@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 - MLG - REPEAT INSPECTION OF MLG BOGIE PIVOT

PIN

MODIFICATION No.: None

This page transmits Revision No.02 of Service Bulletin No.A330-32-3240

ADDITIONAL WORK

**CONF ALL

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

REASON

Revision No. 02 issued to change the ISB to introduce repetitive inspections and to improve the

Accomplishment Instructions. The opportunity is taken to update the effectivity. Config. 002 added.

CHANGES

FRONT MATTER

LANDING GEAR - MLG - REPEAT

INSPECTION OF MLG BOGIE PIVOT PIN

SB TITLE UPDATED

CONFIGURATION UPDATED

R

SUMMARY

EFFECTIVITY OPERATOR LIST UPDATED R

MANPOWER MANPOWER UPDATED

CONFIGURATION UPDATED

R

MANPOWER ADDED N

APPENDICES APPENDICES UPDATED R

PLANNING INFORMATION

EFFECTIVITY EFFECTIVITY RELATED INFORMATION

UPDATED

R

Configuration definition CONFIGURATION LIST UPDATED R

CONF 001 CONFIGURATION DEFINITION UPDATED

CONFIGURATION DESCRIPTION UPDATED

R

CONF 002 CONFIGURATION ADDED N

Material Effectivity MATERIAL EFFECTIVITY UPDATED R

DESCRIPTION DESCRIPTION UPDATED R

DATE: Dec 08/10 SERVICE BULLETIN No.: A330-32-3240

REVISION No.: 02 - Dec 02/11 Page: 1

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@A330

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

COMPLIANCE

Accomplishment Timescale ACCOMPLISHMENT TIMESCALE UPDATED R

MANPOWER MANPOWER UPDATED

CONFIGURATION UPDATED

R

MANPOWER ADDED N

REFERENCES REFERENCED DOCUMENTATION UPDATED

CONFIGURATION UPDATED

R

REFERENCED DOCUMENTATION ADDED N

MATERIAL INFORMATION

MATERIAL - PRICE AND AVAILABILITY

Price and Availability PRICE AND AVAILABILITY UPDATED R

INDUSTRY SUPPORT INFORMATION INDUSTRY SUPPORT INFORMATION UPDATED R

TOOLING

Tools TOOLS UPDATED R

ACCOMPLISHMENT INSTRUCTIONS

TASK 323240- 832-895-001-INSPECTION TASK SOLUTION UPDATED

CAUTION UPDATED

CONFIGURATION UPDATED

R

Task associated data - 001 CONFIGURATION UPDATED R

Task associated data - 002 TASK ASSOCIATED DATA ADDED N

Subtask 323240-910-401-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

R

Subtask 323240-839-401-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

R

Subtask 323240-910-401-001 SUBTASK SOLUTION ADDED N

Subtask 323240-839-401-001 SUBTASK SOLUTION ADDED N

Subtask 323240-941-401-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

R

Subtask 323240-941-401-001 SUBTASK SOLUTION ADDED N

Subtask 323240-020-401-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

REFERENCED DOCUMENTATION UPDATED

FIGURE REFERENCE UPDATED

NOTE UPDATED

QUANTITY UPDATED

WARNING UPDATED

ITEM NUMBER UPDATED

PART NUMBER UPDATED

PART NUMBER DESCRIPTION UPDATED

REFERENCES UPDATED

R

Subtask 323240-210-401-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

R

Subtask 323240-833-401-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

R

DATE: Dec 08/10 SERVICE BULLETIN No.: A330-32-3240

REVISION No.: 02 - Dec 02/11 Page: 2

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@A330

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Subtask 323240-420-401-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

REFERENCED DOCUMENTATION UPDATED

ITEM NUMBER UPDATED

QUANTITY UPDATED

PART NUMBER UPDATED

PART NUMBER DESCRIPTION UPDATED

REFERENCES UPDATED

NOTE UPDATED

R

Subtask 323240-020-401-003 SUBTASK SOLUTION ADDED N

Subtask 323240-210-401-001 SUBTASK SOLUTION ADDED N

Subtask 323240-833-401-001 SUBTASK SOLUTION ADDED N

Subtask 323240-420-401-003 SUBTASK SOLUTION ADDED N

Subtask 323240-710-401-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

REFERENCED DOCUMENTATION UPDATED

WARNING UPDATED

NOTE UPDATED

REFERENCES UPDATED

R

Subtask 323240-710-401-001 SUBTASK SOLUTION ADDED N

Subtask 323240-942-401-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

REFERENCES UPDATED

REFERENCED DOCUMENTATION UPDATED

R

Subtask 323240-942-401-001 SUBTASK SOLUTION ADDED N

Fig. A-UBAAA

Fig. A-UBAAA Sheet 01 SHEET UPDATED R

Fig. A-UCAAA FIGURE SOLUTION ADDED N

Fig. A-UCAAA Sheet 01 SHEET ADDED N

APPENDIX 01 - Inspection Reports

Fig. A-UBBAA FIGURE SOLUTION UPDATED R

Fig. A-UBBAA Sheet 01 SHEET UPDATED R

APPENDIX 02 - 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

Revision No. 01 issued to remove Config 002 and to amend the Inspection Flow Chart and the

Inspection Reporting Sheet.

DATE: Dec 08/10 SERVICE BULLETIN No.: A330-32-3240

REVISION No.: 02 - Dec 02/11 Page: 3

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@A330

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

REVISION SEQUENCE

ORIGINAL: Dec 08/10

REVISION No. : 01 - May 04/11

REVISION No. : 02 - Dec 02/11

DATE: Dec 08/10 SERVICE BULLETIN No.: A330-32-3240

REVISION No.: 02 - Dec 02/11 Page: 4

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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 - MLG - REPEAT INSPECTION OF MLG BOGIE PIVOT

PIN

**CONF ALL

MODIFICATIONS

None

REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES

The bogie pivot pin makes the connection between the landing gear slider and the bogie beam. This

component is a Principal Structural Element (PSE).

In-service feed-backs indicate an increasing number of bogie pivot pin replacements due to unexpected

findings upon removal. Operators report a high number of events related to chrome detachment or

chrome dragging. There have been a number of confirmed crackings of the bogie pivot pins since Entry

Into Service (EIS).

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

Service Bulletin No. A33/34-32-285.

VSB A33/34-32-285 details:

- a Detailed Visual Inspection (DVI) of the bogie pivot pin chromium-plated surface

- a Magnetic Particle Inspection (MPI) of the bogie pivot pin if damage is found to the chromiumplated surface

- a DVI of the pivot pin bushes in the bogie beam and sliding tube.

This inspection will:

- make sure that all damaged bogie pivot pins are repaired or replaced if found damaged

- gather detailed information from the fleet to further investigate this issue and prepare a long term

fix.

DATE: Dec 08/10 SERVICE BULLETIN No.: A330-32-3240

REVISION No.: 02 - Dec 02/11 Page: 1

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@A330

SERVICE BULLETIN

SUMMARY

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 NORMAL JACKING YES

NOTE (1): Service Bulletin must be accomplished.

MATERIAL PRICE INFORMATION

No Material

EFFECTIVITY

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

46W 78V 97X AAR AAW ACA ACI AEA AFL AFR AGC 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 IAC ISS IWD IYE

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

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

TAM TAP TAR TCX THA THY TNA TSC UAE UAF USA VIR VKG

VLK VOZ XAX XLF YZR

The equivalent of this Service Bulletin has been validated on A340 aircraft MSN 0402.

CONCURRENT REQUIREMENTS

None

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

DATE: Dec 08/10 SERVICE BULLETIN No.: A330-32-3240

REVISION No.: 02 - Dec 02/11 Page: 2

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@A330

SERVICE BULLETIN

SUMMARY

MANPOWER

**CONF 001

Task 323240-832-895-001: INSPECTION

TOTAL MANHOURS 9.00

ELAPSED TIME (HOURS) 7.00

Additional manhours related to Vendor SB; refer to:

DO AN INSPECTION/CHECK OF THE PIVOT PIN AND

BUSHES OF THE LH/RH BOGIE BEAM ASSEMBLY

MESSIER-DOWTY Service Bulletin

No. A33/34-32-285

REPAIR OR REPLACE THE BOGIE BEAM PIVOT PIN

AND THE BOGIE BEAM BUSHES

MESSIER-DOWTY Service Bulletin

No. A33/34-32-285

**CONF 002

Task 323240-832-895-001: INSPECTION

TOTAL MANHOURS 9.00

ELAPSED TIME (HOURS) 7.00

Additional manhours related to Vendor SB; refer to:

DO AN INSPECTION/CHECK OF THE PIVOT PIN AND

BUSHES OF THE LH/RH BOGIE BEAM ASSEMBLY

MESSIER-DOWTY Service Bulletin

No. A33/34-32-285

REPAIR OR REPLACE THE BOGIE BEAM PIVOT PIN

AND THE BOGIE BEAM BUSHES

MESSIER-DOWTY Service Bulletin

No. A33/34-32-285

APPENDICES

**CONF ALL

APPENDIX 01 - Inspection Reports

APPENDIX 02 - Elapsed Time Assumption

DATE: Dec 08/10 SERVICE BULLETIN No.: A330-32-3240

REVISION No.: 02 - Dec 02/11 Page: 3

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@A330

SERVICE BULLETIN

SUMMARY

**CONF ALL

G_SB_323240_7_SAAA_01_00

A

PIVOT PIN

SHOCK

ABSORBER

BOGIE

BEAM

ASSEMBLY

LH SHOWN

RH SIMILAR

B

B

A

Figure A-USAAA - Sheet 01

DATE: Dec 08/10 SERVICE BULLETIN No.: A330-32-3240

REVISION No.: 02 - Dec 02/11 Page: 4

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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 - MLG - REPEAT INSPECTION OF MLG BOGIE PIVOT

PIN

MODIFICATION No.: None

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

NOTE: The equivalent of this Service Bulletin has been validated on A340 aircraft

MSN 0402.

NOTE: A booklet including photographs taken during the validation of Service Bulletin

A340-32-4281 is available on AIRBUS World - Maintenance and Engineering -

Service Bulletin Information.

(1) Models

330-202 330-203 330-223 330-223F 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

DATE: Dec 08/10 SERVICE BULLETIN No.: A330-32-3240

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@A330

SERVICE BULLETIN

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

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 1092-1101 1103-1108 1110

1112 1114-1116 1118 1120 1123-1124 1126-1127 1129-1133 1135-1138 1141 1143

1145-1151 1153 1155-1157 1159-1161 1163-1165 1167-1175 1177-1178 1180-1181

1183-1184 1186-1193 1195-1196 1198-1206 1208-1241 1243-1252 1254-1256

1258-1272 1274-1353 1355-1367 1369-1373 1376 1378 1411

(3) Effectivity by Operator

The Operator/MSN relationship is provided for information only and is correct at the time

of issue in accordance with the information available to AIRBUS. Any future changes

resulting from transfer of an aircraft from one operator to another will not be reflected in

this list unless the Service Bulletin is revised for another reason.

OPERATOR MSN

46W 0871 0925

78V 1033 1046 1248 1275 1312 1334

97X 1053

AAR 0640 0676 0708 0772 0803 0845 1001 1055 1151 1211 1326 1340

AAW 0999 1043

ACA 0277 0279 0284 0344 0400 0408 0412 0419

ACI 0507 0510

AEA 0461 0551 0597 0733 0745 0749 0814 0931 0950

AFL 0963 0973 1014 1045 1047 1058 1065 1072 1077 1103 1232 1247

1264 1270 1284 1299 1301 1323 1328 1345 1356 1371

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

0567 0584 0657

AGC 0324

ALK 0303 0306 0311 0313 0404

ASY 0747 0951 0969 1036 1183

AVA 0948 0967 1009 1016 1073 1208 1224 1279 1342 1363

AZA 0272 0339 1123 1135 1218 1225 1252 1283 1308 1313 1327

DATE: Dec 08/10 SERVICE BULLETIN No.: A330-32-3240

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@A330

SERVICE BULLETIN

OPERATOR MSN

BEC 0863

BEL 0030 0037 0045 0082 0095 0229

BER 0120 0127 0171 0288 0322 0403 0432 0444 0454 0469 0476 0493

0739 0828 0911

BMA 0398 0401

BTV 0205 0330

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

0805 0823 0838 0861 0920 1177 1206 1215 1272 1278 1346 1367

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

0884 0890 0903 0909 0930 0941 0944 0957 1087 1110 1130 1187

1199 1216 1237 1260 1282 1304 1330 1333 1353 1373

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

0836 0851 0862 0866 0916 0928 0936 0942 1262 1267 1280 1291

1303 1324 1331 1372

CHH 0875 0881 0906 0919 0982 1159 1168 1178 1190 1255

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 1196 1222 1239 1285 1317 1343

1349 1362 1366

CRK 1031 1034 1039 1042 1051 1054 1059 1062 1115 1277 1286 1322

1325 1358 1369

CRL 0285 0320 1359 1376

CSC 1082 1138 1241

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

0958 0964 1096 1116 1129 1202 1220 1233 1244 1297 1309 1335

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 1292 1305 1314

EDW 0291 1193

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 1167 1205 1226 1245

EVA 0530 0535 0555 0573 0587 0634 0655 0661 0678 0693 0755 1254

1268 1274

FIN 0994 1007 1013 1023 1067 1078 1088 1173

FWI 0253 0758 0965 1021 1265

G8E 0059

GFA 0276 0281 0286 0287 0334 0340 0527 0529 0532 0992

GIA 0138 0140 0144 0148 0153 0165 0988 1020 1028 1052 1184 1214

1261 1288 1364

GRL 0230

HAL 1104 1114 1171 1217 1259 1295 1302 1310 1316

DATE: Dec 08/10 SERVICE BULLETIN No.: A330-32-3240

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@A330

SERVICE BULLETIN

OPERATOR MSN

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

0716 0741 0786

HFY 0096 0211 1008

HVN 0255 0262 0275 0294 0299 0366 0943 0962 1019 1256 1266

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

1351 1361 1370

JST 0506 0508 0513 0522 0842 0853 0940 0945 1198 1251 1258

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

0351 0368 0425 0428 0484 0490 0550 1133 1155 1200 1203

KFR 0874 0891 0927 0939 0946

KKK 0343 0358 0364

KLM 0682 0686 0703 0738 0770 0801 0811 0819 0834 0900 1161 1287

1294 1300

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

1136 1148 1164 1180 1209 1219 1229 1234 1243 1281 1318 1336

1337 1347

MAU 0883 1057

MEA 0926 0984 0995 0998

MNB 1332

MON 0261 0265

MSR 0600 0610 0666 0683 0696 0709 0726 1143 1230 1238 1246

OBS 0833

OHY 0072 0087 0098 0143

OMA 1038 1044 1049 1063 1093 1120 1227

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 1169 1174 1365

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 1002

RSF 0980 0996 1235

SAA 1191 1210 1223 1236 1249 1271

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

SVA 1108 1127 1137 1141 1147 1153 1189 1192

SWR 0249 1000 1018 1026 1029 1084 1089 1101 1145 1181 1188 1276

1290 1355

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

0949 0961 0968 0977 1112 1118 1213 1221

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

DATE: Dec 08/10 SERVICE BULLETIN No.: A330-32-3240

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@A330

SERVICE BULLETIN

OPERATOR MSN

TAR 1411

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 1263 1269 1289 1338

1348

THY 0463 0504 0697 0704 0742 0754 0774 1004 1092 1150 1160 1170

1172 1204 1212 1228 1240 1298 1307 1311 1344

TNA 1357 1378

TSC 0111 0132 0177 0250 0271 0369 0407 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 1186 1250

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

1069 1076 1095 1100

VIR 1195 1201 1231 1296 1315 1329 1341 1352

VKG 0309 0349 0356 0357

VLK 0055 0070 0086

VOZ 0365 0372 1293 1306 1319

XAX 0054 0952 0974 1048 1066 1075 1126 1131 1165 1321 1339

XLF 0501 0635 1360

YZR 1175 1320 1350

DATE: Dec 08/10 SERVICE BULLETIN No.: A330-32-3240

REVISION No.: 02 - Dec 02/11 Page: 5

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SERVICE BULLETIN

(4) Configuration by MSN

MSN CONFIGURATION

0012 0017 0030 0037 0045 0050 0054 0055 0059 0060 0062

0064 0065 0066 0067 0069 0070 0071 0072 0073 0077 0082

0083 0086 0087 0095 0096 0098 0099 0100 0102 0106 0107

0109 0110 0111 0112 0113 0116 0118 0119 0120 0121 0122

0127 0132 0138 0140 0143 0144 0148 0153 0155 0162 0165

0171 0172 0177 0181 0183 0184 0188 0189 0191 0195 0198

0200 0203 0205 0206 0209 0211 0219 0222 0223 0224 0226

0229 0230 0231 0232 0234 0238 0240 0241 0244 0247 0248

0249 0250 0251 0253 0254 0255 0256 0258 0259 0261 0262

0265 0266 0267 0269 0271 0272 0275 0276 0277 0279 0281

0283 0284 0285 0286 0287 0288 0290 0291 0293 0294 0295

0296 0299 0300 0301 0303 0305 0306 0308 0309 0311 0312

0313 0314 0315 0316 0317 0320 0322 0323 0324 0326 0328

0330 0333 0334 0337 0338 0339 0340 0342 0343 0344 0345

0346 0348 0349 0350 0351 0353 0356 0357 0358 0361 0362

0364 0365 0366 0368 0369 0370 0372 0375 0380 0382 0384

0386 0388 0389 0392 0393 0396 0397 0398 0400 0401 0403

0404 0405 0407 0408 0409 0412 0418 0419 0420 0421 0422

0423 0425 0427 0428 0432 0437 0439 0441 0443 0444 0448

0451 0452 0454 0455 0456 0458 0461 0462 0463 0465 0466

0469 0472 0473 0476 0477 0479 0480 0481 0484 0486 0487

0489 0490 0491 0493 0494 0496 0497 0498 0500 0501 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 0737 0739 0741 0743 0745 0746 0749 0752 0755

0760

001

DATE: Dec 08/10 SERVICE BULLETIN No.: A330-32-3240

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SERVICE BULLETIN

MSN CONFIGURATION

0735 0738 0742 0747 0750 0751 0754 0756 0758 0759 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 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

1092 1093 1094 1095 1096 1097 1098 1099 1100 1101 1103

1104 1105 1106 1107 1108 1110 1112 1114 1115 1116 1118

1120 1123 1124 1126 1127 1129 1130 1131 1132 1133 1135

1136 1137 1138 1141 1143 1145 1146 1147 1148 1149 1150

1151 1153 1155 1156 1157 1159 1160 1161 1163 1164 1165

1167 1168 1169 1170 1171 1172 1173 1174 1175 1177 1178

1180 1181 1183 1184 1186 1187 1188 1189 1190 1191 1192

1193 1195 1196 1198 1199 1200 1201 1202 1203 1204 1205

1206 1208 1209 1210 1211 1212 1213 1214 1215 1216 1217

1218 1219 1220 1221 1222 1223 1224 1225 1226 1227 1228

1229 1230 1231 1232 1233 1234 1235 1236 1237 1238 1239

1240 1241 1243 1244 1245 1246 1247 1248 1249 1250 1251

1252 1254 1255 1256 1258 1259 1260 1261 1262 1263 1264

1265 1266 1267 1268 1269 1270 1271 1272 1274 1275 1276

1277 1278 1279 1280 1281 1282 1283 1284 1285 1286 1287

1288 1289 1290 1291 1292 1293 1294 1295 1296 1297 1298

1299 1300 1301 1302 1303 1304 1305 1306 1307 1308 1309

1310 1311 1312 1313 1314 1315 1316 1317 1318 1319 1320

1321 1322 1323 1324 1325 1326 1327 1328 1329 1330 1331

1332 1333 1334 1335 1336 1337 1338 1339 1340 1341 1342

1343 1344 1345 1346 1347 1348 1349 1350 1351 1352 1353

1355 1356 1357 1358 1359 1360 1361 1362 1363 1364 1365

1366 1367 1369 1370 1371 1372 1373 1376 1378 1411

002

DATE: Dec 08/10 SERVICE BULLETIN No.: A330-32-3240

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SERVICE BULLETIN

(5) Configuration definition

**CONF 001

Config. 001 is valid for all aircraft with a basic or growth Main Landing Gear (Pre

Modification 54500H15561) (Pre Service Bulletin No. A330-32-3212).

Aircraft that have embodied Service Bulletin No. A330-32-3212 are to be considered as

Config. 002.

**CONF 002

Config. 002 is valid for all aircraft with an enhanced Main Landing Gear (Post

Modification 54500H15561) (Post Service Bulletin No. A330-32-3212).

(6) Material Effectivity

No Kit

B. CONCURRENT REQUIREMENTS

None

C. REASON

(1) History

The bogie pivot pin makes the connection between the landing gear slider and the bogie

beam. This component is a Principal Structural Element (PSE).

In-service feed-backs indicate an increasing number of bogie pivot pin replacements due

to unexpected findings upon removal. Operators report a high number of events related

to chrome detachment or chrome dragging. There have been a number of confirmed

crackings of the bogie pivot pins since Entry Into Service (EIS).

(2) Objective/Action

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

Messier-Dowty Service Bulletin No. A33/34-32-285.

VSB A33/34-32-285 details:

- a Detailed Visual Inspection (DVI) of the bogie pivot pin chromium-plated surface

- a Magnetic Particle Inspection (MPI) of the bogie pivot pin if damage is found to the

chromium-plated surface

- a DVI of the pivot pin bushes in the bogie beam and sliding tube.

(3) Advantages

This inspection will:

- make sure that all damaged bogie pivot pins are repaired or replaced if found

damaged

DATE: Dec 08/10 SERVICE BULLETIN No.: A330-32-3240

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SERVICE BULLETIN

- gather detailed information from the fleet to further investigate this issue and

prepare a long term fix.

(4) Operational/Maintenance Consequences

None

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

**CONF 001

Task 323240-832-895-001: INSPECTION

(1) REMOVE THE MLG BOGIE BEAM ASSEMBLY PIVOT PIN (LH/RH)

(2) DO AN INSPECTION/CHECK OF THE PIVOT PIN AND BUSHES OF THE LH/RH

BOGIE BEAM ASSEMBLY

(3) REPAIR OR REPLACE THE BOGIE BEAM PIVOT PIN AND THE BOGIE BEAM

BUSHES

(4) INSTALL THE MLG BOGIE BEAM ASSEMBLY PIVOT PIN (LH/RH)

**CONF 002

Task 323240-832-895-001: INSPECTION

(1) REMOVE THE MLG BOGIE BEAM ASSEMBLY PIVOT PIN (LH/RH)

(2) DO AN INSPECTION/CHECK OF THE PIVOT PIN AND BUSHES OF THE LH/RH

BOGIE BEAM ASSEMBLY

(3) REPAIR OR REPLACE THE BOGIE BEAM PIVOT PIN AND THE BOGIE BEAM

BUSHES

(4) INSTALL THE MLG BOGIE BEAM ASSEMBLY PIVOT PIN (LH/RH)

**CONF ALL

E. COMPLIANCE

(1) Classification

MANDATORY: Service Bulletin must be accomplished.

(2) Accomplishment Timescale

Within 26 months after the effective date of the Airworthiness Directive (AD) or the first

flight, whichever occurs later, but not before the accumulation of 12 months since first

flight.

Repeat the inspection at intervals not exceeding 26 months.

DATE: Dec 08/10 SERVICE BULLETIN No.: A330-32-3240

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SERVICE BULLETIN

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). It is anticipated that the AD will confirm the Accomplishment Timescale

given above but reference should be made to the AD for confirmation of the mandated

accomplishment timescale.

NOTE: The threshold and grace period may change subject to the receipt of

further data.

F. APPROVAL

The technical content of this document is approved under authority of Design Organization

Approval No. EASA.21J.031.

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

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

responsible for obtaining approval by its airworthiness authority for any adaptation necessary

before incorporation of the Service Bulletin.

G. MANPOWER

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

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

and may need to be revised upwards to suit operator’s circumstances. The estimates do not

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

and tools, drying times for paints, sealants, etc., and general administration work are also not

included.

**CONF 001

Task 323240-832-895-001: INSPECTION

Get Access 2.00

On Aircraft

REMOVE THE MLG BOGIE BEAM ASSEMBLY PIVOT

PIN (LH/RH)

2.00

INSTALL THE MLG BOGIE BEAM ASSEMBLY PIVOT

PIN (LH/RH)

2.00

Tests 1.00

Close-Up 2.00

TOTAL MANHOURS 9.00

ELAPSED TIME (HOURS) 7.00

Additional manhours related to Vendor SB; refer to:

DO AN INSPECTION/CHECK OF THE PIVOT PIN

AND BUSHES OF THE LH/RH BOGIE BEAM

ASSEMBLY

MESSIER-DOWTY Service Bulletin

No. A33/34-32-285

REPAIR OR REPLACE THE BOGIE BEAM PIVOT PIN

AND THE BOGIE BEAM BUSHES

MESSIER-DOWTY Service Bulletin

No. A33/34-32-285

DATE: Dec 08/10 SERVICE BULLETIN No.: A330-32-3240

REVISION No.: 02 - Dec 02/11 Page: 10

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SERVICE BULLETIN

**CONF 002

Task 323240-832-895-001: INSPECTION

Get Access 2.00

On Aircraft

REMOVE THE MLG BOGIE BEAM ASSEMBLY PIVOT

PIN (LH/RH)

2.00

INSTALL THE MLG BOGIE BEAM ASSEMBLY PIVOT

PIN (LH/RH)

2.00

Tests 1.00

Close-Up 2.00

TOTAL MANHOURS 9.00

ELAPSED TIME (HOURS) 7.00

Additional manhours related to Vendor SB; refer to:

DO AN INSPECTION/CHECK OF THE PIVOT PIN

AND BUSHES OF THE LH/RH BOGIE BEAM

ASSEMBLY

MESSIER-DOWTY Service Bulletin

No. A33/34-32-285

REPAIR OR REPLACE THE BOGIE BEAM PIVOT PIN

AND THE BOGIE BEAM BUSHES

MESSIER-DOWTY Service Bulletin

No. A33/34-32-285

**CONF ALL

H. WEIGHT AND BALANCE

Not Changed

I. ELECTRICAL LOAD DATA

Not Changed

J. REFERENCES

**CONF 001

Aircraft Maintenance Manual (AMM) 07-11-00 12-12-29 12-22-32

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

29-00-00 32-00-00 32-11-14

32-11-15

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

Vendor Service Bulletin (VSB) MESSIER-DOWTY Service Bulletin

No. A33/34-32-285

DATE: Dec 08/10 SERVICE BULLETIN No.: A330-32-3240

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SERVICE BULLETIN

**CONF 002

Aircraft Maintenance Manual (AMM) 07-11-00 12-12-29 12-22-32

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

29-00-00 32-00-00 32-11-14

32-11-15

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

Vendor Service Bulletin (VSB) MESSIER-DOWTY Service Bulletin

No. A33/34-32-285

**CONF ALL

K. PUBLICATION AFFECTED

None

L. INTERCHANGEABILITY/MIXABILITY

Not Applicable

M. SPARES

None

DATE: Dec 08/10 SERVICE BULLETIN No.: A330-32-3240

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SERVICE BULLETIN

2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

(1) Procurement Addresses

Vendor parts are to be procured from:

Messier-Dowty SA

BP 10-78142 Velizy Cedex

France

(2) Price and Availability

Refer to the Vendor Service Bulletin MESSIER-DOWTY VSB No. A33/34-32-285 for the

equipment sales terms.

B. INDUSTRY SUPPORT INFORMATION

No AIRBUS kit will be provided.

Procurement terms for the equipment must be negotiated with the equipment supplier.

C. LIST OF COMPONENTS

No Kit

D. LIST OF MATERIALS - OPERATOR SUPPLIED

(1) Consumable Materials

To accomplish this Service Bulletin it will be necessary to use the consumable items

listed in AMM Task 32-11-14-410-801 and MESSIER-DOWTY VSB No. A33/34-32-285.

(2) Components

To accomplish this Service Bulletin it will be necessary to use the expendable parts

listed in AMM Task 32-11-14-410-801 and MESSIER-DOWTY VSB No. A33/34-32-285.

(3) Equipment

None

E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

None

DATE: Dec 08/10 SERVICE BULLETIN No.: A330-32-3240

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SERVICE BULLETIN

F. TOOLING

(1) Tooling - Price and Availability

None

(2) Tools

Refer to MESSIER-DOWTY VSB No. A33/34-32-285 and AMM task 32-11-14-410-801

for the standard tools necessary.

Refer to MESSIER-DOWTY VSB No. A33/34-32-285 and AMM task 32-11-14-010-801

for the standard tools necessary.

(3) Special Tools

None

DATE: Dec 08/10 SERVICE BULLETIN No.: A330-32-3240

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SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS

Task 323240-832-895-001 - INSPECTION

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 9.00

ELAPSED TIME (HOURS) 7.00

Additional manhours related to Vendor SB; refer to:

MESSIER-DOWTY Service Bulletin No. A33/34-32-285

**CONF 002

Manpower

TOTAL MANHOURS 9.00

ELAPSED TIME (HOURS) 7.00

Additional manhours related to Vendor SB; refer to:

MESSIER-DOWTY Service Bulletin No. A33/34-32-285

DATE: Dec 08/10 SERVICE BULLETIN No.: A330-32-3240

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SERVICE BULLETIN

**CONF ALL

A. GENERAL

**CONF 001

(1) Subtask 323240-910-401-001 - 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 wire-locking, 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.

(2) Subtask 323240-839-401-001 - ADMINISTRATIVE

Manpower Resources

Skills AIRFRAME

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

Service Bulletin.

**CONF 002

(1) Subtask 323240-910-401-001 - 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 wire-locking, 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.

(2) Subtask 323240-839-401-001 - ADMINISTRATIVE

Manpower Resources

Skills AIRFRAME

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

Service Bulletin.

DATE: Dec 08/10 SERVICE BULLETIN No.: A330-32-3240

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SERVICE BULLETIN

**CONF ALL

B. PREPARATION

**CONF 001

(1) Subtask 323240-941-401-001 - JOB SET-UP

Manpower Resources

Skills AIRFRAME

References

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

Task 29-00-00-864-804

Task 32-00-00-481-801

Task 32-00-00-481-802

Task 32-11-14-010-801

Task 32-11-15-000-801

(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) Put Warning Notices in the cockpit to tell persons:

- Do not operate the landing gear or brakes

- Do not operate the Green and Blue hydraulic systems.

(d) Make sure that the Green and Blue hydraulic systems are depressurized (Refer to

AMM Task 29-00-00-864-804).

(e) Depressurize the bogie pitch trimmer (Refer to AMM Task 32-11-15-000-801).

(f) Open the applicable circuit breakers. Do the work steps given in the Job Set-Up

procedure (Refer to AMM Task 32-11-14-010-801).

**CONF 002

(1) Subtask 323240-941-401-001 - JOB SET-UP

Manpower Resources

Skills AIRFRAME

References

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

Task 29-00-00-864-804

Task 32-00-00-481-801

Task 32-00-00-481-802

Task 32-11-14-010-801

Task 32-11-15-000-801

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(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) Put Warning Notices in the cockpit to tell persons:

- Do not operate the landing gear or brakes

- Do not operate the Green and Blue hydraulic systems.

(d) Make sure that the Green and Blue hydraulic systems are depressurized (Refer to

AMM Task 29-00-00-864-804).

(e) Depressurize the bogie pitch trimmer (Refer to AMM Task 32-11-15-000-801).

(f) Open the applicable circuit breakers. Do the work steps given in the Job Set-Up

procedure (Refer to AMM Task 32-11-14-010-801).

**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 323240-020-401-001 - REMOVE THE MLG BOGIE BEAM ASSEMBLY PIVOT

PIN (LH/RH)

Manpower Resources

Manhours 2.00

Minimum number of person 2

Subtask elapsed time 1.00

Skills AIRFRAME

References

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

Task 32-11-14-000-801

Task 32-11-14-010-801

Fig. A-UCAAA

MLG Pivot Pin - Removal/Installation

Sheet 01

NOTE: The worksteps that follow are to be accomplished on the LH and RH

MLG. It is recommended to complete the pivot pin removal, inspection

and pivot pin installation on one MLG and then continue on the other

MLG.

NOTE: For this Inspection Procedure (and possible Repair) you will lift the

aircraft on jacks until the aircraft weight is off the bogie beam and the

pivot pin can be turned.

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(a) Do the "Job Set-Up" procedure (Refer to Removal of MLG Bogie Beam Assembly

for Access, Complete with Wheels and Brakes AMM Task 32-11-14-010-801).

NOTE: It is not necessary to do the "Preparation for Removal" step in

the above procedure, continue with this alternative procedure as

follows:

(b) Remove the Bogie Beam Assembly pivot pin as follows (Refer to Fig. A-UCAAA

Sheet 01):

WARNING: WEAR GOGGLES WHEN YOU REMOVE OR INSTALL

LOCKWIRE. CUT, REMOVE AND DISCARD THE LOCKWIRE AS

YOU DO THE TASK. LOOSE LOCKWIRE CAN CUT OR BLIND

YOU.

1 Cut and discard the lockwire from the bolts, item (1).

2 Remove:

3 Bolt NAS6604H3 Item (1) Retain

3 Washer AN960-416L Item (2) Retain

1 Collar 201042188 Item (3) Retain

3 Install the BOGIE NUT SPANNER PN 460007022, together with the TORQUE

MULTIPLIER PN 460007027 on the nut, item (4). Install the reactor PN

460007028 on the head of the pin, item (5).

4 Remove:

1 Nut 201269613 Item (4) Retain

5 Remove the SPANNER PN 460007022 and TORQUE MULTIPLIER PN

460007027 from the nut, item (4).

6 Lift the aircraft on jacks (Refer to AMM Task 07-11-00-581-801) until the

weight of the aircraft is not on the bogie beam assembly, item (6). The pin,

item (5), can now be turned with the REACTOR PN 460007028.

7 Remove the REACTOR PN 460007028 from the pin, item (5).

NOTE: If it is not possible to turn the pin, item (5), with the aircraft

weight off the bogie beam assembly, refer to AMM Task

32-11-14-000-801 to complete the procedure.

8 Remove:

1 Pin 201254925 Item (5) Retain

or

1 Pin 201269612 Item (5) Retain

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or

1 Pin 201489751 Item (5) Retain

or

1 Pin 201489621 Item (5) Retain

NOTE: Do not remove the bogie beam from the aircraft unless it is

necessary to perform the complete MLG bogie beam assembly

removal procedure (Refer to AMM Task 32-11-14-000-801).

NOTE: These steps are only to get access to the pins and bushes for

an inspection.

NOTE: Bogie Pivot Pins with the Part Number (PN) 201269612 or PN

201489621 are no longer available. If pins with these part

numbers are removed they must be replaced with pin PN

201254925 for aircraft Post Mod 46904 or PN 201489751 for

aircraft Post Mod 43029 and 46904.

(2) Subtask 323240-210-401-001 - DO AN INSPECTION/CHECK OF THE PIVOT PIN

AND BUSHES OF THE LH/RH BOGIE BEAM ASSEMBLY

References

Vendor Service Bulletin (VSB) MESSIER-DOWTY A33/34-32-285

Fig. A-UBAAA

Flowchart

Sheet 01

(a) Do an inspection of the pivot pin and bushes of the LH/RH Bogie Beam Assembly

(Refer to MESSIER-DOWTY Service Bulletin No. A33/34-32-285 and Fig. AUBAAA).

(b) Report all findings and no findings to AIRBUS within 90 days (Refer to APPENDIX

01 - Inspection Reports ).

(c) If the existing bogie beam assembly pivot pin and bushes are in a serviceable

condition (Refer to MESSIER-DOWTY Service Bulletin No. A33/34-32-285) go

to subtask SUBTASK 323240-420-401 001 INSTALL THE MLG BOGIE BEAM

ASSEMBLY PIVOT PIN (LH/RH) .

(d) If the existing bogie beam assembly pivot pin and bushes are not in a serviceable

condition go to subtask SUBTASK 323240-833-401 001 REPAIR OR REPLACE

THE BOGIE BEAM PIVOT PIN AND THE BOGIE BEAM BUSHES .

(3) Subtask 323240-833-401-001 - REPAIR OR REPLACE THE BOGIE BEAM PIVOT PIN

AND THE BOGIE BEAM BUSHES

References

Vendor Service Bulletin (VSB) MESSIER-DOWTY A33/34-32-285

(a) If the bogie beam pivot pin is not in a serviceable condition replace or repair (Refer

to MESSIER-DOWTY Service Bulletin No. A33/34-32-285).

DATE: Dec 08/10 SERVICE BULLETIN No.: A330-32-3240

REVISION No.: 02 - Dec 02/11 Page: 20

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SERVICE BULLETIN

(b) If the bogie beam bushes are not in a serviceable condition replace or repair (Refer

to MESSIER-DOWTY Service Bulletin No. A33/34-32-285).

(4) Subtask 323240-420-401-001 - INSTALL THE MLG BOGIE BEAM ASSEMBLY PIVOT

PIN (LH/RH)

Manpower Resources

Manhours 2.00

Minimum number of person 2

Subtask elapsed time 1.00

Skills AIRFRAME

References

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

Task 12-12-29-611-801

Task 12-22-32-640-801

Task 29-00-00-210-801

Task 29-00-00-863-801

Task 29-00-00-863-802

Task 32-11-14-400-801

Task 32-11-14-410-801

Task 32-11-15-400-801

(a) Do the "Preparation for Installation" procedure (Refer to AMM Task "Installation of

the MLG Bogie Beam Assembly after Access, Complete with Wheels and Brakes"

AMM Task 32-11-14-410-801).

NOTE: It will not be necessary to move the bogie on its wheels, into

position below the applicable shock absorber if the bogie beam was

not removed.

(b) Install from the inboard side:

1 Pin 201254925 Item (5) Retained at

removal

or

1 Pin 201489751 Item (5) Retained at

removal

1 Nut 201269613 Item (4) Retained at

removal

1 Collar 201042188 Item (3) Retained at

removal

3 Washer AN960-416L Item (2) Retained at

removal

3 Bolt NAS6604H3 Item (1) Retained at

removal

DATE: Dec 08/10 SERVICE BULLETIN No.: A330-32-3240

REVISION No.: 02 - Dec 02/11 Page: 21

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SERVICE BULLETIN

and do the "Installation of the Bogie Beam Assembly after Access, Complete with

Wheels and Brakes" procedure (Refer to "Installation of the Bogie Beam Assembly

after Access, Complete with Wheels and Brakes" AMM Task 32-11-14-410-801.

(c) If necessary: Install the bogie beam assembly (Refer to AMM Task

32-11-14-400-801).

(d) Bleed the MLG Bogie Pitch Trimmer (Refer to AMM Task 32-11-15-400-801).

(e) If the bogie beam was removed/installed, lift the aircraft until the wheels are free to

turn (Refer to AMM Task 07-11-00-581-801).

(f) Lubricate the bogie pivot pin (Refer to AMM Task 12-22-32-640-801).

(g) Close these circuit breakers:

PANEL DESIGNATION FIN LOCATION SEE

NOTES

721 HYD PUMP G CTL 9JV 09 U

721 HYD PUMP B CTL 9JC 12 X

722 LGCIU 2 2GA 38 U

722 BSCU SYS 2 2GG 37 U

742 BSCU SYS 1 1GG 62 G

742 LGCIU 1 1GA 63 L

**CONF 002

(1) Subtask 323240-020-401-003 - REMOVE THE MLG BOGIE BEAM ASSEMBLY PIVOT

PIN (LH/RH)

Manpower Resources

Manhours 2.00

Minimum number of person 2

Subtask elapsed time 1.00

Skills AIRFRAME

References

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

Task 32-11-14-000-801

Task 32-11-14-010-801

Fig. A-UCAAA

MLG Pivot Pin - Removal/Installation

Sheet 01

NOTE: The worksteps that follow are to be accomplished on the LH and RH

MLG. It is recommended to complete the pivot pin removal, inspection

and pivot pin installation on one MLG and then continue on the other

MLG.

NOTE: For this Inspection Procedure (and possible Repair) you will lift the

aircraft on jacks until the aircraft weight is off the bogie beam and the

pivot pin can be turned.

DATE: Dec 08/10 SERVICE BULLETIN No.: A330-32-3240

REVISION No.: 02 - Dec 02/11 Page: 22

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SERVICE BULLETIN

(a) Do the "Job Set-Up" procedure (Refer to Removal of MLG Bogie Beam Assembly

for Access, Complete with Wheels and Brakes AMM Task 32-11-14-010-801).

NOTE: It is not necessary to do the "Preparation for Removal" step in

the above procedure, continue with this alternative procedure as

follows:

(b) Remove the Bogie Beam Assembly pivot pin as follows (Refer to Fig. A-UCAAA

Sheet 01):

WARNING: WEAR GOGGLES WHEN YOU REMOVE OR INSTALL

LOCKWIRE. CUT, REMOVE AND DISCARD THE LOCKWIRE AS

YOU DO THE TASK. LOOSE LOCKWIRE CAN CUT OR BLIND

YOU.

1 Cut and discard the lockwire from the bolts, item (1).

2 Remove:

3 Bolt NAS6604H3 Item (1)

3 Washer AN960-416L Item (2)

1 Collar 201042663 Item (3)

3 Install the BOGIE NUT SPANNER PN DRT67212, together with the TORQUE

MULTIPLIER PN 460007027 on the nut, item (4). Install the reactor PN

DRT68817 on the head of the pin, item (5).

4 Remove:

1 Nut 201489622 Item (4)

5 Remove the SPANNER PN DRT67212 and TORQUE MULTIPLIER PN

460007027 from the nut, item (4).

6 Lift the aircraft on jacks (Refer to AMM Task 07-11-00-581-801) until the

weight of the aircraft is not on the bogie beam assembly, item (6). The pin,

item (5), can now be turned with the REACTOR PN DRT68817.

7 Remove the REACTOR PN DRT68817 from the pin, item (5).

NOTE: If it is not possible to turn the pin, item (5), with the aircraft

weight off the bogie beam assembly, refer to AMM Task

32-11-14-000-801 to complete the procedure.

8 Remove:

1 Pin 55-2105029-00 Item (5)

NOTE: Do not remove the bogie beam from the aircraft unless it is

necessary to perform the complete MLG bogie beam assembly

removal procedure (Refer to AMM Task 32-11-14-000-801).

DATE: Dec 08/10 SERVICE BULLETIN No.: A330-32-3240

REVISION No.: 02 - Dec 02/11 Page: 23

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SERVICE BULLETIN

NOTE: These steps are only to get access to the pins and bushes for

an inspection.

(2) Subtask 323240-210-401-001 - DO AN INSPECTION/CHECK OF THE PIVOT PIN

AND BUSHES OF THE LH/RH BOGIE BEAM ASSEMBLY

References

Vendor Service Bulletin (VSB) MESSIER-DOWTY A33/34-32-285

Fig. A-UBAAA

Flowchart

Sheet 01

(a) Do an inspection of the pivot pin and bushes of the LH/RH Bogie Beam Assembly

(Refer to MESSIER-DOWTY Service Bulletin No. A33/34-32-285 and Fig. AUBAAA).

(b) Report all findings and no findings to AIRBUS within 90 days (Refer to APPENDIX

01 - Inspection Reports ).

(c) If the existing bogie beam assembly pivot pin and bushes are in a serviceable

condition (Refer to MESSIER-DOWTY Service Bulletin No. A33/34-32-285) go

to subtask SUBTASK 323240-420-401 003 INSTALL THE MLG BOGIE BEAM

ASSEMBLY PIVOT PIN (LH/RH) .

(d) If the existing bogie beam assembly pivot pin and bushes are not in a serviceable

condition go to subtask SUBTASK 323240-833-401 001 REPAIR OR REPLACE

THE BOGIE BEAM PIVOT PIN AND THE BOGIE BEAM BUSHES .

(3) Subtask 323240-833-401-001 - REPAIR OR REPLACE THE BOGIE BEAM PIVOT PIN

AND THE BOGIE BEAM BUSHES

References

Vendor Service Bulletin (VSB) MESSIER-DOWTY A33/34-32-285

(a) If the bogie beam pivot pin is not in a serviceable condition replace or repair (Refer

to MESSIER-DOWTY Service Bulletin No. A33/34-32-285).

(b) If the bogie beam bushes are not in a serviceable condition replace or repair (Refer

to MESSIER-DOWTY Service Bulletin No. A33/34-32-285).

(4) Subtask 323240-420-401-003 - INSTALL THE MLG BOGIE BEAM ASSEMBLY PIVOT

PIN (LH/RH)

Manpower Resources

Manhours 2.00

Minimum number of person 2

Subtask elapsed time 1.00

Skills AIRFRAME

DATE: Dec 08/10 SERVICE BULLETIN No.: A330-32-3240

REVISION No.: 02 - Dec 02/11 Page: 24

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SERVICE BULLETIN

References

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

Task 12-12-29-611-801

Task 12-22-32-640-801

Task 29-00-00-210-801

Task 29-00-00-863-801

Task 29-00-00-863-802

Task 32-11-14-400-801

Task 32-11-14-410-801

Task 32-11-15-400-801

(a) Do the "Preparation for Installation" procedure (Refer to AMM Task "Installation of

the MLG Bogie Beam Assembly after Access, Complete with Wheels and Brakes"

AMM Task 32-11-14-410-801).

NOTE: It will not be necessary to move the bogie on its wheels, into

position below the applicable shock absorber if the bogie beam was

not removed.

(b) Install:

1 Pin 55-2105029-00 Item (5) Retained at

removal

and

1 Nut 201489622 Item (4) Retained at

removal

1 Collar 201042663 Item (3) Retained at

removal

3 Washer AN960-416L Item (2) Retained at

removal

3 Bolt NAS6604H3 Item (1) Retained at

removal

(c) and do the "Installation of the Bogie Beam Assembly after Access, Complete with

Wheels and Brakes" procedure (Refer to "Installation of the Bogie Beam Assembly

after Access, Complete with Wheels and Brakes" AMM Task 32-11-14-410-801.

(d) If necessary: Install the bogie beam assembly (Refer to AMM Task

32-11-14-400-801).

(e) Bleed the MLG Bogie Pitch Trimmer (Refer to AMM Task 32-11-15-400-801).

(f) If the bogie beam was removed/installed, lift the aircraft until the wheels are free to

turn (Refer to AMM Task 07-11-00-581-801).

(g) Lubricate the bogie pivot pin (Refer to AMM Task 12-22-32-640-801).

DATE: Dec 08/10 SERVICE BULLETIN No.: A330-32-3240

REVISION No.: 02 - Dec 02/11 Page: 25

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SERVICE BULLETIN

(h) Close these circuit breakers:

PANEL DESIGNATION FIN LOCATION SEE

NOTES

721 HYD PUMP G CTL 9JV 09 U

721 HYD PUMP B CTL 9JC 12 X

722 LGCIU 2 2GA 38 U

722 BSCU SYS 2 2GG 37 U

742 BSCU SYS 1 1GG 62 G

742 LGCIU 1 1GA 63 L

**CONF ALL

D. TEST

**CONF 001

(1) Subtask 323240-710-401-001 - Test of the Landing Gear Assembly - Functional and

Operational

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 32-11-14-000-801

Task 32-11-14-400-801

NOTE: Testing is only necessary if the MLG hydraulic dressings and electrical

harnesses have been disconnected.

(a) If it was necessary to perform the complete MLG Bogie Beam Assembly Removal

procedure as per AMM Task 32-11-14-000-801; do the tests as specified in the

AMM Task "Installation of the MLG Bogie Beam Assembly" (Refer to AMM Task

32-11-14-400-801).

**CONF 002

(1) Subtask 323240-710-401-001 - Test of the Landing Gear Assembly - Functional and

Operational

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 32-11-14-000-801

Task 32-11-14-400-801

NOTE: Testing is only necessary if the MLG hydraulic dressings and electrical

harnesses have been disconnected.

DATE: Dec 08/10 SERVICE BULLETIN No.: A330-32-3240

REVISION No.: 02 - Dec 02/11 Page: 26

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SERVICE BULLETIN

(a) If it was necessary to perform the complete MLG Bogie Beam Assembly Removal

procedure as per AMM Task 32-11-14-000-801; do the tests as specified in the

AMM Task "Installation of the MLG Bogie Beam Assembly" (Refer to AMM Task

32-11-14-400-801).

**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 323240-942-401-001 - CLOSE-UP

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 07-11-00-586-801

(a) Lower the aircraft off the jacks (Refer to AMM Task 07-11-00-586-801).

(b) Remove all the fixtures, tools and support equipment used during this procedure.

**CONF 002

(1) Subtask 323240-942-401-001 - CLOSE-UP

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 07-11-00-586-801

(a) Lower the aircraft off the jacks (Refer to AMM Task 07-11-00-586-801).

(b) Remove all the fixtures, tools and support equipment used during this procedure.

DATE: Dec 08/10 SERVICE BULLETIN No.: A330-32-3240

REVISION No.: 02 - Dec 02/11 Page: 27

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SERVICE BULLETIN

**CONF ALL

PERFORM A DETAILED VISUAL INSPECTION OF THE BOGIE

PIVOT PIN AND BOGIE PIVOT PIN BUSHES IN ACCORDANCE

WITH VSB A33/34−32−285.

IS THE BOGIE

PIVOT PIN BASE METAL

CORRODED?

IS THE BOGIE

PIVOT PIN BASE METAL

CRACKED?

INSPECTION REPORT APPENDIX 1

RETURN AIRCRAFT TO SERVICE AND

INFORM AIRBUS OF THE INSPECTION

RESULT WITHIN 90 DAYS USING THE

INSPECTION RESULT WITHIN 90 DAYS USING

REPAIR OR REPLACE COMPONENTS BEFORE

NEXT FLIGHT. RECORD SIZE, POSITION AND 

PHOTOGRAPH AND INFORM AIRBUS OF THE

RECORD SIZE, POSITION

AND PHOTOGRAPH.

PERFORM AN NDT INSPECTION OF THE

BOGIE PIVOT PIN IN ACCORDANCE WITH

VSB A33/34−32−285.

YES

YES RECORD SIZE, POSITION

AND PHOTOGRAPH.

NO

NO YES

RECORD SIZE, POSITION

ORIENTATION AND

PHOTOGRAPH.

NO

IS THE

BOGIE PIVOT PIN

CHROME PLATING NO

YES

DAMAGED?

ARE THE

BUSHES IN THE BOGIE

BEAM OR THE SLIDING

TUBE DAMAGED?

THE INSPECTION REPORT APPENDIX 1

THE INSPECTION REPORT APPENDIX 1

REPLACE COMPONENT BEFORE NEXT

FLIGHT AND INFORM AIRBUS OF THE

INSPECTION RESULT WITHIN 90 DAYS USING

INSPECTION REPORT APPENDIX 1

RETURN AIRCRAFT TO SERVICE AND

INFORM AIRBUS OF THE INSPECTION

RESULT WITHIN 90 DAYS USING THE

OF THE INSPECTION RESULT WITHIN 90 DAYS

REPAIR OR REPLACE COMPONENTS IN

ACCORDANCE WITH VSB A33/34−32−285

BEFORE NEXT FLIGHT AND INFORM AIRBUS

USING THE INSPECTION REPORT APPENDIX 1

G_SB_323240_7_BAAA_01_05

REPEAT INSPECTION

WITHIN 26 MONTHS

REPEAT INSPECTION

WITHIN 26 MONTHS

Figure A-UBAAA - Sheet 01

Flowchart

DATE: Dec 08/10 SERVICE BULLETIN No.: A330-32-3240

REVISION No.: 02 - Dec 02/11 Page: 28

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SERVICE BULLETIN

**CONF ALL

A

LH SHOWN

RH SIMILAR

B

B

A

SHOCK

ABSORBER

G_SB_323240_7_CAAA_01_01

Figure A-UCAAA - Sheet 01

MLG Pivot Pin - Removal/Installation

DATE: Dec 08/10 SERVICE BULLETIN No.: A330-32-3240

REVISION No.: 02 - Dec 02/11 Page: 29

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SERVICE BULLETIN

This Page Intentionally Left Blank

DATE: Dec 08/10 SERVICE BULLETIN No.: A330-32-3240

REVISION No.: 02 - Dec 02/11 Page: 30

7

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SERVICE BULLETIN

APPENDIX 01 - Inspection Reports

**CONF ALL

(1) The results of the inspections, including no findings, replacement or actions to be done, must be

reported to AIRBUS, Department SEEL3, within 90 days on the attached report sheets.

DATE: Dec 08/10 SERVICE BULLETIN No.: A330-32-3240

REVISION No.: 02 - Dec 02/11 Page: 1

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SERVICE BULLETIN

APPENDIX 01 - Inspection Reports

**CONF ALL

G_SB_323240_7_BBAA_01_02

OPERATOR:

MAIN LANDING GEAR LH OR RH (TICK BOX AS NECESSARY)

MLG PART NO:

BOGIE PIVOT PIN PART NO:

LUBRICATION INTERVALS FOR THE BOGIE PIVOT PIN:

TYPE OF GREASE USED

INSPECTION DATE:

MAIN LANDING GEAR REPORT

INSPECTION OF THE BOGIE PIVOT PIN (TICK BOX AS NECESSARY)

AIRCRAFT MSN:

MLG SERIAL NO:

BOGIE PIVOT PIN SERIAL NO:

1. VISUAL INSPECTION OF THE CHROMIUM PLATE SURFACE OF THE BOGIE PIVOT PIN

NIL FINDINGS

CHROMIUM PLATE DAMAGE. IF THIS BOX IS TICKED RECORD THE DAMAGE FOUND

A. IF THE BOX ABOVE IS TICKED WAS THERE DAMAGE TO THE:

BOGIE BEAM BUSH(ES):

SLIDING TUBE BUSH(ES):

B. WAS THE BOGIE PIVOT PIN REPLACED:

YES NO *

YES NO *

YES NO

2. MAGNETIC PARTICLE INSPECTION OF THE BOGIE PIVOT PIN

NIL FINDINGS

BASE METAL CORROSION *

BASE METAL CRACKING *

* PLEASE SEND PHOTOGRAPHIC EVIDENCE OF ANY DAMAGE FOUND AND RECORD THE DAMAGE

BASE METAL CRACK

LENGTH IN mm ORIENTATION (LONGITUDINAL OR CIRCUMFERENTIAL)

1)

2)

3)

4)

WAS THE BOGIE PIVOT PIN REPLACED: YES NO OR REPAIRED YES NO

BUSH CONDITION INFORMATION (TICK BOX AS NECESSARY)

BOGIE PIVOT PIN BUSH PART NO: 201272600, 201485609, 201485612 AND 201485613

NIL FINDINGS

SURFACE DAMAGE

BUSHES CHANGED: YES NO

SLIDING TUBE PIVOT PIN BUSH PART NO: 201270601, 201270782, 201270802, 201487600 AND 201487626

NIL FINDINGS

SURFACE DAMAGE

BUSHES CHANGED: YES NO

(REFER TO VSB A33/34−32−285)

(REFER TO VSB A33/34−32−285)

AIRCRAFT TSN: AIRCRAFT CSN:

BOGIE PIVOT PIN TSN: BOGIE PIVOT PIN CSN:

Figure A-UBBAA - Sheet 01

Inspection Reporting Sheet - MLG LH/RH

DATE: Dec 08/10 SERVICE BULLETIN No.: A330-32-3240

REVISION No.: 02 - Dec 02/11 Page: 2

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SERVICE BULLETIN

APPENDIX 01 - Inspection Reports

**CONF ALL

SLIDER

BOGIE

BEAM

SLIDER

0

DEGREES

90

DEGREES

180

DEGREES

270

DEGREES

360

DEGREES

2

1

4

3

4 3 2 1

PART NUMBER

LOCATION

START INSPECTION

AT DOG TO THE

LEFT OF PART PIN FLANGE

KEY

CHROMIUM DAMAGE

CORROSION

BASE METAL CRACKS

THIS IS AN EXAMPLE OF HOW TO RECORD

DAMAGE ON THE BOGIE PIVOT PIN

NUMBER LOCATION

G_SB_323240_7_BCAA_01_00

Figure A-UBCAA - Sheet 01

Bogie Pivot Pin Example Damage Record Sheet

DATE: Dec 08/10 SERVICE BULLETIN No.: A330-32-3240

REVISION No.: 02 - Dec 02/11 Page: 3

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SERVICE BULLETIN

APPENDIX 01 - Inspection Reports

**CONF ALL

SLIDER

BOGIE

BEAM

SLIDER

0

DEGREES

90

DEGREES

180

DEGREES

270

DEGREES

360

DEGREES

2

1

4

3

4 3 2 1

PART NUMBER

LOCATION

START INSPECTION

AT DOG TO THE

LEFT OF PART PIN FLANGE

MLG BOGIE PIVOT PIN

NUMBER LOCATION

GRID SIZE :−

HORIZONTAL − 20,00mm (0.787in)

VERTICAL − 20,00mm (0.787in)

EXTERNAL

SURFACE

G_SB_323240_7_BDAA_01_00

Figure A-UBDAA - Sheet 01

Bogie Pivot Pin Damage Record Sheet - MLG

DATE: Dec 08/10 SERVICE BULLETIN No.: A330-32-3240

REVISION No.: 02 - Dec 02/11 Page: 4

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SERVICE BULLETIN

APPENDIX 02 - Elapsed Time Assumption

**CONF ALL

For detail concerning the elapsed time assumptions, refer to the Gantt chart shown below:

DATE: Dec 08/10 SERVICE BULLETIN No.: A330-32-3240

REVISION No.: 02 - Dec 02/11 Page: 1

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SERVICE BULLETIN

APPENDIX 02 - Elapsed Time Assumption

**CONF ALL

ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A330−32−3240

GET ACCESS

MH ET/S

TOTAL MANHOURS

SB ELAPSED TIME

11.00

7.00

STEPS

2.00 1.00

0 10

REMOVE THE MLG BOGIE 2.00 1.00

PREPARATION FOR 2.00 2.00

INSTALL THE MLG BOGIE 2.00 1.00

TEST 1.00 1.00

CLOSE−UP 2.00 1.00

MH

ET/S:

PER

MANHOURS

ELAPSED TIME PER STEP

NUMBER OF PERSONS

THIS CHART IS ONLY A PROPOSAL.

OPERATORS MAY DETERMINE THAT ANOTHER WAY

TO DO THE WORK IS MORE SUITABLE FOR THEM.

NOTES:

PER

2

2

1

2

1

2

:

:

SB ELAPSED TIME

(HOURS)

2 4 6 8 12

BEAM ASSEMBLY PIVOT

INSTALLATION

BEAM ASSEMBLY PIVOT

PIN (LH/RH)

PIN (LH/RH)

IF A VSB IS INVOLVED, THE ASSOCIATED MANHOURS

ARE NOT REFLECTED IN THIS GANTT CHART.

G_SB_323240_7_AAAA_01_00

Figure A-UAAAA - Sheet 01

Elapsed Time Assumption

DATE: Dec 08/10 SERVICE BULLETIN No.: A330-32-3240

REVISION No.: 02 - Dec 02/11 Page: 2

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SERVICE BULLETIN

REPORTING SHEET

TITLE: LANDING GEAR - MLG - REPEAT INSPECTION OF MLG BOGIE PIVOT

PIN

MODIFICATION No.: None

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: Dec 08/10 SERVICE BULLETIN No.: A330-32-3240

REVISION No.: 02 - Dec 02/11 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: Dec 08/10 SERVICE BULLETIN No.: A330-32-3240

REVISION No.: 02 - Dec 02/11 Page: 1

7

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