# @A340 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



# MANDATORYMANDATORYMANDATORY
ATA SYSTEM: 21 

### TITLE: AIR CONDITIONING - GENERAL - INSTALL NEW BONDING BRACKETS AFTER FRAME64 LH BETWEEN P33-P34 MODIFICATION No.: 201500D50418 This page transmits Revision No.03 of Service Bulletin No.A340-21-4152 ADDITIONAL WORK **CONF ALL Additional work is required for aircraft which have been modified by revision 00 or revision 01. Additional work is not required for aircraft which have been modified by revision 02. REASON Revision No. 03 issued to update the reason, accomplishment instruction and illustration. CHANGES SUMMARY REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES REASON UPDATED R EFFECTIVITY OPERATOR LIST UPDATED R Fig. A-GSAAA Fig. A-GSAAA Sheet 01 SHEET UPDATED R PLANNING INFORMATION EFFECTIVITY EFFECTIVITY RELATED INFORMATION UPDATED R Configuration definition CONF 001 CONFIGURATION DEFINITION UPDATED R REASON Objective/Action OBJECTIVE/ACTION UPDATED R ACCOMPLISHMENT INSTRUCTIONS TASK 214152- 831-848-001-Modification Subtask 214152-831-201-001 SUBTASK SOLUTION UPDATED R Fig. A-GBAAA DATE: Sep 27/11 SERVICE BULLETIN No.: A340-21-4152 REVISION No.: 03 - Dec 07/12 Page: 1 6

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# @A340 SERVICE BULLETIN REVISION TRANSMITTAL SHEET Fig. A-GBAAA Sheet 01 SHEET UPDATED R Fig. A-GBBAA Fig. A-GBBAA Sheet 01 SHEET UPDATED R Fig. A-GBCAA Fig. A-GBCAA Sheet 01 SHEET UPDATED R FILLING INSTRUCTIONS This Service Bulletin has been generated electronically and is reissued as a complete document. Replace the complete document. Put this Revision Transmittal Sheet in front of the Service Bulletin. HISTORY OF PREVIOUS REVISIONS Revision No. 01 issued to update the effectivity, the Industry support paragraph, add that damaged insulations must be repaired and update the Kit revision indicator. Revision No. 02 issued to add the replacement of the bonding lead from waste water pipe to the new bonding bracket and to improve the position of the bonding clamp at waste water pipe. REVISION SEQUENCE ORIGINAL: Sep 27/11 REVISION No. : 01 - Nov 21/11 REVISION No. : 02 - Mar 29/12 REVISION No. : 03 - Dec 07/12

DATE: Sep 27/11 SERVICE BULLETIN No.: A340-21-4152 REVISION No.: 03 - Dec 07/12 Page: 2 6

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# @A340 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. 

# MANDATORYMANDATORYMANDATORY
ATA SYSTEM: 21 

### TITLE: AIR CONDITIONING - GENERAL - INSTALL NEW BONDING BRACKETS AFTER FRAME64 LH BETWEEN P33-P34 **CONF ALL MODIFICATIONS MODIFICATION CLASSIFICATION MAJOR None MINOR 201500D50418 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 Maintenance experience has shown that the bonding lead from the isolation valve 283HN to Frame (FR)64, between Stringer (STGR)33 and STGR34, is too close to the electrical harness 5871VB and chafing might be possible. The chafing might lead to a non-closure of the isolation valve 283HN through a short circuit of the isolation valve by contact of the chafed bonding lead and wire harness 5871VB. This Service Bulletin details the installation of a new bonding bracket and new bonding lead at STGR34, between FR64 and FR65. The accomplishment of this Service Bulletin will avoid possible chafing between the bonding lead and the electrical harness 5871VB and ensure the correct control of the isolation valve 283HN. GENERAL EVALUATION EVALUATION TABLE COMPLIANCE MANDATORY (1) CANCELS INSPECTION SB NO POTENTIAL AD YES A/C OPERATION AFFECTED NO RELIABILITY AFFECTED YES PAX COMFORT AFFECTED NO COST SAVING NO LROPS AFFECTED NO DATE: Sep 27/11 SERVICE BULLETIN No.: A340-21-4152 REVISION No.: 03 - Dec 07/12 Page: 1 6

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# @A340 SERVICE BULLETIN SUMMARY EVALUATION TABLE STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED NO NOTE (1): Service Bulletin must be accomplished. MATERIAL PRICE INFORMATION MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Kit 214152D01R03 1 33.00 Bracket, Rivet, Screw, Washer Kit 214152D02R01 1 33.00 TOTAL 66.00 EFFECTIVITY This Service Bulletin is applicable to this (these) operator(s) :

47W 56W 83V AAW ABQ AFR AIB ALK ARG CAH CAL CCA CES CPA DGA DLH FIN GAF GFA HFY IBE IRC KAC KNE LAN M3R MAU MDG MSR NMB PAL QAF RJA S3R SAA SAS SFB SLM SVW SWR TAP THT THY UAE VCV VIR XAX CONCURRENT REQUIREMENTS None REFERENCES / REPERCUSSIONS TFU None OEB None AOT None SIL None LINE MAINTENANCE AFFECTED No LIFE LIMIT None OTHER None NATURE OF THE WORK AIRCRAFT YES EQUIPMENT NO HARD NO SOFT NO OBRM NO MANPOWER Task 214152-831-848-001: Modification TOTAL MANHOURS 3.25 ELAPSED TIME (HOURS) 3.25

DATE: Sep 27/11 SERVICE BULLETIN No.: A340-21-4152 REVISION No.: 03 - Dec 07/12 Page: 2 6

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# @A340 SERVICE BULLETIN SUMMARY Task 214152-831-849-001: Modification - ADDITIONAL WORK TOTAL MANHOURS 2.50 ELAPSED TIME (HOURS) 2.50 APPENDICES None

DATE: Sep 27/11 SERVICE BULLETIN No.: A340-21-4152 REVISION No.: 03 - Dec 07/12 Page: 3 6

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# @A340 SERVICE BULLETIN SUMMARY

**CONF ALL



### B



## A 283HN

FR73 FR62

STGR34 FR64 FR63

FR62

STGR33 STGR32



## B 283HN 

### A Z160

NEW BONDING BRACKET

F_SB_214152_6_SAAA_01_02 Figure A-GSAAA - Sheet 01
DATE: Sep 27/11 SERVICE BULLETIN No.: A340-21-4152 REVISION No.: 03 - Dec 07/12 Page: 4 6

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# @A340 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



# MANDATORYMANDATORYMANDATORY
ATA SYSTEM: 21 

### TITLE: AIR CONDITIONING - GENERAL - INSTALL NEW BONDING BRACKETS AFTER FRAME64 LH BETWEEN P33-P34 MODIFICATION No.: 201500D50418 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 340-211 340-212 340-213 340-311 340-312 340-313 (2) Effectivity by MSN 0002-0006 0009 0011 0013-0015 0018-0029 0031-0035 0038 0041 0043-0044 0046-0049 0051-0053 0056-0058 0061 0063 0074-0076 0078-0081 0084-0085 0088-0091 0093-0094 0101 0104 0114-0115 0117 0123 0125-0126 0128-0129 0131 0133-0137 0139 0141-0142 0145-0147 0149-0152 0154 0156-0161 0163-0164 0166-0170 0173-0176 0178-0180 0182 0185-0187 0190 0192-0194 0196-0197 0199 0201-0202 0204 0207-0208 0210 0212-0218 0220-0221 0225 0227-0228 0233 0235-0237 0239 0242-0243 0245-0246 0252 0257 0260 0263-0264 0268 0270 0273-0274 0278 0280 0282 0292 0297 0302 0304 0307 0310 0318-0319 0321 0325 0327 0329 0331-0332 0335 0347 0352 0354-0355 0359 0363 0367 0373-0374 0377-0379 0381 0385 0387 0390 0395 0399 0402 0406 0411 0413-0415 0424 0429-0430 0433-0435 0438 0442 0446-0447 0450 0459 0467 0470 0474 0483 0528 0538 0541 0545-0546 0554 0556 0559 0561-0562 0585 0598 0668 0793 0800 0955

DATE: Sep 27/11 SERVICE BULLETIN No.: A340-21-4152 REVISION No.: 03 - Dec 07/12 Page: 1 6

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# @A340 SERVICE BULLETIN (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 47W 0009 56W 0003 0011 0013 0015 0018 0019 0021 83V 0235 0239 0280 0292 AAW 0151 ABQ 0216 0257 AFR 0029 0078 0084 0186 0207 0237 0245 0246 0260 0307 0310 0377 0399 AIB 0332 ALK 0032 0033 0034 0367 0374 0381 ARG 0048 0063 0074 0080 0085 0093 0094 0123 0126 0128 0373 CAH 0020 0056 CAL 0402 0406 0411 0415 0433 0541 CCA 0192 0199 0201 0242 0243 0264 CES 0129 0131 0141 0161 0182 CPA 0136 0137 0142 0147 0157 0160 0208 0218 0220 0227 0228 DGA 0075 0081 DLH 0024 0027 0028 0035 0052 0053 0135 0158 0213 0233 0252 0297 0304 0321 0325 0327 0335 0347 0352 0354 0379 0390 0434 0447 FIN 0058 0168 0174 GAF 0274 0355 GFA 0212 0215 0282 0554 HFY 0117 0133 IBE 0005 0088 0125 0134 0145 0146 0170 0193 0217 0221 0318 0329 0387 0414 0459 0474 0483 IRC 0002 KAC 0089 0090 0101 0104 KNE 0004 LAN 0167 0359 0363 0429 0442 M3R 0061 MAU 0076 0152 0194 0268 0793 0800 MDG 0210 0319 MSR 0156 0159 0178 NMB 0047 0051 PAL 0173 0176 0187 0196 QAF 0026 0528 RJA 0014 0022 0038 0043 S3R 0204 SAA 0006 0197 0378 SAS 0413 0424 0430 0435 0450 0467 0470 SFB 0046 DATE: Sep 27/11 SERVICE BULLETIN No.: A340-21-4152 REVISION No.: 03 - Dec 07/12 Page: 2 6

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# @A340 SERVICE BULLETIN

OPERATOR MSN SLM 0049 SVW 0955 SWR 0150 0154 0169 0175 0179 0263 0538 0545 0546 0556 0559 0561 0562 0585 0598 TAP 0041 0044 0079 0091 THT 0385 0395 0438 0446 0668 THY 0023 0025 0057 0115 0180 0270 0331 UAE 0139 0149 0163 0166 0185 0190 0202 0236 VCV 0031 0302 VIR 0114 0164 0214 0225 XAX 0273 0278 (4) Configuration by MSN MSN CONFIGURATION 0002 0003 0004 0005 0006 0009 0011 0013 0014 0015 0018 0019 0020 0021 0022 0023 0024 0025 0026 0027 0028 0029 0031 0032 0033 0034 0035 0038 0041 0043 0044 0046 0047 0048 0049 0051 0052 0053 0056 0057 0058 0061 0063 0074 0075 0076 0078 0079 0080 0081 0084 0085 0088 0089 0090 0091 0093 0094 0101 0104 0114 0115 0117 0123 0125 0126 0128 0129 0131 0133 0134 0135 0136 0137 0139 0141 0142 0145 0146 0147 0149 0150 0151 0152 0154 0156 0157 0158 0159 0160 0161 0163 0164 0166 0167 0168 0169 0170 0173 0174 0175 0176 0178 0179 0180 0182 0185 0186 0187 0190 0192 0193 0194 0196 0197 0199 0201 0202 0204 0207 0208 0210 0212 0213 0214 0215 0216 0217 0218 0220 0221 0225 0227 0228 0233 0235 0236 0237 0239 0242 0243 0245 0246 0252 0257 0260 0263 0264 0268 0270 0273 0274 0278 0280 0282 0292 0297 0302 0304 0307 0310 0318 0319 0321 0325 0327 0329 0331 0332 0335 0347 0352 0354 0355 0359 0363 0367 0373 0374 0377 0378 0379 0381 0385 0387 0390 0395 0399 0402 0406 0411 0413 0414 0415 0424 0429 0430 0433 0434 0435 0438 0442 0446 0447 0450 0459 0467 0470 0474 0483 0528 0538 0541 0545 0546 0554 0556 0559 0561 0562 0585 0598 0668 0793 0800 0955 001

(5) Configuration definition **CONF 001 Config. 001 is valid for all the aircraft given in the effectivity of this Service Bulletin as a standard configuration. (6) Material Effectivity MATERIAL QTY PER A/C SEE NOTES Consumable CMLD01 1 Kit 214152D01R03 1 Kit 214152D02R01 1
DATE: Sep 27/11 SERVICE BULLETIN No.: A340-21-4152 REVISION No.: 03 - Dec 07/12 Page: 3 6

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# @A340 SERVICE BULLETIN
B. CONCURRENT REQUIREMENTS None C. REASON (1) History Maintenance experience has shown that the bonding lead from the isolation valve 283HN to Frame (FR)64, between Stringer (STGR)33 and STGR34, is too close to the electrical harness 5871VB and chafing might be possible. The chafing might lead to a non-closure of the isolation valve 283HN through a short circuit of the isolation valve by contact of the chafed bonding lead and wire harness 5871VB. (2) Objective/Action This Service Bulletin details the installation of a new bonding bracket and new bonding lead at STGR34, between FR64 and FR65. (3) Advantages The accomplishment of this Service Bulletin will avoid possible chafing between the bonding lead and the electrical harness 5871VB and ensure the correct control of the isolation valve 283HN. (4) Operational/Maintenance Consequences None D. DESCRIPTION To accomplish this Service Bulletin it is necessary to : Task 214152-831-848-001: Modification (1) Modify the bonding lead installation Task 214152-831-849-001: Modification - ADDITIONAL WORK (1) Modify the bonding lead installation E. COMPLIANCE (1) Classification MANDATORY: Service Bulletin must be accomplished.

DATE: Sep 27/11 SERVICE BULLETIN No.: A340-21-4152 REVISION No.: 03 - Dec 07/12 Page: 4 6

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# @A340 SERVICE BULLETIN (2) Accomplishment Timescale This Service Bulletin has been classified Mandatory. It is expected that an Airworthiness Directive (AD) published by the European Aviation Safety Agency (EASA) will be issued to confirm this classification. The accomplishment timescale, which has not yet been defined, will be given in the AD. F. APPROVAL The technical content of this document is approved under the authority of Design Organisation Approval No. EASA.21J.031. If an aircraft listed in the effectivity has a modification or repair embodied that is not of AIRBUS origin, and which affects the content of this Service Bulletin, the operator is responsible for obtaining approval by its airworthiness authority for any adaptation necessary before incorporation of the Service Bulletin. G. MANPOWER The manpower estimates given in this Service Bulletin are based on the direct labor cost to do the work. These estimates assume that the work will be done by experienced personnel, and may need to be revised upwards to suit operator’s circumstances. The estimates do not include the time to prepare, plan or inspect the work. Manufacture and procurement of parts and tools, drying times for paints, sealants, etc., and general administration work are also not included. Task 214152-831-848-001: Modification Get Access 1.00 On Aircraft Modify the bonding lead installation 1.00 Tests 0.25 Close-Up 1.00 TOTAL MANHOURS 3.25 ELAPSED TIME (HOURS) 3.25 Task 214152-831-849-001: Modification - ADDITIONAL WORK Get Access 1.00 On Aircraft Modify the bonding lead installation 0.25 Tests 0.25 Close-Up 1.00 TOTAL MANHOURS 2.50 ELAPSED TIME (HOURS) 2.50 H. WEIGHT AND BALANCE Not Changed I. ELECTRICAL LOAD DATA Not Changed DATE: Sep 27/11 SERVICE BULLETIN No.: A340-21-4152 REVISION No.: 03 - Dec 07/12 Page: 5 6

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# @A340 SERVICE BULLETIN
J. REFERENCES

Aircraft Maintenance Manual (AMM) 06-20-00 06-30-00 06-31-53 06-41-53 12-34-24 20-28-00 25-53-00 25-80-00 52-30-00 Elec. Std. Practices Manual (ESPM) 20-51-20 20-51-21 20-55-00 Standards Manual (SM) Structural Repair Manual (SRM) 51-42-11 51-44-00 51-44-11 K. PUBLICATION AFFECTED

Illustrated Parts Catalog (IPC) 21-28-04 L. INTERCHANGEABILITY/MIXABILITY Not Applicable M. SPARES None

DATE: Sep 27/11 SERVICE BULLETIN No.: A340-21-4152 REVISION No.: 03 - Dec 07/12 Page: 6 6

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# @A340 SERVICE BULLETIN
2. MATERIAL INFORMATION **CONF ALL A. MATERIAL - PRICE AND AVAILABILITY (1) Procurement Addresses Kit 214152D01R03 Kit 214152D02R01 Customers with aircraft shown in the effectivity of this Service Bulletin should send a purchase order to AIRBUS. Quote the number of this Service Bulletin. The address is: Airbus Material, Logistic and Suppliers Weg beim Jaeger 150 D-22335 Hamburg Germany For ordering by internet: http//spares.airbus.com For ordering modification kits by fax: +49 40 50 76 25 90 For ordering by E-mail: airbus.kit@airbus.com (2) Price and Availability

Kit 214152D01R03 Cost 33.00 USD Availability 90 calendar days from receipt of order The Kit availability given above is the standard lead time from the date of your purchase order. If you require Kits before this time, please include a retrofit planning schedule with your order so that we can try to comply with your requirements. The sales terms (costs and availability) are estimated in relation to economic conditions at the issue date of the Service Bulletin. Kit 214152D02R01 Cost 33.00 USD Availability 90 calendar days from receipt of order The Kit availability given above is the standard lead time from the date of your purchase order. If you require Kits before this time, please include a retrofit planning schedule with your order so that we can try to comply with your requirements. The sales terms (costs and availability) are estimated in relation to economic conditions at the issue date of the Service Bulletin. B. INDUSTRY SUPPORT INFORMATION AIRBUS will share the costs of accomplishment of this Service Bulletin by providing the kits at no charge for orders placed before 31. Dec. 2014.

DATE: Sep 27/11 SERVICE BULLETIN No.: A340-21-4152 REVISION No.: 03 - Dec 07/12 Page: 7 6

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# @A340 SERVICE BULLETIN For the accomplishment of this Service Bulletin before 31. Dec. 2014, AIRBUS will credit the manhours indicated in this Service Bulletin at the 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 214152D01R03 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 6 EN6081D4-04 2 RIVET 7 ABS1577A05 1 BRACKET 8 EN6081D4-05 3 RIVET NOTE: If you find part numbers of hardware components in the related kit(s) which you cannot identify in the LIST OF COMPONENTS of this Service Bulletin, refer to Standards Manual (SM). The SM will give you the correct part number to part number relationship. Kit 214152D02R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 1 NAS1801-3-7 2 SCREW 2 MS21042-3 1 NUT 3 NAS1149C0332R 2 WASHER 9 E0090-10-200NN 1 LEAD (10) E0091-10-160NN NOTE: If you find part numbers of hardware components in the related kit(s) which you cannot identify in the LIST OF COMPONENTS of this Service Bulletin, refer to Standards Manual (SM). The SM will give you the correct part number to part number relationship. D. LIST OF MATERIALS - OPERATOR SUPPLIED (1) Consumable Materials Consumable CMLD01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Cleaning Solvent 11-016 As required Lint-Free Cotton Cloth 19-003 As required (2) Components None (3) Equipment None DATE: Sep 27/11 SERVICE BULLETIN No.: A340-21-4152 REVISION No.: 03 - Dec 07/12 Page: 8 6

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# @A340 SERVICE BULLETIN
E. PARTS TO BE RE-IDENTIFIED BY OPERATOR None F. TOOLING None

DATE: Sep 27/11 SERVICE BULLETIN No.: A340-21-4152 REVISION No.: 03 - Dec 07/12 Page: 9 6

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# @A340 SERVICE BULLETIN

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# @A340 SERVICE BULLETIN
3. ACCOMPLISHMENT INSTRUCTIONS Task 214152-831-848-001 - Modification WARNING: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONS INCLUDED IN THE REFERENCED PROCEDURES. CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY AND MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENANCE WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING, COMPONENTS AND THE WORK AREA AS CLEAN AS POSSIBLE. TO DO THIS: PUT PROTECTION, SUCH AS PLASTIC SHEETING, CLOTHS, ETC; AS NECESSARY ON WIRING AND COMPONENTS. REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND OTHER CONTAMINATION. THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION. IN CASE OF CONTAMINATION REFER TO ESPM 20-55-00. Task Associated Data Zone 160 Manpower TOTAL MANHOURS 3.25 ELAPSED TIME (HOURS) 3.25 A. GENERAL (1) Subtask 214152-910-201-001 - Standard Practices Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-20-00, Page Block 001 06-30-00, Page Block 001 06-31-53, Page Block 001 06-41-53, Page Block 001 Structural Repair Manual (SRM) 51-44-00 (a) For identification of zones (Refer to AMM 06-20-00, Page Block 001). (b) For Stringer (STGR) identification (Refer to AMM 06-30-00, Page Block 001). (c) For Frame (FR) identification (Refer to AMM 06-31-53, Page Block 001). DATE: Sep 27/11 SERVICE BULLETIN No.: A340-21-4152 REVISION No.: 03 - Dec 07/12 Page: 11 6

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# @A340 SERVICE BULLETIN (d) For sidewall panel identification (Refer to AMM 06-41-53, Page Block 001). (e) For fastener hole diameter and drill and deburr data (Refer to SRM 51-44-00). (2) Subtask 214152-839-201-001 - Administrative Manpower Resources Skills NON SPECIFIC Write in the applicable aircraft records that you done all the work given in this Service Bulletin. B. PREPARATION (1) Subtask 214152-941-201-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802 Task 25-53-00-000-801 Task 25-80-00-000-801 Task 52-30-00-010-801 Fig. A-GBAAA Modify the bonding lead installation Sheet 01 Sheet 02 Fig. A-GBBAA Modify the bonding lead installation Sheet 01 Sheet 02 (a) Make sure that the aircraft is electrically grounded (Refer to AMM Task 12-34-24-860-802). (b) Put an access platform in position at the Aft cargo-compartment door. (c) Open the Aft cargo-compartment door (Refer to AMM Task 52-30-00-010-801). (d) If a Cargo Loading System (CLS) is installed, put a warning notice in position on the control panel to tell persons not to operate the CLS. (e) Remove the access panel 151TW (Refer to AMM Task 25-53-00-000-801). (f) In the work area, Zone 160, as shown onFig. A-GBAAA Sheet 01 and Fig. A-GBBAA Sheet 01, remove the insulation blankets (Refer to AMM Task 25-80-00-000-801). C. PROCEDURE (1) Subtask 214152-831-201-001 - Modify the bonding lead installation Work Zones and Access Panels Zone Access/Work location 160 DATE: Sep 27/11 SERVICE BULLETIN No.: A340-21-4152 REVISION No.: 03 - Dec 07/12 Page: 12 6

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# @A340 SERVICE BULLETIN
Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills AIRFRAME Material necessary to do the job Kit 214152D01R03 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 6 EN6081D4-04 2 RIVET 7 ABS1577A05 1 BRACKET 8 EN6081D4-05 3 RIVET Kit 214152D02R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 NAS1801-3-7 2 SCREW 2 MS21042-3 1 NUT 3 NAS1149C0332R 2 WASHER 9 E0090-10-200NN 1 LEAD Consumable CMLD01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Cleaning Solvent 11-016 As required Lint-Free Cotton Cloth 19-003 As required References Aircraft Maintenance Manual (AMM) Task 20-28-00-912-801 25-80-00, Page Block 801 Elec. Std. Practices Manual (ESPM) 20-51-20 20-51-21 Structural Repair Manual (SRM) 51-42-11 51-44-11 Fig. A-GBAAA Modify the bonding lead installation Sheet 01 Sheet 02 Fig. A-GBBAA Modify the bonding lead installation Sheet 01 Sheet 02 (a) As shown on Fig. A-GBAAA Sheet 01 and Fig. A-GBAAA Sheet 02, View C, remove: 1 Nut Item (2) Discard 1 Washer Item (3) Discard
DATE: Sep 27/11 SERVICE BULLETIN No.: A340-21-4152 REVISION No.: 03 - Dec 07/12 Page: 13 6

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# @A340 SERVICE BULLETIN
1 Screw Item (1) Discard and disconnect: 1 Bonding Lead Item (4) Retain 1 Bonding Lead E0091-10-160NN Item (10) Discard (b) As shown on Fig. A-GBAAA Sheet 01 and Fig. A-GBAAA Sheet 02, View E, remove: 1 Nut Item (2) Discard 1 Washer Item (3) Discard 1 Screw Item (1) Discard 1 Bonding Lead E0091-10-160NN Item (10) Discard (c) As shown on Fig. A-GBAAA Sheet 02, View C, at FR64, remove: 2 Rivet Item (6) Discard 1 Bracket Item (5) Discard (d) As shown on Fig. A-GBAAA Sheet 02, View D, close the holes with: 2 Rivet EN6081D4-04 Item 6 (Refer to SRM 51-42-11). (e) Install the new bracket at STGR34, between FR64 and FR65 LH, as shown on Fig. A-GBBAA Sheet 01 and Fig. A-GBBAA Sheet 02, View E. 1 At STGR34 make marks to show the position of the holes. 2 Drill the pilot hole at STGR34 with a diameter of 2.4mm (0.094inch) (Refer to SRM 51-44-11). 3 Temporarily install: 1 Bracket ABS1577A05 Item 7 NOTE: Use the new hole at STGR34. 4 Transfer drill the holes from the bracket, item 7, to STGR34 with a diameter of 3.3mm (0.13inch) (Refer to SRM 51-44-11). 5 Remove the bracket and deburr the holes at STGR34 and the bracket, item 7 (Refer to SRM 51-44-11).

DATE: Sep 27/11 SERVICE BULLETIN No.: A340-21-4152 REVISION No.: 03 - Dec 07/12 Page: 14 6

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# @A340 SERVICE BULLETIN
6 Clean the contact surface of the STGR34 LH and the bracket, item 7, with: Lint-Free Cotton Cloth 19-003 As required
and Cleaning Solvent 11-016 As required

7 Install: 1 Bracket ABS1577A05 Item 7 3 Rivet EN6081D4-05 Item 8 (Refer to SRM 51-42-11). NOTE: Do the electrical bonding of the rivets (Refer to ESPM 20-51-20) and (Refer to AMM Task 20-28-00-912-801). (f) Make a cutout in the insulation blanket in position of the new bracket, item 7, for the installation of the insulation blanket (Refer to AMM 25-80-00, Page Block 801). NOTE: Damaged insulations must be repaired (g) Cut the waste water pipe insulation and move it in the old position. (h) Install the bonding clamp on the new position as shown on Fig. A-GBBAA Sheet 02, View D. (i) On the waste water pipe, as shown Fig. A-GBBAA Sheet 02, View D, install: 1 Bonding Lead E0090-10-200NN Item 9 with: 1 Screw NAS1801-3-7 Item 1 1 Washer NAS1149C0332R Item 3 1 Nut MS21042-3 Item 2 (j) As shown on Fig. A-GBBAA Sheet 02, View C, connect: 1 Lead Bonding Item (4) Retained at removal and: 1 Bonding Lead E0090-10-200NN Item 9 with: 1 Screw NAS1801-3-7 Item 1 DATE: Sep 27/11 SERVICE BULLETIN No.: A340-21-4152 REVISION No.: 03 - Dec 07/12 Page: 15 6

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# @A340 SERVICE BULLETIN
1 Washer NAS1149C0332R Item 3 (k) Do the electrical bonding (Refer to ESPM 20-51-21). D. TEST (1) Subtask 214152-760-201-001 - Test of electrical bonding Work Zones and Access Panels Zone Access/Work location 160 Manpower Resources Skills ELECTRICAL References Aircraft Maintenance Manual (AMM) Task 20-28-00-720-805 (a) Check the electrical bonding of the bonding lead and the new bracket (Refer to AMM Task 20-28-00-720-805). E. CLOSE-UP (1) Subtask 214152-942-201-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 25-53-00-400-801 Task 25-80-00-400-801 Task 52-30-00-410-801 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) In the work area, install the insulation blankets (Refer to AMM Task 25-80-00-400-801). (c) Install the access panel 151TW (Refer to AMM Task 25-53-00-400-801). (d) If installed, remove the warning notice from the CLS. (e) Close the Aft cargo-compartment door (Refer to AMM Task 52-30-00-410-801). (f) Remove the access platform(s).

DATE: Sep 27/11 SERVICE BULLETIN No.: A340-21-4152 REVISION No.: 03 - Dec 07/12 Page: 16 6

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# @A340 SERVICE BULLETIN
Task 214152-831-849-001 - Modification - ADDITIONAL WORK WARNING: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONS INCLUDED IN THE REFERENCED PROCEDURES. CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY AND MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENANCE WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING, COMPONENTS AND THE WORK AREA AS CLEAN AS POSSIBLE. TO DO THIS: PUT PROTECTION, SUCH AS PLASTIC SHEETING, CLOTHS, ETC; AS NECESSARY ON WIRING AND COMPONENTS. REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND OTHER CONTAMINATION. THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION. IN CASE OF CONTAMINATION REFER TO ESPM 20-55-00. Task Associated Data Zone 160 Manpower TOTAL MANHOURS 2.50 ELAPSED TIME (HOURS) 2.50 A. GENERAL (1) Subtask 214152-910-202-001 - Standard Practices Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-20-00, Page Block 001 06-30-00, Page Block 001 06-31-53, Page Block 001 06-41-53, Page Block 001 (a) For identification of zones (Refer to AMM 06-20-00, Page Block 001). (b) For Stringer (STGR) identification (Refer to AMM 06-30-00, Page Block 001). (c) For Frame (FR) identification (Refer to AMM 06-31-53, Page Block 001). (d) For sidewall panel identification (Refer to AMM 06-41-53, Page Block 001).
DATE: Sep 27/11 SERVICE BULLETIN No.: A340-21-4152 REVISION No.: 03 - Dec 07/12 Page: 17 6

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# @A340 SERVICE BULLETIN (2) Subtask 214152-839-202-001 - Administrative Manpower Resources Skills NON SPECIFIC Write in the applicable aircraft records that you done all the work given in this Service Bulletin. B. PREPARATION (1) Subtask 214152-941-202-001 - Job Set-up Manpower Resources Skills ELECTRICAL References Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802 Task 25-53-00-000-801 Task 52-30-00-010-801 (a) Make sure that the aircraft is electrically grounded (Refer to AMM Task 12-34-24-860-802). (b) Put an access platform in position at the Aft cargo-compartment door. (c) Open the Aft cargo-compartment door (Refer to AMM Task 52-30-00-010-801). (d) If a Cargo Loading System (CLS) is installed, put a warning notice in position on the control panel to tell persons not to operate the CLS. (e) Remove the access panel 151TW (Refer to AMM Task 25-53-00-000-801). C. PROCEDURE (1) Subtask 214152-831-202-001 - Modify the bonding lead installation Work Zones and Access Panels Zone Access/Work location 160 Manpower Resources Manhours 0.25 Minimum number of person 1 Subtask elapsed time 0.25 Skills ELECTRICAL

DATE: Sep 27/11 SERVICE BULLETIN No.: A340-21-4152 REVISION No.: 03 - Dec 07/12 Page: 18 6

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# @A340 SERVICE BULLETIN
Material necessary to do the job Kit 214152D02R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 NAS1801-3-7 2 SCREW 2 MS21042-3 1 NUT 3 NAS1149C0332R 2 WASHER 9 E0090-10-200NN 1 LEAD References Elec. Std. Practices Manual (ESPM) 20-51-21 Fig. A-GBCAA Modify the bonding lead installation - ADDITIONAL WORK Sheet 01 Sheet 02 (a) As shown on Fig. A-GBCAA Sheet 01 and Fig. A-GBCAA Sheet 02, View C remove: 1 Washer Item (3) Discard 1 Screw Item (1) Discard and disconnect: 1 Bonding Lead Item (4) Retain 1 Bonding Lead E0091-10-160NN Item (10) Discard (b) As shown on Fig. A-GBCAA Sheet 01 and Fig. A-GBCAA Sheet 02, View D, remove: 1 Nut Item (2) Discard 1 Washer Item (3) Discard 1 Screw Item (1) Discard 1 Bonding Lead E0091-10-160NN Item (10) Discard (c) Cut the waste water pipe insolation and move it to the old position. (d) Install the bonding clamp on the new position, as shown on Fig. A-GBCAA Sheet 02, View D. (e) On the waste water pipe, as shown on Fig. A-GBCAA Sheet 02, View D, install: 1 Bonding Lead E0090-10-200NN Item 9 with:
DATE: Sep 27/11 SERVICE BULLETIN No.: A340-21-4152 REVISION No.: 03 - Dec 07/12 Page: 19 6

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# @A340 SERVICE BULLETIN
1 Screw NAS1801-3-7 Item 1 1 Washer NAS1149C0332R Item 3 1 Nut MS21042-3 Item 2 (f) As shown on Fig. A-GBCAA Sheet 02, View C, connect: 1 Bonding Lead Item (4) Retained at removal 1 Bonding Lead E0090-10-200NN Item 9 with: 1 Screw NAS1801-3-7 Item 1 1 Washer NAS1149C0332R Item 3 (g) Do the electrical bonding (Refer to ESPM 20-51-21). D. TEST (1) Subtask 214152-760-202-001 - Electrical Work Zones and Access Panels Zone Access/Work location 160 Manpower Resources Skills ELECTRICAL References Aircraft Maintenance Manual (AMM) Task 20-28-00-720-805 (a) Check the electrical bonding of the bonding lead (Refer to AMM Task 20-28-00-720-805). E. CLOSE-UP (1) Subtask 214152-942-202-001 - Close-up Work Zones and Access Panels Zone Access/Work location 160 Manpower Resources Skills CABIN References Aircraft Maintenance Manual (AMM) Task 25-53-00-400-801 Task 52-30-00-410-801 DATE: Sep 27/11 SERVICE BULLETIN No.: A340-21-4152 REVISION No.: 03 - Dec 07/12 Page: 20 6

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# @A340 SERVICE BULLETIN (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Install the access panel 151TW (Refer to AMM Task 25-53-00-400-801). (c) If installed, remove the warning notice from the CLS. (d) Close the Aft cargo-compartment door (Refer to AMM Task 52-30-00-410-801). (e) Remove the access platform(s).

DATE: Sep 27/11 SERVICE BULLETIN No.: A340-21-4152 REVISION No.: 03 - Dec 07/12 Page: 21 6

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# @A340 SERVICE BULLETIN

**CONF ALL



### B



## A 283HN

FR73 FR62

STGR34 FR64 FR63

FR62

STGR33 STGR32



## B 283HN 

### A Z160



### E

**C D** 

F_SB_214152_6_BAAA_01_02 Figure A-GBAAA - Sheet 01 Modify the bonding lead installation DATE: Sep 27/11 SERVICE BULLETIN No.: A340-21-4152 REVISION No.: 03 - Dec 07/12 Page: 22 6

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# @A340 SERVICE BULLETIN

**CONF ALL

FR64 (1)

(2) (5) (4)

(6) 

## BEFORE **AFTER**

(3)



## C FR64

6



## D (10)

(1)

(10) (3)

(2) 

## E (8)

F_SB_214152_6_BAAA_02_02 Figure A-GBAAA - Sheet 02 Modify the bonding lead installation DATE: Sep 27/11 SERVICE BULLETIN No.: A340-21-4152 REVISION No.: 03 - Dec 07/12 Page: 23 6

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# @A340 SERVICE BULLETIN

**CONF ALL



### B



## A 283HN

FR73 FR62

STGR34 FR64 FR63

FR62

STGR33 STGR32



## B 283HN



### C **A** Z160



### D

F_SB_214152_6_BBAA_01_02 Figure A-GBBAA - Sheet 01 Modify the bonding lead installation DATE: Sep 27/11 SERVICE BULLETIN No.: A340-21-4152 REVISION No.: 03 - Dec 07/12 Page: 24 6

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# @A340 SERVICE BULLETIN

**CONF ALL

1 3 7 8

9

98.2 mm (3.87 in) (115.0 mm)

(4.53 in) 14.0 mm (0.55 in)

**FWD** FR64 STGR34 STGR34

7 (4) 1

9 3

2 ca. 72.0 mm (2.83 in)
(8) OLD CLAMP

POSITION



## C **D**

**E E** 

F_SB_214152_6_BBAA_02_02 Figure A-GBBAA - Sheet 02 Modify the bonding lead installation DATE: Sep 27/11 SERVICE BULLETIN No.: A340-21-4152 REVISION No.: 03 - Dec 07/12 Page: 25 6

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# @A340 SERVICE BULLETIN

**CONF ALL



### B



## A 283HN

FR73 FR62

STGR34 FR64 FR63

FR62

STGR33 STGR32



## B 283HN



### C **D A**  Z160

F_SB_214152_6_BCAA_01_01 Figure A-GBCAA - Sheet 01 Modify the bonding lead installation - ADDITIONAL WORK DATE: Sep 27/11 SERVICE BULLETIN No.: A340-21-4152 REVISION No.: 03 - Dec 07/12 Page: 26 6

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# @A340 SERVICE BULLETIN

**CONF ALL

STGR34 1 3 (10) (4)

1

(10) 3

2 ca. 72.0 mm (2.83 in)
(8) OLD CLAMP

POSITION 

## C

**D** (1) (3)

9

9 (1) (3)

(2)

F_SB_214152_6_BCAA_02_01 Figure A-GBCAA - Sheet 02 Modify the bonding lead installation - ADDITIONAL WORK DATE: Sep 27/11 SERVICE BULLETIN No.: A340-21-4152 REVISION No.: 03 - Dec 07/12 Page: 27 6

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# @A340 SERVICE BULLETIN REPORTING SHEET 

### TITLE: AIR CONDITIONING - GENERAL - INSTALL NEW BONDING BRACKETS AFTER FRAME64 LH BETWEEN P33-P34 MODIFICATION No.: 201500D50418 Please complete the appropriate item (A or B): A - SB WILL BE embodied YES/NO (if NO please comment) If YES, aircraft concerned (as per SB effectivity by default) and planned dates (month/year) of embodiment:

B - SB HAS BEEN embodied on aircraft: Operator comments:
From Airline: Name/Title: Signature: Date: If operational documentation is affected (see Paragraph 1.K of this SB): If information is needed prior to next normal revision or prior to SB embodiment, please indicate required service(s): Either: Modification Operational Impact (MOI), if available YES/NO Or : Intermediate revision YES/NO Important Information: This SB will only be incorporated in your maintenance and operational documentation if this sheet is returned to Airbus and signed by a duly authorised representative. With the next feasible revision, this will result in - Updating of maintenance documentation to show pre and post SB data. - Updating of maintenance and operational documentation to show post SB data after embodiment. If this SB requires previous or simultaneous accomplishment of other SBs, Airbus shall automatically include them in the manual revisions. Refer to SIL 00-037 for detailed information. Please return this completed sheet to: AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Attn: SDC32 Technical Data and Documentation Services FAX: (+33) 5 61 93 28 06 e-mail: sb.reporting@airbus.com or via your Resident Customer Support Office. Alternatively, SB lists via letters or fax are also accepted.

DATE: Sep 27/11 SERVICE BULLETIN No.: A340-21-4152 REVISION No.: 03 - Dec 07/12 Page: 1 6

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# @A340 SERVICE BULLETIN QUALITY PERCEPTION FORM Use this form to tell us what is your perception of the quality of this Service Bulletin. The reported data that you provide us will be used to analyse areas of difficulties and to take corrective action to further improve the quality of our Service Bulletins. We thank you for the time you have taken in completing this form. (Please rate on a scale of 1 to 4, with 4 being the highest score) - Quality rating of this SB 4321 - Quality rating of the Accomplishment Instructions 4321 - Quality rating of the Illustrations 4321 - Is this SB easy to understand ? Y/N If you have had difficulties in the accomplishment of this SB please quote below the area(s) and give a short description of the issue. Planning Material Instructions X Effectivity X Kit content X Preparation X Reason X List of Materials Operator Supplied X Mod/Inspection X Manpower X Industry support X Test X References X Re-identification X Close-Up X Publication X Tooling X Illustrations Comments:

Operator: Date: Name/Title: Please return this form to: AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Attn : SEM4 Service Bulletins Management FAX : (33) 5 61 93 42 51 Or via your Resident Customer Support Office.

DATE: Sep 27/11 SERVICE BULLETIN No.: A340-21-4152 REVISION No.: 03 - Dec 07/12 Page: 1 6

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