# @A330 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 ATA SYSTEM: 25 

### TITLE: EQUIPMENT/FURNISHINGS - PAX COMPARTMENT - MODIFY CDLS WIRING LOOM IN UPPER COCKPIT DOOR PLATE COVER MODIFICATION No.: 51911D44499 This page transmits Revision No.02 of Service Bulletin No.A330-25-3213 ADDITIONAL WORK **CONF ALL Additional work is required by this revision for aircraft modified by any previous issue of this Service Bulletin. AIRBUS recommends the additional work to be accomplished within one year after the issue of this revision. The additional work consists in: - Replace the fasteners of the cover. REASON Revision No. 02 issued to incorporate changes found necessary and carried out during the accomplishment of this Service Bulletin on aircraft with Manufacturer Serial Number (MSN) 0555, 0573 and 0587. An additional work added for aircraft modified by any previous revisions. NOTE : This revision satisfies the requirements of the subsequent Technical Adaptations (TA) issued for the related MSN: TA MSN TA 80105052/013/2016 0555, 0573 and 0587 CHANGES The main changes of this revision are: - Modification of the Kit 253213D02: . 2 washers ASNA0113-56ADL replaced by NSA5379-3C . 1 washer NAS1149CN949R replaced by NSA5379-3C

DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 1 6

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

# @A330 SERVICE BULLETIN REVISION TRANSMITTAL SHEET . 2 bolts NAS1096-3-14 replaced by MS21250-03006 . 1 cable tie NSA935401-03 added - Introduction of the ADDITIONAL WORK, with the Kit COMPD01 and illustration BFAA created, valid for aircraft modified by any previous issue - Update of sentences in TEST paragraphs - Revision of text and layout - Addition of new sentence in ’ACCOMP LISHMENT INSTRUCTIONS’ paragraph. NOTE : Revised text and layout changes of this revision are not identified with revision bars. SUMMARY MODIFICATIONS Minor editorial or document structure change N REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES Minor editorial or document structure change N GENERAL EVALUATION Minor editorial or document structure change N MATERIAL PRICE INFORMATION Minor editorial or document structure change N EFFECTIVITY Minor editorial or document structure change N CONCURRENT REQUIREMENTS Minor editorial or document structure change N REFERENCES / REPERCUSSIONS Minor editorial or document structure change N NATURE OF THE WORK Minor editorial or document structure change N MANPOWER Minor editorial or document structure change N APPENDICES Minor editorial or document structure change N Fig. A-GSAAA Minor editorial or document structure change N Fig. A-GSAAA Sheet 01 Minor editorial or document structure change N PLANNING INFORMATION EFFECTIVITY Minor editorial or document structure change N Configuration definition Minor editorial or document structure change N CONF 001 Minor editorial or document structure change N Material Effectivity Minor editorial or document structure change N Minor editorial or document structure change N CONCURRENT REQUIREMENTS Minor editorial or document structure change N Minor editorial or document structure change N REASON Minor editorial or document structure change N History Minor editorial or document structure change N Objective/Action Minor editorial or document structure change N Advantages Minor editorial or document structure change N Operational/Maintenance Consequences Minor editorial or document structure change N DESCRIPTION Minor editorial or document structure change N COMPLIANCE Minor editorial or document structure change N DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 2 6

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

# @A330 SERVICE BULLETIN REVISION TRANSMITTAL SHEET Classification Minor editorial or document structure change N Accomplishment Timescale Minor editorial or document structure change N APPROVAL Minor editorial or document structure change N Minor editorial or document structure change N MANPOWER Minor editorial or document structure change N Minor editorial or document structure change N WEIGHT AND BALANCE Minor editorial or document structure change N Minor editorial or document structure change N ELECTRICAL LOAD DATA Minor editorial or document structure change N REFERENCES Minor editorial or document structure change N Minor editorial or document structure change N PUBLICATION AFFECTED Minor editorial or document structure change N Minor editorial or document structure change N INTERCHANGEABILITY/MIXABILITY Minor editorial or document structure change N Minor editorial or document structure change N SPARES Minor editorial or document structure change N MATERIAL INFORMATION MATERIAL - PRICE AND AVAILABILITY Minor editorial or document structure change N Procurement Addresses Minor editorial or document structure change N Price and Availability Minor editorial or document structure change N INDUSTRY SUPPORT INFORMATION Minor editorial or document structure change N LIST OF COMPONENTS Minor editorial or document structure change N Kit 253213D02R02 Minor editorial or document structure change N LIST OF MATERIALS - OPERATOR SUPPLIED Minor editorial or document structure change N Consumable Materials Minor editorial or document structure change N Consumable CMLD01 Minor editorial or document structure change N Components Minor editorial or document structure change N Component COMPD01 Minor editorial or document structure change N Equipment Minor editorial or document structure change N PARTS TO BE RE-IDENTIFIED BY OPERATOR Minor editorial or document structure change N Reidentified part set REIDD01 Minor editorial or document structure change N TOOLING Minor editorial or document structure change N ACCOMPLISHMENT INSTRUCTIONS TASK 253213- 831-848-001-Modification Minor editorial or document structure change N Task associated data - 001 Minor editorial or document structure change N Subtask 253213-910-201-001 Minor editorial or document structure change N Subtask 253213-900-202-001 Minor editorial or document structure change N Subtask 253213-941-201-001 Minor editorial or document structure change N Subtask 253213-862-201-001 Minor editorial or document structure change N
DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 3 6

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

# @A330 SERVICE BULLETIN REVISION TRANSMITTAL SHEET Subtask 253213-010-201-001 Minor editorial or document structure change N Subtask 253213-831-203-001 Minor editorial or document structure change N Subtask 253213-420-201-001 Minor editorial or document structure change N Subtask 253213-861-201-001 Minor editorial or document structure change N Subtask 253213-700-209-001 Minor editorial or document structure change N Subtask 253213-942-209-001 Minor editorial or document structure change N TASK 253213- 831-849-001-Modification - Additional Work for Aircraft Modified by Revision No. 01 or any Previous Issue Minor editorial or document structure change N Task associated data - 001 Minor editorial or document structure change N Subtask 253213-910-202-001 Minor editorial or document structure change N Subtask 253213-839-201-001 Minor editorial or document structure change N Subtask 253213-941-202-001 Minor editorial or document structure change N Subtask 253213-831-204-001 Minor editorial or document structure change N Subtask 253213-942-210-001 Minor editorial or document structure change N Fig. A-GBAAA Minor editorial or document structure change N Fig. A-GBAAA Sheet 01 Minor editorial or document structure change N Fig. A-GBAAA Sheet 02 Minor editorial or document structure change N Fig. A-GBAAA Sheet 03 Minor editorial or document structure change N Fig. A-GBAAA Sheet 04 Minor editorial or document structure change N Fig. A-GBAAA Sheet 05 Minor editorial or document structure change N Fig. A-GBBAA Minor editorial or document structure change N Fig. A-GBBAA Sheet 01 Minor editorial or document structure change N Fig. A-GBBAA Sheet 02 Minor editorial or document structure change N Fig. A-GBCAA Minor editorial or document structure change N Fig. A-GBCAA Sheet 01 Minor editorial or document structure change N Fig. A-GBCAA Sheet 02 Minor editorial or document structure change N Fig. A-GBDAA Minor editorial or document structure change N Fig. A-GBDAA Sheet 01 Minor editorial or document structure change N Fig. A-GBDAA Sheet 02 Minor editorial or document structure change N Fig. A-GBEAA Minor editorial or document structure change N Fig. A-GBEAA Sheet 01 Minor editorial or document structure change N Fig. A-GBEAA Sheet 02 Minor editorial or document structure change N Fig. A-GBEAA Sheet 03 Minor editorial or document structure change N Fig. A-GBEAA Sheet 04 Minor editorial or document structure change N Fig. A-GBEAA Sheet 05 Minor editorial or document structure change N Fig. A-GBEAA Sheet 06 Minor editorial or document structure change N Fig. A-GBEAA Sheet 07 Minor editorial or document structure change N Fig. A-GBFAA Minor editorial or document structure change N Fig. A-GBFAA Sheet 01 Minor editorial or document structure change N Fig. A-GBFAA Sheet 02 Minor editorial or document structure change N DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 4 6

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

# @A330 SERVICE BULLETIN REVISION TRANSMITTAL SHEET Fig. A-GWAAA Minor editorial or document structure change N Fig. A-GWAAA Sheet 01 Minor editorial or document structure change N Fig. A-GWBAA Minor editorial or document structure change N Fig. A-GWBAA Sheet 01 Minor editorial or document structure change N FILING INSTRUCTIONS This Service Bulletin has been generated electronically and is reissued as a complete document. Replace the complete document. Put this Revision Transmittal Sheet in front of the Service Bulletin. HISTORY OF PREVIOUS REVISIONS Revision No. 01 was issued to add the removal/installation of the Anti Hijack Camera, update the effectivity, add some covers to the parts to be re-identified and make some other minor changes. NOTE : This is only applicable for Revision No. 02 and subsequent. If information is required for Revisions issued previous to this, please check your copies of Revision Transmittal Sheets or contact AIRBUS. REVISION SEQUENCE ORIGINAL: Oct 12/04 REVISION No.: 01 - Apr 25/05 REVISION No. : 02 - Aug 12/16

DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 5 6

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

# @A330 SERVICE BULLETIN REVISION TRANSMITTAL SHEET

This Page Intentionally Left Blank

DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 6 6

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

# @A330 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. ATA SYSTEM: 25 

### TITLE: EQUIPMENT/FURNISHINGS - PAX COMPARTMENT - MODIFY CDLS WIRING LOOM IN UPPER COCKPIT DOOR PLATE COVER **CONF ALL MODIFICATIONS MODIFICATION CLASSIFICATION MAJOR None MINOR 51911D44499 NOTE : As per EASA IR 21, a minor change is one that has no appreciable effect on the mass, balance, structural strength, reliability, operational characteristics affecting the airworthiness of the product. All other changes are major changes. REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES During the accomplishment of the Service Bulletin No. A340-25-4181 (EQUIPMENT/FURNISHINGS - PASSENGER COMPARTMENT - INTRODUCE A MODIFIED INT RUSION AND PENETRATION RESISTANCE COCKPIT DOOR), it was found that the electrical harness 7450VB, installed on the cover of the upper cockpit door frame, is accessible from the cabin side. Therefore, the protection of this harness must be improved. This Service Bulletin introduces: - a re-routing of the electrical harness 7450VB - the installation of a protection plate for the electrical harness 7450VB. This Service Bulletin has been validated on A340-600 aircraft MSN 0436. Accomplishment of this Service Bulletin improves cockpit security by denying access to the electrical harness from the cabin side. GENERAL EVALUATION EVALUATION TABLE COMPLIANCE RECOMMENDED (1) CANCELS INSPECTION SB NO POTENTIAL AD NO A/C OPERATION AFFECTED NO RELIABILITY AFFECTED NO PAX COMFORT AFFECTED NO DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 1 6

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

# @A330 SERVICE BULLETIN SUMMARY EVALUATION TABLE COST SAVING NO ETOPS AFFECTED NO STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED NO NOTE (1) : Service Bulletin recommended to be accomplished to prevent significant operational disruptions. MATERIAL PRICE INFORMATION MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Kit 253213D02R02 1 260.00 Bolt, Washer, Screw, Wire protection, Clamp, Nut, Cable Tie Component COMPD01 1 See SB Bolt, Washer EFFECTIVITY This Service Bulletin is applicable to this (these) operator(s) :

38W 51X AAL ABD ACA ACI AEA AFR ALK ARG AZA AZU BEL BER BGH CPA CRL CSA DAL DGA DLH EDW EIN F2I FWI G8E GFA GIA GRL HDA HFY HVN KAL MAS MLM MOV OHY PLM QAF QFA QTR RSY SAI SAS SXD TAE TAM TAP TCX THA THY TSC UAE VKG WRC XAX XLF CONCURRENT REQUIREMENTS Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishment of the following Service Bulletin(s): Service Bulletin No. A330-25-3161 NOTE : Service Bulletin No. A330-25-3161 (EQUIPMENT/F URNISHING - PASSENGER COMPARTMENT - INTRODUCTION A MODIF IED INTRUSION AND PENETRATION RESISTANCE COCKPIT DOOR) applies MOD 500014D44099. REFERENCES / REPERCUSSIONS TFU None OEB None AOT None SIL None ISI 00.00.00198 LINE MAINTENANCE AFFECTED No LIFE LIMIT None NATURE OF THE WORK AIRCRAFT YES EQUIPMENT NO HARD NO DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 2 6

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

# @A330 SERVICE BULLETIN SUMMARY SOFT NO OBRM NO MANPOWER Task 253213-831-848-001: Modification TOTAL MANHOURS 18.50 ELAPSED TIME (HOURS) 14.00

Task 253213-831-849-001: Modification - Additional Work for Aircraft Modified by Revision No. 01 or any Previous Issue TOTAL MANHOURS 1.00 APPENDICES None

DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 3 6

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

# @A330 SERVICE BULLETIN SUMMARY
**CONF ALL

FR16A FR12 

### B A

32MQ 31MQ 30MQ 25MQ
−A KEYPAD 25MQ 317LG 6296VS

6294VS

6295VS 

### A

32MQ 31MQ 30MQ 25MQ
−A KEYPAD 25MQ 317LG 6296VS

6294VS

6295VS FR11 

### B BEFORE B AFTER Z220

40MQ 40MQ 6297VS 6297VS

G_SB_253213_6_SAAA_01_00 Figure A-G SAAA - S heet 01
DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 4 6

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

# @A330 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 ATA SYSTEM: 25 

### TITLE: EQUIPMENT/FURNISHINGS - PAX COMPARTMENT - MODIFY CDLS WIRING LOOM IN UPPER COCKPIT DOOR PLATE COVER MODIFICATION No.: 51911D44499 This document contains AIRBUS PROPRIETARY INFORMATION and shall at all times remain the property of AIRBUS; no intellectual property right or licence is granted by AIRBUS in connection with any information contained in it. It is delivered on the express condition that said document and the information contained in it shall be treated as confidential, shall not be used for any purpose other than that for which it is hereby delivered. It shall not be disclosed in whole or in part to third parties and shall not be duplicated in any manner (except for the purposes of performing the tasks described hereunder and provided that any recipient of such document shall comply with the conditions herein), without AIRBUS prior written consent. 1. PLANNING INFORMATION **CONF ALL A. EFFECTIVITY (1) Models 330-202 330-203 330-223 330-243 330-301 330-303 330-321 330-322 330-323 330-341 330-342 330-343 (2) Effectivity by MSN 0012 0017 0030 0037 0045 0050 0054-0055 0060 0062 0064-0065 0070-0072 0082-0083 0086-0087 0095-0096 0098-0099 0102 0106 0109 0111-0113 0116 0118 0120-0122 0127 0132 0138 0140 0143-0144 0148 0153 0155 0162 0165 0171-0172 0177 0181 0195 0200 0206 0209 0211 0219 0222-0224 0226 0229-0232 0234 0238 0240-0241 0244 0247-0251 0253-0256 0258-0259 0261-0262 0265-0267 0269 0271-0272 0275-0277 0279 0281 0283-0288 0290-0291 0293-0296 0299-0301 0303 0305-0306 0308-0309 0311-0317 0320 0322-0324 0326 0328 0330 0333-0334 0337-0340 0342-0346 0348-0351 0353 0356-0358 0361-0362 0364-0366 0368-0370 0372 0375 0380 0382 0384 0386 0388-0389 0392-0393 0396-0398 0400-0401 0403-0405 0407-0409 0412 0418-0423 0425 0427-0428 0432 0437 0439 0441 0443-0444 0448 0451-0452 0454-0456 0458 0461-0463 0465-0466 0469 0472-0473 0476-0477 0479-0481 0484 0486-0487 0489-0491 0493-0494 0496-0498 0500-0501 0503-0513 0515-0516 0518-0519 0521-0522 0524-0527 0529-0530 0532-0533 0535-0536 0539 0542 0548-0553 0555 0558 0564-0565 0567-0568 0570-0571 0573 0576 0578-0579 0581 0584 0587-0588 0591 0597
DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 1 6

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

# @A330 SERVICE BULLETIN (3) Effectivity by Operator The Operator/MSN relationship is provided for information only and is correct at the time of issue in accordance with the information available to AIRBUS. Any future changes resulting from transfer of an aircraft from one operator to another will not be reflected in this list unless the Service Bulletin is revised for another reason. OPERATOR MSN 38W 0401 51X 0261 AAL 0315 0323 0333 0337 0342 0370 0375 0380 0388 ABD 0343 ACA 0277 0279 0284 0344 0400 0408 0412 0419 ACI 0507 0510 AEA 0461 0505 0526 0551 0597 AFR 0422 0443 0448 0458 0465 0481 0498 0500 0503 0516 0519 0567 0584 ALK 0303 0306 0311 0313 0456 ARG 0290 0300 0358 0364 0587 AZA 0272 0339 AZU 0462 0494 0527 0529 0532 BEL 0030 0037 0045 0082 0095 0229 0249 0324 BER 0288 0322 0403 0432 0444 0454 0469 0476 0493 BGH 0255 CPA 0102 0113 0121 0386 0389 0393 0418 0420 0421 0423 0439 0539 0548 0565 CRL 0285 0320 CSA 0425 DAL 0524 0533 0542 0549 0552 0578 0588 0591 DGA 0240 DLH 0570 0576 0579 EDW 0291 EIN 0269 0330 0397 F2I 0087 0200 FWI 0253 G8E 0294 0299 GFA 0276 0281 0286 0287 0334 0340 GIA 0138 0140 0144 0148 0153 0165 GRL 0230 HDA 0012 0017 0071 0083 0099 0106 0109 0118 0155 0234 0244 0405 0479 0512 0581 HFY 0127 0211 0262 HVN 0275 0366 KAL 0162 0172 0206 0219 0222 0226 0241 0256 0258 0267 0338 0350 0351 0368 0428 0484 0490 0550 MAS 0116 MLM 0451 MOV 0535 DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 2 6

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

# @A330 SERVICE BULLETIN
OPERATOR MSN OHY 0072 0098 0143 0316 0345 0353 0362 0404 0437 PLM 0265 QAF 0487 QFA 0506 0508 0513 0522 0553 0558 0564 QTR 0441 0473 0489 0511 0521 0571 RSY 0096 0120 0171 SAI 0055 0070 0086 SAS 0496 0497 0515 0568 SXD 0530 0555 0573 TAE 0348 TAM 0232 0238 0247 0259 0361 0466 0472 TAP 0181 0195 0223 0305 0308 0312 0317 0365 0372 0477 0486 TCX 0254 0266 0301 0398 THA 0050 0060 0062 0064 0065 0112 0122 0209 0224 0231 0346 THY 0463 0504 TSC 0111 0132 0177 0248 0250 0251 0271 0369 0407 0427 0480 UAE 0283 0293 0295 0314 0326 0328 0382 0384 0392 0396 0409 0452 0455 0491 0509 0518 0525 0536 VKG 0309 0349 0356 0357 WRC 0296 XAX 0054 XLF 0501

DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 3 6

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

# @A330 SERVICE BULLETIN (4) Configuration by MSN MSN CONFIGURATION 0012 0017 0030 0037 0045 0050 0054 0055 0060 0062 0064 0065 0070 0071 0072 0082 0083 0086 0087 0095 0096 0098 0099 0102 0106 0109 0111 0112 0113 0116 0118 0120 0121 0122 0127 0132 0138 0140 0143 0144 0148 0153 0155 0162 0165 0171 0172 0177 0181 0195 0200 0206 0209 0211 0219 0222 0223 0224 0226 0229 0230 0231 0232 0234 0238 0240 0241 0244 0247 0248 0249 0250 0251 0253 0254 0255 0256 0258 0259 0261 0262 0265 0266 0267 0269 0271 0272 0275 0276 0277 0279 0281 0283 0284 0285 0286 0287 0288 0290 0291 0293 0294 0295 0296 0299 0300 0301 0303 0305 0306 0308 0309 0311 0312 0313 0314 0315 0316 0317 0320 0322 0323 0324 0326 0328 0330 0333 0334 0337 0338 0339 0340 0342 0343 0344 0345 0346 0348 0349 0350 0351 0353 0356 0357 0358 0361 0362 0364 0365 0366 0368 0369 0370 0372 0375 0380 0382 0384 0386 0388 0389 0392 0393 0396 0397 0398 0400 0401 0403 0404 0405 0407 0408 0409 0412 0418 0419 0420 0421 0422 0423 0425 0427 0428 0432 0437 0439 0441 0443 0444 0448 0451 0452 0454 0455 0456 0458 0461 0462 0463 0465 0466 0469 0472 0473 0476 0477 0479 0480 0481 0484 0486 0487 0489 0490 0491 0493 0494 0496 0497 0498 0500 0501 0503 0504 0505 0506 0507 0508 0509 0510 0511 0512 0513 0515 0516 0518 0519 0521 0522 0524 0525 0526 0527 0529 0530 0532 0533 0535 0536 0539 0542 0548 0549 0550 0551 0552 0553 0555 0558 0564 0565 0567 0568 0570 0571 0573 0576 0578 0579 0581 0584 0587 0588 0591 0597 001

(5) Configuration definition **CONF 001 Config. 001 is valid for all the aircraft given in the effectivity of this Service Bulletin as a standard configuration. (6) Material Effectivity MATERIAL QTY PER A/C SEE NOTES Kit 253213D02R02 1 Consumable CMLD01 1 Reidentified part set REIDD01 1 Component COMPD01 1 B. CONCURRENT REQUIREMENTS Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishment of the following Service Bulletin(s): Service Bulletin No. A330-25-3161 NOTE : Service Bulletin No. A330-25-3161 (EQUIPMENT/FURNISHING - PASSENGER COMPARTMEN T - INTRODUCTION A MO DIFIED INTRUSION DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 4 6

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

# @A330 SERVICE BULLETIN AND PENETRATION RESISTANCE COCKPIT DOOR) applies MOD 500014D44099. C. REASON (1) History During the accomplishment of the Service Bulletin No. A340-25-4181 (EQUIPMENT/FURNIS HINGS - PASSENGER COMPARTMENT - INTRODUCE A MODIFIED INTRUSION AND PENETRATION RESISTANCE COCKPIT DOOR), it was found that the electrical harness 7450VB, installed on the cover of the upper cockpit door frame, is accessible from the cabin side. Therefore, the protection of this harness must be improved. (2) Objective/Action This Service Bulletin introduces: - a re-routing of the electrical harness 7450VB - the installation of a protection plate for the electrical harness 7450VB. This Service Bulletin has been validated on A340-600 aircraft MSN 0436. (3) Advantages Accomplishment of this Service Bulletin improves cockpit security by denying access to the electrical harness from the cabin side. (4) Operational/Maintenance Consequences None D. DESCRIPTION To accomplish this Service Bulletin it is necessary to : Task 253213-831-848-001: Modification (1) Removal the Electrical Harness 7450VB and the Cover of the Cockpit Door Frame (2) Modify the Cover of the Cockpit Door Frame on Bench (3) Install the Cover and the Electrical Harness 7450VB on the Cockpit Door Frame Task 253213-831-849-001: Modification - Additional Work for Aircraft Modified by Revision No. 01 or any Previous Issue (1) Replace the Fasteners of the Cover

DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 5 6

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

# @A330 SERVICE BULLETIN E. COMPLIANCE (1) Classification RECOMMENDED: Service Bulletin recommended to be accomplished to prevent significant operational disruptions. (2) Accomplishment Timescale Accomplishment of this Service Bulletin is recommended at the earliest opportunity where manpower and facilities are available. F. APPROVAL The technical content of this document is approved under the authority of Design Organisation Approval No. EASA. 21J.031. If an aircraft listed in the effectivity has a modification or repair embodied that is not of AIRBUS origin, and which affects the content of this Service Bulletin, the operator is responsible for obtaining approval by its airworthiness authority for any adaptation necessary before incorporation of the Service Bulletin. G. MANPOWER The manpower estimates given in this Service Bulletin are based on the direct labor cost to do the work. These estimates assume that the work will be done by experienced personnel, and may need to be revised upwards to suit operator’s circumstances. The estimates do not include the time to prepare, plan or inspect the work. Manufacture and procurement of parts and tools, drying times for paints, sealants, etc., and general administration work are also not included. Task 253213-831-848-001: Modification Get Access 3.50 On Aircraft Removal the Electrical Harness 7450VB and the Cover of the Cockpit Door Frame 3.00 Modify the Cover of the Cockpit Door Frame on Bench 2.00 Install the Cover and the Electrical Harness 7450VB on the Cockpit Door Frame 3.00 Tests 3.00 Close-Up 4.00 TOTAL MANHOURS 18.50 ELAPSED TIME (HOURS) 14.00 Task 253213-831-849-001: Modification - Additional Work for Aircraft Modified by Revision No. 01 or any Previous Issue On Aircraft Replace the Fasteners of the Cover 1.00 TOTAL MANHOURS 1.00

DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 6 6

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

# @A330 SERVICE BULLETIN H. WEIGHT AND BALANCE The weight and balance estimates given in this Service Bulletin are based on the Manufacturer’s Empty Weight (MEW) and do not include operator’s items. For the definition of MEW and operator’s items, refer to Weight and Balance Manual (WBM) 01-00-07. Manufacturers Empty Weight 0.401 KG (+0.8840 LB) Effect on Balance 4.117 KGM (+29.778 LB.FT ) I. ELECTRICAL LOAD DATA Not Changed J. REFERENCES

Aircraft Maintenance Manual (AMM) 06-16-00 06-20-00 06-31-53 06-41-53 12-34-24 20-21-11 20-21-15 20-28-00 21-26-00 22-96-00 22-97-00 23-72-51 24-41-00 25-13-44 25-23-42 31-50-00 31-60-00 33-13-00 33-14-00 52-51-00 Consumable Material List (CML) ATA Common Support Data Dictionary (CSDD), Chapter 2 Elec. Std. Practices Manual (ESPM) 20-33-00 20-33-44 20-44-00 20-51-20 20-52-10 20-52-20 20-52-21 20-54-50 20-55-00 Service Bulletin (SB) A330-25-3161 A340-25-4181 Standards Manual (SM) Structural Repair Manual (SRM) 51-42-00 51-44-00 Weight and Balance Manual (WBM) 01-00-07 K. PUBLICATION AFFECTED

Aircraft Maintenance Manual (AMM) 52-51-00 52-51-11 52-51-12 Aircraft Schematic Manual (ASM) 52-51-00 Illustrated Parts Catalog (IPC) 52-51-01 L. INTERCHANGEABILITY/MIXABILITY The interchangeability/mixability possibilities are for new or modified parts introduced by the accomplishment of this Service Bulletin. DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE NOTES Cover F2527487100200 F2528716800400 03 Not Applicable Cover F2527487100400 F2528716800600 03 Not Applicable

DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 7 6

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

# @A330 SERVICE BULLETIN
DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE NOTES Cover F2527487100600 F2528716800800 03 Not Applicable Cover F2527487101000 F2528716801200 03 Not Applicable Cover F2527487101600 F2528716801800 03 Not Applicable Cover F2527487101800 F2528716802000 03 Not Applicable Cover F2527487102200 F2528716802400 03 Not Applicable Cover F2527487102400 F2528716802600 03 Not Applicable Cover F2527487102600 F2528716802800 03 Not Applicable Cover F2527487102800 F2528716803000 03 Not Applicable Cover F2527487103000 F2528716803200 03 Not Applicable Cover F2527487103200 F2528716803400 03 Not Applicable Cover F2527487103400 F2528716803600 03 Not Applicable Cover F2527487103600 F2528716803800 03 Not Applicable Cover F2527487104400 F2528716804600 03 Not Applicable Cover F2527487104600 F2528716804800 03 Not Applicable Cover F2527487104800 F2528716805000 03 Not Applicable Cover F2527487105000 F2528716805200 03 Not Applicable Cover F2527487105200 F2528716805400 03 Not Applicable Cover F2527487105800 F2528716806000 03 Not Applicable Cover F2527487600200 F2528717000200 03 Not Applicable Cover F2527487601600 F2528717001600 03 Not Applicable Cover F2527487603200 F2528717003200 03 Not Applicable Cover F2527487604000 F2528717004000 03 Not Applicable DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 8 6

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

# @A330 SERVICE BULLETIN
DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE NOTES Cover F2527487605000 F2528717005000 03 Not Applicable Cover F2527487605800 F2528717005800 03 Not Applicable Cover F2527487606000 F2528717006000 03 Not Applicable Cover F2527487606200 F2528717006200 03 Not Applicable Cover F2527487606400 F2528717006400 03 Not Applicable Cover F2527487106400 F2528717006400 03 Not Applicable Cover F2527487606600 F2528717006600 03 Not Applicable Cover F2527487106600 F2528717006600 03 Not Applicable Cover F2527487611200 F2528717011200 03 Not Applicable Cover F2527487106800 F2528717006800 03 Not Applicable Cover F2527487601800 F2528717001800 03 Not Applicable NOTE : For definitions of interchangeability codes in column INT., refer to ATA Common Support Data Dictionary (CSDD), Chapter 2. M. SPARES Cover F2527487100200 Cover F2527487100400 Cover F2527487100600 Cover F2527487101000 Cover F2527487101600 Cover F2527487101800 Cover F2527487102200 Cover F2527487102400 Cover F2527487102600 Cover F2527487102800 Cover F2527487103000 Cover F2527487103200 Cover F2527487103400 Cover F2527487103600 Cover F2527487104400 Cover F2527487104600 Cover F2527487104800 Cover F2527487105000 DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 9 6

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

# @A330 SERVICE BULLETIN
Cover F2527487105200 Cover F2527487105800 Cover F2527487106400 Cover F2527487106600 Cover F2527487600200 Cover F2527487601600 Cover F2527487601800 Cover F2527487603200 Cover F2527487604000 Cover F2527487605000 Cover F2527487605800 Cover F2527487606000 Cover F2527487606200 Cover F2527487606400 Cover F2527487606600 Cover F2527487611200 The parts listed here must not be installed anymore on aircraft which have accomplished this Service Bulletin or which have the equivalent production modification embodied.

DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 10 6

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

# @A330 SERVICE BULLETIN 2. MATERIAL INFORMATION **CONF ALL A. MATERIAL - PRICE AND AVAILABILITY (1) Procurement Addresses Customers with aircraft shown in the effectivity of this Service Bulletin should send a purchase order to AIRBUS. Quote the number of this Service Bulletin. The address is : Kit 253213D02R02 AIRBUS Material, Logistics and Suppliers ATP II B, Hein-Sass-Weg 24 21129 HAMBURG GERMANY For ordering by internet: http://spares.airbus.com For ordering by E-mail: airbus.kit@airbus.com Telephone Hotline: +49 40 743 51616 (2) Price and Availability

Kit 253213D02R02 Cost 260.00 USD Availability 90 calendar days from receipt of order The availability given above is the standard lead time from the date of your purchase order. If items are required before this time, please include a retrofit planning schedule with your order so that we can try to comply with your requirements. The sales terms (costs and availability) are estimated in relation to economic conditions. The latest valid price and lead time for ordering purposes shall be obtained through the AirbusSpares portal or through a request for quotation to airbus.kit@airbus.com. B. INDUSTRY SUPPORT INFORMATION AIRBUS will not provide industry support for accomplishment of this Service Bulletin. C. LIST OF COMPONENTS Kit 253213D02R02 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 3 NAS1833C08-370 4 INSERT 4 MS21250-03012 1 BOLT 5 NSA5379-3C 3 WASHER 6 DAN125-4 4 WASHER 7 NAS1102-08-6 4 SCREW 8 F2527496220200 1 WIREPROT DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 11 6

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

# @A330 SERVICE BULLETIN
ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 9 MS21250-03006 2 BOLT 11 MS21919WCH7 4 CLAMP 12 NAS1096-2-10 4 SCREW 13 MS21042L08 4 NUT 14 NAS1149CN832R 8 WASHER 26 NSA935401-03 3 TIE NOTE : If you find part numbers of hardware components in the related kit(s) which you cannot identify in the LIST OF COMPONENTS of this Service Bulletin, refer to Standards Manual (SM). The SM will give you the correct part number to part number relationship. D. LIST OF MATERIALS - OPERATOR SUPPLIED (1) Consumable Materials Consumable CMLD01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Epoxy Adhesive-- Legacy 2 05EML8 As required Non Aqueous Cleaner-General 08BAA9 As required Textile-Lint Free Cotton 14SBA1 As required (2) Components Component COMPD01 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 5 NSA5379-3C 3 WASHER 9 MS21250-03006 2 BOLT NOTE : If you find part numbers of hardware components in the related kit(s) which you cannot identify in the LIST OF COMPONENTS of this Service Bulletin, refer to Standards Manual (SM). The SM will give you the correct part number to part number relationship. NOTE : The above list of components is not an AIRBUS Kit, the required parts shall be ordered as necessary through the given channel. NOTE : The components listed above are only necessary if ADDITIONAL WORK task is to be accomplished. The quantity of these items are to be ordered as required. (3) Equipment None

DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 12 6

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

# @A330 SERVICE BULLETIN E. PARTS TO BE RE-IDENTIFIED BY OPERATOR Reidentified part set REIDD01 ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE NOTES 1 F2528716800400 COVER (1) F2527487100200 1 F2528716800600 COVER (1) F2527487100400 1 F2528716800800 COVER (1) F2527487100600 1 F2528716801200 COVER (1) F2527487101000 1 F2528716801800 COVER (1) F2527487101600 1 F2528716802000 COVER (1) F2527487101800 1 F2528716802400 COVER (1) F2527487102200 1 F2528716802600 COVER (1) F2527487102400 1 F2528716802800 COVER (1) F2527487102600 1 F2528716803000 COVER (1) F2527487102800 1 F2528716803200 COVER (1) F2527487103000 1 F2528716803400 COVER (1) F2527487103200 1 F2528716803600 COVER (1) F2527487103400 1 F2528716803800 COVER (1) F2527487103600 1 F2528716804600 COVER (1) F2527487104400 1 F2528716804800 COVER (1) F2527487104600 1 F2528716805000 COVER (1) F2527487104800 1 F2528716805200 COVER (1) F2527487105000 1 F2528716805400 COVER (1) F2527487105200 1 F2528716806000 COVER (1) F2527487105800 1 F2528717000200 COVER (1) F2527487600200 1 F2528717001600 COVER (1) F2527487601600 1 F2528717001800 COVER (1) F2527487601800 1 F2528717003200 COVER (1) F2527487603200 1 F2528717004000 COVER (1) F2527487604000 1 F2528717005000 COVER (1) F2527487605000 1 F2528717005800 COVER (1) F2527487605800 1 F2528717006000 COVER (1) F2527487606000 1 F2528717006200 COVER (1) F2527487606200 1 F2528717006400 COVER (1) F2527487106400 (1) F2527487606400 1 F2528717006600 COVER (1) F2527487106600 (1) F2527487606600 1 F2528717006800 COVER (1) F2527487106800 1 F2528717011200 COVER (1) F2527487611200

DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 13 6

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

# @A330 SERVICE BULLETIN F. TOOLING None

DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 14 6

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

# @A330 SERVICE BULLETIN 3. ACCOMPLISHMENT INSTRUCTIONS Task 253213-831-848-001 - Modification 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. CAUTION : BEFORE YOU DO WORK ON THE ELECTRICAL CIRCUIT AT THE REAR OF A CIRCUIT BR EAKER PANEL, OPEN THE CIRCUIT BR EAKER 2XD(PANEL 721VU POSITION X5). THEN REMOVE THE CBMU FROM THE RACK. IF YOU DO NOT OBEY THIS PRECAUTION, THERE IS A RISK OF DAMAGE TO THE CBMU FROM UNWANTED VOLTAGE INJECTION. NOTE : The accomplishment instructions of this Service Bulletin include procedures given in other documents or in other sections of the Service Bulletin. When the words ’refer to’ are used and the operator has procedure accepted by the local authorities he belongs to, the accepted alternative procedure can be used. When the words ’in accordance with’ are used then the given procedure must be followed. NOTE : The access and close-up instructions, not comprising return to service tests, in this Service Bulletin do not constitute or affect the technical intent of the Service Bulletin. Operators can therefore, as deemed necessary, omit or add access and/or close-up steps to add flexibility to their maintenance operations as long as the technical intent of the Service Bulletin is met within the set parameters. NOTE : Manual titles given in the accomplishment instructions are referred to by acronyms. Refer to paragraph 1.J., References, for the definition of acronyms. NOTE : This Service Bulletin contains the instructions for the on-aircraft maintenance necessary to ensure the continued airworthiness of the aircraft. For any deviations to the instructions contained herein, contact Airbus for repair instructions and approval. NOTE : Discarded parts must be managed at the operator’s discretion.

DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 15 6

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

# @A330 SERVICE BULLETIN Task Associated Data Zone From 210 to 220 Modified FIN 317LG 7450VB Access Door 831 841 Manpower TOTAL MANHOURS 18.50 ELAPSED TIME (HOURS) 14.00 A. GENERAL (1) Subtask 253213-910-201-001 - Standard Practices Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 06-16-00-912-801 06-20-00, Page Block 001 06-31-53, Page Block 001 06-41-53, Page Block 001 Task 20-21-15-912-801 Task 20-28-00-912-802 Consumable Material List (CML) Elec. Std. Practices Manual (ESPM) 20-33-00 20-33-44 20-51-20 20-52-10 20-54-50 Structural Repair Manual (SRM) 51-42-00 51-44-00 (a) For the Frame (FR) identification, refer to AMM 06-31-53, Page Block 001. (b) For identification of the zones, refer to AMM 06-20-00, Page Block 001. (c) For identification of access panels, refer to AMM 06-41-53 Page Block 001. (d) For the specification of materials (Mat. No.) given in this Service Bulletin, refer to Consumable Material List (CML). (e) For circuit breaker safety practices, refer to AMM Task 06-16-00-912-801. (f) For the general installation of electr ical wire harnesses, refer to ESPM 20-33-00. (g) Tag all the parts you must remove and retain to make the subsequent installation easier. (h) For the cable tie application and tooling, refer to ESPM 20-33-44. DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 16 6

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

# @A330 SERVICE BULLETIN (i) For the protection of the connectors , contacts and termi nals, refer to ESPM 20-54-50. (j) Do a check of the electr ical connectors before you connect them, refer to ESPM 20-52-10. (k) Remove and install fasteners in accordance with SRM 51-42-00. (l) To torque tighten the electrical component fasteners, refer to AMM Task 20-21-15-912-801. (m) Obtain fastener hole diameters and drill data in accordance with SRM 51-44-00. (n) Put all the retained hardware in identified plastic bags and attach the bags to the related unit. (2) Subtask 253213-900-202-001 - Administrative Write in the applicable aircraft records that you have done all the work given in this Service Bulletin. B. PREPARATION (1) Subtask 253213-941-201-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001 Task 12-34-24-860-802 Task 23-72-51-000-801 Task 25-13-44-000-801 Task 25-23-42-000-801 NOTE : The items given in this note shall be considered as the basic Aircraft configuration before you start a maintenance task: - Aircraft on the ground resting on landing gear (the ground safety locks and the wheel chocks are in position on the landing gear) - Engine shut down, thrust reversers closed and locked - Aircraft in clean configuration - Parking brake applied - Aircraft electrical network de-energized - Hydraulic system s depressurized - Access to the cockpit and cabin is available
DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 17 6

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

# @A330 SERVICE BULLETIN - All circuit breakers are in closed position - All controls in NORM, AUTO or OFF position. (a) Make sure that the aircraft is electrically grounded, refer to AMM Task 12-34-24-860-802. (b) If installed, remove the Anti Hijack Camera 12RA, refer to AMM Task 23-72-51-000-801. (c) Remove the ceiling and sidewall panels 211MC, refer to AMM 06-41-53, Page Block 001 and AMM Task 25-13-44-000-801. (d) Remove the cover panels 221AC, refer to AMM 06-41-53, Page Block 001 and AMM Task 25-23-42-000-801. (e) In the cockpit, on the overhead panel, remove all the blanking plates necessary to get access to the modification of the equipment and wiring. (2) Subtask 253213-862-201-001 - De-Energize Electrical Manpower Resources Skills NON SPECIFIC (a) In the cockpit, on the panel 235VU, make sure that these pushbutton switches are released: - BAT 1, BAT 2, APU BAT, - GEN 1, 2, APU GEN, - EXT A (B). (b) Open, safety/lock and tag these circuit breakers: PANEL DESIGNATION FIN LOCATION SEE NOTES 742VU 701PP 10PB1 72 S 742VU 702PP 10PB2 71 S (c) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not to operate the pushbutton switches on the overhead panel: - 211VU (EMER ELEC PWR), - 235VU (ELEC). (d) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not to start the APU. (e) Make sure that the external connector(s) is (are) not connected to the aircraft receptacle(s) EXT PWR A (B).

DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 18 6

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

# @A330 SERVICE BULLETIN (f) Make sure that there is warning notice at the access door 121EL to tell persons not to connect the external power connector(s). C. PROCEDURE (1) Subtask 253213-010-201-001 - Removal the Electrical Harness 7450VB and the Cover of the Cockpit Door Frame Work Zones and Access Panels Zone Access/Work location From 210 Access Door 831, Door 841 To 220 Manpower Resources Manhours 3.00 Minimum number of person 1 Subtask elapsed time 3.00 Skills NON SPECIFIC References Elec. Std. Practices Manual (ESPM) 20-33-00 Structural Repair Manual (SRM) 51-42-00 Fig. A-GBAAA Removal of the Electrical Harness 7450VB Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Fig. A-GWAAA Wiring of the Electrical Harness 7450VB, pre SB A330-25-3213 Sheet 01 Fig. A-GWBAA Wiring of the Electrical Harness 7450VB, post SB A330-25-3213 Sheet 01 Fig. A-GBCAA Modification of the Cover of the Cockpit Door Frame Sheet 01 Sheet 02 Fig. A-GBBAA Removal of the Cover from the Cockpit Door Frame Sheet 01 Sheet 02 (a) From the secure part, Item (28) of the RH cockpit door post, remove in accordance with SRM 51-42-00 and as shown on Fig. A-GBAAA Sheet 04 , View E: 1 Cover Item (20) Retain and 2 Screw Item (21) Retain

DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 19 6

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

# @A330 SERVICE BULLETIN (b) Modify the wiring: Refer to Fig. A-GBAAA Sheet 04 , View F and ESPM 20-33-00 1 Disconnect the plug 25MQA from the key pad 25MQ. 2 From the plug 25MQA, remove: 1 Cable Tie Item (26) Discard 1 Plug Cover Item (27) Retain 2 Screw With Clamp Item (25) Retain 3 Remove the wires of the electrical harness 7450VB, Item (2), from the plug 25MQA. (c) From the RH cockpit door post, remove in accordance with SRM 51-42-00 and as shown on Fig. A-GBAAA Sheet 02 , Fig. A-GBAAA Sheet 03 and Fig. A-GBAAA Sheet 04 , View G, H and J: 1 Secure Part Item (28) Retain 1 Cover Plate Item (29) Retain attached with: 6 Screw Item (30) Retain 5 Spacer Item (31) Retain attached with: 10 Screw Item (32) Retain 6 Clamp Item (35) Retain 3 Clamp Item (36) Retain 9 Spacer Item (37) Retain attached with: 9 Screw Item (33) Retain 9 Washer Item (34) Retain NOTE : Remove and retain the spacers, Item (37), if installed. (d) Modify the wiring Refer to ESPM 20-33-00. DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 20 6

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

# @A330 SERVICE BULLETIN
1 Disconnect the wires of the electrical harness 7450VB, Item (2), from the release latches 30MQ, 31MQ and 32MQ as shown on Fig. A-GBAAA Sheet 01 and Fig. A-GWAAA
. 2 If installed, disconnect the electrical harness 7450VB from the circuit breaker box 40MQ as shown on Fig. A-GBAAA Sheet 05 , View L and Fig. A-GWBAA
. (e) From the cover, Item (1), remove in accordance with SRM 51-42-00 and as shown on Fig. A-GBAAA Sheet 02 and Fig. A-GBAAA Sheet 05 , View K: FIN 317LG 1 Limit Switch Item (38) Retain attached with: 2 Screw Item (39) Retain As required Cable Tie Item (40) Discard (f) Modify the wiring Refer to ESPM 20-33-00 1 Disconnect the wires of the electrical harness 7450VB from the Limit Switch 317LG, Item (38), as shown on Fig. A-GBAAA Sheet 05 , View K. 2 Remove the electrical harness 7450VB, Item (2), from the cover of the cockpit door frame, Item (1), as shown on Fig. A-GBAAA Sheet 02 , in accordance with SRM 51-42-00: (g) From the cockpit door frame, remove in accordance with SRM 51-42-00 and as shown on Fig. A-GBBAA Sheet 02 : 3 Cover Item (45) Retain 1 Cover Item (1) Retain attached with: 1 Screw Item (41) Discard 1 Washer Item (43) Discard and 2 Screw Item (42) Discard 2 Washer Item (44) Discard

DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 21 6

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

# @A330 SERVICE BULLETIN (h) From the cover, Item (1), remove as shown on Fig. A-GBCAA Sheet 01 : 5 Cable Mount Item (46) Discard

(2) Subtask 253213-831-203-001 - Modify the Cover of the Cockpit Door Frame on Bench Manpower Resources Manhours 2.00 Minimum number of person 1 Subtask elapsed time 2.00 Skills NON SPECIFIC Material necessary to do the job Kit 253213D02R02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 3 NAS1833C08-370 4 INSERT Reidentified part set REIDD01 ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE NOTES 1 F2528716800400 COVER (1) F2527487100200 1 F2528716800600 COVER (1) F2527487100400 1 F2528716800800 COVER (1) F2527487100600 1 F2528716801200 COVER (1) F2527487101000 1 F2528716801800 COVER (1) F2527487101600 1 F2528716802000 COVER (1) F2527487101800 1 F2528716802400 COVER (1) F2527487102200 1 F2528716802600 COVER (1) F2527487102400 1 F2528716802800 COVER (1) F2527487102600 1 F2528716803000 COVER (1) F2527487102800 1 F2528716803200 COVER (1) F2527487103000 1 F2528716803400 COVER (1) F2527487103200 1 F2528716803600 COVER (1) F2527487103400 1 F2528716803800 COVER (1) F2527487103600 1 F2528716804600 COVER (1) F2527487104400 1 F2528716804800 COVER (1) F2527487104600 1 F2528716805000 COVER (1) F2527487104800 1 F2528716805200 COVER (1) F2527487105000 1 F2528716805400 COVER (1) F2527487105200 1 F2528716806000 COVER (1) F2527487105800 1 F2528717000200 COVER (1) F2527487600200 1 F2528717001600 COVER (1) F2527487601600 DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 22 6

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

# @A330 SERVICE BULLETIN
ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE NOTES 1 F2528717001800 COVER (1) F2527487601800 1 F2528717003200 COVER (1) F2527487603200 1 F2528717004000 COVER (1) F2527487604000 1 F2528717005000 COVER (1) F2527487605000 1 F2528717005800 COVER (1) F2527487605800 1 F2528717006000 COVER (1) F2527487606000 1 F2528717006200 COVER (1) F2527487606200 1 F2528717006400 COVER (1) F2527487106400 (1) F2527487606400 1 F2528717006600 COVER (1) F2527487106600 (1) F2527487606600 1 F2528717006800 COVER (1) F2527487106800 1 F2528717011200 COVER (1) F2527487611200 Consumable CMLD01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Epoxy Adhesive-- Legacy 2 05EML8Non Aqueous CleanerGeneral 08BAA9 Textile-Lint Free Cotton 14SBA1 References Structural Repair Manual (SRM) 51-44-00 Fig. A-GBBAA Removal of the Cover from the Cockpit Door Frame Sheet 01 Sheet 02 Fig. A-GBCAA Modification of the Cover of the Cockpit Door Frame Sheet 01 Sheet 02 Fig. A-GBDAA Installation of the Cover on the Cockpit Door Frame Sheet 01 Sheet 02 (a) Cut out the cable channels in the upper edge of the cover, Item (1), to the shape that the electrical harness 7450VB can lead in a 90 degrees angle to the FWD direction, as shown on Fig. A-GBCAA Sheet 02 , View A and View B. (b) Round the edges of the cable channel as shown Fig. A-GBCAA Sheet 02 , View A and View B. (c) Drill four holes to the diameter of 14.5 mm (0.57 in.) in the upper edge of the cover, Item (1), as shown on Fig. A-GBCAA Sheet 02 , View C and Section A-A in accordance with SRM 51-44-00.

DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 23 6

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

# @A330 SERVICE BULLETIN (d) Deburr the holes in accordance with SRM 51-44-00 and clean the contact surfaces with: Textile-Lint Free Cotton 14SBA1 As required

made moist with: Non Aqueous Cleaner-General 08BAA9 As required (e) In the upper edge of the cover, Item (1), install, as shown on Fig. A-GBCAA Sheet 02 , View C and Section A-A: 4 Insert NAS1833C08-370 Item 3 with: Epoxy Adhesive-- Legacy 2 05EML8 As required (f) Re-identify the cover, Item (1): 1 Cover F2527487100200 Item (1) becomes: 1 Cover F2528716800400 Item 1 or 1 Cover F2527487100400 Item (1) becomes: 1 Cover F2528716800600 Item 1 or 1 Cover F2527487100600 Item (1) becomes 1 Cover F2528716800800 Item 1 or 1 Cover F2527487101000 Item (1) becomes: 1 Cover F2528716801200 Item 1 or 1 Cover F2527487101600 Item (1) DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 24 6

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

# @A330 SERVICE BULLETIN becomes: 1 Cover F2528716801800 Item 1 or 1 Cover F2527487101800 Item (1) becomes: 1 Cover F2528716802000 Item 1 or 1 Cover F2527487102200 Item (1) becomes: 1 Cover F2528716802400 Item 1 or 1 Cover F2527487102400 Item (1) becomes: 1 Cover F2528716802600 Item 1 or 1 Cover F2527487102600 Item (1) becomes: 1 Cover F2528716802800 Item 1 or 1 Cover F2527487102800 Item (1) becomes: 1 Cover F2528716803000 Item 1 or 1 Cover F2527487103000 Item (1) becomes: 1 Cover F2528716803200 Item 1 or 1 Cover F2527487103200 Item (1) becomes: DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 25 6

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

# @A330 SERVICE BULLETIN
1 Cover F2528716803400 Item 1 or 1 Cover F2527487103400 Item (1) becomes: 1 Cover F2528716803600 Item 1 or 1 Cover F2527487103600 Item (1) becomes: 1 Cover F2528716803800 Item 1 or 1 Cover F2527487104400 Item (1) becomes: 1 Cover F2528716804600 Item 1 or 1 Cover F2527487104600 Item (1) becomes: 1 Cover F2528716804800 Item 1 or 1 Cover F2527487104800 Item (1) becomes: 1 Cover F2528716805000 Item 1 or 1 Cover F2527487105000 Item (1) becomes: 1 Cover F2528716805200 Item 1 or 1 Cover F2527487105200 Item (1) becomes: 1 Cover F2528716805400 Item 1 DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 26 6

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

# @A330 SERVICE BULLETIN

or 1 Cover F2527487105800 Item (1) becomes: 1 Cover F2528716806000 Item 1 or 1 Cover F2527487600200 Item (1) becomes: 1 Cover F2528717000200 Item 1 or 1 Cover F2527487601600 Item (1) becomes: 1 Cover F2528717001600 Item 1 or 1 Cover F2527487601800 Item (1) becomes: 1 Cover F2528717001800 Item 1 or 1 Cover F2527487603200 Item (1) becomes: 1 Cover F2528717003200 Item 1 or 1 Cover F2527487604000 Item (1) becomes: 1 Cover F2528717004000 Item 1 or 1 Cover F2527487605000 Item (1) becomes: 1 Cover F2528717005000 Item 1 or DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 27 6

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

# @A330 SERVICE BULLETIN 1 Cover F2527487605800 Item (1) becomes: 1 Cover F2528717005800 Item 1 or 1 Cover F2527487606000 Item (1) becomes: 1 Cover F2528717006000 Item 1 or 1 Cover F2527487606200 Item (1) becomes: 1 Cover F2528717006200 Item 1 or 1 Cover F2527487606400 Item (1) becomes: 1 Cover F2528717006400 Item 1 or 1 Cover F2527487606600 Item (1) becomes: 1 Cover F2528717006600 Item 1 or 1 Cover F2527487611200 Item (1) becomes: 1 Cover F2528717011200 Item 1 or 1 Cover F2527487106400 Item (1) becomes: 1 Cover F2528717006400 Item 1 or 1 Cover F2527487106600 Item (1) DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 28 6

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

# @A330 SERVICE BULLETIN becomes: 1 Cover F2528717006600 Item 1 or 1 Cover F2527487106800 Item (1) becomes: 1 Cover F2528717006800 Item 1

(3) Subtask 253213-420-201-001 - Install the Cover and the Electrical Harness 7450VB on the Cockpit Door Frame Work Zones and Access Panels Zone Access/Work location From 210 Access Door 831, Door 841 To 220 Manpower Resources Manhours 3.00 Minimum number of person 1 Subtask elapsed time 3.00 Skills NON SPECIFIC Material necessary to do the job Kit 253213D02R02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 4 MS21250-03012 1 BOLT 5 NSA5379-3C 3 WASHER 6 DAN125-4 4 WASHER 7 NAS1102-08-6 4 SCREW 8 F2527496220200 1 WIREPROT 9 MS21250-03006 2 BOLT 11 MS21919WCH7 4 CLAMP 12 NAS1096-2-10 4 SCREW 13 MS21042L08 4 NUT 14 NAS1149CN832R 8 WASHER 26 NSA935401-03 3 TIE References Aircraft Maintenance Manual (AMM) Task 20-21-11-911-801 Elec. Std. Practices Manual (ESPM) 20-33-00 20-33-44 20-44-00 20-52-21 Structural Repair Manual (SRM) 51-42-00 DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 29 6

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

# @A330 SERVICE BULLETIN
References Fig. A-GBDAA Installation of the Cover on the Cockpit Door Frame Sheet 01 Sheet 02 Fig. A-GBEAA Installation of the Electrical Harness 7450VB Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Fig. A-GWAAA Wiring of the Electrical Harness 7450VB, pre SB A330-25-3213 Sheet 01 Fig. A-GWBAA Wiring of the Electrical Harness 7450VB, post SB A330-25-3213 Sheet 01 (a) Install the re-identified cover, Item 1, in accordance with SRM 51-42-00 and as shown on Fig. A-GBDAA Sheet 02 , with: 2 Bolt MS21250-03006 Item 9 2 Washer NSA5379-3C Item 5 and 1 Screw MS21250-03012 Item 4 1 Washer NSA5379-3C Item 5 (b) Install on the cover, Item 1, in accordance with SRM 51-42-00 and as shown on Fig. A-GBDAA Sheet 02 : 3 Cover Item (45) Retained at removal (c) Lead the electrical harness 7450VB, Item (2), to the cover of the cockpit door frame and the RH cockpit door post, as shown on Fig. A-GBEAA Sheet 02 , and Fig. AGBEAA Sheet 07 , View L. (d) Connect the electrical harness 7450VB: Refer to ESPM 20-33-00 1 Connect the wires of the electrical harness 7450VB, Item (2), to the release latches 30MQ, 31MQ and 32MQ, as shown on Fig. A-GBEAA Sheet 01 , Fig. A-GBEAA Sheet 03 and on this Wiring Diagram, Fig. A-GWAAA
. 2 If installed, connect the wires of the electrical harness 7450VB, Item (2), to the circuit breaker box 40MQ as shown on Fig. A-GBEAA Sheet 04 and on this Wiring Diagram, Fig. A-GWBAA DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 30 6

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

# @A330 SERVICE BULLETIN 3 Attach the wires, as shown on Fig. A-GBEAA Sheet 02 , Fig. A-GBEAA Sheet 03 , View D, E, F and Fig. A-GBEAA Sheet 04
. 4 Connect the wires of the electrical harness 7450VB, Item (2), to the limit switch 317LG, Item (38), as shown on this Wiring Diagram, Fig. A-GWBAA
. 5 Attach the additional wire length in a loop to the electrical harness 7450VB, as shown on Fig. A-GBEAA Sheet 07 , View L, with: Refer to ESPM 20-33-44 2 Cable Tie NSA935401-03 Item 26 (e) Install on the cover, Item 1, in accordance with SRM 51-42-00 and as shown on Fig. A-GBEAA Sheet 07 , View L: FIN 317LG 1 Limit Switch Item (38) Retained at removal attach with: 2 Screw Item (39) Retained at removal (f) Install on the RH cockpit door post, in accordance with SRM 51-42-00 and as shown on Fig. A-GBEAA Sheet 02 , Fig. A-GBEAA Sheet 03 , View D, E, F and Fig. A-GBEAA Sheet 04 : Refer to AMM Task 20-21-11-911-801 6 Clamp Item (35) Retained at removal 3 Clamp Item (36) Retained at removal 9 Spacer Item (37) Retained at removal attach with: 9 Screw Item (33) Retained at removal 9 Washer Item (34) Retained at removal NOTE : Install the spacers, Item (37), if retained at removal. 5 Spacer Item (31) Retained at removal attach with: DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 31 6

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

# @A330 SERVICE BULLETIN 10 Screw Item (32) Retained at removal 1 Secure Part Item (28) Retained at removal 1 Cover Plate Item (29) Retained at removal attach with: 6 Screw Item (30) Retained at removal NOTE : Before you install the secure part, Item (38), and the cover plate, Item (29), lead the wires of the key pad plug 25MQA through the hole of the secure part and cover plate as shown on Fig. A-GBEAA Sheet 06 , View J. (g) To the plug 25MQA, connect the wires and install as shown on Fig. A-GBEAA Sheet 06 , View K: Refer to ESPM 20-33-44 1 Plug Cover Item (27) Retained at removal 2 Screw with clamps Item (25) Retained at removal 1 Cable Tie NSA935401-03 Item 26 (h) Connect the plug 25MQA to the key pad 25MQ, refer to ESPM 20-44-00. (i) Install on the secure part of the RH cockpit door post, Item (28), in accordance with SRM 51-42-00 and as shown on Fig. A-GBEAA Sheet 02 and Fig. A-GBEAA Sheet 06 , View J: 1 Cover Item (20) Retained at removal attach with: 2 Screw Item (21) Retained at removal (j) Install on the cover, Item 1, in accordance with SRM 51-42-00 and as shown on Fig. A-GBEAA Sheet 07 , View L and N: 1 Wire Protection F2527496220200 Item 8 attach with: 4 Screw NAS1102-08-6 Item 7 DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 32 6

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

# @A330 SERVICE BULLETIN
4 Washer DAN125-4 Item 6 4 Screw NAS1096-2-10 Item 12 8 Washer NAS1149CN832R Item 14 4 Clamp MS21919WCH7 Item 11 4 Nut MS21042L08 Item 13 (k) Do a continuity test of the modified electrical wires, refer to ESPM 20-52-21. D. TEST (1) Subtask 253213-861-201-001 - Energize Electrical Network Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 21-26-00-710-803 Task 22-96-00-740-801 Task 22-97-00-740-801 Task 24-41-00-861-801 Task 31-50-00-710-803 Task 31-50-00-740-801 Task 31-60-00-710-802 Task 33-13-00-710-801 Task 33-14-00-710-801 Elec. Std. Practices Manual (ESPM) 20-52-20 (a) Job Set-up: 1 In the cockpit, on the panel 235VU, push these pushbutton switches: - GEN 1, GEN 2, - APU GEN (only if the A/C is energized from the external power). 2 Remove the warning notices. 3 Energize the aircraft electrical circuits, ref to AMM Task 24-41-00-861-801. NOTE : If the A/C is energized from the external power, make sure that the pushbutton switches BAT 1, BAT 2, APU BAT and EXT A (B) are pushed. NOTE : If the A/C is energized from APU, make sure that the pushbutton switches BAT 1, BAT 2, APU BAT and APU GEN are pushed.

DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 33 6

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

# @A330 SERVICE BULLETIN
4 Remove the safety clips and/or tags and close/unlock tag these circuit breakers: PANEL DESIGNATION FIN LOCATION SEE NOTES 742VU 701PP 10PB1 72 S 742VU 702PP 10PB2 71 S (b) Preliminary Tests: NOTE : If the aircraft is operated in actual CAT III conditions, you must also do the LAND CAT III capability test, refer to AMM Task 22-97-00-740-801 1 On each connector which was disconnected: - Do the checks as defined by ESPM 20-52-20. NOTE : The functional test and/or operational test requested by this ESPM procedure is g iven hereafter. 2 Do the Operational Test of the Instrument and Panel Integral Lighting, refer to AMM Task 33-13-00-710-801. 3 Do the Operational Test of Lights, refer to AMM Task 33-14-00-710-801. 4 Do the Operational Test of the Avionics-Equipment Ventilation System, refer to AMM Task 21-26-00-710-803. 5 Do the Bite Test of the Auto Flight System (SYSTEM TEST), refer to AMM Task 22-96-00-740-801. 6 Do the Operational Test of the Electronic Centralized Aircraft Monitoring (ECAM) Control Panel, refer to AMM Task 31-50-00-710-803. 7 Do the test of the Flight Warning System (FWS), refer to AMM Task 31-50-00-740-801. 8 Do the Operational Test of the Electronic Instrument System (EIS), refer to AMM Task 31-60-00-710-802. (2) Subtask 253213-700-209-001 - Test Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 52-51-00-710-801 Task 52-51-00-710-802 Task 52-51-00-710-803 Task 52-51-00-710-805 (a) Do the operational test of the Cockpit Door Lock System (CDLS), refer to AMM Task 52-51-00-710-801. DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 34 6

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

# @A330 SERVICE BULLETIN (b) Do the operational test of the cockpit door routine access, refer to AMM Task 52-51-00-710-802. (c) Do the operational test of the cockpit door emergency access, refer to AMM Task 52-51-00-710-803. (d) Do the functional decompression test on the control box 24MQ, refer to AMM Task 52-51-00-710-805. E. CLOSE-UP (1) Subtask 253213-942-209-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 23-72-51-400-801 (a) Install the Anti Hijack Camera 12RA (if removed on SUBTASK 253213-941-201 001 Job Set-up ), refer to AMM Task 23-72-51-400-801. (b) Make sure that the work areas are clean and clear of tools and other items of equipment. (c) Remove the access platform(s). (d) Put the aircraft back to its initial configuration.

DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 35 6

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

# @A330 SERVICE BULLETIN

This Page Intentionally Left Blank

DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 36 6

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

# @A330 SERVICE BULLETIN Task 253213-831-849-001 - Modification - Additional Work for Aircraft Modified by Revision No. 01 or any Previous Issue WARNING : MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE 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. NOTE : The accomplishment instructions of this Service Bulletin include procedures given in other documents or in other sections of the Service Bulletin. When the words ’refer to’ are used and the operator has procedure accepted by the local authorities he belongs to, the accepted alternative procedure can be used. When the words ’in accordance with’ are used then the given procedure must be followed. NOTE : The access and close-up instructions, not comprising return to service tests, in this Service Bulletin do not constitute or affect the technical intent of the Service Bulletin. Operators can therefore, as deemed necessary, omit or add access and/or close-up steps to add flexibility to their maintenance operations as long as the technical intent of the Service Bulletin is met within the set parameters. NOTE : Manual titles given in the accomplishment instructions are referred to by acronyms. Refer to paragraph 1.J., References, for the definition of acronyms. NOTE : This Service Bulletin contains the instructions for the on-aircraft maintenance necessary to ensure the continued airworthiness of the aircraft. For any deviations to the instructions contained herein, contact Airbus for repair instructions and approval. NOTE : Discarded parts must be managed at the operator’s discretion. Task Associated Data Zone 210 Manpower TOTAL MANHOURS 1.00 DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 37 6

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

# @A330 SERVICE BULLETIN A. GENERAL (1) Subtask 253213-910-202-001 - Standard Practices Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-20-00, Page Block 001 06-31-53, Page Block 001 Structural Repair Manual (SRM) 51-42-00, Page Block 001 (a) For the Frame (FR) identification, refer to AMM 06-31-53, Page Block 001. (b) For identification of the zones, refer to AMM 06-20-00, Page Block 001. (c) Remove and install fasteners, in accordance with SRM 51-42-00, Page Block 001. (d) Put all retained hardware in identified plastic bags and attach the bags to the related unit. (2) Subtask 253213-839-201-001 - Administrative Manpower Resources Skills NON SPECIFIC Write in the applicable aircraft records that you have done all the work given in this Service Bulletin. B. PREPARATION (1) Subtask 253213-941-202-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802 NOTE : The items given in this note shall be considered as the basic Aircraft configuration before you start a maintenance task: - Aircraft on the ground resting on landing gear (the ground safety locks and the wheel chocks are in position on the landing gear) - Engine shut down, thrust reversers closed and locked - Aircraft in clean configuration - Parking brake applied - Aircraft electrical network de-energized DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 38 6

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

# @A330 SERVICE BULLETIN - Hydraulic system s depressurized - Access to the cockpit and cabin is available - All circuit breakers are in closed position - All controls in NORM, AUTO or OFF position. (a) Make sure that the aircraft is electrically grounded, refer to AMM Task 12-34-24-860-802. C. PROCEDURE (1) Subtask 253213-831-204-001 - Replace the Fasteners of the Cover Work Zones and Access Panels Zone Access/Work location 210 Work location Frame 11 Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills NON SPECIFIC Material necessary to do the job Component COMPD01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 5 NSA5379-3C 3 WASHER 9 MS21250-03006 2 BOLT NOTE : The above list of components is not an AIRBUS Kit, the required parts shall be ordered as necessary through the given channel. NOTE : The components listed above are only necessary if ADDITIONAL WORK task is to be accomplished. The quantity of these items are to be ordered as required. References Structural Repair Manual (SRM) 51-42-00 Fig. A-GBFAA Replacement of the Fasteners of the Cover of the Cockpit Door Frame - ADDITIONAL WORK Sheet 01 Sheet 02

DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 39 6

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

# @A330 SERVICE BULLETIN (a) Remove, refer to Fig. A-GBFAA : 1 Remove from the cover, Item (1), in accordance with SRM 51-42-00 and as shown on Fig. A-GBFAA Sheet 01 , view A and Fig. A-GBFAA Sheet 02 , view B: 3 Cover Item (45) Retain 2 Screw Item (9) Discard 2 Washer Item (10) Discard 1 Screw Item (4) Retain 1 Washer Item (5) Discard (b) Install, refer to Fig. A-GBFAA : 1 Install in the cover, Item (1), in accordance with SRM 51-42-00, as shown on Fig. A-GBFAA Sheet 01 , view A and Fig. A-GBFAA Sheet 02 , view B: 2 Bolt MS21250-03006 Item 9 2 Washer NSA5379-3C Item 5 1 Screw Item (4) Retained at removal 1 Washer NSA5379-3C Item 5 2 Install on the cover, Item (1), in accordance with SRM 51-42-00, as shown on Fig. A-GBFAA Sheet 01 , view A and Fig. A-GBFAA Sheet 02 , view B: 3 Cover Item (45) Retained at removal D. TEST None E. CLOSE-UP (1) Subtask 253213-942-210-001 - Close-up Manpower Resources Skills NON SPECIFIC (a) Make sure that the work areas are clean and clear of tools and other items or equipment. (b) Put the aircraft back to its initial configuration.
DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 40 6

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

# @A330 SERVICE BULLETIN

**CONF ALL

FR16A FR12



### B B

32MQ 31MQ 30MQ
25MQ
−A KEYPAD 25MQ 317LG 6296VS

6294VS

6295VS FR11 

### A

C A Z220

40MQ 6297VS 1

1 NOTE: INSTALLED AFTER ACCOMPLISHMENT OF SERVICE BULLETIN A330
− 25
−3215. G_SB_253213_6_BAAA_01_00 Figure A-G BAAA - S heet 01 Removal of the Electrical Harness 7450VB DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 41 6

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

# @A330 SERVICE BULLETIN

**CONF ALL6296VS6295VS7450VBGGGGGEDCJJJHH6294VSHHHH5128VNTO 1181VC−A5259VN5199VN(1)(40)(2)(28)(29)(2)7450VB6297VS40MQLK1NOTE:INSTALLED AFTER ACCOMPLISHMENTOF SERVICE BULLETIN A330−25−3215.1(20)

G_SB_253213_6_BAAA_02_00 Figure A-G BAAA - S heet 02 Removal of the Electrical Harness 7450VB DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 42 6

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

# @A330 SERVICE BULLETIN

**CONF ALL

(6 POS.) 

### D

(29) (28) (30)

G_SB_253213_6_BAAA_03_00 Figure A-G BAAA - S heet 03 Removal of the Electrical Harness 7450VB DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 43 6

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

# @A330 SERVICE BULLETIN

**CONF ALL


### E

25MQ
−A



### F 25MQ
−A 

### F

(25) (25) (20)

7450VB 

### (21) (26) (27)
(2) (2)

G

7450VB 

### (2) (31) (32) J H

(37) (34) (33) (35) (36)

2

2 NOTE: REMOVE THE SPACER, ITEM (37), IF INSTALLED 

### (28)

VIEW H VIEW J

G_SB_253213_6_BAAA_04_00 Figure A-G BAAA - S heet 04 Removal of the Electrical Harness 7450VB DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 44 6

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

# @A330 SERVICE BULLETIN

**CONF ALL

40MQ

6297VS
− B,D,F 

### L

(2) K

317LG 

### (38)

(39)

1 NOTE: INSTALLED AFTER ACCOMPLISHMENT OF SERVICE BULLETIN A330
− 25
−3215. 1 

### (1)

7450VB

G_SB_253213_6_BAAA_05_00 Figure A-G BAAA - S heet 05 Removal of the Electrical Harness 7450VB DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 45 6

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

# @A330 SERVICE BULLETIN

**CONF ALL

FR16A FR12 

### A

B B

C (1) A Z220

G_SB_253213_6_BBAA_01_00 Figure A-G BBAA - S heet 01 Removal of the Cover from the Cockpit Door Frame DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 46 6

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

# @A330 SERVICE BULLETIN

**CONF ALL


### C

(45)

(41)

(45) (42) (43)

(45) (44) (1)

G_SB_253213_6_BBAA_02_00 Figure A-G BBAA - S heet 02 Removal of the Cover from the Cockpit Door Frame DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 47 6

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

# @A330 SERVICE BULLETIN

**CONF ALL



### (1) (46) BEFORE

(1) AFTER A B C

G_SB_253213_6_BCAA_01_00 Figure A-GBCAA - Sheet 01 Modification of the Cover of the Cockpit Door Frame DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 48 6

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

# @A330 SERVICE BULLETIN

**CONF ALL(0.51in.)13.0mm

(0.35in.)

R 9.0mm (0.50in.) 12.6mm

EDGES ROUNDED

EXISTING

DUCT(0.24in.)6.0mm (0.56in.) (14.3mm)

(0.20in.)

R 5.0mm

DUCT EXISTING 

### A B

(4.65in.)

118.0mm (12.72in.) 323.0mm (17.96in.) 458.0mm (20.79in.)

528.0mm(0.46in.)11.6mm



### A A C (0.57in.) 14.5mm DIA(0.38in.)9.5mm ADHESIVE (MAT.NO.08
− 010A) SECTION 

### A A 3

(1) (1) (1)

3 3 3 EDGES ROUNDED

G_SB_253213_6_BCAA_02_00 Figure A-GBCAA - Sheet 02 Modification of the Cover of the Cockpit Door Frame DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 49 6

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

# @A330 SERVICE BULLETIN

**CONF ALL

FR16A FR12 

### A

B B

C (1) A Z220

G_SB_253213_6_BDAA_01_00 Figure A-GBDAA - Sheet 01 Installation of the Cover on the Cockpit Door Frame DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 50 6

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

# @A330 SERVICE BULLETIN

**CONF ALL


### C

(45)

4

(45) 9 5

(45) 5 (1)

G_SB_253213_6_BDAA_02_01 Figure A-GBDAA - Sheet 02 Installation of the Cover on the Cockpit Door Frame DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 51 6

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

# @A330 SERVICE BULLETIN

**CONF ALL

FR16A FR12



### B B

FR11 

### A

C A Z220

32MQ 31MQ 30MQ
25MQ
−A KEYPAD 25MQ 317LG 6296VS

6294VS

6295VS 40MQ 6297VS 1

1 NOTE: INSTALLED AFTER ACCOMPLISHMENT OF SERVICE BULLETIN A330
− 25
−3215. G_SB_253213_6_BEAA_01_00 Figure A-G BEAA - S heet 01 Installation of the Electrical Harness 7450VB DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 52 6

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

# @A330 SERVICE BULLETIN

**CONF ALL6296VS6295VS7450VBDDDDDJHCFFFEE6294VSEEEE(28)(29)7450VB(2)(2)L6297VS40MQG1OF SERVICE BULLETIN A330−25−3215.INSTALLED AFTER ACCOMPLISHMENT1NOTE:(20)(1)

G_SB_253213_6_BEAA_02_00 Figure A-G BEAA - S heet 02 Installation of the Electrical Harness 7450VB DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 53 6

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

# @A330 SERVICE BULLETIN

**CONF ALL


### D

7450VB 

### F E

(2) (31) (37) (34) (33) (35) (36)
(32) 2

2 NOTE: INSTALL THE SPACER, ITEM (37) IF REMOVED. 6295VS C32MQ

4 5251
− 5165 (YY24) 2 1 5 6 (YY24) (YY18) 5251
− 5163 5251
− 5164 6295VS E 6295VS D 7450VB (YY20) 5251
− 5162 6295VS A (YY20) 5251
− 5161 6295VS B 6294VS C 6294VS E 4 6 5251
− 5159 5251
− 5160 (YY24) (YY24) 2 1 5 7 (YY24) (YY18) 5251
− 5157 5251
− 5158 6294VS F 6294VS D (YY20) 5251
− 5156 6294VS A (YY20) 5251
− 5155 6294VS B31MQ 6296VS C 4 5251
− 5154 (YY24) 2 1 5 6 (YY24) (YY18) 5251
− 5152 6296VS E 6296VS D (YY20) 5251
− 5151 6296VS A (YY20) 5251
− 5150 6296VS B30MQ
5251
− 5153 7450VB

7450VB VIEW E VIEW F

G_SB_253213_6_BEAA_03_00 Figure A-G BEAA - S heet 03 Installation of the Electrical Harness 7450VB DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 54 6

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

# @A330 SERVICE BULLETIN

**CONF ALL

40MQ

6297VS
− B,D,F 

### G

(2)

CONNECTION

CA L1 5251
− 5194 5251
− 5195 6297VS D 6297VS E U1 UA C1 5251
− 5192 5251
− 5193 6297VS C 7450VB 5251
− 5191 6297VS A40MQ

6297VS F LA 5251
− 5196 6297VS B

5251
− 5120 5251
− 5199 5251
− 5115 5251
− 5198 5251
− 5111 5251
− 5197

G_SB_253213_6_BEAA_04_00 Figure A-G BEAA - S heet 04 Installation of the Electrical Harness 7450VB DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 55 6

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

# @A330 SERVICE BULLETIN

**CONF ALL

(6 POS.) 

### H

(29) (28) (30)

G_SB_253213_6_BEAA_05_00 Figure A-G BEAA - S heet 05 Installation of the Electrical Harness 7450VB DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 56 6

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

# @A330 SERVICE BULLETIN

**CONF ALL 

### J

25MQ
−A



### K

25MQ
−A 

### K

(25) (25) (20)

7450VB 

### (21)

26 (27)
(2) (2)

5251
− 7900 R 1 5251
− 7900 B 2 5251
− 7901 R 3 5251
− 7901 B 4 5251
− 5102 7 5251
− 5101 8 5251
− 5107 9 5251
− 5108 10 5251
− 5104 11 5251
− 5100 1525MQ−A 

# CONNECTION
7450VB 7450VB
7450VB 7450VB 7450VB 7450VB 7450VB 7450VB 7450VB 7450VB G_SB_253213_6_BEAA_06_01 Figure A-G BEAA - S heet 06 Installation of the Electrical Harness 7450VB DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 57 6

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

# @A330 SERVICE BULLETIN

**CONF ALL


### L

317LG FROM 30MQ 31MQ 32MQ 25MQ 5128VN TO 1181VC
−A 5259VN 5199VN 7450VB 

### 26

N N N N 6 7 8

13 14

8 12 14 11 (2) (2)

N 4 3



### (38)

(39)

3 ATTACH THE ADDITIONAL
4 ADD 200.0mm (7,87in.) WIRE LENGHT IN A LOOP TO THE ELECTRICAL HARNESS. TO THE INSTALLATION LENGHT OF THE WIRE. 1 NOTE: INSTALLED AFTER ACCOMPLISHMENT OF SERVICE BULLETIN A330
− 25
−3215. 40MQ 1 

### (1)

G_SB_253213_6_BEAA_07_01 Figure A-G BEAA - S heet 07 Installation of the Electrical Harness 7450VB DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 58 6

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

# @A330 SERVICE BULLETIN

**CONF ALL



## A FR16A Z220

Z210 

### A

FR11 

### B

G_SB_253213_6_BFAA_01_00 Figure A-GBFAA - Sheet 01 Replacement of the Fasteners of the Cover of the Cockpit Door Frame - ADDITIONAL WORK

DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 59 6

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

# @A330 SERVICE BULLETIN

**CONF ALL

(1)

(45) (45) (45) (9) 9 (10)

5
(4) (5) 5



## B

G_SB_253213_6_BFAA_02_00 Figure A-GBFAA - Sheet 02 Replacement of the Fasteners of the Cover of the Cockpit Door Frame - ADDITIONAL WORK

DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 60 6

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

# @A330 SERVICE BULLETIN

**CONF ALL

15 8 B2 5199VN1 7

25MQ KEYPAD

LED2 5102
− CF18 1181VC A

DATA3 DATA2 DATA1 DATA0

4 3 2 1 GND VCC

10 9 LED1 7901
−TK24

7902
− SJ20

7903
− SJ20

7904
− SJ20 A

7900
−TK24

5111
− CF20

5115
− CF20

5120
− CF20 5 6 12 13 11

14 −S −T

− R

−Q

− N W

− K

−J

− I

− H

−G

− F − E

− D

− C

− B

−A Z Y X − M − P

30MQ UPPER RELEASE LATCH

31MQ CENTER RELEASE LATCH

32MQ LOWER RELEASE LATCH 2 1

2 1

2 1 B2 5259VN1 5 5122
− CF18

5 5124
− CF18

5 5126
− CF18 6

6

6 28DC2 5128VN1 4

4 7 4 5101 5100

5103

5105

5107 5108 5104

5106

5109

5112 5113

5118 6296VS

5123
− CF20

5125
− CF20

5127
− CF20 B2 5259VN1 28DC2 5128VN1

B2 5259VN1 28DC2 5128VN1 5116 5117

5121 R B

R B

6294VS

6295VS 5152
−YY18 5151
−YY20 5150
−YY20

5153
−YY24 5154
−YY24 5155
−YY20 5156
−YY20 5157
−YY18 5158
−YY24 5159
−YY24 5160
−YY24 5161
−YY20 5162
−YY20 5163
−YY18 5164
−YY24 5165
−YY24 B A D E C B A D F C E B A D E C EXISTING WIRE

317LG COCKPIT DOOR SWITCH OPEN 1 2 3 3321
−5919
− CF20 3321
−5920
− CF20 B C UNLESS OTHERWISE SPECIFIED PREFIX ALL WIRE IDENTIFICATION WITH ATA NO 5251. UNLESS OTHERWISE SPECIFIED ALL WIRES CF24 GAUGE. UNLESS OTHERWISE SPECIFIED ALL ROUTES ARE 2M. NOTE:

G_SB_253213_6_WAAA_01_00 Figure A-GWAAA - Sheet 01 Wiring of the Electrical Harness 7450VB, pre SB A330-25-3213 DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 61 6

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

# @A330 SERVICE BULLETIN

**CONF ALL

15 8 B2 5199VN1 7

25MQ KEYPAD

LED2 5102
− CF18 1181VC A

DATA3 DATA2 DATA1 DATA0
4 3 2 1 GND VCC

10 9 LED1 7901
−TK24

7902
− SJ20

7903
− SJ20

7904
− SJ20 A

7900
−TK24

5111
− CF20

5115
− CF20

5120
− CF20 5 6 12 13 11

14 −S −T

− R

−Q

− N W

− K

−J

− I

− H

−G

− F − E

− D

− C

− B

−A Z Y
X − M − P

30MQ UPPER RELEASE LATCH

31MQ CENTER RELEASE LATCH

32MQ LOWER RELEASE LATCH 2 1

2 1

2 1 B2 5259VN1 5 5122
− CF18

5 5124
− CF18

5 5126
− CF18 6

6

6 28DC2 5128VN1 4

4 7 4 5101 5100

5103 5105
5107 5108 5104 5106

5109

5112

5113

5118 6296VS

5123
− CF20

5125
− CF20

5127
− CF20 B2 5259VN1 28DC2 5128VN1

B2 5259VN1 28DC2 5128VN1 5116 5117

5121 R B R B

6294VS

6295VS 5152
−YY18 5151
−YY20 5150
−YY20 5153
−YY24 5154
−YY24

5155
−YY20 5156
−YY20 5157
−YY18 5158
−YY24 5159
−YY24 5160
−YY24

5161
−YY20 5162
−YY20 5163
−YY18 5164
−YY24 5165
−YY24 B A D E C

B A D F C E

B A D E C 317LG/COCKPIT DOOR SWITCH OPEN 1 2 3 3321
−5925
− CF20 3321
−5926
− CF20 B C UNLESS OTHERWISE SPECIFIED PREFIX ALL WIRE IDENTIFICATION WITH ATA NO 5251. UNLESS OTHERWISE SPECIFIED ALL WIRES CF24 GAUGE. UNLESS OTHERWISE SPECIFIED ALL ROUTES ARE 2M. NOTE:TTT1.5A1.5A1.5A5191−YY20 U15192−YY20 UA5193−YY20 C15194−YY20 CA5195−YY20 L15196−YY20 LAABCDEF6297VS 40MQ CIRCUIT BREAKER BOX

5197
− CF20

5198
− CF20

5199
− CF20
G_SB_253213_6_WBAA_01_00 Figure A-GWBAA - Sheet 01 Wiring of the Electrical Harness 7450VB, post SB A330-25-3213 DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 62 6

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

# @A330 SERVICE BULLETIN REPORTING SHEET 

### TITLE: EQUIPMENT/FURNISHINGS - PAX COMPARTMENT - MODIFY CDLS WIRING LOOM IN UPPER COCKPIT DOOR PLATE COVER MODIFICATION No.: 51911D44499 Please complete the appropriate item (A or B): A - SB WILL BE embodied YES/NO (if NO please comment) If YES, aircraft concer ned (as per SB effectivity by default) and planned dates (month/year) of embodiment:
B - SB HAS BEEN embodied on aircraft: Operator comments: From Airline: Name/Title: Signature: Date: If operational documentation is affected (see Paragraph 1.K of this SB): If information is needed prior to next normal revision or prior to SB embodiment, please indicate required service(s): Either: Modification Operational Impact (MOI), if available YES/NO Or : Intermediate revision YES/NO Important Information: This SB will only be incorporated in your maintenance and operational documentation if this sheet is returned to Airbus and signed by a duly authorised representative. With the next feasible revision, this will result in - Updating of maintenance documentation to show pre and post SB data. - Updating of maintenance and operational documentation to show post SB data after embodiment. If this SB requires previous or simultaneous accomplishment of other SBs, Airbus shall automatically include them in the manual revisions. Refer to SIL 00-037 for detailed information. Please return this completed sheet to: AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Attn: SDC32 Technical Data and Documentation Services FAX: (+33) 5 61 93 28 06 e-mail: sb.reporting@airbus.com or via your Resident Customer Support Office. Alternatively, SB lists via letters or fax are also accepted.

DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 1 6

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

# @A330 SERVICE BULLETIN QUALITY PERCEPTION FORM Use this form to tell us what is your perception of the quality of this Service Bulletin. The reported data that you provide us will be used to analyse areas of difficulties and to take corrective action to further improve the quality of our Service Bulletins. We thank you for the time you have taken in completing this form. (Please rate on a scale of 1 to 4, with 4 being the highest score) - Quality rating of this SB 4321 - Quality rating of the Accomplishment Instructions 4321 - Quality rating of the Illustrations 4321 - Is this SB easy to understand ? Y/N If you have had difficulties in the accomplishment of this SB please quote below the area(s) and give a short description of the issue. Planning Material Instructions X Effectivity X Kit content X Preparation X Reason X List of Materials Operator Supplied X Mod/Inspection X Manpower X Industry support X Test X References X Re-identification X Close-Up X Publication X Tooling X Illustrations Comments:

Operator: Date: Name/Title: Please return this form to: AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Attn : SEM4 Service Bulletins Management FAX : (33) 5 61 93 42 51 Or via your Resident Customer Support Office.

DATE: Oct 12/04 SERVICE BULLETIN No.: A330-25-3213 REVISION No.: 02 - Aug 12/16 Page: 1 6

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