@A340

SERVICE BULLETIN

SUMMARY

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

This summary is for information only and is not approved for modification of the aircraft.

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 92

TITLE: ELECTRIC AND ELECTRONIC COMMON INSTALLATION - 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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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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SERVICE BULLETIN

SUMMARY

**CONF ALL

STGR12L

STGR14L

A

LH SIDE SHOWN

RH SIDE SYMMETRICAL

FWD B

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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SERVICE BULLETIN

SUMMARY

**CONF ALL

STGR12L

STGR14L

LH SIDE SHOWN

RH SIDE SYMMETRICAL

FWD

AFTER

FR53.9 2M FR53.6

55LG 2M

(56LG)

INSTALL

INSTALL RAMP ASSY

1M

C

WIRING RAMP

FR53.8

F_SB_924084_5_SAAA_02_00

Figure A-FSAAA - Sheet 02

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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 - 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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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.

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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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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

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SERVICE BULLETIN

M. SPARES

None

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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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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

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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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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.

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(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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(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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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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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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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

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

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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

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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

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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

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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

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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

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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

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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

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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

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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

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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

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@A340

SERVICE BULLETIN

**CONF ALL

STGR12L

STGR14L

LH SIDE SHOWN

RH SIDE SYMMETRICAL

FWD B

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

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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

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@A340

SERVICE BULLETIN

**CONF ALL

STGR12L

STGR14L

LH SIDE SHOWN

RH SIDE SYMMETRICAL

FWD

AFTER

FR53.9 31 FR53.6

29

30

LH

RH

F

H

2M

55LG 2M

(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

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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

31 12

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

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SERVICE BULLETIN

**CONF ALL

37

20

25

3

3

18

AFTER

1M 2M

2M

J

K

OR 38 OR 39

37 OR 38 OR 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

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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

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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

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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

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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

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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

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