# @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



# MANDATORYMANDATORYMANDATORY
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 7

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# @A330 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 7

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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 7

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# @A330 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 7

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# @A330 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 7

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# @A330 SERVICE BULLETIN REVISION TRANSMITTAL SHEET

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DATE: Feb 17/15 SERVICE BULLETIN No.: A330-32-3269 REVISION No.: 01 - Dec 03/15 Page: 6 7

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# @A330 SERVICE BULLETIN SUMMARY AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Tel : (33) 5 61 93 33 33 Telex : AIRBU 530526F Fax : (33) 5 61 93 42 51 This summary is for information only and is not approved for modification of the aircraft. 

# MANDATORYMANDATORYMANDATORY
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 7

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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 7

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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 7

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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 7

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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



# MANDATORYMANDATORYMANDATORY
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 REVISION No.: 01 - Dec 03/15 Page: 1 7

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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 REVISION No.: 01 - Dec 03/15 Page: 2 7

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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 REVISION No.: 01 - Dec 03/15 Page: 3 7

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# @A330 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 DATE: Feb 17/15 SERVICE BULLETIN No.: A330-32-3269 REVISION No.: 01 - Dec 03/15 Page: 4 7

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# @A330 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 DATE: Feb 17/15 SERVICE BULLETIN No.: A330-32-3269 REVISION No.: 01 - Dec 03/15 Page: 5 7

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# @A330 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

DATE: Feb 17/15 SERVICE BULLETIN No.: A330-32-3269 REVISION No.: 01 - Dec 03/15 Page: 6 7

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# @A330 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

DATE: Feb 17/15 SERVICE BULLETIN No.: A330-32-3269 REVISION No.: 01 - Dec 03/15 Page: 7 7

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# @A330 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 REVISION No.: 01 - Dec 03/15 Page: 8 7

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# @A330 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.
DATE: Feb 17/15 SERVICE BULLETIN No.: A330-32-3269 REVISION No.: 01 - Dec 03/15 Page: 9 7

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# @A330 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 REVISION No.: 01 - Dec 03/15 Page: 10 7

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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 COMPLIANCE TIME CONDITION ACTION THRESHOLD GRACE PERIOD REPETITIVE INTERVAL If an Upper Cardan Pin on either LH or RH MLG has beenreplaced 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.

DATE: Feb 17/15 SERVICE BULLETIN No.: A330-32-3269 REVISION No.: 01 - Dec 03/15 Page: 11 7

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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-UAAAAgiven 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
DATE: Feb 17/15 SERVICE BULLETIN No.: A330-32-3269 REVISION No.: 01 - Dec 03/15 Page: 12 7

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# @A330 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-UAAAAgiven 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-UAAAAgiven 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

DATE: Feb 17/15 SERVICE BULLETIN No.: A330-32-3269 REVISION No.: 01 - Dec 03/15 Page: 13 7

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# @A330 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

DATE: Feb 17/15 SERVICE BULLETIN No.: A330-32-3269 REVISION No.: 01 - Dec 03/15 Page: 14 7

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# @A330 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 thesubsequent 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 REVISION No.: 01 - Dec 03/15 Page: 15 7

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# @A330 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 REVISION No.: 01 - Dec 03/15 Page: 16 7

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# @A330 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 REVISION No.: 01 - Dec 03/15 Page: 17 7

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# @A330 SERVICE BULLETIN 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 REVISION No.: 01 - Dec 03/15 Page: 18 7

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# @A330 SERVICE BULLETIN

**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
DATE: Feb 17/15 SERVICE BULLETIN No.: A330-32-3269 REVISION No.: 01 - Dec 03/15 Page: 19 7

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# @A330 SERVICE BULLETIN

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 REVISION No.: 01 - Dec 03/15 Page: 20 7

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# @A330 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

DATE: Feb 17/15 SERVICE BULLETIN No.: A330-32-3269 REVISION No.: 01 - Dec 03/15 Page: 21 7

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# @A330 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 REVISION No.: 01 - Dec 03/15 Page: 22 7

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# @A330 SERVICE BULLETIN (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 REVISION No.: 01 - Dec 03/15 Page: 23 7

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# @A330 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.
DATE: Feb 17/15 SERVICE BULLETIN No.: A330-32-3269 REVISION No.: 01 - Dec 03/15 Page: 24 7

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# @A330 SERVICE BULLETIN (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

DATE: Feb 17/15 SERVICE BULLETIN No.: A330-32-3269 REVISION No.: 01 - Dec 03/15 Page: 25 7

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# @A330 SERVICE BULLETIN
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

DATE: Feb 17/15 SERVICE BULLETIN No.: A330-32-3269 REVISION No.: 01 - Dec 03/15 Page: 26 7

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# @A330 SERVICE BULLETIN (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 toAMM 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

DATE: Feb 17/15 SERVICE BULLETIN No.: A330-32-3269 REVISION No.: 01 - Dec 03/15 Page: 27 7

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# @A330 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 toAMM 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 .

DATE: Feb 17/15 SERVICE BULLETIN No.: A330-32-3269 REVISION No.: 01 - Dec 03/15 Page: 28 7

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# @A330 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

DATE: Feb 17/15 SERVICE BULLETIN No.: A330-32-3269 REVISION No.: 01 - Dec 03/15 Page: 29 7

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# @A330 SERVICE BULLETIN (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

DATE: Feb 17/15 SERVICE BULLETIN No.: A330-32-3269 REVISION No.: 01 - Dec 03/15 Page: 30 7

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# @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 32-11-91, 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 Sheet01 Sheet02 Fig. A-UBBAA Inspection of the Side Stay Upper Cardan Pin and Nut Sheet01

DATE: Feb 17/15 SERVICE BULLETIN No.: A330-32-3269 REVISION No.: 01 - Dec 03/15 Page: 31 7

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# @A330 SERVICE BULLETIN

References Fig. A-UFAAA Flow Chart Sheet01 (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

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# @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 Sheet01 Sheet02 Fig. A-UBBAA Inspection of the Side Stay Upper Cardan Pin and Nut Sheet01 Fig. A-UFAAA Flow Chart Sheet01 (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

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# @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 Sheet01 Sheet02 (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

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# @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 Sheet01 Sheet02 (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

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# @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 Sheet01 Sheet02 (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

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# @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 Sheet01 Sheet02

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

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# @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 Sheet01 Sheet02 Fig. A-UFAAA Flow Chart Sheet01 Fig. A-UBBAB Inspection of the Side Stay Upper Cardan Pin and Nut Sheet01
(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 Sheet01 Sheet02 Fig. A-UFAAA Flow Chart Sheet01 Fig. A-UBBAB Inspection of the Side Stay Upper Cardan Pin and Nut Sheet01
(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 Sheet01 Sheet02

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 Sheet01 Sheet02 (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 Sheet01 Sheet02 (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 Sheet01 Sheet02

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 7

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

# @A330 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 7

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

# @A330 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 7

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

# @A330 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 7

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

# @A330 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 7

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

# @A330 SERVICE BULLETIN

**CONF ALL

SEALANT

CARDAN NUT SEALANT

UPPER CARDAN PIN LOCKING ASSEMBLY. NOTE: APPLY MAT NO. 06AAC5 TO COMPLETELY COVER 01 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 7

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

# @A330 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 7

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

# @A330 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 7

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

# @A330 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 7

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

# @A330 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. 2 4 6 8 10 12 14 0 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 7

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

# @A330 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 7

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

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

DATE: Feb 17/15 SERVICE BULLETIN No.: A330-32-3269 REVISION No.: 01 - Dec 03/15 Page: 1 7

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