A310

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

MANDATORY MANDATORY MANDATORY 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. 05 of Service Bulletin No. A310-28-2148

ADDITIONAL WORK

ADDITIONAL WORK 1 was introduced in Revision 02 of this Service Bulletin, and is required for aircraft

modified by issue 00 or Revision 01.

The following work is to be done on aircraft listed in this Service Bulletin issue 00 or Revision 01:

- 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 was introduced in Revision 03 of this Service Bulletin and is required by this

revision for aircraft modified by issue 00 thru Revision 02.

The following work is to be done on aircraft listed in this Service Bulletin issue 00 thru Revision 02:

- installation of an modified bracket on the RH wing.

NOTE : Aircraft in Configuration 03 and 04, as described in this Service Bulletin, could not have

performed it at a previous issue, therefore those aircraft will have to accomplish this Service

Bulletin at Revision No. 04. As a consequence no dedicated ADDITIONAL WORK was

described in this Service Bulletin for aircraft in Configuration 03 and 04.

REASON

Revision No. 05 is issued to :

- remove MSN 0349 from the effectivity and

- add MSN’s 0254, 0273, 0397 and 0400 to the effectivity.

CHANGES

SUMMARY :

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

REVISION No. : 05 - Aug 03/10 Page : 1 of 2

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A310

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

- REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES

- EFFECTIVITY

. Operator’s updated.

PLANNING INFORMATION :

- EFFECTIVITY

. 1.A. updated.

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

FILING INSTRUCTIONS

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

Replace the complete document.

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

HISTORY OF PREVIOUS REVISIONS

Revision No. 01 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.

ORIGINAL : Jan 23/02

REVISION No. : 01 - Oct 29/02

REVISION No. : 02 - Mar 09/07

REVISION No. : 03 - Jun 02/09

REVISION No. : 04 - Apr 14/10

REVISION No. : 05 - Aug 03/10

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

REVISION No. : 05 - Aug 03/10 Page : 2

Printed in France © AIRBUS 2008 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 MANDATORY

ATA SYSTEM : 28

TITLE : ELECTRIC/ELECTRONIC COMMON INSTALLATION - WING - IMPROVE THE 2S-ROUTE IN

THE RH-WING

MODIFICATION No. : 12427D21883, 12435S22116, 13478D23233

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.

EVALUATION TABLE

COMPLIANCE Mandatory CANCELS INSPECTION SB No

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. : 05 - Aug 03/10 Page : 1 of 7

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A310

SERVICE BULLETIN

SUMMARY

MODIFICATION CLASSIFICATION

MAJOR 13478D23233

MINOR 12427D21883 12435S22116

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.

EFFECTIVITY

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

19U 52X 58X 80V 82Z 83V 99Y AFG AIB AIC BAF BBC BLE CFC CSA DAH DEC DGA F2I FDX G8E GAF

HFY I2L IRA IRM IYE JAB JAV K1P KAC KTC KYV KZU MGL MWA PIA QAF R1T RJA ROT RZO SBI

SGX SUD THY TSC UZB WHT

CONCURRENT REQUIREMENTS

None

REFERENCES/REPERCUSSIONS

TFU : None

OEB : None

AOT : None

SIL : None

LIFE LIMIT : None

LINE MAINTENANCE AFFECTED : No

OTHERS : None

NATURE OF THE WORK

AIRCRAFT : YES

EQUIPMENT : NO

HARD : NO

SOFT : NO

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

REVISION No. : 05 - Aug 03/10 Page : 2

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A310

SERVICE BULLETIN

SUMMARY

OBRM : NO

MANPOWER

Config. 01 thru Config. 04

TOTAL MANHOURS 36.00

ELAPSED TIME (HOURS) 14.00

Config. 01 thru Config. 02 ADDITIONAL WORK 1

TOTAL MANHOURS 23.00

ELAPSED TIME (HOURS) 13.00

Config. 01 thru Config. 02 ADDITIONAL WORK 2

TOTAL MANHOURS 3.00

ELAPSED TIME (HOURS) 3.00

MATERIAL INFORMATION

AIRCRAFT DATA

Config. 01 thru Config. 04

Sleeves, clamps, brackets, spacer and related fasteners.

APPENDICES

None

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

REVISION No. : 05 - Aug 03/10 Page : 3

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A310

SERVICE BULLETIN

SUMMARY

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

REVISION No. : 05 - Aug 03/10 Page : 4

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A310

SERVICE BULLETIN

SUMMARY

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

REVISION No. : 05 - Aug 03/10 Page : 5

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A310

SERVICE BULLETIN

SUMMARY

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

REVISION No. : 05 - Aug 03/10 Page : 6

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A310

SERVICE BULLETIN

SUMMARY

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

REVISION No. : 05 - Aug 03/10 Page : 7

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A310

SERVICE BULLETIN

This Page Intentionally Left Blank

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

REVISION No. : 05 - Aug 03/10 Page : 8

Printed in France © AIRBUS 2008 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 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 the 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

A. EFFECTIVITY

(1) Models

310-203 310-204 310-221 310-222 310-304 310-308 310-322 310-324 310-325

(2) Aircraft

(a) Effectivity by MSN

This Service Bulletin is applicable to aircraft 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 0386 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 0480-0492 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 0640 0642 0644 0646-0654 0656 0658 0660 0661 0663 0665 0667

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A310

SERVICE BULLETIN

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

0697 0700 0702 0704 0706

(b) 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

19U 0399

52X 0410

58X 0431

80V 0538 0544

82Z 0550 0551

83V 0427

99Y 0489

AFG 0496 0497

AIB 0686

AIC 0392 0406 0407 0413 0428 0429 0654 0665 0669 0680

BAF 0367 0372

BBC 0594 0642 0700

BLE 0650

CFC 0425 0441 0444 0446 0482

CSA 0672 0674

DAH 0291 0293

DEC 0684 0693 0697

DGA 0418 0421 0422

F2I 0309 0487 0595

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REVISION No. : 05 - Aug 03/10 Page : 2

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A310

SERVICE BULLETIN

OPERATOR MSN

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

I2L 0640

IRA 0338 0370 0375 0379 0389 0390 0436 0671

IRM 0488 0537 0564 0586

IYE 0568 0702 0704

JAB 0320 0419

JAV 0357 0481

K1P 0648

KAC 0647 0649 0663

KTC 0524 0567 0620

KYV 0386

KZU 0592 0622 0646

MGL 0526

MWA 0652

PIA 0473 0585 0587 0590 0653 0656 0660 0676 0678 0682 0687

0689 0691

QAF 0667

R1T 0591

RJA 0416 0445 0490 0491 0531

ROT 0636 0644

RZO 0571 0624 0651 0661

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

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A310

SERVICE BULLETIN

OPERATOR MSN

SBI 0486 0520

SGX 0519 0562

SUD 0437

THY 0476 0478 0480 0502

TSC 0447 0472 0483 0485 0527 0541 0545 0547 0588 0597 0599

0600 0658

UZB 0574 0576 0706

WHT 0448 0494 0573

(c) Effectivity by MSN and Kit/Configuration

The Kits and configurations applicable to these MSNs are given at the end of this list

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 0386

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 0480-0492 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 0640 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

KIT No. QTY PER A/C CONFIGURATION

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

REVISION No. : 05 - Aug 03/10 Page : 4

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SERVICE BULLETIN

282148A01R00 1 01

02

03

04

282148B01R00 1 01

02

03

04

282148D01R00 1 01

02

03

04

282148D02R01 1 01

282148D03R01 1 02

282148D05R01 1 03

282148D06R01 1 04

NOTE : ADDITIONAL WORK 1 : applicable to Configuration 01 and 02 is

required for aircraft that have been modified by accomplishment of this

Service Bulletin from the original issue up to revision 01.

The follow work is to be done :

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.

NOTE : ADDITIONAL WORK 2 : applicable to Configuration 01 and 02 is

required for aircraft that have been modified by accomplishment of this

Service Bulletin from the original issue up to revision 02.

The follow work is to be done :

installation of an modified bracket on the RH wing.

NOTE : Config. 01 is valid for aircraft having Service Bulletin Nos. A310-28-2140

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

NOTE : Config. 02 is valid for aircraft not having Service Bulletin No.

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

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

NOTE : Config. 03 is valid for aircraft having Service Bulletin A310-28-2140

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

accomplished or MOD. No. 7633S7885 not embodied.

NOTE : Config. 04 is valid for aircraft not having Service Bulletin Nos.

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

7633S7885 not embodied.

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

REVISION No. : 05 - Aug 03/10 Page : 5

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SERVICE BULLETIN

(3) Spares

None

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 :

(1) Config. 01

(a) Install a new bracket on the RH wing between rib 8 and rib 9 on the rear sub spar.

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

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

compartment.

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

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

and rib 3 in zone 612.

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

and rib 8 in zone 612.

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

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SERVICE BULLETIN

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

rib 9 (pylon area) in zone 612.

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

and rib 12 in zone 623.

(2) Config. 02

(a) Install a new bracket on the RH wing between rib 8 and rib 9 on the rear sub spar.

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

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

compartment.

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

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

and rib 3 in zone 612.

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

and rib 8 in zone 612.

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

rib 9 (pylon area) in zone 612.

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

and rib 12 in zone 623.

(3) Config. 03

(a) Install a new bracket on the RH wing between rib 8 and rib 9 on the rear sub spar.

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

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

compartment.

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

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

and rib 3 in zone 612.

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

and rib 8 in zone 612.

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

rib 9 (pylon area) in zone 612.

(h) 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. : 05 - Aug 03/10 Page : 7

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SERVICE BULLETIN

(4) Config. 04

(a) Install a new bracket on the RH wing between rib 8 and rib 9 on the rear sub spar.

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

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

compartment.

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

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

and rib 3 in zone 612.

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

and rib 8 in zone 612.

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

rib 9 (pylon area) in zone 612.

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

and rib 12 in zone 623.

(5) Config. 01 ADDITIONAL WORK 1

(a) Preparation

(b) Modification

(c) Test

(d) Close up

(6) Config. 02 ADDITIONAL WORK 1

(a) Preparation

(b) Modification

(c) Test

(d) Close up

(7) Config. 01 thru Config. 02 ADDITIONAL WORK 2

(a) Preparation

(b) Modification

(c) Test

(d) Close up

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

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SERVICE BULLETIN

E. COMPLIANCE

(1) Classification

Mandatory

(2) Accomplishment Timescale

Accomplishment of this Service Bulletin will be rendered 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 mandatory accomplishment

timescale.

F. APPROVAL

Approved under EASA Design Organisation Approval No. EASA 21J.031.

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

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

obtaining approval by its airworthiness authority for any adaptation necessary before incorporation

of the Service Bulletin.

G. MANPOWER

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

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

need to be revised upwards to suit operators’ circumstances. The estimates do not include the

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

time for paints, sealants, etc. and general administration work are also not included.

Config. 01 thru Config. 04

Get Access 11.00

Modify the bracket 1.00

Install cable sleeves in 90VU 2.00

Install cable sleeves in FWD cargo compt 1.00

Install cable sleeves in RH forward inner wing 1.00

Install cable sleeves in RH-wing pylon area 12.00

Install cable sleeves in RH forward outer wing 1.00

Test 3.00

Close-up 4.00

TOTAL MANHOURS 36.00

ELAPSED TIME (HOURS) 14.00

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SERVICE BULLETIN

Config. 01 thru Config. 02 ADDITIONAL WORK 1

Get Access 3.00

Modify the bracket 1.00

Install cable sleeves in RH-wing pylon area 12.00

Install cable sleeves in RH forward outer wing 1.00

Test 3.00

Close-up 3.00

TOTAL MANHOURS 23.00

ELAPSED TIME (HOURS) 13.00

Config. 01 thru Config. 02 ADDITIONAL WORK 2

Get Access 1.00

Modify the bracket 1.00

Close-up 1.00

TOTAL MANHOURS 3.00

ELAPSED TIME (HOURS) 3.00

H. WEIGHT AND BALANCE

Config. 01

Manufacturers Empty Weight : +1.856 kg (+4.0917 lb)

Effect on Balance : +41.089 kgm (+297.196 lb.ft)

Config. 02

Manufacturers Empty Weight : +1.883 kg (+4.1512 lb)

Effect on Balance : +41.705 kgm (+301.652 lb.ft)

Config. 03

Manufacturers Empty Weight : +2.492 kg (+5.4938 lb)

Effect on Balance : +55.177 kgm (+399.095 lb.ft)

Config. 04

Manufacturers Empty Weight : +2.569 kg (+5.6636 lb)

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

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SERVICE BULLETIN

Effect on Balance : +56.889 kgm (+411.478 lb.ft)

ADDITIONAL WORK 1 : Config. 01

Manufacturers Empty Weight : +0.336 kg (+0.7407 lb)

Effect on Balance : +9.186 kgm (+66.442 lb.ft)

ADDITIONAL WORK 1 : Config. 02

Manufacturers Empty Weight : +0.437 kg (+0.9634 lb)

Effect on Balance : +11.948 kgm (+86.419 lb.ft)

ADDITIONAL WORK 2 :Config. 01 thru Config. 02

Not changed

I. ELECTRICAL LOAD DATA

Not changed

J. REFERENCES

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

25-54-10 27-80-00 27-84-00 28-42-44

30-11-00 36-11-00 52-30-00 53-10-55

Elec. Std. Practices Manual (ESPM) : 20-33-00 20-52-00 20-52-21 20-55-00

Structural Repair Manual (SRM) : 51-23-11 51-42-11

Consumable Material List (CML)

Standards Manual (SM)

K. PUBLICATIONS AFFECTED

Aircraft Maintenance Manual (AMM) : 28-42-07

Illustrated Parts Catalog (IPC) : 24-92-03

L. INTERCHANGEABILITY/MIXABILITY

None

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

REVISION No. : 05 - Aug 03/10 Page : 11

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A310

SERVICE BULLETIN

This Page Intentionally Left Blank

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

REVISION No. : 05 - Aug 03/10 Page : 12

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A310

SERVICE BULLETIN

2. MATERIAL INFORMATION

A. MATERIAL - PRICE AND AVAILABILITY

(1) Material

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 :

AIRBUS Material, Logistics and Suppliers

Weg beim Jaeger 150

D-22335 HAMBURG

GERMANY

For ordering by internet:http://spares.airbus.com

For SB Kits by fax: +49 40 50 76 25 90

For Spares by fax: +49 40 50 76 40 12

(2) Price and Availability

Kit 282148A01R00

Cost : 820 US dollars

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 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 282148B01R00

Cost : 90 US dollars

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 : 2210 US dollars

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. : 05 - Aug 03/10 Page : 13

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A310

SERVICE BULLETIN

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

at the issue date of the Service Bulletin.

Kit 282148D02R01

Cost : 1580 US dollars

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 : 1530 US dollars

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 US dollars

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 US dollars

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. : 05 - Aug 03/10 Page : 14

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A310

SERVICE BULLETIN

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

at the issue date of the Service Bulletin.

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 No. QTY UM KEYWORD ITEM OLD PART No. INT INST DISP

1 ABS0596S004 2000 mm sleeve

2 ABS0596S006 2000 mm Sleeve

NSA935401-04 50 Tie

NSA935401-05 100 Tie

NOTE : Refer to the AIRBUS Standards Manual (SM) 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. The SM will give you the correct part number

to part number relationship.

Kit 282148B01R00

ITEM NEW PART No. QTY UM KEYWORD ITEM OLD PART No. INT INST DISP

1 A5725068600000 1 Bracket

2 ASNA0078A502 2 Rivet

NOTE : Refer to the AIRBUS Standards Manual (SM) 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. The SM will give you the correct part number

to part number relationship.

Kit 282148D01R00

ITEM NEW PART No. QTY UM KEYWORD ITEM OLD PART No. INT INST DISP

1 ABS0596S004 12 INSULATR

10 MS21919WCH9 17 CLAMP

11 MS21919WCH13 4 CLAMP

12 MS21919WCH14 4 CLAMP

14 NAS1096-3-19 4 SCREW

15 NSA5527-03-03 6 SPACER

16 NSA8420-2 2 CORD

149 NSA935401-03 8 TIE

150 NSA935401-04 8 TIE

NOTE : Refer to the AIRBUS Standards Manual (SM) 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. The SM will give you the correct part number

to part number relationship.

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

REVISION No. : 05 - Aug 03/10 Page : 15

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A310

SERVICE BULLETIN

Kit 282148D02R01

ITEM NEW PART No. QTY UM KEYWORD ITEM OLD PART No. INT INST DISP

1 ABS0596S004 3 INSULATR

10 MS21919WCH9 1 CLAMP

30 NSA5527-03-01D 2 SPACER

31 NSA5527-03-02D 1 SPACER

109 NSA935805-09 3 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 : Refer to the AIRBUS Standards Manual (SM) 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. The SM will give you the correct part number

to part number relationship.

Kit 282148D03R01

ITEM NEW PART No. QTY UM KEYWORD ITEM OLD PART No. INT INST DISP

1 ABS0596S004 6 INSULATR

10 MS21919WCH9 2 CLAMP

31 NSA5527-03-02D 4 SPACER

109 NSA935805-09 2 CONDUIT

117 NSA935807C09 14 CLAMP

121 NAS1096-3-40 2 SCREW

123 NAS1801-3-31 6 SCREW

126 NSA938184PV1601 14 PIN

130 NSA5527-03-08D 2 SPACER

131 NSA5527-03-07D 2 SPACER

132 B9299071900600 2 EQUIPMNT

149 NSA935401-03 60 TIE

150 NSA935401-04 80 TIE

NOTE : Refer to the AIRBUS Standards Manual (SM) 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. The SM will give you the correct part number

to part number relationship.

Kit 282148D05R01

ITEM NEW PART No. QTY UM KEYWORD ITEM OLD PART No. INT INST DISP

1 ABS0596S004 3 INSULATR

30 NSA5527-03-01D 2 SPACER

31 NSA5527-03-02D 1 SPACER

109 NSA935805-09 * CONDUIT

117 NSA935807C09 12 CLAMP

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

REVISION No. : 05 - Aug 03/10 Page : 16

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A310

SERVICE BULLETIN

ITEM NEW PART No. QTY UM KEYWORD ITEM OLD PART No. INT INST DISP

125 B9299071900200 0 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 : Refer to the AIRBUS Standards Manual (SM) 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. The SM will give you the correct part number

to part number relationship.

Kit 282148D06R01

ITEM NEW PART No. QTY UM KEYWORD ITEM OLD PART No. INT INST DISP

1 ABS0596S004 3 INSULATR

31 NSA5527-03-02D 2 SPACER

109 NSA935805-09 * 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 0 EQUIPMNT

149 NSA935401-03 30 TIE

150 NSA935401-04 30 TIE

NOTE : Refer to the AIRBUS Standards Manual (SM) 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. The SM will give you the correct part number

to part number relationship.

D. LIST OF MATERIALS - OPERATOR SUPPLIED

(1) Consumable Materials

DESCRIPTION REFERENCE TO CML QTY PER A/C INST/DISP

MAT No.

Solvent General Purpose Mat. No. 11-026 As required

storage compound Mat. No. 15-008A As required

Lint-Free Cotton Cloth Mat. No. 19-003 As required

(2) Components

None

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

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A310

SERVICE BULLETIN

E. PARTS TO BE RE-IDENTIFIED BY THE OPERATOR

None

F. TOOLING - PRICE AND AVAILABILITY

None

G. SPECIAL TOOLS

None

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

REVISION No. : 05 - Aug 03/10 Page : 18

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A310

SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS

A. GENERAL

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

IN THE REFERENCED PROCEDURES.

CAUTION : ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP ELECTRICAL

WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY AND MECHANICALLY

SERVICEABLE). WHEN YOU DO MAINTENANCE WORK, REPAIRS OR

MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING, COMPONENTS AND

THE WORK AREA AS CLEAN AS POSSIBLE, TO DO THIS :

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

NECESSARY ON WIRING AND COMPONENTS.

- REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND OTHER

CONTAMINATION.

THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION AND

DAMAGE TO THE ELECTRICAL WIRING INSTALLATION.

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

(1) Preparation

(a) Config. 01 thru Config. 04

1 Make sure that the aircraft is electrically grounded, refer to AMM 24-00-00,

Page block 301.

2 De-energize the aircraft electrical circuits, refer to AMM 24-41-00, Page block

301.

3 Put access platform(s) in position.

4 Open the FWD cargo-compartment door 811, refer to AMM 52-30-00, Page

block 001.

5 In the FWD cargo compartment, at FR38.2, remove the partition panel 132SW,

refer to AMM 53-10-55, Page block 401.

6 In the FWD cargo compartment, remove the sidewall panel 132QW, refer to

AMM 06-41-53, Page block 001and AMM 25-54-10, Page block 201.

7 From the RH-wing, remove the access panel 613RR, refer to AMM 06-41-57,

Page block 001.

8 From the RH-wing, remove these access panels for access, refer to AMM

06-41-57, Page block 001 :

- 612AB, 612AT, 612BB, 612CB, 612DB and 613LR.

- 612HB, 612JB and 612KB.

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

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A310

SERVICE BULLETIN

- 623AB, 623BB, 623CB, 623DB, 623EB, 623FB and 623GB.

(2) Standard Practices

(a) Refer to the AIRBUS 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 the

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 (Mat. No. 15-008A) 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).

B. MODIFICATION

(1) Config. 01

Refer to Kit 282148A01R00

Refer to Kit 282148B01R00

Refer to Kit 282148D01R00

Refer to Kit 282148D02R01

Refer to Figure 1

Refer to Figure 2

Refer to Figure 3

Refer to Figure 4

Refer to Figure 5

Refer to Figure 6

Refer to Figure 7

Refer to Figure 14

Refer to Figure 15

NOTE(1) The sleeves ABS0596S004 and ABS0596S006 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.

(a) Install a new bracket on the RH wing between rib 8 and rib 9 on the rear sub spar.

Refer to Figure 4

Refer to Kit 282148B01R00

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

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A310

SERVICE BULLETIN

1 Remove from the rear sub spar at rib 8 and rib 9, RH wing the items that follow:

2 Rivet NSA54213510DCA Item (2) Discard

1 Bracket A5724630400000 Item (1) Discard

2 Clean the mating surfaces use Lint-Free Cotton Cloth (Mat. No. 19-003) made

moist with Solvent General Purpose (Mat. No. 11-026).

3 Get the items that follow from Kit 282148B01R00:

1 Bracket A5725068600000 Item 1

2 Rivet, Blind ASNA0078A502 Item 2

4 Copy drill the two holes from the old bracket, Item (1) to the new bracket, Item 1

at the location given (Refer to Figure 4).

5 Put the bracket, Item 1 in position on the rear sub spar on the RH wing between

rib 8 and rib 9.

6 Drill two holes through the bracket, Item 1 to a dimension of between 3.965mm

(0.156in) and 4.066mm (0.160in) to match the holes in the rear sub spar.

7 Use Solvent General Purpose (Mat. No. 11-026) and wet install on the RH

wing between rib 8 and rib 9 on the rear sub spar the bracket, Item 1 with

the two rivets, Item 2

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

Kit 282148A01R00

Refer to Figure 1, Sheet 1 and Sheet 2

1 On the Shelf 92VU, only around the wires identified in Figure 1, Sheet 1 and

Sheet 2, from the equipment 15QT-B to the connector 2354VC, install :

1600 mm Sleeve ABS0596S004 Item 1

2 Around the cable bundle of the connector 2354VC-A, install :

400 mm Sleeve ABS0596S004 Item 1

3 Attach the sleeves with :

50 Tie-Cable NSA935401-04

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

compartment.

Refer to Kit 282148A01R00

Refer to Figure 2

1 Around the cable bundle of the pressure seal 20VP, install :

1000 mm Sleeve ABS0596S006 Item 2

2 Attach the sleeves with :

50 Tie-Cable NSA935401-05

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A310

SERVICE BULLETIN

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

Kit 282148A01R00

Refer to Figure 3, Sheets 1 and 2

1 Around the cable bundle of the pressure seal 20VP, install :

1000 mm Sleeve ABS0596S006 Item 2

2 Attach the sleeves with :

50 Tie-Cable NSA935401-05

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

and rib 3 in zone 612.

Refer to Kit 282148D01R00

Refer to Figure 5

1 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

2 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

3 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

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SERVICE BULLETIN

and attach the cable sleeve with :

1 Tie NSA935401-03 Item 149

1 Tie NSA935401-04 Item 150

4 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

1 Clamp MS21919WCH3 Item (23) Retained

1 Spacer NSA5527-03-02D Item (31) Retained

1 Washer NAS1149D0332K Item (40) Retained

1 Screw NAS1096-3-21 Item (50) Retained

1 Clamp MS21919WCH10 Item (100) Retained

1 Clamp MS21919WCH13 Item 11

5 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

3 Spacer NSA5527-03-02D Item (31) Retained

1 Washer NAS1149D0332K Item (40) Retained

1 Screw NAS1096-3-38 Item (54) Retained

1 Clamp MS21919WCH13 Item 11

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

and rib 8 in zone 612.

Refer to Kit 282148D01R00

Refer to Figure 5

1 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

2 Install this cable sleeve around these identified wires from the cable bundle

2S/624VB, as shown in Details A, J, K, L, N and P :

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

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A310

SERVICE BULLETIN

and attach the cable sleeves with :

1 Tie NSA935401-03 Item 149

1 Tie NSA935401-04 Item 150

3 Install this cable sleeve around this identified wire from the cable bundle

2S/624VB, as shown in Details A, J, K, L, N and P :

Wire number 2842-5070

1 Sleeve ABS0596S004 Item 1

and attach the cable sleeves with :

1 Tie NSA935401-03 Item 149

1 Tie NSA935401-04 Item 150

4 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

2 Washer NAS1149D0332K Item (40) Retained

2 Screw NAS1096-3-8 Item (55) Retained

2 Clamp MS21919WCH14 Item 12

(g) Install 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 Kit 282148D02R01

Refer to Figure 7

Refer to Figure 14

Refer to Figure 15

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, Figure 14 and the

Hook-up Chart 2, Lines 2 thru 8, END 1, Figure 15.

2 Remove, refer to Figure 7, Sheet 3, Detail C, 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

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3 Remove, refer to Figure 7, Sheet 4, Detail E, 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 Figure 7, Sheet 5, Detail G, 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 Figure 7, Sheet 6, Detail J, 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 Figure 7, Sheet 7, Detail L, 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 Figure 7, Sheet 8, 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

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SERVICE BULLETIN

8 Remove the identification sleeves from the cable harnesses near the receptacles

40VC and 5006VC as shown Figure 7, Sheet 1, Detail A

placard Item (125) Discard

9 Remove the protection sleeve from the cable harness as shown Figure 7,

Details C, E, G, J, L and P :

1 Sleeve NSA935805-10 Item (109) Discard

10 Cut the conduit to the required length and install as shown Figure 7, Details

D, F, H, K, N and Q :

3 Conduit NSA935805-09 Item 109

- 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, Figure 15

- Three parts, one 520mm (20.47in.) and two 240.0 mm (9.45 in.) to the

remaining electrical wires of route 2S/636VB, refer to Figure 14

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, Figure 14

and the Hook-up Chart 2, lines 2 thru 8, END 1, Figure 15. Use the contact

pins if required :

15 Pin NSA938184PV1601 Item 126

12 Install, refer to Figure 7, Sheet 8, Detail Q, AFTER :

1 Spacer NSA5527-03-02D Item (31) Retained

1 Clamp NSA935807C16 Item (111) Retained

1 Washer NSA935808-01 Item (112) Retained

1 Spacer NSA5527-03-05D Item (114) Retained

2 Clamp NSA935807C09 Item (117) Retained

1 Screw NAS1096-3-25 Item (119) Retained

1 Clamp NSA935807C09 Item 117

13 Install, refer to Figure 7, Sheet 7, Detail N, AFTER :

1 Spacer NSA5527-03-01D Item (30) Retained

1 Spacer NSA5527-03-02D Item (31) Retained

1 Clamp NSA935807C16 Item (111) Retained

1 Washer NSA935808-01 Item (112) Retained

1 Spacer NSA5527-03-05D Item (114) Retained

1 Clamp NSA935807C09 Item (117) Retained

1 Screw NAS1096-3-33 Item (118) Retained

2 Clamp NSA935807C09 Item 117

14 Install, refer to Figure 7, Sheet 6, Detail K, AFTER :

1 Spacer NSA5527-03-01D Item (30) Retained

1 Spacer NSA5527-03-02D Item (31) Retained

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

REVISION No. : 05 - Aug 03/10 Page : 26

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A310

SERVICE BULLETIN

1 Clamp NSA935807C16 Item (111) Retained

1 Spacer NSA5527-03-05D Item (114) Retained

1 Washer NSA1149D0332K Item (115) Retained

1 Clamp NSA935807C09 Item (117) Retained

1 Screw NAS1096-3-33 Item (118) Retained

2 Clamp NSA935807C09 Item 117

15 Install, refer to Figure 7, Sheet 5, Detail H, AFTER :

2 Spacer NSA5527-03-01D Item (30) Retained

2 Spacer NSA5527-03-02D Item (31) Retained

2 Clamp NSA935807C16 Item (111) Retained

2 Spacer NSA5527-03-05D Item (114) Retained

2 Washer NSA1149D0332K Item (115) Retained

2 Clamp NSA935807C09 Item (117) Retained

2 Screw NAS1096-3-33 Item (118) Retained

4 Clamp NSA935807C09 Item 117

16 Install, refer to Figure 7, Sheet 4, Detail F, AFTER :

2 Spacer NSA5527-03-01D Item (30) Retained

1 Spacer NSA5527-03-02D Item (31) Retained

1 Clamp NSA935807C10 Item (110) Retained

1 Clamp NSA935807C16 Item (111) Retained

1 Washer NSA935808-01 Item (112) Retained

1 Clamp NSA935807C09 Item (117) Retained

1 Screw NAS1096-3-33 Item (118) Retained

2 Clamp NSA935807C09 Item 117

17 Install, refer to Figure 7, Sheet 3, Detail D, AFTER :

2 Spacer NSA5527-03-01D Item 30

1 Clamp NSA935807C16 Item (111) Retained

1 Washer NSA935808-01 Item (112) Retained

1 Screw NAS1096-3-23 Item (113) Retained

1 Washer NSA1149D0332K Item (115) Retained

1 Nut NAS1291C3M Item (116) Retained

1 Clamp NSA935807C09 Item (117) Retained

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, Figure 15 with :

2 Sleeve ABS0596S004 Item 1

and

20 Tie NSA935401-03 Item 149

20 Tie NSA935401-04 Item 150

19 Install the identification placards :

1 Placard set B9299071900200 Item 125

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

REVISION No. : 05 - Aug 03/10 Page : 27

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A310

SERVICE BULLETIN

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

and rib 12 in zone 623.

Refer to Kit 282148D01R00

Refer to Kit 282148D02R01

Refer to Figure 6

1 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

2 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

3 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

4 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

5 Remove these items from the bracket between rib 9 and rib 10 and cable bundle

2S/636VB, as shown in Details A and N :

3 Clamp MS21919WCH4 Item (22) Retain

1 Clamp Item (23) Discard

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

REVISION No. : 05 - Aug 03/10 Page : 28

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A310

SERVICE BULLETIN

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

6 Remove these items from the bracket of the rib 9 and cable bundle 2S/636VB,

as shown in Details A and R :

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

7 Install this cable sleeve around these identified wires from the cable bundle

2S/636VB, as shown in Details A, C, E, G, J, L, Q, A 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 Cord NSA8420-2 Item 16

1 Tie NSA935401-03 Item 149

1 Tie NSA935401-04 Item 150

8 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

1 Clamp MS21919WCH3 Item (23) Retained

1 Spacer NSA5527-03-01D Item (30) Retained

1 Spacer NSA5527-03-02D Item (31) Retained

1 Washer NSA935808-01 Item (112) Retained

1 Clamp NSA935807-06 Item (122) Retained

1 Clamp MS21919WCH9 Item 10

2 Spacer NSA5527-03-02D Item 31

1 Screw NAS1096-3-40 Item 121

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

REVISION No. : 05 - Aug 03/10 Page : 29

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A310

SERVICE BULLETIN

9 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

4 Spacer NSA5527-03-01D Item (30) Retained

2 Washer NAS1149D0332K Item (40) Retained

2 Screw NAS1096-3-27 Item (52) Retained

2 Clamp MS21919WCH9 Item 10

10 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

1 Spacer NSA5527-03-01D Item (30) Retained

1 Spacer NSA5527-03-04D Item (32) Retained

1 Washer NAS1149D0332K Item (40) Retained

1 Screw NAS1096-3-22 Item (51) Retained

1 Clamp MS21919WCH9 Item 10

11 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

2 Spacer NSA5527-03-01D Item (30) Retained

2 Washer NAS1149D0332K Item (40) Retained

2 Clamp MS21919WCH9 Item 10

2 Screw NAS1096-3-19 Item 14

12 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

1 Spacer NSA5527-03-01D Item (30) Retained

1 Spacer NSA5527-03-04D Item (32) Retained

1 Washer NAS1149D0332K Item (40) Retained

1 Screw NAS1096-3-22 Item (51) Retained

1 Clamp MS21919WCH9 Item 10

13 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 S :

1 Clamp MS21919WCH5 Item (21) Retained

1 Spacer NSA5527-03-02D Item (31) Retained

1 Spacer NSA5527-03-04D Item (32) Retained

1 Washer NAS1149D0332K Item (40) Retained

1 Screw NAS1096-3-27 Item (52) Retained

1 Clamp MS21919WCH9 Item 10

(2) Config. 02

Refer to Kit 282148A01R00

Refer to Kit 282148B01R00

Refer to Kit 282148D01R00

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

REVISION No. : 05 - Aug 03/10 Page : 30

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A310

SERVICE BULLETIN

Refer to Kit 282148D03R01

Refer to Figure 1

Refer to Figure 2

Refer to Figure 3

Refer to Figure 4

Refer to Figure 5

Refer to Figure 6

Refer to Figure 8

Refer to Figure 15

NOTE(1) The sleeves ABS0596S004 and ABS0596S006 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.

(a) Install a new bracket on the RH wing between rib 8 and rib 9 on the rear sub spar.

Refer to Figure 4

Refer to Kit 282148B01R00

1 Remove from the rear sub spar at rib 8 and rib 9, RH wing the items that follow:

2 Rivet NSA54213510DCA Item (2) Discard

1 Bracket A5724630400000 Item (1) Discard

2 Clean the mating surfaces use Lint-Free Cotton Cloth (Mat. No. 19-003) made

moist with Solvent General Purpose (Mat. No. 11-026).

3 Get the items that follow from Kit 282148B01R00:

1 Bracket A5725068600000 Item 1

2 Rivet, Blind ASNA0078A502 Item 2

4 Copy drill the two holes from the old bracket, Item (1) to the new bracket, Item 1

at the location given (Refer to Figure 4).

5 Put the bracket, Item 1 in position on the rear sub spar on the RH wing between

rib 8 and rib 9.

6 Drill two holes through the bracket, Item 1 to a dimension of between 3.965mm

(0.156in) and 4.066mm (0.160in) to match the holes in the rear sub spar.

7 Use Solvent General Purpose (Mat. No. 11-026) and wet install on the RH

wing between rib 8 and rib 9 on the rear sub spar the bracket, Item 1 with

the two rivets, Item 2

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

Kit 282148A01R00

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

REVISION No. : 05 - Aug 03/10 Page : 31

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A310

SERVICE BULLETIN

Refer to Figure 1, Sheet 1 and Sheet 2

1 On the Shelf 92VU, only around the wires identified in Figure 1, Sheet 1 and

Sheet 2, from the equipment 15QT-B to the connector 2354VC, install :

1600 mm Sleeve ABS0596S004 Item 1

2 Around the cable bundle of the connector 2354VC-A, install :

400 mm Sleeve ABS0596S004 Item 1

3 Attach the sleeves with :

50 Tie-Cable NSA935401-04

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

compartment.

Refer to Kit 282148A01R00

Refer to Figure 2

1 Around the cable bundle of the pressure seal 20VP, install :

1000 mm Sleeve ABS0596S006 Item 2

2 Attach the sleeves with :

50 Tie-Cable NSA935401-05

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

Refer to Kit 282148A01R00

Refer to figure 3, sheets 1 and 2

1 Around the cable bundle of the pressure seal 20VP, install :

1000 mm Sleeve ABS0596S006 Item 2

2 Attach the sleeves with :

50 Tie-Cable NSA935401-05

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

and rib 3 in zone 612.

Refer to Kit 282148D01R00

Refer to Figure 5

1 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. : 05 - Aug 03/10 Page : 32

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A310

SERVICE BULLETIN

2 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

3 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 NSA935401-04 Item 150

4 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

1 Clamp MS21919WCH3 Item (23) Retained

1 Spacer NSA5527-03-02D Item (31) Retained

1 Washer NAS1149D0332K Item (40) Retained

1 Screw NAS1096-3-21 Item (50) Retained

1 Clamp MS21919WCH10 Item (100) Retained

1 Clamp MS21919WCH13 Item 11

5 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

3 Spacer NSA5527-03-02D Item (31) Retained

1 Washer NAS1149D0332K Item (40) Retained

1 Screw NAS1096-3-38 Item (54) Retained

1 Clamp MS21919WCH13 Item 11

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

and rib 8 in zone 612.

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

REVISION No. : 05 - Aug 03/10 Page : 33

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A310

SERVICE BULLETIN

Refer to Kit 282148D01R00

Refer to Figure 5

1 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

2 Install this cable sleeve around these identified wires from the cable bundle

2S/624VB, as shown in Details A, J, K, L, N and P :

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 NSA935401-04 Item 150

3 Install this cable sleeve around this identified wire from the cable bundle

2S/624VB, as shown in Details A, J, K, L, N and P :

Wire number 2842-5070

1 Sleeve ABS0596S004 Item 1

and attach the cable sleeves with :

1 Tie NSA935401-03 Item 149

1 Tie NSA935401-04 Item 150

4 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

2 Washer NAS1149D0332K Item (40) Retained

2 Screw NAS1096-3-8 Item (55) Retained

2 Clamp MS21919WCH14 Item 12

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

rib 9 (pylon area) in zone 612.

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

REVISION No. : 05 - Aug 03/10 Page : 34

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A310

SERVICE BULLETIN

Refer to Kit 282148D03R01

Refer to Figure 8

Refer to Figure 15

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 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, Figure 15.

2 Remove, refer to Figure 8, Sheet 3, Detail C, 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 Figure 8, Sheet 4, Detail E, 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

4 Remove, refer to Figure 8, Sheet 5, Detail G, 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 Figure 8, Sheet 6, Detail J, 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 Figure 8, Sheet 7, Detail L, 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

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

REVISION No. : 05 - Aug 03/10 Page : 35

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A310

SERVICE BULLETIN

7 Remove, refer to Figure 8, Sheet 8, 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

8 Remove the identification placards from the cable harnesses near the

receptacles 52VC and 5006VC as shown Figure 8, Sheet 2, Detail A

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, Figure 15 :

1 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, Figure 15. Use

the contact pins if required :

7 Pin NSA938184PV1601 Item 126

12 Install, refer to Figure 8, Sheet 8, Detail Q, AFTER :

1 Spacer NSA5527-03-02D Item (31) Retained

1 Spacer NSA5527-03-02D Item 31

2 Clamp NSA935807C16 Item (111) Retained

1 Washer NSA935808-01 Item (112) Retained

1 Spacer NSA5527-03-05D Item (114) Retained

1 Clamp NSA935807C09 Item 117

1 Screw NAS1801-3-31 Item 123

1 Spacer NSA5527-03-07D Item 131

13 Install, refer to Figure 8, Sheet 7, Detail N, AFTER :

1 Spacer NSA5527-03-02D Item (31) Retained

2 Clamp NSA935807C16 Item (111) Retained

1 Washer NSA935808-01 Item (112) Retained

1 Spacer NSA5527-03-05D Item (114) Retained

1 Clamp NSA935807C09 Item 117

1 Screw NAS1801-3-31 Item 123

1 Spacer NSA5527-03-08D Item 130

14 Install, refer to Figure 8, Sheet 6, Detail K, AFTER :

2 Spacer NSA5527-03-02D Item (31) Retained

2 Clamp NSA935807C16 Item (111) Retained

1 Washer NSA935808-01 Item (112) Retained

1 Clamp NSA5516-04NV Item (120) Retained

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

REVISION No. : 05 - Aug 03/10 Page : 36

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A310

SERVICE BULLETIN

1 Clamp NSA935807C09 Item 117

2 Screw NAS1801-3-31 Item 123

15 Install, refer to Figure 8, Sheet 5, Detail H, AFTER :

2 Spacer NSA5527-03-02D Item (31) Retained

4 Clamp NSA935807C16 Item (111) Retained

2 Washer NSA935808-01 Item (112) Retained

2 Screw NAS1096-3-23 Item (113) Retained

2 Spacer NSA5527-03-05D Item (114) Retained

2 Clamp NSA935807C09 Item 117

16 Install, refer to Figure 8, Sheet 4, Detail F, AFTER :

1 Spacer NSA5527-03-02D Item (31) Retained

2 Clamp NSA935807C16 Item (111) Retained

1 Washer NSA935808-01 Item (112) Retained

1 Screw NAS1096-3-23 Item (113) Retained

1 Spacer NSA5527-03-05D Item (114) Retained

1 Clamp NSA935807C09 Item 117

17 Install, refer to Figure 8, Sheet 3, Detail D, AFTER :

1 Spacer NSA5527-03-02D Item (31) Retained

2 Clamp NSA935807C16 Item (111) Retained

1 Washer NSA935808-01 Item (112) Retained

1 Screw NAS1096-3-23 Item (113) Retained

1 Spacer NSA5527-03-05D Item (114) Retained

1 Nut NAS1291C3M Item (116) Retained

1 Washer AN960KD10l Item (124) Retained

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, Figure 15 with :

3 Sleeve ABS0596S004 Item 1

and

20 Tie NSA935401-03 Item 149

20 Tie NSA935401-04 Item 150

19 Install the identification placards, refer to Figure 8, Sheet 2 :

1 Equipment B9299071900600 Item 132

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

and rib 12 in zone 623.

Refer to Kit 282148D01R00

Refer to Kit 282148D03R01

Refer to Figure 6

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

REVISION No. : 05 - Aug 03/10 Page : 37

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

1 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

2 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

3 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

4 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

5 Remove these items from the bracket between rib 9 and rib 10 and cable bundle

2S/636VB, as shown in Details A and N :

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

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

REVISION No. : 05 - Aug 03/10 Page : 38

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

6 Remove these items from the bracket of the rib 9 and cable bundle 2S/636VB,

as shown in Details A and R :

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

7 Install this cable sleeve around these identified wires from the cable bundle

2S/636VB, as shown in Details A, C, E, G, J, L, Q, S, T, U and V :

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 Cord NSA8420-2 Item 16

10 Tie NSA935401-03 Item 149

20 Tie NSA935401-04 Item 150

8 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

1 Clamp MS21919WCH3 Item (23) Retained

1 Spacer NSA5527-03-01D Item (30) Retained

1 Spacer NSA5527-03-02D Item (31) Retained

1 Washer NSA935808-01 Item (112) Retained

1 Clamp NSA935807-06 Item (122) Retained

1 Clamp MS21919WCH9 Item 10

1 Spacer NSA5527-03-02D Item 31

1 Screw NAS1096-3-40 Item 121

9 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

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

REVISION No. : 05 - Aug 03/10 Page : 39

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

4 Spacer NSA5527-03-01D Item (30) Retained

2 Washer NAS1149D0332K Item (40) Retained

2 Screw NAS1096-3-27 Item (52) Retained

2 Clamp MS21919WCH9 Item 10

10 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

2 Spacer NSA5527-03-01D Item (30) Retained

2 Spacer NSA5527-03-04D Item (32) Retained

2 Washer NAS1149D0332K Item (40) Retained

2 Screw NAS1096-3-22 Item (51) Retained

2 Clamp MS21919WCH9 Item 10

11 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

2 Spacer NSA5527-03-01D Item (30) Retained

2 Washer NAS1149D0332K Item (40) Retained

2 Clamp MS21919WCH9 Item 10

2 Screw NAS1096-3-19 Item 14

12 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

1 Spacer NSA5527-03-01D Item (30) Retained

1 Spacer NSA5527-03-04D Item (32) Retained

1 Washer NAS1149D0332K Item (40) Retained

1 Screw NAS1096-3-22 Item (51) Retained

1 Clamp MS21919WCH9 Item 10

13 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 S :

1 Clamp MS21919WCH5 Item (21) Retained

1 Spacer NSA5527-03-02D Item (31) Retained

1 Spacer NSA5527-03-04D Item (32) Retained

1 Washer NAS1149D0332K Item (40) Retained

1 Screw NAS1096-3-27 Item (52) Retained

1 Clamp MS21919WCH9 Item 10

(3) Config. 03

Refer to Kit 282148A01R00

Refer to Kit 282148B01R00

Refer to Kit 282148D01R00

Refer to Kit 282148D05R01

Refer to Figure 1

Refer to Figure 2

Refer to Figure 3

Refer to Figure 4

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

REVISION No. : 05 - Aug 03/10 Page : 40

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

Refer to Figure 5

Refer to Figure 6

Refer to Figure 9

Refer to Figure 14

Refer to Figure 15

NOTE(1) The sleeves ABS0596S004 and ABS0596S006 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.

(a) Install a new bracket on the RH wing between rib 8 and rib 9 on the rear sub spar.

Refer to Figure 4

Refer to Kit 282148B01R00

1 Remove from the rear sub spar at rib 8 and rib 9, RH wing the items that follow:

2 Rivet NSA54213510DCA Item (2) Discard

1 Bracket A5724630400000 Item (1) Discard

2 Clean the mating surfaces use Lint-Free Cotton Cloth (Mat. No. 19-003) made

moist with Solvent General Purpose (Mat. No. 11-026).

3 Get the items that follow from Kit 282148B01R00:

1 Bracket A5725068600000 Item 1

2 Rivet, Blind ASNA0078A502 Item 2

4 Copy drill the two holes from the old bracket, Item (1) to the new bracket, Item 1

at the location given (Refer to Figure 4).

5 Put the bracket, Item 1 in position on the rear sub spar on the RH wing between

rib 8 and rib 9.

6 Drill two holes through the bracket, Item 1 to a dimension of between 3.965mm

(0.156in) and 4.066mm (0.160in) to match the holes in the rear sub spar.

7 Use Solvent General Purpose (Mat. No. 11-026) and wet install on the RH

wing between rib 8 and rib 9 on the rear sub spar the bracket, Item 1 with

the two rivets, Item 2

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

Kit 282148A01R00

Refer to Figure 1, Sheet 1 and Sheet 2

1 On the Shelf 92VU, only around the wires identified in Figure 1, Sheet 1 and

Sheet 2, from the equipment 15QT-B to the connector 2354VC, install :

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

REVISION No. : 05 - Aug 03/10 Page : 41

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

1600 mm Sleeve ABS0596S004 Item 1

2 Around the cable bundle of the connector 2354VC-A, install :

400 mm Sleeve ABS0596S004 Item 1

3 Attach the sleeves with :

50 Tie-Cable NSA935401-04

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

compartment.

Refer to Kit 282148A01R00

Refer to Figure 2

1 Around the cable bundle of the pressure seal 20VP, install :

1000 mm Sleeve ABS0596S006 Item 2

2 Attach the sleeves with :

50 Tie-Cable NSA935401-05

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

Kit 282148A01R00

Refer to Figure 3, Sheets 1 and 2

1 Around the cable bundle of the pressure seal 20VP, install :

1000 mm Sleeve ABS0596S006 Item 2

2 Attach the sleeves with :

50 Tie-Cable NSA935401-05

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

and rib 3 in zone 612.

Refer to Kit 282148D01R00

Refer to Figure 5

1 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

2 Remove these items from the riblet and cable bundle 2S/624VB, as shown

in Details A and D :

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

REVISION No. : 05 - Aug 03/10 Page : 42

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

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

3 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 NSA935401-04 Item 150

and

1 Placard set B9299071900200 Item 125

as necessary.

4 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

1 Clamp MS21919WCH3 Item (23) Retained

1 Spacer NSA5527-03-02D Item (31) Retained

1 Washer NAS1149D0332K Item (40) Retained

1 Screw NAS1096-3-21 Item (50) Retained

1 Clamp MS21919WCH10 Item (100) Retained

1 Clamp MS21919WCH13 Item 11

5 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

3 Spacer NSA5527-03-02D Item (31) Retained

1 Washer NAS1149D0332K Item (40) Retained

1 Screw NAS1096-3-38 Item (54) Retained

1 Clamp MS21919WCH13 Item 11

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

REVISION No. : 05 - Aug 03/10 Page : 43

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

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

and rib 8 in zone 612.

Refer to Kit 282148D01R00

Refer to Figure 5

1 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

2 Install this cable sleeve around these identified wires from the cable bundle

2S/624VB, as shown in Details A, J, K, L, N and P :

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 NSA935401-04 Item 150

3 Install this cable sleeve around this identified wire from the cable bundle

2S/624VB, as shown in Details A, J, K, L, N and P :

Wire number 2842-5070

1 Sleeve ABS0596S004 Item 1

and attach the cable sleeves with :

1 Tie NSA935401-03 Item 149

1 Tie NSA935401-04 Item 150

4 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

2 Washer NAS1149D0332K Item (40) Retained

2 Screw NAS1096-3-8 Item (55) Retained

2 Clamp MS21919WCH14 Item 12

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

REVISION No. : 05 - Aug 03/10 Page : 44

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

(g) Install 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 Kit 282148D05R01

Refer to Figure 9

Refer to Figure 14

Refer to Figure 15

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, Figure 14 and the

Hook-up Chart 2, Lines 2 thru 8, END 1, Figure 15.

2 Remove, refer to Figure 9, Sheet 3, Detail C, BEFORE :

2 Spacer NSA5527-03-05D Item (30) Discard

1 Washer NSA935808-01 Item (112) Retain

1 Nut NAS1291C3M Item (116) Retain

1 Clamp NSA935807C10 Item (117) Discard

1 Screw Item (136) Discard

3 Remove, refer to Figure 9, Sheet 4, Detail E, BEFORE :

1 Washer NSA935808-01 Item (112) Retain

1 Screw Item (113) Retain

1 Clamp NSA935807C10 Item (117) Discard

4 Remove, refer to Figure 9, Sheet 5, Detail G, BEFORE :

2 Washer NSA935808-01 Item (112) Retain

2 Screw Item (113) Retain

2 Clamp NSA935807C10 Item (117) Discard

5 Remove, refer to Figure 9, Sheet 6, 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

6 Remove, refer to Figure 9, Sheet 7, Detail L, BEFORE :

1 Washer NSA935808-01 Item (112) Retain

1 Screw Item (113) Retain

1 Clamp NSA935807C10 Item (117) Discard

7 Remove, refer to Figure 9, Sheet 8, Detail P, BEFORE :

1 Washer NSA935808-01 Item (112) Retain

1 Screw Item (113) Retain

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

REVISION No. : 05 - Aug 03/10 Page : 45

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

1 Clamp NSA935807C10 Item (117) Discard

8 Remove the protection sleeve from the cable harness as shown Figure 9,

Details A, C, E, G, J, L and P :

1 Sleeve NSA935805-10 Item (1) Discard

9 Cut the conduit to the required length and install as shown Figure 9, Details

B, D, F, H, K, N, Q and R:

3 Sleeve ABS0596S004 Item 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, Figure 15

10 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, Figure 14

and the Hook-up Chart 2, lines 2 thru 8, END 1, Figure 15. Use the contact

pins if required :

15 Pin NSA938184PV1601 Item 126

11 Install, refer to Figure 9, Sheet 8, Detail Q, AFTER :

1 Washer NSA935808-01 Item (112) Retained

1 Screw Item (113) Retained

2 Clamp NSA935807C09 Item 117

12 Install, refer to Figure 9, Sheet 7, Detail N, AFTER :

1 Washer NSA935808-01 Item (112) Retained

1 Screw Item (113) Retained

2 Clamp NSA935807C09 Item 117

13 Install, refer to Figure 9, Sheet 6, Detail K, AFTER :

1 Spacer NSA5527-03-02D Item 31

1 Washer NSA935808-01 Item (112) Retained

2 Clamp NSA935807C09 Item 117

1 Screw NAS1096-3-42 Item 135

14 Install, refer to Figure 9, Sheet 5, Detail H, AFTER :

2 Washer NSA935808-01 Item (112) Retained

2 Screw Item (113) Retained

4 Clamp NSA935807C09 Item 117

15 Install, refer to Figure 9, Sheet 4, Detail F, AFTER :

1 Washer NSA935808-01 Item (112) Retained

1 Screw Item (113) Retained

2 Clamp NSA935807C09 Item 117

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

REVISION No. : 05 - Aug 03/10 Page : 46

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

16 Install, refer to Figure 9, Sheet 3, Detail D, AFTER :

2 Spacer NSA5527-03-01D Item 30

2 Washer NSA935808-01 Item (112) Retained

2 Nut NAS1291C3M Item (116) Retain

2 Clamp NSA935807C09 Item 117

1 Screw NAS1096-3-30 Item 136

17 Protect the electrical wires for 10QT-A and 10QT-B of route 2S/636VB, refer to

Figure 9, Sheet 9, Detail R, and the Hook-up Chart 2, Figure 15 with :

30 Tie NSA935401-03 Item 149

30 Tie NSA935401-04 Item 150

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

and rib 12 in zone 623.

Refer to Kit 282148D01R00

Refer to Kit 282148D05R01

Refer to Figure 6

1 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

2 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

3 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

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

REVISION No. : 05 - Aug 03/10 Page : 47

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

4 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

5 Remove these items from the bracket between rib 9 and rib 10 and cable bundle

2S/636VB, as shown in Details A and N :

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

6 Remove these items from the bracket of the rib 9 and cable bundle 2S/636VB,

as shown in Details A and R :

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

7 Install this cable sleeve around these identified wires from the cable bundle

2S/636VB, as shown in Details A, C, E, G, J, L, Q, 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 Cord NSA8420-2 Item 16

10 Tie NSA935401-03 Item 149

20 Tie NSA935401-04 Item 150

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

REVISION No. : 05 - Aug 03/10 Page : 48

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

8 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

1 Clamp MS21919WCH3 Item (23) Retained

1 Spacer NSA5527-03-01D Item (30) Retained

1 Spacer NSA5527-03-02D Item (31) Retained

1 Washer NSA935808-01 Item (112) Retained

1 Clamp NSA935807-06 Item (122) Retained

1 Clamp MS21919WCH9 Item 10

1 Spacer NSA5527-03-02D Item 31

1 Screw NAS1096-3-40 Item 121

9 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

4 Spacer NSA5527-03-01D Item (30) Retained

2 Washer NAS1149D0332K Item (40) Retained

2 Screw NAS1096-3-27 Item (52) Retained

2 Clamp MS21919WCH9 Item 10

10 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

1 Spacer NSA5527-03-01D Item (30) Retained

1 Spacer NSA5527-03-04D Item (32) Retained

1 Washer NAS1149D0332K Item (40) Retained

1 Screw NAS1096-3-22 Item (51) Retained

1 Clamp MS21919WCH9 Item 10

11 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

2 Spacer NSA5527-03-01D Item (30) Retained

2 Washer NAS1149D0332K Item (40) Retained

2 Clamp MS21919WCH9 Item 10

2 Screw NAS1096-3-19 Item 14

12 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

1 Spacer NSA5527-03-01D Item (30) Retained

1 Spacer NSA5527-03-04D Item (32) Retained

1 Washer NAS1149D0332K Item (40) Retained

1 Screw NAS1096-3-22 Item (51) Retained

1 Clamp MS21919WCH9 Item 10

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

REVISION No. : 05 - Aug 03/10 Page : 49

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

13 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 S :

1 Clamp MS21919WCH5 Item (21) Retained

1 Spacer NSA5527-03-02D Item (31) Retained

1 Spacer NSA5527-03-04D Item (32) Retained

1 Washer NAS1149D0332K Item (40) Retained

1 Screw NAS1096-3-27 Item (52) Retained

1 Clamp MS21919WCH9 Item 10

(4) Config. 04

Refer to Kit 282148A01R00

Refer to Kit 282148B01R00

Refer to Kit 282148D01R00

Refer to Kit 282148D06R01

Refer to Figure 1

Refer to Figure 2

Refer to Figure 3

Refer to Figure 4

Refer to Figure 5

Refer to Figure 6

Refer to Figure 10

Refer to Figure 15

NOTE(1) The sleeves ABS0596S004 and ABS0596S006 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.

(a) Install a new bracket on the RH wing between rib 8 and rib 9 on the rear sub spar.

Refer to Figure 4

Refer to Kit 282148B01R00

1 Remove from the rear sub spar at rib 8 and rib 9, RH wing the items that follow:

2 Rivet NSA54213510DCA Item (2) Discard

1 Bracket A5724630400000 Item (1) Discard

2 Clean the mating surfaces use Lint-Free Cotton Cloth (Mat. No. 19-003) made

moist with Solvent General Purpose (Mat. No. 11-026).

3 Get the items that follow from Kit 282148B01R00:

1 Bracket A5725068600000 Item 1

2 Rivet, Blind ASNA0078A502 Item 2

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SERVICE BULLETIN

4 Copy drill the two holes from the old bracket, Item (1) to the new bracket, Item 1

at the location given (Refer to Figure 4).

5 Put the bracket, Item 1 in position on the rear sub spar on the RH wing between

rib 8 and rib 9.

6 Drill two holes through the bracket, Item 1 to a dimension of between 3.965mm

(0.156in) and 4.066mm (0.160in) to match the holes in the rear sub spar.

7 Use Solvent General Purpose (Mat. No. 11-026) and wet install on the RH

wing between rib 8 and rib 9 on the rear sub spar the bracket, Item 1 with

the two rivets, Item 2

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

Kit 282148A01R00

Refer to Figure 1, Sheet 1 and Sheet 2

1 On the Shelf 92VU, only around the wires identified in Figure 1, Sheet 1 and

Sheet 2, from the equipment 15QT-B to the connector 2354VC, install :

1600 mm Sleeve ABS0596S004 Item 1

2 Around the cable bundle of the connector 2354VC-A, install :

400 mm Sleeve ABS0596S004 Item 1

3 Attach the sleeves with :

50 Tie-Cable NSA935401-04

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

compartment.

Refer to Kit 282148A01R00

Refer to Figure 2

1 Around the cable bundle of the pressure seal 20VP, install :

1000 mm Sleeve ABS0596S006 Item 2

2 Attach the sleeves with :

50 Tie-Cable NSA935401-05

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

Refer to Kit 282148A01R00

Refer to figure 3, sheets 1 and 2

1 Around the cable bundle of the pressure seal 20VP, install :

1000 mm Sleeve ABS0596S006 Item 2

2 Attach the sleeves with :

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SERVICE BULLETIN

50 Tie-Cable NSA935401-05

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

and rib 3 in zone 612.

Refer to Kit 282148D01R00

Refer to Figure 5

1 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

2 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

3 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 NSA935401-04 Item 150

and

1 Equipment B9299071900600 Item 132

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SERVICE BULLETIN

as necessary.

4 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

1 Clamp MS21919WCH3 Item (23) Retained

1 Spacer NSA5527-03-02D Item (31) Retained

1 Washer NAS1149D0332K Item (40) Retained

1 Screw NAS1096-3-21 Item (50) Retained

1 Clamp MS21919WCH10 Item (100) Retained

1 Clamp MS21919WCH13 Item 11

5 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

3 Spacer NSA5527-03-02D Item (31) Retained

1 Washer NAS1149D0332K Item (40) Retained

1 Screw NAS1096-3-38 Item (54) Retained

1 Clamp MS21919WCH13 Item 11

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

and rib 8 in zone 612.

Refer to Kit 282148D01R00

Refer to Figure 5

1 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

2 Install this cable sleeve around these identified wires from the cable bundle

2S/624VB, as shown in Details A, J, K, L, N and P :

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

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SERVICE BULLETIN

1 Tie NSA935401-04 Item 150

3 Install this cable sleeve around this identified wire from the cable bundle

2S/624VB, as shown in Details A, J, K, L, N and P :

Wire number 2842-5070

1 Sleeve ABS0596S004 Item 1

and attach the cable sleeves with :

1 Tie NSA935401-03 Item 149

1 Tie NSA935401-04 Item 150

4 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

2 Washer NAS1149D0332K Item (40) Retained

2 Screw NAS1096-3-8 Item (55) Retained

2 Clamp MS21919WCH14 Item 12

(g) Install 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 Kit 282148D01R00

Refer to Kit 282148D06R01

Refer to Figure 10

Refer to Figure 15

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 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, Figure 15.

2 Remove, refer to Figure 10, Sheet 3, 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

3 Remove, refer to Figure 10, Sheet 4, Detail E, BEFORE :

1 Washer NSA935808-01 Item (112) Retain

1 Screw NAS1096-3-23 Item (113) Retain

4 Remove, refer to Figure 10, Sheet 5, Detail G, BEFORE :

2 Washer NSA935808-01 Item (112) Retain

2 Screw NAS1096-3-23 Item (113) Retain

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5 Remove, refer to Figure 10, Sheet 6, Detail J, BEFORE :

1 Spacer NSA5527-03-02D Item (31) Retain

1 Screw Item (121) Discard

6 Remove, refer to Figure 10, Sheet 7, Detail L, BEFORE :

1 Screw Item (123) Discard

7 Remove, refer to Figure 10, Sheet 8, Detail P, BEFORE :

1 Screw Item (123) Discard

8 Cut the conduit to the required length and install as shown Figure 10, Details

B and R :

3 Sleeve ABS0596S004 Item 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, Figure 15

9 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, Figure 15. Use

the contact pins if required :

7 Pin NSA938184PV1601 Item 126

10 Install, refer to Figure 10, Sheet 8, Detail Q, 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

11 Install, refer to Figure 10, Sheet 7, Detail N, AFTER :

1 Clamp NSA935807C09 Item 117

1 Screw NAS1801-3-31 Item 123

1 Spacer NSA5527-03-08D Item 130

12 Install, refer to Figure 10, Sheet 6, Detail K, AFTER :

1 Spacer NSA5527-03-02D Item 31

1 Clamp NSA935807C09 Item 117

1 Screw NAS1096-3-40 Item 121

13 Install, refer to Figure 10, Sheet 5, Detail H, AFTER :

2 Washer NSA935808-01 Item (112) Retained

2 Screw NAS1096-3-23 Item (113) Retained

2 Clamp NSA935807C09 Item 117

14 Install, refer to Figure 10, Sheet 4, Detail F, AFTER :

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SERVICE BULLETIN

1 Washer NSA935808-01 Item (112) Retained

1 Screw NAS1096-3-23 Item (113) Retained

1 Clamp NSA935807C09 Item 117

15 Install, refer to Figure 10, Sheet 3, Detail D, AFTER :

1 Washer NSA935808-01 Item (112) Retained

1 Screw NAS1096-3-23 Item (113) Retained

1 Nut NAS1291C3M Item (116) Retained

1 Washer AN960KD10l Item (124) Retained

1 Clamp NSA935807C09 Item 117

16 Protect the electrical wires for 10QT-A and 10QT-B of route 2S/636VB, refer to

the Hook-up Chart 2, Figure 15 and Figure 10, Detail R with :

30 Tie NSA935401-03 Item 149

30 Tie NSA935401-04 Item 150

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

and rib 12 in zone 623.

Refer to Kit 282148D01R00

Refer to Kit 282148D06R01

Refer to Figure 6

1 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

2 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

3 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

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SERVICE BULLETIN

2 Washer NAS1149D0332K Item (40) Retain

2 Screw NAS1096-3-22 Item (51) Retain

4 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

5 Remove these items from the bracket between rib 9 and rib 10 and cable bundle

2S/636VB, as shown in Details A and N :

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

6 Remove these items from the bracket of the rib 9 and cable bundle 2S/636VB,

as shown in Details A and R :

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

7 Install this cable sleeve around these identified wires from the cable bundle

2S/636VB, as shown in Details A, C, E, G, J, L, Q 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

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SERVICE BULLETIN

1 Cord NSA8420-2 Item 16

1 Tie NSA935401-03 Item 149

1 Tie NSA935401-04 Item 150

8 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

1 Clamp MS21919WCH3 Item (23) Retained

1 Spacer NSA5527-03-01D Item (30) Retained

1 Spacer NSA5527-03-02D Item (31) Retained

1 Washer NSA935808-01 Item (112) Retained

1 Clamp NSA935807-06 Item (122) Retained

1 Clamp MS21919WCH9 Item 10

2 Spacer NSA5527-03-02D Item 31

1 Screw NAS1096-3-40 Item 121

9 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

4 Spacer NSA5527-03-01D Item (30) Retained

2 Washer NAS1149D0332K Item (40) Retained

2 Screw NAS1096-3-27 Item (52) Retained

2 Clamp MS21919WCH9 Item 10

10 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

1 Spacer NSA5527-03-01D Item (30) Retained

1 Spacer NSA5527-03-04D Item (32) Retained

1 Washer NAS1149D0332K Item (40) Retained

1 Screw NAS1096-3-22 Item (51) Retained

1 Clamp MS21919WCH9 Item 10

11 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

2 Spacer NSA5527-03-01D Item (30) Retained

2 Washer NAS1149D0332K Item (40) Retained

2 Clamp MS21919WCH9 Item 10

2 Screw NAS1096-3-19 Item 14

12 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

1 Spacer NSA5527-03-01D Item (30) Retained

1 Spacer NSA5527-03-04D Item (32) Retained

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

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SERVICE BULLETIN

1 Washer NAS1149D0332K Item (40) Retained

1 Screw NAS1096-3-22 Item (51) Retained

1 Clamp MS21919WCH9 Item 10

13 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 S :

1 Clamp MS21919WCH5 Item (21) Retained

1 Spacer NSA5527-03-02D Item (31) Retained

1 Spacer NSA5527-03-04D Item (32) Retained

1 Washer NAS1149D0332K Item (40) Retained

1 Screw NAS1096-3-27 Item (52) Retained

1 Clamp MS21919WCH9 Item 10

(5) Config. 01 ADDITIONAL WORK 1

ADDITIONAL WORK 1 is required by this revision for aircraft modified by issue 00 or

Revision 01.

(a) Preparation

1 Make sure that the aircraft is electrically grounded, refer to AMM 24-00-00,

Page block 301.

2 Fully extend the slats, refer to AMM 27-80-00, Page block 301.

3 De-energize the aircraft electrical circuits, refer to AMM 24-41-00, Page block

301.

4 Put the access platform(s) in position.

5 Open the access panels 612AT, 612KB, 612JB, 623AB, 623BB and 623EB.

6 Remove the bleed air duct if necessary, refer to AMM 36-11-00, Page block 401.

(b) Modification

Refer to Kit 282148D02R01

Refer to Figure 11

Refer to Figure 12

Refer to Figure 14

Refer to Figure 15

NOTE(4) Adapt the number of cable ties to the required quantity.

1 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 Figure 11

a At one position, remove these items from the bracket rib 11 and rib 12 and

cable bundle 2S/636VB, as shown in Figure 11, Sheet 1 and Sheet 3

Details A and D :

2 Clamp MS21919WCH4 Item (22) Retain

1 Clamp MS21919WCH4 Item (22) Discard

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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 Install protection sleeve, as shown in Figure 11, Sheet 1 thru Sheet 3,

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 NSA935401-04 Item 150

c Install, as shown in Figure 11, Sheet 1 and Sheet 3 Details A and E :

2 Clamp MS21919WCH4 Item (22) Retained

1 Clamp MS21919WCH3 Item (23) Retained

1 Spacer NSA5527-03-01D Item (30) Retained

1 Spacer NSA5527-03-02D Item (31) Retained

1 Washer NSA935808-01 Item (112) Retained

1 Clamp NSA935807-06 Item (122) Retained

1 Clamp MS21919WCH9 Item 10

1 Spacer NSA5527-03-02D Item 31

1 Screw NAS1096-3-40 Item 121

2 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 Figure 12

Refer to Figure 14

Refer to Figure 15

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.

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, Figure 14

and the Hook-up Chart 2, Lines 2 thru 8, END 1, Figure 15.

b Remove, refer to Figure 12, Sheet 3, Detail C, 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

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

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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 Figure 12, Sheet 4, Detail E, 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 Figure 12, Sheet 5, Detail G, 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 Figure 12, Sheet 6, Detail J, 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 Figure 12, Sheet 7, Detail L, 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 Figure 12, Sheet 8, Detail P, BEFORE :

1 Spacer NSA5527-03-02D Item (31) Retain

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

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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

h Remove the identification sleeves from the cable harnesses near the

receptacles 40VC and 5006VC as shown Figure 12, Sheet 1, Detail A

placard Item (125) Discard

i Remove the protection sleeve from the cable harness :

1 Sleeve Item (109) Discard

j Cut the conduit to the required length and install :

3 Conduit NSA935805-09 Item 109

- 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, Figure 15

- 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 Figure 14

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, Figure 14 and the Hook-up Chart 2, Lines 2 thru 8, END 1, Figure 15.

Use the contact pins if required :

15 Pin NSA938184PV1601 Item 126

l Install, refer to Figure 12, Sheet 8, Detail Q, AFTER :

1 Spacer NSA5527-03-02D Item (31) Retained

1 Clamp NSA935807C16 Item (111) Retained

1 Washer NSA935808-01 Item (112) Retained

1 Spacer NSA5527-03-05D Item (114) Retained

1 Clamp NSA935807C09 Item (117) Retained

1 Screw NAS1096-3-25 Item (119) Retained

2 Clamp NSA935807C09 Item 117

m Install, refer to Figure 12, Sheet 7, Detail N, AFTER :

1 Spacer NSA5527-03-01D Item (30) Retained

1 Spacer NSA5527-03-02D Item (31) Retained

1 Clamp NSA935807C16 Item (111) Retained

1 Washer NSA935808-01 Item (112) Retained

1 Spacer NSA5527-03-05D Item (114) Retained

1 Clamp NSA935807C09 Item (117) Retained

1 Screw NAS1096-3-33 Item (118) Retained

2 Clamp NSA935807C09 Item 117

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

REVISION No. : 05 - Aug 03/10 Page : 62

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

n Install, refer to Figure 12, Sheet 6, Detail K, AFTER :

1 Spacer NSA5527-03-01D Item (30) Retained

1 Spacer NSA5527-03-02D Item (31) Retained

1 Clamp NSA935807C16 Item (111) Retained

1 Spacer NSA5527-03-05D Item (114) Retained

1 Washer NSA1149D0332K Item (115) Retained

1 Clamp NSA935807C09 Item (117) Retained

1 Screw NAS1096-3-33 Item (118) Retained

2 Clamp NSA935807C09 Item 117

o Install, refer to Figure 12, Sheet 5, Detail H, AFTER :

2 Spacer NSA5527-03-01D Item (30) Retained

2 Spacer NSA5527-03-02D Item (31) Retained

2 Clamp NSA935807C16 Item (111) Retained

2 Spacer NSA5527-03-05D Item (114) Retained

2 Washer NSA1149D0332K Item (115) Retained

2 Clamp NSA935807C09 Item (117) Retained

2 Screw NAS1096-3-33 Item (118) Retained

2 Clamp NSA935807C09 Item 117

p Install, refer to Figure 12, Sheet 4, Detail F, AFTER :

2 Spacer NSA5527-03-01D Item (30) Retained

1 Spacer NSA5527-03-02D Item (31) Retained

1 Clamp NSA935807C10 Item (110) Retained

1 Clamp NSA935807C16 Item (111) Retained

1 Washer NSA935808-01 Item (112) Retained

1 Clamp NSA935807C09 Item (117) Retained

1 Screw NAS1096-3-33 Item (118) Retained

2 Clamp NSA935807C09 Item 117

q Install, refer to Figure 12, Sheet 3, Detail D, AFTER :

2 Spacer NSA5527-03-01D Item 30

1 Clamp NSA935807C16 Item (111) Retained

1 Washer NSA935808-01 Item (112) Retained

1 Screw NAS1096-3-23 Item (113) Retained

1 Washer NSA1149D0332K Item (115) Retained

1 Nut NAS1291C3M Item (116) Retained

1 Clamp NSA935807C09 Item (117) Retained

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, Figure 15 and refer to Figure 12, Sheet 2

and Sheet 3 with :

2 Sleeve ABS0596S004 Item 1

cut the sleeve to the required length and install with :

20 Tie NSA935401-03 Item 149

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

REVISION No. : 05 - Aug 03/10 Page : 63

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A310

SERVICE BULLETIN

20 Tie NSA935401-04 Item 150

s Install the identification placards, refer to Figure 12, Sheet 2,

1 Placard set B9299071900200 Item 125

(c) Test

1 Do a continuity test of disconnected wires, refer to ESPM 20-52-21.

2 Do an operational test of the cadensicon sensor, refer to AMM 28-42-44, Page

block 401.

3 Do the operational test, refer to AMM 27-84-00, Page block 501.

4 Do the operational test of the wing ice protection, refer to AMM 30-11-00,

Page block 501.

5 Do the bite test, refer to AMM 36-11-00, Page block 501.

(d) Close up

1 Make sure that the work areas are clean and clear of tools and other items

of equipment.

2 Fully retract the slats, refer to AMM 27-80-00, Page block 301.

3 Close the access panels 612AT, 612KB, 612JB, 623AB, 623BB and 623EB.

4 Remove the access platform.

(6) Config. 02 ADDITIONAL WORK 1

ADDITIONAL WORK 1 is required by this revision for aircraft modified by issue 00 or

Revision 01.

(a) Preparation

1 Make sure that the aircraft is electrically grounded, refer to AMM 24-00-00,

Page block 301.

2 Fully extend the slats, refer to AMM 27-80-00, Page block 301.

3 De-energize the aircraft electrical circuits, refer to AMM 24-41-00, Page block

301.

4 Put the access platform(s) in position.

5 Open the access panels 612AT, 612KB, 612JB, 623AB, 623BB and 623EB.

6 Remove the bleed air duct if necessary, refer to AMM 36-11-00, Page block 401.

(b) Modification

Refer to Kit 282148D03R01

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

REVISION No. : 05 - Aug 03/10 Page : 64

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A310

SERVICE BULLETIN

Refer to Figure 11

Refer to Figure 13

Refer to Figure 15

NOTE(4) Adapt the number of cable ties to the required quantity.

1 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 Figure 11

a At one position, remove these items from the bracket rib 11 and rib 12 and

cable bundle 2S/636VB, as shown in Figure 11, Sheet 1 and Sheet 3

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 Install protection sleeve, as shown in Figure 11, Sheet 1 thru Sheet 3

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 NSA935401-04 Item 150

c Install, as shown in Figure 11, Sheet 1 and Sheet 3 Details A and E :

2 Clamp MS21919WCH4 Item (22) Retained

1 Clamp MS21919WCH3 Item (23) Retained

1 Spacer NSA5527-03-01D Item (30) Retained

1 Spacer NSA5527-03-02D Item (31) Retained

1 Washer NSA935808-01 Item (112) Retained

1 Clamp NSA935807-06 Item (122) Retained

1 Clamp MS21919WCH9 Item 10

1 Spacer NSA5527-03-02D Item 31

1 Screw NAS1096-3-40 Item 121

2 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 Figure 13

Refer to Figure 15

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

REVISION No. : 05 - Aug 03/10 Page : 65

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A310

SERVICE BULLETIN

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.

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, Figure 15.

b Remove, refer to Figure 13, Sheet 3, Detail C, 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 Figure 13, Sheet 4, Detail E, 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 Figure 13, Sheet 5, Detail G, 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 Figure 13, Sheet 6, Detail J, 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 Figure 13, Sheet 7, Detail L, 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 Figure 13, Sheet 8, Detail P, BEFORE :

1 Spacer NSA5527-03-02D Item (31) Retain

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

REVISION No. : 05 - Aug 03/10 Page : 66

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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) Discard

1 Spacer NSA5527-03-05D Item (114) Retain

h Remove the identification placards from the cable harnesses near the

receptacles 40VC and 5006VC as shown Figure 13, Sheet 2, Detail A

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, Figure 15 :

1 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,

Figure 15. Use the contact pins if required :

7 Pin NSA938184PV1601 Item 126

l Install, refer to Figure 13, Sheet 8, Detail Q, AFTER :

1 Spacer NSA5527-03-02D Item (31) Retained

1 Spacer NSA5527-03-02D Item 31

2 Clamp NSA935807C16 Item (111) Retained

1 Washer NSA935808-01 Item (112) Retained

1 Spacer NSA5527-03-05D Item (114) Retained

1 Clamp NSA935807C09 Item 117

1 Screw NAS1801-3-31 Item 123

1 Spacer NSA5527-03-07D Item 131

m Install, refer to Figure 13, Sheet 7, Detail N, AFTER :

1 Spacer NSA5527-03-02D Item (31) Retained

2 Clamp NSA935807C16 Item (111) Retained

1 Washer NSA935808-01 Item (112) Retained

1 Spacer NSA5527-03-05D Item (114) Retained

1 Clamp NSA935807C09 Item 117

1 Screw NAS1801-3-31 Item 123

1 Spacer NSA5527-03-08D Item 130

n Install, refer to Figure 13, Sheet 6, Detail K, AFTER :

2 Spacer NSA5527-03-02D Item (31) Retained

2 Clamp NSA935807C16 Item (111) Retained

1 Washer NSA935808-01 Item (112) Retained

1 Clamp NSA5516-04NV Item (120) Retained

1 Clamp NSA935807C09 Item 117

1 Screw NAS1801-3-31 Item 123

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

REVISION No. : 05 - Aug 03/10 Page : 67

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A310

SERVICE BULLETIN

o Install, refer to Figure 13, Sheet 5, Detail H, AFTER :

2 Spacer NSA5527-03-02D Item (31) Retained

4 Clamp NSA935807C16 Item (111) Retained

2 Washer NSA935808-01 Item (112) Retained

2 Screw NAS1096-3-23 Item (113) Retained

2 Spacer NSA5527-03-05D Item (114) Retained

2 Clamp NSA935807C09 Item 117

p Install, refer to Figure 13, Sheet 4, Detail F, AFTER :

1 Spacer NSA5527-03-02D Item (31) Retained

2 Clamp NSA935807C16 Item (111) Retained

1 Washer NSA935808-01 Item (112) Retained

1 Screw NAS1096-3-23 Item (113) Retained

1 Spacer NSA5527-03-05D Item (114) Retained

1 Clamp NSA935807C09 Item 117

q Install, refer to Figure 13, Sheet 3, Detail D, AFTER :

1 Spacer NSA5527-03-02D Item (31) Retained

2 Clamp NSA935807C16 Item (111) Retained

1 Washer NSA935808-01 Item (112) Retained

1 Screw NAS1096-3-23 Item (113) Retained

1 Spacer NSA5527-03-05D Item (114) Retained

1 Nut NAS1291C3M Item (116) Retained

1 Washer AN960KD10l Item (124) Retained

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, Figure 15 with :

3 Sleeve ABS0596S004 Item 1

and

20 Tie NSA935401-03 Item 149

20 Tie NSA935401-04 Item 150

s Install the identification placards, refer to Figure 13, Sheet 2,

1 Equipment B9299071900600 Item 132

(c) Test

1 Do a continuity test of disconnected wires, refer to ESPM 20-52-21.

2 Do an operational test of the cadensicon sensor, refer to AMM 28-42-44, Page

block 401.

3 Do the operational test, refer to AMM 27-84-00, Page block 501.

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

REVISION No. : 05 - Aug 03/10 Page : 68

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A310

SERVICE BULLETIN

4 Do the operational test of the wing ice protection, refer to AMM 30-11-00,

Page block 501.

5 Do the bite test, refer to AMM 36-11-00, Page block 501.

(d) Close up

1 Make sure that the work areas are clean and clear of tools and other items

of equipment.

2 Fully retract the slats, refer to AMM 27-80-00, Page block 301.

3 Close the access panels 612AT, 612KB, 612JB, 623AB, 623BB and 623EB.

4 Remove the access platform.

(7) Config. 01 thru Config. 02 ADDITIONAL WORK 2

ADDITIONAL WORK 2 is required by this revision for aircraft modified by issue 00 thru

Revision 02.

(a) Preparation

1 Make sure that the aircraft is electrically grounded (Refer to AMM 24-00-00,

Page block 301).

2 De-energize the aircraft electrical circuits (Refer to AMM 24-41-00, Page block

301).

3 Put access platforms in position.

4 Remove access panel 612AT and/or 623AB (RH wing) (Refer to AMM 06-41-57,

Page block 001).

(b) Modification

Refer to Kit 282148B01R00

Refer to Figure 4

1 Remove from the rear sub spar at rib 8 and rib 9, RH wing the items that follow:

2 Rivet NSA54213510DCA Item (2) Discard

1 Bracket A5724630400000 Item (1) Discard

2 Clean the mating surfaces use Lint-Free Cotton Cloth (Mat. No. 19-003) made

moist with Solvent General Purpose (Mat. No. 11-026).

3 Get the items that follow from Kit 282148B01R00:

1 Bracket A5725068600000 Item 1

2 Rivet, Blind ASNA0078A502 Item 2

4 Copy drill the two holes from the old bracket, Item (1) to the new bracket, Item 1

at the location given (Refer to Figure 4).

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

REVISION No. : 05 - Aug 03/10 Page : 69

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A310

SERVICE BULLETIN

5 Put the bracket, Item 1 in position on the rear sub spar on the RH wing between

rib 8 and rib 9.

6 Drill two holes through the bracket, Item 1 to a dimension of between 3.965mm

(0.156in) and 4.066mm (0.160in) to match the holes in the rear sub spar.

7 Use Solvent General Purpose (Mat. No. 11-026) and wet install on the RH wing

between rib 8 and rib 9 on the rear sub spar the bracket, Item 1 with the two

rivets, Item 2.

(c) Test

None

(d) Close up

1 Make sure that the work areas are clean and clear of tools and other items

of equipment.

2 Install access panel 612AT and/or 623AB (RH wing) (Refer to AMM 06-41-57,

Page block 001).

C. TEST

(1) Config. 01 thru Config. 04

(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.

D. CLOSE UP

(1) Config. 01 thru Config. 04

(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) On the RH-wing, install these access panels, refer to AMM 06-41-57, Page block 001:

- 612AB, 612AT, 612BB, 612CB, 612DB and 613LR.

- 612HB, 612JB and 612KB.

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

REVISION No. : 05 - Aug 03/10 Page : 70

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A310

SERVICE BULLETIN

- 623AB, 623BB, 623CB, 623DB, 623EB, 623FB and 623GB.

(d) In the FWD cargo compartment, install the sidewall panel 132QW, refer to AMM

06-41-53, Page block 001and AMM 25-54-10, Page block 201.

(e) In the FWD 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.

(f) Close the FWD cargo-compartment door 811, refer to AMM 52-30-00, Page

block 001.

(g) Remove the access platform(s).

(h) Put the aircraft and the systems in a normal operating configuration.

E. DOCUMENTATION

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. : 05 - Aug 03/10 Page : 71

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A310

SERVICE BULLETIN

Figure 1, Sheet 1

Config. 01 thru 04: Installation of Cable Sleeves in the RH Electronics Rack 90VU (Kit A01)

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

REVISION No. : 05 - Aug 03/10 Page : 72

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A310

SERVICE BULLETIN

Figure 1, Sheet 2

Config. 01 thru 04: Installation of Cable Sleeves in the RH Electronics Rack 90VU (Kit A01)

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

REVISION No. : 05 - Aug 03/10 Page : 73

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A310

SERVICE BULLETIN

Figure 2, Sheet 1

Config. 01 thru 04: Installation of Cable Sleeves in the FWD Cargo Compartment (Kit A01)

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

REVISION No. : 05 - Aug 03/10 Page : 74

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A310

SERVICE BULLETIN

Figure 3, Sheet 1

Config. 01 thru 04: Installation of Cable Sleeves in the RH Forward Wing Root and Krueger Flap (Kit A01)

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

REVISION No. : 05 - Aug 03/10 Page : 75

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A310

SERVICE BULLETIN

Figure 3, Sheet 2

Config. 01 thru 04: Installation of Cable Sleeves in the RH Forward Wing Root and Krueger Flap (Kit A01)

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

REVISION No. : 05 - Aug 03/10 Page : 76

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A310

SERVICE BULLETIN

Figure 4, Sheet 1

Config. 01 thru 04: Location of Bracket between Rib 8 and Rib 9 on the Rear Sub Spar (RH Wing) (Kit

B01), and ADDITIONAL WORK 2

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

REVISION No. : 05 - Aug 03/10 Page : 77

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A310

SERVICE BULLETIN

Figure 5, Sheet 1

Config. 01 thru 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. : 05 - Aug 03/10 Page : 78

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A310

SERVICE BULLETIN

Figure 5, Sheet 2

Config. 01 thru 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. : 05 - Aug 03/10 Page : 79

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A310

SERVICE BULLETIN

Figure 5, Sheet 3

Config. 01 thru 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. : 05 - Aug 03/10 Page : 80

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A310

SERVICE BULLETIN

Figure 5, Sheet 4

Config. 01 thru 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. : 05 - Aug 03/10 Page : 81

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A310

SERVICE BULLETIN

Figure 5, Sheet 5

Config. 01 thru 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. : 05 - Aug 03/10 Page : 82

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A310

SERVICE BULLETIN

Figure 5, Sheet 6

Config. 01 thru 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. : 05 - Aug 03/10 Page : 83

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A310

SERVICE BULLETIN

Figure 5, Sheet 7

Config. 01 thru 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. : 05 - Aug 03/10 Page : 84

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A310

SERVICE BULLETIN

Figure 5, Sheet 8

Config. 01 thru 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. : 05 - Aug 03/10 Page : 85

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A310

SERVICE BULLETIN

Figure 6, Sheet 1

Config. 01 thru 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. : 05 - Aug 03/10 Page : 86

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A310

SERVICE BULLETIN

Figure 6, Sheet 2

Config. 01 thru 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. : 05 - Aug 03/10 Page : 87

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A310

SERVICE BULLETIN

Figure 6, Sheet 3

Config. 01 thru 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. : 05 - Aug 03/10 Page : 88

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A310

SERVICE BULLETIN

Figure 6, Sheet 4

Config. 01 thru 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. : 05 - Aug 03/10 Page : 89

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A310

SERVICE BULLETIN

Figure 6, Sheet 5

Config. 01 thru 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. : 05 - Aug 03/10 Page : 90

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A310

SERVICE BULLETIN

Figure 6, Sheet 6

Config. 01 thru 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. : 05 - Aug 03/10 Page : 91

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

Figure 6, Sheet 7

Config. 01 thru 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. : 05 - Aug 03/10 Page : 92

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

Figure 6, Sheet 8

Config. 01 thru 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. : 05 - Aug 03/10 Page : 93

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

Figure 6, Sheet 9

Config. 01 thru 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. : 05 - Aug 03/10 Page : 94

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

Figure 6, Sheet 10

Config. 01 thru 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. : 05 - Aug 03/10 Page : 95

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

Figure 7, Sheet 1

Config. 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. : 05 - Aug 03/10 Page : 96

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

Figure 7, Sheet 2

Config. 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. : 05 - Aug 03/10 Page : 97

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

Figure 7, Sheet 3

Config. 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. : 05 - Aug 03/10 Page : 98

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

Figure 7, Sheet 4

Config. 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. : 05 - Aug 03/10 Page : 99

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

Figure 7, Sheet 5

Config. 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. : 05 - Aug 03/10 Page : 100

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

Figure 7, Sheet 6

Config. 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. : 05 - Aug 03/10 Page : 101

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

Figure 7, Sheet 7

Config. 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. : 05 - Aug 03/10 Page : 102

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

Figure 7, Sheet 8

Config. 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. : 05 - Aug 03/10 Page : 103

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

Figure 8, Sheet 1

Config. 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. : 05 - Aug 03/10 Page : 104

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

Figure 8, Sheet 2

Config. 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. : 05 - Aug 03/10 Page : 105

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

Figure 8, Sheet 3

Config. 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. : 05 - Aug 03/10 Page : 106

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

Figure 8, Sheet 4

Config. 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. : 05 - Aug 03/10 Page : 107

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

Figure 8, Sheet 5

Config. 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. : 05 - Aug 03/10 Page : 108

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

Figure 8, Sheet 6

Config. 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. : 05 - Aug 03/10 Page : 109

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

Figure 8, Sheet 7

Config. 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. : 05 - Aug 03/10 Page : 110

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

Figure 8, Sheet 8

Config. 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. : 05 - Aug 03/10 Page : 111

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

Figure 9, Sheet 1

Config. 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. : 05 - Aug 03/10 Page : 112

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

Figure 9, Sheet 2

Config. 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. : 05 - Aug 03/10 Page : 113

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

Figure 9, Sheet 3

Config. 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. : 05 - Aug 03/10 Page : 114

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

Figure 9, Sheet 4

Config. 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. : 05 - Aug 03/10 Page : 115

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

Figure 9, Sheet 5

Config. 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. : 05 - Aug 03/10 Page : 116

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

Figure 9, Sheet 6

Config. 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. : 05 - Aug 03/10 Page : 117

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

Figure 9, Sheet 7

Config. 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. : 05 - Aug 03/10 Page : 118

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

Figure 9, Sheet 8

Config. 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. : 05 - Aug 03/10 Page : 119

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

Figure 9, Sheet 9

Config. 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. : 05 - Aug 03/10 Page : 120

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

Figure 10, Sheet 1

Config. 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. : 05 - Aug 03/10 Page : 121

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

Figure 10, Sheet 2

Config. 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. : 05 - Aug 03/10 Page : 122

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

Figure 10, Sheet 3

Config. 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. : 05 - Aug 03/10 Page : 123

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

Figure 10, Sheet 4

Config. 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. : 05 - Aug 03/10 Page : 124

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

Figure 10, Sheet 5

Config. 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. : 05 - Aug 03/10 Page : 125

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

Figure 10, Sheet 6

Config. 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. : 05 - Aug 03/10 Page : 126

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

Figure 10, Sheet 7

Config. 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. : 05 - Aug 03/10 Page : 127

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

Figure 10, Sheet 8

Config. 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. : 05 - Aug 03/10 Page : 128

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

Figure 10, Sheet 9

Config. 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. : 05 - Aug 03/10 Page : 129

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

Figure 11, Sheet 1

Config. 01 thru 02: ADDITIONAL WORK 1 : 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. : 05 - Aug 03/10 Page : 130

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

Figure 11, Sheet 2

Config. 01 thru 02: ADDITIONAL WORK 1 : 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. : 05 - Aug 03/10 Page : 131

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

Figure 11, Sheet 3

Config. 01 thru 02: ADDITIONAL WORK 1 : 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. : 05 - Aug 03/10 Page : 132

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

Figure 12, Sheet 1

Config. 01: ADDITIONAL WORK 1 : 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. : 05 - Aug 03/10 Page : 133

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

Figure 12, Sheet 2

Config. 01: ADDITIONAL WORK 1 : 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. : 05 - Aug 03/10 Page : 134

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

Figure 12, Sheet 3

Config. 01: ADDITIONAL WORK 1 : 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. : 05 - Aug 03/10 Page : 135

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

Figure 12, Sheet 4

Config. 01: ADDITIONAL WORK 1 : 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. : 05 - Aug 03/10 Page : 136

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

Figure 12, Sheet 5

Config. 01: ADDITIONAL WORK 1 : 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. : 05 - Aug 03/10 Page : 137

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

Figure 12, Sheet 6

Config. 01: ADDITIONAL WORK 1 : 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. : 05 - Aug 03/10 Page : 138

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

Figure 12, Sheet 7

Config. 01: ADDITIONAL WORK 1 : 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. : 05 - Aug 03/10 Page : 139

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

Figure 12, Sheet 8

Config. 01: ADDITIONAL WORK 1 : 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. : 05 - Aug 03/10 Page : 140

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

Figure 13, Sheet 1

Config. 02: ADDITIONAL WORK 1 : 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. : 05 - Aug 03/10 Page : 141

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

Figure 13, Sheet 2

Config. 02: ADDITIONAL WORK 1 : 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. : 05 - Aug 03/10 Page : 142

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

Figure 13, Sheet 3

Config. 02: ADDITIONAL WORK 1 : 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. : 05 - Aug 03/10 Page : 143

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

Figure 13, Sheet 4

Config. 02: ADDITIONAL WORK 1 : 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. : 05 - Aug 03/10 Page : 144

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

Figure 13, Sheet 5

Config. 02: ADDITIONAL WORK 1 : 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. : 05 - Aug 03/10 Page : 145

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

Figure 13, Sheet 6

Config. 02: ADDITIONAL WORK 1 : 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. : 05 - Aug 03/10 Page : 146

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

Figure 13, Sheet 7

Config. 02: ADDITIONAL WORK 1 : 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. : 05 - Aug 03/10 Page : 147

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

Figure 13, Sheet 8

Config. 02: ADDITIONAL WORK 1 : 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. : 05 - Aug 03/10 Page : 148

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

Figure 14, Sheet 1

Config. 01 and 03: Hook-up Chart 1

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

REVISION No. : 05 - Aug 03/10 Page : 149

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

Figure 15, Sheet 1

Config. 01 thru 04: Hook-up Chart 2

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

REVISION No. : 05 - Aug 03/10 Page : 150

Printed in France © AIRBUS 2008 All rights reserved
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 embodiement:

.............................................................................................................................................................................

.............................................................................................................................................................................

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 : Advance data................................................................................... YES/NO

Or : Intermediate/Temporary 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: SEDCC1 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. : 05 - Aug 03/10 Page : 1 of 1

Printed in France © AIRBUS 2008 All rights reserved
A310

SERVICE BULLETIN

REPORTING QUALITY

TITLE : ELECTRIC/ELECTRONIC COMMON INSTALLATION - WING - IMPROVE THE 2S-ROUTE IN

THE RH-WING

MODIFICATION No. : 12427D21883, 12435S22116, 13478D23233

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 futher 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 4 3 2 1

-Quality rating of the Accomplishment Instructions 4 3 2 1

-Quality rating of the Illustrations 4 3 2 1

-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 X Mod/Inspection

X Manpower Operator Supplied 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: SEMB 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. : 05 - Aug 03/10 Page : 1 of 1

Printed in France © AIRBUS 2008 All rights reserved