# Airbus Mandatory Service Bulletin A340-92-4078 Copy: Revision 01 ("U.S. DOT/FAA - Service Bulletin - A340-92-4078 R01"), 72 pages: PDF https://openairdocs.org/files/sha256/b7/29/b729df1745c524326cb309b9343d97298ff26361e3141c5ce2fe2def29f62924; text https://openairdocs.org/service-documents/airbus/a340-92-4078/file/b729df1745c5.md. Rights: © Airbus S.A.S. Filed by the FAA in regulations.gov docket FAA-2011-0474; AD 2011-18-20 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication. ## Details - Manufacturer: [Airbus](https://openairdocs.org/service-documents/airbus.md) - Type: Service bulletin (Mandatory Service Bulletin) - Number: A340-92-4078 - Latest revision known: A340-92-4078, Revision 01, dated April 9, 2010 (OpenAirDocs) - Page: https://openairdocs.org/service-documents/airbus/a340-92-4078 ## ADs that cite it (1) (OpenAirDocs) Newest first, with the revision each names, as OpenAirDocs read it from the AD's text. - [AD 2011-18-20](https://openairdocs.org/ad/2011-18-20.md), effective Oct 18, 2011: Revision 01 ## Text (72 pages) Rights: © Airbus S.A.S. Filed by the FAA in regulations.gov docket FAA-2011-0474; AD 2011-18-20 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication. This text is OCR from a scan. OCR can misread letters and numbers. Each page's text from the PDF; open the PDF at a page with #page=N. ### Page 1 (OCR) O+340 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 - CABLE LOOM INSTALLATION - MODIFY WIRE HARNESSES 5376VB/2M AND 5377VB/1M ABOVE DOOR 4 LH/RH MODIFICATION No.: 57349D46767 57562D46785 58924D50009 This page transmits Revision No.01 of Service Bulletin No.A340-92-4078 ADDITIONAL WORK **CONF ALL Additional work is required by this revision for aircraft which are part of configuration 001 modified by any previous issue. The additional work will ensure the interchangeability of the new and the old air outlet at door 4 LH/RH with the introduction of Mod. 58924D50009. The additional work has to be accomplished with Kit 924078D04R00. Additional work is required by this revision for aircraft which are part of configuration 002 modified by any previous issue. The additional work consist of the change of two screws per door, installed to fix the Air Outlet Box Assembly correctly. The additional work has to be accomplished with Kit 924078D03R02. REASON Revision 01 is issued to introduce the Mod. 58924D50009. This modification introduces two new brackets for the installation of the air outlet above door 4 LH/RH to ensure the interchangeability with the old air outlet. 6 DATE: Jun 17/08 SERVICE BULLETIN No.: A340-92-4078 REVISION No.: 01 - Apr 09/10 Page: 1 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 2 (OCR) DA340 SERVICE BULLETIN REVISION TRANSMITTAL SHEET CHANGES FRONT MATTER ELECTRIC AND ELECTRONIC COMMON SB TITLE UPDATED R INSTALLATION - CABLE LOOM CONFIGURATION UPDATED INSTALLATION - MODIFY WIRE HARNESSES 5376VB/2M AND 5377VB/1M ABOVE DOOR 4 LH/RH MODIFICATIONS MODIFICATION NUMBER(S) UPDATED R SUMMARY MODIFICATIONS MODIFICATION CLASSIFICATION UPDATED R REASON/DESCRIPTION/OPERATIONAL REASON UPDATED R CONSEQUENCES MATERIAL PRICE INFORMATION MATERIAL PRICE INFORMATION TABLE R UPDATED CONFIGURATION UPDATED MATERIAL PRICE INFORMATION TABLE ADDED N EFFECTIVITY OPERATOR LIST UPDATED IR REFERENCES / REPERCUSSIONS REFERENCES/REPERCUSSIONS TABLE R UPDATED MANPOWER MANPOWER UPDATED R CONFIGURATION UPDATED MANPOWER ADDED N Fig. A-GSAAA FIGURE SOLUTION UPDATED R Fig. A-GSAAA Sheet 01 SHEET UPDATED R Fig. A-GSAAA Sheet 02 SHEET DELETED D PLANNING INFORMATION EFFECTIVITY EFFECTIVITY RELATED INFORMATION R UPDATED Configuration definition CONFIGURATION LIST UPDATED R CONF 001 CONFIGURATION DEFINITION UPDATED CONFIGURATION DESCRIPTION UPDATED CONF 002 CONFIGURATION ADDED N Material Effectivity MATERIAL EFFECTIVITY UPDATED R CONFIGURATION UPDATED MATERIAL SET QUANTITY UPDATED MATERIAL SET UPDATED MATERIAL EFFECTIVITY ADDED N REASON History HISTORY UPDATED R Objective/Action OBJECTIVE/ACTION UPDATED R Advantages ADVANTAGES UPDATED R Operational/Maintenance OPERATIONAL/MAINTENANCE CONSEQUENCES Consequences UPDATED DESCRIPTION DESCRIPTION UPDATED R COMPLIANCE Accomplishment Timescale ACCOMPLISHMENT TIMESCALE ADDED DATE: Jun 17/08 SERVICE BULLETIN No.: A340-92-4078 REVISION No.: 01 - Apr 09/10 Page: 2 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 3 (OCR) © A340 SERVICE BULLETIN REVISION TRANSMITTAL SHEET Accomplishment Timescale ACCOMPLISHMENT TIMESCALE DELETED FOR D APPLICABLE MSN MANPOWER MANPOWER UPDATED R CONFIGURATION UPDATED MANPOWER ADDED IN WEIGHT AND BALANCE CONFIGURATION UPDATED IR WEIGHT AND BALANCE ADDED N REFERENCES REFERENCED DOCUMENTATION UPDATED CONFIGURATION UPDATED REFERENCED DOCUMENTATION ADDED N PUBLICATION AFFECTED PUBLICATIONS AFFECTED UPDATED R CONFIGURATION UPDATED PUBLICATIONS AFFECTED ADDED N MATERIAL INFORMATION MATERIAL - PRICE AND AVAILABILITY Procurement Addresses PROCUREMENT ADDRESSES UPDATED MATERIAL SET UPDATED Price and Availability PRICE AND AVAILABILITY UPDATED MATERIAL AVAILABILITY UPDATED MATERIAL PRICE UPDATED MATERIAL SET UPDATED INDUSTRY SUPPORT INFORMATION INDUSTRY SUPPORT INFORMATION UPDATED LIST OF COMPONENTS LIST OF COMPONENTS UPDATED Kit 924078D01R04 PART MATERIAL SET UPDATED MATERIAL SET LABEL UPDATED QUANTITY UPDATED PART NUMBER UPDATED ITEM NUMBER UPDATED KEYWORD UPDATED Kit 924078D03R02 PART MATERIAL SET ADDED N Kit 924078D04R00 PART MATERIAL SET ADDED N LIST OF MATERIALS - OPERATOR Minor editorial or document structure change R Consumable Materials CONSUMABLE MATERIALS PARAGRAPH ADDED N Consumable CMLD01 CONSUMABLE MATERIAL SET ADDED N Components COMPONENTS PARAGRAPH ADDED N Equipment ACCOMPLISHMENT INSTRUCTIONS TASK 924078- 831-848-001- MODIFICATION EQUIPMENT PARAGRAPH ADDED N TASK SOLUTION UPDATED CAUTION UPDATED CONFIGURATION UPDATED Task associated data - 001 CONFIGURATION UPDATED MAN HOURS UPDATED ELAPSED TIME UPDATED Task associated data - 002 TASK ASSOCIATED DATA ADDED N Subtask 924078-910-201-001 SUBTASK SOLUTION UPDATED R CONFIGURATION UPDATED REFERENCED DOCUMENTATION UPDATED REFERENCES UPDATED DATE: Jun 17/08 SERVICE BULLETIN No.: A340-92-4078 REVISION No.: 01 - Apr 09/10 Page: 3 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 4 (OCR) ©A340 SERVICE BULLETIN REVISION TRANSMITTAL SHEET Subtask 924078-839-201-001 Subtask 924078-910-201-001 Subtask 924078-839-201-001 SUBTASK SOLUTION UPDATED R CONFIGURATION UPDATED SUBTASK SOLUTION ADDED IN SUBTASK SOLUTION ADDED IN Subtask 924078-941-201-001 SUBTASK SOLUTION UPDATED R CONFIGURATION UPDATED REFERENCED DOCUMENTATION UPDATED REFERENCES UPDATED Subtask 924078-941-201-001 SUBTASK SOLUTION ADDED N Subtask 924078-020-202-001 SUBTASK SOLUTION UPDATED R CONFIGURATION UPDATED FIGURE REFERENCE UPDATED QUANTITY UPDATED PART NUMBER UPDATED REFERENCES UPDATED Subtask 924078-020-201-001 SUBTASK SOLUTION UPDATED IR CONFIGURATION UPDATED CAUTION UPDATED QUANTITY UPDATED ITEM NUMBER UPDATED PART NUMBER UPDATED PART NUMBER DESCRIPTION UPDATED NOTE UPDATED Subtask 924078-831-202-001 SUBTASK SOLUTION UPDATED CONFIGURATION UPDATED QUANTITY UPDATED CONSUMABLE UPDATED PART NUMBER DESCRIPTION UPDATED FIGURE REFERENCE UPDATED MATERIAL LIST UPDATED Subtask 924078-420-201-001 Subtask 924078-420-202-002 Subtask 924078-020-204-001 SUBTASK SOLUTION UPDATED R CONFIGURATION UPDATED QUANTITY UPDATED PART NUMBER UPDATED FIGURE REFERENCE UPDATED PART NUMBER DESCRIPTION UPDATED MATERIAL LIST UPDATED SUBTASK SOLUTION ADDED N SUBTASK SOLUTION UPDATED R CONFIGURATION UPDATED FIGURE REFERENCE UPDATED QUANTITY UPDATED PART NUMBER UPDATED REFERENCES UPDATED Subtask 924078-420-202-001 SUBTASK SOLUTION DELETED FOR D APPLICABLE MSN 6 DATE: Jun 17/08 SERVICE BULLETIN No.: A340-92-4078 REVISION No.: 01 - Apr 09/10 Page: 4 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 5 (OCR) GA340 SERVICE BULLETIN REVISION TRANSMITTAL SHEET Subtask 924078-020-203-001 SUBTASK SOLUTION UPDATED R CONFIGURATION UPDATED CAUTION UPDATED QUANTITY UPDATED ITEM NUMBER UPDATED PART NUMBER UPDATED PART NUMBER DESCRIPTION UPDATED NOTE UPDATED Subtask 924078-831-203-001 SUBTASK SOLUTION UPDATED R CONFIGURATION UPDATED QUANTITY UPDATED CONSUMABLE UPDATED ITEM NUMBER UPDATED PART NUMBER UPDATED PART NUMBER DESCRIPTION UPDATED FIGURE REFERENCE UPDATED MATERIAL LIST UPDATED Subtask 924078-420-203-001 SUBTASK SOLUTION UPDATED R CONFIGURATION UPDATED QUANTITY UPDATED Subtask 924078-420-204-002 Subtask 924078-420-204-001 Subtask 924078-020-202-001 Subtask 924078-020-201-001 Subtask 924078-831-202-002 Subtask 924078-420-201-002 PART NUMBER UPDATED FIGURE REFERENCE UPDATED PART NUMBER DESCRIPTION UPDATED MATERIAL LIST UPDATED SUBTASK SOLUTION ADDED N SUBTASK SOLUTION DELETED FOR D APPLICABLE MSN SUBTASK SOLUTION ADDED SUBTASK SOLUTION ADDED N SUBTASK SOLUTION ADDED IN SUBTASK SOLUTION ADDED N Subtask 924078-420-202-001 SUBTASK SOLUTION ADDED N Subtask 924078-020-204-001 SUBTASK SOLUTION ADDED Subtask 924078-020-203-001 Subtask 924078-831-203-002 Subtask 924078-420-203-002 Subtask 924078-420-204-001 Subtask 924078-942-201-001 Subtask 924078-942-201-001 SUBTASK SOLUTION ADDED IN SUBTASK SOLUTION ADDED N SUBTASK SOLUTION ADDED IN SUBTASK SOLUTION ADDED IN SUBTASK SOLUTION UPDATED R CONFIGURATION UPDATED REFERENCED DOCUMENTATION UPDATED REFERENCES UPDATED SUBTASK SOLUTION ADDED IN TASK 924078- 831-849-001- TASK SOLUTION ADDED N MODIFICATION - ADDITIONAL WORK Task associated data - 001 TASK ASSOCIATED DATA ADDED N Task associated data - 002 Subtask 924078-910-202-001 Subtask 924078-839-202-001 Subtask 924078-910-202-001 TASK ASSOCIATED DATA ADDED N SUBTASK SOLUTION ADDED IN SUBTASK SOLUTION ADDED N SUBTASK SOLUTION ADDED IN Subtask 924078-839-202-001 SUBTASK SOLUTION ADDED N DATE: Jun 17/08 SERVICE BULLETIN No.: A340-92-4078 REVISION No.: 01 - Apr 09/10 Page: 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 6 (OCR) GA340 SERVICE BULLETIN REVISION TRANSMITTAL SHEET Subtask 924078-941-202-001 Subtask 924078-941-202-001 Subtask 924078-831-204-001 Subtask 924078-831-204-002 Subtask 924078-942-202-001 Subtask 924078-942-202-001 Fig. A-GBEAA SUBTASK SOLUTION ADDED IN SUBTASK SOLUTION ADDED N SUBTASK SOLUTION ADDED N SUBTASK SOLUTION ADDED IN SUBTASK SOLUTION ADDED N SUBTASK SOLUTION ADDED IN FIGURE SOLUTION UPDATED R Fig. A-GBEAA Sheet 01 SHEET UPDATED R Fig. A-GBGAA Fig. A-GBGAA Sheet 01 SHEET UPDATED Fig. A-GBJAA Fig. A-GBJAA Sheet 01 SHEET UPDATED Fig. A-GBKAA FIGURE SOLUTION UPDATED CONFIGURATION UPDATED Fig. A-GBKAA Sheet 01 SHEET UPDATED IR Fig. A-GBKAB FIGURE SOLUTION ADDED Fig. A-GBKAB Sheet 01 SHEET ADDED Fig. A-GBLAA FIGURE SOLUTION UPDATED CONFIGURATION UPDATED Fig. A-GBLAA Sheet 01 SHEET UPDATED R Fig. A-GBLAB FIGURE SOLUTION ADDED N Fig. A-GBLAB Sheet 01 SHEET ADDED N Fig. A-GANAA FIGURE SOLUTION ADDED N Fig. A-GANAA Sheet 01 SHEET ADDED N Fig. A-GANAB FIGURE SOLUTION ADDED N Fig. A-GANAB Sheet 01 SHEET ADDED N Fig. A-GAPAA FIGURE SOLUTION ADDED N Fig. A-GAPAA Sheet 01 SHEET ADDED N Fig. A-GAPAB FIGURE SOLUTION ADDED N Fig. A-GAPAB 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 No previous revision REVISION SEQUENCE ORIGINAL: Jun 17/08 REVISION No. : 01 - Apr 09/10 DATE: Jun 17/08 SERVICE BULLETIN No.: А340-92-4078 REVISION No.: 01 - Apr 09/10 Page: 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 7 (OCR) ©A340 SERVICE BULLETIN SUMMARY CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX 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 - CABLE LOOM INSTALLATION - MODIFY WIRE HARNESSES 5376VB/2M AND 5377VB/1M ABOVE DOOR 4 LH/RH **CONF ALL MODIFICATIONS MODIFICATION CLASSIFICATION MAJOR None MINOR 57349D46767 57562D46785 58924D50009 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 Routine inspection has shown contact between the air-conditioning duct and the wire harness in the area between FR74 and FR75 at STGR7. In order to avoid contact between the flexible air conditioning hose and wire harnesses, this Service Bulletin introduces an additional bracket to keep the distance as well as a protective sleeve. After accomplishment of this Service Bulletin there will be sufficient clearance between the air-condition duct and the cable harnesses. GENERAL EVALUATION EVALUATION TABLE COMPLIANCE MANDATORY CANCELS INSPECTION SB NO POTENTIAL AD A/C OPERATION AFFECTED NO RELIABILITY AFFECTED PAX COMFORT AFFECTED NO COST SAVING LROPS AFFECTED NO STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED NO 6 DATE: Jun 17/08 SERVICE BULLETIN No.: A340-92-4078 REVISION No.: 01 - Apr 09/10 Page: 1 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 8 (OCR) ©A340 SERVICE BULLETIN SUMMARY MATERIAL PRICE INFORMATION **CONF 001 MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER PRICE PER MAIN PARTS A/C A/C (USD) Kit 924078D01 R04 304.00 Bracket, mount, washer, screw, sleeve, placard, tie-cable, support Kit 924078D04R00 200.00 Screw, support TOTAL 504.00 **CONF 002 MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER PRICE PER MAIN PARTS A/C A/C (USD) Kit 924078D03R02 256.00 Bracket, mount, washer, screw, sleeve, placard, tie-cable, support EFFECTIVITY **CONF ALL This Service Bulletin is applicable to this (these) operator(s) : 44W 47W 56W 83 V AAW AFR ALK ARG AWW B3R CAL CCA CES CPA DGA DLH FIN GFA HFY IBE KAC LAN LHT M3R MAU MSR NMB OAL PAL QAF R3L RJA I S3R SAA SAS SFW SLM SWR TAP THT THY UAE VCV VIR XAX CONCURRENT REQUIREMENTS None REFERENCES / REPERCUSSIONS TFU None OEB None AOT None SIL None LINE MAINTENANCE AFFECTED LIFE LIMIT None OTHER SBIT: SEMB/914.0013/09 NATURE OF THE WORK AIRCRAFT YES EQUIPMENT NO HARD NO SOFT NO 6 DATE: Jun 17/08 SERVICE BULLETIN No.: A340-92-4078 REVISION No.: 01 - Apr 09/10 Page: 2 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 9 (OCR) GA340 SERVICE BULLETIN SUMMARY OBRM NO MANPOWER **CONF 001 Task 924078-831-848-001: MODIFICATION TOTAL MANHOURS 10.00 ELAPSED TIME (HOURS) 5.50 Task 924078-831-849-001: MODIFICATION - ADDITIONAL WORK TOTAL MANHOURS 1.00 ELAPSED TIME (HOURS) 1.00 **CONF 002 Task 924078-831-848-001: MODIFICATION TOTAL MANHOURS 10.00 ELAPSED TIME (HOURS) 5.50 Task 924078-831-849-001: MODIFICATION - ADDITIONAL WORK TOTAL MANHOURS 0.75 ELAPSED TIME (HOURS) 1.00 APPENDICES **CONF ALL None 6 DATE: Jun 17/08 SERVICE BULLETIN No.: A340-92-4078 REVISION No.: 01 - Apr 09/10 Page: 3 Printed in FRANCE @ AIRBUS S.A.S. 2007. All rights reserved. ### Page 10 (OCR) ©A340 SERVICE BULLETIN SUMMARY **CONF ALL Z270 STGR75 FR73 LH SHOWN RH SYMMETRICAL F_SB_924078_6_SAAA_01_01 Figure A-GSAAA - Sheet 01 DATE: Jun 17/08 SERVICE BULLETIN No.: A340-92-4078 REVISION No.: 01 - Apr 09/10 Page: 4 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 11 (OCR) ©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 - CABLE LOOM INSTALLATION - MODIFY WIRE HARNESSES 5376VB/2M AND 5377VB/1M ABOVE DOOR 4 LH/RH MODIFICATION No.: 57349D46767 57562D46785 58924D50009 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. 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 6 DATE: Jun 17/08 SERVICE BULLETIN No.: A340-92-4078 REVISION No.: 01 - Apr 09/10 Page: 1 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 12 (OCR) DA340 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 0039 0040 AAW 0151 AFR 0029 0078 0084 0168 0174 0186 0207 0210 0237 0245 0246 0260 0307 0310 0319 0373 0377 0399 ALK 0032 0033 0034 0367 0374 ARG 0048 0063 0074 0080 0085 0093 AWW 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 GFA 0097 0103 0133 0212 0215 0282 0554 THFY 0117 IBE 0005 0088 0125 0134 0145 0146 0170 0193 0197 0217 0221 0302 0318 0329 0332 : 0378 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: Jun 17/08 SERVICE BULLETIN No.: A340-92-4078 REVISION No.: 01 - Apr 09/10 Page: 2 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 13 (OCR) GA340 SERVICE BULLETIN OPERATOR MSN SFW 0015 SLM 0049 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 I 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 001 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 002 (5) Configuration definition **CONF 001 Config. 001 is applicable for all aircraft which do not have Mod. 55770 embodied. **CONF 002 Config. 002 is applicable for all aircraft which already have Mod. 55770 embodied. DATE: Jun 17/08 SERVICE BULLETIN No.: A340-92-4078 REVISION No.: 01 - Apr 09/10 Page: 3 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 14 (OCR) ©A340 SERVICE BULLETIN (6) Material Effectivity • **CONF 001 MATERIAL QTY PER A/C SEE NOTES Kit 924078D01 R04 1 (1) Kit 924078D04R00 1 (2) Consumable CMLD01 1 NOTE (1): Operators who have already ordered two Kits 924078D01R00 to use one Kit per door and one differential Kit 92078D04R00, have the same amount of parts as operators who have ordered one Kit 924078D01R04 with the parts used per aircraft. NOTE (2): Kit 924078D04R00 has been created as a differential Kit of Kit 924078D01R00 and Kit 924078D01R04. This new Kit has to be ordered by operators which have already received two Kits 924078D01R00 and for ADDITIONAL WORK. **CONF 002 MATERIAL QTY PER A/C SEE NOTES Kit 924078D03R02 Consumable CMLD01 1 **CONF ALL B. CONCURRENT REQUIREMENTS None C. REASON (1) History Routine inspection has shown contact between the air-conditioning duct and the wire harness in the area between FR74 and FR75 at STGR7. (2) Objective/Action In order to avoid contact between the flexible air conditioning hose and wire harnesses, this Service Bulletin introduces an additional bracket to keep the distance as well as a protective sleeve. (3) Advantages After accomplishment of this Service Bulletin there will be sufficient clearance between the air-condition duct and the cable harnesses. (4) Operational/Maintenance Consequences None 6 DATE: Jun 17/08 SERVICE BULLETIN No.: A340-92-4078 REVISION No.: 01 - Apr 09/10 Page: 4 Printed in FRANCE @ AIRBUS S.A.S. 2007. All rights reserved. ### Page 15 (OCR) DA340 SERVICE BULLETIN D. DESCRIPTION To accomplish this Service Bulletin it is necessary to : • **CONF 001 Task 924078-831-848-001: MODIFICATION (1) Remove the air-condition outlet LH. (2) Remove the cable harnesses between FR74 and FR75, at STGR7 LH (3) Modify the STGR7 LH between FR74 and FR75. (4) Install the cable harness between FR74 and FR75, at STGR7 LH (5) Install the air-condition outlet LH. (6) Remove the air-condition outlet RH. (7) Remove the cable harnesses between FR74 and FR75, at STGR7 RH. (8) Modify the STGR7 RH between FR74 and FR75. (9) Install the cable harnesses between FR74 and FR75, at STGR7 RH. (10) Install the air-condition outlet RH. Task 924078-831-849-001: MODIFICATION - ADDITIONAL WORK (1) Modification of the Support Assembly of the Air Outlet **CONF 002 Task 924078-831-848-001: MODIFICATION (1) Remove the air-condition outlet LH. (2) Remove the cable harnesses between FR74 and FR75, at STGR7 LH (3) Modify the STGR7 LH between FR74 and FR75. (4) Install the cable harness between FR74 and FR75, at STGR7 LH (5) Install the air-condition outlet LH. (6) Remove the air-condition outlet RH. (7) Remove the cable harnesses between FR74 and FR75, at STGR7 RH. (8) Modify the STGR7 RH between FR74 and FR75. (9) Install the cable harnesses between FR74 and FR75, at STGR7 RH. 6 DATE: Jun 17/08 SERVICE BULLETIN No.: A340-92-4078 REVISION No.: 01 - Apr 09/10 Page: 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 16 (OCR) GA340 SERVICE BULLETIN (10) Install the air-condition outlet RH. Task 924078-831-849-001: MODIFICATION - ADDITIONAL WORK (1) Exchange the screws for the Air Outlet Box Assembly **CONF ALL E. COMPLIANCE (1) Classification MANDATORY (2) Accomplishment Timescale Accomplishment of this Service Bulletin is expected to be rendered mandatory by the issue of an Airworthiness Directive (AD) published by the European Aviation Safety Agency (EASA). The expected accomplishment timescale is 24 months from SB issuance date. The AD should confirm this threshold. 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 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 **CONF 001 Task 924078-831-848-001: MODIFICATION Get Access 2.00 On Aircraft Remove the air-condition outlet LH. 0.25 Remove the cable harnesses between FR74 and 0.25 FR75, at STGR7 LH Modify the STGR7 LH between FR74 and FR75. 1.00 Install the cable harness between FR74 and FR75, at 1.00 STGR7 LH Install the air-condition outlet LH. 0.50 Remove the air-condition outlet RH. 0.25 DATE: Jun 17/08 SERVICE BULLETIN No.: A340-92-4078 REVISION No.: 01 - Apr 09/10 Page: 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 17 (OCR) GA340 SERVICE BULLETIN Task 924078-831-848 001: MODIFICATION Remove the cable harnesses between FR74 and 0.25 FR75, at STGR7 RH. Modify the STGR7 RH between FR74 and FR75. 1.00 Install the cable harnesses between FR74 and FR75, 1.00 at STGR7 RH. Install the air-condition outlet RH. 0.50 Close-Up 2.00 TOTAL MANHOURS 10.00 ELAPSED TIME (HOURS) 5.50 Task 924078-831-849-001: MODIFICATION - ADDITIONAL WORK Get Access 0.25 On Aircraft Modification of the Support Assembly of the Air Outlet 0.50 Close-Up 0.25 TOTAL MANHOURS 1.00 ELAPSED TIME (HOURS) 1.00 **CONF 002 Task 924078-831-848-001: MODIFICATION Get Access 2.00 On Aircraft Remove the air-condition outlet LH. 0.25 Remove the cable harnesses between FR74 and 0.25 FR75, at STGR7 LH Modify the STGR7 LH between FR74 and FR75. 1.00 Install the cable harness between FR74 and FR75, at 1.00 STGR7 LH Install the air-condition outlet LH. 0.50 Remove the air-condition outlet RH. 0.25 Remove the cable harnesses between FR74 and 0.25 FR75, at STGR7 RH. Modify the STGR7 RH between FR74 and FR75. 1.00 Install the cable harnesses between FR74 and FR75, 1.00 at STGR7 RH. Install the air-condition outlet RH. 0.50 Close-Up 2.00 TOTAL MANHOURS 10.00 ELAPSED TIME (HOURS) 5.50 Task 924078-831-849-001: MODIFICATION - ADDITIONAL WORK Get Access 0.25 On Aircraft Exchange the screws for the Air Outlet Box Assembly 0.25 Close-Up 0.25 6 DATE: Jun 17/08 SERVICE BULLETIN No.: A340-92-4078 REVISION No.: 01 - Apr 09/10 Page: 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 18 (OCR) GA340 SERVICE BULLETIN Task 924078-831-849-001: MODIFICATION - ADDITIONAL WORK TOTAL MANHOURS 0.75 ELAPSED TIME (HOURS) 1.00 **CONF ALL H. WEIGHT AND BALANCE **CONF 001 Manufacturers Empty Weight +0.4629 LB (+0.210 KG) Effect on Balance +80.373 LB.FT (+11.112 KGM ) **CONF 002 Manufacturers Empty Weight +0.4629 LB (+0.210 KG) Effect on Balance +80.373 LB.FT (+11.112 KGM ) **CONF ALL ELECTRICAL LOAD DATA Not Changed J. REFERENCES **CONF 001 Aircraft Maintenance Manual (AMM) 06-30-00 06-31-53 06-41-53 12-34-24 25-23-42 25-23-47 25-80-00 Elec. Std. Practices Manual (ESPM) 20-32-20 20-33-11 20-33-33 20-33-40 20-33-41 20-33-44 20-55-00 Standards Manual (SM) Structural Repair Manual (SRM) 51-42-11 51-44-11 **CONF 002 Aircraft Maintenance Manual (AMM) 06-30-00 06-31-53 06-41-53 12-34-24 25-23-42 25-23-47 25-80-00 Elec. Std. Practices Manual (ESPM) 20-32-20 20-33-11 20-33-33 20-33-40 20-33-41 20-33-44 20-55-00 Standards Manual (SM) Structural Repair Manual (SRM) 51-42-11 51-44-11 6 DATE: Jun 17/08 SERVICE BULLETIN No.: A340-92-4078 REVISION No.: 01 - Apr 09/10 Page: 8 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 19 (OCR) GA340 SERVICE BULLETIN **CONF ALL K. PUBLICATION AFFECTED **CONF 001 Illustrated Parts Catalog (IPC) 21-24-04 24-92-04 **CONF 002 Illustrated Parts Catalog (IPC) 21-24-04 24-92-04 25-23-04 **CONF ALL L. INTERCHANGEABILITY/MIXABILITY Not Applicable M. SPARES None 6 DATE: Jun 17/08 SERVICE BULLETIN No.: A340-92-4078 REVISION No.: 01 - Apr 09/10 Page: 9 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 20 (OCR) ©A340 SERVICE BULLETIN This Page Intentionally Left Blank 6 DATE: Jun 17/08 SERVICE BULLETIN No.: A340-92-4078 REVISION No.: 01 - Apr 09/10 Page: 10 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 21 (OCR) GA340 SERVICE BULLETIN 2. MATERIAL INFORMATION **CONF ALL A. MATERIAL - PRICE AND AVAILABILITY (1) Procurement Addresses Kit 924078D01R04 Customers with aircraft shown in the Kit 924078D03R02 effectivity of this Service Bulletin should send Kit 924078D04R00 a purchase order to AIRBUS. Quote the number of this Service Bulletin. The address iS: Airbus Spares Support and Services Weg beim Jaeger 150 D-22335 Hamburg Germany For ordering by internet: http://spares.airbus.com For ordering by fax: +49 40 50 76 25 90 (2) Price and Availability Kit 924078D01 R04 Cost 304.00 USD Avallability 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. Kit 924078D03R02 Cost 256.00 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. Kit 924078D04R00 Cost 200.00 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. DATE: Jun 17/08 SERVICE BULLETIN No.: A340-92-4078 REVISION No.: 01 - Apr 09/10 Page: 11 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 22 (OCR) ©A340 SERVICE BULLETIN B. INDUSTRY SUPPORT INFORMATION AIRBUS will provide the material at no charge for orders placed before 17 June 2011. For aircraft under warranty at SB 1st issuance date, AIRBUS will also credit the manhours indicated in this Service Bulletin at the operator's agreed in-house warranty labor rate upon receipt of a warranty claim. c. LIST OF COMPONENTS Kit 924078D01 R04 TEM NEW PARTN QTY (UM) KEYWORD ITEM OLD PART N INT SEE NOTES NSA935401-04 20 TIE 2 ABS0785B05B 2 BRACKET EN6081AD4-06 4 RIVET 4 E0660-01 2 MOUNT 5 NAS1149DN832K 2 WASHER 6 NAS1801-08-8 6 SCREW 7 EN6049-006-25-5 4 (ME) SLEEVE G9237320002200 4 PLACARD 11 NAS1801-08-4 4 SCREW 12 NAS1149CN832R 4 WASHER 14 ASNA0113-40ADL 4 WASHER 16 F2528984503200 4 SUPPORT 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: Operators who have already ordered two Kits 924078D01R00 to use one Kit per door and one differential Kit 92078D04R00, have the same amount of parts as operators who have ordered one Kit 924078D01R04 with the parts used per aircraft. Kit 924078D03R02 ITEM NEW PART N QTY (UM) KEYWORD ITEM OLD PART N INT SEE NOTES NSA935401-04 20 TIE 2 ABS0785B05B 2 BRACKET EN6081AD4-06 4 RIVET 4 E0660-01 2 MOUNT 5 NAS1149DN832K 2 WASHER 6 NAS1801-08-8 2 SCREW 7 EN6049-006-25-5 4 (ME) SLEEVE G9237320002200 4 PLACARD 11 NAS1801-08-4 4 SCREW 12 NAS1149CN832R 4 WASHER 13 F2528984503000 4 SUPPORT 6 DATE: Jun 17/08 SERVICE BULLETIN No.: A340-92-4078 REVISION No.: 01 - Apr 09/10 Page: 12 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 23 (OCR) GA340 SERVICE BULLETIN ITEM NEW PARTN QTY (UM) KEYWORD ITEM OLD PART N INT SEE NOTES 14 ASNA0113-40ADL WASHER 17 NAS1801-08-6 SCREW 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 924078D04R00 ITEM NEW PARTN QTY (UM) KEYWORD ITEM OLD PARTN INT SEE NOTES 6 NAS1801-08-8 4 SCREW 16 F2528984503200 4 SUPPORT 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: Kit 924078D04R00 has been created as a differential Kit of Kit 924078D01R00 and Kit 924078D01R04. This new Kit has to be ordered by operators which have already received two Kits 924078D01R00 and for ADDITIONAL WORK. D. LIST OF MATERIALS - OPERATOR SUPPLIED (1) Consumable Materials Consumable CMLD01 TEM DESCRIPTION REFERENCE TO CML QTY PER A/C SEE MAT. No. NOTES Anti-Corrosion Primer 16-001 As required (polyurethane) (2) Components None (3) Equipment None E. PARTS TO BE RE-IDENTIFIED BY OPERATOR None F. TOOLING None 6 DATE: Jun 17/08 SERVICE BULLETIN No.: A340-92-4078 REVISION No.: 01 - Apr 09/10 Page: 13 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 24 (OCR) GA340 SERVICE BULLETIN This Page Intentionally Left Blank 6 DATE: Jun 17/08 SERVICE BULLETIN No.: A340-92-4078 REVISION No.: 01 - Apr 09/10 Page: 14 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 25 (OCR) GA340 SERVICE BULLETIN 3. ACCOMPLISHMENT INSTRUCTIONS Task 924078-831-848-001 - 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, OLOTHS, 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 • **CONF 001 Zone 270 Manpower TOTAL MANHOURS | 10.00 ELAPSED TIME (HOURS) 5.50 **CONF 002 Zone 270 Manpower TOTAL MANHOURS | 10.00 ELAPSED TIME (HOURS) 5.50 6 DATE: Jun 17/08 SERVICE BULLETIN No.: A340-92-4078 REVISION No.: 01 - Apr 09/10 Page: 15 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 26 (OCR) GA340 SERVICE BULLETIN **CONF ALL A. GENERAL **CONF 001 (1) Subtask 924078-910-201-001 - STANDARD PRACTICES Manpower Resources Skills AIRFRAME References Aircraft Maintenance Manual (AMM) 06-30-00, Page Block 001 06-31-53, Page Block 001 06-41-53, Page Block 001 Task 25-23-42-000-801 Task 25-23-47-000-801 Task 25-80-00-000-801 Elec. Std. Practices Manual (ESPM) 20-32-20 20-33-11 20-33-33 20-33-40 20-33-41 20-33-44 Standards Manual (SM) Structural Repair Manual (SRM) 51-42-11 51-44-11 (a) 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 the Airbus Standards Manual (SM). The SM will give you the correct part number to part number relationship. (b) For Frame (FR) identification, refer to AMM 06-31-53, Page Block 001. (c) For identification of the Stringer (STGR), refer to AMM 06-30-00, Page Block 001. (d) For ceiling panel identification, refer to AMM 06-41-53, Page Block 001. (e) For identification of wire harness, refer to ESPM 20-32-20. (f) For removal and installation of ceiling panels, refer to AMM Task 25-23-42-000-801. (g) For removal and installation of door frame lining, refer to AMM Task 25-23-47-000-801. (h) For removal and installation of thermal and acoustical insulation blankets, refer to AMM Task 25-80-00-000-801. (i) For installation of cable-ties, refer to ESPM 20-33-44. () For wire harness installation, refer to ESPM 20-33-41 and ESPM 20-33-11. DATE: Jun 17/08 SERVICE BULLETIN No.: A340-92-4078 REVISION No.: 01 - Apr 09/10 Page: 16 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 27 (OCR) ©A340 SERVICE BULLETIN (k) For flexible conduit installation, refer to ESPM 20-33-33. (I) For fastener removal and installation, refer to SRM 51-42-11. (m) For fastener drill and hole data, refer to SRM 51-44-11. (n) For wire and bundles identification, refer to ESPM 20-32-20. (o) For attachment description and operation, refer to ESPM 20-33-40. (2) Subtask 924078-839-201-001 - Documentation Manpower Resources Skills AIRFRAME (a) Write in the applicable aircraft records that you have done all the work given in the Service Bulletin. **CONF 002 (1) Subtask 924078-910-201-001 - STANDARD PRACTICES Manpower Resources Skills AIRFRAME References Aircraft Maintenance Manual (AMM) 06-30-00, Page Block 001 06-31-53, Page Block 001 06-41-53, Page Block 001 Task 25-23-42-000-801 Task 25-23-47-000-801 Task 25-80-00-000-801 Elec. Std. Practices Manual (ESPM) 20-32-20 20-33-11 20-33-33 20-33-40 20-33-41 20-33-44 Standards Manual (SM) Structural Repair Manual (SRM) 51-42-11 51-44-11 (a) 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 the Airbus Standards Manual (SM). The SM will give you the correct part number to part number relationship. (b) For Frame (FR) identification, refer to AMM 06-31-53, Page Block 001. (c) For identification of the Stringer (STGR), refer to AMM 06-30-00, Page Block 001. (d) For ceiling panel identification, refer to AMM 06-41-53, Page Block 001. 6 DATE: Jun 17/08 SERVICE BULLETIN No.: A340-92-4078 REVISION No.: 01 - Apr 09/10 Page: 17 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 28 (OCR) GA340 SERVICE BULLETIN (e) For identification of wire harness, refer to ESPM 20-32-20. (f) For removal and installation of ceiling panels, refer to AMM Task 25-23-42-000-801. (g) For removal and installation of door frame lining, refer to AMM Task 25-23-47-000-801. For removal and installation of thermal and acoustical insulation blankets, refer to AMM Task 25-80-00-000-801. (i) For installation of cable-ties, refer to ESPM 20-33-44. For wire harness installation, refer to ESPM 20-33-41 and ESPM 20-33-11. (k) For flexible conduit installation, refer to ESPM 20-33-33. For fastener removal and installation, refer to SRM 51-42-11. (m) For fastener drill and hole data, refer to SRM 51-44-11. (n) For wire and bundles identification, refer to ESPM 20-32-20. (o) For attachment description and operation, refer to ESPM 20-33-40. (2) Subtask 924078-839-201-001 - Documentation Manpower Resources Skills AIRFRAME (a) Write in the applicable aircraft records that you have done all the work given in the Service Bulletin. **CONF ALL B. PREPARATION **CONF 001 (1) Subtask 924078-941-201-001 - JOB SET-UP Work Zones and Access Panels Zone Access/Work location 270 Work location (from Frame 73 to Frame 76 Manpower Resources Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 12-34-24-860-801 Task 25-23-42-000-801 Task 25-23-47-000-801 6 DATE: Jun 17/08 SERVICE BULLETIN No.: A340-92-4078 REVISION No.: 01 - Apr 09/10 Page: 18 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 29 (OCR) ©A340 SERVICE BULLETIN (a) Make sure that the aircraft is electrically grounded, refer to AMM Task 12-34-24-860-801. (b) Get access to the Cabin. Between FR74 and FR76 LH remove the ceiling panels: 271EC, 271DC, 271FC, 271CC, refer to AMM Task 25-23-42-000-801. Between FR74 and FR76 LH remove the door frame lining: 271FW, 271NW, refer to AMM Task 25-23-47-000-801. (e) Between FR74 and FR76 RH remove the ceiling panels: 272EC, 272DC, 272FC, 272CC, refer to AMM Task 25-23-42-000-801. (t) Between FR74 and FR76 RH remove the door frame lining: 272FW, 272NW, refer to AMM Task 25-23-47-000-801. **CONF 002 (1) Subtask 924078-941-201-001 - JOB SET-UP Work Zones and Access Panels Zone Access/Work location 270 Work location from Frame 73 to Frame 76 Manpower Resources Skills _ AIRFRAME References Aircraft Maintenance Manual (AMM) Task 12-34-24-860-801 Task 25-23-42-000-801 Task 25-23-47-000-801 Make sure that the aircraft is electrically grounded, refer to AMM Task 12-34-24-860-801. (b) Get access to the Cabin. (c) Between FR74 and FR76 LH remove the ceiling panels: 271EC, 271DC, 271FC, 271CC, refer to AMM Task 25-23-42-000-801. Between FR74 and FR76 LH remove the door frame lining: 271FW, 271NW, refer to AMM Task 25-23-47-000-801. Between FR74 and FR76 RH remove the ceiling panels: 272EC, 272DC, 272FC, 272CC, refer to AMM Task 25-23-42-000-801. (f) Between FR74 and FR76 RH remove the door frame lining: 272FW, 272NW, refer to AMM Task 25-23-47-000-801. 6 DATE: Jun 17/08 SERVICE BULLETIN No.: A340-92-4078 REVISION No.: 01 - Apr 09/10 Page: 19 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved ### Page 30 (OCR) GA340 SERVICE BULLETIN **CONF ALL C. PROCEDURE **CONF 001 (1) Subtask 924078-020-202-001 - Remove the air-condition outlet LH. Work Zones and Access Panels Zone Access/Work location 270 Work location from Frame 74 to Frame 75 Stringer 7LH Manpower Resources Manhours 0.25 Minimum number of person Subtask elapsed time 0.25 Skills AIRFRAME References Fig. A-GBKAB Sheet 01 Removal of air-condition outlet (a) From the door frame lining item (271FW) LH, item (15), remove as shown on Fig. A-GBKAB Sheet 01 : 2 Screw Item (11) Discard 2 Washer Item (12) Discard Air Outlet Item (10) Retain (2) Subtask 924078-020-201-001 - Remove the cable harnesses between FR74 and FR75, at STGR7 LH Work Zones and Access Panels Zone Access/Work location 270 Work location from Frame 74 to Frame 76 Stringer 7LH Manpower Resources Manhours 0.25 Minimum number of person Subtask elapsed time 0.25 Skills AIRFRAME References Structural Repair Manual (SRM) 51-44-11 Fig. A-GBCAA Sheet 01 Location of the wire harnesses 6 DATE: Jun 17/08 SERVICE BULLETIN No.: A340-92-4078 REVISION No.: 01 - Apr 09/10 Page: 20 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 31 (OCR) © A340 SERVICE BULLETIN References Fig. A-GBEAA Sheet 01 Removal of cable ties, wire harnesses and insulation blankets CAUTION: DO NOT DAMAGE THE WIRE HARNESSES WHEN YOU CUT THE CABLE - TIES. (a) From the cable harnesses between FR74 and FR75 at STGR7 LH, remove as shown on Fig. A-GBCAA Sheet 01 and Fig. A-GBEAA Sheet 01: 4 Tie-Cable Item (1) Discard 2 Screw Item (6) Retain 2 Washer Item (5) Retain 2 Mount Item (4) Retain (3) Subtask 924078-831-202-001 - Modify the STGR7 LH between FR74 and FR75. Work Zones and Access Panels Zone Access/Work location 270 Work location from Frame 74 to Frame 75 Stringer 7LH Manpower Resources Manhours 1.00 Minimum number of person Subtask elapsed time 1.00 Skills AIRFRAME Material necessary to do the job Kit 924078D01R04 TEM NEW PARTN QTY (UM) KEYWORD SEE NOTES 2 ABS0785B05B BRACKET EN6081AD4-06 2 RIVET NOTE: Operators who have already ordered two Kits 924078D01R00 to use one Kit per door and one differential Kit 92078D04R00, have the same amount of parts as operators who have ordered one Kit 924078D01R04 with the parts used per aircraft. Consumable CMLD01 ITEM DESCRIPTION REFERENCE TO OTY PER A/C SEE CML MAT. No NOTES Anti-Corrosion Primer 16-001 As required (polyurethane) 6 DATE: Jun 17/08 SERVICE BULLETIN No.: A340-92-4078 REVISION No.: 01 - Apr 09/10 Page: 21 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 32 (OCR) GA340 SERVICE BULLETIN References Structural Repair Manual (SRM) 51-44-11 Fig. A-GBCAA Sheet 01 Location of the wire harnesses Fig. A-GBGAA Sheet 01 Installation brackets For access to modification area, remove the insulation blankets, as shown on Fiq. A-GBCAA Sheet 01 and Fig. A-GBGAA Sheet 01. (b) Between FR74 and FR75 LH, temporarily put in position: Bracket ABS0785B05B Item 2 refer to Fig. A-GBCAA Sheet 01 and Fig. A-GBGAA Sheet 01. (c) Transfer drill the pilot holes into the STGR7 LH. For the rivets, open up all holes to the final diameter between 3.25 mm (0.1280 in) to 3.35 mm (0.1319 in), refer to SRM 51-44-11. (e) Remove the temporarily installed bracket item 2. (†) Deburr and clean the holes, refer to SRM 51-44-11 (g) Install as shown on Fig. A-GBGAA Sheet 01 : Bracket ABS0785B05B Item 2 with 2 Rivet EN6081AD4-06 Item 3 (h) Clean the work area between FR74 and FR75 at STGR7 LH. Apply the surface protection Anti-Corrosion 16-001 As required Primer (polyurethane) to the rivets, item 3. (4) Subtask 924078-420-201-001 - Install the cable harness between FR74 and FR75, at STGR7 LH Work Zones and Access Panels Zone Access/Work location 270 Work location from Frame 74 to Frame 75 Stringer 7 LH 6 DATE: Jun 17/08 SERVICE BULLETIN No.: A340-92-4078 REVISION No.: 01 - Apr 09/10 Page: 22 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 33 (OCR) GA340 SERVICE BULLETIN Manpower Resources Manhours 1.00 Minimum number of person Subtask elapsed time 1.00 Skills AIRFRAME Material necessary to do the job Kit 924078D01 R04 ITEM NEW PARTN OTY (UM) KEYWORD SEE NOTES NSA935401-04 10 TIE 4 E0660-01 1 MOUNT 5 NAS1149DN832K WASHER 6 NAS1801-08-8 SCREW 7 EN6049-006-25-5 2 (ME) SLEEVE 8 G9237320002200 2 PLACARD NOTE: Operators who have already ordered two Kits 924078D01R00 to use one Kit per door and one differential Kit 92078D04R00, have the same amount of parts as operators who have ordered one Kit 924078D01 R04 with the parts used per aircraft. References Fig. A-GBCAA Sheet 01 Location of the wire harnesses Fig. A-GBJAA Sheet 01 installation insulation blankets, wire harnesses and cable ties (a) Install the insulation blanket, as shown on Fig. A-GBJAA Sheet 01. (b) Between FR74 and FR75, at STGR7 LH, install as shown on Fig. A-GBCAA Sheet 01 and Fig. A-GBJAA Sheet 01, Detail A : 2 Mount Item (4) Retained at removal 2 Washer Item (5) Retained at removal 2 Screw Item (6) Retained at removal (c) Between FR74 and FR75, at STGR7 LH, install as shown on Fig. A-GBCAA Sheet 01 and Fig. A-GBJAA Sheet 01, Detail B : 1 Mount E0660-01 Item 4 1 Washer NAS1149DN832K Item 5 6 DATE: Jun 17/08 SERVICE BULLETIN No.: A340-92-4078 REVISION No.: 01 - Apr 09/10 Page: 23 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 34 (OCR) GA340 SERVICE BULLETIN 1 Screw NAS1801-08-8 Item 6 On the cable harnesses, install as show on Fig. A-GBCAA Sheet 01 and Fig. A- GBJAA Sheet 01 : 2 (ME) Sleeve EN6049-006-25-5 Item 7 2 Placard G9237320002200 Item 8 10 Tie NSA935401-04 Item 1 (5) Subtask 924078-420-202-002 - Install the air-condition outlet LH. Work Zones and Access Panels Zone Access/Work location 270 Work location from Frame 74 to Frame 75 Stringer 7LH Manpower Resources Manhours 0.50 Minimum number of person Subtask elapsed time 0.50 Skills AIRFRAME Material necessary to do the job Kit 924078D01 R04 ITEM NEW PARTN QTY (UM) KEYWORD SEE NOTES NAS1801-08-8 2 SCREW 11 NAS1801-08-4 2 SCREW 12 NAS1149CN832R 2 WASHER 14 ASNA0113-40ADL 2 WASHER 16 F2528984503200 2 SUPPORT NOTE: Operators who have already ordered two Kits 924078D01R00 to use one Kit per door and one differential Kit 92078D04R00, have the same amount of parts as operators who nave ordered one Kit 924078D01 R04 with the parts used per aircraft. References Fig. A-GBLAB Sheet 01 Installation of modify air-condition outlet (a) On the door frame lining (271FW) LH, item (15), install as shown on Fig. A-GBLAB Sheet 01 : 2 Support F2528984503200 Item 16 2 Washer NAS1149CN832R Item 12 6 DATE: Jun 17/08 SERVICE BULLETIN No.: A340-92-4078 REVISION No.: 01 - Apr 09/10 Page: 24 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 35 (OCR) GA340 SERVICE BULLETIN 2 Screw NAS1801-08-4 Item 11 1 Air Outlet Item (10) Retained at removal 2 Washer ASNA0113-40ADL Item 14 2 Screw NAS1801-08-8 Item 6 (6) Subtask 924078-020-204-001 - Remove the air-condition outlet RH. Work Zones and Access Panels Zone Access/Work location 270 Work location from Frame 74 to Frame 75 Stringer 7RH Manpower Resources Manhours 0.25 Minimum number of person Subtask elapsed time 0.25 Skills AIRFRAME References Fig. A-GBKAB Sheet 01 Removal of air-condition outlet (a) From the door frame lining (272FW) RH, item (15), remove as shown on 2 Screw Item (11) Discard 2 Washer Item (12) Discard 1 Air Outlet Item (10) Retain Subtask 924078-020-203-001 - Remove the cable harnesses between FR74 and FR75, at STGR7 RH. Work Zones and Access Panels Zone Access/Work location 270 Work location from Frame 74 to Frame 75 Stringer 7RH Manpower Resources Manhours 0.25 Minimum number of person Subtask elapsed time 0.25 Skills AIRFRAME 6 DATE: Jun 17/08 SERVICE BULLETIN No.: A340-92-4078 REVISION No.: 01 - Apr 09/10 Page: 25 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 36 (OCR) GA340 SERVICE BULLETIN References Fig. A-GBCAA Sheet 01 Location of the wire harnesses Fig. A-GBEAA Sheet 01 Removal of cable ties, wire harnesses and insulation blankets CAUTION: DO NOT DAMAGE THE WIRE HARNESSES WHEN YOU CUT THE CABLE-TIES. (a) From the cable harnesses between FR74 and FR75 at STGR7 RH, remove as shown on Fig. A-GBCAA Sheet 01 and Fig. A-GBEAA Sheet 01: Tie-Cable Item (1) Discard 2 Screw Item (6) Retain 2 Washer Item (%) Retain 2 Mount Item (4) Retain (8) Subtask 924078-831-203-001 - Modify the STGR7 RH between FR74 and FR75. Work Zones and Access Panels Zone Access/Work location 270 Work location from Frame 74 to Frame 75 Stringer 7RH Manpower Resources Manhours 1.00 Minimum number of person Subtask elapsed time 1.000 Skills AIRFRAME Material necessary to do the job Kit 924078D01 R04 ITEM NEW PART N QTY (UM) KEYWORD SEE NOTES 2 ABS0785B05B BRACKET EN6081AD4-06 2 RIVET NOTE: Operators who have already ordered two Kits 924078D01R00 to use one Kit per door and one differential Kit 92078D04R00, have the same amount of parts as operators who have ordered one Kit 924078D01R04 with the parts used per aircraft. 6 DATE: Jun 17/08 SERVICE BULLETIN No.: A340-92-4078 REVISION No.: 01 - Apr 09/10 Page: 26 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 37 (OCR) GA340 SERVICE BULLETIN Consumable CMLD01 ITEM DESCRIPTION REFERENCE TO QTY PER A/C ISEE CML MAT. No. NOTES Anti-Corrosion Primer 16-001 As required (polyurethane) References Structural Repair Manual (SRM) 51-44-11 Fig. A-GBCAA Sheet 01 Location of the wire harnesses Fig. A-GBGAA Sheet 01 Installation brackets Fig. A-GBEAA Sheet 01 Removal of cable ties, wire harnesses and insulation blankets (a) For access to the modification area, remove the insulation blankets, as shown on Fig. A-GBCAA Sheet 01 and Fig. A-GBEAA Sheet 01. Between FR74 and FR75 RH, temporarily put in position as shown on Fig. A- GBCAA Sheet 01 and Fig. A-GBGAA Sheet 01 : Bracket ABS0785B05B Item 2 (c) Transfer drill the pilot holes into the STGR7 RH. For the rivets, open up all holes to final diameter between 3.25 mm (0.1280 in) to 3.35 mm (0.1319 in), refer to SRM 51-44-11. (e) Remove the temporarily installed bracket item 2. (†) Deburr and clean the holes, refer to SRM 51-44-11. (g) Install as shown on Fig. A-GBGAA Sheet 01 : Bracket ABS0785B05B Item 2 with 2 Rivet EN6081AD4-06 Item 3 (h) Clean the work area between FR74 and FR75 at STRG7 RH. Apply the surface protection Anti-Corrosion 16-001 As required Primer (polyurethane) to the rivets, item 3. 6 DATE: Jun 17/08 SERVICE BULLETIN No.: A340-92-4078 REVISION No.: 01 - Apr 09/10 Page: 27 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 38 (OCR) © A340 SERVICE BULLETIN (9) Subtask 924078-420-203-001 - Install the cable harnesses between FR74 and FR75, at STGRY RH. Work Zones and Access Panels Zone Access/Work location 270 Work location from Frame 74 to Frame 75 Stringer 7RH Manpower Resources Manhours 1.00 Minimum number of person Subtask elapsed time 1.00 Skills AIRFRAME Material necessary to do the job Kit 924078D01 R04 ITEM NEW PARTN QTY (UM) KEYWORD SEE NOTES NSA935401-04 10 TIE 4 E0660-01 MOUNT 5 NAS1149DN832K WASHER 6 NAS1801-08-8 SCREW 7 EN6049-006-25-5 2 (ME) SLEEVE G9237320002200 2 PLACARD NOTE: Operators who have already ordered two Kits 924078D01R00 to use one Kit per door and one differential Kit 92078D04R00, have the same amount of parts as operators who have ordered one Kit 924078D01R04 with the parts used per aircraft. References Fig. A-GBCAA Sheet 01 _ocation of the wire harnesses Fig. A-GBGAA Sheet 01 Installation brackets Fig. A-GBJAA Sheet 01 installation insulation blankets, wire harnesses and cable ties (a) Install the insulation blanket, as shown on Fig. A-GBJAA Sheet 01. Between FR74 and FR75 at STGR7 RH, install as shown on Fig. A-GBCAA Sheet 01 and Fig. A-GBJAA Sheet 01, Detail A : 2 Mount Item (4) Retained at removal 2 Washer Item (5) Retained at removal 6 DATE: Jun 17/08 SERVICE BULLETIN No.: A340-92-4078 REVISION No.: 01 - Apr 09/10 Page: 28 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 39 (OCR) GA340 SERVICE BULLETIN 2 Screw Item (6) Retained at removal (c) Between FR74 and FR75 at STGR7 RH, install as shown on Fig. A-GBCAA Sheet 01 and Fig. A-GBJAA Sheet 01, Detail B : Mount E0660-01 Item 4 Washer NAS1149DN832K Item 5 1 Screw NAS1801-08-8 Item 6 On the cable harnesses, install as shown on Fig. A-GBCAA Sheet 01 and Fig. A- GBJAA Sheet 01: 2 (ME) Sleeve EN6049-006-25-5 Item 7 2 Placard G9237320002200 Item 8 10 Tie NSA935401-04 Item 1 (10) Subtask 924078-420-204-002 - Install the air-condition outlet RH. Manpower Resources Manhours 0.50 Minimum number of person Subtask elapsed time 0.50 Skills AIRFRAME Material necessary to do the job Kit 924078D01 R04 ITEM NEW PART N QTY (UM) KEYWORD SEE NOTES 6 NAS1801-08-8 2 SCREW NAS1801-08-4 2 SCREW 12 NAS1149CN832R 2 WASHER 14 ASNA0113-40ADL 2 WASHER 16 F2528984503200 2 SUPPORT NOTE: Operators who have already ordered two Kits 924078D01R00 to use one Kit per door and one differential Kit 92078D04R00, have the same amount of parts as operators who have ordered one Kit 924078D01R04 with the parts used per aircraft. References Fig. A-GBLAB Sheet 01 Installation of modify air-condition outlet DATE: Jun 17/08 SERVICE BULLETIN No.: A340-92-4078 REVISION No.: 01 - Apr 09/10 Page: 29 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 40 (OCR) GA340 SERVICE BULLETIN (a) On the door frame lining (272FW) RH, item (15), install as shown on Fig. A-GBLAB Sheet 01 : 2 Support F2528984503200 Item 16 2 Washer NAS1149CN832R Item 12 2 Screw NAS1801-08-4 Item 11 Air Outlet Item (10) Retained at removal 2 Washer ASNA0113-40ADL Item 14 2 Screw NAS1801-08-8 Item 6 **CONF 002 (1) Subtask 924078-020-202-001 - Remove the air-condition outlet LH. Work Zones and Access Panels Zone Access/Work location 270 Work location from Frame 74 to Frame 75 Stringer 7LH Manpower Resources Manhours 0.25 Minimum number ot person Subtask elapsed time 0.25 Skills AIRFRAME References Fig. A-GBKAA Sheet 01 Removal of air-condition outlet (a) From the door frame lining item (271FW) LH, item (15), remove as shown on : 2 Screw Item (11) Discard 2 Washer Item (12) Discard 1 Air Outlet Item (10) Retain (2) Subtask 924078-020-201-001 - Remove the cable harnesses between FR74 and FR75, at STGR7 LH Work Zones and Access Panels Zone Access/Work location 270 Work location from Frame 74 to Frame 76 Stringer 7LH DATE: Jun 17/08 SERVICE BULLETIN No.: A340-92-4078 REVISION No.: 01 - Apr 09/10 Page: 30 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 41 (OCR) ©A340 SERVICE BULLETIN Manpower Resources Manhours 0.25 Minimum number of person Subtask elapsed time 0.25 Skills AIRFRAME References Structural Repair Manual (SRM) 51-44-11 Fig. A-GBCAA Sheet 01 Location of the wire harnesses Fig. A-GBEAA Sheet 01 Removal of cable ties, wire harnesses and insulation blankets CAUTION DO NOT DAMAGE THE WIRE HARNESSES WHEN YOU OUT THE CABLE - TIES. (a) From the cable harnesses between FR74 and FR75 at STGR7 LH, remove as shown on Fig. A-GBCAA Sheet 01 and Fig. A-GBEAA Sheet 01: 4 Tie-Cable Item (1) Discard 2 Screw Item (6) Retain 2 Washer Item (5) Retain 2 Mount Item (4) Retain (3) Subtask 924078-831-202-002 - Modify the STGR7 LH between FR74 and FR75. Work Zones and Access Panels Zone Access/Work location 270 Work location from Frame 74 to Frame 75 Stringer 7LH Manpower Resources Manhours 1.00 Minimum number of person Subtask elapsed time 1.00 Skills AIRFRAME Material necessary to do the job Kit 924078D03R02. ITEM NEW PARTN QTY (UM) KEYWORD ISEE NOTES 2 ABS0785B05B BRACKET EN6081AD4-06 2 RIVET DATE: Jun 17/08 SERVICE BULLETIN No.: A340-92-4078 REVISION No.: 01 - Apr 09/10 Page: 31 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 42 (OCR) GA340 SERVICE BULLETIN Consumable CMLD01 ITEM DESCRIPTION REFERENCE TO QTY PER A/C SEE CML MAT. No. NOTES Anti-Corrosion Primer 16-001 As required (polyurethane) References Structural Repair Manual (SRM) 51-44-11 Fig. A-GBCAA Sheet 01 Location of the wire harnesses Fig. A-GBGAA Sheet 01 installation orackets (a) For access to modification area, remove the insulation blankets, as shown on Fig. A-GBCAA Sheet 01 and Fig. A-GBGAA Sheet 01. (b) Between FR74 and FR75 LH, temporarily put in position: Bracket ABS0785B05B Item 2 refer to Fig. A-GBCAA Sheet 01 and Fig. A-GBGAA Sheet 01. (c) Transfer drill the pilot holes into the STGR7 LH. (d) For the rivets, open up all holes to the final diameter between 3.25 mm (0.1280 in) to 3.35 mm (0.1319 in), refer to SRM 51-44-11. (e) Remove the temporarily installed bracket item 2. (†) Deburr and clean the holes, refer to SRM 51-44-11 (g) Install as shown on Fig. A-GBGAA Sheet 01 : Bracket ABS0785B05B Item 2 with 2 Rivet EN6081AD4-06 Item 3 (h) Clean the work area between FR74 and FR75 at STGR7 LH. Apply the surface protection Anti-Corrosion 16-001 As required Primer (polyurethane) to the rivets, item 3. DATE: Jun 17/08 SERVICE BULLETIN No.: A340-92-4078 REVISION No.: 01 - Apr 09/10 Page: 32 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 43 (OCR) GA340 SERVICE BULLETIN (4) Subtask 924078-420-201-002 - Install the cable harness between FR74 and FR75, at STGR7 LH Manpower Resources Manhours 1.00 Minimum number of person Subtask elapsed time 1.00 Skills AIRFRAME Materlal necessary to do the job Kit 924078D03R02 TEM NEW PARTN QTY (UM) KEYWORD SEE NOTES NSA935401-04 10 TIE 4 E0660-01 MOUNT 5 NAS1149DN832K WASHER 6 NAS1801-08-8 SCREW 7 EN6049-006-25-5 2 (ME) SLEEVE 8 G9237320002200 2 PLACARD References Fig. A-GBCAA Sheet 01 Location of the wire harnesses Fig. A-GBJAA Sheet 01 installation insulation blankets, wire harnesses and cable ties (a) Install the insulation blanket, as shown on Fig. A-GBJAA Sheet 01. (b) Between FR74 and FR75, at STGR7 LH, install as shown on Fig. A-GBCAA Sheet 01 and Fig. A-GBJAA Sheet 01, Detail A : 2 Mount Item (4) Retained at removal 2 Washer Item (5) Retained at removal 2 Screw Item (6) Retained at removal (C) Between FR74 and FR75, at STGR7 LH, install as shown on Fig. A-GBCAA Sheet 01 and Fig. A-GBJAA Sheet 01, Detail B : 1 Mount E0660-01 Item 4 1 Washer NAS1149DN832K Item 5 1 Screw NAS1801-08-8 Item 6 DATE: Jun 17/08 SERVICE BULLETIN No.: A340-92-4078 REVISION No.: 01 - Apr 09/10 Page: 33 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 44 (OCR) GA340 SERVICE BULLETIN (a) On the cable harnesses, install as show on Fig. A-GBCAA Sheet 01 and Fig. A- GBJAA Sheet 01 : 2 (ME) Sleeve EN6049-006-25-5 Item 7 2 Placard G9237320002200 Item 8 10 Tie NSA935401-04 Item 1 (5) Subtask 924078-420-202-001 - Install the air-condition outlet LH. Work Zones and Access Panels Zone Access/Work location 2/0 Work location from Frame 74 to Frame 75 Rib 7LH Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills AIRFRAME Material necessary to do the job Kit 924078D03R02 ITEM NEW PARTN QTY (UM) KEYWORD I SEE NOTES 11 NAS1801-08-4 2 SCREW 12 NAS1149CN832R WASHER 13 F2528984503000 SUPPORT 14 ASNA0113-40ADL WASHER 17 NAS1801-08-6 SCREW References Fig. A-GBLAA Sheet 01 Installation of modify air-condition outlet On the door frame lining (271FW) LH, item 15, install as shown on Fig. A-GBLAA Sheet 01 : 2 Support F2528984503000 Item 13 2 Washer NAS1149CN832R Item 12 2 Screw NAS1801-08-4 Item 11 1 Air Outlet Item (10) Retained at removal 2 Washer ASNA0113-40ADL Item 14 6 DATE: Jun 17/08 SERVICE BULLETIN No.: A340-92-4078 REVISION No.: 01 - Apr 09/10 Page: 34 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 45 (OCR) GA340 SERVICE BULLETIN 2 Screw NAS1801-08-6 Item 17 (6) Subtask 924078-020-204-001 - Remove the air-condition outlet RH. Work Zones and Access Panels Zone Access/Work location 270 Work location from Frame 74 to Frame 75 Stringer 7RH Manpower Resources Manhours 0.25 Minimum number of person 1 Subtask elapsed time 0.25 Skills AIRFRAME References Fig. A-GBKAA Sheet 01 Removal of air-condition outlet (a) From the door frame lining (272FW) RH, item (15), remove as shown on Fig. A- GBKAA Sheet 01 : 2 Screw Item (11) Discard 2 Washer Item (12) Discard Air Outlet Item (10) Retain (7) Subtask 924078-020-203-001 - Remove the cable harnesses between FR74 and FR75, at STGR7 RH. Work Zones and Access Panels Zone Access/Work location 270 Work location from Frame 74 to Frame 75 Stringer 7RH Manpower Resources Manhours 0.25 Minimum number of person Subtask elapsed time 0.25 Skills AIRFRAME References Fig. A-GBCAA Sheet 01 Location of the wire harnesses Fig. A-GBEAA Sheet 01 Removal of cable ties, wire harnesses and insulation blankets DATE: Jun 17/08 SERVICE BULLETIN No.: A340-92-4078 REVISION No.: 01 - Apr 09/10 Page: 35 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 46 (OCR) DA340 SERVICE BULLETIN CAUTION: DO NOT DAMAGE THE WIRE HARNESSES WHEN YOU CUT THE CABLE-TIES. From the cable harnesses between FR74 and FR75 at STGR7 RH, remove as shown on Fig. A-GBCAA Sheet 01 and Fig. A-GBEAA Sheet 01: 4 Tie-Cable Item (1) Discard 2 Screw Item (6) Retain 2 Washer Item (5) Retain 2 Mount Item (4) Retain (8) Subtask 924078-831-203-002 - Modify the STGR7 RH between FR74 and FR75. Work Zones and Access Panels Zone Access/Work location 270 Work location from Frame 74 to Frame 75 Stringer 7RH Manpower Resources Manhours 1.00 Minimum number of person Subtask elapsed time 1.00 Skills AIRFRAME Material necessary to do the job Kit 924078D03R02 ITEM NEW PART N QTY (UM) KEYWORD SEE NOTES 2 ABS0785B05B BRACKET EN6081AD4-06 2 RIVET Consumable CMLD01 ITEM DESCRIPTION REFERENCE TO QTY PER A/C SEE CML MAT. No. NOTES Anti-Corrosion Primer 16-001 As required (polyurethane) References Structural Repair Manual (SRM) 51-44-11 Fig. A-GBCAA Sheet 01 Location of the wire harnesses Fig. A-GBGAA Sheet 01 Installation brackets 6 DATE: Jun 17/08 SERVICE BULLETIN No.: A340-92-4078 REVISION No.: 01 - Apr 09/10 Page: 36 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 47 (OCR) ©A340 SERVICE BULLETIN Reterences Fig. A-GBEAA Sheet 01 Removal of cable ties, wire harnesses and insulation blankets (a) For access to the modification area, remove the insulation blankets, as shown on Fig. A-GBCAA Sheet 01 and Fig. A-GBEAA Sheet 01. (b) Between FR74 and FR75 RH, temporarily put in position as shown on Fig. A- GBCAA Sheet 01 and Fig. A-GBGAA Sheet 01 : Bracket ABS0785B05B Item 2 (c) Transfer drill the pilot holes into the STGR7 RH. (d) For the rivets, open up all holes to final diameter between 3.25 mm (0.1280 in) to 3.35 mm (0.1319 in), refer to SRM 51-44-11. (e) Remove the temporarily installed bracket item 2. (†) Deburr and clean the holes, refer to SRM 51-44-11. (g) Install as shown on Fig. A-GBGAA Sheet 01 : Bracket ABS0785B05B Item 2 with 2 Rivet EN6081AD4-06 Item 3 (h) Clean the work area between FR74 and FR75 at STRG7 RH. Apply the surface protection Anti-Corrosion 16-001 As required Primer (polyurethane) to the rivets, item 3. (9) Subtask 924078-420-203-002 - Install the cable harnesses between FR74 and FR75, at STGR7 RH. Work Zones and Access Panels Zone Access/Work location 270 Work location from Frame 74 to Frame 75 Stringer 7RH 6 DATE: Jun 17/08 SERVICE BULLETIN No.: A340-92-4078 REVISION No.: 01 - Apr 09/10 Page: 37 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 48 (OCR) GA340 SERVICE BULLETIN Manpower Resources Manhours 1.00 Minimum number of person Subtask elapsed time 1.00 Skills AIRFRAME Material necessary to do the job Kit 924078D03 R02 TEM NEW PAREN QTY (UM) KEYWORD SEE NOTES NSA935401-04 10 TIE 4 E0660-01 MOUNT 5 NAS1149DN832K WASHER 6 NAS1801-08-8 SCREW EN6049-006-25-5 2 (ME) SLEEVE 8 G9237320002200 2 PLACARD References Fig. A-GBJAA Sheet 01 installation insulation blankets, wire harnesses and cable ties Fig. A-GBCAA Sheet 01 ocation of the wire harnesses (a) Install the insulation blanket, as shown on Fig. A-GBJAA Sheet 01. (b) Between FR74 and FR75 at STGR7 RH, install as shown on Fig. A-GBCAA Sheet 01 and Fig. A-GBJAA Sheet 01, Detail A : 2 Mount Item (4) Retained at removal 2 Washer Item (5) Retained at removal 2 Screw Item (6) Retained at removal (c) Between FR74 and FR75 at STGR7 RH, install as shown on Fig. A-GBCAA Sheet 01 and Fig. A-GBJAA Sheet 01, Detail B : 1 Mount E0660-01 Item 4 Washer NAS1149DN832K Item 5 Screw NAS1801-08-8 Item 6 DATE: Jun 17/08 SERVICE BULLETIN No.: A340-92-4078 REVISION No.: 01 - Apr 09/10 Page: 38 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 49 (OCR) ©A340 SERVICE BULLETIN On the cable harnesses, install as shown on Fig. A-GBCAA Sheet 01 and Fig. A- GBJAA Sheet 01: 2 (ME) Sleeve EN6049-006-25-5 Item 7 2 Placard G9237320002200 Item 8 10 Tie NSA935401-04 Item 1 (10) Subtask 924078-420-204-001 - Install the air-condition outlet RH. Work Zones and Access Panels Zone Access/Work location 270 Work location from Frame 74 to Frame 75 Stringer 7RH Manpower Resources Manhours 0.50 Minimum number of person Subtask elapsed time 0.50 Skills AIRFRAME Material necessary to do the job Kit 924078D03R02 ITEM NEW PART N QTY (UM) KEYWORD SEE NOTES 11 NAS1801-08-4 2 SCREW 12 NAS1149CN832R 2 WASHER 13 F2528984503000 2 SUPPORT 14 ASNA0113-40ADL 2 WASHER 17 NAS1801-08-6 2 SCREW References Fig. A-GBLAA Sheet 01 Installation of modify air-condition outlet (a) On the door frame lining (272FW) RH, item (15), install as shown on Fig. A-GBLAA Sheet 01 : 2 Support F2528984503000 Item 13 2 Washer NAS1149CN832R Item 12 2 Screw NAS1801-08-4 Item 11 1 Air Outlet Item (10) Retained at removal 2 Washer ASNA0113-40ADL Item 14 DATE: Jun 17/08 SERVICE BULLETIN No.: A340-92-4078 REVISION No.: 01 - Apr 09/10 Page: 39 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 50 (OCR) © A340 SERVICE BULLETIN 2 Screw NAS1801-08-6 Item 17 **CONF ALL D. TEST • **CONF 001 None **CONF 002 None **CONF ALL E. CLOSE-UP • **CONF 001 (1) Subtask 924078-942-201-001 - CLOSE-UP Work Zones and Access Panels Zone Access/Work location 270 Work location from Frame 74 to Frame 75 Manpower Resources Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 25-23-42-400-801 Task 25-23-47-400-801 (a) Make sure that the work area is clean and clear of tools and other equipment. Between FR74 and FR76 LH install the ceiling panels: 271EC, 271DC, 271FC, 271CC, refer to AMM Task 25-23-42-400-801. Between FR74 and FR76 install LH the door frame lining: 271FW, 271NW, refer to AMM Task 25-23-47-400-801. Between FR74 and FR76 RH install the ceiling panels: 272EC, 272DC, 272FC, 272CC, refer to AMM Task 25-23-42-400-801. Between FR74 and FR76 RH install the door frame lining: 272FW, 272NW, refer to AMM Task 25-23-47-400-801. DATE: Jun 17/08 SERVICE BULLETIN No.: A340-92-4078 REVISION No.: 01 - Apr 09/10 Page: 40 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved ### Page 51 (OCR) GA340 SERVICE BULLETIN **CONF 002 (1) Subtask 924078-942-201-001 - CLOSE-UP Work Zones and Access Panels Zone Access/Work location 270 Work location from Frame 74 to Frame 75 Manpower Resources Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 25-23-42-400-801 Task 25-23-47-400-801 (a) Make sure that the work area is clean and clear of tools and other equipment. Between FR74 and FR76 LH install the ceiling panels: 271EC, 271DC, 271FC, 271CC, refer to AMM Task 25-23-42-400-801. (c) Between FR74 and FR76 install LH the door frame lining: 271FW, 271NW, refer to AMM Task 25-23-47-400-801. Between FR74 and FR76 RH install the ceiling panels: 272EC, 272DC, 272FC, 272CC, refer to AMM Task 25-23-42-400-801. (e) Between FR74 and FR76 RH install the door frame lining: 272FW, 272NW, refer to AMM Task 25-23-47-400-801. 6 DATE: Jun 17/08 SERVICE BULLETIN No.: A340-92-4078 REVISION No.: 01 - Apr 09/10 Page: 41 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 52 (OCR) ©A340 SERVICE BULLETIN This Page Intentionally Left Blank 6 DATE: Jun 17/08 SERVICE BULLETIN No.: A340-92-4078 REVISION No.: 01 - Apr 09/10 Page: 42 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 53 (OCR) ©A340 SERVICE BULLETIN Task 924078-831-849-001 - MODIFICATION - ADDITIONAL WORK **CONF ALL WARNING: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONS INCLUDED IN THE REFERENCED PROCEDURES. CAUTION: 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 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 **CONF 001 Zone 270 Manpower TOTAL MANHOURS 1.00 ELAPSED TIME (HOURS) 1.00 **CONF 002 Zone 270 Manpower TOTAL MANHOURS 0.75 ELAPSED TIME (HOURS) 11.00 6 DATE: Jun 17/08 SERVICE BULLETIN No.: A340-92-4078 REVISION No.: 01 - Apr 09/10 Page: 43 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 54 (OCR) ©A340 SERVICE BULLETIN **CONF ALL A. GENERAL **CONF 001 (1) Subtask 924078-910-202-001 - Standard Practices Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-30-00, Page Block 001 06-31-53, Page Block 001 06-41-53, Page Block 001 Standards Manual (SM) (a) 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 Airbus Standards Manual (SM). The SM will give you the correct part number to part number relationship. (b) For Frame (FR) identification refer to AMM 06-31-53, Page Block 001. (c) For identification of Stringers (STGR), refer to AMM 06-30-00, Page Block 001. (d) For ceiling panel identification, refer to AMM 06-41-53, Page Block 001. (2) Subtask 924078-839-202-001 - Documentation Manpower Resources Skills NON SPECIFIC Write in the applicable aircraft records that you have done all the work given in this Service Bulletin. **CONF 002 (1) Subtask 924078-910-202-001 - Standard Practices Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-30-00, Page Block 001 06-31-53, Page Block 001 06-41-53, Page Block 001 Standards Manual (SM) 6 DATE: Jun 17/08 SERVICE BULLETIN No.: A340-92-4078 REVISION No.: 01 - Apr 09/10 Page: 44 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 55 (OCR) G A340 SERVICE BULLETIN (a) 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 Airbus Standards Manual (SM). The SM will give you the correct part number to part number relationship. (b) For Frame (FR) identification refer to AMM 06-31-53, Page Block 001. (c) For identification of Stringers (STGR), refer to AMM 06-30-00, Page Block 001. (d) For ceiling panel identification, refer to AMM 06-41-53, Page Block 001. (2) Subtask 924078-839-202-001 - Documentation Manpower Resources Skills NON SPECIFIC Write in the applicable aircraft records that you have done all the work given in this Service Bulletin. **CONF ALL B. PREPARATION **CONF 001 (1) Subtask 924078-941-202-001 - Job Set-up Manpower Resources Skills CABIN References Aircraft Maintenance Manual (AMM) Task 12-34-24-860-801 Task 25-23-42-000-801 (a) Make sure that the aircraft is in electrically grounded (Refer to AMM Task 12-34-24-860-801). (b) For access remove the decor panels 271CC, 271DC, 272CC and 272DC (Refer to AMM Task 25-23-42-000-801). **CONF 002 (1) Subtask 924078-941-202-001 - Job Set-up Manpower Resources Skills CABIN References Aircraft Maintenance Manual (AMM) Task 12-34-24-860-801 Task 25-23-42-000-801 (a) Make sure that the aircraft is in electrically grounded (Refer to AMM Task 12-34-24-860-801). 6 DATE: Jun 17/08 SERVICE BULLETIN No.: A340-92-4078 REVISION No.: 01 - Apr 09/10 Page: 45 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 56 (OCR) GA340 SERVICE BULLETIN For access remove the decor panels 271CC, 271DC, 272CC and 272DC (Refer to AMM Task 25-23-42-000-801). **CONF ALL C. PROCEDURE **CONF 001 (1) Subtask 924078-831-204-001 - Modification of the Support Assembly of the Air Outlet Manpower Resources Manhours 0.50 Minimum number of person Subtask elapsed time 0.50 Skills CABIN Material necessary to do the job Kit 924078D04R00 HEM NEW PARTIN QTY (UM) KEYWORD SEE NOTES NAS1801-08-8 4 SCREW 16 F2528984503200 4 SUPPORT NOTE: Kit 924078D04R00 has been created as a differential Kit of Kit 924078D01R00 and Kit 924078D01R04. This new Kit has to be ordered by operators which have already received two Kits 924078D01R00 and for ADDITIONAL WORK. References Fig. A-GANAA Sheet 01 ADDITIONAL WORK: Modification of the Support Assembly of the Air Outlet Fig. A-GAPAA Sheet 01 ADDITIONAL WORK: Modification of the Support Assembly of the Air Outlet (a) On the door frame lining (271FW) LH, item (15), remove as shown on Fig. A- GANAA Sheet 01 : 2 Screw Item (11) Discard 2 Washer Item (14) Retain Support Assy Item (13) Discard 1 Box Assy-Air Outlet Item (10) Retain 2 Screw Item (11) Retain 6 DATE: Jun 17/08 SERVICE BULLETIN No.: A340-92-4078 REVISION No.: 01 - Apr 09/10 Page: 46 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 57 (OCR) DA340 SERVICE BULLETIN 2 Washer Item (12) Retain On the door frame lining (271FW) LH, item (15), install as shown on Fig. A-GAPAA Sheet 01 : 2 Support F2528984503200 Item 16 2 Washer Item (12) Retained at removal 2 Screw Item (11) Retained at removal 1 Box Assy-Air Outlet Item (10) Retained at removal 2 Washer Item (14) Retained at removal 2 Screw NAS1801-08-8 Item 6 (c) On the door frame lining (272FW) RH, item (15), remove as shown on Fig. A- GANAA Sheet 01 : 2 Screw Item (11) Discard 2 Washer Item (14) Retain 1 Support Assy Item (13) Discard Box Assy-Air Outlet Item (10) Retain 2 Screw Item (11) Retain 2 Washer Item (12) Retain (a) On the door frame lining (272FW) RH, item (15), install as shown on Fig. A-GAPAA Sheet 01 : Support F2528984503200 Item 16 2 Washer Item (12) Retained at removal 2 Screw Item (11) Retained at removal 1 Box Assy-Air Outlet Item (10) Retained at removal DATE: Jun 17/08 SERVICE BULLETIN No.: A340-92-4078 REVISION No.: 01 - Apr 09/10 Page: 47 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved ### Page 58 (OCR) GA340 SERVICE BULLETIN 2 Washer Item (14) Retained at removal 2 Screw NAS1801-08-8 Item 6 **CONF 002 (1) Subtask 924078-831-204-002 - Exchange the screws for the Air Outlet Box Assembly Manpower Resources Manhours 0.25 Minimum number of person Subtask elapsed time 0.25 Skills CABIN Material necessary to do the job Kit 924078D03R02 TEM NEW PARTN QTY (UM) KEYWORD SEE NOTES 17 NAS1801-08-6 4 SCREW References Fig. A-GANAB Sheet 01 ADDITIONAL WORK: Exchange of the screws for the Air Outlet Вох Assembly Fig. A-GAPAB Sheet 01 ADDITIONAL WORK: Exchange of the screws for the Air Outlet Box Assembly (a) On the door frame lining (271FW) LH, item (15), remove as shown on Fig. A- GANAB Sheet 01 : 2 Screw Item (11) Discard 2 Washer Item (14) Retain 1 Box Assy-Air Outlet Item (10) Retain (b) On the door frame lining (271FW) LH, item (15), install as shown on Fig. A-GAPAB Sheet 01 : 1 Box Assy-Air Outlet Item (10) Retained at removal 2 Washer Item (14) Retained at removal 2 Screw NAS1801-08-6 Item 17 6 DATE: Jun 17/08 SERVICE BULLETIN No.: A340-92-4078 REVISION No.: 01 - Apr 09/10 Page: 48 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 59 (OCR) GA340 SERVICE BULLETIN On the door frame lining (272FW) RH, item (15), remove as shown on Fig. A- GANAB Sheet 01 : 2 Screw Item (11) Discard 2 Washer Item (14) Retain 1 Box Assy-Air Outlet Item (10) Retain On the door frame lining (272FW) RH, item (15), install as shown on Fig. A-GAPAB Sheet 01 : Box Assy-Air Outlet Item (10) Retained at removal 2 Washer Item (14) Retained at removal 2 Screw NAS1801-08-6 Item 17 **CONF ALL D. TEST **CONF 001 None **CONF 002 None **CONF ALL E. CLOSE-UP **CONF 001 (1) Subtask 924078-942-202-001 - Close-up Work Zones and Access Panels Zone Access/Work location 270 Work location from Frame 74 to Frame 75 Stringer 7 LH/RH Manpower Resources Skills CABIN References Aircraft Maintenance Manual (AMM) Task 25-23-42-400-801 DATE: Jun 17/08 SERVICE BULLETIN No.: A340-92-4078 REVISION No.: 01 - Apr 09/10 Page: 49 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 60 (OCR) DA340 SERVICE BULLETIN (a) Make sure that the work area is clean and clear of tools and other item of equipment. Install the decor panels 271CC, 271DC, 272CC and 272DC (Refer to AMM Task 25-23-42-400-801). **CONF 002 (1) Subtask 924078-942-202-001 - Close-up Work Zones and Access Panels Zone Access/Work location 270 Work location from Frame 74 to Frame 75 Stringer 7 LH/RH Manpower Resources Skills CABIN References Aircraft Maintenance Manual (AMM) Task 25-23-42-400-801 (a) Make sure that the work area is clean and clear of tools and other item of equipment. Install the decor panels 271CC, 271DC, 272CC and 272DC (Refer to AMM Task 25-23-42-400-801). 6 DATE: Jun 17/08 SERVICE BULLETIN No.: A340-92-4078 REVISION No.: 01 - Apr 09/10 Page: 50 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. The text continues at https://openairdocs.org/service-documents/airbus/a340-92-4078/file/b729df1745c5.md?from=61 --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain, except the copies of manufacturers’ service documents, which belong to their rights holders.