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** M A N DA T

O RY M A N DA T

O RY M A N DA TO RY M A N D A

TO RY **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 A D D I T I O N A L WO R K 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. R E A S O N 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 reservedSERVICE 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. C H A N G E S 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

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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. F I L I N G I N S T R U C T I O N S 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. H I S T O R Y O F P R E V I O U S R E V I S I O N S 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

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

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**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 M A N DA T

O RY M A N DA T

O RY M A N DA TO RY M A N DA TO RY **ATA SYSTEM : 25 TITLE : EQUIPMENT/FURNISHINGS - SEMI AUTOMATIC CARGO LOADING - IMPROVE NET**  **ATTACHMENT POINTS OF FIXED YZ-LATCHES MODIFICATION No. :**  32316K7824, 32317K7825 R E A S O N /D E S C R I PT I O N /O P E R A T I O N A L C O N S E Q U E N C E S 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

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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. **E F**  **F E**  **C T**  **I V**  **I T** **Y** 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. C O N C U R R E N T R E Q U I R E M E N T S None R E F E R E N C E S/ R E P E R C U S S I O N S TFU : None OEB : None AOT : None SIL : None LIFE LIMIT : None LINE MAINTENANCE AFFECTED : No OTHERS : None N A T U R E O F T H E WO R K 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 reservedSERVICE BULLETIN SUMMARY

EQUIPMENT : NO HARD : NO SOFT : NO OBRM : NO M A N P OW E R 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 reservedSERVICE 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**  M A T E R I A L I N F O R M A T I O N 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

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Kit 251294D07R00 Spacer assemblies A P P E N D I C E S None

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

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

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

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**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** M A N DA T

O RY M A N DA T

O RY M A N DA TO RY M A N DA TO RY **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. P L**  **A N**  **N I**  **N G**  **I N**  **F O**  **R M**  **A T**  **I O**  **N A. E**  **F F**  **E C**  **T I**  **V I**  **T Y**  (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

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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

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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

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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

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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

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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

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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 reservedSERVICE 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. C O**  **N C**  **U R**  **R E**  **N T**  **R E**  **Q U**  **I R**  **E M**  **E N**  **T S**  None **C. R E** **A S**  **O N**  (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 reservedSERVICE 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. D E**  **S C**  **R I**  **P T**  **I O**  **N** 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 reservedSERVICE 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 reservedSERVICE BULLETIN

**E. C O**  **M P**  **L I**  **A N**  **C E**  (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. A P**  **P R**  **O V**  **A L**  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. M A**  **N P**  **O W**  **E R**  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 reservedSERVICE 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 reservedSERVICE 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. W E**  **I G**  **H T**  **A N**  **D B** **A L** **A N**  **C E**  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 reservedSERVICE 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 reservedSERVICE 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. E L**  **E C**  **T R**  **I C**  **A L**  **L O** **A D**  **D A** 

**T**

**A** Not changed **J. R E**  **F E**  **R E**  **N C**  **E S**  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. P U**  **B L**  **I C**  **A T**  **I O**  **N S**  **A F**  **F E**  **C T**  **E D**  Illustrated Parts Catalog (IPC) : 25-52-02 25-52-04 **L. I N**  **T E**  **R C**  **H A**  **N G**  **E A**  **B I**  **L I**  **T Y**  **/ M**  **I X** **A B**  **I L**  **I T** **Y** 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 reservedSERVICE 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 reservedSERVICE BULLETIN

**2. M A**  **T E**  **R I**  **A L**  **I N**  **F O**  **R M**  **A T**  **I O**  **N A. M**  **A T**  **E R**  **I A**  **L -**  **P R**  **I C**  **E A**  **N D**  **A V** 

**A I**  **L A**  **B I**  **L I**  **T Y**  (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 reservedSERVICE 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. I N**  **D U**  **S T**  **R Y**  **S U**  **P P**  **O R** **T I**  **N F**  **O R**  **M A**  **T I**  **O N**  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 reservedSERVICE 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. L I**  **S T**  **O F**  **C O**  **M P**  **O N**  **E N**  **T S**  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 reservedSERVICE BULLETIN

ITEM NEW PART No. QTY UM KEYWORD ITEM OLD PART No. INT INST DISP 1 D2557232700000 26 SPACER **D. L I**  **S T**  **O F**  **M A**  **T E**  **R I**  **A L**  **S -**  **O P**  **E R**  **A T** **O R**  **S U**  **P P**  **L I**  **E D**  (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. P A**  **R T** **S T** **O B**  **E R**  **E -**  **I D**  **E N**  **T I**  **F I**  **E D**  **B Y**  **T H**  **E O**  **P E**  **R A**  **T O**  **R** None **F. T O**  **O L**  **I N**  **G -**  **P R**  **I C**  **E A**  **N D**  **A V** 

**A I**  **L A**  **B I**  **L I**  **T Y**  To accomplish this Service Bulletin it is necessary to use these tools : ITEM PART NUMBER QTY DESCRIPTION 98D52307515000 2 Safety lock - Actuator **G. S P**  **E C**  **I A**  **L T** **O O**  **L S**  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 reservedSERVICE BULLETIN

**3. A C**  **C O**  **M P**  **L I**  **S H**  **M E**  **N T**  **I N**  **S T**  **R U**  **C T**  **I O**  **N S**  **A. G E**  **N E**  **R A**  **L** 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. M O**  **D I**  **F I**  **C A**  **T I**  **O N**  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 reservedSERVICE 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 reservedSERVICE 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 reservedSERVICE 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 reservedSERVICE 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 reservedSERVICE 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. T E**  **S T**  None **D. C L**  **O S**  **E U**  **P** (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. D O**  **C U**  **M E**  **N T**  **A**

**T I**  **O N**  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 reservedSERVICE 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 reservedSERVICE 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 reservedSERVICE 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 reservedSERVICE 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 reservedSERVICE BULLETIN REPORTING SHEET

**TITLE : EQUIPMENT/FURNISHINGS - SEMI AUTOMATIC CARGO LOADING - IMPROVE NET ATTACHMENT POINTS OF FIXED YZ-LATCHES**  **MODIFICATION No. :** 32316K7824, 32317K7825 P l e a s e c o m p l ete t h e a p p ro p r i ate i te m (A o r B ) : A - SB W I L L B E embodied .................................................................. YES/NO (if NO please comment) If YES, aircraft concerned (as per SB effectivity by default) and planned dates (month/year) of embodiement:

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............................................................................................................................... .............................................. B - SB H AS B E E N embodied on aircraft: ............................................................................................................

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............................................................................................................................... .............................................. Operator comments:..............................................................................................................

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............................................................................................................................... .............................................. From Airline: ...................................................................................................................

..................................... Name/Title: ....................................................................................................................

...................................... Signature:..................... Date: ..................................................... I f o p e rat i o n a l d o c u m e n t at i o n i s affe cte d ( s e e Pa ra g ra p h 1

. K of t h i s S B ) : 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 I m p o rt a n t I n fo r m at i o n : 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. P l e a s e re t u r n t h i s c o m p l ete d s h e et 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 reservedSERVICE 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 C o m m e n ts :

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