# Airbus Service Bulletin A330-34-3342 Copy: Revision 01 ("A330-34-3342 R01"), 35 pages: PDF https://openairdocs.org/files/sha256/00/7a/007afa6c75f156ef11f4a6ac891821500e009cc07e7bc93f52e730425a790f0d; text https://openairdocs.org/service-documents/airbus/a330-34-3342/file/007afa6c75f1.md. Rights: © Airbus S.A.S. Filed by the FAA in regulations.gov docket FAA-2017-1096; AD 2018-06-01 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication. ## Details - Manufacturer: [Airbus](https://openairdocs.org/service-documents/airbus.md) - Type: Service bulletin (Service Bulletin) - Number: A330-34-3342 - Latest revision known: A330-34-3342, Revision 01, dated November 13, 2017 (OpenAirDocs) - Page: https://openairdocs.org/service-documents/airbus/a330-34-3342 ## ADs that cite it (1) (OpenAirDocs) Newest first, with the revision each names, as OpenAirDocs read it from the AD's text. - [AD 2018-06-01](https://openairdocs.org/ad/2018-06-01.md), effective Apr 30, 2018: Revision 01 Also cited in [1 proposed AD](https://openairdocs.org/service-documents/airbus/a330-34-3342/proposed.md). ## Text (35 pages) Rights: © Airbus S.A.S. Filed by the FAA in regulations.gov docket FAA-2017-1096; AD 2018-06-01 incorporates this document by reference. 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: 34 TITLE: NAVIGATION - TCAS - INSTA LL NEW TCAS SOFTWARE TO CORRECT UNJUSTIFIED RESOLUTION ADVISORY MODIFICATION No.: 206608S34248 This page transmits Revision No.01 of Service Bulletin No.A330-34-3342 ADDITIONAL WORK **CONF ALL No additional work is required by this revision for aircraft modified by any previous issue. REASON Revision No. 01 has been issued to update the effectivity and to update the Accomplishment Timescale paragraph. CHANGES The main changes of this revision are: - Update the Effectivity - Update the Compliance Section - Update Standard Sentences SUMMARY REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES REASON UPDATED R EFFECTIVITY OPERATOR LIST UPDATED R CONCURRENT REQUIREMENTS CONCURRENT REQUIREMENTS UPDATED R NATURE OF THE WORK NATURE OF WORK TABLE UPDATED R PLANNING INFORMATION EFFECTIVITY EFFECTIVITY RELATED INFORMATION UPDATED R Configuration definition DATE: Apr 19/17 SERVICE BULLETIN No.: A330-34-3342 REVISION No.: 01 - Nov 13/17 Page: 1 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 2 @A330 SERVICE BULLETIN REVISION TRANSMITTAL SHEET CONF 001 CONFIGURATION DEFINITION UPDATED R CONCURRENT REQUIREMENTS CONCURRENT SB LIST UPDATED R REASON History HISTORY UPDATED R Objective/Action OBJECTIVE/ACTION UPDATED R Advantages ADVANTAGES UPDATED R DESCRIPTION DESCRIPTION UPDATED R COMPLIANCE Accomplishment Timescale ACCOMPLISHMENT TIMESCALE UPDATED R INTERCHANGEABILITY/MIXABILITY INTERCHANGEABILITY/MIXABILITY UPDATED R MATERIAL INFORMATION MATERIAL - PRICE AND AVAILABILITY Price and Availability PRICE AND AVAILABILITY UPDATED R PARTS TO BE RE-IDENTIFIED BY OPERATOR PARTS TO BE RE-IDENTIFIED BY OPERATOR UPDATED R Reidentified part set REIDA01 PART MATERIAL SET UPDATED R ACCOMPLISHMENT INSTRUCTIONS TASK 343342- 831-801-001-Option 1 - Modify the TCAS Computer TASK SOLUTION UPDATED NOTE UPDATED CAUTION UPDATED R Subtask 343342-941-001-001 SUBTASK SOLUTION UPDATED NOTE UPDATED R Subtask 343342-470-001-001 SUBTASK SOLUTION UPDATED REFERENCED DOCUMENTATION UPDATED MATERIAL LIST UPDATED R TASK 343342- 831-802-001-Option 2 - Replace the TCAS Computer TASK SOLUTION UPDATED NOTE UPDATED CAUTION UPDATED R Subtask 343342-941-002-001 SUBTASK SOLUTION UPDATED NOTE 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 No previous revision REVISION SEQUENCE ORIGINAL: Apr 19/17 REVISION No. : 01 - Nov 13/17 DATE: Apr 19/17 SERVICE BULLETIN No.: A330-34-3342 REVISION No.: 01 - Nov 13/17 Page: 2 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 3 @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: 34 TITLE: NAVIGATION - TCAS - INSTA LL NEW TCAS SOFTWARE TO CORRECT UNJUSTIFIED RESOLUTION ADVISORY **CONF ALL MODIFICATIONS MODIFICATION CLASSIFICATION MAJOR 206608S34248 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 Unjustified Traffic Alert and Collision Avoidance System (TCAS) Resolution Advisory (RA) triggered with Honeywell TCAS TPA100-B PN 940-0351-001 have been reported. The unexpected RAs are triggered when two aircraft are crossing at the same flight level or are in vertical convergence but when conditions for RA generation are not satisfied. Usually, the unexpected RA is preceded by a very short Traffic Advisory (TA) and in some cases no audibile TA is provided. The duration of the unexpected RA can be up to 1 minute. The crew then has to comply with the TCAS order that leads to unnecessary avoidance maneuvers. This Service Bulletin is published to advise all operators of A330 aircraft of the issue of HONEYWELL Service Bulletin No. 940-0351-34-0005. This Service Bulletin replaces the TCAS (FIN 1SG) Honeywell TPA-100B change 7.1 PN 940-0351-001 installed with MOD No. 57609S30373 (Service Bulletin No. A330-34-3247 or Service Bulletin No. A330-34-3281 or Service Bulletin No. A330-34-3344) by a new PN 940-0351-005 which corrects unjustified resolution advisory with software changes. The introduction of this new TCAS standard will include the following changes: DATE: Apr 19/17 SERVICE BULLETIN No.: A330-34-3342 REVISION No.: 01 - Nov 13/17 Page: 1 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 4 @A330 SERVICE BULLETIN SUMMARY - Implementation of change 2 of DO-300 to solve the in-service occurrence titled "Eurocontrol report of False TCAS Resolution Advisory with TPA100-B" - Modify Global Positioning System (GPS) check from 500 ms to 200 ms for robustness - Modification linked to minor open anomalies correction and product robustness improvements and enhancements. GENERAL EVALUATION EVALUATION TABLE COMPLIANCE MANDATORY (1) CANCELS INSPECTION SB NO POTENTIAL AD YES A/C OPERATION AFFECTED NO RELIABILITY AFFECTED NO PAX COMFORT AFFECTED NO COST SAVING NO ETOPS AFFECTED NO STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED YES NOTE (1) : Service Bulletin must be accomplished. MATERIAL PRICE INFORMATION MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Equipment BFEA01 1 See SB TCAS Computer EFFECTIVITY This Service Bulletin is applicable to this (these) operator(s) : 36V 43P 56O 64N 83V AAR AEA AFL ALK ARA ARG AVA AZA BEC BEL BER CAL CBJ CCA CES CHH CPA CRK CSN DAH DLH EDW EIN ETD EVE FIN GCR GFA GIA GRL HAL HDA HKC HVN IBE IRA KAC KLM LNI MAS MEA MNB NWS OBS ONE PAL QTR RSY RWD SAA SAI SAS SEY SIA SWR TAP TAR TBA TCX THA THY TNA TPA TPU VIR WOW WRC XAX XLF CONCURRENT REQUIREMENTS Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishment of the following Service Bulletin(s): Service Bulletin No. A330-34-3247 A330-34-3281 A330-34-3344 NOTE : Service Bulletin No. A330-34-3247 (NAVIGATION - TCAS - INSTALL TCAS HONEYWELL TPA-100B , ATSAW CAPABLE) is a concurr ent requirement if MOD No. 57609S30373 has not been embodied before delivery. NOTE : Service Bulletin No. A330-34-3281 (NAVIGATION - TCAS - REPLACE ACSS T2CAS BY TCAS 7.1 FROM HONEYWELL AND EGPWC -003 STANDARD) is a concurrent requirement if MOD No. 57609S30373 has not been embodied before delivery. DATE: Apr 19/17 SERVICE BULLETIN No.: A330-34-3342 REVISION No.: 01 - Nov 13/17 Page: 2 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 5 @A330 SERVICE BULLETIN SUMMARY NOTE : Service Bulletin No. A330-34-3344 (NAVIGATION -TCAS - INSTALL HONEYWELL TCAS TPA100B FROM NO TCAS CONFIGURATION) is a concurrent requirement if MOD No. 57609S30373 has not been embodied before delivery. NOTE : Accomplish either Service Bulletin No. A330-34-3247 or Service Bulletin No. A330-34-3281 or Service Bulletin No. A330-34-3344 as per effectivity specified in these Service Bulletins. REFERENCES / REPERCUSSIONS TFU 34.43.00.022 OEB None AOT None SIL None ISI None LINE MAINTENANCE AFFECTED No LIFE LIMIT None OTHER None NATURE OF THE WORK AIRCRAFT NO EQUIPMENT YES MANPOWER Task 343342-831-801-001: Option 1 - Modify the TCAS Computer TOTAL MANHOURS 1.50 ELAPSED TIME (HOURS) 1.50 Additional manhours relat ed to Vendor SB; refer to: Modify the Traffic Collision Avoidance System (TCAS) Computer by Vendor HONEYWELL Service Bulletin No. 940-0351-34-0005 Honeywell Service Bulletin No. 940-0351-34-0005 Task 343342-831-802-001: Option 2 - Replace the TCAS Computer TOTAL MANHOURS 2.00 ELAPSED TIME (HOURS) 2.00 APPENDICES None DATE: Apr 19/17 SERVICE BULLETIN No.: A330-34-3342 REVISION No.: 01 - Nov 13/17 Page: 3 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 6 @A330 SERVICE BULLETIN SUMMARY **CONF ALL A 800VU FR18 FR20 A 811VU 1SG THE TCAS COMPUTER Z120 MODIFY OR REPLACE G_SB_343342_5_SAAA_01_01 Figure A-FSAAA - Sheet 01 DATE: Apr 19/17 SERVICE BULLETIN No.: A330-34-3342 REVISION No.: 01 - Nov 13/17 Page: 4 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 7 @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: 34 TITLE: NAVIGATION - TCAS - INSTA LL NEW TCAS SOFTWARE TO CORRECT UNJUSTIFIED RESOLUTION ADVISORY MODIFICATION No.: 206608S34248 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 only applicable on aircraft on which Honeywell TCAS TPA100-B PN 940-0351-001 is installed. (1) Models 330-202 330-203 330-223 330-223F 330-243 330-243F 330-301 330-302 330-303 330-321 330-322 330-323 330-342 330-343 (2) Effectivity by MSN 0012 0017 0030 0037 0045 0050 0071 0082-0083 0095-0096 0099 0102 0106 0109 0112-0113 0116 0118 0120-0122 0127 0155 0171 0181 0195 0223 0230 0234 0244 0276 0281 0286-0287 0290 0296 0300 0317 0322 0324 0334 0340 0346 0386 0389 0393 0403 0405 0418 0420-0421 0423 0432 0439 0444 0454 0456 0461 0469 0476 0479 0493 0496-0497 0501 0512 0515 0539 0548 0565 0568 0581 0602 0607 0635 0640-0641 0644 0647 0650 0653-0654 0658 0662 0667 0669-0671 0673 0675-0676 0679 0682 0686 0688 0691-0692 0697 0699 0703-0704 0707-0708 0714 0716-0717 0724-0725 0729-0730 0737-0739 0741-0742 0750-0752 0754 0756 0759 0769-0770 0772 0774 0776 0780 0785-0786 0788 0797 0801 0803 0805 0807 0809-0811 0815 0819 0823-0825 0828 0831-0834 0838-0839 0845 0850 0852 0854-0855 0860-0861 0863 0867-0869 0873-0877 0881 0884 0890-0891 0895 0899-0900 0903-0904 0906 DATE: Apr 19/17 SERVICE BULLETIN No.: A330-34-3342 REVISION No.: 01 - Nov 13/17 Page: 1 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 8 @A330 SERVICE BULLETIN 0909 0911 0914-0915 0919-0920 0925-0927 0930 0934 0939 0941 0944 0946 0948-0949 0957 0959 0961 0963 0967-0968 0973 0975 0977-0978 0982-0984 0986 0988 0991 0994-0995 0997-0998 1000-1001 1004 1006-1007 1009-1010 1012-1016 1018 1020 1023 1026 1028-1029 1032 1045 1047 1051-1053 1055 1058 1062 1065 1067 1070-1073 1077-1078 1081 1084-1085 1087-1089 1092 1097-1099 1101 1103-1105 1107 1110 1112 1114-1115 1118 1124 1130 1132 1136 1145-1146 1148-1151 1156-1157 1159-1161 1163-1164 1167-1168 1170-1173 1175 1177-1178 1180-1181 1184 1187-1188 1190-1191 1193 1195-1196 1199 1201 1204-1206 1208-1217 1219 1221-1224 1226 1228-1229 1231-1232 1234 1236-1237 1239-1240 1243 1245 1247 1249 1255 1259-1264 1267 1269-1272 1276-1282 1284-1292 1294-1296 1298-1305 1307 1310-1311 1314-1318 1320 1322-1326 1328-1333 1336-1338 1340-1350 1352-1353 1355-1358 1360 1362 1364 1366-1369 1371-1375 1377-1378 1380-1389 1392 1395-1396 1398-1406 1408-1410 1413-1414 1418 1421-1422 1425-1431 1434-1438 1440 1442-1444 1446-1450 1453 1456-1461 1463-1464 1467-1471 1474-1477 1479 1482 1484-1490 1492-1494 1496-1497 1500 1503-1504 1506-1511 1515 1517-1521 1523-1525 1530-1532 1534 1536-1541 1544-1548 1550-1551 1553 1557-1560 1562-1563 1565-1570 1573 1575 1577-1578 1580 1584-1588 1591 1593-1595 1597-1598 1603 1606 1608-1609 1613-1615 1617-1618 1621 1625-1626 1630-1634 1636 1639 1641 1643 1645 1648-1649 1653-1658 1660 1663-1666 1668 1671-1673 1675 1677-1678 1680-1681 1685-1686 1688 1691 1693-1695 1697-1700 1703 1708-1711 1714-1715 1719 1722-1723 1725 1728 1730 1732-1733 1736 1740-1742 1744-1745 1747 1750-1761 1763 1765 1768 1771-1773 1776-1777 1779 (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 36V 1164 43P 1053 56O 0116 0127 64N 1751 83V 0171 AAR 0640 0676 0708 0772 0803 0845 1001 1055 1151 1211 1326 1340 1435 1464 1518 AEA 0461 1097 AFL 0963 0973 1014 1045 1047 1058 1065 1072 1077 1103 1232 1247 1264 1270 1284 1299 1301 1323 1328 1345 1356 1371 ALK 0456 ARA 0891 0927 ARG 0290 0300 AVA 1009 1016 1073 1208 1224 1279 1342 1400 1492 AZA 0825 0831 BEC 0863 BEL 0030 0037 0045 0082 0095 0324 1085 BER 0322 0403 0432 0444 0454 0469 0476 0493 0739 0828 0911 0968 1112 DATE: Apr 19/17 SERVICE BULLETIN No.: A330-34-3342 REVISION No.: 01 - Nov 13/17 Page: 2 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 9 @A330 SERVICE BULLETIN OPERATOR MSN CAL 0602 0607 0641 0671 0675 0691 0699 0707 0714 0725 0752 0769 0805 0823 0838 0861 0920 1177 1272 1278 1346 1367 1450 1539 CBJ 0988 1020 1028 1052 1753 1763 CCA 0750 0756 0759 0780 0785 0797 0810 0815 0839 0860 0867 0873 0884 0890 0903 0909 0930 0941 0944 0957 1087 1110 1130 1187 1199 1216 1237 1260 1282 1304 1330 1333 1353 1373 1383 1396 1413 1434 1444 1459 1471 1493 1509 1525 1538 1541 1563 1570 1587 1658 1673 1685 1695 1752 1765 CES 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 CHH 0875 0881 0906 0982 1159 1168 1178 1190 1255 1325 1438 1532 1558 1573 1591 1614 1634 1656 1663 1677 1686 1703 CPA 0102 0113 0121 0386 0389 0393 0418 0420 0421 0423 0439 0539 0548 0565 0679 0776 0850 0855 0895 0915 0959 1163 1196 1222 1239 1285 1317 1343 1349 1362 1366 1387 1409 1436 1443 1618 1621 CRK 1051 1062 1099 1105 1107 1115 1124 1146 1157 1277 1286 1322 1358 1369 1384 1398 1668 CSN 1392 1425 1430 1494 1519 1536 1575 1593 1625 1636 1645 1699 1714 1760 1776 DAH 0644 0647 0650 0653 0667 1613 1630 1649 DLH 1292 1305 1314 1497 EDW 1193 1711 EIN 1742 1744 ETD 0658 0688 0717 0724 0729 0730 0737 0788 0809 0824 0832 0852 0854 0868 0975 0991 1032 1070 1071 1081 1167 1205 1226 1245 1414 1486 1521 1524 1772 EVE 0670 1691 FIN 0994 1007 1013 1023 1067 1078 1088 1173 GCR 0919 1756 1758 1773 GFA 0276 0281 0286 0287 0334 0340 GIA 1184 1214 1261 1288 1364 1410 1446 1474 1548 1560 1577 1585 1654 1671 1698 1709 1723 1733 GRL 0230 HAL 1104 1114 1171 1217 1259 1295 1302 1310 1316 1389 1399 1404 1422 1469 1488 1496 1511 1530 1565 1606 1615 1672 1732 HDA 0012 0017 0071 0083 0099 0106 0109 0118 0155 0234 0244 0405 0479 0512 0581 0669 0673 1457 1503 1523 1545 1557 1567 1598 HKC 1175 1320 HVN 0946 IBE 1377 1385 1405 1426 1437 1490 1507 1515 1694 1700 1710 1719 1728 1736 1740 1747 1755 1761 1777 IRA 1540 1586 KAC 1626 1643 1653 1678 1681 KLM 0682 0686 0703 0738 0770 0801 0925 1161 1287 1294 1300 1381 1580 LNI 1675 1680 1693 DATE: Apr 19/17 SERVICE BULLETIN No.: A330-34-3342 REVISION No.: 01 - Nov 13/17 Page: 3 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 10 @A330 SERVICE BULLETIN OPERATOR MSN MAS 1136 1148 1180 1209 1219 1229 1234 1243 1281 1318 1336 1337 1347 1388 1395 1431 1470 1489 MEA 0926 0984 0995 0998 1725 MNB 1332 NWS 1213 1221 OBS 0833 ONE 1506 1508 1608 1657 PAL 1449 1456 1460 1463 1467 1475 1482 1504 1510 1531 1546 1553 1559 1566 1568 QTR 1350 1386 1406 1578 1584 1594 1688 1708 RSY 0096 0120 RWD 1741 1759 SAA 1191 1210 1223 1236 1249 1271 1745 1754 1757 1779 SAI 0811 0819 0834 0900 SAS 0496 0497 0515 0568 1660 1665 1697 1715 SEY 0751 0807 SIA 0978 0983 0986 1010 1132 1149 1156 1382 1401 1427 1447 1453 1477 1485 1517 1544 1562 1597 1609 1633 1648 1666 SWR 1000 1018 1026 1029 1084 1089 1101 1145 1181 1188 1276 1290 1355 1403 TAP 0181 0195 0223 0317 0877 0899 0904 0914 0934 0997 1006 1012 1015 TAR 1631 1641 TBA 1730 1771 TCX 0948 0967 THA 0050 0112 0122 0346 1263 1269 1289 1338 1348 1374 1408 THY 0697 0704 0742 0754 0774 0869 0874 0876 0939 0949 0961 0977 1004 1092 1118 1150 1160 1170 1172 1204 1212 1228 1240 1298 1307 1311 1344 1418 1442 1458 1476 1487 1550 1722 1750 1768 TNA 1357 1378 TPA 1368 1380 1428 1534 TPU 1448 VIR 1195 1201 1206 1215 1231 1296 1315 1329 1341 1352 WOW 1098 WRC 0296 XAX 0654 0662 0692 0716 0741 0786 XLF 0501 0635 1360 DATE: Apr 19/17 SERVICE BULLETIN No.: A330-34-3342 REVISION No.: 01 - Nov 13/17 Page: 4 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 11 @A330 SERVICE BULLETIN (4) Configuration by MSN MSN CONFIGURATION 0012 0017 0030 0037 0045 0050 0071 0082 0083 0095 0096 0099 0102 0106 0109 0112 0113 0116 0118 0120 0121 0122 0127 0155 0171 0181 0195 0223 0230 0234 0244 0276 0281 0286 0287 0290 0296 0300 0317 0322 0324 0334 0340 0346 0386 0389 0393 0403 0405 0418 0420 0421 0423 0432 0439 0444 0454 0456 0461 0469 0476 0479 0493 0496 0497 0501 0512 0515 0539 0548 0565 0568 0581 0602 0607 0635 0640 0641 0644 0647 0650 0653 0654 0658 0662 0667 0669 0670 0671 0673 0675 0676 0679 0682 0686 0688 0691 0692 0697 0699 0703 0704 0707 0708 0714 0716 0717 0724 0725 0729 0730 0737 0738 0739 0741 0742 0750 0751 0752 0754 0756 0759 0769 0770 0772 0774 0776 0780 0785 0786 0788 0797 0801 0803 0805 0807 0809 0810 0811 0815 0819 0823 0824 0825 0828 0831 0832 0833 0834 0838 0839 0845 0850 0852 0854 0855 0860 0861 0863 0867 0868 0869 0873 0874 0875 0876 0877 0881 0884 0890 0891 0895 0899 0900 0903 0904 0906 0909 0911 0914 0915 0919 0920 0925 0926 0927 0930 0934 0939 0941 0944 0946 0948 0949 0957 0959 0961 0963 0967 0968 0973 0975 0977 0978 0982 0983 0984 0986 0988 0991 0994 0995 0997 0998 1000 1001 1004 1006 1007 1009 1010 1012 1013 1014 1015 1016 1018 1020 1023 1026 1028 1029 1032 1045 1047 1051 1052 1053 1055 1058 1062 1065 1067 1070 1071 1072 1073 1077 1078 1081 1084 1085 1087 1088 1089 1092 1097 1098 1099 1101 1103 1104 1105 1107 1110 1112 1114 1115 1118 1124 1130 1132 1136 1145 1146 1148 1149 1150 1151 1156 1157 1159 1160 1161 1163 1164 1167 1168 1170 1171 1172 1173 1175 1177 1178 1180 1181 1184 1187 1188 1190 1191 1193 1195 1196 1199 1201 1204 1205 1206 1208 1209 1210 1211 1212 1213 1214 1215 1216 1217 1219 1221 1222 1223 1224 1226 1228 1229 1231 1232 1234 1236 1237 1239 1240 1243 1245 1247 1249 1255 1259 1260 1261 1262 1263 1264 1267 1269 1270 1271 1272 1276 1277 1278 1279 1280 1281 1282 1284 1285 1286 1287 1288 1289 1290 1291 1292 1294 1295 1296 1298 1299 1300 1301 1302 1303 1304 1305 1307 1310 1311 1314 1315 1316 1317 1318 1320 1322 1323 1324 1325 1326 1328 1329 1330 1331 1332 1333 1336 1337 1338 1340 1341 1342 1343 1344 1345 1346 1347 1348 1349 1350 1352 1353 1355 1356 1357 1358 1360 1362 1364 1366 1367 1368 1369 1371 1372 1373 1374 1375 1377 1378 1380 1381 1382 1383 1384 1385 1386 1387 1388 1389 1392 1395 1396 1398 1399 1400 1401 1402 1403 1404 1405 1406 1408 1409 1410 1413 1414 1418 1421 1422 1425 1426 1427 1428 1429 1430 1431 1434 1435 1436 1437 1438 1440 1442 1443 1444 1446 1447 1448 1449 1450 1453 1456 1457 1458 1459 1460 1461 1463 1464 1467 1468 1469 1470 1471 1474 1475 1476 1477 1479 1482 1484 1485 1486 1487 1488 1489 1490 1492 1493 1494 1496 1497 1500 1503 1504 1506 1507 1508 1509 1510 1511 1515 1517 1518 1519 1520 1521 1523 1524 1525 1530 1531 1532 1534 1536 1537 001 DATE: Apr 19/17 SERVICE BULLETIN No.: A330-34-3342 REVISION No.: 01 - Nov 13/17 Page: 5 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 12 @A330 SERVICE BULLETIN MSN CONFIGURATION 1538 1539 1540 1541 1544 1545 1546 1547 1548 1550 1551 1553 1557 1558 1559 1560 1562 1563 1565 1566 1567 1568 1569 1570 1573 1575 1577 1578 1580 1584 1585 1586 1587 1588 1591 1593 1594 1595 1597 1598 1603 1606 1608 1609 1613 1614 1615 1617 1618 1621 1625 1626 1630 1631 1632 1633 1634 1636 1639 1641 1643 1645 1648 1649 1653 1654 1655 1656 1657 1658 1660 1663 1664 1665 1666 1668 1671 1672 1673 1675 1677 1678 1680 1681 1685 1686 1688 1691 1693 1694 1695 1697 1698 1699 1700 1703 1708 1709 1710 1711 1714 1715 1719 1722 1723 1725 1728 1730 1732 1733 1736 1740 1741 1742 1744 1745 1747 1750 1751 1752 1753 1754 1755 1756 1757 1758 1759 1760 1761 1763 1765 1768 1771 1772 1773 1776 1777 1779 001 (5) Configuration definition **CONF 001 Config. 001 is valid for all the aircraft given in the effectivity of this Service Bulletin as a standard configuration. (6) Material Effectivity MATERIAL QTY PER A/C SEE NOTES Reidentified part set REIDA01 1 Equipment BFEA01 1 B. CONCURRENT REQUIREMENTS Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishment of the following Service Bulletin(s): Service Bulletin No. A330-34-3247 A330-34-3281 A330-34-3344 NOTE : Service Bulletin No. A330-34-3247 (NAVIGATION - TCAS - INSTALL TCAS HONEYWELL TPA-100B , ATSAW CAPABLE) is a conc urrent requirement if MOD No. 57609S30373 has not been embodied before delivery. NOTE : Service Bulletin No. A330-34-3281 (NAVIGATION - TCAS - REPLACE ACSS T2CAS BY TCAS 7.1 FROM HONEYWELL AND EGPWC -003 STANDARD) is a concurrent requirement if MOD No. 57609S30373 has not been embodied before delivery. NOTE : Service Bulletin No. A330-34-3344 (NAVIGATION -TCAS - INSTALL HONEYWELL TCAS TPA100B FROM NO TCAS CONFIGURATION) is a concurrent requirement if MOD No. 57609S30373 has not been embodied before delivery. NOTE : Accomplish either Service Bulletin No. A330-34-3247 or Service Bulletin No. A330-34-3281 or Service Bulletin No. A330-34-3344 as per effectivity DATE: Apr 19/17 SERVICE BULLETIN No.: A330-34-3342 REVISION No.: 01 - Nov 13/17 Page: 6 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 13 @A330 SERVICE BULLETIN specified in these Service Bulletins. C. REASON (1) History Unjustified Traffic Alert and Collision Avoidance System (TCAS) Resolution Advisory (RA) triggered with Honeywell TCAS TPA100-B PN 940-0351-001 have been reported. The unexpected RAs are triggered when two aircraft are crossing at the same flight level or are in vertical convergence but when conditions for RA generation are not satisfied. Usually, the unexpected RA is preceded by a very short Traffic Advisory (TA) and in some cases no audibile TA is provided. The duration of the unexpected RA can be up to 1 minute. The crew then has to comply with the TCAS order that leads to unnecessary avoidance maneuvers. (2) Objective/Action This Service Bulletin is published to advise all operators of A330 aircraft of the issue of HONEYWELL Service Bulletin No. 940-0351-34-0005. This Service Bulletin replaces the TCAS (FIN 1SG) Honeywell TPA-100B change 7.1 PN 940-0351-001 installed with MOD No. 57609S30373 (Service Bulletin No. A330-34-3247 or Service Bulletin No. A330-34-3281 or Service Bulletin No. A330-34-3344) by a new PN 940-0351-005 which corrects unjustified resolution advisory with software changes. (3) Advantages The introduction of this new TCAS standard will include the following changes: - Implementation of change 2 of DO-300 to solve the in-service occurrence titled "Eurocontrol report of False TCAS Resolution Advisory with TPA100-B" - Modify Global Positioning System (GPS) check from 500 ms to 200 ms for robustness - Modification linked to minor open anomalies correction and product robustness improvements and enhancements. (4) Operational/Maintenance Consequences None D. DESCRIPTION NOTE : To accomplish this Service Bulletin, you have 2 options. To accomplish this Service Bulletin it is necessary to : Task 343342-831-801-001: Option 1 - Modify the TCAS Computer (1) Modify the Traffic Collision Avoidance System (TCAS) Computer by Vendor DATE: Apr 19/17 SERVICE BULLETIN No.: A330-34-3342 REVISION No.: 01 - Nov 13/17 Page: 7 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 14 @A330 SERVICE BULLETIN HONEYWELL Service Bulletin No. 940-0351-34-0005 Task 343342-831-802-001: Option 2 - Replace the TCAS Computer (1) Remove the Traffic Collision Avoidance System (TCAS) Computer (2) Install the Traffic Collision Avoidance System (TCAS) Computer E. COMPLIANCE (1) Classification MANDATORY: Service Bulletin must be accomplished. (2) Accomplishment Timescale This Service Bulletin has been classified Mandatory by the issue of an Airworthiness Directive (AD) published by the European Av iation Safety Agenc y (EASA). The AD must be used as the reference document for the mandated accomplishment timescale. F. APPROVAL The technical content of this document is approved under the authority of Design Organisation Approval No. EASA.21J.031. If an aircraft listed in the effectivity has a modification or repair embodied that is not of AIRBUS origin, and which affects the content of this Service Bulletin, the operator is responsible for obtaining approval by its airworthiness authority for any adaptation necessary before incorporation of the Service Bulletin. 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. Task 343342-831-801-001: Option 1 - Modify the TCAS Computer Get Access 0.50 Tests 0.50 Close-Up 0.50 TOTAL MANHOURS 1.50 ELAPSED TIME (HOURS) 1.50 Additional manhours relat ed to Vendor SB; refer to: Modify the Traffic Collision Avoidance System (TCAS) Computer by Vendor HONEYWELL Service Bulletin No. 940-0351-34-0005 Honeywell Service Bulletin No. 940-0351-34-0005 DATE: Apr 19/17 SERVICE BULLETIN No.: A330-34-3342 REVISION No.: 01 - Nov 13/17 Page: 8 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 15 @A330 SERVICE BULLETIN Task 343342-831-802-001: Option 2 - Replace the TCAS Computer Get Access 0.50 On Aircraft Remove the Traffic Collision Avoidance System (TCAS) Computer 0.25 Install the Traffic Collision Avoidance System (TCAS) Computer 0.25 Tests 0.50 Close-Up 0.50 TOTAL MANHOURS 2.00 ELAPSED TIME (HOURS) 2.00 H. WEIGHT AND BALANCE Not Changed I. ELECTRICAL LOAD DATA Not Changed J. REFERENCES Aircraft Maintenance Manual (AMM) 06-20-00 06-31-53 06-41-53 12-34-24 20-16-00 24-42-00 34-43-00 34-43-34 45-10-00 52-41-00 ATA Common Support Data Dictionary (CSDD), Chapter 2 Elec. Std. Practices Manual (ESPM) 20-55-00 Service Bulletin (SB) A330-34-3247 A330-34-3281 A330-34-3344 Vendor Service Bulletin (VSB) Honeywell Service Bulletin No. 940-0351-34-0005 K. PUBLICATION AFFECTED Aircraft Wiring List (AWL) Illustrated Parts Catalog (IPC) 34-43-08 34-43-34 L. INTERCHANGEABILITY/MIXABILITY The interchangeability/mixability possibilities are for new or modified parts introduced by the accomplishment of this Service Bulletin. DESCRIPTION OLD PART N˚ NEW PART N˚ INT MIXABILITY SEE NOTES TCAS Computer 940-0351-001 940-0351-005 01 Not Applicable NOTE : For definitions of interchangeability codes in column INT., refer to ATA Common Support Data Dictionary (CSDD), Chapter 2. DATE: Apr 19/17 SERVICE BULLETIN No.: A330-34-3342 REVISION No.: 01 - Nov 13/17 Page: 9 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 16 @A330 SERVICE BULLETIN M. SPARES TCAS Computer 940-0351-001 DATE: Apr 19/17 SERVICE BULLETIN No.: A330-34-3342 REVISION No.: 01 - Nov 13/17 Page: 10 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 17 @A330 SERVICE BULLETIN 2. MATERIAL INFORMATION **CONF ALL A. MATERIAL - PRICE AND AVAILABILITY (1) Procurement Addresses Vendor parts are to be procured from Equipment BFEA01 Honeywell International Inc. 15001 N.E. 36 Street Redmond, Washington 98052-5317 U.S.A. Telephone: 800-601-3099 (Toll Free U.S.A./Canada) Telephone: 602-365-3099 (International Direct) Website: www.myaerospace.com (2) Price and Availability Equipment BFEA01 Procurement terms for the equipment must be negotiated with the equipment supplier. Refer to the Honeywell Service Bulletin No. 940-0351-34-0005 for the equipment modification sales terms. B. INDUSTRY SUPPORT INFORMATION AIRBUS will not provide industry support for accomplishment of this Service Bulletin. Industry support terms for the equipment must be negotiated with the equipment supplier. Modification of removed equipment should be negotiated directly with Honeywell as per instructions given in Honeywell Service Bulletin No. 940-0351-34-0005. Refer to the Honeywell Service Bulletin No. 940-0351-34-0005 for the industry support terms of the Vendor Service Bulletin parts and labor. This Service Bulletin is the subject of an AIRBUS monitored retrofit campaign. For the organisation of this retrofit, you are kindly requested to contact AIRBUS retrofit management department. AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX France E-mail: monitored.retrofit@airbus.com DATE: Apr 19/17 SERVICE BULLETIN No.: A330-34-3342 REVISION No.: 01 - Nov 13/17 Page: 11 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 18 @A330 SERVICE BULLETIN C. LIST OF COMPONENTS No Kit D. LIST OF MATERIALS - OPERATOR SUPPLIED (1) Consumable Materials None (2) Components None (3) Equipment Equipment BFEA01 ITEM NEW PART N˚ QTY (UM) KEYWORD ITEM OLD PART N˚ INT SEE NOTES 940-0351-005 1 TCAS 940-0351-001 01 (1) NOTE : For definitions of interchangeability codes in column INT., refer to ATA Common Support Data Dictionary (CSDD), Chapter 2. NOTE : The above list of components is not an AIRBUS Kit, the required parts shall be ordered as necessary through the given channel. NOTE (1) : Modification of the TCAS computer must be done in accordance with Honeywell Service Bulletin No. 940-0351-34-0005. E. PARTS TO BE RE-IDENTIFIED BY OPERATOR Reidentified part set REIDA01 ITEM NEW PART N˚ KEYWORD ITEM OLD PART N˚ SEE NOTES 940-0351-005 TCAS 940-0351-001 (1) NOTE : Parts are re-identified in accordance with the Honeywell Service Bulletin No. 940-0351-34-0005. NOTE (1) : Modification of the TCAS computer must be done in accordance with Honeywell Service Bulletin No. 940-0351-34-0005. F. TOOLING (1) Tooling - Price and Availability None DATE: Apr 19/17 SERVICE BULLETIN No.: A330-34-3342 REVISION No.: 01 - Nov 13/17 Page: 12 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 19 @A330 SERVICE BULLETIN (2) Tools To accomplish this Service Bulletin it is necessary to use the tools listed in the subsequent referenced tasks: - AMM Task 52-41-00-010-801 - AMM Task 34-43-34-000-801 - Honeywell Service Bulletin No. 940-0351-34-0005. NOTE : For TASK 343342-831-801 001 Option 1 - Modify the TCAS Computer , refer to AMM Task 52-41-00-010-801 and for TASK 343342-831-802 001 Option 2 - Replace the TCAS Computer , refer to AMM Task 34-43-34-000-801. (3) Special Tools None DATE: Apr 19/17 SERVICE BULLETIN No.: A330-34-3342 REVISION No.: 01 - Nov 13/17 Page: 13 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 20 @A330 SERVICE BULLETIN This Page Intentionally Left Blank DATE: Apr 19/17 SERVICE BULLETIN No.: A330-34-3342 REVISION No.: 01 - Nov 13/17 Page: 14 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 21 @A330 SERVICE BULLETIN 3. ACCOMPLISHMENT INSTRUCTIONS Task 343342-831-801-001 - Option 1 - Modify the TCAS Computer WARNING : MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONS INCLUDED IN THE REFERENCED PROCEDURES. CAUTION : ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY AND MECHANICALLY SERVICEABLE) . WHEN YOU DO MAINTENANCE WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING, COMPONENTS AND THE WORK AREA AS CLEAN AS POSSIBLE. TO DO THIS: - PUT PROTECTION, SUCH AS PLASTIC SHEETING, CLOTHS, ETC., AS NECESSARY ON WIRING AND COMPONENTS. - REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND OTHER CONTAMINATION. THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION. IF THERE IS CONTAMINATION, REFER TO ESPM 20-55-00. NOTE : The accomplishment instructions of this Service Bulletin include procedures given in other documents or in other sections of the Service Bulletin. When the words ’refer to’ are used and the operator has a procedure accepted by the local authority he belongs to, the accepted alternative procedure can be used. When the words ’in accordance with’ are used then the given procedure must be followed. NOTE : The access and close-up instructions, not comprising return to service tests, in this Service Bulletin do not constitute or affect the technical intent of the Service Bulletin. Operators can therefore, as deemed necessary, omit or add access and/or close-up steps to add flexibility to their maintenance operations as long as the technical intent of the Service Bulletin is met within the set parameters. NOTE : Manual titles given in the accomplishment instructions are referred to by acronyms. Refer to paragraph 1.J., References, for the definition of acronyms. NOTE : This Service Bulletin contains the instructions for the on-aircraft maintenance necessary to ensure the continued airworthiness of the aircraft. For any deviations to the instructions contained herein, contact AIRBUS for further instructions and approval. NOTE : This Service Bulletin is classified mandatory or expected to be classified mandatory by an Airworthiness Directive (AD). The paragraphs 3.C. and 3.D. in these accomplishment instructions are Required for Compliance (RC) and must be done to comply with the AD. To allow more flexibility, the rule "refer to" and "in accordance with" will apply to these paragraphs 3.C. and 3.D. Other paragraphs are recommended and may be deviated from, done as part of other actions or done with accepted methods different from those given in the Service Bulletin, as DATE: Apr 19/17 SERVICE BULLETIN No.: A330-34-3342 REVISION No.: 01 - Nov 13/17 Page: 15 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 22 @A330 SERVICE BULLETIN long as the RC paragraphs can be done and the aircraft can be put back into a serviceable condition. Task Associated Data Zone 120 Modified FIN 1SG Access Door 811 Manpower TOTAL MANHOURS 1.50 ELAPSED TIME (HOURS) 1.50 Additional manhours related to Vendor SB; refer to: Honeywell Service Bulletin No. 940-0351-34-0005 A. GENERAL (1) Subtask 343342-910-001-001 - Standard Practices Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-20-00, Page Block 001 06-31-53, Page Block 001 06-41-53, Page Block 001 Task 20-16-00-912-801 (a) For the identification of zones, refer to AMM 06-20-00, Page Block 001. (b) For the Frame (FR) identification, refer to AMM 06-31-53, Page Block 001. (c) For the identification of access panels, refer to AMM 06-41-53, Page Block 001. (d) For circuit breaker safety practices, refer to AMM Task 20-16-00-912-801. (2) Subtask 343342-839-001-001 - Administrative Manpower Resources Skills NON SPECIFIC Write in the applicable aircraft records that you have done all the work given in this Service Bulletin. DATE: Apr 19/17 SERVICE BULLETIN No.: A330-34-3342 REVISION No.: 01 - Nov 13/17 Page: 16 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 23 @A330 SERVICE BULLETIN B. PREPARATION (1) Subtask 343342-941-001-001 - Job Set-up Work Zones and Access Panels Zone Access/Work location 120 Access Door 811 Work location from Frame 18 to Frame 20 Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802 Task 24-42-00-861-801 Task 52-41-00-010-801 NOTE : For the basic Aircraft configuration, refer to AMM Chapter "Introduction - Aircraft status for maintenance" in Manual Front Matter section. (a) Make sure that the aircraft is electrically grounded, refer to AMM Task 12-34-24-860-802. (b) Put the access platform(s) in position. (c) Open the access door 811, refer to AMM Task 52-41-00-010-801. (d) Energize the Ground Service Network, refer to AMM Task 24-42-00-861-801. C. PROCEDURE (1) Subtask 343342-470-001-001 - Modify the Traffic Collision Avoidance System (TCAS) Computer by Vendor HONEYWEL L Service Bulletin No. 940-0351-34-0005 Work Zones and Access Panels Zone Access/Work location 120 Access Door 811 Work location from Frame 18 to Frame 20 Material necessary to do the job Reidentified part set REIDA01 ITEM NEW PART N˚ KEYWORD ITEM OLD PART N˚ SEE NOTES 940-0351-005 TCAS 940-0351-001 (1) NOTE : Parts are re-identified in accordance with the Honeywell Service Bulletin No. 940-0351-34-0005. NOTE (1) : Modification of the TCAS computer must be done in accordance with Honeywell Service Bulletin No. 940-0351-34-0005. DATE: Apr 19/17 SERVICE BULLETIN No.: A330-34-3342 REVISION No.: 01 - Nov 13/17 Page: 17 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 24 @A330 SERVICE BULLETIN References Aircraft Maintenance Manual (AMM) Task 34-43-00-740-801 Task 45-10-00-860-804 Vendor Service Bulletin (VSB) Honeywell 940-0351-34-0005 (a) Do the BITE test of the Traffic Collision Avoidance System (TCAS), refer to AMM Task 34-43-00-740-801. (b) Do the LRU identification test 1 Job Set-up a Do the Procedure to get acce ss to the SYSTEM REPORT/TEST NAV:RADIO NAV page, refer to AMM Task 45-10-00-860-804. - Push the NEXT PAGE function key (two times) until the TCAS menu page comes into view. b Make sure that these circuit breakers are closed: PANEL DESIGNATION FIN LOCATION SEE NOTES 721VU TCAS 4SG 05 B 721VU PRINTER 1TP 02 D 2 Procedure NOTE : The actions and the results of this procedure occur on the MCDU used. ACTION RESULT 1. On the MCDU: - Push the line key adjacent to the TCAS indication. - Push the line key adjacent to the LRU IDENT indication. On the MCDU: - The TCAS page comes into view. - The LRU IDENTIFICATION page comes into view. 2. On the TCAS LRU IDENTIFICATION page: - Make sure that the old PN of the TCAS is 940-0351-001 3. Print the TCAS LRU IDENTIFICATION page (if the printer is not available, a visual check is acceptable). 3 Close-up a Put the aircraft back to its initial configuration: <1> On the MCDU, push the line key adjacent to the RETURN indication until the CFDS menu page comes into view. DATE: Apr 19/17 SERVICE BULLETIN No.: A330-34-3342 REVISION No.: 01 - Nov 13/17 Page: 18 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 25 @A330 SERVICE BULLETIN (c) Make sure that the aircraft is in ground configuration (Landing Gear down and compressed). (d) Make sure that these circuit breakers are closed: PANEL DESIGNATION FIN LOCATION SEE NOTES 742VU LGCIU 1 1GA 63 L 722VU LGCIU 2 2GA 38 U (1) 721VU L/G SAFETY VLV 3GA 12 S NOTE (1) : The location depends on the aircraft configuration. (e) Do the uploading of the TCAS (1SG) and update TCAS part number label and software label in accordance with Honeywell Service Bulletin No. 940-0351-34-0005. During the accomplishment of the Honeywell Service Bulletin No. 940-0351-34-0005, it is necessary to remove or apply electrical power to the TCAS as described in the following notes: NOTE (1) : To remove the electrical power from the TCAS, open safety/lock and tag this circuit breaker: PANEL DESIGNATION FIN LOCATION SEE NOTES 721VU TCAS 4SG 05 B NOTE (2) : To apply the electrical power to the TCAS, remove the safety clip and tag and close this circuit breaker: PANEL DESIGNATION FIN LOCATION SEE NOTES 721VU TCAS 4SG 05 B FIN 1SG 1 TCAS Computer 940-0351-001 becomes: FIN 1SG 1 TCAS Computer 940-0351-005 D. TEST (1) Subtask 343342-740-001-001 - BITE Test Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 34-43-00-740-801 Task 45-10-00-860-804 DATE: Apr 19/17 SERVICE BULLETIN No.: A330-34-3342 REVISION No.: 01 - Nov 13/17 Page: 19 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 26 @A330 SERVICE BULLETIN (a) Do the BITE test of the Traffic Collision Avoidance System (TCAS), refer to AMM Task 34-43-00-740-801. (b) Do the LRU identification test 1 Job Set-up a Do the procedure to get access to the SYSTEM REPORT/TEST NAV: RADIO NAV page on the MCDU, refer to AMM Task 45-10-00-860-804: - Push the NEXT PAGE function key (two times) until the TCAS menu page comes into view. b Make sure that these circuit breakers are closed: PANEL DESIGNATION FIN LOCATION SEE NOTES 721VU TCAS 4SG 05 B 721VU PRINTER 1TP 02 D 2 Procedure NOTE : The actions and the results of this procedure occur on the MCDU used. ACTION RESULT 1. On the MCDU: - Push the line key adjacent to the TCAS indication. - Push the line key adjacent to the LRU IDENT indication. On the MCDU: - The TCAS page comes into view. - The LRU IDENTIFICATION page comes into view. 2. On the TCAS LRU IDENTIFICATION page: - Make sure that the new PN of the TCAS is 940-0351-005. 3. Print the TCAS LRU IDENTIFICATION page (if the printer is not available, a visual check is acceptable). 3 Close-up a On the MCDU, push the line key adjacent to the RETURN indication until the CFDS menu page comes into view. DATE: Apr 19/17 SERVICE BULLETIN No.: A330-34-3342 REVISION No.: 01 - Nov 13/17 Page: 20 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 27 @A330 SERVICE BULLETIN E. CLOSE-UP (1) Subtask 343342-942-001-001 - Close-up Work Zones and Access Panels Zone Access/Work location 120 Access Door 811 Work location from Frame 18 to Frame 20 Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 52-41-00-410-801 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Close access door 811, refer to AMM Task 52-41-00-410-801. (c) Remove the access platform. (d) Put the aircraft back to its initial configuration. DATE: Apr 19/17 SERVICE BULLETIN No.: A330-34-3342 REVISION No.: 01 - Nov 13/17 Page: 21 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 28 @A330 SERVICE BULLETIN This Page Intentionally Left Blank DATE: Apr 19/17 SERVICE BULLETIN No.: A330-34-3342 REVISION No.: 01 - Nov 13/17 Page: 22 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 29 @A330 SERVICE BULLETIN Task 343342-831-802-001 - Option 2 - Replace the TCAS Computer WARNING : MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONS INCLUDED IN THE REFERENCED PROCEDURES. CAUTION : ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY AND MECHANICALLY SERVICEABLE) . WHEN YOU DO MAINTENANCE WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING, COMPONENTS AND THE WORK AREA AS CLEAN AS POSSIBLE. TO DO THIS: - PUT PROTECTION, SUCH AS PLASTIC SHEETING, CLOTHS, ETC., AS NECESSARY ON WIRING AND COMPONENTS. - REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND OTHER CONTAMINATION. THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION. IF THERE IS CONTAMINATION, REFER TO ESPM 20-55-00. NOTE : The accomplishment instructions of this Service Bulletin include procedures given in other documents or in other sections of the Service Bulletin. When the words ’refer to’ are used and the operator has a procedure accepted by the local authority he belongs to, the accepted alternative procedure can be used. When the words ’in accordance with’ are used then the given procedure must be followed. NOTE : The access and close-up instructions, not comprising return to service tests, in this Service Bulletin do not constitute or affect the technical intent of the Service Bulletin. Operators can therefore, as deemed necessary, omit or add access and/or close-up steps to add flexibility to their maintenance operations as long as the technical intent of the Service Bulletin is met within the set parameters. NOTE : Manual titles given in the accomplishment instructions are referred to by acronyms. Refer to paragraph 1.J., References, for the definition of acronyms. NOTE : This Service Bulletin contains the instructions for the on-aircraft maintenance necessary to ensure the continued airworthiness of the aircraft. For any deviations to the instructions contained herein, contact Airbus for further instructions and approval. NOTE : This Service Bulletin is classified mandatory or expected to be classified mandatory by an Airworthiness Directive (AD). The paragraphs 3.C. and 3.D. in these accomplishment instructions are Required for Compliance (RC) and must be done to comply with the AD. To allow more flexibility, the rule "refer to" and "in accordance with" will apply to these paragraphs 3.C. and 3.D. Other paragraphs are recommended and may be deviated from, done as part of other actions or done with accepted methods different from those given in the Service Bulletin, as long as the RC paragraphs can be done and the aircraft can be put back into a serviceable condition. DATE: Apr 19/17 SERVICE BULLETIN No.: A330-34-3342 REVISION No.: 01 - Nov 13/17 Page: 23 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 30 @A330 SERVICE BULLETIN NOTE : Discarded parts must be managed at the operator’s discretion. Task Associated Data Zone 120 Modified FIN 1SG Access Door 811 Manpower TOTAL MANHOURS 2.00 ELAPSED TIME (HOURS) 2.00 A. GENERAL (1) Subtask 343342-910-002-001 - Standard Practices Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-20-00, Page Block 001 06-31-53, Page Block 001 06-41-53, Page Block 001 Task 20-16-00-912-801 (a) For the identification of zones, refer to AMM 06-20-00, Page Block 001. (b) For the Frame (FR) identification, refer toAMM 06-31-53, Page Block 001. (c) For the identification of access panels, refer toAMM 06-41-53, Page Block 001. (d) For circuit breaker safety practices, refer toAMM Task 20-16-00-912-801. (2) Subtask 343342-839-002-001 - Administrative Manpower Resources Skills NON SPECIFIC Write in the applicable aircraft records that you have done all the work given in this Service Bulletin. B. PREPARATION (1) Subtask 343342-941-002-001 - Job Set-up Work Zones and Access Panels Zone Access/Work location 120 Access Door 811 Work location from Frame 18 to Frame 20 DATE: Apr 19/17 SERVICE BULLETIN No.: A330-34-3342 REVISION No.: 01 - Nov 13/17 Page: 24 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 31 @A330 SERVICE BULLETIN Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802 Task 34-43-34-000-801 NOTE : For the basic Aircraft configuration, refer to AMM Chapter "Introduction - Aircraft status for maintenance" in Manual Front Matter section. (a) Make sure that the aircraft is electrically grounded, refer to AMM Task 12-34-24-860-802. (b) Do the Job Set-up procedure as specified in the Removal of the Traffic Collision Avoidance System (TCAS) Computer, refer to AMM Task 34-43-34-000-801. C. PROCEDURE (1) Subtask 343342-020-002-001 - Remove the Traffic Collision Avoidance System (TCAS) Computer Work Zones and Access Panels Zone Access/Work location 120 Access Door 811 Work location from Frame 18 to Frame 20 Manpower Resources Manhours 0.25 Minimum number of person 1 Subtask elapsed time 0.25 Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 34-43-34-000-801 (a) Do the Removal of the Traffic Collision Avoidance System (TCAS) Computer, refer to AMM Task 34-43-34-000-801. FIN 1SG 1 TCAS Computer 940-0351-001 Discard (2) Subtask 343342-420-001-001 - Install the Traffic Collision Avoidance System (TCAS) Computer Work Zones and Access Panels Zone Access/Work location 120 Access Door 811 Work location from Frame 18 to Frame 20 DATE: Apr 19/17 SERVICE BULLETIN No.: A330-34-3342 REVISION No.: 01 - Nov 13/17 Page: 25 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 32 @A330 SERVICE BULLETIN Manpower Resources Manhours 0.25 Minimum number of person 1 Subtask elapsed time 0.25 Skills NON SPECIFIC Material necessary to do the job Equipment BFEA01 ITEM NEW PART N˚ QTY (UM) KEYWORD SEE NOTES 940-0351-005 1 TCAS NOTE : The above list of components is not an AIRBUS Kit, the required parts shall be ordered as necessary through the given channel. References Aircraft Maintenance Manual (AMM) Task 34-43-34-400-801 (a) Do the Installation of the Traffic Collision Avoidance System (TCAS) Computer, refer to AMM Task 34-43-34-400-801. FIN 1SG 1 TCAS Computer 940-0351-005 D. TEST (1) Subtask 343342-740-002-001 - BITE Test Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 34-43-00-740-801 (a) Do the BITE test of the Traffic Collision Avoidance System (TCAS), refer to AMM Task 34-43-00-740-801. E. CLOSE-UP (1) Subtask 343342-942-002-001 - Close-up Work Zones and Access Panels Zone Access/Work location 120 Access Door 811 Work location from Frame 18 to Frame 20 Manpower Resources Skills NON SPECIFIC DATE: Apr 19/17 SERVICE BULLETIN No.: A330-34-3342 REVISION No.: 01 - Nov 13/17 Page: 26 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 33 @A330 SERVICE BULLETIN References Aircraft Maintenance Manual (AMM) Task 34-43-34-400-801 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Do the Close-up procedure as specified in the Installation of the Traffic Collision Avoidance System (TCAS) Computer, refer to AMM Task 34-43-34-400-801. (c) Put the aircraft back to its initial configuration. DATE: Apr 19/17 SERVICE BULLETIN No.: A330-34-3342 REVISION No.: 01 - Nov 13/17 Page: 27 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 34 @A330 SERVICE BULLETIN Service Bulletin REPORTING TITLE: NAVIGATION - TCAS - INSTA LL NEW TCAS SOFTWARE TO CORRECT UNJUSTIFIED RESOLUTION ADVISORY MODIFICATION No.: 206608S34248 SB Reporting status This Service Bulletin will only be incorporated into affected customized Maintenance and Flight Operations Products if it is duly reported to Airbus. General information The SB Reporting policy is published in ISI 00.00.00135. This document provides information regarding: the SB Reporting means and benefits, the update of customized Maintenance Products and customized Flight Operations Products. If this Service Bulletin has an operational impact, refer to paragraph "Flight Operations Products" for further information on the update of affected Flight Operations Products. SB Reporting procedure Standard practice to report SB is to use the online reporting application on AirbusWorld. Refer to ISI 00.00.00179: - For complete information on reporting means to Airbus. Question 2 "What are the standard practices for SB reporting?" - If this SB requires previous or simultaneous accomplishment of other SBs, Question 3 "What about the reporting of prerequisite Service Bulletin?" NOTE: ISI 00.00.00179 covers all the frequently asked questions about SB Reporting. It is revised on a regular basis. DATE: Apr 19/17 SERVICE BULLETIN No.: A330-34-3342 REVISION No.: 01 - Nov 13/17 Page: 1 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 35 @A330 SERVICE BULLETIN QUALITY PERCEPTION FORM Use this form to tell us what is your perception of the quality of this Service Bulletin. The reported data that you provide us will be used to analyse areas of difficulties and to take corrective action to further improve the quality of our Service Bulletins. We thank you for the time you have taken in completing this form. (Please rate on a scale of 1 to 4, with 4 being the highest score) - Quality rating of this SB 4321 - Quality rating of the Accomplishment Instructions 4321 - Quality rating of the Illustrations 4321 - Is this SB easy to understand ? Y/N If you have had difficulties in the accomplishment of this SB please quote below the area(s) and give a short description of the issue. Planning Material Instructions X Effectivity X Kit content X Preparation X Reason X List of Materials Operator Supplied X Mod/Inspection X Manpower X Industry support X Test X References X Re-identification X Close-Up X Publication X Tooling X Illustrations Comments: Operator: Date: Name/Title: Please return this form to: AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Attn : SEM4 Service Bulletins Management F A X:( 3 3 )56 19 34 25 1 Or via your Resident Customer Support Office. DATE: Apr 19/17 SERVICE BULLETIN No.: A330-34-3342 REVISION No.: 01 - Nov 13/17 Page: 1 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain, except the copies of manufacturers’ service documents, which belong to their rights holders.