@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: 53

TITLE: FUSELAGE - CENTER FUSELAGE - INSPECTION OF RODS IN BELLY

FAIRING

MODIFICATION No.: None

This page transmits Revision No.01 of Service Bulletin No.A330-53-3186

ADDITIONAL WORK

**CONF ALL

No additional work is required by this revision for aircraft modified by any previous issue.

REASON

Revision No. 01 issued to redefine item numbers of the rods at FR39.

CHANGES

SUMMARY

EFFECTIVITY OPERATOR LIST UPDATED R

Fig. A-FSAAA

Fig. A-FSAAA Sheet 01 SHEET UPDATED R

PLANNING INFORMATION

EFFECTIVITY EFFECTIVITY RELATED INFORMATION

UPDATED

R

ACCOMPLISHMENT INSTRUCTIONS

TASK 533186- 832-801-001-Inspection

Subtask 533186-020-003-001 SUBTASK SOLUTION ADDED N

Subtask 533186-020-004-001 SUBTASK SOLUTION ADDED N

Subtask 533186-420-001-001 SUBTASK SOLUTION ADDED N

Subtask 533186-420-002-001 SUBTASK SOLUTION ADDED N

TASK 533186- 832-802-001-Inspection

Subtask 533186-020-001-001 SUBTASK SOLUTION ADDED N

Subtask 533186-020-002-001 SUBTASK SOLUTION ADDED N

DATE: Jan 17/11 SERVICE BULLETIN No.: A330-53-3186

REVISION No.: 01 - Apr 07/11 Page: 1

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@A330

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Subtask 533186-833-001-001 SUBTASK SOLUTION UPDATED

PART NUMBER UPDATED

ITEM NUMBER UPDATED

MATERIAL LIST UPDATED

R

Subtask 533186-833-002-001 SUBTASK SOLUTION UPDATED

PART NUMBER UPDATED

ITEM NUMBER UPDATED

MATERIAL LIST UPDATED

R

Subtask 533186-420-003-001 SUBTASK SOLUTION ADDED N

Subtask 533186-420-004-001 SUBTASK SOLUTION ADDED N

Fig. A-FBAAA

Fig. A-FBAAA Sheet 01 SHEET UPDATED R

Fig. A-FBBAA

Fig. A-FBBAA Sheet 01 SHEET UPDATED R

Fig. A-FBCAA

Fig. A-FBCAA Sheet 01 SHEET UPDATED R

Fig. A-FBCAA Sheet 02 SHEET UPDATED R

Fig. A-FBDAA FIGURE SOLUTION ADDED N

Fig. A-FBDAA Sheet 01 SHEET ADDED N

Appendix 01

Fig. A-FAAAA

Fig. A-FAAAA Sheet 02 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: Jan 17/11

REVISION No. : 01 - Apr 07/11

DATE: Jan 17/11 SERVICE BULLETIN No.: A330-53-3186

REVISION No.: 01 - Apr 07/11 Page: 2

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@A330

SERVICE BULLETIN

SUMMARY

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

This summary is for information only and is not approved for modification of the aircraft.

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 53

TITLE: FUSELAGE - CENTER FUSELAGE - INSPECTION OF RODS IN BELLY

FAIRING

**CONF ALL

MODIFICATIONS

None

REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES

A rod manufacturing process defect has been identified at TAC that could have led to deliver rods with

cracks (crimped end of the rod only).

This Inspection Service Bulletin (ISB) requires to inspect some rods in the belly fairing. Those rods can

be manufactured by either SARMA-SKF or by TAC.

- If they are manufactured by SARMA-SKF, no further action is required.

- If they are manufactured by TAC, it is mandatory within 6 years from the ISB issuance to perform a

Non Destructive Test (NDT) inspection at the crimped end of the rod body.

Cracked TAC rods must be replaced.

Accomplishment of this ISB will prevent any cracks on rods installed on the belly fairing.

GENERAL EVALUATION

EVALUATION TABLE

COMPLIANCE MANDATORY (1) CANCELS INSPECTION SB NO

POTENTIAL AD YES A/C OPERATION AFFECTED NO

RELIABILITY AFFECTED NO PAX COMFORT AFFECTED NO

COST SAVING NO ETOPS AFFECTED NO

STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED NO

NOTE (1): Service Bulletin must be accomplished.

DATE: Jan 17/11 SERVICE BULLETIN No.: A330-53-3186

REVISION No.: 01 - Apr 07/11 Page: 1

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@A330

SERVICE BULLETIN

SUMMARY

MATERIAL PRICE INFORMATION

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Component COMPA01 1 See SB Rod

Component COMPA02 1 See SB Pin

EFFECTIVITY

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

46W 78V 97X 99Y AAR AAW ACA ACI AEA AFL AFR ALK ARA

ASY AVA AZA BEC BEL BMA BTV CAL CCA CES CHH CPA CRK

CRL CSC CSN CYP DAH DAL DGA DLH EDW EIN ETD EVA FIN

FWI GFA GIA GRL HAL HDA HFY HVN I2L IAC ISS IWD IYE

JAI JST KAL KFR KKK KLM LTU LVG MAS MAU MEA MON MSR

MYT OBS OHY OMA PAL QAF QFA QTR RJA RSF SAS SGX SIA

STZ SWR TAM TAP TCX THA THY TSC UAE UAF USA VKG VLK

VOZ XAX XLF

CONCURRENT REQUIREMENTS

None

REFERENCES / REPERCUSSIONS

TFU None

OEB None

AOT None

SIL None

LINE MAINTENANCE AFFECTED No

LIFE LIMIT None

OTHER None

NATURE OF THE WORK

AIRCRAFT YES

EQUIPMENT NO

HARD NO

SOFT NO

OBRM NO

MANPOWER

Task 533186-832-801-001: Inspection

TOTAL MANHOURS 7.25

ELAPSED TIME (HOURS) 7.25

Task 533186-832-802-001: Inspection

TOTAL MANHOURS 13.00

DATE: Jan 17/11 SERVICE BULLETIN No.: A330-53-3186

REVISION No.: 01 - Apr 07/11 Page: 2

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@A330

SERVICE BULLETIN

SUMMARY

Task 533186-832-802-001: Inspection

ELAPSED TIME (HOURS) 13.00

APPENDICES

Appendix 01

DATE: Jan 17/11 SERVICE BULLETIN No.: A330-53-3186

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@A330

SERVICE BULLETIN

SUMMARY

**CONF ALL

A

Z190

FR37

FR39

FR48

FR53.2

FR53.9

B

B

B B

B

B

B B

B

A

MANUFACTURER AND PN TO BE IDENTIFIED

B TYPICAL

C

C

G_SB_533186_5_SAAA_01_02

Figure A-FSAAA - Sheet 01

DATE: Jan 17/11 SERVICE BULLETIN No.: A330-53-3186

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@A330

SERVICE BULLETIN

SUMMARY

**CONF ALL

AREA TO BE

TYPICAL CRACK

INSPECTED

LOCATION

TYPICAL

C

G_SB_533186_5_SAAA_02_00

Figure A-FSAAA - Sheet 02

DATE: Jan 17/11 SERVICE BULLETIN No.: A330-53-3186

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@A330

SERVICE BULLETIN

SUMMARY

This Page Intentionally Left Blank

DATE: Jan 17/11 SERVICE BULLETIN No.: A330-53-3186

REVISION No.: 01 - Apr 07/11 Page: 6

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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: 53

TITLE: FUSELAGE - CENTER FUSELAGE - INSPECTION OF RODS IN BELLY

FAIRING

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

330-202 330-203 330-223 330-243 330-301 330-302 330-303 330-321

330-322 330-323 330-341 330-342 330-343

(2) Effectivity by MSN

0012 0017 0030 0037 0045 0050 0054-0055 0059-0060 0062 0064-0067 0069-0073

0077 0082-0083 0086-0087 0095-0096 0098-0100 0102 0106-0107 0109-0113 0116

0118-0122 0127 0132 0138 0140 0143-0144 0148 0153 0155 0162 0165 0171-0172

0177 0181 0183-0184 0188-0189 0191 0195 0198 0200 0203 0205-0206 0209 0211

0219 0222-0224 0226 0229-0232 0234 0238 0240-0241 0244 0247-0251 0253-0256

0258-0259 0261-0262 0265-0267 0269 0271-0272 0275-0277 0279 0281 0283-0288

0290-0291 0293-0296 0299-0301 0303 0305-0306 0308-0309 0311-0317 0320

0322-0324 0326 0328 0330 0333-0334 0337-0340 0342-0346 0348-0351 0353

0356-0358 0361-0362 0364-0366 0368-0370 0372 0375 0380 0382 0384 0386

0388-0389 0392-0393 0396-0398 0400-0401 0403-0405 0407-0409 0412 0418-0423

0425 0427-0428 0432 0437 0439 0441 0443-0444 0448 0451-0452 0454-0456 0458

0461-0463 0465-0466 0469 0472-0473 0476-0477 0479-0481 0484 0486-0487

0489-0491 0493-0494 0496-0498 0500-0513 0515-0516 0518-0519 0521-0522

DATE: Jan 17/11 SERVICE BULLETIN No.: A330-53-3186

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@A330

SERVICE BULLETIN

0524-0527 0529-0530 0532-0533 0535-0536 0539 0542 0548-0553 0555 0558

0564-0565 0567-0568 0570-0571 0573-0574 0576 0578-0579 0581 0584 0587-0588

0591 0593 0595 0597 0600 0602-0603 0605 0607 0609-0610 0612 0614 0616 0618

0620-0621 0623 0625 0627 0629 0631-0638 0640-0642 0644-0645 0647-0650

0652-0659 0661-0667 0669-0671 0673-0676 0678-0680 0682-0684 0686-0688

0690-0693 0695-0697 0699-0701 0703-0705 0707-0709 0711-0714 0716-0718

0720-0722 0724-0726 0728-0730 0732-0735 0737-0739 0741-0743 0745-0747

0749-0752 0754-0756 0758-0760 0769-0770 0772-0774 0776-0778 0780-0782

0784-0786 0788-0789 0791-0792 0795-0797 0799 0801-0803 0805-0807 0809-0811

0813-0815 0817-0828 0830-0834 0836 0838-0843 0845 0847 0849-0855 0857-0863

0865-0869 0871 0873-0877 0879 0881-0885 0887-0893 0895-0896 0898-0901

0903-0909 0911 0913-0916 0918-0920 0922-0923 0925-0928 0930-0932 0934-0937

0939-0952 0954 0956-0959 0961-0971 0973-0980 0982-0986 0988-0992 0994-0995

0997-1003 1006-1016 1018-1023 1025-1026 1028-1029 1031 1033-1038 1041-1049

1052-1053 1055 1057-1058 1060-1061 1063 1065-1067 1069 1071-1078 1080-1082

1084-1090 1093-1101 1103-1104 1106

(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

46W 0871 0925

78V 1033 1046

97X 1053

99Y 0747 0951

AAR 0640 0676 0708 0772 0803 0845 1001 1055

AAW 0999 1043

ACA 0277 0279 0284 0344 0400 0408 0412 0419

ACI 0507 0510

AEA 0461 0733 0745 0749 0814 0931 0950

AFL 0963 0973 1014 1045 1047 1058 1065 1072 1077 1103

AFR 0422 0443 0448 0458 0465 0481 0498 0500 0502 0503 0516 0519

0567 0584 0657

ALK 0303 0306 0311 0313 0404

ARA 1002

ASY 0969 1036

AVA 0948 0967 1009 1016 1073

AZA 0272 0339

BEC 0863

BEL 0030 0037 0045 0082 0095

BMA 0398 0401

BTV 0205 0330

CAL 0602 0607 0641 0671 0675 0691 0699 0707 0714 0725 0752 0769

0805 0823 0838 0861 0920

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

0884 0890 0903 0909 0930 0941 0944 0957 1087

DATE: Jan 17/11 SERVICE BULLETIN No.: A330-53-3186

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@A330

SERVICE BULLETIN

OPERATOR MSN

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 1034

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

CRK 1031 1042

CRL 0285 0320

CSC 1082

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

0958 0964 1096

CYP 0505 0526

DAH 0644 0647 0650 0653 0667

DAL 0524 0533 0542 0549 0552 0578 0588 0591 0609 0614 0618 0620

0621 0631 0633 0663 0674 0690 0718 0722 0778 0784 0796 0799

0806 0817 0827 0843 0857 0858 0859 0865

DGA 0240

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

0913 0922 0989

EDW 0291

EIN 0059 0269 0397 0841 0847 0985 1025 1106

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

0854 0868 0975 0991 1071 1081

EVA 0530 0535 0555 0573 0587 0634 0655 0661 0678 0693 0755

FIN 0994 1007 1013 1023 1067 1078 1088

FWI 0253 0758 0965 1021

GFA 0276 0281 0286 0287 0334 0340 0527 0529 0532 0992

GIA 0138 0140 0144 0148 0153 0165 0988 1020 1028 1052

GRL 0230

HAL 1104

HDA 0083 0099 0106 0109 0132 0234 0405 0479 0512 0581 0654 0662

0692 0716 0741 0786

HFY 0096 1008

HVN 0087 0255 0262 0275 0294 0299 0366 0943 0962 1019

I2L 0211

IAC 0353 0362

ISS 0665 0802 0822

IWD 0670 1097

IYE 0625 0627 0632

JAI 0751 0807 0825 0831 0882 0885 0888 0901 0923 0932 0947 0956

JST 0506 0508 0513 0522 0842 0853 0940 0945

KAL 0162 0172 0206 0219 0222 0226 0241 0256 0258 0267 0338 0350

0351 0368 0425 0428 0484 0490 0550

KFR 0874 0891 0927 0939 0946

KKK 0343 0358 0364

KLM 0682 0686 0703 0738 0770 0801 0811 0819 0834 0900

DATE: Jan 17/11 SERVICE BULLETIN No.: A330-53-3186

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SERVICE BULLETIN

OPERATOR MSN

LTU 0120 0127 0171 0403 0432 0444 0454 0469 0476 0493 0739 0828

0911

LVG 0551 0597

MAS 0067 0069 0073 0077 0100 0107 0110 0116 0119 0290 0296 0300

MAU 0883 1057

MEA 0926 0984 0995 0998

MON 0261 0265

MSR 0600 0610 0666 0683 0696 0709 0726

MYT 0349

OBS 0833

OHY 0072 0098 0143

OMA 1038 1044 1049 1063 1093

PAL 0183 0184 0188 0189 0191 0198 0200 0203

QAF 0487 0605

QFA 0553 0558 0564 0574 0593 0595 0603 0695 0705 0712 0887 0892

0898 0976 1061 1094

QTR 0441 0473 0489 0511 0521 0571 0612 0616 0623 0637 0638 0659

0680 0684 0711 0721 0734 0743 0746 0760 0789 0792 0813 0820

0826 0849 0893 0907 0918

RJA 0970 0979

RSF 0980

SAS 0496 0497 0515 0568

SGX 0407

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

STZ 0324

SWR 0229 0249 0288 0322 1000 1018 1026 1029 1084 1089 1101

TAM 0232 0238 0247 0259 0361 0466 0472 0477 0486 0700 0869 0876

0949 0961 0968 0977

TAP 0181 0195 0223 0305 0308 0312 0317 0877 0899 0904 0914 0934

TCX 0254 0266 0301 0427 0456 0795

THA 0050 0060 0062 0064 0065 0066 0112 0122 0209 0224 0231 0346

0990 1003 1035 1037 1060 1074 1086 1090

THY 0463 0504 0697 0704 0742 0754 0774

TSC 0111 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

USA 0315 0323 0333 0337 0342 0370 0375 0380 0388 1011 1022 1041

1069 1076 1095 1100

VKG 0309 0356 0357

VLK 0055 0070 0086

VOZ 0365 0372

XAX 0054 0952 0974 1048 1066 1075

XLF 0501 0635

DATE: Jan 17/11 SERVICE BULLETIN No.: A330-53-3186

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SERVICE BULLETIN

(4) Configuration by MSN

MSN CONFIGURATION

0012 0017 0030 0037 0045 0050 0054 0055 0059 0060 0062

0064 0065 0066 0067 0069 0070 0071 0072 0073 0077 0082

0083 0086 0087 0095 0096 0098 0099 0100 0102 0106 0107

0109 0110 0111 0112 0113 0116 0118 0119 0120 0121 0122

0127 0132 0138 0140 0143 0144 0148 0153 0155 0162 0165

0171 0172 0177 0181 0183 0184 0188 0189 0191 0195 0198

0200 0203 0205 0206 0209 0211 0219 0222 0223 0224 0226

0229 0230 0231 0232 0234 0238 0240 0241 0244 0247 0248

0249 0250 0251 0253 0254 0255 0256 0258 0259 0261 0262

0265 0266 0267 0269 0271 0272 0275 0276 0277 0279 0281

0283 0284 0285 0286 0287 0288 0290 0291 0293 0294 0295

0296 0299 0300 0301 0303 0305 0306 0308 0309 0311 0312

0313 0314 0315 0316 0317 0320 0322 0323 0324 0326 0328

0330 0333 0334 0337 0338 0339 0340 0342 0343 0344 0345

0346 0348 0349 0350 0351 0353 0356 0357 0358 0361 0362

0364 0365 0366 0368 0369 0370 0372 0375 0380 0382 0384

0386 0388 0389 0392 0393 0396 0397 0398 0400 0401 0403

0404 0405 0407 0408 0409 0412 0418 0419 0420 0421 0422

0423 0425 0427 0428 0432 0437 0439 0441 0443 0444 0448

0451 0452 0454 0455 0456 0458 0461 0462 0463 0465 0466

0469 0472 0473 0476 0477 0479 0480 0481 0484 0486 0487

0489 0490 0491 0493 0494 0496 0497 0498 0500 0501 0502

0503 0504 0505 0506 0507 0508 0509 0510 0511 0512 0513

0515 0516 0518 0519 0521 0522 0524 0525 0526 0527 0529

0530 0532 0533 0535 0536 0539 0542 0548 0549 0550 0551

0552 0553 0555 0558 0564 0565 0567 0568 0570 0571 0573

0574 0576 0578 0579 0581 0584 0587 0588 0591 0593 0595

0597 0600 0602 0603 0605 0607 0609 0610 0612 0614 0616

0618 0620 0621 0623 0625 0627 0629 0631 0632 0633 0634

0635 0636 0637 0638 0640 0641 0642 0644 0645 0647 0648

0649 0650 0652 0653 0654 0655 0656 0657 0658 0659 0661

0662 0663 0664 0665 0666 0667 0669 0670 0671 0673 0674

0675 0676 0678 0679 0680 0682 0683 0684 0686 0687 0688

0690 0691 0692 0693 0695 0696 0697 0699 0700 0701 0703

0704 0705 0707 0708 0709 0711 0712 0713 0714 0716 0717

0718 0720 0721 0722 0724 0725 0726 0728 0729 0730 0732

0733 0734 0735 0737 0738 0739 0741 0742 0743 0745 0746

0747 0749 0750 0751 0752 0754 0755 0756 0758 0759 0760

0769 0770 0772 0773 0774 0776 0777 0778 0780 0781 0782

0784 0785 0786 0788 0789 0791 0792 0795 0796 0797 0799

0801 0802 0803 0805 0806 0807 0809 0810 0811 0813 0814

0815 0817 0818 0819 0820 0821 0822 0823 0824 0825 0826

0827 0828 0830 0831 0832 0833 0834 0836 0838 0839 0840

0841 0842 0843 0845 0847 0849 0850 0851 0852 0853 0854

0855 0857 0858 0859 0860 0861 0862 0863 0865 0866 0867

0868 0869 0871 0873 0874 0875 0876 0877 0879 0881 0882

0883 0884 0885 0887 0888 0889 0890 0891 0892 0893 0895

0896 0898 0899 0900 0901 0903 0904 0905 0906 0907 0908

0909 0911 0913 0914 0915 0916 0918 0919 0920 0922 0923

001

DATE: Jan 17/11 SERVICE BULLETIN No.: A330-53-3186

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@A330

SERVICE BULLETIN

MSN CONFIGURATION

0925 0926 0927 0928 0930 0931 0932 0934 0935 0936 0937

0939 0940 0941 0942 0943 0944 0945 0946 0947 0948 0949

0950 0951 0952 0954 0956 0957 0958 0959 0961 0962 0963

0964 0965 0966 0967 0968 0969 0970 0971 0973 0974 0975

0976 0977 0978 0979 0980 0982 0983 0984 0985 0986 0988

0989 0990 0991 0992 0994 0995 0997 0998 0999 1000 1001

1002 1003 1006 1007 1008 1009 1010 1011 1012 1013 1014

1015 1016 1018 1019 1020 1021 1022 1023 1025 1026 1028

1029 1031 1033 1034 1035 1036 1037 1038 1041 1042 1043

1044 1045 1046 1047 1048 1049 1052 1053 1055 1057 1058

1060 1061 1063 1065 1066 1067 1069 1071 1072 1073 1074

1075 1076 1077 1078 1080 1081 1082 1084 1085 1086 1087

1088 1089 1090 1093 1094 1095 1096 1097 1098 1099 1100

1101 1103 1104 1106

001

(5) Configuration definition

**CONF 001

Configuration 001 is valid for all the aircraft given in the effectivity of this Service Bulletin

as a standard configuration.

(6) Material Effectivity

MATERIAL QTY PER A/C SEE NOTES

Component COMPA01 1

Component COMPA02 1

Consumable CMLA01 As required

B. CONCURRENT REQUIREMENTS

None

C. REASON

(1) History

A rod manufacturing process defect has been identified at TAC that could have led to

deliver rods with cracks (crimped end of the rod only).

(2) Objective/Action

This Inspection Service Bulletin (ISB) requires to inspect some rods in the belly fairing.

Those rods can be manufactured by either SARMA-SKF or by TAC.

- If they are manufactured by SARMA-SKF, no further action is required.

- If they are manufactured by TAC, it is mandatory within 6 years from the ISB

issuance to perform a Non Destructive Test (NDT) inspection at the crimped end of

the rod body.

Cracked TAC rods must be replaced.

DATE: Jan 17/11 SERVICE BULLETIN No.: A330-53-3186

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SERVICE BULLETIN

(3) Advantages

Accomplishment of this ISB will prevent any cracks on rods installed on the belly fairing.

(4) Operational/Maintenance Consequences

None

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

Task 533186-832-801-001: Inspection

(1) Do a One Time Detailed Inspection of the Rods

Task 533186-832-802-001: Inspection

(1) Do a HFEC Inspection of the TAC Rods

(2) Replace the Upper Rods of the Belly Fairing Structure at FR39

(3) Replace the Lateral Rods of the Belly Fairing Structure at FR39

(4) Replace the Lateral Rods of the Belly Fairing Structure at FR47

(5) Replace the Central Rod of the Belly Fairing Structure at FR47

(6) Replace the Upper Rods of the Belly Fairing Structure at FR53.2

(7) Replace the Lateral Rods of the Belly Fairing Structure at FR53.2

(8) Replace the Center Rods of the Belly Fairing Structure at FR53.2

(9) Replace the Upper Rods of the Belly Fairing Structure at FR53.4

(10) Replace the Lateral Rods of the Belly Fairing Structure at FR53.4

(11) Replace the Lateral Rods of the Belly Fairing Structure at FR53.9

(12) Replace the Rods of the Supports of the MLG Door Uplock at FR48

E. COMPLIANCE

(1) Classification

MANDATORY: Service Bulletin must be accomplished.

DATE: Jan 17/11 SERVICE BULLETIN No.: A330-53-3186

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SERVICE BULLETIN

(2) Accomplishment Timescale

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 given below but

reference should be made to the AD for confirmation of the mandated accomplishment

timescale.

COMPLIANCE TIME (whichever occurs

first)

CONDITION ACTION

THRESHOLD GRACE PERIOD

REPETITIVE

INTERVAL NOT

TO EXCEED

(whichever occurs

first)

CONF 001 Inspect in

accordance with

SUBTASK

533186-832-001

001 Do a One

Time Detailed

Inspection of the

Rods .

Not later than six

years from SB

issuance

- Not applicable

TAC rod found or

manufacturer

cannot be

identified

Do a HFEC

inspection of the

rod in accordance

with SUBTASK

533186-832-003

001 Do a HFEC

Inspection of the

TAC Rods .

Not later than six

years from SB

issuance (See

NOTE)

- Not applicable

Other manufacturer

rod found

No further action. - - -

DATE: Jan 17/11 SERVICE BULLETIN No.: A330-53-3186

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SERVICE BULLETIN

COMPLIANCE TIME (whichever occurs

first)

CONDITION ACTION

THRESHOLD GRACE PERIOD

REPETITIVE

INTERVAL NOT

TO EXCEED

(whichever occurs

first)

If the manufacturer

of the new rod to

be installed is not

TAC, replace the

rod in accordance

with SUBTASK

533186-833-001

001 Replace the

Upper Rods of the

Belly Fairing

Structure at FR39

thru SUBTASK

533186-833-011

001 Replace the

Rods of the

Supports of the

MLG Door Uplock

at FR48

Crack(s) found

If the manufacturer

of the new rod to

be installed is

TAC, do a HFEC

inspection of the

rod.

- In case of

finding, discard

the rod and do

the same with

another rod.

- If no findings,

replace the rod

in accordance

with SUBTASK

533186-833-001

001 Replace

the Upper Rods

of the Belly

Fairing Structure

at FR39

thru SUBTASK

533186-833-011

001 Replace

the Rods of

the Supports of

the MLG Door

Uplock at FR48

Before next flight - Not applicable

DATE: Jan 17/11 SERVICE BULLETIN No.: A330-53-3186

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SERVICE BULLETIN

COMPLIANCE TIME (whichever occurs

first)

CONDITION ACTION

THRESHOLD GRACE PERIOD

REPETITIVE

INTERVAL NOT

TO EXCEED

(whichever occurs

first)

No cracks found No further action. - - -

NOTE: It is not necessary to perform the HFEC inspection on TAC rods

immediately after identification of the rod manufacturer.

Aircraft can go back into service and the HFEC inspection can be

performed later.

However, HFEC inspection must be performed within six years from the

ISB Revision 00 issuance.

NOTE: We recommend to perform the preliminary detailed inspection at the first

C check from SB issuance date, in order to have time to contact AIRBUS

Material, Logistics and suppliers (SMM) and to ensure all rods (and B/E

Aerospoace for associated hardware) availability during the month where

the HFEC inspection will be performed on the aircraft.

F. APPROVAL

Approved under EASA 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 533186-832-801-001: Inspection

Get Access 3.00

On Aircraft

Do a One Time Detailed Inspection of the Rods 0.25

Close-Up 4.00

TOTAL MANHOURS 7.25

ELAPSED TIME (HOURS) 7.25

NOTE: The values given for the inspections are valid only for one rod.

DATE: Jan 17/11 SERVICE BULLETIN No.: A330-53-3186

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SERVICE BULLETIN

Task 533186-832-802-001: Inspection

Get Access 3.00

On Aircraft

Do a HFEC Inspection of the TAC Rods 0.50

Replace the Upper Rods of the Belly Fairing Structure

at FR39

0.50

Replace the Lateral Rods of the Belly Fairing Structure

at FR39

0.50

Replace the Lateral Rods of the Belly Fairing Structure

at FR47

0.50

Replace the Central Rod of the Belly Fairing Structure

at FR47

0.50

Replace the Upper Rods of the Belly Fairing Structure

at FR53.2

0.50

Replace the Lateral Rods of the Belly Fairing Structure

at FR53.2

0.50

Replace the Center Rods of the Belly Fairing Structure

at FR53.2

0.50

Replace the Upper Rods of the Belly Fairing Structure

at FR53.4

0.50

Replace the Lateral Rods of the Belly Fairing Structure

at FR53.4

0.50

Replace the Lateral Rods of the Belly Fairing Structure

at FR53.9

0.50

Replace the Rods of the Supports of the MLG Door

Uplock at FR48

0.50

Close-Up 4.00

TOTAL MANHOURS 13.00

ELAPSED TIME (HOURS) 13.00

H. WEIGHT AND BALANCE

Not Changed

I. ELECTRICAL LOAD DATA

Not Changed

J. REFERENCES

Aircraft Maintenance Manual (AMM) 06-41-53 12-34-24 20-11-11

20-21-11 32-12-00 53-35-11

53-35-13

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

Non Destructive Test Manual (NTM) 51-10-08

Standards Manual (SM)

Structural Repair Manual (SRM) 51-23-12 51-42-00 51-43-00

51-49-00

DATE: Jan 17/11 SERVICE BULLETIN No.: A330-53-3186

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SERVICE BULLETIN

K. PUBLICATION AFFECTED

None

L. INTERCHANGEABILITY/MIXABILITY

Not Applicable

M. SPARES

None

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SERVICE BULLETIN

2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

(1) Procurement Addresses

Customers with aircraft shown in the effectivity of this Service Bulletin should send a

purchase order to AIRBUS. Quote the number of this Service Bulletin. The address is :

Component COMPA01 AIRBUS Material, Logistics and Suppliers

Weg beim Jaeger 150

D-22335 Hamburg

Germany

For ordering by internet:

http://spares.airbus.com

For ordering of single spares by fax: +49 40

50 76 40 13

E-Mail : ifd.spares@airbus.com

Component COMPA02 BAE Aerospoace

10000 NW 15th Terrace

Miami, FL 33172

USA

Tel : EMEA : +49 (0) 40 822 285 31500

US : +1 305 925 2600

ASIA : +1 310 900 1300

Fax : EMEA : +49 (0) 40 822 285 31010

US : +1 305 507 7191

ASIA : +1 310 819 1200

Sita : MIAMMCR

or contact your daily sales contact

E-Mail : AOGdesk_CMG@baeaerospace.com

(2) Price and Availability

No AIRBUS kit will be provided. Parts required to accomplish this Service Bulletin are to

be purchased by a Spares Purchase Order.

B. INDUSTRY SUPPORT INFORMATION

AIRBUS will provide the operator supplied AIRBUS parts at no charge for those aircraft with

findings further to inspection as per this Service Bulletin.

AIRBUS will reimburse the operator supplied standard hardware parts for those aircraft with

findings further to inspection as per this Service Bulletin.

AIRBUS will credit the manhours indicated in this Service Bulletin for inspections that are

performed on aircraft in warranty at the time of such inspection.

Claims for labor allowance should be received not later than 90 days after completion of the

last affected warranted aircraft.

DATE: Jan 17/11 SERVICE BULLETIN No.: A330-53-3186

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SERVICE BULLETIN

C. LIST OF COMPONENTS

No Kit

D. LIST OF MATERIALS - OPERATOR SUPPLIED

(1) Consumable Materials

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO CML

MAT. No.

QTY PER A/C SEE

NOTES

Corrosion Inhibiting Brush

Consistency

09-013B As required

Corrosion Preventive Temporary

Protective Compound

15-005A As required

(2) Components

NOTE: We recommend to perform the preliminary detailed inspection at the first

C check from SB issuance date, in order to have time to contact AIRBUS

Material, Logistics and suppliers (SMM) and to ensure all rods (and B/E

Aerospoace for associated hardware) availability during the month where

the HFEC inspection will be performed on the aircraft.

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE

NOTES

1 F0003010400100 2 ROD

2 F0003010400300 2 ROD

3 F0003010400400 2 ROD

4 F0003010400500 4 ROD

5 F0003010400700 2 ROD

6 F0003010400800 2 ROD

7 F0003010400900 1 ROD

8 F0003010401100 2 ROD

9 F0003010401200 2 ROD

10 F0003010401400 2 ROD

NOTE: The necessary quantity of rods depends on the inspection results.

Component COMPA02

ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE

NOTES

15 MS24665-153 36 PIN

18 MS24665-300 6 PIN

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SERVICE BULLETIN

NOTE: If you find part numbers of hardware components in the related kit(s)

which you cannot identify in the LIST OF COMPONENTS of this Service

Bulletin, refer to Standards Manual (SM). The SM will give you the

correct part number to part number relationship.

NOTE: The necessary quantity of pins depends on the inspection results

(3) Equipment

None

E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

None

F. TOOLING

None

DATE: Jan 17/11 SERVICE BULLETIN No.: A330-53-3186

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This Page Intentionally Left Blank

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SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS

Task 533186-832-801-001 - Inspection

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

INCLUDED IN THE REFERENCED PROCEDURES.

CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP

ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY

AND MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENANCE

WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING,

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

THIS :

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

NECESSARY ON WIRING AND COMPONENTS.

- REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND

OTHER CONTAMINATION.

THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION

AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION.

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

Task Associated Data

Zone

190

Manpower

TOTAL MANHOURS 7.25

ELAPSED TIME (HOURS) 7.25

A. GENERAL

(1) Subtask 533186-839-001-001 - 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 533186-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

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SERVICE BULLETIN

References

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

Task 12-34-24-860-802

Task 32-12-00-010-801

Task 53-35-11-000-801

Task 53-35-13-000-801

Task 53-35-13-000-802

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

12-34-24-860-802).

(b) Open the MLG doors (Refer to AMM Task 32-12-00-010-801).

(c) Remove the following belly fairing access panels :

(Refer to AMM 06-41-53, Page Block 001, AMM Task 53-35-11-000-801, AMM

Task 53-35-13-000-801 and AMM Task 53-35-13-000-802).

191BB, 191CB, 191QB, 192BB, 192CB, 192QB, 195CB, 196GB, 197BB, 197EB,

197GB, 197HB, 198BB, 198EB, 198GB and 198HB

(d) Put access platform(s) in position.

(2) Subtask 533186-020-003-001 - Remove the Aft Fillet Fairing from LH side for

Access

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 53-35-11-000-802

Fig. A-FBDAA

Removal/Installation of the Aft Fillet

Fairing for Access.

Sheet 01

(a) Remove :

Fig. A-FBDAA

(Refer to AMM Task 53-35-11-000-802)

1 Aft Fillet Fairing Item (30) Retain

(3) Subtask 533186-020-004-001 - Remove the Aft Fillet Fairing from RH side for

Access

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 53-35-11-000-802

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References

Fig. A-FBDAA

Removal/Installation of the Aft Fillet

Fairing for Access.

Sheet 01

(a) Remove :

Fig. A-FBDAA

(Refer to AMM Task 53-35-11-000-802)

1 Aft Fillet Fairing Item (31) Retain

C. PROCEDURE

(1) Subtask 533186-832-001-001 - Do a One Time Detailed Inspection of the Rods

Work Zones and Access Panels

Zone Access/Work location

190

Manpower Resources

Manhours 0.25

Minimum number of person 1

Subtask elapsed time 0.25

Skills NON SPECIFIC

References

Fig. A-FBAAA

Area to be Inspected

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Fig. A-FBBAA

Flow Chart

Sheet 01

Sheet 02

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

(b) Do a one time detailed inspection of the rods.

Refer to Fig. A-FBBAA.

1 If the manufacturer of the rod is TAC or if the manufacturer cannot be

identified, go to SUBTASK 533186-832-003 001 Do a HFEC Inspection of the

TAC Rods or go to SUBTASK 533186-942-001 001 Close-up and release

your aircraft, if you intend to do the HFEC inspection later (SUBTASK

533186-832-003 001) but within 6 years from the SB revision 00 issuance.

NOTE: We recommend to perform the preliminary detailed inspection

at the first C check from SB issuance date, in order to

have time to contact AIRBUS Material, Logistics and suppliers

(SMM) and to ensure all rods (and B/E Aerospoace for

associated hardware) availability during the month where the

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SERVICE BULLETIN

HFEC inspection will be performed on the aircraft.

2 If the manufacturer of the rod is not TAC, no further action is required.

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

D. TEST

None

E. CLOSE-UP

(1) Subtask 533186-420-001-001 - Install the Aft Fillet Fairing at LH side

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 53-35-11-400-802

Fig. A-FBDAA

Removal/Installation of the Aft Fillet

Fairing for Access.

Sheet 01

(a) Install :

Fig. A-FBDAA

(Refer to AMM Task 53-35-11-400-802)

1 Aft Fillet Fairing Item (30) Retained at

removal

(2) Subtask 533186-420-002-001 - Install the Aft Fillet Fairing at RH side

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 53-35-11-400-802

Fig. A-FBDAA

Removal/Installation of the Aft Fillet

Fairing for Access.

Sheet 01

(a) Install :

Fig. A-FBDAA

(Refer to AMM Task 53-35-11-400-802)

1 Aft Fillet Fairing Item (31) Retained at

removal

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SERVICE BULLETIN

(3) Subtask 533186-942-001-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

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

Task 32-12-00-410-801

Task 53-35-11-000-801

Task 53-35-13-000-801

Task 53-35-13-000-802

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

equipment.

(b) Remove the access platform(s).

(c) Install the following belly fairing access panels :

(Refer to AMM 06-41-53, Page Block 001, AMM Task 53-35-11-000-801, AMM

Task 53-35-13-000-801 and AMM Task 53-35-13-000-802).

191BB, 191CB, 191QB, 192BB, 192CB, 192QB, 195CB, 196GB, 197BB, 197EB,

197GB, 197HB, 198BB, 198EB, 198GB and 198HB

(d) Close the MLG doors (Refer to AMM Task 32-12-00-410-801).

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

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This Page Intentionally Left Blank

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Task 533186-832-802-001 - Inspection

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

INCLUDED IN THE REFERENCED PROCEDURES.

CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP

ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY

AND MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENANCE

WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING,

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

THIS :

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

NECESSARY ON WIRING AND COMPONENTS.

- REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND

OTHER CONTAMINATION.

THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION

AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION.

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

Task Associated Data

Zone

190

Manpower

TOTAL MANHOURS 13.00

ELAPSED TIME (HOURS) 13.00

A. GENERAL

(1) Subtask 533186-839-002-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

(2) Subtask 533186-910-002-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

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SERVICE BULLETIN

Material necessary to do the job

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Corrosion Inhibiting Brush

Consistency

09-013B As required

Corrosion Preventive

Temporary Protective

Compound

15-005A As required

References

Aircraft Maintenance Manual (AMM) Task 20-11-11-911-803

Task 20-21-11-911-801

Structural Repair Manual (SRM) 51-23-12

51-42-00

51-43-00

51-49-00

(a) Remove and install the fasteners (Refer to SRM 51-42-00).

(b) For alternative and substitute fasteners, refer to SRM 51-43-00.

(c) Torque the standard threaded fasteners (Refer to SRM 51-49-00 and AMM Task

20-21-11-911-801).

(d) Renew the protective finish with :

Corrosion

Preventive

Temporary

Protective

Compound

15-005A As required

(Refer to SRM 51-23-12)

(e) On the head of the fasteners apply :

Corrosion Inhibiting

Brush Consistency

09-013B As required

(f) Secure the rod ends with lock wire (Refer to AMM Task 20-11-11-911-803).

B. PREPARATION

(1) Subtask 533186-941-002-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

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SERVICE BULLETIN

References

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

Task 12-34-24-860-802

Task 32-12-00-010-801

Task 53-35-11-000-801

Task 53-35-13-000-801

Task 53-35-13-000-802

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

12-34-24-860-802).

(b) Open the MLG doors (Refer to AMM Task 32-12-00-010-801).

(c) Remove the following belly fairing access panels :

(Refer to AMM 06-41-53, Page Block 001, AMM Task 53-35-11-000-801, AMM

Task 53-35-13-000-801 and AMM Task 53-35-13-000-802).

191BB, 191CB, 191QB, 192BB, 192CB, 192QB, 195CB, 196GB, 197BB, 197EB,

197GB, 197HB, 198BB, 198EB, 198GB and 198HB

(d) Put access platform(s) in position.

(2) Subtask 533186-020-001-001 - Remove the Aft Fillet Fairing from LH side for

Access

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 53-35-11-000-802

Fig. A-FBDAA

Removal/Installation of the Aft Fillet

Fairing for Access.

Sheet 01

(a) Remove :

Fig. A-FBDAA

(Refer to AMM Task 53-35-11-000-802)

1 Aft Fillet Fairing Item (30) Retain

(3) Subtask 533186-020-002-001 - Remove the Aft Fillet Fairing from RH side for

Access

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 53-35-11-000-802

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References

Fig. A-FBDAA

Removal/Installation of the Aft Fillet

Fairing for Access.

Sheet 01

(a) Remove :

Fig. A-FBDAA

(Refer to AMM Task 53-35-11-000-802)

1 Aft Fillet Fairing Item (31) Retain

C. PROCEDURE

(1) Subtask 533186-832-003-001 - Do a HFEC Inspection of the TAC Rods

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills NON DESTRUCTIVE

TESTING

References

Non Destructive Test Manual (NTM) 51-10-08

Fig. A-FBAAA

Area to be Inspected

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Fig. A-FBBAA

Flow Chart

Sheet 01

Sheet 02

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

(b) Do a HFEC inspection of the TAC rods as per NTM 51-10-08.

Refer to Fig. A-FBBAA.

1 If no crack is found, no further action is required.

2 If crack is found do the following steps.

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

(2) Subtask 533186-833-001-001 - Replace the Upper Rods of the Belly Fairing

Structure at FR39

Work Zones and Access Panels

Zone Access/Work location

190 Work location Frame 39

DATE: Jan 17/11 SERVICE BULLETIN No.: A330-53-3186

REVISION No.: 01 - Apr 07/11 Page: 26

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@A330

SERVICE BULLETIN

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills AIRFRAME

Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

4 F0003010400500 2 ROD

NOTE: The necessary quantity of rods depends on the inspection results.

Component COMPA02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

15 MS24665-153 4 PIN

NOTE: The necessary quantity of pins depends on the inspection results

References

Fig. A-FBCAA

Replacement of the rods

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

(a) Remove from LH side :

Fig. A-FBCAA Sheet 03, Detail F

2 Bolt Item (11) Retain

2 Nut Item (12) Retain

2 Washer Item (13) Retain

2 Washer Item (14) Retain

2 Pin Item (15) Discard

2 Bush Item (16) Retain

2 Bush Item (17) Retain

1 Rod Item (4) Discard

DATE: Jan 17/11 SERVICE BULLETIN No.: A330-53-3186

REVISION No.: 01 - Apr 07/11 Page: 27

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@A330

SERVICE BULLETIN

(b) Install on LH side :

Fig. A-FBCAA Sheet 03, Detail F

NOTE: For the installation of the rod, it has to be adjusted to the correct

length and secured with lock wire on both sides then you can

torque the fasteners.

1 Rod F0003010400500 Item 4

2 Bush Item (16) Retained at

removal

2 Bush Item (17) Retained at

removal

2 Bolt Item (11) Retained at

removal

2 Nut Item (12) Retained at

removal

2 Washer Item (13) Retained at

removal

2 Washer Item (14) Retained at

removal

2 Pin-Cotter MS24665-153 Item 15

(c) Remove from RH side :

Fig. A-FBCAA Sheet 03, Detail F

2 Bolt Item (11) Retain

2 Nut Item (12) Retain

2 Washer Item (13) Retain

2 Washer Item (14) Retain

2 Pin Item (15) Discard

2 Bush Item (16) Retain

2 Bush Item (17) Retain

1 Rod Item (4) Discard

DATE: Jan 17/11 SERVICE BULLETIN No.: A330-53-3186

REVISION No.: 01 - Apr 07/11 Page: 28

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@A330

SERVICE BULLETIN

(d) Install on RH side :

Fig. A-FBCAA Sheet 03, Detail F

NOTE: For the installation of the rod, it has to be adjusted to the correct

length and secured with lock wire on both sides then you can

torque the fasteners.

1 Rod F0003010400500 Item 4

2 Bush Item (16) Retained at

removal

2 Bush Item (17) Retained at

removal

2 Bolt Item (11) Retained at

removal

2 Nut Item (12) Retained at

removal

2 Washer Item (13) Retained at

removal

2 Washer Item (14) Retained at

removal

2 Pin-Cotter MS24665-153 Item 15

(3) Subtask 533186-833-002-001 - Replace the Lateral Rods of the Belly Fairing

Structure at FR39

Work Zones and Access Panels

Zone Access/Work location

190 Work location Frame 39

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills AIRFRAME

Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 F0003010400100 2 ROD

NOTE: The necessary quantity of rods depends on the inspection results.

DATE: Jan 17/11 SERVICE BULLETIN No.: A330-53-3186

REVISION No.: 01 - Apr 07/11 Page: 29

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@A330

SERVICE BULLETIN

Component COMPA02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

15 MS24665-153 4 PIN

NOTE: The necessary quantity of pins depends on the inspection results

References

Fig. A-FBCAA

Replacement of the rods

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

(a) Remove from LH side :

Fig. A-FBCAA Sheet 03, Detail F

2 Bolt Item (11) Retain

2 Nut Item (12) Retain

2 Washer Item (13) Retain

2 Washer Item (14) Retain

2 Pin Item (15) Discard

2 Bush Item (16) Retain

2 Bush Item (17) Retain

1 Rod Item (1) Discard

(b) Install on LH side :

Fig. A-FBCAA Sheet 03, Detail F

NOTE: For the installation of the rod, it has to be adjusted to the correct

length and secured with lock wire on both sides then you can

torque the fasteners.

1 Rod F0003010400100 Item 1

2 Bush Item (16) Retained at

removal

2 Bush Item (17) Retained at

removal

DATE: Jan 17/11 SERVICE BULLETIN No.: A330-53-3186

REVISION No.: 01 - Apr 07/11 Page: 30

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@A330

SERVICE BULLETIN

2 Bolt Item (11) Retained at

removal

2 Nut Item (12) Retained at

removal

2 Washer Item (13) Retained at

removal

2 Washer Item (14) Retained at

removal

2 Pin-Cotter MS24665-153 Item 15

(c) Remove from RH side :

Fig. A-FBCAA Sheet 03, Detail F

2 Bolt Item (11) Retain

2 Nut Item (12) Retain

2 Washer Item (13) Retain

2 Washer Item (14) Retain

2 Pin Item (15) Discard

2 Bush Item (16) Retain

2 Bush Item (17) Retain

1 Rod Item (1) Discard

(d) Install on RH side :

Fig. A-FBCAA Sheet 03, Detail F

NOTE: For the installation of the rod, it has to be adjusted to the correct

length and secured with lock wire on both sides then you can

torque the fasteners.

1 Rod F0003010400100 Item 1

2 Bush Item (16) Retained at

removal

2 Bush Item (17) Retained at

removal

DATE: Jan 17/11 SERVICE BULLETIN No.: A330-53-3186

REVISION No.: 01 - Apr 07/11 Page: 31

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@A330

SERVICE BULLETIN

2 Bolt Item (11) Retained at

removal

2 Nut Item (12) Retained at

removal

2 Washer Item (13) Retained at

removal

2 Washer Item (14) Retained at

removal

2 Pin-Cotter MS24665-153 Item 15

(4) Subtask 533186-833-003-001 - Replace the Lateral Rods of the Belly Fairing

Structure at FR47

Work Zones and Access Panels

Zone Access/Work location

190 Work location Frame 47

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills AIRFRAME

Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

8 F0003010401100 2 ROD

NOTE: The necessary quantity of rods depends on the inspection results.

Component COMPA02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

15 MS24665-153 2 PIN

18 MS24665-300 2 PIN

NOTE: The necessary quantity of pins depends on the inspection results

DATE: Jan 17/11 SERVICE BULLETIN No.: A330-53-3186

REVISION No.: 01 - Apr 07/11 Page: 32

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@A330

SERVICE BULLETIN

References

Fig. A-FBCAA

Replacement of the rods

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

(a) Remove from LH side :

Fig. A-FBCAA Sheet 04, Detail G

1 Bolt Item (20) Retain

1 Bolt Item (21) Retain

2 Nut Item (19) Retain

2 Washer Item (22) Retain

2 Washer Item (23) Retain

1 Pin Item (15) Discard

1 Pin Item (18) Discard

1 Bush Item (24) Retain

1 Bush Item (25) Retain

1 Bush Item (26) Retain

1 Bush Item (27) Retain

1 Rod Item (8) Discard

(b) Install on LH side :

Fig. A-FBCAA Sheet 04, Detail G

NOTE: For the installation of the rod, it has to be adjusted to the correct

length and secured with lock wire on both sides then you can

torque the fasteners.

1 Rod F0003010401100 Item 8

1 Bush Item (24) Retained at

removal

DATE: Jan 17/11 SERVICE BULLETIN No.: A330-53-3186

REVISION No.: 01 - Apr 07/11 Page: 33

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@A330

SERVICE BULLETIN

1 Bush Item (25) Retained at

removal

1 Bush Item (26) Retained at

removal

1 Bush Item (27) Retained at

removal

1 Bolt Item (20) Retained at

removal

1 Bolt Item (21) Retained at

removal

2 Nut Item (19) Retained at

removal

2 Washer Item (22) Retained at

removal

2 Washer Item (23) Retained at

removal

1 Pin-Cotter MS24665-153 Item 15

1 Pin-Cotter MS24665-300 Item 18

(c) Remove from RH side :

Fig. A-FBCAA Sheet 04, Detail G

1 Bolt Item (20) Retain

1 Bolt Item (21) Retain

2 Nut Item (19) Retain

2 Washer Item (22) Retain

2 Washer Item (23) Retain

1 Pin Item (15) Discard

1 Pin Item (18) Discard

1 Bush Item (24) Retain

1 Bush Item (25) Retain

DATE: Jan 17/11 SERVICE BULLETIN No.: A330-53-3186

REVISION No.: 01 - Apr 07/11 Page: 34

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@A330

SERVICE BULLETIN

1 Bush Item (26) Retain

1 Bush Item (27) Retain

1 Rod Item (8) Discard

(d) Install on RH side :

Fig. A-FBCAA Sheet 04, Detail G

NOTE: For the installation of the rod, it has to be adjusted to the correct

length and secured with lock wire on both sides then you can

torque the fasteners.

1 Rod F0003010401100 Item 8

1 Bush Item (24) Retained at

removal

1 Bush Item (25) Retained at

removal

1 Bush Item (26) Retained at

removal

1 Bush Item (27) Retained at

removal

1 Bolt Item (20) Retained at

removal

1 Bolt Item (21) Retained at

removal

2 Nut Item (19) Retained at

removal

2 Washer Item (22) Retained at

removal

2 Washer Item (23) Retained at

removal

1 Pin-Cotter MS24665-153 Item 15

1 Pin-Cotter MS24665-300 Item 18

DATE: Jan 17/11 SERVICE BULLETIN No.: A330-53-3186

REVISION No.: 01 - Apr 07/11 Page: 35

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@A330

SERVICE BULLETIN

(5) Subtask 533186-833-004-001 - Replace the Central Rod of the Belly Fairing

Structure at FR47

Work Zones and Access Panels

Zone Access/Work location

190 Work location Frame 47

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills AIRFRAME

Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

7 F0003010400900 1 ROD

NOTE: The necessary quantity of rods depends on the inspection results.

Component COMPA02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

15 MS24665-153 2 PIN

NOTE: The necessary quantity of pins depends on the inspection results

References

Fig. A-FBCAA

Replacement of the rods

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

(a) Remove :

Fig. A-FBCAA Sheet 03, Detail F

2 Bolt Item (11) Retain

2 Nut Item (12) Retain

2 Washer Item (13) Retain

2 Washer Item (14) Retain

2 Pin Item (15) Discard

DATE: Jan 17/11 SERVICE BULLETIN No.: A330-53-3186

REVISION No.: 01 - Apr 07/11 Page: 36

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@A330

SERVICE BULLETIN

2 Bush Item (16) Retain

2 Bush Item (17) Retain

1 Rod Item (7) Discard

(b) Install :

Fig. A-FBCAA Sheet 03, Detail F

NOTE: For the installation of the rod, it has to be adjusted to the correct

length and secured with lock wire on both sides then you can

torque the fasteners.

1 Rod F0003010400900 Item 7

2 Bush Item (16) Retained at

removal

2 Bush Item (17) Retained at

removal

2 Bolt Item (11) Retained at

removal

2 Nut Item (12) Retained at

removal

2 Washer Item (13) Retained at

removal

2 Washer Item (14) Retained at

removal

2 Pin-Cotter MS24665-153 Item 15

(6) Subtask 533186-833-005-001 - Replace the Upper Rods of the Belly Fairing

Structure at FR53.2

Work Zones and Access Panels

Zone Access/Work location

190 Work location Frame 53.2

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills AIRFRAME

DATE: Jan 17/11 SERVICE BULLETIN No.: A330-53-3186

REVISION No.: 01 - Apr 07/11 Page: 37

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@A330

SERVICE BULLETIN

Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

10 F0003010401400 2 ROD

NOTE: The necessary quantity of rods depends on the inspection results.

Component COMPA02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

15 MS24665-153 4 PIN

NOTE: The necessary quantity of pins depends on the inspection results

References

Fig. A-FBCAA

Replacement of the rods

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

(a) Remove from LH side :

Fig. A-FBCAA Sheet 03, Detail F

2 Bolt Item (11) Retain

2 Nut Item (12) Retain

2 Washer Item (13) Retain

2 Washer Item (14) Retain

2 Pin Item (15) Discard

2 Bush Item (16) Retain

2 Bush Item (17) Retain

1 Rod Item (10) Discard

(b) Install on LH side :

Fig. A-FBCAA Sheet 03, Detail F

NOTE: For the installation of the rod, it has to be adjusted to the correct

length and secured with lock wire on both sides then you can

torque the fasteners.

DATE: Jan 17/11 SERVICE BULLETIN No.: A330-53-3186

REVISION No.: 01 - Apr 07/11 Page: 38

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@A330

SERVICE BULLETIN

1 Rod F0003010401400 Item 10

2 Bush Item (16) Retained at

removal

2 Bush Item (17) Retained at

removal

2 Bolt Item (11) Retained at

removal

2 Nut Item (12) Retained at

removal

2 Washer Item (13) Retained at

removal

2 Washer Item (14) Retained at

removal

2 Pin-Cotter MS24665-153 Item 15

(c) Remove from RH side :

Fig. A-FBCAA Sheet 03, Detail F

2 Bolt Item (11) Retain

2 Nut Item (12) Retain

2 Washer Item (13) Retain

2 Washer Item (14) Retain

2 Pin Item (15) Discard

2 Bush Item (16) Retain

2 Bush Item (17) Retain

1 Rod Item (10) Discard

(d) Install on RH side :

Fig. A-FBCAA Sheet 03, Detail F

NOTE: For the installation of the rod, it has to be adjusted to the correct

length and secured with lock wire on both sides then you can

torque the fasteners.

1 Rod F0003010401400 Item 10

DATE: Jan 17/11 SERVICE BULLETIN No.: A330-53-3186

REVISION No.: 01 - Apr 07/11 Page: 39

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@A330

SERVICE BULLETIN

2 Bush Item (16) Retained at

removal

2 Bush Item (17) Retained at

removal

2 Bolt Item (11) Retained at

removal

2 Nut Item (12) Retained at

removal

2 Washer Item (13) Retained at

removal

2 Washer Item (14) Retained at

removal

2 Pin-Cotter MS24665-153 Item 15

(7) Subtask 533186-833-006-001 - Replace the Lateral Rods of the Belly Fairing

Structure at FR53.2

Work Zones and Access Panels

Zone Access/Work location

190 Work location Frame 53.2

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills AIRFRAME

Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

5 F0003010400700 2 ROD

NOTE: The necessary quantity of rods depends on the inspection results.

Component COMPA02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

18 MS24665-300 4 PIN

NOTE: The necessary quantity of pins depends on the inspection results

DATE: Jan 17/11 SERVICE BULLETIN No.: A330-53-3186

REVISION No.: 01 - Apr 07/11 Page: 40

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@A330

SERVICE BULLETIN

References

Fig. A-FBCAA

Replacement of the rods

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

(a) Remove from LH side :

Fig. A-FBCAA Sheet 04, Detail H

2 Bolt Item (21) Retain

2 Nut Item (19) Retain

4 Washer Item (22) Retain

2 Pin Item (18) Discard

2 Bush Item (26) Retain

2 Bush Item (27) Retain

1 Rod Item (5) Discard

(b) Install on LH side

Fig. A-FBCAA Sheet 04, Detail H

NOTE: For the installation of the rod, it has to be adjusted to the correct

length and secured with lock wire on both sides then you can

torque the fasteners.

1 Rod F0003010400700 Item 5

2 Bush Item (26) Retained at

removal

2 Bush Item (27) Retained at

removal

2 Bolt Item (21) Retained at

removal

2 Nut Item (19) Retained at

removal

4 Washer Item (22) Retained at

removal

DATE: Jan 17/11 SERVICE BULLETIN No.: A330-53-3186

REVISION No.: 01 - Apr 07/11 Page: 41

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@A330

SERVICE BULLETIN

2 Pin-Cotter MS24665-300 Item 18

(c) Remove from RH side :

Fig. A-FBCAA Sheet 04, Detail H

2 Bolt Item (21) Retain

2 Nut Item (19) Retain

4 Washer Item (22) Retain

2 Pin Item (18) Discard

2 Bush Item (26) Retain

2 Bush Item (27) Retain

1 Rod Item (5) Discard

(d) Install on RH side

Fig. A-FBCAA Sheet 04, Detail H

NOTE: For the installation of the rod, it has to be adjusted to the correct

length and secured with lock wire on both sides then you can

torque the fasteners.

1 Rod F0003010400700 Item 5

2 Bush Item (26) Retained at

removal

2 Bush Item (27) Retained at

removal

2 Bolt Item (21) Retained at

removal

2 Nut Item (19) Retained at

removal

4 Washer Item (22) Retained at

removal

2 Pin-Cotter MS24665-300 Item 18

DATE: Jan 17/11 SERVICE BULLETIN No.: A330-53-3186

REVISION No.: 01 - Apr 07/11 Page: 42

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@A330

SERVICE BULLETIN

(8) Subtask 533186-833-007-001 - Replace the Center Rods of the Belly Fairing

Structure at FR53.2

Work Zones and Access Panels

Zone Access/Work location

190 Work location Frame 53.2

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills AIRFRAME

Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

6 F0003010400800 2 ROD

NOTE: The necessary quantity of rods depends on the inspection results.

Component COMPA02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

15 MS24665-153 4 PIN

NOTE: The necessary quantity of pins depends on the inspection results

References

Fig. A-FBCAA

Replacement of the rods

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

(a) Remove from LH side :

Fig. A-FBCAA Sheet 05, Detail J

2 Bolt Item (11) Retain

2 Nut Item (12) Retain

4 Washer Item (13) Retain

2 Pin Item (15) Discard

2 Bush Item (17) Retain

DATE: Jan 17/11 SERVICE BULLETIN No.: A330-53-3186

REVISION No.: 01 - Apr 07/11 Page: 43

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@A330

SERVICE BULLETIN

2 Bush Item (16) Retain

1 Rod Item (6) Discard

(b) Install on LH side :

Fig. A-FBCAA Sheet 05, Detail J

NOTE: For the installation of the rod, it has to be adjusted to the correct

length and secured with lock wire on both sides then you can

torque the fasteners.

1 Rod F0003010400800 Item 6

2 Bush Item (17) Retained at

removal

2 Bush Item (16) Retained at

removal

2 Bolt Item (11) Retained at

removal

2 Nut Item (12) Retained at

removal

4 Washer Item (13) Retained at

removal

2 Pin-Cotter MS24665-153 Item 15

(c) Remove from RH side :

Fig. A-FBCAA Sheet 05, Detail J

2 Bolt Item (11) Retain

2 Nut Item (12) Retain

4 Washer Item (13) Retain

2 Pin Item (15) Discard

2 Bush Item (17) Retain

2 Bush Item (16) Retain

1 Rod Item (6) Discard

DATE: Jan 17/11 SERVICE BULLETIN No.: A330-53-3186

REVISION No.: 01 - Apr 07/11 Page: 44

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@A330

SERVICE BULLETIN

(d) Install on RH side :

Fig. A-FBCAA Sheet 05, Detail J

NOTE: For the installation of the rod, it has to be adjusted to the correct

length and secured with lock wire on both sides then you can

torque the fasteners.

1 Rod F0003010400800 Item 6

2 Bush Item (17) Retained at

removal

2 Bush Item (16) Retained at

removal

2 Bolt Item (11) Retained at

removal

2 Nut Item (12) Retained at

removal

4 Washer Item (13) Retained at

removal

2 Pin-Cotter MS24665-153 Item 15

(9) Subtask 533186-833-008-001 - Replace the Upper Rods of the Belly Fairing

Structure at FR53.4

Work Zones and Access Panels

Zone Access/Work location

190 Work location Frame 53.4

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills AIRFRAME

Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

3 F0003010400400 2 ROD

NOTE: The necessary quantity of rods depends on the inspection results.

DATE: Jan 17/11 SERVICE BULLETIN No.: A330-53-3186

REVISION No.: 01 - Apr 07/11 Page: 45

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@A330

SERVICE BULLETIN

Component COMPA02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

15 MS24665-153 4 PIN

NOTE: The necessary quantity of pins depends on the inspection results

References

Fig. A-FBCAA

Replacement of the rods

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

(a) Remove from LH side :

Fig. A-FBCAA Sheet 05, Detail K

2 Bolt Item (11) Retain

2 Nut Item (12) Retain

4 Washer Item (14) Retain

2 Pin Item (15) Discard

2 Bush Item (17) Retain

2 Bush Item (28) Retain

1 Rod Item (3) Discard

(b) Install on LH side :

Fig. A-FBCAA Sheet 05, Detail K

NOTE: For the installation of the rod, it has to be adjusted to the correct

length and secured with lock wire on both sides then you can

torque the fasteners.

1 Rod F0003010400400 Item 3

2 Bush Item (17) Retained at

removal

2 Bush Item (28) Retained at

removal

2 Bolt Item (11) Retained at

removal

DATE: Jan 17/11 SERVICE BULLETIN No.: A330-53-3186

REVISION No.: 01 - Apr 07/11 Page: 46

5

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@A330

SERVICE BULLETIN

2 Nut Item (12) Retained at

removal

4 Washer Item (14) Retained at

removal

2 Pin-Cotter MS24665-153 Item 15

(c) Remove from RH side :

Fig. A-FBCAA Sheet 05, Detail K

2 Bolt Item (11) Retain

2 Nut Item (12) Retain

4 Washer Item (14) Retain

2 Pin Item (15) Discard

2 Bush Item (17) Retain

2 Bush Item (28) Retain

1 Rod Item (3) Discard

(d) Install on RH side :

Fig. A-FBCAA Sheet 05, Detail K

NOTE: For the installation of the rod, it has to be adjusted to the correct

length and secured with lock wire on both sides then you can

torque the fasteners.

1 Rod F0003010400400 Item 3

2 Bush Item (17) Retained at

removal

2 Bush Item (28) Retained at

removal

2 Bolt Item (11) Retained at

removal

2 Nut Item (12) Retained at

removal

4 Washer Item (14) Retained at

removal

DATE: Jan 17/11 SERVICE BULLETIN No.: A330-53-3186

REVISION No.: 01 - Apr 07/11 Page: 47

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@A330

SERVICE BULLETIN

2 Pin-Cotter MS24665-153 Item 15

(10) Subtask 533186-833-009-001 - Replace the Lateral Rods of the Belly Fairing

Structure at FR53.4

Work Zones and Access Panels

Zone Access/Work location

190 Work location Frame 53.4

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills AIRFRAME

Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

2 F0003010400300 2 ROD

NOTE: The necessary quantity of rods depends on the inspection results.

Component COMPA02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

15 MS24665-153 4 PIN

NOTE: The necessary quantity of pins depends on the inspection results

References

Fig. A-FBCAA

Replacement of the rods

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

(a) Remove from LH side :

Fig. A-FBCAA Sheet 05, Detail K

2 Bolt Item (11) Retain

2 Nut Item (12) Retain

4 Washer Item (14) Retain

2 Pin Item (15) Discard

DATE: Jan 17/11 SERVICE BULLETIN No.: A330-53-3186

REVISION No.: 01 - Apr 07/11 Page: 48

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@A330

SERVICE BULLETIN

2 Bush Item (17) Retain

2 Bush Item (28) Retain

1 Rod Item (2) Discard

(b) Install at LH side :

Fig. A-FBCAA Sheet 05, Detail K

NOTE: For the installation of the rod, it has to be adjusted to the correct

length and secured with lock wire on both sides then you can

torque the fasteners.

1 Rod F0003010400300 Item 2

2 Bush Item (17) Retained at

removal

2 Bush Item (28) Retained at

removal

2 Bolt Item (11) Retained at

removal

2 Nut Item (12) Retained at

removal

4 Washer Item (14) Retained at

removal

2 Pin-Cotter MS24665-153 Item 15

(c) Remove from RH side :

Fig. A-FBCAA Sheet 05, Detail K

2 Bolt Item (11) Retain

2 Nut Item (12) Retain

4 Washer Item (14) Retain

2 Pin Item (15) Discard

2 Bush Item (17) Retain

2 Bush Item (28) Retain

1 Rod Item (2) Discard

DATE: Jan 17/11 SERVICE BULLETIN No.: A330-53-3186

REVISION No.: 01 - Apr 07/11 Page: 49

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@A330

SERVICE BULLETIN

(d) Install at RH side :

Fig. A-FBCAA Sheet 05, Detail K

NOTE: For the installation of the rod, it has to be adjusted to the correct

length and secured with lock wire on both sides then you can

torque the fasteners.

1 Rod F0003010400300 Item 2

2 Bush Item (17) Retained at

removal

2 Bush Item (28) Retained at

removal

2 Bolt Item (11) Retained at

removal

2 Nut Item (12) Retained at

removal

4 Washer Item (14) Retained at

removal

2 Pin-Cotter MS24665-153 Item 15

(11) Subtask 533186-833-010-001 - Replace the Lateral Rods of the Belly Fairing

Structure at FR53.9

Work Zones and Access Panels

Zone Access/Work location

190 Work location Frame 53.9

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills AIRFRAME

Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

4 F0003010400500 2 ROD

NOTE: The necessary quantity of rods depends on the inspection results.

DATE: Jan 17/11 SERVICE BULLETIN No.: A330-53-3186

REVISION No.: 01 - Apr 07/11 Page: 50

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@A330

SERVICE BULLETIN

Component COMPA02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

15 MS24665-153 4 PIN

NOTE: The necessary quantity of pins depends on the inspection results

References

Fig. A-FBCAA

Replacement of the rods

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

(a) Remove from LH side :

Fig. A-FBCAA Sheet 03, Detail F

2 Bolt Item (11) Retain

2 Nut Item (12) Retain

2 Washer Item (13) Retain

2 Washer Item (14) Retain

2 Pin Item (15) Discard

2 Bush Item (16) Retain

2 Bush Item (17) Retain

1 Rod Item (4) Discard

(b) Install at LH side :

Fig. A-FBCAA Sheet 03, Detail F

NOTE: For the installation of the rod, it has to be adjusted to the correct

length and secured with lock wire on both sides then you can

torque the fasteners.

1 Rod F0003010400500 Item 4

2 Bush Item (16) Retained at

removal

2 Bush Item (17) Retained at

removal

DATE: Jan 17/11 SERVICE BULLETIN No.: A330-53-3186

REVISION No.: 01 - Apr 07/11 Page: 51

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@A330

SERVICE BULLETIN

2 Bolt Item (11) Retained at

removal

2 Nut Item (12) Retained at

removal

2 Washer Item (13) Retained at

removal

2 Washer Item (14) Retained at

removal

2 Pin-Cotter MS24665-153 Item 15

(c) Remove from RH side :

Fig. A-FBCAA Sheet 03, Detail F

2 Bolt Item (11) Retain

2 Nut Item (12) Retain

2 Washer Item (13) Retain

2 Washer Item (14) Retain

2 Pin Item (15) Discard

2 Bush Item (16) Retain

2 Bush Item (17) Retain

1 Rod Item (4) Discard

(d) Install at RH side :

Fig. A-FBCAA Sheet 03, Detail F

NOTE: For the installation of the rod, it has to be adjusted to the correct

length and secured with lock wire on both sides then you can

torque the fasteners.

1 Rod F0003010400500 Item 4

2 Bush Item (16) Retained at

removal

2 Bush Item (17) Retained at

removal

DATE: Jan 17/11 SERVICE BULLETIN No.: A330-53-3186

REVISION No.: 01 - Apr 07/11 Page: 52

5

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@A330

SERVICE BULLETIN

2 Bolt Item (11) Retained at

removal

2 Nut Item (12) Retained at

removal

2 Washer Item (13) Retained at

removal

2 Washer Item (14) Retained at

removal

2 Pin-Cotter MS24665-153 Item 15

(12) Subtask 533186-833-011-001 - Replace the Rods of the Supports of the MLG Door

Uplock at FR48

Work Zones and Access Panels

Zone Access/Work location

190 Work location Frame 48

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills AIRFRAME

Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

9 F0003010401200 2 ROD

NOTE: The necessary quantity of rods depends on the inspection results.

Component COMPA02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

15 MS24665-153 4 PIN

NOTE: The necessary quantity of pins depends on the inspection results

References

Fig. A-FBCAA

Replacement of the rods

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

DATE: Jan 17/11 SERVICE BULLETIN No.: A330-53-3186

REVISION No.: 01 - Apr 07/11 Page: 53

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@A330

SERVICE BULLETIN

(a) Remove from LH side :

Fig. A-FBCAA Sheet 06, Detail L

1 Bolt Item (11) Retain

1 Bolt Item (21) Retain

2 Nut Item (12) Retain

2 Washer Item (13) Retain

2 Washer Item (14) Retain

2 Pin Item (15) Discard

1 Bush Item (17) Retain

1 Bush Item (28) Retain

1 Rod Item (9) Discard

(b) Install on LH side :

Fig. A-FBCAA Sheet 06, Detail L

NOTE: For the installation of the rod, it has to be adjusted to the correct

length and secured with lock wire on both sides then you can

torque the fasteners.

1 Rod F0003010401200 Item 9

1 Bush Item (17) Retained at

removal

1 Bush Item (28) Retained at

removal

1 Bolt Item (11) Retained at

removal

1 Bolt Item (21) Retained at

removal

2 Nut Item (12) Retained at

removal

2 Washer Item (13) Retained at

removal

DATE: Jan 17/11 SERVICE BULLETIN No.: A330-53-3186

REVISION No.: 01 - Apr 07/11 Page: 54

5

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@A330

SERVICE BULLETIN

2 Washer Item (14) Retained at

removal

2 Pin-Cotter MS24665-153 Item 15

(c) Remove from RH side :

Fig. A-FBCAA Sheet 06, Detail L

1 Bolt Item (11) Retain

1 Bolt Item (21) Retain

2 Nut Item (12) Retain

2 Washer Item (13) Retain

2 Washer Item (14) Retain

2 Pin Item (15) Discard

1 Bush Item (17) Retain

1 Bush Item (28) Retain

1 Rod Item (9) Discard

(d) Install on RH side :

Fig. A-FBCAA Sheet 06, Detail L

NOTE: For the installation of the rod, it has to be adjusted to the correct

length and secured with lock wire on both sides then you can

torque the fasteners.

1 Rod F0003010401200 Item 9

1 Bush Item (17) Retained at

removal

1 Bush Item (28) Retained at

removal

1 Bolt Item (11) Retained at

removal

1 Bolt Item (21) Retained at

removal

2 Nut Item (12) Retained at

removal

DATE: Jan 17/11 SERVICE BULLETIN No.: A330-53-3186

REVISION No.: 01 - Apr 07/11 Page: 55

5

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@A330

SERVICE BULLETIN

2 Washer Item (13) Retained at

removal

2 Washer Item (14) Retained at

removal

2 Pin-Cotter MS24665-153 Item 15

D. TEST

None

E. CLOSE-UP

(1) Subtask 533186-420-003-001 - Install the Aft Fillet Fairing at LH side

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 53-35-11-400-802

Fig. A-FBDAA

Removal/Installation of the Aft Fillet

Fairing for Access.

Sheet 01

(a) Install :

Fig. A-FBDAA

(Refer to AMM Task 53-35-11-400-802)

1 Aft Fillet Fairing Item (30) Retained at

removal

(2) Subtask 533186-420-004-001 - Install the Aft Fillet Fairing at RH side

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 53-35-11-400-802

Fig. A-FBDAA

Removal/Installation of the Aft Fillet

Fairing for Access.

Sheet 01

(a) Install :

Fig. A-FBDAA

(Refer to AMM Task 53-35-11-400-802)

DATE: Jan 17/11 SERVICE BULLETIN No.: A330-53-3186

REVISION No.: 01 - Apr 07/11 Page: 56

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@A330

SERVICE BULLETIN

1 Aft Fillet Fairing Item (31) Retained at

removal

(3) Subtask 533186-942-002-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

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

Task 32-12-00-410-801

Task 53-35-11-000-801

Task 53-35-13-000-801

Task 53-35-13-000-802

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

equipment.

(b) Remove the access platform(s).

(c) Install the following belly fairing access panels :

(Refer to AMM 06-41-53, Page Block 001, AMM Task 53-35-11-000-801, AMM

Task 53-35-13-000-801 and AMM Task 53-35-13-000-802).

191BB, 191CB, 191QB, 192BB, 192CB, 192QB, 195CB, 196GB, 197BB, 197EB,

197GB, 197HB, 198BB, 198EB, 198GB and 198HB

(d) Close the MLG doors (Refer to AMM Task 32-12-00-410-801).

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

DATE: Jan 17/11 SERVICE BULLETIN No.: A330-53-3186

REVISION No.: 01 - Apr 07/11 Page: 57

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@A330

SERVICE BULLETIN

**CONF ALL

A

Z190

FR53.9

FR53.2

FR48

FR37

FR39

B

C

D

E

A

E

G_SB_533186_5_BAAA_01_01

Figure A-FBAAA - Sheet 01

Area to be Inspected

DATE: Jan 17/11 SERVICE BULLETIN No.: A330-53-3186

REVISION No.: 01 - Apr 07/11 Page: 58

5

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@A330

SERVICE BULLETIN

**CONF ALL

FR53.4

FR53.9

FR53.2

FR47

FR39

F

F

F

F

F

F

F

F

F

F

F

F

F

F

F

F

F

F

F

B

C

D

G_SB_533186_5_BAAA_02_00

Figure A-FBAAA - Sheet 02

Area to be Inspected

DATE: Jan 17/11 SERVICE BULLETIN No.: A330-53-3186

REVISION No.: 01 - Apr 07/11 Page: 59

5

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@A330

SERVICE BULLETIN

**CONF ALL

MANUFACTURER AND PN TO BE IDENTIFIED

F

FR48

F

LH SIDE SHOWN

RH SIDE SYMMETRICAL

E

TYPICAL

G_SB_533186_5_BAAA_03_01

G

G

Figure A-FBAAA - Sheet 03

Area to be Inspected

DATE: Jan 17/11 SERVICE BULLETIN No.: A330-53-3186

REVISION No.: 01 - Apr 07/11 Page: 60

5

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@A330

SERVICE BULLETIN

**CONF ALL

AREA TO BE

TYPICAL CRACK

INSPECTED

LOCATION

TYPICAL

G

G_SB_533186_5_BAAA_04_00

Figure A-FBAAA - Sheet 04

Area to be Inspected

DATE: Jan 17/11 SERVICE BULLETIN No.: A330-53-3186

REVISION No.: 01 - Apr 07/11 Page: 61

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@A330

SERVICE BULLETIN

**CONF ALL

AT THE THRESHOLD GIVEN IN THE PLANNING

INFORMATION PARAGRAPH E.2.

THE MANUFACTURER

NO YES

REPORT TO AIRBUS

REFER TO APPENDIX 01

AS PER NTM 51−10−08 AT THRESHOLD

DO A HFEC INSPECTION OF THE ROD

GIVEN IN THE PLANNING

INFORMATION PARAGRAPH E.2.

NO FURTHER ACTION

NO CRACKS YES

DO A ONE TIME DETAILED INSPECTION OF THE RODS

IDENTIFY THE PART NUMBER AND

THE MANUFACTURER OF THE ROD

OF THE ROD IS TAC OR THE

SEND THE INSPECTION

REPORT TO AIRBUS

REFER TO APPENDIX 01

NO FURTHER ACTION

SEND THE INSPECTION

A−FBBAA SHEET 2

REFER TO FIGURE

QUESTION

ACTION

FINDING

NOTE:

WE RECOMMEND TO PERFORM THE PRELIMINARY DETAILED INSPECTION AT THE FIRST C−

CHECK FROM SB ISSUANCE DATE, IN ORDER TO HAVE TIME TO CONTACT AIRBUS MATERIAL,

LOGISTICS AND SUPPLIERS (SMM) AND TO ENSURE ALL RODS (AND B/E AEROSPACE FOR

ASSOCIATED HARWARE) AVAILABILITY DURING THE MONTH WHEN THE HFEC INSPECTION

WILL BE PERFORMED ON THE AIRCRAFT.

*

*

IT IS NOT NECESSARY TO PERFORM THE HFEC INSPECTION ON TAC RODS IMMEDIATELY AFTER

IDENTIFICATION OF THE ROD MANUFACTURER.

AIRCRAFT CAN GO BACK INTO SERVICE AND THE HFEC INSPECTION CAN BE PERFORMED LATER.

HOWEVER, HFEC INSPECTION MUST BE PERFORMED WITHIN SIX YEARS FROM THE INSPECTION

SERVICE BULLETIN REVISION 00 ISSUANCE.

MANUFACTURER CANNOT

BE IDENTIFIED

G_SB_533186_5_BBAA_01_04

Figure A-FBBAA - Sheet 01

Flow Chart

DATE: Jan 17/11 SERVICE BULLETIN No.: A330-53-3186

REVISION No.: 01 - Apr 07/11 Page: 62

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@A330

SERVICE BULLETIN

**CONF ALL

QUESTION

ACTION

FINDING

MANUFACTURER OF

NO YES

OF THE NEW ROD

DO A HFEC INSPECTION

NO CRACKS YES

THE

THE NEW ROD TO BE

REPORT TO AIRBUS

REFER TO APPENDIX 01

NO FURTHER ACTION

SEND THE INSPECTION

A−FBBAA SHEET 1

FROM FIGURE

INSTALLED IS TAC

AS PER NTM 51−10−08

AS DESCRIBED IN SUBTASK 533186−833−001−001

THRU 533186−833−011−001 BEFORE NEXT FLIGHT

REPLACE THE ROD

TO BE INSTALLED

AND GET A NEW ONE

DISCARD THE ROD

G_SB_533186_5_BBAA_02_01

Figure A-FBBAA - Sheet 02

Flow Chart

DATE: Jan 17/11 SERVICE BULLETIN No.: A330-53-3186

REVISION No.: 01 - Apr 07/11 Page: 63

5

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@A330

SERVICE BULLETIN

**CONF ALL

A

Z190

FR53.9

FR53.2

FR48

FR37

FR39

B

C

D

E

A

E

G_SB_533186_5_BCAA_01_02

Figure A-FBCAA - Sheet 01

Replacement of the rods

DATE: Jan 17/11 SERVICE BULLETIN No.: A330-53-3186

REVISION No.: 01 - Apr 07/11 Page: 64

5

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@A330

SERVICE BULLETIN

**CONF ALL

FR53.4

FR53.9

FR53.2

FR47

FR39

F

F

F

F

F

F

F

F

F

B

C

D

(1)

1

(4)

4

(4)

4

(1)

1

(8)

8

(8)

8

(7)

7

(10)

10

(5)

5

(6)

6

(5)

5

(10)

10

(2)

2

(3)

3

(4)

4

(4)

4

(3)

3 (2)

2

G

K

K

H

J

J

H

K

K

G

G_SB_533186_5_BCAA_02_02

Figure A-FBCAA - Sheet 02

Replacement of the rods

DATE: Jan 17/11 SERVICE BULLETIN No.: A330-53-3186

REVISION No.: 01 - Apr 07/11 Page: 65

5

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@A330

SERVICE BULLETIN

**CONF ALL

FR48

(9)

9

LH SIDE SHOWN

RH SIDE SYMMETRICAL

E

(11)

(14)

(13)

(12)

15

(11)

(14) (13)

(12)

(15)

TYPICAL

F

(15)

(17)

(16)

(16)

15 (17)

L

G_SB_533186_5_BCAA_03_02

Figure A-FBCAA - Sheet 03

Replacement of the rods

DATE: Jan 17/11 SERVICE BULLETIN No.: A330-53-3186

REVISION No.: 01 - Apr 07/11 Page: 66

5

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@A330

SERVICE BULLETIN

**CONF ALL

(21)

(22)

(22)

(19)

18

(21)

(22) (22)

(19)

(18)

TYPICAL

(18)

(27)

(26)

(26)

18 (27)

(20)

(22)

(23)

(19)

15

(21)

(22) (23)

(19)

(18)

TYPICAL

(15)

(24)

(25)

(26)

18 (27)

G

H

G_SB_533186_5_BCAA_04_01

Figure A-FBCAA - Sheet 04

Replacement of the rods

DATE: Jan 17/11 SERVICE BULLETIN No.: A330-53-3186

REVISION No.: 01 - Apr 07/11 Page: 67

5

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@A330

SERVICE BULLETIN

**CONF ALL

(11)

(14)

(14)

(12)

15

(11)

(14) (14)

(12)

(15)

TYPICAL

(15)

(17)

(28)

(28)

15 (17)

(11)

(13)

(13)

(12)

15

(11)

(13) (13)

(12)

(15)

TYPICAL

(15)

(17)

(16)

(16)

15 (17)

J

K

G_SB_533186_5_BCAA_05_01

Figure A-FBCAA - Sheet 05

Replacement of the rods

DATE: Jan 17/11 SERVICE BULLETIN No.: A330-53-3186

REVISION No.: 01 - Apr 07/11 Page: 68

5

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@A330

SERVICE BULLETIN

**CONF ALL

(11)

(13)

(12)

15

(21)

(14) (13)

(12)

(15)

TYPICAL

(15)

(17)

15 (28)

L

(14)

G_SB_533186_5_BCAA_06_01

Figure A-FBCAA - Sheet 06

Replacement of the rods

DATE: Jan 17/11 SERVICE BULLETIN No.: A330-53-3186

REVISION No.: 01 - Apr 07/11 Page: 69

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@A330

SERVICE BULLETIN

**CONF ALL

A

FR37.4

FR39.1

B

(30)

(31)

LH

RH

LH SIDE SHOWN

RH SIDE SYMMETRICAL

B

A

G_SB_533186_5_BDAA_01_00

Figure A-FBDAA - Sheet 01

Removal/Installation of the Aft Fillet Fairing for Access.

DATE: Jan 17/11 SERVICE BULLETIN No.: A330-53-3186

REVISION No.: 01 - Apr 07/11 Page: 70

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@A330

SERVICE BULLETIN

Appendix 01

**CONF ALL

(1) The result of the inspection, including no findings, replacement or actions to be done, must be

forwarded to AIRBUS Department SEES1, on the attached inspection report sheet.

DATE: Jan 17/11 SERVICE BULLETIN No.: A330-53-3186

REVISION No.: 01 - Apr 07/11 Page: 1

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@A330

SERVICE BULLETIN

Appendix 01

**CONF ALL

INSPECTION REPORT

DETAIL LH

TAC ROD

YES

SERVICE BULLETIN No. :

A/C MSN :

FLIGHT CYCLES :

FLIGHT HOURS :

A330−53−3186

DATE OF INSPECTION :

RETURN TO :

AIRBUS

CUSTOMER SERVICES ENGINEERING − SEES1

FUSELAGE (WB/LR) − VERTICAL TAIL PLANE −

INSPECTION METHOD :

CENTER WING BOX (WB/LR)

1 ROUND POINT MAURICE BELLONTE

31707 BLAGNAC CEDEX

FRANCE

FAX +33 (0)5 61 93 36 14

CRACK FOUND ROD REPLACED

G_SB_533186_5_AAAA_01_00

ROD LOCATION

B NO YES NO YES NO

DETAIL RH B YES NO YES NO YES NO

DETAIL LH C YES NO YES NO YES NO

DETAIL RH C YES NO YES NO YES NO

DETAIL LH D YES NO YES NO YES NO

DETAIL RH D YES NO YES NO YES NO

DETAIL E YES NO YES NO YES NO

DETAIL LH F YES NO YES NO YES NO

DETAIL RH F YES NO YES NO YES NO

DETAIL LH G YES NO YES NO YES NO

DETAIL RH G YES NO YES NO YES NO

DETAIL LH H YES NO YES NO YES NO

DETAIL RH H YES NO YES NO YES NO

DETAIL LH J YES NO YES NO YES NO

DETAIL RH J YES NO YES NO YES NO

DETAIL LH K YES NO YES NO YES NO

DETAIL RH K YES NO YES NO YES NO

DETAIL LH L YES NO YES NO YES NO

DETAIL RH L YES NO YES NO YES NO

DETAIL LH M YES NO YES NO YES NO

DETAIL RH M YES NO YES NO YES NO

Figure A-FAAAA - Sheet 01

Inspection Report

DATE: Jan 17/11 SERVICE BULLETIN No.: A330-53-3186

REVISION No.: 01 - Apr 07/11 Page: 2

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@A330

SERVICE BULLETIN

Appendix 01

**CONF ALL

A Z190

FR53.9

FR53.2

FR48

FR37

FR39

A

B

C B

C

M D

G

F

H

E

D

M

K

G F

J

H

L

L

J

K

G_SB_533186_5_AAAA_02_01

Figure A-FAAAA - Sheet 02

Inspection Report

DATE: Jan 17/11 SERVICE BULLETIN No.: A330-53-3186

REVISION No.: 01 - Apr 07/11 Page: 3

5

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

SERVICE BULLETIN

REPORTING SHEET

TITLE: FUSELAGE - CENTER FUSELAGE - INSPECTION OF RODS IN BELLY

FAIRING

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 17/11 SERVICE BULLETIN No.: A330-53-3186

REVISION No.: 01 - Apr 07/11 Page: 1

5

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

SERVICE BULLETIN

QUALITY PERCEPTION FORM

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

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

improve the quality of our Service Bulletins.

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

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

- Quality rating of this SB 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 17/11 SERVICE BULLETIN No.: A330-53-3186

REVISION No.: 01 - Apr 07/11 Page: 1

5

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