@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 - MAIN GEAR - INSPECTION OF SIDE STAY UPPER

CARDAN PIN AND NUT

MODIFICATION No.: None

This page transmits Revision No.01 of Service Bulletin No.A330-32-3269

ADDITIONAL WORK

**CONF ALL

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

REASON

Revision No. 01 issued to:

- revise the configurations to define CONF 001 for Basic Main Landing Gear (MLG), CONF 002 for

Growth MLG and CONF 003 for Enhanced MLG

- update the Reason paragraph

- update the Compliance.

CHANGES

FRONT MATTER

LANDING GEAR - MAIN GEAR -

INSPECTION OF SIDE STAY UPPER

CARDAN PIN AND NUT

CONFIGURATION UPDATED R

SUMMARY

REASON/DESCRIPTION/OPERATIONAL

CONSEQUENCES

REASON UPDATED R

MATERIAL PRICE INFORMATION MATERIAL PRICE INFORMATION TABLE

UPDATED

R

MATERIAL PRICE INFORMATION TABLE

UPDATED

R

MATERIAL PRICE INFORMATION TABLE ADDED N

EFFECTIVITY OPERATOR LIST UPDATED R

DATE: Feb 17/15 SERVICE BULLETIN No.: A330-32-3269

REVISION No.: 01 - Dec 03/15 Page: 1

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

REFERENCES / REPERCUSSIONS REFERENCES/REPERCUSSIONS TABLE

UPDATED

R

MANPOWER MANPOWER ADDED N

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 DEFINITION UPDATED

CONFIGURATION DESCRIPTION UPDATED

R

CONF 003 CONFIGURATION ADDED N

Material Effectivity MATERIAL EFFECTIVITY UPDATED

MATERIAL SET QUANTITY UPDATED

CONFIGURATION UPDATED

MATERIAL SET UPDATED

R

MATERIAL EFFECTIVITY DELETED FOR

APPLICABLE MSN

D

REASON

History HISTORY UPDATED R

Objective/Action OBJECTIVE/ACTION UPDATED R

Operational/Maintenance

Consequences

OPERATIONAL/MAINTENANCE CONSEQUENCES

UPDATED

R

DESCRIPTION DESCRIPTION UPDATED R

COMPLIANCE

Accomplishment Timescale ACCOMPLISHMENT TIMESCALE UPDATED R

MANPOWER MANPOWER UPDATED R

MANPOWER UPDATED R

MANPOWER ADDED N

REFERENCES REFERENCED DOCUMENTATION UPDATED R

REFERENCED DOCUMENTATION UPDATED R

REFERENCED DOCUMENTATION ADDED N

MATERIAL INFORMATION

MATERIAL - PRICE AND AVAILABILITY MATERIAL - PRICE AND AVAILABILITY UPDATED R

Procurement Addresses PROCUREMENT ADDRESSES PARAGRAPH

DELETED

D

Price and Availability PRICE AND AVAILABILITY PARAGRAPH

DELETED

D

LIST OF MATERIALS - OPERATOR

SUPPLIED

Consumable Materials

Consumable CMLB01 CONSUMABLE MATERIAL SET UPDATED

QUANTITY UPDATED

CONSUMABLE UPDATED

R

Equipment EQUIPMENT UPDATED R

Equipement BFEB01 PART MATERIAL SET DELETED D

Equipement BFEB02 PART MATERIAL SET DELETED D

DATE: Feb 17/15 SERVICE BULLETIN No.: A330-32-3269

REVISION No.: 01 - Dec 03/15 Page: 2

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@A330

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

ACCOMPLISHMENT INSTRUCTIONS

TASK 323269- 832-895-001-Inspection TASK SOLUTION UPDATED

NOTE UPDATED

R

Task associated data - 003 TASK ASSOCIATED DATA ADDED N

Subtask 323269-910-401-001 SUBTASK SOLUTION ADDED N

Subtask 323269-839-401-001 SUBTASK SOLUTION ADDED N

Subtask 323269-941-401-001 SUBTASK SOLUTION ADDED N

Subtask 323269-832-401-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

QUANTITY UPDATED

CONFIGURATION UPDATED

ITEM NUMBER UPDATED

PART NUMBER UPDATED

FIGURE REFERENCE UPDATED

PART NUMBER DESCRIPTION UPDATED

REFERENCES UPDATED

R

Subtask 323269-832-402-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

QUANTITY UPDATED

CONFIGURATION UPDATED

ITEM NUMBER UPDATED

PART NUMBER UPDATED

FIGURE REFERENCE UPDATED

PART NUMBER DESCRIPTION UPDATED

REFERENCES UPDATED

R

Subtask 323269-833-401-001 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

ITEM NUMBER UPDATED

PART NUMBER UPDATED

KEYWORD UPDATED

CONSUMABLE UPDATED

REFERENCED DOCUMENTATION UPDATED

CONFIGURATION UPDATED

FIGURE REFERENCE UPDATED

PART NUMBER DESCRIPTION UPDATED

FIN UPDATED

NOTE UPDATED

MATERIAL LIST UPDATED

REFERENCES UPDATED

R

DATE: Feb 17/15 SERVICE BULLETIN No.: A330-32-3269

REVISION No.: 01 - Dec 03/15 Page: 3

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Subtask 323269-833-402-001 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

ITEM NUMBER UPDATED

PART NUMBER UPDATED

KEYWORD UPDATED

CONSUMABLE UPDATED

REFERENCED DOCUMENTATION UPDATED

CONFIGURATION UPDATED

FIGURE REFERENCE UPDATED

PART NUMBER DESCRIPTION UPDATED

FIN UPDATED

NOTE UPDATED

MATERIAL LIST UPDATED

REFERENCES UPDATED

R

Subtask 323269-410-401-001 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

ITEM NUMBER UPDATED

PART NUMBER UPDATED

KEYWORD UPDATED

CONSUMABLE UPDATED

REFERENCED DOCUMENTATION UPDATED

PART NUMBER DESCRIPTION UPDATED

CONFIGURATION UPDATED

FIGURE REFERENCE UPDATED

MATERIAL LIST UPDATED

REFERENCES UPDATED

R

Subtask 323269-410-402-001 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

ITEM NUMBER UPDATED

PART NUMBER UPDATED

KEYWORD UPDATED

CONSUMABLE UPDATED

REFERENCED DOCUMENTATION UPDATED

PART NUMBER DESCRIPTION UPDATED

CONFIGURATION UPDATED

FIGURE REFERENCE UPDATED

MATERIAL LIST UPDATED

REFERENCES UPDATED

R

Subtask 323269-832-401-003 SUBTASK SOLUTION ADDED N

Subtask 323269-832-402-003 SUBTASK SOLUTION ADDED N

Subtask 323269-833-401-003 SUBTASK SOLUTION ADDED N

Subtask 323269-833-402-003 SUBTASK SOLUTION ADDED N

Subtask 323269-410-401-003 SUBTASK SOLUTION ADDED N

Subtask 323269-410-402-003 SUBTASK SOLUTION ADDED N

Subtask 323269-832-401-002 SUBTASK SOLUTION DELETED FOR

APPLICABLE MSN

D

Subtask 323269-832-402-002 SUBTASK SOLUTION DELETED FOR

APPLICABLE MSN

D

Subtask 323269-833-401-002 SUBTASK SOLUTION DELETED FOR

APPLICABLE MSN

D

DATE: Feb 17/15 SERVICE BULLETIN No.: A330-32-3269

REVISION No.: 01 - Dec 03/15 Page: 4

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Subtask 323269-833-402-002 SUBTASK SOLUTION DELETED FOR

APPLICABLE MSN

D

Subtask 323269-410-401-002 SUBTASK SOLUTION DELETED FOR

APPLICABLE MSN

D

Subtask 323269-410-402-002 SUBTASK SOLUTION DELETED FOR

APPLICABLE MSN

D

Subtask 323269-832-401-002 SUBTASK SOLUTION ADDED N

Subtask 323269-832-402-002 SUBTASK SOLUTION ADDED N

Subtask 323269-833-401-002 SUBTASK SOLUTION ADDED N

Subtask 323269-833-402-002 SUBTASK SOLUTION ADDED N

Subtask 323269-410-401-002 SUBTASK SOLUTION ADDED N

Subtask 323269-410-402-002 SUBTASK SOLUTION ADDED N

Subtask 323269-700-401-001 SUBTASK SOLUTION UPDATED

LOCATION UPDATED

R

Subtask 323269-700-401-001 SUBTASK SOLUTION UPDATED

LOCATION UPDATED

R

Subtask 323269-700-401-001 SUBTASK SOLUTION ADDED N

Subtask 323269-942-401-001 SUBTASK SOLUTION ADDED N

Fig. A-UBAAA FIGURE SOLUTION UPDATED

CONFIGURATION UPDATED

R

Fig. A-UBAAA Sheet 01 SHEET UPDATED R

Fig. A-UBAAA Sheet 02 SHEET UPDATED R

Fig. A-UBAAA Sheet 03 SHEET DELETED D

Fig. A-UBAAB FIGURE SOLUTION DELETED FOR APPLICABLE

MSN

D

Fig. A-UBBAA FIGURE SOLUTION UPDATED

CONFIGURATION UPDATED

R

Fig. A-UBBAA Sheet 01 SHEET UPDATED R

Fig. A-UBBAB FIGURE SOLUTION UPDATED

CONFIGURATION UPDATED

R

Fig. A-UBBAB Sheet 01 SHEET UPDATED R

FILLING INSTRUCTIONS

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

Replace the complete document.

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

HISTORY OF PREVIOUS REVISIONS

No previous revision

REVISION SEQUENCE

ORIGINAL: Feb 17/15

REVISION No. : 01 - Dec 03/15

DATE: Feb 17/15 SERVICE BULLETIN No.: A330-32-3269

REVISION No.: 01 - Dec 03/15 Page: 5

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

This Page Intentionally Left Blank

DATE: Feb 17/15 SERVICE BULLETIN No.: A330-32-3269

REVISION No.: 01 - Dec 03/15 Page: 6

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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 - MAIN GEAR - INSPECTION OF SIDE STAY UPPER

CARDAN PIN AND NUT

**CONF ALL

MODIFICATIONS

None

REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES

Inspection of an A330 aircraft fitted with Basic Main Landing Gear (MLG) has shown that the MLG

Side Stay Upper Cardan Pin (UCP) can migrate from its original position and that the UCP nut and

retainer can become detached. The reported MLG sidestay upper cardan pin migration event had been

caused by corrosion, due to lack of jointing compound and inadequate sealant application during MLG

installation. Therefore, this issue affects any MLG that has had a UCP replacement or re-installation,

since Entry Into Service (EIS), irrespective of MLG overhaul.

The loss of the side stay UCP locking function can lead to a complete migration of the UCP and

disconnection of the MLG side stay upper arm from the aircraft structure.

Mandatory All Operators Telex (AOT) A32L003-14 requires all operators to do a gap check of all

applicable UCPs.

As a follow up to the AOT an inspection is considered necessary to capture any corrosion that may be

present on the UCP and associated nut threads. Corrosion may not have been picked up as part of the

AOT checks but may contribute to migration of the UCP. The aim of this inspection Service Bulletin is

to request operators to:

- do a Detailed Inspection (DET) of the Side Stay Upper Cardan Pin Locking Assembly

- check for corrosion, pitting and/or damage to the threads of the UCP and UCP Nut.

- if corrosion, pitting and/or damage is found on the UCP or UCP Nut, the damaged parts are to be

replaced before further flight.

DATE: Feb 17/15 SERVICE BULLETIN No.: A330-32-3269

REVISION No.: 01 - Dec 03/15 Page: 1

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@A330

SERVICE BULLETIN

SUMMARY

Accomplishment of this Inspection Service Bulletin (ISB) will help in the early detection of corrosion

and/or damage to the UCP and nut retainer assembly. This minimizes the possibility of a potential

unsafe condition arising from the disconnection of the upper side stay arm from the aircraft structure.

In addition, to prevent any improper re-installation of an upper cardan pin on a MLG, Airbus amended

the applicable Aircraft Maintenance Manual (AMM) on 01 October 2014.

GENERAL EVALUATION

EVALUATION TABLE

COMPLIANCE MANDATORY (1) CANCELS INSPECTION SB NO

POTENTIAL AD YES A/C OPERATION AFFECTED NO

RELIABILITY AFFECTED NO PAX COMFORT AFFECTED NO

COST SAVING NO ETOPS AFFECTED NO

STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED NO

AIRCRAFT JACKING YES

NOTE (1): Service Bulletin must be accomplished.

MATERIAL PRICE INFORMATION

**CONF 001

No Material

**CONF 002

No Material

**CONF 003

No Material

EFFECTIVITY

**CONF ALL

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

15T 18P 34Z 38W 43P 87Z AAR AAW ABD ACA ACI AEA AFL

AFR AIB ALK ARA ARG ASY AVA AZA AZU BEC BEL BER BGH

CAL CBJ CCA CEB CES CHH CPA CRK CRL CSA CSC CSN DAH

DAL DGA DLH EDW EIN ETD EVA EVE EZX FAF FIN FJI FWI

GAP GFA GIA GRL HAL HDA HFY HVN IAW IBE JAI KAC KAL

KLM LAA LNI MAS MAU MEA MLM MNB MON MSR NMB OBS OHY

OMA ONE PAL QAF QFA QTR RJA RSF RWD RZO SAA SAF SAI

SAS SEY SIA SKY SVA SWR SXD TAE TAM TAP TAR TAX TBA

TCX THA THY TNA TOW TPA TSC UAE UAF USA VIR VKG VOZ

WRC XAX XLF

CONCURRENT REQUIREMENTS

None

DATE: Feb 17/15 SERVICE BULLETIN No.: A330-32-3269

REVISION No.: 01 - Dec 03/15 Page: 2

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@A330

SERVICE BULLETIN

SUMMARY

REFERENCES / REPERCUSSIONS

TFU None

OEB None

AOT A32L003-14

SIL None

ISI 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 323269-832-895-001: Inspection

TOTAL MANHOURS 23.00

ELAPSED TIME (HOURS) 13.00

**CONF 002

Task 323269-832-895-001: Inspection

TOTAL MANHOURS 23.00

ELAPSED TIME (HOURS) 13.00

**CONF 003

Task 323269-832-895-001: Inspection

TOTAL MANHOURS 23.00

ELAPSED TIME (HOURS) 13.00

APPENDICES

**CONF ALL

Appendix 01 - Elapsed Time Assumptions

DATE: Feb 17/15 SERVICE BULLETIN No.: A330-32-3269

REVISION No.: 01 - Dec 03/15 Page: 3

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@A330

SERVICE BULLETIN

SUMMARY

**CONF ALL

NOTE:

AREA OF INSPECTION

SIDE STAY

UPPER CARDAN PIN

LOCKING ASSEMBLY

A

A

SIDE STAY

LH SHOWN

RH SIMILAR

5012GM

(5013GM)

G_SB_323269_7_SAAA_01_01

Figure A-USAAA - Sheet 01

DATE: Feb 17/15 SERVICE BULLETIN No.: A330-32-3269

REVISION No.: 01 - Dec 03/15 Page: 4

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@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 - MAIN GEAR - INSPECTION OF SIDE STAY UPPER

CARDAN PIN AND NUT

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

(1) Models

330-202 330-203 330-223 330-223F 330-243 330-243F 330-301 330-302

330-303 330-323 330-342 330-343

(2) Effectivity by MSN

0030 0037 0045 0054-0055 0070 0086 0181 0195 0211 0222-0223 0226 0229-0230

0232 0238 0240 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 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

DATE: Feb 17/15 SERVICE BULLETIN No.: A330-32-3269

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@A330

SERVICE BULLETIN

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 0994-0998 1000-1004 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 1274-1616

1618-1638 1640-1651 1653-1654 1656-1660 1662-1663 1665-1681 1684-1701

1703-1704 1706 1708-1716 1718-1739 1741-1742 1745 1754 1760

(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

15T 1676

18P 1321

34Z 1483 1491 1542 1554 1592 1635 1651

38W 0401

43P 1053

87Z 0535

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

1435 1464 1518

AAW 1043 1472 1535

ABD 0343

ACA 0277 0279 0284 0344 0400 0408 0412 0419

ACI 0507 0510

AEA 0461 0505 0526 0551 0597 0670 0733 0745 0749 0814 0931 0950

0992 1097 1574

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

AIB 0345 0437 0871 1712

ALK 0303 0306 0311 0313 0404 0456 0627 1564 1583 1604 1650 1669

1687 1689

ARA 0891 0927

ARG 0290 0300 0358 0364 1605 1623 1737

ASY 0747 0892 0951 0969 1036 1183

DATE: Feb 17/15 SERVICE BULLETIN No.: A330-32-3269

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@A330

SERVICE BULLETIN

OPERATOR MSN

AVA 0967 1009 1016 1073 1208 1224 1279 1342 1400 1492 1508

AZA 0272 0339 0825 0831 1123 1135 1218 1225 1252 1283 1308 1313

1327 1354

AZU 0365 0372 0462 0494 0527 0529 0532

BEC 0863

BEL 0030 0037 0045 0229 0249 0324

BER 0288 0322 0403 0432 0444 0454 0469 0476 0493 0665 0739 0822

0828 0911

BGH 0255

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

0805 0823 0838 0861 0920 1177 1272 1278 1346 1367 1450 1539

CBJ 1020 1052

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 1383 1396

1413 1434 1444 1459 1471 1493 1509 1525 1538 1541 1563 1570

1587 1658 1673 1685 1695

CEB 1420 1445 1495 1527 1552 1602

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 1375 1402 1421 1429 1440 1461 1468 1479

1484 1500 1520 1537 1547 1551 1569 1588 1595 1603 1632

CHH 0875 0881 0906 0919 0982 1159 1168 1178 1190 1255 1325 1369

1438 1532 1558 1573 1591 1614 1634 1656 1663 1677 1686 1703

CPA 0386 0389 0393 0418 0420 0421 0423 0439 0539 0548 0565 0679

0776 0850 0855 0895 0915 0959 1163 1196 1222 1239 1285 1317

1343 1349 1362 1366 1387 1409 1436 1443 1503 1523 1545 1557

1567 1598 1618 1621

CRK 1031 1034 1039 1042 1051 1054 1059 1062 1115 1175 1277 1286

1320 1322 1358 1384 1398 1668

CRL 0285 0320 1359 1376

CSA 0425

CSC 1082 1138 1241 1397 1432 1528 1579 1662

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

1392 1425 1430 1494 1519 1536 1575 1593 1625 1636 1645 1699

1714 1760

DAH 0644 0647 0650 0653 0667 1613 1630 1649

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 1627 1628 1637 1679

1701 1716 1720 1721

DGA 0240

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

0913 0922 0989 1292 1305 1314 1497

EDW 0291 1193 1711

EIN 0269 0330 0397 0841 0847 0985 1025 1106 1742

DATE: Feb 17/15 SERVICE BULLETIN No.: A330-32-3269

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SERVICE BULLETIN

OPERATOR MSN

ETD 0658 0688 0717 0724 0729 0730 0737 0788 0807 0809 0824 0832

0852 0854 0868 0885 0975 0991 1032 1070 1071 1081 1167 1205

1226 1245 1414 1486 1521 1524

EVA 0555 0573 0587 0634 0655 0661 0678 0693 0755 1254 1268 1274

1684 1690

EVE 0833 1691

EZX 0261

FAF 1735

FIN 0994 1007 1013 1023 1067 1078 1088 1173

FJI 1394 1416 1465 1692

FWI 0253 0758 0965 1021 1265 1727

GAP 1463

GFA 0276 0281 0286 0287 0334 0340

GIA 0988 1028 1184 1214 1261 1288 1364 1410 1446 1474 1548 1560

1577 1585 1654 1671 1698 1709 1723 1733

GRL 0230

HAL 1104 1114 1171 1217 1259 1295 1302 1310 1316 1389 1399 1404

1422 1469 1488 1496 1511 1530 1565 1606 1615 1672 1732

HDA 0405 0479 0512 0581 0669 0673 1457

HFY 0211 0262 1008

HVN 0275 0294 0299 0366 0943 0946 0962 1019 1256 1266

IAW 1339

IBE 1377 1385 1405 1426 1437 1490 1507 1515 1694 1700 1710 1719

1728 1736

JAI 0888 0923 0947 0956 1351 1361 1370 1391

KAC 1626 1643 1653 1678 1681

KAL 0222 0226 0256 0258 0267 0338 0350 0351 0368 0428 0484 0490

0550 1133 1155 1200 1203 1393 1556 1576 1590 1611 1638 1647

KLM 0682 0686 0703 0738 0770 0801 0811 0819 0834 0900 0925 1161

1287 1294 1300 1381 1580

LAA 1412 1424 1505 1543

LNI 1675 1680 1693

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

1337 1347 1388 1395 1431 1470 1489

MAU 0883 1057

MEA 0926 0984 0995 0998 1725

MLM 0451

MNB 1332

MON 0265

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

NMB 1451 1466

OBS 0802

OHY 0353 0362 0625 0632

OMA 1038 1044 1049 1063 1093 1120 1227 1572 1582 1599

ONE 1506 1540 1586 1608 1657

PAL 1449 1456 1460 1467 1475 1482 1504 1510 1531 1546 1553 1559

1566 1568

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SERVICE BULLETIN

OPERATOR MSN

QAF 0487 0605

QFA 0506 0508 0513 0522 0553 0558 0564 0574 0593 0595 0603 0695

0705 0712 0842 0853 0887 0898 0940 0945 0976 1061 1094 1169

1174 1198 1251 1258 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 1350 1386 1406 1578 1584 1594 1688

1708

RJA 0979 1002

RSF 0980 0996 1235 1379 1478 1516

RWD 1741 1754

RZO 0970

SAA 1191 1210 1223 1236 1249 1271 1745

SAF 1667

SAI 0055 0070 0086

SAS 0496 0497 0515 0568 1660 1665 1697 1715

SEY 0751

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

1107 1124 1132 1149 1156 1382 1401 1427 1447 1453 1477 1485

1517 1544 1562 1597 1609 1633 1648 1666

SKY 1607 1624

SVA 1108 1127 1137 1141 1147 1153 1189 1192 1454 1462 1473 1513

1724 1726 1729 1731 1734 1738 1739

SWR 1000 1018 1026 1029 1084 1089 1101 1145 1181 1188 1276 1290

1355 1403

SXD 0530

TAE 0348

TAM 0232 0238 0247 0259 0361 0466 0472 0700 0968 1112

TAP 0181 0195 0223 0305 0308 0312 0317 0477 0486 0877 0899 0904

0914 0934

TAR 1631 1641

TAX 1619

TBA 1730

TCX 0254 0266 0301 0398 0948

THA 0346 0990 1003 1035 1037 1060 1074 1086 1090 1263 1269 1289

1338 1348 1374 1408

THY 0463 0504 0697 0704 0742 0754 0774 0869 0874 0876 0882 0901

0932 0939 0949 0961 0977 1004 1092 1118 1150 1160 1170 1172

1204 1212 1213 1221 1228 1240 1298 1307 1311 1344 1418 1442

1458 1476 1487 1499 1501 1514 1522 1529 1550 1571 1616 1620

1622 1629 1640 1642 1644 1696 1704 1706 1713 1718 1722

TNA 1146 1157 1357 1378

TOW 1033 1046 1248 1275 1312 1334 1363 1390 1419 1439 1498 1555

1601 1610

TPA 1368 1380 1428 1448 1534

TSC 0250 0271 0369 0407 0427 0480 0795 0966 0971

UAE 0248 0251 0283 0293 0295 0314 0316 0326 0328 0382 0384 0392

0396 0409 0452 0455 0491 0509 0518 0525 0536

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SERVICE BULLETIN

OPERATOR MSN

UAF 1080 1186 1250

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

1069 1076 1095 1100 1415 1417 1441 1455 1480 1502 1512 1526

VIR 1195 1201 1206 1215 1231 1296 1315 1329 1341 1352

VKG 0309 0349 0356 0357

VOZ 1293 1306 1319 1407 1452 1561

WRC 0296

XAX 0054 0654 0662 0692 0716 0741 0786 0952 0974 1048 1066 1075

1126 1131 1165 1411 1423 1433 1481 1533 1549 1581 1589 1596

1600 1612 1646 1659 1670 1674

XLF 0501 0635 1360

(4) Configuration by MSN

MSN CONFIGURATION

0030 0037 0045 0054 0055 0070 0086 001

0181 0195 0211 0222 0223 0226 0229 0230 0232 0238 0240

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

002

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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 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 1354

1355 1356 1357 1358 1359 1360 1361 1362 1363 1364 1365

1366 1367 1368 1369 1370 1371 1372 1373 1374 1375 1376

1377 1378 1379 1380 1381 1382 1383 1384 1385 1386 1387

003

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SERVICE BULLETIN

MSN CONFIGURATION

1388 1389 1390 1391 1392 1393 1394 1395 1396 1397 1398

1399 1400 1401 1402 1403 1404 1405 1406 1407 1408 1409

1410 1411 1412 1413 1414 1415 1416 1417 1418 1419 1420

1421 1422 1423 1424 1425 1426 1427 1428 1429 1430 1431

1432 1433 1434 1435 1436 1437 1438 1439 1440 1441 1442

1443 1444 1445 1446 1447 1448 1449 1450 1451 1452 1453

1454 1455 1456 1457 1458 1459 1460 1461 1462 1463 1464

1465 1466 1467 1468 1469 1470 1471 1472 1473 1474 1475

1476 1477 1478 1479 1480 1481 1482 1483 1484 1485 1486

1487 1488 1489 1490 1491 1492 1493 1494 1495 1496 1497

1498 1499 1500 1501 1502 1503 1504 1505 1506 1507 1508

1509 1510 1511 1512 1513 1514 1515 1516 1517 1518 1519

1520 1521 1522 1523 1524 1525 1526 1527 1528 1529 1530

1531 1532 1533 1534 1535 1536 1537 1538 1539 1540 1541

1542 1543 1544 1545 1546 1547 1548 1549 1550 1551 1552

1553 1554 1555 1556 1557 1558 1559 1560 1561 1562 1563

1564 1565 1566 1567 1568 1569 1570 1571 1572 1573 1574

1575 1576 1577 1578 1579 1580 1581 1582 1583 1584 1585

1586 1587 1588 1589 1590 1591 1592 1593 1594 1595 1596

1597 1598 1599 1600 1601 1602 1603 1604 1605 1606 1607

1608 1609 1610 1611 1612 1613 1614 1615 1616 1618 1619

1620 1621 1622 1623 1624 1625 1626 1627 1628 1629 1630

1631 1632 1633 1634 1635 1636 1637 1638 1640 1641 1642

1643 1644 1645 1646 1647 1648 1649 1650 1651 1653 1654

1656 1657 1658 1659 1660 1662 1663 1665 1666 1667 1668

1669 1670 1671 1672 1673 1674 1675 1676 1677 1678 1679

1680 1681 1684 1685 1686 1687 1688 1689 1690 1691 1692

1693 1694 1695 1696 1697 1698 1699 1700 1701 1703 1704

1706 1708 1709 1710 1711 1712 1713 1714 1715 1716 1718

1719 1720 1721 1722 1723 1724 1725 1726 1727 1728 1729

1730 1731 1732 1733 1734 1735 1736 1737 1738 1739 1741

1742 1745 1754 1760

003

(5) Configuration definition

**CONF 001

Config. 001 is valid for all the aircraft given in the effectivity of this Service Bulletin that

have not embodied Modification No. 54500H15561 and not embodied Modification No.

43029H13154.

NOTE: Aircraft that have accomplished Service Bulletin No. A330-32-3212 are to

be considered as Config 003.

**CONF 002

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

have not embodied Modification No. 54500H15561 and have embodied Modification No.

43029H13154.

NOTE: Aircraft that have accomplished Service Bulletin No. A330-32-3212 are to

be considered as Config 003.

DATE: Feb 17/15 SERVICE BULLETIN No.: A330-32-3269

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SERVICE BULLETIN

**CONF 003

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

have embodied Modification No. 54500H15561 and have embodied Modification No.

43029H13154 or have accomplished Service Bulletin No. A330-32-3212.

(6) Material Effectivity

MATERIAL QTY PER A/C SEE NOTES

Consumable CMLB01 1

B. CONCURRENT REQUIREMENTS

None

C. REASON

(1) History

Inspection of an A330 aircraft fitted with Basic Main Landing Gear (MLG) has shown that

the MLG Side Stay Upper Cardan Pin (UCP) can migrate from its original position

and that the UCP nut and retainer can become detached. The reported MLG sidestay

upper cardan pin migration event had been caused by corrosion, due to lack of jointing

compound and inadequate sealant application during MLG installation. Therefore, this

issue affects any MLG that has had a UCP replacement or re-installation, since Entry

Into Service (EIS), irrespective of MLG overhaul.

The loss of the side stay UCP locking function can lead to a complete migration of the

UCP and disconnection of the MLG side stay upper arm from the aircraft structure.

Mandatory All Operators Telex (AOT) A32L003-14 requires all operators to do a gap

check of all applicable UCPs.

(2) Objective/Action

As a follow up to the AOT an inspection is considered necessary to capture any

corrosion that may be present on the UCP and associated nut threads. Corrosion may

not have been picked up as part of the AOT checks but may contribute to migration of

the UCP. The aim of this inspection Service Bulletin is to request operators to:

- do a Detailed Inspection (DET) of the Side Stay Upper Cardan Pin Locking

Assembly

- check for corrosion, pitting and/or damage to the threads of the UCP and UCP Nut.

- if corrosion, pitting and/or damage is found on the UCP or UCP Nut, the damaged

parts are to be replaced before further flight.

(3) Advantages

Accomplishment of this Inspection Service Bulletin (ISB) will help in the early detection

of corrosion and/or damage to the UCP and nut retainer assembly. This minimizes the

possibility of a potential unsafe condition arising from the disconnection of the upper side

stay arm from the aircraft structure.

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SERVICE BULLETIN

(4) Operational/Maintenance Consequences

In addition, to prevent any improper re-installation of an upper cardan pin on a MLG,

Airbus amended the applicable Aircraft Maintenance Manual (AMM) on 01 October

2014.

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

**CONF 001

Task 323269-832-895-001: Inspection

(1) Inspect the Upper Cardan Pin and Nut on the LH MLG

(2) Inspect the Upper Cardan Pin and Nut on the RH MLG

(3) Replace the Upper Cardan Pin on the LH MLG

(4) Replace the Upper Cardan Pin on the RH MLG

(5) Install the Upper Cardan Pin Nut on the LH MLG

(6) Install the Upper Cardan Pin Nut at the RH MLG

**CONF 002

Task 323269-832-895-001: Inspection

(1) Inspect the Upper Cardan Pin and Nut on the LH MLG

(2) Inspect the Upper Cardan Pin and Nut on the RH MLG

(3) Replace the Upper Cardan Pin on the LH MLG

(4) Replace the Upper Cardan Pin on the RH MLG

(5) Install the Upper Cardan Pin Nut on the LH MLG

(6) Install the Upper Cardan Pin Nut on the RH MLG

**CONF 003

Task 323269-832-895-001: Inspection

(1) Inspect the Upper Cardan Pin and Nut on the LH MLG

(2) Inspect the Upper Cardan Pin and Nut on the RH MLG

(3) Replace the Upper Cardan Pin on the LH MLG

(4) Replace the Upper Cardan Pin on the RH MLG

DATE: Feb 17/15 SERVICE BULLETIN No.: A330-32-3269

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@A330

SERVICE BULLETIN

(5) Install the Upper Cardan Pin Nut on the LH MLG

(6) Install the Upper Cardan Pin Nut on the RH MLG

**CONF ALL

E. COMPLIANCE

(1) Classification

MANDATORY: Service Bulletin must be accomplished.

(2) Accomplishment Timescale

Table 01: Detailed Inspection (DET) of the Upper Cardan Pin (UCP) and nut retainer assembly

CONDITION ACTION COMPLIANCE TIME

THRESHOLD GRACE PERIOD

REPETITIVE

INTERVAL

If an Upper Cardan

Pin on either LH or

RH MLG has been

replaced or reinstalled since

Entry Into Service

(EIS) at the time of

issue of this

Service Bulletin

AND if this action

was accomplished

using the

applicable Airbus

AMM at a revision

dated prior to 01

October 2014.

Inspect the upper

cardan pin and nut

8 years from

installation of the

MLG UCP

or

12 months from

issue of this

Service Bulletin

Whichever occurs

later

None

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

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

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

F. APPROVAL

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

Organisation Approval No. EASA.21J.031.

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

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

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

before incorporation of the Service Bulletin.

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@A330

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 323269-832-895-001: Inspection

Get Access 1.00

On Aircraft

Inspect the Upper Cardan Pin and Nut on the LH MLG 4.00

Inspect the Upper Cardan Pin and Nut on the RH MLG 4.00

Replace the Upper Cardan Pin on the LH MLG 4.00

Replace the Upper Cardan Pin on the RH MLG 4.00

Install the Upper Cardan Pin Nut on the LH MLG 2.00

Install the Upper Cardan Pin Nut at the RH MLG 2.00

Tests 1.00

Close-Up 1.00

TOTAL MANHOURS 23.00

ELAPSED TIME (HOURS) 13.00

NOTE: The minimum manhours necessary to accomplish this Service Bulletin are

those for the Inspection. Depending on the inspection result, additional

manhours can apply.

NOTE: For an explanation of the manhours and elapsed time, refer to the Gantt

Chart, Fig. A-UAAAA given in Appendix 01 - Elapsed Time Assumptions .

**CONF 002

Task 323269-832-895-001: Inspection

Get Access 1.00

On Aircraft

Inspect the Upper Cardan Pin and Nut on the LH MLG 4.00

Inspect the Upper Cardan Pin and Nut on the RH MLG 4.00

Replace the Upper Cardan Pin on the LH MLG 4.00

Replace the Upper Cardan Pin on the RH MLG 4.00

Install the Upper Cardan Pin Nut on the LH MLG 2.00

Install the Upper Cardan Pin Nut on the RH MLG 2.00

Tests 1.00

Close-Up 1.00

TOTAL MANHOURS 23.00

ELAPSED TIME (HOURS) 13.00

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SERVICE BULLETIN

NOTE: The minimum manhours necessary to accomplish this Service Bulletin are

those for the Inspection. Depending on the inspection result, additional

manhours can apply.

NOTE: For an explanation of the manhours and elapsed time, refer to the Gantt

Chart, Fig. A-UAAAA given in Appendix 01 - Elapsed Time Assumptions .

**CONF 003

Task 323269-832-895-001: Inspection

Get Access 1.00

On Aircraft

Inspect the Upper Cardan Pin and Nut on the LH MLG 4.00

Inspect the Upper Cardan Pin and Nut on the RH MLG 4.00

Replace the Upper Cardan Pin on the LH MLG 4.00

Replace the Upper Cardan Pin on the RH MLG 4.00

Install the Upper Cardan Pin Nut on the LH MLG 2.00

Install the Upper Cardan Pin Nut on the RH MLG 2.00

Tests 1.00

Close-Up 1.00

TOTAL MANHOURS 23.00

ELAPSED TIME (HOURS) 13.00

NOTE: The minimum manhours necessary to accomplish this Service Bulletin are

those for the Inspection. Depending on the inspection result, additional

manhours can apply.

NOTE: For an explanation of the manhours and elapsed time, refer to the Gantt

Chart, Fig. A-UAAAA given in Appendix 01 - Elapsed Time Assumptions .

**CONF ALL

H. WEIGHT AND BALANCE

Not Changed

I. ELECTRICAL LOAD DATA

Not Changed

J. REFERENCES

**CONF 001

Aircraft Maintenance Manual (AMM) 06-20-00 07-11-00 12-34-24

20-21-11 32-00-00 32-11-16

32-31-00 32-33-00

Consumable Material List (CML)

Component Maintenance Manual Manufacturer

(CMMm)

32-11-91

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SERVICE BULLETIN

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

**CONF 002

Aircraft Maintenance Manual (AMM) 06-20-00 07-11-00 12-34-24

20-21-11 32-00-00 32-11-16

32-31-00 32-33-00

Consumable Material List (CML)

Component Maintenance Manual Manufacturer

(CMMm)

32-12-07

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

**CONF 003

Aircraft Maintenance Manual (AMM) 06-20-00 07-11-00 12-34-24

20-21-11 32-00-00 32-11-16

32-31-00 32-33-00

Consumable Material List (CML)

Component Maintenance Manual Manufacturer

(CMMm)

32-12-66

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

**CONF ALL

K. PUBLICATION AFFECTED

None

L. INTERCHANGEABILITY/MIXABILITY

Not Applicable

M. SPARES

None

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SERVICE BULLETIN

2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

No Material Set

B. INDUSTRY SUPPORT INFORMATION

AIRBUS will not provide industry support for accomplishment of this Service Bulletin.

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 Materials

listed in the subsequent listed AMM Tasks:

- AMM Task 32-11-16-400-801.

Consumable CMLB01

ITEM DESCRIPTION REFERENCE TO CML

MAT. No.

QTY PER A/C SEE

NOTES

Polysulfide Sealant - General

Purpose Interfay

06AAC5 As required

Non Hardening Jointing Putty-High

Temp

06LDG6 As required

Non Aqueous Cleaner - General 08BAA9 As required

Textile - Lint Free Cotton 14SBA1 As required

(2) Components

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

Components listed in the subsequent listed AMM Tasks:

- AMM Task 32-11-16-400-801.

(3) Equipment

None

E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

None

DATE: Feb 17/15 SERVICE BULLETIN No.: A330-32-3269

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SERVICE BULLETIN

F. TOOLING

(1) Tooling - Price and Availability

None

(2) Tools

To accomplish this Service Bulletin it will be necessary to use the Standard Tools listed

in the subsequent listed AMM Tasks:

- AMM Task 32-11-16-000-801

- AMM Task 32-11-16-400-801.

(3) Special Tools

None

DATE: Feb 17/15 SERVICE BULLETIN No.: A330-32-3269

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SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS

Task 323269-832-895-001 - Inspection

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

INCLUDED IN THE REFERENCED PROCEDURES.

WARNING: MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE

IN POSITION BEFORE YOU START A TASK ON OR NEAR:

- THE FLIGHT CONTROLS

- THE FLIGHT CONTROL SURFACES

- THE LANDING GEAR AND THE RELATED DOORS

- COMPONENTS THAT MOVE.

MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS.

CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP

ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY

AND MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENANCE

WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING,

COMPONENTS AND THE WORK AREA AS CLEAN AS POSSIBLE. TO DO

THIS:

- PUT PROTECTION, SUCH AS PLASTIC SHEETING, CLOTHS, ETC; AS

NECESSARY ON WIRING AND COMPONENTS.

- REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND

OTHER CONTAMINATION.

THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION

AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION.

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

NOTE: The accomplishment instructions of this Service Bulletin include procedures given

in other documents or in other sections of the Service Bulletin. When the words

’refer to’ are used and the operator has a procedure accepted by the local authority

he belongs to, the accepted alternative procedure can be used. When the words ’in

accordance with’ are used then the given procedure must be followed.

NOTE: The access and close-up instructions, not comprising return to service tests, in this

Service Bulletin do not constitute or affect the technical intent of the Service

Bulletin. Operators can therefore, as deemed necessary, omit or add access and/or

close-up steps to add flexibility to their maintenance operations as long as the

technical intent of the Service Bulletin is met within the set parameters.

NOTE: Manual titles given in the accomplishment instructions are referred to by acronyms.

Refer to paragraph 1.J., References, for the definition of acronyms.

NOTE: This Service Bulletin is classified mandatory or expected to be classified mandatory

DATE: Feb 17/15 SERVICE BULLETIN No.: A330-32-3269

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by an Airworthiness Directive (AD). The paragraphs 3.C. and 3.D. in these

accomplishment instructions are Required for Compliance (RC) and must be done

to comply with the AD. Other paragraphs are recommended and may be deviated

from, done as part of other actions or done with accepted methods different from

those given in the Service Bulletin, as long as the RC paragraphs can be done and

the aircraft can be put back into a serviceable condition.

NOTE: The purpose of flow charts is to supplement the information given in the Procedure

and Compliance paragraphs and not to serve as the primary source for tasks or

compliance times given in this Service Bulletin.

NOTE: Discarded parts must be managed at the operator’s discretion.

Task Associated Data

**CONF 001

Zone

731 741

Modified FIN

5012GM 5013GM

Manpower

TOTAL MANHOURS 23.00

ELAPSED TIME (HOURS) 13.00

**CONF 002

Zone

731 741

Modified FIN

5012GM 5013GM

Manpower

TOTAL MANHOURS 23.00

ELAPSED TIME (HOURS) 13.00

**CONF 003

Zone

731 741

Modified FIN

5012GM 5013GM

Manpower

TOTAL MANHOURS 23.00

ELAPSED TIME (HOURS) 13.00

DATE: Feb 17/15 SERVICE BULLETIN No.: A330-32-3269

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**CONF ALL

A. GENERAL

**CONF 001

(1) Subtask 323269-910-401-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

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

Task 07-11-00-581-801

Task 20-21-11-911-801

Consumable Material List (CML)

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

Consumable Materials List (CML).

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

(c) To torque tighten the standard threaded fasteners, refer to AMM Task

20-21-11-911-801.

(d) Obey the maintenance jacking procedures, refer to AMM Task 07-11-00-581-801.

(e) Tag all the parts you must remove and retain to make the subsequent installation

easier.

(f) Put all the retained hardware in identified plastic bags and attach the bags to the

related unit.

(2) Subtask 323269-839-401-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF 002

(1) Subtask 323269-910-401-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

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

Task 07-11-00-581-801

Task 20-21-11-911-801

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References

Consumable Material List (CML)

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

Consumable Materials List (CML).

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

(c) To torque tighten the standard threaded fasteners, refer to AMM Task

20-21-11-911-801.

(d) Obey the maintenance jacking procedures, refer to AMM Task 07-11-00-581-801.

(e) Tag all the parts you must remove and retain to make the subsequent installation

easier.

(f) Put all the retained hardware in identified plastic bags and attach the bags to the

related unit.

(2) Subtask 323269-839-401-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF 003

(1) Subtask 323269-910-401-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

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

Task 07-11-00-581-801

Task 20-21-11-911-801

Consumable Material List (CML)

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

Consumable Materials List (CML).

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

(c) To torque tighten the standard threaded fasteners, refer to AMM Task

20-21-11-911-801.

(d) Obey the maintenance jacking procedures, refer to AMM Task 07-11-00-581-801.

(e) Tag all the parts you must remove and retain to make the subsequent installation

easier.

DATE: Feb 17/15 SERVICE BULLETIN No.: A330-32-3269

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SERVICE BULLETIN

(f) Put all the retained hardware in identified plastic bags and attach the bags to the

related unit.

(2) Subtask 323269-839-401-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF ALL

B. PREPARATION

**CONF 001

(1) Subtask 323269-941-401-001 - Job Set-up

Work Zones and Access Panels

Zone Access/Work location

731

741

Manpower Resources

Skills NON SPECIFIC

References

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

Task 12-34-24-860-802

Task 32-00-00-481-801

Task 32-00-00-481-802

NOTE: The items given in this note shall be considered as the basic Aircraft

configuration before you start a maintenance task:

- Aircraft on the ground resting on landing gear (the ground safety

locks and the wheel chocks are in position on the landing gear)

- Engine shut down, thrust reversers closed and locked

- Aircraft in clean configuration

- Parking brake applied

- Aircraft electrical network de-energized

- Hydraulic systems depressurized

- Access to the cockpit and cabin is available

- All circuit breakers are in closed position

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SERVICE BULLETIN

- All controls in NORM, AUTO or OFF position.

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

12-34-24-860-802.

(b) Do the installation of the Safety Devices on the Landing Gears, refer to AMM Task

32-00-00-481-801.

(c) Do the installation of the Safety Devices on the Landing Gear Doors, refer to AMM

Task 32-00-00-481-802.

(d) Lift the aircraft on jacks, refer to AMM Task 07-11-00-581-801.

**CONF 002

(1) Subtask 323269-941-401-001 - Job Set-up

Work Zones and Access Panels

Zone Access/Work location

731

741

Manpower Resources

Skills NON SPECIFIC

References

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

Task 12-34-24-860-802

Task 32-00-00-481-801

Task 32-00-00-481-802

NOTE: The items given in this note shall be considered as the basic Aircraft

configuration before you start a maintenance task:

- Aircraft on the ground resting on landing gear (the ground safety

locks and the wheel chocks are in position on the landing gear)

- Engine shut down, thrust reversers closed and locked

- Aircraft in clean configuration

- Parking brake applied

- Aircraft electrical network de-energized

- Hydraulic systems depressurized

- Access to the cockpit and cabin is available

- All circuit breakers are in closed position

- All controls in NORM, AUTO or OFF position.

DATE: Feb 17/15 SERVICE BULLETIN No.: A330-32-3269

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

12-34-24-860-802.

(b) Do the installation of the Safety Devices on the Landing Gears, refer to AMM Task

32-00-00-481-801.

(c) Do the installation of the Safety Devices on the Landing Gear Doors, refer to AMM

Task 32-00-00-481-802.

(d) Lift the aircraft on jacks, refer to AMM Task 07-11-00-581-801.

**CONF 003

(1) Subtask 323269-941-401-001 - Job Set-up

Work Zones and Access Panels

Zone Access/Work location

731

741

Manpower Resources

Skills NON SPECIFIC

References

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

Task 12-34-24-860-802

Task 32-00-00-481-801

Task 32-00-00-481-802

NOTE: The items given in this note shall be considered as the basic Aircraft

configuration before you start a maintenance task:

- Aircraft on the ground resting on landing gear (the ground safety

locks and the wheel chocks are in position on the landing gear)

- Engine shut down, thrust reversers closed and locked

- Aircraft in clean configuration

- Parking brake applied

- Aircraft electrical network de-energized

- Hydraulic systems depressurized

- Access to the cockpit and cabin is available

- All circuit breakers are in closed position

- All controls in NORM, AUTO or OFF position.

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

12-34-24-860-802.

DATE: Feb 17/15 SERVICE BULLETIN No.: A330-32-3269

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SERVICE BULLETIN

(b) Do the installation of the Safety Devices on the Landing Gears, refer to AMM Task

32-00-00-481-801.

(c) Do the installation of the Safety Devices on the Landing Gear Doors, refer to AMM

Task 32-00-00-481-802.

(d) Lift the aircraft on jacks, refer to AMM Task 07-11-00-581-801.

**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 323269-832-401-001 - Inspect the Upper Cardan Pin and Nut on the LH

MLG

Work Zones and Access Panels

Zone Access/Work location

731 Work location LH Main Landing Gear

Manpower Resources

Manhours 4.00

Minimum number of person 1

Subtask elapsed time 4.00

Skills AIRFRAME

Material necessary to do the job

Consumable CMLB01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Non Aqueous Cleaner -

General

08BAA9 As required

Textile - Lint Free Cotton 14SBA1 As required

References

Component Maintenance Manual

Manufacturer (CMMm)

32-11-91

Fig. A-UBAAA

Removal and Installation of the Side

Stay Upper Cardan Pin and Nut

Sheet 01

Sheet 02

Fig. A-UFAAA

Flow Chart

Sheet 01

Fig. A-UBBAA

Inspection of the Side Stay Upper

Cardan Pin and Nut

Sheet 01

(a) At the Upper Cardan Pin (UCP), on the LH MLG Side Stay 5012GM, remove the

UCP Nut, refer to CMMm 32-11-91.

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(b) Clean the thread of the UCP Nut with:

Textile - Lint Free

Cotton

14SBA1 As required

made moist with

Non Aqueous

Cleaner - General

08BAA9 As required

(c) Inspect the UCP Nut threads for damage, pitting and corrosion, refer to Fig. AUFAAA Sheet 01 and Fig. A-UBBAA Sheet 01.

1 If no damage, pitting or corrosion is found, retain the UCP Nut.

2 If damage, pitting or corrosion is found, discard the UCP Nut.

(d) Clean the thread of the UCP with:

Textile - Lint Free

Cotton

14SBA1 As required

made moist with

Non Aqueous

Cleaner - General

08BAA9 As required

(e) Inspect the UCP threads for damage, pitting and corrosion, refer to Fig. A-UFAAA

Sheet 01 and Fig. A-UBBAA Sheet 01.

1 If no damage, pitting or corrosion is found, retain the UCP and go to

SUBTASK 323269-410-401 001 Install the Upper Cardan Pin Nut on the LH

MLG .

2 If damage, pitting or corrosion is found go to SUBTASK 323269-833-401 001

Replace the Upper Cardan Pin on the LH MLG .

(2) Subtask 323269-832-402-001 - Inspect the Upper Cardan Pin and Nut on the RH

MLG

Work Zones and Access Panels

Zone Access/Work location

741 Work location RH Main Landing Gear

Manpower Resources

Manhours 4.00

Minimum number of person 1

Subtask elapsed time 4.00

Skills AIRFRAME

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Material necessary to do the job

Consumable CMLB01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Non Aqueous Cleaner -

General

08BAA9 As required

Textile - Lint Free Cotton 14SBA1 As required

References

Component Maintenance Manual

Manufacturer (CMMm)

32-11-91

Fig. A-UBAAA

Removal and Installation of the Side

Stay Upper Cardan Pin and Nut

Sheet 01

Sheet 02

Fig. A-UBBAA

Inspection of the Side Stay Upper

Cardan Pin and Nut

Sheet 01

Fig. A-UFAAA

Flow Chart

Sheet 01

(a) At the Upper Cardan Pin (UCP) on the RH MLG Side Stay 5013GM, remove the

UCP Nut, refer to CMMm 32-11-91.

(b) Clean the thread of the UCP Nut with:

Textile - Lint Free

Cotton

14SBA1 As required

made moist with

Non Aqueous

Cleaner - General

08BAA9 As required

(c) Inspect the UCP Nut threads for damage, pitting and corrosion, refer to Fig. AUFAAA Sheet 01 and Fig. A-UBBAA Sheet 01.

1 If no damage, pitting or corrosion is found, retain the UCP Nut.

2 If damage, pitting or corrosion is found, discard the UCP Nut.

(d) Clean the thread of the UCP with:

Textile - Lint Free

Cotton

14SBA1 As required

made moist with

Non Aqueous

Cleaner - General

08BAA9 As required

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(e) Inspect the UCP threads for damage, pitting and corrosion, refer to Fig. A-UFAAA

Sheet 01 and Fig. A-UBBAA Sheet 01.

1 If no damage, pitting or corrosion is found, retain the UCP and go to

SUBTASK 323269-410-402 001 Install the Upper Cardan Pin Nut at the RH

MLG .

2 If damage, pitting or corrosion is found go to SUBTASK 323269-833-402 001

Replace the Upper Cardan Pin on the RH MLG .

(3) Subtask 323269-833-401-001 - Replace the Upper Cardan Pin on the LH MLG

Work Zones and Access Panels

Zone Access/Work location

731 Work location LH Main Landing Gear

Manpower Resources

Manhours 4.00

Minimum number of person 1

Subtask elapsed time 4.00

Skills AIRFRAME

Material necessary to do the job

Consumable CMLB01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Non Hardening Jointing

Putty-High Temp

06LDG6 As required

References

Aircraft Maintenance Manual (AMM) Task 32-11-16-000-801

Task 32-11-16-400-801

Component Maintenance Manual

Manufacturer (CMMm)

32-11-91

Fig. A-UBAAA

Removal and Installation of the Side

Stay Upper Cardan Pin and Nut

Sheet 01

Sheet 02

(a) At the Upper Cardan Pin joint on the LH MLG Side Stay 5012GM, remove and

discard the UCP, refer to AMM Task 32-11-16-000-801 and CMMm 32-11-91.

(b) At the Upper Cardan Pin joint on the LH MLG Side Stay 5012GM, install a new

UCP, refer to AMM Task 32-11-16-400-801, CMMm 32-11-91 and Fig. A-UBAAA

Sheet 02, to the surface of the threads on the Upper Cardan Pin, apply:

Non Hardening

Jointing Putty-High

Temp

06LDG6 As required

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SERVICE BULLETIN

(c) Go to SUBTASK 323269-410-401 001 Install the Upper Cardan Pin Nut on the LH

MLG .

(4) Subtask 323269-833-402-001 - Replace the Upper Cardan Pin on the RH MLG

Work Zones and Access Panels

Zone Access/Work location

741 Work location RH Main Landing Gear

Manpower Resources

Manhours 4.00

Minimum number of person 1

Subtask elapsed time 4.00

Skills AIRFRAME

Material necessary to do the job

Consumable CMLB01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Non Hardening Jointing

Putty-High Temp

06LDG6 As required

References

Aircraft Maintenance Manual (AMM) Task 32-11-16-000-801

Task 32-11-16-400-801

Component Maintenance Manual

Manufacturer (CMMm)

32-11-91

Fig. A-UBAAA

Removal and Installation of the Side

Stay Upper Cardan Pin and Nut

Sheet 01

Sheet 02

(a) At the Upper Cardan Pin joint on the RH MLG Side Stay 5013GM, remove and

discard the UCP, refer to AMM Task 32-11-16-000-801 and CMMm 32-11-91.

(b) At the Upper Cardan Pin joint on the RH MLG Side Stay 5013GM, install a new

UCP, refer to AMM Task 32-11-16-400-801, CMMm 32-11-91 and Fig. A-UBAAA

Sheet 02, to the surface of the threads on the Upper Cardan Pin, apply:

Non Hardening

Jointing Putty-High

Temp

06LDG6 As required

(c) Go to SUBTASK 323269-410-402 001 Install the Upper Cardan Pin Nut at the RH

MLG .

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SERVICE BULLETIN

(5) Subtask 323269-410-401-001 - Install the Upper Cardan Pin Nut on the LH MLG

Work Zones and Access Panels

Zone Access/Work location

731 Work location LH Main Landing Gear

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills AIRFRAME

Material necessary to do the job

Consumable CMLB01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Polysulfide Sealant -

General Purpose Interfay

06AAC5 As required

Non Hardening Jointing

Putty-High Temp

06LDG6 As required

References

Aircraft Maintenance Manual (AMM) Task 32-11-16-400-801

Component Maintenance Manual

Manufacturer (CMMm)

32-11-91

Fig. A-UBAAA

Removal and Installation of the Side

Stay Upper Cardan Pin and Nut

Sheet 01

Sheet 02

(a) Install the UCP Nut on the LH MLG:

1 If NO damage, pitting or corrosion was found on the UCP Nut, install the

UCP Nut, refer to AMM Task 32-11-16-400-801 and CMMm 32-11-91, to the

threads of the UCP nut and the splines of the UCP, apply:

Non Hardening

Jointing Putty-High

Temp

06LDG6 As required

2 If damage, pitting or corrosion was found on the UCP Nut, discard the UCP

Nut and install a new UCP Nut, refer to AMM Task 32-11-16-400-801 and

CMMm 32-11-91, to the threads of the UCP nut and the splines of the UCP,

apply:

Non Hardening

Jointing Putty-High

Temp

06LDG6 As required

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(b) On the UCP Locking Assembly, refer to Fig. A-UBAAA Sheet 01 and Fig. A-UBAAA

Sheet 02, apply:

Polysulfide Sealant

- General Purpose

Interfay

06AAC5 As required

(6) Subtask 323269-410-402-001 - Install the Upper Cardan Pin Nut at the RH MLG

Work Zones and Access Panels

Zone Access/Work location

741 Work location RH Main Landing Gear

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills AIRFRAME

Material necessary to do the job

Consumable CMLB01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Polysulfide Sealant-General

Purpose Interfay Land

06AAC5 As required

Non Hardening Jointing

Putty-High Temp

06LDG6 As required

References

Aircraft Maintenance Manual (AMM) Task 32-11-16-400-801

Component Maintenance Manual

Manufacturer (CMMm)

32-11-91

Fig. A-UBAAA

Removal and Installation of the Side

Stay Upper Cardan Pin and Nut

Sheet 01

Sheet 02

(a) Install the UCP Nut on the RH MLG:

1 If NO damage, pitting or corrosion was found on the UCP Nut, install the

UCP Nut, refer to AMM Task 32-11-16-400-801 and CMMm 32-11-91, to the

threads of the UCP nut and the splines of the UCP, apply:

Non Hardening

Jointing Putty-High

Temp

06LDG6 As required

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2 If damage, pitting or corrosion was found on the UCP Nut, discard the UCP

Nut and install a new UCP Nut, refer to AMM Task 32-11-16-400-801 and

CMMm 32-11-91, to the threads of the UCP nut and the splines of the UCP,

apply:

Non Hardening

Jointing Putty-High

Temp

06LDG6 As required

(b) On the UCP Locking Assembly, refer to Fig. A-UBAAA Sheet 01 and Fig. A-UBAAA

Sheet 02, apply:

Polysulfide SealantGeneral Purpose

Interfay Land

06AAC5 As required

**CONF 002

(1) Subtask 323269-832-401-003 - Inspect the Upper Cardan Pin and Nut on the LH

MLG

Work Zones and Access Panels

Zone Access/Work location

731 Work location LH Main Landing Gear

Manpower Resources

Manhours 4.00

Minimum number of person 1

Subtask elapsed time 4.00

Skills AIRFRAME

Material necessary to do the job

Consumable CMLB01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Non Aqueous Cleaner -

General

08BAA9 As required

Textile - Lint Free Cotton 14SBA1 As required

References

Component Maintenance Manual

Manufacturer (CMMm)

32-12-07

Fig. A-UBAAA

Removal and Installation of the Side

Stay Upper Cardan Pin and Nut

Sheet 01

Sheet 02

Fig. A-UBBAA

Inspection of the Side Stay Upper

Cardan Pin and Nut

Sheet 01

DATE: Feb 17/15 SERVICE BULLETIN No.: A330-32-3269

REVISION No.: 01 - Dec 03/15 Page: 31

7

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

SERVICE BULLETIN

References

Fig. A-UFAAA

Flow Chart

Sheet 01

(a) At the Upper Cardan Pin (UCP) on the LH MLG Side Stay 5012GM, remove the

UCP Nut, refer to CMMm 32-12-07

(b) Clean the thread of the UCP Nut with:

Textile - Lint Free

Cotton

14SBA1 As required

made moist with

Non Aqueous

Cleaner - General

08BAA9 As required

(c) Inspect the UCP Nut threads for damage, pitting and corrosion, refer to Fig. AUFAAA Sheet 01 and Fig. A-UBBAA Sheet 01.

1 If no damage, pitting or corrosion is found, retain the UCP Nut.

2 If damage, pitting or corrosion is found, discard the UCP Nut.

(d) Clean the UCP thread of the with:

Textile - Lint Free

Cotton

14SBA1 As required

made moist with

Non Aqueous

Cleaner - General

08BAA9 As required

(e) Inspect the UCP threads for damage, pitting and corrosion, refer to Fig. A-UFAAA

Sheet 01 and Fig. A-UBBAA Sheet 01.

1 If no damage, pitting or corrosion is found, retain the UCP and go to

SUBTASK 323269-410-401 003 Install the Upper Cardan Pin Nut on the LH

MLG .

2 If damage, pitting or corrosion is found go to SUBTASK 323269-833-401 003

Replace the Upper Cardan Pin on the LH MLG .

(2) Subtask 323269-832-402-003 - Inspect the Upper Cardan Pin and Nut on the RH

MLG

Work Zones and Access Panels

Zone Access/Work location

741 Work location RH Main Landing Gear

DATE: Feb 17/15 SERVICE BULLETIN No.: A330-32-3269

REVISION No.: 01 - Dec 03/15 Page: 32

7

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

SERVICE BULLETIN

Manpower Resources

Manhours 4.00

Minimum number of person 1

Subtask elapsed time 4.00

Skills AIRFRAME

Material necessary to do the job

Consumable CMLB01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Non Aqueous Cleaner -

General

08BAA9 As required

Textile - Lint Free Cotton 14SBA1 As required

References

Component Maintenance Manual

Manufacturer (CMMm)

32-12-07

Fig. A-UBAAA

Removal and Installation of the Side

Stay Upper Cardan Pin and Nut

Sheet 01

Sheet 02

Fig. A-UBBAA

Inspection of the Side Stay Upper

Cardan Pin and Nut

Sheet 01

Fig. A-UFAAA

Flow Chart

Sheet 01

(a) At the Upper Cardan Pin (UCP), on the RH MLG Side Stay 5013GM, remove the

UCP Nut, refer to CMMm 32-12-07.

(b) Clean the thread of the UCP Nut with:

Textile - Lint Free

Cotton

14SBA1 As required

made moist with

Non Aqueous

Cleaner - General

08BAA9 As required

(c) Inspect the UCP Nut threads for damage, pitting and corrosion, refer to Fig. AUFAAA Sheet 01 and Fig. A-UBBAA Sheet 01.

1 If no damage, pitting or corrosion is found, retain the UCP Nut.

2 If damage, pitting or corrosion is found, discard the UCP Nut.

(d) Clean the thread of the UCP with:

Textile - Lint Free

Cotton

14SBA1 As required

DATE: Feb 17/15 SERVICE BULLETIN No.: A330-32-3269

REVISION No.: 01 - Dec 03/15 Page: 33

7

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

SERVICE BULLETIN

made moist with

Non Aqueous

Cleaner - General

08BAA9 As required

(e) Inspect the UCP threads for damage, pitting and corrosion, refer to Fig. A-UFAAA

Sheet 01 and Fig. A-UBBAA Sheet 01.

1 If no damage, pitting or corrosion is found, retain the UCP and go to

SUBTASK 323269-410-402 003 Install the Upper Cardan Pin Nut on the RH

MLG .

2 If damage, pitting or corrosion is found go to SUBTASK 323269-833-402 003

Replace the Upper Cardan Pin on the RH MLG .

(3) Subtask 323269-833-401-003 - Replace the Upper Cardan Pin on the LH MLG

Work Zones and Access Panels

Zone Access/Work location

731 Work location LH Main Landing Gear

Manpower Resources

Manhours 4.00

Minimum number of person 1

Subtask elapsed time 4.00

Skills AIRFRAME

Material necessary to do the job

Consumable CMLB01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Non Hardening Jointing

Putty-High Temp

06LDG6 As required

References

Aircraft Maintenance Manual (AMM) Task 32-11-16-000-801

Task 32-11-16-400-801

Component Maintenance Manual

Manufacturer (CMMm)

32-12-07

Fig. A-UBAAA

Removal and Installation of the Side

Stay Upper Cardan Pin and Nut

Sheet 01

Sheet 02

(a) At the Upper Cardan Pin joint on the LH MLG Side Stay 5012GM, remove and

discard the UCP, refer to AMM Task 32-11-16-000-801 and CMMm 32-12-07.

DATE: Feb 17/15 SERVICE BULLETIN No.: A330-32-3269

REVISION No.: 01 - Dec 03/15 Page: 34

7

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

SERVICE BULLETIN

(b) At the Upper Cardan Pin joint on the LH MLG Side Stay 5012GM, install a new

UCP, refer to AMM Task 32-11-16-400-801, CMMm 32-12-07 and Fig. A-UBAAA

Sheet 02, to the surface of the threads on the Upper Cardan Pin, apply:

Non Hardening

Jointing Putty-High

Temp

06LDG6 As required

(c) Go to SUBTASK 323269-410-401 003 Install the Upper Cardan Pin Nut on the LH

MLG .

(4) Subtask 323269-833-402-003 - Replace the Upper Cardan Pin on the RH MLG

Work Zones and Access Panels

Zone Access/Work location

741 Work location RH Main Landing Gear

Manpower Resources

Manhours 4.00

Minimum number of person 1

Subtask elapsed time 4.00

Skills AIRFRAME

Material necessary to do the job

Consumable CMLB01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Non Hardening Jointing

Putty-High Temp

06LDG6 As required

References

Aircraft Maintenance Manual (AMM) Task 32-11-16-000-801

Task 32-11-16-400-801

Component Maintenance Manual

Manufacturer (CMMm)

32-12-07

Fig. A-UBAAA

Removal and Installation of the Side

Stay Upper Cardan Pin and Nut

Sheet 01

Sheet 02

(a) At the Upper Cardan Pin joint on the RH MLG Side Stay 5013GM, remove and

discard the UCP, refer to AMM Task 32-11-16-000-801 and CMMm 32-12-07.

(b) At the Upper Cardan Pin joint on the RH MLG Side Stay 5013GM, install a new

UCP, refer to AMM Task 32-11-16-400-801, CMMm 32-12-07 and Fig. A-UBAAA

Sheet 02, to the surface of the threads on the Upper Cardan Pin, apply:

Non Hardening

Jointing Putty-High

Temp

06LDG6 As required

DATE: Feb 17/15 SERVICE BULLETIN No.: A330-32-3269

REVISION No.: 01 - Dec 03/15 Page: 35

7

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

SERVICE BULLETIN

(c) Go to SUBTASK 323269-410-402 003 Install the Upper Cardan Pin Nut on the RH

MLG .

(5) Subtask 323269-410-401-003 - Install the Upper Cardan Pin Nut on the LH MLG

Work Zones and Access Panels

Zone Access/Work location

731 Work location LH Main Landing Gear

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills AIRFRAME

Material necessary to do the job

Consumable CMLB01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Polysulfide Sealant-General

Purpose Interfay Land

06AAC5 As required

Non Hardening Jointing

Putty-High Temp

06LDG6 As required

References

Aircraft Maintenance Manual (AMM) Task 32-11-16-400-801

Component Maintenance Manual

Manufacturer (CMMm)

32-12-07

Fig. A-UBAAA

Removal and Installation of the Side

Stay Upper Cardan Pin and Nut

Sheet 01

Sheet 02

(a) Install the UCP Nut on the LH MLG:

1 If NO damage, pitting or corrosion was found on the UCP Nut, install the

UCP Nut, refer to AMM Task 32-11-16-400-801 and CMMm 32-12-07, to the

threads of the UCP nut and the splines of the UCP, apply:

Non Hardening

Jointing Putty-High

Temp

06LDG6 As required

DATE: Feb 17/15 SERVICE BULLETIN No.: A330-32-3269

REVISION No.: 01 - Dec 03/15 Page: 36

7

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

SERVICE BULLETIN

2 If damage, pitting or corrosion was found on the UCP Nut, discard the UCP

Nut and install a new UCP Nut, refer to AMM Task 32-11-16-400-801 and

CMMm 32-12-07, to the threads of the UCP nut and the splines of the UCP,

apply:

Non Hardening

Jointing Putty-High

Temp

06LDG6 As required

(b) On the UCP Locking Assembly, refer to Fig. A-UBAAA Sheet 01 and Fig. A-UBAAA

Sheet 02, apply:

Polysulfide SealantGeneral Purpose

Interfay Land

06AAC5 As required

(6) Subtask 323269-410-402-003 - Install the Upper Cardan Pin Nut on the RH MLG

Work Zones and Access Panels

Zone Access/Work location

741 Work location RH Main Landing Gear

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills AIRFRAME

Material necessary to do the job

Consumable CMLB01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Polysulfide Sealant-General

Purpose Interfay Land

06AAC5 As required

Non Hardening Jointing

Putty-High Temp

06LDG6 As required

References

Aircraft Maintenance Manual (AMM) Task 32-11-16-400-801

Component Maintenance Manual

Manufacturer (CMMm)

32-12-07

Fig. A-UBAAA

Removal and Installation of the Side

Stay Upper Cardan Pin and Nut

Sheet 01

Sheet 02

DATE: Feb 17/15 SERVICE BULLETIN No.: A330-32-3269

REVISION No.: 01 - Dec 03/15 Page: 37

7

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

SERVICE BULLETIN

(a) Install the UCP Nut on the RH MLG:

1 If NO damage, pitting or corrosion was found on the UCP Nut, install the

UCP Nut, refer to AMM Task 32-11-16-400-801 and CMMm 32-12-07, to the

threads of the UCP nut and the splines of the UCP, apply:

Non Hardening

Jointing Putty-High

Temp

06LDG6 As required

2 If damage, pitting or corrosion was found on the UCP Nut, discard the UCP

Nut and install a new UCP Nut, refer to AMM Task 32-11-16-400-801 and

CMMm 32-12-07, to the threads of the UCP nut and the splines of the UCP,

apply:

Non Hardening

Jointing Putty-High

Temp

06LDG6 As required

(b) On the UCP Locking Assembly, refer to Fig. A-UBAAA Sheet 01 and Fig. A-UBAAA

Sheet 02, apply:

Polysulfide SealantGeneral Purpose

Interfay Land

06AAC5 As required

**CONF 003

(1) Subtask 323269-832-401-002 - Inspect the Upper Cardan Pin and Nut on the LH

MLG

Work Zones and Access Panels

Zone Access/Work location

731 Work location LH Main Landing Gear

Manpower Resources

Manhours 4.00

Minimum number of person 1

Subtask elapsed time 4.00

Skills AIRFRAME

Material necessary to do the job

Consumable CMLB01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Non Aqueous Cleaner -

General

08BAA9 As required

Textile - Lint Free Cotton 14SBA1 As required

DATE: Feb 17/15 SERVICE BULLETIN No.: A330-32-3269

REVISION No.: 01 - Dec 03/15 Page: 38

7

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

SERVICE BULLETIN

References

Component Maintenance Manual

Manufacturer (CMMm)

32-12-66

Fig. A-UBAAA

Removal and Installation of the Side

Stay Upper Cardan Pin and Nut

Sheet 01

Sheet 02

Fig. A-UFAAA

Flow Chart

Sheet 01

Fig. A-UBBAB

Inspection of the Side Stay Upper

Cardan Pin and Nut

Sheet 01

(a) At the Upper Cardan Pin (UCP) on the LH MLG Side Stay 5012GM, remove UCP

Nut, refer to CMMm 32-12-66.

(b) Clean the threads of the UCP Nut with:

Textile - Lint Free

Cotton

14SBA1 As required

made moist with

Non Aqueous

Cleaner - General

08BAA9 As required

(c) Inspect the UCP Nut threads for damage, pitting and corrosion, refer to Fig. AUFAAA Sheet 01 and Fig. A-UBBAB Sheet 01.

1 If no damage, pitting or corrosion is found, retain the UCP Nut.

2 If damage, pitting or corrosion is found, discard the UCP Nut.

(d) Clean the thread of the UCP with:

Textile - Lint Free

Cotton

14SBA1 As required

made moist with

Non Aqueous

Cleaner - General

08BAA9 As required

(e) Inspect the UCP threads for damage, pitting and corrosion, refer to Fig. A-UFAAA

Sheet 01 and Fig. A-UBBAB Sheet 01.

1 If no damage, pitting or corrosion is found, retain the UCP and go to

SUBTASK 323269-410-401 002 Install the Upper Cardan Pin Nut on the LH

MLG .

2 If damage, pitting or corrosion is found go to SUBTASK 323269-833-401 002

Replace the Upper Cardan Pin on the LH MLG .

DATE: Feb 17/15 SERVICE BULLETIN No.: A330-32-3269

REVISION No.: 01 - Dec 03/15 Page: 39

7

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

SERVICE BULLETIN

(2) Subtask 323269-832-402-002 - Inspect the Upper Cardan Pin and Nut on the RH

MLG

Work Zones and Access Panels

Zone Access/Work location

741 Work location RH Main Landing Gear

Manpower Resources

Manhours 4.00

Minimum number of person 1

Subtask elapsed time 4.00

Skills AIRFRAME

Material necessary to do the job

Consumable CMLB01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Non Aqueous Cleaner -

General

08BAA9 As required

Textile - Lint Free Cotton 14SBA1 As required

References

Component Maintenance Manual

Manufacturer (CMMm)

32-12-66

Fig. A-UBAAA

Removal and Installation of the Side

Stay Upper Cardan Pin and Nut

Sheet 01

Sheet 02

Fig. A-UFAAA

Flow Chart

Sheet 01

Fig. A-UBBAB

Inspection of the Side Stay Upper

Cardan Pin and Nut

Sheet 01

(a) At the Upper Cardan Pin (UCP), on the RH MLG Side Stay 5013GM, remove the

UCP Nut, refer to CMMm 32-12-66.

(b) Clean the thread of the UCP Nut with:

Textile - Lint Free

Cotton

14SBA1 As required

made moist with

Non Aqueous

Cleaner - General

08BAA9 As required

(c) Inspect the thread of the UCP Nut threads for damage, pitting and corrosion, refer

to Fig. A-UFAAA Sheet 01 and Fig. A-UBBAB Sheet 01.

1 If no damage, pitting or corrosion is found, retain the UCP Nut.

DATE: Feb 17/15 SERVICE BULLETIN No.: A330-32-3269

REVISION No.: 01 - Dec 03/15 Page: 40

7

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

SERVICE BULLETIN

2 If damage, pitting or corrosion is found, discard the UCP Nut.

(d) Clean the thread of the UCP with:

Textile - Lint Free

Cotton

14SBA1 As required

made moist with

Non Aqueous

Cleaner - General

08BAA9 As required

(e) Inspect the UCP threads for damage, pitting and corrosion, refer to Fig. A-UFAAA

Sheet 01 and Fig. A-UBBAB Sheet 01.

1 If no damage, pitting or corrosion is found, retain the UCP and go to

SUBTASK 323269-410-402 002 Install the Upper Cardan Pin Nut on the RH

MLG .

2 If damage, pitting or corrosion is found go to SUBTASK 323269-833-402 002

Replace the Upper Cardan Pin on the RH MLG .

(3) Subtask 323269-833-401-002 - Replace the Upper Cardan Pin on the LH MLG

Work Zones and Access Panels

Zone Access/Work location

731 Work location LH Main Landing Gear

Manpower Resources

Manhours 4.00

Minimum number of person 1

Subtask elapsed time 4.00

Skills AIRFRAME

Material necessary to do the job

Consumable CMLB01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Non Hardening Jointing

Putty-High Temp

06LDG6 As required

References

Aircraft Maintenance Manual (AMM) Task 32-11-16-000-801

Task 32-11-16-400-801

Component Maintenance Manual

Manufacturer (CMMm)

32-12-66

Fig. A-UBAAA

Removal and Installation of the Side

Stay Upper Cardan Pin and Nut

Sheet 01

Sheet 02

DATE: Feb 17/15 SERVICE BULLETIN No.: A330-32-3269

REVISION No.: 01 - Dec 03/15 Page: 41

7

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

SERVICE BULLETIN

(a) At the Upper Cardan Pin joint on the LH MLG Side Stay 5012GM, remove and

discard the UCP, refer to AMM Task 32-11-16-000-801 and CMMm 32-12-66.

(b) At the Upper Cardan Pin joint on the LH MLG Side Stay 5012GM, install a new

UCP, refer to AMM Task 32-11-16-400-801, CMMm 32-12-66 and Fig. A-UBAAA

Sheet 02, to the surface of the threads on the Upper Cardan Pin, apply:

Non Hardening

Jointing Putty-High

Temp

06LDG6 As required

(c) Go to SUBTASK 323269-410-401 002 Install the Upper Cardan Pin Nut on the LH

MLG .

(4) Subtask 323269-833-402-002 - Replace the Upper Cardan Pin on the RH MLG

Work Zones and Access Panels

Zone Access/Work location

741 Work location RH Main Landing Gear

Manpower Resources

Manhours 4.00

Minimum number of person 1

Subtask elapsed time 4.00

Skills AIRFRAME

Material necessary to do the job

Consumable CMLB01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Non Hardening Jointing

Putty-High Temp

06LDG6 As required

References

Aircraft Maintenance Manual (AMM) Task 32-11-16-000-801

Task 32-11-16-400-801

Component Maintenance Manual

Manufacturer (CMMm)

32-12-66

Fig. A-UBAAA

Removal and Installation of the Side

Stay Upper Cardan Pin and Nut

Sheet 01

Sheet 02

(a) At the Upper Cardan Pin joint on the RH MLG Side Stay 5013GM, remove and

discard the UCP, refer to AMM Task 32-11-16-000-801 and CMMm 32-12-66.

DATE: Feb 17/15 SERVICE BULLETIN No.: A330-32-3269

REVISION No.: 01 - Dec 03/15 Page: 42

7

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

SERVICE BULLETIN

(b) At the Upper Cardan Pin joint on the RH MLG Side Stay 5013GM, install a new

UCP, refer to AMM Task 32-11-16-400-801, CMMm 32-12-66 and Fig. A-UBAAA

Sheet 02, to the surface of the threads on the Upper Cardan Pin, apply:

Non Hardening

Jointing Putty-High

Temp

06LDG6 As required

(c) Go to SUBTASK 323269-410-402 002 Install the Upper Cardan Pin Nut on the RH

MLG .

(5) Subtask 323269-410-401-002 - Install the Upper Cardan Pin Nut on the LH MLG

Work Zones and Access Panels

Zone Access/Work location

731 Work location LH Main Landing Gear

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills AIRFRAME

Material necessary to do the job

Consumable CMLB01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Polysulfide Sealant-General

Purpose Interfay Land

06AAC5 As required

Non Hardening Jointing

Putty-High Temp

06LDG6 As required

References

Aircraft Maintenance Manual (AMM) Task 32-11-16-400-801

Component Maintenance Manual

Manufacturer (CMMm)

32-12-66

Fig. A-UBAAA

Removal and Installation of the Side

Stay Upper Cardan Pin and Nut

Sheet 01

Sheet 02

(a) Install the UCP Nut on the LH MLG:

1 If NO damage, pitting or corrosion was found on the UCP Nut, install the

UCP Nut, refer to AMM Task 32-11-16-400-801 and CMMm 32-12-66, to the

threads of the UCP nut and the splines of the UCP, apply:

Non Hardening

Jointing Putty-High

Temp

06LDG6 As required

DATE: Feb 17/15 SERVICE BULLETIN No.: A330-32-3269

REVISION No.: 01 - Dec 03/15 Page: 43

7

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

SERVICE BULLETIN

2 If damage, pitting or corrosion was found on the UCP Nut, discard the UCP

Nut and install a new UCP Nut, refer to AMM Task 32-11-16-400-801 and

CMMm 32-12-66, to the threads of the UCP nut and the splines of the UCP,

apply:

Non Hardening

Jointing Putty-High

Temp

06LDG6 As required

(b) On the UCP Locking Assembly, refer to Fig. A-UBAAA Sheet 01 and Fig. A-UBAAA

Sheet 02, apply:

Polysulfide SealantGeneral Purpose

Interfay Land

06AAC5 As required

(6) Subtask 323269-410-402-002 - Install the Upper Cardan Pin Nut on the RH MLG

Work Zones and Access Panels

Zone Access/Work location

741 Work location RH Main Landing Gear

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills AIRFRAME

Material necessary to do the job

Consumable CMLB01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Polysulfide Sealant-General

Purpose Interfay Land

06AAC5 As required

Non Hardening Jointing

Putty-High Temp

06LDG6 As required

References

Aircraft Maintenance Manual (AMM) Task 32-11-16-400-801

Component Maintenance Manual

Manufacturer (CMMm)

32-12-66

Fig. A-UBAAA

Removal and Installation of the Side

Stay Upper Cardan Pin and Nut

Sheet 01

Sheet 02

DATE: Feb 17/15 SERVICE BULLETIN No.: A330-32-3269

REVISION No.: 01 - Dec 03/15 Page: 44

7

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

SERVICE BULLETIN

(a) Install the UCP Nut on the RH MLG:

1 If NO damage, pitting or corrosion was found on the UCP Nut, install the

UCP Nut, refer to AMM Task 32-11-16-400-801 and CMMm 32-12-66, to the

threads of the UCP nut and the splines of the UCP, apply:

Non Hardening

Jointing Putty-High

Temp

06LDG6 As required

2 If damage, pitting or corrosion was found on the UCP Nut, discard the UCP

Nut and install a new UCP Nut, refer to AMM Task 32-11-16-400-801 and

CMMm 32-12-66, to the threads of the UCP nut and the splines of the UCP,

apply:

Non Hardening

Jointing Putty-High

Temp

06LDG6 As required

(b) On the UCP Locking Assembly, refer to Fig. A-UBAAA Sheet 01 and Fig. A-UBAAA

Sheet 02, apply:

Polysulfide SealantGeneral Purpose

Interfay Land

06AAC5 As required

**CONF ALL

D. TEST

**CONF 001

(1) Subtask 323269-700-401-001 - Testing

Work Zones and Access Panels

Zone Access/Work location

731 Work location LH Main Landing Gear

741 Work location RH Main Landing Gear

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 32-31-00-710-801

Task 32-31-00-740-801

Task 32-33-00-710-801

NOTE: The worksteps that follow are only necessary if the Upper Cardan Pin

has been replaced.

(a) Do a BITE test of the Normal Extension and Retraction System, refer to AMM Task

32-31-00-740-801.

DATE: Feb 17/15 SERVICE BULLETIN No.: A330-32-3269

REVISION No.: 01 - Dec 03/15 Page: 45

7

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

SERVICE BULLETIN

(b) Do a functional test of the Normal Extension and Retraction, refer to AMM Task

32-31-00-710-801.

(c) Do an operational test of the Free-Fall System, refer to AMM Task

32-33-00-710-801.

**CONF 002

(1) Subtask 323269-700-401-001 - Testing

Work Zones and Access Panels

Zone Access/Work location

731 Work location LH Main Landing Gear

741 Work location RH Main Landing Gear

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 32-31-00-710-801

Task 32-31-00-740-801

Task 32-33-00-710-801

NOTE: The worksteps that follow are only necessary if the Upper Cardan Pin

has been replaced.

(a) Do a BITE test of the Normal Extension and Retraction System, refer to AMM Task

32-31-00-740-801.

(b) Do a functional test of the Normal Extension and Retraction, refer to AMM Task

32-31-00-710-801.

(c) Do an operational test of the Free-Fall System, refer to AMM Task

32-33-00-710-801.

**CONF 003

(1) Subtask 323269-700-401-001 - Testing

Work Zones and Access Panels

Zone Access/Work location

731 Work location LH Main Landing Gear

741 Work location RH Main Landing Gear

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 32-31-00-710-801

Task 32-31-00-740-801

Task 32-33-00-710-801

DATE: Feb 17/15 SERVICE BULLETIN No.: A330-32-3269

REVISION No.: 01 - Dec 03/15 Page: 46

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SERVICE BULLETIN

NOTE: The worksteps that follow are only necessary if the Upper Cardan Pin

has been replaced.

(a) Do a BITE test of the Normal Extension and Retraction System, refer to AMM Task

32-31-00-740-801.

(b) Do a functional test of the Normal Extension and Retraction, refer to AMM Task

32-31-00-710-801.

(c) Do an operational test of the Free-Fall System, refer to AMM Task

32-33-00-710-801.

**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 323269-942-401-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

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

Task 32-11-16-400-801

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

equipment.

(b) Do the Close-up and Close Access procedures as specified in "Installation of the

MLG Side Stay Assembly", refer to AMM Task 32-11-16-400-801.

(c) Lower the aircraft off jacks, refer to AMM Task 07-11-00-586-801.

(d) Put the aircraft back to its initial configuration.

**CONF 002

(1) Subtask 323269-942-401-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

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

Task 32-11-16-400-801

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

equipment.

(b) Do the Close-up and Close Access procedures as specified in "Installation of the

MLG Side Stay Assembly", refer to AMM Task 32-11-16-400-801.

DATE: Feb 17/15 SERVICE BULLETIN No.: A330-32-3269

REVISION No.: 01 - Dec 03/15 Page: 47

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SERVICE BULLETIN

(c) Lower the aircraft off jacks, refer to AMM Task 07-11-00-586-801.

(d) Put the aircraft back to its initial configuration.

**CONF 003

(1) Subtask 323269-942-401-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

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

Task 32-11-16-400-801

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

equipment.

(b) Do the Close-up and Close Access procedures as specified in "Installation of the

MLG Side Stay Assembly", refer to AMM Task 32-11-16-400-801.

(c) Lower the aircraft off jacks, refer to AMM Task 07-11-00-586-801.

(d) Put the aircraft back to its initial configuration.

DATE: Feb 17/15 SERVICE BULLETIN No.: A330-32-3269

REVISION No.: 01 - Dec 03/15 Page: 48

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SERVICE BULLETIN

**CONF ALL

NOTE: THE PURPOSE OF FLOW CHARTS IS TO SUPPLEMENT THE INFORMATION

GIVEN IN THE PROCEDURE AND COMPLIANCE PARAGRAPHS AND NOT TO

SERVE AS THE PRIMARY SOURCE FOR TASKS OR COMPLIANCE TIMES

GIVEN IN THIS SERVICE BULLETIN.

HAS THE LH OR RH

MAIN LANDING GEAR (MLG)

BEEN REPLACED POST ENTRY

YES

INTO SERVICE (EIS)?

REMOVE UPPER CARDAN PIN NUT

WITHIN THE ACCOMPLISHMENT

TIMESCALES DEFINED IN PARA 1.E. (2),

CLEAN THE THREADS OF THE

UPPER CARDAN PIN AND NUT

IS CORROSION, 

PITTING, OR THREAD

DAMAGE OBSERVED ON THE THREADS

OF THE UPPER CARDAN NUT

REASSEMBLE UPPER

CARDAN JOINT

NO FURTHER

ACTION

YES

NEXT FLIGHT

REPLACE DAMAGED

PART(S) BEFORE

NO

NO

AND/OR THE UPPER

CARDAN PIN?

ON THE THREADS OF THE

UPPER CARDAN PIN AND NUT

DO A DETAILED INSPECTION

G_SB_323269_7_FAAA_01_04

Figure A-UFAAA - Sheet 01

Flow Chart

DATE: Feb 17/15 SERVICE BULLETIN No.: A330-32-3269

REVISION No.: 01 - Dec 03/15 Page: 49

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SERVICE BULLETIN

**CONF ALL

A

A

A

A

SIDE STAY

LH SHOWN

RH SIMILAR

5012GM

(5013GM)

G_SB_323269_7_BAAA_01_02

Figure A-UBAAA - Sheet 01

Removal and Installation of the Side Stay Upper Cardan Pin and Nut

DATE: Feb 17/15 SERVICE BULLETIN No.: A330-32-3269

REVISION No.: 01 - Dec 03/15 Page: 50

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SERVICE BULLETIN

**CONF ALL

SEALANT

CARDAN NUT

SEALANT

UPPER CARDAN PIN LOCKING ASSEMBLY.

NOTE:

01 APPLY MAT NO. 06AAC5 TO COMPLETELY COVER

01 01

A A

ASSEMBLY

ILLUSTRATION SHOWS THE COVERAGE OF THE SEALANT

AND IS TYPICAL FOR NUT AND LOCKING ASSEMBLIES

B

B

UPPER

CARDAN PIN

G_SB_323269_7_BAAA_02_03

Figure A-UBAAA - Sheet 02

Removal and Installation of the Side Stay Upper Cardan Pin and Nut

DATE: Feb 17/15 SERVICE BULLETIN No.: A330-32-3269

REVISION No.: 01 - Dec 03/15 Page: 51

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SERVICE BULLETIN

**CONF 001 thru 002

A

A

B

NOTE:

AREA OF INSPECTION

B

SIDE STAY

LH SHOWN

RH SIMILAR

5012GM

(5013GM)

UPPER

CARDAN PIN

UPPER

CARDAN PIN NUT

G_SB_323269_7_BBAA_01_02

Figure A-UBBAA - Sheet 01

Inspection of the Side Stay Upper Cardan Pin and Nut

DATE: Feb 17/15 SERVICE BULLETIN No.: A330-32-3269

REVISION No.: 01 - Dec 03/15 Page: 52

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SERVICE BULLETIN

**CONF 003

A

A

B

NOTE:

AREA OF INSPECTION

B

LH SHOWN

RH SIMILAR

SIDE STAY

5012GM

(5013GM)

UPPER

CARDAN PIN

UPPER

CARDAN PIN NUT

G_SB_323269_7_BBAB_01_02

Figure A-UBBAB - Sheet 01

Inspection of the Side Stay Upper Cardan Pin and Nut

DATE: Feb 17/15 SERVICE BULLETIN No.: A330-32-3269

REVISION No.: 01 - Dec 03/15 Page: 53

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SERVICE BULLETIN

This Page Intentionally Left Blank

DATE: Feb 17/15 SERVICE BULLETIN No.: A330-32-3269

REVISION No.: 01 - Dec 03/15 Page: 54

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SERVICE BULLETIN

Appendix 01 - Elapsed Time Assumptions

**CONF ALL

ELAPSED TIME ASSUMPTION SERVICE BULLETIN No A330−32−3269

SB ELAPSED TIME

(HOURS)

GET ACCESS

MH ET/S

TOTAL MANHOURS

SB ELAPSED TIME

23.00

13.00

STEPS

1.00 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

NOTE:

PER

1

:

: IF A VSB IS INVOLVED, THE ASSOCIATED MANHOURS

ARE NOT REFLECTED IN THIS GANTT CHART.

0 2 4 6 8 10 12 14 16 18 20

INSPECT THE UPPER CARDAN PIN NUT ON THE LH MLG 4.00 4.00 1

INSPECT THE UPPER CARDAN PIN NUT ON THE RH MLG 4.00 4.00 1

REPLACE THE UPPER CARDAN PIN ON THE LH MLG

REPLACE THE UPPER CARDAN PIN ON THE RH MLG

INSTALL THE UPPER CARDAN PIN NUT ON THE LH MLG 2.00 2.00 1

INSTALL THE UPPER CARDAN PIN NUT ON THE RH MLG 2.00 2.00 1

1.00 1.00 1

1.00 1.00 1

4.00 4.00 1

4.00 4.00 1

TEST

CLOSE−UP

G_SB_323269_7_AAAA_01_02

Figure A-UAAAA - Sheet 01

Gantt Chart

DATE: Feb 17/15 SERVICE BULLETIN No.: A330-32-3269

REVISION No.: 01 - Dec 03/15 Page: 1

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SERVICE BULLETIN

REPORTING SHEET

TITLE: LANDING GEAR - MAIN GEAR - INSPECTION OF SIDE STAY UPPER

CARDAN PIN AND NUT

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: Feb 17/15 SERVICE BULLETIN No.: A330-32-3269

REVISION No.: 01 - Dec 03/15 Page: 1

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SERVICE BULLETIN

QUALITY PERCEPTION FORM

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

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

improve the quality of our Service Bulletins.

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

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

- Quality rating of this SB 4321

- Quality rating of the Accomplishment Instructions 4321

- Quality rating of the Illustrations 4321

- Is this SB easy to understand ? Y/N

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

short description of the issue.

Planning Material Instructions

X Effectivity X Kit content X Preparation

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

X Manpower X Industry support X Test

X References X Re-identification X Close-Up

X Publication X Tooling X Illustrations

Comments:

Operator: Date:

Name/Title:

Please return this form to:

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX FRANCE

Attn : SEM4 Service Bulletins Management

FAX : (33) 5 61 93 42 51

Or via your Resident Customer Support Office.

DATE: Feb 17/15 SERVICE BULLETIN No.: A330-32-3269

REVISION No.: 01 - Dec 03/15 Page: 1

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