@A318/A319/A320/A321

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.

ATA SYSTEM: 53

TITLE: FUSELAGE - GENERAL - COLD WORK RIVET HOLES AT UPPER

SHELL S15/21 AND S16/17

**CONF ALL

MODIFICATIONS

MODIFICATION CLASSIFICATION

MAJOR None

MINOR 153139K15425

NOTE: As per EASA IR 21, a minor change is one that has no appreciable effect on the

mass, balance, structural strength, reliability, operational characteristics affecting the

airworthiness of the product. All other changes are major changes.

REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES

During full scale fatigue tests, it was found that a splice plate at the butt joint of the Frame 47 started to

crack.

This Service Bulletin gives the necessary instructions for the cold expansion and rototest of the fastener

area at splice plate of the Frame 47 butt joint.

The accomplishment of this Service Bulletin cancels the requirements of Inspection Service Bulletin No.

A320-53-1260 and will make sure that the splice plate at the butt joint of the Frame 47 does not start to

crack from fatigue.

GENERAL EVALUATION

EVALUATION TABLE

COMPLIANCE RECOMMENDED (1) CANCELS INSPECTION SB YES

POTENTIAL AD NO 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 recommended to be accomplished to prevent significant operational

disruptions.

DATE: Dec 18/12 SERVICE BULLETIN No.: A320-53-1271

REVISION No.: 00 - Dec 18/12 Page: 1

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SERVICE BULLETIN

SUMMARY

MATERIAL PRICE INFORMATION

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 531271D01R00 1 1,150.00 Pins and collars

Standard tool TOOLD01 1 See SB Durable tooling, expendable tooling and

capital tooling

EFFECTIVITY

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

09S 14S 15T 31V 35U 36V 47Y 56W 61T 69X 73W 78T 85T

86W 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

CES CIB CQH CQN CSA CSC CSN CTN CYP D2F DAL DLH EAA

EDW EIN ETD EZD F2I FFT FHE FHY FIN FPY FRN G2X G8E

GIA GIR GSW HAY HDA HRM HVN I2L I2T IAC IBE IBS IRA

ISS JAV JBU JET KAC KCA KHO KMF LAN LBT LBY LFO LLM

LLP LMU MLD MLR MMA MON MSR MXA NMA NVD O2X OHY OZW

PAL PIC PTR QAF QTR RFJ RNV RYW RZO SBN SDM SFW SGG

SGX SHY SKU SLK SNX SOL STU SVR SWM SWR SYR TAE TAI

TAM TAP TAR TCW TCX TNA TOM UAL UDC USA VLE VLG VLK

WHT WTJ XLF YAP

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 531271-831-848-001: Modification

TOTAL MANHOURS 100.00

DATE: Dec 18/12 SERVICE BULLETIN No.: A320-53-1271

REVISION No.: 00 - Dec 18/12 Page: 2

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SERVICE BULLETIN

SUMMARY

Task 531271-831-848-001: Modification

ELAPSED TIME (HOURS) 50.00

APPENDICES

Appendix 01 - Elapsed Time Assumption

DATE: Dec 18/12 SERVICE BULLETIN No.: A320-53-1271

REVISION No.: 00 - Dec 18/12 Page: 3

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SERVICE BULLETIN

SUMMARY

**CONF ALL

Z250

A

Z240

STGR5LH STGR7LH

STGR5RH

STGR7RH

A FR42

FR47

FR50

MODIFICATION AREA

N_SB_531271_6_SAAA_01_00

Figure A-GSAAA - Sheet 01

DATE: Dec 18/12 SERVICE BULLETIN No.: A320-53-1271

REVISION No.: 00 - Dec 18/12 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

ATA SYSTEM: 53

TITLE: FUSELAGE - GENERAL - COLD WORK RIVET HOLES AT UPPER

SHELL S15/21 AND S16/17

MODIFICATION No.: 153139K15425

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

This modification is applicable by Service Bulletin only.

(1) Models

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

0530-0531 0533-0534 0537 0539-0540 0542-0543 0545 0548-0549 0551 0553-0554

0556 0558-0559 0561-0562 0565-0566 0568-0569 0571 0573-0575 0577 0579-0580

0582 0584-0585 0587 0589-0590 0592 0594 0596 0601 0603 0605 0607 0611 0613

0615 0617 0619 0622 0624 0626 0630 0635 0638 0640 0643 0645 0648 0650 0653

0655 0657-0659 0661-0662 0665 0667 0669 0671 0673 0676 0678 0681 0683 0685

0696 0698 0701-0707 0709-0710 0712 0714 0716 0718 0720 0722 0724 0726 0730

0733 0735 0737 0739 0741 0743 0745 0747 0749 0751 0754 0756 0758 0760 0762

0764 0766 0768 0770 0772 0774 0776 0778 0780 0782 0784 0786 0791 0793 0795

DATE: Dec 18/12 SERVICE BULLETIN No.: A320-53-1271

REVISION No.: 00 - Dec 18/12 Page: 1

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SERVICE BULLETIN

0797 0799 0801 0803 0805 0807 0809 0812 0814 0816 0818 0820 0822 0824 0826

0828 0830 0832 0834 0836 0838-0839 0842 0844 0846 0849 0851 0854 0856-0857

0859 0861 0863 0865-0866 0868 0870 0872 0874 0876-0877 0879 0881 0883-0884

0886 0888 0892 0894-0895 0897 0899-0900 0902-0903 0905 0907 0909 0911-0912

0914 0916 0918-0919 0921 0923 0925 0927-0928 0930 0932 0934 0936-0937 0939

0942-0943 0945 0947 0950-0951 0953 0955 0957-0958 0960 0962 0964 0966-0967

0969 0971 0973 0975 0977-0978 0981-0982 0984 0986 0988 0990 0992 0994 0996

0999 1001 1003 1005 1007 1009 1011 1013-1014 1026 1028 1030 1032 1035 1037

1039 1041 1047 1050 1052 1054 1057 1059 1061 1063 1065 1067 1070 1072

1075-1076 1079 1081 1083 1085 1087 1093 1099 1101 1104-1105 1108 1110 1112

1114 1117 1119 1121 1123 1125 1128 1130 1132 1134 1137-1138 1141 1143 1146

1148 1150 1152 1156 1158 1162-1163 1166 1168 1171 1173 1175 1177 1179 1181

1183 1187 1189 1192 1194 1196 1198 1200 1206 1208 1210 1213 1215 1217 1221

1224 1226 1229 1231 1234-1235 1237 1240 1242 1244 1246 1248 1251 1253 1255

1257 1259 1262 1264 1266 1268 1270 1272 1274 1280 1282 1284 1286 1288 1290

1292 1294 1296 1298 1300 1302 1304 1306 1308 1310 1312 1314 1316 1318 1320

1322 1327 1330 1332 1334 1337 1339 1341 1343 1345 1347 1349 1351 1353 1355

1357 1359 1361 1363 1365 1367-1368 1370 1372 1376 1379 1381 1383 1385 1387

1390 1394 1396 1398 1400 1402 1405 1407 1409 1411 1413 1416 1418-1419 1422

1424 1427 1430 1432 1435 1437 1439 1441 1443 1446 1448 1450 1452 1454 1457

1459 1461 1464 1467 1469-1470 1473 1475 1478 1480 1482 1484 1486 1489 1491

1493 1495 1497 1500 1502 1504 1506 1508-1509 1512 1514 1516 1518 1523 1526

1528 1530 1532-1533 1535 1538 1540 1542 1544 1546 1548 1550 1553 1555 1557

1559 1561 1564 1566 1568 1571 1578 1580 1584 1586 1588 1591 1593 1595 1597

1605 1609-1610 1613 1615 1617 1620-1621 1624 1626 1628 1631 1633 1635 1637

1639 1641 1644 1646 1648 1650 1652 1655 1657 1661 1663 1665 1667 1669 1672

1674 1676 1678 1680 1682 1686-1687 1689 1692 1694 1696-1697 1700 1702

(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

31V 0164 0332 0368 0395

35U 0088

36V 0136

47Y 0394

56W 0247 0257 0327 0336

61T 0407

69X 0219 0357

73W 0087

78T 1306 1564

85T 0234

86W 0384

98W 0039 0042 0103 0109 0120

DATE: Dec 18/12 SERVICE BULLETIN No.: A320-53-1271

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SERVICE BULLETIN

OPERATOR MSN

AAF 0244

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

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 1502

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 1661 1665 1687 1689 1696

BEL 1441 1493

BER 1504 1553

BGH 0221 0294 0349 1087

BMA 1014 1177 1418 1424

BTV 0168 0441 0449 0460 0461

C9G 0246 0710 0772 1676

CCA 0876 0921 1296

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

0984 0986 1005 1028 1030 1041 1070 1072 1093 1108 1312 1316

1330 1345 1357 1361 1532 1542 1639

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

CQH 0978 1286 1372 1686

CQN 0696 0698 0704 0705

CSA 1439 1450

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

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

1035 1039 1057

CTN 0258 1009 1237

CYP 0256

D2F 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 1535 1633 1641 1646

DATE: Dec 18/12 SERVICE BULLETIN No.: A320-53-1271

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SERVICE BULLETIN

OPERATOR MSN

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 1337 1365 1367

EAA 0386 0445

EDW 0942 0947 1026

EIN 1242 1394 1443

ETD 0350

EZD 0667 0743 0872 0874

F2I 0391 0615

FFT 1615

FHE 0888 0936 1171 1210

FHY 0580

FIN 1405 1470 1544 1588

FPY 0112 0189 0342 0438

FRN 0409 0466 0497

G2X 0347 1678

G8E 0222 0348 0369 0373 1464

GIA 0839 0892 1635

GIR 0630

GSW 0376

HAY 0716

HDA 0756 0784 0812 0930 1253

HRM 0293

HVN 0590 0594 0601 0605 0607 0611 0617 0619 0648 0650

I2L 0443 1407 1497

I2T 1631 1682

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

IBE 0223 0274 1047 1059 1067 1099 1119 1208 1229 1255 1262 1288

1292 1318 1347 1530 1540 1655 1674 1694

IBS 0158 0173 0176 0207 0224 0266 0323 0356 1101 1516

IRA 0303 0312 0345 0530 0575 0857

ISS 0737 0749 1125 1198

JAV 0029

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

1452 1506 1528 1546 1557 1610 1650

JET 0204 0215 0371 0421 0542 0816 0877

KAC 0181 0182 0195

KCA 0393 0414

KHO 0354 0361 0362 0405

KMF 0480

LAN 1304 1332 1351 1355 1491 1512 1526 1548 1568 1626

LBT 0301 0400 0793 0937 1121 1175 1597

LBY 0558 0561

LFO 0659

DATE: Dec 18/12 SERVICE BULLETIN No.: A320-53-1271

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SERVICE BULLETIN

OPERATOR MSN

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 1571 1637

MSR 0165 0166 0178 0194 0198 0322 0351 0366

MXA 0252 0259 0260 0261 0275 0276 0296 0320 0321 0353

NMA 1697

NVD 0211 0299 0375 0415 0419 0528

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

QTR 1566 1648

RFJ 0814

RNV 0229

RYW 0569

RZO 0795

SBN 0325 0428

SDM 0427 0525 1130 1578 1657

SFW 0671 0994

SGG 0799 0879 1390

SGX 1605

SHY 0138 0148 1194

SKU 0179 0406 0447 1400 1523

SLK 0899 0969 1422 1561

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 0585 0596 0603 0635 0643 0673

0681 0701 0703 0782

SYR 0886 0918 1032 1076 1085 1117

TAE 0657 0934

TAI 1334 1624

TAM 0250 0334 0335 0440 0758 1143 1158 1215 1246 1251 1339 1368

1376 1459 1486 1518 1580 1591 1593 1595 1613 1628 1652 1663

1672 1692

TAP 0870 0945 0960 0982 1181 1206 1231 1667

TAR 0119 0123 0124 0205 0370 0390 0402 0511 0958 0975 1187 1700

DATE: Dec 18/12 SERVICE BULLETIN No.: A320-53-1271

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SERVICE BULLETIN

OPERATOR MSN

TCW 0425 0653

TCX 0424

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 0702 0751 0780 0820 0824 0826 0834 0836 0842

0851 0865 0955 1001 1104 1105 1128 1146 1163 1192 1248 1266

1272 1282 1290 1341 1343 1359 1363 1409 1427 1432 1435 1469

1475 1495 1508 1514 1533 1538 1555 1559 1584 1586 1609 1617

1620 1669 1680 1702

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 0953 1003 1050 1052 1061 1065 1075 1079 1083 1110

1112 1114 1134 1141 1148 1166 1196 1224 1234 1264 1268 1274

1284 1294 1298 1310 1314 1419 1621 1644

VLE 1226

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

1461 1550

VLK 0422 0714 0730 1200 1213 1379

WHT 0726

WTJ 0548

XLF 0343

YAP 0533 0566 0973 1454

DATE: Dec 18/12 SERVICE BULLETIN No.: A320-53-1271

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SERVICE BULLETIN

(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 0548 0549 0551 0553 0554 0556 0558 0559 0561

0562 0565 0566 0568 0569 0571 0573 0574 0575 0577 0579

0580 0582 0584 0585 0587 0589 0590 0592 0594 0596 0601

0603 0605 0607 0611 0613 0615 0617 0619 0622 0624 0626

0630 0635 0638 0640 0643 0645 0648 0650 0653 0655 0657

0658 0659 0661 0662 0665 0667 0669 0671 0673 0676 0678

0681 0683 0685 0696 0698 0701 0702 0703 0704 0705 0706

0707 0709 0710 0712 0714 0716 0718 0720 0722 0724 0726

0730 0733 0735 0737 0739 0741 0743 0745 0747 0749 0751

0754 0756 0758 0760 0762 0764 0766 0768 0770 0772 0774

0776 0778 0780 0782 0784 0786 0791 0793 0795 0797 0799

001

DATE: Dec 18/12 SERVICE BULLETIN No.: A320-53-1271

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SERVICE BULLETIN

MSN CONFIGURATION

0801 0803 0805 0807 0809 0812 0814 0816 0818 0820 0822

0824 0826 0828 0830 0832 0834 0836 0838 0839 0842 0844

0846 0849 0851 0854 0856 0857 0859 0861 0863 0865 0866

0868 0870 0872 0874 0876 0877 0879 0881 0883 0884 0886

0888 0892 0894 0895 0897 0899 0900 0902 0903 0905 0907

0909 0911 0912 0914 0916 0918 0919 0921 0923 0925 0927

0928 0930 0932 0934 0936 0937 0939 0942 0943 0945 0947

0950 0951 0953 0955 0957 0958 0960 0962 0964 0966 0967

0969 0971 0973 0975 0977 0978 0981 0982 0984 0986 0988

0990 0992 0994 0996 0999 1001 1003 1005 1007 1009 1011

1013 1014 1026 1028 1030 1032 1035 1037 1039 1041 1047

1050 1052 1054 1057 1059 1061 1063 1065 1067 1070 1072

1075 1076 1079 1081 1083 1085 1087 1093 1099 1101 1104

1105 1108 1110 1112 1114 1117 1119 1121 1123 1125 1128

1130 1132 1134 1137 1138 1141 1143 1146 1148 1150 1152

1156 1158 1162 1163 1166 1168 1171 1173 1175 1177 1179

1181 1183 1187 1189 1192 1194 1196 1198 1200 1206 1208

1210 1213 1215 1217 1221 1224 1226 1229 1231 1234 1235

1237 1240 1242 1244 1246 1248 1251 1253 1255 1257 1259

1262 1264 1266 1268 1270 1272 1274 1280 1282 1284 1286

1288 1290 1292 1294 1296 1298 1300 1302 1304 1306 1308

1310 1312 1314 1316 1318 1320 1322 1327 1330 1332 1334

1337 1339 1341 1343 1345 1347 1349 1351 1353 1355 1357

1359 1361 1363 1365 1367 1368 1370 1372 1376 1379 1381

1383 1385 1387 1390 1394 1396 1398 1400 1402 1405 1407

1409 1411 1413 1416 1418 1419 1422 1424 1427 1430 1432

1435 1437 1439 1441 1443 1446 1448 1450 1452 1454 1457

1459 1461 1464 1467 1469 1470 1473 1475 1478 1480 1482

1484 1486 1489 1491 1493 1495 1497 1500 1502 1504 1506

1508 1509 1512 1514 1516 1518 1523 1526 1528 1530 1532

1533 1535 1538 1540 1542 1544 1546 1548 1550 1553 1555

1557 1559 1561 1564 1566 1568 1571 1578 1580 1584 1586

1588 1591 1593 1595 1597 1605 1609 1610 1613 1615 1617

1620 1621 1624 1626 1628 1631 1633 1635 1637 1639 1641

1644 1646 1648 1650 1652 1655 1657 1661 1663 1665 1667

1669 1672 1674 1676 1678 1680 1682 1686 1687 1689 1692

1694 1696 1697 1700 1702

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

Kit 531271D01R00 1

Consumable CMLD01 1

Standard tool TOOLD01 1

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B. CONCURRENT REQUIREMENTS

None

C. REASON

(1) History

During full scale fatigue tests, it was found that a splice plate at the butt joint of the

Frame 47 started to crack.

(2) Objective/Action

This Service Bulletin gives the necessary instructions for the cold expansion and rototest

of the fastener area at splice plate of the Frame 47 butt joint.

(3) Advantages

The accomplishment of this Service Bulletin cancels the requirements of Inspection

Service Bulletin No. A320-53-1260 and will make sure that the splice plate at the butt

joint of the Frame 47 does not start to crack from fatigue.

(4) Operational/Maintenance Consequences

None

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

Task 531271-831-848-001: Modification

(1) Remove the fasteners from Frame 47 between STGR 5 and STGR 7, LH and RH

(2) Inspect the holes at Frame 47 between STGR 5 and STGR 7, LH and RH

(3) Cold expand the applicable holes on Frame 47 between STGR 5 and STGR 7, LH

and RH

(4) Install the fasteners on Frame 47 between STGR 5 and STGR 7, LH and RH

E. COMPLIANCE

(1) Classification

RECOMMENDED: Service Bulletin recommended to be accomplished to prevent

significant operational disruptions.

(2) Accomplishment Timescale

Accomplishment of this Service Bulletin is recommended at the earliest opportunity

where manpower and facilities are available.

DATE: Dec 18/12 SERVICE BULLETIN No.: A320-53-1271

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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.

For an explanation of the manhours and elapsed time, refer to Appendix 01 - Elapsed Time

Assumption .

Task 531271-831-848-001: Modification

Get Access 4.50

On Aircraft

Remove the fasteners from Frame 47 between STGR

5 and STGR 7, LH and RH

22.00

Inspect the holes at Frame 47 between STGR 5 and

STGR 7, LH and RH

9.00

Cold expand the applicable holes on Frame 47

between STGR 5 and STGR 7, LH and RH

28.00

Install the fasteners on Frame 47 between STGR 5

and STGR 7, LH and RH

28.00

Tests 2.00

Close-Up 6.50

TOTAL MANHOURS 100.00

ELAPSED TIME (HOURS) 50.00

H. WEIGHT AND BALANCE

Not Changed

I. ELECTRICAL LOAD DATA

Not Changed

J. REFERENCES

Aircraft Maintenance Manual (AMM) 06-20-00 06-31-53 06-41-53

12-34-24 23-33-00 25-21-00

25-21-41 25-23-41 25-24-41

25-80-00 33-51-00 52-10-00

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Consumable Material List (CML)

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

Non Destructive Test Manual (NTM) 51-10-01

Service Information Letter (SIL) SIL 51-012

Standards Manual (SM)

Structural Repair Manual (SRM) 51-21-00 51-24-00 51-42-00

51-43-00 51-44-00 51-44-11

51-46-00 51-46-11 51-48-00

51-75-12 51-76-00 51-78-00

K. PUBLICATION AFFECTED

Aircraft Maintenance Manual (AMM) 53-31-00

L. INTERCHANGEABILITY/MIXABILITY

Not Applicable

M. SPARES

None

DATE: Dec 18/12 SERVICE BULLETIN No.: A320-53-1271

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This Page Intentionally Left Blank

DATE: Dec 18/12 SERVICE BULLETIN No.: A320-53-1271

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2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

(1) Procurement Addresses

Kit 531271D01R00 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:

AIRBUS Material, Logistics and Suppliers

Weg beim Jaeger 150

D-22335 Hamburg

Germany

For ordering by internet:

http://spares.airbus.com

For ordering by fax:

+49 40 50 76 2590

For ordering by E-mail:

airbus.kit@airbus.com

(2) Price and Availability

Kit 531271D01R00

Cost 1,150.00 USD

Availability 90 calendar days from receipt of order

The Kit availability given above is the standard lead time from the date of your purchase

order. If you require Kits before this time, please include a retrofit planning schedule with

your order so that we can try to comply with your requirements. The sales terms (costs

and availability) are estimated in relation to economic conditions at the issue date of

the Service Bulletin. The latest valid price and lead time for ordering purposes shall

be obtained through the AirbusSpares portal or through a request for quotation to

airbus.kit@airbus.com.

B. INDUSTRY SUPPORT INFORMATION

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

C. LIST OF COMPONENTS

Kit 531271D01R00

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

NOTES

1 DAN6-6-4Y 54 PIN

2 DAN6-6-5Y 26 PIN

3 DAN6-6-6Y 40 PIN

4 DAN6-6-7Y 8 PIN

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

NOTES

5 NSA5330-6 128 COLLAR

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

you cannot identify in the LIST OF COMPONENTS of this Service Bulletin,

refer to Standards Manual (SM). The SM will give you the correct part number

to part number relationship.

D. LIST OF MATERIALS - OPERATOR SUPPLIED

(1) Consumable Materials

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO CML

MAT. No.

QTY PER A/C SEE

NOTES

Sealant-Brush Consistency 09-013 As required

Top Coat 16-002 As required

Anti-Corrosion Primer 16-006 As required

(2) Components

None

(3) Equipment

None

E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

None

F. TOOLING

(1) Tooling - Price and Availability

(a) Procurement Addresses

Operators interested in obtaining the FTI tool kits should contact:

Standard tool TOOLD01 Fatigue Technology Inc.

401 Andover Park East

SEATTLE, WA 98188-7605

USA

Internet: www.fatiguetech.com

Phone: (206) 2462010

Fax: (206) 2449886

(b) Price and Availability

None

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(2) Tools

Standard tool TOOLD01

ITEM TOOL N ̊ TOOL NAME QTY SEE

NOTES

DK-A320531271-1 Durable Tooling 1 (1)

EK-A320531271-1 Expendable Tooling 1 (2)

FTIA320531271-1 Capital Tooling 1 (3)

NOTE: FTI has allocated the following tool kit numbers for cold expansion:

For the definition of capital, durable and expendable tools refer to SIL

51-012.

NOTE (1): Durable tool kit No.: DK-A320-53-1271-1

The durable tool kit contains the minimum quantity of durable tools

necessary to accomplish the Service Bulletin on one aircraft. If the

Service Bulletin is to be accomplished on more than one aircraft, the

number of durable kits required can be established by reference to SIL

51-012.

NOTE (2): Expendable tool kit No.: EK-A320-53-1271-1

The expendable tool kit contains the quantity of expendable tools

required to accomplish the Service Bulletin on one aircraft. Order one

expendable tool kit for every aircraft on which this Service Bulletin is to

be accomplished.

NOTE (3): Capital tool kit No.: FTI-A320-53-1271-1

The capital tools provided in this kit are not specific to this Service

Bulletin and are normally already available in operators’ stock as a longterm investment or can be loaned from FTI.

(3) Special Tools

None

DATE: Dec 18/12 SERVICE BULLETIN No.: A320-53-1271

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3. ACCOMPLISHMENT INSTRUCTIONS

Task 531271-831-848-001 - Modification

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

INCLUDED IN THE REFERENCED PROCEDURES.

CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP ELECTRICAL

WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY AND

MECHANICALLY SERVICEABLE).

WHEN YOU DO MAINTENANCE WORK, REPAIRS OR MODIFICATIONS,

ALWAYS KEEP ELECTRICAL WIRING, COMPONENTS AND THE WORK AREA

AS CLEAN AS POSSIBLE. TO DO THIS:

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

NECESSARY ON ELECTRICAL 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

From 243 to 253

From 244 to 254

Manpower

TOTAL MANHOURS 100.00

ELAPSED TIME (HOURS) 50.00

A. GENERAL

(1) Subtask 531271-910-201-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

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

06-31-53, Page Block 001

06-41-53, Page Block 001

Consumable Material List (CML)

Non Destructive Test Manual (NTM) 51-10-01

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References

Structural Repair Manual (SRM) 51-21-00

51-24-00

51-42-00

51-43-00

51-44-00

51-44-11

51-46-00

51-48-00

51-75-12

51-76-00

51-78-00

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

the Consumable Materials List (CML)).

(b) For the location of access panels (Refer to AMM 06-41-53, Page Block 001.

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

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

(e) For fastener removal and installation (Refer to SRM 51-42-00).

(f) For alternative and substitute fasteners (Refer to SRM 51-43-00).

(g) For countersinking data (Refer to SRM 51-46-00).

(h) For fastener hole diameters and drill and de-burr data (Refer to SRM 51-44-00).

(i) Use interference fit for all hi-lok fasteners. For hole and drill data (Refer to SRM

51-44-11).

(j) For application of protective treatment (Refer to SRM 51-21-00).

(k) For application of surface protection on rivets (Refer to SRM 51-75-12).

(l) For application of sealant (Refer to SRM 51-24-00).

(m) For cleaning process (Refer to SRM 51-78-00).

(n) For cold expansion (Refer to SRM 51-48-00).

(o) For rotating probe testing (Refer to NTM 51-10-01).

(p) All structural parts and fasteners must be wet installed.

(q) For sealant repairs (Refer to SRM 51-76-00).

(2) Subtask 531271-839-201-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

B. PREPARATION

(1) Subtask 531271-941-201-001 - Job Set-up

Work Zones and Access Panels

Zone Access/Work location

From 243

To 253

From 244

To 254

Manpower Resources

Skills NON SPECIFIC

References

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

Task 25-21-41-000-001

Task 25-23-41-000-001

Task 25-24-41-000-002

Task 25-80-00-000-001

Task 52-10-00-010-001

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

12-34-24-869-002).

(b) Put an access platform in position below the forward passenger/crew door 831.

(c) Open the forward passenger/crew door 831 (Refer to AMM Task

52-10-00-010-001).

(d) Remove the related passenger seats in the working area of the cabin as necessary

(Refer to AMM Task 25-21-41-000-001).

(e) Remove the doors of the related overhead stowage compartments as necessary

(Refer to AMM Task 25-24-41-000-002).

(f) Remove the ceiling panels 241FC and 251AC (Refer to AMM Task

25-23-41-000-001).

(g) Remove the insulation blankets in the working area as far as necessary (Refer to

AMM Task 25-80-00-000-001).

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C. PROCEDURE

(1) Subtask 531271-831-201-001 - Remove the fasteners from Frame 47 between STGR

5 and STGR 7, LH and RH

Work Zones and Access Panels

Zone Access/Work location

From 243

To 253

From 244

To 254

Manpower Resources

Manhours 22.00

Minimum number of person 2

Subtask elapsed time 11.00

Skills AIRFRAME

References

Fig. A-GBAAA

Modification at Frame 47 LH and RH

Sheet 01

Sheet 02

Sheet 03

Sheet 04

(a) Remove the fasteners from Frame 47 between STGR 5 and STGR 7, LH and RH.

1 At Frame 47 between STGR 5 and STGR 7, LH and RH, remove the

fasteners for a rotating probe inspection.

Refer Fig. A-GBAAA Sheet 01, View A and Fig. A-GBAAA Sheet 02, View B

and C.

Remove:

128 Collar Item (9) Discard

and

128 Fastener Item (10) Discard

(2) Subtask 531271-831-202-001 - Inspect the holes at Frame 47 between STGR 5 and

STGR 7, LH and RH

Work Zones and Access Panels

Zone Access/Work location

From 243

To 253

From 244

To 254

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Manpower Resources

Manhours 9.00

Minimum number of person 2

Subtask elapsed time 4.50

Skills AIRFRAME

References

Non Destructive Test Manual (NTM) Task 51-10-01-250-801

Fig. A-GBAAA

Modification at Frame 47 LH and RH

Sheet 01

Sheet 02

Sheet 03

Sheet 04

(a) Do a High Frequency Eddy Current (HFEC) rotating probe inspection for cracks.

1 Do a HFEC rotating probe inspection for cracks of the related holes at Frame

47.

Refer Fig. A-GBAAA Sheet 01, View A and Fig. A-GBAAA Sheet 03, View D

and E.

Refer to NTM Task 51-10-01-250-801.

a If cracks were found:

- Contact AIRBUS and apply actions defined by AIRBUS accordingly

before next flight.

b If no cracks were found:

- Continue with SUBTASK 531271-831-203 001 Cold expand the

applicable holes on Frame 47 between STGR 5 and STGR 7, LH

and RH .

(3) Subtask 531271-831-203-001 - Cold expand the applicable holes on Frame 47

between STGR 5 and STGR 7, LH and RH

Work Zones and Access Panels

Zone Access/Work location

From 243

To 253

From 244

To 254

Manpower Resources

Manhours 28.00

Minimum number of person 2

Subtask elapsed time 14.00

Skills AIRFRAME

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Material necessary to do the job

Standard tool TOOLD01

ITEM TOOL N ̊ TOOL NAME QTY SEE

NOTES

DK-A320531271-1 Durable Tooling 1 (1)

EK-A320531271-1 Expendable Tooling 1 (2)

FTIA320531271-1 Capital Tooling 1 (3)

NOTE: FTI has allocated the following tool kit numbers for cold expansion:

For the definition of capital, durable and expendable tools refer to SIL

51-012.

NOTE (1): Durable tool kit No.: DK-A320-53-1271-1

The durable tool kit contains the minimum quantity of durable tools

necessary to accomplish the Service Bulletin on one aircraft. If the

Service Bulletin is to be accomplished on more than one aircraft, the

number of durable kits required can be established by reference to SIL

51-012.

NOTE (2): Expendable tool kit No.: EK-A320-53-1271-1

The expendable tool kit contains the quantity of expendable tools

required to accomplish the Service Bulletin on one aircraft. Order one

expendable tool kit for every aircraft on which this Service Bulletin is to

be accomplished.

NOTE (3): Capital tool kit No.: FTI-A320-53-1271-1

The capital tools provided in this kit are not specific to this Service

Bulletin and are normally already available in operators’ stock as a longterm investment or can be loaned from FTI.

References

Structural Repair Manual (SRM) 51-46-11

51-48-00 STDN 6-1-N

Fig. A-GBAAA

Modification at Frame 47 LH and RH

Sheet 01

Sheet 02

Sheet 03

Sheet 04

(a) Cold expand the holes in the butt joints on Frame 47 between STGR 5 and STGR

7, LH and RH.

Refer Fig. A-GBAAA Sheet 01, View A and Fig. A-GBAAA Sheet 03, View D and E.

Refer to SRM 51-48-00 STDN 6-1-N.

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1 Drill and cold work the related holes by using the drill, mandrel and power gun

from the FTI Tool Kits:

DK-A320531271-1 Durable Tooling 1

EK-A320531271-1 Expendable Tooling 1

FTIA320531271-1 Capital Tooling 1

2 Final reaming of the cold expanded holes should be from minimum 5.490 mm

(0.215 in) to maximum 5.510 mm (0.217 in).

3 If necessary rework the countersinks to the related fastener head size (Refer

to SRM 51-46-11).

(4) Subtask 531271-831-204-001 - Install the fasteners on Frame 47 between STGR 5

and STGR 7, LH and RH

Work Zones and Access Panels

Zone Access/Work location

From 243

To 253

From 244

To 254

Manpower Resources

Manhours 28.00

Minimum number of person 2

Subtask elapsed time 14.00

Skills AIRFRAME

Material necessary to do the job

Kit 531271D01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 DAN6-6-4Y 54 PIN

2 DAN6-6-5Y 26 PIN

3 DAN6-6-6Y 40 PIN

4 DAN6-6-7Y 8 PIN

5 NSA5330-6 128 COLLAR

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Sealant-Brush Consistency 09-013

Top Coat 16-002 As required

Anti-Corrosion Primer 16-006

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References

Fig. A-GBAAA

Modification at Frame 47 LH and RH

Sheet 01

Sheet 02

Sheet 03

Sheet 04

(a) Install the fasteners on Frame 47 between STGR 5 and STGR 7, LH and RH.

1 On Frame 47 between STGR 5 and STGR 7, LH and RH, wet install:

Refer Fig. A-GBAAA Sheet 01, View A, Fig. A-GBAAA Sheet 03, View D and

E and Fig. A-GBAAA Sheet 04.

54 Pin DAN6-6-4Y Item 1

26 Pin DAN6-6-5Y Item 2

40 Pin DAN6-6-6Y Item 3

8 Pin DAN6-6-7Y Item 4

128 Collar NSA5330-6 Item 5

with:

Sealant-Brush

Consistency

09-013 As required

2 Protection of the fasteners and collars with:

Anti-Corrosion

Primer

16-006 As required

Top Coat 16-002 As required

D. TEST

(1) Subtask 531271-700-201-001 - Test

Work Zones and Access Panels

Zone Access/Work location

From 243

To 253

From 244

To 254

Manpower Resources

Skills NON SPECIFIC

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References

Aircraft Maintenance Manual (AMM) Task 23-33-00-710-002

Task 23-33-00-740-002

Task 25-21-00-710-002

Task 25-21-00-710-003

Task 25-21-41-710-052

Task 33-51-00-710-009

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

equipment.

(b) Procedure

1 Do the operational test of the emergency lights (Refer to AMM Task

33-51-00-710-009).

2 Do the BITE test of the Passenger Entertainment System (PES) (Refer to

AMM Task 23-33-00-740-002).

3 Do the operational test of the Passenger Entertainment System (PES) (Refer

to AMM Task 23-33-00-710-002).

4 Do the operational test of the in-seat power-supply system (Refer to AMM

Task 25-21-00-710-002).

5 If electrical seats have been installed, do the functional test of the electrical

seats (Refer to AMM Task 25-21-00-710-003).

NOTE: Do the tests for the seats only, that were removed for access.

6 If mechanical seats have been installed, do the test of the passenger seats

with mechanically operating functions (Refer to AMM Task 25-21-41-710-052).

NOTE: Do the tests for the seats only, that were removed for access.

E. CLOSE-UP

(1) Subtask 531271-942-201-001 - Close-up

Work Zones and Access Panels

Zone Access/Work location

From 243

To 253

From 244

To 254

Manpower Resources

Skills NON SPECIFIC

DATE: Dec 18/12 SERVICE BULLETIN No.: A320-53-1271

REVISION No.: 00 - Dec 18/12 Page: 25

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SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) Task 25-21-41-400-001

Task 25-23-41-400-001

Task 25-24-41-400-002

Task 25-80-00-400-001

Task 52-10-00-410-001

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

equipment.

(b) Install the insulation blankets (Refer to AMM Task 25-80-00-400-001).

(c) Install the ceiling panels 241FC and 251AC (Refer to AMM Task

25-23-41-400-001).

(d) Install the doors of the overhead stowage compartments (Refer to AMM Task

25-24-41-400-002).

(e) Install the passenger seats (Refer to AMM Task 25-21-41-400-001).

(f) Close the forward passenger/crew door 831 (Refer to AMM Task

52-10-00-410-001).

(g) Remove the access platforms.

DATE: Dec 18/12 SERVICE BULLETIN No.: A320-53-1271

REVISION No.: 00 - Dec 18/12 Page: 26

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SERVICE BULLETIN

**CONF ALL

Z250

A

Z240

STGR5LH STGR7LH

STGR5RH

STGR7RH

B D

C E

A FR42

FR47

FR50

N_SB_531271_6_BAAA_01_00

Figure A-GBAAA - Sheet 01

Modification at Frame 47 LH and RH

DATE: Dec 18/12 SERVICE BULLETIN No.: A320-53-1271

REVISION No.: 00 - Dec 18/12 Page: 27

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SERVICE BULLETIN

**CONF ALL

LH SHOWN

RH SYMMETRICAL

FWD

BEFORE

STGR5

STGR6

STGR7

FR47

B C

EXISTING FASTENERS

REMOVE FASTENERS, ITEM (10) AND COLLARS, ITEM (9)

NOTE:

N_SB_531271_6_BAAA_02_01

Figure A-GBAAA - Sheet 02

Modification at Frame 47 LH and RH

DATE: Dec 18/12 SERVICE BULLETIN No.: A320-53-1271

REVISION No.: 00 - Dec 18/12 Page: 28

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**CONF ALL

LH SHOWN

RH SYMMETRICAL

FWD

AFTER

STGR5

STGR6

STGR7

FR47

D E

FOR FASTENER SYMBOLS, REFER TO SHEET 4.

EXISTING FASTENERS

COLD EXPANSION STDN 6−1−N IN ACCORDANCE WITH SRM 51−48−00

NOTE:

POSITION OF SPLIT

IN EXPANSION SLEEVE

DURING COLD EXPANSION.

(16 POS)

(16 POS) (16 POS)

(16 POS)

N_SB_531271_6_BAAA_03_01

Figure A-GBAAA - Sheet 03

Modification at Frame 47 LH and RH

DATE: Dec 18/12 SERVICE BULLETIN No.: A320-53-1271

REVISION No.: 00 - Dec 18/12 Page: 29

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**CONF ALLP/N DESCRIPTION ITEM HOLE SYMBOL REMARKS FINAL HOLE DIAMETER

INTERFERENCE FIT

2ND OVERSIZE2ND OVERSIZE

2ND OVERSIZE

2ND OVERSIZE

5.49 mm 5.51 mm

(0.215 in) (0.217 in)

5.49 mm 5.51 mm

(0.215 in) (0.217 in)

5.49 mm 5.51 mm

(0.215 in) (0.217 in)

5.49 mm 5.51 mm

(0.215 in) (0.217 in)

COLLAR 5

PIN DAN6−6−6Y 3

COLLAR 5

PIN DAN6−6−5Y 2

COLLAR 5

PIN DAN6−6−4Y 1

COLLAR 5

PIN DAN6−6−7Y 4

NSA5330−6NSA5330−6NSA5330−6NSA5330−6

INTERFERENCE FITINTERFERENCE FITINTERFERENCE FIT

N_SB_531271_6_BAAA_04_02

MIN MAX

STDN HOLE DIAMETER

STARTING

6−1−N 4.93 mm (0.192 in) (0.195 in) 4.88 mm

MIN MAX

Figure A-GBAAA - Sheet 04

Modification at Frame 47 LH and RH

DATE: Dec 18/12 SERVICE BULLETIN No.: A320-53-1271

REVISION No.: 00 - Dec 18/12 Page: 30

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SERVICE BULLETIN

Appendix 01 - Elapsed Time Assumption

**CONF ALL

ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A320−53−1271

STEPS MH ET/S

01

02

PER

GET ACCESS 4.50 2.25 2

REMOVE THE FASTENERS FROM FRAME 47 BETWEEN 22.00 11.00 2

9.00 4.50 2

COLD EXPAND THE APPLICABLE HOLES ON FRAME 47

STGR 5 AND STGR 7 LH AND RH

INSPECT THE HOLES AT FRAME 47 BETWEEN STGR 5 AND

STGR 7 LH AND RH

SB ELAPSED TIME

(HOURS)

TOTAL MANHOURS

SB ELAPSED TIME

100.00

50.00

0

MH

ET/S:

PER

MANHOURS

ELAPSED TIME PER STEP

NUMBER OF PERSONS

THIS CHART IS ONLY A PROPOSAL.

OPERATORS MAY DETERMINE THAT ANOTHER WAY

TO DO THE WORK IS MORE SUITABLE FOR THEM.

ARE NOT REFLECTED IN THIS GANTT CHART.

01

02

NOTES:

:

: IF A VSB IS INVOLVED, THE ASSOCIATED MANHOURS

28.00 14.00 2

28.00 14.00 2

TEST 2.00 1.00 2

6.50 3.25 2

5

CLOSE−UP

10 15 20 25 30 35 40 45

BETWEEN STGR 5 AND STGR 7 LH AND RH

50

INSTALL THE FASTENERS ON FRAME 47 BETWEEN STGR 5

AND STGR 7 LH AND RH

N_SB_531271_6_AAAA_01_00

Figure A-GAAAA - Sheet 01

Elapsed Time Assumption

DATE: Dec 18/12 SERVICE BULLETIN No.: A320-53-1271

REVISION No.: 00 - Dec 18/12 Page: 1

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SERVICE BULLETIN

REPORTING SHEET

TITLE: FUSELAGE - GENERAL - COLD WORK RIVET HOLES AT UPPER

SHELL S15/21 AND S16/17

MODIFICATION No.: 153139K15425

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: Dec 18/12 SERVICE BULLETIN No.: A320-53-1271

REVISION No.: 00 - Dec 18/12 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: Dec 18/12 SERVICE BULLETIN No.: A320-53-1271

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