# @A330 SERVICE BULLETIN REVISION TRANSMITTAL SHEET AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Tel : (33) 5 61 93 33 33 Telex : AIRBU 530526F Fax : (33) 5 61 93 42 51



# MANDATORYMANDATORYMANDATORY
ATA SYSTEM: 21 

### TITLE: AIR CONDITIONING - GENERAL - INSTALL NEW BONDING BRACKETS AFTER FRAME64 LH BETWEEN P33-P34 MODIFICATION No.: 201500D50418 This page transmits Revision No.03 of Service Bulletin No.A330-21-3165 ADDITIONAL WORK **CONF ALL Additional work is required for aircraft which have been modified by revision 00 or revision 01. Additional work is not required for aircraft which have been modified by revision 02. REASON Revision No. 03 issued to update the reason, accomplishment instruction and illustration. CHANGES SUMMARY REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES REASON UPDATED R EFFECTIVITY OPERATOR LIST UPDATED R Fig. A-GSAAA Fig. A-GSAAA Sheet 01 SHEET UPDATED R PLANNING INFORMATION EFFECTIVITY EFFECTIVITY RELATED INFORMATION UPDATED R REASON Objective/Action OBJECTIVE/ACTION UPDATED R ACCOMPLISHMENT INSTRUCTIONS TASK 213165- 831-848-001-Modification Subtask 213165-831-201-001 SUBTASK SOLUTION UPDATED R TASK 213165- 831-849-001-Modification - ADDITIONAL WORK Subtask 213165-831-202-001 SUBTASK SOLUTION UPDATED R
DATE: Sep 27/11 SERVICE BULLETIN No.: A330-21-3165 REVISION No.: 03 - Dec 07/12 Page: 1 6

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# @A330 SERVICE BULLETIN REVISION TRANSMITTAL SHEET Fig. A-GBAAA Fig. A-GBAAA Sheet 01 SHEET UPDATED R Fig. A-GBBAA Fig. A-GBBAA Sheet 01 SHEET UPDATED R Fig. A-GBCAA Fig. A-GBCAA Sheet 01 SHEET UPDATED R FILLING INSTRUCTIONS This Service Bulletin has been generated electronically and is reissued as a complete document. Replace the complete document. Put this Revision Transmittal Sheet in front of the Service Bulletin. HISTORY OF PREVIOUS REVISIONS Revision No. 01 issued to update the effectivity, the Industry support paragraph, amend an AMM reference and add that damaged insulations must be repaired and update the Kit revision indicator. Revision No. 02 issued to add the replacement of the bonding lead from waste water pipe to the new bonding bracket and to improve the position of the bonding clamp at waste water pipe. REVISION SEQUENCE ORIGINAL: Sep 27/11 REVISION No. : 01 - Nov 21/11 REVISION No. : 02 - Mar 29/12 REVISION No. : 03 - Dec 07/12

DATE: Sep 27/11 SERVICE BULLETIN No.: A330-21-3165 REVISION No.: 03 - Dec 07/12 Page: 2 6

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

# MANDATORYMANDATORYMANDATORY
ATA SYSTEM: 21 

### TITLE: AIR CONDITIONING - GENERAL - INSTALL NEW BONDING BRACKETS AFTER FRAME64 LH BETWEEN P33-P34 **CONF ALL MODIFICATIONS MODIFICATION CLASSIFICATION MAJOR None MINOR 201500D50418 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 Maintenance experience has shown that the bonding lead from the isolation valve 283HN to Frame (FR)64, between Stringer (STGR)33 and STGR34, is too close to the electrical harness 5871VB and chafing might be possible. The chafing might lead to a non-closure of the isolation valve 283HN through a short circuit of the isolation valve by contact of the chafed bonding lead and wire harness 5871VB. This Service Bulletin details the installation of a new bonding bracket and new bonding lead at STGR34, between FR64 and FR65. The accomplishment of this Service Bulletin will avoid possible chafing between the bonding lead and the electrical harness 5871VB and ensure the correct control of the isolation valve 283HN. GENERAL EVALUATION EVALUATION TABLE COMPLIANCE MANDATORY (1) CANCELS INSPECTION SB NO POTENTIAL AD YES A/C OPERATION AFFECTED NO RELIABILITY AFFECTED YES PAX COMFORT AFFECTED NO COST SAVING NO ETOPS AFFECTED NO DATE: Sep 27/11 SERVICE BULLETIN No.: A330-21-3165 REVISION No.: 03 - Dec 07/12 Page: 1 6

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# @A330 SERVICE BULLETIN SUMMARY EVALUATION TABLE STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED NO 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 Kit 213165D01R03 1 33.00 Bracket, Rivet, Screw, Washer Kit 213165D02R01 1 33.00 TOTAL 66.00 EFFECTIVITY This Service Bulletin is applicable to this (these) operator(s) :

11S 46W AAR AAW ACA ACI AEA AFL AFR ALK ASY AVA AZA BEC BEL BER BMA BTV CAL CCA CES CHH CPA CRK CRL CSC CSN DAH DAL DGA DLH EDW EIN ETD EVA FIN FST FWI GFA GIA GRL HAL HDA HFY HVN I2L IAC ISS IWD IYE JAI JAV JST KAL KFR KLM MAS MAU MEA MON MSR OBS OHY OMA P2C PAL QAF QFA QTR RJA RSF RSY RYN SAA SAI SAS SIA SVA SWR TAM TAP TCX THA THY TSC UAE UAF USA VIR VKG VLK VOZ XAX XLF CONCURRENT REQUIREMENTS None REFERENCES / REPERCUSSIONS TFU None OEB None AOT None SIL None LINE MAINTENANCE AFFECTED No LIFE LIMIT None OTHER None NATURE OF THE WORK AIRCRAFT YES EQUIPMENT NO HARD NO SOFT NO OBRM NO

DATE: Sep 27/11 SERVICE BULLETIN No.: A330-21-3165 REVISION No.: 03 - Dec 07/12 Page: 2 6

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# @A330 SERVICE BULLETIN SUMMARY MANPOWER Task 213165-831-848-001: Modification TOTAL MANHOURS 3.25 ELAPSED TIME (HOURS) 3.25 Task 213165-831-849-001: Modification - ADDITIONAL WORK TOTAL MANHOURS 2.50 ELAPSED TIME (HOURS) 2.50 APPENDICES None

DATE: Sep 27/11 SERVICE BULLETIN No.: A330-21-3165 REVISION No.: 03 - Dec 07/12 Page: 3 6

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# @A330 SERVICE BULLETIN SUMMARY

**CONF ALL



### B



## A 283HN

FR73 FR62

STGR34 FR64 FR63

FR62

STGR33 STGR32



## B 283HN

NEW BONDING BRACKET Z160 

### A

G_SB_213165_6_SAAA_01_03 Figure A-GSAAA - Sheet 01
DATE: Sep 27/11 SERVICE BULLETIN No.: A330-21-3165 REVISION No.: 03 - Dec 07/12 Page: 4 6

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# @A330 SERVICE BULLETIN
AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Tel : (33) 5 61 93 33 33 Telex : AIRBU 530526F Fax : (33) 5 61 93 42 51



# MANDATORYMANDATORYMANDATORY
ATA SYSTEM: 21 

### TITLE: AIR CONDITIONING - GENERAL - INSTALL NEW BONDING BRACKETS AFTER FRAME64 LH BETWEEN P33-P34 MODIFICATION No.: 201500D50418 This document contains AIRBUS PROPRIETARY INFORMATION and shall at all times remain the property of AIRBUS; no intellectual property right or licence is granted by AIRBUS in connection with any information contained in it. It is delivered on the express condition that said document and the information contained in it shall be treated as confidential, shall not be used for any purpose other than that for which it is hereby delivered. It shall not be disclosed in whole or in part to third parties and shall not be duplicated in any manner (except for the purposes of performing the tasks described hereunder and provided that any recipient of such document shall comply with the conditions herein), without AIRBUS prior written consent. 1. PLANNING INFORMATION **CONF ALL A. EFFECTIVITY (1) Models 330-202 330-203 330-223 330-243 330-301 330-302 330-303 330-321 330-322 330-323 330-341 330-342 330-343 (2) Effectivity by MSN 0012 0017 0030 0037 0045 0050 0054-0055 0060 0062 0064-0067 0069-0073 0077 0082-0083 0086-0087 0095-0096 0098-0100 0102 0106-0107 0109-0113 0116 0118-0122 0127 0132 0138 0140 0143-0144 0148 0153 0155 0162 0165 0171-0172 0177 0181 0183-0184 0188-0189 0191 0195 0198 0200 0203 0205-0206 0209 0211 0219 0222-0224 0226 0229-0232 0234 0238 0240-0241 0244 0247-0251 0253-0256 0258-0259 0261-0262 0265-0267 0269 0271-0272 0275-0277 0279 0281 0283-0288 0290-0291 0293-0296 0299-0301 0303 0305-0306 0308-0309 0311-0317 0320 0322-0324 0326 0328 0330 0333-0334 0337-0340 0342-0346 0348-0351 0353 0356-0358 0361-0362 0364-0366 0368-0370 0372 0375 0380 0382 0384 0386 0388-0389 0392-0393 0396-0398 0400-0401 0403-0405 0407-0409 0412 0418-0423 0425 0427-0428 0432 0437 0439 0441 0443-0444 0448 0451-0452 0454-0456 0458 0461-0463 0465-0466 0469 0472-0473 0476-0477 0479-0481 0484 0486-0487 0489-0491 0493-0494 0496-0498 0500-0513 0515-0516 0518-0519 0521-0522 DATE: Sep 27/11 SERVICE BULLETIN No.: A330-21-3165 REVISION No.: 03 - Dec 07/12 Page: 1 6

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# @A330 SERVICE BULLETIN

0524-0527 0529-0530 0532-0533 0535-0536 0539 0542 0548-0553 0555 0558 0564-0565 0567-0568 0570-0571 0573-0574 0576 0578-0579 0581 0584 0587-0588 0591 0593 0595 0597 0600 0602-0603 0605 0607 0609-0610 0612 0614 0616 0618 0620-0621 0623 0625 0627 0629 0631-0638 0640-0642 0644-0645 0647-0650 0652-0659 0661-0667 0669-0671 0673-0676 0678-0680 0682-0684 0686-0688 0690-0693 0695-0697 0699-0701 0703-0705 0707-0709 0711-0714 0716-0718 0720-0722 0724-0726 0728-0730 0732-0735 0737-0739 0741-0743 0745-0747 0749-0752 0754-0756 0758-0760 0769-0770 0772-0774 0776-0778 0780-0782 0784-0786 0788-0789 0791-0792 0795-0797 0799 0801-0803 0805-0807 0809-0811 0813-0815 0817-0828 0830-0834 0836 0838-0843 0845 0847 0849-0855 0857-0863 0865-0869 0871 0873-0877 0879 0881-0885 0887-0893 0895-0896 0898-0901 0903-0909 0911 0913-0916 0918-0920 0922-0923 0925-0928 0930-0932 0934-0937 0939-0952 0954 0956-0959 0961-0971 0973-0980 0982-0986 0988-0992 0994-1003 1006-1016 1018-1023 1025-1026 1028-1029 1031 1033-1039 1041-1049 1052-1055 1057-1061 1063 1065-1067 1069 1071-1078 1080-1082 1084-1090 1093-1101 1103-1108 1110 1112 1114 1116 1118 1120 1123-1124 1126-1127 1129-1133 1135 1137-1138 1141 1143 1145-1147 1149-1151 1153 1155-1157 1159-1161 1163 1165 1167-1174 1177-1178 1181 1183-1184 1186-1193 1195-1196 1198-1206 1208-1219 (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 11S 1053 46W 0871 AAR 0640 0676 0708 0772 0803 0845 1001 1055 1151 1211 AAW 0999 1043 ACA 0277 0279 0284 0344 0400 0408 0412 0419 ACI 0507 0510 AEA 0505 0526 0551 0597 0733 0745 0749 0814 0931 0950 AFL 0963 0973 1014 1045 1047 1058 1065 1072 1077 1103 AFR 0422 0443 0448 0458 0465 0481 0498 0500 0502 0503 0516 0519 0567 0584 0657 ALK 0303 0306 0311 0313 0404 0456 0627 ASY 0747 0951 0969 1036 1183 AVA 0948 0967 1009 1016 1073 1208 AZA 0272 0339 1123 1135 1218 BEC 0863 BEL 0030 0037 0045 0082 0095 0229 0249 BER 0120 0127 0288 0322 0403 0432 0444 0454 0469 0476 0493 0665 0739 0828 0911 BMA 0398 0401 BTV 0205 0330 CAL 0602 0607 0641 0671 0675 0691 0699 0707 0714 0725 0752 0769 0805 0823 0838 0861 0920 1177 1206 1215

DATE: Sep 27/11 SERVICE BULLETIN No.: A330-21-3165 REVISION No.: 03 - Dec 07/12 Page: 2 6

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# @A330 SERVICE BULLETIN

OPERATOR MSN 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 CES 0713 0720 0728 0732 0735 0773 0777 0781 0782 0791 0821 0830 0836 0851 0862 0866 0916 0928 0936 0942 CHH 0875 0881 0906 0919 0982 1159 1168 1178 1190 CPA 0012 0017 0071 0102 0113 0118 0121 0155 0386 0389 0393 0418 0420 0421 0423 0439 0539 0548 0565 0669 0673 0679 0776 0850 0855 0895 0915 0959 1163 1196 CRK 1031 1034 1039 1042 1054 1059 CRL 0285 0320 1008 CSC 0462 1082 1138 CSN 0649 0652 0656 0664 0818 0840 0879 0889 0908 0935 0937 0954 0958 0964 1096 1116 1129 1202 DAH 0644 0647 0650 0653 0667 DAL 0524 0533 0542 0549 0552 0578 0588 0591 0609 0614 0618 0620 0621 0631 0633 0663 0674 0690 0718 0722 0778 0784 0796 0799 0806 0817 0827 0843 0857 0858 0859 0865 DGA 0240 DLH 0570 0576 0579 0629 0636 0642 0645 0648 0687 0701 0896 0905 0913 0922 0989 EDW 0291 1193 EIN 0269 0397 0841 0847 0985 1025 1106 ETD 0658 0688 0717 0724 0729 0730 0737 0751 0788 0809 0824 0832 0852 0854 0868 0975 0991 1071 1081 1167 1205 EVA 0530 0535 0555 0573 0587 0634 0655 0661 0678 0693 0755 FIN 0994 1007 1013 1023 1067 1078 1088 1173 FST 1033 1046 FWI 0253 0758 0965 1021 GFA 0276 0281 0286 0287 0334 0340 0527 0529 0532 0992 GIA 0138 0140 0144 0148 0153 0165 0988 1020 1028 1052 1184 1214 GRL 0230 HAL 1104 1114 1171 1217 HDA 0083 0099 0106 0109 0234 0244 0405 0479 0512 0581 0654 0662 0692 0716 0741 0786 HFY 0096 0211 0262 HVN 0275 0294 0299 0366 0943 0962 1019 I2L 0358 0364 IAC 0353 0362 ISS 0802 0822 IWD 0461 0670 1097 IYE 0625 0632 JAI 0807 0825 0831 0882 0885 0888 0901 0923 0932 0947 0956 JAV 0255 JST 0506 0508 0513 0522 0842 0853 0940 0945 1198 KAL 0162 0172 0206 0219 0222 0226 0241 0256 0258 0267 0338 0350 0351 0368 0425 0428 0484 0490 0550 1133 1155 1200 1203 DATE: Sep 27/11 SERVICE BULLETIN No.: A330-21-3165 REVISION No.: 03 - Dec 07/12 Page: 3 6

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# @A330 SERVICE BULLETIN

OPERATOR MSN KFR 0874 0939 0946 KLM 0682 0686 0703 0738 0770 0801 0811 0819 0834 0900 0925 1161 MAS 0067 0069 0073 0077 0100 0107 0110 0116 0119 0290 0296 0300 1209 1219 MAU 0883 1057 MEA 0926 0984 0995 0998 MON 0261 0265 MSR 0600 0610 0666 0683 0696 0709 0726 1143 OBS 0833 OHY 0072 0087 0098 0143 OMA 1038 1044 1049 1063 1093 1120 P2C 0891 0927 PAL 0183 0184 0188 0189 0191 0198 0200 0203 QAF 0487 0605 QFA 0553 0558 0564 0574 0593 0595 0603 0695 0705 0712 0887 0892 0898 0976 1061 1094 1169 1174 QTR 0441 0473 0489 0511 0521 0571 0612 0616 0623 0637 0638 0659 0680 0684 0711 0721 0734 0743 0746 0760 0789 0792 0813 0820 0826 0849 0893 0907 0918 RJA 0970 0979 1002 RSF 0980 0996 RSY 0171 RYN 0343 SAA 1191 1210 SAI 0055 0070 SAS 0496 0497 0515 0568 SIA 0978 0983 0986 0997 1006 1010 1012 1015 1085 1098 1099 1105 1107 1124 1132 1146 1149 1156 1157 SVA 1108 1127 1137 1141 1147 1153 1189 1192 SWR 0324 1000 1018 1026 1029 1084 1089 1101 1145 1181 1188 TAM 0232 0238 0247 0259 0361 0466 0472 0477 0486 0700 0869 0876 0949 0961 0968 0977 1112 1118 1213 TAP 0181 0195 0223 0305 0308 0312 0317 0877 0899 0904 0914 0934 TCX 0254 0266 0301 THA 0050 0060 0062 0064 0065 0066 0112 0122 0209 0224 0231 0346 0990 1003 1035 1037 1060 1074 1086 1090 THY 0463 0504 0697 0704 0742 0754 0774 1150 1160 1170 1172 1204 1212 TSC 0111 0132 0177 0250 0271 0369 0407 0427 0480 0795 0966 0971 UAE 0248 0251 0283 0293 0295 0314 0316 0326 0328 0345 0348 0382 0384 0392 0396 0409 0437 0451 0452 0455 0491 0494 0509 0518 0525 0536 UAF 1080 1186 USA 0315 0323 0333 0337 0342 0370 0375 0380 0388 1011 1022 1041 1069 1076 1095 1100 VIR 1195 1201 VKG 0309 0349 0356 0357 DATE: Sep 27/11 SERVICE BULLETIN No.: A330-21-3165 REVISION No.: 03 - Dec 07/12 Page: 4 6

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# @A330 SERVICE BULLETIN

OPERATOR MSN VLK 0086 VOZ 0365 0372 XAX 0054 0952 0974 1048 1066 1075 1126 1131 1165 XLF 0501 0635

DATE: Sep 27/11 SERVICE BULLETIN No.: A330-21-3165 REVISION No.: 03 - Dec 07/12 Page: 5 6

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# @A330 SERVICE BULLETIN (4) Configuration by MSN MSN CONFIGURATION 0012 0017 0030 0037 0045 0050 0054 0055 0060 0062 0064 0065 0066 0067 0069 0070 0071 0072 0073 0077 0082 0083 0086 0087 0095 0096 0098 0099 0100 0102 0106 0107 0109 0110 0111 0112 0113 0116 0118 0119 0120 0121 0122 0127 0132 0138 0140 0143 0144 0148 0153 0155 0162 0165 0171 0172 0177 0181 0183 0184 0188 0189 0191 0195 0198 0200 0203 0205 0206 0209 0211 0219 0222 0223 0224 0226 0229 0230 0231 0232 0234 0238 0240 0241 0244 0247 0248 0249 0250 0251 0253 0254 0255 0256 0258 0259 0261 0262 0265 0266 0267 0269 0271 0272 0275 0276 0277 0279 0281 0283 0284 0285 0286 0287 0288 0290 0291 0293 0294 0295 0296 0299 0300 0301 0303 0305 0306 0308 0309 0311 0312 0313 0314 0315 0316 0317 0320 0322 0323 0324 0326 0328 0330 0333 0334 0337 0338 0339 0340 0342 0343 0344 0345 0346 0348 0349 0350 0351 0353 0356 0357 0358 0361 0362 0364 0365 0366 0368 0369 0370 0372 0375 0380 0382 0384 0386 0388 0389 0392 0393 0396 0397 0398 0400 0401 0403 0404 0405 0407 0408 0409 0412 0418 0419 0420 0421 0422 0423 0425 0427 0428 0432 0437 0439 0441 0443 0444 0448 0451 0452 0454 0455 0456 0458 0461 0462 0463 0465 0466 0469 0472 0473 0476 0477 0479 0480 0481 0484 0486 0487 0489 0490 0491 0493 0494 0496 0497 0498 0500 0501 0502 0503 0504 0505 0506 0507 0508 0509 0510 0511 0512 0513 0515 0516 0518 0519 0521 0522 0524 0525 0526 0527 0529 0530 0532 0533 0535 0536 0539 0542 0548 0549 0550 0551 0552 0553 0555 0558 0564 0565 0567 0568 0570 0571 0573 0574 0576 0578 0579 0581 0584 0587 0588 0591 0593 0595 0597 0600 0602 0603 0605 0607 0609 0610 0612 0614 0616 0618 0620 0621 0623 0625 0627 0629 0631 0632 0633 0634 0635 0636 0637 0638 0640 0641 0642 0644 0645 0647 0648 0649 0650 0652 0653 0654 0655 0656 0657 0658 0659 0661 0662 0663 0664 0665 0666 0667 0669 0670 0671 0673 0674 0675 0676 0678 0679 0680 0682 0683 0684 0686 0687 0688 0690 0691 0692 0693 0695 0696 0697 0699 0700 0701 0703 0704 0705 0707 0708 0709 0711 0712 0713 0714 0716 0717 0718 0720 0721 0722 0724 0725 0726 0728 0729 0730 0732 0733 0734 0735 0737 0738 0739 0741 0742 0743 0745 0746 0747 0749 0750 0751 0752 0754 0755 0756 0758 0759 0760 0769 0770 0772 0773 0774 0776 0777 0778 0780 0781 0782 0784 0785 0786 0788 0789 0791 0792 0795 0796 0797 0799 0801 0802 0803 0805 0806 0807 0809 0810 0811 0813 0814 0815 0817 0818 0819 0820 0821 0822 0823 0824 0825 0826 0827 0828 0830 0831 0832 0833 0834 0836 0838 0839 0840 0841 0842 0843 0845 0847 0849 0850 0851 0852 0853 0854 0855 0857 0858 0859 0860 0861 0862 0863 0865 0866 0867 0868 0869 0871 0873 0874 0875 0876 0877 0879 0881 0882 0883 0884 0885 0887 0888 0889 0890 0891 0892 0893 0895 0896 0898 0899 0900 0901 0903 0904 0905 0906 0907 0908 0909 0911 0913 0914 0915 0916 0918 0919 0920 0922 0923 0925 001

DATE: Sep 27/11 SERVICE BULLETIN No.: A330-21-3165 REVISION No.: 03 - Dec 07/12 Page: 6 6

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# @A330 SERVICE BULLETIN

MSN CONFIGURATION 0926 0927 0928 0930 0931 0932 0934 0935 0936 0937 0939 0940 0941 0942 0943 0944 0945 0946 0947 0948 0949 0950 0951 0952 0954 0956 0957 0958 0959 0961 0962 0963 0964 0965 0966 0967 0968 0969 0970 0971 0973 0974 0975 0976 0977 0978 0979 0980 0982 0983 0984 0985 0986 0988 0989 0990 0991 0992 0994 0995 0996 0997 0998 0999 1000 1001 1002 1003 1006 1007 1008 1009 1010 1011 1012 1013 1014 1015 1016 1018 1019 1020 1021 1022 1023 1025 1026 1028 1029 1031 1033 1034 1035 1036 1037 1038 1039 1041 1042 1043 1044 1045 1046 1047 1048 1049 1052 1053 1054 1055 1057 1058 1059 1060 1061 1063 1065 1066 1067 1069 1071 1072 1073 1074 1075 1076 1077 1078 1080 1081 1082 1084 1085 1086 1087 1088 1089 1090 1093 1094 1095 1096 1097 1098 1099 1100 1101 1103 1104 1105 1106 1107 1108 1110 1112 1114 1116 1118 1120 1123 1124 1126 1127 1129 1130 1131 1132 1133 1135 1137 1138 1141 1143 1145 1146 1147 1149 1150 1151 1153 1155 1156 1157 1159 1160 1161 1163 1165 1167 1168 1169 1170 1171 1172 1173 1174 1177 1178 1181 1183 1184 1186 1187 1188 1189 1190 1191 1192 1193 1195 1196 1198 1199 1200 1201 1202 1203 1204 1205 1206 1208 1209 1210 1211 1212 1213 1214 1215 1216 1217 1218 1219 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 Consumable CMLD01 1 Kit 213165D01R03 1 Kit 213165D02R01 1 B. CONCURRENT REQUIREMENTS None C. REASON (1) History Maintenance experience has shown that the bonding lead from the isolation valve 283HN to Frame (FR)64, between Stringer (STGR)33 and STGR34, is too close to the electrical harness 5871VB and chafing might be possible. The chafing might lead to a non-closure of the isolation valve 283HN through a short circuit of the isolation valve by contact of the chafed bonding lead and wire harness 5871VB. DATE: Sep 27/11 SERVICE BULLETIN No.: A330-21-3165 REVISION No.: 03 - Dec 07/12 Page: 7 6

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# @A330 SERVICE BULLETIN (2) Objective/Action This Service Bulletin details the installation of a new bonding bracket and new bonding lead at STGR34, between FR64 and FR65. (3) Advantages The accomplishment of this Service Bulletin will avoid possible chafing between the bonding lead and the electrical harness 5871VB and ensure the correct control of the isolation valve 283HN. (4) Operational/Maintenance Consequences None D. DESCRIPTION To accomplish this Service Bulletin it is necessary to : Task 213165-831-848-001: Modification (1) Modify the bonding lead installation Task 213165-831-849-001: Modification - ADDITIONAL WORK (1) Modify the bonding lead installation 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 Aviation Safety Agency (EASA) will be issued to confirm this classification. The accomplishment timescale, which has not yet been defined, will be given in the AD. F. APPROVAL The technical content of this document is approved under the authority of Design Organisation Approval No. EASA.21J.031. If an aircraft listed in the effectivity has a modification or repair embodied that is not of AIRBUS origin, and which affects the content of this Service Bulletin, the operator is responsible for obtaining approval by its airworthiness authority for any adaptation necessary before incorporation of the Service Bulletin.

DATE: Sep 27/11 SERVICE BULLETIN No.: A330-21-3165 REVISION No.: 03 - Dec 07/12 Page: 8 6

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# @A330 SERVICE BULLETIN
G. MANPOWER The manpower estimates given in this Service Bulletin are based on the direct labor cost to do the work. These estimates assume that the work will be done by experienced personnel, and may need to be revised upwards to suit operator’s circumstances. The estimates do not include the time to prepare, plan or inspect the work. Manufacture and procurement of parts and tools, drying times for paints, sealants, etc., and general administration work are also not included. Task 213165-831-848-001: Modification Get Access 1.00 On Aircraft Modify the bonding lead installation 1.00 Tests 0.25 Close-Up 1.00 TOTAL MANHOURS 3.25 ELAPSED TIME (HOURS) 3.25 Task 213165-831-849-001: Modification - ADDITIONAL WORK Get Access 1.00 On Aircraft Modify the bonding lead installation 0.25 Tests 0.25 Close-Up 1.00 TOTAL MANHOURS 2.50 ELAPSED TIME (HOURS) 2.50 H. WEIGHT AND BALANCE Not Changed I. ELECTRICAL LOAD DATA Not Changed J. REFERENCES

Aircraft Maintenance Manual (AMM) 06-20-00 06-30-00 06-31-53 06-41-53 12-34-24 20-28-00 25-53-00 25-80-00 52-30-00 Elec. Std. Practices Manual (ESPM) 20-51-20 20-51-21 20-55-00 Standards Manual (SM) Structural Repair Manual (SRM) 51-42-11 51-44-00 51-44-11 K. PUBLICATION AFFECTED

Illustrated Parts Catalog (IPC) 21-28-04 L. INTERCHANGEABILITY/MIXABILITY Not Applicable DATE: Sep 27/11 SERVICE BULLETIN No.: A330-21-3165 REVISION No.: 03 - Dec 07/12 Page: 9 6

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# @A330 SERVICE BULLETIN
M. SPARES None

DATE: Sep 27/11 SERVICE BULLETIN No.: A330-21-3165 REVISION No.: 03 - Dec 07/12 Page: 10 6

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# @A330 SERVICE BULLETIN
2. MATERIAL INFORMATION **CONF ALL A. MATERIAL - PRICE AND AVAILABILITY (1) Procurement Addresses Kit 213165D01R03 Kit 213165D02R01 Customers with aircraft shown in the effectivity of this Service Bulletin should send a purchase order to AIRBUS. Quote the number of this Service Bulletin. The address is: Airbus Material, Logistic and Suppliers Weg beim Jaeger 150 D-22335 Hamburg Germany For ordering by internet: http//spares.airbus.com For ordering modification kits by fax: +49 40 50 76 25 90 For ordering by E-mail: airbus.kit@airbus.com (2) Price and Availability

Kit 213165D01R03 Cost 33.00 USD Availability 90 calendar days from receipt of order The Kit availability given above is the standard lead time from the date of your purchase order. If you require Kits before this time, please include a retrofit planning schedule with your order so that we can try to comply with your requirements. The sales terms (costs and availability) are estimated in relation to economic conditions at the issue date of the Service Bulletin. Kit 213165D02R01 Cost 33.00 USD Availability 90 calendar days from receipt of order The Kit availability given above is the standard lead time from the date of your purchase order. If you require Kits before this time, please include a retrofit planning schedule with your order so that we can try to comply with your requirements. The sales terms (costs and availability) are estimated in relation to economic conditions at the issue date of the Service Bulletin. B. INDUSTRY SUPPORT INFORMATION AIRBUS will share the costs of accomplishment of this Service Bulletin by providing the kits at no charge for orders placed before 31. Dec. 2014.

DATE: Sep 27/11 SERVICE BULLETIN No.: A330-21-3165 REVISION No.: 03 - Dec 07/12 Page: 11 6

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# @A330 SERVICE BULLETIN For the accomplishment of this Service Bulletin before 31. Dec. 2014, AIRBUS will credit the manhours indicated in this Service Bulletin at the agreed in-house warranty labor rate for claims received not later than 90 days after completion of the last affected aircraft of your fleet. C. LIST OF COMPONENTS Kit 213165D01R03 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 6 EN6081D4-04 2 RIVET 7 ABS1577A05 1 BRACKET 8 EN6081D4-05 3 RIVET NOTE: If you find part numbers of hardware components in the related kit(s) which you cannot identify in the LIST OF COMPONENTS of this Service Bulletin, refer to Standards Manual (SM). The SM will give you the correct part number to part number relationship. Kit 213165D02R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 1 NAS1801-3-7 2 SCREW 2 MS21042-3 1 NUT 3 NAS1149C0332R 2 WASHER 9 E0090-10-200NN 1 LEAD (10) E0091-10-160NN NOTE: If you find part numbers of hardware components in the related kit(s) which you cannot identify in the LIST OF COMPONENTS of this Service Bulletin, refer to Standards Manual (SM). The SM will give you the correct part number to part number relationship. D. LIST OF MATERIALS - OPERATOR SUPPLIED (1) Consumable Materials Consumable CMLD01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Cleaning Solvent 11-016 As required Lint-Free Cotton Cloth 19-003 As required (2) Components None (3) Equipment None
DATE: Sep 27/11 SERVICE BULLETIN No.: A330-21-3165 REVISION No.: 03 - Dec 07/12 Page: 12 6

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# @A330 SERVICE BULLETIN
E. PARTS TO BE RE-IDENTIFIED BY OPERATOR None F. TOOLING None

DATE: Sep 27/11 SERVICE BULLETIN No.: A330-21-3165 REVISION No.: 03 - Dec 07/12 Page: 13 6

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# @A330 SERVICE BULLETIN

This Page Intentionally Left Blank

DATE: Sep 27/11 SERVICE BULLETIN No.: A330-21-3165 REVISION No.: 03 - Dec 07/12 Page: 14 6

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# @A330 SERVICE BULLETIN
3. ACCOMPLISHMENT INSTRUCTIONS Task 213165-831-848-001 - Modification 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. IN CASE OF CONTAMINATION REFER TO ESPM 20-55-00. Task Associated Data Manpower TOTAL MANHOURS 3.25 ELAPSED TIME (HOURS) 3.25 A. GENERAL (1) Subtask 213165-910-201-001 - Standard Practices Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-20-00, Page Block 001 06-30-00, Page Block 001 06-31-53, Page Block 001 06-41-53, Page Block 001 Structural Repair Manual (SRM) 51-44-00 (a) For identification of zones (Refer to AMM 06-20-00, Page Block 001). (b) For Stringer (STGR) identification (Refer to AMM 06-30-00, Page Block 001). (c) For Frame (FR) identification (Refer to AMM 06-31-53, Page Block 001). (d) For sidewall panel identification (Refer to AMM 06-41-53, Page Block 001). DATE: Sep 27/11 SERVICE BULLETIN No.: A330-21-3165 REVISION No.: 03 - Dec 07/12 Page: 15 6

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# @A330 SERVICE BULLETIN (e) For fastener hole diameter and drill and deburr data (Refer to SRM 51-44-00). (2) Subtask 213165-839-201-001 - Administrative Manpower Resources Skills NON SPECIFIC Write in the applicable aircraft records that you done all the work given in this Service Bulletin. B. PREPARATION (1) Subtask 213165-941-201-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802 Task 25-53-00-000-801 Task 25-80-00-000-801 Task 52-30-00-010-801 Fig. A-GBAAA Modify the bonding lead installation Sheet 01 Sheet 02 Fig. A-GBBAA Modify the bonding lead installation Sheet 01 Sheet 02 (a) Make sure that the aircraft is electrically grounded (Refer to AMM Task 12-34-24-860-802). (b) Put an access platform in position at the Aft cargo-compartment door. (c) Open the Aft cargo-compartment door (Refer to AMM Task 52-30-00-010-801). (d) If a Cargo Loading System (CLS) is installed, put a warning notice in position on the control panel to tell persons not to operate the CLS. (e) Remove the access panel 151TW (Refer to AMM Task 25-53-00-000-801). (f) In the work area, Zone 160, as shown on Fig. A-GBAAA Sheet 01 and Fig. A-GBBAA Sheet 01, remove the insulation blankets (Refer to AMM Task 25-80-00-000-801). C. PROCEDURE (1) Subtask 213165-831-201-001 - Modify the bonding lead installation Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills AIRFRAME DATE: Sep 27/11 SERVICE BULLETIN No.: A330-21-3165 REVISION No.: 03 - Dec 07/12 Page: 16 6

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# @A330 SERVICE BULLETIN
Material necessary to do the job Kit 213165D01R03 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 6 EN6081D4-04 2 RIVET 7 ABS1577A05 1 BRACKET 8 EN6081D4-05 3 RIVET Kit 213165D02R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 NAS1801-3-7 2 SCREW 2 MS21042-3 1 NUT 3 NAS1149C0332R 2 WASHER 9 E0090-10-200NN 1 LEAD Consumable CMLD01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Cleaning Solvent 11-016 As required Lint-Free Cotton Cloth 19-003 As required References Aircraft Maintenance Manual (AMM) Task 20-28-00-912-801 25-80-00, Page Block 801 Elec. Std. Practices Manual (ESPM) 20-51-20 20-51-21 Structural Repair Manual (SRM) 51-42-11 51-44-11 Fig. A-GBAAA Modify the bonding lead installation Sheet 01 Sheet 02 Fig. A-GBBAA Modify the bonding lead installation Sheet 01 Sheet 02 (a) As shown on Fig. A-GBAAA Sheet 01 and Fig. A-GBAAA Sheet 02, View C, remove: 1 Nut Item (2) Discard 1 Washer Item (3) Discard 1 Screw Item (1) Discard disconnect: 1 Bonding Lead Item (4) Retain 1 Bonding Lead E0091-10-160NN Item (10) Discard DATE: Sep 27/11 SERVICE BULLETIN No.: A330-21-3165 REVISION No.: 03 - Dec 07/12 Page: 17 6

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# @A330 SERVICE BULLETIN (b) As shown on Fig. A-GBAAA Sheet 01 and Fig. A-GBAAA Sheet 02, View E, remove: 1 Nut Item (2) Discard 1 Washer Item (3) Discard 1 Screw Item (1) Discard 1 Bonding Lead E0091-10-160NN Item (10) Discard (c) As shown on Fig. A-GBAAA Sheet 02, View C, at FR64, remove: 2 Rivet Item (6) Discard 1 Bracket Item (5) Discard (d) As shown on Fig. A-GBAAA Sheet 02, View D, close the holes with: 2 Rivet EN6081D4-04 Item 6 (Refer to SRM 51-42-11). (e) Install the new bracket at STGR34, between FR64 and FR65 LH, as shown on Fig. A-GBBAA Sheet 01 and Fig. A-GBBAA Sheet 02, View E. 1 At STGR34 make marks to show the position of the holes. 2 Drill the pilot hole at STGR34 with a diameter of 2.4mm (0.094inch) (Refer to SRM 51-44-11). 3 Temporarily install: 1 Bracket ABS1577A05 Item 7 NOTE: Use the new hole at STGR34. 4 Transfer drill the holes from the bracket, item 7, to STGR34 with a diameter of 3.3mm (0.13inch) (Refer to SRM 51-44-11). 5 Remove the bracket and deburr the holes at STGR34 and the bracket, item 7 (Refer to SRM 51-44-11). 6 Clean the contact surface of the STGR34 LH and the bracket, item 7, with: Lint-Free Cotton Cloth 19-003 As required
and Cleaning Solvent 11-016 As required

DATE: Sep 27/11 SERVICE BULLETIN No.: A330-21-3165 REVISION No.: 03 - Dec 07/12 Page: 18 6

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# @A330 SERVICE BULLETIN

7 Install: 1 Bracket ABS1577A05 Item 7 3 Rivet EN6081D4-05 Item 8 (Refer to SRM 51-42-11). NOTE: Do the electrical bonding of the rivets (Refer to ESPM 20-51-20) and (Refer to AMM Task 20-28-00-912-801). (f) If installed, make a cutout in the insulation blanket in position of the new bracket, item 7, for the installation of the insulation blanket (Refer to AMM 25-80-00, Page Block 801). NOTE: Damaged insulations must be repaired (g) Cut the waste water pipe insulation and move it in the old position. (h) Install the bonding clamp on the new position as shown on Fig. A-GBBAA Sheet 02, View D. (i) On the waste water pipe, as shown on Fig. A-GBBAA Sheet 02, View D, install: 1 Bonding Lead E0090-10-200NN Item 9 with: 1 Screw NAS1801-3-7 Item 1 1 Washer NAS1149C0332R Item 3 1 Nut MS21042-3 Item 2 (j) As shown on Fig. A-GBBAA Sheet 02, View C, connect: 1 Bonding Lead Item (4) Retained at removal and 1 Bonding Lead E0090-10-200NN Item 9 with: 1 Screw NAS1801-3-7 Item 1 1 Washer NAS1149C0332R Item 3 (k) Do the electrical bonding (Refer to ESPM 20-51-21).

DATE: Sep 27/11 SERVICE BULLETIN No.: A330-21-3165 REVISION No.: 03 - Dec 07/12 Page: 19 6

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# @A330 SERVICE BULLETIN
D. TEST (1) Subtask 213165-760-201-001 - Test of electrical bonding Manpower Resources Skills ELECTRICAL References Aircraft Maintenance Manual (AMM) Task 20-28-00-720-805 (a) Check the electrical bonding of the bonding lead and the new bracket (Refer to AMM Task 20-28-00-720-805). E. CLOSE-UP (1) Subtask 213165-942-201-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 25-53-00-400-801 Task 25-80-00-400-801 Task 52-30-00-410-801 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) In the work area, install the insulation blankets (Refer to AMM Task 25-80-00-400-801). (c) Install the access panel 151TW (Refer to AMM Task 25-53-00-400-801). (d) If installed, remove the warning notice from the CLS. (e) Close the Aft cargo-compartment door (Refer to AMM Task 52-30-00-410-801). (f) Remove the access platform(s).

DATE: Sep 27/11 SERVICE BULLETIN No.: A330-21-3165 REVISION No.: 03 - Dec 07/12 Page: 20 6

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# @A330 SERVICE BULLETIN
Task 213165-831-849-001 - Modification - ADDITIONAL WORK 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. IN CASE OF CONTAMINATION REFER TO ESPM 20-55-00. Task Associated Data Zone 160 Manpower TOTAL MANHOURS 2.50 ELAPSED TIME (HOURS) 2.50 A. GENERAL (1) Subtask 213165-910-202-001 - Standard Practices Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-20-00, Page Block 001 06-30-00, Page Block 001 06-31-53, Page Block 001 06-41-53, Page Block 001 (a) For identification of zones (Refer to AMM 06-20-00, Page Block 001). (b) For Stringer (STGR) identification (Refer to AMM 06-30-00, Page Block 001). (c) For Frame (FR) identification (Refer to AMM 06-31-53, Page Block 001). (d) For sidewall panel identification (Refer to AMM 06-41-53, Page Block 001).

DATE: Sep 27/11 SERVICE BULLETIN No.: A330-21-3165 REVISION No.: 03 - Dec 07/12 Page: 21 6

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# @A330 SERVICE BULLETIN (2) Subtask 213165-839-202-001 - Administrative Manpower Resources Skills NON SPECIFIC Write in the applicable aircraft records that you done all the work given in this Service Bulletin. B. PREPARATION (1) Subtask 213165-941-202-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802 Task 25-53-00-000-801 Task 52-30-00-010-801 (a) Make sure that the aircraft is electrically grounded (Refer to AMM Task 12-34-24-860-802). (b) Put an access platform in position at the Aft cargo-compartment door. (c) Open the Aft cargo-compartment door (Refer to AMM Task 52-30-00-010-801). (d) If a Cargo Loading System (CLS) is installed, put a warning notice in position on the control panel to tell persons not to operate the CLS. (e) Remove the access panel 151TW (Refer to AMM Task 25-53-00-000-801). C. PROCEDURE (1) Subtask 213165-831-202-001 - Modify the bonding lead installation Work Zones and Access Panels Zone Access/Work location 160 Manpower Resources Manhours 0.25 Minimum number of person 1 Subtask elapsed time 0.25 Skills ELECTRICAL

DATE: Sep 27/11 SERVICE BULLETIN No.: A330-21-3165 REVISION No.: 03 - Dec 07/12 Page: 22 6

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# @A330 SERVICE BULLETIN
Material necessary to do the job Kit 213165D02R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 NAS1801-3-7 2 SCREW 2 MS21042-3 1 NUT 3 NAS1149C0332R 2 WASHER 9 E0090-10-200NN 1 LEAD References Elec. Std. Practices Manual (ESPM) 20-51-21 Fig. A-GBCAA Modify the bonding lead installation - ADDITIONAL WORK Sheet 01 Sheet 02 (a) As shown on Fig. A-GBCAA Sheet 01 and Fig. A-GBCAA Sheet 02, View C, remove: 1 Washer Item (3) Discard 1 Screw Item (1) Discard and disconnect: 1 Lead Bonding Item (4) Retain 1 Bonding Lead E0091-10-160NN Item (10) Discard (b) As shown on Fig. A-GBCAA Sheet 01 and Fig. A-GBCAA Sheet 02, View D, remove: 1 Nut Item (2) Discard 1 Washer Item (3) Discard 1 Screw Item (1) Discard 1 Bonding Lead E0091-10-160NN Item (10) Discard (c) If installed, cut the waste water pipe insolation and move it to the old position. (d) Install the bonding clamp on the new position as shown Fig. A-GBCAA Sheet 02, View D. (e) On the waste water pipe, as shown on Fig. A-GBCAA Sheet 02, View D, install: 1 Bonding Lead E0090-10-200NN Item 9 with:
DATE: Sep 27/11 SERVICE BULLETIN No.: A330-21-3165 REVISION No.: 03 - Dec 07/12 Page: 23 6

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# @A330 SERVICE BULLETIN

1 Screw NAS1801-3-7 Item 1 1 Washer NAS1149C0332R Item 3 1 Nut MS21042-3 Item 2 (f) As shown on Fig. A-GBCAA Sheet 02, View C, connect: 1 Lead Bonding Item (4) Retained at removal 1 Bonding Lead E0090-10-200NN Item 9 with: 1 Screw NAS1801-3-7 Item 1 1 Washer NAS1149C0332R Item 3 (g) Do the electrical bonding (Refer to ESPM 20-51-21). D. TEST (1) Subtask 213165-760-202-001 - Electrical Manpower Resources Skills ELECTRICAL References Aircraft Maintenance Manual (AMM) Task 20-28-00-720-805 (a) Check the electrical bonding of the bonding lead (Refer to AMM Task 20-28-00-720-805). E. CLOSE-UP (1) Subtask 213165-942-202-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 25-53-00-400-801 Task 52-30-00-410-801 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Install the access panel 151TW (Refer to AMM Task 25-53-00-400-801). (c) If installed, remove the warning notice from the CLS. (d) Close the Aft cargo-compartment door (Refer to AMM Task 52-30-00-410-801). DATE: Sep 27/11 SERVICE BULLETIN No.: A330-21-3165 REVISION No.: 03 - Dec 07/12 Page: 24 6

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# @A330 SERVICE BULLETIN (e) Remove the access platform(s).

DATE: Sep 27/11 SERVICE BULLETIN No.: A330-21-3165 REVISION No.: 03 - Dec 07/12 Page: 25 6

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# @A330 SERVICE BULLETIN

**CONF ALL



### B



## A 283HN

FR73 FR62

STGR34 FR64 FR63

FR62

STGR33 STGR32



## B 283HN



### C **D E**  Z160 

### A

G_SB_213165_6_BAAA_01_03 Figure A-GBAAA - Sheet 01 Modify the bonding lead installation DATE: Sep 27/11 SERVICE BULLETIN No.: A330-21-3165 REVISION No.: 03 - Dec 07/12 Page: 26 6

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# @A330 SERVICE BULLETIN

**CONF ALL

FR64 (1)

(2) (5) (4)

(6) 

## BEFORE **AFTER**

(3)



## C FR64

6



## D (10)

(1)

(10) (3)

(2) 

## E (8)

G_SB_213165_6_BAAA_02_02 Figure A-GBAAA - Sheet 02 Modify the bonding lead installation DATE: Sep 27/11 SERVICE BULLETIN No.: A330-21-3165 REVISION No.: 03 - Dec 07/12 Page: 27 6

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# @A330 SERVICE BULLETIN

**CONF ALL



### B



## A 283HN

FR73 FR62

STGR34 FR64 FR63

FR62

STGR33 STGR32



## B 283HN



### C **D** Z160 

### A

G_SB_213165_6_BBAA_01_03 Figure A-GBBAA - Sheet 01 Modify the bonding lead installation DATE: Sep 27/11 SERVICE BULLETIN No.: A330-21-3165 REVISION No.: 03 - Dec 07/12 Page: 28 6

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# @A330 SERVICE BULLETIN

**CONF ALL

1 3 7 8

9

98.2 mm (3.87 in) (115.0 mm)

(4.53 in) 14.0 mm (0.55 in)

**FWD** FR64 STGR34 STGR34

7 (4) 1

9 3

2 ca. 72.0 mm (2.83 in)
(8) OLD CLAMP

POSITION



## C **D**

**E E** 

G_SB_213165_6_BBAA_02_02 Figure A-GBBAA - Sheet 02 Modify the bonding lead installation DATE: Sep 27/11 SERVICE BULLETIN No.: A330-21-3165 REVISION No.: 03 - Dec 07/12 Page: 29 6

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# @A330 SERVICE BULLETIN

**CONF ALL



### B



## A 283HN

FR73 FR62

STGR34 FR64 FR63

FR62

STGR33 STGR32



## B 283HN



### C **D** Z160 

### A

G_SB_213165_6_BCAA_01_02 Figure A-GBCAA - Sheet 01 Modify the bonding lead installation - ADDITIONAL WORK DATE: Sep 27/11 SERVICE BULLETIN No.: A330-21-3165 REVISION No.: 03 - Dec 07/12 Page: 30 6

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# @A330 SERVICE BULLETIN

**CONF ALL

STGR34
1 3 (10) (4)

1

(10) 3

2 ca. 72.0 mm (2.83 in)
(8) OLD CLAMP

POSITION 

## C

**D** (1) (3)

9

9 (1) (3)

(2)

G_SB_213165_6_BCAA_02_01 Figure A-GBCAA - Sheet 02 Modify the bonding lead installation - ADDITIONAL WORK DATE: Sep 27/11 SERVICE BULLETIN No.: A330-21-3165 REVISION No.: 03 - Dec 07/12 Page: 31 6

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# @A330 SERVICE BULLETIN REPORTING SHEET 

### TITLE: AIR CONDITIONING - GENERAL - INSTALL NEW BONDING BRACKETS AFTER FRAME64 LH BETWEEN P33-P34 MODIFICATION No.: 201500D50418 Please complete the appropriate item (A or B): A - SB WILL BE embodied YES/NO (if NO please comment) If YES, aircraft concerned (as per SB effectivity by default) and planned dates (month/year) of embodiment:

B - SB HAS BEEN embodied on aircraft: Operator comments:
From Airline: Name/Title: Signature: Date: If operational documentation is affected (see Paragraph 1.K of this SB): If information is needed prior to next normal revision or prior to SB embodiment, please indicate required service(s): Either: Modification Operational Impact (MOI), if available YES/NO Or : Intermediate revision YES/NO Important Information: This SB will only be incorporated in your maintenance and operational documentation if this sheet is returned to Airbus and signed by a duly authorised representative. With the next feasible revision, this will result in - Updating of maintenance documentation to show pre and post SB data. - Updating of maintenance and operational documentation to show post SB data after embodiment. If this SB requires previous or simultaneous accomplishment of other SBs, Airbus shall automatically include them in the manual revisions. Refer to SIL 00-037 for detailed information. Please return this completed sheet to: AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Attn: SDC32 Technical Data and Documentation Services FAX: (+33) 5 61 93 28 06 e-mail: sb.reporting@airbus.com or via your Resident Customer Support Office. Alternatively, SB lists via letters or fax are also accepted.

DATE: Sep 27/11 SERVICE BULLETIN No.: A330-21-3165 REVISION No.: 03 - Dec 07/12 Page: 1 6

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

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

DATE: Sep 27/11 SERVICE BULLETIN No.: A330-21-3165 REVISION No.: 03 - Dec 07/12 Page: 1 6

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