@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

ATA SYSTEM: 27

TITLE: FLIGHT CONTROLS - FLAP - INTERCONNECTING STRUT INSPECTION

MODIFICATION No.: None

This page transmits Revision No.01 of Service Bulletin No.A320-27-1206

ADDITIONAL WORK

**CONF ALL

Additional work is required by this revision unless operators can demonstrate using their records that

aircraft are not fitted with PN D5757030501000 and PN D5757030501200.

REASON

Revision No.01 issued to add 2 additional PN to the accomplishment instructions and to clarify that

target with SN greater than 1600 do not cause incompatibility configuration between target and

proximity sensor. Revision No.00 asks operators to focus on the last four digits for SB reading which is

misleading.

CHANGES

FRONT MATTER

FLIGHT CONTROLS - FLAP -

INTERCONNECTING STRUT

INSPECTION

CONFIGURATION UPDATED R

SUMMARY

REASON/DESCRIPTION/OPERATIONAL

CONSEQUENCES

REASON UPDATED R

EFFECTIVITY OPERATOR LIST UPDATED R

MANPOWER MANPOWER UPDATED R

PLANNING INFORMATION

EFFECTIVITY EFFECTIVITY RELATED INFORMATION

UPDATED

R

REASON

Objective/Action OBJECTIVE/ACTION UPDATED R

DESCRIPTION DESCRIPTION UPDATED R

MANPOWER MANPOWER UPDATED R

REFERENCES REFERENCED DOCUMENTATION UPDATED R

DATE: Jan 28/11 SERVICE BULLETIN No.: A320-27-1206

REVISION No.: 01 - Oct 10/11 Page: 1

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

MATERIAL INFORMATION

MATERIAL - PRICE AND AVAILABILITY

Procurement Addresses PROCUREMENT ADDRESSES UPDATED R

ACCOMPLISHMENT INSTRUCTIONS

TASK 271206- 832-848-001-Inspection

Subtask 271206-210-201-001 PARTNUMBERS HAS BEEN ADDED R

Subtask 271206-941-202-001 SUBTASK SOLUTION UPDATED R

Subtask 271206-700-201-001 SUBTASK SOLUTION UPDATED

REFERENCES UPDATED

R

TASK 271206- 832-849-001-Inspection -

ADDITIONAL WORK

ADDITIONAL WORK HAS BEEN ADDED N

Task associated data - 001 TASK ASSOCIATED DATA ADDED N

Subtask 271206-910-202-001 SUBTASK SOLUTION ADDED N

Subtask 271206-839-202-001 SUBTASK SOLUTION ADDED N

Subtask 271206-941-203-001 SUBTASK SOLUTION ADDED N

Subtask 271206-210-202-001 SUBTASK SOLUTION ADDED N

Subtask 271206-941-204-001 SUBTASK SOLUTION ADDED N

Subtask 271206-700-202-001 SUBTASK SOLUTION ADDED N

Subtask 271206-942-202-001 SUBTASK SOLUTION ADDED N

Fig. A-GFAAA

Fig. A-GFAAA Sheet 01 SHEET UPDATED R

Fig. A-GRAAA

Fig. A-GRAAA Sheet 01 SHEET UPDATED R

FILLING INSTRUCTIONS

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

Replace the complete document.

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

HISTORY OF PREVIOUS REVISIONS

No previous revision

REVISION SEQUENCE

ORIGINAL: Jan 28/11

REVISION No. : 01 - Oct 10/11

DATE: Jan 28/11 SERVICE BULLETIN No.: A320-27-1206

REVISION No.: 01 - Oct 10/11 Page: 2

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SERVICE BULLETIN

SUMMARY

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

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

ATA SYSTEM: 27

TITLE: FLIGHT CONTROLS - FLAP - INTERCONNECTING STRUT INSPECTION

**CONF ALL

MODIFICATIONS

None

REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES

For certain target/proximity sensor combinations on Flap interconnecting strut, engineering investigation

has shown that a "target FAR" signal could not be detected before reaching the mechanical end stop of

the interconnecting strut. In such a case a potential flap down drive disconnection would not be

detected.

This Service Bulletin has been issued to describe the required inspection necessary to identify the

respective struts with the target/proximity sensor combination leading to this issue.

The applicable interconnecting struts are pre Mod. 27956 which have the subsequent part numbers:

- D5757030500000

- D5757030500100

- D5757030500200

- D5757030500600

- D5757030500800

- D5757030501000

- D5757030501200

- D5757032200000

On the above listed interconnecting struts the following combination of proximity sensor/target is not

allowed:

- TARGET SN (with SN) <1600 + Sensor PN 8-372-04 or PN ABS0121-31 with Sensor SN between

C59198 and C59435 or C500000 and higher.

DATE: Jan 28/11 SERVICE BULLETIN No.: A320-27-1206

REVISION No.: 01 - Oct 10/11 Page: 1

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SERVICE BULLETIN

SUMMARY

Accomplishment of this Service Bulletin will ensure the correct combination of Strut/Sensor/Target and

thus the correct function of the Flap system.

GENERAL EVALUATION

EVALUATION TABLE

COMPLIANCE RECOMMENDED (1) CANCELS INSPECTION SB NO

POTENTIAL AD YES A/C OPERATION AFFECTED NO

RELIABILITY AFFECTED NO PAX COMFORT AFFECTED NO

COST SAVING NO ETOPS AFFECTED NO

STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED NO

NOTE (1): Service Bulletin recommended to be accomplished to prevent significant operational

disruptions.

MATERIAL PRICE INFORMATION

No Material

EFFECTIVITY

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

01Z 15T 53Z 59Z 78X 83V 86Z 98X AAF AAN AAR ABQ ACA

ADR AEE AEU AFR AHY AIJ AJM AMU ANA ART AUA AWW AZA

B2V BAW BEL BER BGH BIE BMA BTV C9G CCA CCM CES CIB

CQH CQN CSA CSC CSN CSZ CTN CYP D2F DAL DCS DLH EAA

EDW EIN ETD ETJ EZD F2I FFT FHE FHY FIN FPY FRN G4I

G8E GFA GIR GSW GWI GWY HDA HEJ HVN I2L IAC IBE IRA

IRM ISS IZM JAV JBU JET JKK JST KAC KBR KHO KKK KPS

KZR LAN LBT LBY LFO LIT LLP LMU MAU MDL MHS MLD MLR

MMA MON MSR MXA NMA NVD OHY OZW PAL PIC PTR QAF QTR

RFJ RKM RNV RYW RZO SAS SBI SDM SFW SGG SHJ SHY SKU

SLK SOL STU STZ SVR SWE SWR SYR TAE TAI TAM TAP TAR

TBJ TCW TCX THY TNA TOM UAL UDC UEA USA VBG VKH VLE

VLG VLK VNV VOI VUN WGT WHT WTJ WZZ XLF YAP

CONCURRENT REQUIREMENTS

None

REFERENCES / REPERCUSSIONS

TFU None

OEB None

AOT None

SIL None

LINE MAINTENANCE AFFECTED No

LIFE LIMIT None

OTHER None

DATE: Jan 28/11 SERVICE BULLETIN No.: A320-27-1206

REVISION No.: 01 - Oct 10/11 Page: 2

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SERVICE BULLETIN

SUMMARY

NATURE OF THE WORK

AIRCRAFT YES

EQUIPMENT NO

HARD NO

SOFT NO

OBRM NO

MANPOWER

Task 271206-832-848-001: Inspection

TOTAL MANHOURS 7.25

ELAPSED TIME (HOURS) 3.75

Task 271206-832-849-001: Inspection - ADDITIONAL WORK

TOTAL MANHOURS 7.25

ELAPSED TIME (HOURS) 3.25

APPENDICES

None

DATE: Jan 28/11 SERVICE BULLETIN No.: A320-27-1206

REVISION No.: 01 - Oct 10/11 Page: 3

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SERVICE BULLETIN

SUMMARY

**CONF ALL

B

A

A

LH SHOWN A RH SYMMETRICAL

C

Z600

Z500

INBOARD FLAP

OUTBOARD FLAP

C

INTERCONNECTING STRUT

INBOARD FLAP

OUTBOARD FLAP

FWD

VIEW LOOKING DOWN

LH SHOWN

RH SYMMETRICAL

37CV

39CV

38CV

40CV

LH

LH

RH

RH

B

N_SB_271206_6_SAAA_01_00

Figure A-GSAAA - Sheet 01

DATE: Jan 28/11 SERVICE BULLETIN No.: A320-27-1206

REVISION No.: 01 - Oct 10/11 Page: 4

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

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: 27

TITLE: FLIGHT CONTROLS - FLAP - INTERCONNECTING STRUT INSPECTION

MODIFICATION No.: None

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

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

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

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

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

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

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

AIRBUS prior written consent.

1. PLANNING INFORMATION

**CONF ALL

A. EFFECTIVITY

(1) Models

318-111 318-112 319-111 319-112 319-113 319-114 319-115 319-131

319-132 319-133 320-211 320-212 320-214 320-231 320-232 320-233

321-111 321-112 321-131 321-211 321-212 321-231 321-232

(2) Effectivity by MSN

0029 0039 0042-0059 0061-0078 0080-0090 0093-0097 0099 0102-0104 0109-0128

0132 0135-0155 0157-0162 0164-0176 0178-0179 0181-0183 0185-0192 0194-0224

0226-0237 0239-0270 0272-0279 0281-0303 0305-0312 0314 0316-0337 0339-0362

0364-0373 0375-0396 0398-0432 0434-0466 0468-0480 0482-0535 0537-0546

0548-0601 0603-0631 0633-0707 0709-0752 0754-0788 0790-0955 0957-1043

1045-1185 1187-1217 1219-1277 1279-1373 1375-1812 1814-1818 1821 1823 1825

1827 1829 1832 1834-1836 1838 1840 1842-1843 1845 1847 1849 1852 1854 1856

(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.

DATE: Jan 28/11 SERVICE BULLETIN No.: A320-27-1206

REVISION No.: 01 - Oct 10/11 Page: 1

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SERVICE BULLETIN

OPERATOR MSN

01Z 1589

15T 0764 1494

53Z 1468

59Z 1556

78X 0667 0739 0743 1054 1124

83V 0226

86Z 0164 1706 1750

98X 0342

AAF 0244 0639 0808 0823 1006 1451

AAN 0299 0430 0527

AAR 0802 1174 1227 1356 1511 1636 1670 1734

ABQ 1008

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 1562 1577 1602 1611

1623 1630 1632 1638 1673 1719 1726 1742 1748 1772 1783 1805

1811

ADR 0043 0191 0444

AEE 1727

AEU 0136

AFR 0044 0061 0062 0063 0102 0115 0144 0145 0155 0186 0187 0214

0227 0228 0236 0237 0239 0270 0278 0285 0286 0287 0337 0352

0377 0491 0498 0509 0521 0529 0544 0598 0600 0608 0618 0625

0637 0777 0796 0938 0985 0998 1000 1020 1025 1036 1133 1151

1169 1176 1190 1201 1216 1267 1271 1299 1344 1404 1415 1444

1449 1471 1476 1502 1505 1524 1616 1622 1640 1645 1658 1677

1691 1699 1733

AHY 0331

AIJ 0707 1132 1162 1179 1244 1259 1308 1322 1747 1780

AJM 0624 0626 0628

AMU 0557 0597 0620 0631 0805 0908 0928 1758 1790

ANA 0139 0151 0167 0170 0196 0212 0219 0245 0300 0328 0365 0383

0413 0482 0501 0507 0531 0534 0549 0554 0658 0669 0685

ART 0142 0283 0310 0311 0333 0359 0384 0426 0724

AUA 0552 0570 0581 0768 0776 0797 0920 0935 1137 1150 1189 1385

1387 1458 1478 1504

AWW 0229 0428

AZA 0434 0477 0488 0494 0495 0513 0514 0515 0516 0524 0526 0532

0576 0583 0586 0593 0599 0765 0819 0848 0940 0951 0959 0999

1138 1168 1217 1220 1448 1457 1473 1480 1489 1722 1740 1745

1770 1779

B2V 0185

DATE: Jan 28/11 SERVICE BULLETIN No.: A320-27-1206

REVISION No.: 01 - Oct 10/11 Page: 2

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SERVICE BULLETIN

OPERATOR MSN

BAW 0039 0042 0103 0109 0120 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 1558 1574 1590 1594

1604 1606 1661 1665 1687 1689 1696 1708 1754 1760 1782 1814

1829

BEL 0644 1086 1102 1160 1336 1388 1441 1493

BER 1553 1607 1629 1797 1838

BGH 0221 0294 0305 0349 1087

BIE 0293 0517 0519 0535 0642 0827 0891

BMA 1014 1177 1418 1424 1690 1711

BTV 0168 0361 0441 0449 0460 0461 0710 1676

C9G 0246

CCA 0876 0921 1296 1654 1679 1753

CCM 1068 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 1542 1551

1601 1603 1639 1778 1786

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

CQH 0978 1286 1372 1686 1769 1852

CQN 0696 0698 0704 0705

CSA 0674 0684 1439 1450

CSC 0540 0550 0551 0556 0573 0582 0591 0872 0874 0878 0902 0912

0915 0919 1007 1013 1060 1293 1500

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

1035 1039 1057 1596 1614 1776 1788

CSZ 0994

CTN 0258 0767 0833 1009 1029 1237 1252

CYP 0256 1729 1768

D2F 0211 0243 0251 0326 0344 0354 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 1567 1570 1582

1633 1641 1646 1659 1662 1683 1685 1693 1709 1714 1738 1746

1752 1766 1774 1789 1796 1800 1810 1812 1815

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 0412 0458 0468

0473 0474 0484 0493 0502 0505 0518 0560 0563 0564 0567 0595

0609 0610 0616 0623 0627 0636 0641 0651 0652 0679 0689 0692

0694 0699 0700 0717 0723 0729 0738 0744 0853 0860 0875 0887

0901 1080 1161 1188 1214 1260 1273 1337 1365 1367

EAA 0445

DATE: Jan 28/11 SERVICE BULLETIN No.: A320-27-1206

REVISION No.: 01 - Oct 10/11 Page: 3

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SERVICE BULLETIN

OPERATOR MSN

EDW 0942 0947 1026

EIN 0926 1023 1094 1242 1394 1443 1467

ETD 0350

ETJ 0325 0386

EZD 1074

F2I 0128 0188 0394 0615

FFT 1515 1579 1583 1660 1684 1759 1781 1803 1806

FHE 0888 0936 1171 1210

FHY 0132 0288 0580 0771 0855

FIN 0941 0961 1073 1107 1184 1185 1241 1309 1352 1364 1405 1470

1544 1588 1678 1712 1735 1791 1808

FPY 0112 0438

FRN 0409 0466 0497

G4I 1157 1795

G8E 1464

GFA 0419 0675 0761

GIR 0630

GSW 0376

GWI 1077 1084 1089 1136 1147 1155 1170 1209 1277

GWY 1564 1615 1725

HDA 0633 0756 0784 0812 0930 0993 1024 1253 1695 1721

HEJ 0087 0088

HVN 0590 0594 0601 0605 0607 0611 0617 0619 0648 0650

I2L 0443 0579 0645 0666 0760 0775 1454

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

0080 0089 0090 0095 0096 0097 0247 0257 0308 0314 0327 0336

0396 0398 0416 0423 0431 0432 0451 0469 0480 0486 0490 0492

0499 1668 1718

IBE 0176 0207 0223 0274 1021 1027 1047 1059 1067 1099 1119 1154

1180 1208 1229 1247 1255 1262 1288 1292 1318 1347 1362 1516

1530 1540 1554 1572 1655 1674 1681 1694 1716 1736 1793 1809

1836

IRA 0303 0312 0345 0575 0857

IRM 0530 1202

ISS 0588 0737 0749 1048 1125 1198 1283 1305 1715 1723 1823

IZM 1730

JAV 0029

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

1452 1506 1528 1546 1557 1610 1650 1705 1739 1784 1785 1849

JET 0204 0215 0371 0421 0542 0647 0660 0816 0877

JKK 1183 1276 1333 1349 1366 1383 1407 1497 1631 1682 1749 1843

JST 1195 1408

KAC 0181 0182 0195

KBR 0937 1597

KHO 0362 0405

KKK 0604 0614 0968 0974 1438 1503

KPS 0234

DATE: Jan 28/11 SERVICE BULLETIN No.: A320-27-1206

REVISION No.: 01 - Oct 10/11 Page: 4

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SERVICE BULLETIN

OPERATOR MSN

KZR 1042 1204

LAN 0407 1304 1332 1351 1355 1491 1512 1526 1548 1568 1612 1626

1854

LBT 0222 0301 0348 0400 0793 0970 0995 1121 1175 1744

LBY 0558 0561 1098

LFO 0659

LIT 0646 0654 0794 1016 1172

LLP 1411

LMU 0932 0943

MAU 1592

MDL 0391

MHS 1300 1353

MLD 0249 0622 0741

MLR 0977

MMA 0113 0114 0295 0316

MON 0379 0389 0392 0864 0983 1015 1045 1081 1153 1207 1370 1428

1433 1707 1763 1794

MSR 0165 0166 0178 0194 0198 0322 0351 0366 0680 0687 0715 0725

MXA 0252 0259 0260 0261 0275 0276 0291 0292 0296 0320 0321 0332

0347 0353 0357 0368 0369 0373 0447 1429 1618 1634

NMA 1697 1732

NVD 0375

OHY 0364 0385 0455 0471 0496 0640 0663 0668 0676 0787 0792 0835

0916 0954 0963 1004 1421 1482 1509

OZW 0429

PAL 0706 0745

PIC 0990

PTR 0459 0537

QAF 0927 1335

QTR 1487 1566 1648 1656 1773

RFJ 0814

RKM 1599

RNV 0772 0913

RYW 0569

RZO 0795

SAS 1587 1619 1642 1675 1798 1807 1817

SBI 1071 1078 1090 1091 1126 1129 1131 1149 1164 1167

SDM 0427 0525 0649 1130 1488 1560 1578 1657 1743 1761 1767

SFW 0671

SGG 0799 0879

SHJ 0910

SHY 0138 0148 0811 1194

SKU 0179 0406 1400 1523

SLK 0899 0969 1228 1422 1561 1698

SOL 0302

STU 0420 0436 0446

DATE: Jan 28/11 SERVICE BULLETIN No.: A320-27-1206

REVISION No.: 01 - Oct 10/11 Page: 5

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SERVICE BULLETIN

OPERATOR MSN

STZ 0190 0279 0395

SVR 0140 0157 0203 0220 0735 0815 0841 0991 1012 1063 1152 1484

1720 1751 1777

SWE 0169 0289

SWR 0520 0522 0541 0545 0553 0559 0562 0574 0577 0578 0585 0596

0603 0612 0621 0635 0643 0664 0673 0681 0701 0703 0713 0727

0734 0782 0987 1018 1144 1762

SYR 0886 0918 1032 1076 1085 1117

TAE 0657 0934

TAI 1066 1113 1334 1598 1624 1625

TAM 0250 0334 0335 0440 0758 0976 1010 1092 1096 1103 1139 1143

1158 1215 1246 1251 1339 1368 1376 1459 1486 1518 1575 1580

1591 1593 1595 1608 1613 1628 1652 1663 1672 1692 1703 1717

1757 1771 1775 1801 1802 1804 1818 1825 1827 1832 1835

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

1307 1399 1667 1713 1756 1765 1799 1816

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

1187 1479 1700

TBJ 1485

TCW 0425 0453 0653 1306 1787

TCX 0424 0437 0476 0677 0716 1238 1250

THY 0806 0810 1002 1219 1233 1856

TNA 0538 0555 0606 0731 0746 0791 0822

TOM 0781 0852 1320 1571 1605 1637

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 1555

1559 1569 1573 1581 1584 1585 1586 1600 1609 1617 1620 1627

1647 1649 1653 1664 1669 1671 1680 1688 1702 1728 1731 1737

1741 1755 1821 1840 1842 1845 1847

UDC 0085 0230 0235 0662 0733 0747

UEA 0946 0949 1263

DATE: Jan 28/11 SERVICE BULLETIN No.: A320-27-1206

REVISION No.: 01 - Oct 10/11 Page: 6

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SERVICE BULLETIN

OPERATOR MSN

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 1403 1406 1410 1412 1417 1419

1425 1431 1436 1442 1447 1455 1462 1463 1465 1472 1481 1490

1492 1496 1499 1517 1519 1521 1525 1527 1531 1534 1536 1539

1547 1552 1563 1565 1576 1621 1643 1644 1651 1666 1701 1704

1710 1724 1764 1792

VBG 1199

VKH 0393 0414 0415

VLE 1226

VLG 0143 0146 0158 0173 0199 0224 0240 0241 0264 0266 0323 0356

0992 1101 1221 1396 1413 1430 1461 1550

VLK 0422 0528 0714 0730 1200 1213 1379 1390

VNV 0543 0661

VOI 1140 1159

VUN 1017

WGT 1212

WHT 0726 1256

WTJ 0548

WZZ 0839 0892 1635 1834

XLF 0189 0343 0973

YAP 0533 0566

DATE: Jan 28/11 SERVICE BULLETIN No.: A320-27-1206

REVISION No.: 01 - Oct 10/11 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 0062

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

0128 0132 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 0188 0189 0190 0191 0192

0194 0195 0196 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 0226 0227

0228 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

0286 0287 0288 0289 0290 0291 0292 0293 0294 0295 0296

0297 0298 0299 0300 0301 0302 0303 0305 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 0344

0345 0346 0347 0348 0349 0350 0351 0352 0353 0354 0355

0356 0357 0358 0359 0360 0361 0362 0364 0365 0366 0367

0368 0369 0370 0371 0372 0373 0375 0376 0377 0378 0379

0380 0381 0382 0383 0384 0385 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 0412 0413

0414 0415 0416 0417 0418 0419 0420 0421 0422 0423 0424

0425 0426 0427 0428 0429 0430 0431 0432 0434 0435 0436

0437 0438 0439 0440 0441 0442 0443 0444 0445 0446 0447

0448 0449 0450 0451 0452 0453 0454 0455 0456 0457 0458

0459 0460 0461 0462 0463 0464 0465 0466 0468 0469 0470

0471 0472 0473 0474 0475 0476 0477 0478 0479 0480 0482

0483 0484 0485 0486 0487 0488 0489 0490 0491 0492 0493

0494 0495 0496 0497 0498 0499 0500 0501 0502 0503 0504

0505 0506 0507 0508 0509 0510 0511 0512 0513 0514 0515

0516 0517 0518 0519 0520 0521 0522 0523 0524 0525 0526

0527 0528 0529 0530 0531 0532 0533 0534 0535 0537 0538

0539 0540 0541 0542 0543 0544 0545 0546 0548 0549 0550

0551 0552 0553 0554 0555 0556 0557 0558 0559 0560 0561

0562 0563 0564 0565 0566 0567 0568 0569 0570 0571 0572

0573 0574 0575 0576 0577 0578 0579 0580 0581 0582 0583

0584 0585 0586 0587 0588 0589 0590 0591 0592 0593 0594

0595 0596 0597 0598 0599 0600 0601 0603 0604 0605 0606

0607 0608 0609 0610 0611 0612 0613 0614 0615 0616 0617

001

DATE: Jan 28/11 SERVICE BULLETIN No.: A320-27-1206

REVISION No.: 01 - Oct 10/11 Page: 8

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MSN CONFIGURATION

0618 0619 0620 0621 0622 0623 0624 0625 0626 0627 0628

0629 0630 0631 0633 0634 0635 0636 0637 0638 0639 0640

0641 0642 0643 0644 0645 0646 0647 0648 0649 0650 0651

0652 0653 0654 0655 0656 0657 0658 0659 0660 0661 0662

0663 0664 0665 0666 0667 0668 0669 0670 0671 0672 0673

0674 0675 0676 0677 0678 0679 0680 0681 0682 0683 0684

0685 0686 0687 0688 0689 0690 0691 0692 0693 0694 0695

0696 0697 0698 0699 0700 0701 0702 0703 0704 0705 0706

0707 0709 0710 0711 0712 0713 0714 0715 0716 0717 0718

0719 0720 0721 0722 0723 0724 0725 0726 0727 0728 0729

0730 0731 0732 0733 0734 0735 0736 0737 0738 0739 0740

0741 0742 0743 0744 0745 0746 0747 0748 0749 0750 0751

0752 0754 0755 0756 0757 0758 0759 0760 0761 0762 0763

0764 0765 0766 0767 0768 0769 0770 0771 0772 0773 0774

0775 0776 0777 0778 0779 0780 0781 0782 0783 0784 0785

0786 0787 0788 0790 0791 0792 0793 0794 0795 0796 0797

0798 0799 0800 0801 0802 0803 0804 0805 0806 0807 0808

0809 0810 0811 0812 0813 0814 0815 0816 0817 0818 0819

0820 0821 0822 0823 0824 0825 0826 0827 0828 0829 0830

0831 0832 0833 0834 0835 0836 0837 0838 0839 0840 0841

0842 0843 0844 0845 0846 0847 0848 0849 0850 0851 0852

0853 0854 0855 0856 0857 0858 0859 0860 0861 0862 0863

0864 0865 0866 0867 0868 0869 0870 0871 0872 0873 0874

0875 0876 0877 0878 0879 0880 0881 0882 0883 0884 0885

0886 0887 0888 0889 0890 0891 0892 0893 0894 0895 0896

0897 0898 0899 0900 0901 0902 0903 0904 0905 0906 0907

0908 0909 0910 0911 0912 0913 0914 0915 0916 0917 0918

0919 0920 0921 0922 0923 0924 0925 0926 0927 0928 0929

0930 0931 0932 0933 0934 0935 0936 0937 0938 0939 0940

0941 0942 0943 0944 0945 0946 0947 0948 0949 0950 0951

0952 0953 0954 0955 0957 0958 0959 0960 0961 0962 0963

0964 0965 0966 0967 0968 0969 0970 0971 0972 0973 0974

0975 0976 0977 0978 0979 0980 0981 0982 0983 0984 0985

0986 0987 0988 0989 0990 0991 0992 0993 0994 0995 0996

0997 0998 0999 1000 1001 1002 1003 1004 1005 1006 1007

1008 1009 1010 1011 1012 1013 1014 1015 1016 1017 1018

1019 1020 1021 1022 1023 1024 1025 1026 1027 1028 1029

1030 1031 1032 1033 1034 1035 1036 1037 1038 1039 1040

1041 1042 1043 1045 1046 1047 1048 1049 1050 1051 1052

1053 1054 1055 1056 1057 1058 1059 1060 1061 1062 1063

1064 1065 1066 1067 1068 1069 1070 1071 1072 1073 1074

1075 1076 1077 1078 1079 1080 1081 1082 1083 1084 1085

1086 1087 1088 1089 1090 1091 1092 1093 1094 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 1133 1134 1135 1136 1137 1138 1139 1140

1141 1142 1143 1144 1145 1146 1147 1148 1149 1150 1151

1152 1153 1154 1155 1156 1157 1158 1159 1160 1161 1162

1163 1164 1165 1166 1167 1168 1169 1170 1171 1172 1173

1174 1175 1176 1177 1178 1179 1180 1181 1182 1183 1184

001

DATE: Jan 28/11 SERVICE BULLETIN No.: A320-27-1206

REVISION No.: 01 - Oct 10/11 Page: 9

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MSN CONFIGURATION

1185 1187 1188 1189 1190 1191 1192 1193 1194 1195 1196

1197 1198 1199 1200 1201 1202 1203 1204 1205 1206 1207

1208 1209 1210 1211 1212 1213 1214 1215 1216 1217 1219

1220 1221 1222 1223 1224 1225 1226 1227 1228 1229 1230

1231 1232 1233 1234 1235 1236 1237 1238 1239 1240 1241

1242 1243 1244 1245 1246 1247 1248 1249 1250 1251 1252

1253 1254 1255 1256 1257 1258 1259 1260 1261 1262 1263

1264 1265 1266 1267 1268 1269 1270 1271 1272 1273 1274

1275 1276 1277 1279 1280 1281 1282 1283 1284 1285 1286

1287 1288 1289 1290 1291 1292 1293 1294 1295 1296 1297

1298 1299 1300 1301 1302 1303 1304 1305 1306 1307 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 1333 1334 1335 1336 1337 1338 1339 1340 1341

1342 1343 1344 1345 1346 1347 1348 1349 1350 1351 1352

1353 1354 1355 1356 1357 1358 1359 1360 1361 1362 1363

1364 1365 1366 1367 1368 1369 1370 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 1399 1400 1401 1402 1403 1404 1405 1406 1407 1408

1409 1410 1411 1412 1413 1414 1415 1416 1417 1418 1419

1420 1421 1422 1423 1424 1425 1426 1427 1428 1429 1430

1431 1432 1433 1434 1435 1436 1437 1438 1439 1440 1441

1442 1443 1444 1445 1446 1447 1448 1449 1450 1451 1452

1453 1454 1455 1456 1457 1458 1459 1460 1461 1462 1463

1464 1465 1466 1467 1468 1469 1470 1471 1472 1473 1474

1475 1476 1477 1478 1479 1480 1481 1482 1483 1484 1485

1486 1487 1488 1489 1490 1491 1492 1493 1494 1495 1496

1497 1498 1499 1500 1501 1502 1503 1504 1505 1506 1507

1508 1509 1510 1511 1512 1513 1514 1515 1516 1517 1518

1519 1520 1521 1522 1523 1524 1525 1526 1527 1528 1529

1530 1531 1532 1533 1534 1535 1536 1537 1538 1539 1540

1541 1542 1543 1544 1545 1546 1547 1548 1549 1550 1551

1552 1553 1554 1555 1556 1557 1558 1559 1560 1561 1562

1563 1564 1565 1566 1567 1568 1569 1570 1571 1572 1573

1574 1575 1576 1577 1578 1579 1580 1581 1582 1583 1584

1585 1586 1587 1588 1589 1590 1591 1592 1593 1594 1595

1596 1597 1598 1599 1600 1601 1602 1603 1604 1605 1606

1607 1608 1609 1610 1611 1612 1613 1614 1615 1616 1617

1618 1619 1620 1621 1622 1623 1624 1625 1626 1627 1628

1629 1630 1631 1632 1633 1634 1635 1636 1637 1638 1639

1640 1641 1642 1643 1644 1645 1646 1647 1648 1649 1650

1651 1652 1653 1654 1655 1656 1657 1658 1659 1660 1661

1662 1663 1664 1665 1666 1667 1668 1669 1670 1671 1672

1673 1674 1675 1676 1677 1678 1679 1680 1681 1682 1683

1684 1685 1686 1687 1688 1689 1690 1691 1692 1693 1694

1695 1696 1697 1698 1699 1700 1701 1702 1703 1704 1705

1706 1707 1708 1709 1710 1711 1712 1713 1714 1715 1716

1717 1718 1719 1720 1721 1722 1723 1724 1725 1726 1727

1728 1729 1730 1731 1732 1733 1734 1735 1736 1737 1738

1739 1740 1741 1742 1743 1744 1745 1746 1747 1748 1749

001

DATE: Jan 28/11 SERVICE BULLETIN No.: A320-27-1206

REVISION No.: 01 - Oct 10/11 Page: 10

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MSN CONFIGURATION

1750 1751 1752 1753 1754 1755 1756 1757 1758 1759 1760

1761 1762 1763 1764 1765 1766 1767 1768 1769 1770 1771

1772 1773 1774 1775 1776 1777 1778 1779 1780 1781 1782

1783 1784 1785 1786 1787 1788 1789 1790 1791 1792 1793

1794 1795 1796 1797 1798 1799 1800 1801 1802 1803 1804

1805 1806 1807 1808 1809 1810 1811 1812 1814 1815 1816

1817 1818 1821 1823 1825 1827 1829 1832 1834 1835 1836

1838 1840 1842 1843 1845 1847 1849 1852 1854 1856

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

No Material Set

B. CONCURRENT REQUIREMENTS

None

C. REASON

(1) History

For certain target/proximity sensor combinations on Flap interconnecting strut,

engineering investigation has shown that a "target FAR" signal could not be detected

before reaching the mechanical end stop of the interconnecting strut. In such a case a

potential flap down drive disconnection would not be detected.

(2) Objective/Action

This Service Bulletin has been issued to describe the required inspection necessary to

identify the respective struts with the target/proximity sensor combination leading to this

issue.

The applicable interconnecting struts are pre Mod. 27956 which have the subsequent

part numbers:

- D5757030500000

- D5757030500100

- D5757030500200

- D5757030500600

- D5757030500800

- D5757030501000

DATE: Jan 28/11 SERVICE BULLETIN No.: A320-27-1206

REVISION No.: 01 - Oct 10/11 Page: 11

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- D5757030501200

- D5757032200000

On the above listed interconnecting struts the following combination of proximity

sensor/target is not allowed:

- TARGET SN (with SN) <1600 + Sensor PN 8-372-04 or PN ABS0121-31 with

Sensor SN between C59198 and C59435 or C500000 and higher.

(3) Advantages

Accomplishment of this Service Bulletin will ensure the correct combination of

Strut/Sensor/Target and thus the correct function of the Flap system.

(4) Operational/Maintenance Consequences

None

D. DESCRIPTION

Additional work is required by this revision unless operators can demonstrate using their

records that aircraft are not fitted with PN D5757030501000 and PN D5757030501200.

To accomplish this Service Bulletin it is necessary to :

Task 271206-832-848-001: Inspection

(1) Do a General Visual Inspection (GVI) of the interconnecting strut

Task 271206-832-849-001: Inspection - ADDITIONAL WORK

(1) Do a General Visual Inspection (GVI) of the interconnection strut

E. COMPLIANCE

(1) Classification

RECOMMENDED: Service Bulletin recommended to be accomplished to prevent

significant operational disruptions.

(2) Accomplishment Timescale

It is recommended to accomplish the inspection procedure before 8000FH after issue of

this Service Bulletin.

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

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

Agency (EASA). It is anticipated that the AD will confirm the threshold given above but

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

timescale.

DATE: Jan 28/11 SERVICE BULLETIN No.: A320-27-1206

REVISION No.: 01 - Oct 10/11 Page: 12

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F. APPROVAL

Approved under EASA Design Organisation Approval No. EASA 21J.031.

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

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

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

before incorporation of the Service Bulletin.

G. MANPOWER

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

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

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

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

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

included.

Task 271206-832-848-001: Inspection

Get Access 2.25

On Aircraft

Do a General Visual Inspection (GVI) of the

interconnecting strut

2.00

Tests 1.00

Close-Up 2.00

TOTAL MANHOURS 7.25

ELAPSED TIME (HOURS) 3.75

Task 271206-832-849-001: Inspection - ADDITIONAL WORK

Get Access 2.25

On Aircraft

Do a General Visual Inspection (GVI) of the

interconnection strut

2.00

Tests 1.00

Close-Up 2.00

TOTAL MANHOURS 7.25

ELAPSED TIME (HOURS) 3.25

H. WEIGHT AND BALANCE

Not Changed

I. ELECTRICAL LOAD DATA

Not Changed

DATE: Jan 28/11 SERVICE BULLETIN No.: A320-27-1206

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J. REFERENCES

Aircraft Maintenance Manual (AMM) 06-20-00 12-34-24 27-51-00

27-51-44 27-54-00

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

Illustrated Parts Catalog (IPC) 27-51-44

Service Bulletin (SB) A320-57-1164

K. PUBLICATION AFFECTED

None

L. INTERCHANGEABILITY/MIXABILITY

Not Applicable

M. SPARES

None

DATE: Jan 28/11 SERVICE BULLETIN No.: A320-27-1206

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2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

(1) Procurement Addresses

To replace parts detected during the accomplishment of this Inspection Service Bulletin

the operators 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, Logistic 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

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

be purchased by a Spares Purchase Order.

B. INDUSTRY SUPPORT INFORMATION

For those aircraft with Finding Configuration C further to inspection as per this Service

Bulletin, AIRBUS will provide the parts at no charge. In this case, a copy of the Inspection

Report Sheet must be sent together with the Purchase Order (PO).

In all other cases Airbus will not provide industry support for the accomplishment of this

Service Bulletin.

C. LIST OF COMPONENTS

No Kit

D. LIST OF MATERIALS - OPERATOR SUPPLIED

None

E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

None

F. TOOLING

(1) Tooling - Price and Availability

To accomplish this Service Bulletin it is necessary to use the tools listed in AMM Task

27-51-44-000-001 and AMM Task 27-51-44-820-001.

DATE: Jan 28/11 SERVICE BULLETIN No.: A320-27-1206

REVISION No.: 01 - Oct 10/11 Page: 15

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(2) Tools

None

(3) Special Tools

None

DATE: Jan 28/11 SERVICE BULLETIN No.: A320-27-1206

REVISION No.: 01 - Oct 10/11 Page: 16

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3. ACCOMPLISHMENT INSTRUCTIONS

Task 271206-832-848-001 - 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 THE RELATED DOORS

- COMPONENTS THAT MOVE.

MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS.

WARNING: MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE

LANDING GEAR.

WARNING: IN CASE ELECTRICAL ELEMENTS HAVE TO BE REPAIRED, MAKE SURE

THAT NO AC OR DC POWER SOURCE IS CONNECTED TO THE AIRCRAFT

ELECTRICAL CIRCUITS. THERE IS A RISK OF ELECTROCUTION IF THE AC

OR DC POWER STAYS CONNECTED.

CAUTION: BE CAREFUL WHEN YOU DO MAINTENANCE TASKS ON THE WING

TRAILING EDGE:

- DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE RACEWAYS.

- DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE INSTALLATIONS.

- MAKE SURE THAT THE ELECTRICAL CABLES ARE INSTALLED

CORRECTLY. INCORRECT INSTALLATION CAN CAUSE DAMAGE.

DATE: Jan 28/11 SERVICE BULLETIN No.: A320-27-1206

REVISION No.: 01 - Oct 10/11 Page: 17

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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

580 680

Manpower

TOTAL MANHOURS 7.25

ELAPSED TIME (HOURS) 3.75

A. GENERAL

(1) Subtask 271206-910-201-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

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

(a) For the aircraft zoning (Refer to AMM 06-20-00, Page Block 001).

(2) Subtask 271206-839-201-001 - Documentation

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

DATE: Jan 28/11 SERVICE BULLETIN No.: A320-27-1206

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B. PREPARATION

(1) Subtask 271206-941-201-001 - Job Set-up

Work Zones and Access Panels

Zone Access/Work location

580

680

Manpower Resources

Skills AIRFRAME

References

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

Task 27-51-44-000-001

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

12-34-24-869-002).

(b) Do the Job set-up procedure as given in the removal of the interconnecting strut

(Refer to AMM Task 27-51-44-000-001).

C. PROCEDURE

(1) Subtask 271206-210-201-001 - Do a General Visual Inspection (GVI) of the

interconnecting strut

Work Zones and Access Panels

Zone Access/Work location

580

680

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 27-51-44-000-001

Task 27-51-44-000-002

Task 27-51-44-400-001

Task 27-51-44-400-002

Task 27-54-00-200-001

Illustrated Parts Catalog (IPC) 27-51-44

Service Bulletin (SB) A320-57-1164

Fig. A-GBAAA

Interconnecting strut inspection

Sheet 01

Sheet 02

Fig. A-GFAAA

Flow-chart

Sheet 01

Sheet 02

DATE: Jan 28/11 SERVICE BULLETIN No.: A320-27-1206

REVISION No.: 01 - Oct 10/11 Page: 19

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References

Fig. A-GRAAA

Inspection Report Sheet

Sheet 01

(a) Do a general visual inspection of the interconnecting strut as shown on Fig. AGBAAA Sheet 01, Fig. A-GBAAA Sheet 02, Fig. A-GFAAA Sheet 01 and Fig. AGFAAA Sheet 02.

1 Check if one of the following interconnecting strut part numbers are installed:

- D5757030500000

- D5757030500100

- D5757030500200

- D5757030500600

- D5757030500800

- D5757030501000

- D5757030501200

- D5757032200000

a If none of the above mentioned part numbers are installed (Finding

Configuration A):

- No further action is necessary.

b If an above mentioned part number is installed:

- On the target PN 8-536-01 or PN ABS0121-13, identify the target

serial number, refer to paragraph 3.C.(1)(a)2.

2 Identify the target serial number.

a If the target serial number is hidden behind the interconnecting strut

structure:

- Disconnect the interconnecting strut rod end from the attachment

bracket (Refer to AMM Task 27-51-44-000-001) and turn the rod until

the target serial number becomes visible.

b If the target serial number is not readable, or the SN is lower than 1600:

NOTE: The target SN might be preceded by an A.

- Identify the proximity sensor part number, refer to paragraph

3.C.(1)(a)3.

DATE: Jan 28/11 SERVICE BULLETIN No.: A320-27-1206

REVISION No.: 01 - Oct 10/11 Page: 20

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c If the SN of the target serial number is not lower than 1600 (Finding

Configuration B):

- If removed previously, reinstall the rod end to its original position

(Refer to AMM Task 27-51-44-400-001).

- Re-identify the interconnecting strut (Refer to A320-57-1164) within a

maximum 8000FH from original issue date of this Service Bulletin.

- No further action in accordance with this Service Bulletin is

necessary.

3 Identify the part numbers of the relevant proximity sensors (37CV, 38CV,

39CV, 40CV).

a Remove the proximity sensor (Refer to AMM Task 27-51-44-000-002,

IPC 27-51-44).

b If the sensor part number is not 8-372-04 or PN ABS0121-31 (Finding

Configuration A):

- Reinstall the relevant proximity sensor (Refer to AMM Task

27-51-44-400-002, IPC 27-51-44).

- If removed previously, reinstall the rod end to its original position

(Refer to AMM Task 27-51-44-400-001).

- No further action in accordance with this Service Bulletin is

necessary.

NOTE: From issuance of this Service Bulletin, it is not allowed to

install proximity sensor, PN 8-372-04 or PN ABS0121-31,

on interconnecting struts with the PN’s listed above in

Paragraph 3.C.(1)(a)1.

Embodiment of Service Bulletin 57-1164 allows to

upgrade/reidentify the affected interconnecting struts.

Post SB 57-1164 interconnecting strut part numbers can

be fitted with proximity sensor, PN ABS0121-31 or PN

8-372-04, (IPC 27-51-44 is updated accordingly).

c If the sensor part number is 8-372-04 or PN ABS0121-31, identify the

proximity sensor serial number, refer to paragraph 3.C.(1)(a)4.

4 Identify the serial numbers of the relevant proximity sensors.

a If the proximity sensor serial number is not between C59198 and C59435

or not equal to or higher than C500000 (Finding Configuration A):

- Reinstall the relevant proximity sensor (Refer to AMM Task

27-51-44-400-002, IPC 27-51-44).

DATE: Jan 28/11 SERVICE BULLETIN No.: A320-27-1206

REVISION No.: 01 - Oct 10/11 Page: 21

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- If removed previously, reinstall the rod end to its original position

(Refer to AMM Task 27-51-44-400-001).

- No further action in accordance with this Service Bulletin is

necessary.

b If the proximity sensor serial number is between C59198 and C59435 or

it is C500000 or higher, the operator has two options to proceed before

the next flight (Finding Configuration C):

<1> First option:

<a> Remove the interconnecting strut (Refer to AMM Task

27-51-44-000-001).

NOTE: The removed strut must be discarded

or must be modified and reidentified to

allow its reinstallation on aircraft (Refer to

A320-57-1164).

<b> Install (Refer to AMM Task 27-51-44-400-001):

- An interconnecting strut which is post MOD 27956 (PN

D57570322-002-00 for A318/A319/A320 aircraft or PN

D57570305-016-00 for A321 aircraft).

or

- An interconnecting strut which is pre MOD 27956 but

compliant with Finding Configuration A or B of this Service

Bulletin.

NOTE: A strut pre MOD 27956 and compliant with

Finding Configuration B, has to be reidentified

as per Service Bulletin A320-57-1164

installation on aircraft.

<c> Complete and send the Report Sheet to AIRBUS, refer to Fig.

A-GRAAA Sheet 01.

<d> No further action in accordance with this Service Bulletin is

necessary.

<2> Second option:

Only if the interconnecting strut can not be replaced before the next

flight.

<a> Reinstall the relevant proximity sensor (Refer to AMM Task

27-51-44-400-002, IPC 27-51-44).

<b> If removed previously, reinstall the rod end to its original

position (Refer to AMM Task 27-51-44-400-001).

DATE: Jan 28/11 SERVICE BULLETIN No.: A320-27-1206

REVISION No.: 01 - Oct 10/11 Page: 22

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<c> Inspect the flap down drive (Refer to AMM Task

27-54-00-200-001 steps 4.A.5 thru 4.A.7) in order to operate

the aircraft for a maximum of 50 additional flight cycles.

<d> After a maximum 50 flight cycles, remove the interconnecting

strut (Refer to AMM Task 27-51-44-000-001).

NOTE: The removed strut must be discarded

or must be modified and reidentified to

allow its reinstallation on aircraft (Refer to

A320-57-1164).

<e> Install (Refer to AMM Task 27-51-44-400-001):

- An interconnecting strut which is post MOD 27956 (PN

D57570322-002-00 for A318/A319/A320 aircraft or PN

D57570305-016-00 for A321 aircraft).

or

- An interconnecting strut which is pre MOD 27956 but

compliant with Finding Configuration A or B of this Service

Bulletin.

NOTE: A strut pre MOD 27956 and compliant with

Finding Configuration B, has to be reidentified

as per Service Bulletin A320-57-1164 before

installation on aircraft.

<f> Complete and send the Report Sheet to AIRBUS, refer to Fig.

A-GRAAA Sheet 01.

<g> No further action in accordance with this Service Bulletin is

necessary.

D. TEST

(1) Subtask 271206-941-202-001 - Job Set-up

Manpower Resources

Skills AIRFRAME

(a) Remove the Locking Tool from the flap/slat control lever on panel 114VU.

(b) Make sure that the test area is clear of access platforms and other items of

equipment.

(2) Subtask 271206-700-201-001 - Test

Manpower Resources

Skills NON SPECIFIC

DATE: Jan 28/11 SERVICE BULLETIN No.: A320-27-1206

REVISION No.: 01 - Oct 10/11 Page: 23

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References

Aircraft Maintenance Manual (AMM) Task 27-54-00-710-001

(a) Do an operational test of the flap system (Refer to AMM Task 27-54-00-710-001).

E. CLOSE-UP

(1) Subtask 271206-942-201-001 - Close-up

Work Zones and Access Panels

Zone Access/Work location

580

680

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 27-51-44-400-001

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

equipment.

(b) Do the close-up procedure as given in the installation of the interconnecting strut

(Refer to AMM Task 27-51-44-400-001).

DATE: Jan 28/11 SERVICE BULLETIN No.: A320-27-1206

REVISION No.: 01 - Oct 10/11 Page: 24

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SERVICE BULLETIN

Task 271206-832-849-001 - Inspection - ADDITIONAL WORK

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 THE RELATED DOORS

- COMPONENTS THAT MOVE.

MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS.

WARNING: MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE

LANDING GEAR.

WARNING: IN CASE ELECTRICAL ELEMENTS HAVE TO BE REPAIRED, MAKE SURE

THAT NO AC OR DC POWER SOURCE IS CONNECTED TO THE AIRCRAFT

ELECTRICAL CIRCUITS. THERE IS A RISK OF ELECTROCUTION IF THE AC

OR DC POWER STAYS CONNECTED.

CAUTION: BE CAREFUL WHEN YOU DO MAINTENANCE TASKS ON THE WING

TRAILING EDGE:

- DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE RACEWAYS.

- DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE INSTALLATIONS.

- MAKE SURE THAT THE ELECTRICAL CABLES ARE INSTALLED

CORRECTLY. INCORRECT INSTALLATION CAN CAUSE DAMAGE.

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.

DATE: Jan 28/11 SERVICE BULLETIN No.: A320-27-1206

REVISION No.: 01 - Oct 10/11 Page: 25

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Task Associated Data

Zone

580 680

Manpower

TOTAL MANHOURS 7.25

ELAPSED TIME (HOURS) 3.25

A. GENERAL

(1) Subtask 271206-910-202-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

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

For the aircraft zoning (Refer to AMM 06-20-00, Page Block 001).

(2) Subtask 271206-839-202-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

B. PREPARATION

(1) Subtask 271206-941-203-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

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

Task 27-51-44-000-001

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

12-34-24-869-002).

(b) Do the Job set-up procedure as given in the removal of the interconnection strut

(Refer to AMM Task 27-51-44-000-001).

DATE: Jan 28/11 SERVICE BULLETIN No.: A320-27-1206

REVISION No.: 01 - Oct 10/11 Page: 26

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C. PROCEDURE

(1) Subtask 271206-210-202-001 - Do a General Visual Inspection (GVI) of the

interconnection strut

Work Zones and Access Panels

Zone Access/Work location

580

680

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 27-51-44-000-001

Task 27-51-44-000-002

Task 27-51-44-400-001

Task 27-51-44-400-002

Task 27-54-00-200-001

Illustrated Parts Catalog (IPC) 27-51-44

Service Bulletin (SB) A320-57-1164

Fig. A-GBAAA

Interconnecting strut inspection

Sheet 01

Sheet 02

Fig. A-GFAAA

Flow-chart

Sheet 01

Sheet 02

Fig. A-GRAAA

Inspection Report Sheet

Sheet 01

(a) Do a general visual inspection of the interconnecting strut as shown on Fig. AGBAAA Sheet 01, Fig. A-GBAAA Sheet 02, Fig. A-GFAAA Sheet 01 and Fig. AGFAAA Sheet 02.

1 Check if one of the following interconnecting strut part numbers are installed:

- D5757030501000

- D5757030501200

a If none of the above mentioned part numbers are installed (Finding

Configuration A):

- No further action is necessary.

b If an above mentioned part number is installed:

- On the target PN 8-536-01 or PN ABS0121-13, identify the target

serial number, refer to paragraph 3.C.(1)(a)2.

DATE: Jan 28/11 SERVICE BULLETIN No.: A320-27-1206

REVISION No.: 01 - Oct 10/11 Page: 27

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2 Identify the target serial number.

a If the target serial number is hidden behind the interconnecting strut

structure:

- Disconnect the interconnecting strut rod end from the attachment

bracket (Refer to AMM Task 27-51-44-000-001) and turn the rod until

the target serial number becomes visible.

b If the target serial number is not readable, or the SN is lower than 1600:

NOTE: The target SN might be preceded by an A.

- Identify the proximity sensor part number, refer to paragraph

3.C.(1)(a)3.

c If the SN of the target serial number is not lower than 1600 (Finding

Configuration B):

- If removed previously, reinstall the rod end to its original position

(Refer to AMM Task 27-51-44-400-001).

- Re-identify the interconnecting strut (Refer to A320-57-1164) within a

maximum 8000FH from original issue date of this Service Bulletin.

- No further action in accordance with this Service Bulletin is

necessary.

3 Identify the part numbers of the relevant proximity sensors (37CV, 38CV,

39CV, 40CV).

a Remove the proximity sensor (Refer to AMM Task 27-51-44-000-002,

IPC 27-51-44).

b If the sensor part number is not 8-372-04 or PN ABS0121-31 (Finding

Configuration A):

- Reinstall the relevant proximity sensor (Refer to AMM Task

27-51-44-400-002, IPC 27-51-44).

- If removed previously, reinstall the rod end to its original position

(Refer to AMM Task 27-51-44-400-001).

- No further action in accordance with this Service Bulletin is

necessary.

NOTE: From issuance of this Service Bulletin, it is not allowed to

install proximity sensor, PN 8-372-04 or PN ABS0121-31,

on interconnecting struts with the PN’s listed above in

Paragraph 3.C.(1)(a)1.

Embodiment of Service Bulletin 57-1164 allows to

upgrade/reidentify the affected interconnecting struts.

DATE: Jan 28/11 SERVICE BULLETIN No.: A320-27-1206

REVISION No.: 01 - Oct 10/11 Page: 28

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Post SB 57-1164 interconnecting strut part numbers can

be fitted with proximity sensor, PN ABS0121-31 or PN

8-372-04, (IPC 27-51-44 is updated accordingly).

c If the sensor part number is 8-372-04 or PN ABS0121-31, identify the

proximity sensor serial number, refer to paragraph 3.C.(1)(a)4.

4 Identify the serial numbers of the relevant proximity sensors.

a If the proximity sensor serial number is not between C59198 and C59435

or not equal to or higher than C500000 (Finding Configuration A):

- Reinstall the relevant proximity sensor (Refer to AMM Task

27-51-44-400-002, IPC 27-51-44).

- If removed previously, reinstall the rod end to its original position

(Refer to AMM Task 27-51-44-400-001).

- No further action in accordance with this Service Bulletin is

necessary.

b If the proximity sensor serial number is between C59198 and C59435 or

it is C500000 or higher, the operator has two options to proceed before

the next flight (Finding Configuration C):

<1> First option:

<a> Remove the interconnecting strut (Refer to AMM Task

27-51-44-000-001).

NOTE: The removed strut must be discarded

or must be modified and reidentified to

allow its reinstallation on aircraft (Refer to

A320-57-1164).

<b> Install (Refer to AMM Task 27-51-44-400-001):

- An interconnecting strut which is post MOD 27956 (PN

D57570322-002-00 for A318/A319/A320 aircraft or PN

D57570305-016-00 for A321 aircraft).

or

- An interconnecting strut which is pre MOD 27956 but

compliant with Finding Configuration A or B of this Service

Bulletin.

NOTE: A strut pre MOD 27956 and compliant with

Finding Configuration B, has to be reidentified

as per Service Bulletin A320-57-1164

installation on aircraft.

<c> Complete and send the Report Sheet to AIRBUS, refer to Fig.

A-GRAAA Sheet 01.

DATE: Jan 28/11 SERVICE BULLETIN No.: A320-27-1206

REVISION No.: 01 - Oct 10/11 Page: 29

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<d> No further action in accordance with this Service Bulletin is

necessary.

<2> Second option:

Only if the interconnecting strut can not be replaced before the next

flight.

<a> Reinstall the relevant proximity sensor (Refer to AMM Task

27-51-44-400-002, IPC 27-51-44).

<b> If removed previously, reinstall the rod end to its original

position (Refer to AMM Task 27-51-44-400-001).

<c> Inspect the flap down drive (Refer to AMM Task

27-54-00-200-001 steps 4.A.5 thru 4.A.7) in order to operate

the aircraft for a maximum of 50 additional flight cycles.

<d> After a maximum 50 flight cycles, remove the interconnecting

strut (Refer to AMM Task 27-51-44-000-001).

NOTE: The removed strut must be discarded

or must be modified and reidentified to

allow its reinstallation on aircraft (Refer to

A320-57-1164).

<e> Install (Refer to AMM Task 27-51-44-400-001):

- An interconnecting strut which is post MOD 27956 (PN

D57570322-002-00 for A318/A319/A320 aircraft or PN

D57570305-016-00 for A321 aircraft).

or

- An interconnecting strut which is pre MOD 27956 but

compliant with Finding Configuration A or B of this Service

Bulletin.

NOTE: A strut pre MOD 27956 and compliant with

Finding Configuration B, has to be reidentified

as per Service Bulletin A320-57-1164 before

installation on aircraft.

<f> Complete and send the Report Sheet to AIRBUS, refer to Fig.

A-GRAAA Sheet 01.

<g> No further action in accordance with this Service Bulletin is

necessary.

DATE: Jan 28/11 SERVICE BULLETIN No.: A320-27-1206

REVISION No.: 01 - Oct 10/11 Page: 30

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D. TEST

(1) Subtask 271206-941-204-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

(a) Remove the Locking Tool from the flap/slat control lever on 114VU.

(b) Make sure that the test area is clear of access platforms and other items of

equipment.

(2) Subtask 271206-700-202-001 - Test

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 27-54-00-710-001

(a) Do an operational test of the flap system (Refer to AMM Task 27-54-00-710-001).

E. CLOSE-UP

(1) Subtask 271206-942-202-001 - Close-up

Work Zones and Access Panels

Zone Access/Work location

580

680

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 27-51-00-400-001

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

equipment.

(b) Do the close up procedure as given in the installation of the interconnection strut

(Refer to AMM Task 27-51-00-400-001).

DATE: Jan 28/11 SERVICE BULLETIN No.: A320-27-1206

REVISION No.: 01 - Oct 10/11 Page: 31

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**CONF ALL

B

A

A

LH SHOWN A RH SYMMETRICAL

C

Z600

Z500

INBOARD FLAP

OUTBOARD FLAP

C

INTERCONNECTING STRUT

INBOARD FLAP

OUTBOARD FLAP

FWD

VIEW LOOKING DOWN

LH SHOWN

RH SYMMETRICAL

37CV

39CV

38CV

40CV

LH

LH

RH

RH

B

N_SB_271206_6_BAAA_01_00

D

Figure A-GBAAA - Sheet 01

Interconnecting strut inspection

DATE: Jan 28/11 SERVICE BULLETIN No.: A320-27-1206

REVISION No.: 01 - Oct 10/11 Page: 32

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SERVICE BULLETIN

**CONF ALL

OUTBOARD FLAP

ATTACHMENT

INBOARD FLAP

ATTACHMENT

BRACKET

INTERCONNECTING STRUT

ROD END SENSOR

39CV

40CV

LH

RH

SENSOR

LH

38CV RH

TARGET

TARGET

SENSOR

LH

RH

SENSOR

LH

RH

E FWD

VIEW LOOKING DOWN

PIN

WASHER

SCREW

NUT

37CV

37CV

LH SHOWN

RH SYMMETRICAL

39CV

40CV

38CV

BRACKET WASHER

SCREW

NUT

NUT

WASHER

SCREW

D

SENSOR E

SENSOR

PROXIMITY

PROXIMITY

PROXIMITY

PROXIMITY

N_SB_271206_6_BAAA_02_03

Figure A-GBAAA - Sheet 02

Interconnecting strut inspection

DATE: Jan 28/11 SERVICE BULLETIN No.: A320-27-1206

REVISION No.: 01 - Oct 10/11 Page: 33

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SERVICE BULLETIN

**CONF ALL

WITHIN NEXT 8000 FH

CHECK IF FOLLOWING INTERCONNECTING STRUT P/N

IS INSTALLED ON AIRCRAFT, FOR LH AND RH WING:

D5757030500000 OR D5757030500100 OR

D5757030500200 OR D5757030500600 OR

D5757030501200 OR D5757032200000

IDENTIFY THE TARGET S/N

RE−IDENTIFY

THE INTERCONNECTING STRUT,

AS PER SB A320−57−1164

IS THE

TARGET S/N

READABLE

YES

NO

YES

IDENTIFY

SENSOR S/N

IS THE

SENSOR S/N

BETWEEN C59198 AND

C59435 OR C500000

YES REFER TO FIGURE A−GFAAA, SHEET 02

THE PROXIMITY

PROXIMITY

YES

FINDING CONFIGURATION A

NO FURTHER

ACTION NECESSARY

NO

SENSOR P/N

OR

8−372−04

IS THE

ABS0121−31

S/N LOWER

ARE

THAN 1600

FINDING CONFIGURATION B

AND HIGHER

NO FURTHER

ACTION NECESSARY

YES

NO

NO

NO

OR ABS0121−13,

ON TARGET P/N 8−536−01 

SENSOR P/N

IDENTIFY THE

NOTE:

01 FROM IPC 27−51−44 FEB−11 REVISION, IT IS NOT ALLOWED TO INSTALL SENSOR P/N 8−372−04

01

(OR ABS0121−31) ON STRUT P/N LISTED IN FIRST STEP OF THIS FLOWCHART.

AT NEXT SENSOR FAILURE ON THESE STRUTS, REPLACEMENT OF THE COMPLETE STRUT WILL

BE REQUIRED. EMBODIMENT OF SB A320−57−1164 ALLOWS THE UPGRADE AND THE 

RE−IDENTIFICATION OF THE CONCERNED STRUTS TO ALLOW INSTALLATION OF SENSOR

P/N 8−372−04 (OR ABS0121−31).

D5757030500800 OR D5757030501000 OR

N_SB_271206_6_FAAA_01_09

WITHIN 8000FC MAXIMUM FROM

THE ISSUANCE OF SB A320−27−1206

Figure A-GFAAA - Sheet 01

Flow-chart

DATE: Jan 28/11 SERVICE BULLETIN No.: A320-27-1206

REVISION No.: 01 - Oct 10/11 Page: 34

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**CONF ALL

DO ONE OF THE FOLLOWING

BEFORE THE NEXT FLIGHT

INSPECT

THE FLAP DOWN DRIVE

OR

WITHIN MAXIMUM

50 FLIGHTS

− REMOVE THE INTERCONNECTING STRUT

− INSTALL AN INTERCONNECTING STRUT POST−MOD 27956

OR

− INSTALL A STRUT PRE−MOD 27956 BUT COMPLIANT WITH 

CONTINUED FROM FIGURE A−GFAAA, SHEET 01

IF THE STRUT CAN NOT BE

REPLACED BEFORE

NEXT FLIGHT

COMPLETE AND SEND 

FINDING CONFIGURATION C

 FINDING CONFIGURATION A OR B OF THIS SERVICE BULLETIN

THE INSPECTION REPORT TO AIRBUS

NO FURTHER

ACTION NECESSARY

N_SB_271206_6_FAAA_02_05

Figure A-GFAAA - Sheet 02

Flow-chart

DATE: Jan 28/11 SERVICE BULLETIN No.: A320-27-1206

REVISION No.: 01 - Oct 10/11 Page: 35

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SERVICE BULLETIN

**CONF ALL

Inspection Report 

SERVICE BULLETIN NO:

DATE OF INSPECTION:

A/C MSN:

FLIGHT CYCLES:

FLIGHT HOURS:

INTERCONNECTION STRUT INSPECTION

Please send reporting sheet to:

AIRBUS

CUSTOMER SERVICES ENGINEERING

1 ROND POINT MAURICE BELLONTE

31707 BLANGNAC CEDEX

SENSOR / TARGET IDENTIFICATION TABLE

37CV

SENSOR S/N

39CV

TARGET S/N

FIN No.

LH

Comments:

A320−27−1206

or via Resident Customer Support Office.

SEEL 5

FRANCE +33 (0) 5 61 93 32 73

FLIGHT CONTROL SYSTEMS

INTERCONNECTION STRUT P/N

INTERCONNECTION STRUT S/N

38CV

SENSOR S/N

40CV

TARGET S/N

FIN No.

RH

INTERCONNECTION STRUT P/N

INTERCONNECTION STRUT S/N

YES NO IS ONE SENSOR S/N BETWEEN C59198 AND C59435 

IS TARGET S/N < 1600 ? YES NO

QUESTION 2:

QUESTION 1:

RESULTS: QUESTION 1 QUESTION 2 CONFIG. for LH

YES NO

NO

YES YES

A

B

C

OR HIGHER THAN C500000 ?

N_SB_271206_6_RAAA_01_04

LH

YES NO

YES NO

RH

CONFIG. for RH

A

B

C

Figure A-GRAAA - Sheet 01

Inspection Report Sheet

DATE: Jan 28/11 SERVICE BULLETIN No.: A320-27-1206

REVISION No.: 01 - Oct 10/11 Page: 36

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

REPORTING SHEET

TITLE: FLIGHT CONTROLS - FLAP - INTERCONNECTING STRUT INSPECTION

MODIFICATION No.: None

Please complete the appropriate item (A or B):

A - SB WILL BE embodied YES/NO (if NO please comment)

If YES, aircraft concerned (as per SB effectivity by default) and planned dates (month/year) of

embodiment:

B - SB HAS BEEN embodied on aircraft:

Operator comments:

From Airline:

Name/Title:

Signature: Date:

If operational documentation is affected (see Paragraph 1.K of this SB): If information is needed prior to

next normal revision or prior to SB embodiment, please indicate required service(s):

Either: Modification Operational Impact (MOI), if available YES/NO

Or : Intermediate revision YES/NO

Important Information: This SB will only be incorporated in your maintenance and operational

documentation if this sheet is returned to Airbus and signed by a duly authorised representative. With

the next feasible revision, this will result in

- Updating of maintenance documentation to show pre and post SB data.

- Updating of maintenance and operational documentation to show post SB data after embodiment.

If this SB requires previous or simultaneous accomplishment of other SBs, Airbus shall automatically

include them in the manual revisions. Refer to SIL 00-037 for detailed information.

Please return this completed sheet to:

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX FRANCE

Attn: SDC32 Technical Data and Documentation Services

FAX: (+33) 5 61 93 28 06

e-mail: sb.reporting@airbus.com

or via your Resident Customer Support Office.

Alternatively, SB lists via letters or fax are also accepted.

DATE: Jan 28/11 SERVICE BULLETIN No.: A320-27-1206

REVISION No.: 01 - Oct 10/11 Page: 1

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

QUALITY PERCEPTION FORM

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

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

improve the quality of our Service Bulletins.

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

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

- Quality rating of this SB 4321

- Quality rating of the Accomplishment Instructions 4321

- Quality rating of the Illustrations 4321

- Is this SB easy to understand ? Y/N

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

short description of the issue.

Planning Material Instructions

X Effectivity X Kit content X Preparation

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

X Manpower X Industry support X Test

X References X Re-identification X Close-Up

X Publication X Tooling X Illustrations

Comments:

Operator: Date:

Name/Title:

Please return this form to:

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX FRANCE

Attn : SEM4 Service Bulletins Management

FAX : (33) 5 61 93 42 51

Or via your Resident Customer Support Office.

DATE: Jan 28/11 SERVICE BULLETIN No.: A320-27-1206

REVISION No.: 01 - Oct 10/11 Page: 1

6

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