@A330

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 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

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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.

MANDATORY MANDATORY MANDATORY

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

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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

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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

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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

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@A330

SERVICE BULLETIN

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 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

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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

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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

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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

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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

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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

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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.

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(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.

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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

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M. SPARES

None

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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.

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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

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E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

None

F. TOOLING

None

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This Page Intentionally Left Blank

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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).

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(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

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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

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(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

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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).

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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).

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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).

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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

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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:

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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).

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(e) Remove the access platform(s).

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**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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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

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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

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

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

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SERVICE BULLETIN

QUALITY PERCEPTION FORM

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

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

improve the quality of our Service Bulletins.

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

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

- Quality rating of this SB 4321

- Quality rating of the Accomplishment Instructions 4321

- Quality rating of the Illustrations 4321

- Is this SB easy to understand ? Y/N

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

short description of the issue.

Planning Material Instructions

X Effectivity X Kit content X Preparation

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

X Manpower X Industry support X Test

X References X Re-identification X Close-Up

X Publication X Tooling X Illustrations

Comments:

Operator: Date:

Name/Title:

Please return this form to:

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX FRANCE

Attn : SEM4 Service Bulletins Management

FAX : (33) 5 61 93 42 51

Or via your Resident Customer Support Office.

DATE: Sep 27/11 SERVICE BULLETIN No.: A330-21-3165

REVISION No.: 03 - Dec 07/12 Page: 1

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