@A318/A319/A320/A321

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 - INSPECT THE KEEL BEAM SIDE

PANELS BETWEEN FR40 AND FR42 RH/LH

MODIFICATION No.: None

This page transmits Revision No.04 of Service Bulletin No.A320-53-1060

ADDITIONAL WORK

**CONF ALL

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

REASON

Revision No. 04 issued to:

- Add illustration,

- Amend the Job Set-up and Close-up procedures,

- Update the effectivity,

- Introduce minor changes.

CHANGES

FRONT MATTER

FUSELAGE - CENTER FUSELAGE -

INSPECT THE KEEL BEAM SIDE

PANELS BETWEEN FR40 AND FR42

RH/LH

CONFIGURATION UPDATED R

SUMMARY

EFFECTIVITY OPERATOR LIST UPDATED R

PLANNING INFORMATION

EFFECTIVITY EFFECTIVITY RELATED INFORMATION

UPDATED

R

Configuration definition

CONF 001 CONFIGURATION DEFINITION UPDATED R

DATE: Jun 19/02 SERVICE BULLETIN No.: A320-53-1060

REVISION No.: 04 - Sep 13/12 Page: 1

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

REFERENCES REFERENCED DOCUMENTATION UPDATED R

ACCOMPLISHMENT INSTRUCTIONS

TASK 531060- 832-848-001-INSPECTION

Subtask 531060-910-201-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

Subtask 531060-941-201-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

CONFIGURATION UPDATED

FIGURE REFERENCE UPDATED

REFERENCES UPDATED

R

Subtask 531060-832-201-001 SUBTASK SOLUTION UPDATED

NOTE UPDATED

R

Subtask 531060-942-201-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

FIGURE REFERENCE UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

Fig. A-GBBAA FIGURE SOLUTION ADDED N

Fig. A-GBBAA Sheet 01 SHEET ADDED N

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

Revision No. 01 was issued to change the compliance from Recommended to Mandatory, amend

details for gaining access and update manpower data and inspection references.

Revision No. 02 issued to :

change the inspection method and associated intervals,

update the effectivity,

incorporate minor changes.

Revision No. 03 issued to :

Update the title.

Update the effectivity.

Introduce minor changes.

DATE: Jun 19/02 SERVICE BULLETIN No.: A320-53-1060

REVISION No.: 04 - Sep 13/12 Page: 2

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

REVISION SEQUENCE

ORIGINAL: Jun 19/02

REVISION No.: 01 - Apr 02/04

REVISION No. : 02 - Nov 30/10

REVISION No. : 03 - Jan 20/12

REVISION No. : 04 - Sep 13/12

DATE: Jun 19/02 SERVICE BULLETIN No.: A320-53-1060

REVISION No.: 04 - Sep 13/12 Page: 3

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

This Page Intentionally Left Blank

DATE: Jun 19/02 SERVICE BULLETIN No.: A320-53-1060

REVISION No.: 04 - Sep 13/12 Page: 4

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SERVICE BULLETIN

SUMMARY

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

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

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 53

TITLE: FUSELAGE - CENTER FUSELAGE - INSPECT THE KEEL BEAM SIDE

PANELS BETWEEN FR40 AND FR42 RH/LH

**CONF ALL

MODIFICATIONS

None

REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES

During a structural fatigue test at 110,223 simulated flights, cracks were found in the keel beam side

panel in the riveting below the center wing box at STGR42 LH/RH between FR40 and FR42. At

120,000 simulated flights, a crack was found in the keel beam side panel at the upper elliptical cutout at

STGR42 LH/RH forward of FR41.

This Service Bulletin defines Eddy Current NDT inspection for cracks in the area around the rivets on

both sides of the keel beam side panel below the center wing box at STGR42 LH/RH between FR40

and FR42 and in part of the area of the upper elliptical cutout at STGR42 LH/RH forward of FR41.

The accomplishment of this Service Bulletin will avoid extensive repair and aircraft down time.

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 YES VENDOR SB INVOLVED NO

NOTE (1): Service Bulletin must be accomplished.

MATERIAL PRICE INFORMATION

No Material

DATE: Jun 19/02 SERVICE BULLETIN No.: A320-53-1060

REVISION No.: 04 - Sep 13/12 Page: 1

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SERVICE BULLETIN

SUMMARY

EFFECTIVITY

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

09S 14S 15T 31V 35U 36V 47Y 53Z 56W 59Z 64S 66X 69X

73W 78T 85T 86W 86Z 98W AAF ABQ ACA ADR AFR AGC AHY

AIJ AJM AMU ANA ART AUA AZA AZI B2V BAW BEL BER BGH

BMA BTV C9G CCA CCM CES CIB CQH CQN CSA CSC CSN CTN

CYP D2F DAL DCS DLH EAA EDW EIN ETD EZD F2I FFT FHE

FHY FIN FPY FRN G2X G4I G8E GIA GIR GSW GWI HAY HDA

HRM HVN I2L IAC IBE IBS IRA ISS JAV JBU JET KAC KCA

KHO KKK KMF LAN LBT LBY LFO LLM LLP LMU MLD MLR MMA

MON MSR MXA NVD O2X OHY OZW PAL PIC PTR QAF RFJ RNV

RYW RZO SBI SBN SDM SFW SGG SHJ SHY SKU SLK SNX SOL

STU SVR SWM SWR SYR TAE TAI TAM TAP TAR TBJ TCW TCX

THY TNA TOM UAL UDC USA VLE VLG VLK VOI WGT WHT WTJ

XLF YAP

NOTE: This Service Bulletin is not applicable on A321 aircraft due to the serial embodiment of

Mod. No. 22015K02115.

NOTE: This Service Bulletin is not applicable on A320 aircraft MSN 1542 and subsequent and

on A319 aircraft MSN 1558 and subsequent due to the serial embodiment of Mod. No.

30355K06829.

CONCURRENT REQUIREMENTS

None

REFERENCES / REPERCUSSIONS

TFU None

OEB None

AOT None

SIL None

LINE MAINTENANCE AFFECTED No

LIFE LIMIT None

NATURE OF THE WORK

AIRCRAFT YES

EQUIPMENT NO

HARD NO

SOFT NO

OBRM NO

MANPOWER

Task 531060-832-848-001: INSPECTION

TOTAL MANHOURS 29.00

ELAPSED TIME (HOURS) 18.00

DATE: Jun 19/02 SERVICE BULLETIN No.: A320-53-1060

REVISION No.: 04 - Sep 13/12 Page: 2

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SERVICE BULLETIN

SUMMARY

APPENDICES

None

DATE: Jun 19/02 SERVICE BULLETIN No.: A320-53-1060

REVISION No.: 04 - Sep 13/12 Page: 3

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SERVICE BULLETIN

SUMMARY

**CONF ALL

INSPECTION AREA A

INSPECTION AREA B

A A

B B SIMILAR

A

FR36 FR42

STGR42RH

STGR42LH

A

A

B

B

FR40 FR41 FR42

STGR42LH

A

Z190

N_SB_531060_6_SAAA_01_01

Figure A-GSAAA - Sheet 01

DATE: Jun 19/02 SERVICE BULLETIN No.: A320-53-1060

REVISION No.: 04 - Sep 13/12 Page: 4

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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 - INSPECT THE KEEL BEAM SIDE

PANELS BETWEEN FR40 AND FR42 RH/LH

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

NOTE: This Service Bulletin is not applicable on A321 aircraft due to the serial

embodiment of Mod. No. 22015K02115.

NOTE: This Service Bulletin is not applicable on A320 aircraft MSN 1542 and

subsequent and on A319 aircraft MSN 1558 and subsequent due to the serial

embodiment of Mod. No. 30355K06829.

(1) Models

319-111 319-112 319-113 319-114 319-115 319-131 319-132 319-133

320-211 320-212 320-214 320-231 320-232 320-233

(2) Effectivity by MSN

0029 0039 0042-0059 0061 0063-0078 0080-0090 0093-0097 0099 0102-0104

0109-0127 0135-0155 0157-0162 0164-0176 0178-0179 0181-0183 0185-0187

0189-0192 0194-0195 0197-0224 0227 0229-0237 0239-0270 0272-0279 0281-0285

0287 0289-0303 0306-0312 0314 0316-0337 0339-0343 0345-0362 0365-0373

0375-0384 0386-0396 0398-0411 0413-0432 0435-0436 0438-0452 0454-0457

0459-0466 0469-0472 0475-0476 0478-0480 0482-0483 0485-0487 0489-0492

0496-0497 0499-0501 0503-0504 0506-0508 0510-0512 0523 0525 0527-0528

DATE: Jun 19/02 SERVICE BULLETIN No.: A320-53-1060

REVISION No.: 04 - Sep 13/12 Page: 1

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SERVICE BULLETIN

0530-0531 0533-0534 0537 0539-0540 0542-0543 0545-0546 0548-0549 0551

0553-0554 0556 0558-0559 0561-0562 0565-0566 0568-0569 0571-0575 0577-0580

0582 0584-0585 0587-0590 0592 0594 0596 0598 0600-0601 0603 0605 0607-0613

0615-0619 0621-0627 0629-0630 0634-0641 0643-0651 0653-0662 0665 0667

0669-0673 0676 0678-0679 0681-0683 0685-0686 0688-0691 0693-0698 0700-0707

0709-0714 0716-0724 0726-0730 0732-0745 0747-0752 0754-0760 0762-0764

0766-0770 0772-0774 0776 0778-0780 0782-0786 0788 0790-0791 0793-0795

0797-0801 0803-0805 0807 0809 0812-0814 0816-0818 0820-0822 0824-0826

0828-0834 0836-0840 0842-0847 0849-0851 0853-0854 0856-0863 0865-0877

0879-0886 0888-0890 0892-0900 0902-0907 0909-0914 0916-0919 0921-0925

0927-0934 0936-0939 0942-0953 0955 0957-0958 0960 0962 0964-0967 0969

0971-0973 0975-0982 0984-0986 0988-0990 0992 0994 0996-1003 1005 1007

1009-1011 1013-1014 1016 1018-1020 1022 1025-1026 1028-1041 1043 1046-1059

1061-1079 1081-1093 1095-1132 1134-1143 1145-1152 1154-1160 1162-1173

1175-1184 1187 1189-1194 1196-1198 1200-1201 1203 1205-1206 1208-1213

1215-1217 1221-1226 1228-1232 1234-1237 1239-1240 1242-1249 1251-1259

1261-1272 1274-1275 1277 1279-1292 1294-1298 1300-1306 1308-1332 1334-1355

1357-1365 1367-1373 1375-1398 1400-1402 1404-1407 1409-1411 1413-1416

1418-1420 1422-1424 1426-1427 1429-1430 1432 1434-1435 1437 1439-1441

1443-1446 1448-1450 1452-1454 1456-1457 1459-1461 1463-1464 1466-1471

1473-1475 1477-1480 1482-1486 1488-1491 1493-1495 1497-1498 1500-1502

1504-1510 1512-1516 1518 1520 1522-1524 1526-1530 1532-1535 1537-1538

1540-1541 1543 1545 1547 1549 1551-1552 1556

(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

09S 1300 1353

14S 0283

15T 0764 1494

31V 0164 0332 0368 0395

35U 0088

36V 0136

47Y 0394

53Z 1468

56W 0247 0257 0327 0335 0336

59Z 1556

64S 0407

66X 1068

69X 0219 0357 0588

73W 0087

78T 1306

85T 0234

86W 0384

86Z 1429

DATE: Jun 19/02 SERVICE BULLETIN No.: A320-53-1060

REVISION No.: 04 - Sep 13/12 Page: 2

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SERVICE BULLETIN

OPERATOR MSN

98W 0039 0042 0103 0109 0120

AAF 0244 0639

ABQ 1467

ACA 0059 0068 0073 0084 0122 0126 0127 0141 0149 0150 0154 0159

0174 0175 0183 0210 0231 0232 0233 0242 0248 0253 0254 0255

0265 0277 0284 0290 0309 0324 0330 0341 0378 0403 0404 0546

0572 0634 0656 0670 0672 0682 0688 0691 0693 0695 0697 0711

0719 0721 0728 0732 0736 0740 0742 0752 0757 0769 0773 0779

0785 0800 0813 0817 0829 0831 0840 0845

ADR 0043 0444

AFR 0044 0061 0063 0102 0115 0144 0145 0155 0186 0187 0214 0227

0236 0237 0239 0270 0278 0285 0287 0337 0352 0377 0491 0598

0600 0608 0618 0625 0637 0938 0985 0998 1000 1020 1025 1036

1151 1169 1176 1190 1201 1216 1267 1271 1344 1404 1415 1444

1449 1471 1502 1505 1524

AGC 0190

AHY 0331

AIJ 0169 0707 1132 1162 1179 1244 1259 1308 1322

AJM 0624 0626

AMU 0805 0928

ANA 0139 0151 0167 0170 0212 0245 0300 0328 0365 0383 0413 0482

0501 0507 0531 0534 0549 0554 0658 0669 0685

ART 0142 0279 0310 0311 0333 0359 0426 0724

AUA 0768 0776 0797 1137 1150 1189 1385 1387 1478

AZA 0951 0999 1138 1168 1217 1448 1457 1473 1480 1489

AZI 0527

B2V 0185 0191

BAW 1082 1115 1118 1142 1193 1197 1222 1225 1232 1236 1239 1258

1261 1279 1295 1329 1338 1380 1384 1423 1440 1445 1466 1510

1513 1529 1537

BEL 0644 1086 1102 1160 1336 1388 1441 1493

BER 1504

BGH 0221 0294 0349 1087

BMA 1014 1177 1418 1424

BTV 0168 0441 0449 0460 0461

C9G 0246 0710 0772

CCA 0876 0921 1296

CCM 1145

CES 0665 0754 0828 0838 0854 0883 0897 0909 0914 0925 0939 0967

0984 0986 1005 1028 1030 1041 1070 1072 1093 1108 1285 1303

1312 1316 1330 1345 1357 1361 1377 1386 1532 1541 1551

CIB 0774 0809 0884 0894 0905 0957 0971 1381 1402 1416 1437

CQH 0978 1286 1372

CQN 0696 0698 0704 0705

CSA 1439 1450

CSC 0540 0551 0556 0573 0582 0902 0912 0919 1007 1013 1500

DATE: Jun 19/02 SERVICE BULLETIN No.: A320-53-1060

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SERVICE BULLETIN

OPERATOR MSN

CSN 0709 0712 0718 0720 0722 0849 0859 0881 0895 0900 0950 0966

1035 1039 1057

CTN 0258 0767 0833 1009 1029 1237 1252

CYP 0256

D2F 0204 0215 0243 0251 0326 0411 0478

DAL 0118 0121 0125 0152 0153 0160 0171 0192 0197 0206 0208 0213

0262 0263 0272 0273 0281 0282 0297 0298 0306 0307 0318 0319

0329 0339 0340 0355 0358 0360 0367 0372 0380 0381 0387 0388

0399 0408 0410 0417 0418 0766 0778 0786 0801 0807 0818 0830

0832 0846 0903 0907 0911 0923 0962 0964 0981 0988 0996 1011

1037 1058 1062 1191 1230 1249 1324 1325 1346 1392 1414 1434

1453 1456 1483 1498 1501 1520 1535 1543 1549

DCS 1053

DLH 0069 0070 0071 0072 0078 0083 0086 0093 0094 0104 0110 0111

0116 0117 0135 0137 0147 0161 0162 0172 0200 0201 0202 0209

0216 0217 0218 0267 0268 0269 0346 0382 0401 0609 0610 0616

0623 0627 0636 0641 0646 0651 0654 0679 0689 0694 0700 0717

0723 0729 0738 0744 0794 0853 0860 0875 1016 1172 1337 1365

1367

EAA 0386 0445

EDW 0942 0947 1026

EIN 1242 1394 1443

ETD 0350

EZD 0667 0743 0872 0874 1074

F2I 0391 0615

FFT 1515

FHE 0888 0936 1171 1210

FHY 0580

FIN 1073 1107 1184 1309 1352 1364 1405 1470

FPY 0112 0189 0342 0438

FRN 0409 0466 0497

G2X 0347

G4I 1157

G8E 0222 0348 0369 0373 1464

GIA 0839 0892

GIR 0630

GSW 0376

GWI 1077 1084 1089 1136 1147 1155 1170 1209 1277

HAY 0716 0949

HDA 0756 0784 0812 0930 1253

HRM 0293

HVN 0590 0594 0601 0605 0607 0611 0617 0619 0648 0650

I2L 0443 1407 1497

IAC 0045 0046 0047 0048 0049 0050 0051 0056 0057 0058 0074 0075

0080 0089 0090 0095 0096 0097 0308 0314 0396 0398 0416 0423

0431 0432 0451 0469 0486 0490 0492 0499

DATE: Jun 19/02 SERVICE BULLETIN No.: A320-53-1060

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SERVICE BULLETIN

OPERATOR MSN

IBE 0223 0274 1047 1059 1067 1099 1119 1154 1180 1208 1229 1247

1255 1262 1288 1292 1318 1347 1362 1530 1540

IBS 0158 0173 0176 0207 0224 0266 0323 0356 1101 1516

IRA 0303 0312 0345 0530 0575 0857

ISS 0737 0749 1048 1125 1198 1283 1305

JAV 0029

JBU 1123 1156 1173 1235 1240 1257 1270 1280 1302 1327 1398 1446

1452 1506 1528

JET 0371 0421 0542 0647 0660 0816 0877

KAC 0181 0182 0195

KCA 0393 0414

KHO 0354 0361 0362 0405

KKK 1124

KMF 0480

LAN 1304 1332 1351 1355 1491 1512 1526

LBT 0301 0400 0793 0937 1121 1175

LBY 0558 0561 1098

LFO 0659

LLM 1054

LLP 0739 1411

LMU 0932 0943

MLD 0249 0622 0741

MLR 0977

MMA 0113 0114 0295 0316

MON 0379 0389 0392 1081 1370

MSR 0165 0166 0178 0194 0198 0322 0351 0366

MXA 0252 0259 0260 0261 0275 0276 0296 0320 0321 0353

NVD 0211 0299 0375 0415 0419 0528 1263

O2X 0291 0292 1183 1383

OHY 0455 0471 0496 0543 0640 0661 0676 0916 1482 1509

OZW 0429

PAL 0706 0745

PIC 0990

PTR 0459 0537

QAF 0927 1335

RFJ 0814

RNV 0229 0913

RYW 0569

RZO 0795

SBI 1071 1078 1090 1091 1126 1129 1131 1149 1164 1167

SBN 0325 0428

SDM 0427 0525 0649 1130 1488

SFW 0671 0994

SGG 0799 0879 1390

SHJ 0910

SHY 0138 0148 1194

DATE: Jun 19/02 SERVICE BULLETIN No.: A320-53-1060

REVISION No.: 04 - Sep 13/12 Page: 5

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SERVICE BULLETIN

OPERATOR MSN

SKU 0179 0406 0447 1400 1523

SLK 0899 0969 1228 1422

SNX 0289

SOL 0302

STU 0420 0436 0446

SVR 0140 0157 0203 0220 0735 1063 1152 1484

SWM 0430 0476

SWR 0545 0553 0559 0562 0574 0577 0578 0585 0596 0603 0612 0621

0635 0643 0673 0681 0701 0703 0713 0727 0734 0782 1018

SYR 0886 0918 1032 1076 1085 1117

TAE 0657 0934 0946

TAI 1066 1113 1334

TAM 0250 0334 0440 0758 0976 1010 1092 1096 1103 1139 1143 1158

1215 1246 1251 1339 1368 1376 1459 1486 1518

TAP 0629 0750 0755 0763 0790 0821 0837 0870 0906 0917 0933 0945

0960 0979 0982 1034 1100 1106 1120 1127 1165 1181 1206 1231

TAR 0119 0123 0124 0205 0370 0390 0402 0511 0869 0880 0958 0975

1187 1479

TBJ 1485

TCW 0425 0653

TCX 0424

THY 1002

TNA 0791 0822

TOM 1320

UAL 0435 0439 0442 0450 0452 0454 0456 0457 0462 0463 0464 0465

0470 0472 0475 0479 0483 0485 0487 0489 0500 0503 0504 0506

0508 0510 0512 0523 0539 0568 0571 0587 0589 0592 0613 0638

0655 0678 0683 0686 0690 0702 0748 0751 0759 0780 0783 0788

0798 0804 0820 0824 0825 0826 0834 0836 0842 0843 0847 0850

0851 0858 0862 0865 0867 0871 0873 0882 0893 0898 0944 0948

0952 0955 0965 0980 0989 1001 1022 1031 1104 1105 1128 1146

1163 1192 1211 1243 1248 1266 1272 1282 1290 1291 1321 1341

1343 1359 1363 1401 1409 1420 1426 1427 1432 1435 1460 1469

1474 1475 1477 1495 1507 1508 1514 1522 1533 1538 1545

UDC 0085 0230 0235 0579 0645 0662 0733 0747 0760

USA 0052 0053 0054 0055 0064 0065 0066 0067 0076 0077 0081 0082

0099 0317 0448 0565 0584 0762 0770 0803 0844 0856 0861 0863

0866 0868 0885 0889 0890 0896 0904 0922 0924 0929 0931 0953

0972 0997 1003 1019 1033 1038 1040 1043 1046 1049 1050 1051

1052 1055 1056 1061 1064 1065 1069 1075 1079 1083 1088 1095

1097 1109 1110 1111 1112 1114 1116 1122 1134 1135 1141 1148

1166 1178 1182 1196 1203 1205 1223 1224 1234 1245 1254 1264

1265 1268 1269 1274 1275 1281 1284 1287 1289 1294 1297 1298

1301 1310 1311 1313 1314 1315 1317 1319 1323 1326 1328 1331

1340 1342 1348 1350 1354 1358 1360 1369 1371 1373 1375 1378

1382 1389 1391 1393 1395 1397 1406 1410 1419 1463 1490 1527

1534 1547 1552

VLE 1226

DATE: Jun 19/02 SERVICE BULLETIN No.: A320-53-1060

REVISION No.: 04 - Sep 13/12 Page: 6

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OPERATOR MSN

VLG 0143 0146 0199 0240 0241 0264 0992 1221 1349 1396 1413 1430

1461

VLK 0422 0714 0730 1200 1213 1379

VOI 1140 1159

WGT 1212

WHT 0726 1256

WTJ 0548

XLF 0343

YAP 0533 0566 0973 1454

DATE: Jun 19/02 SERVICE BULLETIN No.: A320-53-1060

REVISION No.: 04 - Sep 13/12 Page: 7

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(4) Configuration by MSN

MSN CONFIGURATION

0029 0039 0042 0043 0044 0045 0046 0047 0048 0049 0050

0051 0052 0053 0054 0055 0056 0057 0058 0059 0061 0063

0064 0065 0066 0067 0068 0069 0070 0071 0072 0073 0074

0075 0076 0077 0078 0080 0081 0082 0083 0084 0085 0086

0087 0088 0089 0090 0093 0094 0095 0096 0097 0099 0102

0103 0104 0109 0110 0111 0112 0113 0114 0115 0116 0117

0118 0119 0120 0121 0122 0123 0124 0125 0126 0127 0135

0136 0137 0138 0139 0140 0141 0142 0143 0144 0145 0146

0147 0148 0149 0150 0151 0152 0153 0154 0155 0157 0158

0159 0160 0161 0162 0164 0165 0166 0167 0168 0169 0170

0171 0172 0173 0174 0175 0176 0178 0179 0181 0182 0183

0185 0186 0187 0189 0190 0191 0192 0194 0195 0197 0198

0199 0200 0201 0202 0203 0204 0205 0206 0207 0208 0209

0210 0211 0212 0213 0214 0215 0216 0217 0218 0219 0220

0221 0222 0223 0224 0227 0229 0230 0231 0232 0233 0234

0235 0236 0237 0239 0240 0241 0242 0243 0244 0245 0246

0247 0248 0249 0250 0251 0252 0253 0254 0255 0256 0257

0258 0259 0260 0261 0262 0263 0264 0265 0266 0267 0268

0269 0270 0272 0273 0274 0275 0276 0277 0278 0279 0281

0282 0283 0284 0285 0287 0289 0290 0291 0292 0293 0294

0295 0296 0297 0298 0299 0300 0301 0302 0303 0306 0307

0308 0309 0310 0311 0312 0314 0316 0317 0318 0319 0320

0321 0322 0323 0324 0325 0326 0327 0328 0329 0330 0331

0332 0333 0334 0335 0336 0337 0339 0340 0341 0342 0343

0345 0346 0347 0348 0349 0350 0351 0352 0353 0354 0355

0356 0357 0358 0359 0360 0361 0362 0365 0366 0367 0368

0369 0370 0371 0372 0373 0375 0376 0377 0378 0379 0380

0381 0382 0383 0384 0386 0387 0388 0389 0390 0391 0392

0393 0394 0395 0396 0398 0399 0400 0401 0402 0403 0404

0405 0406 0407 0408 0409 0410 0411 0413 0414 0415 0416

0417 0418 0419 0420 0421 0422 0423 0424 0425 0426 0427

0428 0429 0430 0431 0432 0435 0436 0438 0439 0440 0441

0442 0443 0444 0445 0446 0447 0448 0449 0450 0451 0452

0454 0455 0456 0457 0459 0460 0461 0462 0463 0464 0465

0466 0469 0470 0471 0472 0475 0476 0478 0479 0480 0482

0483 0485 0486 0487 0489 0490 0491 0492 0496 0497 0499

0500 0501 0503 0504 0506 0507 0508 0510 0511 0512 0523

0525 0527 0528 0530 0531 0533 0534 0537 0539 0540 0542

0543 0545 0546 0548 0549 0551 0553 0554 0556 0558 0559

0561 0562 0565 0566 0568 0569 0571 0572 0573 0574 0575

0577 0578 0579 0580 0582 0584 0585 0587 0588 0589 0590

0592 0594 0596 0598 0600 0601 0603 0605 0607 0608 0609

0610 0611 0612 0613 0615 0616 0617 0618 0619 0621 0622

0623 0624 0625 0626 0627 0629 0630 0634 0635 0636 0637

0638 0639 0640 0641 0643 0644 0645 0646 0647 0648 0649

0650 0651 0653 0654 0655 0656 0657 0658 0659 0660 0661

0662 0665 0667 0669 0670 0671 0672 0673 0676 0678 0679

0681 0682 0683 0685 0686 0688 0689 0690 0691 0693 0694

0695 0696 0697 0698 0700 0701 0702 0703 0704 0705 0706

001

DATE: Jun 19/02 SERVICE BULLETIN No.: A320-53-1060

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MSN CONFIGURATION

0707 0709 0710 0711 0712 0713 0714 0716 0717 0718 0719

0720 0721 0722 0723 0724 0726 0727 0728 0729 0730 0732

0733 0734 0735 0736 0737 0738 0739 0740 0741 0742 0743

0744 0745 0747 0748 0749 0750 0751 0752 0754 0755 0756

0757 0758 0759 0760 0762 0763 0764 0766 0767 0768 0769

0770 0772 0773 0774 0776 0778 0779 0780 0782 0783 0784

0785 0786 0788 0790 0791 0793 0794 0795 0797 0798 0799

0800 0801 0803 0804 0805 0807 0809 0812 0813 0814 0816

0817 0818 0820 0821 0822 0824 0825 0826 0828 0829 0830

0831 0832 0833 0834 0836 0837 0838 0839 0840 0842 0843

0844 0845 0846 0847 0849 0850 0851 0853 0854 0856 0857

0858 0859 0860 0861 0862 0863 0865 0866 0867 0868 0869

0870 0871 0872 0873 0874 0875 0876 0877 0879 0880 0881

0882 0883 0884 0885 0886 0888 0889 0890 0892 0893 0894

0895 0896 0897 0898 0899 0900 0902 0903 0904 0905 0906

0907 0909 0910 0911 0912 0913 0914 0916 0917 0918 0919

0921 0922 0923 0924 0925 0927 0928 0929 0930 0931 0932

0933 0934 0936 0937 0938 0939 0942 0943 0944 0945 0946

0947 0948 0949 0950 0951 0952 0953 0955 0957 0958 0960

0962 0964 0965 0966 0967 0969 0971 0972 0973 0975 0976

0977 0978 0979 0980 0981 0982 0984 0985 0986 0988 0989

0990 0992 0994 0996 0997 0998 0999 1000 1001 1002 1003

1005 1007 1009 1010 1011 1013 1014 1016 1018 1019 1020

1022 1025 1026 1028 1029 1030 1031 1032 1033 1034 1035

1036 1037 1038 1039 1040 1041 1043 1046 1047 1048 1049

1050 1051 1052 1053 1054 1055 1056 1057 1058 1059 1061

1062 1063 1064 1065 1066 1067 1068 1069 1070 1071 1072

1073 1074 1075 1076 1077 1078 1079 1081 1082 1083 1084

1085 1086 1087 1088 1089 1090 1091 1092 1093 1095 1096

1097 1098 1099 1100 1101 1102 1103 1104 1105 1106 1107

1108 1109 1110 1111 1112 1113 1114 1115 1116 1117 1118

1119 1120 1121 1122 1123 1124 1125 1126 1127 1128 1129

1130 1131 1132 1134 1135 1136 1137 1138 1139 1140 1141

1142 1143 1145 1146 1147 1148 1149 1150 1151 1152 1154

1155 1156 1157 1158 1159 1160 1162 1163 1164 1165 1166

1167 1168 1169 1170 1171 1172 1173 1175 1176 1177 1178

1179 1180 1181 1182 1183 1184 1187 1189 1190 1191 1192

1193 1194 1196 1197 1198 1200 1201 1203 1205 1206 1208

1209 1210 1211 1212 1213 1215 1216 1217 1221 1222 1223

1224 1225 1226 1228 1229 1230 1231 1232 1234 1235 1236

1237 1239 1240 1242 1243 1244 1245 1246 1247 1248 1249

1251 1252 1253 1254 1255 1256 1257 1258 1259 1261 1262

1263 1264 1265 1266 1267 1268 1269 1270 1271 1272 1274

1275 1277 1279 1280 1281 1282 1283 1284 1285 1286 1287

1288 1289 1290 1291 1292 1294 1295 1296 1297 1298 1300

1301 1302 1303 1304 1305 1306 1308 1309 1310 1311 1312

1313 1314 1315 1316 1317 1318 1319 1320 1321 1322 1323

1324 1325 1326 1327 1328 1329 1330 1331 1332 1334 1335

1336 1337 1338 1339 1340 1341 1342 1343 1344 1345 1346

1347 1348 1349 1350 1351 1352 1353 1354 1355 1357 1358

1359 1360 1361 1362 1363 1364 1365 1367 1368 1369 1370

001

DATE: Jun 19/02 SERVICE BULLETIN No.: A320-53-1060

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MSN CONFIGURATION

1371 1372 1373 1375 1376 1377 1378 1379 1380 1381 1382

1383 1384 1385 1386 1387 1388 1389 1390 1391 1392 1393

1394 1395 1396 1397 1398 1400 1401 1402 1404 1405 1406

1407 1409 1410 1411 1413 1414 1415 1416 1418 1419 1420

1422 1423 1424 1426 1427 1429 1430 1432 1434 1435 1437

1439 1440 1441 1443 1444 1445 1446 1448 1449 1450 1452

1453 1454 1456 1457 1459 1460 1461 1463 1464 1466 1467

1468 1469 1470 1471 1473 1474 1475 1477 1478 1479 1480

1482 1483 1484 1485 1486 1488 1489 1490 1491 1493 1494

1495 1497 1498 1500 1501 1502 1504 1505 1506 1507 1508

1509 1510 1512 1513 1514 1515 1516 1518 1520 1522 1523

1524 1526 1527 1528 1529 1530 1532 1533 1534 1535 1537

1538 1540 1541 1543 1545 1547 1549 1551 1552 1556

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

MATERIAL QTY PER A/C SEE NOTES

Consumable CMLD01 1

B. CONCURRENT REQUIREMENTS

None

C. REASON

(1) History

During a structural fatigue test at 110,223 simulated flights, cracks were found in the

keel beam side panel in the riveting below the center wing box at STGR42 LH/RH

between FR40 and FR42. At 120,000 simulated flights, a crack was found in the keel

beam side panel at the upper elliptical cutout at STGR42 LH/RH forward of FR41.

(2) Objective/Action

This Service Bulletin defines Eddy Current NDT inspection for cracks in the area around

the rivets on both sides of the keel beam side panel below the center wing box at

STGR42 LH/RH between FR40 and FR42 and in part of the area of the upper elliptical

cutout at STGR42 LH/RH forward of FR41.

(3) Advantages

The accomplishment of this Service Bulletin will avoid extensive repair and aircraft down

time.

DATE: Jun 19/02 SERVICE BULLETIN No.: A320-53-1060

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(4) Operational/Maintenance Consequences

None

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

Task 531060-832-848-001: INSPECTION

(1) Inspect the keel beam side panel below the wing center box at STGR42 LH/RH

between FR40 and FR42 and in part of the area of the upper elliptical cutout at STGR42

LH/RH forward of FR41

E. COMPLIANCE

(1) Classification

MANDATORY: Service Bulletin must be accomplished.

(2) Accomplishment Timescale

For aircraft on which the initial issue or revision No. 01 of this Service Bulletin or the

Structural Significant Item (SSI) 53-31-42 have been accomplished previously :

- Areas without any findings when the initial issue or revision No. 01 of this Service

Bulletin or the Structural Significant Item (SSI) 53-31-42 accomplished :

The further inspections have to be performed in AREA A and AREA B as :

. Threshold for the next inspection (first NDT inspection)

The next inspection (NDT) in accordance with the revision No. 02 of this

Service Bulletin has to be performed within 4,300FC/9,600FH whichever occurs

first after the last visual inspection.

. Intervals for the further repetitive inspection

The further repetitive inspections in accordance with the revision No. 02 of this

Service Bulletin have to be performed at every 12,000 FC or 26,700 FH,

whichever occurs first.

- Areas with crack findings when the initial issue or revision No. 01 of this Service

Bulletin or the Structural Significant Item (SSI) 53-31-42 accomplished :

. Repair at the defined compliance time depending of the crack length :

AREA A :

In case of crack finding less than 5.0 mm (0.197 in.) repair within 7,500

FC/16,700 FH,

For cracks between 5.0 mm (0.197 in.) and not more than 10.0 mm (0.393 in.)

repair within 4,000 FC/8,900 FH,

For cracks between 10.0 mm (0.393 in.) and not more than 15.0 mm (0.591 in.)

repair within 1,700 FC/3,800 FH,

DATE: Jun 19/02 SERVICE BULLETIN No.: A320-53-1060

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For cracks between 15.0 mm (0.591 in.) and not more than 20.0 mm (0.79 in.)

repair within 860 FC/1,800 FH,

And for crack larger than 20.0 mm (0.79 in.) or multiple cracks repair before

next flight.

AREA B :

In case of crack finding contact AIRBUS for further instructions before next

flight.

NOTE: The compliance time defined in revision No. 02 of this Service Bulletin

has to be counted from latest crack length measurement before issuance

of revision No. 02. The instruction given in the initial issue or revision No.

01 of this Service Bulletin are no longer valid.

In the repaired areas no further inspection is required in accordance with this Service

Bulletin.

For aircraft on which the initial issue or revision No. 01 of this Service Bulletin or the

Structural Significant Item (SSI) 53-31-42 have not been accomplished previously :

- Threshold for the first inspection

At the latest of the 2 conditions :

Before accumulation 24,200 FC or 48,400 FH, whichever occurs first

or

within 3,500 FC from April 26, 2003.

- Intervals for the repetitive inspections

. Areas without any findings :

Repetitive inspections must be carried out every 12,000 FC or 26,700 FH,

whichever occurs first.

. Areas with crack findings :

Repair at the defined compliance time depending of the crack length :

AREA A :

In case of crack finding less than 5.0 mm (0.197 in.) repair within 7,500

FC/16,700 FH,

For cracks between 5.0 mm (0.197 in.) and not more than 10.0 mm (0.393 in.)

repair within 4,000 FC/8,900 FH,

For cracks between 10.0 mm (0.393 in.) and not more than 15.0 mm (0.591 in.)

repair within 1,700 FC/3,800 FH,

For cracks between 15.0 mm (0.591 in.) and not more than 20.0 mm (0.79 in.)

repair within 860 FC/1,800 FH,

And for crack larger than 20.0 mm (0.79 in.) or multiple cracks repair before

next flight.

AREA B :

In case of crack finding contact AIRBUS for further instructions before next

flight.

DATE: Jun 19/02 SERVICE BULLETIN No.: A320-53-1060

REVISION No.: 04 - Sep 13/12 Page: 12

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In the repaired areas no further inspection is required in accordance with this Service

Bulletin.

This Service Bulletin has been classified Mandatory by the issue of an Airworthiness

Directive (AD) published by the European Aviation Safety Agency (EASA). The AD must

be used as the reference document for the mandated accomplishment timescale.

F. APPROVAL

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

Organisation Approval No. EASA.21J.031.

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

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

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

before incorporation of the Service Bulletin.

G. MANPOWER

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

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

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

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

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

included.

Task 531060-832-848-001: INSPECTION

Get Access 7.00

On Aircraft

Inspect the keel beam side panel below the wing

center box at STGR42 LH/RH between FR40 and

FR42 and in part of the area of the upper elliptical

cutout at STGR42 LH/RH forward of FR41

12.00

Close-Up 10.00

TOTAL MANHOURS 29.00

ELAPSED TIME (HOURS) 18.00

H. WEIGHT AND BALANCE

Not Changed

I. ELECTRICAL LOAD DATA

Not Changed

J. REFERENCES

Aircraft Maintenance Manual (AMM) 06-20-00 06-31-53 06-40-00

12-34-24 20-16-00 28-13-42

29-10-00 29-13-42 29-14-00

29-24-51 32-12-00 53-35-13

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-33-00 20-55-00

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Non Destructive Test Manual (NTM) 53-30-02

Structural Repair Manual (SRM) 53-31-29

K. PUBLICATION AFFECTED

Impact on scheduled maintenance: Refer to Maintenance Planning Document (MPD).

L. INTERCHANGEABILITY/MIXABILITY

Not Applicable

M. SPARES

None

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2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

None

B. INDUSTRY SUPPORT INFORMATION

AIRBUS will not provide industrial support for accomplishment of this Service Bulletin.

C. LIST OF COMPONENTS

No Kit

D. LIST OF MATERIALS - OPERATOR SUPPLIED

(1) Consumable Materials

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO CML

MAT. No.

QTY PER A/C SEE

NOTES

Corrosion Compound 05-005 As required

Solvent, General Purpose 11-026 As required

Lint-Free Cotton Cloth 19-003 As required

(2) Components

None

(3) Equipment

None

E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

None

F. TOOLING

None

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This Page Intentionally Left Blank

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3. ACCOMPLISHMENT INSTRUCTIONS

Task 531060-832-848-001 - INSPECTION

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

INCLUDED IN THE REFERENCED PROCEDURES.

WARNING: PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION

BEFORE YOU START A TASK ON OR NEAR :

- THE FLIGHT CONTROLS

- THE FLIGHT CONTROL SURFACES

- THE LANDING GEAR AND RELATED DOORS

- ANY COMPONENTS THAT MOVE.

WARNING: BE CAREFUL WHEN YOU USE SOLVENTS/CLEANING AGENTS, SEALANTS

AND OTHER MATERIALS.

OBEY THE MATERIAL MANUFACTURER’S INSTRUCTIONS AND THE LOCAL

REGULATIONS.

MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK

AREA.

DO NOT BREATHE THE FUMES.

DO NOT SMOKE.

DO NOT USE THESE MATERIALS NEAR A FLAME, SPARKS OR SOURCES OF

HEAT.

USE PROTECTIVE CLOTHING, GOGGLES AND GLOVES.

IF YOU GET ONE OF THESE MATERIALS :

- ON YOUR SKIN OR IN YOUR EYES, FLUSH IT AWAY WITH A FLOW OF

CLEAN WATER

- IN YOUR MOUTH, GET IMMEDIATE MEDICAL AID.

IN GENERAL, THESE MATERIALS ARE FLAMMABLE, POISONOUS AND SKIN

IRRITANTS.

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CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP ELECTRICAL

WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY AND

MECHANICALLY SERVICEABLE).

WHEN YOU DO MAINTENANCE WORK, REPAIRS OR MODIFICATIONS,

ALWAYS KEEP ELECTRICAL WIRING, COMPONENTS AND THE WORK AREA

AS CLEAN AS POSSIBLE. TO DO THIS :

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

NECESSARY ON WIRING AND COMPONENTS

- REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND

OTHER CONTAMINATION.

THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION

AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION.

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

Task Associated Data

Zone

190

Access

Door 191KB 192KB 195BB 196BB

Manpower

TOTAL MANHOURS 29.00

ELAPSED TIME (HOURS) 18.00

A. GENERAL

(1) Subtask 531060-910-201-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

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

06-31-53, Page Block 001

06-40-00, Page Block 001

Task 20-16-00-912-001

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-33-00

(a) For the specification of materials (Mat. No.) given in this Service Bulletin (Refer to

Consumable Materials List (CML)).

(b) For circuit breaker safety practices (Refer to AMM Task 20-16-00-912-001).

(c) For the Frame (FR) identification (Refer to AMM 06-31-53, Page Block 001).

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

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

(f) Obey the instructions for the general wiring installation (Refer to ESPM 20-33-00).

(g) Tag all the parts you must remove and retain to make the subsequent installation

easier.

(2) Subtask 531060-839-201-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

B. PREPARATION

(1) Subtask 531060-941-201-001 - Job Set-up

Work Zones and Access Panels

Zone Access/Work location

190 Access Door 195BB, Door 196BB, Door 191KB, Door

192KB

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-869-002

Task 28-13-42-000-001

29-10-00, Page Block 201

Task 29-13-42-000-001

Task 29-14-00-614-001

Task 29-24-51-000-001

Task 32-12-00-010-001

Task 53-35-13-000-002

Fig. A-GBBAA

Clamps of the Electrical Wires

4632VB/2P and 4674VB/2M, between

FR41 and FR42

Sheet 01

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

12-34-24-869-002).

(b) Put access platforms in position at the access doors 195BB,196BB, 191KB and

192KB.

(c) Open the access doors 195BB,196BB, 191KB and 192KB (Refer to AMM Task

53-35-13-000-002).

(d) Open the right main door of the main landing gear (Refer to AMM Task

32-12-00-010-001).

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(e) Open, safety/lock and tag the applicable circuit breakers (Refer to AMM 29-10-00,

Page Block 201).

(f) De-pressurize the Green, Blue and Yellow hydraulic systems (Refer to AMM Task

29-14-00-614-001).

(g) De-pressurize the Green, Blue and Yellow hydraulic reservoirs (Refer to AMM Task

29-14-00-614-001).

(h) Put the warning notices in position to tell persons not to pressurize the hydraulic

systems :

1 in the flight compartment near the hydraulic section 40VU of the overhead

panel.

2 on the ground service panels of the Green, Blue and Yellow hydraulic

systems.

(i) Remove the Yellow Electric Pump, FIN 3075GX (Refer to AMM Task

29-24-51-000-001).

(j) Remove the Yellow Power Accumulator, FIN 3070GM (Refer to AMM Task

29-13-42-000-001).

(k) Remove and retain the clamps of the electrical wires 4632VB/2P and 4674VB/2M,

between FR41 and FR42, as necessary.

Refer to Fig. A-GBBAA Sheet 01.

(l) Remove the vapor seal/separating wall (Refer to AMM Task 28-13-42-000-001).

C. PROCEDURE

(1) Subtask 531060-832-201-001 - Inspect the keel beam side panel below the wing

center box at STGR42 LH/RH between FR40 and FR42 and in part of the area of

the upper elliptical cutout at STGR42 LH/RH forward of FR41

Work Zones and Access Panels

Zone Access/Work location

190

Manpower Resources

Manhours 12.00

Minimum number of person 2

Subtask elapsed time 6.00

Skills NON SPECIFIC

DATE: Jun 19/02 SERVICE BULLETIN No.: A320-53-1060

REVISION No.: 04 - Sep 13/12 Page: 20

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Material necessary to do the job

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Corrosion Compound 05-005 As required

Solvent, General Purpose 11-026 As required

Lint-Free Cotton Cloth 19-003 As required

References

Non Destructive Test Manual (NTM) Task 53-30-02-250-801

Structural Repair Manual (SRM) 53-31-29

Fig. A-GBAAA

Inspection Area

Sheet 01

Sheet 02

Fig. A-GFAAA

Flow Chart

Sheet 01

Sheet 02

NOTE: The inspection is to be performed on the outboard surface only on the

left hand and the right hand sides of the keel beam side panels.

NOTE: The accomplishment of a repair (Refer to SRM 53-31-29 Page Block

201, Para. 5.C. Figure 203) in case of crack findings in AREA A cancels

the inspection requirements of this Service Bulletin in AREA A. The

AREA B must still be inspected.

NOTE: If a previous repair (Refer to SRM 53-31-29 Page Block 201, Para. 5.A.

Figure 201 and/or Para. 5.B. Figure 202) has been done, the inspection

is no longer required in the repaired area. The remaining areas must be

inspected in accordance with this Service Bulletin.

(a) Clean the inspection and work areas with :

Solvent, General

Purpose

11-026 As required

Lint-Free Cotton

Cloth

19-003 As required

(b) The inspections required in this Service Bulletin are to be performed in areas which

have not been repaired by any previous actions. The repaired areas by SRM,

Repair Approval Sheet (RAS) as a final solution are not more subject of this

Service Bulletin.

(c) Do the Eddy Current NDT inspection (Refer to NTM Task 53-30-02-250-801) in the

area around the fastener heads at both sides of the keel beam side panel below

the wing center box at STGR42 LH/RH between FR40 and FR42 and in part of the

area of the upper elliptical cutout at STGR42 LH/RH forward of FR41 in AREA A

and AREA B.

Refer to Fig. A-GBAAA Sheet 01 and Fig. A-GBAAA Sheet 02 Detail B.

DATE: Jun 19/02 SERVICE BULLETIN No.: A320-53-1060

REVISION No.: 04 - Sep 13/12 Page: 21

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Refer to Fig. A-GFAAA Sheet 01 and Fig. A-GFAAA Sheet 02

NOTE: Do the Eddy Current NDT inspection at a threshold of 24,200 FC or

48,400 FH, whichever occurs first.

1 For AREA A :

a In the case of no crack is found:

<1> Repeat this inspection every 12,000 FC or 26,700 FH, whichever

occurs first.

b In the case a single crack is found:

<1> If the crack length is less than 5.0 mm (0.197 in.) :

<a> Repair the AREA A within 7,500 FC or 16,700 FH, whichever

occurs first (Refer to SRM 53-31-29 Page Block 201, Para.

5.C. Figure 203). After repair in AREA A, the AREA B must still

be inspected.

<2> If the crack length is between 5.0 mm (0.197 in.) and not more than

10.0 mm (0.393 in.) :

<a> Repair the AREA A within 4,000 FC or 8,900 FH, whichever

occurs first (Refer to SRM 53-31-29 Page Block 201, Para.

5.C. Figure 203). After repair in AREA A, the AREA B must still

be inspected.

<3> If the crack length is between 10.0 mm (0.393 in.) and not more

than 15.0 mm (0.591 in.) :

<a> Repair the AREA A within 1,700 FC or 3,800 FH, whichever

occurs first (Refer to SRM 53-31-29 Page Block 201, Para.

5.C. Figure 203). After repair in AREA A, the AREA B must still

be inspected.

<4> If the crack length is between 15.0 mm (0.59 in.) and not more than

20.0 mm (0.79 in.) :

<a> Repair the AREA A within 860 FC or 1,800 FH, whichever

occurs first (Refer to SRM 53-31-29 Page Block 201, Para.

5.C. Figure 203). After repair in AREA A, the AREA B must still

be inspected.

<5> If the crack length is more than 20.0 mm (0.79 in.) or in the case of

multiple cracks are found:

<a> Repair the AREA A before the next flight (Refer to SRM

53-31-29 Page Block 201, Para. 5.C. Figure 203). After the

repair in AREA A, the AREA B must still be inspected.

DATE: Jun 19/02 SERVICE BULLETIN No.: A320-53-1060

REVISION No.: 04 - Sep 13/12 Page: 22

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SERVICE BULLETIN

c The repaired area is not more to be inspected by this Service Bulletin.

The non-repaired area has to be inspected by repetitive inspection as

described in this Service Bulletin.

2 For AREA B :

a In the case of no crack is found:

<1> Repeat this inspection every 12,000 FC or 26,700 FH, whichever

occurs first.

NOTE: These new intervals are applicable when the first

Eddy Current NDT inspection has been done in

accordance with this Inspection Service Bulletin.

b In the case of crack is found:

<1> Contact AIRBUS for further repair instructions before next flight.

(d) After inspection apply a layer of :

Corrosion

Compound

05-005 As required

D. TEST

None

E. CLOSE-UP

(1) Subtask 531060-942-201-001 - Close-up

Work Zones and Access Panels

Zone Access/Work location

190 Access Door 195BB, Door 195BB, Door 191KB, Door

192KB

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 28-13-42-400-001

29-10-00, Page Block 201

Task 29-13-42-400-001

Task 29-14-00-614-002

Task 29-24-51-400-001

Task 32-12-00-410-001

Task 53-35-13-400-002

Fig. A-GBBAA

Clamps of the Electrical Wires

4632VB/2P and 4674VB/2M, between

FR41 and FR42

Sheet 01

DATE: Jun 19/02 SERVICE BULLETIN No.: A320-53-1060

REVISION No.: 04 - Sep 13/12 Page: 23

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

equipment.

(b) Install the vapor seal/separating wall (Refer to AMM Task 28-13-42-400-001).

(c) Install the retained clamps of the electrical wires 4632VB/2P and 4674VB/2M,

between FR41 and FR42.

Refer to Fig. A-GBBAA Sheet 01.

(d) Install the Yellow Electric Pump, FIN 3075GX (Refer to AMM Task

29-24-51-400-001).

(e) Install the Yellow Power Accumulator, FIN 3070GM (Refer to AMM Task

29-13-42-400-001).

(f) Remove the safety clip(s) and/or the tag(s) and close/unlock the applicable circuit

breakers (Refer to AMM 29-10-00, Page Block 201).

(g) Remove the warning notices.

(h) Pressurize the Green, Blue and Yellow hydraulic reservoirs (Refer to AMM Task

29-14-00-614-002).

(i) Pressurize the Green, Blue and Yellow hydraulic systems (Refer to AMM Task

29-14-00-614-002).

(j) Close the access doors 195BB, 196BB, 191KB and 192KB (Refer to AMM Task

53-35-13-400-002).

(k) Remove the access platform(s).

(l) Close the right main door of the landing gear (Refer to AMM Task

32-12-00-410-001).

DATE: Jun 19/02 SERVICE BULLETIN No.: A320-53-1060

REVISION No.: 04 - Sep 13/12 Page: 24

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SERVICE BULLETIN

**CONF ALL

FR41

FR42

A

A

Z190

B

CLAMPS FR41 CLAMP

4632VB /2P

4674VB /2M

FWD B

N_SB_531060_6_BBAA_01_01

Figure A-GBBAA - Sheet 01

Clamps of the Electrical Wires 4632VB/2P and 4674VB/2M, between FR41 and FR42

DATE: Jun 19/02 SERVICE BULLETIN No.: A320-53-1060

REVISION No.: 04 - Sep 13/12 Page: 25

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**CONF ALL

FR39 FR40 FR41 FR43

FR42

A

B

FR36 FR42

SIMILAR

STGR42RH

STGR42LH

STGR42LH

A

A

B

B

A

Z190

A A

B B N_SB_531060_6_BAAA_01_01

Figure A-GBAAA - Sheet 01

Inspection Area

DATE: Jun 19/02 SERVICE BULLETIN No.: A320-53-1060

REVISION No.: 04 - Sep 13/12 Page: 26

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**CONF ALL

INSPECTION AREA AINSPECTION AREA B

FWD

B

FR40 FR41 FR42

STGR42LH

N_SB_531060_6_BAAA_02_01

Figure A-GBAAA - Sheet 02

Inspection Area

DATE: Jun 19/02 SERVICE BULLETIN No.: A320-53-1060

REVISION No.: 04 - Sep 13/12 Page: 27

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**CONF ALL

AREA A AREA B

REPAIR THE AREA A WITHIN

WHICHEVER OCCURS FIRST

7.500 FC OR 16.700 FH

REFER TO SHEET 2

NO NO

YES YES

X: CRACK LENGTH

DO THE EDDY−CURRENT NDT INSPECTION

IN INSPECTION AREA A AND AREA B

AROUND THE FASTENER HEAD 

CRACK

FOUND

CRACK

FOUND

REPEAT THE INSPECTION

WHICHEVER OCCURS FIRST

EVERY 12.000 FC OR 26.700 FH

X < 5.0 mm

X < (0.197 in)

REPAIR THE AREA A

WHICHEVER OCCURS FIRST

WITHIN 4.000 FC OR 8.900 FH

5.0mm X 10.0mm

(0.197 in X (0.393 in)

CONTACT AIRBUS

REPAIR INSTRUCTIONS

FOR FURTHER

BEFORE NEXT FLIGHT

REPEAT THE INSPECTION

WHICHEVER OCCURS FIRST

EVERY 12.000 FC OR 26.700 FH

HAS TO BE INSPECTED BY

THE NON−REPAIRED AREA

REPETITIVE INSPECTION AS DESCRIBED

IN THE REPAIRED AREA

REQUIRED IN ACCORDANCE WITH

NO FURTHER INSPECTION IS

THIS SERVICE BULLETIN.

IN THIS SERVICE BULLETIN

SUBJECT OF THIS SERVICE BULLETIN

WHICH HAVE NOT BEEN REPAIRED

THE REPAIRED AREAS ARE NOT MORE

BY ANY PREVIOUS ACTIONS.

THIS SERVICE BULLETIN ARE

TO BE PERFORMED IN AREAS

THE INSPECTIONS REQUIRED IN

REFER TO COMPLIANCE, PARAGRAPH 1.E.(2)

N_SB_531060_6_FAAA_01_08

Figure A-GFAAA - Sheet 01

Flow Chart

DATE: Jun 19/02 SERVICE BULLETIN No.: A320-53-1060

REVISION No.: 04 - Sep 13/12 Page: 28

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**CONF ALL

REFER TO SHEET 1

HAS TO BE INSPECTED BY

THE NON−REPAIRED AREA

REPETITIVE INSPECTION AS DESCRIBED

REPAIR THE AREA A WITHIN

WHICHEVER OCCURS FIRST

1.700 FC OR 3.800 FH

REPAIR THE AREA A WITHIN

WHICHEVER OCCURS FIRST

860 FC OR 1.800 FH

BEFORE NEXT FLIGHT

REPAIR THE AREA A

(0.393 in < X (0.591 in)

X > 20.0mm (0.787 in)

OR MULTIPLE CRACKS

X: CRACK LENGTH

IN THE REPAIRED AREA

REQUIRED IN ACCORDANCE WITH

NO FURTHER INSPECTION IS

THIS SERVICE BULLETIN.

IN THIS SERVICE BULLETIN

10.0mm < X 15.0mm

15.0mm < X 20.0mm

(0.591 in < X (0.787 in)

N_SB_531060_6_FAAA_02_05

Figure A-GFAAA - Sheet 02

Flow Chart

DATE: Jun 19/02 SERVICE BULLETIN No.: A320-53-1060

REVISION No.: 04 - Sep 13/12 Page: 29

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REPORTING SHEET

TITLE: FUSELAGE - CENTER FUSELAGE - INSPECT THE KEEL BEAM SIDE

PANELS BETWEEN FR40 AND FR42 RH/LH

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: Jun 19/02 SERVICE BULLETIN No.: A320-53-1060

REVISION No.: 04 - Sep 13/12 Page: 1

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QUALITY PERCEPTION FORM

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

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

improve the quality of our Service Bulletins.

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

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

- Quality rating of this SB 4321

- Quality rating of the Accomplishment Instructions 4321

- Quality rating of the Illustrations 4321

- Is this SB easy to understand ? Y/N

If you have had difficulties in the accomplishment of this SB please quote below the area(s) and give a

short description of the issue.

Planning Material Instructions

X Effectivity X Kit content X Preparation

X Reason X List of Materials Operator Supplied X Mod/Inspection

X Manpower X Industry support X Test

X References X Re-identification X Close-Up

X Publication X Tooling X Illustrations

Comments:

Operator: Date:

Name/Title:

Please return this form to:

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX FRANCE

Attn : SEM4 Service Bulletins Management

FAX : (33) 5 61 93 42 51

Or via your Resident Customer Support Office.

DATE: Jun 19/02 SERVICE BULLETIN No.: A320-53-1060

REVISION No.: 04 - Sep 13/12 Page: 1

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