relationship.

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

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Kit 282148D05R01

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

NOTES

1 ABS0596S004 3 SLEEVE

30 NSA5527-03-01D 2 SPACER

31 NSA5527-03-02D 1 SPACER

109 NSA935805-09 3 (ME) CONDUIT

117 NSA935807C09 12 CLAMP

125 B9299071900200 1 EQUIPMNT

126 NSA938184PV1601 15 PIN

135 NAS1096-3-42 1 SCREW

136 NAS1096-3-30 1 SCREW

149 NSA935401-03 30 TIE

150 NSA935401-04 30 TIE

NOTE: If you find part numbers of hardware components in the related kit(s) which

you cannot identify in the LIST OF COMPONENTS of this Service Bulletin,

refer to Standards Manual (SM). The SM will give you the correct part number

to part number relationship.

Kit 282148D06R01

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

NOTES

1 ABS0596S004 3 SLEEVE

31 NSA5527-03-02D 2 SPACER

109 NSA935805-09 1.5 (ME) CONDUIT

117 NSA935807C09 7 CLAMP

121 NAS1096-3-40 1 SCREW

123 NAS1801-3-31 2 SCREW

126 NSA938184PV1601 7 PIN

130 NSA5527-03-08D 1 SPACER

131 NSA5527-03-07D 1 SPACER

132 B9299071900600 1 EQUIPMNT

149 NSA935401-03 30 TIE

150 NSA935401-04 30 TIE

NOTE: If you find part numbers of hardware components in the related kit(s) which

you cannot identify in the LIST OF COMPONENTS of this Service Bulletin,

refer to Standards Manual (SM). The SM will give you the correct part number

to part number relationship.

Kit 282148D07R00

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

NOTES

31 NSA5527-03-02D 2 SPACER

110 NSA935807C10 1 CLAMP

112 NAS1149D0332K 1 WASHER

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

NOTES

117 NSA935807C09 3 CLAMP

120 NSA5516-04NV 1 CLAMP

130 NSA5527-03-08D 1 SPACER

135 NAS1096-3-42 1 SCREW

NOTE: If you find part numbers of hardware components in the related kit(s) which

you cannot identify in the LIST OF COMPONENTS of this Service Bulletin,

refer to Standards Manual (SM). The SM will give you the correct part number

to part number relationship.

Kit 282148D08R00

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

NOTES

30 NSA5527-03-01D 1 SPACER

31 NSA5527-03-02D 1 SPACER

111 NSA935807C16 2 CLAMP

112 NSA935808-01 1 WASHER

117 NSA935807C09 1 CLAMP

120 NSA5516-04NV 1 CLAMP

123 NAS1801-3-31 1 SCREW

130 NSA5527-03-08D 1 SPACER

NOTE: If you find part numbers of hardware components in the related kit(s) which

you cannot identify in the LIST OF COMPONENTS of this Service Bulletin,

refer to Standards Manual (SM). The SM will give you the correct part number

to part number relationship.

Kit 282148B01R00

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

NOTES

1 A5725068600000 1 Bracket

2 ASNA0078A502 2 Rivet

NOTE: If you find part numbers of hardware components in the related kit(s) which

you cannot identify in the LIST OF COMPONENTS of this Service Bulletin,

refer to Standards Manual (SM). The SM will give you the correct part number

to part number relationship.

D. LIST OF MATERIALS - OPERATOR SUPPLIED

(1) Consumable Materials

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO CML

MAT. No.

QTY PER A/C SEE

NOTES

Storage compound 15-008A As required

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Consumable CMLB01

ITEM DESCRIPTION REFERENCE TO CML

MAT. No.

QTY PER A/C SEE

NOTES

Corrosion Inhibiting Low Adhesion

Sealant

09-018 As required

Solvent General Purpose 11-026 As required

Lint-Free Cotton Cloth 19-003 As required

(2) Components

None

(3) Equipment

None

E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

None

F. TOOLING

None

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

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This Page Intentionally Left Blank

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

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SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS

Task 282148-831-848-001 - MODIFICATION

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

INCLUDED IN THE REFERENCED PROCEDURES.

WARNING: THIS PROCEDURE USES A FUEL SYSTEM ITEM THAT IS IN A CATEGORY

KNOWN AS A CRITICAL DESIGN CONFIGURATION CONTROL LIMITATION

(CDCCL) CDCCL IDENTIFIES AN ITEM THAT CAN BE THE SOURCE OF A

POSSIBLE FUEL TANK IGNITION. YOU MUST KEEP ALL CDCCL ITEMS IN

THE APPROVED CONFIGURATION. DAMAGE, WEAR OR CHANGES TO A

CDCCL ITEM CAN CAUSE A POSSIBLE FUEL TANK EXPLOSION.

CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP

ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY

AND MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENANCE

WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING,

COMPONENTS AND THE WORK AREA AS CLEAN AS POSSIBLE, TO DO

THIS:

- PUT PROTECTION, SUCH AS PLASTIC SHEETING, CLOTHS, ETC; AS

NECESSARY ON WIRING AND COMPONENTS

- REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND

OTHER CONTAMINATION.

THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION

AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION.

IF THERE IS CONTAMINATION, REFER TO ESPM 20-55-00.

Task Associated Data

**CONF 001

Manpower

TOTAL MANHOURS 40.00

ELAPSED TIME (HOURS) 14.00

**CONF 002

Manpower

TOTAL MANHOURS 32.00

ELAPSED TIME (HOURS) 14.00

**CONF 003

Manpower

TOTAL MANHOURS 32.00

ELAPSED TIME (HOURS) 14.00

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

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**CONF 004

Manpower

TOTAL MANHOURS 32.00

ELAPSED TIME (HOURS) 14.00

**CONF 005

Manpower

TOTAL MANHOURS 40.00

ELAPSED TIME (HOURS) 14.00

**CONF 006

Manpower

TOTAL MANHOURS 32.00

ELAPSED TIME (HOURS) 14.00

**CONF 007

Manpower

TOTAL MANHOURS 32.00

ELAPSED TIME (HOURS) 14.00

**CONF 008

Manpower

TOTAL MANHOURS 32.00

ELAPSED TIME (HOURS) 14.00

**CONF ALL

A. GENERAL

**CONF 001

(1) Subtask 282148-910-401-001 - Standard Practices

Manpower Resources

Skills AIRFRAME

References

Structural Repair Manual (SRM) 51-23-10

51-40-21

51-40-44

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

Consumable Material List (CML).

(b) For fastener hole and drill data (Refer to SRM 51-40-44).

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

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SERVICE BULLETIN

(c) For paint coatings (Refer to SRM 51-23-10).

(d) Installation of fasteners (Refer to SRM 51-40-21).

(2) Subtask 282148-910-204-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

Material necessary to do the job

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Storage compound 15-008A As required

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Consumable Material List (CML)

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

(a) For panel location (Refer to AMM 06-41-53, Page Block 001).

(b) Obey the instructions for the wiring installation (Refer to ESPM 20-33-00).

(c) Apply:

Storage compound 15-008A As required

to the screws after assembly.

(3) Subtask 282148-900-202-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

Write in the applicable aircraft records that you have done all the work given in this

Service Bulletin.

**CONF 002

(1) Subtask 282148-910-401-001 - Standard Practices

Manpower Resources

Skills AIRFRAME

References

Structural Repair Manual (SRM) 51-23-10

51-40-21

51-40-44

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

Consumable Material List (CML).

(b) For fastener hole and drill data (Refer to SRM 51-40-44).

(c) For paint coatings (Refer to SRM 51-23-10).

(d) Installation of fasteners (Refer to SRM 51-40-21).

(2) Subtask 282148-910-204-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

Material necessary to do the job

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Storage compound 15-008A As required

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Consumable Material List (CML)

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

(a) For panel location (Refer to AMM 06-41-53, Page Block 001).

(b) Obey the instructions for the wiring installation (Refer to ESPM 20-33-00).

(c) Apply:

Storage compound 15-008A As required

to the screws after assembly.

(3) Subtask 282148-900-202-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

Write in the applicable aircraft records that you have done all the work given in this

Service Bulletin.

**CONF 003

(1) Subtask 282148-910-401-001 - Standard Practices

Manpower Resources

Skills AIRFRAME

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

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References

Structural Repair Manual (SRM) 51-23-10

51-40-21

51-40-44

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

Consumable Material List (CML).

(b) For fastener hole and drill data (Refer to SRM 51-40-44).

(c) For paint coatings (Refer to SRM 51-23-10).

(d) Installation of fasteners (Refer to SRM 51-40-21).

(2) Subtask 282148-910-204-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

Material necessary to do the job

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Storage compound 15-008A As required

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Consumable Material List (CML)

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

(a) For panel location (Refer to AMM 06-41-53, Page Block 001).

(b) Obey the instructions for the wiring installation (Refer to ESPM 20-33-00).

(c) Apply:

Storage compound 15-008A As required

to the screws after assembly.

(3) Subtask 282148-900-202-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

Write in the applicable aircraft records that you have done all the work given in this

Service Bulletin.

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

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**CONF 004

(1) Subtask 282148-910-401-001 - Standard Practices

Manpower Resources

Skills AIRFRAME

References

Structural Repair Manual (SRM) 51-23-10

51-40-21

51-40-44

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

Consumable Material List (CML).

(b) For fastener hole and drill data (Refer to SRM 51-40-44).

(c) For paint coatings (Refer to SRM 51-23-10).

(d) Installation of fasteners (Refer to SRM 51-40-21).

(2) Subtask 282148-910-204-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

Material necessary to do the job

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Storage compound 15-008A As required

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Consumable Material List (CML)

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

(a) For panel location (Refer to AMM 06-41-53, Page Block 001).

(b) Obey the instructions for the wiring installation (Refer to ESPM 20-33-00).

(c) Apply:

Storage compound 15-008A As required

to the screws after assembly.

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

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SERVICE BULLETIN

(3) Subtask 282148-900-202-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

Write in the applicable aircraft records that you have done all the work given in this

Service Bulletin.

**CONF 005

(1) Subtask 282148-910-401-001 - Standard Practices

Manpower Resources

Skills AIRFRAME

References

Structural Repair Manual (SRM) 51-23-10

51-40-21

51-40-44

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

Consumable Material List (CML).

(b) For fastener hole and drill data (Refer to SRM 51-40-44).

(c) For paint coatings (Refer to SRM 51-23-10).

(d) Installation of fasteners (Refer to SRM 51-40-21).

(2) Subtask 282148-910-204-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

Material necessary to do the job

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Storage compound 15-008A As required

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Consumable Material List (CML)

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

(a) For panel location (Refer to AMM 06-41-53, Page Block 001).

(b) Obey the instructions for the wiring installation (Refer to ESPM 20-33-00).

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

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(c) Apply:

Storage compound 15-008A As required

to the screws after assembly.

(3) Subtask 282148-900-202-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

Write in the applicable aircraft records that you have done all the work given in this

Service Bulletin.

**CONF 006

(1) Subtask 282148-910-401-001 - Standard Practices

Manpower Resources

Skills AIRFRAME

References

Structural Repair Manual (SRM) 51-23-10

51-40-21

51-40-44

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

Consumable Material List (CML).

(b) For fastener hole and drill data (Refer to SRM 51-40-44).

(c) For paint coatings (Refer to SRM 51-23-10).

(d) Installation of fasteners (Refer to SRM 51-40-21).

(2) Subtask 282148-910-204-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

Material necessary to do the job

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Storage compound 15-008A As required

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Consumable Material List (CML)

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

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SERVICE BULLETIN

(a) For panel location (Refer to AMM 06-41-53, Page Block 001).

(b) Obey the instructions for the wiring installation (Refer to ESPM 20-33-00).

(c) Apply:

Storage compound 15-008A As required

to the screws after assembly.

(3) Subtask 282148-900-202-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

Write in the applicable aircraft records that you have done all the work given in this

Service Bulletin.

**CONF 007

(1) Subtask 282148-910-401-001 - Standard Practices

Manpower Resources

Skills AIRFRAME

References

Structural Repair Manual (SRM) 51-23-10

51-40-21

51-40-44

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

Consumable Material List (CML).

(b) For fastener hole and drill data (Refer to SRM 51-40-44).

(c) For paint coatings (Refer to SRM 51-23-10).

(d) Installation of fasteners (Refer to SRM 51-40-21).

(2) Subtask 282148-910-204-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

Material necessary to do the job

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Storage compound 15-008A As required

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

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SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Consumable Material List (CML)

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

(a) For panel location (Refer to AMM 06-41-53, Page Block 001).

(b) Obey the instructions for the wiring installation (Refer to ESPM 20-33-00).

(c) Apply:

Storage compound 15-008A As required

to the screws after assembly.

(3) Subtask 282148-900-202-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

Write in the applicable aircraft records that you have done all the work given in this

Service Bulletin.

**CONF 008

(1) Subtask 282148-910-401-001 - Standard Practices

Manpower Resources

Skills AIRFRAME

References

Structural Repair Manual (SRM) 51-23-10

51-40-21

51-40-44

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

Consumable Material List (CML).

(b) For fastener hole and drill data (Refer to SRM 51-40-44).

(c) For paint coatings (Refer to SRM 51-23-10).

(d) Installation of fasteners (Refer to SRM 51-40-21).

(2) Subtask 282148-910-204-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

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Material necessary to do the job

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Storage compound 15-008A As required

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Consumable Material List (CML)

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

(a) For panel location (Refer to AMM 06-41-53, Page Block 001).

(b) Obey the instructions for the wiring installation (Refer to ESPM 20-33-00).

(c) Apply:

Storage compound 15-008A As required

to the screws after assembly.

(3) Subtask 282148-900-202-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

Write in the applicable aircraft records that you have done all the work given in this

Service Bulletin.

**CONF ALL

B. PREPARATION

**CONF 001

(1) Subtask 282148-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

06-41-57, Page Block 001

24-00-00, Page Block 301

25-54-10, Page Block 201

52-10-00, Page Block 001

52-30-00, Page Block 001

53-10-55, Page Block 401

(a) Make sure that the aircraft is grounded (Refer to AMM 24-00-00, Page Block 301).

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(b) Put the access platform(s) in position.

(c) Open the forward cargo compartment door 811 (Refer to AMM 52-30-00, Page

Block 001).

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

(e) In the forward cargo compartment, at FR38.2, remove the partition panel 132SW

(Refer to AMM 06-41-53, Page Block 001 and AMM 53-10-55, Page Block 401).

(f) In the forward cargo compartment, remove the sidewall panel 132QW (Refer to

AMM 06-41-53, Page Block 001 and AMM 25-54-10, Page Block 201).

(g) From the RH wing, remove the access panel 613RR (Refer to AMM 06-41-57,

Page Block 001).

(2) Subtask 282148-862-001-001 - De-energize Electrical Network (Safety Precautions)

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 24-31-11, Page Block 401

(a) Make sure that the external connector(s) is (are) not connected to the aircraft

receptacle(s) EXT PW.

(b) Make sure that there is (are) warning notice(s) on external power receptacle to tell

persons not to connect an external power source.

(c) Make sure that the EMER EXIT LT pushbutton switch on 436VU is on DISARM

position.

(d) In the cockpit, on the overhead panel 424VU release BAT pushbutton switches.

(e) Put a warning notice on panel 424VU to tell persons not to operate the batteries.

(f) Put a warning notice on the refuel/defuel panel 110VU to tell persons not to operate

the NORMAL BATTERY switch.

(g) Put a warning notice in the cockpit to tell persons not to start the APU.

(h) Put a warning notice in the cockpit to tell persons not to start the ENG1,2.

(i) Battery disconnection :

- For job set-up, refer to removal/installation of the batteries (Refer to AMM

24-31-11, Page Block 401),

- Turn the knurled nut a quarter turn,

- Disconnect the connectors,

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 44

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SERVICE BULLETIN

- Put blanking caps on the disconnected electrical connectors.

**CONF 002

(1) Subtask 282148-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

06-41-57, Page Block 001

24-00-00, Page Block 301

25-54-10, Page Block 201

52-10-00, Page Block 001

52-30-00, Page Block 001

53-10-55, Page Block 401

(a) Make sure that the aircraft is grounded (Refer to AMM 24-00-00, Page Block 301).

(b) Put the access platform(s) in position.

(c) Open the forward cargo compartment door 811 (Refer to AMM 52-30-00, Page

Block 001).

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

(e) In the forward cargo compartment, at FR38.2, remove the partition panel 132SW

(Refer to AMM 06-41-53, Page Block 001 and AMM 53-10-55, Page Block 401).

(f) In the forward cargo compartment, remove the sidewall panel 132QW (Refer to

AMM 06-41-53, Page Block 001 and AMM 25-54-10, Page Block 201).

(g) From the RH wing, remove the access panel 613RR (Refer to AMM 06-41-57,

Page Block 001).

(2) Subtask 282148-862-001-001 - De-energize Electrical Network (Safety Precautions)

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 24-31-11, Page Block 401

(a) Make sure that the external connector(s) is (are) not connected to the aircraft

receptacle(s) EXT PW.

(b) Make sure that there is (are) warning notice(s) on external power receptacle to tell

persons not to connect an external power source.

(c) Make sure that the EMER EXIT LT pushbutton switch on 436VU is on DISARM

position.

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 45

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SERVICE BULLETIN

(d) In the cockpit, on the overhead panel 424VU release BAT pushbutton switches.

(e) Put a warning notice on panel 424VU to tell persons not to operate the batteries.

(f) Put a warning notice on the refuel/defuel panel 110VU to tell persons not to operate

the NORMAL BATTERY switch.

(g) Put a warning notice in the cockpit to tell persons not to start the APU.

(h) Put a warning notice in the cockpit to tell persons not to start the ENG1,2.

(i) Battery disconnection :

- For job set-up, refer to removal/installation of the batteries (Refer to AMM

24-31-11, Page Block 401),

- Turn the knurled nut a quarter turn,

- Disconnect the connectors,

- Put blanking caps on the disconnected electrical connectors.

**CONF 003

(1) Subtask 282148-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

06-41-57, Page Block 001

24-00-00, Page Block 301

25-54-10, Page Block 201

52-10-00, Page Block 001

52-30-00, Page Block 001

53-10-55, Page Block 401

(a) Make sure that the aircraft is grounded (Refer to AMM 24-00-00, Page Block 301).

(b) Put the access platform(s) in position.

(c) Open the forward cargo compartment door 811 (Refer to AMM 52-30-00, Page

Block 001).

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

(e) In the forward cargo compartment, at FR38.2, remove the partition panel 132SW

(Refer to AMM 06-41-53, Page Block 001 and AMM 53-10-55, Page Block 401).

(f) In the forward cargo compartment, remove the sidewall panel 132QW (Refer to

AMM 06-41-53, Page Block 001 and AMM 25-54-10, Page Block 201).

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 46

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SERVICE BULLETIN

(g) From the RH wing, remove the access panel 613RR (Refer to AMM 06-41-57,

Page Block 001).

(2) Subtask 282148-862-001-001 - De-energize Electrical Network (Safety Precautions)

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 24-31-11, Page Block 401

(a) Make sure that the external connector(s) is (are) not connected to the aircraft

receptacle(s) EXT PW.

(b) Make sure that there is (are) warning notice(s) on external power receptacle to tell

persons not to connect an external power source.

(c) Make sure that the EMER EXIT LT pushbutton switch on 436VU is on DISARM

position.

(d) In the cockpit, on the overhead panel 424VU release BAT pushbutton switches.

(e) Put a warning notice on panel 424VU to tell persons not to operate the batteries.

(f) Put a warning notice on the refuel/defuel panel 110VU to tell persons not to operate

the NORMAL BATTERY switch.

(g) Put a warning notice in the cockpit to tell persons not to start the APU.

(h) Put a warning notice in the cockpit to tell persons not to start the ENG1,2.

(i) Battery disconnection :

- For job set-up, refer to removal/installation of the batteries (Refer to AMM

24-31-11, Page Block 401),

- Turn the knurled nut a quarter turn,

- Disconnect the connectors,

- Put blanking caps on the disconnected electrical connectors.

**CONF 004

(1) Subtask 282148-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 47

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SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

06-41-57, Page Block 001

24-00-00, Page Block 301

25-54-10, Page Block 201

52-10-00, Page Block 001

52-30-00, Page Block 001

53-10-55, Page Block 401

(a) Make sure that the aircraft is grounded (Refer to AMM 24-00-00, Page Block 301).

(b) Put the access platform(s) in position.

(c) Open the forward cargo compartment door 811 (Refer to AMM 52-30-00, Page

Block 001).

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

(e) In the forward cargo compartment, at FR38.2, remove the partition panel 132SW

(Refer to AMM 06-41-53, Page Block 001 and AMM 53-10-55, Page Block 401).

(f) In the forward cargo compartment, remove the sidewall panel 132QW (Refer to

AMM 06-41-53, Page Block 001 and AMM 25-54-10, Page Block 201).

(g) From the RH wing, remove the access panel 613RR (Refer to AMM 06-41-57,

Page Block 001).

(2) Subtask 282148-862-001-001 - De-energize Electrical Network (Safety Precautions)

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 24-31-11, Page Block 401

(a) Make sure that the external connector(s) is (are) not connected to the aircraft

receptacle(s) EXT PW.

(b) Make sure that there is (are) warning notice(s) on external power receptacle to tell

persons not to connect an external power source.

(c) Make sure that the EMER EXIT LT pushbutton switch on 436VU is on DISARM

position.

(d) In the cockpit, on the overhead panel 424VU release BAT pushbutton switches.

(e) Put a warning notice on panel 424VU to tell persons not to operate the batteries.

(f) Put a warning notice on the refuel/defuel panel 110VU to tell persons not to operate

the NORMAL BATTERY switch.

(g) Put a warning notice in the cockpit to tell persons not to start the APU.

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 48

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SERVICE BULLETIN

(h) Put a warning notice in the cockpit to tell persons not to start the ENG1,2.

(i) Battery disconnection :

- For job set-up, refer to removal/installation of the batteries (Refer to AMM

24-31-11, Page Block 401),

- Turn the knurled nut a quarter turn,

- Disconnect the connectors,

- Put blanking caps on the disconnected electrical connectors.

**CONF 005

(1) Subtask 282148-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

06-41-57, Page Block 001

24-00-00, Page Block 301

25-54-10, Page Block 201

52-10-00, Page Block 001

52-30-00, Page Block 001

53-10-55, Page Block 401

(a) Make sure that the aircraft is grounded (Refer to AMM 24-00-00, Page Block 301).

(b) Put the access platform(s) in position.

(c) Open the forward cargo compartment door 811 (Refer to AMM 52-30-00, Page

Block 001).

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

(e) In the forward cargo compartment, at FR38.2, remove the partition panel 132SW

(Refer to AMM 06-41-53, Page Block 001 and AMM 53-10-55, Page Block 401).

(f) In the forward cargo compartment, remove the sidewall panel 132QW (Refer to

AMM 06-41-53, Page Block 001 and AMM 25-54-10, Page Block 201).

(g) From the RH wing, remove the access panel 613RR (Refer to AMM 06-41-57,

Page Block 001).

(2) Subtask 282148-862-001-001 - De-energize Electrical Network (Safety Precautions)

Manpower Resources

Skills NON SPECIFIC

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 49

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SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) 24-31-11, Page Block 401

(a) Make sure that the external connector(s) is (are) not connected to the aircraft

receptacle(s) EXT PW.

(b) Make sure that there is (are) warning notice(s) on external power receptacle to tell

persons not to connect an external power source.

(c) Make sure that the EMER EXIT LT pushbutton switch on 436VU is on DISARM

position.

(d) In the cockpit, on the overhead panel 424VU release BAT pushbutton switches.

(e) Put a warning notice on panel 424VU to tell persons not to operate the batteries.

(f) Put a warning notice on the refuel/defuel panel 110VU to tell persons not to operate

the NORMAL BATTERY switch.

(g) Put a warning notice in the cockpit to tell persons not to start the APU.

(h) Put a warning notice in the cockpit to tell persons not to start the ENG1,2.

(i) Battery disconnection :

- For job set-up, refer to removal/installation of the batteries (Refer to AMM

24-31-11, Page Block 401),

- Turn the knurled nut a quarter turn,

- Disconnect the connectors,

- Put blanking caps on the disconnected electrical connectors.

**CONF 006

(1) Subtask 282148-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

06-41-57, Page Block 001

24-00-00, Page Block 301

25-54-10, Page Block 201

52-10-00, Page Block 001

52-30-00, Page Block 001

53-10-55, Page Block 401

(a) Make sure that the aircraft is grounded (Refer to AMM 24-00-00, Page Block 301).

(b) Put the access platform(s) in position.

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 50

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SERVICE BULLETIN

(c) Open the forward cargo compartment door 811 (Refer to AMM 52-30-00, Page

Block 001).

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

(e) In the forward cargo compartment, at FR38.2, remove the partition panel 132SW

(Refer to AMM 06-41-53, Page Block 001 and AMM 53-10-55, Page Block 401).

(f) In the forward cargo compartment, remove the sidewall panel 132QW (Refer to

AMM 06-41-53, Page Block 001 and AMM 25-54-10, Page Block 201).

(g) From the RH wing, remove the access panel 613RR (Refer to AMM 06-41-57,

Page Block 001).

(2) Subtask 282148-862-001-001 - De-energize Electrical Network (Safety Precautions)

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 24-31-11, Page Block 401

(a) Make sure that the external connector(s) is (are) not connected to the aircraft

receptacle(s) EXT PW.

(b) Make sure that there is (are) warning notice(s) on external power receptacle to tell

persons not to connect an external power source.

(c) Make sure that the EMER EXIT LT pushbutton switch on 436VU is on DISARM

position.

(d) In the cockpit, on the overhead panel 424VU release BAT pushbutton switches.

(e) Put a warning notice on panel 424VU to tell persons not to operate the batteries.

(f) Put a warning notice on the refuel/defuel panel 110VU to tell persons not to operate

the NORMAL BATTERY switch.

(g) Put a warning notice in the cockpit to tell persons not to start the APU.

(h) Put a warning notice in the cockpit to tell persons not to start the ENG1,2.

(i) Battery disconnection :

- For job set-up, refer to removal/installation of the batteries (Refer to AMM

24-31-11, Page Block 401),

- Turn the knurled nut a quarter turn,

- Disconnect the connectors,

- Put blanking caps on the disconnected electrical connectors.

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 51

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**CONF 007

(1) Subtask 282148-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

06-41-57, Page Block 001

24-00-00, Page Block 301

25-54-10, Page Block 201

52-10-00, Page Block 001

52-30-00, Page Block 001

53-10-55, Page Block 401

(a) Make sure that the aircraft is grounded (Refer to AMM 24-00-00, Page Block 301).

(b) Put the access platform(s) in position.

(c) Open the forward cargo compartment door 811 (Refer to AMM 52-30-00, Page

Block 001).

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

(e) In the forward cargo compartment, at FR38.2, remove the partition panel 132SW

(Refer to AMM 06-41-53, Page Block 001 and AMM 53-10-55, Page Block 401).

(f) In the forward cargo compartment, remove the sidewall panel 132QW (Refer to

AMM 06-41-53, Page Block 001 and AMM 25-54-10, Page Block 201).

(g) From the RH wing, remove the access panel 613RR (Refer to AMM 06-41-57,

Page Block 001).

(2) Subtask 282148-862-001-001 - De-energize Electrical Network (Safety Precautions)

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 24-31-11, Page Block 401

(a) Make sure that the external connector(s) is (are) not connected to the aircraft

receptacle(s) EXT PW.

(b) Make sure that there is (are) warning notice(s) on external power receptacle to tell

persons not to connect an external power source.

(c) Make sure that the EMER EXIT LT pushbutton switch on 436VU is on DISARM

position.

(d) In the cockpit, on the overhead panel 424VU release BAT pushbutton switches.

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 52

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SERVICE BULLETIN

(e) Put a warning notice on panel 424VU to tell persons not to operate the batteries.

(f) Put a warning notice on the refuel/defuel panel 110VU to tell persons not to operate

the NORMAL BATTERY switch.

(g) Put a warning notice in the cockpit to tell persons not to start the APU.

(h) Put a warning notice in the cockpit to tell persons not to start the ENG1,2.

(i) Battery disconnection :

- For job set-up, refer to removal/installation of the batteries (Refer to AMM

24-31-11, Page Block 401),

- Turn the knurled nut a quarter turn,

- Disconnect the connectors,

- Put blanking caps on the disconnected electrical connectors.

**CONF 008

(1) Subtask 282148-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

06-41-57, Page Block 001

24-00-00, Page Block 301

25-54-10, Page Block 201

52-10-00, Page Block 001

52-30-00, Page Block 001

53-10-55, Page Block 401

(a) Make sure that the aircraft is grounded (Refer to AMM 24-00-00, Page Block 301).

(b) Put the access platform(s) in position.

(c) Open the forward cargo compartment door 811 (Refer to AMM 52-30-00, Page

Block 001).

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

(e) In the forward cargo compartment, at FR38.2, remove the partition panel 132SW

(Refer to AMM 06-41-53, Page Block 001 and AMM 53-10-55, Page Block 401).

(f) In the forward cargo compartment, remove the sidewall panel 132QW (Refer to

AMM 06-41-53, Page Block 001 and AMM 25-54-10, Page Block 201).

(g) From the RH wing, remove the access panel 613RR (Refer to AMM 06-41-57,

Page Block 001).

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 53

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SERVICE BULLETIN

(2) Subtask 282148-862-001-001 - De-energize Electrical Network (Safety Precautions)

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 24-31-11, Page Block 401

(a) Make sure that the external connector(s) is (are) not connected to the aircraft

receptacle(s) EXT PW.

(b) Make sure that there is (are) warning notice(s) on external power receptacle to tell

persons not to connect an external power source.

(c) Make sure that the EMER EXIT LT pushbutton switch on 436VU is on DISARM

position.

(d) In the cockpit, on the overhead panel 424VU release BAT pushbutton switches.

(e) Put a warning notice on panel 424VU to tell persons not to operate the batteries.

(f) Put a warning notice on the refuel/defuel panel 110VU to tell persons not to operate

the NORMAL BATTERY switch.

(g) Put a warning notice in the cockpit to tell persons not to start the APU.

(h) Put a warning notice in the cockpit to tell persons not to start the ENG1,2.

(i) Battery disconnection :

- For job set-up, refer to removal/installation of the batteries (Refer to AMM

24-31-11, Page Block 401),

- Turn the knurled nut a quarter turn,

- Disconnect the connectors,

- Put blanking caps on the disconnected electrical connectors.

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 54

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SERVICE BULLETIN

**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 282148-831-405-001 - Install a New Bracket on the Sub Spar Behind the

Front Spar Between RIB 8 and RIB 9 on the RH Wing

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills AIRFRAME

Material necessary to do the job

Kit 282148B01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 A5725068600000 1 Bracket

2 ASNA0078A502 2 Rivet

Consumable CMLB01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Corrosion Inhibiting Low

Adhesion Sealant

09-018 As required

Solvent General Purpose 11-026 As required

Lint-Free Cotton Cloth 19-003 As required

References

Fig. A-UBAAA

Location of Bracket on the Sub Spar

Behind the Front Spar Between RIB 8

and RIB 9 (RH Wing)

Sheet 01

Refer to Fig. A-UBAAA Sheet 01

(a) Remove from the sub spar behind the front spar between RIB 8 and RIB 9 on the

RH wing, the items that follow:

2 Rivet NSA54213510DCA Item (2) Discard

1 Bracket A5724630400000 Item (1) Discard

(b) Clean the mating surfaces use

Lint-Free Cotton

Cloth

19-003 As required

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 55

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SERVICE BULLETIN

made moist with

Solvent General

Purpose

11-026 As required

(c) Put the

1 Bracket A5725068600000 Item 1

in position on the sub spar behind the front spar between RIB 8 and RIB 9 on the

RH wing (Refer to Fig. A-UBAAA Sheet 01).

(d) Copy drill the two holes from the sub spar through the Bracket, Item 1 to a

dimension of between 4.060 and 4.160 mm (0.160 and 0.164 in.).

(e) Deburr the holes that have been worked.

(f) Use

Corrosion Inhibiting

Low Adhesion

Sealant

09-018 As required

and wet install the

1 Bracket A5725068600000 Item 1

with the

2 Rivet, Blind ASNA0078A502 Item 2

on the sub spar behind the front spar between RIB 8 and RIB 9 on the RH wing.

(2) Subtask 282148-831-004-001 - Install cable sleeves in the RH Electronics Rack

90VU.

Manpower Resources

Manhours 6.00

Minimum number of person 1

Subtask elapsed time 6.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 282148A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 ABS0596S004 2000 (mm) SLEEVE

NSA935401-04 50 TIE

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 56

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References

Fig. A-FCAAA

Installation of Cable Sleeves in the RH

Electronics Rack 90VU.

Sheet 01

Fig. A-FWAAA

Installation of Cable Sleeves in the RH

Electronics Rack 90VU.

Sheet 01

NOTE: The sleeves ABS0596S004 and ABS0596S006 are supplied in pieces of

1000 mm (39.370 inches), cut or assemble these pieces to get the

correct length.

NOTE: The lengths of the sleeves given in this Service Bulletin are approximate

lengths. Adapt the lengths of the sleeves in relation to the aircraft

configuration.

NOTE: Before you install a sleeve, cut and discard the cable ties around the

cable bundle to install the sleeve correctly around the cable bundle.

(a) On the Shelf 92VU, only around the wires identified in figure Fig. A-FWAAA Sheet

01, from the equipment 15QT-B to the connector 2354VC, install:

1600 (mm) Sleeve ABS0596S004 Item 1

(b) Around the cable bundle of the connector 2354VC-A, install:

400 (mm) Sleeve ABS0596S004 Item 1

(c) Attach the sleeves with:

50 Tie-Cable NSA935401-04

(3) Subtask 282148-831-005-001 - Install cable sleeves between FR38.2 and FR39, in

the forward cargo compartment.

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 282148A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

2 ABS0596S006 1000 (mm) SLEEVE

NSA935401-05 50 TIE

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 57

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SERVICE BULLETIN

References

Fig. A-FCBAA

Installation of Cable Sleeves in the

Forward Cargo Compartment.

Sheet 01

NOTE: The sleeves ABS0596S004 and ABS0596S006 are supplied in pieces of

1000 mm (39.370 inches), cut or assemble these pieces to get the

correct length.

NOTE: The lengths of the sleeves given in this Service Bulletin are approximate

lengths. Adapt the lengths of the sleeves in relation to the aircraft

configuration.

NOTE: Before you install a sleeve, cut and discard the cable ties around the

cable bundle to install the sleeve correctly around the cable bundle.

(a) Around the cable bundle of the pressure seal 20VP, install:

1000 (mm) Sleeve ABS0596S006 Item 2

(b) Attach the sleeves with:

50 Tie-Cable NSA935401-05

(4) Subtask 282148-831-006-001 - Install cable sleeves in the RH forward wing root

and krueger flap.

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 282148A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

2 ABS0596S006 1000 (mm) SLEEVE

NSA935401-05 50 TIE

References

Fig. A-FCCAA

Installation of Cable Sleeves in the RH

forward wing root and krueger flap.

Sheet 01

(a) Around the cable bundle of the pressure seal 20VP, install:

1000 (mm) Sleeve ABS0596S006 Item 2

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

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SERVICE BULLETIN

(b) Attach the sleeves with:

50 Tie-Cable NSA935401-05

(5) Subtask 282148-831-208-001 - Install the cable sleeves in the RH-wing forward of

the front spar between rib 2 and rib 3 in zone 612.

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills ELECTRICAL

Material necessary to do the job

Kit 282148D01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 ABS0596S004 1 SLEEVE

11 MS21919WCH13 2 CLAMP

149 NSA935401-03 1 TIE

150 NSA935401-04 1 TIE

References

Fig. A-GBEAA

Improvement of the 2S-Route in the RHWing in Zone 612 (Kit D01)

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

Sheet 07

Sheet 08

NOTE (1): The sleeve ABS0596S004 is supplied in pieces of 1000 mm. Cut or

assemble these pieces to get the correct length.

NOTE (2): The lengths of the sleeves given in this Service Bulletin are approximate

lengths. Adapt the lengths of the sleeves in relation to the aircraft

configuration.

NOTE (3): Before you install a sleeve, cut and discard the cable ties around the

cable bundle to install the sleeve correctly around the cable bundle.

NOTE (4): Adapt the number of cable ties to the required quantity.

Install the cable sleeves in the RH-wing forward of the front spar between rib 2 and rib 3

in zone 612.

Refer to Fig. A-GBEAA Sheet 01, Fig. A-GBEAA Sheet 02, Fig. A-GBEAA Sheet 03, Fig.

A-GBEAA Sheet 04, Fig. A-GBEAA Sheet 05, Fig. A-GBEAA Sheet 06, Fig. A-GBEAA

Sheet 07 and Fig. A-GBEAA Sheet 08

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 59

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SERVICE BULLETIN

(a) Remove these items from the bracket of the rib 2 and cable bundle 2S/624VB, as

shown in Details A and B:

1 Clamp MS21919WCH4 Item (22) Retain

1 Clamp MS21919WCH3 Item (23) Retain

1 Spacer NSA5527-03-02D Item (31) Retain

1 Washer NAS1149D0332K Item (40) Retain

1 Screw NAS1096-3-21 Item (50) Retain

1 Clamp MS21919WCH10 Item (100) Retain

1 Clamp Item (100) Discard

(b) Remove these items from the riblet and cable bundle 2S/624VB, as shown in

Details A and D:

1 Clamp MS21919WCH4 Item (22) Retain

3 Spacer NSA5527-03-02D Item (31) Retain

1 Washer NAS1149D0332K Item (40) Retain

1 Screw NAS1096-3-38 Item (54) Retain

1 Clamp Item (100) Discard

(c) Install this cable sleeve around these identified wires from the cable bundle

2S/624VB, as shown in Details A, C, E and F:

Wire number 2842-5052

Wire number 2842-5053

Wire number 2842-5054

Wire number 2842-5055

Wire number 2842-5056

Wire number 2842-5070

1 Sleeve ABS0596S004 Item 1

and attach the cable sleeve with:

1 Tie NSA935401-03 Item 149

1 Tie-Cable NSA935401-04 Item 150

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 60

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@A310

SERVICE BULLETIN

as necessary.

(d) Install these items to the bracket of the rib 2, cable bundle 2S/624VB and cable

sleeve, Item 1, as shown in Details A and C:

1 Clamp MS21919WCH4 Item (22) Retained at

removal

1 Clamp MS21919WCH3 Item (23) Retained at

removal

1 Spacer NSA5527-03-02D Item (31) Retained at

removal

1 Washer NAS1149D0332K Item (40) Retained at

removal

1 Screw NAS1096-3-21 Item (50) Retained at

removal

1 Clamp MS21919WCH10 Item (100) Retained at

removal

1 Clamp MS21919WCH13 Item 11

(e) Install these items to the riblet, cable bundle 2S/624VB and cable sleeve, Item 1,

as shown in Details A and E:

1 Clamp MS21919WCH4 Item (22) Retained at

removal

3 Spacer NSA5527-03-02D Item (31) Retained at

removal

1 Washer NAS1149D0332K Item (40) Retained at

removal

1 Screw NAS1096-3-38 Item (54) Retained at

removal

1 Clamp MS21919WCH13 Item 11

(6) Subtask 282148-831-209-001 - Install the cable sleeves in the RH-wing forward of

the front spar between rib 7 and rib 8 in zone 612.

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills ELECTRICAL

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 61

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@A310

SERVICE BULLETIN

Material necessary to do the job

Kit 282148D01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 ABS0596S004 2 SLEEVE

12 MS21919WCH14 2 CLAMP

149 NSA935401-03 2 TIE

150 NSA935401-04 2 TIE

References

Fig. A-GBEAA

Improvement of the 2S-Route in the RHWing in Zone 612 (Kit D01)

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

Sheet 07

Sheet 08

NOTE (1): The sleeves ABS0596S004 is supplied in pieces of 1000 mm. Cut or

assemble these pieces to get the correct length.

NOTE (2): The lengths of the sleeves given in this Service Bulletin are approximate

lengths. Adapt the lengths of the sleeves in relation to the aircraft

configuration.

NOTE (3): Before you install a sleeve, cut and discard the cable ties around the

cable bundle to install the sleeve correctly around the cable bundle.

NOTE (4): Adapt the number of cable ties to the required quantity.

Refer to Fig. A-GBEAA Sheet 01, Fig. A-GBEAA Sheet 02, Fig. A-GBEAA Sheet 03, Fig.

A-GBEAA Sheet 04, Fig. A-GBEAA Sheet 05, Fig. A-GBEAA Sheet 06, Fig. A-GBEAA

Sheet 07 and Fig. A-GBEAA Sheet 08

(a) Remove these items from the two brackets of the riblets and cable bundle

2S/624VB, as shown in Details A, H and K:

2 Clamp MS21919WCH4 Item (22) Retain

2 Washer NAS1149D0332K Item (40) Retain

2 Screw NAS1096-3-8 Item (55) Retain

2 Clamp Item (100) Discard

(b) Install this cable sleeve around these identified wires from the cable bundle

2S/624VB, as shown in Details A, J, K, L, M and N:

Wire number 2842-5052

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 62

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SERVICE BULLETIN

Wire number 2842-5053

Wire number 2842-5054

Wire number 2842-5055

Wire number 2842-5056

1 Sleeve ABS0596S004 Item 1

and attach the cable sleeves with:

1 Tie NSA935401-03 Item 149

1 Tie-Cable NSA935401-04 Item 150

(c) Install this cable sleeve around this identified wire from the cable bundle 2S/624VB,

as shown in Details A, J, K, L, M and N:

Wire number 2842-5070

1 Sleeve ABS0596S004 Item 1

and attach the cable sleeves with:

1 Tie NSA935401-03 Item 149

1 Tie-Cable NSA935401-04 Item 150

(d) Install these items to the two brackets of the riblets, cable bundle 2S/624VB and

cable sleeves, Item 1, as shown in Detail A, J and L:

2 Clamp MS21919WCH4 Item (22) Retained at

removal

2 Washer NAS1149D0332K Item (40) Retained at

removal

2 Screw NAS1096-3-8 Item (55) Retained at

removal

2 Clamp MS21919WCH14 Item 12

(7) Subtask 282148-831-210-001 - Install the cable sleeves in the RH-wing forward of

the front spar between rib 8 and rib 9 (pylon area) in zone 612.

Manpower Resources

Manhours 4.00

Minimum number of person 1

Subtask elapsed time 4.00

Skills ELECTRICAL

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 63

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@A310

SERVICE BULLETIN

Material necessary to do the job

Kit 282148D02R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 ABS0596S004 2 SLEEVE

30 NSA5527-03-01D 2 SPACER

109 NSA935805-09 3 (ME) CONDUIT

117 NSA935807C09 13 CLAMP

125 B9299071900200 1 EQUIPMNT

126 NSA938184PV1601 15 PIN

149 NSA935401-03 20 TIE

150 NSA935401-04 20 TIE

References

Fig. A-GBGAA

Improvement of the 2S-Route in the RHWing Pylon Area (Kit D02)

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

Sheet 07

Sheet 08

Fig. A-GHAAA

Hook-up Chart

Sheet 01

Fig. A-GHBAA

Hook-up Chart

Sheet 01

NOTE (1): The sleeves ABS0596S004 is supplied in pieces of 1000 mm. Cut or

assemble these pieces to get the correct length.

NOTE (2): The lengths of the sleeves given in this Service Bulletin are approximate

lengths. Adapt the lengths of the sleeves in relation to the aircraft

configuration.

NOTE (3): Before you install a sleeve, cut and discard the cable ties around the

cable bundle to install the sleeve correctly around the cable bundle.

NOTE (4): Adapt the number of cable ties to the required quantity.

Refer to Fig. A-GBGAA Sheet 01, Fig. A-GBGAA Sheet 02, Fig. A-GBGAA Sheet 03,

Fig. A-GBGAA Sheet 04, Fig. A-GBGAA Sheet 05, Fig. A-GBGAA Sheet 06, Fig. AGBGAA Sheet 07 and Fig. A-GBGAA Sheet 08

Refer to Fig. A-GHAAA Sheet 01 and Fig. A-GHBAA Sheet 01

(a) Disconnect these wires of route 2S from the receptacles 40VC and 5006VC in

accordance with the Hook-up Chart 1, Lines 1 thru 14, END 1, Fig. A-GHAAA

Sheet 01 and the Hook-up Chart 2, Lines 2 thru 8, END 1, Fig. A-GHBAA Sheet

01.

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 64

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SERVICE BULLETIN

(b) Remove, refer to Fig. A-GBGAA Sheet 03, Detail D, BEFORE:

1 Spacer NSA5527-03-02D Item (31) Discard

1 Clamp NSA935807C10 Item (110) Discard

1 Clamp NSA935807C16 Item (111) Retain

1 Washer NSA935808-01 Item (112) Retain

1 Screw NAS1096-3-23 Item (113) Retain

1 Spacer NSA5527-03-05D Item (114) Discard

1 Washer NSA1149D0332K Item (115) Retain

1 Nut NAS1291C3M Item (116) Retain

1 Clamp NSA935807C09 Item (117) Retain

(c) Remove, refer to Fig. A-GBGAA Sheet 04, Detail F, BEFORE:

2 Spacer NSA5527-03-01D Item (30) Retain

1 Spacer NSA5527-03-02D Item (31) Retain

1 Clamp NSA935807C10 Item (110) Retain

1 Clamp NSA935807C10 Item (110) Discard

1 Clamp NSA935807C16 Item (111) Retain

1 Washer NSA935808-01 Item (112) Retain

1 Clamp NSA935807C09 Item (117) Retain

1 Screw NAS1096-3-33 Item (118) Retain

(d) Remove, refer to Fig. A-GBGAA Sheet 05, Detail H, BEFORE:

2 Spacer NSA5527-03-01D Item (30) Retain

2 Spacer NSA5527-03-02D Item (31) Retain

2 Clamp NSA935807C10 Item (110) Discard

2 Clamp NSA935807C16 Item (111) Retain

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 65

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SERVICE BULLETIN

2 Spacer NSA5527-03-05D Item (114) Retain

2 Washer NSA1149D0332K Item (115) Retain

2 Clamp NSA935807C09 Item (117) Retain

2 Screw NAS1096-3-33 Item (118) Retain

(e) Remove, refer to Fig. A-GBGAA Sheet 06, Detail K, BEFORE:

1 Spacer NSA5527-03-01D Item (30) Retain

1 Spacer NSA5527-03-02D Item (31) Retain

1 Clamp NSA935807C10 Item (110) Discard

1 Clamp NSA935807C16 Item (111) Retain

1 Spacer NSA5527-03-05D Item (114) Retain

1 Washer NSA1149D0332K Item (115) Retain

1 Clamp NSA935807C09 Item (117) Retain

1 Screw NAS1096-3-33 Item (118) Retain

(f) Remove, refer to Fig. A-GBGAA Sheet 07, Detail M, BEFORE:

1 Spacer NSA5527-03-01D Item (30) Retain

1 Spacer NSA5527-03-02D Item (31) Retain

1 Clamp NSA935807C10 Item (110) Discard

1 Clamp NSA935807C16 Item (111) Retain

1 Washer NSA935808-01 Item (112) Retain

1 Spacer NSA5527-03-05D Item (114) Retain

1 Clamp NSA935807C09 Item (117) Retain

1 Screw NAS1096-3-33 Item (118) Retain

(g) Remove, refer to Fig. A-GBGAA Sheet 08, Detail P, BEFORE:

1 Spacer NSA5527-03-02D Item (31) Retain

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 66

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SERVICE BULLETIN

1 Clamp NSA935807C10 Item (110) Discard

1 Clamp NSA935807C16 Item (111) Retain

1 Washer NSA935808-01 Item (112) Retain

1 Spacer NSA5527-03-05D Item (114) Retain

1 Clamp NSA935807C09 Item (117) Retain

1 Screw NAS1096-3-25 Item (119) Retain

(h) Remove the identification sleeves from the cable harnesses near the receptacles

40VC and 5006VC as shown Fig. A-GBGAA Sheet 01, Detail A

As

required

placard Item (125) Discard

(i) Remove the protection sleeve from the cable harness as shown Fig. A-GBGAA

Sheet 01, Fig. A-GBGAA Sheet 02, Fig. A-GBGAA Sheet 03, Fig. A-GBGAA Sheet

04, Fig. A-GBGAA Sheet 05, Fig. A-GBGAA Sheet 06, Fig. A-GBGAA Sheet 07

and Fig. A-GBGAA Sheet 08, Details D, F, H, K, M and P:

1 Sleeve NSA935805-10 Item (109) Discard

(j) Cut the conduit to the required length and install as shown Fig. A-GBGAA Sheet

01, Fig. A-GBGAA Sheet 02, Fig. A-GBGAA Sheet 03, Fig. A-GBGAA Sheet 04,

Fig. A-GBGAA Sheet 05, Fig. A-GBGAA Sheet 06, Fig. A-GBGAA Sheet 07 and

Fig. A-GBGAA Sheet 08, Details E, G, J, L, N and Q:

3 (ME) Conduit NSA935805-09 Item 109

1 One part 1500.0 mm (59.06 in.) to the electrical wires for 10QT-A and 10QT-B

of route 2S/636VB, refer to the Hook-up Chart 2, Fig. A-GHBAA Sheet 01

2 Three parts, one 520 mm (20.47 in.) and two 240.0 mm (9.45 in.) to the

remaining electrical wires of route 2S/636VB, refer to Fig. A-GHAAA Sheet 01

(k) Connect the electrical wires of route 2S to the receptacles 40VC and 5006VC in

accordance with the Hook-up Chart 1, Lines 1 thru 14, END 1, Fig. A-GHAAA

Sheet 01 and the Hook-up Chart 2, lines 2 thru 8, END 1, Fig. A-GHBAA Sheet 01.

Use the contact pins if required:

15 Pin NSA938184PV1601 Item 126

(l) Install, refer to Fig. A-GBGAA Sheet 08, Detail Q, AFTER:

1 Spacer NSA5527-03-02D Item (31) Retained at

removal

1 Clamp NSA935807C16 Item (111) Retained at

removal

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 67

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SERVICE BULLETIN

1 Washer NSA935808-01 Item (112) Retained at

removal

1 Spacer NSA5527-03-05D Item (114) Retained at

removal

2 Clamp NSA935807C09 Item (117) Retained at

removal

1 Screw NAS1096-3-25 Item (119) Retained at

removal

1 Clamp NSA935807C09 Item 117

(m) Install, refer to Fig. A-GBGAA Sheet 07, Detail N, AFTER:

1 Spacer NSA5527-03-01D Item (30) Retained at

removal

1 Spacer NSA5527-03-02D Item (31) Retained at

removal

1 Clamp NSA935807C16 Item (111) Retained at

removal

1 Washer NSA935808-01 Item (112) Retained at

removal

1 Spacer NSA5527-03-05D Item (114) Retained at

removal

1 Clamp NSA935807C09 Item (117) Retained at

removal

1 Screw NAS1096-3-33 Item (118) Retained at

removal

2 Clamp NSA935807C09 Item 117

(n) Install, refer to Fig. A-GBGAA Sheet 06, Detail L, AFTER:

1 Spacer NSA5527-03-01D Item (30) Retained at

removal

1 Spacer NSA5527-03-02D Item (31) Retained at

removal

1 Clamp NSA935807C16 Item (111) Retained at

removal

1 Spacer NSA5527-03-05D Item (114) Retained at

removal

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 68

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@A310

SERVICE BULLETIN

1 Washer NSA1149D0332K Item (115) Retained at

removal

1 Clamp NSA935807C09 Item (117) Retained at

removal

1 Screw NAS1096-3-33 Item (118) Retained at

removal

2 Clamp NSA935807C09 Item 117

(o) Install, refer to Fig. A-GBGAA Sheet 05, Detail J, AFTER:

2 Spacer NSA5527-03-01D Item (30) Retained at

removal

2 Spacer NSA5527-03-02D Item (31) Retained at

removal

2 Clamp NSA935807C16 Item (111) Retained at

removal

2 Spacer NSA5527-03-05D Item (114) Retained at

removal

2 Washer NSA1149D0332K Item (115) Retained at

removal

2 Clamp NSA935807C09 Item (117) Retained at

removal

2 Screw NAS1096-3-33 Item (118) Retained at

removal

4 Clamp NSA935807C09 Item 117

(p) Install, refer to Fig. A-GBGAA Sheet 04, Detail G, AFTER:

2 Spacer NSA5527-03-01D Item (30) Retained at

removal

1 Spacer NSA5527-03-02D Item (31) Retained at

removal

1 Clamp NSA935807C10 Item (110) Retained at

removal

1 Clamp NSA935807C16 Item (111) Retained at

removal

1 Washer NSA935808-01 Item (112) Retained at

removal

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 69

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SERVICE BULLETIN

1 Clamp NSA935807C09 Item (117) Retained at

removal

1 Screw NAS1096-3-33 Item (118) Retained at

removal

2 Clamp NSA935807C09 Item 117

(q) Install, refer to Fig. A-GBGAA Sheet 03, Detail E, AFTER:

2 Spacer NSA5527-03-01D Item 30

1 Clamp NSA935807C16 Item (111) Retained at

removal

1 Washer NSA935808-01 Item (112) Retained at

removal

1 Screw NAS1096-3-23 Item (113) Retained at

removal

1 Washer NSA1149D0332K Item (115) Retained at

removal

1 Nut NAS1291C3M Item (116) Retained at

removal

1 Clamp NSA935807C09 Item (117) Retained at

removal

2 Clamp NSA935807C09 Item 117

(r) Protect the electrical wires for 10QT-A and 10QT-B of route 2S/636VB, refer to the

Hook-up Chart 2, Fig. A-GHBAA Sheet 01 with:

2 Sleeve ABS0596S004 Item 1

and

20 Tie NSA935401-03 Item 149

20 Tie-Cable NSA935401-04 Item 150

(s) Install the identification placards:

1 Placard set B9299071900200 Item 125

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 70

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@A310

SERVICE BULLETIN

(8) Subtask 282148-831-211-001 - Install the cable sleeves in the RH-wing forward of

the front spar between rib 9 and rib 12 in zone 623.

Manpower Resources

Manhours 4.00

Minimum number of person 1

Subtask elapsed time 4.00

Skills ELECTRICAL

Material necessary to do the job

Kit 282148D01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 ABS0596S004 3 SLEEVE

10 MS21919WCH9 8 CLAMP

14 NAS1096-3-19 2 SCREW

15 NSA5527-03-03 3 SPACER

16 NSA8420-2 0.5 (ME) CORD

149 NSA935401-03 1 TIE

150 NSA935401-04 1 TIE

Kit 282148D02R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

31 NSA5527-03-02D 2 SPACER

121 NAS1096-3-40 1 SCREW

References

Fig. A-GBFAA

Improvement of the 2S-Route in the RHWing in Zone 623 (Kit D01)

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

Sheet 07

Sheet 08

Sheet 09

Sheet 10

NOTE (1): The sleeves ABS0596S004 is supplied in pieces of 1000 mm. Cut or

assemble these pieces to get the correct length.

NOTE (2): The lengths of the sleeves given in this Service Bulletin are approximate

lengths. Adapt the lengths of the sleeves in relation to the aircraft

configuration.

NOTE (3): Before you install a sleeve, cut and discard the cable ties around the

cable bundle to install the sleeve correctly around the cable bundle.

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 71

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SERVICE BULLETIN

NOTE (4): Adapt the number of cable ties to the required quantity.

Refer to Fig. A-GBFAA Sheet 01, Fig. A-GBFAA Sheet 02, Fig. A-GBFAA Sheet 03, Fig.

A-GBFAA Sheet 04, Fig. A-GBFAA Sheet 05, Fig. A-GBFAA Sheet 06, Fig. A-GBFAA

Sheet 07, Fig. A-GBFAA Sheet 08, Fig. A-GBFAA Sheet 09 and Fig. A-GBFAA Sheet 10

(a) At one position, remove these items from the bracket between rib 11 and rib 12

and cable bundle 2S/636VB, as shown in Details A and D:

2 Clamp MS21919WCH4 Item (22) Retain

1 Clamp MS21919WCH4 Item (22) Discard

1 Clamp MS21919WCH3 Item (23) Retain

1 Spacer NSA5527-03-01D Item (30) Retain

1 Spacer NSA5527-03-02D Item (31) Retain

1 Washer NSA935808-01 Item (112) Retain

1 Screw NAS1096-3-30 Item (121) Discard

1 Clamp NSA935807-06 Item (122) Retain

(b) At two positions, remove these items from the brackets between rib 10 and rib 11

and between rib 11 and rib 12 and cable bundle 2S/636VB, as shown in Details A

and F:

2 Clamp Item (22) Discard

6 Clamp MS21919WCH4 Item (22) Retain

4 Spacer NSA5527-03-01D Item (30) Retain

2 Washer NAS1149D0332K Item (40) Retain

2 Screw NAS1096-3-27 Item (52) Retain

(c) At two positions, remove these items from the brackets of the rib 11 and cable

bundle 2S/636VB, as shown in Details A and H:

2 Clamp MS21919WCH4 Item (22) Retain

1 Clamp Item (23) Discard

1 Spacer NSA5527-03-01D Item (30) Retain

1 Spacer NSA5527-03-04D Item (32) Retain

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 72

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@A310

SERVICE BULLETIN

1 Washer NAS1149D0332K Item (40) Retain

1 Screw NAS1096-3-22 Item (51) Retain

(d) At two positions, remove these items from the brackets of the rib 10 and cable

bundle 2S/636VB, as shown in Details A and K:

2 Clamp Item (22) Discard

2 Clamp MS21919WCH4 Item (22) Retain

2 Spacer NSA5527-03-01D Item (30) Retain

2 Spacer Item (32) Discard

2 Washer NAS1149D0332K Item (40) Retain

2 Screw Item (51) Discard

(e) Remove these items from the bracket between rib 9 and rib 10 and cable bundle

2S/636VB, as shown in Details A and M:

3 Clamp MS21919WCH4 Item (22) Retain

1 Clamp Item (23) Discard

1 Spacer NSA5527-03-01D Item (30) Retain

1 Spacer NSA5527-03-04D Item (32) Retain

1 Washer NAS1149D0332K Item (40) Retain

1 Screw NAS1096-3-22 Item (51) Retain

(f) Remove these items from the bracket of the rib 9 and cable bundle 2S/636VB, as

shown in Details A and T:

1 Clamp Item (21) Discard

1 Clamp MS21919WCH5 Item (21) Retain

1 Spacer NSA5527-03-02D Item (31) Retain

1 Spacer NSA5527-03-04D Item (32) Retain

1 Washer NAS1149D0332K Item (40) Retain

1 Screw NAS1096-3-27 Item (52) Retain

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 73

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@A310

SERVICE BULLETIN

(g) Install this cable sleeve around these identified wires from the cable bundle

2S/636VB, as shown in Details A, C, E, G, J, L, N, A and R:

Wire number 2842-5061

Wire number 2842-5062

Wire number 2842-5063

Wire number 2842-5064

Wire number 2842-5065

Wire number 2842-5071

3 Sleeve ABS0596S004 Item 1

and attach the cable sleeves with:

3 Spacer NSA5527-03-03 Item 15

0.5 (ME) Cord NSA8420-2 Item 16

1 Tie NSA935401-03 Item 149

1 Tie-Cable NSA935401-04 Item 150

(h) At one positions, install these items to the brackets between rib 10 and rib 11 and

between rib 11 and rib 12, cable sleeves, Item 1 and cable bundle 2S/636VB, as

shown in Details A and E:

2 Clamp MS21919WCH4 Item (22) Retained at

removal

1 Clamp MS21919WCH3 Item (23) Retained at

removal

1 Spacer NSA5527-03-01D Item (30) Retained at

removal

1 Spacer NSA5527-03-02D Item (31) Retained at

removal

1 Washer NSA935808-01 Item (112) Retained at

removal

1 Clamp NSA935807-06 Item (122) Retained at

removal

1 Clamp MS21919WCH9 Item 10

2 Spacer NSA5527-03-02D Item 31

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 74

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SERVICE BULLETIN

1 Screw NAS1096-3-40 Item 121

(i) At two positions, install these items to the brackets between rib 10 and rib 11 and

between rib 11 and rib 12, cable sleeves, Item 1 and cable bundle 2S/636VB, as

shown in Details A and G:

6 Clamp MS21919WCH4 Item (22) Retained at

removal

4 Spacer NSA5527-03-01D Item (30) Retained at

removal

2 Washer NAS1149D0332K Item (40) Retained at

removal

2 Screw NAS1096-3-27 Item (52) Retained at

removal

2 Clamp MS21919WCH9 Item 10

(j) At two positions, install these items to the brackets of the rib 11, cable sleeves,

Item 1 and cable bundle 2S/636VB, as shown in Details A and J:

2 Clamp MS21919WCH4 Item (22) Retained at

removal

1 Spacer NSA5527-03-01D Item (30) Retained at

removal

1 Spacer NSA5527-03-04D Item (32) Retained at

removal

1 Washer NAS1149D0332K Item (40) Retained at

removal

1 Screw NAS1096-3-22 Item (51) Retained at

removal

1 Clamp MS21919WCH9 Item 10

(k) At two positions, install these items to the brackets of the rib 10, cable sleeves,

Item 1 and cable bundle 2S/636VB, as shown in Details A and L:

2 Clamp MS21919WCH4 Item (22) Retained at

removal

2 Spacer NSA5527-03-01D Item (30) Retained at

removal

2 Washer NAS1149D0332K Item (40) Retained at

removal

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 75

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SERVICE BULLETIN

2 Clamp MS21919WCH9 Item 10

2 Screw NAS1096-3-19 Item 14

(l) Install these items to the bracket between rib 9 and rib 10, cable sleeves, Item 1

and cable bundle 2S/636VB, as shown in Details A and N:

3 Clamp MS21919WCH4 Item (22) Retained at

removal

1 Spacer NSA5527-03-01D Item (30) Retained at

removal

1 Spacer NSA5527-03-04D Item (32) Retained at

removal

1 Washer NAS1149D0332K Item (40) Retained at

removal

1 Screw NAS1096-3-22 Item (51) Retained at

removal

1 Clamp MS21919WCH9 Item 10

(m) Install these items to the bracket of the rib 9, cable sleeves, Item 1 and cable

bundle 2S/636VB, as shown in Details A and Q:

1 Clamp MS21919WCH5 Item (21) Retained at

removal

1 Spacer NSA5527-03-02D Item (31) Retained at

removal

1 Spacer NSA5527-03-04D Item (32) Retained at

removal

1 Washer NAS1149D0332K Item (40) Retained at

removal

1 Screw NAS1096-3-27 Item (52) Retained at

removal

1 Clamp MS21919WCH9 Item 10

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 76

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SERVICE BULLETIN

**CONF 002

(1) Subtask 282148-831-405-001 - Install a New Bracket on the Sub Spar Behind the

Front Spar Between RIB 8 and RIB 9 on the RH Wing

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills AIRFRAME

Material necessary to do the job

Kit 282148B01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 A5725068600000 1 Bracket

2 ASNA0078A502 2 Rivet

Consumable CMLB01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Corrosion Inhibiting Low

Adhesion Sealant

09-018 As required

Solvent General Purpose 11-026 As required

Lint-Free Cotton Cloth 19-003 As required

References

Fig. A-UBAAA

Location of Bracket on the Sub Spar

Behind the Front Spar Between RIB 8

and RIB 9 (RH Wing)

Sheet 01

Refer to Fig. A-UBAAA Sheet 01

(a) Remove from the sub spar behind the front spar between RIB 8 and RIB 9 on the

RH wing, the items that follow:

2 Rivet NSA54213510DCA Item (2) Discard

1 Bracket A5724630400000 Item (1) Discard

(b) Clean the mating surfaces use

Lint-Free Cotton

Cloth

19-003 As required

made moist with

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 77

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SERVICE BULLETIN

Solvent General

Purpose

11-026 As required

(c) Put the

1 Bracket A5725068600000 Item 1

in position on the sub spar behind the front spar between RIB 8 and RIB 9 on the

RH wing (Refer to Fig. A-UBAAA Sheet 01).

(d) Copy drill the two holes from the sub spar through the Bracket, Item 1 to a

dimension of between 4.060 and 4.160 mm (0.160 and 0.164 in.).

(e) Deburr the holes that have been worked.

(f) Use

Corrosion Inhibiting

Low Adhesion

Sealant

09-018 As required

and wet install the

1 Bracket A5725068600000 Item 1

with the

2 Rivet, Blind ASNA0078A502 Item 2

on the sub spar behind the front spar between RIB 8 and RIB 9 on the RH wing.

(2) Subtask 282148-831-004-001 - Install cable sleeves in the RH Electronics Rack

90VU.

Manpower Resources

Manhours 6.00

Minimum number of person 1

Subtask elapsed time 6.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 282148A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 ABS0596S004 2000 (mm) SLEEVE

NSA935401-04 50 TIE

References

Fig. A-FCAAA

Installation of Cable Sleeves in the RH

Electronics Rack 90VU.

Sheet 01

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 78

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SERVICE BULLETIN

References

Fig. A-FWAAA

Installation of Cable Sleeves in the RH

Electronics Rack 90VU.

Sheet 01

NOTE: The sleeves ABS0596S004 and ABS0596S006 are supplied in pieces of

1000 mm (39.370 inches), cut or assemble these pieces to get the

correct length.

NOTE: The lengths of the sleeves given in this Service Bulletin are approximate

lengths. Adapt the lengths of the sleeves in relation to the aircraft

configuration.

NOTE: Before you install a sleeve, cut and discard the cable ties around the

cable bundle to install the sleeve correctly around the cable bundle.

(a) On the Shelf 92VU, only around the wires identified in figure Fig. A-FWAAA Sheet

01, from the equipment 15QT-B to the connector 2354VC, install:

1600 (mm) Sleeve ABS0596S004 Item 1

(b) Around the cable bundle of the connector 2354VC-A, install:

400 (mm) Sleeve ABS0596S004 Item 1

(c) Attach the sleeves with:

50 Tie-Cable NSA935401-04

(3) Subtask 282148-831-005-001 - Install cable sleeves between FR38.2 and FR39, in

the forward cargo compartment.

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 282148A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

2 ABS0596S006 1000 (mm) SLEEVE

NSA935401-05 50 TIE

References

Fig. A-FCBAA

Installation of Cable Sleeves in the

Forward Cargo Compartment.

Sheet 01

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 79

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SERVICE BULLETIN

NOTE: The sleeves ABS0596S004 and ABS0596S006 are supplied in pieces of

1000 mm (39.370 inches), cut or assemble these pieces to get the

correct length.

NOTE: The lengths of the sleeves given in this Service Bulletin are approximate

lengths. Adapt the lengths of the sleeves in relation to the aircraft

configuration.

NOTE: Before you install a sleeve, cut and discard the cable ties around the

cable bundle to install the sleeve correctly around the cable bundle.

(a) Around the cable bundle of the pressure seal 20VP, install:

1000 (mm) Sleeve ABS0596S006 Item 2

(b) Attach the sleeves with:

50 Tie-Cable NSA935401-05

(4) Subtask 282148-831-006-001 - Install cable sleeves in the RH forward wing root

and krueger flap.

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 282148A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

2 ABS0596S006 1000 (mm) SLEEVE

NSA935401-05 50 TIE

References

Fig. A-FCCAA

Installation of Cable Sleeves in the RH

forward wing root and krueger flap.

Sheet 01

(a) Around the cable bundle of the pressure seal 20VP, install:

1000 (mm) Sleeve ABS0596S006 Item 2

(b) Attach the sleeves with:

50 Tie-Cable NSA935401-05

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 80

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@A310

SERVICE BULLETIN

(5) Subtask 282148-831-208-002 - Install the cable sleeves in the RH-wing forward of

the front spar between rib 2 and rib 3 in zone 612.

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

Material necessary to do the job

Kit 282148D01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 ABS0596S004 1 SLEEVE

11 MS21919WCH13 CLAMP

149 NSA935401-03 1 TIE

150 NSA935401-04 1 TIE

References

Fig. A-GBEAA

Improvement of the 2S-Route in the RHWing in Zone 612 (Kit D01)

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

Sheet 07

Sheet 08

NOTE (1): The sleeves ABS0596S004 is supplied in pieces of 1000 mm. Cut or

assemble these pieces to get the correct length.

NOTE (2): The lengths of the sleeves given in this Service Bulletin are approximate

lengths. Adapt the lengths of the sleeves in relation to the aircraft

configuration.

NOTE (3): Before you install a sleeve, cut and discard the cable ties around the

cable bundle to install the sleeve correctly around the cable bundle.

NOTE (4): Adapt the number of cable ties to the required quantity.

Refer to Fig. A-GBEAA Sheet 01, Fig. A-GBEAA Sheet 02, Fig. A-GBEAA Sheet 03, Fig.

A-GBEAA Sheet 04, Fig. A-GBEAA Sheet 05, Fig. A-GBEAA Sheet 06, Fig. A-GBEAA

Sheet 07 and Fig. A-GBEAA Sheet 08

(a) Remove these items from the bracket of the rib 2 and cable bundle 2S/624VB, as

shown in Details A and B:

1 Clamp MS21919WCH4 Item (22) Retain

1 Clamp MS21919WCH3 Item (23) Retain

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 81

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SERVICE BULLETIN

1 Spacer NSA5527-03-02D Item (31) Retain

1 Washer NAS1149D0332K Item (40) Retain

1 Screw NAS1096-3-21 Item (50) Retain

1 Clamp MS21919WCH10 Item (100) Retain

1 Clamp Item (100) Discard

(b) Remove these items from the riblet and cable bundle 2S/624VB, as shown in

Details A and D:

1 Clamp MS21919WCH4 Item (22) Retain

3 Spacer NSA5527-03-02D Item (31) Retain

1 Washer NAS1149D0332K Item (40) Retain

1 Screw NAS1096-3-38 Item (54) Retain

1 Clamp Item (100) Discard

(c) Install this cable sleeve around these identified wires from the cable bundle

2S/624VB, as shown in Details A, C, E and F:

Wire number 2842-5052

Wire number 2842-5053

Wire number 2842-5054

Wire number 2842-5055

Wire number 2842-5056

Wire number 2842-5070

Install this cable sleeve around these identified wires from the cable bundle

2S/624VB, as shown in Details A, C, E and F:

Wire number 2842-5052

Wire number 2842-5053

Wire number 2842-5054

Wire number 2842-5055

Wire number 2842-5056

Wire number 2842-5070

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 82

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SERVICE BULLETIN

1 Sleeve ABS0596S004 Item 1

and attach the cable sleeve with:

1 Tie NSA935401-03 Item 149

1 Tie-Cable NSA935401-04 Item 150

(d) Install these items to the bracket of the rib 2, cable bundle 2S/624VB and cable

sleeve, Item 1, as shown in Details A and C:

1 Clamp MS21919WCH4 Item (22) Retained at

removal

1 Clamp MS21919WCH3 Item (23) Retained at

removal

1 Spacer NSA5527-03-02D Item (31) Retained at

removal

1 Washer NAS1149D0332K Item (40) Retained at

removal

1 Screw NAS1096-3-21 Item (50) Retained at

removal

1 Clamp MS21919WCH10 Item (100) Retained at

removal

1 Clamp MS21919WCH13 Item 11

(e) Install these items to the riblet, cable bundle 2S/624VB and cable sleeve, Item 1,

as shown in Details A and E:

1 Clamp MS21919WCH4 Item (22) Retained at

removal

3 Spacer NSA5527-03-02D Item (31) Retained at

removal

1 Washer NAS1149D0332K Item (40) Retained at

removal

1 Screw NAS1096-3-38 Item (54) Retained at

removal

1 Clamp MS21919WCH13 Item 11

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 83

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SERVICE BULLETIN

(6) Subtask 282148-831-209-002 - Install the cable sleeves in the RH-wing forward of

the front spar between rib 7 and rib 8 in zone 612.

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

Material necessary to do the job

Kit 282148D01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 ABS0596S004 2 SLEEVE

12 MS21919WCH14 CLAMP

149 NSA935401-03 2 TIE

150 NSA935401-04 2 TIE

References

Fig. A-GBEAA

Improvement of the 2S-Route in the RHWing in Zone 612 (Kit D01)

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

Sheet 07

Sheet 08

NOTE (1): The sleeves ABS0596S004 is are supplied in pieces of 1000 mm. Cut or

assemble these pieces to get the correct length.

NOTE (2): The lengths of the sleeves given in this Service Bulletin are approximate

lengths. Adapt the lengths of the sleeves in relation to the aircraft

configuration.

NOTE (3): Before you install a sleeve, cut and discard the cable ties around the

cable bundle to install the sleeve correctly around the cable bundle.

NOTE (4): Adapt the number of cable ties to the required quantity.

Refer to Fig. A-GBEAA Sheet 01, Fig. A-GBEAA Sheet 02, Fig. A-GBEAA Sheet 03, Fig.

A-GBEAA Sheet 04, Fig. A-GBEAA Sheet 05, Fig. A-GBEAA Sheet 06, Fig. A-GBEAA

Sheet 07 and Fig. A-GBEAA Sheet 08

(a) Remove these items from the two brackets of the riblets and cable bundle

2S/624VB, as shown in Details A, H and K:

2 Clamp MS21919WCH4 Item (22) Retain

2 Washer NAS1149D0332K Item (40) Retain

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 84

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SERVICE BULLETIN

2 Screw NAS1096-3-8 Item (55) Retain

2 Clamp Item (100) Discard

(b) Install this cable sleeve around these identified wires from the cable bundle

2S/624VB, as shown in Details A, J, K, L, M and N:

Wire number 2842-5052

Wire number 2842-5053

Wire number 2842-5054

Wire number 2842-5055

Wire number 2842-5056

1 Sleeve ABS0596S004 Item 1

and attach the cable sleeves with:

1 Tie NSA935401-03 Item 149

1 Tie-Cable NSA935401-04 Item 150

(c) Install this cable sleeve around this identified wire from the cable bundle 2S/624VB,

as shown in Details A, J, K, L, M and N:

Wire number 2842-5070

1 Sleeve ABS0596S004 Item 1

and attach the cable sleeves with:

1 Tie NSA935401-03 Item 149

1 Tie-Cable NSA935401-04 Item 150

(d) Install these items to the two brackets of the riblets, cable bundle 2S/624VB and

cable sleeves, Item 1, as shown in Detail A, J and L:

2 Clamp MS21919WCH4 Item (22) Retained at

removal

2 Washer NAS1149D0332K Item (40) Retained at

removal

2 Screw NAS1096-3-8 Item (55) Retained at

removal

2 Clamp MS21919WCH14 Item 12

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 85

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SERVICE BULLETIN

(7) Subtask 282148-831-210-002 - Install the cable sleeves in the RH-wing forward of

the front spar between rib 8 and rib 9 (pylon area) in zone 612.

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

Material necessary to do the job

Kit 282148D02R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

109 NSA935805-09 CONDUIT

Kit 282148D03R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 ABS0596S004 3 SLEEVE

31 NSA5527-03-02D 1 SPACER

117 NSA935807C09 7 CLAMP

123 NAS1801-3-31 3 SCREW

126 NSA938184PV1601 7 PIN

130 NSA5527-03-08D 1 SPACER

131 NSA5527-03-07D 1 SPACER

132 B9299071900600 1 EQUIPMNT

149 NSA935401-03 20 TIE

150 NSA935401-04 20 TIE

References

Fig. A-GBHAA

Improvement of the 2S-Route in the RHWing Pylon Area (Kit D03)

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

Sheet 07

Sheet 08

Fig. A-GHBAA

Hook-up Chart

Sheet 01

NOTE (1): The sleeves ABS0596S004 is supplied in pieces of 1000 mm. Cut or

assemble these pieces to get the correct length.

NOTE (2): The lengths of the sleeves given in this Service Bulletin are approximate

lengths. Adapt the lengths of the sleeves in relation to the aircraft

configuration.

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 86

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SERVICE BULLETIN

NOTE (3): Before you install a sleeve, cut and discard the cable ties around the

cable bundle to install the sleeve correctly around the cable bundle.

NOTE (4): Adapt the number of cable ties to the required quantity.

Refer to Fig. A-GBHAA Sheet 01, Fig. A-GBHAA Sheet 02, Fig. A-GBHAA Sheet 03,

Fig. A-GBHAA Sheet 04, Fig. A-GBHAA Sheet 05, Fig. A-GBHAA Sheet 06, Fig. AGBHAA Sheet 07 and Fig. A-GBHAA Sheet 08

(a) Disconnect the wires of route 2S from the receptacles 40VC and 5006VC in

accordance with the Hook-up Chart 2, Lines 2 thru 8, END 1, Fig. A-GHBAA Sheet

01.

(b) Remove, refer to Fig. A-GBHAA Sheet 03, Detail D, BEFORE:

1 Spacer NSA5527-03-02D Item (31) Retain

2 Clamp NSA935807C16 Item (111) Retain

1 Washer NSA935808-01 Item (112) Retain

1 Screw NAS1096-3-23 Item (113) Retain

1 Spacer NSA5527-03-05D Item (114) Retain

1 Nut NAS1291C3M Item (116) Retain

1 Washer AN960KD10l Item (124) Retain

(c) Remove, refer to Fig. A-GBHAA Sheet 04, Detail F, BEFORE:

1 Spacer NSA5527-03-02D Item (31) Retain

2 Clamp NSA935807C16 Item (111) Retain

1 Washer NSA935808-01 Item (112) Retain

1 Screw NAS1096-3-23 Item (113) Retain

1 Spacer NSA5527-03-05D Item (114) Retain

(d) Remove, refer to Fig. A-GBHAA Sheet 05, Detail H, BEFORE:

2 Spacer NSA5527-03-02D Item (31) Retain

4 Clamp NSA935807C16 Item (111) Retain

2 Washer NSA935808-01 Item (112) Retain

2 Screw NAS1096-3-23 Item (113) Retain

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 87

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SERVICE BULLETIN

2 Spacer NSA5527-03-05D Item (114) Retain

(e) Remove, refer to Fig. A-GBHAA Sheet 06, Detail K, BEFORE:

1 Spacer NSA5527-03-02D Item (31) Retain

2 Clamp NSA935807C16 Item (111) Retain

1 Washer NSA935808-01 Item (112) Retain

1 Screw NAS1096-3-23 Item (113) Discard

1 Clamp NSA5516-04NV Item (120) Retain

(f) Remove, refer to Fig. A-GBHAA Sheet 07, Detail M, BEFORE:

1 Spacer NSA5527-03-02D Item (31) Retain

2 Clamp NSA935807C16 Item (111) Retain

1 Washer NSA935808-01 Item (112) Retain

1 Screw NAS1096-3-23 Item (113) Discard

1 Spacer NSA5527-03-05D Item (114) Retain

(g) Remove, refer to Fig. A-GBHAA Sheet 08, Detail P, BEFORE:

1 Spacer NSA5527-03-02D Item (31) Retain

2 Clamp NSA935807C16 Item (111) Retain

1 Washer NSA935808-01 Item (112) Retain

1 Screw NAS1096-3-23 Item (113) Discard

1 Spacer NSA5527-03-05D Item (114) Retain

(h) Remove the identification placards from the cable harnesses near the receptacles

52VC and 5006VC as shown Fig. A-GBHAA Sheet 02, Detail A

As

required

placard Item (132) Discard

(i) Remove the disconnected electrical wires from the protection sleeve.

(j) Install to the electrical wires for 10QT-A and 10QT-B of route 2S/636VB, refer to

the Hook-up Chart 2, Lines 2 thru 8, Fig. A-GHBAA Sheet 01:

1 (ME) Conduit NSA935805-09 Item 109

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 88

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SERVICE BULLETIN

(k) Connect the electrical wires of route 2S to the receptacles 40VC and 5006VC in

accordance with the Hook-up Chart 2, Lines 2 thru 8, END 1, Fig. A-GHBAA Sheet

01. Use the contact pins if required:

7 Pin NSA938184PV1601 Item 126

(l) Install, refer to Fig. A-GBHAA Sheet 08, Detail Q, AFTER:

1 Spacer NSA5527-03-02D Item (31) Retained at

removal

1 Spacer NSA5527-03-02D Item 31

2 Clamp NSA935807C16 Item (111) Retained at

removal

1 Washer NSA935808-01 Item (112) Retained at

removal

1 Spacer NSA5527-03-05D Item (114) Retained at

removal

1 Clamp NSA935807C09 Item 117

1 Screw NAS1801-3-31 Item 123

1 Spacer NSA5527-03-07D Item 131

(m) Install, refer to Fig. A-GBHAA Sheet 07, Detail N, AFTER:

1 Spacer NSA5527-03-02D Item (31) Retained at

removal

2 Clamp NSA935807C16 Item (111) Retained at

removal

1 Washer NSA935808-01 Item (112) Retained at

removal

1 Spacer NSA5527-03-05D Item (114) Retained at

removal

1 Clamp NSA935807C09 Item 117

1 Screw NAS1801-3-31 Item 123

1 Spacer NSA5527-03-08D Item 130

(n) Install, refer to Fig. A-GBHAA Sheet 06, Detail L, AFTER:

2 Spacer NSA5527-03-02D Item (31) Retained at

removal

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 89

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SERVICE BULLETIN

2 Clamp NSA935807C16 Item (111) Retained at

removal

1 Washer NSA935808-01 Item (112) Retained at

removal

1 Clamp NSA5516-04NV Item (120) Retained at

removal

1 Clamp NSA935807C09 Item 117

2 Screw NAS1801-3-31 Item 123

(o) Install, refer to Fig. A-GBHAA Sheet 05, Detail J, AFTER:

2 Spacer NSA5527-03-02D Item (31) Retained at

removal

4 Clamp NSA935807C16 Item (111) Retained at

removal

2 Washer NSA935808-01 Item (112) Retained at

removal

2 Screw NAS1096-3-23 Item (113) Retained at

removal

2 Spacer NSA5527-03-05D Item (114) Retained at

removal

2 Clamp NSA935807C09 Item 117

(p) Install, refer to Fig. A-GBHAA Sheet 04, Detail G, AFTER:

1 Spacer NSA5527-03-02D Item (31) Retained at

removal

2 Clamp NSA935807C16 Item (111) Retained at

removal

1 Washer NSA935808-01 Item (112) Retained at

removal

1 Screw NAS1096-3-23 Item (113) Retained at

removal

1 Spacer NSA5527-03-05D Item (114) Retained at

removal

1 Clamp NSA935807C09 Item 117

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 90

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SERVICE BULLETIN

(q) Install, refer to Fig. A-GBHAA Sheet 03, Detail E, AFTER:

1 Spacer NSA5527-03-02D Item (31) Retained at

removal

2 Clamp NSA935807C16 Item (111) Retained at

removal

1 Washer NSA935808-01 Item (112) Retained at

removal

1 Screw NAS1096-3-23 Item (113) Retained at

removal

1 Spacer NSA5527-03-05D Item (114) Retained at

removal

1 Nut NAS1291C3M Item (116) Retained at

removal

1 Washer AN960KD10l Item (124) Retained at

removal

1 Clamp NSA935807C09 Item 117

(r) Protect the electrical wires for 10QT-A and 10QT-B of route 2S/636VB, refer to the

Hook-up Chart 2, Fig. A-GHBAA Sheet 01 with:

3 Sleeve ABS0596S004 Item 1

and

20 Tie NSA935401-03 Item 149

20 Tie-Cable NSA935401-04 Item 150

(s) Install the identification placards, refer to Fig. A-GBHAA Sheet 02:

1 Placard Set B9299071900600 Item 132

(8) Subtask 282148-831-211-002 - Install the cable sleeves in the RH-wing forward of

the front spar between rib 9 and rib 12 in zone 623.

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

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SERVICE BULLETIN

Material necessary to do the job

Kit 282148D01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 ABS0596S004 3 SLEEVE

10 MS21919WCH9 CLAMP

14 NAS1096-3-19 2 SCREW

15 NSA5527-03-03 3 SPACER

16 NSA8420-2 1 (ME) CORD

149 NSA935401-03 10 TIE

150 NSA935401-04 20 TIE

Kit 282148D03R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

31 NSA5527-03-02D 1 SPACER

121 NAS1096-3-40 1 SCREW

References

Fig. A-GBFAA

Improvement of the 2S-Route in the RHWing in Zone 623 (Kit D01)

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

Sheet 07

Sheet 08

Sheet 09

Sheet 10

NOTE (1): The sleeve ABS0596S004 is supplied in pieces of 1000 mm. Cut or

assemble these pieces to get the correct length.

NOTE (2): The lengths of the sleeves given in this Service Bulletin are approximate

lengths. Adapt the lengths of the sleeves in relation to the aircraft

configuration.

NOTE (3): Before you install a sleeve, cut and discard the cable ties around the

cable bundle to install the sleeve correctly around the cable bundle.

NOTE (4): Adapt the number of cable ties to the required quantity.

Refer to Fig. A-GBFAA Sheet 01, Fig. A-GBFAA Sheet 02, Fig. A-GBFAA Sheet 03, Fig.

A-GBFAA Sheet 04, Fig. A-GBFAA Sheet 05, Fig. A-GBFAA Sheet 06, Fig. A-GBFAA

Sheet 07, Fig. A-GBFAA Sheet 08, Fig. A-GBFAA Sheet 09 and Fig. A-GBFAA Sheet 10

(a) At one position, remove these items from the bracket between rib 11 and rib 12

and cable bundle 2S/636VB, as shown in Details A and D:

2 Clamp MS21919WCH4 Item (22) Retain

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

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SERVICE BULLETIN

1 Clamp MS21919WCH4 Item (22) Discard

1 Clamp MS21919WCH3 Item (23) Retain

1 Spacer NSA5527-03-01D Item (30) Retain

1 Spacer NSA5527-03-02D Item (31) Retain

2 Washer NSA935808-01 Item (112) Retain

2 Screw NAS1096-3-30 Item (121) Discard

1 Clamp NSA935807-06 Item (122) Retain

(b) At two positions, remove these items from the brackets between rib 10 and rib 11

and between rib 11 and rib 12 and cable bundle 2S/636VB, as shown in Details A

and F:

2 Clamp Item (22) Discard

6 Clamp MS21919WCH4 Item (22) Retain

4 Spacer NSA5527-03-01D Item (30) Retain

2 Washer NAS1149D0332K Item (40) Retain

2 Screw NAS1096-3-27 Item (52) Retain

(c) At two positions, remove these items from the brackets of the rib 11 and cable

bundle 2S/636VB, as shown in Details A and H:

6 Clamp MS21919WCH4 Item (22) Retain

2 Clamp Item (23) Discard

2 Spacer NSA5527-03-01D Item (30) Retain

2 Spacer NSA5527-03-04D Item (32) Retain

2 Washer NAS1149D0332K Item (40) Retain

2 Screw NAS1096-3-22 Item (51) Retain

(d) At two positions, remove these items from the brackets of the rib 10 and cable

bundle 2S/636VB, as shown in Details A and K:

2 Clamp Item (22) Discard

2 Clamp MS21919WCH4 Item (22) Retain

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

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SERVICE BULLETIN

2 Spacer NSA5527-03-01D Item (30) Retain

2 Spacer Item (32) Discard

2 Washer NAS1149D0332K Item (40) Retain

2 Screw Item (51) Discard

(e) Remove these items from the bracket between rib 9 and rib 10 and cable bundle

2S/636VB, as shown in Details A and M:

3 Clamp MS21919WCH4 Item (22) Retain

1 Clamp Item (23) Discard

1 Spacer NSA5527-03-01D Item (30) Retain

1 Spacer NSA5527-03-04D Item (32) Retain

1 Washer NAS1149D0332K Item (40) Retain

1 Screw NAS1096-3-22 Item (51) Retain

(f) Remove these items from the bracket of the rib 9 and cable bundle 2S/636VB, as

shown in Details A and T:

1 Clamp Item (21) Discard

1 Clamp MS21919WCH5 Item (21) Retain

1 Spacer NSA5527-03-02D Item (31) Retain

1 Spacer NSA5527-03-04D Item (32) Retain

1 Washer NAS1149D0332K Item (40) Retain

1 Screw NAS1096-3-27 Item (52) Retain

(g) Install this cable sleeve around these identified wires from the cable bundle

2S/636VB, as shown in Details A, C, E, G, J, L, N, Q, R, S and T:

Wire number 2842-5061

Wire number 2842-5062

Wire number 2842-5063

Wire number 2842-5064

Wire number 2842-5065

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

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SERVICE BULLETIN

Wire number 2842-5071

3 Sleeve ABS0596S004 Item 1

and attach the cable sleeves with:

3 Spacer NSA5527-03-03 Item 15

1 (ME) Cord NSA8420-2 Item 16

10 Tie NSA935401-03 Item 149

20 Tie-Cable NSA935401-04 Item 150

(h) At one positions, install these items to the brackets between rib 10 and rib 11 and

between rib 11 and rib 12, cable sleeves, Item 1 and cable bundle 2S/636VB, as

shown in Details A and E:

2 Clamp MS21919WCH4 Item (22) Retained at

removal

1 Clamp MS21919WCH3 Item (23) Retained at

removal

1 Spacer NSA5527-03-01D Item (30) Retained at

removal

1 Spacer NSA5527-03-02D Item (31) Retained at

removal

1 Washer NSA935808-01 Item (112) Retained at

removal

1 Clamp NSA935807-06 Item (122) Retained at

removal

1 Clamp MS21919WCH9 Item 10

1 Spacer NSA5527-03-02D Item 31

1 Screw NAS1096-3-40 Item 121

(i) At two positions, install these items to the brackets between rib 10 and rib 11 and

between rib 11 and rib 12, cable sleeves, Item 1 and cable bundle 2S/636VB, as

shown in Details A and G:

6 Clamp MS21919WCH4 Item (22) Retained at

removal

4 Spacer NSA5527-03-01D Item (30) Retained at

removal

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

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SERVICE BULLETIN

2 Washer NAS1149D0332K Item (40) Retained at

removal

2 Screw NAS1096-3-27 Item (52) Retained at

removal

2 Clamp MS21919WCH9 Item 10

(j) At two positions, install these items to the brackets of the rib 11, cable sleeves,

Item 1 and cable bundle 2S/636VB, as shown in Details A and J:

6 Clamp MS21919WCH4 Item (22) Retained at

removal

2 Spacer NSA5527-03-01D Item (30) Retained at

removal

2 Spacer NSA5527-03-04D Item (32) Retained at

removal

2 Washer NAS1149D0332K Item (40) Retained at

removal

2 Screw NAS1096-3-22 Item (51) Retained at

removal

2 Clamp MS21919WCH9 Item 10

(k) At two positions, install these items to the brackets of the rib 10, cable sleeves,

Item 1 and cable bundle 2S/636VB, as shown in Details A and L:

2 Clamp MS21919WCH4 Item (22) Retained at

removal

2 Spacer NSA5527-03-01D Item (30) Retained at

removal

2 Washer NAS1149D0332K Item (40) Retained at

removal

2 Clamp MS21919WCH9 Item 10

2 Screw NAS1096-3-19 Item 14

(l) Install these items to the bracket between rib 9 and rib 10, cable sleeves, Item 1

and cable bundle 2S/636VB, as shown in Details A and Q:

3 Clamp MS21919WCH4 Item (22) Retained at

removal

1 Spacer NSA5527-03-01D Item (30) Retained at

removal

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 96

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SERVICE BULLETIN

1 Spacer NSA5527-03-04D Item (32) Retained at

removal

1 Washer NAS1149D0332K Item (40) Retained at

removal

1 Screw NAS1096-3-22 Item (51) Retained at

removal

1 Clamp MS21919WCH9 Item 10

(m) Install these items to the bracket of the rib 9, cable sleeves, Item 1 and cable

bundle 2S/636VB, as shown in Details A and Q:

1 Clamp MS21919WCH5 Item (21) Retained at

removal

1 Spacer NSA5527-03-02D Item (31) Retained at

removal

1 Spacer NSA5527-03-04D Item (32) Retained at

removal

1 Washer NAS1149D0332K Item (40) Retained at

removal

1 Screw NAS1096-3-27 Item (52) Retained at

removal

1 Clamp MS21919WCH9 Item 10

**CONF 003

(1) Subtask 282148-831-405-001 - Install a New Bracket on the Sub Spar Behind the

Front Spar Between RIB 8 and RIB 9 on the RH Wing

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills AIRFRAME

Material necessary to do the job

Kit 282148B01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 A5725068600000 1 Bracket

2 ASNA0078A502 2 Rivet

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SERVICE BULLETIN

Consumable CMLB01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Corrosion Inhibiting Low

Adhesion Sealant

09-018 As required

Solvent General Purpose 11-026 As required

Lint-Free Cotton Cloth 19-003 As required

References

Fig. A-UBAAA

Location of Bracket on the Sub Spar

Behind the Front Spar Between RIB 8

and RIB 9 (RH Wing)

Sheet 01

Refer to Fig. A-UBAAA Sheet 01

(a) Remove from the sub spar behind the front spar between RIB 8 and RIB 9 on the

RH wing, the items that follow:

2 Rivet NSA54213510DCA Item (2) Discard

1 Bracket A5724630400000 Item (1) Discard

(b) Clean the mating surfaces use

Lint-Free Cotton

Cloth

19-003 As required

made moist with

Solvent General

Purpose

11-026 As required

(c) Put the

1 Bracket A5725068600000 Item 1

in position on the sub spar behind the front spar between RIB 8 and RIB 9 on the

RH wing (Refer to Fig. A-UBAAA Sheet 01).

(d) Copy drill the two holes from the sub spar through the Bracket, Item 1 to a

dimension of between 4.060 and 4.160 mm (0.160 and 0.164 in.).

(e) Deburr the holes that have been worked.

(f) Use

Corrosion Inhibiting

Low Adhesion

Sealant

09-018 As required

and wet install the

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

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SERVICE BULLETIN

1 Bracket A5725068600000 Item 1

with the

2 Rivet, Blind ASNA0078A502 Item 2

on the sub spar behind the front spar between RIB 8 and RIB 9 on the RH wing.

(2) Subtask 282148-831-004-001 - Install cable sleeves in the RH Electronics Rack

90VU.

Manpower Resources

Manhours 6.00

Minimum number of person 1

Subtask elapsed time 6.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 282148A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 ABS0596S004 2000 (mm) SLEEVE

NSA935401-04 50 TIE

References

Fig. A-FCAAA

Installation of Cable Sleeves in the RH

Electronics Rack 90VU.

Sheet 01

Fig. A-FWAAA

Installation of Cable Sleeves in the RH

Electronics Rack 90VU.

Sheet 01

NOTE: The sleeves ABS0596S004 and ABS0596S006 are supplied in pieces of

1000 mm (39.370 inches), cut or assemble these pieces to get the

correct length.

NOTE: The lengths of the sleeves given in this Service Bulletin are approximate

lengths. Adapt the lengths of the sleeves in relation to the aircraft

configuration.

NOTE: Before you install a sleeve, cut and discard the cable ties around the

cable bundle to install the sleeve correctly around the cable bundle.

(a) On the Shelf 92VU, only around the wires identified in figure Fig. A-FWAAA Sheet

01, from the equipment 15QT-B to the connector 2354VC, install:

1600 (mm) Sleeve ABS0596S004 Item 1

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

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SERVICE BULLETIN

(b) Around the cable bundle of the connector 2354VC-A, install:

400 (mm) Sleeve ABS0596S004 Item 1

(c) Attach the sleeves with:

50 Tie-Cable NSA935401-04

(3) Subtask 282148-831-005-001 - Install cable sleeves between FR38.2 and FR39, in

the forward cargo compartment.

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 282148A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

2 ABS0596S006 1000 (mm) SLEEVE

NSA935401-05 50 TIE

References

Fig. A-FCBAA

Installation of Cable Sleeves in the

Forward Cargo Compartment.

Sheet 01

NOTE: The sleeves ABS0596S004 and ABS0596S006 are supplied in pieces of

1000 mm (39.370 inches), cut or assemble these pieces to get the

correct length.

NOTE: The lengths of the sleeves given in this Service Bulletin are approximate

lengths. Adapt the lengths of the sleeves in relation to the aircraft

configuration.

NOTE: Before you install a sleeve, cut and discard the cable ties around the

cable bundle to install the sleeve correctly around the cable bundle.

(a) Around the cable bundle of the pressure seal 20VP, install:

1000 (mm) Sleeve ABS0596S006 Item 2

(b) Attach the sleeves with:

50 Tie-Cable NSA935401-05

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

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SERVICE BULLETIN

(4) Subtask 282148-831-006-001 - Install cable sleeves in the RH forward wing root

and krueger flap.

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 282148A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

2 ABS0596S006 1000 (mm) SLEEVE

NSA935401-05 50 TIE

References

Fig. A-FCCAA

Installation of Cable Sleeves in the RH

forward wing root and krueger flap.

Sheet 01

(a) Around the cable bundle of the pressure seal 20VP, install:

1000 (mm) Sleeve ABS0596S006 Item 2

(b) Attach the sleeves with:

50 Tie-Cable NSA935401-05

(5) Subtask 282148-831-208-003 - Install the cable sleeves in the RH-wing forward of

the front spar between rib 2 and rib 3 in zone 612.

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

Material necessary to do the job

Kit 282148D01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 ABS0596S004 1 SLEEVE

11 MS21919WCH13 CLAMP

149 NSA935401-03 1 TIE

150 NSA935401-04 1 TIE

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@A310

SERVICE BULLETIN

Kit 282148D05R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

125 B9299071900200 1 EQUIPMNT

References

Fig. A-GBEAA

Improvement of the 2S-Route in the RHWing in Zone 612 (Kit D01)

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

Sheet 07

Sheet 08

NOTE (1): The sleeves ABS0596S004 is supplied in pieces of 1000 mm. Cut or

assemble these pieces to get the correct length.

NOTE (2): The lengths of the sleeves given in this Service Bulletin are approximate

lengths. Adapt the lengths of the sleeves in relation to the aircraft

configuration.

NOTE (3): Before you install a sleeve, cut and discard the cable ties around the

cable bundle to install the sleeve correctly around the cable bundle.

NOTE (4): Adapt the number of cable ties to the required quantity.

Refer to Fig. A-GBEAA Sheet 01, Fig. A-GBEAA Sheet 02, Fig. A-GBEAA Sheet 03, Fig.

A-GBEAA Sheet 04, Fig. A-GBEAA Sheet 05, Fig. A-GBEAA Sheet 06, Fig. A-GBEAA

Sheet 07 and Fig. A-GBEAA Sheet 08

(a) Remove these items from the bracket of the rib 2 and cable bundle 2S/624VB, as

shown in Details A and B:

1 Clamp MS21919WCH4 Item (22) Retain

1 Clamp MS21919WCH3 Item (23) Retain

1 Spacer NSA5527-03-02D Item (31) Retain

1 Washer NAS1149D0332K Item (40) Retain

1 Screw NAS1096-3-21 Item (50) Retain

1 Clamp MS21919WCH10 Item (100) Retain

1 Clamp Item (100) Discard

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(b) Remove these items from the riblet and cable bundle 2S/624VB, as shown in

Details A and D:

1 Clamp MS21919WCH4 Item (22) Retain

3 Spacer NSA5527-03-02D Item (31) Retain

1 Washer NAS1149D0332K Item (40) Retain

1 Screw NAS1096-3-38 Item (54) Retain

1 Clamp Item (100) Discard

(c) Install this cable sleeve around these identified wires from the cable bundle

2S/624VB, as shown in Details A, C and F:

Wire number 2842-5052

Wire number 2842-5053

Wire number 2842-5054

Wire number 2842-5055

Wire number 2842-5056

Wire number 2842-5070

1 Sleeve ABS0596S004 Item 1

and attach the cable sleeve with:

1 Tie NSA935401-03 Item 149

1 Tie-Cable NSA935401-04 Item 150

and

1 Placard set B9299071900200 Item 125

as necessary.

(d) Install these items to the bracket of the rib 2, cable bundle 2S/624VB and cable

sleeve, Item 1, as shown in Details A and C:

1 Clamp MS21919WCH4 Item (22) Retained at

removal

1 Clamp MS21919WCH3 Item (23) Retained at

removal

1 Spacer NSA5527-03-02D Item (31) Retained at

removal

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 103

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@A310

SERVICE BULLETIN

1 Washer NAS1149D0332K Item (40) Retained at

removal

1 Screw NAS1096-3-21 Item (50) Retained at

removal

1 Clamp MS21919WCH10 Item (100) Retained at

removal

1 Clamp MS21919WCH13 Item 11

(e) Install these items to the riblet, cable bundle 2S/624VB and cable sleeve, Item 1,

as shown in Details A and E:

1 Clamp MS21919WCH4 Item (22) Retained at

removal

3 Spacer NSA5527-03-02D Item (31) Retained at

removal

1 Washer NAS1149D0332K Item (40) Retained at

removal

1 Screw NAS1096-3-38 Item (54) Retained at

removal

1 Clamp MS21919WCH13 Item 11

(6) Subtask 282148-831-209-003 - Install the cable sleeves in the RH-wing forward of

the front spar between rib 7 and rib 8 in zone 612.

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

Material necessary to do the job

Kit 282148D01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 ABS0596S004 2 SLEEVE

12 MS21919WCH14 CLAMP

149 NSA935401-03 2 TIE

150 NSA935401-04 2 TIE

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SERVICE BULLETIN

References

Fig. A-GBEAA

Improvement of the 2S-Route in the RHWing in Zone 612 (Kit D01)

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

Sheet 07

Sheet 08

NOTE (1): The sleeves ABS0596S004 is supplied in pieces of 1000 mm. Cut or

assemble these pieces to get the correct length.

NOTE (2): The lengths of the sleeves given in this Service Bulletin are approximate

lengths. Adapt the lengths of the sleeves in relation to the aircraft

configuration.

NOTE (3): Before you install a sleeve, cut and discard the cable ties around the

cable bundle to install the sleeve correctly around the cable bundle.

NOTE (4): Adapt the number of cable ties to the required quantity.

Refer to Fig. A-GBEAA Sheet 01, Fig. A-GBEAA Sheet 02, Fig. A-GBEAA Sheet 03, Fig.

A-GBEAA Sheet 04, Fig. A-GBEAA Sheet 05, Fig. A-GBEAA Sheet 06, Fig. A-GBEAA

Sheet 07 and Fig. A-GBEAA Sheet 08

(a) Remove these items from the two brackets of the riblets and cable bundle

2S/624VB, as shown in Details A, H and K:

2 Clamp MS21919WCH4 Item (22) Retain

2 Washer NAS1149D0332K Item (40) Retain

2 Screw NAS1096-3-8 Item (55) Retain

2 Clamp Item (100) Discard

(b) Install this cable sleeve around these identified wires from the cable bundle

2S/624VB, as shown in Details A, J, K, L, M and N:

Wire number 2842-5052

Wire number 2842-5053

Wire number 2842-5054

Wire number 2842-5055

Wire number 2842-5056

1 Sleeve ABS0596S004 Item 1

and attach the cable sleeves with:

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

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SERVICE BULLETIN

1 Tie NSA935401-03 Item 149

1 Tie-Cable NSA935401-04 Item 150

(c) Install this cable sleeve around this identified wire from the cable bundle 2S/624VB,

as shown in Details A, J, K, L, M and N:

Wire number 2842-5070

1 Sleeve ABS0596S004 Item 1

and attach the cable sleeves with:

1 Tie NSA935401-03 Item 149

1 Tie-Cable NSA935401-04 Item 150

(d) Install these items to the two brackets of the riblets, cable bundle 2S/624VB and

cable sleeves, Item 1, as shown in Detail A, J and L:

2 Clamp MS21919WCH4 Item (22) Retained at

removal

2 Washer NAS1149D0332K Item (40) Retained at

removal

2 Screw NAS1096-3-8 Item (55) Retained at

removal

2 Clamp MS21919WCH14 Item 12

(7) Subtask 282148-831-210-003 - Install the cable sleeves in the RH-wing forward of

the front spar between rib 8 and rib 9 (pylon area) in zone 612.

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

Material necessary to do the job

Kit 282148D05R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 ABS0596S004 3 SLEEVE

30 NSA5527-03-01D 2 SPACER

31 NSA5527-03-02D 1 SPACER

109 NSA935805-09 3 (ME) CONDUIT

117 NSA935807C09 12 CLAMP

126 NSA938184PV1601 15 PIN

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 106

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SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

135 NAS1096-3-42 1 SCREW

136 NAS1096-3-30 1 SCREW

149 NSA935401-03 30 TIE

150 NSA935401-04 30 TIE

References

Fig. A-GBJAA

Improvement of the 2S-Route in the RHWing Pylon Area (Kit D05)

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

Sheet 07

Sheet 08

Sheet 09

Fig. A-GHAAA

Hook-up Chart

Sheet 01

Fig. A-GHBAA

Hook-up Chart

Sheet 01

NOTE (1): The sleeves ABS0596S004 is supplied in pieces of 1000 mm. Cut or

assemble these pieces to get the correct length.

NOTE (2): The lengths of the sleeves given in this Service Bulletin are approximate

lengths. Adapt the lengths of the sleeves in relation to the aircraft

configuration.

NOTE (3): Before you install a sleeve, cut and discard the cable ties around the

cable bundle to install the sleeve correctly around the cable bundle.

NOTE (4): Adapt the number of cable ties to the required quantity.

Refer to Fig. A-GBJAA Sheet 01, Fig. A-GBJAA Sheet 02, Fig. A-GBJAA Sheet 03, Fig.

A-GBJAA Sheet 04, Fig. A-GBJAA Sheet 05, Fig. A-GBJAA Sheet 06, Fig. A-GBJAA

Sheet 07, Fig. A-GBJAA Sheet 08 and Fig. A-GBJAA Sheet 09

Refer to Fig. A-GHAAA Sheet 01 and Fig. A-GHBAA Sheet 01

(a) Disconnect these wires of route 2S from the receptacles 40VC and 5006VC in

accordance with the Hook-up Chart 1, Lines 1 thru 14, END 1, Fig. A-GHAAA

Sheet 01 and the Hook-up Chart 2, Lines 2 thru 8, END 1, Fig. A-GHBAA Sheet

01.

(b) Remove, refer to Fig. A-GBJAA Sheet 03, Detail C, BEFORE:

2 Spacer NSA5527-03-05D Item (30) Discard

1 Washer NSA935808-01 Item (112) Retain

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 107

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SERVICE BULLETIN

1 Nut NAS1291C3M Item (116) Retain

1 Clamp NSA935807C10 Item (117) Discard

1 Screw Item (136) Discard

(c) Remove, refer to Fig. A-GBJAA Sheet 04, Detail E, BEFORE:

1 Washer NSA935808-01 Item (112) Retain

1 Screw Item (113) Retain

1 Clamp NSA935807C10 Item (117) Discard

(d) Remove, refer to Fig. A-GBJAA Sheet 05, Detail G, BEFORE:

2 Washer NSA935808-01 Item (112) Retain

2 Screw Item (113) Retain

2 Clamp NSA935807C10 Item (117) Discard

(e) Remove, refer to Fig. A-GBJAA Sheet 06, Detail J, BEFORE:

1 Spacer NSA5527-03-05D Item (30) Discard

1 Washer NSA935808-01 Item (112) Retain

1 Clamp NSA935807C10 Item (117) Discard

1 Screw Item (135) Retain

(f) Remove, refer to Fig. A-GBJAA Sheet 07, Detail L, BEFORE:

1 Washer NSA935808-01 Item (112) Retain

1 Screw Item (113) Retain

1 Clamp NSA935807C10 Item (117) Discard

(g) Remove, refer to Fig. A-GBJAA Sheet 08, Detail N, BEFORE:

1 Washer NSA935808-01 Item (112) Retain

1 Screw Item (113) Retain

1 Clamp NSA935807C10 Item (117) Discard

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 108

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SERVICE BULLETIN

(h) Remove the protection sleeve from the cable harness as shown Fig. A-GBJAA

Sheet 01, Fig. A-GBJAA Sheet 02, Fig. A-GBJAA Sheet 03, Fig. A-GBJAA Sheet

04, Fig. A-GBJAA Sheet 05, Fig. A-GBJAA Sheet 06, Fig. A-GBJAA Sheet 07, Fig.

A-GBJAA Sheet 08 and Fig. A-GBJAA Sheet 09, Details A, C, E, G, J, L and N:

1 Sleeve NSA935805-10 Item (1) Discard

(i) Cut the conduit to the required length and install as shown Refer to Fig. A-GBJAA

Sheet 01, Fig. A-GBJAA Sheet 02, Fig. A-GBJAA Sheet 03, Fig. A-GBJAA Sheet

04, Fig. A-GBJAA Sheet 05, Fig. A-GBJAA Sheet 06, Fig. A-GBJAA Sheet 07, Fig.

A-GBJAA Sheet 08 and Fig. A-GBJAA Sheet 09, Details B, D, F, H, K, M, P and Q:

3 Sleeve ABS0596S004 Item 1

3 (ME) Conduit NSA935805-09 Item 109

1 One part 1500.0 mm (59.06 in.) to the electrical wires for 10QT-A and 10QT-B

of route 2S/636VB, refer to the Hook-up Chart 2, Fig. A-GHBAA Sheet 01

(j) Connect the electrical wires of route 2S to the receptacles 40VC and 5006VC in

accordance with the Hook-up Chart 1, Lines 1 thru 14, END 1, Fig. A-GHAAA

Sheet 01 and the Hook-up Chart 2, lines 2 thru 8, END 1, Fig. A-GHBAA Sheet 01.

Use the contact pins if required:

15 Pin NSA938184PV1601 Item 126

(k) Install, refer to Fig. A-GBJAA Sheet 08, Detail P, AFTER:

1 Washer NSA935808-01 Item (112) Retained at

removal

1 Screw Item (113) Retained at

removal

2 Clamp NSA935807C09 Item 117

(l) Install, refer to Fig. A-GBJAA Sheet 07, Detail M, AFTER:

1 Washer NSA935808-01 Item (112) Retained at

removal

1 Screw Item (113) Retained at

removal

2 Clamp NSA935807C09 Item 117

(m) Install, refer to Fig. A-GBJAA Sheet 06, Detail K, AFTER:

1 Spacer NSA5527-03-02D Item 31

1 Washer NSA935808-01 Item (112) Retained at

removal

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 109

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SERVICE BULLETIN

2 Clamp NSA935807C09 Item 117

1 Screw NAS1096-3-42 Item 135

(n) Install, refer to Fig. A-GBJAA Sheet 05, Detail H, AFTER:

2 Washer NSA935808-01 Item (112) Retained at

removal

2 Screw Item (113) Retained at

removal

4 Clamp NSA935807C09 Item 117

(o) Install, refer to Fig. A-GBJAA Sheet 04, Detail F, AFTER:

1 Washer NSA935808-01 Item (112) Retained at

removal

1 Screw Item (113) Retained at

removal

2 Clamp NSA935807C09 Item 117

(p) Install, refer to Fig. A-GBJAA Sheet 03, Detail D, AFTER:

2 Spacer NSA5527-03-01D Item 30

2 Washer NSA935808-01 Item (112) Retained at

removal

2 Nut NAS1291C3M Item (116) Retained at

removal

2 Clamp NSA935807C09 Item 117

1 Screw NAS1096-3-30 Item 136

(q) Protect the electrical wires for 10QT-A and 10QT-B of route 2S/636VB, refer to Fig.

A-GBJAA Sheet 09, Detail Q, and the Hook-up Chart 2, Fig. A-GHBAA Sheet 01

with:

30 Tie NSA935401-03 Item 149

30 Tie-Cable NSA935401-04 Item 150

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 110

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SERVICE BULLETIN

(8) Subtask 282148-831-211-003 - Install the cable sleeves in the RH-wing forward of

the front spar between rib 9 and rib 12 in zone 623.

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

Material necessary to do the job

Kit 282148D01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 ABS0596S004 3 SLEEVE

10 MS21919WCH9 CLAMP

14 NAS1096-3-19 2 SCREW

15 NSA5527-03-03 3 SPACER

16 NSA8420-2 1 (ME) CORD

149 NSA935401-03 10 TIE

150 NSA935401-04 20 TIE

Kit 282148D05R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

31 NSA5527-03-02D SPACER

135 NAS1096-3-42 SCREW

References

Fig. A-GBFAA

Improvement of the 2S-Route in the RHWing in Zone 623 (Kit D01)

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

Sheet 07

Sheet 08

Sheet 09

Sheet 10

NOTE (1): The sleeve ABS0596S004 is supplied in pieces of 1000 mm. Cut or

assemble these pieces to get the correct length.

NOTE (2): The lengths of the sleeves given in this Service Bulletin are approximate

lengths. Adapt the lengths of the sleeves in relation to the aircraft

configuration.

NOTE (3): Before you install a sleeve, cut and discard the cable ties around the

cable bundle to install the sleeve correctly around the cable bundle.

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 111

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SERVICE BULLETIN

NOTE (4): Adapt the number of cable ties to the required quantity.

Refer to Refer to Fig. A-GBFAA Sheet 01, Fig. A-GBFAA Sheet 02, Fig. A-GBFAA

Sheet 03, Fig. A-GBFAA Sheet 04, Fig. A-GBFAA Sheet 05, Fig. A-GBFAA Sheet 06,

Fig. A-GBFAA Sheet 07, Fig. A-GBFAA Sheet 08, Fig. A-GBFAA Sheet 09 and Fig. AGBFAA Sheet 10

(a) At one position, remove these items from the bracket between rib 11 and rib 12

and cable bundle 2S/636VB, as shown in Details A and D:

2 Clamp MS21919WCH4 Item (22) Retain

1 Clamp MS21919WCH4 Item (22) Discard

1 Clamp MS21919WCH3 Item (23) Retain

1 Spacer NSA5527-03-01D Item (30) Retain

1 Spacer NSA5527-03-02D Item (31) Retain

2 Washer NSA935808-01 Item (112) Retain

2 Screw NAS1096-3-30 Item (121) Discard

1 Clamp NSA935807-06 Item (122) Retain

(b) At two positions, remove these items from the brackets between rib 10 and rib 11

and between rib 11 and rib 12 and cable bundle 2S/636VB, as shown in Details A

and F:

2 Clamp Item (22) Discard

6 Clamp MS21919WCH4 Item (22) Retain

4 Spacer NSA5527-03-01D Item (30) Retain

2 Washer NAS1149D0332K Item (40) Retain

2 Screw NAS1096-3-27 Item (52) Retain

(c) At two positions, remove these items from the brackets of the rib 11 and cable

bundle 2S/636VB, as shown in Details A and H:

6 Clamp MS21919WCH4 Item (22) Retain

2 Clamp Item (23) Discard

2 Spacer NSA5527-03-01D Item (30) Retain

2 Spacer NSA5527-03-04D Item (32) Retain

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 112

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@A310

SERVICE BULLETIN

2 Washer NAS1149D0332K Item (40) Retain

2 Screw NAS1096-3-22 Item (51) Retain

(d) At two positions, remove these items from the brackets of the rib 10 and cable

bundle 2S/636VB, as shown in Details A and K:

2 Clamp Item (22) Discard

2 Clamp MS21919WCH4 Item (22) Retain

2 Spacer NSA5527-03-01D Item (30) Retain

2 Spacer Item (32) Discard

2 Washer NAS1149D0332K Item (40) Retain

2 Screw Item (51) Discard

(e) Remove these items from the bracket between rib 9 and rib 10 and cable bundle

2S/636VB, as shown in Details A and M:

3 Clamp MS21919WCH4 Item (22) Retain

1 Clamp Item (23) Discard

1 Spacer NSA5527-03-01D Item (30) Retain

1 Spacer NSA5527-03-04D Item (32) Retain

1 Washer NAS1149D0332K Item (40) Retain

1 Screw NAS1096-3-22 Item (51) Retain

(f) Remove these items from the bracket of the rib 9 and cable bundle 2S/636VB, as

shown in Details A and T:

1 Clamp Item (21) Discard

1 Clamp MS21919WCH5 Item (21) Retain

1 Spacer NSA5527-03-02D Item (31) Retain

1 Spacer NSA5527-03-04D Item (32) Retain

1 Washer NAS1149D0332K Item (40) Retain

1 Screw NAS1096-3-27 Item (52) Retain

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 113

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SERVICE BULLETIN

(g) Install this cable sleeve around these identified wires from the cable bundle

2S/636VB, as shown in Details A, C, E, G, J, L, N, Q and R:

Wire number 2842-5061

Wire number 2842-5062

Wire number 2842-5063

Wire number 2842-5064

Wire number 2842-5065

Wire number 2842-5071

3 Sleeve ABS0596S004 Item 1

and attach the cable sleeves with:

3 Spacer NSA5527-03-03 Item 15

1 (ME) Cord NSA8420-2 Item 16

10 Tie NSA935401-03 Item 149

20 Tie-Cable NSA935401-04 Item 150

(h) At one positions, install these items to the brackets between rib 10 and rib 11 and

between rib 11 and rib 12, cable sleeves, Item 1 and cable bundle 2S/636VB, as

shown in Details A and E:

2 Clamp MS21919WCH4 Item (22) Retained at

removal

1 Clamp MS21919WCH3 Item (23) Retained at

removal

1 Spacer NSA5527-03-01D Item (30) Retained at

removal

1 Spacer NSA5527-03-02D Item (31) Retained at

removal

1 Washer NSA935808-01 Item (112) Retained at

removal

1 Clamp NSA935807-06 Item (122) Retained at

removal

1 Clamp MS21919WCH9 Item 10

1 Spacer NSA5527-03-02D Item 31

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 114

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@A310

SERVICE BULLETIN

1 Screw NAS1096-3-42 Item 135

(i) At two positions, install these items to the brackets between rib 10 and rib 11 and

between rib 11 and rib 12, cable sleeves, Item 1 and cable bundle 2S/636VB, as

shown in Details A and G:

6 Clamp MS21919WCH4 Item (22) Retained at

removal

4 Spacer NSA5527-03-01D Item (30) Retained at

removal

2 Washer NAS1149D0332K Item (40) Retained at

removal

2 Screw NAS1096-3-27 Item (52) Retained at

removal

2 Clamp MS21919WCH9 Item 10

(j) At two positions, install these items to the brackets of the rib 11, cable sleeves,

Item 1 and cable bundle 2S/636VB, as shown in Details A and J:

2 Clamp MS21919WCH4 Item (22) Retained at

removal

1 Spacer NSA5527-03-01D Item (30) Retained at

removal

1 Spacer NSA5527-03-04D Item (32) Retained at

removal

1 Washer NAS1149D0332K Item (40) Retained at

removal

1 Screw NAS1096-3-22 Item (51) Retained at

removal

1 Clamp MS21919WCH9 Item 10

(k) At two positions, install these items to the brackets of the rib 10, cable sleeves,

Item 1 and cable bundle 2S/636VB, as shown in Details A and L:

2 Clamp MS21919WCH4 Item (22) Retained at

removal

2 Spacer NSA5527-03-01D Item (30) Retained at

removal

2 Washer NAS1149D0332K Item (40) Retained at

removal

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 115

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SERVICE BULLETIN

2 Clamp MS21919WCH9 Item 10

2 Screw NAS1096-3-19 Item 14

(l) Install these items to the bracket between rib 9 and rib 10, cable sleeves, Item 1

and cable bundle 2S/636VB, as shown in Details A and N:

3 Clamp MS21919WCH4 Item (22) Retained at

removal

1 Spacer NSA5527-03-01D Item (30) Retained at

removal

1 Spacer NSA5527-03-04D Item (32) Retained at

removal

1 Washer NAS1149D0332K Item (40) Retained at

removal

1 Screw NAS1096-3-22 Item (51) Retained at

removal

1 Clamp MS21919WCH9 Item 10

(m) Install these items to the bracket of the rib 9, cable sleeves, Item 1 and cable

bundle 2S/636VB, as shown in Details A and Q:

1 Clamp MS21919WCH5 Item (21) Retained at

removal

1 Spacer NSA5527-03-02D Item (31) Retained at

removal

1 Spacer NSA5527-03-04D Item (32) Retained at

removal

1 Washer NAS1149D0332K Item (40) Retained at

removal

1 Screw NAS1096-3-27 Item (52) Retained at

removal

1 Clamp MS21919WCH9 Item 10

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 116

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@A310

SERVICE BULLETIN

**CONF 004

(1) Subtask 282148-831-405-001 - Install a New Bracket on the Sub Spar Behind the

Front Spar Between RIB 8 and RIB 9 on the RH Wing

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills AIRFRAME

Material necessary to do the job

Kit 282148B01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 A5725068600000 1 Bracket

2 ASNA0078A502 2 Rivet

Consumable CMLB01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Corrosion Inhibiting Low

Adhesion Sealant

09-018 As required

Solvent General Purpose 11-026 As required

Lint-Free Cotton Cloth 19-003 As required

References

Fig. A-UBAAA

Location of Bracket on the Sub Spar

Behind the Front Spar Between RIB 8

and RIB 9 (RH Wing)

Sheet 01

Refer to Fig. A-UBAAA Sheet 01

(a) Remove from the sub spar behind the front spar between RIB 8 and RIB 9 on the

RH wing, the items that follow:

2 Rivet NSA54213510DCA Item (2) Discard

1 Bracket A5724630400000 Item (1) Discard

(b) Clean the mating surfaces use

Lint-Free Cotton

Cloth

19-003 As required

made moist with

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 117

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SERVICE BULLETIN

Solvent General

Purpose

11-026 As required

(c) Put the

1 Bracket A5725068600000 Item 1

in position on the sub spar behind the front spar between RIB 8 and RIB 9 on the

RH wing (Refer to Fig. A-UBAAA Sheet 01).

(d) Copy drill the two holes from the sub spar through the Bracket, Item 1 to a

dimension of between 4.060 and 4.160 mm (0.160 and 0.164 in.).

(e) Deburr the holes that have been worked.

(f) Use

Corrosion Inhibiting

Low Adhesion

Sealant

09-018 As required

and wet install the

1 Bracket A5725068600000 Item 1

with the

2 Rivet, Blind ASNA0078A502 Item 2

on the sub spar behind the front spar between RIB 8 and RIB 9 on the RH wing.

(2) Subtask 282148-831-004-001 - Install cable sleeves in the RH Electronics Rack

90VU.

Manpower Resources

Manhours 6.00

Minimum number of person 1

Subtask elapsed time 6.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 282148A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 ABS0596S004 2000 (mm) SLEEVE

NSA935401-04 50 TIE

References

Fig. A-FCAAA

Installation of Cable Sleeves in the RH

Electronics Rack 90VU.

Sheet 01

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 118

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SERVICE BULLETIN

References

Fig. A-FWAAA

Installation of Cable Sleeves in the RH

Electronics Rack 90VU.

Sheet 01

NOTE: The sleeves ABS0596S004 and ABS0596S006 are supplied in pieces of

1000 mm (39.370 inches), cut or assemble these pieces to get the

correct length.

NOTE: The lengths of the sleeves given in this Service Bulletin are approximate

lengths. Adapt the lengths of the sleeves in relation to the aircraft

configuration.

NOTE: Before you install a sleeve, cut and discard the cable ties around the

cable bundle to install the sleeve correctly around the cable bundle.

(a) On the Shelf 92VU, only around the wires identified in figure Fig. A-FWAAA Sheet

01, from the equipment 15QT-B to the connector 2354VC, install:

1600 (mm) Sleeve ABS0596S004 Item 1

(b) Around the cable bundle of the connector 2354VC-A, install:

400 (mm) Sleeve ABS0596S004 Item 1

(c) Attach the sleeves with:

50 Tie-Cable NSA935401-04

(3) Subtask 282148-831-005-001 - Install cable sleeves between FR38.2 and FR39, in

the forward cargo compartment.

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 282148A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

2 ABS0596S006 1000 (mm) SLEEVE

NSA935401-05 50 TIE

References

Fig. A-FCBAA

Installation of Cable Sleeves in the

Forward Cargo Compartment.

Sheet 01

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 119

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SERVICE BULLETIN

NOTE: The sleeves ABS0596S004 and ABS0596S006 are supplied in pieces of

1000 mm (39.370 inches), cut or assemble these pieces to get the

correct length.

NOTE: The lengths of the sleeves given in this Service Bulletin are approximate

lengths. Adapt the lengths of the sleeves in relation to the aircraft

configuration.

NOTE: Before you install a sleeve, cut and discard the cable ties around the

cable bundle to install the sleeve correctly around the cable bundle.

(a) Around the cable bundle of the pressure seal 20VP, install:

1000 (mm) Sleeve ABS0596S006 Item 2

(b) Attach the sleeves with:

50 Tie-Cable NSA935401-05

(4) Subtask 282148-831-006-001 - Install cable sleeves in the RH forward wing root

and krueger flap.

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 282148A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

2 ABS0596S006 1000 (mm) SLEEVE

NSA935401-05 50 TIE

References

Fig. A-FCCAA

Installation of Cable Sleeves in the RH

forward wing root and krueger flap.

Sheet 01

(a) Around the cable bundle of the pressure seal 20VP, install:

1000 (mm) Sleeve ABS0596S006 Item 2

(b) Attach the sleeves with:

50 Tie-Cable NSA935401-05

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 120

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SERVICE BULLETIN

(5) Subtask 282148-831-208-004 - Install the cable sleeves in the RH-wing forward of

the front spar between rib 2 and rib 3 in zone 612.

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

Material necessary to do the job

Kit 282148D01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 ABS0596S004 1 SLEEVE

11 MS21919WCH13 CLAMP

149 NSA935401-03 1 TIE

150 NSA935401-04 1 TIE

Kit 282148D06R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

132 B9299071900600 1 EQUIPMNT

References

Fig. A-GBEAA

Improvement of the 2S-Route in the RHWing in Zone 612 (Kit D01)

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

Sheet 07

Sheet 08

NOTE (1): The sleeves ABS0596S004 is supplied in pieces of 1000 mm. Cut or

assemble these pieces to get the correct length.

NOTE (2): The lengths of the sleeves given in this Service Bulletin are approximate

lengths. Adapt the lengths of the sleeves in relation to the aircraft

configuration.

NOTE (3): Before you install a sleeve, cut and discard the cable ties around the

cable bundle to install the sleeve correctly around the cable bundle.

NOTE (4): Adapt the number of cable ties to the required quantity.

Refer to Fig. A-GBEAA Sheet 01, Fig. A-GBEAA Sheet 02, Fig. A-GBEAA Sheet 03, Fig.

A-GBEAA Sheet 04, Fig. A-GBEAA Sheet 05, Fig. A-GBEAA Sheet 06, Fig. A-GBEAA

Sheet 07 and Fig. A-GBEAA Sheet 08

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 121

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SERVICE BULLETIN

(a) Remove these items from the bracket of the rib 2 and cable bundle 2S/624VB, as

shown in Details A and B:

1 Clamp MS21919WCH4 Item (22) Retain

1 Clamp MS21919WCH3 Item (23) Retain

1 Spacer NSA5527-03-02D Item (31) Retain

1 Washer NAS1149D0332K Item (40) Retain

1 Screw NAS1096-3-21 Item (50) Retain

1 Clamp MS21919WCH10 Item (100) Retain

1 Clamp Item (100) Discard

(b) Remove these items from the riblet and cable bundle 2S/624VB, as shown in

Details A and D:

1 Clamp MS21919WCH4 Item (22) Retain

3 Spacer NSA5527-03-02D Item (31) Retain

1 Washer NAS1149D0332K Item (40) Retain

1 Screw NAS1096-3-38 Item (54) Retain

1 Clamp Item (100) Discard

(c) Install this cable sleeve around these identified wires from the cable bundle

2S/624VB, as shown in Details A, C, E and F:

Wire number 2842-5052

Wire number 2842-5053

Wire number 2842-5054

Wire number 2842-5055

Wire number 2842-5056

Wire number 2842-5070

1 Sleeve ABS0596S004 Item 1

and attach the cable sleeve with:

1 Tie NSA935401-03 Item 149

1 Tie-Cable NSA935401-04 Item 150

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 122

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SERVICE BULLETIN

and

1 Placard Set B9299071900600 Item 132

as necessary.

(d) Install these items to the bracket of the rib 2, cable bundle 2S/624VB and cable

sleeve, Item 1, as shown in Details A and C:

1 Clamp MS21919WCH4 Item (22) Retained at

removal

1 Clamp MS21919WCH3 Item (23) Retained at

removal

1 Spacer NSA5527-03-02D Item (31) Retained at

removal

1 Washer NAS1149D0332K Item (40) Retained at

removal

1 Screw NAS1096-3-21 Item (50) Retained at

removal

1 Clamp MS21919WCH10 Item (100) Retained at

removal

1 Clamp MS21919WCH13 Item 11

(e) Install these items to the riblet, cable bundle 2S/624VB and cable sleeve, Item 1,

as shown in Details A and E:

1 Clamp MS21919WCH4 Item (22) Retained at

removal

3 Spacer NSA5527-03-02D Item (31) Retained at

removal

1 Washer NAS1149D0332K Item (40) Retained at

removal

1 Screw NAS1096-3-38 Item (54) Retained at

removal

1 Clamp MS21919WCH13 Item 11

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 123

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@A310

SERVICE BULLETIN

(6) Subtask 282148-831-209-004 - Install the cable sleeves in the RH-wing forward of

the front spar between rib 7 and rib 8 in zone 612.

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

Material necessary to do the job

Kit 282148D01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 ABS0596S004 2 SLEEVE

12 MS21919WCH14 CLAMP

149 NSA935401-03 2 TIE

150 NSA935401-04 2 TIE

References

Fig. A-GBEAA

Improvement of the 2S-Route in the RHWing in Zone 612 (Kit D01)

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

Sheet 07

Sheet 08

NOTE (1): The sleeves ABS0596S004 is supplied in pieces of 1000 mm. Cut or

assemble these pieces to get the correct length.

NOTE (2): The lengths of the sleeves given in this Service Bulletin are approximate

lengths. Adapt the lengths of the sleeves in relation to the aircraft

configuration.

NOTE (3): Before you install a sleeve, cut and discard the cable ties around the

cable bundle to install the sleeve correctly around the cable bundle.

NOTE (4): Adapt the number of cable ties to the required quantity.

Refer to Fig. A-GBEAA Sheet 01, Fig. A-GBEAA Sheet 02, Fig. A-GBEAA Sheet 03, Fig.

A-GBEAA Sheet 04, Fig. A-GBEAA Sheet 05, Fig. A-GBEAA Sheet 06, Fig. A-GBEAA

Sheet 07 and Fig. A-GBEAA Sheet 08

(a) Remove these items from the two brackets of the riblets and cable bundle

2S/624VB, as shown in Details A, H and K:

2 Clamp MS21919WCH4 Item (22) Retain

2 Washer NAS1149D0332K Item (40) Retain

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 124

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SERVICE BULLETIN

2 Screw NAS1096-3-8 Item (55) Retain

2 Clamp Item (100) Discard

(b) Install this cable sleeve around these identified wires from the cable bundle

2S/624VB, as shown in Details A, J, K, L, M and N:

Wire number 2842-5052

Wire number 2842-5053

Wire number 2842-5054

Wire number 2842-5055

Wire number 2842-5056

1 Sleeve ABS0596S004 Item 1

and attach the cable sleeves with:

1 Tie NSA935401-03 Item 149

1 Tie-Cable NSA935401-04 Item 150

(c) Install this cable sleeve around this identified wire from the cable bundle 2S/624VB,

as shown in Details A, J, K, L, M and N:

Wire number 2842-5070

1 Sleeve ABS0596S004 Item 1

and attach the cable sleeves with:

1 Tie NSA935401-03 Item 149

1 Tie-Cable NSA935401-04 Item 150

(d) Install these items to the two brackets of the riblets, cable bundle 2S/624VB and

cable sleeves, Item 1, as shown in Detail A, J and L:

2 Clamp MS21919WCH4 Item (22) Retained at

removal

2 Washer NAS1149D0332K Item (40) Retained at

removal

2 Screw NAS1096-3-8 Item (55) Retained at

removal

2 Clamp MS21919WCH14 Item 12

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 125

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SERVICE BULLETIN

(7) Subtask 282148-831-210-004 - Install the cable sleeves in the RH-wing forward of

the front spar between rib 8 and rib 9 (pylon area) in zone 612.

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

Material necessary to do the job

Kit 282148D06R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 ABS0596S004 3 SLEEVE

31 NSA5527-03-02D 2 SPACER

109 NSA935805-09 1.5 (ME) CONDUIT

117 NSA935807C09 7 CLAMP

121 NAS1096-3-40 1 SCREW

123 NAS1801-3-31 2 SCREW

126 NSA938184PV1601 7 PIN

130 NSA5527-03-08D 1 SPACER

131 NSA5527-03-07D 1 SPACER

149 NSA935401-03 30 TIE

150 NSA935401-04 30 TIE

References

Fig. A-GBKAA

Improvement of the 2S-Route in the RHWing Pylon Area (Kit D06)

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

Sheet 07

Sheet 08

Sheet 09

Fig. A-GHBAA

Hook-up Chart

Sheet 01

NOTE (1): The sleeves ABS0596S004 is supplied in pieces of 1000 mm. Cut or

assemble these pieces to get the correct length.

NOTE (2): The lengths of the sleeves given in this Service Bulletin are approximate

lengths. Adapt the lengths of the sleeves in relation to the aircraft

configuration.

NOTE (3): Before you install a sleeve, cut and discard the cable ties around the

cable bundle to install the sleeve correctly around the cable bundle.

NOTE (4): Adapt the number of cable ties to the required quantity.

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 126

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SERVICE BULLETIN

Refer to Fig. A-GBKAA Sheet 01, Fig. A-GBKAA Sheet 02, Fig. A-GBKAA Sheet 03, Fig.

A-GBKAA Sheet 04, Fig. A-GBKAA Sheet 05, Fig. A-GBKAA Sheet 06, Fig. A-GBKAA

Sheet 07, Fig. A-GBKAA Sheet 08 and Fig. A-GBKAA Sheet 09

Refer to Fig. A-GHBAA Sheet 01

(a) Disconnect the wires of route 2S from the receptacles 40VC and 5006VC in

accordance with the Hook-up Chart 2, Lines 2 thru 8, END 1, Fig. A-GHBAA Sheet

01.

(b) Remove, refer to Fig. A-GBKAA Sheet 03, Detail C, BEFORE:

1 Washer NSA935808-01 Item (112) Retain

1 Screw NAS1096-3-23 Item (113) Retain

1 Nut NAS1291C3M Item (116) Retain

1 Washer AN960KD10l Item (124) Retain

(c) Remove, refer to Fig. A-GBKAA Sheet 04, Detail E, BEFORE:

1 Washer NSA935808-01 Item (112) Retain

1 Screw NAS1096-3-23 Item (113) Retain

(d) Remove, refer to Fig. A-GBKAA Sheet 05, Detail G, BEFORE:

2 Washer NSA935808-01 Item (112) Retain

2 Screw NAS1096-3-23 Item (113) Retain

(e) Remove, refer to Fig. A-GBKAA Sheet 06, Detail J, BEFORE:

1 Spacer NSA5527-03-02D Item (31) Retain

1 Screw Item (121) Discard

(f) Remove, refer to Fig. A-GBKAA Sheet 07, Detail L, BEFORE:

1 Screw Item (123) Discard

(g) Remove, refer to Fig. A-GBKAA Sheet 08, Detail N, BEFORE:

1 Screw Item (123) Discard

(h) Cut the conduit to the required length and install as shown Fig. A-GBKAA Sheet

01, Fig. A-GBKAA Sheet 02, Fig. A-GBKAA Sheet 03, Fig. A-GBKAA Sheet 04,

Fig. A-GBKAA Sheet 05, Fig. A-GBKAA Sheet 06, Fig. A-GBKAA Sheet 07, Fig. AGBKAA Sheet 08 and Fig. A-GBKAA Sheet 09, Details B and R:

3 Sleeve ABS0596S004 Item 1

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 127

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SERVICE BULLETIN

1.5 (ME) Conduit NSA935805-09 Item 109

1 One part 1500.0 mm (59.06 in.) to the electrical wires for 10QT-A and 10QT-B

of route 2S/636VB, refer to the Hook-up Chart 2, Fig. A-GHBAA Sheet 01

(i) Connect the electrical wires of route 2S to the receptacles 40VC and 5006VC in

accordance with the Hook-up Chart 2, Lines 2 thru 8, END 1, Fig. A-GHBAA Sheet

01. Use the contact pins if required:

7 Pin NSA938184PV1601 Item 126

(j) Install, refer to Fig. A-GBKAA Sheet 08, Detail P, AFTER:

1 Spacer NSA5527-03-02D Item 31

1 Clamp NSA935807C09 Item 117

1 Screw NAS1801-3-31 Item 123

1 Spacer NSA5527-03-07D Item 131

(k) Install, refer to Fig. A-GBKAA Sheet 07, Detail M, AFTER:

1 Clamp NSA935807C09 Item 117

1 Screw NAS1801-3-31 Item 123

1 Spacer NSA5527-03-08D Item 130

(l) Install, refer to Fig. A-GBKAA Sheet 06, Detail K, AFTER:

1 Spacer NSA5527-03-02D Item 31

1 Clamp NSA935807C09 Item 117

1 Screw NAS1096-3-40 Item 121

(m) Install, refer to Fig. A-GBKAA Sheet 05, Detail H, AFTER:

2 Washer NSA935808-01 Item (112) Retained at

removal

2 Screw NAS1096-3-23 Item (113) Retained at

removal

2 Clamp NSA935807C09 Item 117

(n) Install, refer to Fig. A-GBKAA Sheet 04, Detail F, AFTER:

1 Washer NSA935808-01 Item (112) Retained at

removal

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 128

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SERVICE BULLETIN

1 Screw NAS1096-3-23 Item (113) Retained at

removal

1 Clamp NSA935807C09 Item 117

(o) Install, refer to Fig. A-GBKAA Sheet 03, Detail D, AFTER:

1 Washer NSA935808-01 Item (112) Retained at

removal

1 Screw NAS1096-3-23 Item (113) Retained at

removal

1 Nut NAS1291C3M Item (116) Retained at

removal

1 Washer AN960KD10l Item (124) Retained at

removal

1 Clamp NSA935807C09 Item 117

(p) Protect the electrical wires for 10QT-A and 10QT-B of route 2S/636VB, refer to the

Hook-up Chart 2, Fig. A-GHBAA Sheet 01 and Fig. A-GBKAA Sheet 01, Fig. AGBKAA Sheet 02, Fig. A-GBKAA Sheet 03, Fig. A-GBKAA Sheet 04, Fig. AGBKAA Sheet 05, Fig. A-GBKAA Sheet 06, Fig. A-GBKAA Sheet 07, Fig. AGBKAA Sheet 08 and Fig. A-GBKAA Sheet 09, Detail Q with:

30 Tie NSA935401-03 Item 149

30 Tie-Cable NSA935401-04 Item 150

(8) Subtask 282148-831-211-004 - Install the cable sleeves in the RH-wing forward of

the front spar between rib 9 and rib 12 in zone 623.

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

Material necessary to do the job

Kit 282148D01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 ABS0596S004 3 SLEEVE

10 MS21919WCH9 CLAMP

14 NAS1096-3-19 SCREW

15 NSA5527-03-03 SPACER

16 NSA8420-2 CORD

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 129

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SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

150 NSA935401-04 1 TIE

Kit 282148D06R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

31 NSA5527-03-02D 2 SPACER

121 NAS1096-3-40 1 SCREW

References

Fig. A-GBFAA

Improvement of the 2S-Route in the RHWing in Zone 623 (Kit D01)

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

Sheet 07

Sheet 08

Sheet 09

Sheet 10

NOTE (1): The sleeve ABS0596S004 is supplied in pieces of 1000 mm. Cut or

assemble these pieces to get the correct length.

NOTE (2): The lengths of the sleeves given in this Service Bulletin are approximate

lengths. Adapt the lengths of the sleeves in relation to the aircraft

configuration.

NOTE (3): Before you install a sleeve, cut and discard the cable ties around the

cable bundle to install the sleeve correctly around the cable bundle.

NOTE (4): Adapt the number of cable ties to the required quantity.

Refer to Refer to Fig. A-GBFAA Sheet 01, Fig. A-GBFAA Sheet 02, Fig. A-GBFAA

Sheet 03, Fig. A-GBFAA Sheet 04, Fig. A-GBFAA Sheet 05, Fig. A-GBFAA Sheet 06,

Fig. A-GBFAA Sheet 07, Fig. A-GBFAA Sheet 08, Fig. A-GBFAA Sheet 09 and Fig. AGBFAA Sheet 10

(a) At one position, remove these items from the bracket between rib 11 and rib 12

and cable bundle 2S/636VB, as shown in Details A and D:

2 Clamp MS21919WCH4 Item (22) Retain

1 Clamp MS21919WCH4 Item (22) Discard

1 Clamp MS21919WCH3 Item (23) Retain

1 Spacer NSA5527-03-01D Item (30) Retain

1 Spacer NSA5527-03-02D Item (31) Retain

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 130

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@A310

SERVICE BULLETIN

1 Washer NSA935808-01 Item (112) Retain

1 Screw NAS1096-3-30 Item (121) Discard

1 Clamp NSA935807-06 Item (122) Retain

(b) At two positions, remove these items from the brackets between rib 10 and rib 11

and between rib 11 and rib 12 and cable bundle 2S/636VB, as shown in Details A

and F:

2 Clamp Item (22) Discard

6 Clamp MS21919WCH4 Item (22) Retain

4 Spacer NSA5527-03-01D Item (30) Retain

2 Washer NAS1149D0332K Item (40) Retain

2 Screw NAS1096-3-27 Item (52) Retain

(c) At two positions, remove these items from the brackets of the rib 11 and cable

bundle 2S/636VB, as shown in Details A and H:

6 Clamp MS21919WCH4 Item (22) Retain

2 Clamp Item (23) Discard

2 Spacer NSA5527-03-01D Item (30) Retain

2 Spacer NSA5527-03-04D Item (32) Retain

2 Washer NAS1149D0332K Item (40) Retain

2 Screw NAS1096-3-22 Item (51) Retain

(d) At two positions, remove these items from the brackets of the rib 10 and cable

bundle 2S/636VB, as shown in Details A and K:

2 Clamp Item (22) Discard

2 Clamp MS21919WCH4 Item (22) Retain

2 Spacer NSA5527-03-01D Item (30) Retain

2 Spacer Item (32) Discard

2 Washer NAS1149D0332K Item (40) Retain

2 Screw Item (51) Discard

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 131

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SERVICE BULLETIN

(e) Remove these items from the bracket between rib 9 and rib 10 and cable bundle

2S/636VB, as shown in Details A and M:

3 Clamp MS21919WCH4 Item (22) Retain

1 Clamp Item (23) Discard

1 Spacer NSA5527-03-01D Item (30) Retain

1 Spacer NSA5527-03-04D Item (32) Retain

1 Washer NAS1149D0332K Item (40) Retain

1 Screw NAS1096-3-22 Item (51) Retain

(f) Remove these items from the bracket of the rib 9 and cable bundle 2S/636VB, as

shown in Details A and T:

1 Clamp Item (21) Discard

1 Clamp MS21919WCH5 Item (21) Retain

1 Spacer NSA5527-03-02D Item (31) Retain

1 Spacer NSA5527-03-04D Item (32) Retain

1 Washer NAS1149D0332K Item (40) Retain

1 Screw NAS1096-3-27 Item (52) Retain

(g) Install this cable sleeve around these identified wires from the cable bundle

2S/636VB, as shown in Details A, C, E, G, J, L, N and R:

Wire number 2842-5061

Wire number 2842-5062

Wire number 2842-5063

Wire number 2842-5064

Wire number 2842-5065

Wire number 2842-5071

3 Sleeve ABS0596S004 Item 1

and attach the cable sleeves with:

3 Spacer NSA5527-03-03 Item 15

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 132

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SERVICE BULLETIN

1 (ME) Cord NSA8420-2 Item 16

1 Tie-Cable NSA935401-04 Item 150

(h) At one positions, install these items to the brackets between rib 10 and rib 11 and

between rib 11 and rib 12, cable sleeves, Item 1 and cable bundle 2S/636VB, as

shown in Details A and E:

2 Clamp MS21919WCH4 Item (22) Retained at

removal

1 Clamp MS21919WCH3 Item (23) Retained at

removal

1 Spacer NSA5527-03-01D Item (30) Retained at

removal

1 Spacer NSA5527-03-02D Item (31) Retained at

removal

1 Washer NSA935808-01 Item (112) Retained at

removal

1 Clamp NSA935807-06 Item (122) Retained at

removal

1 Clamp MS21919WCH9 Item 10

2 Spacer NSA5527-03-02D Item 31

1 Screw NAS1096-3-40 Item 121

(i) At two positions, install these items to the brackets between rib 10 and rib 11 and

between rib 11 and rib 12, cable sleeves, Item 1 and cable bundle 2S/636VB, as

shown in Details A and G:

6 Clamp MS21919WCH4 Item (22) Retained at

removal

4 Spacer NSA5527-03-01D Item (30) Retained at

removal

2 Washer NAS1149D0332K Item (40) Retained at

removal

2 Screw NAS1096-3-27 Item (52) Retained at

removal

2 Clamp MS21919WCH9 Item 10

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 133

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SERVICE BULLETIN

(j) At two positions, install these items to the brackets of the rib 11, cable sleeves,

Item 1 and cable bundle 2S/636VB, as shown in Details A and J:

2 Clamp MS21919WCH4 Item (22) Retained at

removal

1 Spacer NSA5527-03-01D Item (30) Retained at

removal

1 Spacer NSA5527-03-04D Item (32) Retained at

removal

1 Washer NAS1149D0332K Item (40) Retained at

removal

1 Screw NAS1096-3-22 Item (51) Retained at

removal

1 Clamp MS21919WCH9 Item 10

(k) At two positions, install these items to the brackets of the rib 10, cable sleeves,

Item 1 and cable bundle 2S/636VB, as shown in Details A and L:

2 Clamp MS21919WCH4 Item (22) Retained at

removal

2 Spacer NSA5527-03-01D Item (30) Retained at

removal

2 Washer NAS1149D0332K Item (40) Retained at

removal

2 Clamp MS21919WCH9 Item 10

2 Screw NAS1096-3-19 Item 14

(l) Install these items to the bracket between rib 9 and rib 10, cable sleeves, Item 1

and cable bundle 2S/636VB, as shown in Details A and Q:

3 Clamp MS21919WCH4 Item (22) Retained at

removal

1 Spacer NSA5527-03-01D Item (30) Retained at

removal

1 Spacer NSA5527-03-04D Item (32) Retained at

removal

1 Washer NAS1149D0332K Item (40) Retained at

removal

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 134

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SERVICE BULLETIN

1 Screw NAS1096-3-22 Item (51) Retained at

removal

1 Clamp MS21919WCH9 Item 10

(m) Install these items to the bracket of the rib 9, cable sleeves, Item 1 and cable

bundle 2S/636VB, as shown in Details A and Q:

1 Clamp MS21919WCH5 Item (21) Retained at

removal

1 Spacer NSA5527-03-02D Item (31) Retained at

removal

1 Spacer NSA5527-03-04D Item (32) Retained at

removal

1 Washer NAS1149D0332K Item (40) Retained at

removal

1 Screw NAS1096-3-27 Item (52) Retained at

removal

1 Clamp MS21919WCH9 Item 10

**CONF 005

(1) Subtask 282148-831-405-001 - Install a New Bracket on the Sub Spar Behind the

Front Spar Between RIB 8 and RIB 9 on the RH Wing

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills AIRFRAME

Material necessary to do the job

Kit 282148B01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 A5725068600000 1 Bracket

2 ASNA0078A502 2 Rivet

Consumable CMLB01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Corrosion Inhibiting Low

Adhesion Sealant

09-018 As required

Solvent General Purpose 11-026 As required

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 135

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SERVICE BULLETIN

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Lint-Free Cotton Cloth 19-003 As required

References

Fig. A-UBAAA

Location of Bracket on the Sub Spar

Behind the Front Spar Between RIB 8

and RIB 9 (RH Wing)

Sheet 01

Refer to Fig. A-UBAAA Sheet 01

(a) Remove from the sub spar behind the front spar between RIB 8 and RIB 9 on the

RH wing, the items that follow:

2 Rivet NSA54213510DCA Item (2) Discard

1 Bracket A5724630400000 Item (1) Discard

(b) Clean the mating surfaces use

Lint-Free Cotton

Cloth

19-003 As required

made moist with

Solvent General

Purpose

11-026 As required

(c) Put the

1 Bracket A5725068600000 Item 1

in position on the sub spar behind the front spar between RIB 8 and RIB 9 on the

RH wing (Refer to Fig. A-UBAAA Sheet 01).

(d) Copy drill the two holes from the sub spar through the Bracket, Item 1 to a

dimension of between 4.060 and 4.160 mm (0.160 and 0.164 in.).

(e) Deburr the holes that have been worked.

(f) Use

Corrosion Inhibiting

Low Adhesion

Sealant

09-018 As required

and wet install the

1 Bracket A5725068600000 Item 1

with the

2 Rivet, Blind ASNA0078A502 Item 2

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 136

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SERVICE BULLETIN

on the sub spar behind the front spar between RIB 8 and RIB 9 on the RH wing.

(2) Subtask 282148-831-004-001 - Install cable sleeves in the RH Electronics Rack

90VU.

Manpower Resources

Manhours 6.00

Minimum number of person 1

Subtask elapsed time 6.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 282148A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 ABS0596S004 2000 (mm) SLEEVE

NSA935401-04 50 TIE

References

Fig. A-FCAAA

Installation of Cable Sleeves in the RH

Electronics Rack 90VU.

Sheet 01

Fig. A-FWAAA

Installation of Cable Sleeves in the RH

Electronics Rack 90VU.

Sheet 01

NOTE: The sleeves ABS0596S004 and ABS0596S006 are supplied in pieces of

1000 mm (39.370 inches), cut or assemble these pieces to get the

correct length.

NOTE: The lengths of the sleeves given in this Service Bulletin are approximate

lengths. Adapt the lengths of the sleeves in relation to the aircraft

configuration.

NOTE: Before you install a sleeve, cut and discard the cable ties around the

cable bundle to install the sleeve correctly around the cable bundle.

(a) On the Shelf 92VU, only around the wires identified in figure Fig. A-FWAAA Sheet

01, from the equipment 15QT-B to the connector 2354VC, install:

1600 (mm) Sleeve ABS0596S004 Item 1

(b) Around the cable bundle of the connector 2354VC-A, install:

400 (mm) Sleeve ABS0596S004 Item 1

(c) Attach the sleeves with:

50 Tie-Cable NSA935401-04

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 137

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SERVICE BULLETIN

(3) Subtask 282148-831-005-001 - Install cable sleeves between FR38.2 and FR39, in

the forward cargo compartment.

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 282148A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

2 ABS0596S006 1000 (mm) SLEEVE

NSA935401-05 50 TIE

References

Fig. A-FCBAA

Installation of Cable Sleeves in the

Forward Cargo Compartment.

Sheet 01

NOTE: The sleeves ABS0596S004 and ABS0596S006 are supplied in pieces of

1000 mm (39.370 inches), cut or assemble these pieces to get the

correct length.

NOTE: The lengths of the sleeves given in this Service Bulletin are approximate

lengths. Adapt the lengths of the sleeves in relation to the aircraft

configuration.

NOTE: Before you install a sleeve, cut and discard the cable ties around the

cable bundle to install the sleeve correctly around the cable bundle.

(a) Around the cable bundle of the pressure seal 20VP, install:

1000 (mm) Sleeve ABS0596S006 Item 2

(b) Attach the sleeves with:

50 Tie-Cable NSA935401-05

(4) Subtask 282148-831-006-002 - Install cable sleeves in the RH forward wing root

and krueger flap.

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills NON SPECIFIC

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 138

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SERVICE BULLETIN

Material necessary to do the job

Kit 282148A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

2 ABS0596S006 SLEEVE

NSA935401-05 TIE

References

Fig. A-FCCAB

Installation of Cable Sleeves in the RH

forward wing root and krueger flap.

Sheet 01

NOTE: The sleeves ABS0596S004 and ABS0596S006 are supplied in pieces of

1000 mm (39.370 inches), cut or assemble these pieces to get the

correct length.

NOTE: The lengths of the sleeves given in this Service Bulletin are approximate

lengths. Adapt the lengths of the sleeves in relation to the aircraft

configuration.

NOTE: Before you install a sleeve, cut and discard the cable ties around the

cable bundle to install the sleeve correctly around the cable bundle.

(a) Around the cable bundle of the pressure seal 20VP, install:

1000 (mm) Sleeve ABS0596S006 Item 2

(b) Attach the sleeves with:

50 Tie-Cable NSA935401-05

(5) Subtask 282148-831-208-001 - Install the cable sleeves in the RH-wing forward of

the front spar between rib 2 and rib 3 in zone 612.

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills ELECTRICAL

Material necessary to do the job

Kit 282148D01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 ABS0596S004 1 SLEEVE

11 MS21919WCH13 2 CLAMP

149 NSA935401-03 1 TIE

150 NSA935401-04 1 TIE

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 139

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SERVICE BULLETIN

References

Fig. A-GBEAA

Improvement of the 2S-Route in the RHWing in Zone 612 (Kit D01)

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

Sheet 07

Sheet 08

NOTE (1): The sleeve ABS0596S004 is supplied in pieces of 1000 mm. Cut or

assemble these pieces to get the correct length.

NOTE (2): The lengths of the sleeves given in this Service Bulletin are approximate

lengths. Adapt the lengths of the sleeves in relation to the aircraft

configuration.

NOTE (3): Before you install a sleeve, cut and discard the cable ties around the

cable bundle to install the sleeve correctly around the cable bundle.

NOTE (4): Adapt the number of cable ties to the required quantity.

Install the cable sleeves in the RH-wing forward of the front spar between rib 2 and rib 3

in zone 612.

Refer to Fig. A-GBEAA Sheet 01, Fig. A-GBEAA Sheet 02, Fig. A-GBEAA Sheet 03, Fig.

A-GBEAA Sheet 04, Fig. A-GBEAA Sheet 05, Fig. A-GBEAA Sheet 06, Fig. A-GBEAA

Sheet 07 and Fig. A-GBEAA Sheet 08

(a) Remove these items from the bracket of the rib 2 and cable bundle 2S/624VB, as

shown in Details A and B:

1 Clamp MS21919WCH4 Item (22) Retain

1 Clamp MS21919WCH3 Item (23) Retain

1 Spacer NSA5527-03-02D Item (31) Retain

1 Washer NAS1149D0332K Item (40) Retain

1 Screw NAS1096-3-21 Item (50) Retain

1 Clamp MS21919WCH10 Item (100) Retain

1 Clamp Item (100) Discard

(b) Remove these items from the riblet and cable bundle 2S/624VB, as shown in

Details A and D:

1 Clamp MS21919WCH4 Item (22) Retain

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 140

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SERVICE BULLETIN

3 Spacer NSA5527-03-02D Item (31) Retain

1 Washer NAS1149D0332K Item (40) Retain

1 Screw NAS1096-3-38 Item (54) Retain

1 Clamp Item (100) Discard

(c) Install this cable sleeve around these identified wires from the cable bundle

2S/624VB, as shown in Details A, C, E and F:

Wire number 2842-5052

Wire number 2842-5053

Wire number 2842-5054

Wire number 2842-5055

Wire number 2842-5056

Wire number 2842-5070

1 Sleeve ABS0596S004 Item 1

and attach the cable sleeve with:

1 Tie NSA935401-03 Item 149

1 Tie-Cable NSA935401-04 Item 150

as necessary.

(d) Install these items to the bracket of the rib 2, cable bundle 2S/624VB and cable

sleeve, Item 1, as shown in Details A and C:

1 Clamp MS21919WCH4 Item (22) Retained at

removal

1 Clamp MS21919WCH3 Item (23) Retained at

removal

1 Spacer NSA5527-03-02D Item (31) Retained at

removal

1 Washer NAS1149D0332K Item (40) Retained at

removal

1 Screw NAS1096-3-21 Item (50) Retained at

removal

1 Clamp MS21919WCH10 Item (100) Retained at

removal

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 141

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SERVICE BULLETIN

1 Clamp MS21919WCH13 Item 11

(e) Install these items to the riblet, cable bundle 2S/624VB and cable sleeve, Item 1,

as shown in Details A and E:

1 Clamp MS21919WCH4 Item (22) Retained at

removal

3 Spacer NSA5527-03-02D Item (31) Retained at

removal

1 Washer NAS1149D0332K Item (40) Retained at

removal

1 Screw NAS1096-3-38 Item (54) Retained at

removal

1 Clamp MS21919WCH13 Item 11

(6) Subtask 282148-831-209-001 - Install the cable sleeves in the RH-wing forward of

the front spar between rib 7 and rib 8 in zone 612.

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills ELECTRICAL

Material necessary to do the job

Kit 282148D01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 ABS0596S004 2 SLEEVE

12 MS21919WCH14 2 CLAMP

149 NSA935401-03 2 TIE

150 NSA935401-04 2 TIE

References

Fig. A-GBEAA

Improvement of the 2S-Route in the RHWing in Zone 612 (Kit D01)

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

Sheet 07

Sheet 08

NOTE (1): The sleeves ABS0596S004 is supplied in pieces of 1000 mm. Cut or

assemble these pieces to get the correct length.

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 142

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SERVICE BULLETIN

NOTE (2): The lengths of the sleeves given in this Service Bulletin are approximate

lengths. Adapt the lengths of the sleeves in relation to the aircraft

configuration.

NOTE (3): Before you install a sleeve, cut and discard the cable ties around the

cable bundle to install the sleeve correctly around the cable bundle.

NOTE (4): Adapt the number of cable ties to the required quantity.

Refer to Fig. A-GBEAA Sheet 01, Fig. A-GBEAA Sheet 02, Fig. A-GBEAA Sheet 03, Fig.

A-GBEAA Sheet 04, Fig. A-GBEAA Sheet 05, Fig. A-GBEAA Sheet 06, Fig. A-GBEAA

Sheet 07 and Fig. A-GBEAA Sheet 08

(a) Remove these items from the two brackets of the riblets and cable bundle

2S/624VB, as shown in Details A, H and K:

2 Clamp MS21919WCH4 Item (22) Retain

2 Washer NAS1149D0332K Item (40) Retain

2 Screw NAS1096-3-8 Item (55) Retain

2 Clamp Item (100) Discard

(b) Install this cable sleeve around these identified wires from the cable bundle

2S/624VB, as shown in Details A, J, K, L, M and N:

Wire number 2842-5052

Wire number 2842-5053

Wire number 2842-5054

Wire number 2842-5055

Wire number 2842-5056

1 Sleeve ABS0596S004 Item 1

and attach the cable sleeves with:

1 Tie NSA935401-03 Item 149

1 Tie-Cable NSA935401-04 Item 150

(c) Install this cable sleeve around this identified wire from the cable bundle 2S/624VB,

as shown in Details A, J, K, L, M and N:

Wire number 2842-5070

1 Sleeve ABS0596S004 Item 1

and attach the cable sleeves with:

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 143

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SERVICE BULLETIN

1 Tie NSA935401-03 Item 149

1 Tie-Cable NSA935401-04 Item 150

(d) Install these items to the two brackets of the riblets, cable bundle 2S/624VB and

cable sleeves, Item 1, as shown in Detail A, J and L:

2 Clamp MS21919WCH4 Item (22) Retained at

removal

2 Washer NAS1149D0332K Item (40) Retained at

removal

2 Screw NAS1096-3-8 Item (55) Retained at

removal

2 Clamp MS21919WCH14 Item 12

(7) Subtask 282148-831-210-001 - Install the cable sleeves in the RH-wing forward of

the front spar between rib 8 and rib 9 (pylon area) in zone 612.

Manpower Resources

Manhours 4.00

Minimum number of person 1

Subtask elapsed time 4.00

Skills ELECTRICAL

Material necessary to do the job

Kit 282148D02R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 ABS0596S004 2 SLEEVE

30 NSA5527-03-01D 2 SPACER

109 NSA935805-09 3 (ME) CONDUIT

117 NSA935807C09 13 CLAMP

125 B9299071900200 1 EQUIPMNT

126 NSA938184PV1601 15 PIN

149 NSA935401-03 20 TIE

150 NSA935401-04 20 TIE

References

Fig. A-GBGAA

Improvement of the 2S-Route in the RHWing Pylon Area (Kit D02)

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

Sheet 07

Sheet 08

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 144

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SERVICE BULLETIN

References

Fig. A-GHAAA

Hook-up Chart

Sheet 01

Fig. A-GHBAA

Hook-up Chart

Sheet 01

NOTE (1): The sleeves ABS0596S004 is supplied in pieces of 1000 mm. Cut or

assemble these pieces to get the correct length.

NOTE (2): The lengths of the sleeves given in this Service Bulletin are approximate

lengths. Adapt the lengths of the sleeves in relation to the aircraft

configuration.

NOTE (3): Before you install a sleeve, cut and discard the cable ties around the

cable bundle to install the sleeve correctly around the cable bundle.

NOTE (4): Adapt the number of cable ties to the required quantity.

Refer to Fig. A-GBGAA Sheet 01, Fig. A-GBGAA Sheet 02, Fig. A-GBGAA Sheet 03,

Fig. A-GBGAA Sheet 04, Fig. A-GBGAA Sheet 05, Fig. A-GBGAA Sheet 06, Fig. AGBGAA Sheet 07 and Fig. A-GBGAA Sheet 08

Refer to Fig. A-GHAAA Sheet 01 and Fig. A-GHBAA Sheet 01

(a) Disconnect these wires of route 2S from the receptacles 40VC and 5006VC in

accordance with the Hook-up Chart 1, Lines 1 thru 14, END 1, Fig. A-GHAAA

Sheet 01 and the Hook-up Chart 2, Lines 2 thru 8, END 1, Fig. A-GHBAA Sheet

01.

(b) Remove, refer to Fig. A-GBGAA Sheet 03, Detail D, BEFORE:

1 Spacer NSA5527-03-02D Item (31) Discard

1 Clamp NSA935807C10 Item (110) Discard

1 Clamp NSA935807C16 Item (111) Retain

1 Washer NSA935808-01 Item (112) Retain

1 Screw NAS1096-3-23 Item (113) Retain

1 Spacer NSA5527-03-05D Item (114) Discard

1 Washer NSA1149D0332K Item (115) Retain

1 Nut NAS1291C3M Item (116) Retain

1 Clamp NSA935807C09 Item (117) Retain

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 145

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SERVICE BULLETIN

(c) Remove, refer to Fig. A-GBGAA Sheet 04, Detail F, BEFORE:

2 Spacer NSA5527-03-01D Item (30) Retain

1 Spacer NSA5527-03-02D Item (31) Retain

1 Clamp NSA935807C10 Item (110) Retain

1 Clamp NSA935807C10 Item (110) Discard

1 Clamp NSA935807C16 Item (111) Retain

1 Washer NSA935808-01 Item (112) Retain

1 Clamp NSA935807C09 Item (117) Retain

1 Screw NAS1096-3-33 Item (118) Retain

(d) Remove, refer to Fig. A-GBGAA Sheet 05, Detail H, BEFORE:

2 Spacer NSA5527-03-01D Item (30) Retain

2 Spacer NSA5527-03-02D Item (31) Retain

2 Clamp NSA935807C10 Item (110) Discard

2 Clamp NSA935807C16 Item (111) Retain

2 Spacer NSA5527-03-05D Item (114) Retain

2 Washer NSA1149D0332K Item (115) Retain

2 Clamp NSA935807C09 Item (117) Retain

2 Screw NAS1096-3-33 Item (118) Retain

(e) Remove, refer to Fig. A-GBGAA Sheet 06, Detail K, BEFORE:

1 Spacer NSA5527-03-01D Item (30) Retain

1 Spacer NSA5527-03-02D Item (31) Retain

1 Clamp NSA935807C10 Item (110) Discard

1 Clamp NSA935807C16 Item (111) Retain

1 Spacer NSA5527-03-05D Item (114) Retain

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 146

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SERVICE BULLETIN

1 Washer NSA1149D0332K Item (115) Retain

1 Clamp NSA935807C09 Item (117) Retain

1 Screw NAS1096-3-33 Item (118) Retain

(f) Remove, refer to Fig. A-GBGAA Sheet 07, Detail M, BEFORE:

1 Spacer NSA5527-03-01D Item (30) Retain

1 Spacer NSA5527-03-02D Item (31) Retain

1 Clamp NSA935807C10 Item (110) Discard

1 Clamp NSA935807C16 Item (111) Retain

1 Washer NSA935808-01 Item (112) Retain

1 Spacer NSA5527-03-05D Item (114) Retain

1 Clamp NSA935807C09 Item (117) Retain

1 Screw NAS1096-3-33 Item (118) Retain

(g) Remove, refer to Fig. A-GBGAA Sheet 08, Detail P, BEFORE:

1 Spacer NSA5527-03-02D Item (31) Retain

1 Clamp NSA935807C10 Item (110) Discard

1 Clamp NSA935807C16 Item (111) Retain

1 Washer NSA935808-01 Item (112) Retain

1 Spacer NSA5527-03-05D Item (114) Retain

1 Clamp NSA935807C09 Item (117) Retain

1 Screw NAS1096-3-25 Item (119) Retain

(h) Remove the identification sleeves from the cable harnesses near the receptacles

40VC and 5006VC as shown Fig. A-GBGAA Sheet 01, Detail A

As

required

placard Item (125) Discard

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 147

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SERVICE BULLETIN

(i) Remove the protection sleeve from the cable harness as shown Fig. A-GBGAA

Sheet 01, Fig. A-GBGAA Sheet 02, Fig. A-GBGAA Sheet 03, Fig. A-GBGAA Sheet

04, Fig. A-GBGAA Sheet 05, Fig. A-GBGAA Sheet 06, Fig. A-GBGAA Sheet 07

and Fig. A-GBGAA Sheet 08, Details D, F, H, K, M and P:

1 Sleeve NSA935805-10 Item (109) Discard

(j) Cut the conduit to the required length and install as shown Fig. A-GBGAA Sheet

01, Fig. A-GBGAA Sheet 02, Fig. A-GBGAA Sheet 03, Fig. A-GBGAA Sheet 04,

Fig. A-GBGAA Sheet 05, Fig. A-GBGAA Sheet 06, Fig. A-GBGAA Sheet 07 and

Fig. A-GBGAA Sheet 08, Details E, G, J, L, N and Q:

3 (ME) Conduit NSA935805-09 Item 109

1 One part 1500.0 mm (59.06 in.) to the electrical wires for 10QT-A and 10QT-B

of route 2S/636VB, refer to the Hook-up Chart 2, Fig. A-GHBAA Sheet 01

2 Three parts, one 520 mm (20.47 in.) and two 240.0 mm (9.45 in.) to the

remaining electrical wires of route 2S/636VB, refer to Fig. A-GHAAA Sheet 01

(k) Connect the electrical wires of route 2S to the receptacles 40VC and 5006VC in

accordance with the Hook-up Chart 1, Lines 1 thru 14, END 1, Fig. A-GHAAA

Sheet 01 and the Hook-up Chart 2, lines 2 thru 8, END 1, Fig. A-GHBAA Sheet 01.

Use the contact pins if required:

15 Pin NSA938184PV1601 Item 126

(l) Install, refer to Fig. A-GBGAA Sheet 08, Detail Q, AFTER:

1 Spacer NSA5527-03-02D Item (31) Retained at

removal

1 Clamp NSA935807C16 Item (111) Retained at

removal

1 Washer NSA935808-01 Item (112) Retained at

removal

1 Spacer NSA5527-03-05D Item (114) Retained at

removal

2 Clamp NSA935807C09 Item (117) Retained at

removal

1 Screw NAS1096-3-25 Item (119) Retained at

removal

1 Clamp NSA935807C09 Item 117

(m) Install, refer to Fig. A-GBGAA Sheet 07, Detail N, AFTER:

1 Spacer NSA5527-03-01D Item (30) Retained at

removal

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 148

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1 Spacer NSA5527-03-02D Item (31) Retained at

removal

1 Clamp NSA935807C16 Item (111) Retained at

removal

1 Washer NSA935808-01 Item (112) Retained at

removal

1 Spacer NSA5527-03-05D Item (114) Retained at

removal

1 Clamp NSA935807C09 Item (117) Retained at

removal

1 Screw NAS1096-3-33 Item (118) Retained at

removal

2 Clamp NSA935807C09 Item 117

(n) Install, refer to Fig. A-GBGAA Sheet 06, Detail L, AFTER:

1 Spacer NSA5527-03-01D Item (30) Retained at

removal

1 Spacer NSA5527-03-02D Item (31) Retained at

removal

1 Clamp NSA935807C16 Item (111) Retained at

removal

1 Spacer NSA5527-03-05D Item (114) Retained at

removal

1 Washer NSA1149D0332K Item (115) Retained at

removal

1 Clamp NSA935807C09 Item (117) Retained at

removal

1 Screw NAS1096-3-33 Item (118) Retained at

removal

2 Clamp NSA935807C09 Item 117

(o) Install, refer to Fig. A-GBGAA Sheet 05, Detail J, AFTER:

2 Spacer NSA5527-03-01D Item (30) Retained at

removal

2 Spacer NSA5527-03-02D Item (31) Retained at

removal

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 149

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SERVICE BULLETIN

2 Clamp NSA935807C16 Item (111) Retained at

removal

2 Spacer NSA5527-03-05D Item (114) Retained at

removal

2 Washer NSA1149D0332K Item (115) Retained at

removal

2 Clamp NSA935807C09 Item (117) Retained at

removal

2 Screw NAS1096-3-33 Item (118) Retained at

removal

4 Clamp NSA935807C09 Item 117

(p) Install, refer to Fig. A-GBGAA Sheet 04, Detail G, AFTER:

2 Spacer NSA5527-03-01D Item (30) Retained at

removal

1 Spacer NSA5527-03-02D Item (31) Retained at

removal

1 Clamp NSA935807C10 Item (110) Retained at

removal

1 Clamp NSA935807C16 Item (111) Retained at

removal

1 Washer NSA935808-01 Item (112) Retained at

removal

1 Clamp NSA935807C09 Item (117) Retained at

removal

1 Screw NAS1096-3-33 Item (118) Retained at

removal

2 Clamp NSA935807C09 Item 117

(q) Install, refer to Fig. A-GBGAA Sheet 03, Detail E, AFTER:

2 Spacer NSA5527-03-01D Item 30

1 Clamp NSA935807C16 Item (111) Retained at

removal

1 Washer NSA935808-01 Item (112) Retained at

removal

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 150

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SERVICE BULLETIN

1 Screw NAS1096-3-23 Item (113) Retained at

removal

1 Washer NSA1149D0332K Item (115) Retained at

removal

1 Nut NAS1291C3M Item (116) Retained at

removal

1 Clamp NSA935807C09 Item (117) Retained at

removal

2 Clamp NSA935807C09 Item 117

(r) Protect the electrical wires for 10QT-A and 10QT-B of route 2S/636VB, refer to the

Hook-up Chart 2, Fig. A-GHBAA Sheet 01 with:

2 Sleeve ABS0596S004 Item 1

and

20 Tie NSA935401-03 Item 149

20 Tie-Cable NSA935401-04 Item 150

(s) Install the identification placards:

1 Placard set B9299071900200 Item 125

(8) Subtask 282148-831-211-001 - Install the cable sleeves in the RH-wing forward of

the front spar between rib 9 and rib 12 in zone 623.

Manpower Resources

Manhours 4.00

Minimum number of person 1

Subtask elapsed time 4.00

Skills ELECTRICAL

Material necessary to do the job

Kit 282148D01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 ABS0596S004 3 SLEEVE

10 MS21919WCH9 8 CLAMP

14 NAS1096-3-19 2 SCREW

15 NSA5527-03-03 3 SPACER

16 NSA8420-2 0.5 (ME) CORD

149 NSA935401-03 1 TIE

150 NSA935401-04 1 TIE

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 151

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SERVICE BULLETIN

Kit 282148D02R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

31 NSA5527-03-02D 2 SPACER

121 NAS1096-3-40 1 SCREW

References

Fig. A-GBFAA

Improvement of the 2S-Route in the RHWing in Zone 623 (Kit D01)

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

Sheet 07

Sheet 08

Sheet 09

Sheet 10

NOTE (1): The sleeves ABS0596S004 is supplied in pieces of 1000 mm. Cut or

assemble these pieces to get the correct length.

NOTE (2): The lengths of the sleeves given in this Service Bulletin are approximate

lengths. Adapt the lengths of the sleeves in relation to the aircraft

configuration.

NOTE (3): Before you install a sleeve, cut and discard the cable ties around the

cable bundle to install the sleeve correctly around the cable bundle.

NOTE (4): Adapt the number of cable ties to the required quantity.

Refer to Fig. A-GBFAA Sheet 01, Fig. A-GBFAA Sheet 02, Fig. A-GBFAA Sheet 03, Fig.

A-GBFAA Sheet 04, Fig. A-GBFAA Sheet 05, Fig. A-GBFAA Sheet 06, Fig. A-GBFAA

Sheet 07, Fig. A-GBFAA Sheet 08, Fig. A-GBFAA Sheet 09 and Fig. A-GBFAA Sheet 10

(a) At one position, remove these items from the bracket between rib 11 and rib 12

and cable bundle 2S/636VB, as shown in Details A and D:

2 Clamp MS21919WCH4 Item (22) Retain

1 Clamp MS21919WCH4 Item (22) Discard

1 Clamp MS21919WCH3 Item (23) Retain

1 Spacer NSA5527-03-01D Item (30) Retain

1 Spacer NSA5527-03-02D Item (31) Retain

1 Washer NSA935808-01 Item (112) Retain

1 Screw NAS1096-3-30 Item (121) Discard

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 152

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SERVICE BULLETIN

1 Clamp NSA935807-06 Item (122) Retain

(b) At two positions, remove these items from the brackets between rib 10 and rib 11

and between rib 11 and rib 12 and cable bundle 2S/636VB, as shown in Details A

and F:

2 Clamp Item (22) Discard

6 Clamp MS21919WCH4 Item (22) Retain

4 Spacer NSA5527-03-01D Item (30) Retain

2 Washer NAS1149D0332K Item (40) Retain

2 Screw NAS1096-3-27 Item (52) Retain

(c) At two positions, remove these items from the brackets of the rib 11 and cable

bundle 2S/636VB, as shown in Details A and H:

2 Clamp MS21919WCH4 Item (22) Retain

1 Clamp Item (23) Discard

1 Spacer NSA5527-03-01D Item (30) Retain

1 Spacer NSA5527-03-04D Item (32) Retain

1 Washer NAS1149D0332K Item (40) Retain

1 Screw NAS1096-3-22 Item (51) Retain

(d) At two positions, remove these items from the brackets of the rib 10 and cable

bundle 2S/636VB, as shown in Details A and K:

2 Clamp Item (22) Discard

2 Clamp MS21919WCH4 Item (22) Retain

2 Spacer NSA5527-03-01D Item (30) Retain

2 Spacer Item (32) Discard

2 Washer NAS1149D0332K Item (40) Retain

2 Screw Item (51) Discard

(e) Remove these items from the bracket between rib 9 and rib 10 and cable bundle

2S/636VB, as shown in Details A and M:

3 Clamp MS21919WCH4 Item (22) Retain

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 153

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SERVICE BULLETIN

1 Clamp Item (23) Discard

1 Spacer NSA5527-03-01D Item (30) Retain

1 Spacer NSA5527-03-04D Item (32) Retain

1 Washer NAS1149D0332K Item (40) Retain

1 Screw NAS1096-3-22 Item (51) Retain

(f) Remove these items from the bracket of the rib 9 and cable bundle 2S/636VB, as

shown in Details A and T:

1 Clamp Item (21) Discard

1 Clamp MS21919WCH5 Item (21) Retain

1 Spacer NSA5527-03-02D Item (31) Retain

1 Spacer NSA5527-03-04D Item (32) Retain

1 Washer NAS1149D0332K Item (40) Retain

1 Screw NAS1096-3-27 Item (52) Retain

(g) Install this cable sleeve around these identified wires from the cable bundle

2S/636VB, as shown in Details A, C, E, G, J, L, N, A and R:

Wire number 2842-5061

Wire number 2842-5062

Wire number 2842-5063

Wire number 2842-5064

Wire number 2842-5065

Wire number 2842-5071

3 Sleeve ABS0596S004 Item 1

and attach the cable sleeves with:

3 Spacer NSA5527-03-03 Item 15

0.5 (ME) Cord NSA8420-2 Item 16

1 Tie NSA935401-03 Item 149

1 Tie-Cable NSA935401-04 Item 150

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 154

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SERVICE BULLETIN

(h) At one positions, install these items to the brackets between rib 10 and rib 11 and

between rib 11 and rib 12, cable sleeves, Item 1 and cable bundle 2S/636VB, as

shown in Details A and E:

2 Clamp MS21919WCH4 Item (22) Retained at

removal

1 Clamp MS21919WCH3 Item (23) Retained at

removal

1 Spacer NSA5527-03-01D Item (30) Retained at

removal

1 Spacer NSA5527-03-02D Item (31) Retained at

removal

1 Washer NSA935808-01 Item (112) Retained at

removal

1 Clamp NSA935807-06 Item (122) Retained at

removal

1 Clamp MS21919WCH9 Item 10

2 Spacer NSA5527-03-02D Item 31

1 Screw NAS1096-3-40 Item 121

(i) At two positions, install these items to the brackets between rib 10 and rib 11 and

between rib 11 and rib 12, cable sleeves, Item 1 and cable bundle 2S/636VB, as

shown in Details A and G:

6 Clamp MS21919WCH4 Item (22) Retained at

removal

4 Spacer NSA5527-03-01D Item (30) Retained at

removal

2 Washer NAS1149D0332K Item (40) Retained at

removal

2 Screw NAS1096-3-27 Item (52) Retained at

removal

2 Clamp MS21919WCH9 Item 10

(j) At two positions, install these items to the brackets of the rib 11, cable sleeves,

Item 1 and cable bundle 2S/636VB, as shown in Details A and J:

2 Clamp MS21919WCH4 Item (22) Retained at

removal

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 155

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SERVICE BULLETIN

1 Spacer NSA5527-03-01D Item (30) Retained at

removal

1 Spacer NSA5527-03-04D Item (32) Retained at

removal

1 Washer NAS1149D0332K Item (40) Retained at

removal

1 Screw NAS1096-3-22 Item (51) Retained at

removal

1 Clamp MS21919WCH9 Item 10

(k) At two positions, install these items to the brackets of the rib 10, cable sleeves,

Item 1 and cable bundle 2S/636VB, as shown in Details A and L:

2 Clamp MS21919WCH4 Item (22) Retained at

removal

2 Spacer NSA5527-03-01D Item (30) Retained at

removal

2 Washer NAS1149D0332K Item (40) Retained at

removal

2 Clamp MS21919WCH9 Item 10

2 Screw NAS1096-3-19 Item 14

(l) Install these items to the bracket between rib 9 and rib 10, cable sleeves, Item 1

and cable bundle 2S/636VB, as shown in Details A and N:

3 Clamp MS21919WCH4 Item (22) Retained at

removal

1 Spacer NSA5527-03-01D Item (30) Retained at

removal

1 Spacer NSA5527-03-04D Item (32) Retained at

removal

1 Washer NAS1149D0332K Item (40) Retained at

removal

1 Screw NAS1096-3-22 Item (51) Retained at

removal

1 Clamp MS21919WCH9 Item 10

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 156

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SERVICE BULLETIN

(m) Install these items to the bracket of the rib 9, cable sleeves, Item 1 and cable

bundle 2S/636VB, as shown in Details A and Q:

1 Clamp MS21919WCH5 Item (21) Retained at

removal

1 Spacer NSA5527-03-02D Item (31) Retained at

removal

1 Spacer NSA5527-03-04D Item (32) Retained at

removal

1 Washer NAS1149D0332K Item (40) Retained at

removal

1 Screw NAS1096-3-27 Item (52) Retained at

removal

1 Clamp MS21919WCH9 Item 10

**CONF 006

(1) Subtask 282148-831-405-001 - Install a New Bracket on the Sub Spar Behind the

Front Spar Between RIB 8 and RIB 9 on the RH Wing

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills AIRFRAME

Material necessary to do the job

Kit 282148B01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 A5725068600000 1 Bracket

2 ASNA0078A502 2 Rivet

Consumable CMLB01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Corrosion Inhibiting Low

Adhesion Sealant

09-018 As required

Solvent General Purpose 11-026 As required

Lint-Free Cotton Cloth 19-003 As required

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 157

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SERVICE BULLETIN

References

Fig. A-UBAAA

Location of Bracket on the Sub Spar

Behind the Front Spar Between RIB 8

and RIB 9 (RH Wing)

Sheet 01

Refer to Fig. A-UBAAA Sheet 01

(a) Remove from the sub spar behind the front spar between RIB 8 and RIB 9 on the

RH wing, the items that follow:

2 Rivet NSA54213510DCA Item (2) Discard

1 Bracket A5724630400000 Item (1) Discard

(b) Clean the mating surfaces use

Lint-Free Cotton

Cloth

19-003 As required

made moist with

Solvent General

Purpose

11-026 As required

(c) Put the

1 Bracket A5725068600000 Item 1

in position on the sub spar behind the front spar between RIB 8 and RIB 9 on the

RH wing (Refer to Fig. A-UBAAA Sheet 01).

(d) Copy drill the two holes from the sub spar through the Bracket, Item 1 to a

dimension of between 4.060 and 4.160 mm (0.160 and 0.164 in.).

(e) Deburr the holes that have been worked.

(f) Use

Corrosion Inhibiting

Low Adhesion

Sealant

09-018 As required

and wet install the

1 Bracket A5725068600000 Item 1

with the

2 Rivet, Blind ASNA0078A502 Item 2

on the sub spar behind the front spar between RIB 8 and RIB 9 on the RH wing.

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 158

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SERVICE BULLETIN

(2) Subtask 282148-831-004-001 - Install cable sleeves in the RH Electronics Rack

90VU.

Manpower Resources

Manhours 6.00

Minimum number of person 1

Subtask elapsed time 6.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 282148A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 ABS0596S004 2000 (mm) SLEEVE

NSA935401-04 50 TIE

References

Fig. A-FCAAA

Installation of Cable Sleeves in the RH

Electronics Rack 90VU.

Sheet 01

Fig. A-FWAAA

Installation of Cable Sleeves in the RH

Electronics Rack 90VU.

Sheet 01

NOTE: The sleeves ABS0596S004 and ABS0596S006 are supplied in pieces of

1000 mm (39.370 inches), cut or assemble these pieces to get the

correct length.

NOTE: The lengths of the sleeves given in this Service Bulletin are approximate

lengths. Adapt the lengths of the sleeves in relation to the aircraft

configuration.

NOTE: Before you install a sleeve, cut and discard the cable ties around the

cable bundle to install the sleeve correctly around the cable bundle.

(a) On the Shelf 92VU, only around the wires identified in figure Fig. A-FWAAA Sheet

01, from the equipment 15QT-B to the connector 2354VC, install:

1600 (mm) Sleeve ABS0596S004 Item 1

(b) Around the cable bundle of the connector 2354VC-A, install:

400 (mm) Sleeve ABS0596S004 Item 1

(c) Attach the sleeves with:

50 Tie-Cable NSA935401-04

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 159

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@A310

SERVICE BULLETIN

(3) Subtask 282148-831-005-001 - Install cable sleeves between FR38.2 and FR39, in

the forward cargo compartment.

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 282148A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

2 ABS0596S006 1000 (mm) SLEEVE

NSA935401-05 50 TIE

References

Fig. A-FCBAA

Installation of Cable Sleeves in the

Forward Cargo Compartment.

Sheet 01

NOTE: The sleeves ABS0596S004 and ABS0596S006 are supplied in pieces of

1000 mm (39.370 inches), cut or assemble these pieces to get the

correct length.

NOTE: The lengths of the sleeves given in this Service Bulletin are approximate

lengths. Adapt the lengths of the sleeves in relation to the aircraft

configuration.

NOTE: Before you install a sleeve, cut and discard the cable ties around the

cable bundle to install the sleeve correctly around the cable bundle.

(a) Around the cable bundle of the pressure seal 20VP, install:

1000 (mm) Sleeve ABS0596S006 Item 2

(b) Attach the sleeves with:

50 Tie-Cable NSA935401-05

(4) Subtask 282148-831-006-002 - Install cable sleeves in the RH forward wing root

and krueger flap.

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills NON SPECIFIC

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 160

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@A310

SERVICE BULLETIN

Material necessary to do the job

Kit 282148A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

2 ABS0596S006 SLEEVE

NSA935401-05 TIE

References

Fig. A-FCCAB

Installation of Cable Sleeves in the RH

forward wing root and krueger flap.

Sheet 01

NOTE: The sleeves ABS0596S004 and ABS0596S006 are supplied in pieces of

1000 mm (39.370 inches), cut or assemble these pieces to get the

correct length.

NOTE: The lengths of the sleeves given in this Service Bulletin are approximate

lengths. Adapt the lengths of the sleeves in relation to the aircraft

configuration.

NOTE: Before you install a sleeve, cut and discard the cable ties around the

cable bundle to install the sleeve correctly around the cable bundle.

(a) Around the cable bundle of the pressure seal 20VP, install:

1000 (mm) Sleeve ABS0596S006 Item 2

(b) Attach the sleeves with:

50 Tie-Cable NSA935401-05

(5) Subtask 282148-831-208-002 - Install the cable sleeves in the RH-wing forward of

the front spar between rib 2 and rib 3 in zone 612.

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

Material necessary to do the job

Kit 282148D01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 ABS0596S004 1 SLEEVE

11 MS21919WCH13 CLAMP

149 NSA935401-03 1 TIE

150 NSA935401-04 1 TIE

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 161

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@A310

SERVICE BULLETIN

References

Fig. A-GBEAA

Improvement of the 2S-Route in the RHWing in Zone 612 (Kit D01)

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

Sheet 07

Sheet 08

NOTE (1): The sleeves ABS0596S004 is supplied in pieces of 1000 mm. Cut or

assemble these pieces to get the correct length.

NOTE (2): The lengths of the sleeves given in this Service Bulletin are approximate

lengths. Adapt the lengths of the sleeves in relation to the aircraft

configuration.

NOTE (3): Before you install a sleeve, cut and discard the cable ties around the

cable bundle to install the sleeve correctly around the cable bundle.

NOTE (4): Adapt the number of cable ties to the required quantity.

Refer to Fig. A-GBEAA Sheet 01, Fig. A-GBEAA Sheet 02, Fig. A-GBEAA Sheet 03, Fig.

A-GBEAA Sheet 04, Fig. A-GBEAA Sheet 05, Fig. A-GBEAA Sheet 06, Fig. A-GBEAA

Sheet 07 and Fig. A-GBEAA Sheet 08

(a) Remove these items from the bracket of the rib 2 and cable bundle 2S/624VB, as

shown in Details A and B:

1 Clamp MS21919WCH4 Item (22) Retain

1 Clamp MS21919WCH3 Item (23) Retain

1 Spacer NSA5527-03-02D Item (31) Retain

1 Washer NAS1149D0332K Item (40) Retain

1 Screw NAS1096-3-21 Item (50) Retain

1 Clamp MS21919WCH10 Item (100) Retain

1 Clamp Item (100) Discard

(b) Remove these items from the riblet and cable bundle 2S/624VB, as shown in

Details A and D:

1 Clamp MS21919WCH4 Item (22) Retain

3 Spacer NSA5527-03-02D Item (31) Retain

1 Washer NAS1149D0332K Item (40) Retain

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 162

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SERVICE BULLETIN

1 Screw NAS1096-3-38 Item (54) Retain

1 Clamp Item (100) Discard

(c) Install this cable sleeve around these identified wires from the cable bundle

2S/624VB, as shown in Details A, C, E and F:

Wire number 2842-5052

Wire number 2842-5053

Wire number 2842-5054

Wire number 2842-5055

Wire number 2842-5056

Wire number 2842-5070

Install this cable sleeve around these identified wires from the cable bundle

2S/624VB, as shown in Details A, C, E and F:

Wire number 2842-5052

Wire number 2842-5053

Wire number 2842-5054

Wire number 2842-5055

Wire number 2842-5056

Wire number 2842-5070

1 Sleeve ABS0596S004 Item 1

and attach the cable sleeve with:

1 Tie NSA935401-03 Item 149

1 Tie-Cable NSA935401-04 Item 150

(d) Install these items to the bracket of the rib 2, cable bundle 2S/624VB and cable

sleeve, Item 1, as shown in Details A and C:

1 Clamp MS21919WCH4 Item (22) Retained at

removal

1 Clamp MS21919WCH3 Item (23) Retained at

removal

1 Spacer NSA5527-03-02D Item (31) Retained at

removal

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 163

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@A310

SERVICE BULLETIN

1 Washer NAS1149D0332K Item (40) Retained at

removal

1 Screw NAS1096-3-21 Item (50) Retained at

removal

1 Clamp MS21919WCH10 Item (100) Retained at

removal

1 Clamp MS21919WCH13 Item 11

(e) Install these items to the riblet, cable bundle 2S/624VB and cable sleeve, Item 1,

as shown in Details A and E:

1 Clamp MS21919WCH4 Item (22) Retained at

removal

3 Spacer NSA5527-03-02D Item (31) Retained at

removal

1 Washer NAS1149D0332K Item (40) Retained at

removal

1 Screw NAS1096-3-38 Item (54) Retained at

removal

1 Clamp MS21919WCH13 Item 11

(6) Subtask 282148-831-209-002 - Install the cable sleeves in the RH-wing forward of

the front spar between rib 7 and rib 8 in zone 612.

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

Material necessary to do the job

Kit 282148D01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 ABS0596S004 2 SLEEVE

12 MS21919WCH14 CLAMP

149 NSA935401-03 2 TIE

150 NSA935401-04 2 TIE

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 164

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@A310

SERVICE BULLETIN

References

Fig. A-GBEAA

Improvement of the 2S-Route in the RHWing in Zone 612 (Kit D01)

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

Sheet 07

Sheet 08

NOTE (1): The sleeves ABS0596S004 is are supplied in pieces of 1000 mm. Cut or

assemble these pieces to get the correct length.

NOTE (2): The lengths of the sleeves given in this Service Bulletin are approximate

lengths. Adapt the lengths of the sleeves in relation to the aircraft

configuration.

NOTE (3): Before you install a sleeve, cut and discard the cable ties around the

cable bundle to install the sleeve correctly around the cable bundle.

NOTE (4): Adapt the number of cable ties to the required quantity.

Refer to Fig. A-GBEAA Sheet 01, Fig. A-GBEAA Sheet 02, Fig. A-GBEAA Sheet 03, Fig.

A-GBEAA Sheet 04, Fig. A-GBEAA Sheet 05, Fig. A-GBEAA Sheet 06, Fig. A-GBEAA

Sheet 07 and Fig. A-GBEAA Sheet 08

(a) Remove these items from the two brackets of the riblets and cable bundle

2S/624VB, as shown in Details A, H and K:

2 Clamp MS21919WCH4 Item (22) Retain

2 Washer NAS1149D0332K Item (40) Retain

2 Screw NAS1096-3-8 Item (55) Retain

2 Clamp Item (100) Discard

(b) Install this cable sleeve around these identified wires from the cable bundle

2S/624VB, as shown in Details A, J, K, L, M and N:

Wire number 2842-5052

Wire number 2842-5053

Wire number 2842-5054

Wire number 2842-5055

Wire number 2842-5056

1 Sleeve ABS0596S004 Item 1

and attach the cable sleeves with:

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 165

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SERVICE BULLETIN

1 Tie NSA935401-03 Item 149

1 Tie-Cable NSA935401-04 Item 150

(c) Install this cable sleeve around this identified wire from the cable bundle 2S/624VB,

as shown in Details A, J, K, L, M and N:

Wire number 2842-5070

1 Sleeve ABS0596S004 Item 1

and attach the cable sleeves with:

1 Tie NSA935401-03 Item 149

1 Tie-Cable NSA935401-04 Item 150

(d) Install these items to the two brackets of the riblets, cable bundle 2S/624VB and

cable sleeves, Item 1, as shown in Detail A, J and L:

2 Clamp MS21919WCH4 Item (22) Retained at

removal

2 Washer NAS1149D0332K Item (40) Retained at

removal

2 Screw NAS1096-3-8 Item (55) Retained at

removal

2 Clamp MS21919WCH14 Item 12

(7) Subtask 282148-831-210-002 - Install the cable sleeves in the RH-wing forward of

the front spar between rib 8 and rib 9 (pylon area) in zone 612.

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

Material necessary to do the job

Kit 282148D02R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

109 NSA935805-09 CONDUIT

Kit 282148D03R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 ABS0596S004 3 SLEEVE

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 166

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@A310

SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

31 NSA5527-03-02D 1 SPACER

117 NSA935807C09 7 CLAMP

123 NAS1801-3-31 3 SCREW

126 NSA938184PV1601 7 PIN

130 NSA5527-03-08D 1 SPACER

131 NSA5527-03-07D 1 SPACER

132 B9299071900600 1 EQUIPMNT

149 NSA935401-03 20 TIE

150 NSA935401-04 20 TIE

References

Fig. A-GBHAA

Improvement of the 2S-Route in the RHWing Pylon Area (Kit D03)

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

Sheet 07

Sheet 08

Fig. A-GHBAA

Hook-up Chart

Sheet 01

NOTE (1): The sleeves ABS0596S004 is supplied in pieces of 1000 mm. Cut or

assemble these pieces to get the correct length.

NOTE (2): The lengths of the sleeves given in this Service Bulletin are approximate

lengths. Adapt the lengths of the sleeves in relation to the aircraft

configuration.

NOTE (3): Before you install a sleeve, cut and discard the cable ties around the

cable bundle to install the sleeve correctly around the cable bundle.

NOTE (4): Adapt the number of cable ties to the required quantity.

Refer to Fig. A-GBHAA Sheet 01, Fig. A-GBHAA Sheet 02, Fig. A-GBHAA Sheet 03,

Fig. A-GBHAA Sheet 04, Fig. A-GBHAA Sheet 05, Fig. A-GBHAA Sheet 06, Fig. AGBHAA Sheet 07 and Fig. A-GBHAA Sheet 08

(a) Disconnect the wires of route 2S from the receptacles 40VC and 5006VC in

accordance with the Hook-up Chart 2, Lines 2 thru 8, END 1, Fig. A-GHBAA Sheet

01.

(b) Remove, refer to Fig. A-GBHAA Sheet 03, Detail D, BEFORE:

1 Spacer NSA5527-03-02D Item (31) Retain

2 Clamp NSA935807C16 Item (111) Retain

1 Washer NSA935808-01 Item (112) Retain

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 167

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SERVICE BULLETIN

1 Screw NAS1096-3-23 Item (113) Retain

1 Spacer NSA5527-03-05D Item (114) Retain

1 Nut NAS1291C3M Item (116) Retain

1 Washer AN960KD10l Item (124) Retain

(c) Remove, refer to Fig. A-GBHAA Sheet 04, Detail F, BEFORE:

1 Spacer NSA5527-03-02D Item (31) Retain

2 Clamp NSA935807C16 Item (111) Retain

1 Washer NSA935808-01 Item (112) Retain

1 Screw NAS1096-3-23 Item (113) Retain

1 Spacer NSA5527-03-05D Item (114) Retain

(d) Remove, refer to Fig. A-GBHAA Sheet 05, Detail H, BEFORE:

2 Spacer NSA5527-03-02D Item (31) Retain

4 Clamp NSA935807C16 Item (111) Retain

2 Washer NSA935808-01 Item (112) Retain

2 Screw NAS1096-3-23 Item (113) Retain

2 Spacer NSA5527-03-05D Item (114) Retain

(e) Remove, refer to Fig. A-GBHAA Sheet 06, Detail K, BEFORE:

1 Spacer NSA5527-03-02D Item (31) Retain

2 Clamp NSA935807C16 Item (111) Retain

1 Washer NSA935808-01 Item (112) Retain

1 Screw NAS1096-3-23 Item (113) Discard

1 Clamp NSA5516-04NV Item (120) Retain

(f) Remove, refer to Fig. A-GBHAA Sheet 07, Detail M, BEFORE:

1 Spacer NSA5527-03-02D Item (31) Retain

2 Clamp NSA935807C16 Item (111) Retain

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 168

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SERVICE BULLETIN

1 Washer NSA935808-01 Item (112) Retain

1 Screw NAS1096-3-23 Item (113) Discard

1 Spacer NSA5527-03-05D Item (114) Retain

(g) Remove, refer to Fig. A-GBHAA Sheet 08, Detail P, BEFORE:

1 Spacer NSA5527-03-02D Item (31) Retain

2 Clamp NSA935807C16 Item (111) Retain

1 Washer NSA935808-01 Item (112) Retain

1 Screw NAS1096-3-23 Item (113) Discard

1 Spacer NSA5527-03-05D Item (114) Retain

(h) Remove the identification placards from the cable harnesses near the receptacles

52VC and 5006VC as shown Fig. A-GBHAA Sheet 02, Detail A

As

required

placard Item (132) Discard

(i) Remove the disconnected electrical wires from the protection sleeve.

(j) Install to the electrical wires for 10QT-A and 10QT-B of route 2S/636VB, refer to

the Hook-up Chart 2, Lines 2 thru 8, Fig. A-GHBAA Sheet 01:

1 (ME) Conduit NSA935805-09 Item 109

(k) Connect the electrical wires of route 2S to the receptacles 40VC and 5006VC in

accordance with the Hook-up Chart 2, Lines 2 thru 8, END 1, Fig. A-GHBAA Sheet

01. Use the contact pins if required:

7 Pin NSA938184PV1601 Item 126

(l) Install, refer to Fig. A-GBHAA Sheet 08, Detail Q, AFTER:

1 Spacer NSA5527-03-02D Item (31) Retained at

removal

1 Spacer NSA5527-03-02D Item 31

2 Clamp NSA935807C16 Item (111) Retained at

removal

1 Washer NSA935808-01 Item (112) Retained at

removal

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 169

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SERVICE BULLETIN

1 Spacer NSA5527-03-05D Item (114) Retained at

removal

1 Clamp NSA935807C09 Item 117

1 Screw NAS1801-3-31 Item 123

1 Spacer NSA5527-03-07D Item 131

(m) Install, refer to Fig. A-GBHAA Sheet 07, Detail N, AFTER:

1 Spacer NSA5527-03-02D Item (31) Retained at

removal

2 Clamp NSA935807C16 Item (111) Retained at

removal

1 Washer NSA935808-01 Item (112) Retained at

removal

1 Spacer NSA5527-03-05D Item (114) Retained at

removal

1 Clamp NSA935807C09 Item 117

1 Screw NAS1801-3-31 Item 123

1 Spacer NSA5527-03-08D Item 130

(n) Install, refer to Fig. A-GBHAA Sheet 06, Detail L, AFTER:

2 Spacer NSA5527-03-02D Item (31) Retained at

removal

2 Clamp NSA935807C16 Item (111) Retained at

removal

1 Washer NSA935808-01 Item (112) Retained at

removal

1 Clamp NSA5516-04NV Item (120) Retained at

removal

1 Clamp NSA935807C09 Item 117

2 Screw NAS1801-3-31 Item 123

(o) Install, refer to Fig. A-GBHAA Sheet 05, Detail J, AFTER:

2 Spacer NSA5527-03-02D Item (31) Retained at

removal

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 170

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SERVICE BULLETIN

4 Clamp NSA935807C16 Item (111) Retained at

removal

2 Washer NSA935808-01 Item (112) Retained at

removal

2 Screw NAS1096-3-23 Item (113) Retained at

removal

2 Spacer NSA5527-03-05D Item (114) Retained at

removal

2 Clamp NSA935807C09 Item 117

(p) Install, refer to Fig. A-GBHAA Sheet 04, Detail G, AFTER:

1 Spacer NSA5527-03-02D Item (31) Retained at

removal

2 Clamp NSA935807C16 Item (111) Retained at

removal

1 Washer NSA935808-01 Item (112) Retained at

removal

1 Screw NAS1096-3-23 Item (113) Retained at

removal

1 Spacer NSA5527-03-05D Item (114) Retained at

removal

1 Clamp NSA935807C09 Item 117

(q) Install, refer to Fig. A-GBHAA Sheet 03, Detail E, AFTER:

1 Spacer NSA5527-03-02D Item (31) Retained at

removal

2 Clamp NSA935807C16 Item (111) Retained at

removal

1 Washer NSA935808-01 Item (112) Retained at

removal

1 Screw NAS1096-3-23 Item (113) Retained at

removal

1 Spacer NSA5527-03-05D Item (114) Retained at

removal

1 Nut NAS1291C3M Item (116) Retained at

removal

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 171

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@A310

SERVICE BULLETIN

1 Washer AN960KD10l Item (124) Retained at

removal

1 Clamp NSA935807C09 Item 117

(r) Protect the electrical wires for 10QT-A and 10QT-B of route 2S/636VB, refer to the

Hook-up Chart 2, Fig. A-GHBAA Sheet 01 with:

3 Sleeve ABS0596S004 Item 1

and

20 Tie NSA935401-03 Item 149

20 Tie-Cable NSA935401-04 Item 150

(s) Install the identification placards, refer to Fig. A-GBHAA Sheet 02:

1 Placard Set B9299071900600 Item 132

(8) Subtask 282148-831-211-002 - Install the cable sleeves in the RH-wing forward of

the front spar between rib 9 and rib 12 in zone 623.

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

Material necessary to do the job

Kit 282148D01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 ABS0596S004 3 SLEEVE

10 MS21919WCH9 CLAMP

14 NAS1096-3-19 2 SCREW

15 NSA5527-03-03 3 SPACER

16 NSA8420-2 1 (ME) CORD

149 NSA935401-03 10 TIE

150 NSA935401-04 20 TIE

Kit 282148D03R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

31 NSA5527-03-02D 1 SPACER

121 NAS1096-3-40 1 SCREW

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 172

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SERVICE BULLETIN

References

Fig. A-GBFAA

Improvement of the 2S-Route in the RHWing in Zone 623 (Kit D01)

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

Sheet 07

Sheet 08

Sheet 09

Sheet 10

NOTE (1): The sleeve ABS0596S004 is supplied in pieces of 1000 mm. Cut or

assemble these pieces to get the correct length.

NOTE (2): The lengths of the sleeves given in this Service Bulletin are approximate

lengths. Adapt the lengths of the sleeves in relation to the aircraft

configuration.

NOTE (3): Before you install a sleeve, cut and discard the cable ties around the

cable bundle to install the sleeve correctly around the cable bundle.

NOTE (4): Adapt the number of cable ties to the required quantity.

Refer to Fig. A-GBFAA Sheet 01, Fig. A-GBFAA Sheet 02, Fig. A-GBFAA Sheet 03, Fig.

A-GBFAA Sheet 04, Fig. A-GBFAA Sheet 05, Fig. A-GBFAA Sheet 06, Fig. A-GBFAA

Sheet 07, Fig. A-GBFAA Sheet 08, Fig. A-GBFAA Sheet 09 and Fig. A-GBFAA Sheet 10

(a) At one position, remove these items from the bracket between rib 11 and rib 12

and cable bundle 2S/636VB, as shown in Details A and D:

2 Clamp MS21919WCH4 Item (22) Retain

1 Clamp MS21919WCH4 Item (22) Discard

1 Clamp MS21919WCH3 Item (23) Retain

1 Spacer NSA5527-03-01D Item (30) Retain

1 Spacer NSA5527-03-02D Item (31) Retain

2 Washer NSA935808-01 Item (112) Retain

2 Screw NAS1096-3-30 Item (121) Discard

1 Clamp NSA935807-06 Item (122) Retain

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 173

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SERVICE BULLETIN

(b) At two positions, remove these items from the brackets between rib 10 and rib 11

and between rib 11 and rib 12 and cable bundle 2S/636VB, as shown in Details A

and F:

2 Clamp Item (22) Discard

6 Clamp MS21919WCH4 Item (22) Retain

4 Spacer NSA5527-03-01D Item (30) Retain

2 Washer NAS1149D0332K Item (40) Retain

2 Screw NAS1096-3-27 Item (52) Retain

(c) At two positions, remove these items from the brackets of the rib 11 and cable

bundle 2S/636VB, as shown in Details A and H:

6 Clamp MS21919WCH4 Item (22) Retain

2 Clamp Item (23) Discard

2 Spacer NSA5527-03-01D Item (30) Retain

2 Spacer NSA5527-03-04D Item (32) Retain

2 Washer NAS1149D0332K Item (40) Retain

2 Screw NAS1096-3-22 Item (51) Retain

(d) At two positions, remove these items from the brackets of the rib 10 and cable

bundle 2S/636VB, as shown in Details A and K:

2 Clamp Item (22) Discard

2 Clamp MS21919WCH4 Item (22) Retain

2 Spacer NSA5527-03-01D Item (30) Retain

2 Spacer Item (32) Discard

2 Washer NAS1149D0332K Item (40) Retain

2 Screw Item (51) Discard

(e) Remove these items from the bracket between rib 9 and rib 10 and cable bundle

2S/636VB, as shown in Details A and M:

3 Clamp MS21919WCH4 Item (22) Retain

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 174

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SERVICE BULLETIN

1 Clamp Item (23) Discard

1 Spacer NSA5527-03-01D Item (30) Retain

1 Spacer NSA5527-03-04D Item (32) Retain

1 Washer NAS1149D0332K Item (40) Retain

1 Screw NAS1096-3-22 Item (51) Retain

(f) Remove these items from the bracket of the rib 9 and cable bundle 2S/636VB, as

shown in Details A and T:

1 Clamp Item (21) Discard

1 Clamp MS21919WCH5 Item (21) Retain

1 Spacer NSA5527-03-02D Item (31) Retain

1 Spacer NSA5527-03-04D Item (32) Retain

1 Washer NAS1149D0332K Item (40) Retain

1 Screw NAS1096-3-27 Item (52) Retain

(g) Install this cable sleeve around these identified wires from the cable bundle

2S/636VB, as shown in Details A, C, E, G, J, L, N, Q, R, S and T:

Wire number 2842-5061

Wire number 2842-5062

Wire number 2842-5063

Wire number 2842-5064

Wire number 2842-5065

Wire number 2842-5071

3 Sleeve ABS0596S004 Item 1

and attach the cable sleeves with:

3 Spacer NSA5527-03-03 Item 15

1 (ME) Cord NSA8420-2 Item 16

10 Tie NSA935401-03 Item 149

20 Tie-Cable NSA935401-04 Item 150

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 175

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SERVICE BULLETIN

(h) At one positions, install these items to the brackets between rib 10 and rib 11 and

between rib 11 and rib 12, cable sleeves, Item 1 and cable bundle 2S/636VB, as

shown in Details A and E:

2 Clamp MS21919WCH4 Item (22) Retained at

removal

1 Clamp MS21919WCH3 Item (23) Retained at

removal

1 Spacer NSA5527-03-01D Item (30) Retained at

removal

1 Spacer NSA5527-03-02D Item (31) Retained at

removal

1 Washer NSA935808-01 Item (112) Retained at

removal

1 Clamp NSA935807-06 Item (122) Retained at

removal

1 Clamp MS21919WCH9 Item 10

1 Spacer NSA5527-03-02D Item 31

1 Screw NAS1096-3-40 Item 121

(i) At two positions, install these items to the brackets between rib 10 and rib 11 and

between rib 11 and rib 12, cable sleeves, Item 1 and cable bundle 2S/636VB, as

shown in Details A and G:

6 Clamp MS21919WCH4 Item (22) Retained at

removal

4 Spacer NSA5527-03-01D Item (30) Retained at

removal

2 Washer NAS1149D0332K Item (40) Retained at

removal

2 Screw NAS1096-3-27 Item (52) Retained at

removal

2 Clamp MS21919WCH9 Item 10

(j) At two positions, install these items to the brackets of the rib 11, cable sleeves,

Item 1 and cable bundle 2S/636VB, as shown in Details A and J:

6 Clamp MS21919WCH4 Item (22) Retained at

removal

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 176

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SERVICE BULLETIN

2 Spacer NSA5527-03-01D Item (30) Retained at

removal

2 Spacer NSA5527-03-04D Item (32) Retained at

removal

2 Washer NAS1149D0332K Item (40) Retained at

removal

2 Screw NAS1096-3-22 Item (51) Retained at

removal

2 Clamp MS21919WCH9 Item 10

(k) At two positions, install these items to the brackets of the rib 10, cable sleeves,

Item 1 and cable bundle 2S/636VB, as shown in Details A and L:

2 Clamp MS21919WCH4 Item (22) Retained at

removal

2 Spacer NSA5527-03-01D Item (30) Retained at

removal

2 Washer NAS1149D0332K Item (40) Retained at

removal

2 Clamp MS21919WCH9 Item 10

2 Screw NAS1096-3-19 Item 14

(l) Install these items to the bracket between rib 9 and rib 10, cable sleeves, Item 1

and cable bundle 2S/636VB, as shown in Details A and Q:

3 Clamp MS21919WCH4 Item (22) Retained at

removal

1 Spacer NSA5527-03-01D Item (30) Retained at

removal

1 Spacer NSA5527-03-04D Item (32) Retained at

removal

1 Washer NAS1149D0332K Item (40) Retained at

removal

1 Screw NAS1096-3-22 Item (51) Retained at

removal

1 Clamp MS21919WCH9 Item 10

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 177

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SERVICE BULLETIN

(m) Install these items to the bracket of the rib 9, cable sleeves, Item 1 and cable

bundle 2S/636VB, as shown in Details A and Q:

1 Clamp MS21919WCH5 Item (21) Retained at

removal

1 Spacer NSA5527-03-02D Item (31) Retained at

removal

1 Spacer NSA5527-03-04D Item (32) Retained at

removal

1 Washer NAS1149D0332K Item (40) Retained at

removal

1 Screw NAS1096-3-27 Item (52) Retained at

removal

1 Clamp MS21919WCH9 Item 10

**CONF 007

(1) Subtask 282148-831-405-001 - Install a New Bracket on the Sub Spar Behind the

Front Spar Between RIB 8 and RIB 9 on the RH Wing

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills AIRFRAME

Material necessary to do the job

Kit 282148B01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 A5725068600000 1 Bracket

2 ASNA0078A502 2 Rivet

Consumable CMLB01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Corrosion Inhibiting Low

Adhesion Sealant

09-018 As required

Solvent General Purpose 11-026 As required

Lint-Free Cotton Cloth 19-003 As required

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 178

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SERVICE BULLETIN

References

Fig. A-UBAAA

Location of Bracket on the Sub Spar

Behind the Front Spar Between RIB 8

and RIB 9 (RH Wing)

Sheet 01

Refer to Fig. A-UBAAA Sheet 01

(a) Remove from the sub spar behind the front spar between RIB 8 and RIB 9 on the

RH wing, the items that follow:

2 Rivet NSA54213510DCA Item (2) Discard

1 Bracket A5724630400000 Item (1) Discard

(b) Clean the mating surfaces use

Lint-Free Cotton

Cloth

19-003 As required

made moist with

Solvent General

Purpose

11-026 As required

(c) Put the

1 Bracket A5725068600000 Item 1

in position on the sub spar behind the front spar between RIB 8 and RIB 9 on the

RH wing (Refer to Fig. A-UBAAA Sheet 01).

(d) Copy drill the two holes from the sub spar through the Bracket, Item 1 to a

dimension of between 4.060 and 4.160 mm (0.160 and 0.164 in.).

(e) Deburr the holes that have been worked.

(f) Use

Corrosion Inhibiting

Low Adhesion

Sealant

09-018 As required

and wet install the

1 Bracket A5725068600000 Item 1

with the

2 Rivet, Blind ASNA0078A502 Item 2

on the sub spar behind the front spar between RIB 8 and RIB 9 on the RH wing.

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 179

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SERVICE BULLETIN

(2) Subtask 282148-831-004-001 - Install cable sleeves in the RH Electronics Rack

90VU.

Manpower Resources

Manhours 6.00

Minimum number of person 1

Subtask elapsed time 6.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 282148A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 ABS0596S004 2000 (mm) SLEEVE

NSA935401-04 50 TIE

References

Fig. A-FCAAA

Installation of Cable Sleeves in the RH

Electronics Rack 90VU.

Sheet 01

Fig. A-FWAAA

Installation of Cable Sleeves in the RH

Electronics Rack 90VU.

Sheet 01

NOTE: The sleeves ABS0596S004 and ABS0596S006 are supplied in pieces of

1000 mm (39.370 inches), cut or assemble these pieces to get the

correct length.

NOTE: The lengths of the sleeves given in this Service Bulletin are approximate

lengths. Adapt the lengths of the sleeves in relation to the aircraft

configuration.

NOTE: Before you install a sleeve, cut and discard the cable ties around the

cable bundle to install the sleeve correctly around the cable bundle.

(a) On the Shelf 92VU, only around the wires identified in figure Fig. A-FWAAA Sheet

01, from the equipment 15QT-B to the connector 2354VC, install:

1600 (mm) Sleeve ABS0596S004 Item 1

(b) Around the cable bundle of the connector 2354VC-A, install:

400 (mm) Sleeve ABS0596S004 Item 1

(c) Attach the sleeves with:

50 Tie-Cable NSA935401-04

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 180

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@A310

SERVICE BULLETIN

(3) Subtask 282148-831-005-001 - Install cable sleeves between FR38.2 and FR39, in

the forward cargo compartment.

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 282148A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

2 ABS0596S006 1000 (mm) SLEEVE

NSA935401-05 50 TIE

References

Fig. A-FCBAA

Installation of Cable Sleeves in the

Forward Cargo Compartment.

Sheet 01

NOTE: The sleeves ABS0596S004 and ABS0596S006 are supplied in pieces of

1000 mm (39.370 inches), cut or assemble these pieces to get the

correct length.

NOTE: The lengths of the sleeves given in this Service Bulletin are approximate

lengths. Adapt the lengths of the sleeves in relation to the aircraft

configuration.

NOTE: Before you install a sleeve, cut and discard the cable ties around the

cable bundle to install the sleeve correctly around the cable bundle.

(a) Around the cable bundle of the pressure seal 20VP, install:

1000 (mm) Sleeve ABS0596S006 Item 2

(b) Attach the sleeves with:

50 Tie-Cable NSA935401-05

(4) Subtask 282148-831-006-002 - Install cable sleeves in the RH forward wing root

and krueger flap.

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills NON SPECIFIC

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 181

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@A310

SERVICE BULLETIN

Material necessary to do the job

Kit 282148A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

2 ABS0596S006 SLEEVE

NSA935401-05 TIE

References

Fig. A-FCCAB

Installation of Cable Sleeves in the RH

forward wing root and krueger flap.

Sheet 01

NOTE: The sleeves ABS0596S004 and ABS0596S006 are supplied in pieces of

1000 mm (39.370 inches), cut or assemble these pieces to get the

correct length.

NOTE: The lengths of the sleeves given in this Service Bulletin are approximate

lengths. Adapt the lengths of the sleeves in relation to the aircraft

configuration.

NOTE: Before you install a sleeve, cut and discard the cable ties around the

cable bundle to install the sleeve correctly around the cable bundle.

(a) Around the cable bundle of the pressure seal 20VP, install:

1000 (mm) Sleeve ABS0596S006 Item 2

(b) Attach the sleeves with:

50 Tie-Cable NSA935401-05

(5) Subtask 282148-831-208-003 - Install the cable sleeves in the RH-wing forward of

the front spar between rib 2 and rib 3 in zone 612.

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

Material necessary to do the job

Kit 282148D01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 ABS0596S004 1 SLEEVE

11 MS21919WCH13 CLAMP

149 NSA935401-03 1 TIE

150 NSA935401-04 1 TIE

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 182

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@A310

SERVICE BULLETIN

Kit 282148D05R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

125 B9299071900200 1 EQUIPMNT

References

Fig. A-GBEAA

Improvement of the 2S-Route in the RHWing in Zone 612 (Kit D01)

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

Sheet 07

Sheet 08

NOTE (1): The sleeves ABS0596S004 is supplied in pieces of 1000 mm. Cut or

assemble these pieces to get the correct length.

NOTE (2): The lengths of the sleeves given in this Service Bulletin are approximate

lengths. Adapt the lengths of the sleeves in relation to the aircraft

configuration.

NOTE (3): Before you install a sleeve, cut and discard the cable ties around the

cable bundle to install the sleeve correctly around the cable bundle.

NOTE (4): Adapt the number of cable ties to the required quantity.

Refer to Fig. A-GBEAA Sheet 01, Fig. A-GBEAA Sheet 02, Fig. A-GBEAA Sheet 03, Fig.

A-GBEAA Sheet 04, Fig. A-GBEAA Sheet 05, Fig. A-GBEAA Sheet 06, Fig. A-GBEAA

Sheet 07 and Fig. A-GBEAA Sheet 08

(a) Remove these items from the bracket of the rib 2 and cable bundle 2S/624VB, as

shown in Details A and B:

1 Clamp MS21919WCH4 Item (22) Retain

1 Clamp MS21919WCH3 Item (23) Retain

1 Spacer NSA5527-03-02D Item (31) Retain

1 Washer NAS1149D0332K Item (40) Retain

1 Screw NAS1096-3-21 Item (50) Retain

1 Clamp MS21919WCH10 Item (100) Retain

1 Clamp Item (100) Discard

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 183

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SERVICE BULLETIN

(b) Remove these items from the riblet and cable bundle 2S/624VB, as shown in

Details A and D:

1 Clamp MS21919WCH4 Item (22) Retain

3 Spacer NSA5527-03-02D Item (31) Retain

1 Washer NAS1149D0332K Item (40) Retain

1 Screw NAS1096-3-38 Item (54) Retain

1 Clamp Item (100) Discard

(c) Install this cable sleeve around these identified wires from the cable bundle

2S/624VB, as shown in Details A, C and F:

Wire number 2842-5052

Wire number 2842-5053

Wire number 2842-5054

Wire number 2842-5055

Wire number 2842-5056

Wire number 2842-5070

1 Sleeve ABS0596S004 Item 1

and attach the cable sleeve with:

1 Tie NSA935401-03 Item 149

1 Tie-Cable NSA935401-04 Item 150

and

1 Placard set B9299071900200 Item 125

as necessary.

(d) Install these items to the bracket of the rib 2, cable bundle 2S/624VB and cable

sleeve, Item 1, as shown in Details A and C:

1 Clamp MS21919WCH4 Item (22) Retained at

removal

1 Clamp MS21919WCH3 Item (23) Retained at

removal

1 Spacer NSA5527-03-02D Item (31) Retained at

removal

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 184

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@A310

SERVICE BULLETIN

1 Washer NAS1149D0332K Item (40) Retained at

removal

1 Screw NAS1096-3-21 Item (50) Retained at

removal

1 Clamp MS21919WCH10 Item (100) Retained at

removal

1 Clamp MS21919WCH13 Item 11

(e) Install these items to the riblet, cable bundle 2S/624VB and cable sleeve, Item 1,

as shown in Details A and E:

1 Clamp MS21919WCH4 Item (22) Retained at

removal

3 Spacer NSA5527-03-02D Item (31) Retained at

removal

1 Washer NAS1149D0332K Item (40) Retained at

removal

1 Screw NAS1096-3-38 Item (54) Retained at

removal

1 Clamp MS21919WCH13 Item 11

(6) Subtask 282148-831-209-003 - Install the cable sleeves in the RH-wing forward of

the front spar between rib 7 and rib 8 in zone 612.

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

Material necessary to do the job

Kit 282148D01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 ABS0596S004 2 SLEEVE

12 MS21919WCH14 CLAMP

149 NSA935401-03 2 TIE

150 NSA935401-04 2 TIE

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 185

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SERVICE BULLETIN

References

Fig. A-GBEAA

Improvement of the 2S-Route in the RHWing in Zone 612 (Kit D01)

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

Sheet 07

Sheet 08

NOTE (1): The sleeves ABS0596S004 is supplied in pieces of 1000 mm. Cut or

assemble these pieces to get the correct length.

NOTE (2): The lengths of the sleeves given in this Service Bulletin are approximate

lengths. Adapt the lengths of the sleeves in relation to the aircraft

configuration.

NOTE (3): Before you install a sleeve, cut and discard the cable ties around the

cable bundle to install the sleeve correctly around the cable bundle.

NOTE (4): Adapt the number of cable ties to the required quantity.

Refer to Fig. A-GBEAA Sheet 01, Fig. A-GBEAA Sheet 02, Fig. A-GBEAA Sheet 03, Fig.

A-GBEAA Sheet 04, Fig. A-GBEAA Sheet 05, Fig. A-GBEAA Sheet 06, Fig. A-GBEAA

Sheet 07 and Fig. A-GBEAA Sheet 08

(a) Remove these items from the two brackets of the riblets and cable bundle

2S/624VB, as shown in Details A, H and K:

2 Clamp MS21919WCH4 Item (22) Retain

2 Washer NAS1149D0332K Item (40) Retain

2 Screw NAS1096-3-8 Item (55) Retain

2 Clamp Item (100) Discard

(b) Install this cable sleeve around these identified wires from the cable bundle

2S/624VB, as shown in Details A, J, K, L, M and N:

Wire number 2842-5052

Wire number 2842-5053

Wire number 2842-5054

Wire number 2842-5055

Wire number 2842-5056

1 Sleeve ABS0596S004 Item 1

and attach the cable sleeves with:

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 186

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SERVICE BULLETIN

1 Tie NSA935401-03 Item 149

1 Tie-Cable NSA935401-04 Item 150

(c) Install this cable sleeve around this identified wire from the cable bundle 2S/624VB,

as shown in Details A, J, K, L, M and N:

Wire number 2842-5070

1 Sleeve ABS0596S004 Item 1

and attach the cable sleeves with:

1 Tie NSA935401-03 Item 149

1 Tie-Cable NSA935401-04 Item 150

(d) Install these items to the two brackets of the riblets, cable bundle 2S/624VB and

cable sleeves, Item 1, as shown in Detail A, J and L:

2 Clamp MS21919WCH4 Item (22) Retained at

removal

2 Washer NAS1149D0332K Item (40) Retained at

removal

2 Screw NAS1096-3-8 Item (55) Retained at

removal

2 Clamp MS21919WCH14 Item 12

(7) Subtask 282148-831-210-003 - Install the cable sleeves in the RH-wing forward of

the front spar between rib 8 and rib 9 (pylon area) in zone 612.

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

Material necessary to do the job

Kit 282148D05R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 ABS0596S004 3 SLEEVE

30 NSA5527-03-01D 2 SPACER

31 NSA5527-03-02D 1 SPACER

109 NSA935805-09 3 (ME) CONDUIT

117 NSA935807C09 12 CLAMP

126 NSA938184PV1601 15 PIN

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 187

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@A310

SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

135 NAS1096-3-42 1 SCREW

136 NAS1096-3-30 1 SCREW

149 NSA935401-03 30 TIE

150 NSA935401-04 30 TIE

References

Fig. A-GBJAA

Improvement of the 2S-Route in the RHWing Pylon Area (Kit D05)

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

Sheet 07

Sheet 08

Sheet 09

Fig. A-GHAAA

Hook-up Chart

Sheet 01

Fig. A-GHBAA

Hook-up Chart

Sheet 01

NOTE (1): The sleeves ABS0596S004 is supplied in pieces of 1000 mm. Cut or

assemble these pieces to get the correct length.

NOTE (2): The lengths of the sleeves given in this Service Bulletin are approximate

lengths. Adapt the lengths of the sleeves in relation to the aircraft

configuration.

NOTE (3): Before you install a sleeve, cut and discard the cable ties around the

cable bundle to install the sleeve correctly around the cable bundle.

NOTE (4): Adapt the number of cable ties to the required quantity.

Refer to Fig. A-GBJAA Sheet 01, Fig. A-GBJAA Sheet 02, Fig. A-GBJAA Sheet 03, Fig.

A-GBJAA Sheet 04, Fig. A-GBJAA Sheet 05, Fig. A-GBJAA Sheet 06, Fig. A-GBJAA

Sheet 07, Fig. A-GBJAA Sheet 08 and Fig. A-GBJAA Sheet 09

Refer to Fig. A-GHAAA Sheet 01 and Fig. A-GHBAA Sheet 01

(a) Disconnect these wires of route 2S from the receptacles 40VC and 5006VC in

accordance with the Hook-up Chart 1, Lines 1 thru 14, END 1, Fig. A-GHAAA

Sheet 01 and the Hook-up Chart 2, Lines 2 thru 8, END 1, Fig. A-GHBAA Sheet

01.

(b) Remove, refer to Fig. A-GBJAA Sheet 03, Detail C, BEFORE:

2 Spacer NSA5527-03-05D Item (30) Discard

1 Washer NSA935808-01 Item (112) Retain

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 188

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SERVICE BULLETIN

1 Nut NAS1291C3M Item (116) Retain

1 Clamp NSA935807C10 Item (117) Discard

1 Screw Item (136) Discard

(c) Remove, refer to Fig. A-GBJAA Sheet 04, Detail E, BEFORE:

1 Washer NSA935808-01 Item (112) Retain

1 Screw Item (113) Retain

1 Clamp NSA935807C10 Item (117) Discard

(d) Remove, refer to Fig. A-GBJAA Sheet 05, Detail G, BEFORE:

2 Washer NSA935808-01 Item (112) Retain

2 Screw Item (113) Retain

2 Clamp NSA935807C10 Item (117) Discard

(e) Remove, refer to Fig. A-GBJAA Sheet 06, Detail J, BEFORE:

1 Spacer NSA5527-03-05D Item (30) Discard

1 Washer NSA935808-01 Item (112) Retain

1 Clamp NSA935807C10 Item (117) Discard

1 Screw Item (135) Retain

(f) Remove, refer to Fig. A-GBJAA Sheet 07, Detail L, BEFORE:

1 Washer NSA935808-01 Item (112) Retain

1 Screw Item (113) Retain

1 Clamp NSA935807C10 Item (117) Discard

(g) Remove, refer to Fig. A-GBJAA Sheet 08, Detail N, BEFORE:

1 Washer NSA935808-01 Item (112) Retain

1 Screw Item (113) Retain

1 Clamp NSA935807C10 Item (117) Discard

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 189

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SERVICE BULLETIN

(h) Remove the protection sleeve from the cable harness as shown Fig. A-GBJAA

Sheet 01, Fig. A-GBJAA Sheet 02, Fig. A-GBJAA Sheet 03, Fig. A-GBJAA Sheet

04, Fig. A-GBJAA Sheet 05, Fig. A-GBJAA Sheet 06, Fig. A-GBJAA Sheet 07, Fig.

A-GBJAA Sheet 08 and Fig. A-GBJAA Sheet 09, Details A, C, E, G, J, L and N:

1 Sleeve NSA935805-10 Item (1) Discard

(i) Cut the conduit to the required length and install as shown Refer to Fig. A-GBJAA

Sheet 01, Fig. A-GBJAA Sheet 02, Fig. A-GBJAA Sheet 03, Fig. A-GBJAA Sheet

04, Fig. A-GBJAA Sheet 05, Fig. A-GBJAA Sheet 06, Fig. A-GBJAA Sheet 07, Fig.

A-GBJAA Sheet 08 and Fig. A-GBJAA Sheet 09, Details B, D, F, H, K, M, P and Q:

3 Sleeve ABS0596S004 Item 1

3 (ME) Conduit NSA935805-09 Item 109

1 One part 1500.0 mm (59.06 in.) to the electrical wires for 10QT-A and 10QT-B

of route 2S/636VB, refer to the Hook-up Chart 2, Fig. A-GHBAA Sheet 01

(j) Connect the electrical wires of route 2S to the receptacles 40VC and 5006VC in

accordance with the Hook-up Chart 1, Lines 1 thru 14, END 1, Fig. A-GHAAA

Sheet 01 and the Hook-up Chart 2, lines 2 thru 8, END 1, Fig. A-GHBAA Sheet 01.

Use the contact pins if required:

15 Pin NSA938184PV1601 Item 126

(k) Install, refer to Fig. A-GBJAA Sheet 08, Detail P, AFTER:

1 Washer NSA935808-01 Item (112) Retained at

removal

1 Screw Item (113) Retained at

removal

2 Clamp NSA935807C09 Item 117

(l) Install, refer to Fig. A-GBJAA Sheet 07, Detail M, AFTER:

1 Washer NSA935808-01 Item (112) Retained at

removal

1 Screw Item (113) Retained at

removal

2 Clamp NSA935807C09 Item 117

(m) Install, refer to Fig. A-GBJAA Sheet 06, Detail K, AFTER:

1 Spacer NSA5527-03-02D Item 31

1 Washer NSA935808-01 Item (112) Retained at

removal

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 190

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SERVICE BULLETIN

2 Clamp NSA935807C09 Item 117

1 Screw NAS1096-3-42 Item 135

(n) Install, refer to Fig. A-GBJAA Sheet 05, Detail H, AFTER:

2 Washer NSA935808-01 Item (112) Retained at

removal

2 Screw Item (113) Retained at

removal

4 Clamp NSA935807C09 Item 117

(o) Install, refer to Fig. A-GBJAA Sheet 04, Detail F, AFTER:

1 Washer NSA935808-01 Item (112) Retained at

removal

1 Screw Item (113) Retained at

removal

2 Clamp NSA935807C09 Item 117

(p) Install, refer to Fig. A-GBJAA Sheet 03, Detail D, AFTER:

2 Spacer NSA5527-03-01D Item 30

2 Washer NSA935808-01 Item (112) Retained at

removal

2 Nut NAS1291C3M Item (116) Retained at

removal

2 Clamp NSA935807C09 Item 117

1 Screw NAS1096-3-30 Item 136

(q) Protect the electrical wires for 10QT-A and 10QT-B of route 2S/636VB, refer to Fig.

A-GBJAA Sheet 09, Detail Q, and the Hook-up Chart 2, Fig. A-GHBAA Sheet 01

with:

30 Tie NSA935401-03 Item 149

30 Tie-Cable NSA935401-04 Item 150

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 191

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SERVICE BULLETIN

(8) Subtask 282148-831-211-003 - Install the cable sleeves in the RH-wing forward of

the front spar between rib 9 and rib 12 in zone 623.

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

Material necessary to do the job

Kit 282148D01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 ABS0596S004 3 SLEEVE

10 MS21919WCH9 CLAMP

14 NAS1096-3-19 2 SCREW

15 NSA5527-03-03 3 SPACER

16 NSA8420-2 1 (ME) CORD

149 NSA935401-03 10 TIE

150 NSA935401-04 20 TIE

Kit 282148D05R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

31 NSA5527-03-02D SPACER

135 NAS1096-3-42 SCREW

References

Fig. A-GBFAA

Improvement of the 2S-Route in the RHWing in Zone 623 (Kit D01)

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

Sheet 07

Sheet 08

Sheet 09

Sheet 10

NOTE (1): The sleeve ABS0596S004 is supplied in pieces of 1000 mm. Cut or

assemble these pieces to get the correct length.

NOTE (2): The lengths of the sleeves given in this Service Bulletin are approximate

lengths. Adapt the lengths of the sleeves in relation to the aircraft

configuration.

NOTE (3): Before you install a sleeve, cut and discard the cable ties around the

cable bundle to install the sleeve correctly around the cable bundle.

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 192

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SERVICE BULLETIN

NOTE (4): Adapt the number of cable ties to the required quantity.

Refer to Refer to Fig. A-GBFAA Sheet 01, Fig. A-GBFAA Sheet 02, Fig. A-GBFAA

Sheet 03, Fig. A-GBFAA Sheet 04, Fig. A-GBFAA Sheet 05, Fig. A-GBFAA Sheet 06,

Fig. A-GBFAA Sheet 07, Fig. A-GBFAA Sheet 08, Fig. A-GBFAA Sheet 09 and Fig. AGBFAA Sheet 10

(a) At one position, remove these items from the bracket between rib 11 and rib 12

and cable bundle 2S/636VB, as shown in Details A and D:

2 Clamp MS21919WCH4 Item (22) Retain

1 Clamp MS21919WCH4 Item (22) Discard

1 Clamp MS21919WCH3 Item (23) Retain

1 Spacer NSA5527-03-01D Item (30) Retain

1 Spacer NSA5527-03-02D Item (31) Retain

2 Washer NSA935808-01 Item (112) Retain

2 Screw NAS1096-3-30 Item (121) Discard

1 Clamp NSA935807-06 Item (122) Retain

(b) At two positions, remove these items from the brackets between rib 10 and rib 11

and between rib 11 and rib 12 and cable bundle 2S/636VB, as shown in Details A

and F:

2 Clamp Item (22) Discard

6 Clamp MS21919WCH4 Item (22) Retain

4 Spacer NSA5527-03-01D Item (30) Retain

2 Washer NAS1149D0332K Item (40) Retain

2 Screw NAS1096-3-27 Item (52) Retain

(c) At two positions, remove these items from the brackets of the rib 11 and cable

bundle 2S/636VB, as shown in Details A and H:

6 Clamp MS21919WCH4 Item (22) Retain

2 Clamp Item (23) Discard

2 Spacer NSA5527-03-01D Item (30) Retain

2 Spacer NSA5527-03-04D Item (32) Retain

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 193

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@A310

SERVICE BULLETIN

2 Washer NAS1149D0332K Item (40) Retain

2 Screw NAS1096-3-22 Item (51) Retain

(d) At two positions, remove these items from the brackets of the rib 10 and cable

bundle 2S/636VB, as shown in Details A and K:

2 Clamp Item (22) Discard

2 Clamp MS21919WCH4 Item (22) Retain

2 Spacer NSA5527-03-01D Item (30) Retain

2 Spacer Item (32) Discard

2 Washer NAS1149D0332K Item (40) Retain

2 Screw Item (51) Discard

(e) Remove these items from the bracket between rib 9 and rib 10 and cable bundle

2S/636VB, as shown in Details A and M:

3 Clamp MS21919WCH4 Item (22) Retain

1 Clamp Item (23) Discard

1 Spacer NSA5527-03-01D Item (30) Retain

1 Spacer NSA5527-03-04D Item (32) Retain

1 Washer NAS1149D0332K Item (40) Retain

1 Screw NAS1096-3-22 Item (51) Retain

(f) Remove these items from the bracket of the rib 9 and cable bundle 2S/636VB, as

shown in Details A and T:

1 Clamp Item (21) Discard

1 Clamp MS21919WCH5 Item (21) Retain

1 Spacer NSA5527-03-02D Item (31) Retain

1 Spacer NSA5527-03-04D Item (32) Retain

1 Washer NAS1149D0332K Item (40) Retain

1 Screw NAS1096-3-27 Item (52) Retain

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 194

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@A310

SERVICE BULLETIN

(g) Install this cable sleeve around these identified wires from the cable bundle

2S/636VB, as shown in Details A, C, E, G, J, L, N, Q and R:

Wire number 2842-5061

Wire number 2842-5062

Wire number 2842-5063

Wire number 2842-5064

Wire number 2842-5065

Wire number 2842-5071

3 Sleeve ABS0596S004 Item 1

and attach the cable sleeves with:

3 Spacer NSA5527-03-03 Item 15

1 (ME) Cord NSA8420-2 Item 16

10 Tie NSA935401-03 Item 149

20 Tie-Cable NSA935401-04 Item 150

(h) At one positions, install these items to the brackets between rib 10 and rib 11 and

between rib 11 and rib 12, cable sleeves, Item 1 and cable bundle 2S/636VB, as

shown in Details A and E:

2 Clamp MS21919WCH4 Item (22) Retained at

removal

1 Clamp MS21919WCH3 Item (23) Retained at

removal

1 Spacer NSA5527-03-01D Item (30) Retained at

removal

1 Spacer NSA5527-03-02D Item (31) Retained at

removal

1 Washer NSA935808-01 Item (112) Retained at

removal

1 Clamp NSA935807-06 Item (122) Retained at

removal

1 Clamp MS21919WCH9 Item 10

1 Spacer NSA5527-03-02D Item 31

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 195

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@A310

SERVICE BULLETIN

1 Screw NAS1096-3-42 Item 135

(i) At two positions, install these items to the brackets between rib 10 and rib 11 and

between rib 11 and rib 12, cable sleeves, Item 1 and cable bundle 2S/636VB, as

shown in Details A and G:

6 Clamp MS21919WCH4 Item (22) Retained at

removal

4 Spacer NSA5527-03-01D Item (30) Retained at

removal

2 Washer NAS1149D0332K Item (40) Retained at

removal

2 Screw NAS1096-3-27 Item (52) Retained at

removal

2 Clamp MS21919WCH9 Item 10

(j) At two positions, install these items to the brackets of the rib 11, cable sleeves,

Item 1 and cable bundle 2S/636VB, as shown in Details A and J:

2 Clamp MS21919WCH4 Item (22) Retained at

removal

1 Spacer NSA5527-03-01D Item (30) Retained at

removal

1 Spacer NSA5527-03-04D Item (32) Retained at

removal

1 Washer NAS1149D0332K Item (40) Retained at

removal

1 Screw NAS1096-3-22 Item (51) Retained at

removal

1 Clamp MS21919WCH9 Item 10

(k) At two positions, install these items to the brackets of the rib 10, cable sleeves,

Item 1 and cable bundle 2S/636VB, as shown in Details A and L:

2 Clamp MS21919WCH4 Item (22) Retained at

removal

2 Spacer NSA5527-03-01D Item (30) Retained at

removal

2 Washer NAS1149D0332K Item (40) Retained at

removal

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 196

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@A310

SERVICE BULLETIN

2 Clamp MS21919WCH9 Item 10

2 Screw NAS1096-3-19 Item 14

(l) Install these items to the bracket between rib 9 and rib 10, cable sleeves, Item 1

and cable bundle 2S/636VB, as shown in Details A and N:

3 Clamp MS21919WCH4 Item (22) Retained at

removal

1 Spacer NSA5527-03-01D Item (30) Retained at

removal

1 Spacer NSA5527-03-04D Item (32) Retained at

removal

1 Washer NAS1149D0332K Item (40) Retained at

removal

1 Screw NAS1096-3-22 Item (51) Retained at

removal

1 Clamp MS21919WCH9 Item 10

(m) Install these items to the bracket of the rib 9, cable sleeves, Item 1 and cable

bundle 2S/636VB, as shown in Details A and Q:

1 Clamp MS21919WCH5 Item (21) Retained at

removal

1 Spacer NSA5527-03-02D Item (31) Retained at

removal

1 Spacer NSA5527-03-04D Item (32) Retained at

removal

1 Washer NAS1149D0332K Item (40) Retained at

removal

1 Screw NAS1096-3-27 Item (52) Retained at

removal

1 Clamp MS21919WCH9 Item 10

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 197

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@A310

SERVICE BULLETIN

**CONF 008

(1) Subtask 282148-831-405-001 - Install a New Bracket on the Sub Spar Behind the

Front Spar Between RIB 8 and RIB 9 on the RH Wing

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills AIRFRAME

Material necessary to do the job

Kit 282148B01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 A5725068600000 1 Bracket

2 ASNA0078A502 2 Rivet

Consumable CMLB01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Corrosion Inhibiting Low

Adhesion Sealant

09-018 As required

Solvent General Purpose 11-026 As required

Lint-Free Cotton Cloth 19-003 As required

References

Fig. A-UBAAA

Location of Bracket on the Sub Spar

Behind the Front Spar Between RIB 8

and RIB 9 (RH Wing)

Sheet 01

Refer to Fig. A-UBAAA Sheet 01

(a) Remove from the sub spar behind the front spar between RIB 8 and RIB 9 on the

RH wing, the items that follow:

2 Rivet NSA54213510DCA Item (2) Discard

1 Bracket A5724630400000 Item (1) Discard

(b) Clean the mating surfaces use

Lint-Free Cotton

Cloth

19-003 As required

made moist with

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 198

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SERVICE BULLETIN

Solvent General

Purpose

11-026 As required

(c) Put the

1 Bracket A5725068600000 Item 1

in position on the sub spar behind the front spar between RIB 8 and RIB 9 on the

RH wing (Refer to Fig. A-UBAAA Sheet 01).

(d) Copy drill the two holes from the sub spar through the Bracket, Item 1 to a

dimension of between 4.060 and 4.160 mm (0.160 and 0.164 in.).

(e) Deburr the holes that have been worked.

(f) Use

Corrosion Inhibiting

Low Adhesion

Sealant

09-018 As required

and wet install the

1 Bracket A5725068600000 Item 1

with the

2 Rivet, Blind ASNA0078A502 Item 2

on the sub spar behind the front spar between RIB 8 and RIB 9 on the RH wing.

(2) Subtask 282148-831-004-001 - Install cable sleeves in the RH Electronics Rack

90VU.

Manpower Resources

Manhours 6.00

Minimum number of person 1

Subtask elapsed time 6.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 282148A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 ABS0596S004 2000 (mm) SLEEVE

NSA935401-04 50 TIE

References

Fig. A-FCAAA

Installation of Cable Sleeves in the RH

Electronics Rack 90VU.

Sheet 01

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 199

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SERVICE BULLETIN

References

Fig. A-FWAAA

Installation of Cable Sleeves in the RH

Electronics Rack 90VU.

Sheet 01

NOTE: The sleeves ABS0596S004 and ABS0596S006 are supplied in pieces of

1000 mm (39.370 inches), cut or assemble these pieces to get the

correct length.

NOTE: The lengths of the sleeves given in this Service Bulletin are approximate

lengths. Adapt the lengths of the sleeves in relation to the aircraft

configuration.

NOTE: Before you install a sleeve, cut and discard the cable ties around the

cable bundle to install the sleeve correctly around the cable bundle.

(a) On the Shelf 92VU, only around the wires identified in figure Fig. A-FWAAA Sheet

01, from the equipment 15QT-B to the connector 2354VC, install:

1600 (mm) Sleeve ABS0596S004 Item 1

(b) Around the cable bundle of the connector 2354VC-A, install:

400 (mm) Sleeve ABS0596S004 Item 1

(c) Attach the sleeves with:

50 Tie-Cable NSA935401-04

(3) Subtask 282148-831-005-001 - Install cable sleeves between FR38.2 and FR39, in

the forward cargo compartment.

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 282148A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

2 ABS0596S006 1000 (mm) SLEEVE

NSA935401-05 50 TIE

References

Fig. A-FCBAA

Installation of Cable Sleeves in the

Forward Cargo Compartment.

Sheet 01

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 200

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@A310

SERVICE BULLETIN

NOTE: The sleeves ABS0596S004 and ABS0596S006 are supplied in pieces of

1000 mm (39.370 inches), cut or assemble these pieces to get the

correct length.

NOTE: The lengths of the sleeves given in this Service Bulletin are approximate

lengths. Adapt the lengths of the sleeves in relation to the aircraft

configuration.

NOTE: Before you install a sleeve, cut and discard the cable ties around the

cable bundle to install the sleeve correctly around the cable bundle.

(a) Around the cable bundle of the pressure seal 20VP, install:

1000 (mm) Sleeve ABS0596S006 Item 2

(b) Attach the sleeves with:

50 Tie-Cable NSA935401-05

(4) Subtask 282148-831-006-002 - Install cable sleeves in the RH forward wing root

and krueger flap.

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 282148A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

2 ABS0596S006 SLEEVE

NSA935401-05 TIE

References

Fig. A-FCCAB

Installation of Cable Sleeves in the RH

forward wing root and krueger flap.

Sheet 01

NOTE: The sleeves ABS0596S004 and ABS0596S006 are supplied in pieces of

1000 mm (39.370 inches), cut or assemble these pieces to get the

correct length.

NOTE: The lengths of the sleeves given in this Service Bulletin are approximate

lengths. Adapt the lengths of the sleeves in relation to the aircraft

configuration.

NOTE: Before you install a sleeve, cut and discard the cable ties around the

cable bundle to install the sleeve correctly around the cable bundle.

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 201

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@A310

SERVICE BULLETIN

(a) Around the cable bundle of the pressure seal 20VP, install:

1000 (mm) Sleeve ABS0596S006 Item 2

(b) Attach the sleeves with:

50 Tie-Cable NSA935401-05

(5) Subtask 282148-831-208-004 - Install the cable sleeves in the RH-wing forward of

the front spar between rib 2 and rib 3 in zone 612.

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

Material necessary to do the job

Kit 282148D01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 ABS0596S004 1 SLEEVE

11 MS21919WCH13 CLAMP

149 NSA935401-03 1 TIE

150 NSA935401-04 1 TIE

Kit 282148D06R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

132 B9299071900600 1 EQUIPMNT

References

Fig. A-GBEAA

Improvement of the 2S-Route in the RHWing in Zone 612 (Kit D01)

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

Sheet 07

Sheet 08

NOTE (1): The sleeves ABS0596S004 is supplied in pieces of 1000 mm. Cut or

assemble these pieces to get the correct length.

NOTE (2): The lengths of the sleeves given in this Service Bulletin are approximate

lengths. Adapt the lengths of the sleeves in relation to the aircraft

configuration.

NOTE (3): Before you install a sleeve, cut and discard the cable ties around the

cable bundle to install the sleeve correctly around the cable bundle.

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 202

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SERVICE BULLETIN

NOTE (4): Adapt the number of cable ties to the required quantity.

Refer to Fig. A-GBEAA Sheet 01, Fig. A-GBEAA Sheet 02, Fig. A-GBEAA Sheet 03, Fig.

A-GBEAA Sheet 04, Fig. A-GBEAA Sheet 05, Fig. A-GBEAA Sheet 06, Fig. A-GBEAA

Sheet 07 and Fig. A-GBEAA Sheet 08

(a) Remove these items from the bracket of the rib 2 and cable bundle 2S/624VB, as

shown in Details A and B:

1 Clamp MS21919WCH4 Item (22) Retain

1 Clamp MS21919WCH3 Item (23) Retain

1 Spacer NSA5527-03-02D Item (31) Retain

1 Washer NAS1149D0332K Item (40) Retain

1 Screw NAS1096-3-21 Item (50) Retain

1 Clamp MS21919WCH10 Item (100) Retain

1 Clamp Item (100) Discard

(b) Remove these items from the riblet and cable bundle 2S/624VB, as shown in

Details A and D:

1 Clamp MS21919WCH4 Item (22) Retain

3 Spacer NSA5527-03-02D Item (31) Retain

1 Washer NAS1149D0332K Item (40) Retain

1 Screw NAS1096-3-38 Item (54) Retain

1 Clamp Item (100) Discard

(c) Install this cable sleeve around these identified wires from the cable bundle

2S/624VB, as shown in Details A, C, E and F:

Wire number 2842-5052

Wire number 2842-5053

Wire number 2842-5054

Wire number 2842-5055

Wire number 2842-5056

Wire number 2842-5070

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 203

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SERVICE BULLETIN

1 Sleeve ABS0596S004 Item 1

and attach the cable sleeve with:

1 Tie NSA935401-03 Item 149

1 Tie-Cable NSA935401-04 Item 150

and

1 Placard Set B9299071900600 Item 132

as necessary.

(d) Install these items to the bracket of the rib 2, cable bundle 2S/624VB and cable

sleeve, Item 1, as shown in Details A and C:

1 Clamp MS21919WCH4 Item (22) Retained at

removal

1 Clamp MS21919WCH3 Item (23) Retained at

removal

1 Spacer NSA5527-03-02D Item (31) Retained at

removal

1 Washer NAS1149D0332K Item (40) Retained at

removal

1 Screw NAS1096-3-21 Item (50) Retained at

removal

1 Clamp MS21919WCH10 Item (100) Retained at

removal

1 Clamp MS21919WCH13 Item 11

(e) Install these items to the riblet, cable bundle 2S/624VB and cable sleeve, Item 1,

as shown in Details A and E:

1 Clamp MS21919WCH4 Item (22) Retained at

removal

3 Spacer NSA5527-03-02D Item (31) Retained at

removal

1 Washer NAS1149D0332K Item (40) Retained at

removal

1 Screw NAS1096-3-38 Item (54) Retained at

removal

1 Clamp MS21919WCH13 Item 11

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 204

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@A310

SERVICE BULLETIN

(6) Subtask 282148-831-209-004 - Install the cable sleeves in the RH-wing forward of

the front spar between rib 7 and rib 8 in zone 612.

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

Material necessary to do the job

Kit 282148D01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 ABS0596S004 2 SLEEVE

12 MS21919WCH14 CLAMP

149 NSA935401-03 2 TIE

150 NSA935401-04 2 TIE

References

Fig. A-GBEAA

Improvement of the 2S-Route in the RHWing in Zone 612 (Kit D01)

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

Sheet 07

Sheet 08

NOTE (1): The sleeves ABS0596S004 is supplied in pieces of 1000 mm. Cut or

assemble these pieces to get the correct length.

NOTE (2): The lengths of the sleeves given in this Service Bulletin are approximate

lengths. Adapt the lengths of the sleeves in relation to the aircraft

configuration.

NOTE (3): Before you install a sleeve, cut and discard the cable ties around the

cable bundle to install the sleeve correctly around the cable bundle.

NOTE (4): Adapt the number of cable ties to the required quantity.

Refer to Fig. A-GBEAA Sheet 01, Fig. A-GBEAA Sheet 02, Fig. A-GBEAA Sheet 03, Fig.

A-GBEAA Sheet 04, Fig. A-GBEAA Sheet 05, Fig. A-GBEAA Sheet 06, Fig. A-GBEAA

Sheet 07 and Fig. A-GBEAA Sheet 08

(a) Remove these items from the two brackets of the riblets and cable bundle

2S/624VB, as shown in Details A, H and K:

2 Clamp MS21919WCH4 Item (22) Retain

2 Washer NAS1149D0332K Item (40) Retain

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 205

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SERVICE BULLETIN

2 Screw NAS1096-3-8 Item (55) Retain

2 Clamp Item (100) Discard

(b) Install this cable sleeve around these identified wires from the cable bundle

2S/624VB, as shown in Details A, J, K, L, M and N:

Wire number 2842-5052

Wire number 2842-5053

Wire number 2842-5054

Wire number 2842-5055

Wire number 2842-5056

1 Sleeve ABS0596S004 Item 1

and attach the cable sleeves with:

1 Tie NSA935401-03 Item 149

1 Tie-Cable NSA935401-04 Item 150

(c) Install this cable sleeve around this identified wire from the cable bundle 2S/624VB,

as shown in Details A, J, K, L, M and N:

Wire number 2842-5070

1 Sleeve ABS0596S004 Item 1

and attach the cable sleeves with:

1 Tie NSA935401-03 Item 149

1 Tie-Cable NSA935401-04 Item 150

(d) Install these items to the two brackets of the riblets, cable bundle 2S/624VB and

cable sleeves, Item 1, as shown in Detail A, J and L:

2 Clamp MS21919WCH4 Item (22) Retained at

removal

2 Washer NAS1149D0332K Item (40) Retained at

removal

2 Screw NAS1096-3-8 Item (55) Retained at

removal

2 Clamp MS21919WCH14 Item 12

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 206

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SERVICE BULLETIN

(7) Subtask 282148-831-210-004 - Install the cable sleeves in the RH-wing forward of

the front spar between rib 8 and rib 9 (pylon area) in zone 612.

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

Material necessary to do the job

Kit 282148D06R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 ABS0596S004 3 SLEEVE

31 NSA5527-03-02D 2 SPACER

109 NSA935805-09 1.5 (ME) CONDUIT

117 NSA935807C09 7 CLAMP

121 NAS1096-3-40 1 SCREW

123 NAS1801-3-31 2 SCREW

126 NSA938184PV1601 7 PIN

130 NSA5527-03-08D 1 SPACER

131 NSA5527-03-07D 1 SPACER

149 NSA935401-03 30 TIE

150 NSA935401-04 30 TIE

References

Fig. A-GBKAA

Improvement of the 2S-Route in the RHWing Pylon Area (Kit D06)

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

Sheet 07

Sheet 08

Sheet 09

Fig. A-GHBAA

Hook-up Chart

Sheet 01

NOTE (1): The sleeves ABS0596S004 is supplied in pieces of 1000 mm. Cut or

assemble these pieces to get the correct length.

NOTE (2): The lengths of the sleeves given in this Service Bulletin are approximate

lengths. Adapt the lengths of the sleeves in relation to the aircraft

configuration.

NOTE (3): Before you install a sleeve, cut and discard the cable ties around the

cable bundle to install the sleeve correctly around the cable bundle.

NOTE (4): Adapt the number of cable ties to the required quantity.

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 207

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SERVICE BULLETIN

Refer to Fig. A-GBKAA Sheet 01, Fig. A-GBKAA Sheet 02, Fig. A-GBKAA Sheet 03, Fig.

A-GBKAA Sheet 04, Fig. A-GBKAA Sheet 05, Fig. A-GBKAA Sheet 06, Fig. A-GBKAA

Sheet 07, Fig. A-GBKAA Sheet 08 and Fig. A-GBKAA Sheet 09

Refer to Fig. A-GHBAA Sheet 01

(a) Disconnect the wires of route 2S from the receptacles 40VC and 5006VC in

accordance with the Hook-up Chart 2, Lines 2 thru 8, END 1, Fig. A-GHBAA Sheet

01.

(b) Remove, refer to Fig. A-GBKAA Sheet 03, Detail C, BEFORE:

1 Washer NSA935808-01 Item (112) Retain

1 Screw NAS1096-3-23 Item (113) Retain

1 Nut NAS1291C3M Item (116) Retain

1 Washer AN960KD10l Item (124) Retain

(c) Remove, refer to Fig. A-GBKAA Sheet 04, Detail E, BEFORE:

1 Washer NSA935808-01 Item (112) Retain

1 Screw NAS1096-3-23 Item (113) Retain

(d) Remove, refer to Fig. A-GBKAA Sheet 05, Detail G, BEFORE:

2 Washer NSA935808-01 Item (112) Retain

2 Screw NAS1096-3-23 Item (113) Retain

(e) Remove, refer to Fig. A-GBKAA Sheet 06, Detail J, BEFORE:

1 Spacer NSA5527-03-02D Item (31) Retain

1 Screw Item (121) Discard

(f) Remove, refer to Fig. A-GBKAA Sheet 07, Detail L, BEFORE:

1 Screw Item (123) Discard

(g) Remove, refer to Fig. A-GBKAA Sheet 08, Detail N, BEFORE:

1 Screw Item (123) Discard

(h) Cut the conduit to the required length and install as shown Fig. A-GBKAA Sheet

01, Fig. A-GBKAA Sheet 02, Fig. A-GBKAA Sheet 03, Fig. A-GBKAA Sheet 04,

Fig. A-GBKAA Sheet 05, Fig. A-GBKAA Sheet 06, Fig. A-GBKAA Sheet 07, Fig. AGBKAA Sheet 08 and Fig. A-GBKAA Sheet 09, Details B and R:

3 Sleeve ABS0596S004 Item 1

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

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SERVICE BULLETIN

1.5 (ME) Conduit NSA935805-09 Item 109

1 One part 1500.0 mm (59.06 in.) to the electrical wires for 10QT-A and 10QT-B

of route 2S/636VB, refer to the Hook-up Chart 2, Fig. A-GHBAA Sheet 01

(i) Connect the electrical wires of route 2S to the receptacles 40VC and 5006VC in

accordance with the Hook-up Chart 2, Lines 2 thru 8, END 1, Fig. A-GHBAA Sheet

01. Use the contact pins if required:

7 Pin NSA938184PV1601 Item 126

(j) Install, refer to Fig. A-GBKAA Sheet 08, Detail P, AFTER:

1 Spacer NSA5527-03-02D Item 31

1 Clamp NSA935807C09 Item 117

1 Screw NAS1801-3-31 Item 123

1 Spacer NSA5527-03-07D Item 131

(k) Install, refer to Fig. A-GBKAA Sheet 07, Detail M, AFTER:

1 Clamp NSA935807C09 Item 117

1 Screw NAS1801-3-31 Item 123

1 Spacer NSA5527-03-08D Item 130

(l) Install, refer to Fig. A-GBKAA Sheet 06, Detail K, AFTER:

1 Spacer NSA5527-03-02D Item 31

1 Clamp NSA935807C09 Item 117

1 Screw NAS1096-3-40 Item 121

(m) Install, refer to Fig. A-GBKAA Sheet 05, Detail H, AFTER:

2 Washer NSA935808-01 Item (112) Retained at

removal

2 Screw NAS1096-3-23 Item (113) Retained at

removal

2 Clamp NSA935807C09 Item 117

(n) Install, refer to Fig. A-GBKAA Sheet 04, Detail F, AFTER:

1 Washer NSA935808-01 Item (112) Retained at

removal

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 209

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@A310

SERVICE BULLETIN

1 Screw NAS1096-3-23 Item (113) Retained at

removal

1 Clamp NSA935807C09 Item 117

(o) Install, refer to Fig. A-GBKAA Sheet 03, Detail D, AFTER:

1 Washer NSA935808-01 Item (112) Retained at

removal

1 Screw NAS1096-3-23 Item (113) Retained at

removal

1 Nut NAS1291C3M Item (116) Retained at

removal

1 Washer AN960KD10l Item (124) Retained at

removal

1 Clamp NSA935807C09 Item 117

(p) Protect the electrical wires for 10QT-A and 10QT-B of route 2S/636VB, refer to the

Hook-up Chart 2, Fig. A-GHBAA Sheet 01 and Fig. A-GBKAA Sheet 01, Fig. AGBKAA Sheet 02, Fig. A-GBKAA Sheet 03, Fig. A-GBKAA Sheet 04, Fig. AGBKAA Sheet 05, Fig. A-GBKAA Sheet 06, Fig. A-GBKAA Sheet 07, Fig. AGBKAA Sheet 08 and Fig. A-GBKAA Sheet 09, Detail Q with:

30 Tie NSA935401-03 Item 149

30 Tie-Cable NSA935401-04 Item 150

(8) Subtask 282148-831-211-004 - Install the cable sleeves in the RH-wing forward of

the front spar between rib 9 and rib 12 in zone 623.

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

Material necessary to do the job

Kit 282148D01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 ABS0596S004 3 SLEEVE

10 MS21919WCH9 CLAMP

14 NAS1096-3-19 SCREW

15 NSA5527-03-03 SPACER

16 NSA8420-2 CORD

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 210

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@A310

SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

150 NSA935401-04 1 TIE

Kit 282148D06R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

31 NSA5527-03-02D 2 SPACER

121 NAS1096-3-40 1 SCREW

References

Fig. A-GBFAA

Improvement of the 2S-Route in the RHWing in Zone 623 (Kit D01)

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

Sheet 07

Sheet 08

Sheet 09

Sheet 10

NOTE (1): The sleeve ABS0596S004 is supplied in pieces of 1000 mm. Cut or

assemble these pieces to get the correct length.

NOTE (2): The lengths of the sleeves given in this Service Bulletin are approximate

lengths. Adapt the lengths of the sleeves in relation to the aircraft

configuration.

NOTE (3): Before you install a sleeve, cut and discard the cable ties around the

cable bundle to install the sleeve correctly around the cable bundle.

NOTE (4): Adapt the number of cable ties to the required quantity.

Refer to Refer to Fig. A-GBFAA Sheet 01, Fig. A-GBFAA Sheet 02, Fig. A-GBFAA

Sheet 03, Fig. A-GBFAA Sheet 04, Fig. A-GBFAA Sheet 05, Fig. A-GBFAA Sheet 06,

Fig. A-GBFAA Sheet 07, Fig. A-GBFAA Sheet 08, Fig. A-GBFAA Sheet 09 and Fig. AGBFAA Sheet 10

(a) At one position, remove these items from the bracket between rib 11 and rib 12

and cable bundle 2S/636VB, as shown in Details A and D:

2 Clamp MS21919WCH4 Item (22) Retain

1 Clamp MS21919WCH4 Item (22) Discard

1 Clamp MS21919WCH3 Item (23) Retain

1 Spacer NSA5527-03-01D Item (30) Retain

1 Spacer NSA5527-03-02D Item (31) Retain

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 211

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@A310

SERVICE BULLETIN

1 Washer NSA935808-01 Item (112) Retain

1 Screw NAS1096-3-30 Item (121) Discard

1 Clamp NSA935807-06 Item (122) Retain

(b) At two positions, remove these items from the brackets between rib 10 and rib 11

and between rib 11 and rib 12 and cable bundle 2S/636VB, as shown in Details A

and F:

2 Clamp Item (22) Discard

6 Clamp MS21919WCH4 Item (22) Retain

4 Spacer NSA5527-03-01D Item (30) Retain

2 Washer NAS1149D0332K Item (40) Retain

2 Screw NAS1096-3-27 Item (52) Retain

(c) At two positions, remove these items from the brackets of the rib 11 and cable

bundle 2S/636VB, as shown in Details A and H:

6 Clamp MS21919WCH4 Item (22) Retain

2 Clamp Item (23) Discard

2 Spacer NSA5527-03-01D Item (30) Retain

2 Spacer NSA5527-03-04D Item (32) Retain

2 Washer NAS1149D0332K Item (40) Retain

2 Screw NAS1096-3-22 Item (51) Retain

(d) At two positions, remove these items from the brackets of the rib 10 and cable

bundle 2S/636VB, as shown in Details A and K:

2 Clamp Item (22) Discard

2 Clamp MS21919WCH4 Item (22) Retain

2 Spacer NSA5527-03-01D Item (30) Retain

2 Spacer Item (32) Discard

2 Washer NAS1149D0332K Item (40) Retain

2 Screw Item (51) Discard

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 212

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SERVICE BULLETIN

(e) Remove these items from the bracket between rib 9 and rib 10 and cable bundle

2S/636VB, as shown in Details A and M:

3 Clamp MS21919WCH4 Item (22) Retain

1 Clamp Item (23) Discard

1 Spacer NSA5527-03-01D Item (30) Retain

1 Spacer NSA5527-03-04D Item (32) Retain

1 Washer NAS1149D0332K Item (40) Retain

1 Screw NAS1096-3-22 Item (51) Retain

(f) Remove these items from the bracket of the rib 9 and cable bundle 2S/636VB, as

shown in Details A and T:

1 Clamp Item (21) Discard

1 Clamp MS21919WCH5 Item (21) Retain

1 Spacer NSA5527-03-02D Item (31) Retain

1 Spacer NSA5527-03-04D Item (32) Retain

1 Washer NAS1149D0332K Item (40) Retain

1 Screw NAS1096-3-27 Item (52) Retain

(g) Install this cable sleeve around these identified wires from the cable bundle

2S/636VB, as shown in Details A, C, E, G, J, L, N and R:

Wire number 2842-5061

Wire number 2842-5062

Wire number 2842-5063

Wire number 2842-5064

Wire number 2842-5065

Wire number 2842-5071

3 Sleeve ABS0596S004 Item 1

and attach the cable sleeves with:

3 Spacer NSA5527-03-03 Item 15

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 213

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1 (ME) Cord NSA8420-2 Item 16

1 Tie-Cable NSA935401-04 Item 150

(h) At one positions, install these items to the brackets between rib 10 and rib 11 and

between rib 11 and rib 12, cable sleeves, Item 1 and cable bundle 2S/636VB, as

shown in Details A and E:

2 Clamp MS21919WCH4 Item (22) Retained at

removal

1 Clamp MS21919WCH3 Item (23) Retained at

removal

1 Spacer NSA5527-03-01D Item (30) Retained at

removal

1 Spacer NSA5527-03-02D Item (31) Retained at

removal

1 Washer NSA935808-01 Item (112) Retained at

removal

1 Clamp NSA935807-06 Item (122) Retained at

removal

1 Clamp MS21919WCH9 Item 10

2 Spacer NSA5527-03-02D Item 31

1 Screw NAS1096-3-40 Item 121

(i) At two positions, install these items to the brackets between rib 10 and rib 11 and

between rib 11 and rib 12, cable sleeves, Item 1 and cable bundle 2S/636VB, as

shown in Details A and G:

6 Clamp MS21919WCH4 Item (22) Retained at

removal

4 Spacer NSA5527-03-01D Item (30) Retained at

removal

2 Washer NAS1149D0332K Item (40) Retained at

removal

2 Screw NAS1096-3-27 Item (52) Retained at

removal

2 Clamp MS21919WCH9 Item 10

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 214

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@A310

SERVICE BULLETIN

(j) At two positions, install these items to the brackets of the rib 11, cable sleeves,

Item 1 and cable bundle 2S/636VB, as shown in Details A and J:

2 Clamp MS21919WCH4 Item (22) Retained at

removal

1 Spacer NSA5527-03-01D Item (30) Retained at

removal

1 Spacer NSA5527-03-04D Item (32) Retained at

removal

1 Washer NAS1149D0332K Item (40) Retained at

removal

1 Screw NAS1096-3-22 Item (51) Retained at

removal

1 Clamp MS21919WCH9 Item 10

(k) At two positions, install these items to the brackets of the rib 10, cable sleeves,

Item 1 and cable bundle 2S/636VB, as shown in Details A and L:

2 Clamp MS21919WCH4 Item (22) Retained at

removal

2 Spacer NSA5527-03-01D Item (30) Retained at

removal

2 Washer NAS1149D0332K Item (40) Retained at

removal

2 Clamp MS21919WCH9 Item 10

2 Screw NAS1096-3-19 Item 14

(l) Install these items to the bracket between rib 9 and rib 10, cable sleeves, Item 1

and cable bundle 2S/636VB, as shown in Details A and Q:

3 Clamp MS21919WCH4 Item (22) Retained at

removal

1 Spacer NSA5527-03-01D Item (30) Retained at

removal

1 Spacer NSA5527-03-04D Item (32) Retained at

removal

1 Washer NAS1149D0332K Item (40) Retained at

removal

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 215

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@A310

SERVICE BULLETIN

1 Screw NAS1096-3-22 Item (51) Retained at

removal

1 Clamp MS21919WCH9 Item 10

(m) Install these items to the bracket of the rib 9, cable sleeves, Item 1 and cable

bundle 2S/636VB, as shown in Details A and Q:

1 Clamp MS21919WCH5 Item (21) Retained at

removal

1 Spacer NSA5527-03-02D Item (31) Retained at

removal

1 Spacer NSA5527-03-04D Item (32) Retained at

removal

1 Washer NAS1149D0332K Item (40) Retained at

removal

1 Screw NAS1096-3-27 Item (52) Retained at

removal

1 Clamp MS21919WCH9 Item 10

**CONF ALL

D. TEST

**CONF 001

(1) Subtask 282148-710-201-001 - Operational

Manpower Resources

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) 27-84-00, Page Block 501

28-42-44, Page Block 401

30-11-00, Page Block 501

36-11-00, Page Block 501

Elec. Std. Practices Manual (ESPM) 20-25-21

(a) Do a continuity test of disconnected wires (Refer to ESPM 20-25-21).

(b) Do an operational test of the cadensicon sensor (Refer to AMM 28-42-44, Page

Block 401).

(c) Do the operational test (Refer to AMM 27-84-00, Page Block 501).

(d) Do the operational test of the wing ice protection (Refer to AMM 30-11-00, Page

Block 501).

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 216

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@A310

SERVICE BULLETIN

(e) Do the bite test (Refer to AMM 36-11-00, Page Block 501).

**CONF 002

(1) Subtask 282148-710-201-001 - Operational

Manpower Resources

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) 27-84-00, Page Block 501

28-42-44, Page Block 401

30-11-00, Page Block 501

36-11-00, Page Block 501

Elec. Std. Practices Manual (ESPM) 20-25-21

(a) Do a continuity test of disconnected wires (Refer to ESPM 20-25-21).

(b) Do an operational test of the cadensicon sensor (Refer to AMM 28-42-44, Page

Block 401).

(c) Do the operational test (Refer to AMM 27-84-00, Page Block 501).

(d) Do the operational test of the wing ice protection (Refer to AMM 30-11-00, Page

Block 501).

(e) Do the bite test (Refer to AMM 36-11-00, Page Block 501).

**CONF 003

(1) Subtask 282148-710-201-001 - Operational

Manpower Resources

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) 27-84-00, Page Block 501

28-42-44, Page Block 401

30-11-00, Page Block 501

36-11-00, Page Block 501

Elec. Std. Practices Manual (ESPM) 20-25-21

(a) Do a continuity test of disconnected wires (Refer to ESPM 20-25-21).

(b) Do an operational test of the cadensicon sensor (Refer to AMM 28-42-44, Page

Block 401).

(c) Do the operational test (Refer to AMM 27-84-00, Page Block 501).

(d) Do the operational test of the wing ice protection (Refer to AMM 30-11-00, Page

Block 501).

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 217

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@A310

SERVICE BULLETIN

(e) Do the bite test (Refer to AMM 36-11-00, Page Block 501).

**CONF 004

(1) Subtask 282148-710-201-001 - Operational

Manpower Resources

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) 27-84-00, Page Block 501

28-42-44, Page Block 401

30-11-00, Page Block 501

36-11-00, Page Block 501

Elec. Std. Practices Manual (ESPM) 20-25-21

(a) Do a continuity test of disconnected wires (Refer to ESPM 20-25-21).

(b) Do an operational test of the cadensicon sensor (Refer to AMM 28-42-44, Page

Block 401).

(c) Do the operational test (Refer to AMM 27-84-00, Page Block 501).

(d) Do the operational test of the wing ice protection (Refer to AMM 30-11-00, Page

Block 501).

(e) Do the bite test (Refer to AMM 36-11-00, Page Block 501).

**CONF 005

(1) Subtask 282148-710-201-001 - Operational

Manpower Resources

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) 27-84-00, Page Block 501

28-42-44, Page Block 401

30-11-00, Page Block 501

36-11-00, Page Block 501

Elec. Std. Practices Manual (ESPM) 20-25-21

(a) Do a continuity test of disconnected wires (Refer to ESPM 20-25-21).

(b) Do an operational test of the cadensicon sensor (Refer to AMM 28-42-44, Page

Block 401).

(c) Do the operational test (Refer to AMM 27-84-00, Page Block 501).

(d) Do the operational test of the wing ice protection (Refer to AMM 30-11-00, Page

Block 501).

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 218

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@A310

SERVICE BULLETIN

(e) Do the bite test (Refer to AMM 36-11-00, Page Block 501).

**CONF 006

(1) Subtask 282148-710-201-001 - Operational

Manpower Resources

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) 27-84-00, Page Block 501

28-42-44, Page Block 401

30-11-00, Page Block 501

36-11-00, Page Block 501

Elec. Std. Practices Manual (ESPM) 20-25-21

(a) Do a continuity test of disconnected wires (Refer to ESPM 20-25-21).

(b) Do an operational test of the cadensicon sensor (Refer to AMM 28-42-44, Page

Block 401).

(c) Do the operational test (Refer to AMM 27-84-00, Page Block 501).

(d) Do the operational test of the wing ice protection (Refer to AMM 30-11-00, Page

Block 501).

(e) Do the bite test (Refer to AMM 36-11-00, Page Block 501).

**CONF 007

(1) Subtask 282148-710-201-001 - Operational

Manpower Resources

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) 27-84-00, Page Block 501

28-42-44, Page Block 401

30-11-00, Page Block 501

36-11-00, Page Block 501

Elec. Std. Practices Manual (ESPM) 20-25-21

(a) Do a continuity test of disconnected wires (Refer to ESPM 20-25-21).

(b) Do an operational test of the cadensicon sensor (Refer to AMM 28-42-44, Page

Block 401).

(c) Do the operational test (Refer to AMM 27-84-00, Page Block 501).

(d) Do the operational test of the wing ice protection (Refer to AMM 30-11-00, Page

Block 501).

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 219

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@A310

SERVICE BULLETIN

(e) Do the bite test (Refer to AMM 36-11-00, Page Block 501).

**CONF 008

(1) Subtask 282148-710-201-001 - Operational

Manpower Resources

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) 27-84-00, Page Block 501

28-42-44, Page Block 401

30-11-00, Page Block 501

36-11-00, Page Block 501

Elec. Std. Practices Manual (ESPM) 20-25-21

(a) Do a continuity test of disconnected wires (Refer to ESPM 20-25-21).

(b) Do an operational test of the cadensicon sensor (Refer to AMM 28-42-44, Page

Block 401).

(c) Do the operational test (Refer to AMM 27-84-00, Page Block 501).

(d) Do the operational test of the wing ice protection (Refer to AMM 30-11-00, Page

Block 501).

(e) Do the bite test (Refer to AMM 36-11-00, Page Block 501).

**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 282148-861-002-001 - Energize Electrical Network

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 24-31-11, Page Block 401

(a) Battery re-connection :

- For job set-up, refer to removal/installation of the batteries (Refer to AMM

24-31-11, Page Block 401),

- Remove the blanking cap from the electrical connectors,

- Make sure that the electrical connectors are clean and in correct condition,

- Connect the connector on the battery,

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 220

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@A310

SERVICE BULLETIN

- Turn the knurled nut a quarter turn.

(b) Remove all warning notices.

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

(2) Subtask 282148-942-009-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

06-41-57, Page Block 001

25-54-10, Page Block 201

52-10-00, Page Block 001

52-30-00, Page Block 001

53-10-55, Page Block 401

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

equipment.

(b) On the RH wing, install the access panel 613RR (Refer to AMM 06-41-57, Page

Block 001).

(c) In the forward cargo compartment, install the sidewall panel 132QW (Refer to AMM

06-41-53, Page Block 001 and AMM 25-54-10, Page Block 201).

(d) In the forward cargo compartment, at FR38.2, install the partition panel 132SW

(Refer to AMM 06-41-53, Page Block 001 and AMM 53-10-55, Page Block 401).

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

(f) Close the forward cargo compartment door 811 (Refer to AMM 52-30-00, Page

Block 001).

(g) Remove the access platform(s).

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

**CONF 002

(1) Subtask 282148-861-002-001 - Energize Electrical Network

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 24-31-11, Page Block 401

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 221

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@A310

SERVICE BULLETIN

(a) Battery re-connection :

- For job set-up, refer to removal/installation of the batteries (Refer to AMM

24-31-11, Page Block 401),

- Remove the blanking cap from the electrical connectors,

- Make sure that the electrical connectors are clean and in correct condition,

- Connect the connector on the battery,

- Turn the knurled nut a quarter turn.

(b) Remove all warning notices.

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

(2) Subtask 282148-942-009-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

06-41-57, Page Block 001

25-54-10, Page Block 201

52-10-00, Page Block 001

52-30-00, Page Block 001

53-10-55, Page Block 401

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

equipment.

(b) On the RH wing, install the access panel 613RR (Refer to AMM 06-41-57, Page

Block 001).

(c) In the forward cargo compartment, install the sidewall panel 132QW (Refer to AMM

06-41-53, Page Block 001 and AMM 25-54-10, Page Block 201).

(d) In the forward cargo compartment, at FR38.2, install the partition panel 132SW

(Refer to AMM 06-41-53, Page Block 001 and AMM 53-10-55, Page Block 401).

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

(f) Close the forward cargo compartment door 811 (Refer to AMM 52-30-00, Page

Block 001).

(g) Remove the access platform(s).

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

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 222

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@A310

SERVICE BULLETIN

**CONF 003

(1) Subtask 282148-861-002-001 - Energize Electrical Network

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 24-31-11, Page Block 401

(a) Battery re-connection :

- For job set-up, refer to removal/installation of the batteries (Refer to AMM

24-31-11, Page Block 401),

- Remove the blanking cap from the electrical connectors,

- Make sure that the electrical connectors are clean and in correct condition,

- Connect the connector on the battery,

- Turn the knurled nut a quarter turn.

(b) Remove all warning notices.

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

(2) Subtask 282148-942-009-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

06-41-57, Page Block 001

25-54-10, Page Block 201

52-10-00, Page Block 001

52-30-00, Page Block 001

53-10-55, Page Block 401

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

equipment.

(b) On the RH wing, install the access panel 613RR (Refer to AMM 06-41-57, Page

Block 001).

(c) In the forward cargo compartment, install the sidewall panel 132QW (Refer to AMM

06-41-53, Page Block 001 and AMM 25-54-10, Page Block 201).

(d) In the forward cargo compartment, at FR38.2, install the partition panel 132SW

(Refer to AMM 06-41-53, Page Block 001 and AMM 53-10-55, Page Block 401).

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

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 223

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@A310

SERVICE BULLETIN

(f) Close the forward cargo compartment door 811 (Refer to AMM 52-30-00, Page

Block 001).

(g) Remove the access platform(s).

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

**CONF 004

(1) Subtask 282148-861-002-001 - Energize Electrical Network

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 24-31-11, Page Block 401

(a) Battery re-connection :

- For job set-up, refer to removal/installation of the batteries (Refer to AMM

24-31-11, Page Block 401),

- Remove the blanking cap from the electrical connectors,

- Make sure that the electrical connectors are clean and in correct condition,

- Connect the connector on the battery,

- Turn the knurled nut a quarter turn.

(b) Remove all warning notices.

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

(2) Subtask 282148-942-009-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

06-41-57, Page Block 001

25-54-10, Page Block 201

52-10-00, Page Block 001

52-30-00, Page Block 001

53-10-55, Page Block 401

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

equipment.

(b) On the RH wing, install the access panel 613RR (Refer to AMM 06-41-57, Page

Block 001).

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 224

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@A310

SERVICE BULLETIN

(c) In the forward cargo compartment, install the sidewall panel 132QW (Refer to AMM

06-41-53, Page Block 001 and AMM 25-54-10, Page Block 201).

(d) In the forward cargo compartment, at FR38.2, install the partition panel 132SW

(Refer to AMM 06-41-53, Page Block 001 and AMM 53-10-55, Page Block 401).

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

(f) Close the forward cargo compartment door 811 (Refer to AMM 52-30-00, Page

Block 001).

(g) Remove the access platform(s).

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

**CONF 005

(1) Subtask 282148-861-002-001 - Energize Electrical Network

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 24-31-11, Page Block 401

(a) Battery re-connection :

- For job set-up, refer to removal/installation of the batteries (Refer to AMM

24-31-11, Page Block 401),

- Remove the blanking cap from the electrical connectors,

- Make sure that the electrical connectors are clean and in correct condition,

- Connect the connector on the battery,

- Turn the knurled nut a quarter turn.

(b) Remove all warning notices.

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

(2) Subtask 282148-942-009-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 225

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@A310

SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

06-41-57, Page Block 001

25-54-10, Page Block 201

52-10-00, Page Block 001

52-30-00, Page Block 001

53-10-55, Page Block 401

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

equipment.

(b) On the RH wing, install the access panel 613RR (Refer to AMM 06-41-57, Page

Block 001).

(c) In the forward cargo compartment, install the sidewall panel 132QW (Refer to AMM

06-41-53, Page Block 001 and AMM 25-54-10, Page Block 201).

(d) In the forward cargo compartment, at FR38.2, install the partition panel 132SW

(Refer to AMM 06-41-53, Page Block 001 and AMM 53-10-55, Page Block 401).

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

(f) Close the forward cargo compartment door 811 (Refer to AMM 52-30-00, Page

Block 001).

(g) Remove the access platform(s).

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

**CONF 006

(1) Subtask 282148-861-002-001 - Energize Electrical Network

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 24-31-11, Page Block 401

(a) Battery re-connection :

- For job set-up, refer to removal/installation of the batteries (Refer to AMM

24-31-11, Page Block 401),

- Remove the blanking cap from the electrical connectors,

- Make sure that the electrical connectors are clean and in correct condition,

- Connect the connector on the battery,

- Turn the knurled nut a quarter turn.

(b) Remove all warning notices.

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 226

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@A310

SERVICE BULLETIN

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

(2) Subtask 282148-942-009-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

06-41-57, Page Block 001

25-54-10, Page Block 201

52-10-00, Page Block 001

52-30-00, Page Block 001

53-10-55, Page Block 401

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

equipment.

(b) On the RH wing, install the access panel 613RR (Refer to AMM 06-41-57, Page

Block 001).

(c) In the forward cargo compartment, install the sidewall panel 132QW (Refer to AMM

06-41-53, Page Block 001 and AMM 25-54-10, Page Block 201).

(d) In the forward cargo compartment, at FR38.2, install the partition panel 132SW

(Refer to AMM 06-41-53, Page Block 001 and AMM 53-10-55, Page Block 401).

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

(f) Close the forward cargo compartment door 811 (Refer to AMM 52-30-00, Page

Block 001).

(g) Remove the access platform(s).

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

**CONF 007

(1) Subtask 282148-861-002-001 - Energize Electrical Network

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 24-31-11, Page Block 401

(a) Battery re-connection :

- For job set-up, refer to removal/installation of the batteries (Refer to AMM

24-31-11, Page Block 401),

- Remove the blanking cap from the electrical connectors,

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 227

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@A310

SERVICE BULLETIN

- Make sure that the electrical connectors are clean and in correct condition,

- Connect the connector on the battery,

- Turn the knurled nut a quarter turn.

(b) Remove all warning notices.

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

(2) Subtask 282148-942-009-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

06-41-57, Page Block 001

25-54-10, Page Block 201

52-10-00, Page Block 001

52-30-00, Page Block 001

53-10-55, Page Block 401

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

equipment.

(b) On the RH wing, install the access panel 613RR (Refer to AMM 06-41-57, Page

Block 001).

(c) In the forward cargo compartment, install the sidewall panel 132QW (Refer to AMM

06-41-53, Page Block 001 and AMM 25-54-10, Page Block 201).

(d) In the forward cargo compartment, at FR38.2, install the partition panel 132SW

(Refer to AMM 06-41-53, Page Block 001 and AMM 53-10-55, Page Block 401).

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

(f) Close the forward cargo compartment door 811 (Refer to AMM 52-30-00, Page

Block 001).

(g) Remove the access platform(s).

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

**CONF 008

(1) Subtask 282148-861-002-001 - Energize Electrical Network

Manpower Resources

Skills NON SPECIFIC

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 228

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References

Aircraft Maintenance Manual (AMM) 24-31-11, Page Block 401

(a) Battery re-connection :

- For job set-up, refer to removal/installation of the batteries (Refer to AMM

24-31-11, Page Block 401),

- Remove the blanking cap from the electrical connectors,

- Make sure that the electrical connectors are clean and in correct condition,

- Connect the connector on the battery,

- Turn the knurled nut a quarter turn.

(b) Remove all warning notices.

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

(2) Subtask 282148-942-009-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

06-41-57, Page Block 001

25-54-10, Page Block 201

52-10-00, Page Block 001

52-30-00, Page Block 001

53-10-55, Page Block 401

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

equipment.

(b) On the RH wing, install the access panel 613RR (Refer to AMM 06-41-57, Page

Block 001).

(c) In the forward cargo compartment, install the sidewall panel 132QW (Refer to AMM

06-41-53, Page Block 001 and AMM 25-54-10, Page Block 201).

(d) In the forward cargo compartment, at FR38.2, install the partition panel 132SW

(Refer to AMM 06-41-53, Page Block 001 and AMM 53-10-55, Page Block 401).

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

(f) Close the forward cargo compartment door 811 (Refer to AMM 52-30-00, Page

Block 001).

(g) Remove the access platform(s).

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

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 229

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This Page Intentionally Left Blank

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

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Task 282148-831-853-001 - Modification - ADDITIONAL WORK 1 (Introduced at Rev 02)

**CONF ALL

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

INCLUDED IN THE REFERENCED PROCEDURES.

WARNING: THIS PROCEDURE USES A FUEL SYSTEM ITEM THAT IS IN A CATEGORY

KNOWN AS A CRITICAL DESIGN CONFIGURATION CONTROL LIMITATION

(CDCCL) CDCCL IDENTIFIES AN ITEM THAT CAN BE THE SOURCE OF A

POSSIBLE FUEL TANK IGNITION. YOU MUST KEEP ALL CDCCL ITEMS IN

THE APPROVED CONFIGURATION. DAMAGE, WEAR OR CHANGES TO A

CDCCL ITEM CAN CAUSE A POSSIBLE FUEL TANK EXPLOSION.

CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP

ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY

AND MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENANCE

WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING,

COMPONENTS AND THE WORK AREA AS CLEAN AS POSSIBLE, TO DO

THIS:

- PUT PROTECTION, SUCH AS PLASTIC SHEETING, CLOTHS, ETC; AS

NECESSARY ON WIRING AND COMPONENTS

- REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND

OTHER CONTAMINATION.

THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION

AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION.

IF THERE IS CONTAMINATION, REFER TO ESPM 20-55-00.

Task Associated Data

**CONF 001

Manpower

TOTAL MANHOURS 23.00

ELAPSED TIME (HOURS) 13.00

**CONF 002

Manpower

TOTAL MANHOURS 23.00

ELAPSED TIME (HOURS) 13.00

**CONF 003

Manpower

TOTAL MANHOURS 0.00

ELAPSED TIME (HOURS) 0.00

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 231

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**CONF 004

Manpower

TOTAL MANHOURS 0.00

ELAPSED TIME (HOURS) 0.00

**CONF 005

Manpower

TOTAL MANHOURS 23.00

ELAPSED TIME (HOURS) 13.00

**CONF 006

Manpower

TOTAL MANHOURS 23.00

ELAPSED TIME (HOURS) 13.00

**CONF 007

Manpower

TOTAL MANHOURS 0.00

ELAPSED TIME (HOURS) 0.00

**CONF 008

Manpower

TOTAL MANHOURS 0.00

ELAPSED TIME (HOURS) 0.00

**CONF ALL

A. GENERAL

**CONF 001

(1) Subtask 282148-910-205-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

Material necessary to do the job

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Storage compound 15-008A

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 232

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References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Consumable Material List (CML)

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

Structural Repair Manual (SRM) 51-23-11

51-42-11

(a) For panel location (Refer to AMM 06-41-53, Page Block 001).

(b) Obey the instructions for the wiring installation (Refer to ESPM 20-33-00).

(c) Apply

Storage compound 15-008A As required

to the screws after assembly.

(d) Installation of fasteners (Refer to SRM 51-42-11).

(e) For paint coatings (Refer to SRM 51-23-11).

(2) Subtask 282148-839-203-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

Write in the applicable aircraft records that you have done all the work given in this

Service Bulletin.

**CONF 002

(1) Subtask 282148-910-205-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

Material necessary to do the job

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Storage compound 15-008A

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Consumable Material List (CML)

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

Structural Repair Manual (SRM) 51-23-11

51-42-11

(a) For panel location (Refer to AMM 06-41-53, Page Block 001).

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

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(b) Obey the instructions for the wiring installation (Refer to ESPM 20-33-00).

(c) Apply

Storage compound 15-008A As required

to the screws after assembly.

(d) Installation of fasteners (Refer to SRM 51-42-11).

(e) For paint coatings (Refer to SRM 51-23-11).

(2) Subtask 282148-839-203-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

Write in the applicable aircraft records that you have done all the work given in this

Service Bulletin.

**CONF 003

None

**CONF 004

None

**CONF 005

(1) Subtask 282148-910-205-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

Material necessary to do the job

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Storage compound 15-008A

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Consumable Material List (CML)

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

Structural Repair Manual (SRM) 51-23-11

51-42-11

(a) For panel location (Refer to AMM 06-41-53, Page Block 001).

(b) Obey the instructions for the wiring installation (Refer to ESPM 20-33-00).

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

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(c) Apply

Storage compound 15-008A As required

to the screws after assembly.

(d) Installation of fasteners (Refer to SRM 51-42-11).

(e) For paint coatings (Refer to SRM 51-23-11).

(2) Subtask 282148-839-203-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

Write in the applicable aircraft records that you have done all the work given in this

Service Bulletin.

**CONF 006

(1) Subtask 282148-910-205-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

Material necessary to do the job

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Storage compound 15-008A

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Consumable Material List (CML)

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

Structural Repair Manual (SRM) 51-23-11

51-42-11

(a) For panel location (Refer to AMM 06-41-53, Page Block 001).

(b) Obey the instructions for the wiring installation (Refer to ESPM 20-33-00).

(c) Apply

Storage compound 15-008A As required

to the screws after assembly.

(d) Installation of fasteners (Refer to SRM 51-42-11).

(e) For paint coatings (Refer to SRM 51-23-11).

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 235

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(2) Subtask 282148-839-203-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

Write in the applicable aircraft records that you have done all the work given in this

Service Bulletin.

**CONF 007

None

**CONF 008

None

**CONF ALL

B. PREPARATION

**CONF 001

(1) Subtask 282148-941-205-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

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

24-41-00, Page Block 301

27-80-00, Page Block 301

36-11-00, Page Block 401

ADDITIONAL WORK 1 is required by this revision for aircraft modified by issue 00 or

Revision 01.

(a) Make sure that the aircraft is electrically grounded (Refer to AMM 24-00-00, Page

Block 301).

(b) Fully extend the slats (Refer to AMM 27-80-00, Page Block 301).

(c) De-energize the aircraft electrical circuits (Refer to AMM 24-41-00, Page Block

301).

(d) Put the access platform(s) in position.

(e) Open the access panels 612AT, 612KB, 612JB, 623AB, 623BB and 623EB.

(f) Remove the bleed air duct if necessary (Refer to AMM 36-11-00, Page Block 401).

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 236

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**CONF 002

(1) Subtask 282148-941-205-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

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

24-41-00, Page Block 301

27-80-00, Page Block 301

36-11-00, Page Block 401

ADDITIONAL WORK 1 is required by this revision for aircraft modified by issue 00 or

Revision 01.

(a) Make sure that the aircraft is electrically grounded (Refer to AMM 24-00-00, Page

Block 301).

(b) Fully extend the slats (Refer to AMM 27-80-00, Page Block 301).

(c) De-energize the aircraft electrical circuits (Refer to AMM 24-41-00, Page Block

301).

(d) Put the access platform(s) in position.

(e) Open the access panels 612AT, 612KB, 612JB, 623AB, 623BB and 623EB.

(f) Remove the bleed air duct if necessary (Refer to AMM 36-11-00, Page Block 401).

**CONF 003

None

**CONF 004

None

**CONF 005

(1) Subtask 282148-941-205-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

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

24-41-00, Page Block 301

27-80-00, Page Block 301

36-11-00, Page Block 401

ADDITIONAL WORK 1 is required by this revision for aircraft modified by issue 00 or

Revision 01.

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 237

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(a) Make sure that the aircraft is electrically grounded (Refer to AMM 24-00-00, Page

Block 301).

(b) Fully extend the slats (Refer to AMM 27-80-00, Page Block 301).

(c) De-energize the aircraft electrical circuits (Refer to AMM 24-41-00, Page Block

301).

(d) Put the access platform(s) in position.

(e) Open the access panels 612AT, 612KB, 612JB, 623AB, 623BB and 623EB.

(f) Remove the bleed air duct if necessary (Refer to AMM 36-11-00, Page Block 401).

**CONF 006

(1) Subtask 282148-941-205-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

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

24-41-00, Page Block 301

27-80-00, Page Block 301

36-11-00, Page Block 401

ADDITIONAL WORK 1 is required by this revision for aircraft modified by issue 00 or

Revision 01.

(a) Make sure that the aircraft is electrically grounded (Refer to AMM 24-00-00, Page

Block 301).

(b) Fully extend the slats (Refer to AMM 27-80-00, Page Block 301).

(c) De-energize the aircraft electrical circuits (Refer to AMM 24-41-00, Page Block

301).

(d) Put the access platform(s) in position.

(e) Open the access panels 612AT, 612KB, 612JB, 623AB, 623BB and 623EB.

(f) Remove the bleed air duct if necessary (Refer to AMM 36-11-00, Page Block 401).

**CONF 007

None

**CONF 008

None

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 238

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**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 282148-831-256-001 - Modification

Manpower Resources

Manhours 14.00

Minimum number of person 2

Subtask elapsed time 7.00

Skills ELECTRICAL

Material necessary to do the job

Kit 282148D02R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 ABS0596S004 3 SLEEVE

10 MS21919WCH9 1 CLAMP

30 NSA5527-03-01D 2 SPACER

31 NSA5527-03-02D 1 SPACER

109 NSA935805-09 CONDUIT

117 NSA935807C09 12 CLAMP

121 NAS1096-3-40 1 SCREW

125 B9299071900200 1 EQUIPMNT

126 NSA938184PV1601 15 PIN

149 NSA935401-03 30 TIE

150 NSA935401-04 30 TIE

References

Elec. Std. Practices Manual (ESPM) 20-52-00

Fig. A-GBMAA

Additional Work 1 (Introduced at

Revision 02): Improvement of the 2SRoute in the RH-Wing pylon area (Kit

D02)

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

Sheet 07

Sheet 08

Fig. A-GBLAA

Additional Work 1 (Introduced at

Revision 02): Installation of Protection

Sleeve in the Area of 10QT (Kits D02

and D03)

Sheet 01

Sheet 02

Sheet 03

Fig. A-GHAAA

Hook-up Chart

Sheet 01

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

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References

Fig. A-GHBAA

Hook-up Chart

Sheet 01

ADDITIONAL WORK 1 is required by this revision for aircraft modified by issue 00 or

Revision 01.

Refer to Fig. A-GBMAA Sheet 01, Fig. A-GBMAA Sheet 02, Fig. A-GBMAA Sheet 03,

Fig. A-GBMAA Sheet 04, Fig. A-GBMAA Sheet 05, Fig. A-GBMAA Sheet 06, Fig. AGBMAA Sheet 07 and Fig. A-GBMAA Sheet 08

Refer to Fig. A-GHAAA Sheet 01

Refer to Fig. A-GHBAA Sheet 01

(a) Installation of the cable sleeves in the RH-wing forward of the front spar between

rib 11 and rib 12 in zone 623.

Refer to Fig. A-GBLAA Sheet 01, Fig. A-GBLAA Sheet 02 and Fig. A-GBLAA Sheet

03

1 At one position, remove these items from the bracket rib 11 and rib 12 and

cable bundle 2S/636VB, as shown in Fig. A-GBLAA Sheet 01 and Sheet Fig.

A-GBLAA Sheet 03 Details A and D:

2 Clamp MS21919WCH4 Item (22) Retain

1 Clamp MS21919WCH4 Item (22) Discard

1 Clamp MS21919WCH3 Item (23) Retain

1 Spacer NSA5527-03-01D Item (30) Retain

1 Spacer NSA5527-03-02D Item (31) Retain

2 Washer NSA935808-01 Item (112) Retain

2 Screw NAS1096-3-30 Item (121) Discard

1 Clamp NSA935807-06 Item (122) Retain

2 Install protection sleeve, as shown in Fig. A-GBLAA Sheet 01 thru Sheet Fig.

A-GBLAA Sheet 03, Details A, B and D:

1 Sleeve ABS0596S004 Item 1

and attach the cable sleeves with:

10 Tie NSA935401-03 Item 149

or

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

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10 Tie-Cable NSA935401-04 Item 150

3 Install, as shown in Fig. A-GBLAA Sheet 01 and Sheet Fig. A-GBLAA Sheet

03 Details A and E:

2 Clamp MS21919WCH4 Item (22) Retained at

removal

1 Clamp MS21919WCH3 Item (23) Retained at

removal

1 Spacer NSA5527-03-01D Item (30) Retained at

removal

1 Spacer NSA5527-03-02D Item (31) Retained at

removal

1 Washer NSA935808-01 Item (112) Retained at

removal

1 Clamp NSA935807-06 Item (122) Retained at

removal

1 Clamp MS21919WCH9 Item 10

1 Spacer NSA5527-03-02D Item 31

1 Screw NAS1096-3-40 Item 121

(b) Installation of the cable sleeves in the RH-wing forward of the front spar between

rib 8 and rib 9 (pylon area) in zone 612.

Refer to Fig. A-GBMAA Sheet 01, Fig. A-GBMAA Sheet 02, Fig. A-GBMAA Sheet

03, Fig. A-GBMAA Sheet 04, Fig. A-GBMAA Sheet 05, Fig. A-GBMAA Sheet 06,

Fig. A-GBMAA Sheet 07 and Fig. A-GBMAA Sheet 08

Refer to Fig. A-GHAAA Sheet 01

Refer to Fig. A-GHBAA Sheet 01

NOTE: If other wires are installed in the conduit of route 2S, disconnect

them, change the conduits in accordance with this Service Bulletin,

re-install the wires in the new conduit of route 2S and reconnect the

wires. Do a test in accordance with ESPM 20-52-00.

1 Disconnect these wires of route 2S from the receptacles 40VC and 5006VC in

accordance with the Hook-up Chart 1, Lines 1 thru 14, END 1, Fig. A-GHAAA

Sheet 01 and the Hook-up Chart 2, Lines 2 thru 8, END 1, Fig. A-GHBAA

Sheet 01.

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2 Remove, refer to Fig. A-GBMAA Sheet 03, Detail D, BEFORE:

1 Spacer NSA5527-03-02D Item (31) Discard

1 Clamp NSA935807C10 Item (110) Discard

1 Clamp NSA935807C16 Item (111) Retain

1 Washer NSA935808-01 Item (112) Retain

1 Screw NAS1096-3-23 Item (113) Retain

1 Spacer NSA5527-03-05D Item (114) Discard

1 Washer NSA1149D0332K Item (115) Retain

1 Nut NAS1291C3M Item (116) Retain

1 Clamp NSA935807C09 Item (117) Retain

3 Remove, refer to Fig. A-GBMAA Sheet 04, Detail F, BEFORE:

2 Spacer NSA5527-03-01D Item (30) Retain

1 Spacer NSA5527-03-02D Item (31) Retain

1 Clamp NSA935807C10 Item (110) Retain

1 Clamp NSA935807C10 Item (110) Discard

1 Clamp NSA935807C16 Item (111) Retain

1 Washer NSA935808-01 Item (112) Retain

1 Clamp NSA935807C09 Item (117) Retain

1 Screw NAS1096-3-33 Item (118) Retain

4 Remove, refer to Fig. A-GBMAA Sheet 05, , Detail H, BEFORE:

2 Spacer NSA5527-03-01D Item (30) Retain

2 Spacer NSA5527-03-02D Item (31) Retain

2 Clamp NSA935807C10 Item (110) Discard

2 Clamp NSA935807C16 Item (111) Retain

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2 Spacer NSA5527-03-05D Item (114) Retain

2 Washer NSA1149D0332K Item (115) Retain

2 Clamp NSA935807C09 Item (117) Retain

2 Screw NAS1096-3-33 Item (118) Retain

5 Remove, refer to Fig. A-GBMAA Sheet 06, Detail K, BEFORE:

1 Spacer NSA5527-03-01D Item (30) Retain

1 Spacer NSA5527-03-02D Item (31) Retain

1 Clamp NSA935807C10 Item (110) Discard

1 Clamp NSA935807C16 Item (111) Retain

1 Spacer NSA5527-03-05D Item (114) Retain

1 Washer NSA1149D0332K Item (115) Retain

1 Clamp NSA935807C09 Item (117) Retain

1 Screw NAS1096-3-33 Item (118) Retain

6 Remove, refer to Fig. A-GBMAA Sheet 07, Detail M, BEFORE:

1 Spacer NSA5527-03-01D Item (30) Retain

1 Spacer NSA5527-03-02D Item (31) Retain

1 Clamp NSA935807C10 Item (110) Discard

1 Clamp NSA935807C16 Item (111) Retain

1 Washer NSA935808-01 Item (112) Retain

1 Spacer NSA5527-03-05D Item (114) Retain

1 Clamp NSA935807C09 Item (117) Retain

1 Screw NAS1096-3-33 Item (118) Retain

7 Remove, refer to Fig. A-GBMAA Sheet 08, Detail P, BEFORE:

1 Spacer NSA5527-03-02D Item (31) Retain

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1 Clamp NSA935807C10 Item (110) Discard

1 Clamp NSA935807C16 Item (111) Retain

1 Washer NSA935808-01 Item (112) Retain

1 Spacer NSA5527-03-05D Item (114) Retain

1 Clamp NSA935807C09 Item (117) Retain

1 Screw NAS1096-3-25 Item (119) Retain

8 Remove the identification sleeves from the cable harnesses near the

receptacles 40VC and 5006VC as shown Fig. A-GBMAA Sheet 01, Detail A

As

required

placard Item (125) Discard

9 Remove the protection sleeve from the cable harness:

1 Sleeve Item (109) Discard

10 Cut the conduit to the required length and install:

3 (ME) Conduit NSA935805-09 Item 109

a One part 1500.0 mm (59.06 in.) to the electrical wires for 10QT-A and

10QT-B of route 2S/636VB, refer to the Hook-up Chart 2, Fig. A-GHBAA

Sheet 01

b Three parts, one 520.0 mm (20.47 in.) and two 240.0 mm (9.45 in.) to the

remaining electrical wires of route 2S/636VB, refer to Fig. A-GHAAA

Sheet 01

11 Connect the electrical wires of route 2S to the receptacles 40VC and 5006VC

in accordance with the Hook-up Chart 1, Lines 1 thru 14, END 1, Fig. AGHAAA Sheet 01 and the Hook-up Chart 2, Lines 2 thru 8, END 1, Fig. AGHBAA Sheet 01. Use the contact pins if required:

15 Pin NSA938184PV1601 Item 126

12 Install, refer to Fig. A-GBMAA Sheet 08, Detail Q, AFTER:

1 Spacer NSA5527-03-02D Item (31) Retained at

removal

1 Clamp NSA935807C16 Item (111) Retained at

removal

1 Washer NSA935808-01 Item (112) Retained at

removal

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 244

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@A310

SERVICE BULLETIN

1 Spacer NSA5527-03-05D Item (114) Retained at

removal

1 Clamp NSA935807C09 Item (117) Retained at

removal

1 Screw NAS1096-3-25 Item (119) Retained at

removal

2 Clamp NSA935807C09 Item 117

13 Install, refer to Fig. A-GBMAA Sheet 07, Detail N, AFTER:

1 Spacer NSA5527-03-01D Item (30) Retained at

removal

1 Spacer NSA5527-03-02D Item (31) Retained at

removal

1 Clamp NSA935807C16 Item (111) Retained at

removal

1 Washer NSA935808-01 Item (112) Retained at

removal

1 Spacer NSA5527-03-05D Item (114) Retained at

removal

1 Clamp NSA935807C09 Item (117) Retained at

removal

1 Screw NAS1096-3-33 Item (118) Retained at

removal

2 Clamp NSA935807C09 Item 117

14 Install, refer to Fig. A-GBMAA Sheet 06, Detail L, AFTER:

1 Spacer NSA5527-03-01D Item (30) Retained at

removal

1 Spacer NSA5527-03-02D Item (31) Retained at

removal

1 Clamp NSA935807C16 Item (111) Retained at

removal

1 Spacer NSA5527-03-05D Item (114) Retained at

removal

1 Washer NSA1149D0332K Item (115) Retained at

removal

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 245

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@A310

SERVICE BULLETIN

1 Clamp NSA935807C09 Item (117) Retained at

removal

1 Screw NAS1096-3-33 Item (118) Retained at

removal

2 Clamp NSA935807C09 Item 117

15 Install, refer to Fig. A-GBMAA Sheet 05, Detail J, AFTER:

2 Spacer NSA5527-03-01D Item (30) Retained at

removal

2 Spacer NSA5527-03-02D Item (31) Retained at

removal

2 Clamp NSA935807C16 Item (111) Retained at

removal

2 Spacer NSA5527-03-05D Item (114) Retained at

removal

2 Washer NSA1149D0332K Item (115) Retained at

removal

2 Clamp NSA935807C09 Item (117) Retained at

removal

2 Screw NAS1096-3-33 Item (118) Retained at

removal

2 Clamp NSA935807C09 Item 117

16 Install, refer to Fig. A-GBMAA Sheet 04, Detail G, AFTER:

2 Spacer NSA5527-03-01D Item (30) Retained at

removal

1 Spacer NSA5527-03-02D Item (31) Retained at

removal

1 Clamp NSA935807C10 Item (110) Retained at

removal

1 Clamp NSA935807C16 Item (111) Retained at

removal

1 Washer NSA935808-01 Item (112) Retained at

removal

1 Clamp NSA935807C09 Item (117) Retained at

removal

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 246

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@A310

SERVICE BULLETIN

1 Screw NAS1096-3-33 Item (118) Retained at

removal

2 Clamp NSA935807C09 Item 117

17 Install, refer to Fig. A-GBMAA Sheet 03, Detail E, AFTER:

2 Spacer NSA5527-03-01D Item 30

1 Clamp NSA935807C16 Item (111) Retained at

removal

1 Washer NSA935808-01 Item (112) Retained at

removal

1 Screw NAS1096-3-23 Item (113) Retained at

removal

1 Washer NSA1149D0332K Item (115) Retained at

removal

1 Nut NAS1291C3M Item (116) Retained at

removal

1 Clamp NSA935807C09 Item (117) Retained at

removal

2 Clamp NSA935807C09 Item 117

18 Protect the electrical wires for 10QT-A and 10QT-B of route 2S/636VB, refer

to the Hook-up Chart 2, Fig. A-GHBAA Sheet 01 and refer to Fig. A-GBMAA

Sheet 02 and Sheet Fig. A-GBMAA Sheet 03 with:

2 Sleeve ABS0596S004 Item 1

cut the sleeve to the required length and install with:

20 Tie NSA935401-03 Item 149

20 Tie-Cable NSA935401-04 Item 150

19 Install the identification placards, refer to Fig. A-GBMAA Sheet 02,

1 Placard set B9299071900200 Item 125

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 247

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@A310

SERVICE BULLETIN

**CONF 002

(1) Subtask 282148-831-256-002 - Modification

Manpower Resources

Manhours 14.00

Minimum number of person 2

Subtask elapsed time 7.00

Skills ELECTRICAL

Material necessary to do the job

Kit 282148D03R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 ABS0596S004 SLEEVE

10 MS21919WCH9 1 CLAMP

31 NSA5527-03-02D 2 SPACER

109 NSA935805-09 CONDUIT

117 NSA935807C09 CLAMP

121 NAS1096-3-40 1 SCREW

123 NAS1801-3-31 SCREW

126 NSA938184PV1601 PIN

130 NSA5527-03-08D 1 SPACER

131 NSA5527-03-07D 1 SPACER

132 B9299071900600 EQUIPMNT

149 NSA935401-03 10 TIE

150 NSA935401-04 30 TIE

References

Elec. Std. Practices Manual (ESPM) 20-52-00

Fig. A-GBNAA

Additional Work 1 (Introduced at

Revision 02): Improvement of the 2SRoute in the RH-Wing Pylon Area (Kit

D03)

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

Sheet 07

Sheet 08

Fig. A-GHBAA

Hook-up Chart

Sheet 01

ADDITIONAL WORK 1 is required by this revision for aircraft modified by issue 00 or

Revision 01.

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 248

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@A310

SERVICE BULLETIN

(a) Installation of the cable sleeves in the RH-wing forward of the front spar between

rib 11 and rib 12 in zone 623.

Refer to Fig. A-GBNAA Sheet 01, Fig. A-GBNAA Sheet 02, Fig. A-GBNAA Sheet

03, Fig. A-GBNAA Sheet 04, Fig. A-GBNAA Sheet 05, Fig. A-GBNAA Sheet 06,

Fig. A-GBNAA Sheet 07 and Fig. A-GBNAA Sheet 08

Refer to Fig. A-GHBAA Sheet 01

1 At one position, remove these items from the bracket rib 11 and rib 12 and

cable bundle 2S/636VB, as shown in Fig. A-GBNAA Sheet 01 and Sheet Fig.

A-GBNAA Sheet 03 Details A and D:

2 Clamp MS21919WCH4 Item (22) Retain

1 Clamp MS21919WCH4 Item (22) Discard

1 Clamp MS21919WCH3 Item (23) Retain

1 Spacer NSA5527-03-01D Item (30) Retain

1 Spacer NSA5527-03-02D Item (31) Retain

2 Washer NSA935808-01 Item (112) Retain

2 Screw NAS1096-3-30 Item (121) Discard

1 Clamp NSA935807-06 Item (122) Retain

2 Install protection sleeve, as shown in Fig. A-GBNAA Sheet 01 thru Sheet Fig.

A-GBNAA Sheet 03 Details A, B and C:

1 Sleeve ABS0596S004 Item 1

and attach the cable sleeves with:

10 Tie NSA935401-03 Item 149

or

10 Tie-Cable NSA935401-04 Item 150

3 Install, as shown in Fig. A-GBNAA Sheet 01 and Sheet Fig. A-GBNAA Sheet

03 Details A and E:

2 Clamp MS21919WCH4 Item (22) Retained at

removal

1 Clamp MS21919WCH3 Item (23) Retained at

removal

1 Spacer NSA5527-03-01D Item (30) Retained at

removal

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 249

6

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@A310

SERVICE BULLETIN

1 Spacer NSA5527-03-02D Item (31) Retained at

removal

1 Washer NSA935808-01 Item (112) Retained at

removal

1 Clamp NSA935807-06 Item (122) Retained at

removal

1 Clamp MS21919WCH9 Item 10

1 Spacer NSA5527-03-02D Item 31

1 Screw NAS1096-3-40 Item 121

(b) Installation of the cable sleeves in the RH-wing forward of the front spar between

rib 8 and rib 9 (pylon area) in zone 612.

Refer to Fig. A-GBNAA Sheet 01

Refer to Fig. A-GHBAA Sheet 01

NOTE: If other wires are installed in the conduit of route 2S, disconnect

them, change the conduits in accordance with this Service Bulletin,

re-install the wires in the new conduit of route 2S and reconnect the

wires. Do a test in accordance with ESPM 20-52-00.

1 Disconnect these wires of route 2S from the receptacles 40VC and 5006VC in

accordance with the Hook-up Chart 2, Lines 2 thru 8, END 1, Fig. A-GHBAA

Sheet 01.

2 Remove, refer to Fig. A-GBNAA Sheet 03, Detail D, BEFORE:

1 Spacer NSA5527-03-02D Item (31) Retain

2 Clamp NSA935807C16 Item (111) Retain

1 Washer NSA935808-01 Item (112) Retain

1 Screw NAS1096-3-23 Item (113) Retain

1 Spacer NSA5527-03-05D Item (114) Retain

1 Nut NAS1291C3M Item (116) Retain

1 Washer AN960KD10l Item (124) Retain

3 Remove, refer to Fig. A-GBNAA Sheet 04, Detail F, BEFORE:

1 Spacer NSA5527-03-02D Item (31) Retain

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 250

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@A310

SERVICE BULLETIN

2 Clamp NSA935807C16 Item (111) Retain

1 Washer NSA935808-01 Item (112) Retain

1 Screw NAS1096-3-23 Item (113) Retain

1 Spacer NSA5527-03-05D Item (114) Retain

4 Remove, refer to Fig. A-GBNAA Sheet 05, Detail H, BEFORE:

2 Spacer NSA5527-03-02D Item (31) Retain

4 Clamp NSA935807C16 Item (111) Retain

2 Washer NSA935808-01 Item (112) Retain

2 Screw NAS1096-3-23 Item (113) Retain

2 Spacer NSA5527-03-05D Item (114) Retain

5 Remove, refer to Fig. A-GBNAA Sheet 06, Detail K, BEFORE:

1 Spacer NSA5527-03-02D Item (31) Retain

2 Clamp NSA935807C16 Item (111) Retain

1 Washer NSA935808-01 Item (112) Retain

1 Screw NAS1096-3-23 Item (113) Discard

1 Clamp NSA5516-04NV Item (120) Retain

6 Remove, refer to Fig. A-GBNAA Sheet 07, Detail M, BEFORE:

1 Spacer NSA5527-03-02D Item (31) Retain

2 Clamp NSA935807C16 Item (111) Retain

1 Washer NSA935808-01 Item (112) Retain

1 Screw NAS1096-3-23 Item (113) Discard

1 Spacer NSA5527-03-05D Item (114) Retain

7 Remove, refer to Fig. A-GBNAA Sheet 08, Detail P, BEFORE:

1 Spacer NSA5527-03-02D Item (31) Retain

2 Clamp NSA935807C16 Item (111) Retain

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 251

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@A310

SERVICE BULLETIN

1 Washer NSA935808-01 Item (112) Retain

1 Screw NAS1096-3-23 Item (113) Discard

1 Spacer NSA5527-03-05D Item (114) Retain

8 Remove the identification placards from the cable harnesses near the

receptacles 40VC and 5006VC as shown Fig. A-GBNAA Sheet 02, Detail A

As

required

placard Item (132) Discard

9 Remove the disconnected electrical wires from the protection sleeve.

10 Install to the electrical wires for 10QT-A and 10QT-B of route 2S/636VB, refer

to the Hook-up Chart 2, Lines 2 thru 8, Fig. A-GHBAA Sheet 01:

1 (ME) Conduit NSA935805-09 Item 109

11 Connect the electrical wires of route 2S to the receptacles 40VC and 5006VC

in accordance with the Hook-up Chart 2, Lines 2 thru 8, END 1, Fig. AGHBAA Sheet 01. Use the contact pins if required:

7 Pin NSA938184PV1601 Item 126

12 Install, refer to Fig. A-GBNAA Sheet 08, Detail Q, AFTER:

1 Spacer NSA5527-03-02D Item (31) Retained at

removal

1 Spacer NSA5527-03-02D Item 31

2 Clamp NSA935807C16 Item (111) Retained at

removal

1 Washer NSA935808-01 Item (112) Retained at

removal

1 Spacer NSA5527-03-05D Item (114) Retained at

removal

1 Clamp NSA935807C09 Item 117

1 Screw NAS1801-3-31 Item 123

1 Spacer NSA5527-03-07D Item 131

13 Install, refer to Fig. A-GBNAA Sheet 07, Detail N, AFTER:

1 Spacer NSA5527-03-02D Item (31) Retained at

removal

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 252

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@A310

SERVICE BULLETIN

2 Clamp NSA935807C16 Item (111) Retained at

removal

1 Washer NSA935808-01 Item (112) Retained at

removal

1 Spacer NSA5527-03-05D Item (114) Retained at

removal

1 Clamp NSA935807C09 Item 117

1 Screw NAS1801-3-31 Item 123

1 Spacer NSA5527-03-08D Item 130

14 Install, refer to Fig. A-GBNAA Sheet 06, Detail L, AFTER:

2 Spacer NSA5527-03-02D Item (31) Retained at

removal

2 Clamp NSA935807C16 Item (111) Retained at

removal

1 Washer NSA935808-01 Item (112) Retained at

removal

1 Clamp NSA5516-04NV Item (120) Retained at

removal

1 Clamp NSA935807C09 Item 117

1 Screw NAS1801-3-31 Item 123

15 Install, refer to Fig. A-GBNAA Sheet 05, Detail J, AFTER:

2 Spacer NSA5527-03-02D Item (31) Retained at

removal

4 Clamp NSA935807C16 Item (111) Retained at

removal

2 Washer NSA935808-01 Item (112) Retained at

removal

2 Screw NAS1096-3-23 Item (113) Retained at

removal

2 Spacer NSA5527-03-05D Item (114) Retained at

removal

2 Clamp NSA935807C09 Item 117

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 253

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@A310

SERVICE BULLETIN

16 Install, refer to Fig. A-GBNAA Sheet 04, Detail G, AFTER:

1 Spacer NSA5527-03-02D Item (31) Retained at

removal

2 Clamp NSA935807C16 Item (111) Retained at

removal

1 Washer NSA935808-01 Item (112) Retained at

removal

1 Screw NAS1096-3-23 Item (113) Retained at

removal

1 Spacer NSA5527-03-05D Item (114) Retained at

removal

1 Clamp NSA935807C09 Item 117

17 Install, refer to Fig. A-GBNAA Sheet 03, Detail E, AFTER:

1 Spacer NSA5527-03-02D Item (31) Retained at

removal

2 Clamp NSA935807C16 Item (111) Retained at

removal

1 Washer NSA935808-01 Item (112) Retained at

removal

1 Screw NAS1096-3-23 Item (113) Retained at

removal

1 Spacer NSA5527-03-05D Item (114) Retained at

removal

1 Nut NAS1291C3M Item (116) Retained at

removal

1 Washer AN960KD10l Item (124) Retained at

removal

1 Clamp NSA935807C09 Item 117

18 Protect the electrical wires for 10QT-A and 10QT-B of route 2S/636VB, refer

to the Hook-up Chart 2, Fig. A-GHBAA Sheet 01 with:

3 Sleeve ABS0596S004 Item 1

and

20 Tie NSA935401-03 Item 149

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 254

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@A310

SERVICE BULLETIN

or

20 Tie-Cable NSA935401-04 Item 150

19 Install the identification placards, refer to Fig. A-GBNAA Sheet 02

1 Placard Set B9299071900600 Item 132

**CONF 003

None

**CONF 004

None

**CONF 005

(1) Subtask 282148-831-256-001 - Modification

Manpower Resources

Manhours 14.00

Minimum number of person 2

Subtask elapsed time 7.00

Skills ELECTRICAL

Material necessary to do the job

Kit 282148D02R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 ABS0596S004 3 SLEEVE

10 MS21919WCH9 1 CLAMP

30 NSA5527-03-01D 2 SPACER

31 NSA5527-03-02D 1 SPACER

109 NSA935805-09 CONDUIT

117 NSA935807C09 12 CLAMP

121 NAS1096-3-40 1 SCREW

125 B9299071900200 1 EQUIPMNT

126 NSA938184PV1601 15 PIN

149 NSA935401-03 30 TIE

150 NSA935401-04 30 TIE

References

Elec. Std. Practices Manual (ESPM) 20-52-00

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 255

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@A310

SERVICE BULLETIN

References

Fig. A-GBMAA

Additional Work 1 (Introduced at

Revision 02): Improvement of the 2SRoute in the RH-Wing pylon area (Kit

D02)

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

Sheet 07

Sheet 08

Fig. A-GBLAA

Additional Work 1 (Introduced at

Revision 02): Installation of Protection

Sleeve in the Area of 10QT (Kits D02

and D03)

Sheet 01

Sheet 02

Sheet 03

Fig. A-GHAAA

Hook-up Chart

Sheet 01

Fig. A-GHBAA

Hook-up Chart

Sheet 01

ADDITIONAL WORK 1 is required by this revision for aircraft modified by issue 00 or

Revision 01.

Refer to Fig. A-GBMAA Sheet 01, Fig. A-GBMAA Sheet 02, Fig. A-GBMAA Sheet 03,

Fig. A-GBMAA Sheet 04, Fig. A-GBMAA Sheet 05, Fig. A-GBMAA Sheet 06, Fig. AGBMAA Sheet 07 and Fig. A-GBMAA Sheet 08

Refer to Fig. A-GHAAA Sheet 01

Refer to Fig. A-GHBAA Sheet 01

(a) Installation of the cable sleeves in the RH-wing forward of the front spar between

rib 11 and rib 12 in zone 623.

Refer to Fig. A-GBLAA Sheet 01, Fig. A-GBLAA Sheet 02 and Fig. A-GBLAA Sheet

03

1 At one position, remove these items from the bracket rib 11 and rib 12 and

cable bundle 2S/636VB, as shown in Fig. A-GBLAA Sheet 01 and Sheet Fig.

A-GBLAA Sheet 03 Details A and D:

2 Clamp MS21919WCH4 Item (22) Retain

1 Clamp MS21919WCH4 Item (22) Discard

1 Clamp MS21919WCH3 Item (23) Retain

1 Spacer NSA5527-03-01D Item (30) Retain

1 Spacer NSA5527-03-02D Item (31) Retain

2 Washer NSA935808-01 Item (112) Retain

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 256

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@A310

SERVICE BULLETIN

2 Screw NAS1096-3-30 Item (121) Discard

1 Clamp NSA935807-06 Item (122) Retain

2 Install protection sleeve, as shown in Fig. A-GBLAA Sheet 01 thru Sheet Fig.

A-GBLAA Sheet 03, Details A, B and D:

1 Sleeve ABS0596S004 Item 1

and attach the cable sleeves with:

10 Tie NSA935401-03 Item 149

or

10 Tie-Cable NSA935401-04 Item 150

3 Install, as shown in Fig. A-GBLAA Sheet 01 and Sheet Fig. A-GBLAA Sheet

03 Details A and E:

2 Clamp MS21919WCH4 Item (22) Retained at

removal

1 Clamp MS21919WCH3 Item (23) Retained at

removal

1 Spacer NSA5527-03-01D Item (30) Retained at

removal

1 Spacer NSA5527-03-02D Item (31) Retained at

removal

1 Washer NSA935808-01 Item (112) Retained at

removal

1 Clamp NSA935807-06 Item (122) Retained at

removal

1 Clamp MS21919WCH9 Item 10

1 Spacer NSA5527-03-02D Item 31

1 Screw NAS1096-3-40 Item 121

(b) Installation of the cable sleeves in the RH-wing forward of the front spar between

rib 8 and rib 9 (pylon area) in zone 612.

Refer to Fig. A-GBMAA Sheet 01, Fig. A-GBMAA Sheet 02, Fig. A-GBMAA Sheet

03, Fig. A-GBMAA Sheet 04, Fig. A-GBMAA Sheet 05, Fig. A-GBMAA Sheet 06,

Fig. A-GBMAA Sheet 07 and Fig. A-GBMAA Sheet 08

Refer to Fig. A-GHAAA Sheet 01

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 257

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@A310

SERVICE BULLETIN

Refer to Fig. A-GHBAA Sheet 01

NOTE: If other wires are installed in the conduit of route 2S, disconnect

them, change the conduits in accordance with this Service Bulletin,

re-install the wires in the new conduit of route 2S and reconnect the

wires. Do a test in accordance with ESPM 20-52-00.

1 Disconnect these wires of route 2S from the receptacles 40VC and 5006VC in

accordance with the Hook-up Chart 1, Lines 1 thru 14, END 1, Fig. A-GHAAA

Sheet 01 and the Hook-up Chart 2, Lines 2 thru 8, END 1, Fig. A-GHBAA

Sheet 01.

2 Remove, refer to Fig. A-GBMAA Sheet 03, Detail D, BEFORE:

1 Spacer NSA5527-03-02D Item (31) Discard

1 Clamp NSA935807C10 Item (110) Discard

1 Clamp NSA935807C16 Item (111) Retain

1 Washer NSA935808-01 Item (112) Retain

1 Screw NAS1096-3-23 Item (113) Retain

1 Spacer NSA5527-03-05D Item (114) Discard

1 Washer NSA1149D0332K Item (115) Retain

1 Nut NAS1291C3M Item (116) Retain

1 Clamp NSA935807C09 Item (117) Retain

3 Remove, refer to Fig. A-GBMAA Sheet 04, Detail F, BEFORE:

2 Spacer NSA5527-03-01D Item (30) Retain

1 Spacer NSA5527-03-02D Item (31) Retain

1 Clamp NSA935807C10 Item (110) Retain

1 Clamp NSA935807C10 Item (110) Discard

1 Clamp NSA935807C16 Item (111) Retain

1 Washer NSA935808-01 Item (112) Retain

1 Clamp NSA935807C09 Item (117) Retain

1 Screw NAS1096-3-33 Item (118) Retain

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 258

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SERVICE BULLETIN

4 Remove, refer to Fig. A-GBMAA Sheet 05, , Detail H, BEFORE:

2 Spacer NSA5527-03-01D Item (30) Retain

2 Spacer NSA5527-03-02D Item (31) Retain

2 Clamp NSA935807C10 Item (110) Discard

2 Clamp NSA935807C16 Item (111) Retain

2 Spacer NSA5527-03-05D Item (114) Retain

2 Washer NSA1149D0332K Item (115) Retain

2 Clamp NSA935807C09 Item (117) Retain

2 Screw NAS1096-3-33 Item (118) Retain

5 Remove, refer to Fig. A-GBMAA Sheet 06, Detail K, BEFORE:

1 Spacer NSA5527-03-01D Item (30) Retain

1 Spacer NSA5527-03-02D Item (31) Retain

1 Clamp NSA935807C10 Item (110) Discard

1 Clamp NSA935807C16 Item (111) Retain

1 Spacer NSA5527-03-05D Item (114) Retain

1 Washer NSA1149D0332K Item (115) Retain

1 Clamp NSA935807C09 Item (117) Retain

1 Screw NAS1096-3-33 Item (118) Retain

6 Remove, refer to Fig. A-GBMAA Sheet 07, Detail M, BEFORE:

1 Spacer NSA5527-03-01D Item (30) Retain

1 Spacer NSA5527-03-02D Item (31) Retain

1 Clamp NSA935807C10 Item (110) Discard

1 Clamp NSA935807C16 Item (111) Retain

1 Washer NSA935808-01 Item (112) Retain

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 259

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SERVICE BULLETIN

1 Spacer NSA5527-03-05D Item (114) Retain

1 Clamp NSA935807C09 Item (117) Retain

1 Screw NAS1096-3-33 Item (118) Retain

7 Remove, refer to Fig. A-GBMAA Sheet 08, Detail P, BEFORE:

1 Spacer NSA5527-03-02D Item (31) Retain

1 Clamp NSA935807C10 Item (110) Discard

1 Clamp NSA935807C16 Item (111) Retain

1 Washer NSA935808-01 Item (112) Retain

1 Spacer NSA5527-03-05D Item (114) Retain

1 Clamp NSA935807C09 Item (117) Retain

1 Screw NAS1096-3-25 Item (119) Retain

8 Remove the identification sleeves from the cable harnesses near the

receptacles 40VC and 5006VC as shown Fig. A-GBMAA Sheet 01, Detail A

As

required

placard Item (125) Discard

9 Remove the protection sleeve from the cable harness:

1 Sleeve Item (109) Discard

10 Cut the conduit to the required length and install:

3 (ME) Conduit NSA935805-09 Item 109

a One part 1500.0 mm (59.06 in.) to the electrical wires for 10QT-A and

10QT-B of route 2S/636VB, refer to the Hook-up Chart 2, Fig. A-GHBAA

Sheet 01

b Three parts, one 520.0 mm (20.47 in.) and two 240.0 mm (9.45 in.) to the

remaining electrical wires of route 2S/636VB, refer to Fig. A-GHAAA

Sheet 01

11 Connect the electrical wires of route 2S to the receptacles 40VC and 5006VC

in accordance with the Hook-up Chart 1, Lines 1 thru 14, END 1, Fig. AGHAAA Sheet 01 and the Hook-up Chart 2, Lines 2 thru 8, END 1, Fig. AGHBAA Sheet 01. Use the contact pins if required:

15 Pin NSA938184PV1601 Item 126

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 260

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@A310

SERVICE BULLETIN

12 Install, refer to Fig. A-GBMAA Sheet 08, Detail Q, AFTER:

1 Spacer NSA5527-03-02D Item (31) Retained at

removal

1 Clamp NSA935807C16 Item (111) Retained at

removal

1 Washer NSA935808-01 Item (112) Retained at

removal

1 Spacer NSA5527-03-05D Item (114) Retained at

removal

1 Clamp NSA935807C09 Item (117) Retained at

removal

1 Screw NAS1096-3-25 Item (119) Retained at

removal

2 Clamp NSA935807C09 Item 117

13 Install, refer to Fig. A-GBMAA Sheet 07, Detail N, AFTER:

1 Spacer NSA5527-03-01D Item (30) Retained at

removal

1 Spacer NSA5527-03-02D Item (31) Retained at

removal

1 Clamp NSA935807C16 Item (111) Retained at

removal

1 Washer NSA935808-01 Item (112) Retained at

removal

1 Spacer NSA5527-03-05D Item (114) Retained at

removal

1 Clamp NSA935807C09 Item (117) Retained at

removal

1 Screw NAS1096-3-33 Item (118) Retained at

removal

2 Clamp NSA935807C09 Item 117

14 Install, refer to Fig. A-GBMAA Sheet 06, Detail L, AFTER:

1 Spacer NSA5527-03-01D Item (30) Retained at

removal

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 261

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SERVICE BULLETIN

1 Spacer NSA5527-03-02D Item (31) Retained at

removal

1 Clamp NSA935807C16 Item (111) Retained at

removal

1 Spacer NSA5527-03-05D Item (114) Retained at

removal

1 Washer NSA1149D0332K Item (115) Retained at

removal

1 Clamp NSA935807C09 Item (117) Retained at

removal

1 Screw NAS1096-3-33 Item (118) Retained at

removal

2 Clamp NSA935807C09 Item 117

15 Install, refer to Fig. A-GBMAA Sheet 05, Detail J, AFTER:

2 Spacer NSA5527-03-01D Item (30) Retained at

removal

2 Spacer NSA5527-03-02D Item (31) Retained at

removal

2 Clamp NSA935807C16 Item (111) Retained at

removal

2 Spacer NSA5527-03-05D Item (114) Retained at

removal

2 Washer NSA1149D0332K Item (115) Retained at

removal

2 Clamp NSA935807C09 Item (117) Retained at

removal

2 Screw NAS1096-3-33 Item (118) Retained at

removal

2 Clamp NSA935807C09 Item 117

16 Install, refer to Fig. A-GBMAA Sheet 04, Detail G, AFTER:

2 Spacer NSA5527-03-01D Item (30) Retained at

removal

1 Spacer NSA5527-03-02D Item (31) Retained at

removal

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 262

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@A310

SERVICE BULLETIN

1 Clamp NSA935807C10 Item (110) Retained at

removal

1 Clamp NSA935807C16 Item (111) Retained at

removal

1 Washer NSA935808-01 Item (112) Retained at

removal

1 Clamp NSA935807C09 Item (117) Retained at

removal

1 Screw NAS1096-3-33 Item (118) Retained at

removal

2 Clamp NSA935807C09 Item 117

17 Install, refer to Fig. A-GBMAA Sheet 03, Detail E, AFTER:

2 Spacer NSA5527-03-01D Item 30

1 Clamp NSA935807C16 Item (111) Retained at

removal

1 Washer NSA935808-01 Item (112) Retained at

removal

1 Screw NAS1096-3-23 Item (113) Retained at

removal

1 Washer NSA1149D0332K Item (115) Retained at

removal

1 Nut NAS1291C3M Item (116) Retained at

removal

1 Clamp NSA935807C09 Item (117) Retained at

removal

2 Clamp NSA935807C09 Item 117

18 Protect the electrical wires for 10QT-A and 10QT-B of route 2S/636VB, refer

to the Hook-up Chart 2, Fig. A-GHBAA Sheet 01 and refer to Fig. A-GBMAA

Sheet 02 and Sheet Fig. A-GBMAA Sheet 03 with:

2 Sleeve ABS0596S004 Item 1

cut the sleeve to the required length and install with:

20 Tie NSA935401-03 Item 149

20 Tie-Cable NSA935401-04 Item 150

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 263

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@A310

SERVICE BULLETIN

19 Install the identification placards, refer to Fig. A-GBMAA Sheet 02,

1 Placard set B9299071900200 Item 125

**CONF 006

(1) Subtask 282148-831-256-002 - Modification

Manpower Resources

Manhours 14.00

Minimum number of person 2

Subtask elapsed time 7.00

Skills ELECTRICAL

Material necessary to do the job

Kit 282148D03R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 ABS0596S004 SLEEVE

10 MS21919WCH9 1 CLAMP

31 NSA5527-03-02D 2 SPACER

109 NSA935805-09 CONDUIT

117 NSA935807C09 CLAMP

121 NAS1096-3-40 1 SCREW

123 NAS1801-3-31 SCREW

126 NSA938184PV1601 PIN

130 NSA5527-03-08D 1 SPACER

131 NSA5527-03-07D 1 SPACER

132 B9299071900600 EQUIPMNT

149 NSA935401-03 10 TIE

150 NSA935401-04 30 TIE

References

Elec. Std. Practices Manual (ESPM) 20-52-00

Fig. A-GBNAA

Additional Work 1 (Introduced at

Revision 02): Improvement of the 2SRoute in the RH-Wing Pylon Area (Kit

D03)

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

Sheet 07

Sheet 08

Fig. A-GHBAA

Hook-up Chart

Sheet 01

ADDITIONAL WORK 1 is required by this revision for aircraft modified by issue 00 or

Revision 01.

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 264

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SERVICE BULLETIN

(a) Installation of the cable sleeves in the RH-wing forward of the front spar between

rib 11 and rib 12 in zone 623.

Refer to Fig. A-GBNAA Sheet 01, Fig. A-GBNAA Sheet 02, Fig. A-GBNAA Sheet

03, Fig. A-GBNAA Sheet 04, Fig. A-GBNAA Sheet 05, Fig. A-GBNAA Sheet 06,

Fig. A-GBNAA Sheet 07 and Fig. A-GBNAA Sheet 08

Refer to Fig. A-GHBAA Sheet 01

1 At one position, remove these items from the bracket rib 11 and rib 12 and

cable bundle 2S/636VB, as shown in Fig. A-GBNAA Sheet 01 and Sheet Fig.

A-GBNAA Sheet 03 Details A and D:

2 Clamp MS21919WCH4 Item (22) Retain

1 Clamp MS21919WCH4 Item (22) Discard

1 Clamp MS21919WCH3 Item (23) Retain

1 Spacer NSA5527-03-01D Item (30) Retain

1 Spacer NSA5527-03-02D Item (31) Retain

2 Washer NSA935808-01 Item (112) Retain

2 Screw NAS1096-3-30 Item (121) Discard

1 Clamp NSA935807-06 Item (122) Retain

2 Install protection sleeve, as shown in Fig. A-GBNAA Sheet 01 thru Sheet Fig.

A-GBNAA Sheet 03 Details A, B and C:

1 Sleeve ABS0596S004 Item 1

and attach the cable sleeves with:

10 Tie NSA935401-03 Item 149

or

10 Tie-Cable NSA935401-04 Item 150

3 Install, as shown in Fig. A-GBNAA Sheet 01 and Sheet Fig. A-GBNAA Sheet

03 Details A and E:

2 Clamp MS21919WCH4 Item (22) Retained at

removal

1 Clamp MS21919WCH3 Item (23) Retained at

removal

1 Spacer NSA5527-03-01D Item (30) Retained at

removal

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 265

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@A310

SERVICE BULLETIN

1 Spacer NSA5527-03-02D Item (31) Retained at

removal

1 Washer NSA935808-01 Item (112) Retained at

removal

1 Clamp NSA935807-06 Item (122) Retained at

removal

1 Clamp MS21919WCH9 Item 10

1 Spacer NSA5527-03-02D Item 31

1 Screw NAS1096-3-40 Item 121

(b) Installation of the cable sleeves in the RH-wing forward of the front spar between

rib 8 and rib 9 (pylon area) in zone 612.

Refer to Fig. A-GBNAA Sheet 01

Refer to Fig. A-GHBAA Sheet 01

NOTE: If other wires are installed in the conduit of route 2S, disconnect

them, change the conduits in accordance with this Service Bulletin,

re-install the wires in the new conduit of route 2S and reconnect the

wires. Do a test in accordance with ESPM 20-52-00.

1 Disconnect these wires of route 2S from the receptacles 40VC and 5006VC in

accordance with the Hook-up Chart 2, Lines 2 thru 8, END 1, Fig. A-GHBAA

Sheet 01.

2 Remove, refer to Fig. A-GBNAA Sheet 03, Detail D, BEFORE:

1 Spacer NSA5527-03-02D Item (31) Retain

2 Clamp NSA935807C16 Item (111) Retain

1 Washer NSA935808-01 Item (112) Retain

1 Screw NAS1096-3-23 Item (113) Retain

1 Spacer NSA5527-03-05D Item (114) Retain

1 Nut NAS1291C3M Item (116) Retain

1 Washer AN960KD10l Item (124) Retain

3 Remove, refer to Fig. A-GBNAA Sheet 04, Detail F, BEFORE:

1 Spacer NSA5527-03-02D Item (31) Retain

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 266

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@A310

SERVICE BULLETIN

2 Clamp NSA935807C16 Item (111) Retain

1 Washer NSA935808-01 Item (112) Retain

1 Screw NAS1096-3-23 Item (113) Retain

1 Spacer NSA5527-03-05D Item (114) Retain

4 Remove, refer to Fig. A-GBNAA Sheet 05, Detail H, BEFORE:

2 Spacer NSA5527-03-02D Item (31) Retain

4 Clamp NSA935807C16 Item (111) Retain

2 Washer NSA935808-01 Item (112) Retain

2 Screw NAS1096-3-23 Item (113) Retain

2 Spacer NSA5527-03-05D Item (114) Retain

5 Remove, refer to Fig. A-GBNAA Sheet 06, Detail K, BEFORE:

1 Spacer NSA5527-03-02D Item (31) Retain

2 Clamp NSA935807C16 Item (111) Retain

1 Washer NSA935808-01 Item (112) Retain

1 Screw NAS1096-3-23 Item (113) Discard

1 Clamp NSA5516-04NV Item (120) Retain

6 Remove, refer to Fig. A-GBNAA Sheet 07, Detail M, BEFORE:

1 Spacer NSA5527-03-02D Item (31) Retain

2 Clamp NSA935807C16 Item (111) Retain

1 Washer NSA935808-01 Item (112) Retain

1 Screw NAS1096-3-23 Item (113) Discard

1 Spacer NSA5527-03-05D Item (114) Retain

7 Remove, refer to Fig. A-GBNAA Sheet 08, Detail P, BEFORE:

1 Spacer NSA5527-03-02D Item (31) Retain

2 Clamp NSA935807C16 Item (111) Retain

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 267

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@A310

SERVICE BULLETIN

1 Washer NSA935808-01 Item (112) Retain

1 Screw NAS1096-3-23 Item (113) Discard

1 Spacer NSA5527-03-05D Item (114) Retain

8 Remove the identification placards from the cable harnesses near the

receptacles 40VC and 5006VC as shown Fig. A-GBNAA Sheet 02, Detail A

As

required

placard Item (132) Discard

9 Remove the disconnected electrical wires from the protection sleeve.

10 Install to the electrical wires for 10QT-A and 10QT-B of route 2S/636VB, refer

to the Hook-up Chart 2, Lines 2 thru 8, Fig. A-GHBAA Sheet 01:

1 (ME) Conduit NSA935805-09 Item 109

11 Connect the electrical wires of route 2S to the receptacles 40VC and 5006VC

in accordance with the Hook-up Chart 2, Lines 2 thru 8, END 1, Fig. AGHBAA Sheet 01. Use the contact pins if required:

7 Pin NSA938184PV1601 Item 126

12 Install, refer to Fig. A-GBNAA Sheet 08, Detail Q, AFTER:

1 Spacer NSA5527-03-02D Item (31) Retained at

removal

1 Spacer NSA5527-03-02D Item 31

2 Clamp NSA935807C16 Item (111) Retained at

removal

1 Washer NSA935808-01 Item (112) Retained at

removal

1 Spacer NSA5527-03-05D Item (114) Retained at

removal

1 Clamp NSA935807C09 Item 117

1 Screw NAS1801-3-31 Item 123

1 Spacer NSA5527-03-07D Item 131

13 Install, refer to Fig. A-GBNAA Sheet 07, Detail N, AFTER:

1 Spacer NSA5527-03-02D Item (31) Retained at

removal

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 268

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@A310

SERVICE BULLETIN

2 Clamp NSA935807C16 Item (111) Retained at

removal

1 Washer NSA935808-01 Item (112) Retained at

removal

1 Spacer NSA5527-03-05D Item (114) Retained at

removal

1 Clamp NSA935807C09 Item 117

1 Screw NAS1801-3-31 Item 123

1 Spacer NSA5527-03-08D Item 130

14 Install, refer to Fig. A-GBNAA Sheet 06, Detail L, AFTER:

2 Spacer NSA5527-03-02D Item (31) Retained at

removal

2 Clamp NSA935807C16 Item (111) Retained at

removal

1 Washer NSA935808-01 Item (112) Retained at

removal

1 Clamp NSA5516-04NV Item (120) Retained at

removal

1 Clamp NSA935807C09 Item 117

1 Screw NAS1801-3-31 Item 123

15 Install, refer to Fig. A-GBNAA Sheet 05, Detail J, AFTER:

2 Spacer NSA5527-03-02D Item (31) Retained at

removal

4 Clamp NSA935807C16 Item (111) Retained at

removal

2 Washer NSA935808-01 Item (112) Retained at

removal

2 Screw NAS1096-3-23 Item (113) Retained at

removal

2 Spacer NSA5527-03-05D Item (114) Retained at

removal

2 Clamp NSA935807C09 Item 117

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 269

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@A310

SERVICE BULLETIN

16 Install, refer to Fig. A-GBNAA Sheet 04, Detail G, AFTER:

1 Spacer NSA5527-03-02D Item (31) Retained at

removal

2 Clamp NSA935807C16 Item (111) Retained at

removal

1 Washer NSA935808-01 Item (112) Retained at

removal

1 Screw NAS1096-3-23 Item (113) Retained at

removal

1 Spacer NSA5527-03-05D Item (114) Retained at

removal

1 Clamp NSA935807C09 Item 117

17 Install, refer to Fig. A-GBNAA Sheet 03, Detail E, AFTER:

1 Spacer NSA5527-03-02D Item (31) Retained at

removal

2 Clamp NSA935807C16 Item (111) Retained at

removal

1 Washer NSA935808-01 Item (112) Retained at

removal

1 Screw NAS1096-3-23 Item (113) Retained at

removal

1 Spacer NSA5527-03-05D Item (114) Retained at

removal

1 Nut NAS1291C3M Item (116) Retained at

removal

1 Washer AN960KD10l Item (124) Retained at

removal

1 Clamp NSA935807C09 Item 117

18 Protect the electrical wires for 10QT-A and 10QT-B of route 2S/636VB, refer

to the Hook-up Chart 2, Fig. A-GHBAA Sheet 01 with:

3 Sleeve ABS0596S004 Item 1

and

20 Tie NSA935401-03 Item 149

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 270

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@A310

SERVICE BULLETIN

or

20 Tie-Cable NSA935401-04 Item 150

19 Install the identification placards, refer to Fig. A-GBNAA Sheet 02

1 Placard Set B9299071900600 Item 132

**CONF 007

None

**CONF 008

None

**CONF ALL

D. TEST

**CONF 001

(1) Subtask 282148-700-202-001 - Testing

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 27-84-00, Page Block 501

28-42-44, Page Block 401

30-11-00, Page Block 501

36-11-00, Page Block 501

Elec. Std. Practices Manual (ESPM) 20-52-21

ADDITIONAL WORK 1 is required by this revision for aircraft modified by issue 00 or

Revision 01.

(a) Do a continuity test of disconnected wires (Refer to ESPM 20-52-21).

(b) Do an operational test of the cadensicon sensor (Refer to AMM 28-42-44, Page

Block 401).

(c) Do the operational test (Refer to AMM 27-84-00, Page Block 501).

(d) Do the operational test of the wing ice protection (Refer to AMM 30-11-00, Page

Block 501).

(e) Do the bite test (Refer to AMM 36-11-00, Page Block 501).

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 271

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@A310

SERVICE BULLETIN

**CONF 002

(1) Subtask 282148-700-202-001 - Testing

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 27-84-00, Page Block 501

28-42-44, Page Block 401

30-11-00, Page Block 501

36-11-00, Page Block 501

Elec. Std. Practices Manual (ESPM) 20-52-21

ADDITIONAL WORK 1 is required by this revision for aircraft modified by issue 00 or

Revision 01.

(a) Do a continuity test of disconnected wires (Refer to ESPM 20-52-21).

(b) Do an operational test of the cadensicon sensor (Refer to AMM 28-42-44, Page

Block 401).

(c) Do the operational test (Refer to AMM 27-84-00, Page Block 501).

(d) Do the operational test of the wing ice protection (Refer to AMM 30-11-00, Page

Block 501).

(e) Do the bite test (Refer to AMM 36-11-00, Page Block 501).

**CONF 003

None

**CONF 004

None

**CONF 005

(1) Subtask 282148-700-202-001 - Testing

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 27-84-00, Page Block 501

28-42-44, Page Block 401

30-11-00, Page Block 501

36-11-00, Page Block 501

Elec. Std. Practices Manual (ESPM) 20-52-21

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 272

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@A310

SERVICE BULLETIN

ADDITIONAL WORK 1 is required by this revision for aircraft modified by issue 00 or

Revision 01.

(a) Do a continuity test of disconnected wires (Refer to ESPM 20-52-21).

(b) Do an operational test of the cadensicon sensor (Refer to AMM 28-42-44, Page

Block 401).

(c) Do the operational test (Refer to AMM 27-84-00, Page Block 501).

(d) Do the operational test of the wing ice protection (Refer to AMM 30-11-00, Page

Block 501).

(e) Do the bite test (Refer to AMM 36-11-00, Page Block 501).

**CONF 006

(1) Subtask 282148-700-202-001 - Testing

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 27-84-00, Page Block 501

28-42-44, Page Block 401

30-11-00, Page Block 501

36-11-00, Page Block 501

Elec. Std. Practices Manual (ESPM) 20-52-21

ADDITIONAL WORK 1 is required by this revision for aircraft modified by issue 00 or

Revision 01.

(a) Do a continuity test of disconnected wires (Refer to ESPM 20-52-21).

(b) Do an operational test of the cadensicon sensor (Refer to AMM 28-42-44, Page

Block 401).

(c) Do the operational test (Refer to AMM 27-84-00, Page Block 501).

(d) Do the operational test of the wing ice protection (Refer to AMM 30-11-00, Page

Block 501).

(e) Do the bite test (Refer to AMM 36-11-00, Page Block 501).

**CONF 007

None

**CONF 008

None

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 273

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@A310

SERVICE BULLETIN

**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 282148-942-204-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 27-28-00, Page Block 301

ADDITIONAL WORK 1 is required by this revision for aircraft modified by issue 00 or

Revision 01.

Close up

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

equipment.

(b) Fully retract the slats (Refer to AMM 27-28-00, Page Block 301).

(c) Close the access panels 612AT, 612KB, 612JB, 623AB, 623BB and 623EB.

(d) Remove the access platform.

**CONF 002

(1) Subtask 282148-942-204-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 27-28-00, Page Block 301

ADDITIONAL WORK 1 is required by this revision for aircraft modified by issue 00 or

Revision 01.

Close up

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

equipment.

(b) Fully retract the slats (Refer to AMM 27-28-00, Page Block 301).

(c) Close the access panels 612AT, 612KB, 612JB, 623AB, 623BB and 623EB.

(d) Remove the access platform.

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 274

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@A310

SERVICE BULLETIN

**CONF 003

None

**CONF 004

None

**CONF 005

(1) Subtask 282148-942-204-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 27-28-00, Page Block 301

ADDITIONAL WORK 1 is required by this revision for aircraft modified by issue 00 or

Revision 01.

Close up

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

equipment.

(b) Fully retract the slats (Refer to AMM 27-28-00, Page Block 301).

(c) Close the access panels 612AT, 612KB, 612JB, 623AB, 623BB and 623EB.

(d) Remove the access platform.

**CONF 006

(1) Subtask 282148-942-204-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 27-28-00, Page Block 301

ADDITIONAL WORK 1 is required by this revision for aircraft modified by issue 00 or

Revision 01.

Close up

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

equipment.

(b) Fully retract the slats (Refer to AMM 27-28-00, Page Block 301).

(c) Close the access panels 612AT, 612KB, 612JB, 623AB, 623BB and 623EB.

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 275

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@A310

SERVICE BULLETIN

(d) Remove the access platform.

**CONF 007

None

**CONF 008

None

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 276

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@A310

SERVICE BULLETIN

Task 282148-831-849-001 - Modification - ADDITIONAL WORK 2 (Introduced at Rev 03)

**CONF ALL

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

INCLUDED IN THE REFERENCED PROCEDURES.

WARNING: THIS PROCEDURE USES A FUEL SYSTEM ITEM THAT IS IN A CATEGORY

KNOWN AS A CRITICAL DESIGN CONFIGURATION CONTROL LIMITATION

(CDCCL) CDCCL IDENTIFIES AN ITEM THAT CAN BE THE SOURCE OF A

POSSIBLE FUEL TANK IGNITION. YOU MUST KEEP ALL CDCCL ITEMS IN

THE APPROVED CONFIGURATION. DAMAGE, WEAR OR CHANGES TO A

CDCCL ITEM CAN CAUSE A POSSIBLE FUEL TANK EXPLOSION.

CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP

ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY

AND MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENANCE

WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING,

COMPONENTS AND THE WORK AREA AS CLEAN AS POSSIBLE, TO DO

THIS:

- PUT PROTECTION, SUCH AS PLASTIC SHEETING, CLOTHS, ETC; AS

NECESSARY ON WIRING AND COMPONENTS

- REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND

OTHER CONTAMINATION.

THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION

AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION.

IF THERE IS CONTAMINATION, REFER TO ESPM 20-55-00.

Task Associated Data

**CONF 001

Zone

612 623

Access

Panel 612AT 623AB

Manpower

TOTAL MANHOURS 3.00

ELAPSED TIME (HOURS) 3.00

**CONF 002

Zone

612 623

Access

Panel 612AT 623AB

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 277

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SERVICE BULLETIN

Manpower

TOTAL MANHOURS 3.00

ELAPSED TIME (HOURS) 3.00

**CONF 003

Manpower

TOTAL MANHOURS 0.00

ELAPSED TIME (HOURS) 0.00

**CONF 004

Manpower

TOTAL MANHOURS 0.00

ELAPSED TIME (HOURS) 0.00

**CONF 005

Zone

612 623

Access

Panel 612AT 623AB

Manpower

TOTAL MANHOURS 3.00

ELAPSED TIME (HOURS) 3.00

**CONF 006

Zone

612 623

Access

Panel 612AT 623AB

Manpower

TOTAL MANHOURS 3.00

ELAPSED TIME (HOURS) 3.00

**CONF 007

Manpower

TOTAL MANHOURS 0.00

ELAPSED TIME (HOURS) 0.00

**CONF 008

Manpower

TOTAL MANHOURS 0.00

ELAPSED TIME (HOURS) 0.00

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 278

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@A310

SERVICE BULLETIN

**CONF ALL

A. GENERAL

**CONF 001

(1) Subtask 282148-839-401-001 - Administrative

Manpower Resources

Skills UTILITY

Write in the applicable aircraft records that you have done all the work given in the

Service Bulletin.

(2) Subtask 282148-910-206-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

Elec. Std. Practices Manual (ESPM) 20-25-21

(a) Do a continuity test of disconnected wires (Refer to ESPM 20-25-21).

**CONF 002

(1) Subtask 282148-839-401-001 - Administrative

Manpower Resources

Skills UTILITY

Write in the applicable aircraft records that you have done all the work given in the

Service Bulletin.

(2) Subtask 282148-910-206-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

Elec. Std. Practices Manual (ESPM) 20-25-21

(a) Do a continuity test of disconnected wires (Refer to ESPM 20-25-21).

**CONF 003

(1) Subtask 282148-839-401-001 - Administrative

Manpower Resources

Skills UTILITY

Write in the applicable aircraft records that you have done all the work given in the

Service Bulletin.

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 279

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@A310

SERVICE BULLETIN

**CONF 004

(1) Subtask 282148-839-401-001 - Administrative

Manpower Resources

Skills UTILITY

Write in the applicable aircraft records that you have done all the work given in the

Service Bulletin.

**CONF 005

(1) Subtask 282148-839-401-001 - Administrative

Manpower Resources

Skills UTILITY

Write in the applicable aircraft records that you have done all the work given in the

Service Bulletin.

(2) Subtask 282148-910-206-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

Elec. Std. Practices Manual (ESPM) 20-25-21

(a) Do a continuity test of disconnected wires (Refer to ESPM 20-25-21).

**CONF 006

(1) Subtask 282148-839-401-001 - Administrative

Manpower Resources

Skills UTILITY

Write in the applicable aircraft records that you have done all the work given in the

Service Bulletin.

(2) Subtask 282148-910-206-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

Elec. Std. Practices Manual (ESPM) 20-25-21

(a) Do a continuity test of disconnected wires (Refer to ESPM 20-25-21).

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 280

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SERVICE BULLETIN

**CONF 007

(1) Subtask 282148-839-401-001 - Administrative

Manpower Resources

Skills UTILITY

Write in the applicable aircraft records that you have done all the work given in the

Service Bulletin.

**CONF 008

(1) Subtask 282148-839-401-001 - Administrative

Manpower Resources

Skills UTILITY

Write in the applicable aircraft records that you have done all the work given in the

Service Bulletin.

**CONF ALL

B. PREPARATION

**CONF 001

(1) Subtask 282148-941-402-001 - Job Set-up

Work Zones and Access Panels

Zone Access/Work location

612 Access Panel 612AT

623 Access Panel 623AB

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001

24-00-00, Page Block 301

24-41-00, Page Block 301

(a) Make sure that the aircraft is electrically grounded (Refer to AMM 24-00-00, Page

Block 301).

(b) De-energize the aircraft electrical circuits (Refer to AMM 24-41-00, Page Block

301).

(c) Put access platforms in position.

(d) Remove access panel(s) 612AT and/or 623AB (RH wing) (Refer to AMM 06-41-57,

Page Block 001).

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 281

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@A310

SERVICE BULLETIN

**CONF 002

(1) Subtask 282148-941-402-001 - Job Set-up

Work Zones and Access Panels

Zone Access/Work location

612 Access Panel 612AT

623 Access Panel 623AB

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001

24-00-00, Page Block 301

24-41-00, Page Block 301

(a) Make sure that the aircraft is electrically grounded (Refer to AMM 24-00-00, Page

Block 301).

(b) De-energize the aircraft electrical circuits (Refer to AMM 24-41-00, Page Block

301).

(c) Put access platforms in position.

(d) Remove access panel(s) 612AT and/or 623AB (RH wing) (Refer to AMM 06-41-57,

Page Block 001).

**CONF 003

None

**CONF 004

None

**CONF 005

(1) Subtask 282148-941-402-001 - Job Set-up

Work Zones and Access Panels

Zone Access/Work location

612 Access Panel 612AT

623 Access Panel 623AB

Manpower Resources

Skills AIRFRAME

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 282

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@A310

SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001

24-00-00, Page Block 301

24-41-00, Page Block 301

(a) Make sure that the aircraft is electrically grounded (Refer to AMM 24-00-00, Page

Block 301).

(b) De-energize the aircraft electrical circuits (Refer to AMM 24-41-00, Page Block

301).

(c) Put access platforms in position.

(d) Remove access panel(s) 612AT and/or 623AB (RH wing) (Refer to AMM 06-41-57,

Page Block 001).

**CONF 006

(1) Subtask 282148-941-402-001 - Job Set-up

Work Zones and Access Panels

Zone Access/Work location

612 Access Panel 612AT

623 Access Panel 623AB

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001

24-00-00, Page Block 301

24-41-00, Page Block 301

(a) Make sure that the aircraft is electrically grounded (Refer to AMM 24-00-00, Page

Block 301).

(b) De-energize the aircraft electrical circuits (Refer to AMM 24-41-00, Page Block

301).

(c) Put access platforms in position.

(d) Remove access panel(s) 612AT and/or 623AB (RH wing) (Refer to AMM 06-41-57,

Page Block 001).

**CONF 007

None

**CONF 008

None

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 283

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SERVICE BULLETIN

**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 282148-831-402-001 - Introduce a New Bracket on the Sub Spar Behind

the Front Spar Between RIB 8 and RIB 9 on the RH Wing

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills AIRFRAME

Material necessary to do the job

Kit 282148B01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 A5725068600000 1 Bracket

2 ASNA0078A502 2 Rivet

Consumable CMLB01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Corrosion Inhibiting Low

Adhesion Sealant

09-018 As required

Solvent General Purpose 11-026 As required

Lint-Free Cotton Cloth 19-003 As required

References

Fig. A-UBCAA

Additional Work 2 (Introduced at

Revision 03)- Location of Bracket on the

Sub Spar Behind the Front Spar

Between RIB 8 and RIB 9 (RH Wing)

Sheet 01

Refer to Fig. A-UBCAA Sheet 01

(a) Remove from the sub spar behind the front spar between RIB 8 and RIB 9 on the

RH wing, the items that follow:

2 Rivet NSA54213510DCA Item (2) Discard

1 Bracket A5724630400000 Item (1) Discard

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 284

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SERVICE BULLETIN

(b) Clean the mating surfaces use

Lint-Free Cotton

Cloth

19-003 As required

made moist with

Solvent General

Purpose

11-026 As required

(c) Put the

1 Bracket A5725068600000 Item 1

in position on the sub spar behind the front spar between RIB 8 and RIB 9 on the

RH wing (Refer to Fig. A-UBCAA Sheet 01).

(d) Copy drill the two holes from the sub spar through the Bracket, Item 1 to a

dimension of between 4.060 and 4.160 mm (0.160 and 0.164 in.).

(e) Deburr the holes that have been worked.

(f) Use

Corrosion Inhibiting

Low Adhesion

Sealant

09-018 As required

and wet install the

1 Bracket A5725068600000 Item 1

with the

2 Rivet, Blind ASNA0078A502 Item 2

on the sub spar behind the front spar between RIB 8 and RIB 9 on the RH wing.

**CONF 002

(1) Subtask 282148-831-402-001 - Introduce a New Bracket on the Sub Spar Behind

the Front Spar Between RIB 8 and RIB 9 on the RH Wing

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills AIRFRAME

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 285

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SERVICE BULLETIN

Material necessary to do the job

Kit 282148B01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 A5725068600000 1 Bracket

2 ASNA0078A502 2 Rivet

Consumable CMLB01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Corrosion Inhibiting Low

Adhesion Sealant

09-018 As required

Solvent General Purpose 11-026 As required

Lint-Free Cotton Cloth 19-003 As required

References

Fig. A-UBCAA

Additional Work 2 (Introduced at

Revision 03)- Location of Bracket on the

Sub Spar Behind the Front Spar

Between RIB 8 and RIB 9 (RH Wing)

Sheet 01

Refer to Fig. A-UBCAA Sheet 01

(a) Remove from the sub spar behind the front spar between RIB 8 and RIB 9 on the

RH wing, the items that follow:

2 Rivet NSA54213510DCA Item (2) Discard

1 Bracket A5724630400000 Item (1) Discard

(b) Clean the mating surfaces use

Lint-Free Cotton

Cloth

19-003 As required

made moist with

Solvent General

Purpose

11-026 As required

(c) Put the

1 Bracket A5725068600000 Item 1

in position on the sub spar behind the front spar between RIB 8 and RIB 9 on the

RH wing (Refer to Fig. A-UBCAA Sheet 01).

(d) Copy drill the two holes from the sub spar through the Bracket, Item 1 to a

dimension of between 4.060 and 4.160 mm (0.160 and 0.164 in.).

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 286

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@A310

SERVICE BULLETIN

(e) Deburr the holes that have been worked.

(f) Use

Corrosion Inhibiting

Low Adhesion

Sealant

09-018 As required

and wet install the

1 Bracket A5725068600000 Item 1

with the

2 Rivet, Blind ASNA0078A502 Item 2

on the sub spar behind the front spar between RIB 8 and RIB 9 on the RH wing.

**CONF 003

None

**CONF 004

None

**CONF 005

(1) Subtask 282148-831-402-001 - Introduce a New Bracket on the Sub Spar Behind

the Front Spar Between RIB 8 and RIB 9 on the RH Wing

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills AIRFRAME

Material necessary to do the job

Kit 282148B01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 A5725068600000 1 Bracket

2 ASNA0078A502 2 Rivet

Consumable CMLB01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Corrosion Inhibiting Low

Adhesion Sealant

09-018 As required

Solvent General Purpose 11-026 As required

Lint-Free Cotton Cloth 19-003 As required

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 287

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@A310

SERVICE BULLETIN

References

Fig. A-UBCAA

Additional Work 2 (Introduced at

Revision 03)- Location of Bracket on the

Sub Spar Behind the Front Spar

Between RIB 8 and RIB 9 (RH Wing)

Sheet 01

Refer to Fig. A-UBCAA Sheet 01

(a) Remove from the sub spar behind the front spar between RIB 8 and RIB 9 on the

RH wing, the items that follow:

2 Rivet NSA54213510DCA Item (2) Discard

1 Bracket A5724630400000 Item (1) Discard

(b) Clean the mating surfaces use

Lint-Free Cotton

Cloth

19-003 As required

made moist with

Solvent General

Purpose

11-026 As required

(c) Put the

1 Bracket A5725068600000 Item 1

in position on the sub spar behind the front spar between RIB 8 and RIB 9 on the

RH wing (Refer to Fig. A-UBCAA Sheet 01).

(d) Copy drill the two holes from the sub spar through the Bracket, Item 1 to a

dimension of between 4.060 and 4.160 mm (0.160 and 0.164 in.).

(e) Deburr the holes that have been worked.

(f) Use

Corrosion Inhibiting

Low Adhesion

Sealant

09-018 As required

and wet install the

1 Bracket A5725068600000 Item 1

with the

2 Rivet, Blind ASNA0078A502 Item 2

on the sub spar behind the front spar between RIB 8 and RIB 9 on the RH wing.

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 288

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@A310

SERVICE BULLETIN

**CONF 006

(1) Subtask 282148-831-402-001 - Introduce a New Bracket on the Sub Spar Behind

the Front Spar Between RIB 8 and RIB 9 on the RH Wing

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills AIRFRAME

Material necessary to do the job

Kit 282148B01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 A5725068600000 1 Bracket

2 ASNA0078A502 2 Rivet

Consumable CMLB01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Corrosion Inhibiting Low

Adhesion Sealant

09-018 As required

Solvent General Purpose 11-026 As required

Lint-Free Cotton Cloth 19-003 As required

References

Fig. A-UBCAA

Additional Work 2 (Introduced at

Revision 03)- Location of Bracket on the

Sub Spar Behind the Front Spar

Between RIB 8 and RIB 9 (RH Wing)

Sheet 01

Refer to Fig. A-UBCAA Sheet 01

(a) Remove from the sub spar behind the front spar between RIB 8 and RIB 9 on the

RH wing, the items that follow:

2 Rivet NSA54213510DCA Item (2) Discard

1 Bracket A5724630400000 Item (1) Discard

(b) Clean the mating surfaces use

Lint-Free Cotton

Cloth

19-003 As required

made moist with

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 289

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@A310

SERVICE BULLETIN

Solvent General

Purpose

11-026 As required

(c) Put the

1 Bracket A5725068600000 Item 1

in position on the sub spar behind the front spar between RIB 8 and RIB 9 on the

RH wing (Refer to Fig. A-UBCAA Sheet 01).

(d) Copy drill the two holes from the sub spar through the Bracket, Item 1 to a

dimension of between 4.060 and 4.160 mm (0.160 and 0.164 in.).

(e) Deburr the holes that have been worked.

(f) Use

Corrosion Inhibiting

Low Adhesion

Sealant

09-018 As required

and wet install the

1 Bracket A5725068600000 Item 1

with the

2 Rivet, Blind ASNA0078A502 Item 2

on the sub spar behind the front spar between RIB 8 and RIB 9 on the RH wing.

**CONF 007

None

**CONF 008

None

**CONF ALL

D. TEST

**CONF 001

None

**CONF 002

None

**CONF 003

None

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 290

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@A310

SERVICE BULLETIN

**CONF 004

None

**CONF 005

None

**CONF 006

None

**CONF 007

None

**CONF 008

None

**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 282148-942-402-001 - Close-up

Work Zones and Access Panels

Zone Access/Work location

612 Access Panel 612AT

623 Access Panel 623AB

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001

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

equipment.

(b) Install access panel(s) 612AT and/or 623AB (RH wing) (Refer to AMM 06-41-57,

Page Block 001).

**CONF 002

(1) Subtask 282148-942-402-001 - Close-up

Work Zones and Access Panels

Zone Access/Work location

612 Access Panel 612AT

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 291

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@A310

SERVICE BULLETIN

623 Access Panel 623AB

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001

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

equipment.

(b) Install access panel(s) 612AT and/or 623AB (RH wing) (Refer to AMM 06-41-57,

Page Block 001).

**CONF 003

None

**CONF 004

None

**CONF 005

(1) Subtask 282148-942-402-001 - Close-up

Work Zones and Access Panels

Zone Access/Work location

612 Access Panel 612AT

623 Access Panel 623AB

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001

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

equipment.

(b) Install access panel(s) 612AT and/or 623AB (RH wing) (Refer to AMM 06-41-57,

Page Block 001).

**CONF 006

(1) Subtask 282148-942-402-001 - Close-up

Work Zones and Access Panels

Zone Access/Work location

612 Access Panel 612AT

623 Access Panel 623AB

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 292

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@A310

SERVICE BULLETIN

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001

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

equipment.

(b) Install access panel(s) 612AT and/or 623AB (RH wing) (Refer to AMM 06-41-57,

Page Block 001).

**CONF 007

None

**CONF 008

None

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 293

6

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@A310

SERVICE BULLETIN

This Page Intentionally Left Blank

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 294

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@A310

SERVICE BULLETIN

Task 282148-831-850-001 - Modification - ADDITIONAL WORK 3 (Introduced at Rev 06)

**CONF ALL

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

INCLUDED IN THE REFERENCED PROCEDURES.

WARNING: THIS PROCEDURE USES A FUEL SYSTEM ITEM THAT IS IN A CATEGORY

KNOWN AS A CRITICAL DESIGN CONFIGURATION CONTROL LIMITATION

(CDCCL) CDCCL IDENTIFIES AN ITEM THAT CAN BE THE SOURCE OF A

POSSIBLE FUEL TANK IGNITION. YOU MUST KEEP ALL CDCCL ITEMS IN

THE APPROVED CONFIGURATION. DAMAGE, WEAR OR CHANGES TO A

CDCCL ITEM CAN CAUSE A POSSIBLE FUEL TANK EXPLOSION.

CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP

ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY

AND MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENANCE

WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING,

COMPONENTS AND THE WORK AREA AS CLEAN AS POSSIBLE. TO DO

THIS:

- PUT PROTECTION, SUCH AS PLASTIC SHEETING, CLOTHS, ETC; AS

NECESSARY ON WIRING AND COMPONENTS

- REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND

OTHER CONTAMINATION.

THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION

AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION.

IF THERE IS CONTAMINATION, REFER TO ESPM 20-55-00.

Task Associated Data

**CONF 001

Manpower

TOTAL MANHOURS 0.00

ELAPSED TIME (HOURS) 0.00

**CONF 002

Manpower

TOTAL MANHOURS 0.00

ELAPSED TIME (HOURS) 0.00

**CONF 003

Manpower

TOTAL MANHOURS 3.00

ELAPSED TIME (HOURS) 3.00

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 295

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@A310

SERVICE BULLETIN

**CONF 004

Manpower

TOTAL MANHOURS 3.00

ELAPSED TIME (HOURS) 3.00

**CONF 005

Manpower

TOTAL MANHOURS 0.00

ELAPSED TIME (HOURS) 0.00

**CONF 006

Manpower

TOTAL MANHOURS 0.00

ELAPSED TIME (HOURS) 0.00

**CONF 007

Manpower

TOTAL MANHOURS 3.00

ELAPSED TIME (HOURS) 3.00

**CONF 008

Manpower

TOTAL MANHOURS 3.00

ELAPSED TIME (HOURS) 3.00

**CONF ALL

A. GENERAL

**CONF 001

None

**CONF 002

None

**CONF 003

(1) Subtask 282148-910-203-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 296

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@A310

SERVICE BULLETIN

Material necessary to do the job

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Storage compound 15-008A As required

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-25-21

20-33-00

Standards Manual (SM)

Structural Repair Manual (SRM) 51-23-11

51-42-11

(a) Refer to the AIRBUS (Refer to Standards Manual (SM)) if you find part numbers for

the hardware components in the related kit(s) which you can not identify in the LIST

OF COMPONENTS of this Service Bulletin. The SM will give you the correct part

number to part number relationship.

(b) For material specification (Mat. No.) given in this Service Bulletin (Refer to

Consumable Material List (CML)).

(c) For panel location (Refer to AMM 06-41-53, Page Block 001).

(d) Obey the instructions for the wiring installation (Refer to ESPM 20-33-00).

(e) Apply

Storage compound 15-008A As required

to the screws after assembly.

(f) Installation of fasteners (Refer to SRM 51-42-11).

(g) For paint coatings (Refer to SRM 51-23-11).

(h) Do a continuity test of disconnected wires (Refer to ESPM 20-25-21).

(2) Subtask 282148-839-201-001 - Documentation

Manpower Resources

Skills NON SPECIFIC

Write in the applicable aircraft records that you have done all the work given in this

Service Bulletin.

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 297

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@A310

SERVICE BULLETIN

**CONF 004

(1) Subtask 282148-910-203-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

Material necessary to do the job

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Storage compound 15-008A As required

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-25-21

20-33-00

Standards Manual (SM)

Structural Repair Manual (SRM) 51-23-11

51-42-11

(a) Refer to the AIRBUS (Refer to Standards Manual (SM)) if you find part numbers for

the hardware components in the related kit(s) which you can not identify in the LIST

OF COMPONENTS of this Service Bulletin. The SM will give you the correct part

number to part number relationship.

(b) For material specification (Mat. No.) given in this Service Bulletin (Refer to

Consumable Material List (CML)).

(c) For panel location (Refer to AMM 06-41-53, Page Block 001).

(d) Obey the instructions for the wiring installation (Refer to ESPM 20-33-00).

(e) Apply

Storage compound 15-008A As required

to the screws after assembly.

(f) Installation of fasteners (Refer to SRM 51-42-11).

(g) For paint coatings (Refer to SRM 51-23-11).

(h) Do a continuity test of disconnected wires (Refer to ESPM 20-25-21).

(2) Subtask 282148-839-201-001 - Documentation

Manpower Resources

Skills NON SPECIFIC

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 298

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@A310

SERVICE BULLETIN

Write in the applicable aircraft records that you have done all the work given in this

Service Bulletin.

**CONF 005

None

**CONF 006

None

**CONF 007

(1) Subtask 282148-910-203-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

Material necessary to do the job

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Storage compound 15-008A As required

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-25-21

20-33-00

Standards Manual (SM)

Structural Repair Manual (SRM) 51-23-11

51-42-11

(a) Refer to the AIRBUS (Refer to Standards Manual (SM)) if you find part numbers for

the hardware components in the related kit(s) which you can not identify in the LIST

OF COMPONENTS of this Service Bulletin. The SM will give you the correct part

number to part number relationship.

(b) For material specification (Mat. No.) given in this Service Bulletin (Refer to

Consumable Material List (CML)).

(c) For panel location (Refer to AMM 06-41-53, Page Block 001).

(d) Obey the instructions for the wiring installation (Refer to ESPM 20-33-00).

(e) Apply

Storage compound 15-008A As required

to the screws after assembly.

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 299

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@A310

SERVICE BULLETIN

(f) Installation of fasteners (Refer to SRM 51-42-11).

(g) For paint coatings (Refer to SRM 51-23-11).

(h) Do a continuity test of disconnected wires (Refer to ESPM 20-25-21).

(2) Subtask 282148-839-201-001 - Documentation

Manpower Resources

Skills NON SPECIFIC

Write in the applicable aircraft records that you have done all the work given in this

Service Bulletin.

**CONF 008

(1) Subtask 282148-910-203-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

Material necessary to do the job

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Storage compound 15-008A As required

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-25-21

20-33-00

Standards Manual (SM)

Structural Repair Manual (SRM) 51-23-11

51-42-11

(a) Refer to the AIRBUS (Refer to Standards Manual (SM)) if you find part numbers for

the hardware components in the related kit(s) which you can not identify in the LIST

OF COMPONENTS of this Service Bulletin. The SM will give you the correct part

number to part number relationship.

(b) For material specification (Mat. No.) given in this Service Bulletin (Refer to

Consumable Material List (CML)).

(c) For panel location (Refer to AMM 06-41-53, Page Block 001).

(d) Obey the instructions for the wiring installation (Refer to ESPM 20-33-00).

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 300

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@A310

SERVICE BULLETIN

(e) Apply

Storage compound 15-008A As required

to the screws after assembly.

(f) Installation of fasteners (Refer to SRM 51-42-11).

(g) For paint coatings (Refer to SRM 51-23-11).

(h) Do a continuity test of disconnected wires (Refer to ESPM 20-25-21).

(2) Subtask 282148-839-201-001 - Documentation

Manpower Resources

Skills NON SPECIFIC

Write in the applicable aircraft records that you have done all the work given in this

Service Bulletin.

**CONF ALL

B. PREPARATION

**CONF 001

None

**CONF 002

None

**CONF 003

(1) Subtask 282148-941-203-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001

24-00-00, Page Block 301

24-41-00, Page Block 301

(a) Make sure that the aircraft is electrically grounded (Refer to AMM 24-00-00, Page

Block 301).

(b) De-energise the aircraft electrical circuits (Refer to AMM 24-41-00, Page Block

301).

(c) Put access platforms in position.

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 301

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@A310

SERVICE BULLETIN

(d) Remove access panels 612AT and/or 623AB (RH wing) (Refer to AMM 06-41-57,

Page Block 001).

**CONF 004

(1) Subtask 282148-941-203-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001

24-00-00, Page Block 301

24-41-00, Page Block 301

(a) Make sure that the aircraft is electrically grounded (Refer to AMM 24-00-00, Page

Block 301).

(b) De-energise the aircraft electrical circuits (Refer to AMM 24-41-00, Page Block

301).

(c) Put access platforms in position.

(d) Remove access panels 612AT and/or 623AB (RH wing) (Refer to AMM 06-41-57,

Page Block 001).

**CONF 005

None

**CONF 006

None

**CONF 007

(1) Subtask 282148-941-203-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001

24-00-00, Page Block 301

24-41-00, Page Block 301

(a) Make sure that the aircraft is electrically grounded (Refer to AMM 24-00-00, Page

Block 301).

(b) De-energise the aircraft electrical circuits (Refer to AMM 24-41-00, Page Block

301).

(c) Put access platforms in position.

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 302

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@A310

SERVICE BULLETIN

(d) Remove access panels 612AT and/or 623AB (RH wing) (Refer to AMM 06-41-57,

Page Block 001).

**CONF 008

(1) Subtask 282148-941-203-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001

24-00-00, Page Block 301

24-41-00, Page Block 301

(a) Make sure that the aircraft is electrically grounded (Refer to AMM 24-00-00, Page

Block 301).

(b) De-energise the aircraft electrical circuits (Refer to AMM 24-41-00, Page Block

301).

(c) Put access platforms in position.

(d) Remove access panels 612AT and/or 623AB (RH wing) (Refer to AMM 06-41-57,

Page Block 001).

**CONF ALL

C. PROCEDURE

**CONF 001

None

**CONF 002

None

**CONF 003

(1) Subtask 282148-831-253-001 - Modification

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 303

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@A310

SERVICE BULLETIN

Material necessary to do the job

Kit 282148D02R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

126 NSA938184PV1601 15 PIN

Kit 282148D07R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

31 NSA5527-03-02D 2 SPACER

110 NSA935807C10 1 CLAMP

112 NAS1149D0332K 1 WASHER

117 NSA935807C09 3 CLAMP

120 NSA5516-04NV 1 CLAMP

130 NSA5527-03-08D 1 SPACER

135 NAS1096-3-42 1 SCREW

References

Fig. A-GBPAB

Additional Work 3 - Improvement of the

2S-Route in the RH-Wing Pylon Area

Sheet 01

Fig. A-GHAAA

Hook-up Chart

Sheet 01

Fig. A-GHBAA

Hook-up Chart

Sheet 01

(a) Disconnect these wires of route 2S from the receptacles 40VC and 5006VC in

accordance with the Hook-up Chart 1, Lines 1 thru 14, END 1, Fig. A-GHAAA

Sheet 01 and the Hook-up Chart 2, Lines 2 thru 8, END 1, Fig. A-GHBAA Sheet

01.

(b) Remove, refer to Fig. A-GBPAB Sheet 01

1 Spacer NSA5527-03-05D Item (114) Discard

3 Clamp NSA935807C09 Item (117) Discard

1 Spacer NSA5527-03-02D Item (31) Discard

1 Clamp NSA5516-04NV Item (120) Discard

1 Screw NAS1096-3-28 Item (151) Discard

1 Clamp NSA935807C10 Item (110) Discard

1 Spacer Item (152) Discard

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 304

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@A310

SERVICE BULLETIN

(c) Install, refer to Fig. A-GBPAB Sheet 01

1 Screw NAS1096-3-42 Item 135

1 Washer NAS1149D0332K Item 112

1 Clamp NSA5516-04NV Item 120

2 Spacer NSA5527-03-02D Item 31

1 Spacer NSA5527-03-08D Item 130

3 Clamp NSA935807C09 Item 117

1 Clamp NSA935807C10 Item 110

(d) Connect the electrical wires of route 2S to the receptacles 40VC and 5006VC in

accordance with the Hook-up Chart 1, Lines 1 thru 14, END 1, Fig. A-GHAAA

Sheet 01 and the Hook-up Chart 2, lines 2 thru 8, END 1, Fig. A-GHBAA Sheet 01.

Use the contact pins if required:

15 Pin NSA938184PV1601 Item 126

**CONF 004

(1) Subtask 282148-831-253-003 - Modification

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

Material necessary to do the job

Kit 282148D02R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

126 NSA938184PV1601 15 PIN

Kit 282148D08R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

30 NSA5527-03-01D 1 SPACER

31 NSA5527-03-02D 1 SPACER

111 NSA935807C16 2 CLAMP

112 NSA935808-01 1 WASHER

117 NSA935807C09 1 CLAMP

120 NSA5516-04NV 1 CLAMP

123 NAS1801-3-31 1 SCREW

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 305

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@A310

SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

130 NSA5527-03-08D 1 SPACER

References

Fig. A-GBPAA

Additional Work 3 - Improvement of the

2S-Route in the RH-Wing Pylon Area

Sheet 01

Fig. A-GHBAA

Hook-up Chart

Sheet 01

(a) Disconnect these wires of route 2S from the receptacles 40VC and 5006VC in

accordance with the Hook-up Chart 2, Lines 2 thru 8, END 1, Fig. A-GHBAA Sheet

01.

(b) Remove, refer to Fig. A-GBPAA Sheet 01

1 Spacer NSA5527-03-05D Item (114) Discard

1 Clamp NSA935807C09 Item (117) Discard

1 Spacer NSA5527-03-01D Item (30) Discard

1 Clamp NSA5516-04NV Item (120) Discard

2 Clamp NSA935807C16 Item (111) Discard

1 Spacer NSA5527-03-08D Item (130) Discard

1 Washer NSA935808-01 Item (112) Discard

1 Screw NAS1801-3-31 Discard

(c) Install, refer to Fig. A-GBPAA Sheet 01

1 Screw NAS1801-3-31 Item 123

1 Clamp NSA5516-04NV Item 120

1 Spacer NSA5527-03-01D Item 30

1 Spacer NSA5527-03-02D Item 31

1 Spacer NSA5527-03-08D Item 130

1 Clamp NSA935807C09 Item 117

2 Clamp NSA935807C16 Item 111

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 306

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@A310

SERVICE BULLETIN

1 Washer NSA935808-01 Item 112

(d) Connect the electrical wires of route 2S to the receptacles 40VC and 5006VC in

accordance with the Hook-up Chart 2, lines 2 thru 8, END 1, Fig. A-GHBAA Sheet

01. Use the contact pins if required:

15 Pin NSA938184PV1601 Item 126

**CONF 005

None

**CONF 006

None

**CONF 007

(1) Subtask 282148-831-253-001 - Modification

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

Material necessary to do the job

Kit 282148D02R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

126 NSA938184PV1601 15 PIN

Kit 282148D07R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

31 NSA5527-03-02D 2 SPACER

110 NSA935807C10 1 CLAMP

112 NAS1149D0332K 1 WASHER

117 NSA935807C09 3 CLAMP

120 NSA5516-04NV 1 CLAMP

130 NSA5527-03-08D 1 SPACER

135 NAS1096-3-42 1 SCREW

References

Fig. A-GBPAB

Additional Work 3 - Improvement of the

2S-Route in the RH-Wing Pylon Area

Sheet 01

Fig. A-GHAAA

Hook-up Chart

Sheet 01

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 307

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@A310

SERVICE BULLETIN

References

Fig. A-GHBAA

Hook-up Chart

Sheet 01

(a) Disconnect these wires of route 2S from the receptacles 40VC and 5006VC in

accordance with the Hook-up Chart 1, Lines 1 thru 14, END 1, Fig. A-GHAAA

Sheet 01 and the Hook-up Chart 2, Lines 2 thru 8, END 1, Fig. A-GHBAA Sheet

01.

(b) Remove, refer to Fig. A-GBPAB Sheet 01

1 Spacer NSA5527-03-05D Item (114) Discard

3 Clamp NSA935807C09 Item (117) Discard

1 Spacer NSA5527-03-02D Item (31) Discard

1 Clamp NSA5516-04NV Item (120) Discard

1 Screw NAS1096-3-28 Item (151) Discard

1 Clamp NSA935807C10 Item (110) Discard

1 Spacer Item (152) Discard

(c) Install, refer to Fig. A-GBPAB Sheet 01

1 Screw NAS1096-3-42 Item 135

1 Washer NAS1149D0332K Item 112

1 Clamp NSA5516-04NV Item 120

2 Spacer NSA5527-03-02D Item 31

1 Spacer NSA5527-03-08D Item 130

3 Clamp NSA935807C09 Item 117

1 Clamp NSA935807C10 Item 110

(d) Connect the electrical wires of route 2S to the receptacles 40VC and 5006VC in

accordance with the Hook-up Chart 1, Lines 1 thru 14, END 1, Fig. A-GHAAA

Sheet 01 and the Hook-up Chart 2, lines 2 thru 8, END 1, Fig. A-GHBAA Sheet 01.

Use the contact pins if required:

15 Pin NSA938184PV1601 Item 126

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 308

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@A310

SERVICE BULLETIN

**CONF 008

(1) Subtask 282148-831-253-003 - Modification

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

Material necessary to do the job

Kit 282148D02R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

126 NSA938184PV1601 15 PIN

Kit 282148D08R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

30 NSA5527-03-01D 1 SPACER

31 NSA5527-03-02D 1 SPACER

111 NSA935807C16 2 CLAMP

112 NSA935808-01 1 WASHER

117 NSA935807C09 1 CLAMP

120 NSA5516-04NV 1 CLAMP

123 NAS1801-3-31 1 SCREW

130 NSA5527-03-08D 1 SPACER

References

Fig. A-GBPAA

Additional Work 3 - Improvement of the

2S-Route in the RH-Wing Pylon Area

Sheet 01

Fig. A-GHBAA

Hook-up Chart

Sheet 01

(a) Disconnect these wires of route 2S from the receptacles 40VC and 5006VC in

accordance with the Hook-up Chart 2, Lines 2 thru 8, END 1, Fig. A-GHBAA Sheet

01.

(b) Remove, refer to Fig. A-GBPAA Sheet 01

1 Spacer NSA5527-03-05D Item (114) Discard

1 Clamp NSA935807C09 Item (117) Discard

1 Spacer NSA5527-03-01D Item (30) Discard

1 Clamp NSA5516-04NV Item (120) Discard

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 309

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@A310

SERVICE BULLETIN

2 Clamp NSA935807C16 Item (111) Discard

1 Spacer NSA5527-03-08D Item (130) Discard

1 Washer NSA935808-01 Item (112) Discard

1 Screw NAS1801-3-31 Discard

(c) Install, refer to Fig. A-GBPAA Sheet 01

1 Screw NAS1801-3-31 Item 123

1 Clamp NSA5516-04NV Item 120

1 Spacer NSA5527-03-01D Item 30

1 Spacer NSA5527-03-02D Item 31

1 Spacer NSA5527-03-08D Item 130

1 Clamp NSA935807C09 Item 117

2 Clamp NSA935807C16 Item 111

1 Washer NSA935808-01 Item 112

(d) Connect the electrical wires of route 2S to the receptacles 40VC and 5006VC in

accordance with the Hook-up Chart 2, lines 2 thru 8, END 1, Fig. A-GHBAA Sheet

01. Use the contact pins if required:

15 Pin NSA938184PV1601 Item 126

**CONF ALL

D. TEST

**CONF 001

None

**CONF 002

None

**CONF 003

None

**CONF 004

None

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 310

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@A310

SERVICE BULLETIN

**CONF 005

None

**CONF 006

None

**CONF 007

None

**CONF 008

None

**CONF ALL

E. CLOSE-UP

**CONF 001

None

**CONF 002

None

**CONF 003

(1) Subtask 282148-942-202-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001

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

equipment.

(b) Install access panels 612AT and/or 623AB (RH wing) (Refer to AMM 06-41-57,

Page Block 001).

**CONF 004

(1) Subtask 282148-942-202-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 311

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@A310

SERVICE BULLETIN

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

equipment.

(b) Install access panels 612AT and/or 623AB (RH wing) (Refer to AMM 06-41-57,

Page Block 001).

**CONF 005

None

**CONF 006

None

**CONF 007

(1) Subtask 282148-942-202-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001

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

equipment.

(b) Install access panels 612AT and/or 623AB (RH wing) (Refer to AMM 06-41-57,

Page Block 001).

**CONF 008

(1) Subtask 282148-942-202-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001

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

equipment.

(b) Install access panels 612AT and/or 623AB (RH wing) (Refer to AMM 06-41-57,

Page Block 001).

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 312

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@A310

SERVICE BULLETIN

**CONF ALL

PYLON

FRONT SPAR

SCREW JACK 1TRACK 1

SCREW JACK 2

TRACK 3

Z612

D

E

F

RIB2

RIB4

RIB8

RIB7

RIB3 624VB /2S

A

3R/1S

B_SB_282148_6_BEAA_01_00

B

C

M

H

J

K

A

L

Figure A-GBEAA - Sheet 01

Improvement of the 2S-Route in the RH-Wing in Zone 612 (Kit D01)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 313

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

**CONF ALL

RIB2

RIB2

2842−5052 TO 2842−5056

AND 2842−5070

(MAT. NO. 15−008)

WIRE NUMBERS

3R/1S

3R/1S

NOTE:

1M

2M

1M

2M

624VB /2S

(31)

(22)

(40)

(100)

(50)

(23)

(100)

624VB /2S

5006VC

624VB /2S

TO 40VC

AND

(23)

(50)

(31)

(40)

(22)

(100)

1

11

B_SB_282148_6_BEAA_02_00

AFTER

BEFORE

B

C

Figure A-GBEAA - Sheet 02

Improvement of the 2S-Route in the RH-Wing in Zone 612 (Kit D01)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 314

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

**CONF ALL

2842−5052 TO 2842−5056

AND 2842−5070

(MAT. NO. 15−008)

WIRE NUMBERS

3R/1S

3R/1S

NOTE:

624VB /2S

(31)

(22) (40)

(100)

624VB /2S

5006VC

624VB /2S

TO 40VC

AND

(31)

(40) (22)

(54)

(54)

618VB /2G

618VB /2E

618VB /2G

618VB /2E

1

11

AFTER

BEFORE

B_SB_282148_6_BEAA_03_00

D

E

Figure A-GBEAA - Sheet 03

Improvement of the 2S-Route in the RH-Wing in Zone 612 (Kit D01)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 315

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

**CONF ALL

DIMENSIONS

mm

A

B

C

(in.)

1000.0 39.37

100.0 3.94

30.0 1.18

A

B C B

TO

TIE

TIE

1

TO 40VC AND 624VB /2S 5006VC

624VB /2S

616VB

642VB

G

624VB /2S

624VB /2S

40VC 5006VC

616VB642VB

AND

F

G

TYPICAL INSTALLATION OF SLEEVES

B_SB_282148_6_BEAA_04_00

Figure A-GBEAA - Sheet 04

Improvement of the 2S-Route in the RH-Wing in Zone 612 (Kit D01)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 316

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

**CONF ALL

(MAT. NO. 15−008)

3R/1S

3R/1S

NOTE:

624VB /2S

(22)

(40)

(100)

624VB /2S

5006VC

624VB /2S

TO 40VC

TO

(40)

(22)

TIE

TIE

2842−5052 TO 2842−5056

WIRE NUMBER 2842−5070

WIRE NUMBERS

(100)

(55)

(40)

(55)

(22)

12

(22)

(55)

12

(40)

(55)

624VB /2S

B_SB_282148_6_BEAA_05_00

AFTER

BEFORE

H

J

Figure A-GBEAA - Sheet 05

Improvement of the 2S-Route in the RH-Wing in Zone 612 (Kit D01)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 317

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

**CONF ALL

3R/1S/1M

624VB /2S

624VB /2S

2S/1M

B_SB_282148_6_BEAA_06_00

BEFORE

K

Figure A-GBEAA - Sheet 06

Improvement of the 2S-Route in the RH-Wing in Zone 612 (Kit D01)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 318

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

**CONF ALL

3R/1S/1M

NOTE:

624VB /2S

624VB /2S

2842−5052 TO 2842−5056

WIRE NUMBER 2842−5070

WIRE NUMBERS

2S/1M

1

B_SB_282148_6_BEAA_07_00

AFTER

L

Figure A-GBEAA - Sheet 07

Improvement of the 2S-Route in the RH-Wing in Zone 612 (Kit D01)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 319

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

**CONF ALL

DIMENSIONS

mm

A

B

C

(in.)

1000.0 39.37

100.0 3.94

30.0 1.18

A

B C B

TO

TIE

TIE

1

624VB /2S

TO 40VC 

5006VC

624VB /2S

616VB

642VB

624VB /2S

624VB /2S

40VC

5006VC

TO

616VB642VB

TYPICAL INSTALLATION OF SLEEVES

624VB /2STO

624VB /2S

B_SB_282148_6_BEAA_08_00

N

N

M

Figure A-GBEAA - Sheet 08

Improvement of the 2S-Route in the RH-Wing in Zone 612 (Kit D01)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 320

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

**CONF ALL

PYLON

FRONT SPAR

TRACK 4

SCREW JACK 3

1M

1S

MASTER TRACK 5

RIB12

RIB11

RIB10

RIB9

636VB /2S

636VB /2M

Z623

B_SB_282148_6_BFAA_01_00

A

B

C

D

E

F

G

H

J

F

G

R

S

K

L

K

L

M

N

P

Q

A

Figure A-GBFAA - Sheet 01

Improvement of the 2S-Route in the RH-Wing in Zone 623 (Kit D01)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 321

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

**CONF ALL

TO 10QT − B

636VB /2S

B_SB_282148_6_BFAA_02_00

TO 10QT − B

1

636VB /2S 636VB /2M

636VB /2S

636VB /2M

1S

1M

1S

1M

BEFORE

AFTER

B

C

Figure A-GBFAA - Sheet 02

Improvement of the 2S-Route in the RH-Wing in Zone 623 (Kit D01)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 322

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

**CONF ALL

30

TYPICAL

TYPICAL

1S

1M

TO 10QT − A

1S

TO 10QT − A

APPLY (MAT. NO. 15−008)

NOTE:

636VB /2S

636VB /2M

121

(22)

(121)

(122)

(112)

(22)

(23)

(31)

(30)

(112)

(122)

(23) (31)

(30)

1

636VB /2S

636VB /2M

10

B_SB_282148_6_BLAA_03_00

BEFORE

AFTER

D

E

(22)

(2 POS)

B_SB_282148_6_BFAA_03_00

Figure A-GBFAA - Sheet 03

Improvement of the 2S-Route in the RH-Wing in Zone 623 (Kit D01)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 323

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

**CONF ALL

APPLY (MAT. NO. 15−008)

NOTE:

636VB /2S

636VB /2M

636VB /2S

636VB /2M

1S

1M

TYPICAL

1S

1M

TYPICAL

AND

TO

(30)

(22)

(40)

(52)

(22)

636VB /2S

1

10

(30)

(22) (40)

(52)

(22)

B_SB_282148_6_BFAA_04_00

AFTER

BEFORE

F

G

10QTA

10QTB

Figure A-GBFAA - Sheet 04

Improvement of the 2S-Route in the RH-Wing in Zone 623 (Kit D01)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 324

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

**CONF ALL

APPLY (MAT. NO. 15−008)

NOTE:

636VB /2S

636VB /2M

636VB /2S

636VB /2M

TYPICAL

TYPICAL

1S

1M

1S

1M

TO

AND

636VB /2S

10

(32)

(30)

(22)

(22)

(51)

(40)

(32)

(22)

(23)

(30)

(22)

(51)

(40)

AFTER

BEFORE

H

1

J

B_SB_282148_6_BFAA_05_00

10QTA

10QTB

Figure A-GBFAA - Sheet 05

Improvement of the 2S-Route in the RH-Wing in Zone 623 (Kit D01)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 325

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

**CONF ALL

APPLY (MAT. NO. 15−008)

NOTE:

636VB /2S

636VB /2M

TYPICAL

TYPICAL

1M/1S

TO

AND

636VB /2S

1 10

(30)

(22)

(40)

(32)

(30)

(22) (51)

(40)

14

636VB2M /2S

1M/1S

B_SB_282148_6_BFAA_06_00

AFTER

BEFORE

K

L

10QTA

10QTB

Figure A-GBFAA - Sheet 06

Improvement of the 2S-Route in the RH-Wing in Zone 623 (Kit D01)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 326

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

**CONF ALL

APPLY (MAT. NO. 15−008A)

NOTE:

636VB /2S

636VB /2M

636VB /2S

636VB /2M

1S

1M

1S

1M

TO

AND

636VB /2S

1

10

(32) (30)

(22)

(22)

(51)

(40)

(32)

(22)

(23)

(30)

(22)

(51)

(40)

B_SB_282148_6_BFAA_07_00

AFTER

BEFORE

M

N

10QTA

10QTB

Figure A-GBFAA - Sheet 07

Improvement of the 2S-Route in the RH-Wing in Zone 623 (Kit D01)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 327

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

**CONF ALL

636VB2M /2S

1M/1S

52VP

44VP 5002VP

2S

2M 1M/1S

1M

636VB /2M

(32)

(31)

(40)

(52)

(21) (21)

B_SB_282148_6_BFAA_08_00

BEFORE

P

Figure A-GBFAA - Sheet 08

Improvement of the 2S-Route in the RH-Wing in Zone 623 (Kit D01)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 328

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

**CONF ALL

APPLY (MAT. NO. 15−008)

NOTE:

636VB2M /2S

1M/1S

1M

636VB /2M

(32)

(31)

(40)

(52)

(21)

52VP

44VP 5002VP

2S

2M 1M/1S

1

TO

AND

636VB /2S

10

B_SB_282148_6_BFAA_09_00

AFTER

Q

10QTA

10QTB

Figure A-GBFAA - Sheet 09

Improvement of the 2S-Route in the RH-Wing in Zone 623 (Kit D01)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 329

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

**CONF ALL

WIRE NUMBERS 2842−5061 TO 5065 AND 2842−5071

NOTE:

DIMENSIONS

mm

A

B

C

(in.)

1000.0 39.370

100.0 3.937

30.0 1.181

A

B C B

TYPICAL INSTALLATION OF SLEEVES

TO

TIE

TIE

TYPICAL INSTALLATION OFWIRE CROSSING

TIE OR

636VB /2S

636VB /2S

1

636VB /2S

636VB /2S

15

16

B_SB_282148_6_BFAA_10_00

S

T

T

R

10QTA 10QTB AND

TO AND 10QTB 10QTA

Figure A-GBFAA - Sheet 10

Improvement of the 2S-Route in the RH-Wing in Zone 623 (Kit D01)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 330

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

**CONF 001, 005

AFTER SB A310−36−2015 OR

MODIFICATION 7633S8497

NOTE:

P

636VB /2S

(125)

52VP

44VP

52VP

636VB /2S

636VB /2S

2212VC

38VC

5006VC

5006VC 40VC

40VC

636VB /2S

636VB2S

(125)

(125)

(125)

(125)

(125)

Z612

B_SB_282148_6_BGAA_01_00

BEFORE

A B

D

F

H

H

K

M

A

C

Figure A-GBGAA - Sheet 01

Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D02)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 331

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

**CONF 001, 005

AFTER SB A310−36−2015 OR

MODIFICATION 7633S8497

NOTE:

N

Q

52VP

44VP

52VP

2212VC

5006VC

5006VC

40VC

40VC

1

125

125

125 636VB

125

125

125

125 636VB

125

109

125

2S

2S / QT

2S 2S / QT

125

B_SB_282148_6_BGAA_02_00

AFTER

TYPICAL PLACARD

INSTALLATION

C

1

E G

J

J

L

C

B

Figure A-GBGAA - Sheet 02

Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D02)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 332

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

**CONF 001, 005

B_SB_282148_6_BGAA_03_00

APPLY (MAT. NO. 15−008)

NOTE:

636VB /2S

636VB /2M

636VB /2S

636VB /2M

636VB /2S TO 10QT

CLAMP

CLAMP

(109)

(110)

(111)

(113)

(112)

(31)

(114)

(117) (115)

(116)

109

117

(112)

(113)

(117)

(115)

(116)

(111)

AFTER

BEFORE

D

E

30

Figure A-GBGAA - Sheet 03

Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D02)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 333

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

**CONF 001, 005

APPLY (MAT. NO. 15−008)

NOTE:

636VB /2S

636VB /2M

636VB /2S

636VB /2M

636VB /2S TO

(109)

(110)

(111)

(112)

(31)

(117)

109 117

(117)

(111)

TO PYLON

TO 

TO PYLON

TO 2212VC

(30)

(118)

(30)

(112)

(118)

2212VC

(110)

(31)

(30)

(30)

117

109

B_SB_282148_6_BGAA_04_00

AFTER

BEFORE

F

G

10QT

Figure A-GBGAA - Sheet 04

Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D02)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 334

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

**CONF 001, 005

APPLY (MAT. NO. 15−008)

NOTE:

636VB /2S

636VB /2M

636VB /2S

636VB /2M

636VB /2S TO

(109) (110)

(111)

(117)

109 117

(117)

(111)

TO 

TO 2212VC

(30)

(118)

(118)

2212VC

(31)

(30)

117

109

TYPICAL

TYPICAL AFTER SB A310−36−2015 OR

MODIFICATION 7633S8497

TO PYLON

CLAMP

CLAMP

TO PYLON

(115)

(114)

(31)

(114)

(115)

B_SB_282148_6_BGAA_05_00

AFTER

BEFORE

H

J

10QT

Figure A-GBGAA - Sheet 05

Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D02)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 335

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

**CONF 001, 005

APPLY (MAT. NO. 15−008)

NOTE:

636VB /2S

636VB /2M

636VB /2S

636VB /2M

636VB /2S

(109)

(110) (111)

(117)

109

117

(117)

(111)

TO 

TO 2212VC

(30)

(118)

(118)

2212VC

(31)

(30)

117

109

AFTER SB A310−36−2015 OR

MODIFICATION 7633S8497

TO PYLON

CLAMP

CLAMP

TO PYLON

(115)

(114)

(31)

(114)

CONDUIT

CONDUIT

(115)

AFTER

BEFORE

K

L

B_SB_282148_6_BGAA_06_00

TO 10QT

Figure A-GBGAA - Sheet 06

Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D02)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 336

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

**CONF 001, 005

APPLY (MAT. NO. 15−008)

NOTE:

636VB /2S

636VB /2M

636VB /2S

636VB /2M

636VB /2S

(109)

(110)

(111)

(117)

109

(111)

(30)

(112)

(118)

(31)

(30)

117

109

(114)

(31)

(114)

644VB1M /1S

(118)

(112)

644VB1M /1S

(117)

117

AFTER

BEFORE

M

N

B_SB_282148_6_BGAA_07_00

TO 10QT

Figure A-GBGAA - Sheet 07

Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D02)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 337

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

**CONF 001, 005

APPLY (MAT. NO. 15−008)

NOTE:

636VB /2S

636VB /2M

636VB /2S

636VB /2M

636VB /2S

(109) (110)

(111)

(117)

109

(111)

(112)

(31)

117

109

(114)

(31)

(114)

644VB1M /1S

(112)

644VB1M /1S

(117)

(119)

(119)

(2 POS)

AFTER

BEFORE

P

Q

B_SB_282148_6_BGAA_08_00

TO 10QT

Figure A-GBGAA - Sheet 08

Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D02)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 338

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

**CONF 002, 006

AFTER SB A310−36−2015 OR

MODIFICATION 7633S8497

NOTE:

P

52VP

44VP

52VP

636VB /2S

(132)

(132)

5006VC 40VC

38VC

5006VC

(132)

Z612

BEFORE

D

F

H

H

K

M

A

B_SB_282148_6_BHAA_01_00

A B

C

Figure A-GBHAA - Sheet 01

Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D03)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 339

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

**CONF 002, 006

AFTER SB A310−36−2015 OR

MODIFICATION 7633S8497

NOTE:

52VP

44VP

5006VC

40VC

40VC

636VB

126

636VB

109

132

N

Q

132

132

132

132

132

1

132

132

132

132

2S

2S / QT

2S

2S / QT

AFTER

TYPICAL PLACARD

INSTALLATION

C

E

G

J

J

L

52VP

C

B

B_SB_282148_6_BHAA_02_00

5006VC

Figure A-GBHAA - Sheet 02

Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D03)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 340

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

**CONF 002, 006

636VB /2S

636VB /2M

636VB /2S

636VB /2M

(111)

(113)

(31)

(114)

(116)

109

117

(113)

(116)

(111)

CLAMP

CLAMP

(112)

(31)

(124)

(124)

(112)

(114)

BEFORE

AFTER

B_SB_282148_6_BHAA_03_00

D

E

Figure A-GBHAA - Sheet 03

Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D03)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 341

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

**CONF 002, 006

636VB /2S

636VB /2M

636VB /2S

636VB /2M

(111)

(112)

(31)

(111)

(112)

(31)

117

109

(113)

(114)

(113)

(114)

B_SB_282148_6_BHAA_04_00

BEFORE

AFTER

F

G

Figure A-GBHAA - Sheet 04

Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D03)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 342

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

**CONF 002, 006

636VB /2S

636VB /2M

636VB /2S

636VB /2M

(111)

(112) (31)

(111)

(112) (31)

117 109

(113) (114)

(113) (114)

B_SB_282148_6_BHAA_05_00

BEFORE

AFTER

H

J

Figure A-GBHAA - Sheet 05

Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D03)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 343

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

**CONF 002, 006

636VB /2S

636VB /2M

636VB /2S

636VB /2M

(111)

(112)

(31)

(111)

(31)

117

109

(123)

(120)

123

(120)

(112)

(31)

BEFORE

AFTER

K

L

B_SB_282148_6_BHAA_06_00

Figure A-GBHAA - Sheet 06

Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D03)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 344

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

**CONF 002, 006

636VB /2S

636VB /2M

636VB /2S

636VB /2M

(111)

(112)

(31)

(111)

(31)

117

109

123

(112)

(114)

(113)

(114)

130

B_SB_282148_6_BHAA_07_00

BEFORE

AFTER

M

N

Figure A-GBHAA - Sheet 07

Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D03)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 345

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

**CONF 002, 006

636VB /2S

636VB /2M

636VB /2S

636VB /2M

(111)

(112)

(31)

(111)

(31)

117

109

123

(112)

(114)

(113)

131

31

(114)

BEFORE

AFTER

P

Q

B_SB_282148_6_BHAA_08_00

Figure A-GBHAA - Sheet 08

Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D03)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 346

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

**CONF 003, 007

E

G

C

L

A B

J

Z612

5006VC 40VC

636VB /2S

38VC

636VB /2S

44VP

52VP

(1)

B_SB_282148_6_BJAA_01_00

BEFORE

A

G

N

Figure A-GBJAA - Sheet 01

Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D05)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 347

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

**CONF 003, 007

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

NOTE:

D

F

H

H

M

ELEC. WIRES 636VB/2S THRU 5006VC (2842−5071)

ELEC. WIRES 636VB/2S THRU 52VP (2842−5061, 2842−5062, 2842−5063, 2842−5064, 2842−5065 AND 2842−5071)

(3 POS)

K

5006VC 40VC

636VB /2S

636VB /2S

44VP

52VP

38VC

1

B_SB_282148_6_BJAA_02_00

AFTER

B

Q

P

Figure A-GBJAA - Sheet 02

Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D05)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 348

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

**CONF 003, 007

117

117

136

30

(112)

(116)

(136)

(112)

(116)

644VB /1S

644VB /1M

636VB /2M

644VB /1S

644VB /1M

636VB /2M

636VB /2S

ELEC. WIRES 636VB/2S THRU 10QT (2842−5061, 2842−5062,

NOTE:

 2842−5063, 2842−5064, 2842−5065 AND 2842−5071)

636VB /2S

(117)

(30)

B_SB_282148_6_BJAA_03_00

BEFORE

AFTER

C

D

Figure A-GBJAA - Sheet 03

Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D05)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 349

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

**CONF 003, 007

117

117

(117)

(112)

(113)

(112)

(113)

644VB /1S

644VB /1M

2212VC

636VB /2M

644VB /1S

644VB /1M

2212VC

636VB /2M

TO

ELEC. WIRES 636VB/2S THRU 10QT (2842−5061, 2842−5062,

NOTE:

 2842−5063, 2842−5064, 2842−5065 AND 2842−5071)

TO

B_SB_282148_6_BJAA_04_00

BEFORE

AFTER

E

F

Figure A-GBJAA - Sheet 04

Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D05)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 350

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

**CONF 003, 007

ELEC. WIRES 636VB/2S THRU 10QT (2842−5061, 2842−5062,

NOTE:

 2842−5063, 2842−5064, 2842−5065 AND 2842−5071)

117

117

(117)

(112)

(113)

(112)

(113)

644VB /1S

644VB /1M

2212VC

636VB /2M

644VB /1S

644VB /1M

2212VC

636VB /2M

TO

TO

636VB /2S

636VB /2S

BEFORE

AFTER

G

H

B_SB_282148_6_BJAA_05_00

Figure A-GBJAA - Sheet 05

Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D05)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 351

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

**CONF 003, 007

ELEC. WIRES 636VB/2S THRU 10QT (2842−5061, 2842−5062,

NOTE:

 2842−5063, 2842−5064, 2842−5065 AND 2842−5071)

117

117

(117)

(112)

(112)

644VB /1S

644VB /1M

2212VC

636VB /2M

644VB /1S

644VB /1M

2212VC

636VB /2M

TO

TO

636VB /2S

636VB /2S

31

(135)

135

(30)

BEFORE

AFTER

J

K

B_SB_282148_6_BJAA_06_00

Figure A-GBJAA - Sheet 06

Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D05)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 352

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

**CONF 003, 007

ELEC. WIRES 636VB/2S THRU 10QT (2842−5061, 2842−5062,

NOTE:

 2842−5063, 2842−5064, 2842−5065 AND 2842−5071)

117

117

(117)

(112)

(113)

(112)

(113)

644VB /1S

644VB /1M

636VB /2M

644VB /1S

644VB /1M

636VB /2M

636VB /2S

636VB /2S

B_SB_282148_6_BJAA_07_00

BEFORE

AFTER

M

L

Figure A-GBJAA - Sheet 07

Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D05)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 353

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

**CONF 003, 007

117

117

(117)

(112)

(113)

(112)

(113)

644VB /1S

644VB /1M

636VB /2M

644VB /1S

644VB /1M

636VB /2M

636VB /2S

636VB /2S

ELEC. WIRES 636VB/2S THRU 10QT (2842−5061, 2842−5062,

NOTE:

 2842−5063, 2842−5064, 2842−5065 AND 2842−5071) B_SB_282148_6_BJAA_08_00

BEFORE

AFTER

N

P

Figure A-GBJAA - Sheet 08

Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D05)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 354

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

**CONF 003, 007

TO 10QT−A AND 10QT−B

A

A

TO 10QT−A AND 10QT−B

ALL 100.0 mm

(ALL 3.94 in)

1000.0 mm

(39.37 in)

THE ENDS OF THE PROTECTION SLEEVES, ITEM 1, MUST OVERLAP

NOTE:

636VB /2S

636VB /2S

1

149

150

150

636VB /2S

636VB /2S

1

B_SB_282148_6_BJAA_09_00

Q

A A

Figure A-GBJAA - Sheet 09

Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D05)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 355

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

**CONF 004, 008

E

A B

C

G

G

J

L

A

Z612

5006VC 40VC

38VC

44VP

52VP

B_SB_282148_6_BKAA_01_00

BEFORE

N

Figure A-GBKAA - Sheet 01

Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D06)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 356

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

**CONF 004, 008

D

F

H

H

K

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

NOTE:

ELEC. WIRES 636VB/2S THRU 5006VC (2842−5071)

ELEC. WIRES 636VB/2S THRU 52VP (2842−5061, 2842−5062, 2842−5063, 2842−5064, 2842−5065 AND 2842−5071)

(3 POS)

5006VC 40VC

44VP

52VP

38VC

1

B_SB_282148_6_BKAA_02_00

AFTER

Q

M

P

B

Figure A-GBKAA - Sheet 02

Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D06)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 357

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

**CONF 004, 008

117

(112)

(116)

(112)

(116)

644VB /1S

644VB /1M

636VB /2M

644VB /1S

644VB /1M

636VB /2M

636VB /2S

ELEC. WIRES 636VB/2S THRU 10QT (2842−5061, 2842−5062,

NOTE:

 2842−5063, 2842−5064, 2842−5065 AND 2842−5071)

636VB /2S

(113)

(124)

(113)

(124)

B_SB_282148_6_BKAA_03_00

BEFORE

AFTER

C

D

Figure A-GBKAA - Sheet 03

Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D06)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 358

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

**CONF 004, 008

117

(112)

(112)

644VB /1S

644VB /1M

636VB /2M

644VB /1S

644VB /1M

636VB /2M

636VB /2S

ELEC. WIRES 636VB/2S THRU 10QT (2842−5061, 2842−5062,

NOTE:

 2842−5063, 2842−5064, 2842−5065 AND 2842−5071)

636VB /2S

(113)

(113)

B_SB_282148_6_BKAA_04_00

BEFORE

AFTER

E

F

Figure A-GBKAA - Sheet 04

Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D06)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 359

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

**CONF 004, 008

117

(112)

(112)

644VB /1S

644VB /1M

636VB /2M

644VB /1S

644VB /1M

636VB /2M

636VB /2S

ELEC. WIRES 636VB/2S THRU 10QT (2842−5061, 2842−5062,

NOTE:

 2842−5063, 2842−5064, 2842−5065 AND 2842−5071)

636VB /2S

(113)

(113)

B_SB_282148_6_BKAA_05_00

BEFORE

AFTER

G

H

Figure A-GBKAA - Sheet 05

Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D06)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 360

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

**CONF 004, 008

117

644VB /1S

644VB /1M

636VB /2M

644VB /1S

644VB /1M

636VB /2M

636VB /2S

ELEC. WIRES 636VB/2S THRU 10QT (2842−5061, 2842−5062,

NOTE:

 2842−5063, 2842−5064, 2842−5065 AND 2842−5071)

636VB /2S

(31)

31

(112)

(120)

(120)

121

636VB /2M

(31)

BEFORE

AFTER

J

K

B_SB_282148_6_BKAA_06_00

Figure A-GBKAA - Sheet 06

Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D06)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 361

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

**CONF 004, 008

117

644VB /1S

644VB /1M

636VB /2M

644VB /1S

644VB /1M

636VB /2M

636VB /2S

ELEC. WIRES 636VB/2S THRU 10QT (2842−5061, 2842−5062,

NOTE:

 2842−5063, 2842−5064, 2842−5065 AND 2842−5071)

636VB /2S

(123)

130

123

B_SB_282148_6_BKAA_07_00

BEFORE

AFTER

L

M

Figure A-GBKAA - Sheet 07

Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D06)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 362

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

**CONF 004, 008

117

644VB /1S

644VB /1M

636VB /2M

644VB /1S

644VB /1M

636VB /2M

636VB /2S

ELEC. WIRES 636VB/2S THRU 10QT (2842−5061, 2842−5062,

NOTE:

 2842−5063, 2842−5064, 2842−5065 AND 2842−5071)

636VB /2S

(123)

123

131

31

B_SB_282148_6_BKAA_08_00

BEFORE

AFTER

N

P

Figure A-GBKAA - Sheet 08

Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D06)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 363

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

**CONF 004, 008

TO 10QT−A AND 10QT−B

A

A

TO 10QT−A AND 10QT−B

ALL 100.0 mm

(ALL 3.94 in)

1000.0 mm

(39.37 in)

THE ENDS OF THE PROTECTION SLEEVES, ITEM 1, MUST OVERLAP

NOTE:

636VB /2S

636VB /2S

1

149

150

150

636VB /2S

636VB /2S

1

B_SB_282148_6_BKAA_09_00

Q

A A

Figure A-GBKAA - Sheet 09

Improvement of the 2S-Route in the RH-Wing Pylon Area (Kit D06)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 364

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

**CONF 001, 003, 005, 007

1 481 40VC W NSA938184PV1601 3155−5202 2S DE22/DK22 1400 55 481 5110VS−A 0 NSA936809RG0002

LINE

ZONE OR

PANEL

ELEC.

IDENT TERM. TERMINAL P/N WIRE

IDENT

INSTRUCTIONS

TERMINAL P/N ELEC.

IDENT TERM. ZONE OR

PANEL

LENGTH

MM INCH

COL ROUTE GAUGE

2 481 40VC −D NSA938184PV1601 2781−5154R 2S PE22/PG22 624 32CV−B A EN3155−019F2018 52VP T

3 481 40VC −E NSA938184PV1601 2781−5155B 2S PE22/PG22 20000 787 624 32CV−B B EN3155−019F2018 52VP U

4 481 40VC Z NSA938184PV1601 3621−5014B 2S PE22/PG22 1550 61 481 B NSA938185SV1601

5 481 40VC X NSA938184PV1601 3621−5015R 2S PE22/PG22 481 5110VS−A 0 NSA936809RG0002

6 481 40VC −F NSA938184PV1601 2781−5156B 2S QE24/QG24 20000 787 624 C EN3155−019F2018

7 481 40VC −G NSA938184PV1601 2781−5157R 2S QE24/QG24 624 32CV−B D EN3155−019F2018 52VP W

8 481 40VC −H NSA938184PV1601 2781−5158Y 2S QE24/QG24 624 E EN3155−019F2018

9 481 40VC V NSA938184PV1601 3611−5071R 2S PG22 1500 60 481 2212CV 1 E0446DW2001

10 481 40VC U NSA938184PV1601 3611−5072B 2S PG22 1500 60 481 2

11 481 40VC T NSA938184PV1601 3611−5073R 2S PG22 1500 60 481 2212CV 3

12 481 40VC S NSA938184PV1601 3611−5074B 2S PG22 1500 60 481 4

13 481 40VC R NSA938184PV1601 3611−5075R 2S PG22 1500 60 481 2212CV 5

14 481 40VC −A NSA938184PV1601 3611−5076B 2S PG22 481 6

15 481 4HX−A C NSA938184PV1601 3621−5018 2S DM20 481 408VN/DC 0 NSA936501TA2004

16

17 482 54HA−A A NSA938185SV1601 3611−65B 2S PG22 481 34VC T NSA938184PV1601

18 482 54HA−A B NSA938185SV1601 3611−66R 2S PG22 481 S NSA938184PV1601

19 482 54HA−A D NSA938185SV1601 3611−67B 2S PG22 481 34VC R NSA938184PV1601

20 482 54HA−A E NSA938185SV1601 3611−68R 2S PG22 481 P NSA938184PV1601

21

22

23

24

25

4HX−A

32CV−B 52VP V

32CV−B 52VP X

2212CV

2212CV

2212CV

34VC

34VC

1500 60

1400 56

1300 52

1300 52

1300 52

1300 52

END 1 LEAD END 2

ELT. EQUIPMENT 10 D929 97017 000 00 "A"

EQUIPMENT B929−90719−000−00

SB A310−28−2148, CONVERSION ONLY AFTER MOD 07633 OR SB A310−36−2015 AND SB−A310−2B−2140 (MOD 12173)

E = EXISTING WIRE (PART OF 5606VB / 10 D929 91506 000 00)

E0446DW2001

E0446DW2001

E0446DW2001

E0446DW2001

E0446DW2001

B_SB_282148_6_HAAA_01_00

Figure A-GHAAA - Sheet 01

Hook-up Chart

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 365

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

**CONF ALL

1 481 5006VC B NSA938184PV1601 2842−5058 2S(QT) DE22/DK22 200 8 481 5006VC 50711*

LINE

ZONE OR

PANEL

ELEC.

IDENT TERM. TERMINAL P/N WIRE

IDENT

INSTRUCTIONS

TERMINAL P/N ELEC.

IDENT TERM. ZONE OR

PANEL

LENGTH

MM INCH

COL ROUTE GAUGE

2 481 40VC −J NSA938184PV1601 2842−5061 2S(QT) DE24/DK24 623 10QT−B E EN3155−019F2018 52VP Y

3 481 40VC −K NSA938184PV1601 2842−5062 2S(QT) DE24/DK24 4500 177 623 10QT−B D EN3155−019F2018 52VP Z

4 481 40VC −M NSA938184PV1601 2842−5063 2S(QT) DE24/DK24 4500 177 623 C EN3155−019F2018

5 481 40VC −N NSA938184PV1601 2842−5064 2S(QT) DE24/DK24 623 10QT−B B EN3155−019F2018

6 481 40VC −P NSA938184PV1601 2842−5065 2S(QT) DE24/DK24 4500 177 623 A EN3155−019F2018

7 481 5006VC A NSA938184PV1601 2842−5071 2S(QT) SG24/SW24 623 10QT−A A EN3155−019F2018 52VP R

8 481 5006VC − 2842−50711 2S(QT) SG24/SW24 623 −

9

10

11

12

13

14

15

16

17

18

19

20

21

22

23

24

25

10QT−B

10QT−B 52VP −C

10QT−A

END 1 LEAD END 2

2S(QT) ROUTE

B_SB_282148_6_HBAA_01_00

52VP −B

52VP −A

4500

4500

177

177

Figure A-GHBAA - Sheet 01

Hook-up Chart

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 366

6

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@A310

SERVICE BULLETIN

**CONF ALL

FR20

ELECTRONICS RACK

A

2354VC

92VU

15QTB

1

1

90VU

A

B_SB_282148_5_CAAA_01_01

Figure A-FCAAA - Sheet 01

Installation of Cable Sleeves in the RH Electronics Rack 90VU.

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 367

6

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@A310

SERVICE BULLETIN

**CONF ALL

2S−4A

2S

2S

AFTER

FR38.1

FR38.2

FR39

FR40

A

FR39

FR38.2

20VP

20VCA

1904VCA B

2

A

B

B_SB_282148_5_CBAA_01_01

Figure A-FCBAA - Sheet 01

Installation of Cable Sleeves in the Forward Cargo Compartment.

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 368

6

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@A310

SERVICE BULLETIN

**CONF 001 thru 004

FR39

FR40

A

2S

AFTER

TO FWD

WING

2

FR40

FR39

20VP

B

A B

B_SB_282148_5_CCAA_01_03

Figure A-FCCAA - Sheet 01

Installation of Cable Sleeves in the RH forward wing root and krueger flap.

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 369

6

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@A310

SERVICE BULLETIN

**CONF 005 thru 008

FR39

FR40

AFTER A

B

A

TO FWD

WING

2S

FR40

FR39

20VP

2

B

B_SB_282148_5_CCAB_01_01

Figure A-FCCAB - Sheet 01

Installation of Cable Sleeves in the RH forward wing root and krueger flap.

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 370

6

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@A310

SERVICE BULLETIN

**CONF ALL

Figure A-FWAAA - Sheet 01

Installation of Cable Sleeves in the RH Electronics Rack 90VU.

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 371

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

**CONF ALL

CENTERLINE

PYLON

D NOSE

1

SUB SPAR

VIEW LOOKING FWD

WOFZ 0.0

WDFX −53.0 (1)

SUB SPAR

VIEW LOOKING FWD

WOFZ 0.0

WDFX −53.0

RIB8 RIB9

(0.35 in)

2

(2)

AFTER

8.89 mm

A B

A

B

(0.35 in)

8.89 mm

B_SB_282148_7_BAAA_01_00

Figure A-UBAAA - Sheet 01

Location of Bracket on the Sub Spar Behind the Front Spar Between RIB 8 and RIB 9 (RH Wing)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 372

6

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@A310

SERVICE BULLETIN

**CONF 001 thru 002, 005 thru 006

PYLON

FRONT SPAR TRACK 4

SCREW JACK 3 1M

1S

MASTER TRACK 5

RIB12

RIB11

RIB10

RIB9

636VB /2S

636VB /2M

Z623

B_SB_282148_6_BLAA_01_00

B

C

D

E

A

A

Figure A-GBLAA - Sheet 01

Additional Work 1 (Introduced at Revision 02): Installation of Protection Sleeve in the Area of 10QT

(Kits D02 and D03)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 373

6

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@A310

SERVICE BULLETIN

**CONF 001 thru 002, 005 thru 006

TO 10QT − B

TO 10QT − B

1

636VB /2S 636VB /2M

636VB /2S

636VB /2M

1S

1M

1S

1M

B_SB_282148_6_BLAA_02_00

BEFORE

AFTER

B

C

Figure A-GBLAA - Sheet 02

Additional Work 1 (Introduced at Revision 02): Installation of Protection Sleeve in the Area of 10QT

(Kits D02 and D03)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 374

6

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@A310

SERVICE BULLETIN

**CONF 001 thru 002, 005 thru 006

TYPICAL

TYPICAL

1S

1M

TO 10QT − A

1S

TO 10QT − A

APPLY (MAT. NO. 15−008A)

NOTE:

636VB /2S

636VB /2M

121

(22)

(121)

(122)

(112)

(22)

(23)

(31)

(30)

(112)

(122)

(23) (31)

(30)

1

636VB /2S

636VB /2M

10

636VB /2S

B_SB_282148_6_BLAA_03_00

BEFORE

AFTER

D

E

(22)

Figure A-GBLAA - Sheet 03

Additional Work 1 (Introduced at Revision 02): Installation of Protection Sleeve in the Area of 10QT

(Kits D02 and D03)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 375

6

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@A310

SERVICE BULLETIN

**CONF 001, 005

AFTER SB A310−36−2015 OR

MODIFICATION 7633S8497

NOTE:

P

636VB /2S

(125)

52VP

44VP

52VP

636VB /2S

636VB /2S

2212VC

38VC

5006VC

5006VC 40VC

40VC

636VB /2S

636VB2S

(125)

(125)

(125)

(125)

(125)

Z612

B_SB_282148_6_BMAA_01_00

BEFORE

A B

D

F

K

H

H

M

C

A

Figure A-GBMAA - Sheet 01

Additional Work 1 (Introduced at Revision 02): Improvement of the 2S-Route in the RH-Wing pylon area

(Kit D02)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 376

6

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@A310

SERVICE BULLETIN

**CONF 001, 005

AFTER SB A310−36−2015 OR

MODIFICATION 7633S8497

NOTE:

N

Q

52VP

44VP

52VP

2212VC

5006VC

40VC

40VC

(125)

1

125

125

125 636VB

1

125

125

125

125

126

636VB

125

109

125

2S

2S / QT

2S 2S / QT

B_SB_282148_6_BMAA_02_00

AFTER

TYPICAL PLACARD

INSTALLATION

C

C

E G

J

L

J

B

5006VC

Figure A-GBMAA - Sheet 02

Additional Work 1 (Introduced at Revision 02): Improvement of the 2S-Route in the RH-Wing pylon area

(Kit D02)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 377

6

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@A310

SERVICE BULLETIN

**CONF 001, 005

APPLY (MAT. NO. 15−008)

NOTE:

636VB /2S

636VB /2M

636VB /2S

636VB /2M

CLAMP

CLAMP

(109)

(110)

(111)

(113)

(112)

(31)

(114)

(117) (115)

(116)

109

(112)

(113)

(117)

(115)

(116)

(111)

B_SB_282148_6_BMAA_03_00

AFTER

BEFORE

D

E

30

Figure A-GBMAA - Sheet 03

Additional Work 1 (Introduced at Revision 02): Improvement of the 2S-Route in the RH-Wing pylon area

(Kit D02)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 378

6

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@A310

SERVICE BULLETIN

**CONF 001, 005

APPLY (MAT. NO. 15−008)

NOTE:

636VB /2S

636VB /2M

636VB /2S

636VB /2M

636VB /2S

(109)

(110)

(111)

(112)

(31)

(117)

109 117

(117)

(111)

TO PYLON

TO 

TO PYLON

TO 2212VC

(30)

(118)

(30)

(112)

(118)

2212VC

(110)

(31)

(30)

(30)

117

109

B_SB_282148_6_BMAA_04_00

AFTER

BEFORE

F

G

Figure A-GBMAA - Sheet 04

Additional Work 1 (Introduced at Revision 02): Improvement of the 2S-Route in the RH-Wing pylon area

(Kit D02)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 379

6

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@A310

SERVICE BULLETIN

**CONF 001, 005

APPLY (MAT. NO. 15−008)

NOTE:

636VB /2S

636VB /2M

636VB /2S

636VB /2M

636VB /2S

(109) (110)

(111)

(117)

109 117

(117)

(111)

TO 

TO 2212VC

(30)

(118)

(118)

2212VC

(31)

(30)

117

109

TYPICAL

TYPICAL AFTER SB A310−36−2015 OR

MODIFICATION 7633S8497

TO PYLON

CLAMP

CLAMP

TO PYLON

(115)

(114)

(31)

(114)

(115)

B_SB_282148_6_BMAA_05_00

BEFORE

AFTER

H

J

Figure A-GBMAA - Sheet 05

Additional Work 1 (Introduced at Revision 02): Improvement of the 2S-Route in the RH-Wing pylon area

(Kit D02)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 380

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

**CONF 001, 005

APPLY (MAT. NO. 15−008)

NOTE:

636VB /2S

636VB /2M

636VB /2S

636VB /2M

(109)

(110) (111)

(117)

109

117

(117)

(111)

TO 

TO 2212VC

(30)

(118)

(118)

2212VC

(31)

(30)

117

109

AFTER SB A310−36−2015 OR

MODIFICATION 7633S8497

TO PYLON

CLAMP

CLAMP

TO PYLON

(115)

(114)

(31)

(114)

CONDUIT

CONDUIT

(115)

B_SB_282148_6_BMAA_06_00

BEFORE

AFTER

K

L

Figure A-GBMAA - Sheet 06

Additional Work 1 (Introduced at Revision 02): Improvement of the 2S-Route in the RH-Wing pylon area

(Kit D02)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 381

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

**CONF 001, 005

APPLY (MAT. NO. 15−008)

NOTE:

636VB /2S

636VB /2M

636VB /2S

636VB /2M

636VB /2S

(109)

(110)

(111)

(117)

109

(117)

(111)

(30)

(112)

(118)

(31)

(30)

117

109

(114)

(31)

(114)

644VB1M /1S

(118)

(112)

644VB1M /1S

(117)

B_SB_282148_6_BMAA_07_00

BEFORE

AFTER

M

N

Figure A-GBMAA - Sheet 07

Additional Work 1 (Introduced at Revision 02): Improvement of the 2S-Route in the RH-Wing pylon area

(Kit D02)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 382

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

**CONF 001, 005

APPLY (MAT. NO. 15−008)

NOTE:

636VB /2S

636VB /2M

636VB /2S

636VB /2M

636VB /2S TO

(109) (110)

(111)

(117)

109

(111)

(112)

(31)

117

109

(114)

(31)

(114)

644VB1M /1S

(112)

644VB1M /1S

(117)

(119)

(119)

B_SB_282148_6_BMAA_08_00

BEFORE

AFTER

P

Q

10QT

Figure A-GBMAA - Sheet 08

Additional Work 1 (Introduced at Revision 02): Improvement of the 2S-Route in the RH-Wing pylon area

(Kit D02)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 383

6

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@A310

SERVICE BULLETIN

**CONF 001 thru 002, 005 thru 006

AFTER

TO FWD

WING

VALID FOR AIRCRAFT UP TO MSN 0442

2

FR40

FR39

B

FR39

FR40

A

A B C

B_SB_282148_6_BCAA_01_00

2S

20VP

8VP

Figure A-UBCAA - Sheet 01

Additional Work 2 (Introduced at Revision 03)- Location of Bracket on the Sub Spar Behind the Front

Spar Between RIB 8 and RIB 9 (RH Wing)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 384

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

**CONF 002, 006

AFTER SB A310−36−2015 OR

MODIFICATION 7633S8497

NOTE:

P

52VP

44VP

52VP

636VB /2S

(132)

(132)

5006VC 40VC

38VC

5006VC

(132)

Z612

BEFORE

A B

A

C

D

F

H

H

K

M

B_SB_282148_6_BNAA_01_00

Figure A-GBNAA - Sheet 01

Additional Work 1 (Introduced at Revision 02): Improvement of the 2S-Route in the RH-Wing Pylon

Area (Kit D03)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 385

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

**CONF 002, 006

AFTER SB A310−36−2015 OR

MODIFICATION 7633S8497

NOTE:

52VP

44VP

52VP

5006VC

40VC

40VC

636VB

126

636VB

109

132

N

Q

132

132

132

132

132

1

132

132

132

132

B_SB_282148_6_BNAA_02_00

AFTER

TYPICAL PLACARD

INSTALLATION

B

C

E

G

J

J

L

C

2S

2S /QT

2S

2S /QT

5006VC

Figure A-GBNAA - Sheet 02

Additional Work 1 (Introduced at Revision 02): Improvement of the 2S-Route in the RH-Wing Pylon

Area (Kit D03)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 386

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

**CONF 002, 006

636VB /2S

636VB /2M

636VB /2S

636VB /2M

(111)

(113)

(31)

(114)

(116)

109

117

(113)

(117)

(116)

(111)

CLAMP

CLAMP

(112)

(31)

(124)

(124)

(112)

B_SB_282148_6_BNAA_03_00

BEFORE

AFTER

D

E

Figure A-GBNAA - Sheet 03

Additional Work 1 (Introduced at Revision 02): Improvement of the 2S-Route in the RH-Wing Pylon

Area (Kit D03)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 387

6

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@A310

SERVICE BULLETIN

**CONF 002, 006

636VB /2S

636VB /2M

636VB /2S

636VB /2M

(111)

(112)

(31)

(111)

(112) (31)

117

109

(113)

(114)

(113) (114)

B_SB_282148_6_BNAA_04_00

BEFORE

AFTER

F

G

Figure A-GBNAA - Sheet 04

Additional Work 1 (Introduced at Revision 02): Improvement of the 2S-Route in the RH-Wing Pylon

Area (Kit D03)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 388

6

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@A310

SERVICE BULLETIN

**CONF 002, 006

636VB /2S

636VB /2M

636VB /2S

636VB /2M

(111)

(112) (31)

(111)

(112) (31)

117 109

(113) (114)

(113) (114)

B_SB_282148_6_BNAA_05_00

BEFORE

AFTER

H

J

Figure A-GBNAA - Sheet 05

Additional Work 1 (Introduced at Revision 02): Improvement of the 2S-Route in the RH-Wing Pylon

Area (Kit D03)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 389

6

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@A310

SERVICE BULLETIN

**CONF 002, 006

636VB /2S

636VB /2M

636VB /2S

636VB /2M

(111)

(112)

(31)

(111)

(31)

117

109

(123)

(120)

123

(120)

(112)

(31)

B_SB_282148_6_BNAA_06_00

BEFORE

AFTER

K

L

Figure A-GBNAA - Sheet 06

Additional Work 1 (Introduced at Revision 02): Improvement of the 2S-Route in the RH-Wing Pylon

Area (Kit D03)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 390

6

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@A310

SERVICE BULLETIN

**CONF 002, 006

636VB /2S

636VB /2M

636VB /2S

636VB /2M

(111)

(112)

(31)

(111)

(31)

117

109

123

(112)

(114)

(113)

(114)

130

B_SB_282148_6_BNAA_07_00

BEFORE

AFTER

M

N

Figure A-GBNAA - Sheet 07

Additional Work 1 (Introduced at Revision 02): Improvement of the 2S-Route in the RH-Wing Pylon

Area (Kit D03)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 391

6

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@A310

SERVICE BULLETIN

**CONF 002, 006

636VB /2S

636VB /2M

636VB /2S

636VB /2M

(111)

(112)

(31)

(111)

(31)

117

109

123

(112)

(114)

(113)

131

31

114

B_SB_282148_6_BNAA_08_00

BEFORE

AFTER

P

Q

Figure A-GBNAA - Sheet 08

Additional Work 1 (Introduced at Revision 02): Improvement of the 2S-Route in the RH-Wing Pylon

Area (Kit D03)

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 392

6

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@A310

SERVICE BULLETIN

**CONF 004, 008

636VB /2S

(125)

52VP

44VP

52VP

636VB /2S

636VB /2S

2212VC

38VC

5006VC

5006VC 40VC

40VC

636VB /2S

636VB2S

(125)

(125)

(125)

(125)

(125)

Z612

A

B_SB_282148_6_BPAA_01_00

A

A

B

B

AFTER

BEFORE

(111)

(123)

(111)

(120)

(112)

(130)

(117) (30)

(114)

111 117 111

120

112

123

130

31

A A

B B

A

(30)

Figure A-GBPAA - Sheet 01

Additional Work 3 - Improvement of the 2S-Route in the RH-Wing Pylon Area

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 393

6

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@A310

SERVICE BULLETIN

**CONF 003, 007

636VB /2S

(125)

52VP

44VP

52VP

636VB /2S

636VB /2S

2212VC

38VC

5006VC

5006VC 40VC

40VC

636VB /2S

636VB2S

(125)

(125)

(125)

(125)

(125)

Z612

A

A

A

B

B

AFTER

BEFORE

A

(110) (117)

(151)

(31) (120)

(117) (114)

(152)

110 117

112

120

130 31

A A

B B

B_SB_282148_6_BPAB_01_01

135

Figure A-GBPAB - Sheet 01

Additional Work 3 - Improvement of the 2S-Route in the RH-Wing Pylon Area

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 394

6

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@A310

SERVICE BULLETIN

REPORTING SHEET

TITLE: ELECTRIC/ELECTRONIC COMMON INSTALLATION - WING - IMPROVE

THE 2S-ROUTE IN THE RH-WING

MODIFICATION No.: 12427D21883 12435S22116 13478D23233

Please complete the appropriate item (A or B):

A - SB WILL BE embodied YES/NO (if NO please comment)

If YES, aircraft concerned (as per SB effectivity by default) and planned dates (month/year) of

embodiment:

B - SB HAS BEEN embodied on aircraft:

Operator comments:

From Airline:

Name/Title:

Signature: Date:

If operational documentation is affected (see Paragraph 1.K of this SB): If information is needed prior to

next normal revision or prior to SB embodiment, please indicate required service(s):

Either: Modification Operational Impact (MOI), if available YES/NO

Or : Intermediate revision YES/NO

Important Information: This SB will only be incorporated in your maintenance and operational

documentation if this sheet is returned to Airbus and signed by a duly authorised representative. With

the next feasible revision, this will result in

- Updating of maintenance documentation to show pre and post SB data.

- Updating of maintenance and operational documentation to show post SB data after embodiment.

If this SB requires previous or simultaneous accomplishment of other SBs, Airbus shall automatically

include them in the manual revisions. Refer to SIL 00-037 for detailed information.

Please return this completed sheet to:

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX FRANCE

Attn: SDC32 Technical Data and Documentation Services

FAX: (+33) 5 61 93 28 06

e-mail: sb.reporting@airbus.com

or via your Resident Customer Support Office.

Alternatively, SB lists via letters or fax are also accepted.

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 1

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

QUALITY PERCEPTION FORM

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

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

improve the quality of our Service Bulletins.

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

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

- Quality rating of this SB 4321

- Quality rating of the Accomplishment Instructions 4321

- Quality rating of the Illustrations 4321

- Is this SB easy to understand ? Y/N

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

short description of the issue.

Planning Material Instructions

X Effectivity X Kit content X Preparation

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

X Manpower X Industry support X Test

X References X Re-identification X Close-Up

X Publication X Tooling X Illustrations

Comments:

Operator: Date:

Name/Title:

Please return this form to:

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX FRANCE

Attn : SEM4 Service Bulletins Management

FAX : (33) 5 61 93 42 51

Or via your Resident Customer Support Office.

DATE: Jan 23/02 SERVICE BULLETIN No.: A310-28-2148

REVISION No.: 06 - Aug 31/11 Page: 1

6

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