# Airbus Service Bulletin A330-53-3226 Copy: A330-53-3226 R03 ("A330-53-3226 R03"), 733 pages: PDF https://openairdocs.org/files/sha256/ec/bb/ecbb690536b4a1d72612e99ae25e79012ddff6cd6d0f121c07eaba979cdf8a2b; text https://openairdocs.org/service-documents/airbus/a330-53-3226/file/ecbb690536b4.md. Rights: © Airbus S.A.S. Filed by the FAA in regulations.gov docket FAA-2019-0318, the docket of AD 2019-19-09. Not covered by OpenAirDocs’ CC0 dedication. ## Details - Manufacturer: [Airbus](https://openairdocs.org/service-documents/airbus.md) - Type: Service bulletin (Service Bulletin) - Number: A330-53-3226 - Latest revision known: A330-53-3226, Revision 01, dated March 3, 2016 (OpenAirDocs) - Page: https://openairdocs.org/service-documents/airbus/a330-53-3226 Also cited in [1 proposed AD](https://openairdocs.org/service-documents/airbus/a330-53-3226/proposed.md). ## Text (733 pages) Rights: © Airbus S.A.S. Filed by the FAA in regulations.gov docket FAA-2019-0318, the docket of AD 2019-19-09. Not covered by OpenAirDocs’ CC0 dedication. Each page's text from the PDF; open the PDF at a page with #page=N. ### Page 1 @A330 SERVICE BULLETIN REVISION TRANSMITTAL SHEET AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE T e l:( 3 3 )56 19 33 33 3 Telex : AIRBU 530526F F a x:( 3 3 )56 19 34 25 1 MANDATORY MANDATORY MANDATORY ATA SYSTEM: 53 TITLE: FUSELAGE - CENTER FUSELAG E - REINFORCE CIRCUMFERENTIAL JOINT BETWEEN FR53.6-FR53.7 FOR EMERGENCY DOOR TYPE 1 AREA MODIFICATION No.: 204309D50888 204309D50892 204309D50893 204309D50904 This page transmits Revision No.03 of Service Bulletin No.A330-53-3226 ADDITIONAL WORK **CONF ALL No additional work is required by this revision for aircraft modified by any previous issue. REASON Revision No. 03 issued to incorporate changes found necessary and carried out during the accomplishment of this Service Bulletin on aircraft with Manufacturer Serial Number (MSN)s 0118 and 0083. NOTE : This revision satisfies the requirements of the subsequent Technical Adaptation(s) (TA) issued for the related MSN(s): TA MSN(s) 80251266/023/2018 0118 80084877/104/2017 0083 DATE: Jan 15/15 SERVICE BULLETIN No.: A330-53-3226 REVISION No.: 03 - Sep 10/18 Page: 1 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 2 @A330 SERVICE BULLETIN REVISION TRANSMITTAL SHEET 80226560/063/2018 0050, 0060, 0062, 0064-0065, 0071, 0083, 0099, 0102, 0109, 0112-0113, 0116, 0118, 0121-0122, 0138, 0140, 0143-0144, 0148, 0153, 0155, 0162, 0165, 0172, 0181, 0195, 0200, 0206, 0209, 0219, 0222-0224, 0226, 0229-0232, 0238, 0240-0241, 0244, 0247-0249, 0251, 0253, 0255-0256, 0258-0259, 0262, 0267, 0269, 0275-0277, 0279, 0281, 0283-0284, 0286-0288, 0290-0291, 0293-0296, 0299-0300, 0303, 0305-0306, 0308, 0311-0317, 0322-0324, 0326, 0328, 0330, 0333-0334, 0337-0338, 0340, 0342-0346, 0348, 0350-0351, 0358, 0361, 0364-0366, 0368, 0370, 0372, 0375, 0380, 0382, 0384, 0386, 0388-0389, 0392-0393, 0396-0398, 0400-0401, 0404, 0408-0409, 0412, 0418-0423, 0437, 0439, 0443, 0448, 0451-0452, 0455, 0458, 0462, 0465-0466, 0472-0473, 0477, 0481, 0486-0487, 0489, 0491, 0494, 0496-0498, 0500, 0502-0503, 0505-0511, 0513, 0515-0516, 0518-0519, 0521-0522, 0524-0527, 0529-0530, 0532-0533, 0535-0536, 0539, 0542, 0548-0549, 0552, 0555, 0565, 0567-0568, 0570-0571, 0573, 0576, 0578-0579, 0584, 0587-0588, 0591, 0600, 0605, 0609-0610, 0612, 0614, 0616, 0618, 0620-0621, 0623, 0625, 0629, 0631-0634, 0636-0638, 0640, 0642, 0644-0645, 0647-0650, 0652-0653, 0655-0657, 0659, 0661, 0663-0667, 0674, 0676, 0678-0679, 0682-0684, 0686-0687, 0690, 0693, 0696-0697, 0700-0701, 0703-0704, 0708-0709, 0713, 0717-0718, 0720, 0722, 0724, 0726, 0728-0730, 0732, 0735, 0737-0738, 0742-0743, 0746-0747, 0750-0751, 0754-0756, 0759-0760, 0770, 0772-0774, 0776-0778, 0780-0782, 0784-0785, 0788, 0791-0792, 0796-0797, 0799, 0801, 0803, 0806-0807, 0809-0811, 0815, 0817-0822, 0824-0825, 0827, 0830-0832, 0834, 0836, 0839-0843, 0845, 0849-0855, 0857-0860, 0862-0863, 0865-0869, 0871, 0873-0877, 0879, 0881-0885, 0887-0892, 0895-0896 and 0898-0901 DATE: Jan 15/15 SERVICE BULLETIN No.: A330-53-3226 REVISION No.: 03 - Sep 10/18 Page: 2 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 3 @A330 SERVICE BULLETIN REVISION TRANSMITTAL SHEET 80226560/063/2018 0903-0906, 0908-0909, 0913-0916, 0919, 0922-0923, 0925-0928, 0930, 0932, 0934-0937, 0939-0949, 0951, 0954, 0956-0959, 0961-0964, 0967-0970, 0973, 0975-0980, 0982-0984, 0986, 0988-0991, 0994-0998, 1000, 1002-1003, 1006-1007, 1009-1016, 1018-1020, 1022-1023, 1026, 1028-1029, 1031, 1033-1039, 1041-1047, 1049, 1052-1054, 1057, 1059-1061, 1063, 1067, 1069, 1071, 1073-1074, 1076, 1078, 1080-1082, 1084-1086, 1088-1090, 1093-1096, 1098-1101, 1104-1105, 1107-1108, 1112, 1114, 1116, 1118, 1120, 1123-1124, 1127, 1129, 1132-1133, 1135, 1137-1138, 1141, 1143, 1145-1147, 1149-1150, 1153, 1155-1157, 1159-1161, 1163, 1167-1174, 1178, 1181, 1183-1184, 1186, 1188-1192, 1196, 1198, 1200, 1202-1205, 1208-1210, 1212-1214, 1217-1230, 1233-1241, 1243-1246, 1248-1252, 1255-1256, 1258-1264, 1266-1267, 1269, 1271, 1275-1277, 1279-1283, 1285-1295, 1297-1298, 1300, 1302-1314, 1316-1319, 1322, 1324-1325, 1327, 1330-1331, 1334-1338, 1342-1343, 1347-1349, 1354-1355, 1358, 1362-1366, 1369, 1372, 1374-1375, 1377, 1379, 1381-1382, 1384-1385, 1387-1390, 1392-1405, 1407-1410, 1412, 1415-1417, 1419, 1421-1422, 1424-1427, 1429-1432, 1434, 1436-1441, 1443-1444, 1446-1447, 1451-1455, 1457-1459, 1461-1462, 1465-1466, 1468-1474, 1476-1480, 1483-1492, 1494, 1496-1503, 1505, 1507-1508, 1511-1517, 1519-1521, 1523, 1526, 1528-1530, 1532, 1535-1537, 1540, 1542-1545, 1547-1548, 1551, 1554-1558, 1560-1562, 1565, 1567, 1569, 1571-1577, 1579-1580, 1582, 1585-1586, 1588, 1590-1593, 1595, 1597-1599, 1601, 1603, 1605-1611, 1613-1618, 1620-1645, 1647-1649, 1651, 1653-1657, 1660, 1662-1668, 1671-1672, 1676-1679, 1681, 1686, 1694, 1696-1701, 1703-1704, 1706, 1709-1710, 1713-1716, 1718-1721, 1723, 1725, 1728, 1730, 1732-1733, 1735-1737, 1740-1741, 1745-1748, 1751, 1753-1763, 1769, 1771, 1773, 1775-1777, 1779-1780, 1782-1785, 1787-1788, 1792-1793, 1796, 1798-1799, 1801, 1804-1805, 1808-1809, 1814-1816, 1818, 1821-1822, 1825-1826 and 1847 DATE: Jan 15/15 SERVICE BULLETIN No.: A330-53-3226 REVISION No.: 03 - Sep 10/18 Page: 3 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 4 @A330 SERVICE BULLETIN REVISION TRANSMITTAL SHEET - Add CONF 005 - Update item number for Part Number (PN) EN6114K3X11 - Update item number for PN NSA9117-23 - Update typo error in . **CONF 001 SUBTASK 533226-831-214 001 Do the Modification of the RH Emergency Exit Door . **CONF 002 SUBTASK 533226-831-214 002 Do the Modification of the RH Emergency Exit Door . **CONF 003 SUBTASK 533226-831-214 003 Do the Modification of the RH Emergency Exit Door . **CONF 004 SUBTASK 533226-831-214 004 Do the Modification of the RH Emergency Exit Door. - Update item number in **CONF 001 thru 002, 005 Fig. A-GBAAA Sheet 04 - Update retrofitted modifications table to add CONF 005. CHANGES The main changes of this revision are: - PLANNING INFORMATION paragraph updated: . Effectivity updated . Effectivity note updated . Man-hours and elapsed time updated for CONF 003 and CONF 004 . Man-hours and elapsed time note updated . Weight and balance note updated. - MATERIAL INFORMATION paragraph updated: . Procurement address updated for Kit 533226D01R04, Kit 533226D02R05, Kit 533226D03R03, Kit 533226D04R03, Kit 533226D05R03, Kit 533226D06R02, Kit 533226D07R04, Kit 533226D08R04, Kit 533226D09R01, Kit 533226D10R01 and Kit 533226D11R02. . Description updated for Consumable . Industry support information updated. - ACCOMPLISHMENT INSTRUCTIONS paragraph updated: DATE: Jan 15/15 SERVICE BULLETIN No.: A330-53-3226 REVISION No.: 03 - Sep 10/18 Page: 4 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 5 @A330 SERVICE BULLETIN REVISION TRANSMITTAL SHEET . CAUTION note updated . Notes updated in Warning and caution section . Standard practices section updated . Note updated in Job Set-up section. FRONT MATTER FUSELAGE - CENTER FUSELAGE - REINFORCE CIRCUMFERENTIAL JOINT BETWEEN FR53.6-FR53.7 FOR EMERGENCY DOOR TYPE 1 AREA 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 UPDATED R MATERIAL PRICE INFORMATION TABLE UPDATED R MATERIAL PRICE INFORMATION TABLE ADDED N EFFECTIVITY OPERATOR LIST UPDATED R NATURE OF THE WORK NATURE OF WORK TABLE UPDATED R MANPOWER MANPOWER UPDATED R MANPOWER UPDATED R MANPOWER ADDED N APPENDICES APPENDICES UPDATED R Fig. A-GSAAA FIGURE SOLUTION UPDATED CONFIGURATION UPDATED R Fig. A-GSAAA Sheet 01 SHEET UPDATED R Fig. A-GSAAB Fig. A-GSAAB Sheet 01 SHEET UPDATED R PLANNING INFORMATION EFFECTIVITY EFFECTIVITY RELATED INFORMATION UPDATED R Configuration definition CONFIGURATION LIST UPDATED R CONF 001 CONFIGURATION DEFINITION UPDATED CONFIGURATION DESCRIPTION UPDATED R CONF 002 CONFIGURATION DEFINITION UPDATED CONFIGURATION DESCRIPTION UPDATED R CONF 003 CONFIGURATION DEFINITION UPDATED CONFIGURATION DESCRIPTION UPDATED R CONF 004 CONFIGURATION DEFINITION UPDATED CONFIGURATION DESCRIPTION UPDATED R DATE: Jan 15/15 SERVICE BULLETIN No.: A330-53-3226 REVISION No.: 03 - Sep 10/18 Page: 5 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 6 @A330 SERVICE BULLETIN REVISION TRANSMITTAL SHEET CONF 005 CONFIGURATION ADDED N Material Effectivity MATERIAL EFFECTIVITY ADDED N REASON Objective/Action OBJECTIVE/ACTION UPDATED R DESCRIPTION DESCRIPTION UPDATED R MANPOWER MANPOWER UPDATED R MANPOWER UPDATED R MANPOWER UPDATED R MANPOWER UPDATED R MANPOWER ADDED N WEIGHT AND BALANCE Minor editorial or document structure change R CONFIGURATION UPDATED R Minor editorial or document structure change R Minor editorial or document structure change R REFERENCES REFERENCED DOCUMENTATION UPDATED R REFERENCED DOCUMENTATION UPDATED R REFERENCED DOCUMENTATION UPDATED R REFERENCED DOCUMENTATION UPDATED R REFERENCED DOCUMENTATION ADDED N MATERIAL INFORMATION MATERIAL - PRICE AND AVAILABILITY Procurement Addresses PROCUREMENT ADDRESSES UPDATED MATERIAL SET UPDATED R Price and Availability PRICE AND AVAILABILITY UPDATED MATERIAL PRICE UPDATED MATERIAL AVAILABILITY UPDATED MATERIAL SET UPDATED R INDUSTRY SUPPORT INFORMATION INDUSTRY SUPPORT INFORMATION UPDATED R LIST OF COMPONENTS LIST OF COMPONENTS UPDATED R Kit 533226D01R04 PART MATERIAL SET UPDATED KEYWORD UPDATED ITEM NUMBER UPDATED PART NUMBER UPDATED QUANTITY UPDATED R Kit 533226D02R05 PART MATERIAL SET UPDATED KEYWORD UPDATED ITEM NUMBER UPDATED PART NUMBER UPDATED QUANTITY UPDATED R Kit 533226D03R03 PART MATERIAL SET UPDATED KEYWORD UPDATED ITEM NUMBER UPDATED PART NUMBER UPDATED QUANTITY UPDATED R DATE: Jan 15/15 SERVICE BULLETIN No.: A330-53-3226 REVISION No.: 03 - Sep 10/18 Page: 6 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 7 @A330 SERVICE BULLETIN REVISION TRANSMITTAL SHEET Kit 533226D04R03 PART MATERIAL SET UPDATED KEYWORD UPDATED ITEM NUMBER UPDATED PART NUMBER UPDATED QUANTITY UPDATED R Kit 533226D05R03 PART MATERIAL SET UPDATED KEYWORD UPDATED ITEM NUMBER UPDATED PART NUMBER UPDATED QUANTITY UPDATED R Kit 533226D06R02 PART MATERIAL SET UPDATED KEYWORD UPDATED ITEM NUMBER UPDATED PART NUMBER UPDATED QUANTITY UPDATED R Kit 533226D07R04 PART MATERIAL SET UPDATED KEYWORD UPDATED ITEM NUMBER UPDATED PART NUMBER UPDATED QUANTITY UPDATED R Kit 533226D08R04 PART MATERIAL SET UPDATED KEYWORD UPDATED ITEM NUMBER UPDATED PART NUMBER UPDATED QUANTITY UPDATED R Kit 533226D09R01 PART MATERIAL SET UPDATED KEYWORD UPDATED ITEM NUMBER UPDATED PART NUMBER UPDATED QUANTITY UPDATED R Kit 533226D10R01 PART MATERIAL SET UPDATED KEYWORD UPDATED ITEM NUMBER UPDATED PART NUMBER UPDATED QUANTITY UPDATED R Kit 533226D12R00 PART MATERIAL SET ADDED N Kit 533226D13R00 PART MATERIAL SET ADDED N LIST OF MATERIALS - OPERATOR SUPPLIED Consumable Materials Consumable CMLD01 CONSUMABLE MATERIAL SET UPDATED CONSUMABLE UPDATED QUANTITY UPDATED R PARTS TO BE RE-IDENTIFIED BY OPERATOR PARTS TO BE RE-IDENTIFIED BY OPERATOR UPDATED R TOOLING Tooling - Price and Availability Procurement Addresses PROCUREMENT ADDRESSES UPDATED R Tools TOOLS UPDATED R DATE: Jan 15/15 SERVICE BULLETIN No.: A330-53-3226 REVISION No.: 03 - Sep 10/18 Page: 7 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 8 @A330 SERVICE BULLETIN REVISION TRANSMITTAL SHEET Standard tool TOOLD01 TOOL MATERIAL SET UPDATED R Standard tool TOOLD02 TOOL MATERIAL SET UPDATED R Standard tool TOOLD04 TOOL MATERIAL SET UPDATED QUANTITY UPDATED R Standard tool TOOLD05 TOOL MATERIAL SET UPDATED QUANTITY UPDATED R ACCOMPLISHMENT INSTRUCTIONS TASK 533226- 831-848-001-Modification TASK SOLUTION UPDATED NOTE UPDATED CAUTION UPDATED R Task associated data - 003 ELAPSED TIME UPDATED R Task associated data - 004 ELAPSED TIME UPDATED R Task associated data - 005 TASK ASSOCIATED DATA ADDED N Subtask 533226-910-201-001 SUBTASK SOLUTION UPDATED REFERENCED DOCUMENTATION UPDATED R Subtask 533226-910-201-001 SUBTASK SOLUTION UPDATED REFERENCED DOCUMENTATION UPDATED R Subtask 533226-910-201-001 SUBTASK SOLUTION UPDATED REFERENCED DOCUMENTATION UPDATED R Subtask 533226-910-201-001 SUBTASK SOLUTION UPDATED REFERENCED DOCUMENTATION UPDATED R Subtask 533226-910-201-001 SUBTASK SOLUTION ADDED N Subtask 533226-839-201-001 SUBTASK SOLUTION ADDED N Subtask 533226-941-201-001 SUBTASK SOLUTION UPDATED NOTE UPDATED R Subtask 533226-941-201-001 SUBTASK SOLUTION UPDATED NOTE UPDATED R Subtask 533226-941-201-001 SUBTASK SOLUTION UPDATED NOTE UPDATED R Subtask 533226-941-201-001 SUBTASK SOLUTION UPDATED NOTE UPDATED R Subtask 533226-941-201-001 SUBTASK SOLUTION ADDED N Subtask 533226-010-201-001 SUBTASK SOLUTION ADDED N Subtask 533226-831-215-001 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED QUANTITY UPDATED MATERIAL LIST UPDATED R Subtask 533226-831-216-001 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED MATERIAL LIST UPDATED R Subtask 533226-831-218-001 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED REFERENCED DOCUMENTATION UPDATED MATERIAL LIST UPDATED R Subtask 533226-831-220-001 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED REFERENCED DOCUMENTATION UPDATED MATERIAL LIST UPDATED R DATE: Jan 15/15 SERVICE BULLETIN No.: A330-53-3226 REVISION No.: 03 - Sep 10/18 Page: 8 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 9 @A330 SERVICE BULLETIN REVISION TRANSMITTAL SHEET Subtask 533226-831-222-001 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED REFERENCED DOCUMENTATION UPDATED MATERIAL LIST UPDATED R Subtask 533226-831-224-001 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED REFERENCED DOCUMENTATION UPDATED MATERIAL LIST UPDATED R Subtask 533226-831-226-001 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED REFERENCED DOCUMENTATION UPDATED MATERIAL LIST UPDATED R Subtask 533226-831-228-001 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED REFERENCED DOCUMENTATION UPDATED MATERIAL LIST UPDATED R Subtask 533226-831-230-001 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED REFERENCED DOCUMENTATION UPDATED MATERIAL LIST UPDATED R Subtask 533226-831-232-001 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED REFERENCED DOCUMENTATION UPDATED MATERIAL LIST UPDATED R Subtask 533226-831-236-001 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED MATERIAL LIST UPDATED R Subtask 533226-831-237-001 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED MATERIAL LIST UPDATED R Subtask 533226-831-240-001 SUBTASK SOLUTION UPDATED KEYWORD UPDATED ITEM NUMBER UPDATED PART NUMBER UPDATED QUANTITY UPDATED CONSUMABLE UPDATED MATERIAL LIST UPDATED R Subtask 533226-831-243-001 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED MATERIAL LIST UPDATED R Subtask 533226-831-244-001 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED MATERIAL LIST UPDATED R Subtask 533226-831-247-001 SUBTASK SOLUTION UPDATED KEYWORD UPDATED ITEM NUMBER UPDATED PART NUMBER UPDATED QUANTITY UPDATED CONSUMABLE UPDATED MATERIAL LIST UPDATED R DATE: Jan 15/15 SERVICE BULLETIN No.: A330-53-3226 REVISION No.: 03 - Sep 10/18 Page: 9 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 10 @A330 SERVICE BULLETIN REVISION TRANSMITTAL SHEET Subtask 533226-831-250-001 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED NOTE UPDATED MATERIAL LIST UPDATED R Subtask 533226-831-251-001 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED CONFIGURATION UPDATED MATERIAL LIST UPDATED FIGURE REFERENCE UPDATED R Subtask 533226-831-213-001 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED MATERIAL LIST UPDATED R Subtask 533226-831-206-001 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED MATERIAL LIST UPDATED R Subtask 533226-831-212-001 SUBTASK SOLUTION UPDATED KEYWORD UPDATED ITEM NUMBER UPDATED PART NUMBER UPDATED QUANTITY UPDATED CONSUMABLE UPDATED MATERIAL LIST UPDATED R Subtask 533226-831-214-001 SUBTASK SOLUTION UPDATED KEYWORD UPDATED ITEM NUMBER UPDATED PART NUMBER UPDATED QUANTITY UPDATED CONSUMABLE UPDATED MATERIAL LIST UPDATED R Subtask 533226-831-215-001 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED QUANTITY UPDATED MATERIAL LIST UPDATED R Subtask 533226-831-216-001 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED MATERIAL LIST UPDATED R Subtask 533226-831-218-002 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED REFERENCED DOCUMENTATION UPDATED MATERIAL LIST UPDATED R Subtask 533226-831-220-002 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED REFERENCED DOCUMENTATION UPDATED MATERIAL LIST UPDATED R Subtask 533226-831-222-002 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED REFERENCED DOCUMENTATION UPDATED MATERIAL LIST UPDATED R DATE: Jan 15/15 SERVICE BULLETIN No.: A330-53-3226 REVISION No.: 03 - Sep 10/18 Page: 10 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 11 @A330 SERVICE BULLETIN REVISION TRANSMITTAL SHEET Subtask 533226-831-224-002 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED REFERENCED DOCUMENTATION UPDATED MATERIAL LIST UPDATED R Subtask 533226-831-227-002 SUBTASK SOLUTION UPDATED R Subtask 533226-831-226-002 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED REFERENCED DOCUMENTATION UPDATED MATERIAL LIST UPDATED R Subtask 533226-831-228-002 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED REFERENCED DOCUMENTATION UPDATED MATERIAL LIST UPDATED R Subtask 533226-831-230-002 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED REFERENCED DOCUMENTATION UPDATED MATERIAL LIST UPDATED R Subtask 533226-831-232-002 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED REFERENCED DOCUMENTATION UPDATED MATERIAL LIST UPDATED R Subtask 533226-831-236-002 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED MATERIAL LIST UPDATED R Subtask 533226-831-237-002 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED MATERIAL LIST UPDATED R Subtask 533226-831-240-002 SUBTASK SOLUTION UPDATED KEYWORD UPDATED ITEM NUMBER UPDATED PART NUMBER UPDATED QUANTITY UPDATED CONSUMABLE UPDATED MATERIAL LIST UPDATED R Subtask 533226-831-243-002 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED MATERIAL LIST UPDATED R Subtask 533226-831-244-002 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED MATERIAL LIST UPDATED R Subtask 533226-831-247-002 SUBTASK SOLUTION UPDATED KEYWORD UPDATED ITEM NUMBER UPDATED PART NUMBER UPDATED QUANTITY UPDATED CONSUMABLE UPDATED MATERIAL LIST UPDATED R DATE: Jan 15/15 SERVICE BULLETIN No.: A330-53-3226 REVISION No.: 03 - Sep 10/18 Page: 11 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 12 @A330 SERVICE BULLETIN REVISION TRANSMITTAL SHEET Subtask 533226-831-250-001 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED NOTE UPDATED MATERIAL LIST UPDATED R Subtask 533226-831-251-001 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED CONFIGURATION UPDATED MATERIAL LIST UPDATED FIGURE REFERENCE UPDATED R Subtask 533226-831-213-003 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED MATERIAL LIST UPDATED R Subtask 533226-831-212-002 SUBTASK SOLUTION UPDATED KEYWORD UPDATED ITEM NUMBER UPDATED PART NUMBER UPDATED QUANTITY UPDATED CONSUMABLE UPDATED MATERIAL LIST UPDATED R Subtask 533226-831-214-002 SUBTASK SOLUTION UPDATED KEYWORD UPDATED ITEM NUMBER UPDATED PART NUMBER UPDATED QUANTITY UPDATED CONSUMABLE UPDATED MATERIAL LIST UPDATED R Subtask 533226-831-215-001 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED QUANTITY UPDATED MATERIAL LIST UPDATED R Subtask 533226-831-216-001 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED MATERIAL LIST UPDATED R Subtask 533226-831-218-003 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED REFERENCED DOCUMENTATION UPDATED MATERIAL LIST UPDATED R Subtask 533226-831-220-003 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED REFERENCED DOCUMENTATION UPDATED MATERIAL LIST UPDATED R Subtask 533226-831-226-003 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED REFERENCED DOCUMENTATION UPDATED MATERIAL LIST UPDATED R Subtask 533226-831-228-003 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED REFERENCED DOCUMENTATION UPDATED MATERIAL LIST UPDATED R DATE: Jan 15/15 SERVICE BULLETIN No.: A330-53-3226 REVISION No.: 03 - Sep 10/18 Page: 12 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 13 @A330 SERVICE BULLETIN REVISION TRANSMITTAL SHEET Subtask 533226-831-236-003 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED MATERIAL LIST UPDATED R Subtask 533226-831-237-003 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED MATERIAL LIST UPDATED R Subtask 533226-831-240-003 SUBTASK SOLUTION UPDATED KEYWORD UPDATED ITEM NUMBER UPDATED PART NUMBER UPDATED QUANTITY UPDATED CONSUMABLE UPDATED MATERIAL LIST UPDATED R Subtask 533226-831-243-003 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED MATERIAL LIST UPDATED R Subtask 533226-831-244-003 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED MATERIAL LIST UPDATED R Subtask 533226-831-247-003 SUBTASK SOLUTION UPDATED KEYWORD UPDATED ITEM NUMBER UPDATED PART NUMBER UPDATED QUANTITY UPDATED CONSUMABLE UPDATED MATERIAL LIST UPDATED R Subtask 533226-831-250-001 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED NOTE UPDATED MATERIAL LIST UPDATED R Subtask 533226-831-251-001 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED CONFIGURATION UPDATED MATERIAL LIST UPDATED FIGURE REFERENCE UPDATED R Subtask 533226-831-212-003 SUBTASK SOLUTION UPDATED KEYWORD UPDATED ITEM NUMBER UPDATED PART NUMBER UPDATED QUANTITY UPDATED CONSUMABLE UPDATED MATERIAL LIST UPDATED R Subtask 533226-831-214-003 SUBTASK SOLUTION UPDATED KEYWORD UPDATED ITEM NUMBER UPDATED PART NUMBER UPDATED QUANTITY UPDATED CONSUMABLE UPDATED MATERIAL LIST UPDATED R DATE: Jan 15/15 SERVICE BULLETIN No.: A330-53-3226 REVISION No.: 03 - Sep 10/18 Page: 13 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 14 @A330 SERVICE BULLETIN REVISION TRANSMITTAL SHEET Subtask 533226-831-215-001 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED QUANTITY UPDATED MATERIAL LIST UPDATED R Subtask 533226-831-216-001 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED MATERIAL LIST UPDATED R Subtask 533226-831-218-004 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED REFERENCED DOCUMENTATION UPDATED MATERIAL LIST UPDATED R Subtask 533226-831-220-004 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED REFERENCED DOCUMENTATION UPDATED MATERIAL LIST UPDATED R Subtask 533226-831-226-004 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED REFERENCED DOCUMENTATION UPDATED MATERIAL LIST UPDATED R Subtask 533226-831-228-004 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED REFERENCED DOCUMENTATION UPDATED MATERIAL LIST UPDATED R Subtask 533226-831-236-004 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED MATERIAL LIST UPDATED R Subtask 533226-831-240-004 SUBTASK SOLUTION UPDATED KEYWORD UPDATED ITEM NUMBER UPDATED PART NUMBER UPDATED QUANTITY UPDATED CONSUMABLE UPDATED MATERIAL LIST UPDATED R Subtask 533226-831-243-004 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED MATERIAL LIST UPDATED R Subtask 533226-831-247-004 SUBTASK SOLUTION UPDATED KEYWORD UPDATED ITEM NUMBER UPDATED PART NUMBER UPDATED QUANTITY UPDATED CONSUMABLE UPDATED MATERIAL LIST UPDATED R Subtask 533226-831-250-001 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED NOTE UPDATED MATERIAL LIST UPDATED R DATE: Jan 15/15 SERVICE BULLETIN No.: A330-53-3226 REVISION No.: 03 - Sep 10/18 Page: 14 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 15 @A330 SERVICE BULLETIN REVISION TRANSMITTAL SHEET Subtask 533226-831-251-001 SUBTASK SOLUTION UPDATED CONSUMABLE UPDATED CONFIGURATION UPDATED MATERIAL LIST UPDATED FIGURE REFERENCE UPDATED R Subtask 533226-831-212-004 SUBTASK SOLUTION UPDATED KEYWORD UPDATED ITEM NUMBER UPDATED PART NUMBER UPDATED QUANTITY UPDATED CONSUMABLE UPDATED MATERIAL LIST UPDATED R Subtask 533226-831-214-004 SUBTASK SOLUTION UPDATED KEYWORD UPDATED ITEM NUMBER UPDATED PART NUMBER UPDATED QUANTITY UPDATED CONSUMABLE UPDATED MATERIAL LIST UPDATED R Subtask 533226-831-215-001 SUBTASK SOLUTION ADDED N Subtask 533226-831-216-001 SUBTASK SOLUTION ADDED N Subtask 533226-831-201-006 SUBTASK SOLUTION ADDED N Subtask 533226-831-207-004 SUBTASK SOLUTION ADDED N Subtask 533226-831-248-001 SUBTASK SOLUTION ADDED N Subtask 533226-831-249-001 SUBTASK SOLUTION ADDED N Subtask 533226-831-217-005 SUBTASK SOLUTION ADDED N Subtask 533226-832-209-005 SUBTASK SOLUTION ADDED N Subtask 533226-831-219-005 SUBTASK SOLUTION ADDED N Subtask 533226-832-210-005 SUBTASK SOLUTION ADDED N Subtask 533226-831-221-005 SUBTASK SOLUTION ADDED N Subtask 533226-832-211-005 SUBTASK SOLUTION ADDED N Subtask 533226-831-256-004 SUBTASK SOLUTION ADDED N Subtask 533226-832-218-004 SUBTASK SOLUTION ADDED N Subtask 533226-831-218-005 SUBTASK SOLUTION ADDED N Subtask 533226-831-220-005 SUBTASK SOLUTION ADDED N Subtask 533226-831-222-005 SUBTASK SOLUTION ADDED N Subtask 533226-831-224-005 SUBTASK SOLUTION ADDED N Subtask 533226-831-225-005 SUBTASK SOLUTION ADDED N Subtask 533226-832-213-005 SUBTASK SOLUTION ADDED N Subtask 533226-831-227-005 SUBTASK SOLUTION ADDED N Subtask 533226-832-214-005 SUBTASK SOLUTION ADDED N Subtask 533226-831-229-005 SUBTASK SOLUTION ADDED N Subtask 533226-832-215-005 SUBTASK SOLUTION ADDED N Subtask 533226-831-231-005 SUBTASK SOLUTION ADDED N Subtask 533226-832-216-005 SUBTASK SOLUTION ADDED N Subtask 533226-831-226-005 SUBTASK SOLUTION ADDED N Subtask 533226-831-228-005 SUBTASK SOLUTION ADDED N Subtask 533226-831-230-005 SUBTASK SOLUTION ADDED N DATE: Jan 15/15 SERVICE BULLETIN No.: A330-53-3226 REVISION No.: 03 - Sep 10/18 Page: 15 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 16 @A330 SERVICE BULLETIN REVISION TRANSMITTAL SHEET Subtask 533226-831-232-005 SUBTASK SOLUTION ADDED N Subtask 533226-831-233-005 SUBTASK SOLUTION ADDED N Subtask 533226-831-234-005 SUBTASK SOLUTION ADDED N Subtask 533226-831-235-005 SUBTASK SOLUTION ADDED N Subtask 533226-831-238-005 SUBTASK SOLUTION ADDED N Subtask 533226-831-239-005 SUBTASK SOLUTION ADDED N Subtask 533226-831-236-005 SUBTASK SOLUTION ADDED N Subtask 533226-831-237-005 SUBTASK SOLUTION ADDED N Subtask 533226-831-240-005 SUBTASK SOLUTION ADDED N Subtask 533226-831-241-006 SUBTASK SOLUTION ADDED N Subtask 533226-831-242-005 SUBTASK SOLUTION ADDED N Subtask 533226-832-217-005 SUBTASK SOLUTION ADDED N Subtask 533226-831-245-005 SUBTASK SOLUTION ADDED N Subtask 533226-831-246-005 SUBTASK SOLUTION ADDED N Subtask 533226-831-243-005 SUBTASK SOLUTION ADDED N Subtask 533226-831-244-005 SUBTASK SOLUTION ADDED N Subtask 533226-831-247-005 SUBTASK SOLUTION ADDED N Subtask 533226-831-252-001 SUBTASK SOLUTION ADDED N Subtask 533226-831-253-001 SUBTASK SOLUTION ADDED N Subtask 533226-831-254-001 SUBTASK SOLUTION ADDED N Subtask 533226-831-255-001 SUBTASK SOLUTION ADDED N Subtask 533226-831-250-001 SUBTASK SOLUTION ADDED N Subtask 533226-831-251-002 SUBTASK SOLUTION ADDED N Subtask 533226-831-213-004 SUBTASK SOLUTION ADDED N Subtask 533226-831-206-004 SUBTASK SOLUTION ADDED N Subtask 533226-831-212-005 SUBTASK SOLUTION ADDED N Subtask 533226-831-214-005 SUBTASK SOLUTION ADDED N Subtask 533226-710-201-001 SUBTASK SOLUTION ADDED N Subtask 533226-942-201-001 SUBTASK SOLUTION ADDED N Fig. A-GBAAA FIGURE SOLUTION UPDATED CONFIGURATION UPDATED R Fig. A-GBAAA Sheet 01 SHEET UPDATED R Fig. A-GBAAA Sheet 02 SHEET UPDATED R Fig. A-GBAAA Sheet 03 SHEET UPDATED R Fig. A-GBAAA Sheet 04 SHEET UPDATED R Fig. A-GBBAA Fig. A-GBBAA Sheet 01 SHEET UPDATED R Fig. A-GBBAA Sheet 02 SHEET UPDATED R Fig. A-GBBAA Sheet 03 SHEET UPDATED R Fig. A-GBBAA Sheet 04 SHEET UPDATED R Fig. A-GBBAA Sheet 05 SHEET UPDATED R Fig. A-GBBAA Sheet 06 SHEET UPDATED R Fig. A-GBBAA Sheet 07 SHEET UPDATED R Fig. A-GBBAA Sheet 08 SHEET UPDATED R Fig. A-GBBAA Sheet 09 SHEET UPDATED R DATE: Jan 15/15 SERVICE BULLETIN No.: A330-53-3226 REVISION No.: 03 - Sep 10/18 Page: 16 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 17 @A330 SERVICE BULLETIN REVISION TRANSMITTAL SHEET Fig. A-GBBAA Sheet 10 SHEET UPDATED R Fig. A-GBBAB FIGURE SOLUTION UPDATED CONFIGURATION UPDATED R Fig. A-GBBAB Sheet 01 SHEET UPDATED R Fig. A-GBBAB Sheet 02 SHEET UPDATED R Fig. A-GBBAB Sheet 03 SHEET UPDATED R Fig. A-GBBAB Sheet 04 SHEET UPDATED R Fig. A-GBBAB Sheet 05 SHEET UPDATED R Fig. A-GBBAB Sheet 06 SHEET UPDATED R Fig. A-GBBAB Sheet 07 SHEET UPDATED R Fig. A-GBBAB Sheet 08 SHEET UPDATED R Fig. A-GBBAB Sheet 09 SHEET UPDATED R Fig. A-GBBAB Sheet 10 SHEET UPDATED R Fig. A-GBBAC Fig. A-GBBAC Sheet 01 SHEET UPDATED R Fig. A-GBBAC Sheet 02 SHEET UPDATED R Fig. A-GBBAC Sheet 03 SHEET UPDATED R Fig. A-GBBAC Sheet 04 SHEET UPDATED R Fig. A-GBBAC Sheet 05 SHEET UPDATED R Fig. A-GBBAC Sheet 06 SHEET UPDATED R Fig. A-GBBAC Sheet 07 SHEET UPDATED R Fig. A-GBBAC Sheet 08 SHEET UPDATED R Fig. A-GBBAD Fig. A-GBBAD Sheet 01 SHEET UPDATED R Fig. A-GBBAD Sheet 02 SHEET UPDATED R Fig. A-GBBAD Sheet 03 SHEET UPDATED R Fig. A-GBBAD Sheet 04 SHEET UPDATED R Fig. A-GBBAD Sheet 05 SHEET UPDATED R Fig. A-GBBAD Sheet 06 SHEET UPDATED R Fig. A-GBBAD Sheet 07 SHEET UPDATED R Fig. A-GBCAA Fig. A-GBCAA Sheet 01 SHEET UPDATED R Fig. A-GBCAA Sheet 02 SHEET UPDATED R Fig. A-GBCAA Sheet 03 SHEET UPDATED R Fig. A-GBCAA Sheet 04 SHEET UPDATED R Fig. A-GBCAA Sheet 05 SHEET UPDATED R Fig. A-GBCAA Sheet 06 SHEET UPDATED R Fig. A-GBCAA Sheet 07 SHEET UPDATED R Fig. A-GBCAA Sheet 08 SHEET UPDATED R Fig. A-GBCAA Sheet 09 SHEET UPDATED R Fig. A-GBCAA Sheet 10 SHEET UPDATED R DATE: Jan 15/15 SERVICE BULLETIN No.: A330-53-3226 REVISION No.: 03 - Sep 10/18 Page: 17 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 18 @A330 SERVICE BULLETIN REVISION TRANSMITTAL SHEET Fig. A-GBCAA Sheet 11 SHEET UPDATED R Fig. A-GBCAB Fig. A-GBCAB Sheet 01 SHEET UPDATED R Fig. A-GBCAB Sheet 02 SHEET UPDATED R Fig. A-GBCAB Sheet 03 SHEET UPDATED R Fig. A-GBCAB Sheet 04 SHEET UPDATED R Fig. A-GBCAB Sheet 05 SHEET UPDATED R Fig. A-GBCAB Sheet 06 SHEET UPDATED R Fig. A-GBCAB Sheet 07 SHEET UPDATED R Fig. A-GBCAB Sheet 08 SHEET UPDATED R Fig. A-GBCAB Sheet 09 SHEET UPDATED R Fig. A-GBCAB Sheet 10 SHEET UPDATED R Fig. A-GBCAC Fig. A-GBCAC Sheet 01 SHEET UPDATED R Fig. A-GBCAC Sheet 02 SHEET UPDATED R Fig. A-GBCAC Sheet 03 SHEET UPDATED R Fig. A-GBCAC Sheet 04 SHEET UPDATED R Fig. A-GBCAC Sheet 05 SHEET UPDATED R Fig. A-GBCAC Sheet 06 SHEET UPDATED R Fig. A-GBCAC Sheet 07 SHEET UPDATED R Fig. A-GBCAC Sheet 08 SHEET UPDATED R Fig. A-GBCAD Fig. A-GBCAD Sheet 01 SHEET UPDATED R Fig. A-GBCAD Sheet 02 SHEET UPDATED R Fig. A-GBCAD Sheet 03 SHEET UPDATED R Fig. A-GBCAD Sheet 04 SHEET UPDATED R Fig. A-GBCAD Sheet 05 SHEET UPDATED R Fig. A-GBCAD Sheet 06 SHEET UPDATED R Fig. A-GBCAD Sheet 07 SHEET UPDATED R Fig. A-GBCAE FIGURE SOLUTION ADDED N Fig. A-GBCAE Sheet 01 SHEET ADDED N Fig. A-GBCAE Sheet 02 SHEET ADDED N Fig. A-GBCAE Sheet 03 SHEET ADDED N Fig. A-GBCAE Sheet 04 SHEET ADDED N Fig. A-GBCAE Sheet 05 SHEET ADDED N Fig. A-GBCAE Sheet 06 SHEET ADDED N Fig. A-GBCAE Sheet 07 SHEET ADDED N Fig. A-GBCAE Sheet 08 SHEET ADDED N Fig. A-GBCAE Sheet 09 SHEET ADDED N Fig. A-GBCAE Sheet 10 SHEET ADDED N Fig. A-GBCAE Sheet 11 SHEET ADDED N DATE: Jan 15/15 SERVICE BULLETIN No.: A330-53-3226 REVISION No.: 03 - Sep 10/18 Page: 18 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 19 @A330 SERVICE BULLETIN REVISION TRANSMITTAL SHEET Fig. A-GBCAE Sheet 12 SHEET ADDED N Fig. A-GBDAA Fig. A-GBDAA Sheet 01 SHEET UPDATED R Fig. A-GBDAA Sheet 02 SHEET UPDATED R Fig. A-GBDAA Sheet 03 SHEET UPDATED R Fig. A-GBDAA Sheet 04 SHEET UPDATED R Fig. A-GBEAA Fig. A-GBEAA Sheet 01 SHEET UPDATED R Fig. A-GBEAA Sheet 02 SHEET UPDATED R Appendix 01 - Manpower Gantt Chart APPENDIX CONTENT APPENDIX CONTENT ADDED N Fig. A-GAAAA FIGURE SOLUTION UPDATED CONFIGURATION UPDATED R Fig. A-GAAAB FIGURE SOLUTION UPDATED CONFIGURATION UPDATED R Fig. A-GAAAB Sheet 01 SHEET UPDATED R Fig. A-GAAAC FIGURE SOLUTION ADDED N Fig. A-GAAAC Sheet 01 SHEET ADDED N Appendix 04 - Retrof itted Modifications APPENDIX CONTENT APPENDIX CONTENT UPDATED R FILING INSTRUCTIONS This Service Bulletin has been generated electronically and is reissued as a complete document. Replace the complete document. Put this Revision Transmittal Sheet in front of the Service Bulletin. HISTORY OF PREVIOUS REVISIONS Revision No. 01 issued to: change compliance from Recommended to Mandatory, add compliance time table in paragraph accomplishment timescale, remove the FTI tool kits TOOLD06, TOOLD08, TOOLD09, TOOLD10, TOOLD11, TOOLD12, TOOLD13, TOOLD14, TOOLD15, TOOLD16 and TOOLD17. Revision No. 02 issued to: Reintroduce the jacking procedure Add the procedure to rework the tooling holes at the existing inner doublers at the lower door frame area Add the minimum allowable edge margins for the shims installation at the upper door area DATE: Jan 15/15 SERVICE BULLETIN No.: A330-53-3226 REVISION No.: 03 - Sep 10/18 Page: 19 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 20 @A330 SERVICE BULLETIN REVISION TRANSMITTAL SHEET Update the kits to correct the grip length of some fasteners. REVISION SEQUENCE ORIGINAL: Jan 15/15 REVISION No. : 01 - Mar 03/16 REVISION No. : 02 - Oct 27/16 REVISION No. : 03 - Sep 10/18 DATE: Jan 15/15 SERVICE BULLETIN No.: A330-53-3226 REVISION No.: 03 - Sep 10/18 Page: 20 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 21 @A330 SERVICE BULLETIN SUMMARY AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE T e l:( 3 3 )56 19 33 33 3 Telex : AIRBU 530526F F a x:( 3 3 )56 19 34 25 1 This summary is for information only and is not approved for modification of the aircraft. MANDATORY MANDATORY MANDATORY ATA SYSTEM: 53 TITLE: FUSELAGE - CENTER FUSELAG E - REINFORCE CIRCUMFERENTIAL JOINT BETWEEN FR53.6-FR53.7 FOR EMERGENCY DOOR TYPE 1 AREA **CONF ALL MODIFICATIONS MODIFICATION CLASSIFICATION MAJOR 204309D50888 204309D50892 204309D50893 204309D50904 MINOR None NOTE : As per EASA IR 21, a minor change is one that has no appreciable effect on the mass, balance, structural strength, reliability, operational characteristics affecting the airworthiness of the product. All other changes are major changes. REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES Following Widespread Fatigue Damage (WFD) analysis, it has been demonstrated that some structural areas require reinforcements before reaching the Design Service Goal (DSG). The circumferential joint between Frames (FR) Frame 53.6 and Frame 53.7 of emergency exit door type 1 has been identified as such area. This modification comprises the structural reinforcement as follows: - For aircraft in Config. 001: . install external, circumferential doubler between Frame 53.6 and Frame 53.7, STGR4-30 LH/RH . install additional shim for door cover plate . install additional shim for 0 deg aligned rain gutter . install modified scuff plate due to external doubler . install additional cold worked holes (rivet with interference fit) at upper and lower door frame shell. DATE: Jan 15/15 SERVICE BULLETIN No.: A330-53-3226 REVISION No.: 03 - Sep 10/18 Page: 1 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 22 @A330 SERVICE BULLETIN SUMMARY - For aircraft in Config. 002: . install external, circumferential doubler between Frame 53.6 and Frame 53.7, STGR4-30 LH/RH . install additional shim for door cover plate . install additional shim for 5 deg aligned rain gutter . install modified scuff plate due to external doubler - For aircraft in Config. 003: . install external, circumferential doubler between Frame 53.6 and Frame 53.7, STGR4-30 LH/RH . install additional shim for door cover plate . install additional shim for 5 deg aligned rain gutter - For aircraft in Config. 004: . install external, circumferential doubler between Frame 53.6 and Frame 53.7, STGR4-29 LH/RH . install additional shim for door cover plate - For aircraft in Config. 005: . install external, circumferential doubler between Frame 53.6 and Frame 53.7, STGR4-30 LH/RH . install additional shim for door cover plate . install additional shim for 5 deg aligned rain gutter . install modified scuff plate due to external doubler The accomplishment of this Service Bulletin will improve the fatigue life of the circumferential joint between Frame 53.6 and Frame 53.7, STGR4-30 LH/RH. This Service Bulletin is based on the aircraft configuration as known by AIRBUS (first aircraft delivery configuration and modified by the reported incorporation of AIRBUS Service Bulletins). Prior to Service Bulletin embodiment, specific attention must be paid to structural damage which may exist and to repairs which were performed on the aircraft because they may be affected by the Service Bulletin. It must be verified that all allowable damage limits and repairs performed (both in accordance with the SRM and outside of the SRM) are still applicable and effective to the new Service Bulletin configuration. There may be additional or modified maintenance requirements, such as temporary limits or additional inspections that apply with respect to the Service Bulletin configuration. There may be additional or modified maintenance requirements, such as temporary limits or additional inspections that apply with respect to the Service Bulletin configuration. DATE: Jan 15/15 SERVICE BULLETIN No.: A330-53-3226 REVISION No.: 03 - Sep 10/18 Page: 2 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 23 @A330 SERVICE BULLETIN SUMMARY AIRBUS disclaims any liability for the effect which the Service Bulletin may have on repairs performed on the aircraft before embodiment of the Service Bulletin. If the post Service Bulletin repair status is not covered by the SRM and for repairs outside of the SRM covered by a RAS issued by AIRBUS, AIRBUS Customer Services Repair Engineering Support (SEOE) should be contacted. Repair review will be done by AIRBUS at conditions of the Customer Services Catalogue. 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 YES VENDOR SB INVOLVED NO SPECIAL JACKING YES DE-FUELLING/VENTILATION YES NOTE (1) : Service Bulletin must be accomplished. MATERIAL PRICE INFORMATION **CONF 001 MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Kit 533226D01R04 1 21,020.00 Doublers, Shims, Plates, Nuts, Bolts, Screws, Washers Kit 533226D05R03 1 21,020.00 Shims, Doublers, Plates, Nuts, Bolts, Screws, Washers, Rivets Kit 533226D09R01 1 582.00 Shim, Screw, Nut, Rivets and Plate Kit 533226D10R01 1 582.00 Shim, Screw, Nut, Rivets and Plate Kit 533226D11R02 1 265.00 Bolts, Rivets TOTAL 43,469.00 Standard tool TOOLD01 1 See SB FTI Capital Tooling Standard tool TOOLD02 1 See SB FTI Durable Tooling Standard tool TOOLD03 1 See SB FTI Expendable Tooling **CONF 002 MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Kit 533226D02R05 1 20,860.00 Shims, Doublers, Plates, Nuts, Bolts, Screws, Washers, Rivets Kit 533226D06R02 1 20,860.00 Shims, Doublers, Plates, Nuts, Bolts, Screws, Washers, Rivets Kit 533226D09R01 1 582.00 Shim, Screw, Nut, Rivets and Plate DATE: Jan 15/15 SERVICE BULLETIN No.: A330-53-3226 REVISION No.: 03 - Sep 10/18 Page: 3 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 24 @A330 SERVICE BULLETIN SUMMARY MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Kit 533226D10R01 1 582.00 Shim, Screw, Nut, Rivets and Plate Kit 533226D11R02 1 265.00 Bolts, Rivets TOTAL 43,149.00 Standard tool TOOLD01 1 See SB FTI Capital Tooling Standard tool TOOLD04 1 See SB FTI Durable Tooling Standard tool TOOLD05 1 See SB FTI Expendable Tooling **CONF 003 MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Kit 533226D03R03 1 17,210.00 Shims, Doublers, Nuts, Bolts, Rivets Kit 533226D07R04 1 17,210.00 Shims, Doublers, Plates, Nuts, Bolts, Screws, Washers, Rivets Kit 533226D09R01 1 582.00 Shim, Screw, Nut, Rivets and Plate Kit 533226D10R01 1 582.00 Shim, Screw, Nut, Rivets and Plate Kit 533226D11R02 1 265.00 Bolts, Rivets TOTAL 35,849.00 Standard tool TOOLD01 1 See SB FTI Capital Tooling Standard tool TOOLD04 1 See SB FTI Durable Tooling Standard tool TOOLD07 1 See SB FTI Expendable Tooling **CONF 004 MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Kit 533226D04R03 1 17,210.00 Shims, Doublers, Nuts, Bolts Kit 533226D08R04 1 17,210.00 Shims, Doublers, Plates, Nuts, Bolts, Screws, Washers, Rivets Kit 533226D09R01 1 582.00 Shim, Screw, Nut, Rivets and Plate Kit 533226D10R01 1 582.00 Shim, Screw, Nut, Rivets and Plate Kit 533226D11R02 1 265.00 Bolts, Rivets TOTAL 35,849.00 Standard tool TOOLD01 1 See SB FTI Capital Tooling Standard tool TOOLD04 1 See SB FTI Durable Tooling Standard tool TOOLD07 1 See SB FTI Expendable Tooling DATE: Jan 15/15 SERVICE BULLETIN No.: A330-53-3226 REVISION No.: 03 - Sep 10/18 Page: 4 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 25 @A330 SERVICE BULLETIN SUMMARY **CONF 005 MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Kit 533226D12R00 1 20,900.00 Shims, Doublers, Plates, Nuts, Bolts, Screws, Washers, Rivets Kit 533226D13R00 1 20,900.00 Shims, Doublers, Plates, Nuts, Bolts, Screws, Washers, Rivets Kit 533226D09R01 1 582.00 Shim, Screw, Nut, Rivets and Plate Kit 533226D10R01 1 582.00 Shim, Screw, Nut, Rivets and Plate Kit 533226D11R02 1 265.00 Bolts, Rivets TOTAL 43,229.00 Standard tool TOOLD01 1 See SB FTI Capital Tooling Standard tool TOOLD04 1 See SB FTI Durable Tooling Standard tool TOOLD05 1 See SB FTI Expendable Tooling EFFECTIVITY **CONF ALL This Service Bulletin is applicable to this (these) operator(s) : 01Q 12P 18Q 36P 38W 39V 41N 46O 56O 57L 64N 83V 87Z 97X AAL AAR AAW ABR ACA ACI AEA AFL AFR AIB ALD ALK ARG ASL ASY AVA AZA AZU BEC BEL BOS CBJ CCA CES CHH CPA CRK CSC CSN D2F DAH DAL DGA DLH EIN ETD EVA F2I FAF FIN FJI FWI G8E GCR GFA GIA GRL HAL HDA HFY HVN IBE IRA ISS JAI JAV KAC KAL KLM LAA LMU MAS MAU MEA MLM MSR NMB NWS OHY OMA ONE P2C QAF QFA QTR RNA RSF RSY RWD RZO SAA SAF SAI SAS SIA SVA SWR SXD TAE TAM TAP TAR TBA TCX THA THY TOW TSC U6A UAE UAF VIR VOZ WOW WRC XAX CONCURRENT REQUIREMENTS None REFERENCES / REPERCUSSIONS TFU None OEB None AOT None SIL 51-012 ISI None LINE MAINTENANCE AFFECTED No LIFE LIMIT None OTHER None DATE: Jan 15/15 SERVICE BULLETIN No.: A330-53-3226 REVISION No.: 03 - Sep 10/18 Page: 5 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 26 @A330 SERVICE BULLETIN SUMMARY NATURE OF THE WORK AIRCRAFT YES EQUIPMENT NO MANPOWER **CONF 001 Task 533226-831-848-001: Modification TOTAL MANHOURS 317.00 ELAPSED TIME (HOURS) 69.00 **CONF 002 Task 533226-831-848-001: Modification TOTAL MANHOURS 317.00 ELAPSED TIME (HOURS) 69.00 **CONF 003 Task 533226-831-848-001: Modification TOTAL MANHOURS 266.00 ELAPSED TIME (HOURS) 56.25 **CONF 004 Task 533226-831-848-001: Modification TOTAL MANHOURS 256.00 ELAPSED TIME (HOURS) 53.75 **CONF 005 Task 533226-831-848-001 : Modification TOTAL MANHOURS 317.00 ELAPSED TIME (HOURS) 69.00 APPENDICES **CONF ALL Appendix 01 - Manpower Gantt Chart Appendix 02 - Zero Stress Jacking Appendix 03 - Re-identification of the Emergency Exit Doors Appendix 04 - Retrofitted Modifications DATE: Jan 15/15 SERVICE BULLETIN No.: A330-53-3226 REVISION No.: 03 - Sep 10/18 Page: 6 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 27 @A330 SERVICE BULLETIN SUMMARY **CONF 001 thru 002, 005 STGR26 STGR30 FR53.5 A FR53.7B STGR4 FR50 FR72 A Z260 REINFORCEMENT OF CIRCUMFERENTIAL JOINT BY INTRODUCING DOUBLER AND SHIM G_SB_533226_6_SAAA_01_02 Figure A-GSAAA - Sheet 01 DATE: Jan 15/15 SERVICE BULLETIN No.: A330-53-3226 REVISION No.: 03 - Sep 10/18 Page: 7 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 28 @A330 SERVICE BULLETIN SUMMARY **CONF 003 thru 004 STGR26 STGR30 FR53.5 A FR53.7B STGR4 FR50 FR72 A Z260 REINFORCEMENT OF CIRCUMFERENTIAL JOINT BY INTRODUCING DOUBLER G_SB_533226_6_SAAB_01_02 Figure A-GSAAB - Sheet 01 DATE: Jan 15/15 SERVICE BULLETIN No.: A330-53-3226 REVISION No.: 03 - Sep 10/18 Page: 8 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 29 @A330 SERVICE BULLETIN AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE T e l:( 3 3 )56 19 33 33 3 Telex : AIRBU 530526F F a x:( 3 3 )56 19 34 25 1 MANDATORY MANDATORY MANDATORY ATA SYSTEM: 53 TITLE: FUSELAGE - CENTER FUSELAG E - REINFORCE CIRCUMFERENTIAL JOINT BETWEEN FR53.6-FR53.7 FOR EMERGENCY DOOR TYPE 1 AREA MODIFICATION No.: 204309D50888 204309D50892 204309D50893 204309D50904 This document contains AIRBUS PROPRIETARY INFORMATION and shall at all times remain the property of AIRBUS; no intellectual property right or licence is granted by AIRBUS in connection with any information contained in it. It is delivered on the express condition that said document and the information contained in it shall be treated as confidential, shall not be used for any purpose other than that for which it is hereby delivered. It shall not be disclosed in whole or in part to third parties and shall not be duplicated in any manner (except for the purposes of performing the tasks described hereunder and provided that any recipient of such document shall comply with the conditions herein), without AIRBUS prior written consent. 1. PLANNING INFORMATION **CONF ALL A. EFFECTIVITY NOTE : This Service Bulletin is applicable on aircraft on which MOD No. 40161D17512 has not been embodied. NOTE : This Service Bulletin is applicable to aircraft on which MOD No. 206136D52210, MOD No. 206136D52225, MOD No. 206136D52226 and MOD No. 206136D52227 (Service Bulletin No. A330-53-3273) are not embodied. (1) Models 330-202 330-203 330-223 330-243 330-301 330-302 330-303 330-321 330-322 330-323 330-341 330-342 330-343 (2) Effectivity by MSN 0050 0060 0062 0065 0071 0083 0099 0102 0109 0112-0113 0116 0118 0121-0122 0138 0140 0143-0144 0148 0153 0155 0162 0165 0172 0181 0195 0200 0206 0209 0219 0222-0224 0226 0229-0232 0238 0240-0241 0244 0247-0249 0251 0253 0255-0256 0258-0259 0262 0267 0269 0275-0277 0279 0281 0283-0284 0286-0288 DATE: Jan 15/15 SERVICE BULLETIN No.: A330-53-3226 REVISION No.: 03 - Sep 10/18 Page: 1 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 30 @A330 SERVICE BULLETIN 0290-0291 0293 0295-0296 0300 0303 0305-0306 0308 0311-0317 0322-0324 0326 0328 0330 0333-0334 0337-0338 0340 0342-0346 0348 0350-0351 0358 0361 0364-0366 0368 0370 0372 0375 0380 0382 0384 0386 0388-0389 0392-0393 0396-0398 0400-0401 0404 0408-0409 0412 0418-0423 0437 0439 0443 0448 0451-0452 0455 0458 0462 0465-0466 0472-0473 0477 0481 0486-0487 0489 0491 0494 0496-0498 0500 0502-0503 0505-0511 0513 0515-0516 0518-0519 0521-0522 0524-0527 0529-0530 0532-0533 0535-0536 0539 0542 0548-0549 0552 0555 0565 0567-0568 0570-0571 0573 0576 0578-0579 0584 0587-0588 0591 0600 0605 0609-0610 0612 0614 0616 0618 0620-0621 0623 0625 0629 0631-0634 0636-0638 0640 0642 0644-0645 0647-0650 0652-0653 0655-0657 0659 0661 0663-0667 0674 0676 0678-0679 0682-0684 0686-0687 0690 0693 0696-0697 0700-0701 0703-0704 0708-0709 0713 0717-0718 0720 0722 0724 0726 0728-0730 0732 0735 0737-0738 0742-0743 0746-0747 0750-0751 0754-0756 0759-0760 0770 0772-0774 0776-0778 0780-0782 0784-0785 0788 0791-0792 0796-0797 0799 0801 0803 0806-0807 0809-0811 0815 0817-0822 0824-0825 0827 0830-0832 0834 0836 0839-0843 0845 0849-0855 0857-0860 0862-0863 0865-0869 0871 0873-0877 0879 0881-0885 0887-0892 0895-0896 0898-0901 0903-0906 0908-0909 0913-0916 0919 0922-0923 0925-0928 0930 0932 0934-0937 0939-0949 0951 0954 0956-0959 0961-0964 0967-0970 0973 0975-0980 0982-0984 0986 0988-0991 0994-0998 1000 1002-1003 1006-1007 1009-1016 1018-1020 1022-1023 1026 1028-1029 1031 1033-1039 1041-1047 1049 1052-1054 1057 1059-1061 1063 1067 1069 1071 1073-1074 1076 1078 1080-1082 1084-1086 1088-1090 1093-1096 1098-1101 1104-1105 1107-1108 1112 1114 1116 1118 1120 1123-1124 1127 1129 1132-1133 1135 1137-1138 1141 1143 1145-1147 1149-1150 1153 1155-1157 1159-1161 1163 1167-1174 1178 1181 1183-1184 1186 1188-1192 1196 1198 1200 1202-1205 1208-1210 1212-1214 1217-1230 1233-1241 1243-1246 1248-1252 1255-1256 1258-1264 1266-1267 1269 1271 1275-1277 1279-1283 1285-1295 1297-1298 1300 1302-1314 1316-1319 1322 1324-1325 1327 1330-1331 1334-1338 1342-1343 1347-1349 1354-1355 1358 1362-1366 1369 1372 1374-1375 1377 1379 1381-1382 1384-1385 1387-1390 1392-1405 1407-1410 1412 1415-1417 1419 1421-1422 1425-1427 1429-1432 1434 1436-1441 1443-1444 1446-1447 1451-1455 1457-1459 1461-1462 1465-1466 1468-1474 1476-1480 1483-1492 1494 1496-1503 1505 1507-1508 1511-1517 1519-1521 1523 1526 1528-1530 1532 1535-1537 1540 1542-1545 1547-1548 1551 1554-1558 1560-1562 1565 1567 1569 1571-1577 1579-1580 1582 1585-1586 1588 1590-1593 1595 1597-1599 1601 1603 1605-1611 1613-1618 1620-1645 1647-1649 1651 1653-1657 1660 1662-1668 1671-1672 1676-1679 1681 1686 1694 1696-1701 1703-1704 1706 1709-1710 1713-1716 1718-1721 1723 1725 1728 1730 1732-1733 1735-1737 1740-1741 1745-1748 1751 1753-1763 1769 1771 1773 1775-1777 1779-1780 1782-1785 1787-1788 1792-1793 1796 1798-1799 1801 1804-1805 1808-1809 1814-1816 1818 1821-1823 1825-1826 1830 1833 1835 1841-1842 1845-1848 1852 1854 1856-1859 1864 1868-1869 1872-1873 1877-1878 1881-1883 1885-1886 1891 1894 1905 1911-1912 1916 1919 1928 1932 1936 (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 01Q 1830 12P 1787 1848 1883 1891 DATE: Jan 15/15 SERVICE BULLETIN No.: A330-53-3226 REVISION No.: 03 - Sep 10/18 Page: 2 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 31 @A330 SERVICE BULLETIN OPERATOR MSN 18Q 1019 36P 1911 1919 38W 0401 39V 0255 41N 1676 46O 0655 56O 0231 57L 0735 64N 1751 83V 0366 87Z 0535 97X 1053 AAL 0315 0323 0333 0337 0342 0370 0375 0380 0388 1011 1022 1041 1069 1076 1095 1100 1415 1417 1441 1455 1480 1502 1512 1526 AAR 0640 0676 0708 0772 0803 0845 AAW 1043 1472 1535 ABR 0116 ACA 0277 0279 0284 0344 0400 0408 0412 0419 ACI 0507 0510 AEA 0505 0526 1574 AFL 0963 0973 1014 1045 1047 1264 AFR 0422 0443 0448 0458 0465 0481 0498 0500 0502 0503 0516 0519 0567 0584 0657 AIB 0871 ALD 0326 0328 0392 ALK 0303 0306 0311 0313 ARG 0290 0300 0358 0364 0587 0634 1605 1623 1737 1748 ASL 0885 ASY 0747 0892 0898 0951 0969 1036 1183 AVA 1009 1016 1073 1224 1279 1342 1400 AZA 0825 0831 1123 1135 1218 1225 1252 1283 1308 1313 1327 1354 AZU 0365 0372 0462 0494 0527 0529 0532 BEC 0863 BEL 0229 0249 0291 0324 0895 0915 0959 1010 1085 BOS 1864 1882 CBJ 0988 1020 1028 1052 1753 1763 1775 1782 1847 CCA 0750 0756 0759 0780 0785 0797 0810 0815 0839 0860 0867 0873 0884 0890 0903 0909 0930 0941 0944 0957 1237 1260 1282 1304 1330 1396 1434 1444 1459 1471 CES 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 1617 1632 1639 1655 1664 1788 1796 1798 1801 1804 1809 1816 1833 1841 1842 1868 1869 1873 1881 1905 CHH 0875 0881 0906 0919 0982 1159 1168 1178 1190 1255 1325 1438 1532 1558 1573 1591 1614 1634 1656 1663 1677 1686 1703 DATE: Jan 15/15 SERVICE BULLETIN No.: A330-53-3226 REVISION No.: 03 - Sep 10/18 Page: 3 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 32 @A330 SERVICE BULLETIN OPERATOR MSN CPA 0102 0113 0121 0386 0389 0393 0418 0420 0421 0423 0439 0539 0548 0565 0679 0776 0850 0855 1163 1196 1222 1239 1285 1317 1343 1349 1362 1366 1387 1409 1436 1443 1618 1621 CRK 0396 0452 1031 1034 1039 1042 1054 1059 1099 1105 1107 1124 1146 1157 1277 1286 1322 1358 1369 1384 1398 1668 CSC 1082 1138 1241 1397 1432 1528 1579 1662 1746 1780 1825 1856 1912 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 1776 1793 1814 1815 1818 1821 1826 1846 1852 1858 1885 1894 D2F 0209 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 1769 1783 DGA 0240 DLH 0570 0576 0579 0629 0636 0642 0645 0648 0687 0701 0896 0905 0913 0922 0989 1292 1305 1314 1497 EIN 0269 0330 0397 0841 ETD 0717 0724 0729 0730 0737 0788 0809 0824 0832 0852 0854 0868 0975 0991 1071 1081 1167 1205 1226 1245 1486 1521 EVA 0678 0693 0755 F2I 0200 0275 FAF 1735 1808 1916 FIN 0994 1007 1013 1023 1067 1078 1088 1173 FJI 0751 0807 1394 1416 1465 FWI 0253 0343 G8E 0288 GCR 1756 1758 1773 1805 GFA 0276 0281 0286 0287 0334 0340 GIA 0138 0140 0144 0148 0153 0165 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 1823 HDA 0071 0083 0099 0109 0118 0155 0244 1457 1503 1523 1545 1557 1567 1598 HFY 0262 HVN 0943 0962 1256 1266 IBE 1377 1385 1405 1426 1437 1490 1507 1515 1694 1700 1710 1719 1728 1736 1740 1747 1755 1761 1777 1784 1835 1854 1877 1932 1936 IRA 1540 1586 ISS 0521 0571 JAI 0888 0923 0947 0956 DATE: Jan 15/15 SERVICE BULLETIN No.: A330-53-3226 REVISION No.: 03 - Sep 10/18 Page: 4 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 33 @A330 SERVICE BULLETIN OPERATOR MSN JAV 0409 KAC 1626 1643 1653 1678 1681 KAL 0162 0172 0206 0219 0222 0226 0241 0256 0258 0267 0338 0350 0351 0368 1133 1155 1200 1203 1393 1556 1576 1590 1611 1638 1647 KLM 0682 0686 0703 0738 0770 0801 0925 1161 1287 1294 1300 1381 1580 LAA 1412 1505 1543 LMU 0661 MAS 0665 0822 0968 1112 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 MSR 0600 0610 0666 0683 0696 0709 0726 1143 1230 1238 1246 NMB 1451 1466 NWS 0979 1002 OHY 0316 0345 0404 0437 0491 0509 0525 0625 0632 OMA 1038 1044 1049 1063 1093 1120 1227 1572 1582 1599 ONE 1208 1492 1508 1608 1657 P2C 0891 0927 QAF 0487 0605 QFA 0506 0508 0513 0522 0842 0853 0887 0940 0945 0976 1061 1094 1169 1174 1198 1251 1258 1365 QTR 0473 0489 0511 0623 0637 0638 0659 0743 0746 0760 0792 0820 0849 RNA 1872 1878 RSF 0980 0996 1235 1379 1478 1516 RSY 0283 0293 0295 0472 0700 0946 RWD 1741 1759 RZO 0970 SAA 1191 1210 1223 1236 1249 1271 1745 1754 1757 1779 1792 SAF 1667 1762 1799 1822 1857 1886 SAI 0811 0819 0834 0900 SAS 0496 0497 0515 0568 1660 1665 1697 1715 1928 SIA 0978 0983 0986 1132 1149 1156 1382 1401 1427 1447 1453 1477 1485 1517 1544 1562 1597 1609 1633 1648 1666 SVA 1108 1127 1137 1141 1147 1153 1189 1192 1454 1462 1473 1513 SWR 1000 1018 1026 1029 1084 1089 1101 1145 1181 1188 1276 1290 1355 1403 SXD 0530 0555 0573 0612 0616 0684 TAE 0348 TAM 0232 0238 0247 0259 0361 0466 TAP 0181 0195 0223 0305 0308 0312 0317 0477 0486 0877 0899 0904 0914 0934 0997 1006 1012 1015 TAR 1631 1641 TBA 1730 1771 1785 1845 1859 DATE: Jan 15/15 SERVICE BULLETIN No.: A330-53-3226 REVISION No.: 03 - Sep 10/18 Page: 5 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 34 @A330 SERVICE BULLETIN OPERATOR MSN TCX 0398 0948 0967 THA 0050 0060 0062 0112 0122 0346 0990 1003 1035 1037 1060 1074 1086 1090 1263 1269 1289 1338 1348 1374 1408 THY 0697 0704 0742 0754 0774 0869 0874 0876 0882 0901 0932 0939 0949 0961 0977 1118 1150 1160 1170 1172 1204 1212 1213 1221 1228 1240 1298 1307 1311 1458 1476 1483 1487 1491 1499 1501 1514 1529 1542 1554 1571 1592 1616 1620 1622 1629 1635 1640 1642 1644 1651 1696 1704 1706 1713 1718 TOW 1033 1046 1248 1275 1312 1334 1363 1390 1419 1439 1498 1555 1601 1610 TSC 0248 0251 0314 0455 0518 0536 0728 0732 U6A 0065 0143 0224 UAE 0382 0384 UAF 1080 1186 1250 VIR 0322 VOZ 1293 1306 1319 1407 1452 1561 WOW 1098 1607 1624 WRC 0296 XAX 0713 0720 (4) Configuration by MSN MSN CONFIGURATION 0050 0060 0062 0065 0071 0083 0099 0102 0109 0112 001 0113 0116 0118 0121 0122 005 0138 0140 0143 0144 0148 0153 0155 0162 0165 0172 0181 0195 0200 0206 0209 0219 0222 0223 0224 0226 0229 0230 0231 0232 0238 0240 0241 0244 0247 0248 0249 0251 0253 0255 0256 0258 0259 0262 0267 0269 0275 0276 0277 0279 0281 0283 0284 0286 0287 0288 0290 0291 0293 0295 0296 0300 0303 0305 0306 0308 0311 0312 0313 0314 0315 0316 0317 0322 0323 0324 0326 0328 0330 0333 0334 0337 0338 0340 0342 0343 0344 0345 0346 0348 0350 0351 0358 0361 0364 0365 0366 0368 0370 0372 0375 0380 0382 0384 0386 0388 0389 0392 0393 0396 0397 0398 0400 0401 0404 0408 0409 0412 0418 0419 0420 0421 0422 0423 0437 0439 0443 0448 0451 0452 0455 0458 0462 0465 0466 0472 0473 0477 0481 0486 0487 0489 0491 0494 0496 0497 0498 0500 0502 0503 0505 0506 0507 0508 0509 0510 0511 0513 0515 0516 0518 0519 0521 0522 0524 0525 0526 0527 0529 0530 0532 0533 0535 0536 0539 0542 0548 0549 0552 0555 0565 0567 0568 0570 0571 0573 0576 0578 0579 0584 0587 0588 0591 0600 0605 0609 0610 0612 0614 0616 0618 0620 0621 0623 0625 0629 002 DATE: Jan 15/15 SERVICE BULLETIN No.: A330-53-3226 REVISION No.: 03 - Sep 10/18 Page: 6 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 35 @A330 SERVICE BULLETIN MSN CONFIGURATION 0631 0632 0633 0634 0636 0637 0638 0640 0642 0644 0645 0647 0648 0649 0650 0652 0653 0655 0656 0657 0659 0661 0663 0664 0665 0666 0667 0674 0676 0678 0679 0682 0683 0684 0686 0687 0690 0693 0696 0697 0700 0701 0703 0704 0708 0709 0713 0717 0718 0720 0722 0724 0726 0728 0729 0730 0732 0735 0737 0738 0742 0743 0746 0747 0750 0751 0754 0755 0756 0759 0760 0770 0772 0773 0774 0776 0777 0778 0780 0781 0782 0784 0785 0788 0791 0792 0796 0797 0799 0801 0803 0806 0807 0809 0810 0811 0815 0817 0818 0819 0820 0821 0822 0824 0825 0827 0830 0831 0832 0834 0836 0839 0840 0841 0842 0843 0845 0849 0850 0851 0852 0853 0854 0855 0857 0858 0859 0860 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 0895 0896 0898 0899 0900 0901 0903 0904 0905 0906 0908 0909 0913 0914 0915 0916 0919 0922 0923 0925 0926 0927 0928 0930 0932 0934 0935 0936 0937 0939 0940 0941 0942 0943 0944 0945 0946 0947 0948 0949 0951 0954 0956 0957 0958 0959 0961 0962 0963 0964 0967 0968 0969 0970 0973 0975 0976 0977 0978 0979 0980 0982 0983 0984 0986 0988 0989 0990 0991 0994 0995 0996 0997 0998 1000 1002 1003 1006 1007 1009 1010 1011 1012 1013 1014 1015 1016 1018 1019 1020 1022 1023 1026 1028 1029 1031 1033 1034 1035 1036 1037 1038 1039 1041 1042 1043 1044 1045 1046 1047 1049 1052 1053 1054 1057 1059 1060 1061 1063 1067 1069 1071 1073 1074 1076 1078 1080 1081 1082 1084 1085 1086 1088 1089 1090 1093 1094 1095 1096 1098 1099 1100 1101 1104 1105 1107 1108 1112 1114 1116 1118 1120 1123 1124 1127 1129 1132 1133 1135 1137 1138 1141 1143 1145 1146 1147 1149 1150 1153 1155 1156 1157 1159 1160 1161 1163 1167 1168 1169 1170 1171 1172 1173 1174 1178 1181 1183 1184 1186 1188 1189 1190 1191 1192 1196 1198 1200 1202 1203 1204 1205 1208 1209 1210 1212 1213 1214 1217 1218 1219 1220 1221 1222 1223 1224 1225 1226 1227 1228 1229 1230 1233 1234 1235 1236 1237 1238 1239 1240 1241 1243 1244 1245 1246 1248 1249 1250 1251 1252 1255 1256 1258 1259 1260 1261 1262 1263 1264 1266 1267 1269 1271 1275 1276 1277 1279 1280 1281 1282 1283 1285 1286 1287 1288 1289 1290 1291 1292 1293 1294 1295 1297 1298 1300 1302 1303 1304 1305 1306 1307 1308 1309 1310 1311 1312 1313 1314 1316 1317 1318 1319 1322 1324 1325 1327 1330 1331 1334 1335 1336 1337 1338 1342 1343 1347 1348 1349 1354 1355 1358 1362 1363 1364 1365 1366 1369 1372 1374 1375 1377 003 DATE: Jan 15/15 SERVICE BULLETIN No.: A330-53-3226 REVISION No.: 03 - Sep 10/18 Page: 7 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 36 @A330 SERVICE BULLETIN MSN CONFIGURATION 1379 1381 1382 1384 1385 1387 1388 1389 1390 1392 1393 1394 1395 1396 1397 1398 1399 1400 1401 1402 1403 1404 1405 1407 1408 1409 1410 1412 1415 1416 1417 1419 1421 1422 1425 1426 1427 1429 1430 1431 1432 1434 1436 1437 1438 1439 1440 1441 1443 1444 1446 1447 1451 1452 1453 1454 1455 1457 1458 1459 1461 1462 1465 1466 1468 1469 1470 1471 1472 1473 1474 1476 1477 1478 1479 1480 1483 1484 1485 1486 1487 1488 1489 1490 1491 1492 1494 1496 1497 1498 1499 1500 1501 1502 1503 1505 1507 1508 1511 1512 1513 1514 1515 1516 1517 1519 1520 1521 1523 1526 1528 1529 1530 1532 1535 1536 1537 1540 1542 1543 1544 1545 1547 1548 1551 1554 1555 1556 1557 1558 1560 1561 1562 1565 1567 1569 1571 1572 1573 1574 1575 1576 1577 1579 1580 1582 1585 1586 1588 1590 1591 1592 1593 1595 1597 1598 1599 1601 1603 1605 1606 1607 1608 1609 1610 1611 1613 1614 1615 1616 1617 1618 1620 1621 1622 1623 1624 1625 1626 1627 1628 1629 1630 1631 1632 1633 1634 1635 1636 1637 1638 1639 1640 1641 1642 1643 1644 1645 1647 1648 1649 1651 1653 1654 1655 1656 1657 1660 1662 1663 1664 1665 1666 1667 1668 1671 1672 1676 1677 1678 1679 1681 1686 1694 1696 1697 1698 1699 1700 1701 1703 1704 1706 1709 1710 1713 1714 1715 1716 1718 1719 1720 1721 1723 1725 1728 1730 1732 1733 1735 1736 1737 1740 1741 1745 1746 1747 1748 1751 1753 1754 1755 1756 1757 1758 1759 1760 1761 1762 1763 1769 1771 1773 1775 1776 1777 1779 1780 1782 1783 1784 1785 1787 1788 1792 1793 1796 1798 1799 1801 1804 1805 1808 1809 1814 1815 1816 1818 1821 1822 1823 1825 1826 1830 1833 1835 1841 1842 1845 1846 1847 1848 1852 1854 1856 1857 1858 1859 1864 1868 1869 1872 1873 1877 1878 1881 1882 1883 1885 1886 1891 1894 1905 1911 1912 1916 1919 1928 1932 1936 004 (5) Configuration definition **CONF 001 Config. 001 is valid for aircraft on which: - MOD No. 202436D50514, - MOD No. 41848D19279, - MOD No. 43120D40069 and - MOD No. 51331D44374 are not embodied. **CONF 002 Config. 002 is valid for aircraft on which: - MOD No. 41848D19279 and - MOD No. 43120D40069 are embodied. and on which: - MOD No. 202436D50514 and - MOD No. 51331D44374 are not embodied. **CONF 003 Config. 003 is valid for aircraft on which: - MOD No. 41848D19279, DATE: Jan 15/15 SERVICE BULLETIN No.: A330-53-3226 REVISION No.: 03 - Sep 10/18 Page: 8 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 37 @A330 SERVICE BULLETIN - MOD No. 43120D40069 and - MOD No. 51331D44374 are embodied. and on which: - MOD No. 202436D50514 is not embodied. **CONF 004 Config. 004 is valid for aircraft on which: - MOD No. 202436D50514, - MOD No. 41848D19279, - MOD No. 43120D40069 and - MOD No. 51331D44374 are embodied. **CONF 005 Config. 005 is valid for aircraft on which: - MOD No. 41848D19279 is embodied. and on which: - MOD No. 202436D50514, - MOD No. 43120D40069 and - MOD No. 51331D44374 are not embodied. For the retrofitted modifications after accomplishment of this Service Bulletin, refer to Appendix 04 - Retrofitted Modifications . (6) Material Effectivity **CONF 001 MATERIAL QTY PER A/C SEE NOTES Consumable CMLD01 1 Kit 533226D01R04 1 Kit 533226D05R03 1 Kit 533226D09R01 1 Kit 533226D10R01 1 Standard tool TOOLD01 1 Standard tool TOOLD02 1 Standard tool TOOLD03 1 Kit 533226D11R02 1 **CONF 002 MATERIAL QTY PER A/C SEE NOTES Consumable CMLD01 1 Kit 533226D02R05 1 Kit 533226D06R02 1 Kit 533226D09R01 1 Kit 533226D10R01 1 Standard tool TOOLD01 1 Standard tool TOOLD04 1 Standard tool TOOLD05 1 Kit 533226D11R02 1 DATE: Jan 15/15 SERVICE BULLETIN No.: A330-53-3226 REVISION No.: 03 - Sep 10/18 Page: 9 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 38 @A330 SERVICE BULLETIN **CONF 003 MATERIAL QTY PER A/C SEE NOTES Consumable CMLD01 1 Kit 533226D03R03 1 Kit 533226D07R04 1 Kit 533226D09R01 1 Kit 533226D10R01 1 Standard tool TOOLD01 1 Standard tool TOOLD04 1 Standard tool TOOLD07 1 Kit 533226D11R02 1 **CONF 004 MATERIAL QTY PER A/C SEE NOTES Consumable CMLD01 1 Kit 533226D04R03 1 Kit 533226D08R04 1 Kit 533226D09R01 1 Kit 533226D10R01 1 Standard tool TOOLD01 1 Standard tool TOOLD04 1 Standard tool TOOLD07 1 Kit 533226D11R02 1 **CONF 005 MATERIAL QTY PER A/C SEE NOTES Consumable CMLD01 1 Kit 533226D12R00 1 Kit 533226D13R00 1 Kit 533226D09R01 1 Kit 533226D10R01 1 Standard tool TOOLD01 1 Standard tool TOOLD04 1 Standard tool TOOLD05 1 Kit 533226D11R02 1 **CONF ALL B. CONCURRENT REQUIREMENTS None DATE: Jan 15/15 SERVICE BULLETIN No.: A330-53-3226 REVISION No.: 03 - Sep 10/18 Page: 10 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 39 @A330 SERVICE BULLETIN C. REASON (1) History Following Widespread Fatigue Damage (WFD) analysis, it has been demonstrated that some structural areas require reinforcements before reaching the Design Service Goal (DSG). The circumferential joint between Frames (FR) Frame 53.6 and Frame 53.7 of emergency exit door type 1 has been identified as such area. (2) Objective/Action This modification comprises the structural reinforcement as follows: - For aircraft in Config. 001: . install external, circumferential doubler between Frame 53.6 and Frame 53.7, STGR4-30 LH/RH . install additional shim for door cover plate . install additional shim for 0 deg aligned rain gutter . install modified scuff plate due to external doubler . install additional cold worked holes (rivet with interference fit) at upper and lower door frame shell. - For aircraft in Config. 002: . install external, circumferential doubler between Frame 53.6 and Frame 53.7, STGR4-30 LH/RH . install additional shim for door cover plate . install additional shim for 5 deg aligned rain gutter . install modified scuff plate due to external doubler - For aircraft in Config. 003: . install external, circumferential doubler between Frame 53.6 and Frame 53.7, STGR4-30 LH/RH . install additional shim for door cover plate . install additional shim for 5 deg aligned rain gutter - For aircraft in Config. 004: . install external, circumferential doubler between Frame 53.6 and Frame 53.7, STGR4-29 LH/RH . install additional shim for door cover plate DATE: Jan 15/15 SERVICE BULLETIN No.: A330-53-3226 REVISION No.: 03 - Sep 10/18 Page: 11 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 40 @A330 SERVICE BULLETIN - For aircraft in Config. 005: . install external, circumferential doubler between Frame 53.6 and Frame 53.7, STGR4-30 LH/RH . install additional shim for door cover plate . install additional shim for 5 deg aligned rain gutter . install modified scuff plate due to external doubler (3) Advantages The accomplishment of this Service Bulletin will improve the fatigue life of the circumferential joint between Fram e 53.6 and Frame 53.7, STGR4-30 LH/RH. (4) Operational/Maintenance Consequences This Service Bulletin is based on the aircraft configuration as known by AIRBUS (first aircraft delivery configuration and modified by the reported incorporation of AIRBUS Service Bulletins). Prior to Service Bulletin embodiment, specific attention must be paid to structural damage which may exist and to repairs which were performed on the aircraft because they may be affected by the Service Bulletin. It must be verified that all allowable damage limits and repairs performed (both in accordance with the SRM and outside of the SRM) are still applicable and effective to the new Service Bulletin configuration. There may be additional or modified maintenance requirements, such as temporary limits or additional inspections that apply with respect to the Service Bulletin configuration. There may be additional or modified maintenance requirements, such as temporary limits or additional inspections that apply with respect to the Service Bulletin configuration. AIRBUS disclaims any liability for the effect which the Service Bulletin may have on repairs performed on the aircraft before embodiment of the Service Bulletin. If the post Service Bulletin repair status is not covered by the SRM and for repairs outside of the SRM covered by a RAS issued by AIRBUS, AIRBUS Customer Services Repair Engineering Support (SEOE) should be contacted. Repair review will be done by AIRBUS at conditions of the Customer Services Catalogue. D. DESCRIPTION To accomplish this Service Bulletin it is necessary to : **CONF 001 Task 533226-831-848-001: Modification (1) Perform Paint-Stripping of the Aircraft Skin at the Modification Area LH (2) Perform Paint-Stripping of the Aircraft Skin at the Modification Area RH DATE: Jan 15/15 SERVICE BULLETIN No.: A330-53-3226 REVISION No.: 03 - Sep 10/18 Page: 12 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 41 @A330 SERVICE BULLETIN (3) Remove the Scuff Plates from the LH Emergency Exit Door (4) Remove the Scuff Plates from the RH Emergency Exit Door (5) Remove Cross Plate from the Emergency Door Upper Area, LH (6) Remove Cross Plate from the Emergency Door Upper Area, RH (7) Remove Fasteners at Upper Forward Corner of the Door Frame at Emergency Exit Door Type 1 LH (8) Do the Inspection of Fastener Holes at Upper Forward Corner of the Door Frame at Emergency Exit Door Type 1 LH (9) Remove Fasteners at Upper Aft Corner of the Door Frame at Emergency Exit Door T y p e1L H (10) Do the Inspection of the Fastener Holes at Upper Aft Corner of the Door Frame at Emergency Exit Door Type 1 LH (11) Remove Fasteners at Lower Aft Corner of the Door Frame at Emergency Exit Door T y p e1L H (12) Do the Inspection of the Fastener Holes at Lower Aft Corner of the Door Frame at Emergency Exit Door Type 1 LH (13) Remove Fasteners at Lower Forward Corner of the Door Frame at Emergency Exit Door Type 1 LH (14) Do the Inspection of Fastener Holes at Lower Forward Corner of the Door Frame at Emergency Exit Door Type 1 LH (15) Do the Modification of Upper Forward Corner of the Door Frame at Emergency Exit Door Type 1 LH (16) Do the Modification of Upper Aft Corner of the Door Frame at Emergency Exit Door T y p e1L H (17) Do the Modification of Lower Aft Corner of the Door Frame at Emergency Exit Door T y p e1L H (18) Do the Modification of the Lower Forward Corner of the Door Frame at Emergency Exit Door Type 1 LH (19) Remove Fasteners at Upper Forward Corner of the Door Frame at Emergency Exit Door Type 1 RH (20) Do the Inspection of Fastener Holes at Upper Forward Corner of the Door Frame at Emergency Exit Door Type 1 RH (21) Remove Fasteners at Upper Aft Corner of the Door Frame at Emergency Exit Door T y p e1R H (22) Do the Inpection of Fastener Holes at Upper Aft Corner of the Door Frame at DATE: Jan 15/15 SERVICE BULLETIN No.: A330-53-3226 REVISION No.: 03 - Sep 10/18 Page: 13 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 42 @A330 SERVICE BULLETIN Emergency Exit Door Type 1 RH (23) Remove Fasteners at Lower Aft Corner of the Door Frame at Emergency Exit Door T y p e1R H (24) Do the Inspection of Fastener Holes at Lower Aft Corner of the Door Frame at Emergency Exit Door Type 1 RH (25) Remove Fasteners at Lower Forward Corner of the Door Frame at Emergency Exit Door Type 1 RH (26) Do the Inspection of Fastener Holes at Lower Forward Corner of the Door Frame at Emergency Exit Door Type 1 RH (27) Do the Modification of Upper Forward Corner of the Door Frame at Emergency Exit Door Type 1 RH (28) Do the Modification of Upper Aft Corner of the Door Frame at Emergency Exit Door T y p e1R H (29) Do the Modification of Lower Aft Corner of the Door Frame at Emergency Exit Door T y p e1R H (30) Do the Modification of Lower Forward Corner of the Door Frame at Emergency Exit Door Type 1 RH (31) Remove Rain Gutter at Emergency Exit Door Type 1 Area LH (32) Remove Fasteners between FR53.6 and FR53.7 and between STGR4 and STGR15A, LH (33) Do the Inspection of the Fastener Holes between FR53.6 and FR53.7 and between STGR4 and STGR15A, LH (34) Remove Fasteners between FR53.6 and FR53.7 and between STGR26 and STGR30, LH (35) Do the Inspection of the Fastener Holes between FR53.6 and FR53.7 and between STGR26 and STGR30, LH (36) Install Doubler at Circumferential Joint between FR53.6 and FR53.7 and between STGR4 and STGR15A, LH (37) Install Rain Gutter at Emergency Exit Door Type 1 Area LH (38) Install Doubler at Circumferential Joint between FR53.6 and FR53.7 and between STGR26 and STGR30, LH (39) Remove Rain Gutter at Emergency Exit Door Type 1 Area RH (40) Remove Fasteners between FR53.6 and FR53.7 and between STGR4 and STGR15A, RH (41) Do the Inspection of the Fasteners Holes between FR53.6 and FR53.7 and DATE: Jan 15/15 SERVICE BULLETIN No.: A330-53-3226 REVISION No.: 03 - Sep 10/18 Page: 14 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 43 @A330 SERVICE BULLETIN between STGR4 and STGR15A, RH (42) Remove Fasteners from between FR53.6 and FR53.7 and between STGR26 and STGR30, RH (43) Do the Inspection of the Fastener Holes between FR53.6 and FR53.7 and between STGR26 and STGR30, RH (44) Install Doubler at Circumferential Joint between FR53.6 and FR53.7 and between STGR4 and STGR15A, RH (45) Install Rain Gutter at Emergency Exit Door Type 1 Area RH (46) Install Doubler at Circumferential Joint between FR53.6 and FR53.7 and between STGR26 and STGR30, RH (47) Apply Protections to the Upper Door Frame Area, LH (48) Apply Protections to the Lower Door Frame Area, LH (49) Apply Protections to the Upper Door Frame Area, RH (50) Apply Protections to the Lower Door Frame Area, RH (51) Install Cross Plate of the Emergency Door Upper Area, LH (52) Install Cross Plate of the Emergency Door Upper Area, RH (53) Install the Scuff Plates to the LH Emergency Exit Door (54) Install the Scuff Plates to the RH Emergency Exit Door (55) Do the Modification of the LH Emergency Exit Door (56) Do the Modification of the RH Emergency Exit Door **CONF 002 Task 533226-831-848-001: Modification (1) Perform Paint-Stripping of the Aircraft Skin at the Modification Area LH (2) Perform Paint-Stripping of the Aircraft Skin at the Modification Area RH (3) Remove the Scuff Plates from the LH Emergency Exit Door (4) Remove the Scuff Plates from the RH Emergency Exit Door (5) Remove Cross Plate from the Emergency Door Upper Area, LH (6) Remove Cross Plate from the Emergency Door Upper Area, RH (7) Remove Fasteners at Upper Forward Corner of the Door Frame at Emergency Exit Door Type 1 LH DATE: Jan 15/15 SERVICE BULLETIN No.: A330-53-3226 REVISION No.: 03 - Sep 10/18 Page: 15 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 44 @A330 SERVICE BULLETIN (8) Do the Inspection of Fastener Holes at Upper Forward Corner of the Door Frame at Emergency Exit Door Type 1 LH (9) Remove Fasteners at Upper Aft Corner of the Door Frame at Emergency Exit Door T y p e1L H (10) Do the Inspection of the Fastener Holes at Upper Aft Corner of the Door Frame at Emergency Exit Door Type 1 LH (11) Remove Fasteners at Lower Aft Corner of the Door Frame at Emergency Exit Door T y p e1L H (12) Do the Inspection of the Fastener Holes at Lower Aft Corner of the Door Frame at Emergency Exit Door Type 1 LH (13) Remove Fasteners at Lower Forward Corner of the Door Frame at Emergency Exit Door Type 1 LH (14) Do the Inspection of Fastener Holes at Lower Forward Corner of the Door Frame at Emergency Exit Door Type 1 LH (15) Do the Modification of Upper Forward Corner of the Door Frame at Emergency Exit Door Type 1 LH (16) Do the Modification of Upper Aft Corner of the Door Frame at Emergency Exit Door T y p e1L H (17) Do the Modification of Lower Aft Corner of the Door Frame at Emergency Exit Door T y p e1L H (18) Do the Modification of the Lower Forward Corner of the Door Frame at Emergency Exit Door Type 1 LH (19) Remove Fasteners at Upper Forward Corner of the Door Frame at Emergency Exit Door Type 1 RH (20) Do the Inspection of Fastener Holes at Upper Forward Corner of the Door Frame at Emergency Exit Door Type 1 RH (21) Remove Fasteners at Upper Aft Corner of the Door Frame at Emergency Exit Door T y p e1R H (22) Do the Inspection of Fastener Holes at Upper Aft Corner of the Door Frame at Emergency Exit Door Type 1 RH (23) Remove Fasteners at Lower Aft Corner of the Door Frame at Emergency Exit Door T y p e1R H (24) Do the Inspection of Fastener Holes at Lower Aft Corner of the Door Frame at Emergency Exit Door Type 1 RH (25) Remove Fasteners at Lower Forward Corner of the Door Frame at Emergency Exit Door Type 1 RH DATE: Jan 15/15 SERVICE BULLETIN No.: A330-53-3226 REVISION No.: 03 - Sep 10/18 Page: 16 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 45 @A330 SERVICE BULLETIN (26) Do the Inspection of Fastener Holes at Lower Forward Corner of the Door Frame at Emergency Exit Door Type 1 RH (27) Do the Modification of Upper Forward Corner of the Door Frame at Emergency Exit Door Type 1 RH (28) Do the Modification of Upper Aft Corner of the Door Frame at Emergency Exit Door T y p e1R H (29) Do the Modification of the Lower Aft Corner of the Door Frame at Emergency Exit Door Type 1 RH (30) Do the Modification of Lower Forward Corner of the Door Frame at Emergency Exit Door Type 1 RH (31) Remove Rain Gutter at Emergency Exit Door Type 1 Area LH (32) Remove Fasteners between FR53.6 and FR53.7 and between STGR4 and STGR15A, LH (33) Do the Inspection of the Fastener Holes between FR53.6 and FR53.7 and between STGR4 and STGR15A, LH (34) Remove Fasteners between FR53.6 and FR53.7 and between STGR26 and STGR30, LH (35) Do the Inspection of the Fastener Holes between FR53.6 and FR53.7 and between STGR26 and STGR30, LH (36) Install Doubler at Circumferential Joint between FR53.6 and FR53.7 and between STGR4 and STGR15A, LH (37) Install Rain Gutter at Emergency Exit Door Type 1 Area LH (38) Install Doubler at Circumferential Joint between FR53.6 and FR53.7 and between STGR26 and STGR30, LH (39) Remove Rain Gutter at Emergency Exit Door Type 1 Area RH (40) Remove Fasteners between FR53.6 and FR53.7 and between STGR4 and STGR15A, RH (41) Do the Inspection of the Fasteners Holes between FR53.6 and FR53.7 and between STGR4 and STGR15A, RH (42) Remove Fasteners from between FR53.6 and FR53.7 and between STGR26 and STGR30, RH (43) Do the Inspection of the Fastener Holes between FR53.6 and FR53.7 and between STGR26 and STGR30, RH (44) Install Doubler at Circumferential Joint between FR53.6 and FR53.7 and between STGR4 and STGR15A, RH DATE: Jan 15/15 SERVICE BULLETIN No.: A330-53-3226 REVISION No.: 03 - Sep 10/18 Page: 17 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 46 @A330 SERVICE BULLETIN (45) Install Rain Gutter at Emergency Exit Door Type 1 Area RH (46) Install Doubler at Circumferential Joint between FR53.6 and FR53.7 and between STGR26 and STGR30, RH (47) Apply Protections to the Upper Door Frame Area, LH (48) Apply Protections to the Lower Door Frame Area, LH (49) Apply Protections to the Upper Door Frame Area, RH (50) Apply Protections to the Lower Door Frame Area, RH (51) Install Cross Plate of the Emergency Door Upper Area, LH (52) Install Cross Plate of the Emergency Door Upper Area, RH (53) Install the Scuff Plates to the LH Emergency Exit Door (54) Install the Scuff Plates to the RH Emergency Exit Door (55) Do the Modification of the LH Emergency Exit Door (56) Do the Modification of the RH Emergency Exit Door **CONF 003 Task 533226-831-848-001: Modification (1) Perform Paint-Stripping of the Aircraft Skin at the Modification Area LH (2) Perform Paint-Stripping of the Aircraft Skin at the Modification Area RH (3) Remove Cross Plate from the Emergency Door Upper Area, LH (4) Remove Cross Plate from the Emergency Door Upper Area, RH (5) Remove Fasteners at Upper Forward Corner of the Door Frame at Emergency Exit Door Type 1 LH (6) Do the Inspection of Fastener Holes at Upper Forward Corner of the Door Frame at Emergency Exit Door Type 1 LH (7) Remove Fasteners at Upper Aft Corner of the Door Frame at Emergency Exit Door T y p e1L H (8) Do the Inspection of the Fastener Holes at Upper Aft Corner of the Door Frame at Emergency Exit Door Type 1 LH (9) Do the Modification of Upper Forward Corner of the Door Frame at Emergency Exit Door Type 1 LH (10) Do the Modification of Upper Aft Corner of the Door Frame at Emergency Exit Door T y p e1L H DATE: Jan 15/15 SERVICE BULLETIN No.: A330-53-3226 REVISION No.: 03 - Sep 10/18 Page: 18 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 47 @A330 SERVICE BULLETIN (11) Remove Fasteners at Upper Forward Corner of the Door Frame at Emergency Exit Door Type 1 RH (12) Do the Inspection of Fastener Holes at Upper Forward Corner of the Door Frame at Emergency Exit Door Type 1 RH (13) Remove Fasteners at Upper Aft Corner of the Door Frame at Emergency Exit Door T y p e1R H (14) Do the Inspection of Fastener Holes at Upper Aft Corner of the Door Frame at Emergency Exit Door Type 1 RH (15) Do the Modification of Upper Forward Corner of the Door Frame at Emergency Exit Door Type 1 RH (16) Do the Modification of Upper Aft Corner of the Door Frame at Emergency Exit Door T y p e1R H (17) Remove Rain Gutter at Emergency Exit Door Type 1 Area LH (18) Remove Fasteners between FR53.6 and FR53.7 and between STGR4 and STGR15A, LH (19) Do the Inspection of the Fastener Holes between FR53.6 and FR53.7 and between STGR4 and STGR15A, LH (20) Remove Fasteners between FR53.6 and FR53.7 and between STGR26 and STGR30, LH (21) Do the Inspection of the Fastener Holes between FR53.6 and FR53.7 and between STGR26 and STGR30, LH (22) Install Doubler at Circumferential Joint between FR53.6 and FR53.7 and between STGR4 and STGR15A, LH (23) Install Rain Gutter at Emergency Exit Door Type 1 Area LH (24) Install Doubler at Circumferential Joint between FR53.6 and FR53.7 and between STGR26 and STGR30, LH (25) Remove Rain Gutter at Emergency Exit Door Type 1 Area RH (26) Remove Fasteners between FR53.6 and FR53.7 and between STGR4 and STGR15A, RH (27) Do the Inspection of the Fasteners Holes between FR53.6 and FR53.7 and between STGR4 and STGR15A, RH (28) Remove Fasteners from between FR53.6 and FR53.7 and between STGR26 and STGR30, RH (29) Do the Inspection of the Fastener Holes between FR53.6 and FR53.7 and between STGR26 and STGR30, RH DATE: Jan 15/15 SERVICE BULLETIN No.: A330-53-3226 REVISION No.: 03 - Sep 10/18 Page: 19 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 48 @A330 SERVICE BULLETIN (30) Install Doubler at Circumferential Joint between FR53.6 and FR53.7 and between STGR4 and STGR15A, RH (31) Install Rain Gutter at Emergency Exit Door Type 1 Area RH (32) Install Doubler at Circumferential Joint between FR53.6 and FR53.7 and between STGR26 and STGR30, RH (33) Apply Protections to the Upper Door Frame Area, LH (34) Apply Protections to the Lower Door Frame Area, LH (35) Apply Protections to the Upper Door Frame Area, RH (36) Apply Protections to the Lower Door Frame Area, RH (37) Install Cross Plate of the Emergency Door Upper Area, LH (38) Install Cross Plate of the Emergency Door Upper Area, RH (39) Do the Modification of the LH Emergency Exit Door (40) Do the Modification of the RH Emergency Exit Door **CONF 004 Task 533226-831-848-001: Modification (1) Perform Paint-Stripping of the Aircraft Skin at the Modification Area LH (2) Perform Paint-Stripping of the Aircraft Skin at the Modification Area RH (3) Remove Cross Plate from the Emergency Door Upper Area, LH (4) Remove Cross Plate from the Emergency Door Upper Area, RH (5) Remove Fasteners at Upper Forward Corner of the Door Frame at Emergency Exit Door Type 1 LH (6) Do the Inspection of Fastener Holes at Upper Forward Corner of the Door Frame at Emergency Exit Door Type 1 LH (7) Remove Fasteners at Upper Aft Corner of the Door Frame at Emergency Exit Door T y p e1L H (8) Do the Inspection of the Fastener Holes at Upper Aft Corner of the Door Frame at Emergency Exit Door Type 1 LH (9) Do the Modification of Upper Forward Corner of the Door Frame at Emergency Exit Door Type 1 LH (10) Do the Modification of Upper Aft Corner of the Door Frame at Emergency Exit Door T y p e1L H DATE: Jan 15/15 SERVICE BULLETIN No.: A330-53-3226 REVISION No.: 03 - Sep 10/18 Page: 20 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 49 @A330 SERVICE BULLETIN (11) Remove Fasteners at Upper Forward Corner of the Door Frame at Emergency Exit Door Type 1 RH (12) Do the Inspection of Fastener Holes at Upper Forward Corner of the Door Frame at Emergency Exit Door Type 1 RH (13) Remove Fasteners at Upper Aft Corner of the Door Frame at Emergency Exit Door T y p e1R H (14) Do the Inspection of Fastener Holes at Upper Aft Corner of the Door Frame at Emergency Exit Door Type 1 RH (15) Do the Modification of Upper Forward Corner of the Door Frame at Emergency Exit Door Type 1 RH (16) Do the Modification of Upper Aft Corner of the Door Frame at Emergency Exit Door T y p e1R H (17) Remove Fasteners between FR53.6 and FR53.7 and between STGR4 and STGR15A, LH (18) Do the Inspection of the Fastener Holes between FR53.6 and FR53.7 and between STGR4 and STGR15A, LH (19) Remove Fasteners between FR53.6 and FR53.7 and between STGR26 and STGR30, LH (20) Do the Inspection of the Fastener Holes between FR53.6 and FR53.7 and between STGR26 and STGR30, LH (21) Install Doubler at Circumferential Joint between FR53.6 and FR53.7 and between STGR4 and STGR15A, LH (22) Install Doubler at Circumferential Joint between FR53.6 and FR53.7 and between STGR26 and STGR30, LH (23) Remove Fasteners between FR53.6 and FR53.7 and between STGR4 and STGR15A, RH (24) Do the Inspection of the Fasteners Holes between FR53.6 and FR53.7 and between STGR4 and STGR15A, RH (25) Remove Fasteners from between FR53.6 and FR53.7 and between STGR26 and STGR30, RH (26) Do the Inspection of the Fastener Holes between FR53.6 and FR53.7 and between STGR26 and STGR30, RH (27) Install Doubler at Circumferential Joint between FR53.6 and FR53.7 and between STGR4 and STGR15A, RH (28) Install Doubler at Circumferential Joint between FR53.6 and FR53.7 and between STGR26 and STGR30, RH DATE: Jan 15/15 SERVICE BULLETIN No.: A330-53-3226 REVISION No.: 03 - Sep 10/18 Page: 21 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 50 @A330 SERVICE BULLETIN (29) Apply Protections to the Upper Door Frame Area, LH (30) Apply Protections to the Lower Door Frame Area, LH (31) Apply Protections to the Upper Door Frame Area, RH (32) Apply Protections to the Lower Door Frame Area, RH (33) Install Cross Plate of the Emergency Door Upper Area, LH (34) Install Cross Plate of the Emergency Door Upper Area, RH (35) Do the Modification of the LH Emergency Exit Door (36) Do the Modification of the RH Emergency Exit Door **CONF 005 Task 533226-831-848-001 : Modification (1) Perform Paint-Stripping of the Aircraft Skin at the Modification Area LH (2) Perform Paint-Stripping of the Aircraft Skin at the Modification Area RH (3) Remove the Scuff Plates from the LH Emergency Exit Door (4) Remove the Scuff Plates from the RH Emergency Exit Door (5) Remove Cross Plate from the Emergency Door Upper Area, LH (6) Remove Cross Plate from the Emergency Door Upper Area, RH (7) Remove Fasteners at Upper Forward Corner of the Door Frame at Emergency Exit Door Type 1 LH (8) Do the Inspection of Fastener Holes at Upper Forward Corner of the Door Frame at Emergency Exit Door Type 1 LH (9) Remove Fasteners at Upper Aft Corner of the Door Frame at Emergency Exit Door T y p e1L H (10) Do the Inspection of the Fastener Holes at Upper Aft Corner of the Door Frame at Emergency Exit Door Type 1 LH (11) Remove Fasteners at Lower Aft Corner of the Door Frame at Emergency Exit Door T y p e1L H (12) Do the Inspection of the Fastener Holes at Lower Aft Corner of the Door Frame at Emergency Exit Door Type 1 LH (13) Remove Fasteners at Lower Forward Corner of the Door Frame at Emergency Exit Door Type 1 LH (14) Do the Inspection of Fastener Holes at Lower Forward Corner of the Door Frame at DATE: Jan 15/15 SERVICE BULLETIN No.: A330-53-3226 REVISION No.: 03 - Sep 10/18 Page: 22 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 51 @A330 SERVICE BULLETIN Emergency Exit Door Type 1 LH (15) Do the Modification of Upper Forward Corner of the Door Frame at Emergency Exit Door Type 1 LH (16) Do the Modification of Upper Aft Corner of the Door Frame at Emergency Exit Door T y p e1L H (17) Do the Modification of Lower Aft Corner of the Door Frame at Emergency Exit Door T y p e1L H (18) Do the Modification of the Lower Forward Corner of the Door Frame at Emergency Exit Door Type 1 LH (19) Remove Fasteners at Upper Forward Corner of the Door Frame at Emergency Exit Door Type 1 RH (20) Do the Inspection of Fastener Holes at Upper Forward Corner of the Door Frame at Emergency Exit Door Type 1 RH (21) Remove Fasteners at Upper Aft Corner of the Door Frame at Emergency Exit Door T y p e1R H (22) Do the Inspection of Fastener Holes at Upper Aft Corner of the Door Frame at Emergency Exit Door Type 1 RH (23) Remove Fasteners at Lower Aft Corner of the Door Frame at Emergency Exit Door T y p e1R H (24) Do the Inspection of Fastener Holes at Lower Aft Corner of the Door Frame at Emergency Exit Door Type 1 RH (25) Remove Fasteners at Lower Forward Corner of the Door Frame at Emergency Exit Door Type 1 RH (26) Do the Inspection of Fastener Holes at Lower Forward Corner of the Door Frame at Emergency Exit Door Type 1 RH (27) Do the Modification of Upper Forward Corner of the Door Frame at Emergency Exit Door Type 1 RH (28) Do the Modification of Upper Aft Corner of the Door Frame at Emergency Exit Door T y p e1R H (29) Do the Modification of the Lower Aft Corner of the Door Frame at Emergency Exit Door Type 1 RH (30) Do the Modification of Lower Forward Corner of the Door Frame at Emergency Exit Door Type 1 RH (31) Remove Rain Gutter at Emergency Exit Door Type 1 Area LH (32) Remove Fasteners between FR53.6 and FR53.7 and between STGR4 and STGR15A, LH DATE: Jan 15/15 SERVICE BULLETIN No.: A330-53-3226 REVISION No.: 03 - Sep 10/18 Page: 23 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 52 @A330 SERVICE BULLETIN (33) Do the Inspection of the Fastener Holes between FR53.6 and FR53.7 and between STGR4 and STGR15A, LH (34) Remove Fasteners between FR53.6 and FR53.7 and between STGR26 and STGR30, LH (35) Do the Inspection of the Fastener Holes between FR53.6 and FR53.7 and between STGR26 and STGR30, LH (36) Install Doubler at Circumferential Joint between FR53.6 and FR53.7 and between STGR4 and STGR15A, LH (37) Install Rain Gutter at Emergency Exit Door Type 1 Area LH (38) Install Doubler at Circumferential Joint between FR53.6 and FR53.7 and between STGR26 and STGR30, LH (39) Remove Rain Gutter at Emergency Exit Door Type 1 Area RH (40) Remove Fasteners between FR53.6 and FR53.7 and between STGR4 and STGR15A, RH (41) Do the Inspection of the Fasteners Holes between FR53.6 and FR53.7 and between STGR4 and STGR15A, RH (42) Remove Fasteners from between FR53.6 and FR53.7 and between STGR26 and STGR30, RH (43) Do the Inspection of the Fastener Holes between FR53.6 and FR53.7 and between STGR26 and STGR30, RH (44) Install Doubler at Circumferential Joint between FR53.6 and FR53.7 and between STGR4 and STGR15A, RH (45) Install Rain Gutter at Emergency Exit Door Type 1 Area RH (46) Install Doubler at Circumferential Joint between FR53.6 and FR53.7 and between STGR26 and STGR30, RH (47) Apply Protections to the Upper Door Frame Area, LH (48) Apply Protections to the Lower Door Frame Area, LH (49) Apply Protections to the Upper Door Frame Area, RH (50) Apply Protections to the Lower Door Frame Area, RH (51) Install Cross Plate of the Emergency Door Upper Area, LH (52) Install Cross Plate of the Emergency Door Upper Area, RH (53) Install the Scuff Plates to the LH Emergency Exit Door (54) Install the Scuff Plates to the RH Emergency Exit Door DATE: Jan 15/15 SERVICE BULLETIN No.: A330-53-3226 REVISION No.: 03 - Sep 10/18 Page: 24 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 53 @A330 SERVICE BULLETIN (55) Do the Modification of the LH Emergency Exit Door (56) Do the Modification of the RH Emergency Exit Door **CONF ALL E. COMPLIANCE (1) Classification MANDATORY: Service Bulletin must be accomplished. (2) Accomplishment Timescale This Service Bulletin has been classified Mandatory. It is expected that an Airworthiness Directive (AD) published by the European Av iation Safety Agenc y (EASA) will be issued to confirm this classification. It is anticipated that the AD will confirm the thresholds given but reference should be made to the AD for confirmation of the mandated accomplishment timescale. Table 1, all Config. - Compliance Time Threshold from first flight (whichever occurs first) Grace period Weight Variant (WV) Group * Flight Cycles (FC) Flight Hours (FH) Months (M) Short Range (SR) ** 26100 91600 12 Group 32A Long Range (LR) *** 21000 137200 12 SR ** 19900 69900 12 Group 32E LR *** 16200 105100 12 SR ** 34400 103300 12 Group 33A LR *** 27800 187300 12 SR ** 19900 59800 12 Group 33B LR *** 16100 108400 12 SR ** 15600 46800 12 Group 33C Group 33D Group 33E LR *** 12600 84800 12 NOTE :* - For definitions of WV Groups, refer to Airworthiness Limitation Section (ALS) Part 2. NOTE :* * - FC-optimized set, optimized for aircraft in SR operations. NOTE : *** - FH-optimized set, optimized for aircraft in LR operations. DATE: Jan 15/15 SERVICE BULLETIN No.: A330-53-3226 REVISION No.: 03 - Sep 10/18 Page: 25 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 54 @A330 SERVICE BULLETIN F. APPROVAL The technical content of this document is approved under the authority of Design Organisation Approval No. EASA.21J.031. If an aircraft listed in the effectivity has a modification or repair embodied that is not of AIRBUS origin, and which affects the content of this Service Bulletin, the operator is responsible for obtaining approval by its airworthiness authority for any adaptation necessary before incorporation of the Service Bulletin. G. MANPOWER The manpower estimates given in this Service Bulletin are based on the direct labor cost to do the work. These estimates assume that the work will be done by experienced personnel, and may need to be revised upwards to suit operator’s circumstances. The estimates do not include the time to prepare, plan or inspect the work. Manufacture and procurement of parts and tools, drying times for paints, sealants, etc., and general administration work are also not included. **CONF 001 Task 533226-831-848-001: Modification Get Access 26.00 On Aircraft Perform Paint-Stripping of the Aircraft Skin at the Modification Area LH 1.00 Perform Paint-Stripping of the Aircraft Skin at the Modification Area RH 1.00 Remove the Scuff Plates from the LH Emergency Exit Door 2.00 Remove the Scuff Plates from the RH Emergency Exit Door 2.00 Remove Cross Plate from the Emergency Door Upper Area, LH 6.00 Remove Cross Plate from the Emergency Door Upper Area, RH 6.00 Remove Fasteners at Upper Forward Corner of the Door Frame at Emergency Exit Door Type 1 LH 1.00 Do the Inspection of Fastener Holes at Upper Forward Corner of the Door Frame at Emergency Exit Door Type 1 LH 0.50 Remove Fasteners at Upper Aft Corner of the Door Frame at Emergency Exit Door Type 1 LH 1.00 Do the Inspection of the Fastener Holes at Upper Aft Corner of the Door Frame at Emergency Exit Door Type 1 LH 0.50 Remove Fasteners at Lower Aft Corner of the Door Frame at Emergency Exit Door Type 1 LH 1.00 DATE: Jan 15/15 SERVICE BULLETIN No.: A330-53-3226 REVISION No.: 03 - Sep 10/18 Page: 26 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 55 @A330 SERVICE BULLETIN Task 533226-831-848-001: Modification Do the Inspection of the Fastener Holes at Lower Aft Corner of the Door Frame at Emergency Exit Door Type 1 LH 0.50 Remove Fasteners at Lower Forward Corner of the Door Frame at Emergency Exit Door Type 1 LH 1.00 Do the Inspection of Fastener Holes at Lower Forward Corner of the Door Frame at Emergency Exit Door Type 1 LH 0.50 Do the Modification of Upper Forward Corner of the Door Frame at Emergency Exit Door Type 1 LH 8.00 Do the Modification of Upper Aft Corner of the Door Frame at Emergency Exit Door Type 1 LH 8.00 Do the Modification of Lower Aft Corner of the Door Frame at Emergency Exit Door Type 1 LH 8.00 Do the Modification of the Lower Forward Corner of the Door Frame at Emergency Exit Door Type 1 LH 8.00 Remove Fasteners at Upper Forward Corner of the Door Frame at Emergency Exit Door Type 1 RH 1.00 Do the Inspection of Fastener Holes at Upper Forward Corner of the Door Frame at Emergency Exit Door Type 1 RH 0.50 Remove Fasteners at Upper Aft Corner of the Door Frame at Emergency Exit Door Type 1 RH 1.00 Do the Inpection of Fastener Holes at Upper Aft Corner of the Door Frame at Emergency Exit Door Type 1 RH 0.50 Remove Fasteners at Lower Aft Corner of the Door Frame at Emergency Exit Door Type 1 RH 1.00 Do the Inspection of Fastener Holes at Lower Aft Corner of the Door Frame at Emergency Exit Door Type 1 RH 0.50 Remove Fasteners at Lower Forward Corner of the Door Frame at Emergency Exit Door Type 1 RH 1.00 Do the Inspection of Fastener Holes at Lower Forward Corner of the Door Frame at Emergency Exit Door Type 1 RH 0.50 Do the Modification of Upper Forward Corner of the Door Frame at Emergency Exit Door Type 1 RH 8.00 Do the Modification of Upper Aft Corner of the Door Frame at Emergency Exit Door Type 1 RH 8.00 Do the Modification of Lower Aft Corner of the Door Frame at Emergency Exit Door Type 1 RH 8.00 Do the Modification of Lower Forward Corner of the Door Frame at Emergency Exit Door Type 1 RH 8.00 Remove Rain Gutter at Emergency Exit Door Type 1 Area LH 1.00 DATE: Jan 15/15 SERVICE BULLETIN No.: A330-53-3226 REVISION No.: 03 - Sep 10/18 Page: 27 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 56 @A330 SERVICE BULLETIN Task 533226-831-848-001: Modification Remove Fasteners between FR53.6 and FR53.7 and between STGR4 and STGR15A, LH 10.00 Do the Inspection of the Fastener Holes between FR53.6 and FR53.7 and between STGR4 and STGR15A, LH 1.50 Remove Fasteners between FR53.6 and FR53.7 and between STGR26 and STGR30, LH 4.00 Do the Inspection of the Fastener Holes between FR53.6 and FR53.7 and between STGR26 and STGR30, LH 1.00 Install Doubler at Circumferential Joint between FR53.6 and FR53.7 and between STGR4 and STGR15A, LH 28.00 Install Rain Gutter at Emergency Exit Door Type 1 Area LH 4.00 Install Doubler at Circumferential Joint between FR53.6 and FR53.7 and between STGR26 and STGR30, LH 19.00 Remove Rain Gutter at Emergency Exit Door Type 1 Area RH 1.00 Remove Fasteners between FR53.6 and FR53.7 and between STGR4 and STGR15A, RH 10.00 Do the Inspection of the Fasteners Holes between FR53.6 and FR53.7 and between STGR4 and STGR15A, RH 1.50 Remove Fasteners from between FR53.6 and FR53.7 and between STGR26 and STGR30, RH 4.00 Do the Inspection of the Fastener Holes between FR53.6 and FR53.7 and between STGR26 and STGR30, RH 1.00 Install Doubler at Circumferential Joint between FR53.6 and FR53.7 and between STGR4 and STGR15A, RH 28.00 Install Rain Gutter at Emergency Exit Door Type 1 Area RH 4.00 Install Doubler at Circumferential Joint between FR53.6 and FR53.7 and between STGR26 and STGR30, RH 19.00 Apply Protections to the Upper Door Frame Area, LH 0.25 Apply Protections to the Lower Door Frame Area, LH 0.25 Apply Protections to the Upper Door Frame Area, RH 0.25 Apply Protections to the Lower Door Frame Area, RH 0.25 Install Cross Plate of the Emergency Door Upper Area, LH 6.00 Install Cross Plate of the Emergency Door Upper Area, RH 6.00 Install the Scuff Plates to the LH Emergency Exit Door 6.00 Install the Scuff Plates to the RH Emergency Exit Door 3.00 Do the Modification of the LH Emergency Exit Door 6.00 Do the Modification of the RH Emergency Exit Door 6.00 DATE: Jan 15/15 SERVICE BULLETIN No.: A330-53-3226 REVISION No.: 03 - Sep 10/18 Page: 28 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 57 @A330 SERVICE BULLETIN Task 533226-831-848-001: Modification Tests 2.00 Close-Up 24.00 TOTAL MANHOURS 317.00 ELAPSED TIME (HOURS) 69.00 NOTE : For an explanation of the manhours and elapsed time, refer to the Gantt Chart, Fig. A-GAAAA given in Appendix 01 - Manpower Gantt Chart. **CONF 002 Task 533226-831-848-001: Modification Get Access 26.00 On Aircraft Perform Paint-Stripping of the Aircraft Skin at the Modification Area LH 1.00 Perform Paint-Stripping of the Aircraft Skin at the Modification Area RH 1.00 Remove the Scuff Plates from the LH Emergency Exit Door 2.00 Remove the Scuff Plates from the RH Emergency Exit Door 2.00 Remove Cross Plate from the Emergency Door Upper Area, LH 6.00 Remove Cross Plate from the Emergency Door Upper Area, RH 6.00 Remove Fasteners at Upper Forward Corner of the Door Frame at Emergency Exit Door Type 1 LH 1.00 Do the Inspection of Fastener Holes at Upper Forward Corner of the Door Frame at Emergency Exit Door Type 1 LH 0.50 Remove Fasteners at Upper Aft Corner of the Door Frame at Emergency Exit Door Type 1 LH 1.00 Do the Inspection of the Fastener Holes at Upper Aft Corner of the Door Frame at Emergency Exit Door Type 1 LH 0.50 Remove Fasteners at Lower Aft Corner of the Door Frame at Emergency Exit Door Type 1 LH 1.00 Do the Inspection of the Fastener Holes at Lower Aft Corner of the Door Frame at Emergency Exit Door Type 1 LH 0.50 Remove Fasteners at Lower Forward Corner of the Door Frame at Emergency Exit Door Type 1 LH 1.00 Do the Inspection of Fastener Holes at Lower Forward Corner of the Door Frame at Emergency Exit Door Type 1 LH 0.50 Do the Modification of Upper Forward Corner of the Door Frame at Emergency Exit Door Type 1 LH 8.00 DATE: Jan 15/15 SERVICE BULLETIN No.: A330-53-3226 REVISION No.: 03 - Sep 10/18 Page: 29 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 58 @A330 SERVICE BULLETIN Task 533226-831-848-001: Modification Do the Modification of Upper Aft Corner of the Door Frame at Emergency Exit Door Type 1 LH 8.00 Do the Modification of Lower Aft Corner of the Door Frame at Emergency Exit Door Type 1 LH 8.00 Do the Modification of the Lower Forward Corner of the Door Frame at Emergency Exit Door Type 1 LH 8.00 Remove Fasteners at Upper Forward Corner of the Door Frame at Emergency Exit Door Type 1 RH 1.00 Do the Inspection of Fastener Holes at Upper Forward Corner of the Door Frame at Emergency Exit Door Type 1 RH 0.50 Remove Fasteners at Upper Aft Corner of the Door Frame at Emergency Exit Door Type 1 RH 1.00 Do the Inspection of Fastener Holes at Upper Aft Corner of the Door Frame at Emergency Exit Door Type 1 RH 0.50 Remove Fasteners at Lower Aft Corner of the Door Frame at Emergency Exit Door Type 1 RH 1.00 Do the Inspection of Fastener Holes at Lower Aft Corner of the Door Frame at Emergency Exit Door Type 1 RH 0.50 Remove Fasteners at Lower Forward Corner of the Door Frame at Emergency Exit Door Type 1 RH 1.00 Do the Inspection of Fastener Holes at Lower Forward Corner of the Door Frame at Emergency Exit Door Type 1 RH 0.50 Do the Modification of Upper Forward Corner of the Door Frame at Emergency Exit Door Type 1 RH 8.00 Do the Modification of Upper Aft Corner of the Door Frame at Emergency Exit Door Type 1 RH 8.00 Do the Modification of the Lower Aft Corner of the Door Frame at Emergency Exit Door Type 1 RH 8.00 Do the Modification of Lower Forward Corner of the Door Frame at Emergency Exit Door Type 1 RH 8.00 Remove Rain Gutter at Emergency Exit Door Type 1 Area LH 1.00 Remove Fasteners between FR53.6 and FR53.7 and between STGR4 and STGR15A, LH 10.00 Do the Inspection of the Fastener Holes between FR53.6 and FR53.7 and between STGR4 and STGR15A, LH 1.50 Remove Fasteners between FR53.6 and FR53.7 and between STGR26 and STGR30, LH 4.00 Do the Inspection of the Fastener Holes between FR53.6 and FR53.7 and between STGR26 and STGR30, LH 1.00 DATE: Jan 15/15 SERVICE BULLETIN No.: A330-53-3226 REVISION No.: 03 - Sep 10/18 Page: 30 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 59 @A330 SERVICE BULLETIN Task 533226-831-848-001: Modification Install Doubler at Circumferential Joint between FR53.6 and FR53.7 and between STGR4 and STGR15A, LH 28.00 Install Rain Gutter at Emergency Exit Door Type 1 Area LH 4.00 Install Doubler at Circumferential Joint between FR53.6 and FR53.7 and between STGR26 and STGR30, LH 19.00 Remove Rain Gutter at Emergency Exit Door Type 1 Area RH 1.00 Remove Fasteners between FR53.6 and FR53.7 and between STGR4 and STGR15A, RH 10.00 Do the Inspection of the Fasteners Holes between FR53.6 and FR53.7 and between STGR4 and STGR15A, RH 1.50 Remove Fasteners from between FR53.6 and FR53.7 and between STGR26 and STGR30, RH 4.00 Do the Inspection of the Fastener Holes between FR53.6 and FR53.7 and between STGR26 and STGR30, RH 1.00 Install Doubler at Circumferential Joint between FR53.6 and FR53.7 and between STGR4 and STGR15A, RH 28.00 Install Rain Gutter at Emergency Exit Door Type 1 Area RH 4.00 Install Doubler at Circumferential Joint between FR53.6 and FR53.7 and between STGR26 and STGR30, RH 19.00 Apply Protections to the Upper Door Frame Area, LH 0.25 Apply Protections to the Lower Door Frame Area, LH 0.25 Apply Protections to the Upper Door Frame Area, RH 0.25 Apply Protections to the Lower Door Frame Area, RH 0.25 Install Cross Plate of the Emergency Door Upper Area, LH 6.00 Install Cross Plate of the Emergency Door Upper Area, RH 6.00 Install the Scuff Plates to the LH Emergency Exit Door 6.00 Install the Scuff Plates to the RH Emergency Exit Door 3.00 Do the Modification of the LH Emergency Exit Door 6.00 Do the Modification of the RH Emergency Exit Door 6.00 Tests 2.00 Close-Up 24.00 TOTAL MANHOURS 317.00 ELAPSED TIME (HOURS) 69.00 NOTE : For an explanation of the manhours and elapsed time, refer to the Gantt Chart, Fig. A-GAAAA given in Appendix 01 - Manpower Gantt Chart. DATE: Jan 15/15 SERVICE BULLETIN No.: A330-53-3226 REVISION No.: 03 - Sep 10/18 Page: 31 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 60 @A330 SERVICE BULLETIN **CONF 003 Task 533226-831-848-001: Modification Get Access 26.00 On Aircraft Perform Paint-Stripping of the Aircraft Skin at the Modification Area LH 1.00 Perform Paint-Stripping of the Aircraft Skin at the Modification Area RH 1.00 Remove Cross Plate from the Emergency Door Upper Area, LH 6.00 Remove Cross Plate from the Emergency Door Upper Area, RH 6.00 Remove Fasteners at Upper Forward Corner of the Door Frame at Emergency Exit Door Type 1 LH 1.00 Do the Inspection of Fastener Holes at Upper Forward Corner of the Door Frame at Emergency Exit Door Type 1 LH 0.50 Remove Fasteners at Upper Aft Corner of the Door Frame at Emergency Exit Door Type 1 LH 1.00 Do the Inspection of the Fastener Holes at Upper Aft Corner of the Door Frame at Emergency Exit Door Type 1 LH 0.50 Do the Modification of Upper Forward Corner of the Door Frame at Emergency Exit Door Type 1 LH 8.00 Do the Modification of Upper Aft Corner of the Door Frame at Emergency Exit Door Type 1 LH 8.00 Remove Fasteners at Upper Forward Corner of the Door Frame at Emergency Exit Door Type 1 RH 1.00 Do the Inspection of Fastener Holes at Upper Forward Corner of the Door Frame at Emergency Exit Door Type 1 RH 0.50 Remove Fasteners at Upper Aft Corner of the Door Frame at Emergency Exit Door Type 1 RH 1.00 Do the Inspection of Fastener Holes at Upper Aft Corner of the Door Frame at Emergency Exit Door Type 1 RH 0.50 Do the Modification of Upper Forward Corner of the Door Frame at Emergency Exit Door Type 1 RH 8.00 Do the Modification of Upper Aft Corner of the Door Frame at Emergency Exit Door Type 1 RH 8.00 Remove Rain Gutter at Emergency Exit Door Type 1 Area LH 1.00 Remove Fasteners between FR53.6 and FR53.7 and between STGR4 and STGR15A, LH 10.00 Do the Inspection of the Fastener Holes between FR53.6 and FR53.7 and between STGR4 and STGR15A, LH 1.50 DATE: Jan 15/15 SERVICE BULLETIN No.: A330-53-3226 REVISION No.: 03 - Sep 10/18 Page: 32 6 Printed in FRANCE © AIRBUS S.A.S. 2007. 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