@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: 32

TITLE: LANDING GEAR - NOSE GEAR - ADDITION OF PRIMER PAINT TO THE

CADMIUM AROUND THE DOWEL BUSH HOLES ON THE MAIN FITTING

MODIFICATION No.: 200616H16400

This page transmits Revision No.01 of Service Bulletin No.A330-32-3241

ADDITIONAL WORK

**CONF ALL

No additional work is required by this revision for aircraft modified by any previous issue.

REASON

Revision No. 1 issued to correct AMM references. The opportunity has been taken to update the

effectivity and to make other minor changes.

CHANGES

SUMMARY

REASON/DESCRIPTION/OPERATIONAL

CONSEQUENCES

REASON UPDATED R

EFFECTIVITY OPERATOR LIST UPDATED R

MANPOWER MANPOWER UPDATED R

MANPOWER UPDATED R

MANPOWER UPDATED R

MANPOWER UPDATED R

APPENDICES APPENDICES UPDATED R

PLANNING INFORMATION

EFFECTIVITY EFFECTIVITY RELATED INFORMATION

UPDATED

R

Configuration definition

CONF 004 CONFIGURATION DEFINITION UPDATED

CONFIGURATION DESCRIPTION UPDATED

R

REASON

DATE: Nov 26/10 SERVICE BULLETIN No.: A330-32-3241

REVISION No.: 01 - Oct 06/11 Page: 1

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@A330

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Operational/Maintenance

Consequences

OPERATIONAL/MAINTENANCE CONSEQUENCES

UPDATED

R

APPROVAL APPROVAL UPDATED R

MANPOWER MANPOWER UPDATED R

MANPOWER UPDATED R

MANPOWER UPDATED R

MANPOWER UPDATED R

REFERENCES REFERENCED DOCUMENTATION UPDATED R

REFERENCED DOCUMENTATION UPDATED R

REFERENCED DOCUMENTATION UPDATED R

REFERENCED DOCUMENTATION UPDATED R

PUBLICATION AFFECTED PUBLICATIONS AFFECTED UPDATED R

ACCOMPLISHMENT INSTRUCTIONS

TASK 323241- 831-895-001-

MODIFICATION

TASK SOLUTION UPDATED

CAUTION UPDATED

R

Task associated data - 001 ELAPSED TIME UPDATED R

Task associated data - 002 ELAPSED TIME UPDATED R

Task associated data - 003 ELAPSED TIME UPDATED R

Task associated data - 004 ELAPSED TIME UPDATED R

Subtask 323241-941-401-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

NOTE UPDATED

REFERENCES UPDATED

R

Subtask 323241-941-401-002 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

NOTE UPDATED

REFERENCES UPDATED

R

Subtask 323241-941-401-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

NOTE UPDATED

REFERENCES UPDATED

R

Subtask 323241-941-401-002 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

NOTE UPDATED

REFERENCES UPDATED

R

Subtask 323241-020-401-002 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

R

Subtask 323241-420-401-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

Subtask 323241-020-401-002 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

R

Subtask 323241-420-401-001 SUBTASK SOLUTION ADDED N

Subtask 323241-420-401-002 SUBTASK SOLUTION DELETED FOR

APPLICABLE MSN

D

Subtask 323241-020-401-003 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

R

Subtask 323241-420-401-002 SUBTASK SOLUTION ADDED N

DATE: Nov 26/10 SERVICE BULLETIN No.: A330-32-3241

REVISION No.: 01 - Oct 06/11 Page: 2

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@A330

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Subtask 323241-420-401-001 SUBTASK SOLUTION DELETED FOR

APPLICABLE MSN

D

Subtask 323241-020-401-003 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

R

Subtask 323241-420-401-002 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

Subtask 323241-710-401-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

Subtask 323241-710-401-001 SUBTASK SOLUTION ADDED N

Subtask 323241-710-401-002 SUBTASK SOLUTION DELETED FOR

APPLICABLE MSN

D

Subtask 323241-710-401-002 SUBTASK SOLUTION ADDED N

Subtask 323241-710-401-001 SUBTASK SOLUTION DELETED FOR

APPLICABLE MSN

D

Subtask 323241-710-401-002 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

Subtask 323241-942-401-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

R

Subtask 323241-942-401-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

R

Subtask 323241-942-401-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

R

Subtask 323241-942-401-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

R

APPENDIX 01 : ELAPSED TIME ASSUMPTION

APPENDIX CONTENT APPENDIX CONTENT ADDED N

Fig. A-UAAAA FIGURE SOLUTION ADDED N

Fig. A-UAAAA Sheet 01 SHEET ADDED N

FILLING INSTRUCTIONS

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

Replace the complete document.

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

HISTORY OF PREVIOUS REVISIONS

No previous revision

REVISION SEQUENCE

ORIGINAL: Nov 26/10

REVISION No. : 01 - Oct 06/11

DATE: Nov 26/10 SERVICE BULLETIN No.: A330-32-3241

REVISION No.: 01 - Oct 06/11 Page: 3

7

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@A330

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

This Page Intentionally Left Blank

DATE: Nov 26/10 SERVICE BULLETIN No.: A330-32-3241

REVISION No.: 01 - Oct 06/11 Page: 4

7

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@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: 32

TITLE: LANDING GEAR - NOSE GEAR - ADDITION OF PRIMER PAINT TO THE

CADMIUM AROUND THE DOWEL BUSH HOLES ON THE MAIN FITTING

**CONF ALL

MODIFICATIONS

MODIFICATION CLASSIFICATION

MAJOR 200616H16400

MINOR None

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

Corrosion has been found on the main fitting of the NLG leg in the vicinity of the dowel pin bushes

retaining the lower steering flange on 15 A330/A340 aircraft. The majority of parts have been reworked

and returned to service.

Due to the potential consequence of the failure of the NLG leg main fitting, the widespread occurrence

of the corrosion throughout the A330/A340 fleet and the lack of opportunity for detection on certain

aircraft other than overhaul, modifications are required to eliminate the root cause of the corrosion.

This Service Bulletin is published to advise all operators of A330 aircraft of the issue of MESSIERDOWTY Service Bulletin No. D23581-32-066. MESSIER-DOWTY Service Bulletin No. D23581-32-066

is a cover Service Bulletin and introduces MESSIER-DOWTY Service Bulletin No. D23581-32-064 and

MESSIER-DOWTY Service Bulletin No. D23581-32-065.

This Service Bulletin (in conjunction with MESSIER-DOWTY Service Bulletin No. D23581-32-064)

introduces paint to the bare cadmium around the dowel hole in order to provide further protection

against cadmium degradation that is the root cause of the corrosion found in this area of the main

fitting.

DATE: Nov 26/10 SERVICE BULLETIN No.: A330-32-3241

REVISION No.: 01 - Oct 06/11 Page: 1

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@A330

SERVICE BULLETIN

SUMMARY

Accomplishment of this Service Bulletin, together with Service Bulletin A330-32-3242 (Mod. No.

200615H16360) (in conjunction with MESSIER-DOWTY Service Bulletin No. D23581-32-065), will make

sure that no corrosion exists in the vicinity of the dowel pin bushes and the likelihood of further

corrosion in the area will be reduced to an absolute minimum.

NOTE: Service Bulletin A330-32-3242 (Mod. No. 200615H16360) (in conjunction with

MESSIER-DOWTY Service Bulletin No. D23581-32-065), introduces an amended

interference fit between the bronze bushes and the steel (300M) main fitting and

amends the bush material from UZ19A6 to C63020.

The NLG main fitting, Primary Structural Element (PSE), part number change will be introduced into the

ALS Part 1 at the next scheduled revision.

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 YES

KIT PRICE (USD) SEE SB HIGH JACKING (NOSE) YES

NOTE (1): Service Bulletin must be accomplished.

MATERIAL PRICE INFORMATION

**CONF 001

No Material

**CONF 002

No Material

**CONF 003

No Material

**CONF 004

No Material

EFFECTIVITY

**CONF ALL

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

DATE: Nov 26/10 SERVICE BULLETIN No.: A330-32-3241

REVISION No.: 01 - Oct 06/11 Page: 2

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@A330

SERVICE BULLETIN

SUMMARY

44W 46W 78V 97X AAR AAW ACA ACI AEA AFL AFR ALK ASY

AVA AZA BEC BEL BER BMA BTV CAL CCA CES CHH CPA CRK

CRL CSC CSN CYP DAH DAL DGA DLH EDW EIN ETD EVA FIN

FWI G8E GFA GIA GRL HAL HDA HFY HVN I2L IAC ISS IWD

IYE JAI JST KAL KFR KKK KLM MAS MAU MEA MON MSR OBS

OHY OMA PAL QAF QFA QTR RJA RSF SAS SIA STZ SVA SWR

TAM TAP TCX THA THY TSC UAE UAF USA VKG VLK VOZ XAX

XLF

CONCURRENT REQUIREMENTS

Prior or simultaneous accomplishment of the following Service Bulletin(s) or the equivalent production

modification(s) is recommended:

Service Bulletin No. A330-32-3242 Mod. No. 200615H16360

REFERENCES / REPERCUSSIONS

TFU None

OEB None

AOT None

SIL None

LINE MAINTENANCE AFFECTED No

LIFE LIMIT None

OTHER None

NATURE OF THE WORK

AIRCRAFT YES

EQUIPMENT YES

HARD NO

SOFT NO

OBRM NO

MANPOWER

**CONF 001

Task 323241-831-895-001: MODIFICATION

TOTAL MANHOURS 12.00

ELAPSED TIME (HOURS) 6.00

Additional manhours related to Vendor SB; refer to:

MODIFY THE NLG/RNLG MESSIER-DOWTY Service Bulletin

No. D23581-32-066

MESSIER-DOWTY Service Bulletin

No. D23581-32-064

MESSIER-DOWTY Service Bulletin

No. D23581-32-065

RE-IDENTIFY THE NLG LEG AND MAIN

FITTING/SHOCK ABSORBER

MESSIER-DOWTY Service Bulletin

No. D23581-32-064

DATE: Nov 26/10 SERVICE BULLETIN No.: A330-32-3241

REVISION No.: 01 - Oct 06/11 Page: 3

7

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@A330

SERVICE BULLETIN

SUMMARY

**CONF 002

Task 323241-831-895-001: MODIFICATION

TOTAL MANHOURS 12.00

ELAPSED TIME (HOURS) 6.00

Additional manhours related to Vendor SB; refer to:

MODIFY THE NLG/RNLG MESSIER-DOWTY Service Bulletin

No. D23581-32-066

MESSIER-DOWTY Service Bulletin

No. D23581-32-064

MESSIER-DOWTY Service Bulletin

No. D23581-32-065

RE-IDENTIFY THE RNLG LEG AND MAIN

FITTING/SHOCK ABSORBER

MESSIER-DOWTY Service Bulletin

No. D23581-32-064

**CONF 003

Task 323241-831-895-001: MODIFICATION

TOTAL MANHOURS 12.00

ELAPSED TIME (HOURS) 6.00

Additional manhours related to Vendor SB; refer to:

MODIFY THE NLG/RNLG MESSIER-DOWTY Service Bulletin

No. D23581-32-066

MESSIER-DOWTY Service Bulletin

No. D23581-32-064

MESSIER-DOWTY Service Bulletin

No. D23581-32-065

RE-IDENTIFY THE NLG LEG AND MAIN

FITTING/SHOCK ABSORBER

MESSIER-DOWTY Service Bulletin

No. D23581-32-064

**CONF 004

Task 323241-831-895-001: MODIFICATION

TOTAL MANHOURS 12.00

ELAPSED TIME (HOURS) 6.00

Additional manhours related to Vendor SB; refer to:

MODIFY THE NLG/RNLG MESSIER-DOWTY Service Bulletin

No. D23581-32-066

MESSIER-DOWTY Service Bulletin

No. D23581-32-064

MESSIER-DOWTY Service Bulletin

No. D23581-32-065

RE-IDENTIFY THE RNLG LEG AND MAIN

FITTING/SHOCK ABSORBER

MESSIER-DOWTY Service Bulletin

No. D23581-32-064

DATE: Nov 26/10 SERVICE BULLETIN No.: A330-32-3241

REVISION No.: 01 - Oct 06/11 Page: 4

7

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@A330

SERVICE BULLETIN

SUMMARY

APPENDICES

**CONF ALL

APPENDIX 01 : ELAPSED TIME ASSUMPTION

DATE: Nov 26/10 SERVICE BULLETIN No.: A330-32-3241

REVISION No.: 01 - Oct 06/11 Page: 5

7

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@A330

SERVICE BULLETIN

SUMMARY

This Page Intentionally Left Blank

DATE: Nov 26/10 SERVICE BULLETIN No.: A330-32-3241

REVISION No.: 01 - Oct 06/11 Page: 6

7

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: 32

TITLE: LANDING GEAR - NOSE GEAR - ADDITION OF PRIMER PAINT TO THE

CADMIUM AROUND THE DOWEL BUSH HOLES ON THE MAIN FITTING

MODIFICATION No.: 200616H16400

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

330-202 330-203 330-223 330-243 330-243F 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 0059-0060 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

0489-0491 0493-0494 0496-0498 0500-0513 0515-0516 0518-0519 0521-0522

DATE: Nov 26/10 SERVICE BULLETIN No.: A330-32-3241

REVISION No.: 01 - Oct 06/11 Page: 1

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@A330

SERVICE BULLETIN

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 0925-0928 0930-0932 0934-0937

0939-0952 0954 0956-0959 0961-0971 0973-0980 0982-0986 0988-0992 0994-1004

1006-1016 1018-1023 1025-1026 1028-1029 1031-1039 1041-1049 1051-1055

1057-1063 1065-1067 1069-1078 1080-1082 1084-1090 1093-1101 1103-1108 1110

1112 1114 1116 1118 1120 1123-1124 1126-1127 1129-1133 1135 1137-1138 1141

1143 1145-1147 1149-1151 1153 1155-1157 1159-1161 1163

(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

44W 1002

46W 0871 0925

78V 1033 1046

97X 1053

AAR 0640 0676 0708 0772 0803 0845 1001 1055 1151

AAW 0999 1043

ACA 0277 0279 0284 0344 0400 0408 0412 0419

ACI 0507 0510

AEA 0461 0597 0733 0745 0749 0814 0931 0950

AFL 0963 0973 1014 1045 1047 1058 1065 1072 1077 1103

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

0567 0584 0657

ALK 0303 0306 0311 0313 0404

ASY 0747 0951 0969 1036

AVA 0948 0967 1009 1016 1073

AZA 0272 0339 1123 1135

BEC 0863

BEL 0030 0037 0045 0082 0095

BER 0120 0127 0171 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

DATE: Nov 26/10 SERVICE BULLETIN No.: A330-32-3241

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@A330

SERVICE BULLETIN

OPERATOR MSN

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

0884 0890 0903 0909 0930 0941 0944 0957 1087 1110 1130

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 1159

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 1163

CRK 1031 1034 1039 1042 1051 1054 1059 1062

CRL 0285 0320

CSC 1082 1138

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

0958 0964 1096 1116 1129

CYP 0505 0526

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 1025 1106

ETD 0658 0688 0717 0724 0729 0730 0737 0788 0809 0824 0832 0852

0854 0868 0975 0991 1032 1070 1071 1081

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

FIN 0994 1007 1013 1023 1067 1078 1088

FWI 0253 0758 0965 1021

G8E 0059

GFA 0276 0281 0286 0287 0334 0340 0527 0529 0532 0992

GIA 0138 0140 0144 0148 0153 0165 0988 1020 1028 1052

GRL 0230

HAL 1104 1114

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

0716 0741 0786

HFY 0096 1008

HVN 0255 0262 0275 0294 0299 0366 0943 0962 1019

I2L 0211 0407 0551

IAC 0353 0362

ISS 0665 0802 0822

IWD 0670 1097

IYE 0625 0627 0632

JAI 0751 0807 0825 0831 0882 0885 0888 0901 0923 0932 0947 0956

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 1133 1155

KFR 0874 0891 0927 0939 0946

DATE: Nov 26/10 SERVICE BULLETIN No.: A330-32-3241

REVISION No.: 01 - Oct 06/11 Page: 3

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@A330

SERVICE BULLETIN

OPERATOR MSN

KKK 0343 0358 0364

KLM 0682 0686 0703 0738 0770 0801 0811 0819 0834 0900 1161

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

MAU 0883 1057

MEA 0926 0984 0995 0998

MON 0261 0265

MSR 0600 0610 0666 0683 0696 0709 0726 1143

OBS 0833

OHY 0072 0087 0098 0143

OMA 1038 1044 1049 1063 1093 1120

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 1061 1094

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

RSF 0980 0996

SAS 0496 0497 0515 0568

SIA 0978 0983 0986 0997 1006 1010 1012 1015 1085 1098 1099 1105

1107 1124 1132 1146 1149 1156 1157

STZ 0324

SVA 1108 1127 1137 1141 1147 1153

SWR 0229 0249 0288 0322 1000 1018 1026 1029 1084 1089 1101 1145

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

0949 0961 0968 0977 1112 1118

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

TCX 0254 0266 0301 0427 0456 0795

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

0990 1003 1035 1037 1060 1074 1086 1090

THY 0463 0504 0697 0704 0742 0754 0774 1004 1150 1160

TSC 0111 0132 0177 0250 0271 0369 0480 0966 0971

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

0384 0392 0396 0409 0437 0451 0452 0455 0462 0491 0494 0509

0518 0525 0536

UAF 1080

USA 0315 0323 0333 0337 0342 0370 0375 0380 0388 1011 1022 1041

1069 1076 1095 1100

VKG 0309 0349 0356 0357

VLK 0055 0070 0086

VOZ 0365 0372

XAX 0054 0952 0974 1048 1066 1075 1126 1131

XLF 0501 0635

DATE: Nov 26/10 SERVICE BULLETIN No.: A330-32-3241

REVISION No.: 01 - Oct 06/11 Page: 4

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SERVICE BULLETIN

(4) Configuration by MSN

MSN CONFIGURATION

0012 0072 0082 0087 0095 0120 0121 003 004

DATE: Nov 26/10 SERVICE BULLETIN No.: A330-32-3241

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@A330

SERVICE BULLETIN

MSN CONFIGURATION

0017 0127 0143 0155 0162 0171 0172 0181 0195 0206 0219

0222 0223 0226 0229 0230 0232 0238 0240 0241 0244 0247

0248 0249 0250 0251 0253 0254 0255 0256 0258 0259 0261

0262 0265 0266 0267 0269 0271 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

0925 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 0980 0982 0983 0984 0985 0986 0988

0989 0990 0991 0992 0994 0995 0996 0997 0998 0999 1000

004

DATE: Nov 26/10 SERVICE BULLETIN No.: A330-32-3241

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@A330

SERVICE BULLETIN

MSN CONFIGURATION

1001 1002 1003 1004 1006 1007 1008 1009 1010 1011 1012

1013 1014 1015 1016 1018 1019 1020 1021 1022 1023 1025

1026 1028 1029 1031 1032 1033 1034 1035 1036 1037 1038

1039 1041 1042 1043 1044 1045 1046 1047 1048 1049 1051

1052 1053 1054 1055 1057 1058 1059 1060 1061 1062 1063

1065 1066 1067 1069 1070 1071 1072 1073 1074 1075 1076

1077 1078 1080 1081 1082 1084 1085 1086 1087 1088 1089

1090 1093 1094 1095 1096 1097 1098 1099 1100 1101 1103

1104 1105 1106 1107 1108 1110 1112 1114 1116 1118 1120

1123 1124 1126 1127 1129 1130 1131 1132 1133 1135 1137

1138 1141 1143 1145 1146 1147 1149 1150 1151 1153 1155

1156 1157 1159 1160 1161 1163

004

0030 0037 0045 0050 0054 0055 0059 0060 0062 0064 0065

0066 0067 0069 0070 0071 0073 0077 0083 0086 0096 0099

0100 0102 0106 0107 0109 0110 0111 0112 0113 0116 0118

0119 0122

001 002

0098 0132 0138 0140 0144 0148 0153 0165 0177 0183 0184

0188 0189 0191 0198 0200 0203 0205 0209 0211 0224 0231

0234 0272

002

(5) Configuration definition

**CONF 001

Config. 01 is valid for aircraft that are Pre Modification 42392H13043 (Service Bulletin

A330-32-3116 (LANDING GEAR - NOSE GEAR - FIT REINFORCED NOSE GEAR))

and Pre Modification 43442H13038 (Service Bulletin A330-32-3030 (LANDING GEAR -

NOSE GEAR - NLG WITH OVERSTEER WARNING)).

**CONF 002

Config. 02 is valid for aircraft that are Post Modification 42392H13043 (Service Bulletin

A330-32-3116 (LANDING GEAR - NOSE GEAR - FIT REINFORCED NOSE GEAR))

and Pre Modification 43442H13038 (Service Bulletin A330-32-3030 (LANDING GEAR -

NOSE GEAR - NLG WITH OVERSTEER WARNING)).

**CONF 003

Config. 03 is valid for aircraft that are Pre Modification 42392H13043 (Service Bulletin

A330-32-3116 (LANDING GEAR - NOSE GEAR - FIT REINFORCED NOSE GEAR))

and Post Modification 43442H13038 (Service Bulletin A330-32-3030 (LANDING GEAR -

NOSE GEAR - NLG WITH OVERSTEER WARNING)).

**CONF 004

Config. 04 is valid for aircraft that are Post Modification 42392H13043 (Service Bulletin

A330-32-3116 (LANDING GEAR - NOSE GEAR - FIT REINFORCED NOSE GEAR))

and Post Modification 43442H13038 (Service Bulletin A330-32-3030 (LANDING GEAR -

NOSE GEAR - NLG WITH OVERSTEER WARNING)).

DATE: Nov 26/10 SERVICE BULLETIN No.: A330-32-3241

REVISION No.: 01 - Oct 06/11 Page: 7

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@A330

SERVICE BULLETIN

(6) Material Effectivity

**CONF 001, 003

MATERIAL QTY PER A/C SEE NOTES

Reidentified part set REIDB01 1

**CONF 002, 004

MATERIAL QTY PER A/C SEE NOTES

Reidentified part set REIDB02 1

**CONF ALL

B. CONCURRENT REQUIREMENTS

Prior or simultaneous accomplishment of the following Service Bulletin(s) or the equivalent

production modification(s) is recommended:

Service Bulletin No. A330-32-3242 Mod. No. 200615H16360

C. REASON

(1) History

Corrosion has been found on the main fitting of the NLG leg in the vicinity of the dowel

pin bushes retaining the lower steering flange on 15 A330/A340 aircraft. The majority of

parts have been reworked and returned to service.

Due to the potential consequence of the failure of the NLG leg main fitting, the

widespread occurrence of the corrosion throughout the A330/A340 fleet and the lack

of opportunity for detection on certain aircraft other than overhaul, modifications are

required to eliminate the root cause of the corrosion.

(2) Objective/Action

This Service Bulletin is published to advise all operators of A330 aircraft of the issue

of MESSIER-DOWTY Service Bulletin No. D23581-32-066. MESSIER-DOWTY Service

Bulletin No. D23581-32-066 is a cover Service Bulletin and introduces MESSIERDOWTY Service Bulletin No. D23581-32-064 and MESSIER-DOWTY Service Bulletin

No. D23581-32-065.

This Service Bulletin (in conjunction with MESSIER-DOWTY Service Bulletin No.

D23581-32-064) introduces paint to the bare cadmium around the dowel hole in order to

provide further protection against cadmium degradation that is the root cause of the

corrosion found in this area of the main fitting.

DATE: Nov 26/10 SERVICE BULLETIN No.: A330-32-3241

REVISION No.: 01 - Oct 06/11 Page: 8

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SERVICE BULLETIN

(3) Advantages

Accomplishment of this Service Bulletin, together with Service Bulletin A330-32-3242

(Mod. No. 200615H16360) (in conjunction with MESSIER-DOWTY Service Bulletin No.

D23581-32-065), will make sure that no corrosion exists in the vicinity of the dowel pin

bushes and the likelihood of further corrosion in the area will be reduced to an absolute

minimum.

NOTE: Service Bulletin A330-32-3242 (Mod. No. 200615H16360) (in conjunction

with MESSIER-DOWTY Service Bulletin No. D23581-32-065), introduces

an amended interference fit between the bronze bushes and the steel

(300M) main fitting and amends the bush material from UZ19A6 to

C63020.

(4) Operational/Maintenance Consequences

The NLG main fitting, Primary Structural Element (PSE), part number change will be

introduced into the ALS Part 1 at the next scheduled revision.

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

**CONF 001

Task 323241-831-895-001: MODIFICATION

(1) REMOVE NLG/RNLG LEG COMPONENTS

(2) MODIFY THE NLG/RNLG

(3) INSTALL THE NLG/RNLG LEG COMPONENTS

(4) RE-IDENTIFY THE NLG LEG AND MAIN FITTING/SHOCK ABSORBER

**CONF 002

Task 323241-831-895-001: MODIFICATION

(1) REMOVE NLG/RNLG LEG COMPONENTS

(2) MODIFY THE NLG/RNLG

(3) INSTALL THE NLG/RNLG LEG COMPONENTS

(4) RE-IDENTIFY THE RNLG LEG AND MAIN FITTING/SHOCK ABSORBER

**CONF 003

Task 323241-831-895-001: MODIFICATION

(1) REMOVE NLG/RNLG LEG COMPONENTS

(2) MODIFY THE NLG/RNLG

DATE: Nov 26/10 SERVICE BULLETIN No.: A330-32-3241

REVISION No.: 01 - Oct 06/11 Page: 9

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@A330

SERVICE BULLETIN

(3) INSTALL THE NLG/RNLG LEG COMPONENTS

(4) RE-IDENTIFY THE NLG LEG AND MAIN FITTING/SHOCK ABSORBER

**CONF 004

Task 323241-831-895-001: MODIFICATION

(1) REMOVE NLG/RNLG LEG COMPONENTS

(2) MODIFY THE NLG/RNLG

(3) INSTALL THE NLG/RNLG LEG COMPONENTS

(4) RE-IDENTIFY THE RNLG LEG AND MAIN FITTING/SHOCK ABSORBER

**CONF ALL

E. COMPLIANCE

(1) Classification

MANDATORY: Service Bulletin must be accomplished.

(2) Accomplishment Timescale

Accomplishment of this Service Bulletin is expected to be rendered mandatory by the

issue of an Airworthiness Directive (AD) published by the European Aviation Safety

Agency (EASA). The accomplishment timescale, which has not yet been defined, will be

given in the AD.

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.

DATE: Nov 26/10 SERVICE BULLETIN No.: A330-32-3241

REVISION No.: 01 - Oct 06/11 Page: 10

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@A330

SERVICE BULLETIN

**CONF 001

Task 323241-831-895-001: MODIFICATION

Get Access 2.00

On Aircraft

REMOVE NLG/RNLG LEG COMPONENTS 2.00

INSTALL THE NLG/RNLG LEG COMPONENTS 2.00

Tests 4.00

Close-Up 2.00

TOTAL MANHOURS 12.00

ELAPSED TIME (HOURS) 6.00

Additional manhours related to Vendor SB; refer to:

MODIFY THE NLG/RNLG MESSIER-DOWTY Service Bulletin

No. D23581-32-066

MESSIER-DOWTY Service Bulletin

No. D23581-32-064

MESSIER-DOWTY Service Bulletin

No. D23581-32-065

RE-IDENTIFY THE NLG LEG AND MAIN

FITTING/SHOCK ABSORBER

MESSIER-DOWTY Service Bulletin

No. D23581-32-064

**CONF 002

Task 323241-831-895-001: MODIFICATION

Get Access 2.00

On Aircraft

REMOVE NLG/RNLG LEG COMPONENTS 2.00

INSTALL THE NLG/RNLG LEG COMPONENTS 2.00

Tests 4.00

Close-Up 2.00

TOTAL MANHOURS 12.00

ELAPSED TIME (HOURS) 6.00

Additional manhours related to Vendor SB; refer to:

MODIFY THE NLG/RNLG MESSIER-DOWTY Service Bulletin

No. D23581-32-066

MESSIER-DOWTY Service Bulletin

No. D23581-32-064

MESSIER-DOWTY Service Bulletin

No. D23581-32-065

RE-IDENTIFY THE RNLG LEG AND MAIN

FITTING/SHOCK ABSORBER

MESSIER-DOWTY Service Bulletin

No. D23581-32-064

**CONF 003

Task 323241-831-895-001: MODIFICATION

Get Access 2.00

On Aircraft

DATE: Nov 26/10 SERVICE BULLETIN No.: A330-32-3241

REVISION No.: 01 - Oct 06/11 Page: 11

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@A330

SERVICE BULLETIN

Task 323241-831-895-001: MODIFICATION

REMOVE NLG/RNLG LEG COMPONENTS 2.00

INSTALL THE NLG/RNLG LEG COMPONENTS 2.00

Tests 4.00

Close-Up 2.00

TOTAL MANHOURS 12.00

ELAPSED TIME (HOURS) 6.00

Additional manhours related to Vendor SB; refer to:

MODIFY THE NLG/RNLG MESSIER-DOWTY Service Bulletin

No. D23581-32-066

MESSIER-DOWTY Service Bulletin

No. D23581-32-064

MESSIER-DOWTY Service Bulletin

No. D23581-32-065

RE-IDENTIFY THE NLG LEG AND MAIN

FITTING/SHOCK ABSORBER

MESSIER-DOWTY Service Bulletin

No. D23581-32-064

**CONF 004

Task 323241-831-895-001: MODIFICATION

Get Access 2.00

On Aircraft

REMOVE NLG/RNLG LEG COMPONENTS 2.00

INSTALL THE NLG/RNLG LEG COMPONENTS 2.00

Tests 4.00

Close-Up 2.00

TOTAL MANHOURS 12.00

ELAPSED TIME (HOURS) 6.00

Additional manhours related to Vendor SB; refer to:

MODIFY THE NLG/RNLG MESSIER-DOWTY Service Bulletin

No. D23581-32-066

MESSIER-DOWTY Service Bulletin

No. D23581-32-064

MESSIER-DOWTY Service Bulletin

No. D23581-32-065

RE-IDENTIFY THE RNLG LEG AND MAIN

FITTING/SHOCK ABSORBER

MESSIER-DOWTY Service Bulletin

No. D23581-32-064

**CONF ALL

H. WEIGHT AND BALANCE

Not Changed

I. ELECTRICAL LOAD DATA

Not Changed

DATE: Nov 26/10 SERVICE BULLETIN No.: A330-32-3241

REVISION No.: 01 - Oct 06/11 Page: 12

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@A330

SERVICE BULLETIN

J. REFERENCES

**CONF 001

Aircraft Maintenance Manual (AMM) 07-11-00 12-12-32 12-14-32

12-34-24 20-11-11 20-21-11

29-00-00 32-00-00 32-21-27

32-31-00 32-49-00 32-51-00

32-51-27 32-51-41

ATA Common Support Data Dictionary (CSDD),

Chapter 2

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

Service Bulletin (SB) A330-32-3242

Vendor Service Bulletin (VSB) MESSIER-DOWTY Service Bulletin

No. D23581-32-064

MESSIER-DOWTY Service Bulletin

No. D23581-32-065

MESSIER-DOWTY Service Bulletin

No. D23581-32-066

**CONF 002

Aircraft Maintenance Manual (AMM) 07-11-00 12-12-32 12-14-32

12-34-24 20-11-11 20-21-11

29-00-00 32-00-00 32-21-27

32-31-00 32-49-00 32-51-00

32-51-27 32-51-41

ATA Common Support Data Dictionary (CSDD),

Chapter 2

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

Service Bulletin (SB) A330-32-3242

Vendor Service Bulletin (VSB) MESSIER-DOWTY Service Bulletin

No. D23581-32-064

MESSIER-DOWTY Service Bulletin

No. D23581-32-065

MESSIER-DOWTY Service Bulletin

No. D23581-32-066

**CONF 003

Aircraft Maintenance Manual (AMM) 07-11-00 12-12-32 12-14-32

12-34-24 20-11-11 20-21-11

29-00-00 32-00-00 32-21-27

32-31-00 32-49-00 32-51-00

32-51-27 32-51-41 32-53-00

32-53-12

DATE: Nov 26/10 SERVICE BULLETIN No.: A330-32-3241

REVISION No.: 01 - Oct 06/11 Page: 13

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@A330

SERVICE BULLETIN

ATA Common Support Data Dictionary (CSDD),

Chapter 2

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

Service Bulletin (SB) A330-32-3242

Vendor Service Bulletin (VSB) MESSIER-DOWTY Service Bulletin

No. D23581-32-064

MESSIER-DOWTY Service Bulletin

No. D23581-32-065

MESSIER-DOWTY Service Bulletin

No. D23581-32-066

**CONF 004

Aircraft Maintenance Manual (AMM) 07-11-00 12-12-32 12-14-32

12-34-24 20-11-11 20-21-11

29-00-00 32-00-00 32-21-27

32-31-00 32-49-00 32-51-00

32-51-27 32-51-41 32-53-00

32-53-12

ATA Common Support Data Dictionary (CSDD),

Chapter 2

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

Service Bulletin (SB) A330-32-3242

Vendor Service Bulletin (VSB) MESSIER-DOWTY Service Bulletin

No. D23581-32-064

MESSIER-DOWTY Service Bulletin

No. D23581-32-065

MESSIER-DOWTY Service Bulletin

No. D23581-32-066

**CONF ALL

K. PUBLICATION AFFECTED

Illustrated Parts Catalog (IPC) 32-21-11 32-21-13

L. INTERCHANGEABILITY/MIXABILITY

**CONF 001

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE

NOTES

Leg Assy D23285101-XX D23285101-27 01 Not

Applicable

Leg Assy D23285101-XXX D23285101-127 01 Not

Applicable

Leg Assy D23285151-XX D23285151-27 01 Not

Applicable

Leg Assy D23285151-XXX D23285151-127 01 Not

Applicable

DATE: Nov 26/10 SERVICE BULLETIN No.: A330-32-3241

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SERVICE BULLETIN

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE

NOTES

Leg Assy D23285001-XX D23285001-33 01 Not

Applicable

Leg Assy D23285001-XXX D23285001-133 01 Not

Applicable

Leg Assy D23285051-XX D23285051-33 01 Not

Applicable

Leg Assy D23285051-XXX D23285051-133 01 Not

Applicable

Leg Assy D23285001-XX D23285001-323 01 Not

Applicable

Leg Assy D23285051-XX D23285051-323 01 Not

Applicable

Leg Assy D23285001-XX D23285001-223 01 Not

Applicable

Leg Assy D23285051-XX D23285051-223 01 Not

Applicable

Leg Assy D23285101-XX D23285101-317 01 Not

Applicable

Leg Assy D23285151-XX D23285151-317 01 Not

Applicable

Leg Assy D23285101-XX D23285101-217 01 Not

Applicable

Leg Assy D23285151-XX D23285151-217 01 Not

Applicable

Main Fitting Shock

Absorber

D23286100-XX D23286100-18 01 Not

Applicable

Main Fitting Shock

Absorber

D23286100-XXX D23286100-118 01 Not

Applicable

Main Fitting Shock

Absorber

D23286001-XX D23286001-22 01 Not

Applicable

Main Fitting Shock

Absorber

D23286001-XXX D23286001-122 01 Not

Applicable

Main Fitting Shock

Absorber

D23286001-XX D23286001-315 01 Not

Applicable

Main Fitting Shock

Absorber

D23286001-XX D23286001-215 01 Not

Applicable

Main Fitting Shock

Absorber

D23286100-XX D23286100-311 01 Not

Applicable

Main Fitting Shock

Absorber

D23286100-XX D23286100-211 01 Not

Applicable

NOTE: For definitions of interchangeability codes in column INT., refer to ATA

Common Support Data Dictionary (CSDD), Chapter 2.

DATE: Nov 26/10 SERVICE BULLETIN No.: A330-32-3241

REVISION No.: 01 - Oct 06/11 Page: 15

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SERVICE BULLETIN

**CONF 002

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE

NOTES

Leg Assy D23581100-XX D23581100-18 01 Not

Applicable

Leg Assy D23581100-XXX D23581100-118 01 Not

Applicable

Leg Assy D23581150-XX D23581150-18 01 Not

Applicable

Leg Assy D23581150-XXX D23581150-118 01 Not

Applicable

Leg Assy D23581200 D23581200-1 01 Not

Applicable

Leg Assy D23581300-XX D23581300-18 01 Not

Applicable

Leg Assy D23581300-XXX D23581300-118 01 Not

Applicable

Leg Assy D23581350-XX D23581350-18 01 Not

Applicable

Leg Assy D23581350-XXX D23581350-118 01 Not

Applicable

Main Fitting Shock

Absorber

D23582100-XX D23582100-11 01 Not

Applicable

Main Fitting Shock

Absorber

D23582100-XXX D23582100-112 01 Not

Applicable

Main Fitting Shock

Absorber

D23582100-XXX D23582100-311 01 Not

Applicable

Main Fitting Shock

Absorber

D23582100-XXX D23582100-212 01 Not

Applicable

Main Fitting Shock

Absorber

D23582200 D23582200-1 01 Not

Applicable

Main Fitting Shock

Absorber

D23582210 D23582210-1 01 Not

Applicable

Main Fitting Shock

Absorber

D23582300-XX D23582300-11 01 Not

Applicable

Main Fitting Shock

Absorber

D23582300-XXX D23582300-112 01 Not

Applicable

Main Fitting Shock

Absorber

D23582300-XXX D23582300-311 01 Not

Applicable

Main Fitting Shock

Absorber

D23582300-XXX D23582300-212 01 Not

Applicable

NOTE: For definitions of interchangeability codes in column INT., refer to ATA

Common Support Data Dictionary (CSDD), Chapter 2.

DATE: Nov 26/10 SERVICE BULLETIN No.: A330-32-3241

REVISION No.: 01 - Oct 06/11 Page: 16

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**CONF 003

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE

NOTES

Leg Assy D23285101-XX D23285101-27 01 Not

Applicable

Leg Assy D23285101-XXX D23285101-127 01 Not

Applicable

Leg Assy D23285151-XX D23285151-27 01 Not

Applicable

Leg Assy D23285151-XXX D23285151-127 01 Not

Applicable

Leg Assy D23285001-XX D23285001-33 01 Not

Applicable

Leg Assy D23285001-XXX D23285001-133 01 Not

Applicable

Leg Assy D23285051-XX D23285051-33 01 Not

Applicable

Leg Assy D23285051-XXX D23285051-133 01 Not

Applicable

Leg Assy D23285001-XX D23285001-323 01 Not

Applicable

Leg Assy D23285051-XX D23285051-323 01 Not

Applicable

Leg Assy D23285001-XX D23285001-223 01 Not

Applicable

Leg Assy D23285051-XX D23285051-223 01 Not

Applicable

Leg Assy D23285101-XX D23285101-317 01 Not

Applicable

Leg Assy D23285151-XX D23285151-317 01 Not

Applicable

Leg Assy D23285101-XX D23285101-217 01 Not

Applicable

Leg Assy D23285151-XX D23285151-217 01 Not

Applicable

Main Fitting Shock

Absorber

D23286100-XX D23286100-18 01 Not

Applicable

Main Fitting Shock

Absorber

D23286100-XXX D23286100-118 01 Not

Applicable

Main Fitting Shock

Absorber

D23286001-XX D23286001-22 01 Not

Applicable

Main Fitting Shock

Absorber

D23286001-XXX D23286001-122 01 Not

Applicable

Main Fitting Shock

Absorber

D23286001-XX D23286001-315 01 Not

Applicable

DATE: Nov 26/10 SERVICE BULLETIN No.: A330-32-3241

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DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE

NOTES

Main Fitting Shock

Absorber

D23286001-XX D23286001-215 01 Not

Applicable

Main Fitting Shock

Absorber

D23286100-XX D23286100-311 01 Not

Applicable

Main Fitting Shock

Absorber

D23286100-XX D23286100-211 01 Not

Applicable

NOTE: For definitions of interchangeability codes in column INT., refer to ATA

Common Support Data Dictionary (CSDD), Chapter 2.

**CONF 004

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE

NOTES

Leg Assy D23581100-XX D23581100-18 01 Not

Applicable

Leg Assy D23581100-XXX D23581100-118 01 Not

Applicable

Leg Assy D23581150-XX D23581150-18 01 Not

Applicable

Leg Assy D23581150-XXX D23581150-118 01 Not

Applicable

Leg Assy D23581200 D23581200-1 01 Not

Applicable

Leg Assy D23581300-XX D23581300-18 01 Not

Applicable

Leg Assy D23581300-XXX D23581300-118 01 Not

Applicable

Leg Assy D23581350-XX D23581350-18 01 Not

Applicable

Leg Assy D23581350-XXX D23581350-118 01 Not

Applicable

Main Fitting Shock

Absorber

D23582100-XX D23582100-11 01 Not

Applicable

Main Fitting Shock

Absorber

D23582100-XXX D23582100-112 01 Not

Applicable

Main Fitting Shock

Absorber

D23582100-XXX D23582100-311 01 Not

Applicable

Main Fitting Shock

Absorber

D23582100-XXX D23582100-212 01 Not

Applicable

Main Fitting Shock

Absorber

D23582200 D23582200-1 01 Not

Applicable

Main Fitting Shock

Absorber

D23582210 D23582210-1 01 Not

Applicable

DATE: Nov 26/10 SERVICE BULLETIN No.: A330-32-3241

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SERVICE BULLETIN

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE

NOTES

Main Fitting Shock

Absorber

D23582300-XX D23582300-11 01 Not

Applicable

Main Fitting Shock

Absorber

D23582300-XXX D23582300-112 01 Not

Applicable

Main Fitting Shock

Absorber

D23582300-XXX D23582300-311 01 Not

Applicable

Main Fitting Shock

Absorber

D23582300-XXX D23582300-212 01 Not

Applicable

NOTE: For definitions of interchangeability codes in column INT., refer to ATA

Common Support Data Dictionary (CSDD), Chapter 2.

**CONF ALL

M. SPARES

None

DATE: Nov 26/10 SERVICE BULLETIN No.: A330-32-3241

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This Page Intentionally Left Blank

DATE: Nov 26/10 SERVICE BULLETIN No.: A330-32-3241

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SERVICE BULLETIN

2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

(1) Procurement Addresses

Modification of removed equipment should be negotiated directly with

MESSIER_DOWTY as per instructions given in Vendor Service Bulletin (VSB) No.

D23581-32-064.

(2) Price and Availability

Refer to the MESSIER-DOWTY VSB No. D23581-32-064 for the equipment modification

sales terms.

B. INDUSTRY SUPPORT INFORMATION

Refer to the MESSIER-DOWTY VSB No. D23581-32-064 for the industry support terms.

C. LIST OF COMPONENTS

No Kit

D. LIST OF MATERIALS - OPERATOR SUPPLIED

(1) Consumable Materials

NOTE: To accomplish this Service Bulletin it will be necessary to use the

consumable items listed in AMM 32-51-41-000-801.

(2) Components

NOTE: To accomplish this Service Bulletin it will be necessary to use the

expendable parts listed in AMM 32-51-41-000-801.

(3) Equipment

None

E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

Refer to the MESSIER-DOWTY VSB No. D23581-32-064 for the re-identification of the parts.

Reidentified part set REIDB01

ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE

NOTES

D23285001-133 Leg D23285001-XXX

D23285001-223 Leg D23285001-XX

D23285001-323 Leg D23285001-XX

D23285001-33 Leg D23285001-XX

DATE: Nov 26/10 SERVICE BULLETIN No.: A330-32-3241

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ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE

NOTES

D23285051-133 Leg D23285051-XXX

D23285051-223 Leg D23285051-XX

D23285051-323 Leg D23285051-XX

D23285051-33 Leg D23285051-XX

D23285101-127 Leg D23285101-XXX

D23285101-217 Leg D23285101-XX

D23285101-27 Leg D23285101-XX

D23285101-317 Leg D23285101-XX

D23285151-127 Leg D23285151-XXX

D23285151-217 Leg D23285151-XX

D23285151-27 Leg D23285151-XX

D23285151-317 Leg D23285151-XX

D23286001-122 Fitting D23286001-XXX

D23286001-215 Fitting D23286001-XX

D23286001-22 Fitting D23286001-XX

D23286001-315 Fitting D23286001-XX

D23286100-118 Fitting D23286100-XXX

D23286100-18 Fitting D23286100-XX

D23286100-211 Fitting D23286100-XX

D23286100-311 Fitting D23286100-XX

Reidentified part set REIDB02

ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE

NOTES

D23581100-118 Leg D23581100-XXX

D23581100-18 Leg D23581100-XX

D23581150-118 Leg D23581150-XXX

D23581150-18 Leg D23581150-XX

D23581200-1 Leg D23581200

D23581300-118 Leg D23581300-XXX

D23581300-18 Leg D23581300-XX

D23581350-118 Leg D23581350-XXX

D23581350-18 Leg D23581350-XX

D23582100-11 Fitting D23582100-XX

D23582100-112 Fitting D23582100-XXX

D23582100-212 Fitting D23582100-XXX

D23582100-311 Fitting D23582100-XXX

D23582200-1 Fitting D23582200

D23582210-1 Fitting D23582210

D23582300-11 Fitting D23582300-XX

DATE: Nov 26/10 SERVICE BULLETIN No.: A330-32-3241

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ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE

NOTES

D23582300-112 Fitting D23582300-XXX

D23582300-212 Fitting D23582300-XXX

D23582300-311 Fitting D23582300-XXX

F. TOOLING

(1) Tooling - Price and Availability

Refer to the MESSIER-DOWTY VSB No. D23581-32-064 for tooling price information.

(2) Tools

NOTE: To accomplish this Service Bulletin it will be necessary to use the

standard tools listed in AMM 32-51-41-000-801.

(3) Special Tools

Refer to the MESSIER-DOWTY VSB No. D23581-32-064 for special tooling information.

DATE: Nov 26/10 SERVICE BULLETIN No.: A330-32-3241

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SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS

Task 323241-831-895-001 - MODIFICATION

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.

Task Associated Data

**CONF 001

Manpower

TOTAL MANHOURS 12.00

ELAPSED TIME (HOURS) 6.00

Additional manhours related to Vendor SB; refer to:

MESSIER-DOWTY Service Bulletin No. D23581-32-066

MESSIER-DOWTY Service Bulletin No. D23581-32-064

MESSIER-DOWTY Service Bulletin No. D23581-32-065

**CONF 002

Manpower

TOTAL MANHOURS 12.00

ELAPSED TIME (HOURS) 6.00

Additional manhours related to Vendor SB; refer to:

MESSIER-DOWTY Service Bulletin No. D23581-32-066

MESSIER-DOWTY Service Bulletin No. D23581-32-064

MESSIER-DOWTY Service Bulletin No. D23581-32-065

DATE: Nov 26/10 SERVICE BULLETIN No.: A330-32-3241

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SERVICE BULLETIN

**CONF 003

Manpower

TOTAL MANHOURS 12.00

ELAPSED TIME (HOURS) 6.00

Additional manhours related to Vendor SB; refer to:

MESSIER-DOWTY Service Bulletin No. D23581-32-066

MESSIER-DOWTY Service Bulletin No. D23581-32-064

MESSIER-DOWTY Service Bulletin No. D23581-32-065

**CONF 004

Manpower

TOTAL MANHOURS 12.00

ELAPSED TIME (HOURS) 6.00

Additional manhours related to Vendor SB; refer to:

MESSIER-DOWTY Service Bulletin No. D23581-32-066

MESSIER-DOWTY Service Bulletin No. D23581-32-064

MESSIER-DOWTY Service Bulletin No. D23581-32-065

**CONF ALL

A. GENERAL

**CONF 001

(1) Subtask 323241-839-401-001 - ADMINISTRATIVE

Manpower Resources

Skills AIRFRAME

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

Service Bulletin.

(2) Subtask 323241-910-401-001 - STANDARD PRACTICES

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 20-11-11-911-803

Task 20-21-11-911-801

(a) For wirelocking, refer to AMM Task 20-11-11-911-803.

(b) For torque tightening of standard threaded fasteners, refer to AMM Task

20-21-11-911-801.

DATE: Nov 26/10 SERVICE BULLETIN No.: A330-32-3241

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SERVICE BULLETIN

**CONF 002

(1) Subtask 323241-839-401-001 - ADMINISTRATIVE

Manpower Resources

Skills AIRFRAME

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

Service Bulletin.

(2) Subtask 323241-910-401-001 - STANDARD PRACTICES

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 20-11-11-911-803

Task 20-21-11-911-801

(a) For wirelocking, refer to AMM Task 20-11-11-911-803.

(b) For torque tightening of standard threaded fasteners, refer to AMM Task

20-21-11-911-801.

**CONF 003

(1) Subtask 323241-839-401-001 - ADMINISTRATIVE

Manpower Resources

Skills AIRFRAME

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

Service Bulletin.

(2) Subtask 323241-910-401-001 - STANDARD PRACTICES

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 20-11-11-911-803

Task 20-21-11-911-801

(a) For wirelocking, refer to AMM Task 20-11-11-911-803.

(b) For torque tightening of standard threaded fasteners, refer to AMM Task

20-21-11-911-801.

DATE: Nov 26/10 SERVICE BULLETIN No.: A330-32-3241

REVISION No.: 01 - Oct 06/11 Page: 27

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SERVICE BULLETIN

**CONF 004

(1) Subtask 323241-839-401-001 - ADMINISTRATIVE

Manpower Resources

Skills AIRFRAME

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

Service Bulletin.

(2) Subtask 323241-910-401-001 - STANDARD PRACTICES

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 20-11-11-911-803

Task 20-21-11-911-801

(a) For wirelocking, refer to AMM Task 20-11-11-911-803.

(b) For torque tightening of standard threaded fasteners, refer to AMM Task

20-21-11-911-801.

**CONF ALL

B. PREPARATION

**CONF 001

(1) Subtask 323241-941-401-001 - JOB SET-UP

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 07-11-00-581-801

Task 07-11-00-581-802

Task 12-14-32-614-814

Task 12-34-24-860-802

Task 29-00-00-864-801

Task 32-00-00-481-801

Task 32-00-00-481-802

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

12-34-24-860-802).

(b) Make sure that the safety devices are installed in the landing gear and landing gear

doors (Refer to AMM Task 32-00-00-481-801 and AMM Task 32-00-00-481-802).

DATE: Nov 26/10 SERVICE BULLETIN No.: A330-32-3241

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(c) On the NLG, do a check of the suffix number of the Part Number on the NLG leg

nameplate and the main fitting/shock absorber nameplate:

- If the NLG (65 ̊) leg PN D23285101 suffix is -27 and the main fitting/shock

absorber PN D23286100 suffix is -18, record that this Service Bulletin is

accomplished, no more work is necessary.

- If the NLG (65 ̊) leg PN D23285151 suffix is -27 and the main fitting/shock

absorber PN D23286100 suffix is -18, record that this Service Bulletin is

accomplished, no more work is necessary.

- If the Std NLG (65 ̊) leg PN D23285001 suffix is -33 and the main fitting/shock

absorber PN D23286001 suffix is -22, record that this Service Bulletin is

accomplished, no more work is necessary.

- If the WBS NLG (65 ̊) leg PN D23285051 suffix is -33 and the main

fitting/shock absorber PN D23286001 suffix is -22, record that this Service

Bulletin is accomplished, no more work is necessary.

- If the Std NLG (60 ̊) leg PN D23285101 suffix is -127 and the main

fitting/shock absorber PN D23286100 suffix is -118, record that this Service

Bulletin is accomplished, no more work is necessary.

- If the WBS NLG (60 ̊) leg PN D23285151 suffix is -127 and the main

fitting/shock absorber PN D23286100 suffix is -118, record that this Service

Bulletin is accomplished, no more work is necessary.

- If the Std NLG (60 ̊) leg PN D23285001 suffix is -133 and the main

fitting/shock absorber PN D23286001 suffix is -122, record that this Service

Bulletin is accomplished, no more work is necessary.

- If the WBS NLG (60 ̊) leg PN D23285051 suffix is -133 and the main

fitting/shock absorber PN D23286001 suffix is -122, record that this Service

Bulletin is accomplished, no more work is necessary.

- If the WBS NLG (60 ̊) leg PN D23285001 suffix is -323 and the main

fitting/shock absorber PN D23286001 suffix is -315, record that this Service

Bulletin is accomplished, no more work is necessary.

- If the WBS NLG (60 ̊) leg PN D23285051 suffix is -323 and the main

fitting/shock absorber PN D23286001 suffix is -315, record that this Service

Bulletin is accomplished, no more work is necessary.

- If the WBS NLG (60 ̊) leg PN D23285101 suffix is -317 and the main

fitting/shock absorber PN D23286001 suffix is -311, record that this Service

Bulletin is accomplished, no more work is necessary.

- If the WBS NLG (60 ̊) leg PN D23285151 suffix is -317 and the main

fitting/shock absorber PN D23286001 suffix is -311, record that this Service

Bulletin is accomplished, no more work is necessary.

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- If the WBS NLG (65 ̊) leg PN D23285001 suffix is -223 and the main

fitting/shock absorber PN D23286001 suffix is -215, record that this Service

Bulletin is accomplished, no more work is necessary.

- If the WBS NLG (65 ̊) leg PN D23285051 suffix is -223 and the main

fitting/shock absorber PN D23286001 suffix is -215, record that this Service

Bulletin is accomplished, no more work is necessary.

- If the WBS NLG (65 ̊) leg PN D23285101 suffix is -217 and the main

fitting/shock absorber PN D23286001 suffix is -211, record that this Service

Bulletin is accomplished, no more work is necessary.

- If the WBS NLG (65 ̊) leg PN D23285151 suffix is -217 and the main

fitting/shock absorber PN D23286001 suffix is -211, record that this Service

Bulletin is accomplished, no more work is necessary.

- If the NLG (65 ̊) leg PN D23285101 suffix is -26 or less and the main

fitting/shock absorber PN D23286100 suffix is -17 or less, do the worksteps

that follow.

- If the NLG (65 ̊) leg PN D23285151 suffix is -26 or less and the main

fitting/shock absorber PN D23286100 suffix is -17 or less, do the worksteps

that follow.

- If the Std NLG (65 ̊) leg PN D23285001 suffix is -32 or less and the main

fitting/shock absorber PN D23286001 suffix is -21 or less, do the worksteps

that follow.

- If the WBS NLG (65 ̊) leg PN D23285051 suffix is -32 or less and the main

fitting/shock absorber PN D23286001 suffix is -21 or less, do the worksteps

that follow.

- If the Std NLG (60 ̊) leg PN D23285101 suffix is -126 or less and the main

fitting/shock absorber PN D23286100 suffix is -117 or less, do the worksteps

that follow.

- If the WBS NLG (60 ̊) leg PN D23285151 suffix is -126 or less and the main

fitting/shock absorber PN D23286100 suffix is -117 or less, do the worksteps

that follow.

- If the Std NLG (60 ̊) leg PN D23285001 suffix is -132 or less and the main

fitting/shock absorber PN D23286001 suffix is -121 or less, do the worksteps

that follow.

- If the WBS NLG (60 ̊) leg PN D23285051 suffix is -132 or less and the main

fitting/shock absorber PN D23286001 suffix is -121 or less, do the worksteps

that follow.

- If the WBS NLG (60 ̊) leg PN D23285001 suffix is -322 or less and the main

fitting/shock absorber PN D23286001 suffix is -314 or less, do the worksteps

that follow.

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SERVICE BULLETIN

- If the WBS NLG (60 ̊) leg PN D23285051 suffix is -322 or less and the main

fitting/shock absorber PN D23286001 suffix is -314 or less, do the worksteps

that follow.

- If the WBS NLG (60 ̊) leg PN D23285101 suffix is -316 or less and the main

fitting/shock absorber PN D23286001 suffix is -310 or less, do the worksteps

that follow.

- If the WBS NLG (60 ̊) leg PN D23285151 suffix is -316 or less and the main

fitting/shock absorber PN D23286001 suffix is -310 or less, do the worksteps

that follow.

- If the WBS NLG (65 ̊) leg PN D23285001 suffix is -222 or less and the main

fitting/shock absorber PN D23286001 suffix is -214 or less, do the worksteps

that follow.

- If the WBS NLG (65 ̊) leg PN D23285051 suffix is -222 or less and the main

fitting/shock absorber PN D23286001 suffix is -214 or less, do the worksteps

that follow.

- If the WBS NLG (65 ̊) leg PN D23285101 suffix is -216 or less and the main

fitting/shock absorber PN D23286001 suffix is -210 or less, do the worksteps

that follow.

- If the WBS NLG (65 ̊) leg PN D23285151 suffix is -216 or less and the main

fitting/shock absorber PN D23286001 suffix is -210 or less, do the worksteps

that follow.

(d) Depressurize the Green hydraulic system (Refer to AMM 29-00-00-864-801).

(e) Depressurize the NWS accumulator (Refer to AMM Task 12-14-32-614-814).

(f) Lift the aircraft to a convenient height (Refer to AMM Task 07-11-00-581-801 or

AMM Task 07-11-00-581-802.

NOTE: Lifting the aircraft until a until a distance of 2.2 m (7.21 ft) exists

between the ground and the bottom of the NLG main fitting may be

necessary if further steps in this SB reveal corrosion on the slider.

**CONF 002

(1) Subtask 323241-941-401-002 - JOB SET-UP

Manpower Resources

Skills AIRFRAME

DATE: Nov 26/10 SERVICE BULLETIN No.: A330-32-3241

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SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) Task 07-11-00-581-801

Task 07-11-00-581-802

Task 12-14-32-614-814

Task 12-34-24-860-802

Task 29-00-00-864-801

Task 32-00-00-481-801

Task 32-00-00-481-802

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

12-34-24-860-802).

(b) Make sure that the safety devices are installed in the landing gear and landing gear

doors (Refer to AMM Task 32-00-00-481-801 and AMM Task 32-00-00-481-802).

(c) On the Std RNLG, do a check of the suffix number of the Part Number on the NLG

leg nameplate and the main fitting/shock absorber nameplate:

- If the RNLG (65 ̊) leg PN D23581100 suffix is -18 and the main fitting/shock

absorber PN D23582100 suffix is -11 or -112, record that this Service Bulletin

is accomplished, no more work is necessary.

- If the RNLG (65 ̊) leg PN D23581150 suffix is -18 and the main fitting/shock

absorber PN D23582100 suffix is -11 or -112, record that this Service Bulletin

is accomplished, no more work is necessary.

- If the RNLG (65 ̊) leg PN D23581300 suffix is -18 and the main fitting/shock

absorber PN D23582300 suffix is -11 or -112, record that this Service Bulletin

is accomplished, no more work is necessary.

- If the WBS RNLG (65 ̊) leg PN D23581350 suffix is -18 and the main

fitting/shock absorber PN D23582300 suffix is -11 or -112, record that this

Service Bulletin is accomplished, no more work is necessary.

- If the Std RNLG (60 ̊) leg PN D23581100 suffix is -118 and the main

fitting/shock absorber PN D23582100 suffix is -311 or -212, record that this

Service Bulletin is accomplished, no more work is necessary.

- If the WBS RNLG (60 ̊) leg PN D23581150 suffix is -118 and the main

fitting/shock absorber PN D23582100 suffix is -311 or -212, record that this

Service Bulletin is accomplished, no more work is necessary.

- If the Std RNLG (60 ̊) leg PN D23581300 suffix is -118 and the main

fitting/shock absorber PN D23582300 suffix is -311 or -212, record that this

Service Bulletin is accomplished, no more work is necessary.

- If the WBS RNLG (60 ̊) leg PN D23581350 suffix is -118 and the main

fitting/shock absorber PN D23582300 suffix is -311 or -212, record that this

Service Bulletin is accomplished, no more work is necessary.

- If the WBS RNLG (65 ̊) leg PN D23581200 suffix is -1 and the main

fitting/shock absorber PN D23582200 suffix is -1, record that this Service

Bulletin is accomplished, no more work is necessary.

DATE: Nov 26/10 SERVICE BULLETIN No.: A330-32-3241

REVISION No.: 01 - Oct 06/11 Page: 32

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@A330

SERVICE BULLETIN

- If the WBS RNLG (65 ̊) leg PN D23581200 suffix is -1 and the main

fitting/shock absorber PN D23582210 suffix is -1, record that this Service

Bulletin is accomplished, no more work is necessary.

- If the RNLG (65 ̊) leg PN D23581100 suffix is -17 or less and the main

fitting/shock absorber PN D23582100 suffix is -10 or less, or -111 or less do

the worksteps that follow.

- If the RNLG (65 ̊) leg PN D23581150 suffix is -17 or less and the main

fitting/shock absorber PN D23582100 suffix is -10 or less, or -111 or less do

the worksteps that follow.

- If the RNLG (65 ̊) leg PN D23581300 suffix is -17 or less and the main

fitting/shock absorber PN D23582300 suffix is -10 or less, or -111 or less do

the worksteps that follow.

- If the WBS RNLG (65 ̊) leg PN D23581350 suffix is -17 or less and the main

fitting/shock absorber PN D23582300 suffix is -10 or less, or -111 or less do

the worksteps that follow.

- If the Std RNLG (60 ̊) leg PN D23581100 suffix is -117 or less and the main

fitting/shock absorber PN D23582100 suffix is -310 or less, or -211 or less do

the worksteps that follow.

- If the WBS RNLG (60 ̊) leg PN D23581150 suffix is -117 or less and the main

fitting/shock absorber PN D23582100 suffix is -310 or less, or -211 or less do

the worksteps that follow.

- If the Std RNLG (60 ̊) leg PN D23581300 suffix is -117 or less and the main

fitting/shock absorber PN D23582300 suffix is -310 or less, or -211 or less do

the worksteps that follow.

- If the WBS RNLG (60 ̊) leg PN D23581350 suffix is -117 or less and the main

fitting/shock absorber PN D23582300 suffix is -310 or less, or -211 or less do

the worksteps that follow.

- If the WBS RNLG (65 ̊) leg PN D23581200 has no suffix and the main

fitting/shock absorber PN D23582200 has no suffix do the worksteps that

follow.

- If the WBS RNLG (65 ̊) leg PN D23581200 has no suffix and the main

fitting/shock absorber PN D23582210 has no suffix do the worksteps that

follow.

(d) Depressurize the Green hydraulic system (Refer to AMM 29-00-00-864-801).

(e) Depressurize the NWS accumulator (Refer to AMM Task 12-14-32-614-814).

(f) Lift the aircraft to a convenient height (Refer to AMM Task 07-11-00-581-801 or

AMM Task 07-11-00-581-802.

NOTE: Lifting the aircraft until a until a distance of 2.2 m (7.21 ft) exists

between the ground and the bottom of the NLG main fitting may be

DATE: Nov 26/10 SERVICE BULLETIN No.: A330-32-3241

REVISION No.: 01 - Oct 06/11 Page: 33

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@A330

SERVICE BULLETIN

necessary if further steps in this SB reveal corrosion on the slider.

**CONF 003

(1) Subtask 323241-941-401-001 - JOB SET-UP

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 07-11-00-581-801

Task 07-11-00-581-802

Task 12-14-32-614-814

Task 12-34-24-860-802

Task 29-00-00-864-801

Task 32-00-00-481-801

Task 32-00-00-481-802

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

12-34-24-860-802).

(b) Make sure that the safety devices are installed in the landing gear and landing gear

doors (Refer to AMM Task 32-00-00-481-801 and AMM Task 32-00-00-481-802).

(c) On the NLG, do a check of the suffix number of the Part Number on the NLG leg

nameplate and the main fitting/shock absorber nameplate:

- If the NLG (65 ̊) leg PN D23285101 suffix is -27 and the main fitting/shock

absorber PN D23286100 suffix is -18, record that this Service Bulletin is

accomplished, no more work is necessary.

- If the NLG (65 ̊) leg PN D23285151 suffix is -27 and the main fitting/shock

absorber PN D23286100 suffix is -18, record that this Service Bulletin is

accomplished, no more work is necessary.

- If the Std NLG (65 ̊) leg PN D23285001 suffix is -33 and the main fitting/shock

absorber PN D23286001 suffix is -22, record that this Service Bulletin is

accomplished, no more work is necessary.

- If the WBS NLG (65 ̊) leg PN D23285051 suffix is -33 and the main

fitting/shock absorber PN D23286001 suffix is -22, record that this Service

Bulletin is accomplished, no more work is necessary.

- If the Std NLG (60 ̊) leg PN D23285101 suffix is -127 and the main

fitting/shock absorber PN D23286100 suffix is -118, record that this Service

Bulletin is accomplished, no more work is necessary.

- If the WBS NLG (60 ̊) leg PN D23285151 suffix is -127 and the main

fitting/shock absorber PN D23286100 suffix is -118, record that this Service

Bulletin is accomplished, no more work is necessary.

DATE: Nov 26/10 SERVICE BULLETIN No.: A330-32-3241

REVISION No.: 01 - Oct 06/11 Page: 34

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@A330

SERVICE BULLETIN

- If the Std NLG (60 ̊) leg PN D23285001 suffix is -133 and the main

fitting/shock absorber PN D23286001 suffix is -122, record that this Service

Bulletin is accomplished, no more work is necessary.

- If the WBS NLG (60 ̊) leg PN D23285051 suffix is -133 and the main

fitting/shock absorber PN D23286001 suffix is -122, record that this Service

Bulletin is accomplished, no more work is necessary.

- If the WBS NLG (60 ̊) leg PN D23285001 suffix is -323 and the main

fitting/shock absorber PN D23286001 suffix is -315, record that this Service

Bulletin is accomplished, no more work is necessary.

- If the WBS NLG (60 ̊) leg PN D23285051 suffix is -323 and the main

fitting/shock absorber PN D23286001 suffix is -315, record that this Service

Bulletin is accomplished, no more work is necessary.

- If the WBS NLG (60 ̊) leg PN D23285101 suffix is -317 and the main

fitting/shock absorber PN D23286001 suffix is -311, record that this Service

Bulletin is accomplished, no more work is necessary.

- If the WBS NLG (60 ̊) leg PN D23285151 suffix is -317 and the main

fitting/shock absorber PN D23286001 suffix is -311, record that this Service

Bulletin is accomplished, no more work is necessary.

- If the WBS NLG (65 ̊) leg PN D23285001 suffix is -223 and the main

fitting/shock absorber PN D23286001 suffix is -215, record that this Service

Bulletin is accomplished, no more work is necessary.

- If the WBS NLG (65 ̊) leg PN D23285051 suffix is -223 and the main

fitting/shock absorber PN D23286001 suffix is -215, record that this Service

Bulletin is accomplished, no more work is necessary.

- If the WBS NLG (65 ̊) leg PN D23285101 suffix is -217 and the main

fitting/shock absorber PN D23286001 suffix is -211, record that this Service

Bulletin is accomplished, no more work is necessary.

- If the WBS NLG (65 ̊) leg PN D23285151 suffix is -217 and the main

fitting/shock absorber PN D23286001 suffix is -211, record that this Service

Bulletin is accomplished, no more work is necessary.

- If the NLG (65 ̊) leg PN D23285101 suffix is -26 or less and the main

fitting/shock absorber PN D23286100 suffix is -17 or less, do the worksteps

that follow.

- If the NLG (65 ̊) leg PN D23285151 suffix is -26 or less and the main

fitting/shock absorber PN D23286100 suffix is -17 or less, do the worksteps

that follow.

- If the Std NLG (65 ̊) leg PN D23285001 suffix is -32 or less and the main

fitting/shock absorber PN D23286001 suffix is -21 or less, do the worksteps

that follow.

DATE: Nov 26/10 SERVICE BULLETIN No.: A330-32-3241

REVISION No.: 01 - Oct 06/11 Page: 35

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@A330

SERVICE BULLETIN

- If the WBS NLG (65 ̊) leg PN D23285051 suffix is -32 or less and the main

fitting/shock absorber PN D23286001 suffix is -21 or less, do the worksteps

that follow.

- If the Std NLG (60 ̊) leg PN D23285101 suffix is -126 or less and the main

fitting/shock absorber PN D23286100 suffix is -117 or less, do the worksteps

that follow.

- If the WBS NLG (60 ̊) leg PN D23285151 suffix is -126 or less and the main

fitting/shock absorber PN D23286100 suffix is -117 or less, do the worksteps

that follow.

- If the Std NLG (60 ̊) leg PN D23285001 suffix is -132 or less and the main

fitting/shock absorber PN D23286001 suffix is -121 or less, do the worksteps

that follow.

- If the WBS NLG (60 ̊) leg PN D23285051 suffix is -132 or less and the main

fitting/shock absorber PN D23286001 suffix is -121 or less, do the worksteps

that follow.

- If the WBS NLG (60 ̊) leg PN D23285001 suffix is -322 or less and the main

fitting/shock absorber PN D23286001 suffix is -314 or less, do the worksteps

that follow.

- If the WBS NLG (60 ̊) leg PN D23285051 suffix is -322 or less and the main

fitting/shock absorber PN D23286001 suffix is -314 or less, do the worksteps

that follow.

- If the WBS NLG (60 ̊) leg PN D23285101 suffix is -316 or less and the main

fitting/shock absorber PN D23286001 suffix is -310 or less, do the worksteps

that follow.

- If the WBS NLG (60 ̊) leg PN D23285151 suffix is -316 or less and the main

fitting/shock absorber PN D23286001 suffix is -310 or less, do the worksteps

that follow.

- If the WBS NLG (65 ̊) leg PN D23285001 suffix is -222 or less and the main

fitting/shock absorber PN D23286001 suffix is -214 or less, do the worksteps

that follow.

- If the WBS NLG (65 ̊) leg PN D23285051 suffix is -222 or less and the main

fitting/shock absorber PN D23286001 suffix is -214 or less, do the worksteps

that follow.

- If the WBS NLG (65 ̊) leg PN D23285101 suffix is -216 or less and the main

fitting/shock absorber PN D23286001 suffix is -210 or less, do the worksteps

that follow.

- If the WBS NLG (65 ̊) leg PN D23285151 suffix is -216 or less and the main

fitting/shock absorber PN D23286001 suffix is -210 or less, do the worksteps

that follow.

(d) Depressurize the Green hydraulic system (Refer to AMM 29-00-00-864-801).

DATE: Nov 26/10 SERVICE BULLETIN No.: A330-32-3241

REVISION No.: 01 - Oct 06/11 Page: 36

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SERVICE BULLETIN

(e) Depressurize the NWS accumulator (Refer to AMM Task 12-14-32-614-814).

(f) Lift the aircraft to a convenient height (Refer to AMM Task 07-11-00-581-801 or

AMM Task 07-11-00-581-802.

NOTE: Lifting the aircraft until a until a distance of 2.2 m (7.21 ft) exists

between the ground and the bottom of the NLG main fitting may be

necessary if further steps in this SB reveal corrosion on the slider.

**CONF 004

(1) Subtask 323241-941-401-002 - JOB SET-UP

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 07-11-00-581-801

Task 07-11-00-581-802

Task 12-14-32-614-814

Task 12-34-24-860-802

Task 29-00-00-864-801

Task 32-00-00-481-801

Task 32-00-00-481-802

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

12-34-24-860-802).

(b) Make sure that the safety devices are installed in the landing gear and landing gear

doors (Refer to AMM Task 32-00-00-481-801 and AMM Task 32-00-00-481-802).

(c) On the Std RNLG, do a check of the suffix number of the Part Number on the NLG

leg nameplate and the main fitting/shock absorber nameplate:

- If the RNLG (65 ̊) leg PN D23581100 suffix is -18 and the main fitting/shock

absorber PN D23582100 suffix is -11 or -112, record that this Service Bulletin

is accomplished, no more work is necessary.

- If the RNLG (65 ̊) leg PN D23581150 suffix is -18 and the main fitting/shock

absorber PN D23582100 suffix is -11 or -112, record that this Service Bulletin

is accomplished, no more work is necessary.

- If the RNLG (65 ̊) leg PN D23581300 suffix is -18 and the main fitting/shock

absorber PN D23582300 suffix is -11 or -112, record that this Service Bulletin

is accomplished, no more work is necessary.

- If the WBS RNLG (65 ̊) leg PN D23581350 suffix is -18 and the main

fitting/shock absorber PN D23582300 suffix is -11 or -112, record that this

Service Bulletin is accomplished, no more work is necessary.

- If the Std RNLG (60 ̊) leg PN D23581100 suffix is -118 and the main

fitting/shock absorber PN D23582100 suffix is -311 or -212, record that this

Service Bulletin is accomplished, no more work is necessary.

DATE: Nov 26/10 SERVICE BULLETIN No.: A330-32-3241

REVISION No.: 01 - Oct 06/11 Page: 37

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SERVICE BULLETIN

- If the WBS RNLG (60 ̊) leg PN D23581150 suffix is -118 and the main

fitting/shock absorber PN D23582100 suffix is -311 or -212, record that this

Service Bulletin is accomplished, no more work is necessary.

- If the Std RNLG (60 ̊) leg PN D23581300 suffix is -118 and the main

fitting/shock absorber PN D23582300 suffix is -311 or -212, record that this

Service Bulletin is accomplished, no more work is necessary.

- If the WBS RNLG (60 ̊) leg PN D23581350 suffix is -118 and the main

fitting/shock absorber PN D23582300 suffix is -311 or -212, record that this

Service Bulletin is accomplished, no more work is necessary.

- If the WBS RNLG (65 ̊) leg PN D23581200 suffix is -1 and the main

fitting/shock absorber PN D23582200 suffix is -1, record that this Service

Bulletin is accomplished, no more work is necessary.

- If the WBS RNLG (65 ̊) leg PN D23581200 suffix is -1 and the main

fitting/shock absorber PN D23582210 suffix is -1, record that this Service

Bulletin is accomplished, no more work is necessary.

- If the RNLG (65 ̊) leg PN D23581100 suffix is -17 or less and the main

fitting/shock absorber PN D23582100 suffix is -10 or less, or -111 or less do

the worksteps that follow.

- If the RNLG (65 ̊) leg PN D23581150 suffix is -17 or less and the main

fitting/shock absorber PN D23582100 suffix is -10 or less, or -111 or less do

the worksteps that follow.

- If the RNLG (65 ̊) leg PN D23581300 suffix is -17 or less and the main

fitting/shock absorber PN D23582300 suffix is -10 or less, or -111 or less do

the worksteps that follow.

- If the WBS RNLG (65 ̊) leg PN D23581350 suffix is -17 or less and the main

fitting/shock absorber PN D23582300 suffix is -10 or less, or -111 or less do

the worksteps that follow.

- If the Std RNLG (60 ̊) leg PN D23581100 suffix is -117 or less and the main

fitting/shock absorber PN D23582100 suffix is -310 or less, or -211 or less do

the worksteps that follow.

- If the WBS RNLG (60 ̊) leg PN D23581150 suffix is -117 or less and the main

fitting/shock absorber PN D23582100 suffix is -310 or less, or -211 or less do

the worksteps that follow.

- If the Std RNLG (60 ̊) leg PN D23581300 suffix is -117 or less and the main

fitting/shock absorber PN D23582300 suffix is -310 or less, or -211 or less do

the worksteps that follow.

- If the WBS RNLG (60 ̊) leg PN D23581350 suffix is -117 or less and the main

fitting/shock absorber PN D23582300 suffix is -310 or less, or -211 or less do

the worksteps that follow.

DATE: Nov 26/10 SERVICE BULLETIN No.: A330-32-3241

REVISION No.: 01 - Oct 06/11 Page: 38

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SERVICE BULLETIN

- If the WBS RNLG (65 ̊) leg PN D23581200 has no suffix and the main

fitting/shock absorber PN D23582200 has no suffix do the worksteps that

follow.

- If the WBS RNLG (65 ̊) leg PN D23581200 has no suffix and the main

fitting/shock absorber PN D23582210 has no suffix do the worksteps that

follow.

(d) Depressurize the Green hydraulic system (Refer to AMM 29-00-00-864-801).

(e) Depressurize the NWS accumulator (Refer to AMM Task 12-14-32-614-814).

(f) Lift the aircraft to a convenient height (Refer to AMM Task 07-11-00-581-801 or

AMM Task 07-11-00-581-802.

NOTE: Lifting the aircraft until a until a distance of 2.2 m (7.21 ft) exists

between the ground and the bottom of the NLG main fitting may be

necessary if further steps in this SB reveal corrosion on the slider.

**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 323241-020-401-002 - REMOVE NLG/RNLG LEG COMPONENTS

Manpower Resources

Manhours 2.00

Minimum number of person 2

Subtask elapsed time 1.00

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 32-21-27-000-801

Task 32-51-27-000-802

Task 32-51-41-000-801

(a) Depressurize the NLG shock absorber. To do this, operate the charging valve at

the top of the shock absorber as follows:

1 Remove the blanking cap from the charging valve.

2 Slowly open the valve to release the nitrogen pressure from the shock

absorber.

(b) Remove the NWS gearboxes for access (Refer to AMM Task 32-51-41-000-801).

(c) Disconnect the torque links assembly (Refer to AMM Task 32-21-27-000-801).

(d) Disconnect the two steering-actuator rods from the bushed-sleeve, then remove

the lower attachment pins from the lower flange (Refer to AMM Task

32-51-27-000-802).

DATE: Nov 26/10 SERVICE BULLETIN No.: A330-32-3241

REVISION No.: 01 - Oct 06/11 Page: 39

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@A330

SERVICE BULLETIN

(e) Disconnect the Nose Wheel Steering (NWS) actuators, if necessary remove and

retain them (Refer to AMM Task 32-51-27-000-802).

(2) Subtask 323241-831-401-001 - MODIFY THE NLG/RNLG

References

Service Bulletin (SB) A330-32-3242

Vendor Service Bulletin (VSB) MESSIER-DOWTY D23581-32-064

MESSIER-DOWTY D23581-32-065

MESSIER-DOWTY D23581-32-066

(a) Refer to MESSIER-DOWTY Service Bulletin No. D23581-32-066 and MESSIERDOWTY Service Bulletin No. D23581-32-064 to inspect and modify the NLG/RNLG.

(b) If corrosion is found, it is recommended to accomplish A330-32-3242 (Refer to

MESSIER-DOWTY Service Bulletin No. D23581-32-065).

(3) Subtask 323241-420-401-001 - INSTALL THE NLG/RNLG LEG COMPONENTS

Manpower Resources

Manhours 2.00

Minimum number of person 2

Subtask elapsed time 1.00

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 12-12-32-611-805

Task 12-14-32-614-812

Task 29-00-00-863-801

Task 32-21-27-400-801

Task 32-51-00-440-801

Task 32-51-27-400-802

Task 32-51-41-400-801

(a) Install the Nose Wheel Steering (NWS) actuators (Refer to AMM Task

32-51-27-400-802).

(b) Install the NWS gearboxes (Refer to AMM Task 32-51-41-400-801).

(c) Install the lower attachment pins in the lower flange and connect the two steeringactuator rods to the bushed-sleeve (Refer to AMM Task 32-51-27-400-802).

(d) Connect the torque links assembly (Refer to AMM Task 32-21-27-400-801).

(e) Pressurize the NLG shock absorber (Refer to AMM Task 12-12-32-611-805).

(f) Reactivate the NWS (Refer to AMM Task 32-51-00-440-801).

(g) Pressurize the accumulator in the NWS hydraulic block (Refer to AMM Task

12-14-32-614-812).

(h) Pressurize the Green hydraulic system (Refer to AMM 29-00-00-863-801).

DATE: Nov 26/10 SERVICE BULLETIN No.: A330-32-3241

REVISION No.: 01 - Oct 06/11 Page: 40

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SERVICE BULLETIN

(4) Subtask 323241-930-401-001 - RE-IDENTIFY THE NLG LEG AND MAIN

FITTING/SHOCK ABSORBER

Material necessary to do the job

Reidentified part set REIDB01

ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE

NOTES

D23285001-133 Leg

D23285001-223 Leg

D23285001-323 Leg

D23285001-33 Leg

D23285051-133 Leg

D23285051-223 Leg

D23285051-323 Leg

D23285051-33 Leg

D23285101-127 Leg

D23285101-217 Leg

D23285101-27 Leg

D23285101-317 Leg

D23285151-127 Leg

D23285151-217 Leg

D23285151-27 Leg

D23285151-317 Leg

D23286001-122 Fitting

D23286001-215 Fitting

D23286001-22 Fitting

D23286001-315 Fitting

D23286100-118 Fitting

D23286100-18 Fitting

D23286100-211 Fitting

D23286100-311 Fitting

References

Vendor Service Bulletin (VSB) MESSIER-DOWTY D23581-32-064

(a) Refer to MESSIER-DOWTY Service Bulletin No. D23581-32-064 and re-identify

these NLG parts:

1 Leg Assy D23285101-27

1 Leg Assy D23285101-127

1 Leg Assy D23285151-27

DATE: Nov 26/10 SERVICE BULLETIN No.: A330-32-3241

REVISION No.: 01 - Oct 06/11 Page: 41

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SERVICE BULLETIN

1 Leg Assy D23285151-127

1 Leg Assy D23285001-33

1 Leg Assy D23285001-133

1 Leg Assy D23285051-33

1 Leg Assy D23285051-133

1 Leg Assy D23285001-323

1 Leg Assy D23285051-323

1 Leg Assy D23285001-223

1 Leg-Assy D23285051-223

1 Leg Assy D23285101-317

1 Leg Assy D23285151-317

1 Leg Assy D23285101-217

1 Leg Assy D23285151-217

(b) Refer to MESSIER-DOWTY Service Bulletin No. D23581-32-064 and re-identify

these Main Fitting Shock Absorbers:

1 Main Fitting Shock

Absorber

D23286100-18

1 Main Fitting Shock

Absorber

D23286100-118

1 Main Fitting Shock

Absorber

D23286001-22

1 Main Fitting Shock

Absorber

D23286001-122

1 Main Fitting Shock

Absorber

D23286001-315

1 Main Fitting Shock

Absorber

D23286001-215

1 Main Fitting Shock

Absorber

D23286100-311

DATE: Nov 26/10 SERVICE BULLETIN No.: A330-32-3241

REVISION No.: 01 - Oct 06/11 Page: 42

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SERVICE BULLETIN

1 Main Fitting Shock

Absorber

D23286100-211

**CONF 002

(1) Subtask 323241-020-401-002 - REMOVE NLG/RNLG LEG COMPONENTS

Manpower Resources

Manhours 2.00

Minimum number of person 2

Subtask elapsed time 1.00

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 32-21-27-000-801

Task 32-51-27-000-802

Task 32-51-41-000-801

(a) Depressurize the NLG shock absorber. To do this, operate the charging valve at

the top of the shock absorber as follows:

1 Remove the blanking cap from the charging valve.

2 Slowly open the valve to release the nitrogen pressure from the shock

absorber.

(b) Remove the NWS gearboxes for access (Refer to AMM Task 32-51-41-000-801).

(c) Disconnect the torque links assembly (Refer to AMM Task 32-21-27-000-801).

(d) Disconnect the two steering-actuator rods from the bushed-sleeve, then remove

the lower attachment pins from the lower flange (Refer to AMM Task

32-51-27-000-802).

(e) Disconnect the Nose Wheel Steering (NWS) actuators, if necessary remove and

retain them (Refer to AMM Task 32-51-27-000-802).

(2) Subtask 323241-831-401-001 - MODIFY THE NLG/RNLG

References

Service Bulletin (SB) A330-32-3242

Vendor Service Bulletin (VSB) MESSIER-DOWTY D23581-32-064

MESSIER-DOWTY D23581-32-065

MESSIER-DOWTY D23581-32-066

(a) Refer to MESSIER-DOWTY Service Bulletin No. D23581-32-066 and MESSIERDOWTY Service Bulletin No. D23581-32-064 to inspect and modify the NLG/RNLG.

(b) If corrosion is found, it is recommended to accomplish A330-32-3242 (Refer to

MESSIER-DOWTY Service Bulletin No. D23581-32-065).

DATE: Nov 26/10 SERVICE BULLETIN No.: A330-32-3241

REVISION No.: 01 - Oct 06/11 Page: 43

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@A330

SERVICE BULLETIN

(3) Subtask 323241-420-401-001 - INSTALL THE NLG/RNLG LEG COMPONENTS

Manpower Resources

Manhours 2.00

Minimum number of person 2

Subtask elapsed time 1.00

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 12-12-32-611-805

Task 12-14-32-614-812

Task 29-00-00-863-801

Task 32-21-27-400-801

Task 32-51-00-440-801

Task 32-51-27-400-802

Task 32-51-41-400-801

(a) Install the Nose Wheel Steering (NWS) actuators (Refer to AMM Task

32-51-27-400-802).

(b) Install the NWS gearboxes (Refer to AMM Task 32-51-41-400-801).

(c) Install the lower attachment pins in the lower flange and connect the two steeringactuator rods to the bushed-sleeve (Refer to AMM Task 32-51-27-400-802).

(d) Connect the torque links assembly (Refer to AMM Task 32-21-27-400-801).

(e) Pressurize the NLG shock absorber (Refer to AMM Task 12-12-32-611-805).

(f) Reactivate the NWS (Refer to AMM Task 32-51-00-440-801).

(g) Pressurize the accumulator in the NWS hydraulic block (Refer to AMM Task

12-14-32-614-812).

(h) Pressurize the Green hydraulic system (Refer to AMM 29-00-00-863-801).

(4) Subtask 323241-930-401-002 - RE-IDENTIFY THE RNLG LEG AND MAIN

FITTING/SHOCK ABSORBER

Material necessary to do the job

Reidentified part set REIDB02

ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE

NOTES

D23581100-118 Leg

D23581100-18 Leg

D23581150-118 Leg

D23581150-18 Leg

D23581200-1 Leg

D23581300-118 Leg

DATE: Nov 26/10 SERVICE BULLETIN No.: A330-32-3241

REVISION No.: 01 - Oct 06/11 Page: 44

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SERVICE BULLETIN

ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE

NOTES

D23581300-18 Leg

D23581350-118 Leg

D23581350-18 Leg

D23582100-11 Fitting

D23582100-112 Fitting

D23582100-212 Fitting

D23582100-311 Fitting

D23582200-1 Fitting

D23582210-1 Fitting

D23582300-11 Fitting

D23582300-112 Fitting

D23582300-212 Fitting

D23582300-311 Fitting

References

Vendor Service Bulletin (VSB) MESSIER-DOWTY D23581-32-064

(a) Refer to MESSIER-DOWTY Service Bulletin No. D23581-32-064 and re-identify

these RNLG parts:

1 Leg Assy D23581200-1

1 Leg Assy D23581100-18

1 Leg Assy D23581100-118

1 Leg Assy D23581150-18

1 Leg Assy D23581150-118

1 Leg Assy D23581300-18

1 Leg Assy D23581300-118

1 Leg Assy D23581350-18

1 Leg Assy D23581350-118

(b) Refer to MESSIER-DOWTY Service Bulletin No. D23581-32-064 and re-identify

these Main Fitting Shock Absorbers:

1 Main Fitting Shock

Absorber

D23582200-1

DATE: Nov 26/10 SERVICE BULLETIN No.: A330-32-3241

REVISION No.: 01 - Oct 06/11 Page: 45

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@A330

SERVICE BULLETIN

1 Main Fitting Shock

Absorber

D23582210-1

1 Main Fitting Shock

Absorber

D23582100-11

1 Main Fitting Shock

Absorber

D23582100-112

1 Main Fitting Shock

Absorber

D23582100-311

1 Main Fitting Shock

Absorber

D23582100-212

1 Main Fitting Shock

Absorber

D23582300-11

1 Main Fitting Shock

Absorber

D23582300-112

1 Main Fitting Shock

Absorber

D23582300-311

1 Main Fitting Shock

Absorber

D23582300-212

**CONF 003

(1) Subtask 323241-020-401-003 - REMOVE NLG/RNLG LEG COMPONENTS

Manpower Resources

Manhours 2.00

Minimum number of person 2

Subtask elapsed time 1.00

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 32-21-27-000-801

Task 32-51-27-000-802

Task 32-51-41-000-801

Task 32-53-12-000-801

(a) Depressurize the NLG shock absorber. To do this, operate the charging valve at

the top of the shock absorber as follows:

1 Remove the blanking cap from the charging valve.

2 Slowly open the valve to release the nitrogen pressure from the shock

absorber.

(b) Remove the NWS gearboxes for access (Refer to AMM Task 32-51-41-000-801).

DATE: Nov 26/10 SERVICE BULLETIN No.: A330-32-3241

REVISION No.: 01 - Oct 06/11 Page: 46

7

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@A330

SERVICE BULLETIN

(c) Disconnect the torque links assembly (Refer to AMM Task 32-21-27-000-801).

(d) Disconnect the two steering-actuator rods from the bushed-sleeve, then remove

the lower attachment pins from the lower flange (Refer to AMM Task

32-51-27-000-802).

(e) Disconnect the Nose Wheel Steering (NWS) actuators, if necessary remove and

retain them (Refer to AMM Task 32-51-27-000-802).

(f) Remove the Electrical Box - Oversteer Warning NLG for access (Refer to AMM

Task 32-53-12-000-801).

(2) Subtask 323241-831-401-001 - MODIFY THE NLG/RNLG

References

Service Bulletin (SB) A330-32-3242

Vendor Service Bulletin (VSB) MESSIER-DOWTY D23581-32-064

MESSIER-DOWTY D23581-32-065

MESSIER-DOWTY D23581-32-066

(a) Refer to MESSIER-DOWTY Service Bulletin No. D23581-32-066 and MESSIERDOWTY Service Bulletin No. D23581-32-064 to inspect and modify the NLG/RNLG.

(b) If corrosion is found, it is recommended to accomplish A330-32-3242 (Refer to

MESSIER-DOWTY Service Bulletin No. D23581-32-065).

(3) Subtask 323241-420-401-002 - INSTALL THE NLG/RNLG LEG COMPONENTS

Manpower Resources

Manhours 2.00

Minimum number of person 2

Subtask elapsed time 1.00

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 12-12-32-611-805

Task 12-14-32-614-812

Task 29-00-00-863-801

Task 32-21-27-400-801

Task 32-51-00-440-801

Task 32-51-27-400-802

Task 32-51-41-400-801

Task 32-53-12-400-801

(a) Install the Nose Wheel Steering (NWS) actuators (Refer to AMM Task

32-51-27-400-802).

(b) Install the NWS gearboxes (Refer to AMM Task 32-51-41-400-801).

(c) Install the Electrical Box - Oversteer Warning NLG (Refer to AMM Task

32-53-12-400-801).

DATE: Nov 26/10 SERVICE BULLETIN No.: A330-32-3241

REVISION No.: 01 - Oct 06/11 Page: 47

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@A330

SERVICE BULLETIN

(d) Install the lower attachment pins in the lower flange and connect the two steeringactuator rods to the bushed-sleeve (Refer to AMM Task 32-51-27-400-802).

(e) Connect the torque links assembly (Refer to AMM Task 32-21-27-400-801).

(f) Pressurize the NLG shock absorber (Refer to AMM Task 12-12-32-611-805).

(g) Reactivate the NWS (Refer to AMM Task 32-51-00-440-801).

(h) Pressurize the accumulator in the NWS hydraulic block (Refer to AMM Task

12-14-32-614-812).

(i) Pressurize the Green hydraulic system (Refer to AMM 29-00-00-863-801).

(4) Subtask 323241-930-401-001 - RE-IDENTIFY THE NLG LEG AND MAIN

FITTING/SHOCK ABSORBER

Material necessary to do the job

Reidentified part set REIDB01

ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE

NOTES

D23285001-133 Leg

D23285001-223 Leg

D23285001-323 Leg

D23285001-33 Leg

D23285051-133 Leg

D23285051-223 Leg

D23285051-323 Leg

D23285051-33 Leg

D23285101-127 Leg

D23285101-217 Leg

D23285101-27 Leg

D23285101-317 Leg

D23285151-127 Leg

D23285151-217 Leg

D23285151-27 Leg

D23285151-317 Leg

D23286001-122 Fitting

D23286001-215 Fitting

D23286001-22 Fitting

D23286001-315 Fitting

D23286100-118 Fitting

D23286100-18 Fitting

D23286100-211 Fitting

D23286100-311 Fitting

DATE: Nov 26/10 SERVICE BULLETIN No.: A330-32-3241

REVISION No.: 01 - Oct 06/11 Page: 48

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@A330

SERVICE BULLETIN

References

Vendor Service Bulletin (VSB) MESSIER-DOWTY D23581-32-064

(a) Refer to MESSIER-DOWTY Service Bulletin No. D23581-32-064 and re-identify

these NLG parts:

1 Leg Assy D23285101-27

1 Leg Assy D23285101-127

1 Leg Assy D23285151-27

1 Leg Assy D23285151-127

1 Leg Assy D23285001-33

1 Leg Assy D23285001-133

1 Leg Assy D23285051-33

1 Leg Assy D23285051-133

1 Leg Assy D23285001-323

1 Leg Assy D23285051-323

1 Leg Assy D23285001-223

1 Leg-Assy D23285051-223

1 Leg Assy D23285101-317

1 Leg Assy D23285151-317

1 Leg Assy D23285101-217

1 Leg Assy D23285151-217

(b) Refer to MESSIER-DOWTY Service Bulletin No. D23581-32-064 and re-identify

these Main Fitting Shock Absorbers:

1 Main Fitting Shock

Absorber

D23286100-18

1 Main Fitting Shock

Absorber

D23286100-118

1 Main Fitting Shock

Absorber

D23286001-22

DATE: Nov 26/10 SERVICE BULLETIN No.: A330-32-3241

REVISION No.: 01 - Oct 06/11 Page: 49

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@A330

SERVICE BULLETIN

1 Main Fitting Shock

Absorber

D23286001-122

1 Main Fitting Shock

Absorber

D23286001-315

1 Main Fitting Shock

Absorber

D23286001-215

1 Main Fitting Shock

Absorber

D23286100-311

1 Main Fitting Shock

Absorber

D23286100-211

**CONF 004

(1) Subtask 323241-020-401-003 - REMOVE NLG/RNLG LEG COMPONENTS

Manpower Resources

Manhours 2.00

Minimum number of person 2

Subtask elapsed time 1.00

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 32-21-27-000-801

Task 32-51-27-000-802

Task 32-51-41-000-801

Task 32-53-12-000-801

(a) Depressurize the NLG shock absorber. To do this, operate the charging valve at

the top of the shock absorber as follows:

1 Remove the blanking cap from the charging valve.

2 Slowly open the valve to release the nitrogen pressure from the shock

absorber.

(b) Remove the NWS gearboxes for access (Refer to AMM Task 32-51-41-000-801).

(c) Disconnect the torque links assembly (Refer to AMM Task 32-21-27-000-801).

(d) Disconnect the two steering-actuator rods from the bushed-sleeve, then remove

the lower attachment pins from the lower flange (Refer to AMM Task

32-51-27-000-802).

(e) Disconnect the Nose Wheel Steering (NWS) actuators, if necessary remove and

retain them (Refer to AMM Task 32-51-27-000-802).

(f) Remove the Electrical Box - Oversteer Warning NLG for access (Refer to AMM

Task 32-53-12-000-801).

DATE: Nov 26/10 SERVICE BULLETIN No.: A330-32-3241

REVISION No.: 01 - Oct 06/11 Page: 50

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@A330

SERVICE BULLETIN

(2) Subtask 323241-831-401-001 - MODIFY THE NLG/RNLG

References

Service Bulletin (SB) A330-32-3242

Vendor Service Bulletin (VSB) MESSIER-DOWTY D23581-32-064

MESSIER-DOWTY D23581-32-065

MESSIER-DOWTY D23581-32-066

(a) Refer to MESSIER-DOWTY Service Bulletin No. D23581-32-066 and MESSIERDOWTY Service Bulletin No. D23581-32-064 to inspect and modify the NLG/RNLG.

(b) If corrosion is found, it is recommended to accomplish A330-32-3242 (Refer to

MESSIER-DOWTY Service Bulletin No. D23581-32-065).

(3) Subtask 323241-420-401-002 - INSTALL THE NLG/RNLG LEG COMPONENTS

Manpower Resources

Manhours 2.00

Minimum number of person 2

Subtask elapsed time 1.00

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 12-12-32-611-805

Task 12-14-32-614-812

Task 29-00-00-863-801

Task 32-21-27-400-801

Task 32-51-00-440-801

Task 32-51-27-400-802

Task 32-51-41-400-801

Task 32-53-12-400-801

(a) Install the Nose Wheel Steering (NWS) actuators (Refer to AMM Task

32-51-27-400-802).

(b) Install the NWS gearboxes (Refer to AMM Task 32-51-41-400-801).

(c) Install the Electrical Box - Oversteer Warning NLG (Refer to AMM Task

32-53-12-400-801).

(d) Install the lower attachment pins in the lower flange and connect the two steeringactuator rods to the bushed-sleeve (Refer to AMM Task 32-51-27-400-802).

(e) Connect the torque links assembly (Refer to AMM Task 32-21-27-400-801).

(f) Pressurize the NLG shock absorber (Refer to AMM Task 12-12-32-611-805).

(g) Reactivate the NWS (Refer to AMM Task 32-51-00-440-801).

(h) Pressurize the accumulator in the NWS hydraulic block (Refer to AMM Task

12-14-32-614-812).

DATE: Nov 26/10 SERVICE BULLETIN No.: A330-32-3241

REVISION No.: 01 - Oct 06/11 Page: 51

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SERVICE BULLETIN

(i) Pressurize the Green hydraulic system (Refer to AMM 29-00-00-863-801).

(4) Subtask 323241-930-401-002 - RE-IDENTIFY THE RNLG LEG AND MAIN

FITTING/SHOCK ABSORBER

Material necessary to do the job

Reidentified part set REIDB02

ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE

NOTES

D23581100-118 Leg

D23581100-18 Leg

D23581150-118 Leg

D23581150-18 Leg

D23581200-1 Leg

D23581300-118 Leg

D23581300-18 Leg

D23581350-118 Leg

D23581350-18 Leg

D23582100-11 Fitting

D23582100-112 Fitting

D23582100-212 Fitting

D23582100-311 Fitting

D23582200-1 Fitting

D23582210-1 Fitting

D23582300-11 Fitting

D23582300-112 Fitting

D23582300-212 Fitting

D23582300-311 Fitting

References

Vendor Service Bulletin (VSB) MESSIER-DOWTY D23581-32-064

(a) Refer to MESSIER-DOWTY Service Bulletin No. D23581-32-064 and re-identify

these RNLG parts:

1 Leg Assy D23581200-1

1 Leg Assy D23581100-18

1 Leg Assy D23581100-118

1 Leg Assy D23581150-18

1 Leg Assy D23581150-118

DATE: Nov 26/10 SERVICE BULLETIN No.: A330-32-3241

REVISION No.: 01 - Oct 06/11 Page: 52

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@A330

SERVICE BULLETIN

1 Leg Assy D23581300-18

1 Leg Assy D23581300-118

1 Leg Assy D23581350-18

1 Leg Assy D23581350-118

(b) Refer to MESSIER-DOWTY Service Bulletin No. D23581-32-064 and re-identify

these Main Fitting Shock Absorbers:

1 Main Fitting Shock

Absorber

D23582200-1

1 Main Fitting Shock

Absorber

D23582210-1

1 Main Fitting Shock

Absorber

D23582100-11

1 Main Fitting Shock

Absorber

D23582100-112

1 Main Fitting Shock

Absorber

D23582100-311

1 Main Fitting Shock

Absorber

D23582100-212

1 Main Fitting Shock

Absorber

D23582300-11

1 Main Fitting Shock

Absorber

D23582300-112

1 Main Fitting Shock

Absorber

D23582300-311

1 Main Fitting Shock

Absorber

D23582300-212

**CONF ALL

D. TEST

**CONF 001

(1) Subtask 323241-710-401-001 - TESTING

Manpower Resources

Skills AIRFRAME

DATE: Nov 26/10 SERVICE BULLETIN No.: A330-32-3241

REVISION No.: 01 - Oct 06/11 Page: 53

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SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) Task 32-31-00-740-801

Task 32-49-00-740-801

Task 32-51-00-720-801

Task 32-51-00-740-801

(a) Do the Functional test of the NWS (Refer to AMM Task 32-51-00-720-801).

(b) Do the BITE test of the NWS (Refer to AMM Task 32-51-00-740-801).

(c) Do the BITE test of the NLG Normal Retraction and Extension (Refer to AMM Task

32-31-00-740-801).

(d) For aircraft fitted with a TPIS system, do the BITE test of the TPIS (Refer to AMM

Task 32-49-00-740-801).

**CONF 002

(1) Subtask 323241-710-401-001 - TESTING

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 32-31-00-740-801

Task 32-49-00-740-801

Task 32-51-00-720-801

Task 32-51-00-740-801

(a) Do the Functional test of the NWS (Refer to AMM Task 32-51-00-720-801).

(b) Do the BITE test of the NWS (Refer to AMM Task 32-51-00-740-801).

(c) Do the BITE test of the NLG Normal Retraction and Extension (Refer to AMM Task

32-31-00-740-801).

(d) For aircraft fitted with a TPIS system, do the BITE test of the TPIS (Refer to AMM

Task 32-49-00-740-801).

**CONF 003

(1) Subtask 323241-710-401-002 - TESTING

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 32-31-00-740-801

Task 32-49-00-740-801

Task 32-51-00-720-801

Task 32-51-00-740-801

Task 32-53-00-720-801

DATE: Nov 26/10 SERVICE BULLETIN No.: A330-32-3241

REVISION No.: 01 - Oct 06/11 Page: 54

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SERVICE BULLETIN

(a) Do the Functional test of the NWS (Refer to AMM Task 32-51-00-720-801).

(b) Do the BITE test of the NWS (Refer to AMM Task 32-51-00-740-801).

(c) Do the BITE test of the NLG Normal Retraction and Extension (Refer to AMM Task

32-31-00-740-801).

(d) For aircraft fitted with a TPIS system, do the BITE test of the TPIS (Refer to AMM

Task 32-49-00-740-801).

(e) Do the Operational test of the Steering Angle Protection System (Refer to AMM

Task 32-53-00-720-801).

**CONF 004

(1) Subtask 323241-710-401-002 - TESTING

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 32-31-00-740-801

Task 32-49-00-740-801

Task 32-51-00-720-801

Task 32-51-00-740-801

Task 32-53-00-720-801

(a) Do the Functional test of the NWS (Refer to AMM Task 32-51-00-720-801).

(b) Do the BITE test of the NWS (Refer to AMM Task 32-51-00-740-801).

(c) Do the BITE test of the NLG Normal Retraction and Extension (Refer to AMM Task

32-31-00-740-801).

(d) For aircraft fitted with a TPIS system, do the BITE test of the TPIS (Refer to AMM

Task 32-49-00-740-801).

(e) Do the Operational test of the Steering Angle Protection System (Refer to AMM

Task 32-53-00-720-801).

**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 323241-942-401-001 - CLOSE-UP

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 07-11-00-586-802

DATE: Nov 26/10 SERVICE BULLETIN No.: A330-32-3241

REVISION No.: 01 - Oct 06/11 Page: 55

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SERVICE BULLETIN

(a) Lower the aircraft on to the ground (Refer to AMM 07-11-00-586-802).

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

equipment.

**CONF 002

(1) Subtask 323241-942-401-001 - CLOSE-UP

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 07-11-00-586-802

(a) Lower the aircraft on to the ground (Refer to AMM 07-11-00-586-802).

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

equipment.

**CONF 003

(1) Subtask 323241-942-401-001 - CLOSE-UP

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 07-11-00-586-802

(a) Lower the aircraft on to the ground (Refer to AMM 07-11-00-586-802).

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

equipment.

**CONF 004

(1) Subtask 323241-942-401-001 - CLOSE-UP

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 07-11-00-586-802

(a) Lower the aircraft on to the ground (Refer to AMM 07-11-00-586-802).

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

equipment.

DATE: Nov 26/10 SERVICE BULLETIN No.: A330-32-3241

REVISION No.: 01 - Oct 06/11 Page: 56

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@A330

SERVICE BULLETIN

APPENDIX 01 : ELAPSED TIME ASSUMPTION

**CONF ALL

For detail concerning the additional work elapsed time assumptions, refer to the Gantt chart shown

below:

DATE: Nov 26/10 SERVICE BULLETIN No.: A330-32-3241

REVISION No.: 01 - Oct 06/11 Page: 1

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@A330

SERVICE BULLETIN

APPENDIX 01 : ELAPSED TIME ASSUMPTION

**CONF ALL

ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A330−32−3241

GET ACCESS

MH ET/S

TOTAL MANHOURS

SB ELAPSED TIME

12.00

6.00

STEPS

2.00 1.00

0 10

REMOVE NLG LEG 2.00 1.00

INSTALL NLG LEG 2.00 1.00

TEST 4.00 2.00

CLOSE−UP 2.00 1.00

MH

ET/S:

PER

MANHOURS

ELAPSED TIME PER STEP

NUMBER OF PERSONS

01

02

THIS CHART IS ONLY A PROPOSAL.

OPERATORS MAY DETERMINE THAT ANOTHER WAY

TO DO THE WORK IS MORE SUITABLE FOR THEM.

01

02

NOTES:

PER

2

2

2

2

2

:

:

SB ELAPSED TIME

(HOURS)

2 4 6 8 12

IF A VSB IS INVOLVED, THE ASSOCIATED MANHOURS

ARE NOT REFLECTED IN THIS GANTT CHART.

COMPONENTS

COMPONENTS

G_SB_323241_7_AAAA_01_00

Figure A-UAAAA - Sheet 01

Elapsed Time assumption

DATE: Nov 26/10 SERVICE BULLETIN No.: A330-32-3241

REVISION No.: 01 - Oct 06/11 Page: 2

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@A330

SERVICE BULLETIN

REPORTING SHEET

TITLE: LANDING GEAR - NOSE GEAR - ADDITION OF PRIMER PAINT TO THE

CADMIUM AROUND THE DOWEL BUSH HOLES ON THE MAIN FITTING

MODIFICATION No.: 200616H16400

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: Nov 26/10 SERVICE BULLETIN No.: A330-32-3241

REVISION No.: 01 - Oct 06/11 Page: 1

7

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: Nov 26/10 SERVICE BULLETIN No.: A330-32-3241

REVISION No.: 01 - Oct 06/11 Page: 1

7

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