# @A340 SERVICE BULLETIN SUMMARY AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Tel : (33) 5 61 93 33 33 Telex : AIRBU 530526F Fax : (33) 5 61 93 42 51 This summary is for information only and is not approved for modification of the aircraft. 

# MANDATORYMANDATORYMANDATORY ATA SYSTEM: 92 

### TITLE: ELECTRIC AND ELECTRONIC COMMON INSTALLATION - GENERAL - RE-ROUTING OF HARNESSES AT DOOR 3 AREA, LH AND RH SIDE **CONF ALL MODIFICATIONS MODIFICATION CLASSIFICATION MAJOR 201669S31758 MINOR 202319S32230 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 During aircraft production, potential contact between hatrack rod and harness 1523VB at Left Hand side (LH) and 1524VB Right Hand side (RH) between frame Frame 53.6 and Frame 53.8 and , between Stringer 14 and Stringer 15 has been identified. No findings have been reported from in-service aircraft. This contact could generate a chafing on the wirings leading to a potential effect on the oxygen container opening. This Service Bulletin requests the modification of the routing of the harnesses 1523VB (LH) and 1524VB (RH) at the level of the door 3 area LH and RH side. Accomplishment of this Service Bulletin will contribute to prevent potential wire chafing between the harnesses 1523VB (LH)/1524VB (RH) and the hatrack rods. 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 COST SAVING NO LROPS AFFECTED NO STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED NO
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# @A340 SERVICE BULLETIN SUMMARY 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 924084A01R00 1 527.00 Ramp assy, Wiring ramp Kit 924084A02R00 1 530.00 Ramp assy, Wiring ramp TOTAL 1,057.00 EFFECTIVITY This Service Bulletin is applicable to this (these) operator(s) :

FIN SAA SVW SWR CONCURRENT REQUIREMENTS None REFERENCES / REPERCUSSIONS TFU None OEB None AOT None SIL None LINE MAINTENANCE AFFECTED No LIFE LIMIT None OTHER None NATURE OF THE WORK AIRCRAFT YES EQUIPMENT NO HARD NO SOFT NO OBRM NO MANPOWER Task 924084-831-801-001: Modification TOTAL MANHOURS 6.00 ELAPSED TIME (HOURS) 3.00 APPENDICES Appendix 01 - Elapsed Time Assumption

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# @A340 SERVICE BULLETIN SUMMARY

**CONF ALL

STGR12L

STGR14L 

### A

LH SIDE SHOWN RH SIDE SYMMETRICAL 

## B **FWD** 

## A

STGR17L Z844

Z834



## BEFORE
FR53.9 FR53.8 FR53.7 FR53.6

1M 2M

55LG (56LG) 2M

FR53.5 FR53.9 

### B **C**

**B C** 

F_SB_924084_5_SAAA_01_00 Figure A-FSAAA - Sheet 01

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# @A340 SERVICE BULLETIN SUMMARY

**CONF ALL

STGR12L

STGR14L

LH SIDE SHOWN RH SIDE SYMMETRICAL **FWD** 

## AFTER

FR53.9 FR53.6 2M

2M 55LG (56LG)

INSTALL INSTALL RAMP ASSY

1M


## C WIRING RAMP

FR53.8

F_SB_924084_5_SAAA_02_00 Figure A-FSAAA - Sheet 02

DATE: Jan 11/13 SERVICE BULLETIN No.: A340-92-4084 REVISION No.: 00 - Jan 11/13 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



# MANDATORYMANDATORYMANDATORY ATA SYSTEM: 92 

### TITLE: ELECTRIC AND ELECTRONIC COMMON INSTALLATION - GENERAL - RE-ROUTING OF HARNESSES AT DOOR 3 AREA, LH AND RH SIDE MODIFICATION No.: 201669S31758 202319S32230 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 NOTE: This Service Bulletin is applicable only to aircraft on which Mod. No. 40161D17512 (INTRODUCE "TYPE A DOOR") is not embodied and on which Mod. No. 48825D42865 (DEFINE AND DESIGN ADAPTATIONS FOR CABIN COMPONENTS DUE TO ENHANCEMENT PROGRAM) is embodied. This Service Bulletin is not applicable on aircraft on which Mod. No. 55606D51404 is embodied (INSTALL A GASEOUS OXYGEN SYSTEM FOR A340-300 ENHANCED). (1) Models 340-313 (2) Effectivity by MSN 0544 0582 0585 0590 0598 0643 0646 0651 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 FIN 0921 0938 SAA 0544 0582 0590 0643 0646 0651 SVW 0955 SWR 0585 0598 (4) Configuration by MSN MSN CONFIGURATION 0544 0582 0585 0590 0598 0643 0646 0651 0921 0938 0955 001 (5) Configuration definition **CONF 001 Config. 001 is valid for all the aircraft given in the effectivity of this Service Bulletin as a standard configuration. (6) Material Effectivity MATERIAL QTY PER A/C SEE NOTES Kit 924084A01R00 1 Kit 924084A02R00 1 B. CONCURRENT REQUIREMENTS None C. REASON (1) History During aircraft production, potential contact between hatrack rod and harness 1523VB at Left Hand side (LH) and 1524VB Right Hand side (RH) between frame Frame 53.6 and Frame 53.8 and , between Stringer 14 and Stringer 15 has been identified. No findings have been reported from in-service aircraft. This contact could generate a chafing on the wirings leading to a potential effect on the oxygen container opening. (2) Objective/Action This Service Bulletin requests the modification of the routing of the harnesses 1523VB (LH) and 1524VB (RH) at the level of the door 3 area LH and RH side. (3) Advantages Accomplishment of this Service Bulletin will contribute to prevent potential wire chafing between the harnesses 1523VB (LH)/1524VB (RH) and the hatrack rods. DATE: Jan 11/13 SERVICE BULLETIN No.: A340-92-4084 REVISION No.: 00 - Jan 11/13 Page: 2 5

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# @A340 SERVICE BULLETIN (4) Operational/Maintenance Consequences None D. DESCRIPTION To accomplish this Service Bulletin it is necessary to : Task 924084-831-801-001: Modification (1) Remove the brackets of the Routes 1M and 2M between FR53.6 and FR53.8, LH Side (2) Remove the brackets of the Routes 1M and 2M between FR53.6 and FR53.8, RH Side (3) Install the Ramp assy and the Wiring Ramp between FR53.6 and FR53.8, LH Side (4) Install the Ramp assy and the Wiring Ramp between FR53.6 and FR53.8, RH Side (5) Modify the routing of the routes 1M and 2M between FR53.6 and FR53.8, LH Side (6) Modify the routing of the routes 1M and 2M between FR53.6 and FR53.8, RH Side E. COMPLIANCE (1) Classification MANDATORY: Service Bulletin must be accomplished. (2) Accomplishment Timescale This Service Bulletin has been classified Mandatory. It is expected that an Airworthiness Directive (AD) published by the European Aviation Safety Agency (EASA) will be issued to confirm this classification. The accomplishment timescale, which has not yet been defined, will be given in the AD. F. APPROVAL The technical content of this document is approved under the authority of Design Organisation Approval No. EASA.21J.031. If an aircraft listed in the effectivity has a modification or repair embodied that is not of AIRBUS origin, and which affects the content of this Service Bulletin, the operator is responsible for obtaining approval by its airworthiness authority for any adaptation necessary before incorporation of the Service Bulletin.

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# @A340 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 924084-831-801-001: Modification Get Access 1.00 On Aircraft Remove the brackets of the Routes 1M and 2M between FR53.6 and FR53.8, LH Side 0.50 Remove the brackets of the Routes 1M and 2M between FR53.6 and FR53.8, RH Side 0.50 Install the Ramp assy and the Wiring Ramp between FR53.6 and FR53.8, LH Side 1.00 Install the Ramp assy and the Wiring Ramp between FR53.6 and FR53.8, RH Side 1.00 Modify the routing of the routes 1M and 2M between FR53.6 and FR53.8, LH Side 0.50 Modify the routing of the routes 1M and 2M between FR53.6 and FR53.8, RH Side 0.50 Close-Up 1.00 TOTAL MANHOURS 6.00 ELAPSED TIME (HOURS) 3.00 H. WEIGHT AND BALANCE Not Changed I. ELECTRICAL LOAD DATA Not Changed J. REFERENCES

Aircraft Maintenance Manual (AMM) 06-20-00 06-31-53 12-34-24 52-10-00 Elec. Std. Practices Manual (ESPM) 20-25-51 20-33-44 20-53-00 20-55-00 Standards Manual (SM) Structural Repair Manual (SRM) 51-42-00 51-43-00 K. PUBLICATION AFFECTED None L. INTERCHANGEABILITY/MIXABILITY Not Applicable DATE: Jan 11/13 SERVICE BULLETIN No.: A340-92-4084 REVISION No.: 00 - Jan 11/13 Page: 4 5

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# @A340 SERVICE BULLETIN
M. SPARES None

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# @A340 SERVICE BULLETIN

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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 924084A01R00 Kit 924084A02R00 AIRBUS Material, Logistics and Suppliers Weg beim Jaeger 150 D-22335 HAMBURG GERMANY For ordering by internet: http://spares.airbus.com For ordering by fax: +49 40 50 76 2590 For ordering by E-mail: airbus.kit@airbus.com (2) Price and Availability

Kit 924084A01R00 Cost 527.00 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 items are required before this time, please include a retrofit planning schedule with your order so that we can try to comply with your requirements. The sales terms (costs and availability) are estimated in relation to economic conditions. The latest valid price and lead time for ordering purposes shall be obtained through the AirbusSpares portal or through a request for quotation to airbus.kit@airbus.com. Kit 924084A02R00 Cost 530.00 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 items are required before this time, please include a retrofit planning schedule with your order so that we can try to comply with your requirements. The sales terms (costs and availability) are estimated in relation to economic conditions. The latest valid price and lead time for ordering purposes shall be obtained through the AirbusSpares portal or through a request for quotation to airbus.kit@airbus.com. B. INDUSTRY SUPPORT INFORMATION Airbus will provide the kits at no charge for orders placed before Dec 31/15. For aircraft under warranty at Jul 01/10, Airbus will credit the manhours indicated in this Service Bulletin at the agreed in-house warranty labor rate for claims received not later than 90 days after completion of the last affected aircraft of your fleet.

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# @A340 SERVICE BULLETIN
C. LIST OF COMPONENTS Kit 924084A01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 3 NAS1149F0332P 10 WASHER 8 NSA5050-3 5 NUT 12 NSA935504-03 1 BRACKET 18 NAS1801-3-7 3 SCREW 20 NSA5527-03-13 2 SPACER 21 NSA5159-19 1 STUD 22 NSA5527-03-12 1 SPACER 23 NSA5159-23 1 STUD 24 NSA5527-03-03 1 SPACER 25 NAS1801-3-20 2 SCREW 29 F9241964500000 1 RAMP 31 F9241965000000 1 RAMP 37 NSA5516-06ND 5 CLAMP 38 NSA5516-07ND 5 CLAMP 39 NSA5516-08ND 5 CLAMP NSA935401-03 10 TIE NSA935401-05 10 TIE NSA935401-08 10 TIE 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 924084A02R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 3 NAS1149F0332P 10 WASHER 8 NSA5050-3 5 NUT 12 NSA935504-03 1 BRACKET 18 NAS1801-3-7 3 SCREW 20 NSA5527-03-13 2 SPACER 21 NSA5159-19 1 STUD 22 NSA5527-03-12 1 SPACER 23 NSA5159-23 1 STUD 24 NSA5527-03-03 1 SPACER 25 NAS1801-3-20 2 SCREW 30 F9241964500100 1 RAMP 31 F9241965000000 1 RAMP 37 NSA5516-06ND 5 CLAMP 38 NSA5516-07ND 5 CLAMP 39 NSA5516-08ND 5 CLAMP NSA935401-03 10 TIE DATE: Jan 11/13 SERVICE BULLETIN No.: A340-92-4084 REVISION No.: 00 - Jan 11/13 Page: 8 5

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# @A340 SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES NSA935401-05 10 TIE NSA935401-08 10 TIE NOTE: If you find part numbers of hardware components in the related kit(s) which you cannot identify in the LIST OF COMPONENTS of this Service Bulletin, refer to Standards Manual (SM). The SM will give you the correct part number to part number relationship. D. LIST OF MATERIALS - OPERATOR SUPPLIED None E. PARTS TO BE RE-IDENTIFIED BY OPERATOR None F. TOOLING None

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# @A340 SERVICE BULLETIN

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# @A340 SERVICE BULLETIN
3. ACCOMPLISHMENT INSTRUCTIONS Task 924084-831-801-001 - 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. IN CASE OF CONTAMINATION REFER TO ESPM 20-55-00. Task Associated Data Zone 834 844 Access Door 832 842 Manpower TOTAL MANHOURS 6.00 ELAPSED TIME (HOURS) 3.00 A. GENERAL (1) Subtask 924084-910-001-001 - Standard Practices Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-20-00, Page Block 001 06-31-53, Page Block 001 Elec. Std. Practices Manual (ESPM) 20-25-51 20-33-44 20-53-00 Structural Repair Manual (SRM) 51-42-00 51-43-00 (a) For the Frame (FR) identification, refer to AMM 06-31-53, Page Block 001. DATE: Jan 11/13 SERVICE BULLETIN No.: A340-92-4084 REVISION No.: 00 - Jan 11/13 Page: 11 5

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# @A340 SERVICE BULLETIN (b) For the identification of zones, refer to AMM 06-20-00, Page Block 001. (c) Remove and install fasteners in accordance with SRM 51-42-00. (d) Obtain alternative and substitute fastener data, in accordance with SRM 51-43-00. (e) For the cable tie application and tooling, refer to ESPM 20-33-44 and ESPM 20-25-51. (f) For Electrical Items inspection/check refer to ESPM 20-53-00. (2) Subtask 924084-839-001-001 - 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 924084-941-001-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 12-34-24-860-002 Task 52-10-00-010-801 (a) Make sure that the aircraft is electrically grounded (Refer to AMM Task 12-34-24-860-002). (b) Put access platform(s) in position at doors 832 or 842. (c) Open the passenger/crew door 832 or 842 (Refer to AMM Task 52-10-00-010-801). (2) Subtask 924084-010-001-001 - Remove the Door Frame Linings between FR53.5 and FR53.8, LH Side Work Zones and Access Panels Zone Access/Work location 834 Access Door 832 Manpower Resources Skills NON SPECIFIC References Fig. A-FBBAA Removal/Installation of the Door Frame linings between FR53.5 and FR53.8 Sheet 01

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# @A340 SERVICE BULLETIN (a) Remove the door frame linings between FR53.5 and FR53.8, LH Side: Refer to Fig. A-FBBAA Sheet 01 1 Door Frame Lining Item (32) Retain 1 Door Frame Lining Item (34) Retain 1 Door Frame Lining Item (35) Retain

(3) Subtask 924084-010-002-001 - Remove the Door Frame Linings between FR53.5 and FR53.8, RH Side Work Zones and Access Panels Zone Access/Work location 844 Access Door 842 Manpower Resources Skills NON SPECIFIC References Fig. A-FBBAA Removal/Installation of the Door Frame linings between FR53.5 and FR53.8 Sheet 01
(a) Remove the door frame linings between FR53.5 and FR53.8, RH Side: Refer to Fig. A-FBBAA Sheet 01 1 Door Frame Lining Item (33) Retain 1 Door Frame Lining Item (34) Retain 1 Door Frame Lining Item (36) Retain C. PROCEDURE (1) Subtask 924084-831-001-001 - Remove the brackets of the Routes 1M and 2M between FR53.6 and FR53.8, LH Side Work Zones and Access Panels Zone Access/Work location 834 Access Door 832 Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills AIRFRAME

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# @A340 SERVICE BULLETIN
References Structural Repair Manual (SRM) 51-42-00 Fig. A-FBAAA Installation of the Ramp Assy and the Wiring Ramp between FR53.6 and FR53.8 Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 (a) Remove the brackets as shown on Fig. A-FBAAA Sheet 01 and Fig. A-FBAAA Sheet 02, Details D and E. In accordance with SRM 51-42-00: 1 Remove the existing mountings as shown on detail D on Fig. A-FBAAA Sheet 02: a If the existing mountings are as shown in case 1: <1> Remove: 2 Screw Item (4) Discard 2 Bracket Item (2) Discard 2 Spacer Item (1) Discard 2 Washer Item (3) Discard b If the existing mountings are as shown in case 2: <1> Remove: 2 Screw Item (7) Discard 2 Bracket Item (2) Discard 2 Spacer Item (1) Discard 2 Washer Item (3) Discard 2 Nut Item (8) Discard 2 Remove the existing mounting as shown on detail E on Fig. A-FBAAA Sheet 02: a If the existing mounting is as shown in case 1: <1> Remove: 1 Screw Item (4) Discard

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# @A340 SERVICE BULLETIN 2 Bracket Item (2) Discard 1 Spacer Item (6) Discard 1 Washer Item (3) Discard 1 Nut Item (17) Discard b If the existing mounting is as shown in case 2: <1> Remove: 1 Screw Item (4) Discard 1 Bracket Item (2) Discard 1 Spacer Item (1) Discard 1 Washer Item (3) Discard
c If the existing mounting is as shown in case 3: <1> Remove: 1 Screw Item (7) Discard 1 Bracket Item (2) Discard 1 Spacer Item (1) Discard 1 Washer Item (3) Discard 1 Nut Item (8) Discard NOTE: There is no need to disconnect the harness. (2) Subtask 924084-831-002-001 - Remove the brackets of the Routes 1M and 2M between FR53.6 and FR53.8, RH Side Work Zones and Access Panels Zone Access/Work location 844 Access Door 842 Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills AIRFRAME

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# @A340 SERVICE BULLETIN
References Structural Repair Manual (SRM) 51-42-00 Fig. A-FBAAA Installation of the Ramp Assy and the Wiring Ramp between FR53.6 and FR53.8 Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 (a) Remove the brackets as shown on Fig. A-FBAAA Sheet 01 and Fig. A-FBAAA Sheet 02, Details D and E. In accordance with SRM 51-42-00: 1 Remove the existing mountings as shown on detail D on Fig. A-FBAAA Sheet 02: a If the existing mountings are as shown in case 1: <1> Remove: 2 Screw Item (4) Discard 2 Bracket Item (2) Discard 2 Spacer Item (1) Discard 2 Washer Item (3) Discard b If the existing mountings are as shown in case 2: <1> Remove: 2 Screw Item (7) Discard 2 Bracket Item (2) Discard 2 Spacer Item (1) Discard 2 Washer Item (3) Discard 2 Nut Item (8) Discard 2 Remove the existing mounting as shown on detail E on Fig. A-FBAAA Sheet 02: a If the existing mounting is as shown in case 1: <1> Remove: 1 Screw Item (4) Discard

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# @A340 SERVICE BULLETIN 2 Bracket Item (2) Discard 1 Spacer Item (6) Discard 1 Washer Item (3) Discard 1 Nut Item (17) Discard b If the existing mounting is as shown in case 2: <1> Remove: 1 Screw Item (4) Discard 1 Bracket Item (2) Discard 1 Spacer Item (1) Discard 1 Washer Item (3) Discard
c If the existing mounting is as shown in case 3: <1> Remove: 1 Screw Item (7) Discard 1 Bracket Item (2) Discard 1 Spacer Item (1) Discard 1 Washer Item (3) Discard 1 Nut Item (8) Discard NOTE: There is no need to disconnect the harness. (3) Subtask 924084-831-003-001 - Install the Ramp assy and the Wiring Ramp between FR53.6 and FR53.8, LH Side Work Zones and Access Panels Zone Access/Work location 834 Access Door 832 Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills AIRFRAME

DATE: Jan 11/13 SERVICE BULLETIN No.: A340-92-4084 REVISION No.: 00 - Jan 11/13 Page: 17 5

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# @A340 SERVICE BULLETIN Material necessary to do the job Kit 924084A01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 3 NAS1149F0332P 7 WASHER 8 NSA5050-3 5 NUT 12 NSA935504-03 1 BRACKET 18 NAS1801-3-7 2 SCREW 21 NSA5159-19 1 STUD 22 NSA5527-03-12 1 SPACER 23 NSA5159-23 1 STUD 24 NSA5527-03-03 1 SPACER 29 F9241964500000 1 RAMP 31 F9241965000000 1 RAMP References Elec. Std. Practices Manual (ESPM) 20-53-00 Structural Repair Manual (SRM) 51-42-00 51-43-00 Fig. A-FBAAA Installation of the Ramp Assy and the Wiring Ramp between FR53.6 and FR53.8 Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 (a) Install the ramp assy and the wiring ramp between FR53.6 and FR53.8, LH side: Refer to Fig. A-FBAAA Sheet 03 and Fig. A-FBAAA Sheet 04

. In accordance with SRM 51-42-00 and SRM 51-43-00: NOTE: Before Installation of the mountings inspect the cables, refer to ESPM 20-53-00. 1 Install the ramp assy as shown on Fig. A-FBAAA Sheet 01, Fig. A-FBAAA Sheet 03 and Fig. A-FBAAA Sheet 04: 1 Ramp Assy F9241964500000 Item 29 attach with: 2 Screw NAS1801-3-7 Item 18 2 Washer NAS1149F0332P Item 3 2 Nut NSA5050-3 Item 8 2 Install the wiring ramp: 1 Ramp F9241965000000 Item 31 DATE: Jan 11/13 SERVICE BULLETIN No.: A340-92-4084 REVISION No.: 00 - Jan 11/13 Page: 18 5

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# @A340 SERVICE BULLETIN attach with the mounting as shown on Fig. A-FBAAA Sheet 03 and Fig. AFBAAA Sheet 04, Detail G: 1 Stud NSA5159-23 Item 23 1 Spacer NSA5527-03-03 Item 24 2 Washer NAS1149F0332P Item 3 1 Nut NSA5050-3 Item 8 3 Attach the ramp assy and the wiring ramp with the mounting as shown on Fig. A-FBAAA Sheet 04, Detail H: 1 Stud NSA5159-19 Item 21 1 Bracket NSA935504-03 Item 12 3 Washer NAS1149F0332P Item 3 1 Spacer NSA5527-03-12 Item 22 2 Nut NSA5050-3 Item 8

(4) Subtask 924084-831-004-001 - Install the Ramp assy and the Wiring Ramp between FR53.6 and FR53.8, RH Side Work Zones and Access Panels Zone Access/Work location 844 Access Door 842 Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills AIRFRAME Material necessary to do the job Kit 924084A02R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 3 NAS1149F0332P 7 WASHER 8 NSA5050-3 5 NUT 12 NSA935504-03 1 BRACKET 18 NAS1801-3-7 2 SCREW 21 NSA5159-19 1 STUD 22 NSA5527-03-12 1 SPACER 23 NSA5159-23 1 STUD 24 NSA5527-03-03 1 SPACER DATE: Jan 11/13 SERVICE BULLETIN No.: A340-92-4084 REVISION No.: 00 - Jan 11/13 Page: 19 5

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# @A340 SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 30 F9241964500100 1 RAMP 31 F9241965000000 1 RAMP References Elec. Std. Practices Manual (ESPM) 20-53-00 Structural Repair Manual (SRM) 51-42-00 51-43-00 Fig. A-FBAAA Installation of the Ramp Assy and the Wiring Ramp between FR53.6 and FR53.8 Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 (a) Install the ramp assy and the wiring ramp between FR53.6 and FR53.8, RH side: Refer to Fig. A-FBAAA Sheet 03 and Fig. A-FBAAA Sheet 04

. In accordance with SRM 51-42-00 and SRM 51-43-00: NOTE: Before Installation of the mountings inspect the cables, refer to ESPM 20-53-00. 1 Install the ramp assy as shown on Fig. A-FBAAA Sheet 01, Fig. A-FBAAA Sheet 03 and Fig. A-FBAAA Sheet 04: 1 Ramp Assy F9241964500100 Item 30 attach with: 2 Screw NAS1801-3-7 Item 18 2 Washer NAS1149F0332P Item 3 2 Nut NSA5050-3 Item 8 2 Install the wiring ramp: 1 Ramp F9241965000000 Item 31 attach with the mounting as shown on Fig. A-FBAAA Sheet 03 and Fig. AFBAAA Sheet 04, Detail G: 1 Stud NSA5159-23 Item 23 1 Spacer NSA5527-03-03 Item 24 2 Washer NAS1149F0332P Item 3 1 Nut NSA5050-3 Item 8

DATE: Jan 11/13 SERVICE BULLETIN No.: A340-92-4084 REVISION No.: 00 - Jan 11/13 Page: 20 5

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# @A340 SERVICE BULLETIN
3 Attach the ramp assy and the wiring ramp with the mounting as shown on Fig. A-FBAAA Sheet 04, Detail H: 1 Stud NSA5159-19 Item 21 1 Bracket NSA935504-03 Item 12 3 Washer NAS1149F0332P Item 3 1 Spacer NSA5527-03-12 Item 22 2 Nut NSA5050-3 Item 8

(5) Subtask 924084-831-007-001 - Modify the routing of the routes 1M and 2M between FR53.6 and FR53.8, LH Side Work Zones and Access Panels Zone Access/Work location 834 Access Door 832 Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills AIRFRAME Material necessary to do the job Kit 924084A01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 3 NAS1149F0332P 3 WASHER 18 NAS1801-3-7 1 SCREW 20 NSA5527-03-13 2 SPACER 25 NAS1801-3-20 2 SCREW 37 NSA5516-06ND 5 CLAMP 38 NSA5516-07ND 5 CLAMP 39 NSA5516-08ND 5 CLAMP NSA935401-03 10 TIE NSA935401-05 10 TIE NSA935401-08 10 TIE References Elec. Std. Practices Manual (ESPM) 20-53-00 Structural Repair Manual (SRM) 51-42-00 51-43-00

DATE: Jan 11/13 SERVICE BULLETIN No.: A340-92-4084 REVISION No.: 00 - Jan 11/13 Page: 21 5

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# @A340 SERVICE BULLETIN
References Fig. A-FBAAA Installation of the Ramp Assy and the Wiring Ramp between FR53.6 and FR53.8 Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 (a) Install the mountings on the ramp assy as shown on Fig. A-FBAAA Sheet 04 and Fig. A-FBAAA Sheet 05, Detail J: In accordance with SRM 51-42-00 and SRM 51-43-00: NOTE: Before Installation of the mountings inspect the cables, refer to ESPM 20-53-00. 2 Screw NAS1801-3-20 Item 25 2 Washer NAS1149F0332P Item 3 4 Clamp NSA5516-06ND Item 37 or 4 Clamp NSA5516-07ND Item 38 or 4 Clamp NSA5516-08ND Item 39 2 Spacer NSA5527-03-13 Item 20 (b) Install the mounting on the ramp assy as shown on Fig. A-FBAAA Sheet 04 and Fig. A-FBAAA Sheet 05, Detail K: In accordance with SRM 51-42-00 and SRM 51-43-00: NOTE: Before Installation of the mountings inspect the cables, refer to ESPM 20-53-00. 1 Screw NAS1801-3-7 Item 18 1 Washer NAS1149F0332P Item 3 1 Clamp NSA5516-06ND Item 37 or 1 Clamp NSA5516-07ND Item 38 or 1 Clamp NSA5516-08ND Item 39

DATE: Jan 11/13 SERVICE BULLETIN No.: A340-92-4084 REVISION No.: 00 - Jan 11/13 Page: 22 5

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# @A340 SERVICE BULLETIN (c) Attach the routes 1M and 2M: - in the clamps installed on the ramp assy. - on the wiring ramp with: 10 Tie-Cable NSA935401-03 10 Tie-Cable NSA935401-05 10 Tie-Cable NSA935401-08

(6) Subtask 924084-831-008-001 - Modify the routing of the routes 1M and 2M between FR53.6 and FR53.8, RH Side Work Zones and Access Panels Zone Access/Work location 844 Access Door 842 Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills AIRFRAME Material necessary to do the job Kit 924084A02R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 3 NAS1149F0332P 3 WASHER 18 NAS1801-3-7 1 SCREW 20 NSA5527-03-13 2 SPACER 25 NAS1801-3-20 2 SCREW 37 NSA5516-06ND 5 CLAMP 38 NSA5516-07ND 5 CLAMP 39 NSA5516-08ND 5 CLAMP NSA935401-03 10 TIE NSA935401-05 10 TIE NSA935401-08 10 TIE References Elec. Std. Practices Manual (ESPM) 20-53-00 Structural Repair Manual (SRM) 51-42-00 51-43-00 Fig. A-FBAAA Installation of the Ramp Assy and the Wiring Ramp between FR53.6 and FR53.8 Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 DATE: Jan 11/13 SERVICE BULLETIN No.: A340-92-4084 REVISION No.: 00 - Jan 11/13 Page: 23 5

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# @A340 SERVICE BULLETIN (a) Install the mountings on the ramp assy as shown on Fig. A-FBAAA Sheet 04 and Fig. A-FBAAA Sheet 05, Detail J: In accordance with SRM 51-42-00 and SRM 51-43-00: NOTE: Before Installation of the mountings inspect the cables, refer to ESPM 20-53-00. 2 Screw NAS1801-3-20 Item 25 2 Washer NAS1149F0332P Item 3 4 Clamp NSA5516-06ND Item 37 or 4 Clamp NSA5516-07ND Item 38 or 4 Clamp NSA5516-08ND Item 39 2 Spacer NSA5527-03-13 Item 20 (b) Install the mounting on the ramp assy as shown on Fig. A-FBAAA Sheet 04 and Fig. A-FBAAA Sheet 05, Detail K: In accordance with SRM 51-42-00 and SRM 51-43-00: NOTE: Before Installation of the mountings inspect the cables, refer to ESPM 20-53-00. 1 Screw NAS1801-3-7 Item 18 1 Washer NAS1149F0332P Item 3 1 Clamp NSA5516-06ND Item 37 or 1 Clamp NSA5516-07ND Item 38 or 1 Clamp NSA5516-08ND Item 39 (c) Attach the routes 1M and 2M: - in the clamps installed on the ramp assy. - on the wiring ramp with: 10 Tie-Cable NSA935401-03

DATE: Jan 11/13 SERVICE BULLETIN No.: A340-92-4084 REVISION No.: 00 - Jan 11/13 Page: 24 5

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# @A340 SERVICE BULLETIN
10 Tie-Cable NSA935401-05 10 Tie-Cable NSA935401-08 D. TEST None E. CLOSE-UP (1) Subtask 924084-410-001-001 - Install the Door Frame Linings between FR53.5 and FR53.8, LH Side Work Zones and Access Panels Zone Access/Work location 834 Access Door 832 Manpower Resources Skills NON SPECIFIC References Fig. A-FBBAA Removal/Installation of the Door Frame linings between FR53.5 and FR53.8 Sheet 01
(a) Install the door frame linings between FR53.5 and FR53.8, LH Side: Refer to Fig. A-FBBAA Sheet 01 1 Door Frame Lining Item (32) Retained at removal 1 Door Frame Lining Item (34) Retained at removal 1 Door Frame Lining Item (35) Retained at removal (2) Subtask 924084-410-002-001 - Install the Door Frame Linings between FR53.5 and FR53.8, RH Side Work Zones and Access Panels Zone Access/Work location 844 Access Door 842 Manpower Resources Skills NON SPECIFIC

DATE: Jan 11/13 SERVICE BULLETIN No.: A340-92-4084 REVISION No.: 00 - Jan 11/13 Page: 25 5

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# @A340 SERVICE BULLETIN
References Fig. A-FBBAA Removal/Installation of the Door Frame linings between FR53.5 and FR53.8 Sheet 01
(a) Install the door frame linings between FR53.5 and FR53.8, RH Side: Refer to Fig. A-FBBAA Sheet 01 1 Door Frame Lining Item (33) Retained at removal 1 Door Frame Lining Item (34) Retained at removal 1 Door Frame Lining Item (36) Retained at removal (3) Subtask 924084-942-001-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 52-10-00-410-801 (a) Make sure that the work areas are clean and clear of tools and others items of equipment. (b) Close the passenger/crew door 832 and 842 (Refer to AMM Task 52-10-00-410-801). (c) Remove the access platform(s). (d) Restore the systems and the aircraft to normal operating condition.

DATE: Jan 11/13 SERVICE BULLETIN No.: A340-92-4084 REVISION No.: 00 - Jan 11/13 Page: 26 5

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# @A340 SERVICE BULLETIN

**CONF ALL

STGR12L

STGR14L

LH SIDE SHOWN RH SIDE SYMMETRICAL 

## B **FWD** 

## A

STGR17L 

## BEFORE
FR53.9 FR53.8 FR53.7 FR53.6

1M 2M

55LG (56LG) 2M

FR53.5 FR53.9 

### B **C**

**B C** 

**E D**  **D A**  Z844

Z834

F_SB_924084_5_BAAA_01_00 Figure A-FBAAA - Sheet 01 Installation of the Ramp Assy and the Wiring Ramp between FR53.6 and FR53.8
DATE: Jan 11/13 SERVICE BULLETIN No.: A340-92-4084 REVISION No.: 00 - Jan 11/13 Page: 27 5

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# @A340 SERVICE BULLETIN

**CONF ALL 

## BEFORE
(7) (2) (1)

(3) (8)



## D

**E** 

## OR

CASE 1 CASE 2 1M 2M

(4)

(2) (6)
(3) (17) (7) (2) (1)

(3) (8) (4) (2) (1)

(3) 2M

1M 1M 2M 1M 2M

CASE 1 CASE 2 CASE 3 

## OR OR (4) (2) (1)

(3) 1M 2M

F_SB_924084_5_BAAA_02_00 Figure A-FBAAA - Sheet 02 Installation of the Ramp Assy and the Wiring Ramp between FR53.6 and FR53.8
DATE: Jan 11/13 SERVICE BULLETIN No.: A340-92-4084 REVISION No.: 00 - Jan 11/13 Page: 28 5

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# @A340 SERVICE BULLETIN

**CONF ALL

STGR12L

STGR14L

LH SIDE SHOWN RH SIDE SYMMETRICAL **FWD** 

## AFTER

FR53.9 FR53.6 31 29 30 LH RH



### F
**H** 2M

2M 55LG (56LG)

1M



## C FR53.8



### G

F_SB_924084_5_BAAA_03_01 Figure A-FBAAA - Sheet 03 Installation of the Ramp Assy and the Wiring Ramp between FR53.6 and FR53.8
DATE: Jan 11/13 SERVICE BULLETIN No.: A340-92-4084 REVISION No.: 00 - Jan 11/13 Page: 29 5

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# @A340 SERVICE BULLETIN

**CONF ALL

18 8 3 18 8 3

STGR14L

STGR17L 

## AFTER

**FWD**

**FWD** LH SIDE SHOWN RH SIDE SYMMETRICAL LH SIDE SHOWN RH SIDE SYMMETRICAL LH SIDE SHOWN RH SIDE SYMMETRICAL FR53.7

2M 

### J **J K** 

1M 2M



## F

**G H**  3 3 8 24 23

1M 2M

29 30 LH RH 31

1M 2M 29 30 12 31

8 8

22 21

3
3 LH RH

F_SB_924084_5_BAAA_04_04 Figure A-FBAAA - Sheet 04 Installation of the Ramp Assy and the Wiring Ramp between FR53.6 and FR53.8
DATE: Jan 11/13 SERVICE BULLETIN No.: A340-92-4084 REVISION No.: 00 - Jan 11/13 Page: 30 5

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# @A340 SERVICE BULLETIN

**CONF ALL

37 20 25 3

3 18 

## AFTER

1M 2M

2M 

## J

**K** OR38OR 39

37OR38OR 39

F_SB_924084_5_BAAA_05_00 Figure A-FBAAA - Sheet 05 Installation of the Ramp Assy and the Wiring Ramp between FR53.6 and FR53.8
DATE: Jan 11/13 SERVICE BULLETIN No.: A340-92-4084 REVISION No.: 00 - Jan 11/13 Page: 31 5

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# @A340 SERVICE BULLETIN

**CONF ALL

FR53.8 FR53.5



### B **C D** 

(32) (33)

(35) (36) (34) LH RH

LH RH 

## A

**B C** 

**D** LH SIDE SHOWN RH SIDE SYMMETRICAL 

### A Z844

Z834

F_SB_924084_5_BBAA_01_00 Figure A-FBBAA - Sheet 01 Removal/Installation of the Door Frame linings between FR53.5 and FR53.8
DATE: Jan 11/13 SERVICE BULLETIN No.: A340-92-4084 REVISION No.: 00 - Jan 11/13 Page: 32 5

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# @A340 SERVICE BULLETIN Appendix 01 - Elapsed Time Assumption **CONF ALL (1) The following chart is only a proposal operators may determine that another way to do the work is more suitable for them.

DATE: Jan 11/13 SERVICE BULLETIN No.: A340-92-4084 REVISION No.: 00 - Jan 11/13 Page: 1 5

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# @A340 SERVICE BULLETIN Appendix 01 - Elapsed Time Assumption

**CONF ALL

**ELAPSED TIME ASSUMPTION SERVICE BULLETIN No. A340−92−4084**

GET ACCESS MH ET/S

TOTAL MANHOURS SB ELAPSED TIME 6.00 3.00 STEPS

1.00 0.50

0 REMOVE BRACKETS OF ROUTES 0.50 0.50

CLOSE−UP 1.00 0.50

MH ET/S: PER MANHOURS ELAPSED TIME PER STEP NUMBER OF PERSONS 01 02

THIS CHART IS ONLY A PROPOSAL. OPERATORS MAY DETERMINE THAT ANOTHER WAY TO DO THE WORK IS MORE SUITABLE FOR THEM. 01
02 **NOTES:** PER

2
1

2

: : SB ELAPSED TIME (HOURS) 1 2 3

IF A VSB IS INVOLVED, THE ASSOCIATED MANHOURS ARE NOT REFLECTED IN THIS GANTT CHART. 1M AND 2M, LH SIDE

INSTALL THE RAMP ASSY AND THE 1.00 1.00 1 WIRING RAMP, LH SIDE

MODIFY THE ROUTING OF THE ROUTES 0.50 0.50 1 1M AND 2M, LH SIDE REMOVE BRACKETS OF ROUTES 0.50 0.50 1 1M AND 2M, RH SIDE

INSTALL THE RAMP ASSY AND THE 1.00 1.00 1 WIRING RAMP, RH SIDE

MODIFY THE ROUTING OF THE ROUTES 0.50 0.50 1 1M AND 2M, RH SIDE

F_SB_924084_5_AAAA_01_00 Figure A-FAAAA - Sheet 01 Elapsed Time Assumption
DATE: Jan 11/13 SERVICE BULLETIN No.: A340-92-4084 REVISION No.: 00 - Jan 11/13 Page: 2 5

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# @A340 SERVICE BULLETIN REPORTING SHEET 

### TITLE: ELECTRIC AND ELECTRONIC COMMON INSTALLATION - GENERAL - RE-ROUTING OF HARNESSES AT DOOR 3 AREA, LH AND RH SIDE MODIFICATION No.: 201669S31758 202319S32230 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: Jan 11/13 SERVICE BULLETIN No.: A340-92-4084 REVISION No.: 00 - Jan 11/13 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 4321 - Quality rating of the Accomplishment Instructions 4321 - Quality rating of the Illustrations 4321 - Is this SB easy to understand ? Y/N If you have had difficulties in the accomplishment of this SB please quote below the area(s) and give a short description of the issue. Planning Material Instructions X Effectivity X Kit content X Preparation X Reason X List of Materials Operator Supplied X Mod/Inspection X Manpower X Industry support X Test X References X Re-identification X Close-Up X Publication X Tooling X Illustrations Comments:

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

DATE: Jan 11/13 SERVICE BULLETIN No.: A340-92-4084 REVISION No.: 00 - Jan 11/13 Page: 1 5

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