# @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



# MANDATORY MANDATORY MANDATORY
ATA SYSTEM: 92 

### TITLE: ELECTRIC AND ELECTRONIC COMMON INSTALLATION - IMPROVE EMP ELECTRICAL CONNECTOR AND SLEEVE. MODIFICATION No.: 58773S30712 This page transmits Revision No.02 of Service Bulletin No.A340-92-4081 ADDITIONAL WORK **CONF ALL No additional work is required by this revision for aircraft modified by any previous issue. REASON Revision No. 02 issued to take into account connector PN MS3456KT24-10S : - Material paragraph modified, COMPA01 added, - Accomplishment instructions paragraph modified. CHANGES SUMMARY GENERAL EVALUATION GENERAL EVALUATION TABLE UPDATED R MATERIAL PRICE INFORMATION MATERIAL PRICE INFORMATION TABLE UPDATED R EFFECTIVITY OPERATOR LIST UPDATED R REFERENCES / REPERCUSSIONS REFERENCES/REPERCUSSIONS TABLE UPDATED R PLANNING INFORMATION EFFECTIVITY EFFECTIVITY RELATED INFORMATION UPDATED R Material Effectivity MATERIAL EFFECTIVITY UPDATED MATERIAL SET QUANTITY UPDATED MATERIAL SET UPDATED R
COMPLIANCE Classification CLASSIFICATION UPDATED R Accomplishment Timescale ACCOMPLISHMENT TIMESCALE UPDATED R DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-4081 REVISION No.: 02 - Sep 01/10 Page: 1 5

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# @A340 SERVICE BULLETIN REVISION TRANSMITTAL SHEET MANPOWER MANPOWER UPDATED R REFERENCES REFERENCED DOCUMENTATION UPDATED R MATERIAL INFORMATION MATERIAL - PRICE AND AVAILABILITY Procurement Addresses PROCUREMENT ADDRESSES UPDATED MATERIAL SET UPDATED R Price and Availability PRICE AND AVAILABILITY UPDATED MATERIAL SET UPDATED R INDUSTRY SUPPORT INFORMATION INDUSTRY SUPPORT INFORMATION UPDATED R LIST OF COMPONENTS Kit 924081A01R02 PART MATERIAL SET UPDATED MATERIAL SET LABEL UPDATED R LIST OF MATERIALS - OPERATOR SUPPLIED Minor editorial or document structure change R Consumable Materials CONSUMABLE MATERIALS PARAGRAPH ADDED N Components COMPONENTS PARAGRAPH ADDED N Component COMPA01 PART MATERIAL SET ADDED N Equipment EQUIPMENT PARAGRAPH ADDED N ACCOMPLISHMENT INSTRUCTIONS TASK 924081- 831-801-001-Modification Subtask 924081-910-001-001 SUBTASK SOLUTION UPDATED REFERENCED DOCUMENTATION UPDATED REFERENCES UPDATED R
Subtask 924081-941-001-001 SUBTASK SOLUTION UPDATED R Subtask 924081-831-003-001 SUBTASK SOLUTION UPDATED QUANTITY UPDATED PART NUMBER UPDATED KEYWORD UPDATED CONFIGURATION UPDATED FIGURE REFERENCE UPDATED NOTE UPDATED REFERENCED DOCUMENTATION UPDATED FIN UPDATED PART NUMBER DESCRIPTION UPDATED MATERIAL LIST UPDATED REFERENCES UPDATED R

Subtask 924081-831-002-001 SUBTASK SOLUTION UPDATED QUANTITY UPDATED PART NUMBER UPDATED KEYWORD UPDATED CONFIGURATION UPDATED FIGURE REFERENCE UPDATED NOTE UPDATED REFERENCED DOCUMENTATION UPDATED FIN UPDATED PART NUMBER DESCRIPTION UPDATED MATERIAL LIST UPDATED REFERENCES UPDATED R

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-4081 REVISION No.: 02 - Sep 01/10 Page: 2 5

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# @A340 SERVICE BULLETIN REVISION TRANSMITTAL SHEET Subtask 924081-831-004-001 SUBTASK SOLUTION UPDATED QUANTITY UPDATED PART NUMBER UPDATED KEYWORD UPDATED CONFIGURATION UPDATED FIGURE REFERENCE UPDATED FIN UPDATED NOTE UPDATED REFERENCED DOCUMENTATION UPDATED PART NUMBER DESCRIPTION UPDATED MATERIAL LIST UPDATED REFERENCES UPDATED R

Fig. A-FADAA Fig. A-FADAA Sheet 01 SHEET UPDATED R Fig. A-FAEAA FIGURE SOLUTION ADDED N Fig. A-FAEAA Sheet 01 SHEET ADDED 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 Revision No. 01 issued to change the commercial policy and to create a Kit. REVISION SEQUENCE ORIGINAL: Sep 02/09 REVISION No. : 01 - Feb 22/10 REVISION No. : 02 - Sep 01/10

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-4081 REVISION No.: 02 - Sep 01/10 Page: 3 5

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# @A340 SERVICE BULLETIN REVISION TRANSMITTAL SHEET

This Page Intentionally Left Blank

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-4081 REVISION No.: 02 - Sep 01/10 Page: 4 5

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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. 

# MANDATORY MANDATORY MANDATORY
ATA SYSTEM: 92 

### TITLE: ELECTRIC AND ELECTRONIC COMMON INSTALLATION - IMPROVE EMP ELECTRICAL CONNECTOR AND SLEEVE. **CONF ALL MODIFICATIONS MODIFICATION CLASSIFICATION MAJOR None MINOR 58773S30712 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 Several A330/A340 aircraft family operators have reported in service occurrences of hydraulic pump electrical motor connector internal arcing resulting in false hydraulic system overheat Electronic Centralized Aircraft Monitoring (ECAM) warnings and/or hydraulic pump electrical motor malfunction. Investigations have shown that under some conditions of the cables and the connectors rear grommet manufacturing tolerances, there is a possible path for fluid ingress resulting in the connector internal arcing and hydraulic system failure. This modification introduces heat shrink sleeves to the rear of the gauge 12 and 10 cable contacts and a sealing plug to the connector free cavity to increase the water tightness of the hydraulic pump electrical motor connectors 1JCA, 1JJA and 1JVA. The accomplishment of this Service Bulletin will prevent the possible hydraulic pump electrical motor connectors fluid ingress from the rear of the connector grommet and will prevent the false hydraulic system overheat ECAM warnings and/or hydraulic pump electrical motor malfunction. GENERAL EVALUATION EVALUATION TABLE COMPLIANCE MANDATORY (1) CANCELS INSPECTION SB NO POTENTIAL AD YES A/C OPERATION AFFECTED NO RELIABILITY AFFECTED NO PAX COMFORT AFFECTED NO DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-4081 REVISION No.: 02 - Sep 01/10 Page: 1 5

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# @A340 SERVICE BULLETIN SUMMARY EVALUATION TABLE COST SAVING NO LROPS AFFECTED NO 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 924081A01R02 1 877.00 Tubing-heat, Tie-cables, Sealing plugs, Sockets, Sleeve reducers Component COMPA01 1 See SB Sockets, Sleeve reducers EFFECTIVITY This Service Bulletin is applicable to this (these) operator(s) :

44W 47W 56W 83V AAW AFR AIB ALK ARG B3R CAL CCA CES CPA DGA DLH FIN GFA HFY IBE KAC LAN LHT M3R MAU MSR NMB OAL PAL QAF R3L RJA S3R SAA SAS SFW 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 OIT : SE 999.0040/09 dated 25 May 2009 OTHER SBIT : SEMB/914.0742/09 OTHER SBIT : SEMB F92M10018658 dated 6 May 2010 OTHER SBIT : 10-0034 dated 23 August 2010 NATURE OF THE WORK AIRCRAFT YES EQUIPMENT NO HARD NO SOFT NO OBRM NO

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-4081 REVISION No.: 02 - Sep 01/10 Page: 2 5

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# @A340 SERVICE BULLETIN SUMMARY MANPOWER Task 924081-831-801-001: Modification TOTAL MANHOURS 12.50 ELAPSED TIME (HOURS) 4.50 APPENDICES Appendix 01

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-4081 REVISION No.: 02 - Sep 01/10 Page: 3 5

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# @A340 SERVICE BULLETIN SUMMARY

**CONF ALL

F_SB_924081_5_SAAA_01_00 1JCA

1JJA 1JVA

Figure A-FSAAA - Sheet 01
DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-4081 REVISION No.: 02 - Sep 01/10 Page: 4 5

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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



# MANDATORY MANDATORY MANDATORY
ATA SYSTEM: 92 

### TITLE: ELECTRIC AND ELECTRONIC COMMON INSTALLATION - IMPROVE EMP ELECTRICAL CONNECTOR AND SLEEVE. MODIFICATION No.: 58773S30712 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 0002-0009 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 0097 0101 0103-0104 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 0544-0546 0554 0556 0559 0561-0562 0582 0585 0590 0598 0643 0646 0651 0668 0793 0800 0835 0844 0921 0938 0955
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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 44W 0007 47W 0009 56W 0013 83V 0040 AAW 0151 AFR 0029 0078 0084 0168 0174 0186 0207 0210 0237 0245 0246 0260 0307 0310 0319 0373 0377 0399 AIB 0197 0378 ALK 0032 0033 0034 0367 0374 ARG 0048 0063 0074 0080 0085 0093 0094 B3R 0046 CAL 0402 0406 0411 0415 0433 0541 CCA 0192 0199 0201 0242 0243 0264 CES 0129 0131 0141 0161 0182 CPA 0123 0126 0128 0136 0137 0142 0147 0157 0160 0208 0218 0220 0227 0228 0381 DGA 0075 0081 DLH 0020 0024 0027 0028 0035 0052 0053 0056 0135 0158 0213 0233 0252 0297 0304 0321 0325 0327 0335 0347 0352 0354 0355 0379 0390 0434 0447 FIN 0058 0835 0844 0921 0938 GFA 0039 0097 0103 0133 0212 0215 0282 0554 HFY 0117 IBE 0005 0088 0125 0134 0145 0146 0170 0193 0217 0221 0302 0318 0329 0332 0387 0414 0459 0474 0483 KAC 0089 0090 0101 0104 LAN 0167 0359 0363 0429 0442 LHT 0274 M3R 0061 MAU 0076 0152 0194 0268 0793 0800 MSR 0156 0159 0178 NMB 0047 0051 OAL 0235 0239 0280 0292 PAL 0173 0176 0187 0196 QAF 0026 0528 R3L 0004 RJA 0014 0022 0038 0043 S3R 0204 SAA 0006 0008 0011 0018 0019 0021 0544 0582 0590 0643 0646 0651 SAS 0413 0424 0430 0435 0450 0467 0470 DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-4081 REVISION No.: 02 - Sep 01/10 Page: 2 5

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# @A340 SERVICE BULLETIN

OPERATOR MSN SFW 0015 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 0216 0257 0270 0331 UAE 0139 0149 0163 0166 0185 0190 0202 0236 VCV 0031 VIR 0002 0003 0114 0164 0214 0225 XAX 0273 0278 (4) Configuration by MSN MSN CONFIGURATION 0002 0003 0004 0005 0006 0007 0008 0009 0011 0013 0014 0015 0018 0019 0020 0021 0022 0023 0024 0025 0026 0027 0028 0029 0031 0032 0033 0034 0035 0038 0039 0040 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 0097 0101 0103 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 0544 0545 0546 0554 0556 0559 0561 0562 0582 0585 0590 0598 0643 0646 0651 0668 0793 0800 0835 0844 0921 0938 0955 001

(5) Configuration definition **CONF 001 Config. 01 is valid for all the aircraft given in the effectivity of this Service Bulletin as a standard configuration. NOTE: On the same aircraft, it is possible to find both connectors PN ASNE0233-24-10S and PN MS3456KT24-10S.

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-4081 REVISION No.: 02 - Sep 01/10 Page: 3 5

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# @A340 SERVICE BULLETIN (6) Material Effectivity MATERIAL QTY PER A/C SEE NOTES Kit 924081A01R02 1 Component COMPA01 1 B. CONCURRENT REQUIREMENTS None C. REASON (1) History Several A330/A340 aircraft family operators have reported in service occurrences of hydraulic pump electrical motor connector internal arcing resulting in false hydraulic system overheat Electronic Centralized Aircraft Monitoring (ECAM) warnings and/or hydraulic pump electrical motor malfunction. Investigations have shown that under some conditions of the cables and the connectors rear grommet manufacturing tolerances, there is a possible path for fluid ingress resulting in the connector internal arcing and hydraulic system failure. (2) Objective/Action This modification introduces heat shrink sleeves to the rear of the gauge 12 and 10 cable contacts and a sealing plug to the connector free cavity to increase the water tightness of the hydraulic pump electrical motor connectors 1JCA, 1JJA and 1JVA. (3) Advantages The accomplishment of this Service Bulletin will prevent the possible hydraulic pump electrical motor connectors fluid ingress from the rear of the connector grommet and will prevent the false hydraulic system overheat ECAM warnings and/or hydraulic pump electrical motor malfunction. (4) Operational/Maintenance Consequences None D. DESCRIPTION To accomplish this Service Bulletin it is necessary to : Task 924081-831-801-001: Modification (1) Modify the equipment 1JCA (2) Modify the equipment 1JJA (3) Modify the equipment 1JVA

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-4081 REVISION No.: 02 - Sep 01/10 Page: 4 5

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# @A340 SERVICE BULLETIN
E. COMPLIANCE (1) Classification MANDATORY: Service Bulletin must be accomplished. (2) Accomplishment Timescale Accomplishment of this Service Bulletin is requested within 3600 FH from AD effective date. Accomplishment of this Service Bulletin has been rendered mandatory by the issue of an Airworthiness Directive (AD) published by the European Aviation Safety Agency (EASA). The AD must be used as the reference document for the mandatory accomplishment timescale. F. APPROVAL Approved under EASA Design Organisation Approval No. EASA 21J.031. If an aircraft listed in the effectivity has a modification or repair embodied that is not of AIRBUS origin, and which affects the content of this Service Bulletin, the operator is responsible for obtaining approval by its airworthiness authority for any adaptation necessary before incorporation of the Service Bulletin. G. MANPOWER The manpower estimates given in this Service Bulletin are based on the direct labor cost to do the work. These estimates assume that the work will be done by experienced personnel, and may need to be revised upwards to suit 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 924081-831-801-001: Modification Get Access 3.00 On Aircraft Modify the equipment 1JCA 2.00 Modify the equipment 1JJA 2.00 Modify the equipment 1JVA 2.00 Tests 0.50 Close-Up 3.00 TOTAL MANHOURS 12.50 ELAPSED TIME (HOURS) 4.50 NOTE: For detail concerning the elapsed time assumptions, refer to Appendix 01 . H. WEIGHT AND BALANCE Not Changed

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-4081 REVISION No.: 02 - Sep 01/10 Page: 5 5

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# @A340 SERVICE BULLETIN
I. ELECTRICAL LOAD DATA Not Changed J. REFERENCES

Aircraft Maintenance Manual (AMM) 06-31-53 06-41-53 12-34-24 29-21-51 29-22-51 29-23-51 Aircraft Wiring List (AWL) Elec. Std. Practices Manual (ESPM) 20-33-00 20-33-34 20-42-12 20-48-23 20-48-41 20-55-00 Standards Manual (SM) K. PUBLICATION AFFECTED None L. INTERCHANGEABILITY/MIXABILITY Not Applicable M. SPARES None

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-4081 REVISION No.: 02 - Sep 01/10 Page: 6 5

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# @A340 SERVICE BULLETIN
2. MATERIAL INFORMATION **CONF ALL A. MATERIAL - PRICE AND AVAILABILITY (1) Procurement Addresses 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 : Kit 924081A01R02 AIRBUS Material, Logistics 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 of single spares by fax: +49 40 50 76 40 13 (2) Price and Availability

Kit 924081A01R02 Cost 877.00 USD Availability 60 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. B. INDUSTRY SUPPORT INFORMATION AIRBUS will provide this Service Bulletin kit at no charge for orders placed before December 2012. AIRBUS will also credit the manhours indicated in this Service Bulletin at the operator’s agreed in-house warranty labor rate. Some Operators will require reducer PN NSA938186-04 and socket PN NSA938192DC0802 for connector PN MS3456KT24-10S as an alternative to PN ASNE0233-24-10S. These two parts should be sourced directly by the Operator and will be reimbursed by Airbus. Claims must be received not later than 90 days after completion of the last affected aircraft of your fleet C. LIST OF COMPONENTS Kit 924081A01R02 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES E0347DR0801 6 SOCKET E0347DR0801 E0616BB0800 30 PLUG E0718-02 1 (M) TUBING E0718-03 1 (M) TUBING DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-4081 REVISION No.: 02 - Sep 01/10 Page: 7 5

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# @A340 SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES NSA935401-04 30 TIE NSA938186-03 6 REDUCER 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. NOTE: For information, kits 924081A01R00 and 924081A01R02 contents are identical. D. LIST OF MATERIALS - OPERATOR SUPPLIED (1) Consumable Materials None (2) Components Component COMPA01 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES NSA938186-04 3 REDUCER NSA938192DC0802 6 SOCKET NSA938192DC0802 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. (3) Equipment None E. PARTS TO BE RE-IDENTIFIED BY OPERATOR None F. TOOLING None

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-4081 REVISION No.: 02 - Sep 01/10 Page: 8 5

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# @A340 SERVICE BULLETIN
3. ACCOMPLISHMENT INSTRUCTIONS Task 924081-831-801-001 - 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. IF THERE IS CONTAMINATION, REFER TO ESPM 20-55-00. Task Associated Data Zone 147 195 196 Modified FIN 1JCA 1JJA 1JVA Manpower TOTAL MANHOURS 12.50 ELAPSED TIME (HOURS) 4.50 A. GENERAL (1) Subtask 924081-910-001-001 - Standard Practices Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-31-53, Page Block 001 06-41-53, Page Block 001 Task 12-34-24-860-802 Elec. Std. Practices Manual (ESPM) 20-33-00 20-33-34 20-42-12 20-48-23 20-48-41 (a) Obey the instructions for the general wiring installation, (Refer to ESPM 20-33-00).
DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-4081 REVISION No.: 02 - Sep 01/10 Page: 9 5

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# @A340 SERVICE BULLETIN (b) Obey the instructions for the heat shrink sleeves installation, (Refer to ESPM 20-33-34). (c) For the description and the primary characteristics of the heat shrink sleeves, (Refer to ESPM 20-42-12). (d) Obey the instructions for the crimping, (Refer to ESPM 20-48-23). (e) Obey the instructions for the blanking plugs installation, (Refer to ESPM 20-48-41). (f) For the identification of the frames (FR), (Refer to AMM 06-31-53, Page Block 001). (g) For the identification of the access panels, (Refer to AMM 06-41-53, Page Block 001). (2) Subtask 924081-839-001-001 - Administrative Manpower Resources Skills NON SPECIFIC Write in the applicable aircraft records that you have done all the work given in this Service Bulletin. B. PREPARATION (1) Subtask 924081-941-001-001 - Job Set-Up Work Zones and Access Panels Zone Access/Work location 195 196 147 Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802 Task 29-21-51-000-801 Task 29-22-51-000-801 Task 29-23-51-000-801 (a) Make sure that the aircraft is electrically grounded (Refer to AMM Task 12-34-24-860-802). (b) Put access platform(s) in position. (c) Do the preparation procedure as specified in the removal of the Green Electric Pump (1JV), (Refer to AMM Task 29-21-51-000-801). (d) Do the preparation procedure as specified in the removal of the Blue Electric Pump (1JC), (Refer to AMM Task 29-22-51-000-801). DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-4081 REVISION No.: 02 - Sep 01/10 Page: 10 5

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# @A340 SERVICE BULLETIN (e) Do the preparation procedure as specified in the removal of the Yellow Electric Pump (1JJ), (Refer to AMM Task 29-23-51-000-801). C. PROCEDURE (1) Subtask 924081-831-003-001 - Modify the equipment 1JCA Work Zones and Access Panels Zone Access/Work location 195 Work location from Frame 46 to Frame 47 Manpower Resources Manhours 2.00 Minimum number of person 1 Subtask elapsed time 2.00 Skills NON SPECIFIC Material necessary to do the job Kit 924081A01R02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES E0347DR0801 2 SOCKET E0616BB0800 10 PLUG E0718-02 1 (M) TUBING E0718-03 1 (M) TUBING NSA935401-04 10 TIE NSA938186-03 2 REDUCER NOTE: For information, kits 924081A01R00 and 924081A01R02 contents are identical. Component COMPA01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES NSA938186-04 1 REDUCER NSA938192DC0802 2 SOCKET References Aircraft Wiring List (AWL) Fig. A-FADAA Installation of the heat shrinking sleeves Sheet 01 Fig. A-FAAAA Location of the equipment Sheet 01 Fig. A-FAEAA Installation of the heat shrinking sleeves Sheet 01

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-4081 REVISION No.: 02 - Sep 01/10 Page: 11 5

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# @A340 SERVICE BULLETIN (a) If connector PN ASNE0233-24-10S is installed : 1 Disconnect the plug 1JCA. 2 Disconnect the wire 2922-0099 (gauge DK10) from the plug 1JCA (if installed). 3 Remove : 1 Socket E0347DR0801 Discard from the wire. 4 Install on the wire : 1 (M) Tubing-Heat-Shrinkable E0718-03 NOTE : Cut the tubing-heat at 25 mm (0.984 in.). 5 Install on the wire : 1 Socket E0347DR0801 with : 1 Reducer NSA938186-03 NOTE: The sleeve has to be shrunk on the cable insulator. NOTE: Put the sleeve front at the edge of the cable’s stripped extremity. 6 Disconnect the wire 2922-0100 (gauge CF12 or DK12) from the plug 1JCA (if installed). 7 Remove : 1 Socket E0347DR0801 Discard from the wire. NOTE: If a tubing heat shrinkable sleeve is already installed on the wire, remove it. 8 Install on the wire : 1 (M) Tubing-Heat-Shrinkable E0718-02 NOTE : Cut the tubing-heat at 35 mm (1.378 in.) and 1 (M) Tubing-Heat-Shrinkable E0718-02 NOTE: Cut the tubing-heat at 30 mm (1.181 in.)
DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-4081 REVISION No.: 02 - Sep 01/10 Page: 12 5

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# @A340 SERVICE BULLETIN
and 1 (M) Tubing-Heat-Shrinkable E0718-03 NOTE: Cut the tubing-heat at 25 mm (0.984 in.). and 1 Socket E0347DR0801 with : 1 Reducer NSA938186-03 NOTE: The sleeves have to be shrunk on the cable insulator. NOTE: Put each sleeve front at the edge of the cable’s stripped extremity (Refer to Fig. A-FADAA). 9 Reconnect the wires on the plug 1JCA (Refer to Aircraft Wiring List (AWL)). 10 Use if necessary : 10 Tie-Cable NSA935401-04 11 On the plug, at the location on which the holes are not occupied, install : 10 Plug-Sealing E0616BB0800 12 Reconnect the plug 1JCA. (b) If connector PN MS3456KT24-10S is installed : 1 Disconnect the plug 1JCA. 2 Disconnect the wire 2922-0099 (gauge DK10) from the plug 1JCA (if installed). 3 Remove : 1 Socket NSA938192DC0802 Discard from the wire. 4 Install on the wire : 1 (M) Tubing-Heat-Shrinkable E0718-03 NOTE: Cut the tubing-heat at 25 mm (0.984 in.). 5 Install on the wire : 1 Socket NSA938192DC0802 with : DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-4081 REVISION No.: 02 - Sep 01/10 Page: 13 5

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# @A340 SERVICE BULLETIN

1 Reducer NSA938186-03 NOTE: The sleeve has to be shrunk on the cable insulator. NOTE: Put the sleeve front at the edge of the cable’s stripped extremity. 6 Disconnect the wire 2922-0100 (gauge CF12 or DK12) from the plug 1JCA (if installed). 7 Remove : 1 Socket NSA938192DC0802 Discard from the wire. NOTE: If a tubing heat shrinkable sleeve is already installed on the wire, remove it. 8 Install on the wire : 1 (M) Tubing-Heat-Shrinkable E0718-02 NOTE: Cut the tubing-heat at 35 mm (1.378 in.) and 1 (M) Tubing-Heat-Shrinkable E0718-03 NOTE: Cut the tubing-heat at 30 mm (1.181 in.) and 1 (M) Tubing-Heat-Shrinkable E0718-03 NOTE: Cut the tubing-heat at 25 mm (0.984 in.). and 1 Socket NSA938192DC0802 with : 1 Reducer NSA938186-04 NOTE: The sleeves have to be shrunk on the cable insulator. NOTE: Put each sleeve front at the edge of the cable’s stripped extremity (Refer to Fig. A-FAEAA). 9 Reconnect the wires on the plug 1JCA (Refer to Aircraft Wiring List (AWL)).

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-4081 REVISION No.: 02 - Sep 01/10 Page: 14 5

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# @A340 SERVICE BULLETIN
10 Use if necessary : 10 Tie-Cable NSA935401-04 11 On the plug, at the location on which the holes are not occupied, install : 10 Plug-Sealing E0616BB0800 12 Reconnect the plug 1JCA. (2) Subtask 924081-831-002-001 - Modify the equipment 1JJA Work Zones and Access Panels Zone Access/Work location 196 Work location from Frame 45 to Frame 46 Manpower Resources Manhours 2.00 Minimum number of person 1 Subtask elapsed time 2.00 Skills NON SPECIFIC Material necessary to do the job Kit 924081A01R02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES E0347DR0801 2 SOCKET E0616BB0800 10 PLUG E0718-02 1 (M) TUBING E0718-03 1 (M) TUBING NSA935401-04 10 TIE NSA938186-03 2 REDUCER NOTE: For information, kits 924081A01R00 and 924081A01R02 contents are identical. Component COMPA01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES NSA938186-04 1 REDUCER NSA938192DC0802 2 SOCKET References Aircraft Wiring List (AWL) Fig. A-FABAA Location of the equipment Sheet 01 Fig. A-FADAA Installation of the heat shrinking sleeves Sheet 01
DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-4081 REVISION No.: 02 - Sep 01/10 Page: 15 5

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# @A340 SERVICE BULLETIN

References Fig. A-FAEAA Installation of the heat shrinking sleeves Sheet 01 (a) If connector PN ASNE0233-24-10S is installed : 1 Disconnect the plug 1JJA. 2 Disconnect the wire 2923-0211 (gauge DK10) from the plug 1JJA (if installed). 3 Remove : 1 Socket E0347DR0801 Discard from the wire. 4 Install on the wire : 1 (M) Tubing-Heat-Shrinkable E0718-03 NOTE : Cut the tubing-heat at 25 mm (0.984 in.). 5 Install on the wire : 1 Socket E0347DR0801 with : 1 Reducer NSA938186-03 NOTE: The sleeve has to be shrunk on the cable insulator. NOTE: Put the sleeve front at the edge of the cable’s stripped extremity. 6 Disconnect the wire 2923-0212 (gauge CF12 or DK12) from the plug 1JJA (if installed). 7 Remove : 1 Socket E0347DR0801 Discard from the wire. NOTE: If a tubing heat shrinkable sleeve is already installed on the wire, remove it. 8 Install on the wire : 1 (M) Tubing-Heat-Shrinkable E0718-02 NOTE : Cut the tubing-heat at 35 mm (1.378 in.) and DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-4081 REVISION No.: 02 - Sep 01/10 Page: 16 5

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# @A340 SERVICE BULLETIN
1 (M) Tubing-Heat-Shrinkable E0718-02 NOTE: Cut the tubing-heat at 30 mm (1.181 in.) and 1 (M) Tubing-Heat-Shrinkable E0718-03 NOTE: Cut the tubing-heat at 25 mm (0.984 in.). and 1 Socket E0347DR0801 with : 1 Reducer NSA938186-03 NOTE: The sleeves have to be shrunk on the cable insulator. NOTE: Put each sleeve front at the edge of the cable’s stripped extremity (Refer to Fig. A-FADAA). 9 Reconnect the wires on the plug 1JJA (Refer to Aircraft Wiring List (AWL)). 10 Use if necessary : 10 Tie-Cable NSA935401-04 11 On the plug, at the location on which the holes are not occupied, install : 10 Plug-Sealing E0616BB0800 12 Reconnect the plug 1JJA. (b) If connector PN MS3456KT24-10S is installed : 1 Disconnect the plug 1JJA. 2 Disconnect the wire 2923-0211 (gauge DK10) from the plug 1JJA (if installed). 3 Remove : 1 Socket NSA938192DC0802 Discard from the wire. 4 Install on the wire : 1 (M) Tubing-Heat-Shrinkable E0718-03 NOTE: Cut the tubing-heat at 25 mm (0.984 in.).
DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-4081 REVISION No.: 02 - Sep 01/10 Page: 17 5

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# @A340 SERVICE BULLETIN
5 Install on the wire : 1 Socket NSA938192DC0802 with : 1 Reducer NSA938186-03 NOTE: The sleeve has to be shrunk on the cable insulator. NOTE: Put the sleeve front at the edge of the cable’s stripped extremity. 6 Disconnect the wire 2923-0212 (gauge CF12 or DK12) from the plug 1JJA (if installed). 7 Remove : 1 Socket NSA938192DC0802 Discard from the wire. NOTE: If a tubing heat shrinkable sleeve is already installed on the wire, remove it. 8 Install on the wire : 1 (M) Tubing-Heat-Shrinkable E0718-02 NOTE: Cut the tubing-heat at 35 mm (1.378 in.) and 1 (M) Tubing-Heat-Shrinkable E0718-03 NOTE: Cut the tubing-heat at 30 mm (1.181 in.) and 1 (M) Tubing-Heat-Shrinkable E0718-03 NOTE: Cut the tubing-heat at 25 mm (0.984 in.). and 1 Socket NSA938192DC0802 with : 1 Reducer NSA938186-04 NOTE: The sleeves have to be shrunk on the cable insulator. NOTE: Put each sleeve front at the edge of the cable’s stripped extremity (Refer to Fig. A-FAEAA). DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-4081 REVISION No.: 02 - Sep 01/10 Page: 18 5

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# @A340 SERVICE BULLETIN
9 Reconnect the wires on the plug 1JJA (Refer to Aircraft Wiring List (AWL)). 10 Use if necessary : 10 Tie-Cable NSA935401-04 11 On the plug, at the location on which the holes are not occupied, install : 10 Plug-Sealing E0616BB0800 12 Reconnect the plug 1JJA. (3) Subtask 924081-831-004-001 - Modify the equipment 1JVA Work Zones and Access Panels Zone Access/Work location 147 Work location from Frame 53.1 to Frame 53.2 Manpower Resources Manhours 2.00 Minimum number of person 1 Subtask elapsed time 2.00 Skills NON SPECIFIC Material necessary to do the job Kit 924081A01R02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES E0347DR0801 2 SOCKET E0616BB0800 10 PLUG E0718-02 1 (M) TUBING E0718-03 1 (M) TUBING NSA935401-04 10 TIE NSA938186-03 2 REDUCER NOTE: For information, kits 924081A01R00 and 924081A01R02 contents are identical. Component COMPA01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES NSA938186-04 1 REDUCER NSA938192DC0802 2 SOCKET References Aircraft Wiring List (AWL) Fig. A-FACAA Location of the equipment Sheet 01

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-4081 REVISION No.: 02 - Sep 01/10 Page: 19 5

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# @A340 SERVICE BULLETIN

References Fig. A-FADAA Installation of the heat shrinking sleeves Sheet 01 Fig. A-FAEAA Installation of the heat shrinking sleeves Sheet 01 (a) If connector PN ASNE0233-24-10S is installed : 1 Disconnect the plug 1JVA. 2 Disconnect the wire 2921-0183 (gauge DK10) from the plug 1JVA (if installed). 3 Remove : 1 Socket E0347DR0801 Discard from the wire. 4 Install on the wire : 1 (M) Tubing-Heat-Shrinkable E0718-03 NOTE : Cut the tubing-heat at 25 mm (0.984 in.). 5 Install on the wire : 1 Socket E0347DR0801 with : 1 Reducer NSA938186-03 NOTE: The sleeve has to be shrunk on the cable insulator. NOTE: Put the sleeve front at the edge of the cable’s stripped extremity. 6 Disconnect the wire 2921-0184 (gauge CF12 or DK12) from the plug 1JVA (if installed). 7 Remove : 1 Socket E0347DR0801 from the wire. NOTE: If a tubing heat shrinkable sleeve is already installed on the wire, remove it. 8 Install on the wire : 1 (M) Tubing-Heat-Shrinkable E0718-02 NOTE : Cut the tubing-heat at 35 mm (1.378 in.) DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-4081 REVISION No.: 02 - Sep 01/10 Page: 20 5

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# @A340 SERVICE BULLETIN
and 1 (M) Tubing-Heat-Shrinkable E0718-02 NOTE: Cut the tubing-heat at 30 mm (1.181 in.) and 1 (M) Tubing-Heat-Shrinkable E0718-03 NOTE: Cut the tubing-heat at 25 mm (0.984 in.). 1 Socket E0347DR0801 with : 1 Reducer NSA938186-03 NOTE: The sleeves have to be shrunk on the cable insulator. NOTE: Put each sleeve front at the edge of the cable’s stripped extremity (Refer to Fig. A-FADAA). 9 Reconnect the wires on the plug 1JVA (Refer to Aircraft Wiring List (AWL)). 10 Use if necessary : 10 Tie-Cable NSA935401-04 11 On the plug, at the location on which the holes are not occupied, install : 10 Plug-Sealing E0616BB0800 12 Reconnect the plug 1JVA. (b) If connector PN MS3456KT24-10S is installed : 1 Disconnect the plug 1JVA. 2 Disconnect the wire 2921-0183 (gauge DK10) from the plug 1JVA (if installed). 3 Remove : 1 Socket NSA938192DC0802 Discard from the wire. 4 Install on the wire : 1 (M) Tubing-Heat-Shrinkable E0718-03 NOTE: Cut the tubing-heat at 25 mm (0.984 in.).

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-4081 REVISION No.: 02 - Sep 01/10 Page: 21 5

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# @A340 SERVICE BULLETIN
5 Install on the wire : 1 Socket NSA938192DC0802 with : 1 Reducer NSA938186-03 NOTE: The sleeve has to be shrunk on the cable insulator. NOTE: Put the sleeve front at the edge of the cable’s stripped extremity. 6 Disconnect the wire 2921-0184 (gauge CF12 or DK12) from the plug 1JVA (if installed). 7 Remove : 1 Socket NSA938192DC0802 Discard from the wire. NOTE: If a tubing heat shrinkable sleeve is already installed on the wire, remove it. 8 Install on the wire : 1 (M) Tubing-Heat-Shrinkable E0718-02 NOTE: Cut the tubing-heat at 35 mm (1.378 in.) and 1 (M) Tubing-Heat-Shrinkable E0718-03 NOTE: Cut the tubing-heat at 30 mm (1.181 in.) and 1 (M) Tubing-Heat-Shrinkable E0718-03 NOTE: Cut the tubing-heat at 25 mm (0.984 in.). and 1 Socket NSA938192DC0802 with : 1 Reducer NSA938186-04 NOTE: The sleeves have to be shrunk on the cable insulator. NOTE: Put each sleeve front at the edge of the cable’s stripped extremity (Refer to Fig. A-FAEAA). DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-4081 REVISION No.: 02 - Sep 01/10 Page: 22 5

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# @A340 SERVICE BULLETIN
9 Reconnect the wires on the plug 1JVA (Refer to Aircraft Wiring List (AWL)). 10 Use if necessary : 10 Tie-Cable NSA935401-04 11 On the plug, at the location on which the holes are not occupied, install : 10 Plug-Sealing E0616BB0800 12 Reconnect the plug 1JVA. D. TEST (1) Subtask 924081-865-001-001 - C/B CLOSING Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 29-21-51-400-801 Task 29-22-51-400-801 Task 29-23-51-400-801 (a) Remove the safety clips and tags and close the circuit breakers as specified after the installation of the green electric pump (1JV), (Refer to AMM Task 29-21-51-400-801). (b) Remove the safety clips and tags and close the circuit breakers as specified after the installation of the blue electric pump (1JC), (Refer to AMM Task 29-22-51-400-801) (c) Remove the safety clips and tags and close the circuit breakers as specified after the installation of the yellow electric pump (1JJ), (Refer to AMM Task 29-23-51-400-801) (2) Subtask 924081-710-001-001 - OPERATIONAL Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 29-21-51-400-801 Task 29-22-51-400-801 Task 29-23-51-400-801 (a) Do the test procedure as specified after the installation of the Green Electric Pump (1JV), (Refer to AMM Task 29-21-51-400-801). (b) Do the test procedure as specified after the installation of the Blue Electric Pump (1JC), (Refer to AMM Task 29-22-51-400-801).

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-4081 REVISION No.: 02 - Sep 01/10 Page: 23 5

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# @A340 SERVICE BULLETIN (c) Do the test procedure as specified after the installation of the Yellow Electric Pump (1JJ), (Refer to AMM Task 29-23-51-400-801). E. CLOSE-UP (1) Subtask 924081-942-001-001 - CLOSE-UP Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 29-21-51-400-801 Task 29-22-51-400-801 Task 29-23-51-400-801 (a) Do the close-up procedure as specified after the installation of the Green Electric Pump (1JV), (Refer to AMM Task 29-21-51-400-801). (b) Do the close-up procedure as specified after the installation of the Blue Electric Pump (1JC), (Refer to AMM Task 29-22-51-400-801). (c) Do the close-up procedure as specified after the installation of the Yellow Electric Pump (1JJ), (Refer to AMM Task 29-23-51-400-801). (d) Make sure that the work areas are clean and clear of tools and other items of equipment. (e) Restore the systems and the aircraft to normal operating condition. (f) Remove the access platform(s).

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-4081 REVISION No.: 02 - Sep 01/10 Page: 24 5

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# @A340 SERVICE BULLETIN

**CONF ALL

FR46 FR47



### A

Z195



### B
1JC 

## A

1JCA 

## B BLUE ELECTRIC PUMP

F_SB_924081_5_AAAA_01_00 Figure A-FAAAA - Sheet 01

Location of the equipment DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-4081 REVISION No.: 02 - Sep 01/10 Page: 25 5

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# @A340 SERVICE BULLETIN

**CONF ALL

FR45 FR46

Z196 

### A

**B**

1JJ

1JJA 

## B **A** YELLOW ELECTRIC PUMP

F_SB_924081_5_ABAA_01_00 Figure A-FABAA - Sheet 01

Location of the equipment DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-4081 REVISION No.: 02 - Sep 01/10 Page: 26 5

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# @A340 SERVICE BULLETIN

**CONF ALL

1JV 

### B



## B **A**

1JVA

F_SB_924081_5_ACAA_01_00 Z147 FR53.2 FR53.1



## A FR53.1 FR53.2

GREEN ELECTRIC PUMP

Figure A-FACAA - Sheet 01

Location of the equipment DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-4081 REVISION No.: 02 - Sep 01/10 Page: 27 5

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# @A340 SERVICE BULLETIN

**CONF ALL

CABLE GAUGE CF12 OR DK12 (L : 25 mm (0.984 in )) SLEEVE ASNE0718−03

HEAT−SHRINKING

(L : 30 mm (1.181 in )) SLEEVE ASNE0718−02 HEAT−SHRINKING

CONTACT (L : 35 mm (1.378 in )) SLEEVE ASNE0718−02 HEAT−SHRINKING

01

F_SB_924081_5_ADAA_01_03 **NOTE:** THIS INSTALLATION IS VALID FOR CONNECTOR PN ASNE0233−24−10S 01 Figure A-FADAA - Sheet 01 Installation of the heat shrinking sleeves DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-4081 REVISION No.: 02 - Sep 01/10 Page: 28 5

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# @A340 SERVICE BULLETIN

**CONF ALL

CABLE GAUGE CF12 OR DK12 (L : 25 mm (0.984 in )) SLEEVE ASNE0718−03

HEAT−SHRINKING

(L : 30 mm (1.181 in )) SLEEVE ASNE0718−03 HEAT−SHRINKING

CONTACT (L : 35 mm (1.378 in )) SLEEVE ASNE0718−02 HEAT−SHRINKING

01

F_SB_924081_5_AEAA_01_02 **NOTE:** THIS INSTALLATION IS VALID FOR CONNECTOR PN MS3456KT24−10S 01 Figure A-FAEAA - Sheet 01 Installation of the heat shrinking sleeves DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-4081 REVISION No.: 02 - Sep 01/10 Page: 29 5

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# @A340 SERVICE BULLETIN

This Page Intentionally Left Blank

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-4081 REVISION No.: 02 - Sep 01/10 Page: 30 5

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# @A340 SERVICE BULLETIN Appendix 01 **CONF ALL (1) For detail concerning the elapsed time assumption of the modification, refer to the Gantt chart shown below :

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-4081 REVISION No.: 02 - Sep 01/10 Page: 1 5

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# @A340 SERVICE BULLETIN Appendix 01

**CONF ALL

**ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A330−92−3088**

ELAPSED TIME (HOURS)

**NOTE:** THIS CHART IS ONLY A PROPOSAL. OPERATORS MAY DETERMINE THAT ANOTHER WAY TO DO THE WORK IS MORE SUITABLE FOR THEM. MH ET PER

MH: ET: PER: MANHOURS ELAPSED TIME NUMBER OF PERSONS

TOTAL MANHOURS (MH) ELAPSED TIME (ET) 12.50 4.50 STEPS

0 5 4 3 2 1 GET ACCESS 3.00 1.00 3

MODIF. OF THE EQUIPMENT 1JJ−A 2.00 2.00 1 **MODIFICATION 6.00 2.00**  **3**

MODIF. OF THE EQUIPMENT 1JV−A 2.00 2.00 1

TEST 0.50 0.50 1

CLOSE−UP 3.00 1.00 3 MODIF. OF THE EQUIPMENT 1JC−A 2.00 2.00 1

F_SB_924081_5_BAAA_01_01 Figure A-FBAAA - Sheet 01 Gantt Chart DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-4081 REVISION No.: 02 - Sep 01/10 Page: 2 5

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# @A340 SERVICE BULLETIN REPORTING SHEET 

### TITLE: ELECTRIC AND ELECTRONIC COMMON INSTALLATION - IMPROVE EMP ELECTRICAL CONNECTOR AND SLEEVE. MODIFICATION No.: 58773S30712 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 02/09 SERVICE BULLETIN No.: A340-92-4081 REVISION No.: 02 - Sep 01/10 Page: 1 5

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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 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 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 02/09 SERVICE BULLETIN No.: A340-92-4081 REVISION No.: 02 - Sep 01/10 Page: 1 5

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