# 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** M A N DA T

O RY M A N DA T

O RY M A N DA TO RY M A N D A

TO RY **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 A D D I T I O N A L WO R K 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. R E A S O N Revision No. 05 is issued to : - remove MSN 0349 from the effectivity and - add MSN’s 0254, 0273, 0397 and 0400 to the effectivity. C H A N G E S SUMMARY : DATE : Jan 23/02 SERVICE BULLETIN No. : A310-28-2148

REVISION No. : 05 - Aug 03/10 Page : 1 of 2 Printed in France © AIRBUS 2008 All rights reserved

# 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. F I L I N G I N S T R U CT I O N S 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. H I S T O R Y O F P R E V I O U S R E V I S I O N S 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 M A N DA T

O RY M A N DA T

O RY M A N DA TO RY M A N DA TO RY **ATA SYSTEM : 28 TITLE : ELECTRIC/ELECTRONIC COMMON INSTALLATION - WING - IMPROVE THE 2S-ROUTE IN**  **THE RH-WING MODIFICATION No. :**  12427D21883, 12435S22116, 13478D23233 R E A S O N/D E S C R I PT I O N/O P E RA T I O N A L C O N S E Q U E N C E S 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 Printed in France © AIRBUS 2008 All rights reserved

# 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. **E F**  **F E**  **C T**  **I V**  **I T** **Y** 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 C O N C U R R E N T R E Q U I R E M E N T S None R E F E R E N C E S/R E P E R C U S S I O N S TFU : None OEB : None AOT : None SIL : None LIFE LIMIT : None LINE MAINTENANCE AFFECTED : No OTHERS : None N A T U R E O F T H E WO R K 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 Printed in France © AIRBUS 2008 All rights reserved

# A310 SERVICE BULLETIN SUMMARY

OBRM : NO M A N P OW E R 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**  M A T E R I A L I N FO R M A T I O N AIRCRAFT DATA Config. 01 thru Config. 04 Sleeves, clamps, brackets, spacer and related fasteners. A P P E N D I C E S None

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

REVISION No. : 05 - Aug 03/10 Page : 3 Printed in France © AIRBUS 2008 All rights reserved

# A310 SERVICE BULLETIN SUMMARY

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

REVISION No. : 05 - Aug 03/10 Page : 4 Printed in France © AIRBUS 2008 All rights reserved

# A310 SERVICE BULLETIN SUMMARY

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

REVISION No. : 05 - Aug 03/10 Page : 5 Printed in France © AIRBUS 2008 All rights reserved

# A310 SERVICE BULLETIN SUMMARY

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

REVISION No. : 05 - Aug 03/10 Page : 6 Printed in France © AIRBUS 2008 All rights reserved

# A310 SERVICE BULLETIN SUMMARY

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

REVISION No. : 05 - Aug 03/10 Page : 7 Printed in France © AIRBUS 2008 All rights reserved

# 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** M A N DA T

O RY M A N DA T

O RY M A N DA TO RY M A N DA TO RY **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. P L** **A N**  **N I**  **N G**  **I N**  **F O**  **R M**  **A T**  **I O**  **N A. E**  **F F**  **E C** **T I**  **V I**  **T Y**  (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

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

REVISION No. : 05 - Aug 03/10 Page : 1 of 150 Printed in France © AIRBUS 2008 All rights reserved

# 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

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

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

REVISION No. : 05 - Aug 03/10 Page : 3 Printed in France © AIRBUS 2008 All rights reserved

# 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 Printed in France © AIRBUS 2008 All rights reserved

# A310 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 Printed in France © AIRBUS 2008 All rights reserved

# A310 SERVICE BULLETIN

(3) Spares None **B. C O**  **N C**  **U R**  **R E**  **N T**  **R E**  **Q U**  **I R**  **E M**  **E N**  **T S**  None **C. R E** **A S**  **O N**  (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. D E**  **S C**  **R I**  **P T**  **I O**  **N** 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

REVISION No. : 05 - Aug 03/10 Page : 6 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. (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 Printed in France © AIRBUS 2008 All rights reserved

# A310 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

REVISION No. : 05 - Aug 03/10 Page : 8 Printed in France © AIRBUS 2008 All rights reserved

# A310 SERVICE BULLETIN

**E. C O**  **M P**  **L I**  **A N**  **C E**  (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. A P**  **P R**  **O V**  **A L**  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. M A**  **N P**  **O W**  **E R**  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**  DATE : Jan 23/02 SERVICE BULLETIN No. : A310-28-2148

REVISION No. : 05 - Aug 03/10 Page : 9 Printed in France © AIRBUS 2008 All rights reserved

# A310 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. W E**  **I G**  **H T**  **A N**  **D B** **A L** **A N**  **C E**  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

REVISION No. : 05 - Aug 03/10 Page : 10 Printed in France © AIRBUS 2008 All rights reserved

# A310 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. E L**  **E C** **T R**  **I C** **A L**  **L O** **A D**  **D A** 

**T**

**A** Not changed **J. R E**  **F E**  **R E**  **N C**  **E S**  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. P U**  **B L**  **I C** **A T**  **I O**  **N S**  **A F**  **F E**  **C T**  **E D**  Aircraft Maintenance Manual (AMM) : 28-42-07 Illustrated Parts Catalog (IPC) : 24-92-03 **L. I N**  **T E**  **R C**  **H A**  **N G**  **E A**  **B I**  **L I**  **T Y**  **/ M**  **I X** **A B**  **I L**  **I T** **Y** None

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

REVISION No. : 05 - Aug 03/10 Page : 11 Printed in France © AIRBUS 2008 All rights reserved

# 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 Printed in France © AIRBUS 2008 All rights reserved

# A310 SERVICE BULLETIN

**2. M A**  **T E**  **R I**  **A L**  **I N**  **F O**  **R M**  **A T**  **I O**  **N A. M**  **A T**  **E R**  **I A**  **L -**  **P R**  **I C**  **E A**  **N D**  **A V** 

**A I**  **L A**  **B I**  **L I** **T Y**  (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 Printed in France © AIRBUS 2008 All rights reserved

# A310 SERVICE BULLETIN

The sales terms (costs and availability) are estimated in relation to the economic conditions at the issue date of the Service Bulletin. Kit 282148D02R01 Cost : 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 Printed in France © AIRBUS 2008 All rights reserved

# A310 SERVICE BULLETIN

The sales terms (costs and availability) are estimated in relation to the economic conditions at the issue date of the Service Bulletin. **B. I N**  **D U**  **S T**  **R Y**  **S U**  **P P**  **O R** **T I**  **N F** **O R**  **M A**  **T I**  **O N**  Airbus will not provide industry support for accomplishment of this Service Bulletin. **C. L I**  **S T**  **O F**  **C O**  **M P**  **O N**  **E N**  **T S**  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 Printed in France © AIRBUS 2008 All rights reserved

# 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 Printed in France © AIRBUS 2008 All rights reserved

# 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. L I**  **S T**  **O F**  **M A**  **T E**  **R I**  **A L** **S -**  **O P**  **E R**  **A T** **O R**  **S U**  **P P**  **L I**  **E D**  (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

REVISION No. : 05 - Aug 03/10 Page : 17 Printed in France © AIRBUS 2008 All rights reserved

# A310 SERVICE BULLETIN

**E. P A**  **R T** **S T** **O B**  **E R**  **E -**  **I D**  **E N**  **T I**  **F I**  **E D**  **B Y**  **T H**  **E O**  **P E**  **R A**  **T O**  **R** None **F. T O**  **O L**  **I N**  **G -**  **P R**  **I C**  **E A**  **N D**  **A V** 

**A I**  **L A**  **B I**  **L I** **T Y**  None **G. S P**  **E C**  **I A**  **L T** **O O**  **L S**  None

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

REVISION No. : 05 - Aug 03/10 Page : 18 Printed in France © AIRBUS 2008 All rights reserved

# A310 SERVICE BULLETIN

**3. A C**  **C O**  **M P**  **L I**  **S H**  **M E**  **N T**  **I N**  **S T**  **R U**  **C T**  **I O**  **N S**  **A. G E**  **N E**  **R A**  **L** 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

REVISION No. : 05 - Aug 03/10 Page : 19 Printed in France © AIRBUS 2008 All rights reserved

# 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. M O**  **D I**  **F I**  **C A**  **T I**  **O N**  (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 sle eve, 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

REVISION No. : 05 - Aug 03/10 Page : 20 Printed in France © AIRBUS 2008 All rights reserved

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

REVISION No. : 05 - Aug 03/10 Page : 21 Printed in France © AIRBUS 2008 All rights reserved

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

REVISION No. : 05 - Aug 03/10 Page : 22 Printed in France © AIRBUS 2008 All rights reserved

# A310 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 sle eve, 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 DATE : Jan 23/02 SERVICE BULLETIN No. : A310-28-2148

REVISION No. : 05 - Aug 03/10 Page : 23 Printed in France © AIRBUS 2008 All rights reserved

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

REVISION No. : 05 - Aug 03/10 Page : 24 Printed in France © AIRBUS 2008 All rights reserved

# A310 SERVICE BULLETIN

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

REVISION No. : 05 - Aug 03/10 Page : 25 Printed in France © AIRBUS 2008 All rights reserved

# A310 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 1 0 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 1 1 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 1 2 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 1 3 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 1 4 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 Printed in France © AIRBUS 2008 All rights reserved

# 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 1 5 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 1 6 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 1 7 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 1 8 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 1 9 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 Printed in France © AIRBUS 2008 All rights reserved

# 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 Printed in France © AIRBUS 2008 All rights reserved

# 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 Printed in France © AIRBUS 2008 All rights reserved

# 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 1 0 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 1 1 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 1 2 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 1 3 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 Printed in France © AIRBUS 2008 All rights reserved

# 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 sle eve, 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 Printed in France © AIRBUS 2008 All rights reserved

# 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 Printed in France © AIRBUS 2008 All rights reserved

# 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 sle eve, 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 Printed in France © AIRBUS 2008 All rights reserved

# 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 Printed in France © AIRBUS 2008 All rights reserved

# 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 Printed in France © AIRBUS 2008 All rights reserved

# 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 sle eve. 1 0 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 1 1 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 1 2 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 1 3 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 1 4 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 Printed in France © AIRBUS 2008 All rights reserved

# A310 SERVICE BULLETIN

1 Clamp NSA935807C09 Item 117 2 Screw NAS1801-3-31 Item 123 1 5 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 1 6 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 1 7 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 1 8 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 1 9 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 1 0 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 1 1 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 1 2 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 1 3 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 sle eve, 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 sle eve, 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 1 0 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 1 1 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 1 2 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 1 3 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 1 4 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 1 5 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

1 6 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 1 7 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 1 0 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 1 1 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 1 2 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

1 3 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 sle eve, 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

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

REVISION No. : 05 - Aug 03/10 Page : 50 Printed in France © AIRBUS 2008 All rights reserved

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

REVISION No. : 05 - Aug 03/10 Page : 51 Printed in France © AIRBUS 2008 All rights reserved

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

REVISION No. : 05 - Aug 03/10 Page : 52 Printed in France © AIRBUS 2008 All rights reserved

# A310 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 sle eve, 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 DATE : Jan 23/02 SERVICE BULLETIN No. : A310-28-2148

REVISION No. : 05 - Aug 03/10 Page : 53 Printed in France © AIRBUS 2008 All rights reserved

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

REVISION No. : 05 - Aug 03/10 Page : 54 Printed in France © AIRBUS 2008 All rights reserved

# A310 SERVICE BULLETIN

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 1 0 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 1 1 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 1 2 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 1 3 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 1 4 Install, refer to Figure 10, Sheet 4, Detail F, AFTER : DATE : Jan 23/02 SERVICE BULLETIN No. : A310-28-2148

REVISION No. : 05 - Aug 03/10 Page : 55 Printed in France © AIRBUS 2008 All rights reserved

# A310 SERVICE BULLETIN

1 Washer NSA935808-01 Item (112) Retained 1 Screw NAS1096-3-23 Item (113) Retained 1 Clamp NSA935807C09 Item 117 1 5 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 1 6 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 DATE : Jan 23/02 SERVICE BULLETIN No. : A310-28-2148

REVISION No. : 05 - Aug 03/10 Page : 56 Printed in France © AIRBUS 2008 All rights reserved

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

REVISION No. : 05 - Aug 03/10 Page : 57 Printed in France © AIRBUS 2008 All rights reserved

# A310 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 1 0 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 1 1 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 1 2 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

REVISION No. : 05 - Aug 03/10 Page : 58 Printed in France © AIRBUS 2008 All rights reserved

# A310 SERVICE BULLETIN

1 Washer NAS1149D0332K Item (40) Retained 1 Screw NAS1096-3-22 Item (51) Retained 1 Clamp MS21919WCH9 Item 10 1 3 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 DATE : Jan 23/02 SERVICE BULLETIN No. : A310-28-2148

REVISION No. : 05 - Aug 03/10 Page : 59 Printed in France © AIRBUS 2008 All rights reserved

# A310 SERVICE BULLETIN

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 sle eve, 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

REVISION No. : 05 - Aug 03/10 Page : 60 Printed in France © AIRBUS 2008 All rights reserved

# A310 SERVICE BULLETIN

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

REVISION No. : 05 - Aug 03/10 Page : 61 Printed in France © AIRBUS 2008 All rights reserved

# A310 SERVICE BULLETIN

1 Clamp NSA935807C10 Item (110) Discard 1 Clamp NSA935807C16 Item (111) Retain 1 Washer NSA935808-01 Item (112) Retain 1 Spacer NSA5527-03-05D Item (114) Retain 1 Clamp NSA935807C09 Item (117) Retain 1 Screw NAS1096-3-25 Item (119) Retain

h Remove the identification sleeves from the cable harnesses near the receptacles 40VC and 5006VC as shown 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 Printed in France © AIRBUS 2008 All rights reserved

# 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 Printed in France © AIRBUS 2008 All rights reserved

# 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 sle eve, 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 Printed in France © AIRBUS 2008 All rights reserved

# 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 Printed in France © AIRBUS 2008 All rights reserved

# 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 sle eve. 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 Printed in France © AIRBUS 2008 All rights reserved

# 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 Printed in France © AIRBUS 2008 All rights reserved

# 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 Printed in France © AIRBUS 2008 All rights reserved

# 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. T E**  **S T**  (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. C L** **O S**  **E U**  **P** (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 Printed in France © AIRBUS 2008 All rights reserved

# 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. D O**  **C U**  **M E**  **N T**  **A**

**T I**  **O N**  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 Printed in France © AIRBUS 2008 All rights reserved

# 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 Printed in France © AIRBUS 2008 All rights reserved

# 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 Printed in France © AIRBUS 2008 All rights reserved

# 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 Printed in France © AIRBUS 2008 All rights reserved

# 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 Printed in France © AIRBUS 2008 All rights reserved

# 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 Printed in France © AIRBUS 2008 All rights reserved

# 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 Printed in France © AIRBUS 2008 All rights reserved

# 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 Printed in France © AIRBUS 2008 All rights reserved

# 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 Printed in France © AIRBUS 2008 All rights reserved

# 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 Printed in France © AIRBUS 2008 All rights reserved

# 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 Printed in France © AIRBUS 2008 All rights reserved

# 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 Printed in France © AIRBUS 2008 All rights reserved

# 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 Printed in France © AIRBUS 2008 All rights reserved

# 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 Printed in France © AIRBUS 2008 All rights reserved

# 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 Printed in France © AIRBUS 2008 All rights reserved

# 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 Printed in France © AIRBUS 2008 All rights reserved

# 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 Printed in France © AIRBUS 2008 All rights reserved

# 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 Printed in France © AIRBUS 2008 All rights reserved

# 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 Printed in France © AIRBUS 2008 All rights reserved

# 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 Printed in France © AIRBUS 2008 All rights reserved

# 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 P l e as e co m p l ete t h e a p p ro p r i ate i te m (A o r B ) : A - SB W I L L B E 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 H AS B E E N embodied on aircraft: ............................................................................................................

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

............................................................................................................................... .............................................. Operator comments:..............................................................................................................

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

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

............................................................................................................................... .............................................. From Airline: ...................................................................................................................

..................................... Name/Title: ....................................................................................................................

...................................... Signature:..................... Date: ..................................................... I f o p e rat i o n a l d o c u m e n t at i o n i s affe cte d ( s e e Pa rag ra p h 1

. K of t h i s S B ) : 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 I m p o rt a n t I n fo r m at i o n : 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. P l e as e re t u r n t h i s co m p l ete d s h e et 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 C o m m e n ts :

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