SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

MANDATORY MANDATORY MANDATORY MANDATORY

ATA SYSTEM : 25

TITLE : EQUIPMENT/FURNISHINGS - SEMI AUTOMATIC CARGO LOADING - IMPROVE NET

ATTACHMENT POINTS OF FIXED YZ-LATCHES

MODIFICATION No. : 32316K7824, 32317K7825

This page transmits Revision No. 06 of Service Bulletin No. A320-25-1294

ADDITIONAL WORK

ADDITIONAL WORK 1 is required by this revision for aircraft MSNs 0750, 0755, 0763, 0790, 0821,

0837, 0906, 0917, 0933, 0979 and 1034 modified by Revision 04 or any previous issue.

ADDITIONAL WORK 1 is required by this revision for aircraft MSNs 0588, 0612, 0713, 0727, 0734,

0869, 0880, 1018, 1048, 1073 and 1086 modified by Revision 05 or any previous issue.

ADDITIONAL WORK 2 is required by this revision for aircraft MSNs 0012, 0014, 0016, 0365, 0371,

0566, 0573, 0582, 0590, 0594, 0607, 0611, 0617, 0619, 0648, 0650, 0658, 0669, 1054, 1059, 1063,

1067, 1101, 1119, 1132, 1137, 1138, 1150, 1162, 1168, 1177, 1179, 1181, 1187, 1189, 1200, 1206,

1864, 1871, 1873, 1874, 1879 and 1885 modified by Revision 05 or any previous issue.

ADDITIONAL WORK 3 is required by this revision for aircraft MSNs 0771, 0802, 0811, 0855, 0963,

0987, 1008, 1276, 1333, 1366 and 1798 modified by Revision 05 or any previous issue.

REASON

This Revision is issued to :

- update Kits D02, D04 and D05

- delete aircraft MSNs 0002, 0010, 0013, 0020, 0021, 0033, 0035, 0100, 0101, 0108, 0129, 0133

and 0177 from the Effectivity, update the effectivity and operators

- add ADDITIONAL WORK 1, add aircraft MSNs 0588, 0612, 0713, 0727, 0734, 0869, 0880, 1018,

1048, 1073 and 1086

- add ADDITIONAL WORK 2, for aircraft MSNs 0012, 0014, 0016, 0365, 0371, 0566, 0573, 0582,

0590, 0594, 0607, 0611, 0617, 0619, 0648, 0650, 0658, 0669, 1054, 1059, 1063, 1067, 1101,

1119, 1132, 1137, 1138, 1150, 1162, 1168, 1177, 1179, 1181, 1187, 1189, 1200, 1206, 1864,

1871, 1873, 1874, 1879 and 1885

DATE : Mar 14/03 SERVICE BULLETIN No. : A320-25-1294

REVISION No. : 06 - Jul 23/10 Page : 1 of 3

Printed in France © AIRBUS 2008 All rights reserved
SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

- add ADDITIONAL WORK 3, for aircraft MSNs 0771, 0802, 0811, 0855, 0963, 0987, 1008, 1276,

1333, 1366 and 1798

- introduce minor changes.

CHANGES

SUMMARY :

- REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES

. MODIFICATION CLASSIFICATION table added.

- EFFECTIVITY

. Operators updated.

- MANPOWER

. Manpower for ADDITIONAL WORK 2 and 3 added.

PLANNING INFORMATION :

- EFFECTIVITY

. 1.A. Aircraft MSNs 0002, 0010, 0013, 0020, 0021, 0033, 0035, 0100, 0101, 0108, 0129, 0133

and 0177 deleted, effectivity and operators updated. Effectivity by MSN and Kit/Configuration

updated and NOTEs amended.

- DESCRIPTION

. 1.D.(8) Applicable aircraft updated.

. 1.D.(9) Work step for ADDITIONAL WORK 2 added.

. 1.D.(10) Work step for ADDITIONAL WORK 3 added.

- MANPOWER

. 1.G. Manpower for ADDITIONAL WORK 2 and 3 added.

- WEIGHT AND BALANCE

. 1.H. Weight and Balance data for ADDITIONAL WORK 1, 2 and 3 added.

- INDUSTRY SUPPORT

. 2.B. Sentence updated.

- TOOLING - PRICE AND AVAILABILITY

. 2.F. Quantity of tooling updated.

DATE : Mar 14/03 SERVICE BULLETIN No. : A320-25-1294

REVISION No. : 06 - Jul 23/10 Page : 2

Printed in France © AIRBUS 2008 All rights reserved
SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

ACCOMPLISHMENT INSTRUCTIONS :

- MODIFICATION

. 3.B.(8) Applicable aircraft updated.

. 3.B.(9) Work step for ADDITIONAL WORK 2 added.

. 3.B.(10) Work step for ADDITIONAL WORK 3 added.

NOTE : Layout changes due to computerization of this revision are not identified.

FILING INSTRUCTIONS

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

Replace the complete document.

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

HISTORY OF PREVIOUS REVISIONS

Revision No. 01 was issued to change the Compliance from Recommended to Mandatory and to

update the effectivity.,

Revision No. 02 was issued to remove all aircraft from the effectivity, which have accomplished Service

Bulletin Nos. A320-25-1251 and A320-25-1252, remove the Kit 251294D02 for MSN 1366, update the

Effectivity, update the kit allocation per aircraft and to introduce minor changes.

Revision No. 03 was issued to add aircraft MSNs 0190, 0203, 0220, 0221, 0222, 0234, 0235, 0302,

0305, 0395, 0407, 0420, 0436, 0491 and 0726 to the effectivity.

Revision No. 04 was issued to delete aircraft MSN 0018 from the effectivity and to add aircraft MSNs

0577 and 0585 to the effectivity and update the operators.

Revision No. 05 was issued to delete the aircraft MSNs 0004, 0006, 0017 and 0036 from the effectivity,

add the aircraft MSNs 0243, 0249, 0250, 0251, 0252, 0259, 0260, 0261, 0275, 0276, 0296, 0320, 0321,

0332, 0334, 0335, 0353, 0361, 0368, 0369, 0440 and 0870 to the effectivity and to add ADDITIONAL

WORK with Kit D04 for aircraft MSNs 0750, 0755, 0763, 0790, 0821, 0837, 0906, 0917, 0933, 0979

and 1034.

ORIGINAL : Mar 14/03

REVISION No. : 01 - Mar 27/06

REVISION No. : 02 - Sep 05/06

REVISION No. : 03 - Jan 22/07

REVISION No. : 04 - Mar 13/08

REVISION No. : 05 - Jan 22/09

REVISION No. : 06 - Jul 23/10

DATE : Mar 14/03 SERVICE BULLETIN No. : A320-25-1294

REVISION No. : 06 - Jul 23/10 Page : 3

Printed in France © AIRBUS 2008 All rights reserved
SERVICE BULLETIN

This Page Intentionally Left Blank

DATE : Mar 14/03 SERVICE BULLETIN No. : A320-25-1294

REVISION No. : 06 - Jul 23/10 Page : 4

Printed in France © AIRBUS 2008 All rights reserved
SERVICE BULLETIN

SUMMARY

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

This summary is for information only and is

not approved for modification of the aircraft

MANDATORY MANDATORY MANDATORY MANDATORY

ATA SYSTEM : 25

TITLE : EQUIPMENT/FURNISHINGS - SEMI AUTOMATIC CARGO LOADING - IMPROVE NET

ATTACHMENT POINTS OF FIXED YZ-LATCHES

MODIFICATION No. : 32316K7824, 32317K7825

REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES

A review of the Cargo Loading System (CLS) by the AIRBUS stress department has shown an area where

improvements could be introduced at the net attachment points of YZ-Latches :

- PN D2557235000000 thru -00600,

- PN D2557238000000/-00200/-00600/-00800.

This Service Bulletin details the procedure to install two spacer assemblies (supporting ring with spring ring)

at each net attachment point of the YZ-latches of the CLS in the FWD and AFT cargo-compartments.

The accomplishment of this Service Bulletin will improve the net attachment points.

EVALUATION TABLE

COMPLIANCE Mandatory 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

KIT PRICE (USD) See SB

DATE : Mar 14/03 SERVICE BULLETIN No. : A320-25-1294

REVISION No. : 06 - Jul 23/10 Page : 1 of 9

Printed in France © AIRBUS 2008 All rights reserved
SERVICE BULLETIN

SUMMARY

MODIFICATION CLASSIFICATION

MAJOR None

MINOR 32316K7824 32317K7825

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.

EFFECTIVITY

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

39Z 47W 69X 76U 86Z 98X AAF AAR ABQ ACA ADR AEU AFR AIJ AMU ANA ART AUA AZA B2V BAW

BEL BER BGH BIE BMA C9G CCM CSA CSC CSZ CTN CYP D2F DLH EIN ETD F2I FFT FHY FIN G2X

G8E GFA HVN IAC IBE IRA ISR ISS JET JKK KBR KKK KZR LBT LTU MAU MLD MMA MON MSR MXA

NMA OHY RFJ SAS SHY STZ SVR SWR TAE TAM TAP TAR TAS THY TNA VLE VLG VLK

The solution with modification 32316K7824 and 32317K7825 is a retro solution. The serial solution with

modification 32244K7774 and 32245K7775 (new designed YZ-latch) is embodied on aircraft MSN 1850 ,

1859 , 1869 , 1878 , 1893 and subsequent.

This Service Bulletin is only applicable on aircraft equipped with CLS.

This Service Bulletin is not applicable to YZ-Latches PN D2557238000400.

CONCURRENT REQUIREMENTS

None

REFERENCES/REPERCUSSIONS

TFU : None

OEB : None

AOT : None

SIL : None

LIFE LIMIT : None

LINE MAINTENANCE AFFECTED : No

OTHERS : None

NATURE OF THE WORK

AIRCRAFT : YES

DATE : Mar 14/03 SERVICE BULLETIN No. : A320-25-1294

REVISION No. : 06 - Jul 23/10 Page : 2

Printed in France © AIRBUS 2008 All rights reserved
SERVICE BULLETIN

SUMMARY

EQUIPMENT : NO

HARD : NO

SOFT : NO

OBRM : NO

MANPOWER

Kit 251294D01R00

TOTAL MANHOURS 4.75

ELAPSED TIME (HOURS) 3.00

Kit 251294D02R00

TOTAL MANHOURS 5.75

ELAPSED TIME (HOURS) 3.50

Kit 251294D03R00

TOTAL MANHOURS 7.50

ELAPSED TIME (HOURS) 4.50

Kit 251294D04R00

TOTAL MANHOURS 5.25

ELAPSED TIME (HOURS) 3.25

Kit 251294D05R00

TOTAL MANHOURS 6.50

ELAPSED TIME (HOURS) 4.00

Kit 251294D06R00

TOTAL MANHOURS 7.50

ELAPSED TIME (HOURS) 4.50

Kit 251294D07R00

DATE : Mar 14/03 SERVICE BULLETIN No. : A320-25-1294

REVISION No. : 06 - Jul 23/10 Page : 3

Printed in France © AIRBUS 2008 All rights reserved
SERVICE BULLETIN

SUMMARY

TOTAL MANHOURS 5.25

ELAPSED TIME (HOURS) 3.25

Kit 251294D04R00 ADDITIONAL WORK 1

TOTAL MANHOURS 5.25

ELAPSED TIME (HOURS) 3.25

Kit 251294D02R00 and Kit 251294D05R00 ADDITIONAL WORK 2

TOTAL MANHOURS 12.75

ELAPSED TIME (HOURS) 6.00

Kit 251294D03R00 and Kit 251294D06R00 ADDITIONAL WORK 3

TOTAL MANHOURS 15.00

ELAPSED TIME (HOURS) 7.50

MATERIAL INFORMATION

AIRCRAFT DATA

Kit 251294D01R00

Spacer assemblies

Kit 251294D02R00

Spacer assemblies

Kit 251294D03R00

Spacer assemblies

Kit 251294D04R00

Spacer assemblies

Kit 251294D05R00

Spacer assemblies

Kit 251294D06R00

Spacer assemblies

DATE : Mar 14/03 SERVICE BULLETIN No. : A320-25-1294

REVISION No. : 06 - Jul 23/10 Page : 4

Printed in France © AIRBUS 2008 All rights reserved
SERVICE BULLETIN

SUMMARY

Kit 251294D07R00

Spacer assemblies

APPENDICES

None

DATE : Mar 14/03 SERVICE BULLETIN No. : A320-25-1294

REVISION No. : 06 - Jul 23/10 Page : 5

Printed in France © AIRBUS 2008 All rights reserved
SERVICE BULLETIN

SUMMARY

DATE : Mar 14/03 SERVICE BULLETIN No. : A320-25-1294

REVISION No. : 06 - Jul 23/10 Page : 6

Printed in France © AIRBUS 2008 All rights reserved
SERVICE BULLETIN

SUMMARY

DATE : Mar 14/03 SERVICE BULLETIN No. : A320-25-1294

REVISION No. : 06 - Jul 23/10 Page : 7

Printed in France © AIRBUS 2008 All rights reserved
SERVICE BULLETIN

SUMMARY

DATE : Mar 14/03 SERVICE BULLETIN No. : A320-25-1294

REVISION No. : 06 - Jul 23/10 Page : 8

Printed in France © AIRBUS 2008 All rights reserved
SERVICE BULLETIN

SUMMARY

DATE : Mar 14/03 SERVICE BULLETIN No. : A320-25-1294

REVISION No. : 06 - Jul 23/10 Page : 9

Printed in France © AIRBUS 2008 All rights reserved
SERVICE BULLETIN

This Page Intentionally Left Blank

DATE : Mar 14/03 SERVICE BULLETIN No. : A320-25-1294

REVISION No. : 06 - Jul 23/10 Page : 10

Printed in France © AIRBUS 2008 All rights reserved
SERVICE BULLETIN

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

MANDATORY MANDATORY MANDATORY MANDATORY

ATA SYSTEM : 25

TITLE : EQUIPMENT/FURNISHINGS - SEMI AUTOMATIC CARGO LOADING - IMPROVE NET

ATTACHMENT POINTS OF FIXED YZ-LATCHES

MODIFICATION No. : 32316K7824, 32317K7825

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 the 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

A. EFFECTIVITY

(1) Models

319-111 319-112 319-114 319-131 319-132 320-111 320-211 320-212 320-214 320-231

320-232 321-111 321-112 321-131 321-211 321-212 321-231 321-232

(2) Aircraft

(a) Effectivity by MSN

This Service Bulletin is applicable to aircraft MSN :

0003 0005 0007 0008 0012 0014 0016 0019 0039 0042-0044 0059 0061-0063

0068-0073 0078 0083 0084 0086 0093 0094 0102-0104 0109-0111 0113-0117 0120

0122 0126-0128 0130 0135-0139 0141 0143-0151 0154-0156 0158 0159 0161 0162

0167 0170 0172-0176 0180 0183-0188 0190 0191 0196 0199-0204 0207 0209-0212

0214-0224 0226-0228 0231-0237 0239-0246 0248-0261 0264-0270 0274-0279

0283-0287 0290 0295 0296 0300 0302 0303 0305 0308-0312 0314 0316 0320 0321

0323 0324 0328 0330 0332-0335 0337 0341 0342 0346 0350 0352 0353 0356 0359

0361 0365 0368 0369 0371 0376-0378 0382-0384 0386 0395 0401 0403-0405 0407

0409 0412 0413 0420 0426 0434 0436 0440 0458 0468 0473 0474 0477 0482 0484

0488 0491 0493-0495 0498 0501 0502 0505 0507 0509 0513-0522 0524 0526 0529

0531-0535 0538 0541 0544 0545 0548-0550 0552-0555 0557 0559 0560 0562-0564

0566 0567 0570 0573 0574 0576-0578 0581-0583 0585 0586 0588 0590 0593-0596

DATE : Mar 14/03 SERVICE BULLETIN No. : A320-25-1294

REVISION No. : 06 - Jul 23/10 Page : 1 of 30

Printed in France © AIRBUS 2008 All rights reserved
SERVICE BULLETIN

0599 0601 0603 0605-0607 0611 0612 0617 0619-0621 0629 0631 0635 0642 0643

0648 0650 0652 0658 0664 0669 0673-0675 0680 0681 0684 0685 0687 0692 0699

0701 0703 0713 0715 0725-0727 0731 0734 0746 0750 0755 0761 0763 0765 0768

0771 0776 0777 0782 0790 0791 0796 0797 0802 0805 0806 0810 0811 0815 0819

0821 0822 0827 0835 0837 0841 0848 0855 0864 0869 0870 0880 0887 0891 0901

0906 0908 0917 0920 0926 0933-0935 0940 0941 0945 0951 0956 0958-0961 0963

0968 0970 0974 0975 0979 0982 0987 0991 0992 0994 0995 0999 1008 1009 1012

1014 1018 1021 1023 1027 1034 1042 1045 1047 1048 1054 1059 1060 1063 1067

1068 1073 1080-1082 1086 1087 1094 1099-1102 1106 1107 1115 1118-1120 1124

1127 1132 1133 1137 1138 1142 1144 1145 1150 1151 1153 1154 1160-1162 1165

1168 1174 1177 1179-1181 1183-1185 1187-1190 1193 1197 1200 1201 1204

1206-1208 1214-1217 1220-1222 1225-1227 1229 1231 1232 1236 1237 1239 1241

1242 1244 1247 1255 1258 1260-1262 1267 1271 1273 1276 1279 1283 1288 1292

1293 1295 1299 1305 1307-1309 1318 1322 1329 1333 1336-1338 1347 1349 1352

1356 1362 1364-1367 1370 1379 1380 1383-1385 1387 1388 1394 1396 1399 1405

1407 1413 1418 1423 1424 1428-1430 1433 1439-1441 1443 1445 1448 1450 1454

1457 1458 1461 1466 1467 1470 1473 1476 1478-1480 1484 1489 1493 1494 1497

1502 1504 1510 1511 1513 1516 1529 1530 1537 1540 1544 1550 1553 1554 1558

1572 1574 1587 1588 1590 1592 1594 1602 1604 1606 1611 1619 1623 1629 1631

1632 1636 1638 1642 1655 1658 1661 1665 1667 1670 1674 1675 1678 1681 1682

1687 1689 1691 1694 1696 1697 1700 1708 1712 1713 1715 1716 1719 1722 1723

1726 1729 1732 1734-1736 1740 1745 1748 1749 1754 1758 1760 1762 1768 1770

1772 1779 1782 1783 1790 1791 1793 1797-1799 1806-1809 1811 1814 1816 1817

1829 1836 1838 1864 1871 1873 1874 1879 1885

(b) 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

39Z 0956

47W 1494

69X 0588

76U 0302

86Z 0409

98X 0342

AAF 0244

AAR 0802 1227 1356 1511 1636 1734

ABQ 1008

DATE : Mar 14/03 SERVICE BULLETIN No. : A320-25-1294

REVISION No. : 06 - Jul 23/10 Page : 2

Printed in France © AIRBUS 2008 All rights reserved
SERVICE BULLETIN

OPERATOR MSN

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 1602

1611 1623 1632 1638 1719 1726 1748 1772 1783 1811 1864 1874

ADR 0043

AEU 0136

AFR 0005 0007 0012 0014 0016 0019 0044 0061 0062 0063 0102 0115

0128 0130 0144 0145 0155 0156 0184 0186 0187 0188 0214

0226 0227 0228 0235 0236 0237 0239 0270 0278 0285 0286

0287 0337 0352 0377 0491 0498 0509 0521 0529 0544 0777

0796 1133 1151 1190 1201 1216 1267 1271 1299 1476 1502

1658 1691 1873 1879 1885

AIJ 1132 1162 1179 1244 1308 1322

AMU 0557 0620 0631 0805 0908 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 0283 0310 0311 0333 0359 0726

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

1387 1458 1478

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 0191

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 1871

BEL 1086 1160 1336 1388

BER 1629

BGH 0221 0305

BIE 0517 0519 0535 0642 0827 0891

BMA 0835 1014 1174 1177 1418 1424

DATE : Mar 14/03 SERVICE BULLETIN No. : A320-25-1294

REVISION No. : 06 - Jul 23/10 Page : 3

Printed in France © AIRBUS 2008 All rights reserved
SERVICE BULLETIN

OPERATOR MSN

C9G 0246

CCM 0533 0548 1068 1145

CSA 0674 0684 1439 1450

CSC 0550 0573 0582 1060 1293

CSZ 0994

CTN 0258 1009 1237

CYP 0180 0256 0295 0316 1729 1768

D2F 0211 0243 0251 0376 0407

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 0652 0692 0699 0887 0901 1080 1161 1188 1214

1260 1273 1337 1365 1367

EIN 0815 0841 0926 0991 1023 1094 1242 1394 1443 1467

ETD 0350

F2I 0008

FFT 1806

FHY 0771 0855

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

1544 1588 1678 1712 1735 1791 1808

G2X 0234

G8E 0003

GFA 0675 0761

HVN 0590 0594 0601 0605 0607 0611 0617 0619 0648 0650

IAC 0257 0308 0314 0386

IBE 0158 0173 0176 0207 0223 0224 0266 0274 0323 0356 1021 1027

1047 1059 1067 1087 1099 1101 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

DATE : Mar 14/03 SERVICE BULLETIN No. : A320-25-1294

REVISION No. : 06 - Jul 23/10 Page : 4

Printed in France © AIRBUS 2008 All rights reserved
SERVICE BULLETIN

OPERATOR MSN

IRA 0303 0312

ISR 0384 0426

ISS 1048 1102 1283 1305 1715 1723

JET 0204 0215 0371

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

KBR 1454

KKK 0968 0974

KZR 1042 1204

LBT 0222 0970 0995

LTU 1385 1441 1493 1504 1553 1797 1838

MAU 1592

MLD 0249

MMA 0113 0114

MON 0864 1045 1081 1153 1207 1370 1428 1433

MSR 0680 0687 0715 0725

MXA 0252 0259 0260 0261 0275 0276 0296 0320 0321 0332 0353 0361

0368 0369 0405 0566 1429

NMA 1697 1732

OHY 0963

RFJ 1124

SAS 1587 1619 1642 1675 1798 1807 1817

SHY 0138 0148 0811 1670

STZ 0190 0279 0395 0420 0436

SVR 0203 0220 1012 1063 1484

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

DATE : Mar 14/03 SERVICE BULLETIN No. : A320-25-1294

REVISION No. : 06 - Jul 23/10 Page : 5

Printed in France © AIRBUS 2008 All rights reserved
SERVICE BULLETIN

OPERATOR MSN

TAE 0934

TAM 0250 0334 0335 0440 1215

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 1799 1816

TAR 0869 0880 0958 0975 1187 1479 1700

TAS 1054

THY 0806 0810

TNA 0538 0555 0606 0731 0746 0791 0822

VLE 1226

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

1461 1550

VLK 1200 1379

The solution with modification 32316K7824 and 32317K7825 is a retro solution.

The serial solution with modification 32244K7774 and 32245K7775 (new designed

YZ-latch) is embodied on MSN 1850 , 1859 , 1869 , 1878 , 1893 and subsequent.

This Service Bulletin is only applicable on aircraft equipped with CLS.

This Service Bulletin is not applicable to YZ-Latches PN D2557238000400.

(c) Effectivity by MSN and Kit/Configuration

The Kits and configurations applicable to these MSNs are given at the end of this list

0578 0588 0612 0621 0629 0713 0727 0734 0750 0755 0763 0790 0821 0837 0869

0880 0906 0917 0933 0979 1018 1034 1048 1068 1073 1082 1086 1100 1102

1106-1107 1115 1118 1120 1124 1127 1142 1145 1151 1154 1160 1165 1180 1184

1190 1193 1197 1201 1216 1222 1225 1232 1236 1239 1247 1258 1261 1267 1271

1279 1283 1295 1305 1309 1329 1336 1338 1352 1362 1364 1380 1384 1388 1423

1429 1440 1445 1466 1479 1494 1510 1513 1529 1537 1558 1574 1590 1592 1594

1604 1606 1722 1729 1740 1745 1758 1768 1770 1779 1790-1791 1808

KIT No. QTY PER A/C CONFIGURATION

251294D01 1 None

251294D04 1 None

The Kits and configurations applicable to these MSNs are given at the end of this list

DATE : Mar 14/03 SERVICE BULLETIN No. : A320-25-1294

REVISION No. : 06 - Jul 23/10 Page : 6

Printed in France © AIRBUS 2008 All rights reserved
SERVICE BULLETIN

1349 1497 1631 1682 1749

KIT No. QTY PER A/C CONFIGURATION

251294D02 1 None

The Kits and configurations applicable to these MSNs are given at the end of this list

0003 0005 0007-0008 0012 0014 0016 0019 0039 0042-0044 0059 0061-0063

0068-0073 0078 0083-0084 0086 0093-0094 0102-0104 0109-0111 0113-0117

0120 0122 0126-0128 0130 0135-0139 0141 0143-0151 0154-0156 0158-0159

0161-0162 0167 0170 0172-0176 0180 0183-0188 0190-0191 0196 0199-0204 0207

0209-0212 0214-0224 0226-0228 0231-0237 0239-0246 0248-0261 0264-0270

0274-0279 0283-0287 0290 0295-0296 0300 0302-0303 0305 0308-0312 0314

0316 0320-0321 0323-0324 0328 0330 0332-0335 0337 0341-0342 0346 0350

0352-0353 0356 0359 0361 0365 0368-0369 0371 0376-0378 0382-0384 0386 0395

0401 0403-0405 0407 0409 0413 0420 0426 0436 0440 0482 0491 0501 0507 0531

0533-0534 0545 0548-0549 0553-0554 0559 0562 0566 0573-0574 0577 0582 0585

0590 0594 0596 0601 0603 0605 0607 0611 0617 0619 0635 0643 0648 0650 0658

0669 0673 0681 0685 0701 0703 0726 0768 0776 0782 0791 0797 0805 0822 0870

0934 0945 0951 0958 0960 0975 0982 0992 0994 0999 1009 1014 1047 1054 1059

1063 1067 1081 1087 1099 1101 1119 1132 1137-1138 1150 1162 1168 1177 1179

1181 1183 1187 1189 1200 1206 1208 1215 1217 1221 1226 1229 1231 1237 1242

1244 1255 1262 1288 1292 1308 1318 1322 1337 1347 1365 1367 1370 1379 1383

1385 1387 1394 1396 1405 1407 1413 1418 1424 1430 1439 1441 1443 1448 1450

1454 1457 1461 1467 1470 1473 1478 1480 1484 1489 1493 1502 1504 1516 1530

1540 1544 1550 1553 1588 1655 1661 1665 1667 1674 1678 1687 1689 1694

1696-1697 1700 1708 1712 1715 1719 1723 1732 1735-1736 1754 1760 1762 1782

1793 1797 1799 1806 1809 1814 1816 1829 1838 1864 1871 1873-1874 1879 1885

KIT No. QTY PER A/C CONFIGURATION

251294D02 1 None

251294D05 1 None

The Kits and configurations applicable to these MSNs are given at the end of this list

0412 0434 0458 0468 0473-0474 0477 0484 0488 0493-0495 0498 0502 0505 0509

0513-0522 0524 0526 0529 0532 0535 0538 0541 0544 0550 0552 0555 0557 0560

0563-0564 0567 0570 0576 0581 0583 0586 0593 0595 0599 0606 0620 0631 0642

0652 0664 0674-0675 0680 0684 0687 0692 0699 0715 0725 0731 0746 0761 0765

0777 0796 0806 0810 0815 0819 0827 0835 0841 0848 0864 0887 0891 0901 0908

0920 0926 0935 0940-0941 0956 0959 0961 0968 0970 0974 0991 0995 1012 1021

1023 1027 1045 1060 1080 1094 1133 1144 1153 1161 1174 1185 1188 1204 1207

1214 1220 1227 1241 1260 1273 1276 1293 1299 1307 1333 1356 1366 1399

1428 1433 1458 1476 1511 1554 1572 1587 1602 1611 1619 1623 1629 1632

1636 1638 1642 1658 1670 1675 1681 1691 1713 1716 1726 1734 1748 1772

1783 1807 1811 1817 1836

KIT No. QTY PER A/C CONFIGURATION

DATE : Mar 14/03 SERVICE BULLETIN No. : A320-25-1294

REVISION No. : 06 - Jul 23/10 Page : 7

Printed in France © AIRBUS 2008 All rights reserved
SERVICE BULLETIN

251294D03 1 None

251294D06 1 None

The Kits and configurations applicable to these MSNs are given at the end of this list

0771 0802 0811 0855 0963 0987 1008 1042 1798

KIT No. QTY PER A/C CONFIGURATION

251294D03 1 None

251294D07 1 None

NOTE : ADDITIONAL WORK 1 : with Kit D04 is required by this revision for

aircraft MSNs 0588, 0612, 0713, 0727, 0734, 0750, 0755, 0763, 0790,

0821, 0837, 0869, 0880, 0906, 0917, 0933, 0979, 1018, 1034, 1048,

1073 and 1086.

NOTE : ADDITIONAL WORK 2 :

- with Kit D02 is required by this revision for aircraft MSNs 1054, 1059,

1063, 1067, 1101, 1119, 1132, 1137, 1138, 1150, 1162, 1168, 1177,

1179, 1181, 1187, 1189, 1200 and 1206.

- with Kit D05 is required by this revision for aircraft MSNs 0010,

0012-0014, 0016, 0365, 0371, 0566, 0573, 0582, 0590, 0594, 0607,

0611, 0617, 0619, 0648, 0650, 0658, 0669, 1349, 1497, 1631, 1682,

1749, 1864, 1871, 1873, 1874, 1879 and 1885.

(3) Spares

None

B. CONCURRENT REQUIREMENTS

None

C. REASON

(1) History

A review of the Cargo Loading System (CLS) by the AIRBUS stress department has

shown an area where improvements could be introduced at the net attachment points of

YZ-Latches :

- PN D2557235000000 thru -00600,

- PN D2557238000000/-00200/-00600/-00800.

(2) Objective/Action

DATE : Mar 14/03 SERVICE BULLETIN No. : A320-25-1294

REVISION No. : 06 - Jul 23/10 Page : 8

Printed in France © AIRBUS 2008 All rights reserved
SERVICE BULLETIN

This Service Bulletin details the procedure to install two spacer assemblies (supporting ring

with spring ring) at each net attachment point of the YZ-latches of the CLS in the FWD

and AFT cargo-compartments.

(3) Advantages

The accomplishment of this Service Bulletin will improve the net attachment points.

(4) Operational/Maintenance Consequences

None

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

(1) Kit 251294D01R00

(a) Install spacer assemblies to the YZ-latches of the CLS in the FWD

cargo-compartment.

(2) Kit 251294D02R00

(a) Install spacer assemblies to the YZ-latches of the CLS in the FWD

cargo-compartment.

(3) Kit 251294D03R00

(a) Install spacer assemblies to the YZ-latches of the CLS in the FWD

cargo-compartment.

(4) Kit 251294D04R00

(a) Install spacer assemblies to the YZ-latches of the CLS in the AFT

cargo-compartment.

(5) Kit 251294D05R00

(a) Install spacer assemblies to the YZ-latches of the CLS in the AFT

cargo-compartment.

(6) Kit 251294D06R00

(a) Install spacer assemblies to the YZ-latches of the CLS in the AFT

cargo-compartment.

(7) Kit 251294D07R00

(a) Install spacer assemblies to the YZ-latches of the CLS in the AFT

cargo-compartment.

(8) ADDITIONAL WORK 1 Kit 251294D04R00

DATE : Mar 14/03 SERVICE BULLETIN No. : A320-25-1294

REVISION No. : 06 - Jul 23/10 Page : 9

Printed in France © AIRBUS 2008 All rights reserved
SERVICE BULLETIN

(a) Preparation

(b) Modification

Install spacer assemblies to the YZ-latches of the CLS in the AFT

cargo-compartment.

(c) Test

(d) Close up

(9) ADDITIONAL WORK 2 Kit 251294D02R00 and Kit 251294D05R00

(a) Preparation

(b) Modification

Kit 251294D02R00 :

Install spacer assemblies to the YZ-latches of the CLS in the FWD

cargo-compartment.

Kit 251294D05R00 :

Install spacer assemblies to the YZ-latches of the CLS in the AFT

cargo-compartment.

(c) Test

(d) Close up

(10) ADDITIONAL WORK 3 Kit 251294D03R00 and Kit 251294D06R00

(a) Preparation

(b) Modification

Kit 251294D03R00 :

Install spacer assemblies to the YZ-latches of the CLS in the FWD

cargo-compartment.

Kit 251294D06R00 :

Install spacer assemblies to the YZ-latches of the CLS in the AFT

cargo-compartment.

(c) Test

(d) Close up

DATE : Mar 14/03 SERVICE BULLETIN No. : A320-25-1294

REVISION No. : 06 - Jul 23/10 Page : 10

Printed in France © AIRBUS 2008 All rights reserved
SERVICE BULLETIN

E. COMPLIANCE

(1) Classification

Mandatory

(2) Accomplishment Timescale

Accomplishment of this Service Bulletin has been rendered mandatory by the issue of an

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

The AD must be used as the reference document for the mandatory accomplishment

timescale.

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 operators’ circumstances. The estimates do not include the

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

time for paints, sealants, etc. and general administration work are also not included.

Kit 251294D01R00

Get Access 1.50

Modification 1.50

Close-up 1.75

TOTAL MANHOURS 4.75

ELAPSED TIME (HOURS) 3.00

Kit 251294D02R00

Get Access 1.50

Modification 2.50

Close-up 1.75

TOTAL MANHOURS 5.75

ELAPSED TIME (HOURS) 3.50

DATE : Mar 14/03 SERVICE BULLETIN No. : A320-25-1294

REVISION No. : 06 - Jul 23/10 Page : 11

Printed in France © AIRBUS 2008 All rights reserved
SERVICE BULLETIN

Kit 251294D03R00

Get Access 1.50

Modification 4.25

Close-up 1.75

TOTAL MANHOURS 7.50

ELAPSED TIME (HOURS) 4.50

Kit 251294D04R00

Get Access 1.50

Modification 2.00

Close-up 1.75

TOTAL MANHOURS 5.25

ELAPSED TIME (HOURS) 3.25

Kit 251294D05R00

Get Access 1.50

Modification 3.25

Close-up 1.75

TOTAL MANHOURS 6.50

ELAPSED TIME (HOURS) 4.00

Kit 251294D06R00

Get Access 1.50

Modification 4.25

Close-up 1.75

TOTAL MANHOURS 7.50

ELAPSED TIME (HOURS) 4.50

Kit 251294D07R00

Get Access 1.50

Modification 2.00

DATE : Mar 14/03 SERVICE BULLETIN No. : A320-25-1294

REVISION No. : 06 - Jul 23/10 Page : 12

Printed in France © AIRBUS 2008 All rights reserved
SERVICE BULLETIN

Close-up 1.75

TOTAL MANHOURS 5.25

ELAPSED TIME (HOURS) 3.25

Kit 251294D04R00 ADDITIONAL WORK 1

Get Access 1.50

Modification 2.00

Close-up 1.75

TOTAL MANHOURS 5.25

ELAPSED TIME (HOURS) 3.25

Kit 251294D02R00 and Kit 251294D05R00 ADDITIONAL WORK 2

Get Access 3.00

Modification FWD 2.50

Modification AFT 3.75

Close-up 3.50

TOTAL MANHOURS 12.75

ELAPSED TIME (HOURS) 6.00

Kit 251294D03R00 and Kit 251294D06R00 ADDITIONAL WORK 3

Get Access 3.00

Modification FWD 4.25

Modification AFT 4.25

Close-up 3.50

TOTAL MANHOURS 15.00

ELAPSED TIME (HOURS) 7.50

H. WEIGHT AND BALANCE

Kit 251294D01R00

Manufacturers Empty Weight : +0.13 kg (+0.2865 lb)

Effect on Balance : +1.48 kgm (+10.704 lb.ft)

DATE : Mar 14/03 SERVICE BULLETIN No. : A320-25-1294

REVISION No. : 06 - Jul 23/10 Page : 13

Printed in France © AIRBUS 2008 All rights reserved
SERVICE BULLETIN

Kit 251294D02R00

Manufacturers Empty Weight : +0.21 kg (+0.4629 lb)

Effect on Balance : +2.65 kgm (+19.167 lb.ft)

Kit 251294D03R00

Manufacturers Empty Weight : +0.38 kg (+0.8377 lb)

Effect on Balance : +5.39 kgm (+38.985 lb.ft)

Kit 251294D04R00

Manufacturers Empty Weight : +0.18 kg (+0.3968 lb)

Effect on Balance : +3.39 kgm (+24.519 lb.ft)

Kit 251294D05R00

Manufacturers Empty Weight : +0.29 kg (+0.6393 lb)

Effect on Balance : +7.06 kgm (+51.064 lb.ft)

Kit 251294D06R00

Manufacturers Empty Weight : +0.38 kg (+0.8377 lb)

Effect on Balance : +11.32 kgm (+81.877 lb.ft)

Kit 251294D07R00

Manufacturers Empty Weight : +0.18 kg (+0.3968 lb)

Effect on Balance : +5.90 kgm (+42.674 lb.ft)

Kit 251294D04R00 ADDITIONAL WORK 1

Manufacturers Empty Weight : +0.18 kg (+0.3968 lb)

Effect on Balance : +3.39 kgm (+24.519 lb.ft)

Kit 251294D02R00 and Kit 251294D05R00 ADDITIONAL WORK 2

Manufacturers Empty Weight : +0.50 kg (+1.1023 lb)

Effect on Balance : +9.71 kgm (+70.232 lb.ft)

Kit 251294D03R00 ADDITIONAL WORK 3

Manufacturers Empty Weight : +0.38 kg (+0.8377 lb)

Effect on Balance : +5.39 kgm (+38.985 lb.ft)

DATE : Mar 14/03 SERVICE BULLETIN No. : A320-25-1294

REVISION No. : 06 - Jul 23/10 Page : 14

Printed in France © AIRBUS 2008 All rights reserved
SERVICE BULLETIN

Kit 251294D06R00 ADDITIONAL WORK 3

Manufacturers Empty Weight : +0.38 kg (+0.8377 lb)

Effect on Balance : +11.32 kgm (+81.877 lb.ft)

I. ELECTRICAL LOAD DATA

Not changed

J. REFERENCES

Aircraft Maintenance Manual (AMM) : 12-34-24 25-52-44 52-30-00

Tool Equipment Manual (TEM) : 52-31-00

Consumable Material List (CML)

K. PUBLICATIONS AFFECTED

Illustrated Parts Catalog (IPC) : 25-52-02 25-52-04

L. INTERCHANGEABILITY/MIXABILITY

Not applicable

DATE : Mar 14/03 SERVICE BULLETIN No. : A320-25-1294

REVISION No. : 06 - Jul 23/10 Page : 15

Printed in France © AIRBUS 2008 All rights reserved
SERVICE BULLETIN

This Page Intentionally Left Blank

DATE : Mar 14/03 SERVICE BULLETIN No. : A320-25-1294

REVISION No. : 06 - Jul 23/10 Page : 16

Printed in France © AIRBUS 2008 All rights reserved
SERVICE BULLETIN

2. MATERIAL INFORMATION

A. MATERIAL - PRICE AND AVAILABILITY

(1) Material

This Service Bulletin is the subject of an AIRBUS monitored retrofit campaign.

(2) Price and Availability

Kit 251294D01R00

Cost : 833 US dollars

Availability : 150 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 the Kit(s) 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 the economic conditions

at the issue date of the Service Bulletin.

Kit 251294D02R00

Cost : 1665 US dollars

Availability : 150 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 the Kit(s) 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 the economic conditions

at the issue date of the Service Bulletin.

Kit 251294D03R00

Cost : 2656 US dollars

Availability : 150 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 the Kit(s) 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 the economic conditions

at the issue date of the Service Bulletin.

Kit 251294D04R00

Cost : 1200 US dollars

DATE : Mar 14/03 SERVICE BULLETIN No. : A320-25-1294

REVISION No. : 06 - Jul 23/10 Page : 17

Printed in France © AIRBUS 2008 All rights reserved
SERVICE BULLETIN

Availability : 150 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 the Kit(s) 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 the economic conditions

at the issue date of the Service Bulletin.

Kit 251294D05R00

Cost : 2064 US dollars

Availability : 150 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 the Kit(s) 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 the economic conditions

at the issue date of the Service Bulletin.

Kit 251294D06R00

Cost : 2656 US dollars

Availability : 150 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 the Kit(s) 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 the economic conditions

at the issue date of the Service Bulletin.

Kit 251294D07R00

Cost : 1200 US dollars

Availability : 150 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 the Kit(s) 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 the economic conditions

at the issue date of the Service Bulletin.

B. INDUSTRY SUPPORT INFORMATION

For the organisation of this retrofit, operators are kindly requested to contact AIRBUS retrofit

management department.

DATE : Mar 14/03 SERVICE BULLETIN No. : A320-25-1294

REVISION No. : 06 - Jul 23/10 Page : 18

Printed in France © AIRBUS 2008 All rights reserved
SERVICE BULLETIN

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 67 19 06 22

E-mail : monitored.retrofit@airbus.com

Fax : (33) 5 61 93 27 45

Modification of parts/equipment is at no charge for the Operator. AIRBUS will also credit the

man-hours indicated in this Service Bulletin at the Operator’s agreed in-house warranty labor rate

for claims received not later than 90 days after completion of the last affected aircraft of your fleet.

C. LIST OF COMPONENTS

Kit 251294D01R00

ITEM NEW PART No. QTY UM KEYWORD ITEM OLD PART No. INT INST DISP

1 D2557232700000 18 SPACER

Kit 251294D02R00

ITEM NEW PART No. QTY UM KEYWORD ITEM OLD PART No. INT INST DISP

1 D2557232700000 30 SPACER

Kit 251294D03R00

ITEM NEW PART No. QTY UM KEYWORD ITEM OLD PART No. INT INST DISP

1 D2557232700000 54 SPACER

Kit 251294D04R00

ITEM NEW PART No. QTY UM KEYWORD ITEM OLD PART No. INT INST DISP

1 D2557232700000 26 SPACER

Kit 251294D05R00

ITEM NEW PART No. QTY UM KEYWORD ITEM OLD PART No. INT INST DISP

1 D2557232700000 42 SPACER

Kit 251294D06R00

ITEM NEW PART No. QTY UM KEYWORD ITEM OLD PART No. INT INST DISP

1 D2557232700000 54 SPACER

Kit 251294D07R00

DATE : Mar 14/03 SERVICE BULLETIN No. : A320-25-1294

REVISION No. : 06 - Jul 23/10 Page : 19

Printed in France © AIRBUS 2008 All rights reserved
SERVICE BULLETIN

ITEM NEW PART No. QTY UM KEYWORD ITEM OLD PART No. INT INST DISP

1 D2557232700000 26 SPACER

D. LIST OF MATERIALS - OPERATOR SUPPLIED

(1) Consumable Materials

DESCRIPTION REFERENCE TO CML QTY PER A/C INST/DISP

MAT No.

Corrosion inhibitor Mat. No. 05-005D As required

Corrosion protective agent Mat. No. 15-005A As required

(2) Components

None

E. PARTS TO BE RE-IDENTIFIED BY THE OPERATOR

None

F. TOOLING - PRICE AND AVAILABILITY

To accomplish this Service Bulletin it is necessary to use these tools :

ITEM PART NUMBER QTY DESCRIPTION

98D52307515000 2 Safety lock - Actuator

G. SPECIAL TOOLS

None

DATE : Mar 14/03 SERVICE BULLETIN No. : A320-25-1294

REVISION No. : 06 - Jul 23/10 Page : 20

Printed in France © AIRBUS 2008 All rights reserved
SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS

A. GENERAL

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

IN THE REFERENCED PROCEDURES.

(1) Preparation

(a) Make sure that the aircraft is electrically grounded, refer to AMM 12-34-24, Page

block 201.

(b) Kit 251294D01R00 thru Kit 251294D03R00

1 Put the access platform in position below the FWD cargo-compartment door.

2 Open the FWD cargo-compartment door, refer to AMM 52-30-00, Page block

201.

3 Install the door-actuator safety lock to the FWD cargo-compartment door,

refer to TEM 52-31-00.

4 Remove the affected divider net for access.

(c) Kit 251294D04R00 thru Kit 251294D07R00

1 Put the access platform in position below the AFT cargo-compartment door.

2 Open the AFT cargo-compartment door, refer to AMM 52-30-00, Page block 201.

3 Install the door-actuator safety lock to the AFT cargo-compartment door, refer to

TEM 52-31-00.

(d) Open, safety and tag this (these) circuit breaker(s) :

- refer to AMM 25-52-44, Page block 401.

(e) Put the warning notices in position to tell the persons not to operate the cargo

loading systems.

(f) Remove the affected divider net(s) for access.

(2) Standard Practices

(a) Refer to the Consumable Material List (CML) for the specification of materials (Mat.

No.) that you must use to accomplish this Service Bulletin.

(b) Install the spacer assemblies with corrosion inhibitor (Mat. No. 05-005D) and

corrosion protective agent (Mat. No. 15-005A).

B. MODIFICATION

NOTE : Install the spacer assemblies with a 90 deg. point pliers.

DATE : Mar 14/03 SERVICE BULLETIN No. : A320-25-1294

REVISION No. : 06 - Jul 23/10 Page : 21

Printed in France © AIRBUS 2008 All rights reserved
SERVICE BULLETIN

(1) Kit 251294D01R00

Refer to Figure 1

(a) Install to the YZ-latches of the CLS in the FWD cargo-compartment :

18 spacer assembly D2557232700000 Item 1

(2) Kit 251294D02R00

Refer to Figure 2

(a) Install to the YZ-latches of the CLS in the FWD cargo-compartment :

30 spacer assembly D2557232700000 Item 1

(3) Kit 251294D03R00

Refer to Figure 3

(a) Install to the YZ-latches of the CLS in the FWD cargo-compartment :

54 spacer assembly D2557232700000 Item 1

(4) Kit 251294D04R00

Refer to Figure 1

(a) Install to the YZ-latches of the CLS in the AFT cargo-compartment :

26 spacer assembly D2557232700000 Item 1

(5) Kit 251294D05R00

Refer to Figure 2

(a) Install to the YZ-latches of the CLS in the AFT cargo-compartment :

42 spacer assembly D2557232700000 Item 1

(6) Kit 251294D06R00

Refer to Figure 3

(a) Install to the YZ-latches of the CLS in the AFT cargo-compartment :

54 spacer assembly D2557232700000 Item 1

(7) Kit 251294D07R00

Refer to Figure 4

(a) Install to the YZ-latches of the CLS in the AFT cargo-compartment :

26 spacer assembly D2557232700000 Item 1

(8) ADDITIONAL WORK 1 Kit 251294D04R00

NOTE : ADDITIONAL WORK 1 : with Kit D04 is required by this revision for aircraft

MSNs 0750, 0755, 0763, 0790, 0821, 0837, 0906, 0917, 0933, 0979 and 1034

modified by Revision 04 or any previous issue.

(a) Preparation

1 Put the access platform in position below the AFT cargo-compartment door.

2 Open the AFT cargo-compartment door, refer to AMM 52-30-00, Page block 201.

DATE : Mar 14/03 SERVICE BULLETIN No. : A320-25-1294

REVISION No. : 06 - Jul 23/10 Page : 22

Printed in France © AIRBUS 2008 All rights reserved
SERVICE BULLETIN

3 Install the door-actuator safety lock to the AFT cargo-compartment door, refer to

TEM 52-31-00.

(b) For material specifications (Mat. No.) given in this Service Bulletin, refer to

Consumable Material List (CML) .

(c) Install the spacer assemblies with corrosion inhibitor (Mat. No. 05-005D) and

corrosion protective agent (Mat. No. 15-005A).

(d) Modification

1 Kit 251294D04R00

Refer to Figure 1

a Install to the YZ-latches of the CLS in the AFT cargo-compartment :

26 spacer assembly D2557232700000 Item 1

(e) Test

None

(f) Close up

1 Make sure that the work areas are clean and clear of tools and other items

of equipment.

2 Install the divider net(s).

3 Remove the warnings notices.

4 Close, safety and tag this (these) circuit breaker(s) :

- refer to AMM 25-52-44, Page block 401.

5 Remove the door-actuator safety lock from the AFT cargo-compartment door,

refer to TEM 52-31-00.

6 Close the AFT cargo-compartment door, refer to AMM 52-30-00, Page block 201.

7 Remove the access platform from the AFT cargo-compartment door.

(9) ADDITIONAL WORK 2 Kit 251294D02R00 and Kit 251294D05R00

NOTE : ADDITIONAL WORK 2 :

- with Kit D02 is required by this revision for aircraft MSNs 1054, 1059, 1063,

1067, 1101, 1119, 1132, 1137, 1138, 1150, 1162, 1168, 1177, 1179, 1181,

1187, 1189, 1200 and 1206 modified by Revision 05 or any previous issue.

NOTE : ADDITIONAL WORK 2 :

- with Kit D05 is required by this revision for aircraft MSNs 0012-0014, 0016,

0365, 0371, 0566, 0573, 0582, 0590, 0594, 0607, 0611, 0617, 0619, 0648,

0650, 0658, 0669, 1864, 1871, 1873, 1874, 1879 and 1885 modified by

Revision 05 or any previous issue.

DATE : Mar 14/03 SERVICE BULLETIN No. : A320-25-1294

REVISION No. : 06 - Jul 23/10 Page : 23

Printed in France © AIRBUS 2008 All rights reserved
SERVICE BULLETIN

(a) Preparation

1 Put the access platforms in position below the FWD and AFT cargo-compartment

doors.

2 Open the FWD and AFT cargo-compartment doors, refer to AMM 52-30-00,

Page block 201.

3 Install the door-actuator safety locks to the FWD and AFT cargo-compartment

doors, refer to TEM 52-31-00.

(b) For material specifications (Mat. No.) given in this Service Bulletin, refer to

Consumable Material List (CML) .

(c) Install the spacer assemblies with corrosion inhibitor (Mat. No. 05-005D) and

corrosion protective agent (Mat. No. 15-005A).

(d) Modification

1 Kit 251294D02R00

Refer to Figure 2

a Install to the YZ-latches of the CLS in the FWD cargo-compartment :

30 spacer assembly D2557232700000 Item 1

2 Kit 251294D05R00

Refer to Figure 2

a Install to the YZ-latches of the CLS in the AFT cargo-compartment :

42 spacer assembly D2557232700000 Item 1

(e) Test

None

(f) Close up

1 Make sure that the work areas are clean and clear of tools and other items

of equipment.

2 Install the divider net(s).

3 Remove the warnings notices.

4 Close, safety and tag this (these) circuit breaker(s) :

- refer to AMM 25-52-44, Page block 401.

5 Remove the door-actuator safety locks from the FWD and AFT

cargo-compartment doors, refer to TEM 52-31-00.

6 Close the FWD and AFT cargo-compartment doors, refer to AMM 52-30-00,

Page block 201.

DATE : Mar 14/03 SERVICE BULLETIN No. : A320-25-1294

REVISION No. : 06 - Jul 23/10 Page : 24

Printed in France © AIRBUS 2008 All rights reserved
SERVICE BULLETIN

7 Remove the access platforms from the FWD and AFT cargo-compartment doors.

(10) ADDITIONAL WORK 3 Kit 251294D03R00 and Kit 251294D06R00

NOTE : ADDITIONAL WORK 3 :

- with Kit D03 is required by this revision for aircraft MSNs 0771, 0802, 0811,

0855, 0963, 0987, 1008 and 1798 modified by Revision 05 or any previous

issue.

NOTE : ADDITIONAL WORK 3 :

- with Kit D06 is required by this revision for aircraft MSNs 1276, 1333 and

1366 modified by Revision 05 or any previous issue.

(a) Preparation

1 Put the access platforms in position below the FWD and AFT cargo-compartment

doors.

2 Open the FWD and AFT cargo-compartment doors, refer to AMM 52-30-00,

Page block 201.

3 Install the door-actuator safety locks to the FWD and AFT cargo-compartment

doors, refer to TEM 52-31-00.

(b) For material specifications (Mat. No.) given in this Service Bulletin, refer to

Consumable Material List (CML) .

(c) Install the spacer assemblies with corrosion inhibitor (Mat. No. 05-005D) and

corrosion protective agent (Mat. No. 15-005A).

(d) Modification

1 Kit 251294D03R00

Refer to Figure 3

a Install to the YZ-latches of the CLS in the FWD cargo-compartment :

54 spacer assembly D2557232700000 Item 1

2 Kit 251294D06R00

Refer to Figure 3

a Install to the YZ-latches of the CLS in the AFT cargo-compartment :

54 spacer assembly D2557232700000 Item 1

(e) Test

None

(f) Close up

1 Make sure that the work areas are clean and clear of tools and other items

of equipment.

DATE : Mar 14/03 SERVICE BULLETIN No. : A320-25-1294

REVISION No. : 06 - Jul 23/10 Page : 25

Printed in France © AIRBUS 2008 All rights reserved
SERVICE BULLETIN

2 Install the divider net(s).

3 Remove the warnings notices.

4 Close, safety and tag this (these) circuit breaker(s) :

- refer to AMM 25-52-44, Page block 401.

5 Remove the door-actuator safety locks from the FWD and AFT

cargo-compartment doors, refer to TEM 52-31-00.

6 Close the FWD and AFT cargo-compartment doors, refer to AMM 52-30-00,

Page block 201.

7 Remove the access platforms from the FWD and AFT cargo-compartment doors.

C. TEST

None

D. CLOSE UP

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

(2) Install the divider net(s).

(3) Remove the warnings notices.

(4) Close, safety and tag this (these) circuit breaker(s) :

- refer to AMM 25-52-44, Page block 401.

(5) Kit 251294D01R00 thru Kit 251294D03R00

(a) Remove the door-actuator safety lock from the FWD cargo-compartment door,

refer to TEM 52-31-00.

(b) Close the FWD cargo-compartment door, refer to AMM 52-30-00, Page block 201.

(c) Remove the access platform from the FWD cargo-compartment door.

(6) Kit 251294D04R00 thru Kit 251294D07R00

(a) Remove the door-actuator safety lock from the AFT cargo-compartment door,

refer to TEM 52-31-00.

(b) Close the AFT cargo-compartment door, refer to AMM 52-30-00, Page block 201.

(c) Remove the access platform from the AFT cargo-compartment door.

E. DOCUMENTATION

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

DATE : Mar 14/03 SERVICE BULLETIN No. : A320-25-1294

REVISION No. : 06 - Jul 23/10 Page : 26

Printed in France © AIRBUS 2008 All rights reserved
SERVICE BULLETIN

Figure 1, Sheet 1

Installation of the Spacer Assemblies (Kit D01 and Kit D04)

DATE : Mar 14/03 SERVICE BULLETIN No. : A320-25-1294

REVISION No. : 06 - Jul 23/10 Page : 27

Printed in France © AIRBUS 2008 All rights reserved
SERVICE BULLETIN

Figure 2, Sheet 1

Installation of the Spacer Assemblies (Kit D02 and Kit D05)

DATE : Mar 14/03 SERVICE BULLETIN No. : A320-25-1294

REVISION No. : 06 - Jul 23/10 Page : 28

Printed in France © AIRBUS 2008 All rights reserved
SERVICE BULLETIN

Figure 3, Sheet 1

Installation of the Spacer Assemblies (Kit D03 and Kit D06)

DATE : Mar 14/03 SERVICE BULLETIN No. : A320-25-1294

REVISION No. : 06 - Jul 23/10 Page : 29

Printed in France © AIRBUS 2008 All rights reserved
SERVICE BULLETIN

Figure 4, Sheet 1

Installation of the Spacer Assemblies (Kit D07)

DATE : Mar 14/03 SERVICE BULLETIN No. : A320-25-1294

REVISION No. : 06 - Jul 23/10 Page : 30

Printed in France © AIRBUS 2008 All rights reserved
SERVICE BULLETIN

REPORTING SHEET

TITLE : EQUIPMENT/FURNISHINGS - SEMI AUTOMATIC CARGO LOADING - IMPROVE NET

ATTACHMENT POINTS OF FIXED YZ-LATCHES

MODIFICATION No. : 32316K7824, 32317K7825

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 embodiement:

.............................................................................................................................................................................

.............................................................................................................................................................................

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 : Advance data................................................................................... YES/NO

Or : Intermediate/Temporary 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: SEDCC1 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 : Mar 14/03 SERVICE BULLETIN No. : A320-25-1294

REVISION No. : 06 - Jul 23/10 Page : 1 of 1

Printed in France © AIRBUS 2008 All rights reserved
SERVICE BULLETIN

REPORTING QUALITY

TITLE : EQUIPMENT/FURNISHINGS - SEMI AUTOMATIC CARGO LOADING - IMPROVE NET

ATTACHMENT POINTS OF FIXED YZ-LATCHES

MODIFICATION No. : 32316K7824, 32317K7825

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 futher improve the quality

of our Service Bulletins.

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

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

-Quality rating of this SB 4 3 2 1

-Quality rating of the Accomplishment Instructions 4 3 2 1

-Quality rating of the Illustrations 4 3 2 1

-Is this SB easy to understand ? Y / N

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

description of the issue.

Planning Material Instructions

X Effectivity X Kit Content X Preparation

X Reason X List of Materials X Mod/Inspection

X Manpower Operator Supplied 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: SEMB Service Bulletins Management

FAX: (+33) 5 61 93 42 51

Or via your Resident Customer Support Office.

DATE : Mar 14/03 SERVICE BULLETIN No. : A320-25-1294

REVISION No. : 06 - Jul 23/10 Page : 1 of 1

Printed in France © AIRBUS 2008 All rights reserved