@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: 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

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

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

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

SUMMARY

**CONF 001

STGR12L

STGR14L

A

LH SIDE SHOWN

RH SIDE SYMMETRICAL

FWD B

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

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

SUMMARY

**CONF 001

STGR12L

STGR14L

LH SIDE SHOWN

RH SIDE SYMMETRICAL

FWD

AFTER

FR53.9 2M FR53.6

55LG 2M

(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

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

SUMMARY

**CONF 002

STGR12L

STGR14L

A

LH SIDE SHOWN

RH SIDE SYMMETRICAL

FWD B

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

FWD B

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 31 FR53.6

29

30

LH

RH

F

H

2M

55LG 2M

(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

31 12

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

OR 38 OR 39

37 OR 38 OR 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

FWD B

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

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

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

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