@A330

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 71

TITLE: POWER PLANT - AIR INTAKE COWL - INSPECTION ON T700 OF THE

AIR INTAKE COWL.

MODIFICATION No.: None

This page transmits Revision No.01 of Service Bulletin No.A330-71-3024

ADDITIONAL WORK

**CONF ALL

REASON

Revision 01 issued to take into account the case when affected inlet cowl is replaced by a new one that

has accumulated more than 5,000FC/20,000FH and to update the operator list.

CHANGES

SUMMARY

REASON/DESCRIPTION/OPERATIONAL

CONSEQUENCES

REASON UPDATED R

EFFECTIVITY OPERATOR LIST UPDATED R

Fig. A-FSAAA

Fig. A-FSAAA Sheet 01 SHEET UPDATED R

PLANNING INFORMATION

EFFECTIVITY EFFECTIVITY RELATED INFORMATION

UPDATED

R

REASON

History HISTORY UPDATED R

COMPLIANCE

Accomplishment Timescale ACCOMPLISHMENT TIMESCALE UPDATED R

ACCOMPLISHMENT INSTRUCTIONS

TASK 713024- 832-801-001-Inspection

Subtask 713024-220-001-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

R

Subtask 713024-220-002-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

R

DATE: May 11/11 SERVICE BULLETIN No.: A330-71-3024

REVISION No.: 01 - Sep 27/11 Page: 1

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

TASK 713024- 833-801-001-Repair

Subtask 713024-833-003-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

FIGURE REFERENCE UPDATED

REFERENCES UPDATED

R

Subtask 713024-833-004-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

FIGURE REFERENCE UPDATED

REFERENCES UPDATED

R

Fig. A-FBAAA

Fig. A-FBAAA Sheet 01 SHEET UPDATED R

Fig. A-FBBAA Flow Chart updated R

Fig. A-FBBAA Sheet 01 SHEET UPDATED R

Appendix 01 : Inspection Report

Fig. A-FAAAA

Fig. A-FAAAA Sheet 01 SHEET UPDATED R

Appendix 02 : Elapsed Time Assumptions of the Inspection

Fig. A-FABAA

Fig. A-FABAA Sheet 01 SHEET UPDATED R

FILLING INSTRUCTIONS

This Service Bulletin has been generated electronically and is reissued as a complete document.

Replace the complete document.

Put this Revision Transmittal Sheet in front of the Service Bulletin.

HISTORY OF PREVIOUS REVISIONS

No previous revision

REVISION SEQUENCE

ORIGINAL: May 11/11

REVISION No. : 01 - Sep 27/11

DATE: May 11/11 SERVICE BULLETIN No.: A330-71-3024

REVISION No.: 01 - Sep 27/11 Page: 2

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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: 71

TITLE: POWER PLANT - AIR INTAKE COWL - INSPECTION ON T700 OF THE

AIR INTAKE COWL.

**CONF ALL

MODIFICATIONS

None

REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES

There have been two reported events where extensive damage was found on Engine Nose Cowls most

probably induced by the collapse of one inlet acoustic panel due to disbond.

Inspections performed demonstrated that :

- There is a disbonding in-service issue on the engine air intake cowl acoustic panels.

- Several panels can be affected at any position within an intake and both intakes can be affected.

- Damage can extend beyond structural Allowable Damage Limits (ADL) or current Repairable

Damage Limits (RDL).

This Service Bulletin is published to advise operators of A330 aircraft equipped with Trent 700 engines

of the issue of ROLLS-ROYCE Service Bulletin No. RB.211-71-AG419.

This Service Bulletin requires inspecting and/or repairing air intake cowl by ROLLS-ROYCE Service

Bulletin No. RB.211-71-AG419.

The aim of this inspection is to introduce a repetitive inspection (tap test) of the 3 inner acoustic panels

of the T700 engine air intake cowl.

Accomplishment of this Service Bulletin will ensure the structural integrity of the inner acoustic panels.

GENERAL EVALUATION

EVALUATION TABLE

COMPLIANCE MANDATORY (1) CANCELS INSPECTION SB NO

DATE: May 11/11 SERVICE BULLETIN No.: A330-71-3024

REVISION No.: 01 - Sep 27/11 Page: 1

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SERVICE BULLETIN

SUMMARY

EVALUATION TABLE

POTENTIAL AD YES A/C OPERATION AFFECTED NO

RELIABILITY AFFECTED NO PAX COMFORT AFFECTED NO

COST SAVING NO ETOPS AFFECTED NO

STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED YES

NOTE (1): Service Bulletin must be accomplished.

MATERIAL PRICE INFORMATION

No Material

EFFECTIVITY

This Service Bulletin is applicable to this (these) operator(s) :

68W 78V 97X ACA AEA AFL ALK AVA BEC BMA CAL CCA CES

CHH CPA CRK CRL CSC CSN CYP DLH EDW ETD GFA GIA HAL

HDA HFY I2L IWD IYE JAI MEA MON MSR OBS OHY OMA SAA

SAS SIA SVA SWR TCX THA THY TSC UAE UAF USA VIR VKG

VOZ XAX XLF YZR

CONCURRENT REQUIREMENTS

None

REFERENCES / REPERCUSSIONS

TFU None

OEB None

AOT None

SIL None

LINE MAINTENANCE AFFECTED No

LIFE LIMIT None

OTHER None

NATURE OF THE WORK

AIRCRAFT YES

EQUIPMENT NO

HARD NO

SOFT NO

OBRM NO

MANPOWER

Task 713024-832-801-001: Inspection

TOTAL MANHOURS 20.00

ELAPSED TIME (HOURS) 11.00

Task 713024-833-801-001: Repair

TOTAL MANHOURS 2.00

DATE: May 11/11 SERVICE BULLETIN No.: A330-71-3024

REVISION No.: 01 - Sep 27/11 Page: 2

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@A330

SERVICE BULLETIN

SUMMARY

Task 713024-833-801-001: Repair

ELAPSED TIME (HOURS) 1.00

Additional manhours related to Vendor SB; refer to:

Repair or Replace the Affected Air Intake Cowl of the LH

Engine.

ROLLS-ROYCE Service Bulletin No.

RB.211-71-AG419

Repair or Replace the Affected Air Intake Cowl of the RH

Engine.

ROLLS-ROYCE Service Bulletin No.

RB.211-71-AG419

APPENDICES

Appendix 01 : Inspection Report

Appendix 02 : Elapsed Time Assumptions of the Inspection

Appendix 03 : Elapsed Time Assumptions of the Repair

DATE: May 11/11 SERVICE BULLETIN No.: A330-71-3024

REVISION No.: 01 - Sep 27/11 Page: 3

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SERVICE BULLETIN

SUMMARY

**CONF ALL

Z410

Z420

A

A B

ACOUSTIC LINER SEGMENTS (3 OFF)

0 DEGREES

RADIAL

RADIAL 63 DEGREES

EEC INLET

RADIAL 80.5 DEGREES

EEC OUTLET

135 DEGREES

RADIAL

225 DEGREES

RADIAL

RADIAL 345 DEGREES

PROBE P2T2

PANEL 3

PANEL 2

PANEL 1

NOTE:

INNER ACOUSTIC PANELS TO BE INSPECTED

B

A

G_SB_713024_5_SAAA_01_01

Figure A-FSAAA - Sheet 01

DATE: May 11/11 SERVICE BULLETIN No.: A330-71-3024

REVISION No.: 01 - Sep 27/11 Page: 4

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@A330

SERVICE BULLETIN

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 71

TITLE: POWER PLANT - AIR INTAKE COWL - INSPECTION ON T700 OF THE

AIR INTAKE COWL.

MODIFICATION No.: None

This document contains AIRBUS PROPRIETARY INFORMATION and shall at all times remain the

property of AIRBUS; no intellectual property right or licence is granted by AIRBUS in connection with

any information contained in it. It is delivered on the express condition that said document and the

information contained in it shall be treated as confidential, shall not be used for any purpose other than

that for which it is hereby delivered. It shall not be disclosed in whole or in part to third parties and shall

not be duplicated in any manner (except for the purposes of performing the tasks described hereunder

and provided that any recipient of such document shall comply with the conditions herein), without

AIRBUS prior written consent.

1. PLANNING INFORMATION

**CONF ALL

A. EFFECTIVITY

(1) Models

330-243 330-243F 330-341 330-342 330-343

(2) Effectivity by MSN

0012 0017 0071 0083 0098-0099 0102 0106 0109 0111 0113 0118 0121 0132 0138

0140 0144 0148 0153 0155 0165 0177 0234 0244 0248 0250-0251 0254 0261

0265-0266 0271 0276-0277 0279 0281 0283-0287 0293 0295 0301 0303 0306 0309

0311 0313-0314 0316 0320 0326 0328 0334 0340 0344-0345 0348-0349 0356-0357

0365 0369 0372 0382 0384 0386 0389 0392-0393 0396 0398 0400-0401 0404-0405

0407-0409 0412 0418-0421 0423 0427 0437 0439 0451-0452 0455-0456 0461-0462

0479-0480 0491 0494 0496-0497 0501 0505 0509 0512 0515 0518 0525-0527 0529

0532 0536 0539 0548 0551 0565 0568 0570 0576 0579 0581 0597 0600 0610 0625

0627 0629 0632 0635-0636 0642 0645 0648-0649 0652 0654 0656 0658 0662 0664

0666 0669-0670 0673 0679 0683 0687-0688 0692 0696 0701 0709 0713 0716-0717

0720 0724 0726 0728-0730 0732 0735 0737 0741 0750-0751 0756 0759 0773

0776-0777 0780-0782 0785-0786 0788 0791 0795 0797 0807 0809-0810 0815 0818

0821 0824 0830 0832-0833 0836 0839-0840 0850-0852 0854-0855 0860 0862-0863

0866-0868 0873 0875 0879 0881 0884 0889-0890 0895-0896 0903 0905-0906

0908-0909 0913 0915-0916 0919 0922 0926 0928 0930 0935-0937 0941-0942 0944

DATE: May 11/11 SERVICE BULLETIN No.: A330-71-3024

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SERVICE BULLETIN

0948 0952 0954 0957-0959 0963-0964 0966-0967 0971 0973-0975 0978 0982-0984

0986 0988-0992 0995 0997-0998 1000 1003-1004 1006 1008-1012 1014-1016 1018

1020 1022 1026 1028-1029 1032-1033 1035 1037-1038 1041 1044-1049 1051-1053

1058 1060 1062-1063 1065-1066 1069-1077 1080-1082 1084-1087 1089-1090

1092-1093 1095 1097-1101 1103-1105 1107-1108 1110 1114-1115 1120 1124

1126-1127 1130-1132 1137-1138 1141 1143 1145-1147 1149-1150 1153 1156-1157

1159-1160 1163 1165 1167-1168 1170-1172 1175 1178 1181 1184 1186-1193

1195-1196 1199 1201 1204-1206 1208 1210 1212 1214-1217 1222-1224 1226-1228

1230-1232 1236-1241 1245-1250 1255 1259-1264 1267 1269-1271 1275-1277

1279-1280 1282 1284-1286 1288-1291 1293 1295-1296 1298-1299 1303

(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

68W 1115

78V 1033 1046 1248 1275

97X 1053

ACA 0277 0279 0284 0344 0400 0408 0412 0419

AEA 0461 0597

AFL 0963 0973 1014 1045 1047 1058 1065 1072 1077 1103 1232 1247

1270 1284 1299

ALK 0303 0306 0311 0313 0404

AVA 0948 0967 1009 1016 1073 1208 1224 1279

BEC 0863

BMA 0398 0401

CAL 1206 1215

CCA 0750 0756 0759 0780 0785 0797 0810 0815 0839 0860 0867 0873

0884 0890 0903 0909 0930 0941 0944 0957 1087 1110 1130 1187

1199 1216 1237 1260 1282

CES 0713 0720 0728 0732 0735 0773 0777 0781 0782 0791 0821 0830

0836 0851 0862 0866 0916 0928 0936 0942 1262 1267 1280 1291

1303

CHH 0875 0881 0906 0919 0982 1159 1168 1178 1190

CPA 0012 0017 0071 0102 0113 0118 0121 0155 0244 0386 0389 0393

0418 0420 0421 0423 0439 0539 0548 0565 0669 0673 0679 0776

0850 0855 0895 0915 0959 1163 1196 1222 1239 1285

CRK 1051 1062 1255 1277 1286

CRL 0285 0320

CSC 1082 1138 1241

CSN 0649 0652 0656 0664 0818 0840 0879 0889 0908 0935 0937 0954

0958 0964

CYP 0505 0526

DLH 0570 0576 0579 0629 0636 0642 0645 0648 0687 0701 0896 0905

0913 0922 0989

EDW 1193

DATE: May 11/11 SERVICE BULLETIN No.: A330-71-3024

REVISION No.: 01 - Sep 27/11 Page: 2

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SERVICE BULLETIN

OPERATOR MSN

ETD 0658 0688 0717 0724 0729 0730 0737 0788 0809 0824 0832 0852

0854 0868 0975 0991 1032 1070 1071 1081 1167 1205 1226 1245

GFA 0276 0281 0286 0287 0334 0340 0527 0529 0532 0992

GIA 0138 0140 0144 0148 0153 0165 0988 1020 1028 1052 1184 1214

1261 1288

HAL 1104 1114 1171 1217 1259 1295

HDA 0083 0099 0106 0109 0234 0405 0479 0512 0581 0654 0662 0692

0716 0741 0786

HFY 1008

I2L 0407 0551

IWD 0670 1097

IYE 0625 0627 0632

JAI 0751 0807

MEA 0926 0984 0995 0998

MON 0261 0265

MSR 0600 0610 0666 0683 0696 0709 0726 1143 1230 1238 1246 1264

OBS 0833

OHY 0098

OMA 1038 1044 1049 1063 1093 1120 1227

SAA 1191 1210 1223 1236 1249 1271

SAS 0496 0497 0515 0568

SIA 0978 0983 0986 0997 1006 1010 1012 1015 1085 1098 1099 1105

1107 1124 1132 1146 1149 1156 1157

SVA 1108 1127 1137 1141 1147 1153 1189 1192

SWR 1000 1018 1026 1029 1084 1089 1101 1145 1181 1188 1276 1290

TCX 0254 0266 0301 0427 0456 0795

THA 0990 1003 1035 1037 1060 1074 1086 1090 1263 1269 1289

THY 1004 1092 1150 1160 1170 1172 1204 1212 1228 1240 1298

TSC 0111 0132 0177 0250 0271 0369 0480 0966 0971

UAE 0248 0251 0283 0293 0295 0314 0316 0326 0328 0345 0348 0382

0384 0392 0396 0409 0437 0451 0452 0455 0462 0491 0494 0509

0518 0525 0536

UAF 1080 1186 1250

USA 1011 1022 1041 1069 1076 1095 1100

VIR 1195 1201 1231 1296

VKG 0309 0349 0356 0357

VOZ 0365 0372 1293

XAX 0952 0974 1048 1066 1075 1126 1131 1165

XLF 0501 0635

YZR 1175

DATE: May 11/11 SERVICE BULLETIN No.: A330-71-3024

REVISION No.: 01 - Sep 27/11 Page: 3

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SERVICE BULLETIN

(4) Configuration by MSN

MSN CONFIGURATION

0012 0017 0071 0083 0098 0099 0102 0106 0109 0111 0113

0118 0121 0132 0138 0140 0144 0148 0153 0155 0165 0177

0234 0244 0248 0250 0251 0254 0261 0265 0266 0271 0276

0277 0279 0281 0283 0284 0285 0286 0287 0293 0295 0301

0303 0306 0309 0311 0313 0314 0316 0320 0326 0328 0334

0340 0344 0345 0348 0349 0356 0357 0365 0369 0372 0382

0384 0386 0389 0392 0393 0396 0398 0400 0401 0404 0405

0407 0408 0409 0412 0418 0419 0420 0421 0423 0427 0437

0439 0451 0452 0455 0456 0461 0462 0479 0480 0491 0494

0496 0497 0501 0505 0509 0512 0515 0518 0525 0526 0527

0529 0532 0536 0539 0548 0551 0565 0568 0570 0576 0579

0581 0597 0600 0610 0625 0627 0629 0632 0635 0636 0642

0645 0648 0649 0652 0654 0656 0658 0662 0664 0666 0669

0670 0673 0679 0683 0687 0688 0692 0696 0701 0709 0713

0716 0717 0720 0724 0726 0728 0729 0730 0732 0735 0737

0741 0750 0751 0756 0759 0773 0776 0777 0780 0781 0782

0785 0786 0788 0791 0795 0797 0807 0809 0810 0815 0818

0821 0824 0830 0832 0833 0836 0839 0840 0850 0851 0852

0854 0855 0860 0862 0863 0866 0867 0868 0873 0875 0879

0881 0884 0889 0890 0895 0896 0903 0905 0906 0908 0909

0913 0915 0916 0919 0922 0926 0928 0930 0935 0936 0937

0941 0942 0944 0948 0952 0954 0957 0958 0959 0963 0964

0966 0967 0971 0973 0974 0975 0978 0982 0983 0984 0986

0988 0989 0990 0991 0992 0995 0997 0998 1000 1003 1004

1006 1008 1009 1010 1011 1012 1014 1015 1016 1018 1020

1022 1026 1028 1029 1032 1033 1035 1037 1038 1041 1044

1045 1046 1047 1048 1049 1051 1052 1053 1058 1060 1062

1063 1065 1066 1069 1070 1071 1072 1073 1074 1075 1076

1077 1080 1081 1082 1084 1085 1086 1087 1089 1090 1092

1093 1095 1097 1098 1099 1100 1101 1103 1104 1105 1107

1108 1110 1114 1115 1120 1124 1126 1127 1130 1131 1132

1137 1138 1141 1143 1145 1146 1147 1149 1150 1153 1156

1157 1159 1160 1163 1165 1167 1168 1170 1171 1172 1175

1178 1181 1184 1186 1187 1188 1189 1190 1191 1192 1193

1195 1196 1199 1201 1204 1205 1206 1208 1210 1212 1214

1215 1216 1217 1222 1223 1224 1226 1227 1228 1230 1231

1232 1236 1237 1238 1239 1240 1241 1245 1246 1247 1248

1249 1250 1255 1259 1260 1261 1262 1263 1264 1267 1269

1270 1271 1275 1276 1277 1279 1280 1282 1284 1285 1286

1288 1289 1290 1291 1293 1295 1296 1298 1299 1303

001

(5) Configuration definition

**CONF 001

Config. 001 is valid for all aircraft given in the effectivity of this Service Bulletin as a

standard configuration.

(6) Material Effectivity

None

DATE: May 11/11 SERVICE BULLETIN No.: A330-71-3024

REVISION No.: 01 - Sep 27/11 Page: 4

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SERVICE BULLETIN

B. CONCURRENT REQUIREMENTS

None

C. REASON

(1) History

There have been two reported events where extensive damage was found on Engine

Nose Cowls most probably induced by the collapse of one inlet acoustic panel due to

disbond.

Inspections performed demonstrated that :

- There is a disbonding in-service issue on the engine air intake cowl acoustic panels.

- Several panels can be affected at any position within an intake and both intakes can

be affected.

- Damage can extend beyond structural Allowable Damage Limits (ADL) or current

Repairable Damage Limits (RDL).

(2) Objective/Action

This Service Bulletin is published to advise operators of A330 aircraft equipped with

Trent 700 engines of the issue of ROLLS-ROYCE Service Bulletin No. RB.211-71-

AG419.

This Service Bulletin requires inspecting and/or repairing air intake cowl by ROLLSROYCE Service Bulletin No. RB.211-71-AG419.

The aim of this inspection is to introduce a repetitive inspection (tap test) of the 3 inner

acoustic panels of the T700 engine air intake cowl.

(3) Advantages

Accomplishment of this Service Bulletin will ensure the structural integrity of the inner

acoustic panels.

(4) Operational/Maintenance Consequences

None

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

Task 713024-832-801-001: Inspection

(1) Do a Detailed Inspection of the Acoustic Panels on the LH Engine Air Intake Cowl.

(2) Do a Detailed Inspection of the Acoustic Panels on the RH Engine Air Intake Cowl.

DATE: May 11/11 SERVICE BULLETIN No.: A330-71-3024

REVISION No.: 01 - Sep 27/11 Page: 5

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SERVICE BULLETIN

Task 713024-833-801-001: Repair

(1) Repair or Replace the Affected Air Intake Cowl of the LH Engine.

(2) Repair or Replace the Affected Air Intake Cowl of the RH Engine.

E. COMPLIANCE

(1) Classification

MANDATORY: Service Bulletin must be accomplished.

(2) Accomplishment Timescale

Accomplishment of this Service Bulletin is required at thresholds and/or intervals given in

the table below :

CONDITION ACTION COMPLIANCE TIME

THRESHOLD GRACE PERIOD

REPETITIVE

INTERVAL NOT

TO EXCEED

LH side engine Inspect in

accordance with

SUBTASK

713024-220-001

001 Do a Detailed

Inspection of the

Acoustic Panels on

the LH Engine Air

Intake Cowl.

Within 24 months

after engine air

intake has

accumulated 5,000

FC or 20,000 FH

(whichever occurs

first since first

installation on an

aeroplane)

24 months 24 months. Less in

case of finding

(refer to ROLLSROYCE Service

Bulletin No.

RB.211-71-AG419)

RH side engine Inspect in

accordance with

SUBTASK

713024-220-002

001 Do a Detailed

Inspection of the

Acoustic Panels on

the RH Engine Air

Intake Cowl.

Within 24 months

after engine air

intake has

accumulated 5,000

FC or 20,000 FH

(whichever occurs

first since first

installation on an

aeroplane)

24 months 24 months. Less in

case of finding

(refer to ROLLSROYCE Service

Bulletin No.

RB.211-71-AG419)

Damage found

more than ADL

Replace the

affected air intake

cowl

Before next flight See NOTE (1)

Damage lower

than ADL

Refer to ROLLSROYCE Service

Bulletin No.

RB.211-71-AG419

Refer to ROLLS-ROYCE Service

Bulletin No. RB.211-71-AG419

Refer to ROLLSROYCE Service

Bulletin No.

RB.211-71-AG419

Table 1 : Special detailed Inspection of Acoustic Panels on Engine Air Intake Cowls.

NOTE (1): In case of Air Intake cowl replacement refer to figure A-FBBAA flow chart

for instruction.

NOTE: When the history on an Air Intake is partial or unknow, please refer to

DATE: May 11/11 SERVICE BULLETIN No.: A330-71-3024

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@A330

SERVICE BULLETIN

ROLLS-ROYCE Service Bulletin No. RB.211-71-AG419 to define the life

of the component.

Accomplishment of this Service Bulletin is expected to be rendered mandatory by the

issue of an Airworthiness Directive (AD) published by the European Aviation Safety

Agency (EASA). It is anticipated that the AD will confirm the (thresholds and/or intervals

and/or date) given above but reference should be made to the AD for confirmation of the

mandated accomplishment timescale.

F. APPROVAL

The technical content of this document is approved under the authority of Design

Organisation Approval No. EASA.21J.031.

If an aircraft listed in the effectivity has a modification or repair embodied that is not of

AIRBUS origin, and which affects the content of this Service Bulletin, the operator is

responsible for obtaining approval by its airworthiness authority for any adaptation necessary

before incorporation of the Service Bulletin.

G. MANPOWER

The manpower estimates given in this Service Bulletin are based on the direct labor cost to

do the work. These estimates assume that the work will be done by experienced personnel,

and may need to be revised upwards to suit operator’s circumstances. The estimates do not

include the time to prepare, plan or inspect the work. Manufacture and procurement of parts

and tools, drying times for paints, sealants, etc., and general administration work are also not

included.

Task 713024-832-801-001: Inspection

Get Access 1.00

On Aircraft

Do a Detailed Inspection of the Acoustic Panels on the

LH Engine Air Intake Cowl.

9.00

Do a Detailed Inspection of the Acoustic Panels on the

RH Engine Air Intake Cowl.

9.00

Close-Up 1.00

TOTAL MANHOURS 20.00

ELAPSED TIME (HOURS) 11.00

NOTE: For detail concerning the elapsed time assumptions of the inspection, Refer to

Appendix 02 : Elapsed Time Assumptions of the Inspection .

Task 713024-833-801-001: Repair

Get Access 1.00

Close-Up 1.00

TOTAL MANHOURS 2.00

ELAPSED TIME (HOURS) 1.00

Additional manhours related to Vendor SB; refer to:

DATE: May 11/11 SERVICE BULLETIN No.: A330-71-3024

REVISION No.: 01 - Sep 27/11 Page: 7

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SERVICE BULLETIN

Task 713024-833-801-001: Repair

Repair or Replace the Affected Air Intake Cowl of the

LH Engine.

ROLLS-ROYCE Service Bulletin No.

RB.211-71-AG419

Repair or Replace the Affected Air Intake Cowl of the

RH Engine.

ROLLS-ROYCE Service Bulletin No.

RB.211-71-AG419

NOTE: For detail concerning the elapsed time assumptions of the repair, Refer to

Appendix 03 : Elapsed Time Assumptions of the Repair .

H. WEIGHT AND BALANCE

Not Changed

I. ELECTRICAL LOAD DATA

Not Changed

J. REFERENCES

Aircraft Maintenance Manual (AMM) 12-34-24

Elec. Std. Practices Manual (ESPM) 20-55-00

Vendor Service Bulletin (VSB) ROLLS-ROYCE Service Bulletin

No. RB.211-71-AG419

K. PUBLICATION AFFECTED

None

L. INTERCHANGEABILITY/MIXABILITY

Not Applicable

M. SPARES

None

DATE: May 11/11 SERVICE BULLETIN No.: A330-71-3024

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SERVICE BULLETIN

2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

(1) Procurement Addresses

Modification of removed equipment should be negotiated directly with ROLLS-ROYCE as

per instructions given in ROLLS-ROYCE Service Bulletin No. RB.211-71-AG419.

(2) Price and Availability

Refer to the ROLLS-ROYCE Service Bulletin No. RB.211-71-AG419 for the equipment

modification sales terms.

B. INDUSTRY SUPPORT INFORMATION

Refer to the ROLLS-ROYCE Service Bulletin No. RB.211-71-AG419 for the industry support

terms.

C. LIST OF COMPONENTS

No Kit

D. LIST OF MATERIALS - OPERATOR SUPPLIED

None

E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

None

F. TOOLING

(1) Tooling - Price and Availability

To accomplish this Service Bulletin it is necessary to use the tools listed in ROLLSROYCE Service Bulletin No. RB.211-71-AG419.

(2) Tools

None

(3) Special Tools

None

DATE: May 11/11 SERVICE BULLETIN No.: A330-71-3024

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SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS

Task 713024-832-801-001 - Inspection

WARNING: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND THE CAUTIONS

INCLUDED IN THE REFERENCED PROCEDURES.

CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP

ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY

AND MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENANCE

WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING,

COMPONENTS AND THE WORK AREA AS CLEAN AS POSSIBLE. TO DO

THIS :

- PUT PROTECTION, SUCH AS PLASTIC SHEETING, CLOTHS, ETC. AS

NECESSARY ON WIRING AND COMPONENTS,

- REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND

OTHER CONTAMINATION.

THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION

AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION.

IF THERE IS CONTAMINATION, REFER TO ESPM 20-55-00.

Task Associated Data

Zone

410 420

Manpower

TOTAL MANHOURS 20.00

ELAPSED TIME (HOURS) 11.00

A. GENERAL

(1) Subtask 713024-839-001-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

Write in the applicable aircraft records that you have done all the work given in this

Service Bulletin.

B. PREPARATION

(1) Subtask 713024-941-001-001 - Job Set-up for LH Engine

Work Zones and Access Panels

Zone Access/Work location

410

DATE: May 11/11 SERVICE BULLETIN No.: A330-71-3024

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SERVICE BULLETIN

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802

(a) Make sure that the aircraft is electrically grounded (Refer to AMM Task

12-34-24-860-802).

(b) Put access platform(s) in position

(c) Open, safety and tag these circuit breakers :

PANEL DESIGNATION FIN LOCATION SEE

NOTES

722VU FADEC B ENG 1 13KS1 46 K (1)

722VU FADEC B ENG 1 13KS1 44 D (1)

742VU FADEC A ENG 1 12KS1 74 N (1)

742VU FADEC A ENG 1 12KS1 73 Q (1)

NOTE (1): The location of the CB depends on the A/C configuration.

(2) Subtask 713024-941-003-001 - Job Set-up for RH Engine

Work Zones and Access Panels

Zone Access/Work location

420

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802

(a) Make sure that the aircraft is electrically grounded (Refer to AMM Task

12-34-24-860-802).

(b) Put access platform(s) in position

(c) Open, safety and tag these circuit breakers :

PANEL DESIGNATION FIN LOCATION SEE

NOTES

722VU FADEC B ENG 2 13KS2 43 D (1)

722VU FADEC B ENG 2 13KS2 49 K (1)

742VU FADEC A ENG 2 12KS2 73 Q (1)

742VU FADEC A ENG 2 12KS2 74 Q (1)

NOTE (1): The location of the CB depends on the A/C configuration.

DATE: May 11/11 SERVICE BULLETIN No.: A330-71-3024

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C. PROCEDURE

(1) Subtask 713024-220-001-001 - Do a Detailed Inspection of the Acoustic Panels on

the LH Engine Air Intake Cowl.

Work Zones and Access Panels

Zone Access/Work location

410

Manpower Resources

Manhours 9.00

Minimum number of person 1

Subtask elapsed time 9.00

Skills NON SPECIFIC

References

Vendor Service Bulletin (VSB) ROLLS-ROYCE RB.211-71-AG419

Fig. A-FBAAA

Area to be Inspected

Sheet 01

Fig. A-FBBAA

Flow Chart

Sheet 01

(a) For the inspection area, refer to Fig. A-FBAAA Sheet 01

(b) Do a detailed inspection of the inlet acoustic panels in the engine air intake cowl,

refer to Fig. A-FBBAA Sheet 01 and to the ROLLS-ROYCE Service Bulletin No.

RB.211-71-AG419.

1 If the inlet acoustic panels in the engine air intake cowl is damage :

- Refer to TASK 713024-833-801 001 Repair .

2 If the inlet acoustic panels in the engine air intake cowl is not damage :

- Next visual inspection in 24 months.

(c) For the inspection report, refer to Appendix 01 : Inspection Report .

(2) Subtask 713024-220-002-001 - Do a Detailed Inspection of the Acoustic Panels on

the RH Engine Air Intake Cowl.

Work Zones and Access Panels

Zone Access/Work location

420

Manpower Resources

Manhours 9.00

Minimum number of person 1

Subtask elapsed time 9.00

Skills NON SPECIFIC

DATE: May 11/11 SERVICE BULLETIN No.: A330-71-3024

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SERVICE BULLETIN

References

Vendor Service Bulletin (VSB) ROLLS-ROYCE RB.211-71-AG419

Fig. A-FBAAA

Area to be Inspected

Sheet 01

Fig. A-FBBAA

Flow Chart

Sheet 01

(a) For the inspection area, refer to Fig. A-FBAAA Sheet 01

(b) Do a detailed inspection of the inlet acoustic panels in the engine air intake cowl,

refer to Fig. A-FBBAA Sheet 01 and to the ROLLS-ROYCE Service Bulletin No.

RB.211-71-AG419.

1 If the inlet acoustic panels in the engine air intake cowl is damage :

- Refer to TASK 713024-833-801 001 Repair .

2 If the inlet acoustic panels in the engine air intake cowl is not damage :

- Next visual inspection in 24 months.

(c) For the inspection report, refer to Appendix 01 : Inspection Report .

D. TEST

None

E. CLOSE-UP

(1) Subtask 713024-942-001-001 - Close-up for LH Engine

Work Zones and Access Panels

Zone Access/Work location

410

Manpower Resources

Skills NON SPECIFIC

(a) Close the following circuit breakers :

PANEL DESIGNATION FIN LOCATION SEE

NOTES

722VU FADEC B ENG 1 13KS1 46 K (1)

722VU FADEC B ENG 1 13KS1 44 D (1)

742VU FADEC A ENG 1 12KS1 74 N (1)

742VU FADEC A ENG 1 12KS1 73 Q (1)

NOTE (1): The location of the CB depends on the A/C configuration.

(b) Make sure that the work areas are clean and clear of tools and other items of

equipment

DATE: May 11/11 SERVICE BULLETIN No.: A330-71-3024

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SERVICE BULLETIN

(c) Remove the access platform(s)

(d) Restore the systems and the aircraft to normal operating conditions.

(2) Subtask 713024-942-003-001 - Close-up for RH Engine

Work Zones and Access Panels

Zone Access/Work location

420

Manpower Resources

Skills NON SPECIFIC

(a) Close the following circuit breakers :

PANEL DESIGNATION FIN LOCATION SEE

NOTES

722VU FADEC B ENG 2 13KS2 43 D (1)

722VU FADEC B ENG 2 13KS2 49 K (1)

742VU FADEC A ENG 2 12KS2 73 Q (1)

742VU FADEC A ENG 2 12KS2 74 Q (1)

NOTE (1): The location of the CB depends on the A/C configuration.

(b) Make sure that the work areas are clean and clear of tools and other items of

equipment

(c) Remove the access platform(s)

(d) Restore the systems and the aircraft to normal operating conditions.

DATE: May 11/11 SERVICE BULLETIN No.: A330-71-3024

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DATE: May 11/11 SERVICE BULLETIN No.: A330-71-3024

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SERVICE BULLETIN

Task 713024-833-801-001 - Repair

WARNING: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND THE CAUTIONS

INCLUDED IN THE REFERENCED PROCEDURES.

CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP

ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY

AND MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENANCE

WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING,

COMPONENTS AND THE WORK AREA AS CLEAN AS POSSIBLE. TO DO

THIS :

- PUT PROTECTION, SUCH AS PLASTIC SHEETING, CLOTHS, ETC. AS

NECESSARY ON WIRING AND COMPONENTS,

- REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND

OTHER CONTAMINATION.

THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION

AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION.

IF THERE IS CONTAMINATION, REFER TO ESPM 20-55-00.

Task Associated Data

Zone

410 420

Manpower

TOTAL MANHOURS 2.00

ELAPSED TIME (HOURS) 1.00

Additional manhours related to Vendor SB; refer to:

ROLLS-ROYCE Service Bulletin No. RB.211-71-AG419

A. GENERAL

(1) Subtask 713024-839-002-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

Write in the applicable aircraft records that you have done all the work given in this

Service Bulletin.

B. PREPARATION

(1) Subtask 713024-941-002-001 - Job Set-up for LH Engine

Work Zones and Access Panels

Zone Access/Work location

410

DATE: May 11/11 SERVICE BULLETIN No.: A330-71-3024

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SERVICE BULLETIN

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802

(a) Make sure that the aircraft is electrically grounded (Refer to AMM Task

12-34-24-860-802).

(b) Put access platform(s) in position

(c) Open, safety and tag the following circuit breakers :

PANEL DESIGNATION FIN LOCATION SEE

NOTES

722VU FADEC B ENG 1 13KS1 46 K (1)

722VU FADEC B ENG 1 13KS1 44 D (1)

742VU FADEC A ENG 1 12KS1 74 N (1)

742VU FADEC A ENG 1 12KS1 73 Q (1)

NOTE (1): The location of the CB depends on the A/C configuration.

(2) Subtask 713024-941-004-001 - Job Set-up for RH Engine

Work Zones and Access Panels

Zone Access/Work location

420

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802

(a) Make sure that the aircraft is electrically grounded (Refer to AMM Task

12-34-24-860-802).

(b) Put access platform(s) in position

(c) Open, safety and tag the following circuit breakers :

PANEL DESIGNATION FIN LOCATION SEE

NOTES

722VU FADEC B ENG 2 13KS2 43 D (1)

722VU FADEC B ENG 2 13KS2 49 K (1)

742VU FADEC A ENG 2 12KS2 73 Q (1)

742VU FADEC A ENG 2 12KS2 74 Q (1)

NOTE (1): The location of the CB depends on the A/C configuration.

DATE: May 11/11 SERVICE BULLETIN No.: A330-71-3024

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C. PROCEDURE

(1) Subtask 713024-833-003-001 - Repair or Replace the Affected Air Intake Cowl of

the LH Engine.

Work Zones and Access Panels

Zone Access/Work location

410

References

Vendor Service Bulletin (VSB) ROLLS-ROYCE RB.211-71-AG419

Fig. A-FBBAA

Flow Chart

Sheet 01

(a) Follow the instructions given in the Vendor Service Bulletin to repair or replace

the affected Air Intake Cowl of the LH Engine (Refer to ROLLS-ROYCE Service

Bulletin No. RB.211-71-AG419).

NOTE (1): In case of Air Intake cowl replacement refer to Fig. A-FBBAA Sheet

01 flow chart for instruction.

(2) Subtask 713024-833-004-001 - Repair or Replace the Affected Air Intake Cowl of

the RH Engine.

Work Zones and Access Panels

Zone Access/Work location

420

References

Vendor Service Bulletin (VSB) ROLLS-ROYCE RB.211-71-AG419

Fig. A-FBBAA

Flow Chart

Sheet 01

(a) Follow the instructions given in the Vendor Service Bulletin to repair or replace

the affected Air Intake Cowl of the RH Engine (Refer to ROLLS-ROYCE Service

Bulletin No. RB.211-71-AG419).

NOTE (1): In case of Air Intake cowl replacement refer to Fig. A-FBBAA Sheet

01 flow chart for instruction.

D. TEST

None

E. CLOSE-UP

(1) Subtask 713024-942-002-001 - Close-up for LH Engine

Work Zones and Access Panels

Zone Access/Work location

410

DATE: May 11/11 SERVICE BULLETIN No.: A330-71-3024

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SERVICE BULLETIN

Manpower Resources

Skills NON SPECIFIC

(a) Close the following circuit breakers :

PANEL DESIGNATION FIN LOCATION SEE

NOTES

722VU FADEC B ENG 1 13KS1 46 K (1)

722VU FADEC B ENG 1 13KS1 44 D (1)

742VU FADEC A ENG 1 12KS1 74 N (1)

742VU FADEC A ENG 1 12KS1 73 Q (1)

NOTE (1): The location of the CB depends on the A/C configuration.

(b) Make sure that the work areas are clean and clear of tools and other items of

equipment

(c) Remove the access platform(s)

(d) Restore the systems and the aircraft to normal operating conditions.

(2) Subtask 713024-942-004-001 - Close-up for RH Engine

Work Zones and Access Panels

Zone Access/Work location

420

Manpower Resources

Skills NON SPECIFIC

(a) Close the following circuit breakers :

PANEL DESIGNATION FIN LOCATION SEE

NOTES

722VU FADEC B ENG 2 13KS2 43 D (1)

722VU FADEC B ENG 2 13KS2 49 K (1)

742VU FADEC A ENG 2 12KS2 73 Q (1)

742VU FADEC A ENG 2 12KS2 74 Q (1)

NOTE (1): The location of the CB depends on the A/C configuration.

(b) Make sure that the work areas are clean and clear of tools and other items of

equipment

(c) Remove the access platform(s)

(d) Restore the systems and the aircraft to normal operating conditions.

DATE: May 11/11 SERVICE BULLETIN No.: A330-71-3024

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SERVICE BULLETIN

**CONF ALL

Z410

Z420

A

A B

ACOUSTIC LINER SEGMENTS (3 OFF)

0 DEGREES

RADIAL

RADIAL 63 DEGREES

EEC INLET

RADIAL 80.5 DEGREES

EEC OUTLET

135 DEGREES

RADIAL

225 DEGREES

RADIAL

RADIAL 345 DEGREES

PROBE P2T2

PANEL 3

PANEL 2

PANEL 1

NOTE:

INNER ACOUSTIC PANELS TO BE INSPECTED

B

A

G_SB_713024_5_BAAA_01_01

Figure A-FBAAA - Sheet 01

Area to be Inspected

DATE: May 11/11 SERVICE BULLETIN No.: A330-71-3024

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SERVICE BULLETIN

**CONF ALL

ROLLS ROYCE SERVICE BULLETIN RB.211−71−AG419 AT THE THRESHOLD

GIVEN IN THE PLANNING INFORMATION PARAGRAPH 1.E.(2).

NO DAMAGE FOUND ? YES

DO A DETAILED INSPECTION ON BOTH ENGINES THROUGH TAP

TEST OF THE 3 INNER ACOUSTIC PANELS OF AIR INTAKE COWLS AS PER

AT THE INTERVAL GIVEN IN

DO REPEAT INSPECTION

THE PLANNING INFORMATION

PARAGRAPH 1.E.(2).

SEND TO AIRBUS THE

INSPECTION REPORT

NO

YES

MORE THAN ADL

AS DEFINED IN ROLLS ROYCE

SERVICE BULETIN

OR

COWL ON WING BEFORE

REPAIR THE AFFECTED INTAKE

NEXT FLIGHT IF THE FINDINGS

ARE WITHIN THE RDL

AS DEFINED IN

REPLACE THE

AFFECTED AIR

DAMAGE

INSPECTIONS OF THE

DO REPETITIVE

AFFECTED INTAKE COWL

AT THE INTERVALS GIVEN

THE ROLLS ROYCE SERVICE

BULLETIN RB.211−71−AG419.

RB.211−71−AG419

IN THE ROLLS ROYCE

SERVICE BULLETIN

INTAKE COWL

QUESTION ACTION FINDING

BEFORE NEXT

FLIGHT.

SEND TO AIRBUS

THE INSPECTION

REPORT

RB.211−71−AG419.

NO

INTAKE COWL USED FOR

REPLACEMENT HAS ACCUMULATED

MORE THAN 5,000FC OR 20,000FH

ENGINE AIR

(WHICHEVER OCCURS

YES

NO

INTAKE COWL USED

FOR REPLACEMENT HAS

ALREADY BEEN

ENGINE AIR

INSPECTED

YES

TAP TEST OF THE 3 INNER ACOUSTIC

DO A DETAILED INSPECTION THROUGH

PANELS OF THE AIR INLET COWL

AS PER ROLLS ROYCE SERVICE BULLETIN

RB.211−71−AG419 WITHIN 24 MONTHS

AFTER AIR INTAKE COWL HAS

ACCUMULATED 5,000FC OR 20,000FH

FIRST)

(WHICHEVER OCCURS FIRST)

TAP TEST OF THE 3 INNER ACOUSTIC

DO A DETAILED INSPECTION THROUGH

PANELS OF THE AIR INLET COWL

AS PER ROLLS ROYCE SERVICE BULLETIN

RB.211−71−AG419

BEFORE INSTALLATION

ON AIRPLANE

G_SB_713024_5_BBAA_01_07

Figure A-FBBAA - Sheet 01

Flow Chart

DATE: May 11/11 SERVICE BULLETIN No.: A330-71-3024

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SERVICE BULLETIN

Appendix 01 : Inspection Report

**CONF ALL

The results of the inspection, including no findings, replacement or actions to be done, must be

forwarded to AIRBUS Department SEEE1, on the attached inspection report sheets.

DATE: May 11/11 SERVICE BULLETIN No.: A330-71-3024

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SERVICE BULLETIN

Appendix 01 : Inspection Report

**CONF ALL

SERVICE BULLETIN No. :

A/C MSN :

FLIGHT CYCLES :

FLIGHT HOURS :

A330−71−3024

DATE OF INSPECTION :

INSPECTION METHOD : DETAILED

INSPECTION

INSPECTION REPORT

PLEASE RECORD OTHER FINDINGS :

COWL ACOUSTIC PANELS ?

YES NO

LH ENGINE

AFFECTED PANEL

PANEL 1 PANEL 2 PANEL 3

YES NO

RH ENGINE

AFFECTED PANEL

PANEL 1 PANEL 2 PANEL 3

G_SB_713024_5_AAAA_01_02

DAMAGE FOUND ON THE ENGINE AIR INTAKE

COWL ACOUSTIC PANELS ?

DAMAGE FOUND ON THE ENGINE AIR INTAKE

Figure A-FAAAA - Sheet 01

Inspection Report

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SERVICE BULLETIN

Appendix 02 : Elapsed Time Assumptions of the Inspection

**CONF ALL

(1) For detail concerning the elapsed time assumptions, refer to the Gantt chart shown in the next

page :

DATE: May 11/11 SERVICE BULLETIN No.: A330-71-3024

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SERVICE BULLETIN

Appendix 02 : Elapsed Time Assumptions of the Inspection

**CONF ALL

ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A330−71−3024

MH ET/S

TOTAL MANHOURS

SB ELAPSED TIME

20.00

11.00

STEPS

1.00 1.00

0 10

9.00 9.00

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.

MANHOURS GIVEN IN VENDOR SERVICE BULLETINS

ARE NOT REFLECTED IN THIS GANTT CHART.

01

02

NOTES:

PER

1

1

:

:

SB ELAPSED TIME

(HOURS)

2 4 6 8

GET ACCESS

CLOSE−UP

ACOUSTIC PANELS ON THE

INSPECTION OF THE

LH ENGINE AIR INTAKE

1 3 579

1.00 1.00 1

9.00 9.00 1

G_SB_713024_5_ABAA_01_02

11

COWL

ACOUSTIC PANELS ON THE

INSPECTION OF THE

RH ENGINE AIR INTAKE

COWL

Figure A-FABAA - Sheet 01

Gantt chart

DATE: May 11/11 SERVICE BULLETIN No.: A330-71-3024

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SERVICE BULLETIN

Appendix 03 : Elapsed Time Assumptions of the Repair

**CONF ALL

(1) For detail concerning the elapsed time assumptions, refer to the Gantt chart shown in the next

page :

DATE: May 11/11 SERVICE BULLETIN No.: A330-71-3024

REVISION No.: 01 - Sep 27/11 Page: 1

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SERVICE BULLETIN

Appendix 03 : Elapsed Time Assumptions of the Repair

**CONF ALL

ELAPSED TIME

(HOURS)

NOTE: THIS CHART IS ONLY A PROPOSAL.

OPERATORS MAY DETERMINE THAT ANOTHER WAY

TO DO THE WORK IS MORE SUITABLE FOR THEM.

MH ET PER

MH:

ET:

PER:

MANHOURS

ELAPSED TIME

NUMBER OF PERSONS

TOTAL MANHOURS (MH)

ELAPSED TIME (ET)

2.00

1.00

STEPS

0 1.5

JOB SET−UP FOR THE LH ENGINE 0.50 0.50 1

CLOSE−UP FOR THE LH ENGINE 0.50 0.50 1

ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A330−71−3024

0.5 1

0.50 0.50 1

0.50 0.50 1

2

G_SB_713024_5_ACAA_01_00

JOB SET−UP FOR THE RH ENGINE

CLOSE−UP FOR THE LH ENGINE

Figure A-FACAA - Sheet 01

Gantt chart

DATE: May 11/11 SERVICE BULLETIN No.: A330-71-3024

REVISION No.: 01 - Sep 27/11 Page: 2

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SERVICE BULLETIN

REPORTING SHEET

TITLE: POWER PLANT - AIR INTAKE COWL - INSPECTION ON T700 OF THE

AIR INTAKE COWL.

MODIFICATION No.: None

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: May 11/11 SERVICE BULLETIN No.: A330-71-3024

REVISION No.: 01 - Sep 27/11 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: May 11/11 SERVICE BULLETIN No.: A330-71-3024

REVISION No.: 01 - Sep 27/11 Page: 1

5

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