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@A318/A319/A320/A321
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET AIRBUS
CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE T e l:( 3 3 )56 19 33 33 3 Telex : AIRBU 530526F F a x:( 3 3 )56 19 34 25 1 ATA SYSTEM: 92 TITLE: ELECTRIC AND ELECTRONIC COMMON INSTALLATION - ADD ANTI-
CHAFING PROTECTION AT RACEWAY GAPS MODIFICATION No.: 37504J2648 This page transmits Revision No.01 of Service Bulletin No.A320-92-1049
ADDITIONAL WORK **CONF ALL No additional work is required by this revision for aircraft modified by any previous issue.
REASON Revision 01 issued to delete all references to modification of the leading edge raceways (as no CF cables were installed in leading edge raceways), Revision 01 now only addresses the trailing edge and wing tip raceways. The Weight and Balance and Material Information is amended accordingly.
The opportunity is taken to update the aircraft effectivity.
CHANGES
SUMMARY
MODIFICATIONS Minor editorial or document structure change N
REASON/DESCRIPTION/OPERATIONAL
CONSEQUENCES Reference to leading edge raceways deleted N
GENERAL EVALUATION Minor editorial or document structure change N
MATERIAL PRICE INFORMATION Minor editorial or document structure change N Minor editorial or document structure change N Minor editorial or document structure change N
EFFECTIVITY Minor editorial or document structure change N
CONCURRENT REQUIREMENTS Minor editorial or document structure change N
REFERENCES / REPERCUSSIONS Minor editorial or document structure change N
NATURE OF THE WORK Minor editorial or document structure change N
MANPOWER Minor editorial or document structure change N Minor editorial or document structure change N Minor editorial or document structure change N DATE: Jul 23/07 SERVICE BULLETIN No.: A320-92-1049 REVISION No.: 01 - Nov 28/11 Page: 1 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET
APPENDICES Minor editorial or document structure change N Fig. A-USAAA Minor editorial or document structure change N Fig. A-USAAA Sheet 01 Minor editorial or document structure change N
PLANNING INFORMATION
EFFECTIVITY Effectivity updated N Configuration definition Minor editorial or document structure change N CONF 001 Minor editorial or document structure change N CONF 002 Minor editorial or document structure change N CONF 003 Minor editorial or document structure change N Material Effectivity Minor editorial or document structure change N Minor editorial or document structure change N Minor editorial or document structure change N Minor editorial or document structure change N
CONCURRENT REQUIREMENTS Minor editorial or document structure change N Minor editorial or document structure change N REASON Minor editorial or document structure change N History Minor editorial or document structure change N Objective/Action Reference to leading edge raceways deleted N Advantages Minor editorial or document structure change N Operational/Maintenance Consequences Minor editorial or document structure change N
DESCRIPTION Reference to leading edge raceways deleted N
COMPLIANCE Minor editorial or document structure change N Classification Minor editorial or document structure change N Accomplishment Timescale Minor editorial or document structure change N
APPROVAL Approval standard sentence updated N Minor editorial or document structure change N
MANPOWER Manhours adjusted to allow for deletion of leading edge raceways N Minor editorial or document structure change N Minor editorial or document structure change N Minor editorial or document structure change N
WEIGHT AND BALANCE Weight & Balance updated and standard sentence added N Minor editorial or document structure change N
ELECTRICAL LOAD DATA Minor editorial or document structure change N
REFERENCES WBM and SB reference added N Minor editorial or document structure change N Minor editorial or document structure change N Minor editorial or document structure change N
PUBLICATION AFFECTED Minor editorial or document structure change N DATE: Jul 23/07 SERVICE BULLETIN No.: A320-92-1049 REVISION No.: 01 - Nov 28/11 Page: 2 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET Minor editorial or document structure change N
INTERCHANGEABILITY/MIXABILITY Minor editorial or document structure change N SPARES Minor editorial or document structure change N
MATERIAL INFORMATION
MATERIAL - PRICE AND AVAILABILITY Minor editorial or document structure change N Procurement Addresses Address updated N Price and Availability Price and availability updated N
INDUSTRY SUPPORT INFORMATION Industry Support Information updated N
LIST OF COMPONENTS Kits B01 and B02 raised to revision 02 N Kit 921049B01R02 Minor editorial or document structure change N Kit 921049B02R02 Minor editorial or document structure change N
LIST OF MATERIALS - OPERATOR
SUPPLIED Minor editorial or document structure change N
PARTS TO BE RE-IDENTIFIED BY
OPERATOR Minor editorial or document structure change N
TOOLING Minor editorial or document structure change N
ACCOMPLISHMENT INSTRUCTIONS TASK 921049- 831-895-001-
MODIFICATION Installation of Protective Strips to leading edge deleted N Task associated data - 001 Minor editorial or document structure change N Task associated data - 002 Minor editorial or document structure change N Task associated data - 003 Minor editorial or document structure change N Subtask 921049-910-401-001 Standard Practice references added for tie-wraps and for wing panel zone location N Subtask 921049-839-401-001 Minor editorial or document structure change N Subtask 921049-910-401-001 Standard Practice references added for tie-wraps and for wing panel zone location N Subtask 921049-839-401-001 Minor editorial or document structure change N Subtask 921049-910-401-001 Standard Practice references added for tie-wraps and for wing panel zone location N Subtask 921049-839-401-001 Minor editorial or document structure change N Subtask 921049-941-401-001 Removal of leading edge access panels deleted N Subtask 921049-941-401-001 Removal of leading edge access panels deleted N Subtask 921049-941-401-002 Removal of leading edge access panels deleted N Subtask 921049-831-408-001 NOTE added to clarify the installation of the protective strip at positions where SB A320-24-1062 has been accomplished N Subtask 921049-831-409-001 Minor editorial or document structure change N Subtask 921049-831-410-001 NOTE added to clarify the installation of the protective strip at positions where SB A320-24-1062 has been accomplished N Subtask 921049-831-411-001 Minor editorial or document structure change N DATE: Jul 23/07 SERVICE BULLETIN No.: A320-92-1049 REVISION No.: 01 - Nov 28/11 Page: 3 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET Subtask 921049-831-414-001 NOTE added to clarify the installation of the protective strip at positions where SB A320-24-1062 has been accomplished N Subtask 921049-831-415-001 Minor editorial or document structure change N Subtask 921049-831-408-002 NOTE added to clarify the installation of the protective strip at positions where SB A320-24-1062 has been accomplished N Subtask 921049-831-409-002 Minor editorial or document structure change N Subtask 921049-831-410-002 NOTE added to clarify the installation of the protective strip at positions where SB A320-24-1062 has been accomplished N Subtask 921049-831-411-002 Minor editorial or document structure change N Subtask 921049-831-414-003 NOTE added to clarify the installation of the protective strip at positions where SB A320-24-1062 has been accomplished N Subtask 921049-831-415-003 Minor editorial or document structure change N Subtask 921049-831-408-002 NOTE added to clarify the installation of the protective strip at positions where SB A320-24-1062 has been accomplished N Subtask 921049-831-409-002 Minor editorial or document structure change N Subtask 921049-831-410-002 NOTE added to clarify the installation of the protective strip at positions where SB A320-24-1062 has been accomplished N Subtask 921049-831-411-002 Minor editorial or document structure change N Subtask 921049-942-401-001 Installation of leading edge access panels deleted N Subtask 921049-942-401-001 Installation of leading edge access panels deleted N Subtask 921049-942-401-002 Installation of leading edge access panels deleted N Fig. A-UBAAA Minor editorial or document structure change N Fig. A-UBAAA Sheet 01 Minor editorial or document structure change N Fig. A-UBAAB Minor editorial or document structure change N Fig. A-UBAAB Sheet 01 Minor editorial or document structure change N Fig. A-UBBAA Minor editorial or document structure change N Fig. A-UBBAA Sheet 01 Minor editorial or document structure change N Fig. A-UBBAA Sheet 02 Minor editorial or document structure change N Fig. A-UBBAA Sheet 03 Minor editorial or document structure change N Fig. A-UBBAA Sheet 04 Minor editorial or document structure change N Fig. A-UBBAA Sheet 05 Minor editorial or document structure change N Fig. A-UBBAB Minor editorial or document structure change N Fig. A-UBBAB Sheet 01 Minor editorial or document structure change N Fig. A-UBBAB Sheet 02 Minor editorial or document structure change N Fig. A-UBBAB Sheet 03 Minor editorial or document structure change N Fig. A-UBBAB Sheet 04 Minor editorial or document structure change N Fig. A-UBCAA Minor editorial or document structure change N DATE: Jul 23/07 SERVICE BULLETIN No.: A320-92-1049 REVISION No.: 01 - Nov 28/11 Page: 4 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET Fig. A-UBCAA Sheet 01 Minor editorial or document structure change N
FILLING INSTRUCTIONS This Service Bulletin has been generated electronically and is reissued as a complete document.
Replace the complete document.
Put this Revision Transmittal Sheet in front of the Service Bulletin.
HISTORY OF PREVIOUS REVISIONS No previous revision
REVISION SEQUENCE ORIGINAL: Jul 23/07 REVISION No. : 01 - Nov 28/11 DATE: Jul 23/07 SERVICE BULLETIN No.: A320-92-1049 REVISION No.: 01 - Nov 28/11 Page: 5 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET This Page Intentionally Left Blank DATE: Jul 23/07 SERVICE BULLETIN No.: A320-92-1049 REVISION No.: 01 - Nov 28/11 Page: 6 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321
SERVICE BULLETIN
SUMMARY AIRBUS
CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE T e l:( 3 3 )56 19 33 33 3 Telex : AIRBU 530526F F a x:( 3 3 )56 19 34 25 1 This summary is for information only and is not approved for modification of the aircraft.
ATA SYSTEM: 92 TITLE: ELECTRIC AND ELECTRONIC COMMON INSTALLATION - ADD ANTI-
CHAFING PROTECTION AT RACEWAY GAPS **CONF ALL
MODIFICATIONS
MODIFICATION CLASSIFICATION MAJOR None MINOR 37504J2648 NOTE : As per EASA IR 21, a minor change is one that has no appreciable effect on the mass, balance, structural strength, reliability, operational characteristics affecting the airworthiness of the product. All other changes are major changes.
REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES There have been in-service reports of Operators experiencing wire chafing in the raceways which resulted in short circuits. Investigation has established that the wire chafings, initiated at raceway gaps, were either due to maintenance operations or due to structure vibrations. The aircraft that are affected have CF type cable installed in the trailing edge (Pre Mod. No. 22626J0827).
Aircraft that are Post Mod. No. 22626J0827, have the more robust DK type of cable and are not affected.
There are two standards of raceway installed. Modification 20609J0261 introduced a raceway constructed of an extruded section with support brackets.
SIL 92-003 has been published to provide guidance for the inspection of electrical installations in the wing leading and trailing edges.
This Service Bulletin introduces Protective Strips to be installed at all raceway gaps and exits in the trailing edge and wing tip. This Service Bulletin is only applicable to aircraft that are Pre Mod. No.
22626J0827.
Accomplishment of this Service Bulletin will give increased protection to the cables at the raceway gaps and therefore prevent short circuits and potential arc tracking caused by damaged cables.
DATE: Jul 23/07 SERVICE BULLETIN No.: A320-92-1049 REVISION No.: 01 - Nov 28/11 Page: 1 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321
SERVICE BULLETIN
SUMMARY
GENERAL EVALUATION
EVALUATION TABLE
COMPLIANCE RECOMMENDED (1)
CANCELS INSPECTION SB NO
POTENTIAL AD NO
A/C OPERATION AFFECTED NO
RELIABILITY AFFECTED NO
PAX COMFORT AFFECTED NO
COST SAVING NO
ETOPS AFFECTED NO
STRUCTURAL LIFE EXTN NO
VENDOR SB INVOLVED NO NOTE
(1) : Service Bulletin recommended to be accomplished to prevent significant operational disruptions.
MATERIAL PRICE INFORMATION **CONF 001
MATERIAL PRICE INFORMATION TABLE
MATERIAL SET
QTY PER A/C
PRICE PER
A/C (USD)
MAIN PARTS Kit 921049B01R02 2 13,000.00 Protective Strips, Protective Sleeves, Tiewraps **CONF 002
MATERIAL PRICE INFORMATION TABLE
MATERIAL SET
QTY PER A/C
PRICE PER
A/C (USD)
MAIN PARTS Kit 921049B02R02 2 11,320.00 Protective Strips, Protective Sleeves, Tiewraps **CONF 003
MATERIAL PRICE INFORMATION TABLE
MATERIAL SET
QTY PER A/C
PRICE PER
A/C (USD)
MAIN PARTS Kit 921049B02R02 2 11,320.00 Protective Strips, Protective Sleeves, Tiewraps
EFFECTIVITY **CONF ALL This Service Bulletin is applicable to this (these) operator(s) :
83V 86Z AAF AAN ACA ADR AEU AFR AHY ANA ART AWW B2V BAW BGH BIE BTV C9G CTN CYP D2F DAL DLH ETJ F2I FHY
FPY HEJ IAC IBE IRA JAV JET KAC KPS LBT MLD MMA MSR
MXA SHY SKU SOL STZ SVR SWE TAM TAR UDC USA VLG XLF DATE: Jul 23/07 SERVICE BULLETIN No.: A320-92-1049 REVISION No.: 01 - Nov 28/11 Page: 2 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321
SERVICE BULLETIN
SUMMARY
CONCURRENT REQUIREMENTS The prior or simultaneous accomplishment of the Service Bulletin that follows is recommended:
Service Bulletin No. A320-24-1062 NOTE : Service Bulletin A320-24-1062 introduces additional protection to the ’S’ routes in the trailing edge raceways.
REFERENCES / REPERCUSSIONS TFU None OEB None AOT None SIL 92-003
LINE MAINTENANCE AFFECTED No
LIFE LIMIT None OTHER None
NATURE OF THE WORK
AIRCRAFT YES
EQUIPMENT NO HARD NO SOFT NO OBRM NO
MANPOWER **CONF 001 Task 921049-831-895-001: MODIFICATION
TOTAL MANHOURS
38.00
ELAPSED TIME (HOURS)
33.00 **CONF 002 Task 921049-831-895-001: MODIFICATION
TOTAL MANHOURS
31.50
ELAPSED TIME (HOURS)
24.00 **CONF 003 Task 921049-831-895-001: MODIFICATION
TOTAL MANHOURS
28.00
ELAPSED TIME (HOURS)
23.00
APPENDICES **CONF ALL None DATE: Jul 23/07 SERVICE BULLETIN No.: A320-92-1049 REVISION No.: 01 - Nov 28/11 Page: 3 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321
SERVICE BULLETIN
SUMMARY **CONF ALL
PROTECTIVE STRIP
FOR RACEWAY GAPS N_SB_921049_7_SAAA_01_00
FRONT SPAR
REAR SPAR ZONE 574/674
RACEWAY
TRAILING EDGE
RACEWAY RIB 27
RACEWAYS
LH WING SHOWN
RH WING SIMILAR Figure A-USAAA - Sheet 01 DATE: Jul 23/07 SERVICE BULLETIN No.: A320-92-1049 REVISION No.: 01 - Nov 28/11 Page: 4 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321
SERVICE BULLETIN AIRBUS
CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE T e l:( 3 3 )56 19 33 33 3 Telex : AIRBU 530526F F a x:( 3 3 )56 19 34 25 1 ATA SYSTEM: 92 TITLE: ELECTRIC AND ELECTRONIC COMMON INSTALLATION - ADD ANTI-
CHAFING PROTECTION AT RACEWAY GAPS MODIFICATION No.: 37504J2648 This document contains AIRBUS PROPRIETARY INFORMATION and shall at all times remain the property of AIRBUS; no intellectual property right or licence is granted by AIRBUS in connection with any information contained in it. It is delivered on the express condition that said document and the information contained in it shall be treated as confidential, shall not be used for any purpose other than that for which it is hereby delivered. It shall not be disclosed in whole or in part to third parties and shall not be duplicated in any manner (except for the purposes of performing the tasks described hereunder and provided that any recipient of such document shall comply with the conditions herein), without AIRBUS prior written consent.
1. PLANNING INFORMATION **CONF ALL A. EFFECTIVITY
(1) Models 320-211 320-212 320-231
(2) Effectivity by MSN 0029 0039 0042-0059 0061-0078 0080-0090 0093-0097 0099 0102-0104 0109-0128 0132 0135-0155 0157-0162 0164-0176 0178-0179 0181-0183 0185-0192 0194-0224 0226-0237 0239-0270 0272-0279 0281-0303 0305-0312 0314 0316-0337 0339
(3) Effectivity by Operator The Operator/MSN relationship is provided for information only and is correct at the time of issue in accordance with the information available to AIRBUS. Any future changes resulting from transfer of an aircraft from one operator to another will not be reflected in this list unless the Service Bulletin is revised for another reason.
OPERATOR MSN 83V 0226 86Z 0164 AAF 0244 AAN 0299 DATE: Jul 23/07 SERVICE BULLETIN No.: A320-92-1049 REVISION No.: 01 - Nov 28/11 Page: 1 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321
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 ADR 0043 AEU 0136 AFR 0044 0061 0062 0063 0102 0115 0144 0145 0155 0186 0187 0214 0227 0228 0236 0237 0239 0270 0278 0285 0286 0287 0337 AHY 0331 ANA 0139 0151 0167 0170 0196 0212 0219 0245 0300 0328 ART 0142 0283 0310 0311 0333 AWW 0229 B2V 0185 0191 BAW 0039 0042 0103 0109 0120 BGH 0221 0294 0305 BIE 0293 BTV 0168 C9G 0246 CTN 0258 CYP 0256 D2F 0211 0243 0251 0326 DAL 0118 0121 0125 0152 0153 0160 0171 0192 0197 0206 0208 0213 0262 0263 0272 0273 0281 0282 0297 0298 0306 0307 0318 0319 0329 0339 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 ETJ 0325 F2I 0128 0188 FHY 0132 0288 FPY 0112 HEJ 0087 0088 IAC 0045 0046 0047 0048 0049 0050 0051 0056 0057 0058 0074 0075 0080 0089 0090 0095 0096 0097 0247 0257 0308 0314 0327 0336 IBE 0176 0207 0223 0274 IRA 0303 0312 JAV 0029 JET 0204 0215 KAC 0181 0182 0195 KPS 0234 LBT 0222 0301 MLD 0249 MMA 0113 0114 0295 0316 MSR 0165 0166 0178 0194 0198 0322 MXA 0252 0259 0260 0261 0275 0276 0291 0292 0296 0320 0321 0332 SHY 0138 0148 SKU 0179 SOL 0302 DATE: Jul 23/07 SERVICE BULLETIN No.: A320-92-1049 REVISION No.: 01 - Nov 28/11 Page: 2 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.