# @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: 92 

### TITLE: ELECTRIC AND ELECTRONIC COMMON INSTALLATION - GENERAL - RE-ROUTING OF HARNESSES AT DOOR 3 AREA, LH AND RH SIDE **CONF ALL MODIFICATIONS MODIFICATION CLASSIFICATION MAJOR 201669S31758 MINOR 202319S32230 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 During aircraft production, potential contact between hatrack rod and harness 1523VB at Left Hand side (LH) and 1524VB Right Hand side (RH) between frame Frame 53.6 and Frame 53.8 and, between Stringer 14 and Stringer 15 has been identified. No findings have been reported from in-service aircraft. This contact could generate a chafing on the wirings leading to a potential effect on the oxygen container opening. This Service Bulletin requests the modification of the routing of the harnesses 1523VB (LH) and 1524VB (RH) at the level of the door 3 area LH and RH side. Accomplishment of this Service Bulletin will contribute to prevent potential wire chafing between the harnesses 1523VB (LH)/1524VB (RH) and the hatrack rods. GENERAL EVALUATION EVALUATION TABLE COMPLIANCE MANDATORY (1) CANCELS INSPECTION SB NO POTENTIAL AD YES A/C OPERATION AFFECTED NO RELIABILITY AFFECTED NO PAX COMFORT AFFECTED NO COST SAVING NO ETOPS AFFECTED NO STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED NO
DATE: Jan 11/13 SERVICE BULLETIN No.: A330-92-3098 REVISION No.: 00 - Jan 11/13 Page: 1 5

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# @A330 SERVICE BULLETIN SUMMARY NOTE (1): Service Bulletin must be accomplished. MATERIAL PRICE INFORMATION **CONF 001 MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Kit 923098A01R00 1 527.00 Ramp assy, Wiring ramp Kit 923098A02R00 1 530.00 Ramp assy, Wiring ramp TOTAL 1,057.00 **CONF 002 MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Kit 923098A03R00 1 393.00 Ramp assy Kit 923098A04R00 1 393.00 Ramp assy TOTAL 786.00 EFFECTIVITY **CONF ALL This Service Bulletin is applicable to this (these) operator(s) :

11S 46W AAR AAW AFL ARA ASY AVA AZA BEC BER CCA CES CHH CPA CRK CSN DAH DAL DLH EIN ETD EVA FIN FST GIA HAL HVN ISS IYE JAI JST KAL KFR KLM MAS MAU MEA MSR OMA QAF QFA QTR RJA RSF SAA SIA SVA SWR TAM TAP THY UAF USA 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 DATE: Jan 11/13 SERVICE BULLETIN No.: A330-92-3098 REVISION No.: 00 - Jan 11/13 Page: 2 5

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# @A330 SERVICE BULLETIN SUMMARY EQUIPMENT NO HARD NO SOFT NO OBRM NO MANPOWER **CONF 001 Task 923098-831-801-001: Modification TOTAL MANHOURS 6.00 ELAPSED TIME (HOURS) 3.00 **CONF 002 Task 923098-831-801-001: Modification TOTAL MANHOURS 5.00 ELAPSED TIME (HOURS) 2.50 APPENDICES **CONF ALL Appendix 01 - Elapsed Time Assumption

DATE: Jan 11/13 SERVICE BULLETIN No.: A330-92-3098 REVISION No.: 00 - Jan 11/13 Page: 3 5

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# @A330 SERVICE BULLETIN SUMMARY

**CONF 001

STGR12L

STGR14L 

### A

LH SIDE SHOWN RH SIDE SYMMETRICAL 

## B **FWD** 

## A

STGR17L Z844

Z834



## BEFORE
FR53.9 FR53.8 FR53.7 FR53.6

1M 2M

55LG (56LG) 2M

FR53.5 FR53.9 

### B **C**

**B C** 

G_SB_923098_5_SAAA_01_00 Figure A-FSAAA - Sheet 01

DATE: Jan 11/13 SERVICE BULLETIN No.: A330-92-3098 REVISION No.: 00 - Jan 11/13 Page: 4 5

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# @A330 SERVICE BULLETIN SUMMARY

**CONF 001

STGR12L

STGR14L

LH SIDE SHOWN RH SIDE SYMMETRICAL **FWD** 

## AFTER

FR53.9 FR53.6 2M

2M 55LG (56LG)

INSTALL INSTALL RAMP ASSY

1M


## C WIRING RAMP

FR53.8

G_SB_923098_5_SAAA_02_00 Figure A-FSAAA - Sheet 02

DATE: Jan 11/13 SERVICE BULLETIN No.: A330-92-3098 REVISION No.: 00 - Jan 11/13 Page: 5 5

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# @A330 SERVICE BULLETIN SUMMARY

**CONF 002

STGR12L

STGR14L 

### A

LH SIDE SHOWN RH SIDE SYMMETRICAL 

## B **FWD** Z844

Z834



## BEFORE FR53.9 FR53.8 FR53.7 FR53.6

1M 2M 

## A FR53.5 FR53.9 

### B **C**

**B C** 

LINING BRACKET

G_SB_923098_5_SAAB_01_02 Figure A-FSAAB - Sheet 01

DATE: Jan 11/13 SERVICE BULLETIN No.: A330-92-3098 REVISION No.: 00 - Jan 11/13 Page: 6 5

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# @A330 SERVICE BULLETIN SUMMARY

**CONF 002

STGR12L

STGR14L

LH SIDE SHOWN RH SIDE SYMMETRICAL **FWD**

## AFTER

FR53.9 FR53.8 FR53.7 FR53.6

1M 2M



### F



## C INSTALL RAMP ASSY

G_SB_923098_5_SAAB_02_00 Figure A-FSAAB - Sheet 02

DATE: Jan 11/13 SERVICE BULLETIN No.: A330-92-3098 REVISION No.: 00 - Jan 11/13 Page: 7 5

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# @A330 SERVICE BULLETIN SUMMARY

This Page Intentionally Left Blank

DATE: Jan 11/13 SERVICE BULLETIN No.: A330-92-3098 REVISION No.: 00 - Jan 11/13 Page: 8 5

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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: 92 

### TITLE: ELECTRIC AND ELECTRONIC COMMON INSTALLATION - GENERAL - RE-ROUTING OF HARNESSES AT DOOR 3 AREA, LH AND RH SIDE MODIFICATION No.: 201669S31758 202319S32230 This document contains AIRBUS PROPRIETARY INFORMATION and shall at all times remain the property of AIRBUS; no intellectual property right or licence is granted by AIRBUS in connection with any information contained in it. It is delivered on the express condition that said document and the information contained in it shall be treated as confidential, shall not be used for any purpose other than that for which it is hereby delivered. It shall not be disclosed in whole or in part to third parties and shall not be duplicated in any manner (except for the purposes of performing the tasks described hereunder and provided that any recipient of such document shall comply with the conditions herein), without AIRBUS prior written consent. 1. PLANNING INFORMATION **CONF ALL A. EFFECTIVITY NOTE: This Service Bulletin is applicable only to aircraft on which Mod. No. 40161D17512 (INTRODUCE "TYPE A DOOR") is not embodied and on which Mod. No. 48825D42865 (DEFINE AND DESIGN ADAPTATIONS FOR CABIN COMPONENTS DUE TO ENHANCEMENT PROGRAM) is embodied. This Service Bulletin is not applicable on aircraft on which Mod. No. 52485D47698 is embodied (INSTALL A GASEOUS OXYGEN SYSTEM FOR A330-200 ENHANCED). (1) Models 330-202 330-203 330-223 330-243 330-302 330-323 330-342 330-343 (2) Effectivity by MSN 0506 0508 0513 0522 0524 0530 0533 0535 0542 0549 0552 0555 0570-0571 0573 0576 0578-0579 0587-0588 0591 0600 0605 0609-0610 0612 0614 0616 0618 0620-0621 0623 0625 0629 0631-0634 0636-0638 0640 0642 0644-0645 0647-0648 0650 0653 0655 0659 0661 0663 0665-0667 0674 0676 0678-0679 0682-0684 0686-0687 0690 0693 0696-0697 0700-0701 0703-0704 0708-0709 0713 0717-0718 0720 0722 0724 0726 0728-0730 0732 0735 0737-0738 0742-0743 0746-0747 0751 DATE: Jan 11/13 SERVICE BULLETIN No.: A330-92-3098 REVISION No.: 00 - Jan 11/13 Page: 1 5

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# @A330 SERVICE BULLETIN
0754-0755 0760 0770 0772-0774 0776-0778 0780-0782 0784-0785 0788 0791-0792 0796-0797 0799 0801 0803 0806-0807 0809-0811 0815 0817 0819-0822 0824-0825 0827 0830-0832 0834 0836 0841-0843 0845 0849-0855 0857-0860 0862-0863 0865-0869 0871 0873-0877 0881-0885 0887-0888 0890-0892 0895-0896 0898-0901 0903-0906 0909 0913-0916 0919 0922-0923 0926-0928 0932 0934 0936-0937 0939-0940 0942-0943 0945-0949 0951 0954 0956 0958-0959 0961-0964 0967-0970 0973 0975-0980 0983-0984 0986 0989 0991 0994-1000 1002 1006-1007 1009-1016 1018-1020 1022-1023 1026 1029 1031 1033-1034 1036 1038-1039 1041-1047 1049 1052-1054 1057 1059 1061 1063 1067 1069 1071 1073 1076 1078 1080-1081 1084-1085 1088-1089 1093-1096 1098-1101 1104-1105 1107-1108 1112 1114 1116 1118 1120 1123-1124 1127 1129 1132-1133 1135 1137 1141 1143 1145-1147 1149-1150 1153 1155-1157 1159-1161 1163 1167-1174 1178 1181 1183-1184 1186 1188-1192 1196 1198 1200 1202-1205 1208-1210 1212-1214 1217-1230 1233-1240 1243-1246 1248-1252 1256 1258-1262 1264 1266-1267 1271 (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 AAW 0999 1043 AFL 0963 0973 1014 1045 1047 1264 ARA 0891 0927 ASY 0747 0951 0969 1036 1183 AVA 0948 0967 1009 1016 1073 1208 1224 AZA 1123 1135 1218 1225 1252 BEC 0863 BER 0665 CCA 0780 0785 0797 0810 0815 0860 0867 0873 0884 0890 0903 0909 1237 1260 CES 0713 0720 0728 0732 0735 0773 0777 0781 0782 0791 0821 0830 0836 0851 0862 0866 0916 0928 0936 0942 1262 1267 CHH 0875 0881 0906 0919 1159 1168 1178 1190 CPA 0679 0776 0850 0855 0895 0915 0959 1163 1196 1222 1239 CRK 1031 1034 1039 1042 1054 1059 CSN 0937 0954 0958 0964 1096 1116 1129 1202 1220 1233 1244 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 DLH 0570 0576 0579 0629 0636 0642 0645 0648 0687 0701 0896 0905 0913 0922 0989 EIN 0841

DATE: Jan 11/13 SERVICE BULLETIN No.: A330-92-3098 REVISION No.: 00 - Jan 11/13 Page: 2 5

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# @A330 SERVICE BULLETIN
OPERATOR MSN ETD 0717 0724 0729 0730 0737 0751 0788 0809 0824 0832 0852 0854 0868 0975 0991 1071 1081 1167 1205 1226 1245 EVA 0530 0535 0555 0573 0587 0634 0655 0661 0678 0693 0755 FIN 0994 1007 1013 1023 1067 1078 1088 1173 FST 1033 1046 1248 GIA 1020 1052 1184 1214 1261 HAL 1104 1114 1171 1217 1259 HVN 0943 0962 1019 1256 1266 ISS 0822 IYE 0625 0632 JAI 0807 0825 0831 0882 0885 0888 0901 0923 0932 0947 0956 JST 0506 0508 0513 0522 0842 0853 0940 0945 1198 1251 1258 KAL 1133 1155 1200 1203 KFR 0874 0939 0946 KLM 0682 0686 0703 0738 0770 0801 0811 0819 0834 0900 1161 MAS 1209 1219 1229 1234 1243 MAU 0883 1057 MEA 0926 0984 0995 0998 MSR 0600 0610 0666 0683 0696 0709 0726 1143 1230 1238 1246 OMA 1038 1044 1049 1063 1093 1120 1227 QAF 0605 QFA 0887 0892 0898 0976 1061 1094 1169 1174 QTR 0571 0612 0616 0623 0637 0638 0659 0684 0743 0746 0760 0792 0820 0849 RJA 0970 0979 1002 RSF 0980 0996 1235 SAA 1191 1210 1223 1236 1249 1271 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 1000 1018 1026 1029 1084 1089 1101 1145 1181 1188 TAM 0700 0869 0876 0949 0961 0968 0977 1112 1118 1213 1221 TAP 0877 0899 0904 0914 0934 THY 0697 0704 0742 0754 0774 1150 1160 1170 1172 1204 1212 1228 1240 UAF 1080 1186 1250 USA 1011 1022 1041 1069 1076 1095 1100 (4) Configuration by MSN MSN CONFIGURATION 0506 0508 0513 0522 0530 0535 0555 0573 0587 0634 0655 0661 0678 0693 0755 0842 0853 0887 0892 0898 0940 0945 0976 1061 1094 1123 1133 1135 1155 1169 1174 1198 1200 1203 1218 1225 1251 1252 1258 002

DATE: Jan 11/13 SERVICE BULLETIN No.: A330-92-3098 REVISION No.: 00 - Jan 11/13 Page: 3 5

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# @A330 SERVICE BULLETIN
MSN CONFIGURATION 0524 0533 0542 0549 0552 0570 0571 0576 0578 0579 0588 0591 0600 0605 0609 0610 0612 0614 0616 0618 0620 0621 0623 0625 0629 0631 0632 0633 0636 0637 0638 0640 0642 0644 0645 0647 0648 0650 0653 0659 0663 0665 0666 0667 0674 0676 0679 0682 0683 0684 0686 0687 0690 0696 0697 0700 0701 0703 0704 0708 0709 0713 0717 0718 0720 0722 0724 0726 0728 0729 0730 0732 0735 0737 0738 0742 0743 0746 0747 0751 0754 0760 0770 0772 0773 0774 0776 0777 0778 0780 0781 0782 0784 0785 0788 0791 0792 0796 0797 0799 0801 0803 0806 0807 0809 0810 0811 0815 0817 0819 0820 0821 0822 0824 0825 0827 0830 0831 0832 0834 0836 0841 0843 0845 0849 0850 0851 0852 0854 0855 0857 0858 0859 0860 0862 0863 0865 0866 0867 0868 0869 0871 0873 0874 0875 0876 0877 0881 0882 0883 0884 0885 0888 0890 0891 0895 0896 0899 0900 0901 0903 0904 0905 0906 0909 0913 0914 0915 0916 0919 0922 0923 0926 0927 0928 0932 0934 0936 0937 0939 0942 0943 0946 0947 0948 0949 0951 0954 0956 0958 0959 0961 0962 0963 0964 0967 0968 0969 0970 0973 0975 0977 0978 0979 0980 0983 0984 0986 0989 0991 0994 0995 0996 0997 0998 0999 1000 1002 1006 1007 1009 1010 1011 1012 1013 1014 1015 1016 1018 1019 1020 1022 1023 1026 1029 1031 1033 1034 1036 1038 1039 1041 1042 1043 1044 1045 1046 1047 1049 1052 1053 1054 1057 1059 1063 1067 1069 1071 1073 1076 1078 1080 1081 1084 1085 1088 1089 1093 1095 1096 1098 1099 1100 1101 1104 1105 1107 1108 1112 1114 1116 1118 1120 1124 1127 1129 1132 1137 1141 1143 1145 1146 1147 1149 1150 1153 1156 1157 1159 1160 1161 1163 1167 1168 1170 1171 1172 1173 1178 1181 1183 1184 1186 1188 1189 1190 1191 1192 1196 1202 1204 1205 1208 1209 1210 1212 1213 1214 1217 1219 1220 1221 1222 1223 1224 1226 1227 1228 1229 1230 1233 1234 1235 1236 1237 1238 1239 1240 1243 1244 1245 1246 1248 1249 1250 1256 1259 1260 1261 1262 1264 1266 1267 1271 001

(5) Configuration definition **CONF 001 Config. 001 is valid for aircraft equipped with ballasts (55LG and 56LG) and not equipped with lining brackets. **CONF 002 Config. 002 is valid for aircraft not equipped with ballasts (55LG and 56LG) and equipped with lining brackets. (6) Material Effectivity **CONF 001 MATERIAL QTY PER A/C SEE NOTES Kit 923098A01R00 1
DATE: Jan 11/13 SERVICE BULLETIN No.: A330-92-3098 REVISION No.: 00 - Jan 11/13 Page: 4 5

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# @A330 SERVICE BULLETIN

MATERIAL QTY PER A/C SEE NOTES Kit 923098A02R00 1 **CONF 002 MATERIAL QTY PER A/C SEE NOTES Kit 923098A03R00 1 Kit 923098A04R00 1 **CONF ALL B. CONCURRENT REQUIREMENTS None C. REASON (1) History During aircraft production, potential contact between hatrack rod and harness 1523VB at Left Hand side (LH) and 1524VB Right Hand side (RH) between frame Frame 53.6 and Frame 53.8 and, between Stringer 14 and Stringer 15 has been identified. No findings have been reported from in-service aircraft. This contact could generate a chafing on the wirings leading to a potential effect on the oxygen container opening. (2) Objective/Action This Service Bulletin requests the modification of the routing of the harnesses 1523VB (LH) and 1524VB (RH) at the level of the door 3 area LH and RH side. (3) Advantages Accomplishment of this Service Bulletin will contribute to prevent potential wire chafing between the harnesses 1523VB (LH)/1524VB (RH) and the hatrack rods. (4) Operational/Maintenance Consequences None D. DESCRIPTION To accomplish this Service Bulletin it is necessary to : **CONF 001 Task 923098-831-801-001: Modification (1) Remove the brackets of the Routes 1M and 2M between FR53.6 and FR53.8, LH Side (2) Remove the brackets of the Routes 1M and 2M between FR53.6 and FR53.8, RH Side

DATE: Jan 11/13 SERVICE BULLETIN No.: A330-92-3098 REVISION No.: 00 - Jan 11/13 Page: 5 5

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# @A330 SERVICE BULLETIN (3) Install the Ramp assy and the Wiring Ramp between FR53.6 and FR53.8, LH Side (4) Install the Ramp assy and the Wiring Ramp between FR53.6 and FR53.8, RH Side (5) Modify the routing of the routes 1M and 2M between FR53.6 and FR53.8, LH Side (6) Modify the routing of the routes 1M and 2M between FR53.6 and FR53.8, RH Side **CONF 002 Task 923098-831-801-001: Modification (1) Remove the brackets of the Routes 1M and 2M between FR53.6 and FR53.8, LH Side (2) Remove the brackets of the Routes 1M and 2M between FR53.6 and FR53.8, RH Side (3) Install the Ramp assy between FR53.6 and FR53.8, LH Side (4) Install the Ramp assy between FR53.6 and FR53.8, RH Side (5) Modify the routing of the routes 1M and 2M between FR53.6 and FR53.8, LH Side (6) Modify the routing of the routes 1M and 2M between FR53.6 and FR53.8, RH Side **CONF ALL E. COMPLIANCE (1) Classification MANDATORY: Service Bulletin must be accomplished. (2) Accomplishment Timescale This Service Bulletin has been classified Mandatory. It is expected that an Airworthiness Directive (AD) published by the European 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: Jan 11/13 SERVICE BULLETIN No.: A330-92-3098 REVISION No.: 00 - Jan 11/13 Page: 6 5

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# @A330 SERVICE BULLETIN
G. MANPOWER The manpower estimates given in this Service Bulletin are based on the direct labor cost to do the work. These estimates assume that the work will be done by experienced personnel, and may need to be revised upwards to suit operator’s circumstances. The estimates do not include the time to prepare, plan or inspect the work. Manufacture and procurement of parts and tools, drying times for paints, sealants, etc., and general administration work are also not included. **CONF 001 Task 923098-831-801-001: Modification Get Access 1.00 On Aircraft Remove the brackets of the Routes 1M and 2M between FR53.6 and FR53.8, LH Side 0.50 Remove the brackets of the Routes 1M and 2M between FR53.6 and FR53.8, RH Side 0.50 Install the Ramp assy and the Wiring Ramp between FR53.6 and FR53.8, LH Side 1.00 Install the Ramp assy and the Wiring Ramp between FR53.6 and FR53.8, RH Side 1.00 Modify the routing of the routes 1M and 2M between FR53.6 and FR53.8, LH Side 0.50 Modify the routing of the routes 1M and 2M between FR53.6 and FR53.8, RH Side 0.50 Close-Up 1.00 TOTAL MANHOURS 6.00 ELAPSED TIME (HOURS) 3.00 NOTE: For details concerning the elapsed time assumption refer to Appendix 01 - Elapsed Time Assumption . **CONF 002 Task 923098-831-801-001: Modification Get Access 1.00 On Aircraft Remove the brackets of the Routes 1M and 2M between FR53.6 and FR53.8, LH Side 0.50 Remove the brackets of the Routes 1M and 2M between FR53.6 and FR53.8, RH Side 0.50 Install the Ramp assy between FR53.6 and FR53.8, LH Side 0.50 Install the Ramp assy between FR53.6 and FR53.8, RH Side 0.50 Modify the routing of the routes 1M and 2M between FR53.6 and FR53.8, LH Side 0.50

DATE: Jan 11/13 SERVICE BULLETIN No.: A330-92-3098 REVISION No.: 00 - Jan 11/13 Page: 7 5

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# @A330 SERVICE BULLETIN
Task 923098-831-801-001: Modification Modify the routing of the routes 1M and 2M between FR53.6 and FR53.8, RH Side 0.50 Close-Up 1.00 TOTAL MANHOURS 5.00 ELAPSED TIME (HOURS) 2.50 NOTE: For details concerning the elapsed time assumption refer to Appendix 01 - Elapsed Time Assumption . **CONF ALL H. WEIGHT AND BALANCE Not Changed I. ELECTRICAL LOAD DATA Not Changed J. REFERENCES **CONF 001 Aircraft Maintenance Manual (AMM) 06-20-00 06-31-53 12-34-24 52-10-00 Elec. Std. Practices Manual (ESPM) 20-25-51 20-33-44 20-53-00 20-55-00 Standards Manual (SM) Structural Repair Manual (SRM) 51-42-00 51-43-00 **CONF 002 Aircraft Maintenance Manual (AMM) 06-20-00 06-31-53 12-34-24 52-10-00 Elec. Std. Practices Manual (ESPM) 20-25-51 20-33-44 20-53-00 20-55-00 Standards Manual (SM) Structural Repair Manual (SRM) 51-42-00 51-43-00 **CONF ALL K. PUBLICATION AFFECTED None L. INTERCHANGEABILITY/MIXABILITY Not Applicable M. SPARES None DATE: Jan 11/13 SERVICE BULLETIN No.: A330-92-3098 REVISION No.: 00 - Jan 11/13 Page: 8 5

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# @A330 SERVICE BULLETIN
2. MATERIAL INFORMATION **CONF ALL A. MATERIAL - PRICE AND AVAILABILITY (1) Procurement Addresses 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: Kit 923098A01R00 Kit 923098A02R00 Kit 923098A03R00 Kit 923098A04R00 AIRBUS Material, Logistics and Suppliers Weg beim Jaeger 150 D-22335 HAMBURG GERMANY For ordering by internet: http://spares.airbus.com For ordering by fax: +49 40 50 76 2590 For ordering by E-mail: airbus.kit@airbus.com (2) Price and Availability

Kit 923098A01R00 Cost 527.00 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 items are required 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. The latest valid price and lead time for ordering purposes shall be obtained through the AirbusSpares portal or through a request for quotation to airbus.kit@airbus.com. Kit 923098A02R00 Cost 530.00 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 items are required 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. The latest valid price and lead time for ordering purposes shall be obtained through the AirbusSpares portal or through a request for quotation to airbus.kit@airbus.com. Kit 923098A03R00 Cost 393.00 USD Availability 90 calendar days from receipt of order

DATE: Jan 11/13 SERVICE BULLETIN No.: A330-92-3098 REVISION No.: 00 - Jan 11/13 Page: 9 5

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# @A330 SERVICE BULLETIN The Kit availability given above is the standard lead time from the date of your purchase order. If items are required 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. The latest valid price and lead time for ordering purposes shall be obtained through the AirbusSpares portal or through a request for quotation to airbus.kit@airbus.com. Kit 923098A04R00 Cost 393.00 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 items are required 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. The latest valid price and lead time for ordering purposes shall be obtained through the AirbusSpares portal or through a request for quotation to airbus.kit@airbus.com. B. INDUSTRY SUPPORT INFORMATION Airbus will provide the kits at no charge for orders placed before Dec 31/15. For aircraft under warranty at Jul 01/10, 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 923098A01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 3 NAS1149F0332P 10 WASHER 8 NSA5050-3 5 NUT 12 NSA935504-03 1 BRACKET 18 NAS1801-3-7 3 SCREW 20 NSA5527-03-13 2 SPACER 21 NSA5159-19 1 STUD 22 NSA5527-03-12 1 SPACER 23 NSA5159-23 1 STUD 24 NSA5527-03-03 1 SPACER 25 NAS1801-3-20 2 SCREW 29 F9241964500000 1 RAMP 31 F9241965000000 1 RAMP 37 NSA5516-06ND 5 CLAMP 38 NSA5516-07ND 5 CLAMP 39 NSA5516-08ND 5 CLAMP NSA935401-03 10 TIE NSA935401-05 10 TIE NSA935401-08 10 TIE
DATE: Jan 11/13 SERVICE BULLETIN No.: A330-92-3098 REVISION No.: 00 - Jan 11/13 Page: 10 5

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# @A330 SERVICE BULLETIN
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 923098A02R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 3 NAS1149F0332P 10 WASHER 8 NSA5050-3 5 NUT 12 NSA935504-03 1 BRACKET 18 NAS1801-3-7 3 SCREW 20 NSA5527-03-13 2 SPACER 21 NSA5159-19 1 STUD 22 NSA5527-03-12 1 SPACER 23 NSA5159-23 1 STUD 24 NSA5527-03-03 1 SPACER 25 NAS1801-3-20 2 SCREW 30 F9241964500100 1 RAMP 31 F9241965000000 1 RAMP 37 NSA5516-06ND 5 CLAMP 38 NSA5516-07ND 5 CLAMP 39 NSA5516-08ND 5 CLAMP NSA935401-03 10 TIE NSA935401-05 10 TIE NSA935401-08 10 TIE 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 923098A03R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 3 NAS1149F0332P 7 WASHER 8 NSA5050-3 3 NUT 10 ABS0355-02 1 BRACKET 14 NAS1801-3-22 3 SCREW 18 NAS1801-3-7 3 SCREW 20 NSA5527-03-13 3 SPACER 28 NAS1801-08-7 1 SCREW 29 F9241964500000 1 RAMP 37 NSA5516-06ND 6 CLAMP 38 NSA5516-07ND 6 CLAMP 39 NSA5516-08ND 6 CLAMP NSA935401-03 5 TIE NSA935401-05 5 TIE DATE: Jan 11/13 SERVICE BULLETIN No.: A330-92-3098 REVISION No.: 00 - Jan 11/13 Page: 11 5

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# @A330 SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES NSA935401-08 5 TIE 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 923098A04R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 3 NAS1149F0332P 7 WASHER 8 NSA5050-3 3 NUT 10 ABS0355-02 1 BRACKET 14 NAS1801-3-22 3 SCREW 18 NAS1801-3-7 3 SCREW 20 NSA5527-03-13 3 SPACER 28 NAS1801-08-7 1 SCREW 30 F9241964500100 1 RAMP 37 NSA5516-06ND 6 CLAMP 38 NSA5516-07ND 6 CLAMP 39 NSA5516-08ND 6 CLAMP NSA935401-03 5 TIE NSA935401-05 5 TIE NSA935401-08 5 TIE 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 None E. PARTS TO BE RE-IDENTIFIED BY OPERATOR None F. TOOLING None

DATE: Jan 11/13 SERVICE BULLETIN No.: A330-92-3098 REVISION No.: 00 - Jan 11/13 Page: 12 5

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# @A330 SERVICE BULLETIN
3. ACCOMPLISHMENT INSTRUCTIONS Task 923098-831-801-001 - 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 **CONF 001 Zone 834 844 Access Door 832 842 Manpower TOTAL MANHOURS 6.00 ELAPSED TIME (HOURS) 3.00 **CONF 002 Zone 834 844 Access Door 832 842 Manpower TOTAL MANHOURS 5.00 ELAPSED TIME (HOURS) 2.50

DATE: Jan 11/13 SERVICE BULLETIN No.: A330-92-3098 REVISION No.: 00 - Jan 11/13 Page: 13 5

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# @A330 SERVICE BULLETIN
**CONF ALL A. GENERAL **CONF 001 (1) Subtask 923098-910-001-001 - Standard Practices Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-20-00, Page Block 001 06-31-53, Page Block 001 Elec. Std. Practices Manual (ESPM) 20-25-51 20-33-44 20-53-00 Structural Repair Manual (SRM) 51-42-00 51-43-00 (a) For the Frame (FR) identification, refer to AMM 06-31-53, Page Block 001. (b) For the identification of zones, refer to AMM 06-20-00, Page Block 001. (c) Remove and install fasteners in accordance with SRM 51-42-00. (d) Obtain alternative and substitute fastener data, in accordance with SRM 51-43-00. (e) For the cable tie application and tooling, refer to ESPM 20-33-44 and ESPM 20-25-51. (f) For Electrical Item inspection/check, refer to ESPM 20-53-00. (2) Subtask 923098-839-002-001 - Administrative Manpower Resources Skills NON SPECIFIC Write in the applicable aircraft records that you have done all the work given in this Service Bulletin. **CONF 002 (1) Subtask 923098-910-001-001 - Standard Practices Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-20-00, Page Block 001 06-31-53, Page Block 001

DATE: Jan 11/13 SERVICE BULLETIN No.: A330-92-3098 REVISION No.: 00 - Jan 11/13 Page: 14 5

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# @A330 SERVICE BULLETIN
References Elec. Std. Practices Manual (ESPM) 20-25-51 20-33-44 20-53-00 Structural Repair Manual (SRM) 51-42-00 51-43-00 (a) For the Frame (FR) identification, refer to AMM 06-31-53, Page Block 001. (b) For the identification of zones, refer to AMM 06-20-00, Page Block 001. (c) Remove and install fasteners in accordance with SRM 51-42-00. (d) Obtain alternative and substitute fastener data, in accordance with SRM 51-43-00. (e) For the cable tie application and tooling, refer to ESPM 20-33-44 and ESPM 20-25-51. (f) For Electrical Item inspection/check, refer to ESPM 20-53-00. (2) Subtask 923098-839-002-001 - Administrative Manpower Resources Skills NON SPECIFIC Write in the applicable aircraft records that you have done all the work given in this Service Bulletin. **CONF ALL B. PREPARATION **CONF 001 (1) Subtask 923098-941-001-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 12-34-24-860-002 Task 52-10-00-010-801 (a) Make sure that the aircraft is electrically grounded (Refer to AMM Task 12-34-24-860-002). (b) Put access platform(s) in position at doors 832 or 842. (c) Open the passenger/crew door 832 or 842 (Refer to AMM Task 52-10-00-010-801).

DATE: Jan 11/13 SERVICE BULLETIN No.: A330-92-3098 REVISION No.: 00 - Jan 11/13 Page: 15 5

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# @A330 SERVICE BULLETIN (2) Subtask 923098-010-001-001 - Remove the Door Frame Linings between FR53.5 and FR53.8, LH Side Work Zones and Access Panels Zone Access/Work location 834 Access Door 832 Manpower Resources Skills NON SPECIFIC References Fig. A-FBBAA Removal/Installation of the Door Frame linings between FR53.5 and FR53.8 Sheet 01
(a) Remove the door frame linings between FR53.5 and FR53.8, LH Side: Refer to Fig. A-FBBAA Sheet 01 1 Door Frame Lining Item (32) Retain 1 Door Frame Lining Item (34) Retain 1 Door Frame Lining Item (35) Retain

(3) Subtask 923098-010-002-001 - Remove the Door Frame Linings between FR53.5 and FR53.8, RH Side Work Zones and Access Panels Zone Access/Work location 844 Access Door 842 Manpower Resources Skills NON SPECIFIC References Fig. A-FBBAA Removal/Installation of the Door Frame linings between FR53.5 and FR53.8 Sheet 01
(a) Remove the door frame linings between FR53.5 and FR53.8, RH Side: Refer to Fig. A-FBBAA Sheet 01 1 Door Frame Lining Item (33) Retain 1 Door Frame Lining Item (34) Retain 1 Door Frame Lining Item (36) Retain

DATE: Jan 11/13 SERVICE BULLETIN No.: A330-92-3098 REVISION No.: 00 - Jan 11/13 Page: 16 5

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# @A330 SERVICE BULLETIN
**CONF 002 (1) Subtask 923098-941-001-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 12-34-24-860-002 Task 52-10-00-010-801 (a) Make sure that the aircraft is electrically grounded (Refer to AMM Task 12-34-24-860-002). (b) Put access platform(s) in position at doors 832 or 842. (c) Open the passenger/crew door 832 or 842 (Refer to AMM Task 52-10-00-010-801). (2) Subtask 923098-010-001-001 - Remove the Door Frame Linings between FR53.5 and FR53.8, LH Side Work Zones and Access Panels Zone Access/Work location 834 Access Door 832 Manpower Resources Skills NON SPECIFIC References Fig. A-FBBAA Removal/Installation of the Door Frame linings between FR53.5 and FR53.8 Sheet 01
(a) Remove the door frame linings between FR53.5 and FR53.8, LH Side: Refer to Fig. A-FBBAA Sheet 01 1 Door Frame Lining Item (32) Retain 1 Door Frame Lining Item (34) Retain 1 Door Frame Lining Item (35) Retain

(3) Subtask 923098-010-002-001 - Remove the Door Frame Linings between FR53.5 and FR53.8, RH Side Work Zones and Access Panels Zone Access/Work location 844 Access Door 842

DATE: Jan 11/13 SERVICE BULLETIN No.: A330-92-3098 REVISION No.: 00 - Jan 11/13 Page: 17 5

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# @A330 SERVICE BULLETIN Manpower Resources Skills NON SPECIFIC References Fig. A-FBBAA Removal/Installation of the Door Frame linings between FR53.5 and FR53.8 Sheet 01
(a) Remove the door frame linings between FR53.5 and FR53.8, RH Side: Refer to Fig. A-FBBAA Sheet 01 1 Door Frame Lining Item (33) Retain 1 Door Frame Lining Item (34) Retain 1 Door Frame Lining Item (36) Retain **CONF ALL C. PROCEDURE **CONF 001 (1) Subtask 923098-831-001-001 - Remove the brackets of the Routes 1M and 2M between FR53.6 and FR53.8, LH Side Work Zones and Access Panels Zone Access/Work location 834 Access Door 832 Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills AIRFRAME References Structural Repair Manual (SRM) 51-42-00 Fig. A-FBAAA Installation of the Ramp Assy and the Wiring Ramp between FR53.6 and FR53.8 Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 (a) Remove the brackets as shown on Fig. A-FBAAA Sheet 01 and Fig. A-FBAAA Sheet 02, Details D and E. In accordance with SRM 51-42-00:

DATE: Jan 11/13 SERVICE BULLETIN No.: A330-92-3098 REVISION No.: 00 - Jan 11/13 Page: 18 5

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# @A330 SERVICE BULLETIN
1 Remove the existing mountings as shown on detail D on Fig. A-FBAAA Sheet 02: a If the existing mountings are as shown in case 1: <1> Remove: 2 Screw Item (4) Discard 2 Bracket Item (2) Discard 2 Spacer Item (1) Discard 2 Washer Item (3) Discard b If the existing mountings are as shown in case 2: <1> Remove: 2 Screw Item (7) Discard 2 Bracket Item (2) Discard 2 Spacer Item (1) Discard 2 Washer Item (3) Discard 2 Nut Item (8) Discard 2 Remove the existing mounting as shown on detail E on Fig. A-FBAAA Sheet 02: a If the existing mounting is as shown in case 1: <1> Remove: 1 Screw Item (4) Discard 2 Bracket Item (2) Discard 1 Spacer Item (6) Discard 1 Washer Item (3) Discard 1 Nut Item (17) Discard b If the existing mounting is as shown in case 2: <1> Remove: 1 Screw Item (4) Discard
DATE: Jan 11/13 SERVICE BULLETIN No.: A330-92-3098 REVISION No.: 00 - Jan 11/13 Page: 19 5

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# @A330 SERVICE BULLETIN 1 Bracket Item (2) Discard 1 Spacer Item (1) Discard 1 Washer Item (3) Discard
c If the existing mounting is as shown in case 3: <1> Remove: 1 Screw Item (7) Discard 1 Bracket Item (2) Discard 1 Spacer Item (1) Discard 1 Washer Item (3) Discard 1 Nut Item (8) Discard NOTE: There is no need to disconnect the harness. (2) Subtask 923098-831-002-001 - Remove the brackets of the Routes 1M and 2M between FR53.6 and FR53.8, RH Side Work Zones and Access Panels Zone Access/Work location 844 Access Door 842 Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills AIRFRAME References Structural Repair Manual (SRM) 51-42-00 Fig. A-FBAAA Installation of the Ramp Assy and the Wiring Ramp between FR53.6 and FR53.8 Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 (a) Remove the brackets as shown on Fig. A-FBAAA Sheet 01 and Fig. A-FBAAA Sheet 02, Details D and E. In accordance with SRM 51-42-00:

DATE: Jan 11/13 SERVICE BULLETIN No.: A330-92-3098 REVISION No.: 00 - Jan 11/13 Page: 20 5

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# @A330 SERVICE BULLETIN
1 Remove the existing mountings as shown on detail D on Fig. A-FBAAA Sheet 02: a If the existing mountings are as shown in case 1: <1> Remove: 2 Screw Item (4) Discard 2 Bracket Item (2) Discard 2 Spacer Item (1) Discard 2 Washer Item (3) Discard b If the existing mountings are as shown in case 2: <1> Remove: 2 Screw Item (7) Discard 2 Bracket Item (2) Discard 2 Spacer Item (1) Discard 2 Washer Item (3) Discard 2 Nut Item (8) Discard 2 Remove the existing mounting as shown on detail E on Fig. A-FBAAA Sheet 02: a If the existing mounting is as shown in case 1: <1> Remove: 1 Screw Item (4) Discard 2 Bracket Item (2) Discard 1 Spacer Item (6) Discard 1 Washer Item (3) Discard 1 Nut Item (17) Discard b If the existing mounting is as shown in case 2: <1> Remove: 1 Screw Item (4) Discard
DATE: Jan 11/13 SERVICE BULLETIN No.: A330-92-3098 REVISION No.: 00 - Jan 11/13 Page: 21 5

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# @A330 SERVICE BULLETIN 1 Bracket Item (2) Discard 1 Spacer Item (1) Discard 1 Washer Item (3) Discard
c If the existing mounting is as shown in case 3: <1> Remove: 1 Screw Item (7) Discard 1 Bracket Item (2) Discard 1 Spacer Item (1) Discard 1 Washer Item (3) Discard 1 Nut Item (8) Discard NOTE: There is no need to disconnect the harness. (3) Subtask 923098-831-003-001 - Install the Ramp assy and the Wiring Ramp between FR53.6 and FR53.8, LH Side Work Zones and Access Panels Zone Access/Work location 834 Access Door 832 Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills AIRFRAME Material necessary to do the job Kit 923098A01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 3 NAS1149F0332P 7 WASHER 8 NSA5050-3 5 NUT 12 NSA935504-03 1 BRACKET 18 NAS1801-3-7 2 SCREW 21 NSA5159-19 1 STUD 22 NSA5527-03-12 1 SPACER 23 NSA5159-23 1 STUD 24 NSA5527-03-03 1 SPACER 29 F9241964500000 1 RAMP DATE: Jan 11/13 SERVICE BULLETIN No.: A330-92-3098 REVISION No.: 00 - Jan 11/13 Page: 22 5

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# @A330 SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 31 F9241965000000 1 RAMP References Elec. Std. Practices Manual (ESPM) 20-53-00 Structural Repair Manual (SRM) 51-42-00 51-43-00 Fig. A-FBAAA Installation of the Ramp Assy and the Wiring Ramp between FR53.6 and FR53.8 Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 (a) Install the ramp assy and the wiring ramp between FR53.6 and FR53.8, LH side: Refer to Fig. A-FBAAA Sheet 03 and Fig. A-FBAAA Sheet 04

. In accordance with SRM 51-42-00 and SRM 51-43-00: NOTE: Before Installation of the mountings inspect the cables, refer to ESPM 20-53-00. 1 Install the ramp assy as shown on Fig. A-FBAAA Sheet 01, Fig. A-FBAAA Sheet 03 and Fig. A-FBAAA Sheet 04: 1 Ramp Assy F9241964500000 Item 29 attach with: 2 Screw NAS1801-3-7 Item 18 2 Washer NAS1149F0332P Item 3 2 Nut NSA5050-3 Item 8 2 Install the wiring ramp: 1 Ramp F9241965000000 Item 31 attach with the mounting as shown on Fig. A-FBAAA Sheet 03 and Fig. AFBAAA Sheet 04, Detail G: 1 Stud NSA5159-23 Item 23 1 Spacer NSA5527-03-03 Item 24 2 Washer NAS1149F0332P Item 3 1 Nut NSA5050-3 Item 8

DATE: Jan 11/13 SERVICE BULLETIN No.: A330-92-3098 REVISION No.: 00 - Jan 11/13 Page: 23 5

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# @A330 SERVICE BULLETIN
3 Attach the ramp assy and the wiring ramp with the mounting as shown on Fig. A-FBAAA Sheet 04, Detail H: 1 Stud NSA5159-19 Item 21 1 Bracket NSA935504-03 Item 12 3 Washer NAS1149F0332P Item 3 1 Spacer NSA5527-03-12 Item 22 2 Nut NSA5050-3 Item 8

(4) Subtask 923098-831-004-001 - Install the Ramp assy and the Wiring Ramp between FR53.6 and FR53.8, RH Side Work Zones and Access Panels Zone Access/Work location 844 Access Door 842 Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills AIRFRAME Material necessary to do the job Kit 923098A02R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 3 NAS1149F0332P 7 WASHER 8 NSA5050-3 5 NUT 12 NSA935504-03 1 BRACKET 18 NAS1801-3-7 2 SCREW 21 NSA5159-19 1 STUD 22 NSA5527-03-12 1 SPACER 23 NSA5159-23 1 STUD 24 NSA5527-03-03 1 SPACER 30 F9241964500100 1 RAMP 31 F9241965000000 1 RAMP References Elec. Std. Practices Manual (ESPM) 20-53-00 Structural Repair Manual (SRM) 51-42-00 51-43-00

DATE: Jan 11/13 SERVICE BULLETIN No.: A330-92-3098 REVISION No.: 00 - Jan 11/13 Page: 24 5

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# @A330 SERVICE BULLETIN
References Fig. A-FBAAA Installation of the Ramp Assy and the Wiring Ramp between FR53.6 and FR53.8 Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 (a) Install the ramp assy and the wiring ramp between FR53.6 and FR53.8, RH side: Refer to Fig. A-FBAAA Sheet 03 and Fig. A-FBAAA Sheet 04

. In accordance with SRM 51-42-00 and SRM 51-43-00: NOTE: Before Installation of the mountings inspect the cables, refer to ESPM 20-53-00. 1 Install the ramp assy as shown on Fig. A-FBAAA Sheet 01, Fig. A-FBAAA Sheet 03 and Fig. A-FBAAA Sheet 04: 1 Ramp Assy F9241964500100 Item 30 attach with: 2 Screw NAS1801-3-7 Item 18 2 Washer NAS1149F0332P Item 3 2 Nut NSA5050-3 Item 8 2 Install the wiring ramp: 1 Ramp F9241965000000 Item 31 attach with the mounting as shown on Fig. A-FBAAA Sheet 03 and Fig. AFBAAA Sheet 04, Detail G: 1 Stud NSA5159-23 Item 23 1 Spacer NSA5527-03-03 Item 24 2 Washer NAS1149F0332P Item 3 1 Nut NSA5050-3 Item 8 3 Attach the ramp assy and the wiring ramp with the mounting as shown on Fig. A-FBAAA Sheet 04, Detail H: 1 Stud NSA5159-19 Item 21 1 Bracket NSA935504-03 Item 12 3 Washer NAS1149F0332P Item 3
DATE: Jan 11/13 SERVICE BULLETIN No.: A330-92-3098 REVISION No.: 00 - Jan 11/13 Page: 25 5

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# @A330 SERVICE BULLETIN 1 Spacer NSA5527-03-12 Item 22 2 Nut NSA5050-3 Item 8

(5) Subtask 923098-831-007-001 - Modify the routing of the routes 1M and 2M between FR53.6 and FR53.8, LH Side Work Zones and Access Panels Zone Access/Work location 834 Access Door 832 Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills AIRFRAME Material necessary to do the job Kit 923098A01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 3 NAS1149F0332P 3 WASHER 18 NAS1801-3-7 1 SCREW 20 NSA5527-03-13 2 SPACER 25 NAS1801-3-20 2 SCREW 37 NSA5516-06ND 5 CLAMP 38 NSA5516-07ND 5 CLAMP 39 NSA5516-08ND 5 CLAMP NSA935401-03 10 TIE NSA935401-05 10 TIE NSA935401-08 10 TIE References Elec. Std. Practices Manual (ESPM) 20-53-00 Structural Repair Manual (SRM) 51-42-00 51-43-00 Fig. A-FBAAA Installation of the Ramp Assy and the Wiring Ramp between FR53.6 and FR53.8 Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 (a) Install the mountings on the ramp assy as shown on Fig. A-FBAAA Sheet 04 and Fig. A-FBAAA Sheet 05, Detail J: In accordance with SRM 51-42-00 and SRM 51-43-00: NOTE: Before Installation of the mountings inspect the cables, refer to ESPM 20-53-00. DATE: Jan 11/13 SERVICE BULLETIN No.: A330-92-3098 REVISION No.: 00 - Jan 11/13 Page: 26 5

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# @A330 SERVICE BULLETIN
2 Screw NAS1801-3-20 Item 25 2 Washer NAS1149F0332P Item 3 4 Clamp NSA5516-06ND Item 37 or 4 Clamp NSA5516-07ND Item 38 or 4 Clamp NSA5516-08ND Item 39 2 Spacer NSA5527-03-13 Item 20 (b) Install the mounting on the ramp assy as shown on Fig. A-FBAAA Sheet 04 and Fig. A-FBAAA Sheet 05, Detail K: In accordance with SRM 51-42-00 and SRM 51-43-00: NOTE: Before Installation of the mountings inspect the cables, refer to ESPM 20-53-00. 1 Screw NAS1801-3-7 Item 18 1 Washer NAS1149F0332P Item 3 1 Clamp NSA5516-06ND Item 37 or 1 Clamp NSA5516-07ND Item 38 or 1 Clamp NSA5516-08ND Item 39 (c) Attach the routes 1M and 2M: - in the clamps installed on the ramp assy. - on the wiring ramp with: 10 Tie-Cable NSA935401-03 10 Tie-Cable NSA935401-05 10 Tie-Cable NSA935401-08

DATE: Jan 11/13 SERVICE BULLETIN No.: A330-92-3098 REVISION No.: 00 - Jan 11/13 Page: 27 5

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# @A330 SERVICE BULLETIN (6) Subtask 923098-831-008-001 - Modify the routing of the routes 1M and 2M between FR53.6 and FR53.8, RH Side Work Zones and Access Panels Zone Access/Work location 844 Access Door 842 Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills AIRFRAME Material necessary to do the job Kit 923098A02R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 3 NAS1149F0332P 3 WASHER 18 NAS1801-3-7 1 SCREW 20 NSA5527-03-13 2 SPACER 25 NAS1801-3-20 2 SCREW 37 NSA5516-06ND 5 CLAMP 38 NSA5516-07ND 5 CLAMP 39 NSA5516-08ND 5 CLAMP NSA935401-03 10 TIE NSA935401-05 10 TIE NSA935401-08 10 TIE References Elec. Std. Practices Manual (ESPM) 20-53-00 Structural Repair Manual (SRM) 51-42-00 51-43-00 Fig. A-FBAAA Installation of the Ramp Assy and the Wiring Ramp between FR53.6 and FR53.8 Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 (a) Install the mountings on the ramp assy as shown on Fig. A-FBAAA Sheet 04 and Fig. A-FBAAA Sheet 05, Detail J: In accordance with SRM 51-42-00 and SRM 51-43-00: NOTE: Before Installation of the mountings inspect the cables, refer to ESPM 20-53-00 2 Screw NAS1801-3-20 Item 25 2 Washer NAS1149F0332P Item 3 DATE: Jan 11/13 SERVICE BULLETIN No.: A330-92-3098 REVISION No.: 00 - Jan 11/13 Page: 28 5

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# @A330 SERVICE BULLETIN 4 Clamp NSA5516-06ND Item 37 or 4 Clamp NSA5516-07ND Item 38 or 4 Clamp NSA5516-08ND Item 39 2 Spacer NSA5527-03-13 Item 20 (b) Install the mounting on the ramp assy as shown on Fig. A-FBAAA Sheet 04 and Fig. A-FBAAA Sheet 05, Detail K: In accordance with SRM 51-42-00 and SRM 51-43-00: NOTE: Before Installation of the mountings inspect the cables, refer to ESPM 20-53-00. 1 Screw NAS1801-3-7 Item 18 1 Washer NAS1149F0332P Item 3 1 Clamp NSA5516-06ND Item 37 or 1 Clamp NSA5516-07ND Item 38 or 1 Clamp NSA5516-08ND Item 39 (c) Attach the routes 1M and 2M: - in the clamps installed on the ramp assy. - on the wiring ramp with: 10 Tie-Cable NSA935401-03 10 Tie-Cable NSA935401-05 10 Tie-Cable NSA935401-08 **CONF 002 (1) Subtask 923098-831-001-002 - Remove the brackets of the Routes 1M and 2M between FR53.6 and FR53.8, LH Side Work Zones and Access Panels Zone Access/Work location 834 Access Door 832 DATE: Jan 11/13 SERVICE BULLETIN No.: A330-92-3098 REVISION No.: 00 - Jan 11/13 Page: 29 5

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# @A330 SERVICE BULLETIN Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills AIRFRAME References Structural Repair Manual (SRM) 51-42-00 Fig. A-FBAAB Installation of the Ramp Assy between FR53.6 and FR53.8 Sheet 01 Sheet 02 Sheet 03 Sheet 04 (a) Remove the brackets as shown on Fig. A-FBAAB Sheet 01 and Fig. A-FBAAB Sheet 02, Details D and E. In accordance with SRM 51-42-00: 1 Remove the mountings as shown on detail D on Fig. A-FBAAB Sheet 02: a If the existing mounting is as shown in case 1: <1> Remove: 2 Screw Item (14) Discard 2 Bracket Item (2) Discard 2 Spacer Item (1) Discard 2 Washer Item (3) Discard b If the existing mounting is as shown in case 2: <1> Remove: 2 Screw Item (14) Discard 2 Bracket Item (2) Discard 2 Spacer Item (1) Discard 2 Washer Item (3) Discard 2 Nut Item (8) Discard

DATE: Jan 11/13 SERVICE BULLETIN No.: A330-92-3098 REVISION No.: 00 - Jan 11/13 Page: 30 5

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# @A330 SERVICE BULLETIN
2 Remove the mounting as shown on detail E on Fig. A-FBAAB Sheet 02: a If the existing mounting is as shown in case 1: <1> Remove: 1 Screw Item (4) Discard 1 Bracket Item (12) Discard 1 Spacer Item (6) Discard 1 Bracket Item (5) Discard 1 Washer Item (3) Discard 1 Nut Item (17) Discard b If the existing mounting is as shown in case 2: <1> Remove: 1 Screw Item (4) Discard 1 Bracket Item (2) Discard 1 Spacer Item (1) Discard 1 Washer Item (3) Discard
c If the existing mounting is as shown in case 3: <1> Remove: 1 Screw Item (7) Discard 1 Bracket Item (2) Discard 1 Spacer Item (1) Discard 1 Washer Item (3) Discard 2 Nut Item (8) Discard NOTE: There is no need to disconnect the harness. NOTE: If a mounting is installed on the rib stiffening between FR53.7 and FR53.8, remove and discard it.

DATE: Jan 11/13 SERVICE BULLETIN No.: A330-92-3098 REVISION No.: 00 - Jan 11/13 Page: 31 5

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# @A330 SERVICE BULLETIN (2) Subtask 923098-831-002-002 - Remove the brackets of the Routes 1M and 2M between FR53.6 and FR53.8, RH Side Work Zones and Access Panels Zone Access/Work location 844 Access Door 842 Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills AIRFRAME References Structural Repair Manual (SRM) 51-42-00 Fig. A-FBAAB Installation of the Ramp Assy between FR53.6 and FR53.8 Sheet 01 Sheet 02 Sheet 03 Sheet 04 (a) Remove the brackets as shown on Fig. A-FBAAB Sheet 01 and Fig. A-FBAAB Sheet 02, Details D and E. In accordance with SRM 51-42-00: 1 Remove the mountings as shown on detail D on Fig. A-FBAAB Sheet 02: a If the existing mounting is as shown in case 1: <1> Remove: 2 Screw Item (14) Discard 2 Bracket Item (2) Discard 2 Spacer Item (1) Discard 2 Washer Item (3) Discard b If the existing mounting is as shown in case 2: <1> Remove: 2 Screw Item (14) Discard 2 Bracket Item (2) Discard 2 Spacer Item (1) Discard 2 Washer Item (3) Discard
DATE: Jan 11/13 SERVICE BULLETIN No.: A330-92-3098 REVISION No.: 00 - Jan 11/13 Page: 32 5

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# @A330 SERVICE BULLETIN 2 Nut Item (8) Discard 2 Remove the mounting as shown on detail E on Fig. A-FBAAB Sheet 02: a If the existing mounting is as shown in case 1: <1> Remove: 1 Screw Item (4) Discard 1 Bracket Item (12) Discard 1 Spacer Item (6) Discard 1 Bracket Item (5) Discard 1 Washer Item (3) Discard 1 Nut Item (17) Discard b If the existing mounting is as shown in case 2: <1> Remove: 1 Screw Item (4) Discard 1 Bracket Item (2) Discard 1 Spacer Item (1) Discard 1 Washer Item (3) Discard
c If the existing mounting is as shown in case 3: <1> Remove: 1 Screw Item (7) Discard 1 Bracket Item (2) Discard 1 Spacer Item (1) Discard 1 Washer Item (3) Discard 2 Nut Item (8) Discard NOTE: There is no need to disconnect the harness. NOTE: If a mounting is installed on the rib stiffening between FR53.7 and FR53.8, remove and discard it.
DATE: Jan 11/13 SERVICE BULLETIN No.: A330-92-3098 REVISION No.: 00 - Jan 11/13 Page: 33 5

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# @A330 SERVICE BULLETIN (3) Subtask 923098-831-005-001 - Install the Ramp assy between FR53.6 and FR53.8, LH Side Work Zones and Access Panels Zone Access/Work location 834 Access Door 832 Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills AIRFRAME Material necessary to do the job Kit 923098A03R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 3 NAS1149F0332P 3 WASHER 8 NSA5050-3 3 NUT 18 NAS1801-3-7 3 SCREW 29 F9241964500000 1 RAMP References Elec. Std. Practices Manual (ESPM) 20-53-00 Structural Repair Manual (SRM) 51-42-00 51-43-00 Fig. A-FBAAB Installation of the Ramp Assy between FR53.6 and FR53.8 Sheet 01 Sheet 02 Sheet 03 Sheet 04 (a) Install the ramp assy between FR53.6 and FR53.8, LH side: Refer to Fig. A-FBAAB Sheet 03 and Fig. A-FBAAB Sheet 04

. In accordance with SRM 51-42-00 and SRM 51-43-00: NOTE: Before Installation of the mountings inspect the cables, refer to ESPM 20-53-00. 1 Install the ramp assy: 1 Ramp Assy F9241964500000 Item 29 attach with: 3 Screw NAS1801-3-7 Item 18 3 Washer NAS1149F0332P Item 3
DATE: Jan 11/13 SERVICE BULLETIN No.: A330-92-3098 REVISION No.: 00 - Jan 11/13 Page: 34 5

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# @A330 SERVICE BULLETIN
3 Nut NSA5050-3 Item 8

(4) Subtask 923098-831-006-001 - Install the Ramp assy between FR53.6 and FR53.8, RH Side Work Zones and Access Panels Zone Access/Work location 844 Access Door 842 Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills AIRFRAME Material necessary to do the job Kit 923098A04R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 3 NAS1149F0332P 3 WASHER 8 NSA5050-3 3 NUT 18 NAS1801-3-7 3 SCREW 30 F9241964500100 1 RAMP References Elec. Std. Practices Manual (ESPM) 20-53-00 Structural Repair Manual (SRM) 51-42-00 51-43-00 Fig. A-FBAAB Installation of the Ramp Assy between FR53.6 and FR53.8 Sheet 01 Sheet 02 Sheet 03 Sheet 04 (a) Install the ramp assy between FR53.6 and FR53.8, RH side: Refer to Fig. A-FBAAB Sheet 03 and Fig. A-FBAAB Sheet 04

. In accordance with SRM 51-42-00 and SRM 51-43-00: NOTE: Before Installation of the mountings inspect the cables, refer to ESPM 20-53-00. 1 Install the ramp assy: 1 Ramp Assy F9241964500100 Item 30 attach with: 3 Screw NAS1801-3-7 Item 18
DATE: Jan 11/13 SERVICE BULLETIN No.: A330-92-3098 REVISION No.: 00 - Jan 11/13 Page: 35 5

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# @A330 SERVICE BULLETIN
3 Washer NAS1149F0332P Item 3 3 Nut NSA5050-3 Item 8 (b) Attach the routes 1M and 2M in the clamps installed on the ramp assy. (5) Subtask 923098-831-007-002 - Modify the routing of the routes 1M and 2M between FR53.6 and FR53.8, LH Side Work Zones and Access Panels Zone Access/Work location 834 Access Door 832 Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills AIRFRAME Material necessary to do the job Kit 923098A03R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 3 NAS1149F0332P 4 WASHER 10 ABS0355-02 1 BRACKET 14 NAS1801-3-22 3 SCREW 20 NSA5527-03-13 3 SPACER 28 NAS1801-08-7 1 SCREW 37 NSA5516-06ND 6 CLAMP 38 NSA5516-07ND 6 CLAMP 39 NSA5516-08ND 6 CLAMP NSA935401-03 5 TIE NSA935401-05 5 TIE NSA935401-08 5 TIE References Elec. Std. Practices Manual (ESPM) 20-53-00 Structural Repair Manual (SRM) 51-42-00 51-43-00 Fig. A-FBAAB Installation of the Ramp Assy between FR53.6 and FR53.8 Sheet 01 Sheet 02 Sheet 03 Sheet 04 (a) Install the bracket on the rib stiffening between FR53.7 and FR53.8 as shown on Fig. A-FBAAB Sheet 04, Detail G: In accordance with SRM 51-42-00 and SRM 51-43-00:
DATE: Jan 11/13 SERVICE BULLETIN No.: A330-92-3098 REVISION No.: 00 - Jan 11/13 Page: 36 5

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# @A330 SERVICE BULLETIN
NOTE: Before Installation of the mountings inspect the cables, refer to ESPM 20-53-00. 1 Bracket ABS0355-02 Item 10 attach with: 1 Screw NAS1801-08-7 Item 28 1 Washer NAS1149F0332P Item 3 (b) Install the mountings on the ramp assy as shown on Fig. A-FBAAB Sheet 04, Detail H: In accordance with SRM 51-42-00 and SRM 51-43-00: NOTE: Before Installation of the mountings inspect the cables, refer to ESPM 20-53-00. 3 Screw NAS1801-3-22 Item 14 3 Washer NAS1149F0332P Item 3 6 Clamp NSA5516-06ND Item 37 or 6 Clamp NSA5516-07ND Item 38 or 6 Clamp NSA5516-08ND Item 39 3 Spacer NSA5527-03-13 Item 20 (c) Attach the routes 1M and 2M: - in the clamps installed on the ramp assy. - on bracket as shown on Fig. A-FBAAB Sheet 04, Detail G with: 5 Tie-Cable NSA935401-03 5 Tie-Cable NSA935401-05 5 Tie-Cable NSA935401-08

(6) Subtask 923098-831-008-002 - Modify the routing of the routes 1M and 2M between FR53.6 and FR53.8, RH Side Work Zones and Access Panels Zone Access/Work location 844 Access Door 842
DATE: Jan 11/13 SERVICE BULLETIN No.: A330-92-3098 REVISION No.: 00 - Jan 11/13 Page: 37 5

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

# @A330 SERVICE BULLETIN Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills AIRFRAME Material necessary to do the job Kit 923098A04R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 3 NAS1149F0332P 4 WASHER 10 ABS0355-02 1 BRACKET 14 NAS1801-3-22 3 SCREW 20 NSA5527-03-13 3 SPACER 28 NAS1801-08-7 1 SCREW 37 NSA5516-06ND 6 CLAMP 38 NSA5516-07ND 6 CLAMP 39 NSA5516-08ND 6 CLAMP NSA935401-03 5 TIE NSA935401-05 5 TIE NSA935401-08 5 TIE References Elec. Std. Practices Manual (ESPM) 20-53-00 Structural Repair Manual (SRM) 51-42-00 51-43-00 Fig. A-FBAAB Installation of the Ramp Assy between FR53.6 and FR53.8 Sheet 01 Sheet 02 Sheet 03 Sheet 04 (a) Install the bracket on the rib stiffening between FR53.7 and FR53.8 as shown on Fig. A-FBAAB Sheet 04, Detail G: In accordance with SRM 51-42-00 and SRM 51-43-00: NOTE: Before Installation of the mountings inspect the cables, refer to ESPM 20-53-00. 1 Bracket ABS0355-02 Item 10 attach with: 1 Screw NAS1801-08-7 Item 28 1 Washer NAS1149F0332P Item 3

DATE: Jan 11/13 SERVICE BULLETIN No.: A330-92-3098 REVISION No.: 00 - Jan 11/13 Page: 38 5

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# @A330 SERVICE BULLETIN (b) Install the mountings on the ramp assy as shown on Fig. A-FBAAB Sheet 04, Detail H: In accordance with SRM 51-42-00 and SRM 51-43-00: NOTE: Before Installation of the mountings inspect the cables, refer to ESPM 20-53-00. 3 Screw NAS1801-3-22 Item 14 3 Washer NAS1149F0332P Item 3 6 Clamp NSA5516-06ND Item 37 or 6 Clamp NSA5516-07ND Item 38 or 6 Clamp NSA5516-08ND Item 39 3 Spacer NSA5527-03-13 Item 20 (c) Attach the routes 1M and 2M: - in the clamps installed on the ramp assy. - on bracket as shown on Fig. A-FBAAB Sheet 04, Detail G with: 5 Tie-Cable NSA935401-03 5 Tie-Cable NSA935401-05 5 Tie-Cable NSA935401-08 **CONF ALL D. TEST **CONF 001 None **CONF 002 None

DATE: Jan 11/13 SERVICE BULLETIN No.: A330-92-3098 REVISION No.: 00 - Jan 11/13 Page: 39 5

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# @A330 SERVICE BULLETIN
**CONF ALL E. CLOSE-UP **CONF 001 (1) Subtask 923098-410-001-001 - Install the Door Frame Linings between FR53.5 and FR53.8, LH Side Work Zones and Access Panels Zone Access/Work location 834 Access Door 832 Manpower Resources Skills NON SPECIFIC References Fig. A-FBBAA Removal/Installation of the Door Frame linings between FR53.5 and FR53.8 Sheet 01
(a) Install the door frame linings between FR53.5 and FR53.8, LH Side: Refer to Fig. A-FBBAA Sheet 01 1 Door Frame Lining Item (32) Retained at removal 1 Door Frame Lining Item (34) Retained at removal 1 Door Frame Lining Item (35) Retained at removal (2) Subtask 923098-410-002-001 - Install the Door Frame Linings between FR53.5 and FR53.8, RH Side Work Zones and Access Panels Zone Access/Work location 844 Access Door 842 Manpower Resources Skills NON SPECIFIC References Fig. A-FBBAA Removal/Installation of the Door Frame linings between FR53.5 and FR53.8 Sheet 01
(a) Install the door frame linings between FR53.5 and FR53.8, RH Side: Refer to Fig. A-FBBAA Sheet 01 DATE: Jan 11/13 SERVICE BULLETIN No.: A330-92-3098 REVISION No.: 00 - Jan 11/13 Page: 40 5

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# @A330 SERVICE BULLETIN 1 Door Frame Lining Item (33) Retained at removal 1 Door Frame Lining Item (34) Retained at removal 1 Door Frame Lining Item (36) Retained at removal (3) Subtask 923098-942-001-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 52-10-00-410-801 (a) Make sure that the work areas are clean and clear of tools and others items of equipment. (b) Close the passenger/crew door 832 and 842 (Refer to AMM Task 52-10-00-410-801). (c) Remove the access platform(s). (d) Restore the systems and the aircraft to normal operating condition. **CONF 002 (1) Subtask 923098-410-001-001 - Install the Door Frame Linings between FR53.5 and FR53.8, LH Side Work Zones and Access Panels Zone Access/Work location 834 Access Door 832 Manpower Resources Skills NON SPECIFIC References Fig. A-FBBAA Removal/Installation of the Door Frame linings between FR53.5 and FR53.8 Sheet 01
(a) Install the door frame linings between FR53.5 and FR53.8, LH Side: Refer to Fig. A-FBBAA Sheet 01 1 Door Frame Lining Item (32) Retained at removal

DATE: Jan 11/13 SERVICE BULLETIN No.: A330-92-3098 REVISION No.: 00 - Jan 11/13 Page: 41 5

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

# @A330 SERVICE BULLETIN 1 Door Frame Lining Item (34) Retained at removal 1 Door Frame Lining Item (35) Retained at removal (2) Subtask 923098-410-002-001 - Install the Door Frame Linings between FR53.5 and FR53.8, RH Side Work Zones and Access Panels Zone Access/Work location 844 Access Door 842 Manpower Resources Skills NON SPECIFIC References Fig. A-FBBAA Removal/Installation of the Door Frame linings between FR53.5 and FR53.8 Sheet 01
(a) Install the door frame linings between FR53.5 and FR53.8, RH Side: Refer to Fig. A-FBBAA Sheet 01 1 Door Frame Lining Item (33) Retained at removal 1 Door Frame Lining Item (34) Retained at removal 1 Door Frame Lining Item (36) Retained at removal (3) Subtask 923098-942-001-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 52-10-00-410-801 (a) Make sure that the work areas are clean and clear of tools and others items of equipment. (b) Close the passenger/crew door 832 and 842 (Refer to AMM Task 52-10-00-410-801). (c) Remove the access platform(s). (d) Restore the systems and the aircraft to normal operating condition.
DATE: Jan 11/13 SERVICE BULLETIN No.: A330-92-3098 REVISION No.: 00 - Jan 11/13 Page: 42 5

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

# @A330 SERVICE BULLETIN

**CONF 001

STGR12L

STGR14L 

### A

LH SIDE SHOWN RH SIDE SYMMETRICAL 

## B **FWD** 

## A

STGR17L Z844

Z834



## BEFORE
FR53.9 FR53.8 FR53.7 FR53.6

1M 2M

55LG (56LG) 2M

FR53.5 FR53.9 

### B **C**

**B C** 

**E D**  **D**

G_SB_923098_5_BAAA_01_01 Figure A-FBAAA - Sheet 01 Installation of the Ramp Assy and the Wiring Ramp between FR53.6 and FR53.8
DATE: Jan 11/13 SERVICE BULLETIN No.: A330-92-3098 REVISION No.: 00 - Jan 11/13 Page: 43 5

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

# @A330 SERVICE BULLETIN

**CONF 001 

## BEFORE
(7) (2) (1)

(3) (8)



## D

**E** 

## OR

CASE 1 CASE 2 1M 2M

(4)

(2) (6)
(3) (17) (7) (2) (1)

(3) (8) (4) (2) (1)

(3) 2M

1M 1M 2M 1M 2M

CASE 1 CASE 2 CASE 3 

## OR OR (4) (2) (1)

(3) 1M 2M

G_SB_923098_5_BAAA_02_00 Figure A-FBAAA - Sheet 02 Installation of the Ramp Assy and the Wiring Ramp between FR53.6 and FR53.8
DATE: Jan 11/13 SERVICE BULLETIN No.: A330-92-3098 REVISION No.: 00 - Jan 11/13 Page: 44 5

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

# @A330 SERVICE BULLETIN

**CONF 001

STGR12L

STGR14L

LH SIDE SHOWN RH SIDE SYMMETRICAL **FWD** 

## AFTER

FR53.9 FR53.6 31 29 30 LH RH



### F
**H** 2M

2M 55LG (56LG)

1M



## C FR53.8



### G

G_SB_923098_5_BAAA_03_01 Figure A-FBAAA - Sheet 03 Installation of the Ramp Assy and the Wiring Ramp between FR53.6 and FR53.8
DATE: Jan 11/13 SERVICE BULLETIN No.: A330-92-3098 REVISION No.: 00 - Jan 11/13 Page: 45 5

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

# @A330 SERVICE BULLETIN

**CONF 001

18 8 3 18 8 3

STGR14L

STGR17L 

## AFTER

**FWD**

**FWD** LH SIDE SHOWN RH SIDE SYMMETRICAL LH SIDE SHOWN RH SIDE SYMMETRICAL LH SIDE SHOWN RH SIDE SYMMETRICAL FR53.7

2M 

### J **J K** 

1M 2M



## F

**G H**  3 3 8 24 23

1M 2M

29 30 LH RH 31

1M 2M 29 30 12 31

8 8

22 21

3
3 LH RH

G_SB_923098_5_BAAA_04_05 Figure A-FBAAA - Sheet 04 Installation of the Ramp Assy and the Wiring Ramp between FR53.6 and FR53.8
DATE: Jan 11/13 SERVICE BULLETIN No.: A330-92-3098 REVISION No.: 00 - Jan 11/13 Page: 46 5

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

# @A330 SERVICE BULLETIN

**CONF 001

37 20 25 3

3 18 

## AFTER

1M 2M

2M 

## J

**K** OR38OR 39

37OR38OR 39

G_SB_923098_5_BAAA_05_01 Figure A-FBAAA - Sheet 05 Installation of the Ramp Assy and the Wiring Ramp between FR53.6 and FR53.8
DATE: Jan 11/13 SERVICE BULLETIN No.: A330-92-3098 REVISION No.: 00 - Jan 11/13 Page: 47 5

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

# @A330 SERVICE BULLETIN

**CONF 002

STGR12L

STGR14L 

### A

LH SIDE SHOWN RH SIDE SYMMETRICAL 

## B **FWD** Z844

Z834



## BEFORE FR53.9 FR53.8 FR53.7 FR53.6

1M 2M



### E 

## A FR53.5 FR53.9 

### B **C**

**B C** 

**D D** 

G_SB_923098_5_BAAB_01_01 Figure A-FBAAB - Sheet 01 Installation of the Ramp Assy between FR53.6 and FR53.8
DATE: Jan 11/13 SERVICE BULLETIN No.: A330-92-3098 REVISION No.: 00 - Jan 11/13 Page: 48 5

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

# @A330 SERVICE BULLETIN

**CONF 002 

## BEFORE
(14) (2) (1)

(3) (8)



## D

**E** 

## OR

CASE 1 CASE 2 1M 2M

(4)

(12) (6)
(3) (17) (7) (2) (1)

(3) (8) (4) (2) (1)

(3) 2M

1M 1M 2M 1M 2M

CASE 1 CASE 2 CASE 3 

## OR OR (14) (2) (1)

(3) 1M 2M

(5)

G_SB_923098_5_BAAB_02_01 Figure A-FBAAB - Sheet 02 Installation of the Ramp Assy between FR53.6 and FR53.8
DATE: Jan 11/13 SERVICE BULLETIN No.: A330-92-3098 REVISION No.: 00 - Jan 11/13 Page: 49 5

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

# @A330 SERVICE BULLETIN

**CONF 002

STGR12L

STGR14L

LH SIDE SHOWN RH SIDE SYMMETRICAL **FWD**

## AFTER

FR53.9 FR53.8 FR53.7 FR53.6

1M 2M

29 30 LH RH 

### F



## C

G_SB_923098_5_BAAB_03_00 Figure A-FBAAB - Sheet 03 Installation of the Ramp Assy between FR53.6 and FR53.8
DATE: Jan 11/13 SERVICE BULLETIN No.: A330-92-3098 REVISION No.: 00 - Jan 11/13 Page: 50 5

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

# @A330 SERVICE BULLETIN

**CONF 002

3 28 10 STGR14L

STGR17L

**FWD** 

## AFTER

FR53.7 18 8 3 LH SIDE SHOWN RH SIDE SYMMETRICAL

2M

1M 20

14 3 2M

1M 

## F

**G H**  **G H**  **H H** 

FR53.7 FR53.6 2M

1M

RH SIDE SHOWN LH SIDE SYMMETRICAL 37 OR 38 OR 39

37 OR 38 OR 39

G_SB_923098_5_BAAB_04_04 Figure A-FBAAB - Sheet 04 Installation of the Ramp Assy between FR53.6 and FR53.8
DATE: Jan 11/13 SERVICE BULLETIN No.: A330-92-3098 REVISION No.: 00 - Jan 11/13 Page: 51 5

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

# @A330 SERVICE BULLETIN

**CONF ALL

FR53.8 FR53.5



### B **C D** 

**A** Z844

Z834

(32) (33)

(35) (36) (34) LH RH

LH RH 

## A

**B C** 

**D** LH SIDE SHOWN RH SIDE SYMMETRICAL

G_SB_923098_5_BBAA_01_02 Figure A-FBBAA - Sheet 01 Removal/Installation of the Door Frame linings between FR53.5 and FR53.8
DATE: Jan 11/13 SERVICE BULLETIN No.: A330-92-3098 REVISION No.: 00 - Jan 11/13 Page: 52 5

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

# @A330 SERVICE BULLETIN Appendix 01 - Elapsed Time Assumption **CONF ALL (1) The following chart is only a proposal operators may determine that another way to do the work is more suitable for them.

DATE: Jan 11/13 SERVICE BULLETIN No.: A330-92-3098 REVISION No.: 00 - Jan 11/13 Page: 1 5

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

# @A330 SERVICE BULLETIN Appendix 01 - Elapsed Time Assumption

**CONF 001

**ELAPSED TIME ASSUMPTION SERVICE BULLETIN No. A330−92−3098**

GET ACCESS MH ET/S

TOTAL MANHOURS SB ELAPSED TIME 6.00 3.00 STEPS

1.00 0.50

0 REMOVE BRACKETS OF ROUTES 0.50 0.50

CLOSE−UP 1.00 0.50

MH ET/S: PER MANHOURS ELAPSED TIME PER STEP NUMBER OF PERSONS 01 02

THIS CHART IS ONLY A PROPOSAL. OPERATORS MAY DETERMINE THAT ANOTHER WAY TO DO THE WORK IS MORE SUITABLE FOR THEM. 01
02 **NOTES:** PER

2
1

2

: : SB ELAPSED TIME (HOURS) 1 2 3

IF A VSB IS INVOLVED, THE ASSOCIATED MANHOURS ARE NOT REFLECTED IN THIS GANTT CHART. 1M AND 2M, LH SIDE

INSTALL THE RAMP ASSY AND THE 1.00 1.00 1 WIRING RAMP, LH SIDE

MODIFY THE ROUTING OF THE ROUTES 0.50 0.50 1 1M AND 2M, LH SIDE REMOVE BRACKETS OF ROUTES 0.50 0.50 1 1M AND 2M, RH SIDE

INSTALL THE RAMP ASSY AND THE 1.00 1.00 1 WIRING RAMP, RH SIDE

MODIFY THE ROUTING OF THE ROUTES 0.50 0.50 1 1M AND 2M, RH SIDE

G_SB_923098_5_AAAA_01_00 Figure A-FAAAA - Sheet 01 Elapsed Time Assumption
DATE: Jan 11/13 SERVICE BULLETIN No.: A330-92-3098 REVISION No.: 00 - Jan 11/13 Page: 2 5

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

# @A330 SERVICE BULLETIN Appendix 01 - Elapsed Time Assumption

**CONF 002

**ELAPSED TIME ASSUMPTION SERVICE BULLETIN No. A330−92−3098**

GET ACCESS MH ET/S

TOTAL MANHOURS SB ELAPSED TIME 5.00 2.50 STEPS

1.00 0.50

0 REMOVE BRACKETS OF ROUTES 0.50 0.50

CLOSE−UP 1.00 0.50

MH ET/S: PER MANHOURS ELAPSED TIME PER STEP NUMBER OF PERSONS 01 02

THIS CHART IS ONLY A PROPOSAL. OPERATORS MAY DETERMINE THAT ANOTHER WAY TO DO THE WORK IS MORE SUITABLE FOR THEM. 01
02 **NOTES:** PER

2
1

2

: : SB ELAPSED TIME (HOURS) 1 2 3

IF A VSB IS INVOLVED, THE ASSOCIATED MANHOURS ARE NOT REFLECTED IN THIS GANTT CHART. 1M AND 2M, LH SIDE

INSTALL THE RAMP ASSY, LH SIDE 0.50 0.50 1

MODIFY THE ROUTING OF THE ROUTES 0.50 0.50 1 1M AND 2M, LH SIDE REMOVE BRACKETS OF ROUTES 0.50 0.50 1 1M AND 2M, RH SIDE

INSTALL THE RAMP ASSY, RH SIDE 0.50 0.50 1

MODIFY THE ROUTING OF THE ROUTES 0.50 0.50 1 1M AND 2M, RH SIDE

G_SB_923098_5_AAAB_01_00 Figure A-FAAAB - Sheet 01 Elapsed Time Assumption
DATE: Jan 11/13 SERVICE BULLETIN No.: A330-92-3098 REVISION No.: 00 - Jan 11/13 Page: 3 5

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# @A330 SERVICE BULLETIN REPORTING SHEET 

### TITLE: ELECTRIC AND ELECTRONIC COMMON INSTALLATION - GENERAL - RE-ROUTING OF HARNESSES AT DOOR 3 AREA, LH AND RH SIDE MODIFICATION No.: 201669S31758 202319S32230 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: Jan 11/13 SERVICE BULLETIN No.: A330-92-3098 REVISION No.: 00 - Jan 11/13 Page: 1 5

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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: Jan 11/13 SERVICE BULLETIN No.: A330-92-3098 REVISION No.: 00 - Jan 11/13 Page: 1 5

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