@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: 71

TITLE: INSPECTION ON TRENT 700 OF THE AIR INLET COWL FOR PICCOLO

TUBE FRACTURE

**CONF ALL

MODIFICATIONS

None

REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES

During Shop Visit, several Trent 700 air intake cowl primary assembly structures have been found with

cracks in the forward bulkhead web, web stiffeners, angles and - to a lesser extent - on the Thermal

Anti Ice (TAI) Piccolo Tube.

Analysis of the effects of cracking on these structures have identified a need to inspect the primary

assembly and to rectify the damage found.

Inspections performed demonstrated :

- Threat of damage to engine due to operation in icing conditions with reduced thermal anti-ice

performance due to broken piccolo tube.

- Impact on Nose Cowl structural integrity in case of forward bulkhead damage in conjunction with

broken piccolo tube.

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-AG416.

This inspection Service Bulletin requires inspection of air intake cowl as per ROLLS-ROYCE Service

Bulletin No. RB.211-71-AG416.

The aim of this inspection is to perform inspection of TRENT 700 nose cowls, including :

- Internal inspection of piccolo tube,

- Detailed inspection of piccolo tube mount links,

DATE: Jan 10/11 SERVICE BULLETIN No.: A330-71-3025

REVISION No.: 00 - Jan 10/11 Page: 1

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SERVICE BULLETIN

SUMMARY

- Inspection of aft side of front bulkhead and Outer Boundary Angle (OBA).

Inspection concerns intake having accumulated more than 5000FC. For intakes with unknown history,

method of the yearly fleet leader shall apply.

For intakes with a life greater than 5000FC since new, accomplish the initial inspection of the primary

structure within 24 months from issue of this Service Bulletin.

For intakes with a life less than 5000FC since new, accomplish the initial inspection of the primary

structure within 24 months after intake cowl has accumulated 5000FC.

Accomplishment of this Inspection Service Bulletin will ensure the structural integrity of the Air intake

cowl.

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 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 AFL ALK AVA BEC BMA CCA CES CHH CPA

CRL CSC CSN CYP DLH EDW ETD GFA GIA HAL HDA HFY IWD

IYE JAI LVG MEA MON MSR MXA OBS OHY OMA SAA SAS SGX

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

XLF

CONCURRENT REQUIREMENTS

None

REFERENCES / REPERCUSSIONS

TFU None

OEB None

AOT None

SIL None

LINE MAINTENANCE AFFECTED No

LIFE LIMIT None

OTHER None

DATE: Jan 10/11 SERVICE BULLETIN No.: A330-71-3025

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SERVICE BULLETIN

SUMMARY

NATURE OF THE WORK

AIRCRAFT YES

EQUIPMENT NO

HARD NO

SOFT NO

OBRM NO

MANPOWER

Task 713025-832-801-001: Inspection

TOTAL MANHOURS 4.00

ELAPSED TIME (HOURS) 2.00

Additional manhours related to Vendor SB; refer to:

Detailed Inspection of the Air Intake Cowl on the Engine 1

(4030EM1)

ROLLS-ROYCE Service Bulletin No.

RB.211-71-AG416

Detailed Inspection of the Air Intake Cowl on the Engine 2

(4030EM2)

ROLLS-ROYCE Service Bulletin No.

RB.211-71-AG416

Task 713025-833-801-001: Repair

TOTAL MANHOURS 16.00

ELAPSED TIME (HOURS) 5.00

APPENDICES

Appendix 01

Appendix 02

DATE: Jan 10/11 SERVICE BULLETIN No.: A330-71-3025

REVISION No.: 00 - Jan 10/11 Page: 3

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SERVICE BULLETIN

SUMMARY

**CONF ALL

A

A

AREA TO BE

INSPECTED

Z411 (Z421)

B

Z410

Z420

A

B

G_SB_713025_5_SAAA_01_00

Figure A-FSAAA - Sheet 01

DATE: Jan 10/11 SERVICE BULLETIN No.: A330-71-3025

REVISION No.: 00 - Jan 10/11 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: INSPECTION ON TRENT 700 OF THE AIR INLET COWL FOR PICCOLO

TUBE FRACTURE

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: Jan 10/11 SERVICE BULLETIN No.: A330-71-3025

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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 1097-1100 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 1178 1181 1184 1186-1193 1195-1196 1199

(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 1051 1062 1115

78V 1033 1046

97X 1053

ACA 0277 0279 0284 0344 0400 0408 0412 0419

AFL 0963 0973 1014 1045 1047 1058 1065 1072 1077

ALK 0303 0306 0311 0313 0404

AVA 0948 0967 1009 1016 1073

BEC 0863

BMA 0398 0401

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

0884 0890 0903 0909 0930 0941 0944 0957 1087 1130 1187 1199

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

0836 0851 0862 0866 0916 0928 0936 0942

CHH 0875 0881 0906 0919 0982 1159 1168 1178 1190

CPA 0012 0017 0071 0083 0099 0102 0109 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

CRL 0285 0320

CSC 1082 1138

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 0369 1193

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

0854 0868 0975 0991 1032 1070 1071 1081 1167

GFA 0276 0281 0286 0287 0334 0340 0527 0529 0532 0992

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

HAL 1114 1171

HDA 0106 0132 0234 0405 0479 0512 0581 0654 0662 0692 0716 0741

0786

HFY 1008

DATE: Jan 10/11 SERVICE BULLETIN No.: A330-71-3025

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@A330

SERVICE BULLETIN

OPERATOR MSN

IWD 0670 0833 1097

IYE 0625 0632

JAI 0751 0807

LVG 0551 0597 0627

MEA 0926 0984 0995 0998

MON 0261 0265

MSR 0600 0610 0666 0683 0696 0709 0726 1143

MXA 0966 0971

OBS 0461

OHY 0098

OMA 1038 1044 1049 1063 1093 1120

SAA 1191

SAS 0496 0497 0515 0568

SGX 0407

SIA 0978 0983 0986 0997 1006 1010 1012 1015 1085 1098 1099 1124

1132 1146 1149 1156 1157

SVA 1127 1137 1141 1147 1153 1189 1192

SWR 1000 1018 1026 1029 1084 1089 1145 1181 1188

TCX 0254 0266 0301 0427 0456 0795

THA 0990 1003 1035 1037 1060 1074 1086 1090

THY 1004 1092 1150 1160 1170 1172

TSC 0111 0177 0250 0271 0480

UAE 0248 0251 0283 0293 0295 0314 0316 0326 0328 0345 0348 0365

0372 0382 0384 0392 0396 0409 0437 0451 0452 0455 0462 0491

0494 0509 0518 0525 0536

UAF 1080 1186

USA 1011 1022 1041 1069 1076 1095 1100

VIR 1195

VKG 0309 0349 0356 0357

XAX 0952 0974 1048 1066 1075 1126 1131 1165

XLF 0501 0635

DATE: Jan 10/11 SERVICE BULLETIN No.: A330-71-3025

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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 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 1178 1181 1184 1186 1187 1188 1189 1190

1191 1192 1193 1195 1196 1199

001

(5) Configuration definition

**CONF 001

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

standard configuration.

(6) Material Effectivity

None

B. CONCURRENT REQUIREMENTS

None

DATE: Jan 10/11 SERVICE BULLETIN No.: A330-71-3025

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SERVICE BULLETIN

C. REASON

(1) History

During Shop Visit, several Trent 700 air intake cowl primary assembly structures have

been found with cracks in the forward bulkhead web, web stiffeners, angles and - to a

lesser extent - on the Thermal Anti Ice (TAI) Piccolo Tube.

Analysis of the effects of cracking on these structures have identified a need to inspect

the primary assembly and to rectify the damage found.

Inspections performed demonstrated :

- Threat of damage to engine due to operation in icing conditions with reduced

thermal anti-ice performance due to broken piccolo tube.

- Impact on Nose Cowl structural integrity in case of forward bulkhead damage in

conjunction with broken piccolo tube.

(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-

AG416.

This inspection Service Bulletin requires inspection of air intake cowl as per ROLLSROYCE Service Bulletin No. RB.211-71-AG416.

The aim of this inspection is to perform inspection of TRENT 700 nose cowls, including :

- Internal inspection of piccolo tube,

- Detailed inspection of piccolo tube mount links,

- Inspection of aft side of front bulkhead and Outer Boundary Angle (OBA).

Inspection concerns intake having accumulated more than 5000FC. For intakes with

unknown history, method of the yearly fleet leader shall apply.

For intakes with a life greater than 5000FC since new, accomplish the initial inspection

of the primary structure within 24 months from issue of this Service Bulletin.

For intakes with a life less than 5000FC since new, accomplish the initial inspection of

the primary structure within 24 months after intake cowl has accumulated 5000FC.

(3) Advantages

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

the Air intake cowl.

(4) Operational/Maintenance Consequences

None

DATE: Jan 10/11 SERVICE BULLETIN No.: A330-71-3025

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SERVICE BULLETIN

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

Task 713025-832-801-001: Inspection

(1) Detailed Inspection of the Air Intake Cowl on the Engine 1 (4030EM1)

(2) Detailed Inspection of the Air Intake Cowl on the Engine 2 (4030EM2)

Task 713025-833-801-001: Repair

(1) Replace the Air Intake Cowl of the Engine 1 (4030EM1)

(2) Replace the Air Intake Cowl of the Engine 2 (4030EM2)

E. COMPLIANCE

(1) Classification

MANDATORY: Service Bulletin must be accomplished.

(2) Accomplishment Timescale

CONDITION ACTION COMPLIANCE TIME

THRESHOLD GRACE PERIOD

REPETITIVE

INTERVAL NOT

TO EXCEED

Air intake cowl

having

accumulated more

than 5000FC

Aircraft equipped

with T700 engine

Do the inspection

of the piccolo tube,

refer to Fig. AFBBAA Sheet 01

and Table 2 For units without

known history,

yearly fleet leader

method shall apply

24 months Not applicable

Table 1 : Detailed Inspection of the Air Intake Cowl

CONDITION ACTION COMPLIANCE TIME

THRESHOLD

REPETITIVE

INTERVAL NOT

TO EXCEED

Piccolo tube

cracked or

fractured

Replace the

affected intake

cowl, refer to

TASK

713025-833-801

001 Repair

Before the next flight Refer to Fig. AFBBAA Sheet 04

and Table 5

DATE: Jan 10/11 SERVICE BULLETIN No.: A330-71-3025

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SERVICE BULLETIN

CONDITION ACTION COMPLIANCE TIME

THRESHOLD

REPETITIVE

INTERVAL NOT

TO EXCEED

Piccolo tube not

cracked and not

fractured

Do the inspection

of the piccolo tube

links, refer to Fig.

A-FBBAA Sheet 02

and Table 3

Not applicable Not applicable

Table 2 : Detailed Inspection of the Air Intake Cowl Piccolo Tube (Fig. A-FBBAA Sheet 01)

CONDITION ACTION COMPLIANCE TIME

THRESHOLD

REPETITIVE

INTERVAL NOT

TO EXCEED

No piccolo link

found broken

Do a detailed

inspection of the

OBA and bulkhead

for the inspected

intake cowl, refer

to Fig. A-FBBAA

Sheet 03 and

Table 4

Not applicable Not applicable

1 thru 3 piccolo

link (s) found

broken and the

opposite intake

cowl has less than

5000FC

Do a detailed

inspection of the

OBA and bulkhead

for the inspected

intake cowl, refer

to Fig. A-FBBAA

Sheet 03 and

Table 4

Not applicable Not applicable

1 thru 3 piccolo

link(s) found

broken and the

opposite intake

cowl has more

than 5000FC

Do the detailed

inspection of the

opposite engine

intake cowl for

broken links, refer

to Fig. A-FBBAA

Sheet 02

Not applicable Not applicable

Intake A : 1 link

broken

Intake B : 0 link

broken

Do a detailed

inspection of the

OBA and bulkhead

for the intake cowl

A, refer to Fig. AFBBAA Sheet 03

and Table 4

Not applicable Not applicable

DATE: Jan 10/11 SERVICE BULLETIN No.: A330-71-3025

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SERVICE BULLETIN

CONDITION ACTION COMPLIANCE TIME

THRESHOLD

REPETITIVE

INTERVAL NOT

TO EXCEED

Replace the intake

cowl A or B, refer

to TASK

713025-833-801

001 Repair

Before the next flight Refer to Fig. AFBBAA Sheet 04

and Table 5

Intake A : 1 link

broken

Intake B : 1 link

broken

Do a detailed

inspection of the

OBA and bulkhead

for the remaining

intake cowl, refer

to Fig. A-FBBAA

Sheet 03 and

Table 4

Not applicable Not applicable

Replace the intake

cowl B, refer to

TASK

713025-833-801

001 Repair

Before the next flight Refer to Fig. AFBBAA Sheet 04

and Table 5

Intake A : 1 link

broken

Intake B : 2 or 3

links broken

Do a detailed

inspection of the

OBA and bulkhead

for the intake cowl

A, refer to Fig. AFBBAA Sheet 03

and Table 4

Not applicable Not applicable

Replace the intake

cowl B, refer to

TASK

713025-833-801

001 Repair

Before the next flight Refer to Fig. AFBBAA Sheet 04

and Table 5

Intake A : 1 link

broken

Intake B : 4 or

more links broken

Do a detailed

inspection of the

OBA and bulkhead

for the intake cowl

A, refer to Fig. AFBBAA Sheet 03

and Table 4

Not applicable Not applicable

DATE: Jan 10/11 SERVICE BULLETIN No.: A330-71-3025

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SERVICE BULLETIN

CONDITION ACTION COMPLIANCE TIME

THRESHOLD

REPETITIVE

INTERVAL NOT

TO EXCEED

Replace the intake

cowl B, refer to

TASK

713025-833-801

001 Repair

Before the next flight Refer to Fig. AFBBAA Sheet 04

and Table 5

Intake A : 1 link

broken

Intake B : Piccolo

tube broken

Do a detailed

inspection of the

OBA and bulkhead

for the intake cowl

A, refer to Fig. AFBBAA Sheet 03

and Table 4

Not applicable Not applicable

Replace the intake

cowl A, refer to

TASK

713025-833-801

001 Repair

Before 100FC Refer to Fig. AFBBAA Sheet 04

and Table 5

Intake A : 2 links

broken

Intake B : 0 link

broken

Do a detailed

inspection of the

OBA and bulkhead

for intake cowl B,

refer to Fig. AFBBAA Sheet 03

and Table 4

Not applicable Not applicable

Replace the intake

cowl A, refer to

TASK

713025-833-801

001 Repair

Before the next flight Refer to Fig. AFBBAA Sheet 04

and Table 5

Intake A : 2 links

broken

Intake B : 1 link

broken

Do a detailed

inspection of the

OBA and bulkhead

for the intake cowl

B, refer to Fig. AFBBAA Sheet 03

and Table 4

Not applicable Not applicable

Replace the intake

cowl A or B, refer

to TASK

713025-833-801

001 Repair

Before the next flight Refer to Fig. AFBBAA Sheet 04

and Table 5

Intake A : 2 links

broken

Intake B : 2 links

broken

Replace the

remaining intake

cowl, refer to

TASK

713025-833-801

001 Repair

Before 100FC Refer to Fig. AFBBAA Sheet 04

and Table 5

DATE: Jan 10/11 SERVICE BULLETIN No.: A330-71-3025

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@A330

SERVICE BULLETIN

CONDITION ACTION COMPLIANCE TIME

THRESHOLD

REPETITIVE

INTERVAL NOT

TO EXCEED

Replace the intake

cowl B, refer to

TASK

713025-833-801

001 Repair

Before the next flight Refer to Fig. AFBBAA Sheet 04

and Table 5

Intake A : 2 links

broken

Intake B : 3 links

broken

Replace the intake

cowl A, refer to

TASK

713025-833-801

001 Repair

Before 100FC Refer to Fig. AFBBAA Sheet 04

and Table 5

Replace the intake

cowl B, refer to

TASK

713025-833-801

001 Repair

Before the next flight Refer to Fig. AFBBAA Sheet 04

and Table 5

Intake A : 2 links

broken

Intake B : 4 or

more links broken

Replace the intake

cowl A, refer to

TASK

713025-833-801

001 Repair

Before 100FC Refer to Fig. AFBBAA Sheet 04

and Table 5

Replace the intake

cowl B, refer to

TASK

713025-833-801

001 Repair

Before the next flight Refer to Fig. AFBBAA Sheet 04

and Table 5

Intake A : 2 links

broken

Intake B : Piccolo

tube broken

Replace the intake

cowl A, refer to

TASK

713025-833-801

001 Repair

Before 100FC Refer to Fig. AFBBAA Sheet 04

and Table 5

Replace the intake

cowl A, refer to

TASK

713025-833-801

001 Repair

Before 100FC Refer to Fig. AFBBAA Sheet 04

and Table 5

Intake A : 3 links

broken

Intake B : 0 link

broken

Do a detailed

inspection of the

OBA and bulkhead

for intake cowl B,

refer to Fig. AFBBAA Sheet 03

and Table 4

Not applicable Not applicable

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CONDITION ACTION COMPLIANCE TIME

THRESHOLD

REPETITIVE

INTERVAL NOT

TO EXCEED

Replace the intake

cowl A, refer to

TASK

713025-833-801

001 Repair

Before the next flight Refer to Fig. AFBBAA Sheet 04

and Table 5

Intake A : 3 links

broken

Intake B : 1 link

broken

Do a detailed

inspection of the

OBA and bulkhead

for intake cowl B,

refer to Fig. AFBBAA Sheet 03

and Table 4

Not applicable Not applicable

Replace the intake

cowl A, refer to

TASK

713025-833-801

001 Repair

Before the next flight Refer to Fig. AFBBAA Sheet 04

and Table 5

Intake A : 3 links

broken

Intake B : 2 links

broken

Replace the intake

cowl B, refer to

TASK

713025-833-801

001 Repair

Before 100FC Refer to Fig. AFBBAA Sheet 04

and Table 5

Replace the intake

cowl A or B, refer

to TASK

713025-833-801

001 Repair

Before the next flight Refer to Fig. AFBBAA Sheet 04

and Table 5

Intake A : 3 links

broken

Intake B : 3 links

broken

Replace the

remaining intake

cowl, refer to

TASK

713025-833-801

001 Repair

Before 100FC Refer to Fig. AFBBAA Sheet 04

and Table 5

Replace the intake

cowl B, refer to

TASK

713025-833-801

001 Repair

Before the next flight Refer to Fig. AFBBAA Sheet 04

and Table 5

Intake A : 3 links

broken

Intake B : 4 or

more links broken

Replace the intake

cowl A, refer to

TASK

713025-833-801

001 Repair

Before 100FC Refer to Fig. AFBBAA Sheet 04

and Table 5

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CONDITION ACTION COMPLIANCE TIME

THRESHOLD

REPETITIVE

INTERVAL NOT

TO EXCEED

Replace the intake

cowl B, refer to

TASK

713025-833-801

001 Repair

Before the next flight Refer to Fig. AFBBAA Sheet 04

and Table 5

Intake A : 3 links

broken

Intake B : Piccolo

tube broken

Replace the intake

cowl A, refer to

TASK

713025-833-801

001 Repair

Before 100FC Refer to Fig. AFBBAA Sheet 04

and Table 5

4 or more piccolo

links found broken

Replace the

affected air intake

cowl, refer to

TASK

713025-833-801

001 Repair

Before the next flight Refer to Fig. AFBBAA Sheet 04

and Table 5

Table 3 : Detailed Inspection of the Broken Piccolo Tubes Links (Fig. A-FBBAA Sheet 02)

CONDITION ACTION COMPLIANCE TIME

THRESHOLD

REPETITIVE

INTERVAL NOT

TO EXCEED

Repeat the piccolo

tube and link

inspections every

2500FC, refer to

Fig. A-FBBAA

Sheet 01 and

Table 2

Crack(s) within

allowed damage

limit as defined in

ROLLS-ROYCE

Service Bulletin

No. RB.211-71-

AG416

Send the

inspection report

Not applicable

Repeat the OBA

and bulkhead

inspection :

Interval given in

the ROLLSROYCE Service

Bulletin No.

RB.211-71-AG416

and refer to Fig. AFBBAA Sheet 03

and Table 4

OBA crack less

than 22in

(558.8mm) and

bulkhead crack

less than 13in

(330.2mm)

Replace the

affected air intake

cowl, refer to

TASK

713025-833-801

001 Repair

Before 100FC Refer to Fig. AFBBAA Sheet 04

and Table 5

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CONDITION ACTION COMPLIANCE TIME

THRESHOLD

REPETITIVE

INTERVAL NOT

TO EXCEED

OBA crack more

than 22in

(558.8mm) or

bulkhead crack

more than 13in

(330.2mm)

Replace the

affected air intake

cowl, refer to

TASK

713025-833-801

001 Repair

Before the next flight Refer to Fig. AFBBAA Sheet 04

and Table 5

Table 4 : Detailed Inspection of OBA and Bulkhead (Fig. A-FBBAA Sheet 03)

CONDITION ACTION COMPLIANCE TIME

THRESHOLD

REPETITIVE

INTERVAL NOT

TO EXCEED

Replacement

intake cowl has

accumulated less

than 5000FC

Send the

inspection report

Not applicable Repeat the piccolo

tube and link

inspections when

the intake cowl has

accumulated more

than 5000FC, refer

to Fig. A-FBBAA

Sheet 01 and

Table 2

Repeat the piccolo

tube and link

inspections every

2500FC, refer to

Fig. A-FBBAA

Sheet 01 and

Table 2

Replacement

intake cowl has

accumulated more

than 5000FC

Send the

inspection report

Not applicable

Repeat the OBA

and bulkhead

inspection :

Interval given in

the ROLLSROYCE Service

Bulletin No.

RB.211-71-AG416

and refer to Fig. AFBBAA Sheet 03

and Table 4

Table 5 : Condition of the Air Intake Cowl Replacement (Fig. A-FBBAA Sheet 04)

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.

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F. APPROVAL

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

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 713025-832-801-001: Inspection

Get Access 2.00

Close-Up 2.00

TOTAL MANHOURS 4.00

ELAPSED TIME (HOURS) 2.00

Additional manhours related to Vendor SB; refer to:

Detailed Inspection of the Air Intake Cowl on the

Engine 1 (4030EM1)

ROLLS-ROYCE Service Bulletin No.

RB.211-71-AG416

Detailed Inspection of the Air Intake Cowl on the

Engine 2 (4030EM2)

ROLLS-ROYCE Service Bulletin No.

RB.211-71-AG416

Task 713025-833-801-001: Repair

Get Access 2.00

On Aircraft

Replace the Air Intake Cowl of the Engine 1

(4030EM1)

6.00

Replace the Air Intake Cowl of the Engine 2

(4030EM2)

6.00

Close-Up 2.00

TOTAL MANHOURS 16.00

ELAPSED TIME (HOURS) 5.00

NOTE: For the elapsed time assumptions , refer to Appendix 02 .

H. WEIGHT AND BALANCE

Not Changed

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I. ELECTRICAL LOAD DATA

Not Changed

J. REFERENCES

Aircraft Maintenance Manual (AMM) 06-20-00 06-40-00 06-41-53

06-41-54 12-34-24 71-61-41

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

Vendor Service Bulletin (VSB) ROLLS-ROYCE Service Bulletin

No. RB.211-71-AG416

K. PUBLICATION AFFECTED

None

L. INTERCHANGEABILITY/MIXABILITY

Not Applicable

M. SPARES

None

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This Page Intentionally Left Blank

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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 Service Bulletin No. RB.211-71-AG416.

(2) Price and Availability

Refer to the vendor Service Bulletin ROLLS-ROYCE for the equipment modification

sales terms.

B. INDUSTRY SUPPORT INFORMATION

Refer to the Vendor Service Bulletin (VSB) for the industry support terms.

C. LIST OF COMPONENTS

No Kit

D. LIST OF MATERIALS - OPERATOR SUPPLIED

(1) Consumable Materials

To accomplish this TASK 713025-833-801 001 Repair , it is necessary to use the

expendable parts listed in the AMM 71-61-41, Page Block 401.

(2) Components

None

(3) Equipment

None

E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

None

F. TOOLING

(1) Tooling - Price and Availability

To accomplish this TASK 713025-833-801 001 Repair , it is necessary to use the tools

listed in AMM 71-61-41, Page Block 401.

(2) Tools

For intakes with a life greater than 5000FC since new, accomplish the initial inspection

of the primary structure within 24 months

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(3) Special Tools

None

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3. ACCOMPLISHMENT INSTRUCTIONS

Task 713025-832-801-001 - Inspection

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

INCLUDED IN THE REFERENCED PROCEDURES.

WARNING: YOU MUST BE CAREFUL WHEN YOU DO WORK ON THE ENGINE PARTS

AFTER THE ENGINE IS SHUTDOWN. THE ENGINE PARTS CAN STAY HOT

FOR ALMOST 1 HOUR.

CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP

ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY

AND MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENANCE

WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING,

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

THIS :

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

NECESSARY ON WIRING AND COMPONENTS.

- REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND

OTHER CONTAMINATION.

THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION

AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION.

IN CASE OF CONTAMINATION REFER TO ESPM 20-55-00.

Task Associated Data

Zone

411 421

Manpower

TOTAL MANHOURS 4.00

ELAPSED TIME (HOURS) 2.00

Additional manhours related to Vendor SB; refer to:

ROLLS-ROYCE Service Bulletin No. RB.211-71-AG416

A. GENERAL

(1) Subtask 713025-910-002-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-20-00, Page Block 001

06-40-00, Page Block 001

(a) For the identification of Zones (Refer to AMM 06-20-00, Page Block 001).

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SERVICE BULLETIN

(b) For the identification of access panels (Refer to AMM 06-40-00, Page Block 001).

(2) Subtask 713025-839-001-001 - 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 713025-941-001-001 - Job Set-up of the Engine 1 (4030EM1)

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

06-41-54, Page Block 001

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 the access platform(s) in position.

(c) Open the access door 811(Refer to AMM 06-41-53, Page Block 001).

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

PANEL DESIGNATION FIN LOCATION SEE

NOTES

722VU FADEC B ENG 1 13KS1 44 D

742VU FADEC A ENG 1 12KS1 73 Q

(e) Remove the access panel of the Thermal Anti Ice (TAI), 411AL (Refer to AMM

06-41-54, Page Block 001).

(f) Remove the access panel of the P20T20 probe, 411AR (Refer to AMM 06-41-54,

Page Block 001).

(2) Subtask 713025-941-002-001 - Job Set-up of the Engine 2 (4030EM2)

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

06-41-54, Page Block 001

Task 12-34-24-860-802

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

12-34-24-860-802).

(b) Put the access platform(s) in position.

(c) Open the access door 811 (Refer to AMM 06-41-53, Page Block 001).

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

PANEL DESIGNATION FIN LOCATION SEE

NOTES

722VU FADEC B ENG 2 13KS2 49 K

742VU FADEC A ENG 2 12KS2 74 Q

(e) Remove the access panel of the Thermal Anti Ice (TAI), 421AL (Refer to AMM

06-41-54, Page Block 001).

(f) Remove the access panel of the P20T20 probe, 421AR (Refer to AMM 06-41-54,

Page Block 001).

C. PROCEDURE

(1) Subtask 713025-220-001-001 - Detailed Inspection of the Air Intake Cowl on the

Engine 1 (4030EM1)

Work Zones and Access Panels

Zone Access/Work location

411

References

Vendor Service Bulletin (VSB) ROLLS-ROYCE RB.211-71-AG416

Fig. A-FBAAA

Area to be Inspected

Sheet 01

Fig. A-FBBAA

Flow Chart

Sheet 01

Sheet 02

Sheet 03

Sheet 04

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

(b) Do a detailed inspection, refer to Fig. A-FBBAA Sheet 01, Fig. A-FBBAA Sheet 02,

Fig. A-FBBAA Sheet 03, Fig. A-FBBAA Sheet 04 and refer to ROLLS-ROYCE

Service Bulletin No. RB.211-71-AG416.

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

(2) Subtask 713025-220-002-001 - Detailed Inspection of the Air Intake Cowl on the

Engine 2 (4030EM2)

Work Zones and Access Panels

Zone Access/Work location

421

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References

Vendor Service Bulletin (VSB) ROLLS-ROYCE RB.211-71-AG416

Fig. A-FBAAA

Area to be Inspected

Sheet 01

Fig. A-FBBAA

Flow Chart

Sheet 01

Sheet 02

Sheet 03

Sheet 04

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

(b) Do a detailed inspection, refer to Fig. A-FBBAA Sheet 01, Fig. A-FBBAA Sheet 02,

Fig. A-FBBAA Sheet 03, Fig. A-FBBAA Sheet 04 and refer to ROLLS-ROYCE

Service Bulletin No. RB.211-71-AG416.

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

D. TEST

None

E. CLOSE-UP

(1) Subtask 713025-942-001-001 - Close-up of the Engine 1 (4030EM1)

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

06-41-54, Page Block 001

(a) Install the access panel of the TAI, 411AL (Refer to AMM 06-41-54, Page Block

001).

(b) Install the access panel of the P20T20 probe, 411AR (Refer to AMM 06-41-54,

Page Block 001).

(c) Remove the safety clip tags and close these circuit breakers :

PANEL DESIGNATION FIN LOCATION SEE

NOTES

722VU FADEC B ENG 1 13KS1 44 D

742VU FADEC A ENG 1 12KS1 73 Q

(d) Close the access door 811 (Refer to AMM 06-41-53, Page Block 001).

(e) Remove the access platform(s).

(f) Restore the systems and the aircraft to normal operating condition.

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(2) Subtask 713025-942-002-001 - Close-up of the Engine 2 (4030EM2)

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

06-41-54, Page Block 001

(a) Install the access panel of the TAI, 421AL (Refer to AMM 06-41-54, Page Block

001).

(b) Install the access panel of the P20T20 probe, 421AR (Refer to AMM 06-41-54,

Page Block 001).

(c) Remove the safety clip tags and close these circuit breakers :

PANEL DESIGNATION FIN LOCATION SEE

NOTES

722VU FADEC B ENG 2 13KS2 49 K

742VU FADEC A ENG 2 12KS2 74 Q

(d) Close the access door 811 (Refer to AMM 06-41-53, Page Block 001).

(e) Remove the access platform(s).

(f) Restore the systems and the aircraft to normal operating condition.

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Task 713025-833-801-001 - Repair

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

INCLUDED IN THE REFERENCED PROCEDURES.

WARNING: YOU MUST BE CAREFUL WHEN YOU DO WORK ON THE ENGINE PARTS

AFTER THE ENGINE IS SHUTDOWN. THE ENGINE PARTS CAN STAY HOT

FOR ALMOST 1 HOUR.

CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP

ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY

AND MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENANCE

WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING,

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

THIS :

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

NECESSARY ON WIRING AND COMPONENTS.

- REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND

OTHER CONTAMINATION.

THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION

AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION.

IN CASE OF CONTAMINATION REFER TO ESPM 20-55-00.

Task Associated Data

Zone

411 421

Modified FIN

4030EM1 4030EM2

Manpower

TOTAL MANHOURS 16.00

ELAPSED TIME (HOURS) 5.00

A. GENERAL

(1) Subtask 713025-910-003-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-20-00, Page Block 001

06-40-00, Page Block 001

(a) For the identification of Zones (Refer to AMM 06-20-00, Page Block 001).

(b) For the identification of access panels (Refer to AMM 06-40-00, Page Block 001).

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(c) Tag the parts that you must remove and retain to make the subsequent installation

easier.

(d) Put all the retained hardware in identified plastic bags and attach the bags to the

related unit.

(2) Subtask 713025-839-002-001 - 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 713025-941-003-001 - Job Set-up of the Engine 1 (4030EM1)

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Task 12-34-24-860-802

Task 71-61-41-000-802

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

12-34-24-860-802).

(b) Put the access platform(s) in position.

(c) Open the access door 811 (Refer to AMM 06-41-53, Page Block 001).

(d) Do the job set-up procedure as specified in the removal of the air intake cowl

(Refer to AMM Task 71-61-41-000-802).

(2) Subtask 713025-941-004-001 - Job Set-up of the Engine 2 (4030EM2)

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Task 12-34-24-860-802

Task 71-61-41-000-802

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

12-34-24-860-802).

(b) Put the access platform(s) in position.

(c) Open the access door 811 (Refer to AMM 06-41-53, Page Block 001).

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(d) Do the job set-up procedure as specified in the removal of the air intake cowl

(Refer to AMM Task 71-61-41-000-802).

C. PROCEDURE

(1) Subtask 713025-960-001-001 - Replace the Air Intake Cowl of the Engine 1

(4030EM1)

Work Zones and Access Panels

Zone Access/Work location

411

Manpower Resources

Manhours 6.00

Minimum number of person 2

Subtask elapsed time 3

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 71-61-41-000-802

Task 71-61-41-400-802

(a) Remove the air intake cowl on the engine 4030EM1 (Refer to AMM Task

71-61-41-000-802).

(b) Install the new air intake cowl on the engine 4030EM1 (Refer to AMM Task

71-61-41-400-802).

NOTE: Replacement intake cowl shall have less than 5000FC or have

already been inspected without findings on the piccolo tube or links

and with cracks size on OBA and bulkhead within ADL.

(2) Subtask 713025-960-002-001 - Replace the Air Intake Cowl of the Engine 2

(4030EM2)

Work Zones and Access Panels

Zone Access/Work location

421

Manpower Resources

Manhours 6.00

Minimum number of person 2

Subtask elapsed time 3

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 71-61-41-000-802

Task 71-61-41-400-802

(a) Remove the air intake cowl on the engine 4030EM2 (Refer to AMM Task

71-61-41-000-802).

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(b) Install the new air intake cowl on the engine 4030EM2 (Refer to AMM Task

71-61-41-400-802).

NOTE: Replacement intake cowl shall have less than 5000FC or have

already been inspected without findings on the piccolo tube or links

and with cracks size on OBA and bulkhead within ADL.

D. TEST

None

E. CLOSE-UP

(1) Subtask 713025-942-003-001 - Close-up of the Engine 1 (4030EM1)

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Task 71-61-41-400-802

(a) Do the close-up procedure as specified in the installation of the air intake cowl

(Refer to AMM Task 71-61-41-400-802)

(b) Close the access door 811 (Refer to AMM 06-41-53, Page Block 001).

(c) Remove the access platform(s).

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

(2) Subtask 713025-942-004-001 - Close-up of the Engine 2 (4030EM2)

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Task 71-61-41-400-802

(a) Do the close-up procedure as specified in the installation of the air intake cowl

(Refer to AMM Task 71-61-41-400-802)

(b) Close the access door 811(Refer to AMM 06-41-53, Page Block 001).

(c) Remove the access platform(s).

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

DATE: Jan 10/11 SERVICE BULLETIN No.: A330-71-3025

REVISION No.: 00 - Jan 10/11 Page: 28

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SERVICE BULLETIN

**CONF ALL

A

A Z411 (Z421)

B

Z410

Z420

A

B

TUBE LINK

PICCOLO TUBE

BULKHEAD AND OBA

G_SB_713025_5_BAAA_01_01

Figure A-FBAAA - Sheet 01

Area to be Inspected

DATE: Jan 10/11 SERVICE BULLETIN No.: A330-71-3025

REVISION No.: 00 - Jan 10/11 Page: 29

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SERVICE BULLETIN

**CONF ALL

QUESTION

ACTION

FINDING

AT THE THRESHOLD AND INTERVAL GIVEN IN THE PLANNING INFORMATION

YES CRACKED OR NO

DO A DETAILED INSPECTION OF THE AIR INTAKE COWL PICCOLO

TUBE ON THE ENGINE AS SPECIFIED IN VSB No. RB.211−71−AG416

REPLACE THE AFFECTED INTAKE COWL

BEFORE NEXT FLIGHT

REFER TO TASK 713025−833−001

TUBE

FRACTURED

SEE SHEET 02

FROM SHEET 03

FROM SHEET 04

SEE SHEET 04

G_SB_713025_5_BBAA_01_03

Figure A-FBBAA - Sheet 01

Flow Chart

DATE: Jan 10/11 SERVICE BULLETIN No.: A330-71-3025

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@A330

SERVICE BULLETIN

**CONF ALL

QUESTION

ACTION

FINDING

YES FOUND NO

DO A DETAILED INSPECTION OF THE PICCOLO

TUBE LINKS AS SPECIFIED IN VSB No. RB.211−71−AG416

LINK(S)

BROKEN

SEE SHEET 03

INTAKE A

01

NB OF LINKS FOUND BROKEN

NOTE:

FROM SHEET 1

YES FOUND

1−3 LINK(S)

BROKEN

COWL 5000 FC NO YES OPPOSITE INTAKE YES LINKS FOUND NO

4 OR MORE

BROKEN

REPLACE THE INTAKE COWL

BEFORE NEXT FLIGHT DO A DETAILED INSPECTION OF THE OPPOSITE ENGINE

INTAKE COWL FOR PICCOLO TUBE AND BROKEN LINKS

AS SPECIFIED IN VSB No. RB.211−71−AG416 REFER TO TASK 713025−833−001

SEE SHEET 03

SEE NOTE FOR ACTIONS SEE SHEET 04 01

FOR INSPECTED

INTAKE COWL

INTAKE B

1

1

1

1

1

2

2

0

1

2 OR 3

4 OR MORE

BROKEN PICCOLO

0

1

2

3

4 OR MORE

BROKEN PICCOLO

0

1

2

3

4 OR MORE

BROKEN PICCOLO

2

2

2

2

3

3

3

3

3

3

ACTION FOR INTAKE A (INSPECTED INTAKE) ACTION FOR INTAKE B (OPPOSITE INTAKE)

SEE SHEET 03

BEFORE NEXT FLIGHT REPLACE A OR B − SEE SHEET 3 FOR REMAINING COWL

SEE SHEET 03

SEE SHEET 03

SEE SHEET 03

NO ACTION

REPLACE BEFORE NEXT FLIGHT

REPLACE BEFORE NEXT FLIGHT

REPLACE BEFORE NEXT FLIGHT

SEE SHEET 03

SEE SHEET 03

REPLACE WITHIN 100FC

REPLACE BEFORE NEXT FLIGHT

BEFORE NEXT FLIGHT REPLACE A OR B − REPLACE REMAINING COWL WITHIN 100FC

REPLACE BEFORE NEXT FLIGHT

REPLACE BEFORE NEXT FLIGHT

REPLACE BEFORE NEXT FLIGHT

REPLACE BEFORE NEXT FLIGHT

REPLACE BEFORE NEXT FLIGHT

BEFORE NEXT FLIGHT REPLACE A OR B − REPLACE REMAINING COWL WITHIN 100FC

SEE SHEET 03

SEE SHEET 03

REPLACE WITHIN 100FC

REPLACE WITHIN 100FC

REPLACE WITHIN 100FC

REPLACE WITHIN 100FC

REPLACE WITHIN 100FC

REPLACE BEFORE NEXT FLIGHT

REPLACE BEFORE NEXT FLIGHT

REPLACE WITHIN 100FC

REPLACE WITHIN 100FC

NO

NOTE:

FOR REPLACEMENT OF THE INTAKE COWL,

REFER TO SUBTASK 713025−833−001 AND SEE SHEET 4

G_SB_713025_5_BBAA_02_03

Figure A-FBBAA - Sheet 02

Flow Chart

DATE: Jan 10/11 SERVICE BULLETIN No.: A330-71-3025

REVISION No.: 00 - Jan 10/11 Page: 31

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SERVICE BULLETIN

**CONF ALL

QUESTION

ACTION

FINDING

DO A DETAILED INSPECTION OF THE OUTER BONDARY ANGLE (OBA)

AND BULKHEAD AS SPECIFIED IN VSB No. RB.211−71−AG416

FROM SHEET 04

YES DAMAGE LIMIT AS DEFINED IN NO

WITHIN ALLOWED

VSB No. RB.211−71−AG416

REPLACE THE AFFECTED

BEFORE NEXT FLIGHT

INTAKE COWL

REFER TO

SUBTASK 713025−833−001

SEND TO AIRBUS INSPECTION REPORT

REPEAT THE PICCOLO TUBE AND

LINK INSPECTIONS EVERY 2500FC

REFER TO APPENDIX 1

SEE SHEET 01

REPEAT THE OBA AND

BULKHEAD INSPECTION AT THE

INTERVAL DEFINED IN THE

VSB No. RB.211−71−AG416

AND

CRACK 22 in (558.8 mm)

YES NO

OBA

REPLACE THE AFFECTED

WITHIN 100FC

INTAKE COWL

REFER TO

CRACK 13 in (330.2 mm)

OR BULKHEAD

SUBTASK 713025−833−001

FROM SHEET 02

SEE SHEET 04

AS PER VSB No. RB.211−71−AG416

G_SB_713025_5_BBAA_03_02

Figure A-FBBAA - Sheet 03

Flow Chart

DATE: Jan 10/11 SERVICE BULLETIN No.: A330-71-3025

REVISION No.: 00 - Jan 10/11 Page: 32

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SERVICE BULLETIN

**CONF ALL

QUESTION

ACTION

FINDING

FROM SHEET 03

NO INTAKE COWL HAS ACCUMULATED YES

REPLACEMENT

MORE THAN 5000FC

INSPECTION REPORT

REPEAT THE PICCOLO TUBE

 AND LINK INSPECTIONS

REFER TO APPENDIX 1

REPEAT THE OBA AND

BULKHEAD INSPECTION AT THE

INTERVAL DEFINED IN THE

VSB No. RB.211−71−AG416

AND

FROM SHEET 02

FROM SHEET 01

SEND TO AIRBUS

SEE SHEET 01

EVERY 2500FC AS PER

VSB No. RB.211−71−AG416

INSPECTION REPORT

REFER TO APPENDIX 1

SEND TO AIRBUS

SEE SHEET 03

INSPECTION REPORT

REFER TO APPENDIX 1

SEND TO AIRBUS

SEE SHEET 01

NOTE:

REPLACEMENT INTAKE COWL SHALL HAVE LESS THAN 5000FC OR HAVE ALREADY BEEN INSPECTED

WITHOUT FINDINGS ON THE PICCOLO TUBE OR LINKS AND WITH

CRACKS SIZE ON OBA AND BULKHEAD WITHIN ADL G_SB_713025_5_BBAA_04_01

Figure A-FBBAA - Sheet 04

Flow Chart

DATE: Jan 10/11 SERVICE BULLETIN No.: A330-71-3025

REVISION No.: 00 - Jan 10/11 Page: 33

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SERVICE BULLETIN

This Page Intentionally Left Blank

DATE: Jan 10/11 SERVICE BULLETIN No.: A330-71-3025

REVISION No.: 00 - Jan 10/11 Page: 34

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@A330

SERVICE BULLETIN

Appendix 01

**CONF ALL

(1) Inspection Report

(a) 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 sheet.

DATE: Jan 10/11 SERVICE BULLETIN No.: A330-71-3025

REVISION No.: 00 - Jan 10/11 Page: 1

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@A330

SERVICE BULLETIN

Appendix 01

**CONF ALL

INSPECTION REPORT

SERVICE BULLETIN No. :

A/C MSN :

FLIGHT CYCLES :

FLIGHT HOURS :

A330−71−3025

DATE OF INSPECTION :

RETURN TO :

AIRBUS

CUSTOMER SERVICES ENGINEERING − SEEE1

PROPULSION SYSTEMS RR, IAE

INSPECTION METHOD :

1 ROND POINT MAURICE BELLONTE

31707 BLAGNAC CEDEX

FRANCE

FAX +33 (0)5 61 93 36 14 DETAILED INSPECTION

AIR INTAKE COWL OF THE ENGINE 1 (4030EM1)

INSPECTION PERFORMED NO YES

PICCOLO TUBE CRACKED NO YES

LINK BROKEN NO YES

1 LINK BROKEN

2 OR 3 LINKS BROKEN

4 OR MORE LINKS BROKEN

OBA/BULKHEAD CRACKED NO YES

WITHIN ALLOWED DAMAGE LIMIT

OBA CRACK 22 in (558.8 mm)

BULKHEAD CRACK 13 in (330.2 mm)

AIR INTAKE COWL REPLACED NO YES

AIR INTAKE COWL OF THE ENGINE 2 (4030EM2)

INTAKE 5000FC INTAKE 5000FC

INSPECTION PERFORMED NO YES

PICCOLO TUBE CRACKED NO YES

LINK BROKEN NO YES

1 LINK BROKEN

2 OR 3 LINKS BROKEN

4 OR MORE LINKS BROKEN

OBA/BULKHEAD CRACKED NO YES

WITHIN ALLOWED DAMAGE LIMIT

OBA CRACK 22 in (558.8 mm)

BULKHEAD CRACK 13 in (330.2 mm)

AIR INTAKE COWL REPLACED NO YES

INTAKE 5000FC INTAKE 5000FC

G_SB_713025_5_AAAA_01_02

Figure A-FAAAA - Sheet 01

Inspection Report

DATE: Jan 10/11 SERVICE BULLETIN No.: A330-71-3025

REVISION No.: 00 - Jan 10/11 Page: 2

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SERVICE BULLETIN

Appendix 01

**CONF ALL

A

A Z411 (Z421)

B

Z410

Z420

A

B

G_SB_713025_5_AAAA_02_00

C D

Figure A-FAAAA - Sheet 02

Inspection Report

DATE: Jan 10/11 SERVICE BULLETIN No.: A330-71-3025

REVISION No.: 00 - Jan 10/11 Page: 3

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SERVICE BULLETIN

Appendix 01

**CONF ALL

650 mm

(25.59 in)

729 mm

(28.70 in)

570 mm

(22.44 in)

600 mm

(23.62 in)

790 mm

(31.10 in)

620 mm

(24.41 in)

820 mm

(32.28 in)

800 mm

(31.50 in)

600 mm

(23.62 in)

01 INTERMEDIAIRE LINK.

02 MAIN LINK.

NOTE:

01

01

01

01

01

01

02

02

02

02

02

02

RAD 150 RAD 157.5

RAD 132.5

RAD 103.2

RAD 72

RAD 45

RAD 18

RAD 342

RAD 315

RAD 279

RAD 256.7

RAD 214.2

RAD 184

G_SB_713025_5_AAAA_03_00

650 mm

(25.59 in)

780 mm

(30.71 in)

180 mm

(7.09 in)

C

PICCOLO TUBE

Figure A-FAAAA - Sheet 03

Inspection Report

DATE: Jan 10/11 SERVICE BULLETIN No.: A330-71-3025

REVISION No.: 00 - Jan 10/11 Page: 4

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@A330

SERVICE BULLETIN

Appendix 01

**CONF ALL

G_SB_713025_5_AAAA_04_00

650 mm

(25.59 in)

720 mm

(28.35 in)

650 mm

(25.59 in)

600 mm

(23.62 in)

800 mm

(31.50 in)

600 mm

(23.62 in)

800 mm

(31.50 in)

800 mm

(31.50 in)

800 mm

(31.50 in)

600 mm

(23.62 in)

600 mm

(23.62 in)

01 INTERMEDIAIRE LINK.

02 MAIN LINK.

NOTE:

01

01

01

01

01

01

02

02

02

02

02

02

RAD 150

RAD 157.5

RAD 132.5

RAD 103.2

RAD 72

RAD 45

RAD 18

RAD 342

RAD 315

RAD 279

RAD 256.7

RAD 214.2

RAD 184

FWD BULKHEAD

D

Figure A-FAAAA - Sheet 04

Inspection Report

DATE: Jan 10/11 SERVICE BULLETIN No.: A330-71-3025

REVISION No.: 00 - Jan 10/11 Page: 5

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SERVICE BULLETIN

Appendix 01

This Page Intentionally Left Blank

DATE: Jan 10/11 SERVICE BULLETIN No.: A330-71-3025

REVISION No.: 00 - Jan 10/11 Page: 6

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SERVICE BULLETIN

Appendix 02

**CONF ALL

(1) Refer to the subsequent Gantt Chart for the detail concerning the elapsed time assumptions.

DATE: Jan 10/11 SERVICE BULLETIN No.: A330-71-3025

REVISION No.: 00 - Jan 10/11 Page: 1

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SERVICE BULLETIN

Appendix 02

**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)

16.00

5.00

STEPS

0 3

GET ACCESS ENGINE 1 1.00 1.00 1

CLOSE−UP ENGINE 1 1.00 1.00 1

6.00 3.00 2 REPLACE AIR INTAKE COWL

ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A330−71−3025

1 2

1.00 1.00 1

1.00 1.00 1

6.00 3.00 2

ENGINE 1

4 5

G_SB_713025_5_ABAA_01_00

GET ACCESS ENGINE 2

CLOSE−UP ENGINE 2

REPLACE AIR INTAKE COWL

ENGINE 2

Figure A-FABAA - Sheet 01

Gantt Chart

DATE: Jan 10/11 SERVICE BULLETIN No.: A330-71-3025

REVISION No.: 00 - Jan 10/11 Page: 2

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SERVICE BULLETIN

REPORTING SHEET

TITLE: INSPECTION ON TRENT 700 OF THE AIR INLET COWL FOR PICCOLO

TUBE FRACTURE

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: Jan 10/11 SERVICE BULLETIN No.: A330-71-3025

REVISION No.: 00 - Jan 10/11 Page: 1

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SERVICE BULLETIN

QUALITY PERCEPTION FORM

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

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

improve the quality of our Service Bulletins.

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

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

- Quality rating of this SB 4 3 2 1

- Quality rating of the Accomplishment Instructions 4 3 2 1

- Quality rating of the Illustrations 4 3 2 1

- 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 10/11 SERVICE BULLETIN No.: A330-71-3025

REVISION No.: 00 - Jan 10/11 Page: 1

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