@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

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 33

TITLE: LIGHTS - SERVICE AREA LIGHTING - REMOVE SERVICE AREA

LIGHTS IN SECTION 19 ACCORDING TO SFAR 88 REQUIREMENTS.

MODIFICATION No.: 201683D46730

This page transmits Revision No.01 of Service Bulletin No.A330-33-3041

ADDITIONAL WORK

**CONF ALL

REASON

The Revision No.01 issued to:

- update the effectivity.

- amend the KitD02.

CHANGES

SUMMARY

MATERIAL PRICE INFORMATION MATERIAL PRICE INFORMATION TABLE

UPDATED

R

MATERIAL PRICE INFORMATION TABLE

UPDATED

R

MATERIAL PRICE INFORMATION TABLE

UPDATED

R

EFFECTIVITY OPERATOR LIST UPDATED R

PLANNING INFORMATION

EFFECTIVITY EFFECTIVITY RELATED INFORMATION

UPDATED

R

Configuration definition

CONF 002 CONFIGURATION DEFINITION UPDATED R

Material Effectivity MATERIAL EFFECTIVITY UPDATED R

MATERIAL EFFECTIVITY UPDATED

MATERIAL SET UPDATED

R

DATE: Jan 03/12 SERVICE BULLETIN No.: A330-33-3041

REVISION No.: 01 - Jul 10/12 Page: 1

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

MATERIAL INFORMATION

MATERIAL - PRICE AND AVAILABILITY

Procurement Addresses PROCUREMENT ADDRESSES UPDATED

MATERIAL SET UPDATED

R

Price and Availability PRICE AND AVAILABILITY UPDATED

MATERIAL AVAILABILITY UPDATED

MATERIAL PRICE UPDATED

MATERIAL SET UPDATED

R

LIST OF COMPONENTS

Kit 333041D02R01 PART MATERIAL SET UPDATED

MATERIAL SET LABEL UPDATED

PART NUMBER UPDATED

R

ACCOMPLISHMENT INSTRUCTIONS

TASK 333041- 831-848-001-Modification

Subtask 333041-831-205-002 SUBTASK SOLUTION UPDATED

PART NUMBER UPDATED

MATERIAL LIST UPDATED

R

FILLING INSTRUCTIONS

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

Replace the complete document.

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

HISTORY OF PREVIOUS REVISIONS

No previous revision

REVISION SEQUENCE

ORIGINAL: Jan 03/12

REVISION No. : 01 - Jul 10/12

DATE: Jan 03/12 SERVICE BULLETIN No.: A330-33-3041

REVISION No.: 01 - Jul 10/12 Page: 2

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.

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 33

TITLE: LIGHTS - SERVICE AREA LIGHTING - REMOVE SERVICE AREA

LIGHTS IN SECTION 19 ACCORDING TO SFAR 88 REQUIREMENTS.

**CONF ALL

MODIFICATIONS

MODIFICATION CLASSIFICATION

MAJOR None

MINOR 201683D46730

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

To obey SFAR88 instructions for in-service aircraft, the maintenance lights in section 19 (5LJ, 6LJ, 7LJ

and 8LJ) are to be removed.

This Service Bulletin gives the procedure to remove the maintenance lights 5LJ, 6LJ, 7LJ and 8LJ.

The affected circuit breakers are to be opened and safetied. Related wires and connections that

are no longer used are to be stowed properly. Installation positions (for unit installation and ground

connections) must be protected with sealants and anti-corrosion treatments as applicable.

With the accomplishment of this Service Bulletin the applicable aircraft obey the instructions of SFAR88

for the de-activation of maintenance maintenance lights 5LJ, 6LJ, 7LJ and 8LJ.

GENERAL EVALUATION

EVALUATION TABLE

COMPLIANCE MANDATORY (1) CANCELS INSPECTION SB NO

POTENTIAL AD YES A/C OPERATION AFFECTED NO

RELIABILITY AFFECTED NO PAX COMFORT AFFECTED NO

COST SAVING NO ETOPS AFFECTED NO

STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED NO

NOTE (1): Service Bulletin must be accomplished.

DATE: Jan 03/12 SERVICE BULLETIN No.: A330-33-3041

REVISION No.: 01 - Jul 10/12 Page: 1

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@A330

SERVICE BULLETIN

SUMMARY

MATERIAL PRICE INFORMATION

**CONF 001

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 333041D01R02 1 242.00 Caps, clip, placard set and ties

**CONF 002

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 333041D01R02 1 242.00 Caps, clip, placard set and ties

**CONF 003

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 333041D01R02 1 242.00 Caps, clip, placard set and ties

Kit 333041D02R01 1 37.00 Clamp, washer, screw and spacer

TOTAL 279.00

EFFECTIVITY

**CONF ALL

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

46W AAR ACA ACI AEA AFL AFR ALK ASY AVA AZA BEC BEL

BER BMA BTV CAL CCA CES CHH CPA CRL CSC CSN DAH DAL

DGA DLH EDW EIN ETD EVA FWI GFA GIA GRL HDA HFY HVN

I2L IAC ISS IWD IYE JAI JAV JST KAL KFR KKK KLM MAS

MAU MEA MON MSR OBS OHY P2C PAL QAF QFA QTR RJA RSY

SAS SIA SWR TAM TAP TCX THA THY TSC UAE USA VKG VLK

VOZ XAX XLF

CONCURRENT REQUIREMENTS

None

REFERENCES / REPERCUSSIONS

TFU None

OEB None

AOT None

SIL None

LINE MAINTENANCE AFFECTED No

LIFE LIMIT None

DATE: Jan 03/12 SERVICE BULLETIN No.: A330-33-3041

REVISION No.: 01 - Jul 10/12 Page: 2

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Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

SUMMARY

OTHER None

NATURE OF THE WORK

AIRCRAFT NO

EQUIPMENT YES

HARD NO

SOFT NO

OBRM NO

MANPOWER

**CONF 001

Task 333041-831-848-001: Modification

TOTAL MANHOURS 5.75

ELAPSED TIME (HOURS) 5.75

**CONF 002

Task 333041-831-848-001: Modification

TOTAL MANHOURS 5.75

ELAPSED TIME (HOURS) 5.75

**CONF 003

Task 333041-831-848-001: Modification

TOTAL MANHOURS 5.75

ELAPSED TIME (HOURS) 5.75

APPENDICES

**CONF ALL

None

DATE: Jan 03/12 SERVICE BULLETIN No.: A330-33-3041

REVISION No.: 01 - Jul 10/12 Page: 3

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Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

SUMMARY

**CONF ALL

Z270

A

FR77

FR75

FR72

5005VE

FR76

A

Z310

FR83

FR87

4LJ

FR84

5872VB /2M

FR85

BEFORE

6LJ

5012VN /DC2 FR88

7LJ

8LJ

5315VN /DC2

5420VN /DC2

5LJ

5011VN /DC2

B

C

B C

D

D

D

D

5LJ

6LJ

7LJ

8LJ

LH

RH

LH

RH

D

TYPICAL

AFTER

TYPICAL

E

E

5872VB /2M

G_SB_333041_6_SAAA_01_01

Figure A-GSAAA - Sheet 01

DATE: Jan 03/12 SERVICE BULLETIN No.: A330-33-3041

REVISION No.: 01 - Jul 10/12 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

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 33

TITLE: LIGHTS - SERVICE AREA LIGHTING - REMOVE SERVICE AREA

LIGHTS IN SECTION 19 ACCORDING TO SFAR 88 REQUIREMENTS.

MODIFICATION No.: 201683D46730

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

This modification is applicable by Service Bulletin only.

(1) Models

330-202 330-203 330-223 330-243 330-301 330-302 330-303 330-321

330-322 330-323 330-341 330-342 330-343

(2) Effectivity by MSN

0012 0017 0030 0037 0045 0050 0054-0055 0060 0062 0064-0067 0069-0073 0077

0082-0083 0086-0087 0095-0096 0098-0100 0102 0106-0107 0109-0113 0116

0118-0122 0127 0132 0138 0140 0143-0144 0148 0153 0155 0162 0165 0171-0172

0177 0181 0183-0184 0188-0189 0191 0195 0198 0200 0203 0205-0206 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

DATE: Jan 03/12 SERVICE BULLETIN No.: A330-33-3041

REVISION No.: 01 - Jul 10/12 Page: 1

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@A330

SERVICE BULLETIN

0489-0491 0493-0494 0496-0498 0500-0513 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 0573-0574 0576 0578-0579 0581 0584 0587-0588

0591 0593 0595 0597 0600 0602-0603 0605 0607 0609-0610 0612 0614 0616 0618

0620-0621 0623 0625 0627 0629 0631-0638 0640-0642 0644-0645 0647-0650

0652-0659 0661-0667 0669-0671 0673-0676 0678-0680 0682-0684 0686-0688

0690-0693 0695-0697 0699-0701 0703-0705 0707-0709 0711-0714 0716-0718

0720-0722 0724-0726 0728-0730 0732-0735 0737-0739 0741-0743 0745-0747

0749-0752 0754-0756 0758-0760 0769-0770 0772-0774 0776-0778 0780-0782

0784-0786 0788-0789 0791-0792 0795-0797 0799 0801-0803 0805-0807 0809-0811

0813-0815 0817-0828 0830-0834 0836 0838-0843 0845 0847 0849-0855 0857-0863

0865-0869 0871 0873-0877 0879 0881-0885 0887-0893 0895-0896 0898-0901

0903-0909 0911 0913-0916 0918-0920 0922-0923 0926-0928 0930-0932 0934-0937

0939-0952 0954 0956-0959 0961-0971 0973-0979 0982-0986 0988-0991

(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

46W 0871

AAR 0640 0676 0708 0772 0803 0845

ACA 0277 0279 0284 0344 0400 0408 0412 0419

ACI 0507 0510

AEA 0461 0505 0526 0551 0597 0733 0745 0749 0814 0931 0950

AFL 0963 0973

AFR 0422 0443 0448 0458 0465 0481 0498 0500 0502 0503 0516 0519

0567 0584 0657

ALK 0303 0306 0311 0313 0404 0456 0627

ASY 0747 0951 0969

AVA 0948 0967

AZA 0272 0339

BEC 0863

BEL 0030 0037 0045 0082 0095 0229 0249

BER 0120 0127 0288 0322 0403 0432 0444 0454 0469 0476 0493 0739

0828 0911

BMA 0398 0401

BTV 0205 0330

CAL 0602 0607 0641 0671 0675 0691 0699 0707 0714 0725 0752 0769

0805 0823 0838 0861 0920

CCA 0750 0756 0759 0780 0785 0797 0810 0815 0839 0860 0867 0873

0884 0890 0903 0909 0930 0941 0944 0957

CES 0713 0720 0728 0732 0735 0773 0777 0781 0782 0791 0821 0830

0836 0851 0862 0866 0916 0928 0936 0942

CHH 0875 0881 0906 0919 0982

DATE: Jan 03/12 SERVICE BULLETIN No.: A330-33-3041

REVISION No.: 01 - Jul 10/12 Page: 2

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Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

OPERATOR MSN

CPA 0012 0017 0071 0102 0113 0118 0121 0155 0244 0386 0389 0393

0418 0420 0421 0423 0439 0539 0548 0565 0669 0673 0679 0776

0850 0855 0895 0915 0959

CRL 0285 0320

CSC 0462

CSN 0649 0652 0656 0664 0818 0840 0879 0889 0908 0935 0937 0954

0958 0964

DAH 0644 0647 0650 0653 0667

DAL 0524 0533 0542 0549 0552 0578 0588 0591 0609 0614 0618 0620

0621 0631 0633 0663 0674 0690 0718 0722 0778 0784 0796 0799

0806 0817 0827 0843 0857 0858 0859 0865

DGA 0240

DLH 0570 0576 0579 0629 0636 0642 0645 0648 0687 0701 0896 0905

0913 0922 0989

EDW 0291

EIN 0269 0397 0841 0847 0985

ETD 0658 0688 0717 0724 0729 0730 0737 0751 0788 0809 0824 0832

0852 0854 0868 0975 0991

EVA 0530 0535 0555 0573 0587 0634 0655 0661 0678 0693 0755

FWI 0253 0758 0965

GFA 0276 0281 0286 0287 0334 0340 0527 0529 0532

GIA 0138 0140 0144 0148 0153 0165 0988

GRL 0230

HDA 0083 0099 0106 0109 0234 0405 0479 0512 0581 0654 0662 0692

0716 0741 0786

HFY 0096 0211

HVN 0262 0275 0294 0299 0366 0943 0962

I2L 0364

IAC 0353 0362

ISS 0665 0802 0822

IWD 0670

IYE 0625 0632

JAI 0807 0825 0831 0882 0885 0888 0901 0923 0932 0947 0956

JAV 0255

JST 0506 0508 0513 0522 0842 0853 0940 0945

KAL 0162 0172 0206 0219 0222 0226 0241 0256 0258 0267 0338 0350

0351 0368 0425 0428 0484 0490 0550

KFR 0874 0939 0946

KKK 0343 0358

KLM 0682 0686 0703 0738 0770 0801 0811 0819 0834 0900

MAS 0067 0069 0073 0077 0100 0107 0110 0116 0119 0290 0296 0300

MAU 0883

MEA 0926 0984

MON 0261 0265

MSR 0600 0610 0666 0683 0696 0709 0726

OBS 0833

OHY 0072 0087 0098 0143

DATE: Jan 03/12 SERVICE BULLETIN No.: A330-33-3041

REVISION No.: 01 - Jul 10/12 Page: 3

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@A330

SERVICE BULLETIN

OPERATOR MSN

P2C 0891 0927

PAL 0183 0184 0188 0189 0191 0198 0200 0203

QAF 0487 0605

QFA 0553 0558 0564 0574 0593 0595 0603 0695 0705 0712 0887 0892

0898 0976

QTR 0441 0473 0489 0511 0521 0571 0612 0616 0623 0637 0638 0659

0680 0684 0711 0721 0734 0743 0746 0760 0789 0792 0813 0820

0826 0849 0893 0907 0918

RJA 0970 0979

RSY 0171

SAS 0496 0497 0515 0568

SIA 0978 0983 0986

SWR 0324

TAM 0232 0238 0247 0259 0361 0466 0472 0477 0486 0700 0869 0876

0949 0961 0968 0977

TAP 0181 0195 0223 0305 0308 0312 0317 0877 0899 0904 0914 0934

TCX 0254 0266 0301

THA 0050 0060 0062 0064 0065 0066 0112 0122 0209 0224 0231 0346

0990

THY 0463 0504 0697 0704 0742 0754 0774

TSC 0111 0132 0177 0250 0271 0369 0407 0427 0480 0795 0966 0971

UAE 0248 0251 0283 0293 0295 0314 0316 0326 0328 0345 0348 0382

0384 0392 0396 0409 0437 0451 0452 0455 0491 0494 0509 0518

0525 0536

USA 0315 0323 0333 0337 0342 0370 0375 0380 0388

VKG 0309 0349 0356 0357

VLK 0055 0070 0086

VOZ 0365 0372

XAX 0054 0952 0974

XLF 0501 0635

(4) Configuration by MSN

MSN CONFIGURATION

0012 0017 0030 0037 0045 0050 0054 0055 0060 0062 0064

0065 0066 0067 0069 0070 0071 0072 0073 0077 0082 0083

0086 0087 0095 0096 0098 0099 0100 0102 0106 0107 0109

0110 0111 0112 0113 0116 0118 0119 0120 0121 0122 0127

0132 0138 0140 0143 0144 0148 0153 0155 0162 0165 0171

0172 0177 0183 0184 0188 0189 0191

003

0181 0195 0198 0200 0203 0205 0206 0209 0211 0219 0222

0223 0224 0226 0229 0230 0231

001

DATE: Jan 03/12 SERVICE BULLETIN No.: A330-33-3041

REVISION No.: 01 - Jul 10/12 Page: 4

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@A330

SERVICE BULLETIN

MSN CONFIGURATION

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 0502 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 0574 0576 0578

0579 0581 0584 0587 0588 0591 0593 0595 0597 0600 0602

0603 0605 0607 0609 0610 0612 0614 0616 0618 0620 0621

0623 0625 0627 0629 0631 0632 0633 0634 0635 0636 0637

0638 0640 0641 0642 0644 0645 0647 0648 0649 0650 0652

0653 0654 0655 0656 0657 0658 0659 0661 0662 0663 0664

0665 0666 0667 0669 0670 0671 0673 0674 0675 0676 0678

0679 0680 0682 0683 0684 0686 0687 0688 0690 0691 0692

0693 0695 0696 0697 0699 0700 0701 0703 0704 0705 0707

0708 0709 0711 0712 0713 0714 0716 0717 0718 0720 0721

0722 0724 0725 0726 0728 0729 0730 0732 0733 0734 0735

0737 0738 0739 0741 0742 0743 0745 0746 0747 0749 0750

0751 0752 0754 0755 0756 0758 0759 0760 0769 0770 0772

0773 0774 0776 0777 0778 0780 0781 0782 0784 0785 0786

0788 0789 0791 0792 0795 0796 0797 0799 0801 0802 0803

0805 0806 0807 0809 0810 0811 0813 0814 0815 0817 0818

0819 0820 0821 0822 0823 0824 0825 0826 0827 0828 0830

0831 0832 0833 0834 0836 0838 0839 0840 0841 0842 0843

0845 0847 0849 0850 0851 0852 0853 0854 0855 0857 0858

0859 0860 0861 0862 0863 0865 0866 0867 0868 0869 0871

0873 0874 0875 0876 0877 0879 0881 0882 0883 0884 0885

0887 0888 0889 0890 0891 0892 0893 0895 0896 0898 0899

0900 0901 0903 0904 0905 0906 0907 0908 0909 0911 0913

0914 0915 0916 0918 0919 0920 0922 0923 0926 0927 0928

0930 0931 0932 0934 0935 0936 0937 0939 0940 0941 0942

0943 0944 0945 0946 0947 0948 0949 0950 0951 0952 0954

0956 0957 0958 0959 0961 0962 0963 0964 0965 0966 0967

0968 0969 0970 0971 0973 0974 0975 0976 0977 0978 0979

0982 0983 0984 0985 0986 0988 0989 0990 0991

002

DATE: Jan 03/12 SERVICE BULLETIN No.: A330-33-3041

REVISION No.: 01 - Jul 10/12 Page: 5

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Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

(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.

**CONF 002

Config. 002 is valid for all the aircraft given in the effectivity of this Service Bulletin as a

standard configuration.

**CONF 003

Config. 003 is valid for all the aircraft given in the effectivity of this Service Bulletin as a

standard configuration.

(6) Material Effectivity

NOTE: The Kit 333041D01R02 and the Kit 333041D02R01 are not necessary, if

Service Bulletin No. A330-33-3042 will be embodied at the same time.

**CONF 001 thru 002

MATERIAL QTY PER A/C SEE NOTES

Kit 333041D01R02 1

Consumable CMLD01 1

**CONF 003

MATERIAL QTY PER A/C SEE NOTES

Kit 333041D01R02 1

Kit 333041D02R01 1

Consumable CMLD01 1

**CONF ALL

B. CONCURRENT REQUIREMENTS

None

C. REASON

(1) History

To obey SFAR88 instructions for in-service aircraft, the maintenance lights in section 19

(5LJ, 6LJ, 7LJ and 8LJ) are to be removed.

(2) Objective/Action

This Service Bulletin gives the procedure to remove the maintenance lights 5LJ, 6LJ,

7LJ and 8LJ. The affected circuit breakers are to be opened and safetied. Related wires

and connections that are no longer used are to be stowed properly. Installation positions

(for unit installation and ground connections) must be protected with sealants and anticorrosion treatments as applicable.

DATE: Jan 03/12 SERVICE BULLETIN No.: A330-33-3041

REVISION No.: 01 - Jul 10/12 Page: 6

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

(3) Advantages

With the accomplishment of this Service Bulletin the applicable aircraft obey the

instructions of SFAR88 for the de-activation of maintenance maintenance lights 5LJ, 6LJ,

7LJ and 8LJ.

(4) Operational/Maintenance Consequences

None

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

**CONF 001

Task 333041-831-848-001: Modification

(1) Modify the circuit breaker panel 5005VE

(2) Modify the electrical wiring of the button toggle 4LJ

(3) Remove the maintenance light 5LJ and modify the electrical wire

(4) Remove the maintenance light 6LJ and modify the electrical wire

(5) Remove the maintenance lights 7LJ and 8LJ and modify the electrical wires

**CONF 002

Task 333041-831-848-001: Modification

(1) Modify the circuit breaker panel 5005VE

(2) Modify the electrical wiring of the button toggle 4LJ

(3) Remove the maintenance light 5LJ and modify the electrical wire

(4) Remove the maintenance light 6LJ and modify the electrical wire

(5) Remove the maintenance lights 7LJ and 8LJ and modify the electrical wires

**CONF 003

Task 333041-831-848-001: Modification

(1) Modify the circuit breaker panel 5005VE

(2) Modify the electrical wiring of the button toggle 4LJ

(3) Remove the maintenance light 5LJ and modify the electrical wire

(4) Remove the maintenance light 6LJ and modify the electrical wire

DATE: Jan 03/12 SERVICE BULLETIN No.: A330-33-3041

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(5) Remove the maintenance lights 7LJ and 8LJ and modify the electrical wires

**CONF ALL

E. COMPLIANCE

(1) Classification

MANDATORY: Service Bulletin must be accomplished.

(2) Accomplishment Timescale

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

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

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

F. APPROVAL

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

**CONF 001

Task 333041-831-848-001: Modification

Get Access 0.25

On Aircraft

Modify the circuit breaker panel 5005VE 0.25

Modify the electrical wiring of the button toggle 4LJ 0.50

Remove the maintenance light 5LJ and modify the

electrical wire

1.00

Remove the maintenance light 6LJ and modify the

electrical wire

1.00

Remove the maintenance lights 7LJ and 8LJ and

modify the electrical wires

2.00

Tests 0.50

Close-Up 0.25

TOTAL MANHOURS 5.75

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Task 333041-831-848-001: Modification

ELAPSED TIME (HOURS) 5.75

**CONF 002

Task 333041-831-848-001: Modification

Get Access 0.25

On Aircraft

Modify the circuit breaker panel 5005VE 0.25

Modify the electrical wiring of the button toggle 4LJ 0.50

Remove the maintenance light 5LJ and modify the

electrical wire

1.00

Remove the maintenance light 6LJ and modify the

electrical wire

1.00

Remove the maintenance lights 7LJ and 8LJ and

modify the electrical wires

2.00

Tests 0.50

Close-Up 0.25

TOTAL MANHOURS 5.75

ELAPSED TIME (HOURS) 5.75

**CONF 003

Task 333041-831-848-001: Modification

Get Access 0.25

On Aircraft

Modify the circuit breaker panel 5005VE 0.25

Modify the electrical wiring of the button toggle 4LJ 0.50

Remove the maintenance light 5LJ and modify the

electrical wire

1.00

Remove the maintenance light 6LJ and modify the

electrical wire

1.00

Remove the maintenance lights 7LJ and 8LJ and

modify the electrical wires

2.00

Tests 0.50

Close-Up 0.25

TOTAL MANHOURS 5.75

ELAPSED TIME (HOURS) 5.75

**CONF ALL

H. WEIGHT AND BALANCE

**CONF 001 thru 002

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

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

MEW and operator’s items refer to Weight and Balance Manual (WBM) Chapter 1-00-07.

DATE: Jan 03/12 SERVICE BULLETIN No.: A330-33-3041

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Only for aircraft model A330-200

Manufactures Empty Weight -1.558 KG -3.4347 LB

Effect on Balance -88.569 KGM -640.619 LB.FT

Only for aircraft model A330-300

Manufactures Empty Weight -1.558 KG -3.4347 LB

Effect on Balance -96,870 KGM -700.660 LB.FT

**CONF 003

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

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

MEW and operator’s items refer to Weight and Balance Manual (WBM) Chapter 1-00-07.

Manufacturers Empty Weight -1.550 KG (-3.4171 LB)

Effect on Balance -96.356 KGM (-696.943 LB.FT )

**CONF ALL

I. ELECTRICAL LOAD DATA

Not Changed

J. REFERENCES

**CONF 001

Aircraft Maintenance Manual (AMM) 06-20-00 06-31-53 06-41-53

12-34-24 20-16-00 20-28-00

24-41-00 31-18-00 33-31-00

33-31-11 52-10-00

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-25-51 20-33-00 20-33-44

20-42-13 20-51-21 20-51-22

20-54-55 20-55-00

Service Bulletin (SB) A330-33-3042

Standards Manual (SM)

Weight and Balance Manual (WBM) Weight and Balance Manual

(WBM) Chapter 1-00-07

**CONF 002

Aircraft Maintenance Manual (AMM) 06-20-00 06-31-53 06-41-53

12-34-24 20-16-00 20-28-00

24-41-00 31-18-00 33-31-00

33-31-11 52-10-00

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-25-51 20-33-00 20-33-44

20-42-13 20-51-21 20-51-22

20-54-55 20-55-00

Service Bulletin (SB) A330-33-3042

Standards Manual (SM)

DATE: Jan 03/12 SERVICE BULLETIN No.: A330-33-3041

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Weight and Balance Manual (WBM) Weight and Balance Manual

(WBM) Chapter 1-00-07

**CONF 003

Aircraft Maintenance Manual (AMM) 06-20-00 06-31-53 06-41-53

12-34-24 20-16-00 20-28-00

24-41-00 31-18-00 33-31-00

33-31-11 52-10-00

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-25-51 20-33-00 20-33-44

20-42-13 20-51-21 20-51-22

20-54-55 20-55-00

Service Bulletin (SB) A330-33-3042

Standards Manual (SM)

Weight and Balance Manual (WBM) Weight and Balance Manual

(WBM) Chapter 1-00-07

**CONF ALL

K. PUBLICATION AFFECTED

Aircraft Maintenance Manual (AMM) 33-31-00 33-31-11

Aircraft Schematic Manual (ASM) 33-31-00

Illustrated Parts Catalog (IPC) 33-31-04

L. INTERCHANGEABILITY/MIXABILITY

Not Applicable

M. SPARES

None

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This Page Intentionally Left Blank

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2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

(1) Procurement Addresses

Kit 333041D01R02

Kit 333041D02R01

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 ordering by fax : +49 40 50 76 25 90

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

(2) Price and Availability

Kit 333041D01R02

Cost 242.00 USD

Availability 45 calendar days from receipt of order

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

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

your order so that we can try to comply with your requirements. The sales terms (costs

and availability) are estimated in relation to economic conditions at the issue date of

the Service Bulletin. 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.

Kit 333041D02R01

Cost 37.00 USD

Availability 45 calendar days from receipt of order

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

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

your order so that we can try to comply with your requirements. The sales terms (costs

and availability) are estimated in relation to economic conditions at the issue date of

the Service Bulletin. 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.

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C. LIST OF COMPONENTS

Kit 333041D01R02

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

NOTES

1 NSA936603CC0100 5 CAP

2 NSA935401-03 15 TIE

3 ABS0772A01A 1 CLIP

4 F9239025710000 1 PLCRDSET

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

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

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

to part number relationship.

Kit 333041D02R01

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

NOTES

5 MS21919WCH2 2 CLAMP

6 NAS1149C0332R 2 WASHER

7 NAS1096-2-12 2 SCREW

8 NSA5527-03-01 2 SPACER

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

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

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

to part number relationship.

D. LIST OF MATERIALS - OPERATOR SUPPLIED

(1) Consumable Materials

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO CML

MAT. No.

QTY PER A/C SEE

NOTES

Electrical Coating (Blue Color) 07-001 As required

Sealant 09-007 As required

Lockwire Stainlss Stl Or Nickel Alloy 19-018 As required

(2) Components

None

(3) Equipment

None

E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

None

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F. TOOLING

None

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This Page Intentionally Left Blank

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3. ACCOMPLISHMENT INSTRUCTIONS

Task 333041-831-848-001 - Modification

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

INCLUDED IN THE REFERENCED PROCEDURES

WARNING: MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE

LANDING GEAR.

WARNING: PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION

BEFORE YOU START A TASK ON OR NEAR:

- THE FLIGHT CONTROLS

- THE FLIGHT CONTROL SURFACES

- THE LANDING GEAR AND THE RELATED DOORS

- COMPONENTS THAT MOVE.

WARNING: LET THE LIGHT BECOME COOL BEFORE YOU TOUCH IT. THIS LIGHT

BECOMES VERY HOT WHEN IT IS ON, AND IT CAN BURN YOU IF YOU

TOUCH IT.

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 ELECTRICAL WIRING AND COMPONENTS.

- REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND

OTHER CONTAMINATION.

THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION

AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION.

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

Task Associated Data

**CONF 001

Zone

270 310

Modified FIN

4LJ 5LJ 6LJ 7LJ 8LJ

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Manpower

TOTAL MANHOURS 5.75

ELAPSED TIME (HOURS) 5.75

**CONF 002

Zone

270 310

Modified FIN

4LJ 5LJ 6LJ 7LJ 8LJ

Manpower

TOTAL MANHOURS 5.75

ELAPSED TIME (HOURS) 5.75

**CONF 003

Zone

270 310

Modified FIN

4LJ 5LJ 6LJ 7LJ 8LJ

Manpower

TOTAL MANHOURS 5.75

ELAPSED TIME (HOURS) 5.75

**CONF ALL

A. GENERAL

**CONF 001

(1) Subtask 333041-910-201-001 - Standard Practices

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) 06-20-00, Page Block 001

06-31-53, Page Block 001

06-41-53, Page Block 001

20-28-00, Page Block 201

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-25-51

20-33-00

20-33-44

20-51-21

Standards Manual (SM)

(a) For the specification of materials (Mat. No.) given in this Service Bulletin (Refer to

Consumable Materials List (CML)).

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(b) For the identification of zones (Refer to AMM 06-20-00, Page Block 001).

(c) For the Frame (FR) identification (Refer to AMM 06-31-53, Page Block 001).

(d) For the identification of the access panels (Refer to AMM 06-41-53, Page Block

001).

(e) Do the electrical bonding (Refer to AMM 20-28-00, Page Block 201 and ESPM

20-51-21).

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

(g) For the cable tie application and tooling (Refer to ESPM 20-25-51 and ESPM

20-33-44).

(2) Subtask 333041-839-201-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF 002

(1) Subtask 333041-910-201-001 - Standard Practices

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) 06-20-00, Page Block 001

06-31-53, Page Block 001

06-41-53, Page Block 001

20-28-00, Page Block 201

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-25-51

20-33-00

20-33-44

20-51-21

Standards Manual (SM)

(a) For the specification of materials (Mat. No.) given in this Service Bulletin (Refer to

Consumable Materials List (CML)).

(b) For the identification of zones (Refer to AMM 06-20-00, Page Block 001).

(c) For the Frame (FR) identification (Refer to AMM 06-31-53, Page Block 001).

(d) For the identification of the access panels (Refer to AMM 06-41-53, Page Block

001).

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(e) Do the electrical bonding (Refer to AMM 20-28-00, Page Block 201 and ESPM

20-51-21).

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

(g) For the cable tie application and tooling (Refer to ESPM 20-25-51 and ESPM

20-33-44).

(2) Subtask 333041-839-201-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF 003

(1) Subtask 333041-910-201-001 - Standard Practices

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) 06-20-00, Page Block 001

06-31-53, Page Block 001

06-41-53, Page Block 001

20-28-00, Page Block 201

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-25-51

20-33-00

20-33-44

20-51-21

Standards Manual (SM)

(a) For the specification of materials (Mat. No.) given in this Service Bulletin (Refer to

Consumable Materials List (CML)).

(b) For the identification of zones (Refer to AMM 06-20-00, Page Block 001).

(c) For the Frame (FR) identification (Refer to AMM 06-31-53, Page Block 001).

(d) For the identification of the access panels (Refer to AMM 06-41-53, Page Block

001).

(e) Do the electrical bonding (Refer to AMM 20-28-00, Page Block 201 and ESPM

20-51-21).

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

(g) For the cable tie application and tooling (Refer to ESPM 20-25-51 and ESPM

20-33-44).

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(2) Subtask 333041-839-201-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF ALL

B. PREPARATION

**CONF 001

(1) Subtask 333041-941-201-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802

Task 24-41-00-861-801

Task 52-10-00-010-801

(a) Make sure that the aircraft is electrically grounded (Refer to AMM Task

12-34-24-860-802).

(b) Energize the aircraft electrical circuits (Refer to AMM Task 24-41-00-861-801).

(c) Put access platform(s) in position below the access door 312AR.

(d) Open the access door 312AR.

(e) Put access platform(s) in position below the AFT passenger/crew door 833.

(f) Open the AFT passenger/crew door 833 (Refer to AMM Task 52-10-00-010-801).

**CONF 002

(1) Subtask 333041-941-201-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802

Task 24-41-00-861-801

Task 52-10-00-010-801

(a) Make sure that the aircraft is electrically grounded (Refer to AMM Task

12-34-24-860-802).

(b) Energize the aircraft electrical circuits (Refer to AMM Task 24-41-00-861-801).

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(c) Put access platform(s) in position below the access door 312AR.

(d) Open the access door 312AR.

(e) Put access platform(s) in position below the AFT passenger/crew door 833.

(f) Open the AFT passenger/crew door 833 (Refer to AMM Task 52-10-00-010-801).

**CONF 003

(1) Subtask 333041-941-201-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802

Task 24-41-00-861-801

Task 52-10-00-010-801

(a) Make sure that the aircraft is electrically grounded (Refer to AMM Task

12-34-24-860-802).

(b) Energize the aircraft electrical circuits (Refer to AMM Task 24-41-00-861-801).

(c) Put access platform(s) in position below the access door 312AR.

(d) Open the access door 312AR.

(e) Put access platform(s) in position below the AFT passenger/crew door 833.

(f) Open the AFT passenger/crew door 833 (Refer to AMM Task 52-10-00-010-801).

**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 333041-831-201-001 - Modify the circuit breaker panel 5005VE

Work Zones and Access Panels

Zone Access/Work location

270

Manpower Resources

Manhours 0.25

Minimum number of person 1

Subtask elapsed time 0.25

Skills ELECTRICAL

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Material necessary to do the job

Kit 333041D01R02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

3 ABS0772A01A 1 CLIP

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Lockwire Stainlss Stl Or

Nickel Alloy

19-018 As required

References

Aircraft Maintenance Manual (AMM) Task 20-16-00-912-801

Task 31-18-00-010-801

Fig. A-GBAAA

Modification of the Circuit Breaker Panel

5005VE

Sheet 01

Fig. A-GWCAA

Wiring 3

Sheet 01

(a) Modify the circuit breaker panel 5005VE:

WARNING: WEAR GOGGLES WHEN YOU REMOVE OR INSTALL

LOCKWIRE. CUT, REMOVE AND DISCARD THE LOCKWIRE AS

YOU DO THE TASK. LOOSE LOCKWIRE CAN CUT OR BLIND

YOU.

1 Open, safety/lock and tag this circuit breaker:

Refer to AMM Task 31-18-00-010-801.

Refer to AMM Task 20-16-00-912-801.

Refer to Fig. A-GBAAA Sheet 01, View C and D.

Refer to Fig. A-GWCAA Sheet 01.

PANEL DESIGNATION FIN LOCATION SEE

NOTES

5005VE LIGHT SEC19 1LJ D06

and install:

1 Clip-Locking ABS0772A01A Item 3

with:

Lockwire Stainlss

Stl Or Nickel Alloy

19-018 As required

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(2) Subtask 333041-831-202-001 - Modify the electrical wiring of the button toggle 4LJ

Work Zones and Access Panels

Zone Access/Work location

310

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills ELECTRICAL

Material necessary to do the job

Kit 333041D01R02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 NSA936603CC0100 1 CAP

2 NSA935401-03 3 TIE

4 F9239025710000 1 PLCRDSET

References

Elec. Std. Practices Manual (ESPM) 20-42-13

20-54-55

Fig. A-GBBAA

Modification of the Electrical Wiring of

the Button Toggle 4LJ

Sheet 01

Fig. A-GWAAA

Wiring 1

Sheet 01

Fig. A-GWBAA

Wiring 2

Sheet 01

Fig. A-GHAAA

Hookup Chart

Sheet 01

(a) Modify the electrical wire 5003 and the button toggle 4LJ:

Refer to ESPM 20-42-13 and ESPM 20-54-55.

Refer to Fig. A-GBBAA Sheet 01, View B to D.

Refer to Fig. A-GWAAA Sheet 01.

Refer to Fig. A-GWBAA Sheet 01.

Refer to Fig. A-GHAAA Sheet 01, Lines 1 and 2.

1 Remove the electrical wire 5003 from the button toggle 4LJ.

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2 Stow the electrical wire 5003, install:

1 Cap NSA936603CC0100 Item 1

3 Tie-Cable NSA935401-03 Item 2

3 Install:

1 Placard set F9239025710000 Item 4

(3) Subtask 333041-831-203-001 - Remove the maintenance light 5LJ and modify the

electrical wire

Work Zones and Access Panels

Zone Access/Work location

310

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

Material necessary to do the job

Kit 333041D01R02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 NSA936603CC0100 1 CAP

2 NSA935401-03 3 TIE

4 F9239025710000 1 PLCRDSET

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Electrical Coating (Blue

Color)

07-001 As required

Sealant 09-007 As required

References

Aircraft Maintenance Manual (AMM) Task 33-31-11-000-801

Elec. Std. Practices Manual (ESPM) 20-42-13

20-51-22

20-54-55

Fig. A-GBCAA

Removal of the Maintenance Light 5LJ

and Modification of the Electrical Wire

Sheet 01

Sheet 02

Fig. A-GWAAA

Wiring 1

Sheet 01

DATE: Jan 03/12 SERVICE BULLETIN No.: A330-33-3041

REVISION No.: 01 - Jul 10/12 Page: 25

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@A330

SERVICE BULLETIN

References

Fig. A-GWBAA

Wiring 2

Sheet 01

Fig. A-GHAAA

Hookup Chart

Sheet 01

WARNING: LET THE LIGHT BECOME COOL BEFORE YOU TOUCH IT. THIS

LIGHT BECOMES VERY HOT WHEN IT IS ON, AND IT CAN BURN

YOU IF YOU TOUCH IT.

(a) Remove the maintenance light 5LJ:

Refer to AMM Task 33-31-11-000-801.

Refer to Fig. A-GBCAA Sheet 01, View B.

1 Remove:

FIN 5LJ

1 Light-Service Area 2LA002606-01 Item (11) Discard

4 Screw NAS1096-3-7 Item (12) Discard

4 Washer NAS1149DN816K Item (13) Discard

2 Nut Item (14) Discard

2 Washer Item (15) Discard

(b) Remove the electrical wire 5016.

Refer to Fig. A-GBCAA Sheet 02, View E to G.

Refer to Fig. A-GWAAA Sheet 01.

Refer to Fig. A-GWBAA Sheet 01.

Refer to Fig. A-GHAAA Sheet 01, Line 13.

1 Remove the bonding connection of the maintenance light 5LJ and the

maintenance socket 11LJ:

1 Nut MS21042-08 Item (17) Retain

1 Washer NAS1149C0332R Item (6) Retain

1 Screw NAS1096-3-8 Item (16) Retain

2 Remove the electrical wire 5016.

DATE: Jan 03/12 SERVICE BULLETIN No.: A330-33-3041

REVISION No.: 01 - Jul 10/12 Page: 26

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@A330

SERVICE BULLETIN

3 Re-install the bonding connection of the maintenance socket 11LJ:

1 Nut MS21042-08 Item (17) Retained at

removal

1 Washer NAS1149C0332R Item (6) Retained at

removal

1 Screw NAS1096-3-8 Item (16) Retained at

removal

4 Apply to the bonding connection 5011VN/DC2:

Refer to ESPM 20-51-22.

Sealant 09-007 As required

and

Electrical Coating

(Blue Color)

07-001 As required

(c) Stow the electrical wire 5008, install:

Refer to ESPM 20-42-13 and ESPM 20-54-55.

Refer to Fig. A-GHAAA Sheet 01, Lines 9 and 10.

1 Cap NSA936603CC0100 Item 1

3 Tie-Cable NSA935401-03 Item 2

1 Install:

1 Placard set F9239025710000 Item 4

(4) Subtask 333041-831-204-001 - Remove the maintenance light 6LJ and modify the

electrical wire

Work Zones and Access Panels

Zone Access/Work location

310

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

DATE: Jan 03/12 SERVICE BULLETIN No.: A330-33-3041

REVISION No.: 01 - Jul 10/12 Page: 27

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

Material necessary to do the job

Kit 333041D01R02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 NSA936603CC0100 1 CAP

2 NSA935401-03 3 TIE

4 F9239025710000 1 PLCRDSET

References

Aircraft Maintenance Manual (AMM) Task 33-31-11-000-801

Elec. Std. Practices Manual (ESPM) 20-42-13

20-54-55

Fig. A-GBDAA

Removal of the Maintenance Light 6LJ

and Modification of the Electrical Wiring

Sheet 01

Sheet 02

Fig. A-GHAAA

Hookup Chart

Sheet 01

Fig. A-GWAAA

Wiring 1

Sheet 01

Fig. A-GWBAA

Wiring 2

Sheet 01

WARNING: LET THE LIGHT BECOME COOL BEFORE YOU TOUCH IT. THIS

LIGHT BECOMES VERY HOT WHEN IT IS ON, AND IT CAN BURN

YOU IF YOU TOUCH IT.

(a) Remove the maintenance light 6LJ:

Refer to AMM Task 33-31-11-000-801.

Refer to Fig. A-GBDAA Sheet 01, View B.

1 Remove:

FIN 6LJ

1 Light-Service Area 2LA002606-01 Item (11) Discard

4 Screw NAS1096-3-7 Item (12) Discard

4 Washer NAS1149DN816K Item (13) Discard

2 Nut Item (14) Discard

2 Washer Item (15) Discard

(b) Remove the electrical wire 5014

Refer to Fig. A-GBDAA Sheet 02, View D.

DATE: Jan 03/12 SERVICE BULLETIN No.: A330-33-3041

REVISION No.: 01 - Jul 10/12 Page: 28

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@A330

SERVICE BULLETIN

Refer to Fig. A-GWAAA Sheet 01.

Refer to Fig. A-GWBAA Sheet 01.

Refer to Fig. A-GHAAA Sheet 01, Line 11.

1 Remove the bonding connection of the maintenance light 6LJ:

1 Nut MS21042-08 Item (17) Discard

1 Washer NAS1149C0332R Item (6) Discard

1 Screw NAS1096-3-8 Item (16) Discard

2 Remove the electrical wire 5014.

(c) Stow the electrical wire 5005, install:

Refer to ESPM 20-42-13 and ESPM 20-54-55.

Refer to Fig. A-GHAAA Sheet 01, Lines 3 and 4.

1 Cap NSA936603CC0100 Item 1

3 Tie-Cable NSA935401-03 Item 2

1 Install:

1 Placard set F9239025710000 Item 4

(5) Subtask 333041-831-205-001 - Remove the maintenance lights 7LJ and 8LJ and

modify the electrical wires

Work Zones and Access Panels

Zone Access/Work location

310

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills ELECTRICAL

Material necessary to do the job

Kit 333041D01R02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 NSA936603CC0100 2 CAP

2 NSA935401-03 6 TIE

4 F9239025710000 2 PLCRDSET

DATE: Jan 03/12 SERVICE BULLETIN No.: A330-33-3041

REVISION No.: 01 - Jul 10/12 Page: 29

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) Task 33-31-11-000-801

Elec. Std. Practices Manual (ESPM) 20-42-13

20-54-55

Fig. A-GBEAA

Removal of the Maintenance Light 7LJ

and 8LJ and Modification of the

Electrical Wiring

Sheet 01

Sheet 02

Sheet 03

Fig. A-GHAAA

Hookup Chart

Sheet 01

Fig. A-GWAAA

Wiring 1

Sheet 01

Fig. A-GWBAA

Wiring 2

Sheet 01

WARNING: LET THE LIGHT BECOME COOL BEFORE YOU TOUCH IT. THIS

LIGHT BECOMES VERY HOT WHEN IT IS ON, AND IT CAN BURN

YOU IF YOU TOUCH IT.

(a) Remove the maintenance lights 7LJ and 8LJ:

Refer to AMM Task 33-31-11-000-801.

Refer to Fig. A-GBEAA Sheet 01, View B.

1 Remove:

FIN 7LJ

1 Light-Service Area 2LA002606-01 Item (11) Discard

FIN 8LJ

1 Light-Service Area 2LA002606-01 Item (11) Discard

8 Screw NAS1096-3-7 Item (12) Discard

8 Washer NAS1149DN816K Item (13) Discard

4 Nut Item (14) Discard

4 Washer Item (15) Discard

(b) Remove the electrical wires 5015 and 5017

Refer to Fig. A-GBEAA Sheet 01, View E to G.

Refer to Fig. A-GWAAA Sheet 01.

Refer to Fig. A-GWBAA Sheet 01.

Refer to Fig. A-GHAAA Sheet 01, Lines 12 and 14.

DATE: Jan 03/12 SERVICE BULLETIN No.: A330-33-3041

REVISION No.: 01 - Jul 10/12 Page: 30

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

1 Remove the bonding connection of the maintenance lights 7LJ and 8LJ:

2 Nut MS21042-08 Item (17) Discard

2 Washer NAS1149C0332R Item (6) Discard

2 Screw NAS1096-3-8 Item (16) Discard

2 Remove the electrical wires 5015 and 5017.

(c) Stow the electrical wires 5007 and 5006, install:

Refer to ESPM 20-42-13 and ESPM 20-54-55.

Refer to Fig. A-GHAAA Sheet 01, Lines 5, 6, 7 and 8.

2 Cap NSA936603CC0100 Item 1

6 Tie-Cable NSA935401-03 Item 2

1 Install:

2 Placard set F9239025710000 Item 4

**CONF 002

(1) Subtask 333041-831-201-001 - Modify the circuit breaker panel 5005VE

Work Zones and Access Panels

Zone Access/Work location

270

Manpower Resources

Manhours 0.25

Minimum number of person 1

Subtask elapsed time 0.25

Skills ELECTRICAL

Material necessary to do the job

Kit 333041D01R02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

3 ABS0772A01A 1 CLIP

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Lockwire Stainlss Stl Or

Nickel Alloy

19-018 As required

DATE: Jan 03/12 SERVICE BULLETIN No.: A330-33-3041

REVISION No.: 01 - Jul 10/12 Page: 31

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) Task 20-16-00-912-801

Task 31-18-00-010-801

Fig. A-GBAAA

Modification of the Circuit Breaker Panel

5005VE

Sheet 01

Fig. A-GWCAA

Wiring 3

Sheet 01

(a) Modify the circuit breaker panel 5005VE:

WARNING: WEAR GOGGLES WHEN YOU REMOVE OR INSTALL

LOCKWIRE. CUT, REMOVE AND DISCARD THE LOCKWIRE AS

YOU DO THE TASK. LOOSE LOCKWIRE CAN CUT OR BLIND

YOU.

1 Open, safety/lock and tag this circuit breaker:

Refer to AMM Task 31-18-00-010-801.

Refer to AMM Task 20-16-00-912-801.

Refer to Fig. A-GBAAA Sheet 01, View C and D.

Refer to Fig. A-GWCAA Sheet 01.

PANEL DESIGNATION FIN LOCATION SEE

NOTES

5005VE LIGHT SEC19 1LJ D06

and install:

1 Clip-Locking ABS0772A01A Item 3

with:

Lockwire Stainlss

Stl Or Nickel Alloy

19-018 As required

(2) Subtask 333041-831-202-001 - Modify the electrical wiring of the button toggle 4LJ

Work Zones and Access Panels

Zone Access/Work location

310

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills ELECTRICAL

DATE: Jan 03/12 SERVICE BULLETIN No.: A330-33-3041

REVISION No.: 01 - Jul 10/12 Page: 32

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

Material necessary to do the job

Kit 333041D01R02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 NSA936603CC0100 1 CAP

2 NSA935401-03 3 TIE

4 F9239025710000 1 PLCRDSET

References

Elec. Std. Practices Manual (ESPM) 20-42-13

20-54-55

Fig. A-GBBAA

Modification of the Electrical Wiring of

the Button Toggle 4LJ

Sheet 01

Fig. A-GWAAA

Wiring 1

Sheet 01

Fig. A-GWBAA

Wiring 2

Sheet 01

Fig. A-GHAAA

Hookup Chart

Sheet 01

(a) Modify the electrical wire 5003 and the button toggle 4LJ:

Refer to ESPM 20-42-13 and ESPM 20-54-55.

Refer to Fig. A-GBBAA Sheet 01, View B to D.

Refer to Fig. A-GWAAA Sheet 01.

Refer to Fig. A-GWBAA Sheet 01.

Refer to Fig. A-GHAAA Sheet 01, Lines 1 and 2.

1 Remove the electrical wire 5003 from the button toggle 4LJ.

2 Stow the electrical wire 5003, install:

1 Cap NSA936603CC0100 Item 1

3 Tie-Cable NSA935401-03 Item 2

3 Install:

1 Placard set F9239025710000 Item 4

DATE: Jan 03/12 SERVICE BULLETIN No.: A330-33-3041

REVISION No.: 01 - Jul 10/12 Page: 33

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@A330

SERVICE BULLETIN

(3) Subtask 333041-831-203-002 - Remove the maintenance light 5LJ and modify the

electrical wire

Work Zones and Access Panels

Zone Access/Work location

310

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

Material necessary to do the job

Kit 333041D01R02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 NSA936603CC0100 1 CAP

2 NSA935401-03 3 TIE

4 F9239025710000 1 PLCRDSET

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Electrical Coating (Blue

Color)

07-001 As required

Sealant 09-007 As required

References

Aircraft Maintenance Manual (AMM) Task 33-31-11-000-801

Elec. Std. Practices Manual (ESPM) 20-42-13

20-51-22

20-54-55

Fig. A-GBCAB

Removal of the Maintenance Light 5LJ

and Modification of the Electrical Wiring

Sheet 01

Sheet 02

Fig. A-GWAAA

Wiring 1

Sheet 01

Fig. A-GWBAA

Wiring 2

Sheet 01

Fig. A-GHAAA

Hookup Chart

Sheet 01

WARNING: LET THE LIGHT BECOME COOL BEFORE YOU TOUCH IT. THIS

LIGHT BECOMES VERY HOT WHEN IT IS ON, AND IT CAN BURN

YOU IF YOU TOUCH IT.

DATE: Jan 03/12 SERVICE BULLETIN No.: A330-33-3041

REVISION No.: 01 - Jul 10/12 Page: 34

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

(a) Remove the maintenance light 5LJ:

Refer to AMM Task 33-31-11-000-801.

Refer to Fig. A-GBCAB Sheet 01View B.

1 Remove:

FIN 5LJ

1 Light-Service Area 2LA002606-01 Item (11) Discard

4 Screw NAS1096-3-7 Item (12) Discard

4 Washer NAS1149DN816K Item (13) Discard

2 Nut Item (14) Discard

2 Washer Item (15) Discard

(b) Remove the electrical wire 5016.

Refer to Fig. A-GBCAB Sheet 02, View E to G.

Refer to Fig. A-GWAAA Sheet 01.

Refer to Fig. A-GWBAA Sheet 01.

Refer to Fig. A-GHAAA Sheet 01, Line 13.

1 Remove the bonding connection of the maintenance light 5LJ and the

maintenance socket 11LJ:

1 Nut MS21042-08 Item (17) Retain

1 Washer NAS1149C0332R Item (6) Retain

1 Screw NAS1096-3-8 Item (16) Retain

2 Remove the electrical wire 5016.

3 Re-install the bonding connection of the maintenance socket 11LJ:

1 Nut MS21042-08 Item (17) Retained at

removal

1 Washer NAS1149C0332R Item (6) Retained at

removal

1 Screw NAS1096-3-8 Item (16) Retained at

removal

DATE: Jan 03/12 SERVICE BULLETIN No.: A330-33-3041

REVISION No.: 01 - Jul 10/12 Page: 35

6

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@A330

SERVICE BULLETIN

4 Apply to the bonding connection 5011VN/DC2:

Refer to ESPM 20-51-22.

Sealant 09-007 As required

and

Electrical Coating

(Blue Color)

07-001 As required

(c) Stow the electrical wire 5008, install:

Refer to ESPM 20-42-13 and ESPM 20-54-55.

Refer to Fig. A-GHAAA Sheet 01, Lines 9 and 10.

1 Cap NSA936603CC0100 Item 1

3 Tie-Cable NSA935401-03 Item 2

1 Install:

1 Placard set F9239025710000 Item 4

(4) Subtask 333041-831-204-001 - Remove the maintenance light 6LJ and modify the

electrical wire

Work Zones and Access Panels

Zone Access/Work location

310

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

Material necessary to do the job

Kit 333041D01R02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 NSA936603CC0100 1 CAP

2 NSA935401-03 3 TIE

4 F9239025710000 1 PLCRDSET

References

Aircraft Maintenance Manual (AMM) Task 33-31-11-000-801

Elec. Std. Practices Manual (ESPM) 20-42-13

20-54-55

DATE: Jan 03/12 SERVICE BULLETIN No.: A330-33-3041

REVISION No.: 01 - Jul 10/12 Page: 36

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

References

Fig. A-GBDAA

Removal of the Maintenance Light 6LJ

and Modification of the Electrical Wiring

Sheet 01

Sheet 02

Fig. A-GHAAA

Hookup Chart

Sheet 01

Fig. A-GWAAA

Wiring 1

Sheet 01

Fig. A-GWBAA

Wiring 2

Sheet 01

WARNING: LET THE LIGHT BECOME COOL BEFORE YOU TOUCH IT. THIS

LIGHT BECOMES VERY HOT WHEN IT IS ON, AND IT CAN BURN

YOU IF YOU TOUCH IT.

(a) Remove the maintenance light 6LJ:

Refer to AMM Task 33-31-11-000-801.

Refer to Fig. A-GBDAA Sheet 01, View B.

1 Remove:

FIN 6LJ

1 Light-Service Area 2LA002606-01 Item (11) Discard

4 Screw NAS1096-3-7 Item (12) Discard

4 Washer NAS1149DN816K Item (13) Discard

2 Nut Item (14) Discard

2 Washer Item (15) Discard

(b) Remove the electrical wire 5014

Refer to Fig. A-GBDAA Sheet 02, View D.

Refer to Fig. A-GWAAA Sheet 01.

Refer to Fig. A-GWBAA Sheet 01.

Refer to Fig. A-GHAAA Sheet 01, Line 11.

1 Remove the bonding connection of the maintenance light 6LJ:

1 Nut MS21042-08 Item (17) Discard

1 Washer NAS1149C0332R Item (6) Discard

1 Screw NAS1096-3-8 Item (16) Discard

DATE: Jan 03/12 SERVICE BULLETIN No.: A330-33-3041

REVISION No.: 01 - Jul 10/12 Page: 37

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@A330

SERVICE BULLETIN

2 Remove the electrical wire 5014.

(c) Stow the electrical wire 5005, install:

Refer to ESPM 20-42-13 and ESPM 20-54-55.

Refer to Fig. A-GHAAA Sheet 01, Lines 3 and 4.

1 Cap NSA936603CC0100 Item 1

3 Tie-Cable NSA935401-03 Item 2

1 Install:

1 Placard set F9239025710000 Item 4

(5) Subtask 333041-831-205-001 - Remove the maintenance lights 7LJ and 8LJ and

modify the electrical wires

Work Zones and Access Panels

Zone Access/Work location

310

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills ELECTRICAL

Material necessary to do the job

Kit 333041D01R02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 NSA936603CC0100 2 CAP

2 NSA935401-03 6 TIE

4 F9239025710000 2 PLCRDSET

References

Aircraft Maintenance Manual (AMM) Task 33-31-11-000-801

Elec. Std. Practices Manual (ESPM) 20-42-13

20-54-55

Fig. A-GBEAA

Removal of the Maintenance Light 7LJ

and 8LJ and Modification of the

Electrical Wiring

Sheet 01

Sheet 02

Sheet 03

Fig. A-GHAAA

Hookup Chart

Sheet 01

Fig. A-GWAAA

Wiring 1

Sheet 01

DATE: Jan 03/12 SERVICE BULLETIN No.: A330-33-3041

REVISION No.: 01 - Jul 10/12 Page: 38

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

References

Fig. A-GWBAA

Wiring 2

Sheet 01

WARNING: LET THE LIGHT BECOME COOL BEFORE YOU TOUCH IT. THIS

LIGHT BECOMES VERY HOT WHEN IT IS ON, AND IT CAN BURN

YOU IF YOU TOUCH IT.

(a) Remove the maintenance lights 7LJ and 8LJ:

Refer to AMM Task 33-31-11-000-801.

Refer to Fig. A-GBEAA Sheet 01, View B.

1 Remove:

FIN 7LJ

1 Light-Service Area 2LA002606-01 Item (11) Discard

FIN 8LJ

1 Light-Service Area 2LA002606-01 Item (11) Discard

8 Screw NAS1096-3-7 Item (12) Discard

8 Washer NAS1149DN816K Item (13) Discard

4 Nut Item (14) Discard

4 Washer Item (15) Discard

(b) Remove the electrical wires 5015 and 5017

Refer to Fig. A-GBEAA Sheet 01, View E to G.

Refer to Fig. A-GWAAA Sheet 01.

Refer to Fig. A-GWBAA Sheet 01.

Refer to Fig. A-GHAAA Sheet 01, Lines 12 and 14.

1 Remove the bonding connection of the maintenance lights 7LJ and 8LJ:

2 Nut MS21042-08 Item (17) Discard

2 Washer NAS1149C0332R Item (6) Discard

2 Screw NAS1096-3-8 Item (16) Discard

2 Remove the electrical wires 5015 and 5017.

DATE: Jan 03/12 SERVICE BULLETIN No.: A330-33-3041

REVISION No.: 01 - Jul 10/12 Page: 39

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

(c) Stow the electrical wires 5007 and 5006, install:

Refer to ESPM 20-42-13 and ESPM 20-54-55.

Refer to Fig. A-GHAAA Sheet 01, Lines 5, 6, 7 and 8.

2 Cap NSA936603CC0100 Item 1

6 Tie-Cable NSA935401-03 Item 2

1 Install:

2 Placard set F9239025710000 Item 4

**CONF 003

(1) Subtask 333041-831-201-001 - Modify the circuit breaker panel 5005VE

Work Zones and Access Panels

Zone Access/Work location

270

Manpower Resources

Manhours 0.25

Minimum number of person 1

Subtask elapsed time 0.25

Skills ELECTRICAL

Material necessary to do the job

Kit 333041D01R02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

3 ABS0772A01A 1 CLIP

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Lockwire Stainlss Stl Or

Nickel Alloy

19-018 As required

References

Aircraft Maintenance Manual (AMM) Task 20-16-00-912-801

Task 31-18-00-010-801

Fig. A-GBAAA

Modification of the Circuit Breaker Panel

5005VE

Sheet 01

Fig. A-GWCAA

Wiring 3

Sheet 01

DATE: Jan 03/12 SERVICE BULLETIN No.: A330-33-3041

REVISION No.: 01 - Jul 10/12 Page: 40

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

(a) Modify the circuit breaker panel 5005VE:

WARNING: WEAR GOGGLES WHEN YOU REMOVE OR INSTALL

LOCKWIRE. CUT, REMOVE AND DISCARD THE LOCKWIRE AS

YOU DO THE TASK. LOOSE LOCKWIRE CAN CUT OR BLIND

YOU.

1 Open, safety/lock and tag this circuit breaker:

Refer to AMM Task 31-18-00-010-801.

Refer to AMM Task 20-16-00-912-801.

Refer to Fig. A-GBAAA Sheet 01, View C and D.

Refer to Fig. A-GWCAA Sheet 01.

PANEL DESIGNATION FIN LOCATION SEE

NOTES

5005VE LIGHT SEC19 1LJ D06

and install:

1 Clip-Locking ABS0772A01A Item 3

with:

Lockwire Stainlss

Stl Or Nickel Alloy

19-018 As required

(2) Subtask 333041-831-202-002 - Modify the electrical wiring of the button toggle 4LJ

Work Zones and Access Panels

Zone Access/Work location

310

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills ELECTRICAL

Material necessary to do the job

Kit 333041D01R02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 NSA936603CC0100 1 CAP

2 NSA935401-03 3 TIE

4 F9239025710000 1 PLCRDSET

DATE: Jan 03/12 SERVICE BULLETIN No.: A330-33-3041

REVISION No.: 01 - Jul 10/12 Page: 41

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

References

Elec. Std. Practices Manual (ESPM) 20-42-13

20-54-55

Fig. A-GBBAB

Modification of the Electrical Wire 5003

of the Button Toggle 4LJ

Sheet 01

Fig. A-GWAAA

Wiring 1

Sheet 01

Fig. A-GWBAA

Wiring 2

Sheet 01

Fig. A-GHAAA

Hookup Chart

Sheet 01

(a) Modify the electrical wire 5003 and the button toggle 4LJ:

Refer to ESPM 20-42-13 and ESPM 20-54-55.

Refer to Fig. A-GBBAB Sheet 01, View B to D.

Refer to Fig. A-GWAAA Sheet 01.

Refer to Fig. A-GWBAA Sheet 01.

Refer to Fig. A-GHAAA Sheet 01, Lines 1 and 2.

1 Remove the electrical wire 5003 from the button toggle 4LJ.

2 Stow the electrical wire 5003, install:

1 Cap NSA936603CC0100 Item 1

3 Tie-Cable NSA935401-03 Item 2

3 Install:

1 Placard set F9239025710000 Item 4

(3) Subtask 333041-831-203-003 - Remove the maintenance light 5LJ and modify the

electrical wire

Work Zones and Access Panels

Zone Access/Work location

310

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

DATE: Jan 03/12 SERVICE BULLETIN No.: A330-33-3041

REVISION No.: 01 - Jul 10/12 Page: 42

6

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SERVICE BULLETIN

Material necessary to do the job

Kit 333041D01R02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 NSA936603CC0100 1 CAP

2 NSA935401-03 3 TIE

4 F9239025710000 1 PLCRDSET

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Electrical Coating (Blue

Color)

07-001 As required

Sealant 09-007 As required

References

Aircraft Maintenance Manual (AMM) Task 33-31-11-000-801

Elec. Std. Practices Manual (ESPM) 20-42-13

20-51-22

20-54-55

Fig. A-GBCAC

Removal of the Maintenance Light 5LJ

and Modification of the Electrical Wiring

Sheet 01

Sheet 02

Fig. A-GWAAA

Wiring 1

Sheet 01

Fig. A-GWBAA

Wiring 2

Sheet 01

Fig. A-GHAAA

Hookup Chart

Sheet 01

WARNING: LET THE LIGHT BECOME COOL BEFORE YOU TOUCH IT. THIS

LIGHT BECOMES VERY HOT WHEN IT IS ON, AND IT CAN BURN

YOU IF YOU TOUCH IT.

(a) Remove the maintenance light 5LJ:

Refer to AMM Task 33-31-11-000-801.

Refer to Fig. A-GBCAC Sheet 01, View B.

1 Remove:

FIN 5LJ

1 Light-Service Area 2LA002606-01 Item (11) Discard

4 Screw NAS1096-3-7 Item (12) Discard

4 Washer NAS1149DN816K Item (13) Discard

DATE: Jan 03/12 SERVICE BULLETIN No.: A330-33-3041

REVISION No.: 01 - Jul 10/12 Page: 43

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SERVICE BULLETIN

2 Nut Item (14) Discard

2 Washer Item (15) Discard

(b) Remove the electrical wire 5016.

Refer to Fig. A-GBCAC Sheet 02, View E to G.

Refer to Fig. A-GWAAA Sheet 01.

Refer to Fig. A-GWBAA Sheet 01.

Refer to Fig. A-GHAAA Sheet 01, Line 13.

1 Remove the bonding connection of the maintenance light 5LJ and the

maintenance socket 11LJ:

Refer to Fig. A-GBCAC Sheet 02, View D.

1 Nut MS21042-08 Item (17) Retain

1 Washer NAS1149C0332R Item (6) Retain

1 Screw NAS1096-3-8 Item (16) Retain

2 Remove the electrical wire 5016.

3 Re-install the bonding connection of the maintenance socket 11LJ:

1 Nut MS21042-08 Item (17) Retained at

removal

1 Washer NAS1149C0332R Item (6) Retained at

removal

1 Screw NAS1096-3-8 Item (16) Retained at

removal

4 Apply to the bonding connection 5011VN/DC2:

Refer to ESPM 20-51-22.

Sealant 09-007 As required

and

Electrical Coating

(Blue Color)

07-001 As required

(c) Stow the electrical wire 5008, install:

Refer to ESPM 20-42-13 and ESPM 20-54-55.

DATE: Jan 03/12 SERVICE BULLETIN No.: A330-33-3041

REVISION No.: 01 - Jul 10/12 Page: 44

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SERVICE BULLETIN

Refer to Fig. A-GHAAA Sheet 01, Lines 9 and 10.

1 Cap NSA936603CC0100 Item 1

3 Tie-Cable NSA935401-03 Item 2

1 Install:

1 Placard set F9239025710000 Item 4

(4) Subtask 333041-831-204-001 - Remove the maintenance light 6LJ and modify the

electrical wire

Work Zones and Access Panels

Zone Access/Work location

310

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

Material necessary to do the job

Kit 333041D01R02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 NSA936603CC0100 1 CAP

2 NSA935401-03 3 TIE

4 F9239025710000 1 PLCRDSET

References

Aircraft Maintenance Manual (AMM) Task 33-31-11-000-801

Elec. Std. Practices Manual (ESPM) 20-42-13

20-54-55

Fig. A-GBDAA

Removal of the Maintenance Light 6LJ

and Modification of the Electrical Wiring

Sheet 01

Sheet 02

Fig. A-GHAAA

Hookup Chart

Sheet 01

Fig. A-GWAAA

Wiring 1

Sheet 01

Fig. A-GWBAA

Wiring 2

Sheet 01

WARNING: LET THE LIGHT BECOME COOL BEFORE YOU TOUCH IT. THIS

LIGHT BECOMES VERY HOT WHEN IT IS ON, AND IT CAN BURN

YOU IF YOU TOUCH IT.

DATE: Jan 03/12 SERVICE BULLETIN No.: A330-33-3041

REVISION No.: 01 - Jul 10/12 Page: 45

6

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SERVICE BULLETIN

(a) Remove the maintenance light 6LJ:

Refer to AMM Task 33-31-11-000-801.

Refer to Fig. A-GBDAA Sheet 01, View B.

1 Remove:

FIN 6LJ

1 Light-Service Area 2LA002606-01 Item (11) Discard

4 Screw NAS1096-3-7 Item (12) Discard

4 Washer NAS1149DN816K Item (13) Discard

2 Nut Item (14) Discard

2 Washer Item (15) Discard

(b) Remove the electrical wire 5014

Refer to Fig. A-GBDAA Sheet 02, View D.

Refer to Fig. A-GWAAA Sheet 01.

Refer to Fig. A-GWBAA Sheet 01.

Refer to Fig. A-GHAAA Sheet 01, Line 11.

1 Remove the bonding connection of the maintenance light 6LJ:

1 Nut MS21042-08 Item (17) Discard

1 Washer NAS1149C0332R Item (6) Discard

1 Screw NAS1096-3-8 Item (16) Discard

2 Remove the electrical wire 5014.

(c) Stow the electrical wire 5005, install:

Refer to ESPM 20-42-13 and ESPM 20-54-55.

Refer to Fig. A-GHAAA Sheet 01, Lines 3 and 4.

1 Cap NSA936603CC0100 Item 1

3 Tie-Cable NSA935401-03 Item 2

1 Install:

1 Placard set F9239025710000 Item 4

DATE: Jan 03/12 SERVICE BULLETIN No.: A330-33-3041

REVISION No.: 01 - Jul 10/12 Page: 46

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SERVICE BULLETIN

(5) Subtask 333041-831-205-002 - Remove the maintenance lights 7LJ and 8LJ and

modify the electrical wires

Work Zones and Access Panels

Zone Access/Work location

310

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills ELECTRICAL

Material necessary to do the job

Kit 333041D01R02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 NSA936603CC0100 2 CAP

2 NSA935401-03 6 TIE

4 F9239025710000 2 PLCRDSET

Kit 333041D02R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

5 MS21919WCH2 2 CLAMP

6 NAS1149C0332R 2 WASHER

7 NAS1096-2-12 2 SCREW

8 NSA5527-03-01 2 SPACER

References

Aircraft Maintenance Manual (AMM) Task 33-31-11-000-801

Elec. Std. Practices Manual (ESPM) 20-42-13

20-54-55

Fig. A-GBEAB

Removal of the Maintenance Light 7LJ

and 8LJ and Modification of the

Electrical Wiring

Sheet 01

Sheet 02

Sheet 03

Fig. A-GHAAA

Hookup Chart

Sheet 01

Fig. A-GWAAA

Wiring 1

Sheet 01

Fig. A-GWBAA

Wiring 2

Sheet 01

WARNING: LET THE LIGHT BECOME COOL BEFORE YOU TOUCH IT. THIS

LIGHT BECOMES VERY HOT WHEN IT IS ON, AND IT CAN BURN

YOU IF YOU TOUCH IT.

DATE: Jan 03/12 SERVICE BULLETIN No.: A330-33-3041

REVISION No.: 01 - Jul 10/12 Page: 47

6

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@A330

SERVICE BULLETIN

(a) Remove the maintenance lights 7LJ and 8LJ:

Refer to AMM Task 33-31-11-000-801.

Refer to Fig. A-GBEAB Sheet 01, View B.

1 Remove:

FIN 7LJ

1 Light-Service Area 2LA002606-01 Item (11) Discard

FIN 8LJ

1 Light-Service Area 2LA002606-01 Item (11) Discard

8 Screw NAS1096-3-7 Item (12) Discard

8 Washer NAS1149DN816K Item (13) Discard

4 Nut Item (14) Discard

4 Washer Item (15) Discard

(b) Remove the electrical wires 5015 and 5017

Refer to Fig. A-GBEAB Sheet 01, View E to G.

Refer to Fig. A-GWAAA Sheet 01.

Refer to Fig. A-GWBAA Sheet 01.

Refer to Fig. A-GHAAA Sheet 01, Lines 12 and 14.

1 Remove the bonding connection of the maintenance lights 7LJ and 8LJ:

2 Nut MS21042-08 Item (17) Discard

2 Washer NAS1149C0332R Item (6) Discard

2 Screw NAS1096-3-8 Item (16) Discard

2 Remove the electrical wires 5015 and 5017.

3 Install:

2 Clamp MS21919WCH2 Item 5

2 Washer NAS1149C0332R Item 6

2 Screw NAS1096-2-12 Item 7

2 Spacer NSA5527-03-01 Item 8

DATE: Jan 03/12 SERVICE BULLETIN No.: A330-33-3041

REVISION No.: 01 - Jul 10/12 Page: 48

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SERVICE BULLETIN

(c) Stow the electrical wires 5007 and 5006, install:

Refer to ESPM 20-42-13 and ESPM 20-54-55.

Refer to Fig. A-GHAAA Sheet 01, Lines 5, 6, 7 and 8.

2 Cap NSA936603CC0100 Item 1

6 Tie-Cable NSA935401-03 Item 2

1 Install:

2 Placard set F9239025710000 Item 4

**CONF ALL

D. TEST

**CONF 001

(1) Subtask 333041-700-201-001 - Test

Work Zones and Access Panels

Zone Access/Work location

310

Manpower Resources

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) Task 33-31-00-720-801

(a) Make sure that the resistance (ohmic) of the bonding connection 5011VN/DC2 of

the maintenance socket 11LJ is correct.

(b) Do the functional test of the maintenance socket 11LJ (Refer to AMM Task

33-31-00-720-801).

**CONF 002

(1) Subtask 333041-700-201-001 - Test

Work Zones and Access Panels

Zone Access/Work location

310

Manpower Resources

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) Task 33-31-00-720-801

DATE: Jan 03/12 SERVICE BULLETIN No.: A330-33-3041

REVISION No.: 01 - Jul 10/12 Page: 49

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SERVICE BULLETIN

(a) Make sure that the resistance (ohmic) of the bonding connection 5011VN/DC2 of

the maintenance socket 11LJ is correct.

(b) Do the functional test of the maintenance socket 11LJ (Refer to AMM Task

33-31-00-720-801).

**CONF 003

(1) Subtask 333041-700-201-001 - Test

Work Zones and Access Panels

Zone Access/Work location

310

Manpower Resources

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) Task 33-31-00-720-801

(a) Make sure that the resistance (ohmic) of the bonding connection 5011VN/DC2 of

the maintenance socket 11LJ is correct.

(b) Do the functional test of the maintenance socket 11LJ (Refer to AMM Task

33-31-00-720-801).

**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 333041-942-201-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 24-41-00-862-801

Task 52-10-00-410-801

(a) Make sure that the work areas are clean and clear of tools and other items of

equipment.

(b) Close the access door 312AR.

(c) De-energize the aircraft electrical circuits (Refer to AMM Task 24-41-00-862-801).

(d) Remove the access platform(s).

(e) Close the AFT passenger/crew door 833 (Refer to AMM Task 52-10-00-410-801).

DATE: Jan 03/12 SERVICE BULLETIN No.: A330-33-3041

REVISION No.: 01 - Jul 10/12 Page: 50

6

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@A330

SERVICE BULLETIN

**CONF 002

(1) Subtask 333041-942-201-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 24-41-00-862-801

Task 52-10-00-410-801

(a) Make sure that the work areas are clean and clear of tools and other items of

equipment.

(b) Close the access door 312AR.

(c) De-energize the aircraft electrical circuits (Refer to AMM Task 24-41-00-862-801).

(d) Remove the access platform(s).

(e) Close the AFT passenger/crew door 833 (Refer to AMM Task 52-10-00-410-801).

**CONF 003

(1) Subtask 333041-942-201-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 24-41-00-862-801

Task 52-10-00-410-801

(a) Make sure that the work areas are clean and clear of tools and other items of

equipment.

(b) Close the access door 312AR.

(c) De-energize the aircraft electrical circuits (Refer to AMM Task 24-41-00-862-801).

(d) Remove the access platform(s).

(e) Close the AFT passenger/crew door 833 (Refer to AMM Task 52-10-00-410-801).

DATE: Jan 03/12 SERVICE BULLETIN No.: A330-33-3041

REVISION No.: 01 - Jul 10/12 Page: 51

6

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@A330

SERVICE BULLETIN

**CONF ALL

LIGHT

C

NOTE:

01 SAFETY THE CLIP WITH LOCKWIRE (MAT. NO. 19−018)

3 01

D

SEC19

1LJ

Z270

A

B

FR77

FR75

FR72 5005VE

FR76 C

APU

LAV

AFT&MID PAX & CABIN ATTND

D

G_SB_333041_6_BAAA_01_00

B

A

Figure A-GBAAA - Sheet 01

Modification of the Circuit Breaker Panel 5005VE

DATE: Jan 03/12 SERVICE BULLETIN No.: A330-33-3041

REVISION No.: 01 - Jul 10/12 Page: 52

6

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@A330

SERVICE BULLETIN

**CONF 001 thru 002

Z310

A

5872VB /2M

FR83

FR87

A

4LJ

FR84

B C

BEFORE

AFTER

5872VB /2M

FR84

4LJ

B

F

W

D

4LJ C F

W

D

FR84

D

MOD. 201683

SB33−3041

2

1

4

D

AFTER

TO

4LJ

G_SB_333041_6_BBAA_01_01

Figure A-GBBAA - Sheet 01

Modification of the Electrical Wiring of the Button Toggle 4LJ

DATE: Jan 03/12 SERVICE BULLETIN No.: A330-33-3041

REVISION No.: 01 - Jul 10/12 Page: 53

6

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@A330

SERVICE BULLETIN

**CONF 003

Z310

A

FR83

FR87

A

4LJ

FR84

B C

BEFORE

5872VB /2M

FR84

4LJ

B

VIEW LOOKING FWD

VIEW LOOKING FWD

AFTER

C

4LJ

5872VB /2M

FR84

STGR33RH

STGR34RH

STGR33RH

STGR34RH

D

MOD. 201683

SB33−3041

2

1

4

D

AFTER

TO

4LJ

G_SB_333041_6_BBAB_01_01

Figure A-GBBAB - Sheet 01

Modification of the Electrical Wire 5003 of the Button Toggle 4LJ

DATE: Jan 03/12 SERVICE BULLETIN No.: A330-33-3041

REVISION No.: 01 - Jul 10/12 Page: 54

6

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@A330

SERVICE BULLETIN

**CONF 001

Z310

A

B

(14)

(15)

(11)

(12)

(13)

(4 POS)

(4 POS)

5872VB /2M

5LJ

11LJ

FR83

FR85

FR87

FR85

B

A

C E

5011VN /DC2

5LJ

G_SB_333041_6_BCAA_01_01

Figure A-GBCAA - Sheet 01

Removal of the Maintenance Light 5LJ and Modification of the Electrical Wire

DATE: Jan 03/12 SERVICE BULLETIN No.: A330-33-3041

REVISION No.: 01 - Jul 10/12 Page: 55

6

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@A330

SERVICE BULLETIN

**CONF 001

5872VB /2M 5LJ

BEFORE

AFTER

FR85

C F

W

D

D

5011VN /DC2

TO 5LJ

TO 11LJ

(16)

(6)

(17)

D

F

W

D

E

5872VB /2M

5011VN /DC2

BEFORE

TO 11LJ

AFTER

F

F

G

(16)

(6)

(17)

FR85

MOD. 201683

SB33−3041

2

1

4

AFTER

G

G_SB_333041_6_BCAA_02_02

Figure A-GBCAA - Sheet 02

Removal of the Maintenance Light 5LJ and Modification of the Electrical Wire

DATE: Jan 03/12 SERVICE BULLETIN No.: A330-33-3041

REVISION No.: 01 - Jul 10/12 Page: 56

6

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@A330

SERVICE BULLETIN

**CONF 002

Z310

A

B

(14)

(15)

(11)

(12)

(13)

(4 POS)

(4 POS)

5872VB /2M

5LJ

11LJ

FR83

FR85

FR87

FR85

B

A

C E

5011VN /DC2

5LJ

G_SB_333041_6_BCAB_01_01

Figure A-GBCAB - Sheet 01

Removal of the Maintenance Light 5LJ and Modification of the Electrical Wiring

DATE: Jan 03/12 SERVICE BULLETIN No.: A330-33-3041

REVISION No.: 01 - Jul 10/12 Page: 57

6

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@A330

SERVICE BULLETIN

**CONF 002

TO 5LJ

TO 11LJ

(16)

(6)

(17)

D

BEFORE

TO 11LJ

AFTER

F (16)

(6)

(17)

G_SB_333041_6_BCAB_02_02

MOD. 201683

SB33−3041

2

1

4

AFTER

G

5LJ

BEFORE

AFTER

FR85

C F

W

D

D

G F

FR85

F

W

D

E

5011VN /DC2

5011VN /DC2

5872VB /2M

5872VB /2M

Figure A-GBCAB - Sheet 02

Removal of the Maintenance Light 5LJ and Modification of the Electrical Wiring

DATE: Jan 03/12 SERVICE BULLETIN No.: A330-33-3041

REVISION No.: 01 - Jul 10/12 Page: 58

6

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@A330

SERVICE BULLETIN

**CONF 003

Z310

A

B

(14)

(15)

(11)

(12)

(13)

(4 POS)

(4 POS)

5872VB /2M

5LJ

11LJ

FR83

FR85

FR87

FR85

B

A

C E

5011VN /DC2

5LJ

G_SB_333041_6_BCAC_01_01

Figure A-GBCAC - Sheet 01

Removal of the Maintenance Light 5LJ and Modification of the Electrical Wiring

DATE: Jan 03/12 SERVICE BULLETIN No.: A330-33-3041

REVISION No.: 01 - Jul 10/12 Page: 59

6

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@A330

SERVICE BULLETIN

**CONF 003

5872VB /2M

5LJ

BEFORE

AFTER

FR85

C F

W

D

5011VN /DC2

TO 5LJ

TO 11LJ

(16)

(6)

(17)

D

F

W

D

E

5872VB /2M

5011VN /DC2

BEFORE

TO 11LJ

AFTER

F (16)

(6)

(17)

D

11LJ

G

F

11LJ

FR85

G_SB_333041_6_BCAC_02_02

MOD. 201683

SB33−3041

2

1

4

AFTER

G

Figure A-GBCAC - Sheet 02

Removal of the Maintenance Light 5LJ and Modification of the Electrical Wiring

DATE: Jan 03/12 SERVICE BULLETIN No.: A330-33-3041

REVISION No.: 01 - Jul 10/12 Page: 60

6

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@A330

SERVICE BULLETIN

**CONF ALL

Z310

A

(14) B (15)

(11)

(12)

(13)

(4 POS)

(4 POS)

5872VB /2M

FR83

FR85

FR87

FR85

A

6LJ

5012VN /DC2

B

C E

6LJ

G_SB_333041_6_BDAA_01_01

Figure A-GBDAA - Sheet 01

Removal of the Maintenance Light 6LJ and Modification of the Electrical Wiring

DATE: Jan 03/12 SERVICE BULLETIN No.: A330-33-3041

REVISION No.: 01 - Jul 10/12 Page: 61

6

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@A330

SERVICE BULLETIN

**CONF ALL

5872VB /2M

BEFORE

AFTER

D

5872VB /2M

TO 6LJ (16)

(6)

(17) 6LJ

STGR18RH

STGR20RH

STGR20RH

STGR18RH

C

VIEW LOOKING FWD

5012VN /DC2

D

BEFORE

E

VIEW LOOKING FWD

F

FR83

FR83

MOD. 201683

SB33−3041

2

1

4

AFTER

F

G_SB_333041_6_BDAA_02_02

Figure A-GBDAA - Sheet 02

Removal of the Maintenance Light 6LJ and Modification of the Electrical Wiring

DATE: Jan 03/12 SERVICE BULLETIN No.: A330-33-3041

REVISION No.: 01 - Jul 10/12 Page: 62

6

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@A330

SERVICE BULLETIN

**CONF 001 thru 002

Z310

A

B

5872VB /2M

TYPICAL

FR83

FR85

FR88

A

7LJ

8LJ

B

C E

5315VN /DC2

5420VN /DC2

(14)

(15)

(11)

(12)

(13)

(4 POS)

(4 POS)

7LJ

8LJ

LH

RH

G_SB_333041_6_BEAA_01_02

Figure A-GBEAA - Sheet 01

Removal of the Maintenance Light 7LJ and 8LJ and Modification of the Electrical Wiring

DATE: Jan 03/12 SERVICE BULLETIN No.: A330-33-3041

REVISION No.: 01 - Jul 10/12 Page: 63

6

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@A330

SERVICE BULLETIN

**CONF 001 thru 002

5872VB /2M

C

(16)

(6)

(17)

BEFORE

D

5315VN /DC2

5420VN /DC2

7LJ

8LJ

LH

RH

TYPICAL

RH

LH

F

W

D

FR88

BEFORE

D

G_SB_333041_6_BEAA_02_01

TYPICAL

TO 7LJ LH

TO 8LJ RH

Figure A-GBEAA - Sheet 02

Removal of the Maintenance Light 7LJ and 8LJ and Modification of the Electrical Wiring

DATE: Jan 03/12 SERVICE BULLETIN No.: A330-33-3041

REVISION No.: 01 - Jul 10/12 Page: 64

6

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@A330

SERVICE BULLETIN

**CONF 001 thru 002

TYPICAL

F

W

D

E

AFTER

F

FR80

5872VB /2M

MOD. 201683

SB33−3041

2

1

4

AFTER

F

G_SB_333041_6_BEAA_03_02

Figure A-GBEAA - Sheet 03

Removal of the Maintenance Light 7LJ and 8LJ and Modification of the Electrical Wiring

DATE: Jan 03/12 SERVICE BULLETIN No.: A330-33-3041

REVISION No.: 01 - Jul 10/12 Page: 65

6

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SERVICE BULLETIN

**CONF 003

Z310

A

B

(12)

(13)

(4 POS)

(4 POS)

TYPICAL

C E

FR83

FR85

FR87

A

7LJ

8LJ

B

5315VN /DC2

5420VN /DC2

(14)

(15)

5872VB /2M

(11) 7LJ

8LJ

LH

RH

G_SB_333041_6_BEAB_01_02

Figure A-GBEAB - Sheet 01

Removal of the Maintenance Light 7LJ and 8LJ and Modification of the Electrical Wiring

DATE: Jan 03/12 SERVICE BULLETIN No.: A330-33-3041

REVISION No.: 01 - Jul 10/12 Page: 66

6

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@A330

SERVICE BULLETIN

**CONF 003

5872VB /2M

5315VN /DC2

5420VN /DC2

G_SB_333041_6_BEAB_02_00

C

VIEW LOOKING FWD

BEFORE

TO 7LJ LH

(16)

(6)

(17)

TO 8LJ RH

TYPICAL

D

D

7LJ

8LJ

LH

RH

TYPICAL

RH

LH

BEFORE

Figure A-GBEAB - Sheet 02

Removal of the Maintenance Light 7LJ and 8LJ and Modification of the Electrical Wiring

DATE: Jan 03/12 SERVICE BULLETIN No.: A330-33-3041

REVISION No.: 01 - Jul 10/12 Page: 67

6

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@A330

SERVICE BULLETIN

**CONF 003

AFTER

6

E

VIEW LOOKING FWD

TYPICAL

F

G

8 5

7

AFTER

G

5872VB /2M

MOD. 201683

SB33−3041

2

1

4

AFTER

F

G_SB_333041_6_BEAB_03_02

Figure A-GBEAB - Sheet 03

Removal of the Maintenance Light 7LJ and 8LJ and Modification of the Electrical Wiring

DATE: Jan 03/12 SERVICE BULLETIN No.: A330-33-3041

REVISION No.: 01 - Jul 10/12 Page: 68

6

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@A330

SERVICE BULLETIN

**CONF ALL

UNLESS OTHERWISE SPECIFIED PREFIX ALL WIRE IDENTIFICATION WITH ATA−NO.3331

UNLESS OTHERWISE SPECIFIED ALL WIRES ARE CF18 GAUGE

UNLESS OTHERWISE SPECIFIED ALL ROUTES ARE 2M

1

5200VT

312

BEFORE

5003

NOTE:

G_SB_333041_6_WAAA_01_00

F

G

H

J

K

B

C

A

D

E

1

2

4LJ

312

5005

5006

5007

5008

6LJ

312

5014

8LJ

312

5015

2

1

2

1

1

2

1

2

5012VN

DC2

5420VN

DC2

50165017

5011VN

DC2

5315VN

DC2

EXISTING WIRE

5LJ

311

7LJ

311

Figure A-GWAAA - Sheet 01

Wiring 1

DATE: Jan 03/12 SERVICE BULLETIN No.: A330-33-3041

REVISION No.: 01 - Jul 10/12 Page: 69

6

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@A330

SERVICE BULLETIN

**CONF ALL

UNLESS OTHERWISE SPECIFIED PREFIX ALL WIRE IDENTIFICATION WITH ATA−NO.3331

UNLESS OTHERWISE SPECIFIED ALL WIRES ARE CF18 GAUGE

UNLESS OTHERWISE SPECIFIED ALL ROUTES ARE 2M

1

5200VT

312

AFTER

5003

NOTE:

F

G

H

J

K

B

C

A

D

E

1

2

4LJ

312

5005

5006

5007

5008

EXISTING WIRE

G_SB_333041_6_WBAA_01_00

REROUTED WIRE

STOWED WIRE

Figure A-GWBAA - Sheet 01

Wiring 2

DATE: Jan 03/12 SERVICE BULLETIN No.: A330-33-3041

REVISION No.: 01 - Jul 10/12 Page: 70

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

**CONF ALL

UNLESS OTHERWISE SPECIFIED PREFIX ALL WIRE IDENTIFICATION WITH ATA−NO.3331

UNLESS OTHERWISE SPECIFIED ALL WIRES ARE CF18 GAUGE

UNLESS OTHERWISE SPECIFIED ALL ROUTES ARE 2M

BEFORE

NOTE:

EXISTING WIRE

1 2

7.5A

1LJ

1 2

4LJ

312

5040

5005VE

AFT CIRCUIT BREAKER PANEL

AFTER

1 2

7.5A

1LJ

1 2

4LJ

312

5040

5005VE

AFT CIRCUIT BREAKER PANEL

28V DC

GROUND

BUS

28V DC

GROUND

BUS

G_SB_333041_6_WCAA_01_01

Figure A-GWCAA - Sheet 01

Wiring 3

DATE: Jan 03/12 SERVICE BULLETIN No.: A330-33-3041

REVISION No.: 01 - Jul 10/12 Page: 71

6

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SERVICE BULLETIN

**CONF ALL

L

I

N

E ZONE OR

PANEL TERM. TERMINAL P/N WIREIDENT C0L ROUTE GAUGE

LENGTH

MM INCH

ZONE OR

PANEL

ELEC.

IDENT TERM. TERMINAL P/N

INSTRUCTIONS

END 1 LEAD END 2

10

11

12

13

14

15

16

17

18

19

20

21

22

23

24

25

1

2

3

4

5

6

7

8

9

ELEC.

IDENT.

3331−5003

3331−5003

3331−5005

3331−5005

3331−5006

3331−5006

3331−5007

3331−5007

3331−5008

3331−5008

312 4LJ

312

2

STOW

2M CF18

2M

2M

2M

2M

2M

2M

2M

2M

2M

CF18

CF18

CF18

CF18

CF18

CF18

CF18

CF18

CF18

312

312

5200VT

5200VT

312

312

311

311

6LJ

8LJ

7LJ

5LJ

1A

1A

STOW

STOW

STOW

STOW

1

1

1

1

312

312

312

312

312

312

312

312

5200VT

5200VT

5200VT

5200VT

5200VT

5200VT

5200VT

5200VT

1B

1B

1C

1C

1D

1E

1D

1E

NSA936501TA1602

EN3155−016M2018

EN3155−016M2018

EN3155−016M2018

EN3155−016M2018

EN3155−016M2018

EN3155−016M2018

EN3155−016M2018

EN3155−016M2018

EN3155−016M2018

EN3155−016M2018

NSA936501TA1602

NSA936501TA1602

NSA936501TA1602

NSA936501TA1602

NSA936603CC0100

NSA936603CC0100

NSA936603CC0100

NSA936603CC0100

NSA936603CC0100

BEFORE

AFTER

BEFORE

BEFORE

BEFORE

BEFORE

AFTER

AFTER

AFTER

AFTER

312

312

311

311

6LJ

8LJ

5LJ

7LJ

2

2

2

2

NSA936501TA1602

NSA936501TA1602

NSA936501TA1602

NSA936501TA1602

3331−5014

3331−5015

3331−5016

3331−5017

2M

2M

2M

2M

CF18

CF18

CF18

CF18

312

312

311

311

5012VN

5420VN

5011VN

5315VN

DC2

DC2

DC2

DC2

DELETE

DELETE

DELETE

DELETE

F929−97007−000−00

NSA936501TA1604

NSA936501TA1604

NSA936501TA1604

NSA936501TA1604

312 6LJ

312 8LJ

311 7LJ

311 5LJ

Figure A-GHAAA - Sheet 01

Hookup Chart

DATE: Jan 03/12 SERVICE BULLETIN No.: A330-33-3041

REVISION No.: 01 - Jul 10/12 Page: 72

6

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SERVICE BULLETIN

REPORTING SHEET

TITLE: LIGHTS - SERVICE AREA LIGHTING - REMOVE SERVICE AREA

LIGHTS IN SECTION 19 ACCORDING TO SFAR 88 REQUIREMENTS.

MODIFICATION No.: 201683D46730

Please complete the appropriate item (A or B):

A - SB WILL BE embodied YES/NO (if NO please comment)

If YES, aircraft concerned (as per SB effectivity by default) and planned dates (month/year) of

embodiment:

B - SB HAS BEEN embodied on aircraft:

Operator comments:

From Airline:

Name/Title:

Signature: Date:

If operational documentation is affected (see Paragraph 1.K of this SB): If information is needed prior to

next normal revision or prior to SB embodiment, please indicate required service(s):

Either: Modification Operational Impact (MOI), if available YES/NO

Or : Intermediate revision YES/NO

Important Information: This SB will only be incorporated in your maintenance and operational

documentation if this sheet is returned to Airbus and signed by a duly authorised representative. With

the next feasible revision, this will result in

- Updating of maintenance documentation to show pre and post SB data.

- Updating of maintenance and operational documentation to show post SB data after embodiment.

If this SB requires previous or simultaneous accomplishment of other SBs, Airbus shall automatically

include them in the manual revisions. Refer to SIL 00-037 for detailed information.

Please return this completed sheet to:

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX FRANCE

Attn: SDC32 Technical Data and Documentation Services

FAX: (+33) 5 61 93 28 06

e-mail: sb.reporting@airbus.com

or via your Resident Customer Support Office.

Alternatively, SB lists via letters or fax are also accepted.

DATE: Jan 03/12 SERVICE BULLETIN No.: A330-33-3041

REVISION No.: 01 - Jul 10/12 Page: 1

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SERVICE BULLETIN

QUALITY PERCEPTION FORM

Use this form to tell us what is your perception of the quality of this Service Bulletin. The reported data

that you provide us will be used to analyse areas of difficulties and to take corrective action to further

improve the quality of our Service Bulletins.

We thank you for the time you have taken in completing this form.

(Please rate on a scale of 1 to 4, with 4 being the highest score)

- Quality rating of this SB 4321

- Quality rating of the Accomplishment Instructions 4321

- Quality rating of the Illustrations 4321

- Is this SB easy to understand ? Y/N

If you have had difficulties in the accomplishment of this SB please quote below the area(s) and give a

short description of the issue.

Planning Material Instructions

X Effectivity X Kit content X Preparation

X Reason X List of Materials Operator Supplied X Mod/Inspection

X Manpower X Industry support X Test

X References X Re-identification X Close-Up

X Publication X Tooling X Illustrations

Comments:

Operator: Date:

Name/Title:

Please return this form to:

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX FRANCE

Attn : SEM4 Service Bulletins Management

FAX : (33) 5 61 93 42 51

Or via your Resident Customer Support Office.

DATE: Jan 03/12 SERVICE BULLETIN No.: A330-33-3041

REVISION No.: 01 - Jul 10/12 Page: 1

6

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