@A340-500/600

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: 26

TITLE: FIRE PROTECTION-LDCC FIRE EXTINGUISHING-REPLACE FMCU (3

BOTTLES) BY FMS (2 BOTTLES) FOR A340-600 A/C

**CONF ALL

MODIFICATIONS

MODIFICATION CLASSIFICATION

MAJOR 200000D46917

MINOR None

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

Related to the Lower Deck Cargo Compartment (LDCC) fire extinguisher system, the aircraft A340-600

are equipped with different systems :

- 3 fire extinguisher bottles (Halon) with 4 Flow Metering Compact Units (FMCU)

or

- 2 fire extinguisher bottles (Halon) with 2 Flow Metering Systems (FMS).

For the harmonization of the aircraft fleet and as a corrective action, the 3-bottle-system will be reduced

to a 2-bottle-system. The Flow Metering Systems (FMS), the electrical control, electrical monitoring and

cockpit indication will be adapted to ensure proper function of the LDCC fire extinguishing system. The

interaction of the LDCC fire extinguishing system with other systems is modified by reprogramming of

the Smoke Detection Control Unit (SDCU).

This Service Bulletin details the procedure to convert the fire extinguishing system from a three bottle

solution with four Flow Metering Compact Units (FMCU) into a two bottle solution with two Flow

Metering Systems (FMS).

Additionally, the accomplishment of this Service Bulletin will have a positive affect on the fleet

commonality and the weight reduction.

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 1

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

SUMMARY

The Operational/Maintenance Consequences of this Service Bulletin is covered by the update of the

affected publications detailed in ’PLANNING INFORMATION’

GENERAL EVALUATION

EVALUATION TABLE

COMPLIANCE MANDATORY (1) CANCELS INSPECTION SB NO

POTENTIAL AD YES A/C OPERATION AFFECTED NO

RELIABILITY AFFECTED YES PAX COMFORT AFFECTED NO

COST SAVING NO LROPS AFFECTED NO

STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED NO

KIT PRICE (USD) See SB

NOTE (1): Service Bulletin must be accomplished.

MATERIAL PRICE INFORMATION

**CONF 001

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 265020D01R03 1 9,060.00 Tubes, Restrictors, Fittings, Hoses,

Section, Brackets, Placards, Tees,

Reducers, Unions, Leads, Attaching

Parts

Kit 265020D02R04 1 438.00 Brackets, Angles, Attaching Parts

Kit 265020D03R01 1 155.00 Labels, Contacts, Caps, Tees

Kit 265020D05R00 1 54.00 Clamps, Sleeves and Attaching Parts

Kit 265020A01R00 1 1,630.00 Bundle, front plate, placard set, modules,

cable ties

Kit 265020A02R00 1 1,580.00 Integrally Lighted Plate

TOTAL 12,917.00

Component COMPD01 1 See SB Lockwire

Equipment BFEZ01 1 See SB Filters, Reducers, Valves, Switches

Standard tool TOOLD01 1 See SB Swaging Tool

**CONF 002

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 265020D02R04 1 438.00 Brackets, Angles, Attaching Parts

Kit 265020D03R01 1 155.00 Labels, Contacts, Caps, Tees

Kit 265020D04R01 1 9,160.00 Tubes, Restrictors, Fittings, Hoses,

Section, Brackets, Placards, Tees,

Reducers, Unions, Leads, Attaching

Parts

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 2

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

SUMMARY

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 265020D05R00 1 54.00 Clamps, Sleeves and Attaching Parts

Kit 265020A01R00 1 1,630.00 Bundle, front plate, placard set, modules,

cable ties

Kit 265020A03R00 1 1,580.00 Integrally Lighted Plate

TOTAL 13,017.00

Component COMPD01 1 See SB Lockwire

Equipment BFEZ04 1 See SB Filters, Reducers, Valves, Switches

Standard tool TOOLD01 1 See SB Swaging Tool

**CONF 003

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 265020D02R04 1 438.00 Brackets, Angles, Attaching Parts

Kit 265020D03R01 1 155.00 Labels, Contacts, Caps, Tees

Kit 265020D04R01 1 9,160.00 Tubes, Restrictors, Fittings, Hoses,

Section, Brackets, Placards, Tees,

Reducers, Unions, Leads, Attaching

Parts

Kit 265020D05R00 1 54.00 Clamps, Sleeves and Attaching Parts

Kit 265020A01R00 1 1,630.00 Bundle, front plate, placard set, modules,

cable ties

Kit 265020A04R00 1 1,170.00 Integrally Lighted Plate

TOTAL 12,607.00

Component COMPD01 1 See SB Lockwire

Equipment BFEZ04 1 See SB Filters, Reducers, Valves, Switches

Standard tool TOOLD01 1 See SB Swaging Tool

**CONF 004

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 265020D01R03 1 9,060.00 Tubes, Restrictors, Fittings, Hoses,

Section, Brackets, Placards, Tees,

Reducers, Unions, Leads, Attaching

Parts

Kit 265020D02R04 1 438.00 Brackets, Angles, Attaching Parts

Kit 265020D03R01 1 155.00 Labels, Contacts, Caps, Tees

Kit 265020D05R00 1 54.00 Clamps, Sleeves and Attaching Parts

Kit 265020A01R00 1 1,630.00 Bundle, front plate, placard set, modules,

cable ties

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 3

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

SUMMARY

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 265020A05R00 1 1,580.00 Integrally Lighted Plate

TOTAL 12,917.00

Component COMPD01 1 See SB Lockwire

Equipment BFEZ01 1 See SB Filters, Reducers, Valves, Switches

Standard tool TOOLD01 1 See SB Swaging Tool

**CONF 005

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 265020D02R04 1 438.00 Brackets, Angles, Attaching Parts

Kit 265020D03R01 1 155.00 Labels, Contacts, Caps, Tees

Kit 265020D04R01 1 9,160.00 Tubes, Restrictors, Fittings, Hoses,

Section, Brackets, Placards, Tees,

Reducers, Unions, Leads, Attaching

Parts

Kit 265020D05R00 1 54.00 Clamps, Sleeves and Attaching Parts

Kit 265020A01R00 1 1,630.00 Bundle, front plate, placard set, modules,

cable ties

Kit 265020A06R00 1 1,580.00 Integrally Lighted Plate

TOTAL 13,017.00

Component COMPD01 1 See SB Lockwire

Equipment BFEZ04 1 See SB Filters, Reducers, Valves, Switches

Standard tool TOOLD01 1 See SB Swaging Tool

**CONF 006

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 265020D01R03 1 9,060.00 Tubes, Restrictors, Fittings, Hoses,

Section, Brackets, Placards, Tees,

Reducers, Unions, Leads, Attaching

Parts

Kit 265020D02R04 1 438.00 Brackets, Angles, Attaching Parts

Kit 265020D03R01 1 155.00 Labels, Contacts, Caps, Tees

Kit 265020D05R00 1 54.00 Clamps, Sleeves and Attaching Parts

Kit 265020A01R00 1 1,630.00 Bundle, front plate, placard set, modules,

cable ties

Kit 265020A07R00 1 1,580.00 Integrally Lighted Plate

TOTAL 12,917.00

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 4

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

SUMMARY

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Component COMPD01 1 See SB Lockwire

Equipment BFEZ01 1 See SB Filters, Reducers, Valves, Switches

Standard tool TOOLD01 1 See SB Swaging Tool

EFFECTIVITY

**CONF ALL

This Service Bulletin is applicable to this (these) operator(s) :

CES CHH DLH IBE SAA THA VIR

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

**CONF 001

Task 265020-831-848-001: MODIFICATION

TOTAL MANHOURS 166.50

ELAPSED TIME (HOURS) 89.00

**CONF 002

Task 265020-831-848-001: MODIFICATION

TOTAL MANHOURS 166.50

ELAPSED TIME (HOURS) 89.00

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 5

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

SUMMARY

**CONF 003

Task 265020-831-848-001: MODIFICATION

TOTAL MANHOURS 166.50

ELAPSED TIME (HOURS) 89.00

**CONF 004

Task 265020-831-848-001: MODIFICATION

TOTAL MANHOURS 166.50

ELAPSED TIME (HOURS) 89.00

**CONF 005

Task 265020-831-848-001: MODIFICATION

TOTAL MANHOURS 166.50

ELAPSED TIME (HOURS) 89.00

**CONF 006

Task 265020-831-848-001: MODIFICATION

TOTAL MANHOURS 166.50

ELAPSED TIME (HOURS) 89.00

APPENDICES

**CONF ALL

Appendix 01

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 6

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

SUMMARY

**CONF ALL

1LP9

FR2

FR1

FR14

FR18

FR20

2M

1M

FR10.A

MODIFICATION OF THE

EQUIPMENT AND THE

WIRING IN 751VU

MODIFICATION OF THE

EQUIPMENT AND THE

WIRING IN 740VU

MODIFICATION OF THE

EQUIPMENT AND THE

WIRING IN 800VU

MODIFICATION OF THE

EQUIPMENT AND THE

WIRING IN 710VU

MODIFICATION OF THE

EQUIPMENT AND THE

WIRING IN 752VU

MODIFICATION OF THE

EQUIPMENT AND THE

WIRING IN 212VU

2016VC

2044VC

F_SB_265020_5_SAAA_01_01

Figure A-FSAAA - Sheet 01

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 7

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

SUMMARY

**CONF ALL

A

Z130

F_SB_265020_6_SAAA_01_00

FR36

FR37

FR37.1

BOTTLE

4010WX

4005WX

EXTINGUISHER

FIRE

BOTTLE

EXTINGUISHER

FIRE

A

Figure A-GSAAA - Sheet 01

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 8

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

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: 26

TITLE: FIRE PROTECTION-LDCC FIRE EXTINGUISHING-REPLACE FMCU (3

BOTTLES) BY FMS (2 BOTTLES) FOR A340-600 A/C

MODIFICATION No.: 200000D46917

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

This Service Bulletin has been validated on A340-600 aircraft MSN 0601.

(1) Models

340-642

(2) Effectivity by MSN

0371 0376 0383 0391 0410 0416-0417 0426 0431 0436 0440 0449 0453 0460 0468

0475 0482 0488 0514 0517 0523 0531 0534 0537 0540 0543 0547 0557 0566 0569

0575 0577 0580 0583 0586 0601 0604 0606 0615 0617 0619 0622 0626 0630 0639

0672 0677 0681 0689 0702 0706 0710 0719 0723 0727 0736 0744 0753 0764-0765

0768 0787

(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.

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 1

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

OPERATOR MSN

CES 0468 0488 0514 0577 0586

CHH 0436 0453 0475

DLH 0482 0517 0523 0537 0540 0543 0566 0569 0580 0583

IBE 0431 0440 0460 0601 0604 0606 0617 0619 0672 0702 0727 0744

SAA 0410 0417 0426 0531 0534 0547 0557 0626 0630

THA 0677 0681 0689 0710 0719

VIR 0371 0376 0383 0391 0416 0449 0575 0615 0622 0639 0706 0723

0736 0753 0764 0765 0768 0787

(4) Configuration by MSN

MSN CONFIGURATION

0371 0376 0383 0391 0416 0449 0575 0615 0622 0639 0706

0723 0736 0753 0764 0765 0768 0787

001

0410 0417 0426 0531 0534 0547 0557 0626 0630 002

0431 0440 0460 0601 0604 0606 0617 0619 0672 0702 0727

0744

003

0436 0453 0468 0475 0488 0514 0577 0586 006

0482 0517 0523 0537 0540 0543 0566 0569 0580 0583 004

0677 0681 0689 0710 0719 005

(5) Configuration definition

**CONF 001

Config. 001 is valid for aircraft on which :

- Mod.No. 47090D42196 (FIRE PROTECTION - GENERAL - ADAPT BASIC

DEFINITION OF LDCC FIRE DETECTION AND EXTING. FOR A340-600/-500) is

embodied.

- Mod.No. 47182D43173 (FIRE PROTECTION - LDCC FIRE EXTINGUISHING -

INSTALL H.T.L. EXTINGUISHER BOTTLES IN FWD C.C. FOR A340-600) is not

embodied.

and

- Mod. No. 47107D43119 (DEFINE VENTILATION AND TEMPERATURE CONTROL OF

FWD CARGO-COMPARTMENT FOR A340-600) is not embodied,

- Mod. No. 47106D43116 (DEFINE VENTILATION OF AFT CARGO-COMPARTMENT

FOR A340-500/600) is not embodied,

- Mod. No. 47109D43121 (DEFINE VENTILATION AND TEMPERATURE CONTROL OF

AFT CARGO-COMPARTMENT FOR A340-600) is not embodied,

- Mod. No. 47883D43434 (INSTALL SYSTEM PROVISIONS FOR A FIXED CREW

REST IN THE BULK COMPARTMENT) is not embodied,

- Mod. No. 50406D45729 (INSTALL A TEMPERATURE SENSOR) is not embodied.

**CONF 002

Config. 002 is valid for aircraft on which :

- Mod.No. 47090D42196 (FIRE PROTECTION - GENERAL - ADAPT BASIC

DEFINITION OF LDCC FIRE DETECTION AND EXTING. FOR A340-600/-500) is

embodied.

- Mod.No. 47182D43173 (FIRE PROTECTION - LDCC FIRE EXTINGUISHING -

INSTALL H.T.L. EXTINGUISHER BOTTLES IN FWD C.C. FOR A340-600) is embodied.

and

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 2

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

- Mod. No. 47107D43119 (DEFINE VENTILATION AND TEMPERATURE CONTROL OF

FWD CARGO-COMPARTMENT FOR A340-600) is embodied,

- Mod. No. 47106D43116 (DEFINE VENTILATION OF AFT CARGO-COMPARTMENT

FOR A340-500/600) is not embodied,

- Mod. No. 47109D43121 (DEFINE VENTILATION AND TEMPERATURE CONTROL OF

AFT CARGO-COMPARTMENT FOR A340-600) is not embodied,

- Mod. No. 47883D43434 (INSTALL SYSTEM PROVISIONS FOR A FIXED CREW

REST IN THE BULK COMPARTMENT) is not embodied,

- Mod. No. 50406D45729 (INSTALL A TEMPERATURE SENSOR) is not embodied.

**CONF 003

Config. 003 is valid for aircraft on which :

- Mod.No. 47090D42196 (FIRE PROTECTION - GENERAL - ADAPT BASIC

DEFINITION OF LDCC FIRE DETECTION AND EXTING. FOR A340-600/-500) is

embodied.

- Mod.No. 47182D43173 (FIRE PROTECTION - LDCC FIRE EXTINGUISHING -

INSTALL H.T.L. EXTINGUISHER BOTTLES IN FWD C.C. FOR A340-600) is embodied.

and

- Mod. No. 47107D43119 (DEFINE VENTILATION AND TEMPERATURE CONTROL OF

FWD CARGO-COMPARTMENT FOR A340-600) is embodied,

- Mod. No. 47106D43116 (DEFINE VENTILATION OF AFT CARGO-COMPARTMENT

FOR A340-500/600) is embodied,

- Mod. No. 47109D43121 (DEFINE VENTILATION AND TEMPERATURE CONTROL OF

AFT CARGO-COMPARTMENT FOR A340-600) is not embodied,

- Mod. No. 47883D43434 (INSTALL SYSTEM PROVISIONS FOR A FIXED CREW

REST IN THE BULK COMPARTMENT) is not embodied,

- Mod. No. 50406D45729 (INSTALL A TEMPERATURE SENSOR) is not embodied.

**CONF 004

Config. 004 is valid for aircraft on which :

- Mod.No. 47090D42196 (FIRE PROTECTION - GENERAL - ADAPT BASIC

DEFINITION OF LDCC FIRE DETECTION AND EXTING. FOR A340-600/-500) is

embodied.

- Mod.No. 47182D43173 (FIRE PROTECTION - LDCC FIRE EXTINGUISHING -

INSTALL H.T.L. EXTINGUISHER BOTTLES IN FWD C.C. FOR A340-600) is not

embodied.

and

- Mod. No. 47107D43119 (DEFINE VENTILATION AND TEMPERATURE CONTROL OF

FWD CARGO-COMPARTMENT FOR A340-600) is embodied,

- Mod. No. 47106D43116 (DEFINE VENTILATION OF AFT CARGO-COMPARTMENT

FOR A340-500/600) is not embodied,

- Mod. No. 47109D43121 (DEFINE VENTILATION AND TEMPERATURE CONTROL OF

AFT CARGO-COMPARTMENT FOR A340-600) is not embodied,

- Mod. No. 47883D43434 (INSTALL SYSTEM PROVISIONS FOR A FIXED CREW

REST IN THE BULK COMPARTMENT) is not embodied,

- Mod. No. 50406D45729 (INSTALL A TEMPERATURE SENSOR) is embodied.

**CONF 005

Config. 005 is valid for aircraft on which :

- Mod.No. 47090D42196 (FIRE PROTECTION - GENERAL - ADAPT BASIC

DEFINITION OF LDCC FIRE DETECTION AND EXTING. FOR A340-600/-500) is

embodied.

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 3

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

- Mod.No. 47182D43173 (FIRE PROTECTION - LDCC FIRE EXTINGUISHING -

INSTALL H.T.L. EXTINGUISHER BOTTLES IN FWD C.C. FOR A340-600) is embodied.

and

- Mod. No. 47107D43119 (DEFINE VENTILATION AND TEMPERATURE CONTROL OF

FWD CARGO-COMPARTMENT FOR A340-600) is embodied,

- Mod. No. 47106D43116 (DEFINE VENTILATION OF AFT CARGO-COMPARTMENT

FOR A340-500/600) is embodied,

- Mod. No. 47109D43121 (DEFINE VENTILATION AND TEMPERATURE CONTROL OF

AFT CARGO-COMPARTMENT FOR A340-600) is not embodied,

- Mod. No. 47883D43434 (INSTALL SYSTEM PROVISIONS FOR A FIXED CREW

REST IN THE BULK COMPARTMENT) is embodied,

- Mod. No. 50406D45729 (INSTALL A TEMPERATURE SENSOR) is not embodied.

**CONF 006

Config. 006 is valid for aircraft on which :

- Mod.No. 47090D42196 (FIRE PROTECTION - GENERAL - ADAPT BASIC

DEFINITION OF LDCC FIRE DETECTION AND EXTING. FOR A340-600/-500) is

embodied.

- Mod.No. 47182D43173 (FIRE PROTECTION - LDCC FIRE EXTINGUISHING -

INSTALL H.T.L. EXTINGUISHER BOTTLES IN FWD C.C. FOR A340-600) is not

embodied.

and

- Mod. No. 47107D43119 (DEFINE VENTILATION AND TEMPERATURE CONTROL OF

FWD CARGO-COMPARTMENT FOR A340-600) is not embodied,

- Mod. No. 47106D43116 (DEFINE VENTILATION OF AFT CARGO-COMPARTMENT

FOR A340-500/600) is embodied,

- Mod. No. 47109D43121 (DEFINE VENTILATION AND TEMPERATURE CONTROL OF

AFT CARGO-COMPARTMENT FOR A340-600) is embodied,

- Mod. No. 47883D43434 (INSTALL SYSTEM PROVISIONS FOR A FIXED CREW

REST IN THE BULK COMPARTMENT) is embodied,

- Mod. No. 50406D45729 (INSTALL A TEMPERATURE SENSOR) is not embodied.

(6) Material Effectivity

**CONF 001

MATERIAL QTY PER A/C SEE NOTES

Kit 265020D01R03 1

Kit 265020D02R04 1

Kit 265020D03R01 1

Kit 265020D05R00 1

Component COMPD01 1

Equipment BFEZ01 1

Consumable CMLD01 1

Standard tool TOOLD01 1

Kit 265020A01R00 1

Kit 265020A02R00 1

Consumable CMLA01 1

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 4

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF 002

MATERIAL QTY PER A/C SEE NOTES

Kit 265020D02R04 1

Kit 265020D03R01 1

Kit 265020D04R01 1

Kit 265020D05R00 1

Component COMPD01 1

Equipment BFEZ04 1

Consumable CMLD01 1

Standard tool TOOLD01 1

Kit 265020A01R00 1

Kit 265020A03R00 1

Consumable CMLA01 1

**CONF 003

MATERIAL QTY PER A/C SEE NOTES

Kit 265020D02R04 1

Kit 265020D03R01 1

Kit 265020D04R01 1

Kit 265020D05R00 1

Component COMPD01 1

Equipment BFEZ04 1

Consumable CMLD01 1

Standard tool TOOLD01 1

Kit 265020A01R00 1

Kit 265020A04R00 1

Consumable CMLA01 1

**CONF 004

MATERIAL QTY PER A/C SEE NOTES

Kit 265020D01R03 1

Kit 265020D02R04 1

Kit 265020D03R01 1

Kit 265020D05R00 1

Component COMPD01 1

Equipment BFEZ01 1

Consumable CMLD01 1

Standard tool TOOLD01 1

Kit 265020A01R00 1

Kit 265020A05R00 1

Consumable CMLA01 1

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 5

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF 005

MATERIAL QTY PER A/C SEE NOTES

Kit 265020D02R04 1

Kit 265020D03R01 1

Kit 265020D04R01 1

Kit 265020D05R00 1

Component COMPD01 1

Equipment BFEZ04 1

Consumable CMLD01 1

Standard tool TOOLD01 1

Kit 265020A01R00 1

Kit 265020A06R00 1

Consumable CMLA01 1

**CONF 006

MATERIAL QTY PER A/C SEE NOTES

Kit 265020D01R03 1

Kit 265020D02R04 1

Kit 265020D03R01 1

Kit 265020D05R00 1

Component COMPD01 1

Equipment BFEZ01 1

Consumable CMLD01 1

Standard tool TOOLD01 1

Kit 265020A01R00 1

Kit 265020A07R00 1

Consumable CMLA01 1

**CONF ALL

B. CONCURRENT REQUIREMENTS

None

C. REASON

(1) History

Related to the Lower Deck Cargo Compartment (LDCC) fire extinguisher system, the

aircraft A340-600 are equipped with different systems :

- 3 fire extinguisher bottles (Halon) with 4 Flow Metering Compact Units (FMCU)

or

- 2 fire extinguisher bottles (Halon) with 2 Flow Metering Systems (FMS).

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 6

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@A340-500/600

SERVICE BULLETIN

For the harmonization of the aircraft fleet and as a corrective action, the 3-bottlesystem will be reduced to a 2-bottle-system. The Flow Metering Systems (FMS), the

electrical control, electrical monitoring and cockpit indication will be adapted to ensure

proper function of the LDCC fire extinguishing system. The interaction of the LDCC fire

extinguishing system with other systems is modified by reprogramming of the Smoke

Detection Control Unit (SDCU).

(2) Objective/Action

This Service Bulletin details the procedure to convert the fire extinguishing system from

a three bottle solution with four Flow Metering Compact Units (FMCU) into a two bottle

solution with two Flow Metering Systems (FMS).

(3) Advantages

Additionally, the accomplishment of this Service Bulletin will have a positive affect on the

fleet commonality and the weight reduction.

(4) Operational/Maintenance Consequences

The Operational/Maintenance Consequences of this Service Bulletin is covered by the

update of the affected publications detailed in ’PLANNING INFORMATION’

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

**CONF 001

Task 265020-831-848-001: MODIFICATION

(1) Modify the Equipment and the Wiring in the RH Overhead Panel 212VU.

(2) Modify the Equipment and the Wiring in the Emergency Power Center 740VU.

(3) Modify the Equipment and the Wiring in the AC/DC Main Power Center 710VU.

(4) Modify the Equipment and the Wiring in the LH Relay Box 751VU.

(5) Modify the Equipment and the Wiring in the RH Relay Box 752VU.

(6) Modify the Equipment and the Wiring in the Main Rack 800VU.

(7) Modify the Wiring between the Main Rack Shelf 801VU and the LH Relay Box

751VU.

(8) Modify the Wiring between the Main Rack Shelf 802VU and the RH Relay Box

752VU.

(9) Modify the Wiring between the Emergency Power Center 740VU and the LH Relay

Box 751VU.

(10) Modify the Wiring between the AC/DC Main Power Center 715VU and the RH

Relay Box 752VU.

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 7

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@A340-500/600

SERVICE BULLETIN

(11) Modify the Wiring between the Main Rack Shelf 801VU and the Avionics

Compartment at FR2.

(12) Modify the Wiring between the RH Overhead Panel 212VU and the Avionics

Compartment (LH Side).

(13) Modify the Wiring between the RH Overhead Panel 212VU and the Avionics

Compartment (RH Side).

(14) Remove the Fire Extinguishing Bottles, 4010WX, 4005WX and 4020WX.

(15) Remove the 4 Flow Metering Compact Units (FMCU), FIN 4031WX, 4032WX,

4033WX and 4034WX.

(16) Remove the plumbing installations and placards.

(17) Remove the brackets and the insulation blankets between FR35RH thru FR37.1RH.

(18) Install the brackets, modify the insulation blankets and close the rivet holes between

FR35RH thru FR37.1RH.

(19) Modify the equipment and the wiring of the FMCU/FMS outlet pressure switches

4031WX, 4032WX, 4033WX, 4034WX, 4016WX and 4018WX of the fire extinguishing

bottles Nos. 2 and 3.

(20) Modify the equipment and the wiring of the fire extinguishing bottle No. 3 (AFT),

4020WX, and relocated fire extinguishing bottle No. 2 (AFT), 4010WX.

(21) Modify the Equipment and the Wiring of the previous Fire Extinguishing Bottle No. 2

(FWD), 4010WX.

(22) Put the electrical wires of the connectors 4031WX-A, 4032WX-A 4011WX-A,

4012WX-A and 4013WX-A in a stowage position.

(23) Adapt the plumbing installation.

(24) Install the U-section.

(25) Install the Flow Metering Systems (FMS) for the Fire Ext. Bottles No. 1 and No. 2

on the U-section.

(26) Install the Fire Extinguishing Bottles 4005WX and 4010WX.

(27) Install the new identification placards.

**CONF 002

Task 265020-831-848-001: MODIFICATION

(1) Modify the Equipment and the Wiring in the RH Overhead Panel 212VU.

(2) Modify the Equipment and the Wiring in the Emergency Power Center 740VU.

(3) Modify the Equipment and the Wiring in the AC/DC Main Power Center 710VU.

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 8

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@A340-500/600

SERVICE BULLETIN

(4) Modify the Equipment and the Wiring in the LH Relay Box 751VU.

(5) Modify the Equipment and the Wiring in the RH Relay Box 752VU.

(6) Modify the Equipment and the Wiring in the Main Rack 800VU.

(7) Modify the Wiring between the Main Rack Shelf 801VU and the LH Relay Box

751VU.

(8) Modify the Wiring between the Main Rack Shelf 802VU and the RH Relay Box

752VU.

(9) Modify the Wiring between the Emergency Power Center 740VU and the LH Relay

Box 751VU.

(10) Modify the Wiring between the AC/DC Main Power Center 715VU and the RH

Relay Box 752VU.

(11) Modify the Wiring between the Main Rack Shelf 801VU and the Avionics

Compartment at FR2.

(12) Modify the Wiring between the RH Overhead Panel 212VU and the Avionics

Compartment (LH Side).

(13) Modify the Wiring between the RH Overhead Panel 212VU and the Avionics

Compartment (RH Side).

(14) Remove the Fire Extinguishing Bottles, 4010WX, 4005WX and 4020WX.

(15) Remove the 4 Flow Metering Compact Units (FMCU), FIN 4031WX, 4032WX,

4033WX and 4034WX.

(16) Remove the plumbing installations and placards.

(17) Remove the brackets and the insulation blankets between FR35RH thru FR37.1RH.

(18) Install the brackets, modify the insulation blankets and close the rivet holes between

FR35RH thru FR37.1RH.

(19) Modify the equipment and the wiring of the FMCU/FMS outlet pressure switches

4031WX, 4032WX, 4033WX, 4034WX, 4016WX and 4018WX of the fire extinguishing

bottles Nos. 2 and 3.

(20) Modify the equipment and the wiring of the fire extinguishing bottle No. 3 (AFT),

4020WX, and relocated fire extinguishing bottle No. 2 (AFT), 4010WX.

(21) Modify the Equipment and the Wiring of the previous Fire Extinguishing Bottle No. 2

(FWD), 4010WX.

(22) Put the electrical wires of the connectors 4031WX-A, 4032WX-A 4011WX-A,

4012WX-A and 4013WX-A in a stowage position.

(23) Adapt the plumbing installation.

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 9

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@A340-500/600

SERVICE BULLETIN

(24) Install the U-section.

(25) Install the Flow Metering Systems (FMS) for the Fire Ext. Bottles No. 1 and No. 2

on the U-section.

(26) Install the Fire Extinguishing Bottles 4005WX and 4010WX.

(27) Install the new identification placards.

**CONF 003

Task 265020-831-848-001: MODIFICATION

(1) Modify the Equipment and the Wiring in the RH Overhead Panel 212VU.

(2) Modify the Equipment and the Wiring in the Emergency Power Center 740VU.

(3) Modify the Equipment and the Wiring in the AC/DC Main Power Center 710VU.

(4) Modify the Equipment and the Wiring in the LH Relay Box 751VU.

(5) Modify the Equipment and the Wiring in the RH Relay Box 752VU.

(6) Modify the Equipment and the Wiring in the Main Rack 800VU.

(7) Modify the Wiring between the Main Rack Shelf 801VU and the LH Relay Box

751VU.

(8) Modify the Wiring between the Main Rack Shelf 802VU and the RH Relay Box

752VU.

(9) Modify the Wiring between the Emergency Power Center 740VU and the LH Relay

Box 751VU.

(10) Modify the Wiring between the AC/DC Main Power Center 715VU and the RH

Relay Box 752VU.

(11) Modify the Wiring between the Main Rack Shelf 801VU and the Avionics

Compartment at FR2.

(12) Modify the Wiring between the RH Overhead Panel 212VU and the Avionics

Compartment (LH Side).

(13) Modify the Wiring between the RH Overhead Panel 212VU and the Avionics

Compartment (RH Side).

(14) Remove the Fire Extinguishing Bottles, 4010WX, 4005WX and 4020WX.

(15) Remove the 4 Flow Metering Compact Units (FMCU), FIN 4031WX, 4032WX,

4033WX and 4034WX.

(16) Remove the plumbing installations and placards.

(17) Remove the brackets and the insulation blankets between FR35RH thru FR37.1RH.

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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@A340-500/600

SERVICE BULLETIN

(18) Install the brackets, modify the insulation blankets and close the rivet holes between

FR35RH thru FR37.1RH.

(19) Modify the equipment and the wiring of the FMCU/FMS outlet pressure switches

4031WX, 4032WX, 4033WX, 4034WX, 4016WX and 4018WX of the fire extinguishing

bottles Nos. 2 and 3.

(20) Modify the equipment and the wiring of the fire extinguishing bottle No. 3 (AFT),

4020WX, and relocated fire extinguishing bottle No. 2 (AFT), 4010WX.

(21) Modify the Equipment and the Wiring of the previous Fire Extinguishing Bottle No. 2

(FWD), 4010WX.

(22) Put the electrical wires of the connectors 4031WX-A, 4032WX-A 4011WX-A,

4012WX-A and 4013WX-A in a stowage position.

(23) Adapt the plumbing installation.

(24) Install the U-section.

(25) Install the Flow Metering Systems (FMS) for the Fire Ext. Bottles No. 1 and No. 2

on the U-section.

(26) Install the Fire Extinguishing Bottles 4005WX and 4010WX.

(27) Install the new identification placards.

**CONF 004

Task 265020-831-848-001: MODIFICATION

(1) Modify the Equipment and the Wiring in the RH Overhead Panel 212VU.

(2) Modify the Equipment and the Wiring in the Emergency Power Center 740VU.

(3) Modify the Equipment and the Wiring in the AC/DC Main Power Center 710VU.

(4) Modify the Equipment and the Wiring in the LH Relay Box 751VU.

(5) Modify the Equipment and the Wiring in the RH Relay Box 752VU.

(6) Modify the Equipment and the Wiring in the Main Rack 800VU.

(7) Modify the Wiring between the Main Rack Shelf 801VU and the LH Relay Box

751VU.

(8) Modify the Wiring between the Main Rack Shelf 802VU and the RH Relay Box

752VU.

(9) Modify the Wiring between the Emergency Power Center 740VU and the LH Relay

Box 751VU.

(10) Modify the Wiring between the AC/DC Main Power Center 715VU and the RH

Relay Box 752VU.

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 11

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@A340-500/600

SERVICE BULLETIN

(11) Modify the Wiring between the Main Rack Shelf 801VU and the Avionics

Compartment at FR2.

(12) Modify the Wiring between the RH Overhead Panel 212VU and the Avionics

Compartment (LH Side).

(13) Modify the Wiring between the RH Overhead Panel 212VU and the Avionics

Compartment (RH Side).

(14) Remove the Fire Extinguishing Bottles, 4010WX, 4005WX and 4020WX.

(15) Remove the 4 Flow Metering Compact Units (FMCU), FIN 4031WX, 4032WX,

4033WX and 4034WX.

(16) Remove the plumbing installations and placards.

(17) Remove the brackets and the insulation blankets between FR35RH thru FR37.1RH.

(18) Install the brackets, modify the insulation blankets and close the rivet holes between

FR35RH thru FR37.1RH.

(19) Modify the equipment and the wiring of the FMCU/FMS outlet pressure switches

4031WX, 4032WX, 4033WX, 4034WX, 4016WX and 4018WX of the fire extinguishing

bottles Nos. 2 and 3.

(20) Modify the equipment and the wiring of the fire extinguishing bottle No. 3 (AFT),

4020WX, and relocated fire extinguishing bottle No. 2 (AFT), 4010WX.

(21) Modify the Equipment and the Wiring of the previous Fire Extinguishing Bottle No. 2

(FWD), 4010WX.

(22) Put the electrical wires of the connectors 4031WX-A, 4032WX-A 4011WX-A,

4012WX-A and 4013WX-A in a stowage position.

(23) Adapt the plumbing installation.

(24) Install the U-section.

(25) Install the Flow Metering Systems (FMS) for the Fire Ext. Bottles No. 1 and No. 2

on the U-section.

(26) Install the Fire Extinguishing Bottles 4005WX and 4010WX.

(27) Install the new identification placards.

**CONF 005

Task 265020-831-848-001: MODIFICATION

(1) Modify the Equipment and the Wiring in the RH Overhead Panel 212VU.

(2) Modify the Equipment and the Wiring in the Emergency Power Center 740VU.

(3) Modify the Equipment and the Wiring in the AC/DC Main Power Center 710VU.

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 12

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@A340-500/600

SERVICE BULLETIN

(4) Modify the Equipment and the Wiring in the LH Relay Box 751VU.

(5) Modify the Equipment and the Wiring in the RH Relay Box 752VU.

(6) Modify the Equipment and the Wiring in the Main Rack 800VU.

(7) Modify the Wiring between the Main Rack Shelf 801VU and the LH Relay Box

751VU.

(8) Modify the Wiring between the Main Rack Shelf 802VU and the RH Relay Box

752VU.

(9) Modify the Wiring between the Emergency Power Center 740VU and the LH Relay

Box 751VU.

(10) Modify the Wiring between the AC/DC Main Power Center 715VU and the RH

Relay Box 752VU.

(11) Modify the Wiring between the Main Rack Shelf 801VU and the Avionics

Compartment at FR2.

(12) Modify the Wiring between the RH Overhead Panel 212VU and the Avionics

Compartment (LH Side).

(13) Modify the Wiring between the RH Overhead Panel 212VU and the Avionics

Compartment (RH Side).

(14) Remove the Fire Extinguishing Bottles, 4010WX, 4005WX and 4020WX.

(15) Remove the 4 Flow Metering Compact Units (FMCU), FIN 4031WX, 4032WX,

4033WX and 4034WX.

(16) Remove the plumbing installations and placards.

(17) Remove the brackets and the insulation blankets between FR35RH thru FR37.1RH.

(18) Install the brackets, modify the insulation blankets and close the rivet holes between

FR35RH thru FR37.1RH.

(19) Modify the equipment and the wiring of the FMCU/FMS outlet pressure switches

4031WX, 4032WX, 4033WX, 4034WX, 4016WX and 4018WX of the fire extinguishing

bottles Nos. 2 and 3.

(20) Modify the equipment and the wiring of the fire extinguishing bottle No. 3 (AFT),

4020WX, and relocated fire extinguishing bottle No. 2 (AFT), 4010WX.

(21) Modify the Equipment and the Wiring of the previous Fire Extinguishing Bottle No. 2

(FWD), 4010WX.

(22) Put the electrical wires of the connectors 4031WX-A, 4032WX-A 4011WX-A,

4012WX-A and 4013WX-A in a stowage position.

(23) Adapt the plumbing installation.

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 13

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@A340-500/600

SERVICE BULLETIN

(24) Install the U-section.

(25) Install the Flow Metering Systems (FMS) for the Fire Ext. Bottles No. 1 and No. 2

on the U-section.

(26) Install the Fire Extinguishing Bottles 4005WX and 4010WX.

(27) Install the new identification placards.

**CONF 006

Task 265020-831-848-001: MODIFICATION

(1) Modify the Equipment and the Wiring in the RH Overhead Panel 212VU.

(2) Modify the Equipment and the Wiring in the Emergency Power Center 740VU.

(3) Modify the Equipment and the Wiring in the AC/DC Main Power Center 710VU.

(4) Modify the Equipment and the Wiring in the LH Relay Box 751VU.

(5) Modify the Equipment and the Wiring in the RH Relay Box 752VU.

(6) Modify the Equipment and the Wiring in the Main Rack 800VU.

(7) Modify the Wiring between the Main Rack Shelf 801VU and the LH Relay Box

751VU.

(8) Modify the Wiring between the Main Rack Shelf 802VU and the RH Relay Box

752VU.

(9) Modify the Wiring between the Emergency Power Center 740VU and the LH Relay

Box 751VU.

(10) Modify the Wiring between the AC/DC Main Power Center 715VU and the RH

Relay Box 752VU.

(11) Modify the Wiring between the Main Rack Shelf 801VU and the Avionics

Compartment at FR2.

(12) Modify the Wiring between the RH Overhead Panel 212VU and the Avionics

Compartment (LH Side).

(13) Modify the Wiring between the RH Overhead Panel 212VU and the Avionics

Compartment (RH Side).

(14) Remove the Fire Extinguishing Bottles, 4010WX, 4005WX and 4020WX.

(15) Remove the 4 Flow Metering Compact Units (FMCU), FIN 4031WX, 4032WX,

4033WX and 4034WX.

(16) Remove the plumbing installations and placards.

(17) Remove the brackets and the insulation blankets between FR35RH thru FR37.1RH.

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 14

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@A340-500/600

SERVICE BULLETIN

(18) Install the brackets, modify the insulation blankets and close the rivet holes between

FR35RH thru FR37.1RH.

(19) Modify the equipment and the wiring of the FMCU/FMS outlet pressure switches

4031WX, 4032WX, 4033WX, 4034WX, 4016WX and 4018WX of the fire extinguishing

bottles Nos. 2 and 3.

(20) Modify the equipment and the wiring of the fire extinguishing bottle No. 3 (AFT),

4020WX, and relocated fire extinguishing bottle No. 2 (AFT), 4010WX.

(21) Modify the Equipment and the Wiring of the previous Fire Extinguishing Bottle No. 2

(FWD), 4010WX.

(22) Put the electrical wires of the connectors 4031WX-A, 4032WX-A 4011WX-A,

4012WX-A and 4013WX-A in a stowage position.

(23) Adapt the plumbing installation.

(24) Install the U-section.

(25) Install the Flow Metering Systems (FMS) for the Fire Ext. Bottles No. 1 and No. 2

on the U-section.

(26) Install the Fire Extinguishing Bottles 4005WX and 4010WX.

(27) Install the new identification placards.

**CONF ALL

E. COMPLIANCE

(1) Classification

MANDATORY: Service Bulletin must be accomplished.

(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 accomplishment timescale, which has not yet been defined, will be

given in the AD.

F. APPROVAL

Approved under EASA Design Organisation Approval No. EASA 21J.031.

If an aircraft listed in the effectivity has a modification or repair embodied that is not of

AIRBUS origin, and which affects the content of this Service Bulletin, the operator is

responsible for obtaining approval by its airworthiness authority for any adaptation necessary

before incorporation of the Service Bulletin.

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 15

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@A340-500/600

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.

**CONF 001

Task 265020-831-848-001: MODIFICATION

Get Access 17.50

On Aircraft

Modify the Equipment and the Wiring in the RH

Overhead Panel 212VU.

12.00

Modify the Equipment and the Wiring in the Emergency

Power Center 740VU.

3.50

Modify the Equipment and the Wiring in the AC/DC

Main Power Center 710VU.

3.50

Modify the Equipment and the Wiring in the LH Relay

Box 751VU.

3.50

Modify the Equipment and the Wiring in the RH Relay

Box 752VU.

3.50

Modify the Equipment and the Wiring in the Main Rack

800VU.

8.00

Modify the Wiring between the Main Rack Shelf 801VU

and the LH Relay Box 751VU.

3.50

Modify the Wiring between the Main Rack Shelf 802VU

and the RH Relay Box 752VU.

3.50

Modify the Wiring between the Emergency Power

Center 740VU and the LH Relay Box 751VU.

3.50

Modify the Wiring between the AC/DC Main Power

Center 715VU and the RH Relay Box 752VU.

3.50

Modify the Wiring between the Main Rack Shelf 801VU

and the Avionics Compartment at FR2.

3.50

Modify the Wiring between the RH Overhead Panel

212VU and the Avionics Compartment (LH Side).

10.00

Modify the Wiring between the RH Overhead Panel

212VU and the Avionics Compartment (RH Side).

10.00

Remove the Fire Extinguishing Bottles, 4010WX,

4005WX and 4020WX.

3.00

Remove the 4 Flow Metering Compact Units (FMCU),

FIN 4031WX, 4032WX, 4033WX and 4034WX.

4.00

Remove the plumbing installations and placards. 2.50

Remove the brackets and the insulation blankets

between FR35RH thru FR37.1RH.

3.50

Install the brackets, modify the insulation blankets and

close the rivet holes between FR35RH thru FR37.1RH.

7.00

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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SERVICE BULLETIN

Task 265020-831-848-001: MODIFICATION

Modify the equipment and the wiring of the FMCU/FMS

outlet pressure switches 4031WX, 4032WX, 4033WX,

4034WX, 4016WX and 4018WX of the fire

extinguishing bottles Nos. 2 and 3.

1.50

Modify the equipment and the wiring of the fire

extinguishing bottle No. 3 (AFT), 4020WX, and

relocated fire extinguishing bottle No. 2 (AFT),

4010WX.

1.00

Modify the Equipment and the Wiring of the previous

Fire Extinguishing Bottle No. 2 (FWD), 4010WX.

1.50

Put the electrical wires of the connectors 4031WX-A,

4032WX-A 4011WX-A, 4012WX-A and 4013WX-A in a

stowage position.

2.50

Adapt the plumbing installation. 3.00

Install the U-section. 1.00

Install the Flow Metering Systems (FMS) for the Fire

Ext. Bottles No. 1 and No. 2 on the U-section.

4.00

Install the Fire Extinguishing Bottles 4005WX and

4010WX.

2.00

Install the new identification placards. 1.50

Tests 22.00

Close-Up 17.50

TOTAL MANHOURS 166.50

ELAPSED TIME (HOURS) 89.00

**CONF 002

Task 265020-831-848-001: MODIFICATION

Get Access 17.50

On Aircraft

Modify the Equipment and the Wiring in the RH

Overhead Panel 212VU.

12.00

Modify the Equipment and the Wiring in the Emergency

Power Center 740VU.

3.50

Modify the Equipment and the Wiring in the AC/DC

Main Power Center 710VU.

3.50

Modify the Equipment and the Wiring in the LH Relay

Box 751VU.

3.50

Modify the Equipment and the Wiring in the RH Relay

Box 752VU.

3.50

Modify the Equipment and the Wiring in the Main Rack

800VU.

8.00

Modify the Wiring between the Main Rack Shelf 801VU

and the LH Relay Box 751VU.

3.50

Modify the Wiring between the Main Rack Shelf 802VU

and the RH Relay Box 752VU.

3.50

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 17

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@A340-500/600

SERVICE BULLETIN

Task 265020-831-848-001: MODIFICATION

Modify the Wiring between the Emergency Power

Center 740VU and the LH Relay Box 751VU.

3.50

Modify the Wiring between the AC/DC Main Power

Center 715VU and the RH Relay Box 752VU.

3.50

Modify the Wiring between the Main Rack Shelf 801VU

and the Avionics Compartment at FR2.

3.50

Modify the Wiring between the RH Overhead Panel

212VU and the Avionics Compartment (LH Side).

10.00

Modify the Wiring between the RH Overhead Panel

212VU and the Avionics Compartment (RH Side).

10.00

Remove the Fire Extinguishing Bottles, 4010WX,

4005WX and 4020WX.

3.00

Remove the 4 Flow Metering Compact Units (FMCU),

FIN 4031WX, 4032WX, 4033WX and 4034WX.

4.00

Remove the plumbing installations and placards. 2.50

Remove the brackets and the insulation blankets

between FR35RH thru FR37.1RH.

3.50

Install the brackets, modify the insulation blankets and

close the rivet holes between FR35RH thru FR37.1RH.

7.00

Modify the equipment and the wiring of the FMCU/FMS

outlet pressure switches 4031WX, 4032WX, 4033WX,

4034WX, 4016WX and 4018WX of the fire

extinguishing bottles Nos. 2 and 3.

1.50

Modify the equipment and the wiring of the fire

extinguishing bottle No. 3 (AFT), 4020WX, and

relocated fire extinguishing bottle No. 2 (AFT),

4010WX.

1.00

Modify the Equipment and the Wiring of the previous

Fire Extinguishing Bottle No. 2 (FWD), 4010WX.

1.50

Put the electrical wires of the connectors 4031WX-A,

4032WX-A 4011WX-A, 4012WX-A and 4013WX-A in a

stowage position.

2.50

Adapt the plumbing installation. 3.00

Install the U-section. 1.00

Install the Flow Metering Systems (FMS) for the Fire

Ext. Bottles No. 1 and No. 2 on the U-section.

4.00

Install the Fire Extinguishing Bottles 4005WX and

4010WX.

2.00

Install the new identification placards. 1.50

Tests 22.00

Close-Up 17.50

TOTAL MANHOURS 166.50

ELAPSED TIME (HOURS) 89.00

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 18

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF 003

Task 265020-831-848-001: MODIFICATION

Get Access 17.50

On Aircraft

Modify the Equipment and the Wiring in the RH

Overhead Panel 212VU.

12.00

Modify the Equipment and the Wiring in the Emergency

Power Center 740VU.

3.50

Modify the Equipment and the Wiring in the AC/DC

Main Power Center 710VU.

3.50

Modify the Equipment and the Wiring in the LH Relay

Box 751VU.

3.50

Modify the Equipment and the Wiring in the RH Relay

Box 752VU.

3.50

Modify the Equipment and the Wiring in the Main Rack

800VU.

8.00

Modify the Wiring between the Main Rack Shelf 801VU

and the LH Relay Box 751VU.

3.50

Modify the Wiring between the Main Rack Shelf 802VU

and the RH Relay Box 752VU.

3.50

Modify the Wiring between the Emergency Power

Center 740VU and the LH Relay Box 751VU.

3.50

Modify the Wiring between the AC/DC Main Power

Center 715VU and the RH Relay Box 752VU.

3.50

Modify the Wiring between the Main Rack Shelf 801VU

and the Avionics Compartment at FR2.

3.50

Modify the Wiring between the RH Overhead Panel

212VU and the Avionics Compartment (LH Side).

10.00

Modify the Wiring between the RH Overhead Panel

212VU and the Avionics Compartment (RH Side).

10.00

Remove the Fire Extinguishing Bottles, 4010WX,

4005WX and 4020WX.

3.00

Remove the 4 Flow Metering Compact Units (FMCU),

FIN 4031WX, 4032WX, 4033WX and 4034WX.

4.00

Remove the plumbing installations and placards. 2.50

Remove the brackets and the insulation blankets

between FR35RH thru FR37.1RH.

3.50

Install the brackets, modify the insulation blankets and

close the rivet holes between FR35RH thru FR37.1RH.

7.00

Modify the equipment and the wiring of the FMCU/FMS

outlet pressure switches 4031WX, 4032WX, 4033WX,

4034WX, 4016WX and 4018WX of the fire

extinguishing bottles Nos. 2 and 3.

1.50

Modify the equipment and the wiring of the fire

extinguishing bottle No. 3 (AFT), 4020WX, and

relocated fire extinguishing bottle No. 2 (AFT),

4010WX.

1.00

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 19

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

Task 265020-831-848-001: MODIFICATION

Modify the Equipment and the Wiring of the previous

Fire Extinguishing Bottle No. 2 (FWD), 4010WX.

1.50

Put the electrical wires of the connectors 4031WX-A,

4032WX-A 4011WX-A, 4012WX-A and 4013WX-A in a

stowage position.

2.50

Adapt the plumbing installation. 3.00

Install the U-section. 1.00

Install the Flow Metering Systems (FMS) for the Fire

Ext. Bottles No. 1 and No. 2 on the U-section.

4.00

Install the Fire Extinguishing Bottles 4005WX and

4010WX.

2.00

Install the new identification placards. 1.50

Tests 22.00

Close-Up 17.50

TOTAL MANHOURS 166.50

ELAPSED TIME (HOURS) 89.00

**CONF 004

Task 265020-831-848-001: MODIFICATION

Get Access 17.50

On Aircraft

Modify the Equipment and the Wiring in the RH

Overhead Panel 212VU.

12.00

Modify the Equipment and the Wiring in the Emergency

Power Center 740VU.

3.50

Modify the Equipment and the Wiring in the AC/DC

Main Power Center 710VU.

3.50

Modify the Equipment and the Wiring in the LH Relay

Box 751VU.

3.50

Modify the Equipment and the Wiring in the RH Relay

Box 752VU.

3.50

Modify the Equipment and the Wiring in the Main Rack

800VU.

8.00

Modify the Wiring between the Main Rack Shelf 801VU

and the LH Relay Box 751VU.

3.50

Modify the Wiring between the Main Rack Shelf 802VU

and the RH Relay Box 752VU.

3.50

Modify the Wiring between the Emergency Power

Center 740VU and the LH Relay Box 751VU.

3.50

Modify the Wiring between the AC/DC Main Power

Center 715VU and the RH Relay Box 752VU.

3.50

Modify the Wiring between the Main Rack Shelf 801VU

and the Avionics Compartment at FR2.

3.50

Modify the Wiring between the RH Overhead Panel

212VU and the Avionics Compartment (LH Side).

10.00

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 20

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

Task 265020-831-848-001: MODIFICATION

Modify the Wiring between the RH Overhead Panel

212VU and the Avionics Compartment (RH Side).

10.00

Remove the Fire Extinguishing Bottles, 4010WX,

4005WX and 4020WX.

3.00

Remove the 4 Flow Metering Compact Units (FMCU),

FIN 4031WX, 4032WX, 4033WX and 4034WX.

4.00

Remove the plumbing installations and placards. 2.50

Remove the brackets and the insulation blankets

between FR35RH thru FR37.1RH.

3.50

Install the brackets, modify the insulation blankets and

close the rivet holes between FR35RH thru FR37.1RH.

7.00

Modify the equipment and the wiring of the FMCU/FMS

outlet pressure switches 4031WX, 4032WX, 4033WX,

4034WX, 4016WX and 4018WX of the fire

extinguishing bottles Nos. 2 and 3.

1.50

Modify the equipment and the wiring of the fire

extinguishing bottle No. 3 (AFT), 4020WX, and

relocated fire extinguishing bottle No. 2 (AFT),

4010WX.

1.00

Modify the Equipment and the Wiring of the previous

Fire Extinguishing Bottle No. 2 (FWD), 4010WX.

1.50

Put the electrical wires of the connectors 4031WX-A,

4032WX-A 4011WX-A, 4012WX-A and 4013WX-A in a

stowage position.

2.50

Adapt the plumbing installation. 3.00

Install the U-section. 1.00

Install the Flow Metering Systems (FMS) for the Fire

Ext. Bottles No. 1 and No. 2 on the U-section.

4.00

Install the Fire Extinguishing Bottles 4005WX and

4010WX.

2.00

Install the new identification placards. 1.50

Tests 22.00

Close-Up 17.50

TOTAL MANHOURS 166.50

ELAPSED TIME (HOURS) 89.00

**CONF 005

Task 265020-831-848-001: MODIFICATION

Get Access 17.50

On Aircraft

Modify the Equipment and the Wiring in the RH

Overhead Panel 212VU.

12.00

Modify the Equipment and the Wiring in the Emergency

Power Center 740VU.

3.50

Modify the Equipment and the Wiring in the AC/DC

Main Power Center 710VU.

3.50

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 21

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

Task 265020-831-848-001: MODIFICATION

Modify the Equipment and the Wiring in the LH Relay

Box 751VU.

3.50

Modify the Equipment and the Wiring in the RH Relay

Box 752VU.

3.50

Modify the Equipment and the Wiring in the Main Rack

800VU.

8.00

Modify the Wiring between the Main Rack Shelf 801VU

and the LH Relay Box 751VU.

3.50

Modify the Wiring between the Main Rack Shelf 802VU

and the RH Relay Box 752VU.

3.50

Modify the Wiring between the Emergency Power

Center 740VU and the LH Relay Box 751VU.

3.50

Modify the Wiring between the AC/DC Main Power

Center 715VU and the RH Relay Box 752VU.

3.50

Modify the Wiring between the Main Rack Shelf 801VU

and the Avionics Compartment at FR2.

3.50

Modify the Wiring between the RH Overhead Panel

212VU and the Avionics Compartment (LH Side).

10.00

Modify the Wiring between the RH Overhead Panel

212VU and the Avionics Compartment (RH Side).

10.00

Remove the Fire Extinguishing Bottles, 4010WX,

4005WX and 4020WX.

3.00

Remove the 4 Flow Metering Compact Units (FMCU),

FIN 4031WX, 4032WX, 4033WX and 4034WX.

4.00

Remove the plumbing installations and placards. 2.50

Remove the brackets and the insulation blankets

between FR35RH thru FR37.1RH.

3.50

Install the brackets, modify the insulation blankets and

close the rivet holes between FR35RH thru FR37.1RH.

7.00

Modify the equipment and the wiring of the FMCU/FMS

outlet pressure switches 4031WX, 4032WX, 4033WX,

4034WX, 4016WX and 4018WX of the fire

extinguishing bottles Nos. 2 and 3.

1.50

Modify the equipment and the wiring of the fire

extinguishing bottle No. 3 (AFT), 4020WX, and

relocated fire extinguishing bottle No. 2 (AFT),

4010WX.

1.00

Modify the Equipment and the Wiring of the previous

Fire Extinguishing Bottle No. 2 (FWD), 4010WX.

1.50

Put the electrical wires of the connectors 4031WX-A,

4032WX-A 4011WX-A, 4012WX-A and 4013WX-A in a

stowage position.

2.50

Adapt the plumbing installation. 3.00

Install the U-section. 1.00

Install the Flow Metering Systems (FMS) for the Fire

Ext. Bottles No. 1 and No. 2 on the U-section.

4.00

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 22

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

Task 265020-831-848-001: MODIFICATION

Install the Fire Extinguishing Bottles 4005WX and

4010WX.

2.00

Install the new identification placards. 1.50

Tests 22.00

Close-Up 17.50

TOTAL MANHOURS 166.50

ELAPSED TIME (HOURS) 89.00

**CONF 006

Task 265020-831-848-001: MODIFICATION

Get Access 17.50

On Aircraft

Modify the Equipment and the Wiring in the RH

Overhead Panel 212VU.

12.00

Modify the Equipment and the Wiring in the Emergency

Power Center 740VU.

3.50

Modify the Equipment and the Wiring in the AC/DC

Main Power Center 710VU.

3.50

Modify the Equipment and the Wiring in the LH Relay

Box 751VU.

3.50

Modify the Equipment and the Wiring in the RH Relay

Box 752VU.

3.50

Modify the Equipment and the Wiring in the Main Rack

800VU.

8.00

Modify the Wiring between the Main Rack Shelf 801VU

and the LH Relay Box 751VU.

3.50

Modify the Wiring between the Main Rack Shelf 802VU

and the RH Relay Box 752VU.

3.50

Modify the Wiring between the Emergency Power

Center 740VU and the LH Relay Box 751VU.

3.50

Modify the Wiring between the AC/DC Main Power

Center 715VU and the RH Relay Box 752VU.

3.50

Modify the Wiring between the Main Rack Shelf 801VU

and the Avionics Compartment at FR2.

3.50

Modify the Wiring between the RH Overhead Panel

212VU and the Avionics Compartment (LH Side).

10.00

Modify the Wiring between the RH Overhead Panel

212VU and the Avionics Compartment (RH Side).

10.00

Remove the Fire Extinguishing Bottles, 4010WX,

4005WX and 4020WX.

3.00

Remove the 4 Flow Metering Compact Units (FMCU),

FIN 4031WX, 4032WX, 4033WX and 4034WX.

4.00

Remove the plumbing installations and placards. 2.50

Remove the brackets and the insulation blankets

between FR35RH thru FR37.1RH.

3.50

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 23

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

Task 265020-831-848-001: MODIFICATION

Install the brackets, modify the insulation blankets and

close the rivet holes between FR35RH thru FR37.1RH.

7.00

Modify the equipment and the wiring of the FMCU/FMS

outlet pressure switches 4031WX, 4032WX, 4033WX,

4034WX, 4016WX and 4018WX of the fire

extinguishing bottles Nos. 2 and 3.

1.50

Modify the equipment and the wiring of the fire

extinguishing bottle No. 3 (AFT), 4020WX, and

relocated fire extinguishing bottle No. 2 (AFT),

4010WX.

1.00

Modify the Equipment and the Wiring of the previous

Fire Extinguishing Bottle No. 2 (FWD), 4010WX.

1.50

Put the electrical wires of the connectors 4031WX-A,

4032WX-A 4011WX-A, 4012WX-A and 4013WX-A in a

stowage position.

2.50

Adapt the plumbing installation. 3.00

Install the U-section. 1.00

Install the Flow Metering Systems (FMS) for the Fire

Ext. Bottles No. 1 and No. 2 on the U-section.

4.00

Install the Fire Extinguishing Bottles 4005WX and

4010WX.

2.00

Install the new identification placards. 1.50

Tests 22.00

Close-Up 17.50

TOTAL MANHOURS 166.50

ELAPSED TIME (HOURS) 89.00

**CONF ALL

H. WEIGHT AND BALANCE

**CONF 001, 004, 006

The weight and balance estimates given in this Service Bulletin are based on the

Manufacturer’s Empty Weight (MEW) and do not include operator item’s. For the definition of

MEW and operator’s items refer to Weight and Balance Manual (WBM) Chapter 1-00-07.

Manufacturers Empty Weight -43.312 KG (-95.4856 LB)

Effect on Balance -1050.411 KGM (-7597.622 LB.FT )

**CONF 002 thru 003, 005

The weight and balance estimates given in this Service Bulletin are based on the

Manufacturer’s Empty Weight (MEW) and do not include operator item’s. For the definition of

MEW and operator’s items refer to Weight and Balance Manual (WBM) Chapter 1-00-07.

Manufacturers Empty Weight -43.152 KG (-95.1329 LB)

Effect on Balance -1046.439 KGM (-7568.893 LB.FT )

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 24

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF ALL

I. ELECTRICAL LOAD DATA

(1) Direct Current (DC) Load Changes

The values given below show the increase (+) or decrease (-) of the electrical load

resulting from the accomplishment of this Service Bulletin.

- Circuit Breaker : 1WX (existing)

Designation : CRG FIRE EXTNG/A

Busbar : 701PP

Nominal Power : 384W

Electrical Load Delta : -192W

- Circuit Breaker : 2WX (existing)

Designation : CRG FIRE EXTNG/B

Busbar : 202PP

Nominal Power : 384W

Electrical Load Delta : -192W

(2) Alternating Current (AC) Load Changes

Not Changed

J. REFERENCES

**CONF 001

Aircraft Maintenance Manual (AMM) 06-31-53 06-41-53 11-00-00

12-34-24 20-21-00 20-21-12

20-21-15 20-23-11 20-28-00

21-20-00 21-26-00 21-28-00

21-31-00 21-63-00 22-96-00

22-97-00 23-36-00 23-51-00

23-51-12 23-71-00 23-71-34

23-73-00 23-81-00 23-81-13

24-41-00 25-11-00 25-11-51

25-13-44 25-52-00 25-80-00

26-16-00 26-16-34 26-23-00

26-23-41 26-23-43 27-51-00

27-81-00 27-96-00 28-24-00

28-51-00 29-13-00 30-21-00

30-45-00 31-50-00 31-60-00

32-31-00 33-13-00 33-14-00

33-44-00 36-11-00 45-22-21

52-10-00 52-30-00 52-71-00

71-00-00

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 25

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-25-51 20-33-00 20-33-34

20-52-10 20-52-21 20-55-00

Process and Material Specification (PMS) Process and Material Specification

(PMS) 01-07-06

Process and Material Specification

(PMS) 01-07-10

Standards Manual (SM)

Structural Repair Manual (SRM) 51-42-11 51-43-00 51-44-11

51-47-00

Weight and Balance Manual (WBM) Weight and Balance Manual

(WBM) Chapter 1-00-07

**CONF 002

Aircraft Maintenance Manual (AMM) 06-31-53 06-41-53 11-00-00

12-34-24 20-21-00 20-21-12

20-21-15 20-23-11 20-28-00

21-20-00 21-26-00 21-28-00

21-31-00 21-63-00 22-96-00

22-97-00 23-36-00 23-51-00

23-51-12 23-71-00 23-71-34

23-73-00 23-81-00 23-81-13

24-41-00 25-11-00 25-11-51

25-13-44 25-52-00 25-80-00

26-16-00 26-16-34 26-23-00

26-23-41 26-23-43 27-51-00

27-81-00 27-96-00 28-24-00

28-51-00 29-13-00 30-21-00

30-45-00 31-50-00 31-60-00

32-31-00 33-13-00 33-14-00

33-44-00 36-11-00 45-22-21

52-10-00 52-30-00 52-71-00

71-00-00

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-25-51 20-33-00 20-33-34

20-52-10 20-52-21 20-55-00

Process and Material Specification (PMS) Process and Material Specification

(PMS) 01-07-06

Process and Material Specification

(PMS) 01-07-10

Standards Manual (SM)

Structural Repair Manual (SRM) 51-42-11 51-43-00 51-44-11

51-47-00

Weight and Balance Manual (WBM) Weight and Balance Manual

(WBM) Chapter 1-00-07

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 26

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF 003

Aircraft Maintenance Manual (AMM) 06-31-53 06-41-53 11-00-00

12-34-24 20-21-00 20-21-12

20-21-15 20-23-11 20-28-00

21-20-00 21-26-00 21-28-00

21-31-00 21-63-00 22-96-00

22-97-00 23-36-00 23-51-00

23-51-12 23-71-00 23-71-34

23-73-00 23-81-00 23-81-13

24-41-00 25-11-00 25-11-51

25-13-44 25-52-00 25-80-00

26-16-00 26-16-34 26-23-00

26-23-41 26-23-43 27-51-00

27-81-00 27-96-00 28-24-00

28-51-00 29-13-00 30-21-00

30-45-00 31-50-00 31-60-00

32-31-00 33-13-00 33-14-00

33-44-00 36-11-00 45-22-21

52-10-00 52-30-00 52-71-00

71-00-00

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-25-51 20-33-00 20-33-34

20-52-10 20-52-21 20-55-00

Process and Material Specification (PMS) Process and Material Specification

(PMS) 01-07-06

Process and Material Specification

(PMS) 01-07-10

Standards Manual (SM)

Structural Repair Manual (SRM) 51-42-11 51-43-00 51-44-11

51-47-00

Weight and Balance Manual (WBM) Weight and Balance Manual

(WBM) Chapter 1-00-07

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 27

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF 004

Aircraft Maintenance Manual (AMM) 06-31-53 06-41-53 11-00-00

12-34-24 20-21-00 20-21-12

20-21-15 20-23-11 20-28-00

21-20-00 21-26-00 21-28-00

21-31-00 21-63-00 22-96-00

22-97-00 23-36-00 23-51-00

23-51-12 23-71-00 23-71-34

23-73-00 23-81-00 23-81-13

24-41-00 25-11-00 25-11-51

25-13-44 25-52-00 25-80-00

26-16-00 26-16-34 26-23-00

26-23-41 26-23-43 27-51-00

27-81-00 27-96-00 28-24-00

28-51-00 29-13-00 30-21-00

30-45-00 31-50-00 31-60-00

32-31-00 33-13-00 33-14-00

33-44-00 36-11-00 45-22-21

52-10-00 52-30-00 52-71-00

71-00-00

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-25-51 20-33-00 20-33-34

20-52-10 20-52-21 20-55-00

Process and Material Specification (PMS) Process and Material Specification

(PMS) 01-07-06

Process and Material Specification

(PMS) 01-07-10

Standards Manual (SM)

Structural Repair Manual (SRM) 51-42-11 51-43-00 51-44-11

51-47-00

Weight and Balance Manual (WBM) Weight and Balance Manual

(WBM) Chapter 1-00-07

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 28

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF 005

Aircraft Maintenance Manual (AMM) 06-31-53 06-41-53 11-00-00

12-34-24 20-21-00 20-21-12

20-21-15 20-23-11 20-28-00

21-20-00 21-26-00 21-28-00

21-31-00 21-63-00 22-96-00

22-97-00 23-36-00 23-51-00

23-51-12 23-71-00 23-71-34

23-73-00 23-81-00 23-81-13

24-41-00 25-11-00 25-11-51

25-13-44 25-52-00 25-80-00

26-16-00 26-16-34 26-23-00

26-23-41 26-23-43 27-51-00

27-81-00 27-96-00 28-24-00

28-51-00 29-13-00 30-21-00

30-45-00 31-50-00 31-60-00

32-31-00 33-13-00 33-14-00

33-44-00 36-11-00 45-22-21

52-10-00 52-30-00 52-71-00

71-00-00

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-25-51 20-33-00 20-33-34

20-52-10 20-52-21 20-55-00

Process and Material Specification (PMS) Process and Material Specification

(PMS) 01-07-06

Process and Material Specification

(PMS) 01-07-10

Standards Manual (SM)

Structural Repair Manual (SRM) 51-42-11 51-43-00 51-44-11

51-47-00

Weight and Balance Manual (WBM) Weight and Balance Manual

(WBM) Chapter 1-00-07

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 29

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SERVICE BULLETIN

**CONF 006

Aircraft Maintenance Manual (AMM) 06-31-53 06-41-53 11-00-00

12-34-24 20-21-00 20-21-12

20-21-15 20-23-11 20-28-00

21-20-00 21-26-00 21-28-00

21-31-00 21-63-00 22-96-00

22-97-00 23-36-00 23-51-00

23-51-12 23-71-00 23-71-34

23-73-00 23-81-00 23-81-13

24-41-00 25-11-00 25-11-51

25-13-44 25-52-00 25-80-00

26-16-00 26-16-34 26-23-00

26-23-41 26-23-43 27-51-00

27-81-00 27-96-00 28-24-00

28-51-00 29-13-00 30-21-00

30-45-00 31-50-00 31-60-00

32-31-00 33-13-00 33-14-00

33-44-00 36-11-00 45-22-21

52-10-00 52-30-00 52-71-00

71-00-00

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-25-51 20-33-00 20-33-34

20-52-10 20-52-21 20-55-00

Process and Material Specification (PMS) Process and Material Specification

(PMS) 01-07-06

Process and Material Specification

(PMS) 01-07-10

Standards Manual (SM)

Structural Repair Manual (SRM) 51-42-11 51-43-00 51-44-11

51-47-00

Weight and Balance Manual (WBM) Weight and Balance Manual

(WBM) Chapter 1-00-07

**CONF ALL

K. PUBLICATION AFFECTED

Aircraft Maintenance Manual (AMM) 26-23-00 26-23-41 26-23-42

26-23-14 26-23-18 26-23-21

26-23-23 26-23-25 26-23-43

Aircraft Schematic Manual (ASM) 26-16-00 26-23-00 33-14-00

Aircraft Wiring List (AWL)

Aircraft Wiring Manual (AWM) 26-16-13 26-23-01 26-23-02

26-23-03 26-23-11 26-23-12

33-14-03 33-14-30 91-12-12

91-17-51 91-17-52

Flight Crew Operating Manual (FCOM) Vol. 1

Vol. 3

Illustrated Parts Catalog (IPC) 26-23-02 26-23-08 33-13-08

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 30

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SERVICE BULLETIN

Master Minimum Equipment List (MMEL)

Maintenance Planning Document (MPD) 262300-02-1

262300-04-2

262300-05-1

262300-13-1

262300-14-1

262300-15-1

This Service Bulletin has an operational impact. Please inform AIRBUS, at least four weeks

in advance, in case you need your operational documentation to be amended by an

intermediate revision prior to Service Bulletin embodiment. For this purpose, please request

the intermediate revision by fax, telex or mail to :

SEDCC, AIRBUS - Customer Services Directorate

Fax No.: 33 (0) 5 61 93 28 06

Sita No.: TLSBP7X

E-mail: sb.reporting@airbus.com

These amendments will be confirmed by the next normal revision of operational

documentation, once your Service Bulletin accomplishment report has been sent, as usual, to

our Customer Services Directorate (SEDCC).

L. INTERCHANGEABILITY/MIXABILITY

Not Applicable

M. SPARES

Plate-Integrally Lighted F33110259A00

Plate-Integrally Lighted F33110261A00

Plate-Integrally Lighted F33110305A00

Plate-Integrally Lighted F33110321A00

Plate-Integrally Lighted F33110330A00

Plate-Integrally Lighted F33110359A00

Plate Assy- Front 212VU F9251602100000

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 31

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@A340-500/600

SERVICE BULLETIN

This Page Intentionally Left Blank

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 32

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SERVICE BULLETIN

2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

(1) Procurement Addresses

Kit 265020D01R03

Kit 265020D02R04

Kit 265020D03R01

Kit 265020D04R01

Kit 265020D05R00

Kit 265020A01R00

Kit 265020A02R00

Kit 265020A03R00

Kit 265020A04R00

Kit 265020A05R00

Kit 265020A06R00

Kit 265020A07R00

Customers with aircraft shown in the

effectivity of this Service Bulletin should send

a purchase order to AIRBUS. Quote the

number of this Service Bulletin. The address

is :

AIRBUS Material, Logistics and Suppliers

Weg beim Jaeger 150

D-22335 Hamburg

Germany

For ordering by internet :

http://spares.airbus.com

For SB Kits by fax : +49 40 50 76 25 90

For Spares by fax : +49 40 50 76 40 12

Equipment BFEZ01

Equipment BFEZ04

Vendor part PN QA06753-03 is to be

procured from :

PALL AEROSPACE

CARDREW INDUSTRIAL ESTATE

REDRUTH, TR15 1SS

UNITED KINGDOM

Equipment BFEZ01

Equipment BFEZ04

Vendor part PN E61751-00-0001 is to be

procured from :

DAE SYSTEMS GMBH

REVALSTRASSE 1

23560 LUEBECK

GERMANY

Equipment BFEZ01

Equipment BFEZ04

Vendor part PN TP0714033 is to be procured

from :

AIRSCREW-HOWDEN LTD

111 WINDMILL ROAD

SUNBURY-ON-THAMES, TW16 7EF

UNITED KINGDOM

Equipment BFEZ01

Equipment BFEZ04

Vendor part PN HTE400115 is to be procured

from :

EATON AEROSPACE LIMITED

ABBEY PARK, SOUTHAMPTON ROAD

TITCHFIELD, FAREHAM,HANTS, PO14 4QA

UNITED KINGDOM

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 33

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SERVICE BULLETIN

(2) Price and Availability

Kit 265020A01R00

Cost 1,630.00 USD

Availability 90 calendar days from receipt of order

The Kit availability given above is the standard lead time from the date of your purchase

order. If you require Kits before this time, please include a retrofit planning schedule with

your order so that we can try to comply with your requirements.

The sales terms (costs and availability) are estimated in relation to economic conditions

at the issue date of the Service Bulletin.

Kit 265020A02R00

Cost 1,580.00 USD

Availability 90 calendar days from receipt of order

The Kit availability given above is the standard lead time from the date of your purchase

order. If you require Kits before this time, please include a retrofit planning schedule with

your order so that we can try to comply with your requirements.

The sales terms (costs and availability) are estimated in relation to economic conditions

at the issue date of the Service Bulletin.

Kit 265020A03R00

Cost 1,580.00 USD

Availability 90 calendar days from receipt of order

The Kit availability given above is the standard lead time from the date of your purchase

order. If you require Kits before this time, please include a retrofit planning schedule with

your order so that we can try to comply with your requirements.

The sales terms (costs and availability) are estimated in relation to economic conditions

at the issue date of the Service Bulletin.

Kit 265020A04R00

Cost 1,170.00 USD

Availability 90 calendar days from receipt of order

The Kit availability given above is the standard lead time from the date of your purchase

order. If you require Kits before this time, please include a retrofit planning schedule with

your order so that we can try to comply with your requirements.

The sales terms (costs and availability) are estimated in relation to economic conditions

at the issue date of the Service Bulletin.

Kit 265020A05R00

Cost 1,580.00 USD

Availability 90 calendar days from receipt of order

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 34

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SERVICE BULLETIN

The Kit availability given above is the standard lead time from the date of your purchase

order. If you require Kits before this time, please include a retrofit planning schedule with

your order so that we can try to comply with your requirements.

The sales terms (costs and availability) are estimated in relation to economic conditions

at the issue date of the Service Bulletin.

Kit 265020A06R00

Cost 1,580.00 USD

Availability 90 calendar days from receipt of order

The Kit availability given above is the standard lead time from the date of your purchase

order. If you require Kits before this time, please include a retrofit planning schedule with

your order so that we can try to comply with your requirements.

The sales terms (costs and availability) are estimated in relation to economic conditions

at the issue date of the Service Bulletin.

Kit 265020A07R00

Cost 1,580.00 USD

Availability 90 calendar days from receipt of order

The Kit availability given above is the standard lead time from the date of your purchase

order. If you require Kits before this time, please include a retrofit planning schedule with

your order so that we can try to comply with your requirements.

The sales terms (costs and availability) are estimated in relation to economic conditions

at the issue date of the Service Bulletin.

Kit 265020D01R03

Cost 9,060.00 USD

Availability 90 calendar days from receipt of order

The Kit availability given above is the standard lead time from the date of your purchase

order. If you require Kits before this time, please include a retrofit planning schedule with

your order so that we can try to comply with your requirements.

The sales terms (costs and availability) are estimated in relation to economic conditions

at the issue date of the Service Bulletin.

Kit 265020D02R04

Cost 438.00 USD

Availability 90 calendar days from receipt of order

The Kit availability given above is the standard lead time from the date of your purchase

order. If you require Kits before this time, please include a retrofit planning schedule with

your order so that we can try to comply with your requirements.

The sales terms (costs and availability) are estimated in relation to economic conditions

at the issue date of the Service Bulletin.

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 35

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SERVICE BULLETIN

Kit 265020D03R01

Cost 155.00 USD

Availability 90 calendar days from receipt of order

The Kit availability given above is the standard lead time from the date of your purchase

order. If you require Kits before this time, please include a retrofit planning schedule with

your order so that we can try to comply with your requirements.

The sales terms (costs and availability) are estimated in relation to economic conditions

at the issue date of the Service Bulletin.

Kit 265020D04R01

Cost 9,160.00 USD

Availability 90 calendar days from receipt of order

The Kit availability given above is the standard lead time from the date of your purchase

order. If you require Kits before this time, please include a retrofit planning schedule with

your order so that we can try to comply with your requirements.

The sales terms (costs and availability) are estimated in relation to economic conditions

at the issue date of the Service Bulletin.

Kit 265020D05R00

Cost 54.00 USD

Availability 90 calendar days from receipt of order

The Kit availability given above is the standard lead time from the date of your purchase

order. If you require Kits before this time, please include a retrofit planning schedule with

your order so that we can try to comply with your requirements.

The sales terms (costs and availability) are estimated in relation to economic conditions

at the issue date of the Service Bulletin.

B. INDUSTRY SUPPORT INFORMATION

For the organisation of this retrofit, operators are kindly requested to contact AIRBUS retrofit

management department.

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

France

Tel : (33) 5 67 19 06 22

E-mail : monitored.retrofit@airbus.com

Fax : (33) 5 61 93 27 45

AIRBUS will provide the Airbus kits at no charge, equipment are at no charge for the

operator. Airbus will also credit the man- hours indicated in this Service Bulletin. Credit will be

at the operator’s agreed in-house warranty labor rate for claims received not later than 90

days after completion of the last affected aircraft of your fleet.

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 36

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SERVICE BULLETIN

C. LIST OF COMPONENTS

Kit 265020A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE

NOTES

2 ASNA2083BG2-10 7 Screw

6 NSA937901MA2206 1 Module

7 NSA937901FM 2 Module

10 F9251088400000 1 Plate (10) F9251602100000

F1131101500000 1 Placard

F9000095226495 1 Bundle

NAS1102-04-5 44 Screw

NSA935401-03 350 TIE

NSA935401-05 700 TIE

NSA935401-08 600 Tie

NSA936604CA0931 28 Cap

NSA937901E2 1 Label

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 265020A02R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE

NOTES

1 F33110238A00 1 Plate (1) F33110259A00

Kit 265020A03R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE

NOTES

1 F33110263A00 1 Plate (1) F33110261A00

Kit 265020A04R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE

NOTES

1 F33110427A00 1 Plate (1) F33110330A00

Kit 265020A05R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE

NOTES

1 F33110381A00 1 Plate (1) F33110321A00

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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SERVICE BULLETIN

Kit 265020A06R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE

NOTES

1 F33110354A00 1 Plate (1) F33110359A00

Kit 265020A07R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE

NOTES

1 F33110444A00 1 Plate (1) F33110305A00

Kit 265020D01R03

ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE

NOTES

100 NAS1726-5E 8 NUT

101 NAS1305-2 8 BOLT

103 NAS1304-9 2 BOLT

104 NAS1726-4E 4 NUT

106 NAS1149F0332P 8 WASHER

113 NAS1726-3E 5 NUT

121 NSA5516A18NJ 4 CLAMP

125 NSA855008D10 1 TEE

132 A2627048220400 6 FITTING

133 NSA8202-6 8 ORING

134 A2627048221600 2 FITTING

139 NAS1304-12 2 BOLT

140 NAS1149D0432K 10 WASHER

141 NSA5355-5CA 2 WASHER

143 NAS1801-3-8 10 SCREW

144 NAS1149C0332R 13 WASHER

145 NAS1801-3-7 7 SCREW

146 NAS1100E4-34 6 SCREW

147 A2627048920000 2 WASHER

148 NSA5516A06NJ 4 CLAMP

152 E0090-10-320NN 2 LEAD

153 E0090-10-350NN 2 LEAD

155 NSA5527-03-03 2 SPACER

157 NAS1801-3-12 2 SCREW

158 NSA855006D10 2 UNION

159 NAS1801-3-10 2 SCREW

160 MS21103-4 2 CLAMP

212 G2627008001400 1 SECTION

213 F2627008100000 1 BRACKET

219 G2627006001000 1 TUBE

220 E0090-10-135NN 1 LEAD

221 G2627006000800 1 TUBE

222 G2627006001800 1 TUBE

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 38

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SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE

NOTES

223 F2627006003600 1 TUBE

224 A2627048220200 2 RESTRCTR

225 F2627006001400 1 TUBE

226 F2627006000000 1 TUBE

227 F2627007200000 1 HOSE

228 F2627007200200 1 HOSE

229 G2627006002000 1 TUBE

230 G2627006001200 1 TUBE

231 G2627006001400 1 TUBE

232 G2627006001600 1 TUBE

233 NSA855140-22D 1 CROSS

234 G2627005013200 1 TUBE

235 MS21902W10 1 UNION

236 A2627045107800 1 TUBE

237 NSA855113-34D 1 TEE

238 G2627005003400 1 TUBE

239 MS21916W10-4 2 REDUCER

240 F2627004120800 1 PLACARD

241 F2627004121400 1 PLACARD

242 F2627004121200 1 PLACARD

243 F2627004120400 1 PLACARD

244 F2627004120600 1 PLACARD

245 F2627004121600 1 PLACARD

246 F2627004121800 1 PLACARD

247 F2627004121000 1 PLACARD

248 G2627004020200 1 PLACARD

251 G2627005013000 1 TUBE

253 G2627005002000 1 TUBE

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 265020D02R04

ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE

NOTES

170 EN6081D4-09 28 RIVET

171 EN6081D6-14 30 RIVET

252 F5397757020200 2 ANGLE

253 F5397462009600 1 BRACKET

254 F5397462009800 1 BRACKET

281 ABS1577A05 1 BRACKET

282 ABS0787B05B 1 BRACKET

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 39

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SERVICE BULLETIN

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 265020D03R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE

NOTES

173 G9237018016600 1 PLCRDSET

174 NSA935401-04 20 TIE

175 NSA935401-05 30 TIE

176 EN3155-003F1614 2 CONTACT

177 NSA936603CC0100 23 CAP

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 265020D04R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE

NOTES

100 NAS1726-5E 8 NUT

101 NAS1305-2 8 BOLT

103 NAS1304-9 2 BOLT

104 NAS1726-4E 4 NUT

105 NAS563-11 4 BOLT

106 NAS1149F0332P 12 WASHER

113 NAS1726-3E 5 NUT

121 NSA5516A18NJ 4 CLAMP

125 NSA855008D10 1 TEE

132 A2627048220400 6 FITTING

133 NSA8202-6 8 ORING

134 A2627048221600 2 FITTING

139 NAS1304-12 2 BOLT

140 NAS1149D0432K 10 WASHER

141 NSA5355-5CA 2 WASHER

143 NAS1801-3-8 10 SCREW

144 NAS1149C0332R 13 WASHER

145 NAS1801-3-7 7 SCREW

146 NAS1100E4-34 6 SCREW

147 A2627048920000 2 WASHER

148 NSA5516A06NJ 4 CLAMP

152 E0090-10-320NN 2 LEAD

153 E0090-10-350NN 2 LEAD

155 NSA5527-03-03 2 SPACER

157 NAS1801-3-12 2 SCREW

158 NSA855006D10 2 UNION

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE

NOTES

159 NAS1801-3-10 2 SCREW

160 MS21103-4 2 CLAMP

212 G2627008001400 1 SECTION

213 F2627008100000 1 BRACKET

219 G2627006001000 1 TUBE

220 E0090-10-135NN 1 LEAD

221 G2627006000800 1 TUBE

222 G2627006001800 1 TUBE

223 F2627006003600 1 TUBE

224 A2627048220200 2 RESTRCTR

225 F2627006001400 1 TUBE

226 F2627006000000 1 TUBE

227 F2627007200000 1 HOSE

228 F2627007200200 1 HOSE

229 G2627006002000 1 TUBE

230 G2627006001200 1 TUBE

231 G2627006001400 1 TUBE

232 G2627006001600 1 TUBE

233 NSA855140-22D 1 CROSS

234 G2627005013200 1 TUBE

235 MS21902W10 1 UNION

236 A2627045107800 1 TUBE

237 NSA855113-34D 1 TEE

238 G2627005003400 1 TUBE

239 MS21916W10-4 2 REDUCER

240 F2627004120800 1 PLACARD

241 F2627004121400 1 PLACARD

242 F2627004121200 1 PLACARD

243 F2627004120400 1 PLACARD

244 F2627004120600 1 PLACARD

245 F2627004121600 1 PLACARD

246 F2627004121800 1 PLACARD

247 F2627004121000 1 PLACARD

248 G2627004020200 1 PLACARD

251 G2627005013000 1 TUBE

253 G2627005002000 1 TUBE

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 265020D05R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE

NOTES

266 NSA935401-03 25 TIE

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE

NOTES

269 NAS1149CN816R 4 WASHER

270 MS21919WCH8 4 CLAMP

271 NAS1801-08-23 2 SCREW

272 NAS1801-08-29 1 SCREW

274 NSA935809-09 4 SLEEVE

275 NAS1801-08-25 1 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.

D. LIST OF MATERIALS - OPERATOR SUPPLIED

(1) Consumable Materials

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO CML

MAT. No.

QTY PER A/C SEE

NOTES

Pure Mineral Vaseline Or PetroLatum04-012 As required

Electrical Bond Varnish 07-001B As required

Sealant, High Temperature 08-007C As required

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO CML

MAT. No.

QTY PER A/C SEE

NOTES

Oil, Hydraulic Petroleum Fluid 02-001 As required

Silicone Grease Pneumatic Syst

And Seals

04-011 As required

Electrical Bonding Coating (blue

Color)

07-001D As required

Abrasion Resistant Coating (Teflon

Polyuret)

07-003 As required

Internal Polyurethane Varnish 07-017 As required

General Purpose Adhesive

Honeycomb Filler

08-554 As required

Corrosion Inhibiting Fillet

Consistency

09-016 As required

Solvent General Purpose 11-026 As required

Low Voc Anti-Corrosion Primer 16-006F As required

Lint-Free Cotton Cloth 19-003 As required

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 42

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(2) Components

Component COMPD01

ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE

NOTES

LN9424A100 WIRE

(3) Equipment

Equipment BFEZ01

ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE

NOTES

214 QA06753-03 2 FILTER

215 E61751-00-0001 2 REDUCER

216 TP0714033 2 SWITCH

217 HTE400115 2 VALVE

Equipment BFEZ04

ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE

NOTES

214 QA06753-03 2 FILTER

215 E61751-00-0001 2 REDUCER

216 TP0714033 2 SWITCH

217 HTE400115 2 VALVE

E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

None

F. TOOLING

(1) Tooling - Price and Availability

None

(2) Tools

Operators interested in obtaining the tool kit and with aircraft shown in the effectivity of

this Service Bulletin should contact PERMASWAGE. The address is :

(1) Standard tool TOOLD01 :

PERMASWAGE

Zone Industrielle des Dames

BP 25

78344 Les Clayes Sous Bois Cedex

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 43

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

FRANCE

Tel. : +33 (0) 1 30 79 17 20

Fax : +33 (0) 1 34 81 02 21

E-mail : contact@permaswage.com

NOTE: Use these swaging tools of the D12000 series :

- Head assembly D12210-56 with power unit D12010-52.

Standard tool TOOLD01

ITEM TOOL N ̊ TOOL NAME QTY SEE

NOTES

D12102C07-02 PERMASWAGE Repair Kit

D12000 Series

2

(3) Special Tools

None

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 44

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS

Task 265020-831-848-001 - MODIFICATION

WARNING: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONS

INCLUDED IN THE REFERENCED PROCEDURES

WARNING: MAKE SURE THAT THE EXIT HATCH IS OPEN AND THAT IT STAYS OPEN

WHEN YOU DO THE TEST OF THE SMOKE DETECTION/FIRE EXTINGUISHING

SYSTEMS. THIS IS TO PREVENT ACCIDENTAL OPERATION OF THE FIRE

EXTINGUISHER AND THE RISK OF INJURY AND/OR SUFFOCATION.

WARNING: BE VERY CAREFUL WHEN YOU MOVE A FILLED FIRE EXTINGUISHER

BOTTLE. A HEAVY SHOCK COULD CAUSE UNWANTED DISCHARGE AND

INJURY TO PERSONS.

WARNING: WEAR GOGGLES/EYE PROTECTORS AND PROTECTIVE BREATHING

EQUIPMENT WHEN YOU DO THE TEST OF THE SMOKE DETECTION

SYSTEM. THIS GIVES YOU PROTECTION IF THE FIRE EXTINGUISHER

ACCIDENTALLY DISCHARGES.

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 ELECTRICAL 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

120 121 122 131 132 200 210 212 800

From 121 to 211

From 212 to 121

From 212 to 122

Modified FIN

212LF 582VT 582VT2 582VT3 703VT 703VT20 1712VT 1712VT17 2900VT 2900VT50

5WX 5WX1 5WXA 10WX 10WXA 11WX 11WXA 12WX 12WXA 13WX 13WXA

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 45

6

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@A340-500/600

SERVICE BULLETIN

Access

Door 132AZ 821 831 841

Panel 131AW 131BA 131BW 132CW 132NM 132PM 132RM 211EW

Manpower

TOTAL MANHOURS 166.50

ELAPSED TIME (HOURS) 89.00

**CONF 002

Zone

120 121 122 131 132 200 210 212 800

From 121 to 211

From 212 to 121

From 212 to 122

Modified FIN

212LF 582VT 582VT2 582VT3 703VT 703VT20 1712VT 1712VT17 2900VT 2900VT50

5WX 5WX1 5WXA 10WX 10WXA 11WX 11WXA 12WX 12WXA 13WX 13WXA

Access

Door 132AZ 821 831 841

Panel 131AW 131BA 131BW 132CW 132NM 132PM 132RM 211EW

Manpower

TOTAL MANHOURS 166.50

ELAPSED TIME (HOURS) 89.00

**CONF 003

Zone

120 121 122 131 132 200 210 212 800

From 121 to 211

From 212 to 121

From 212 to 122

Modified FIN

212LF 582VT 582VT2 582VT3 703VT 703VT20 1712VT 1712VT17 2900VT 2900VT50

5WX 5WX1 5WXA 10WX 10WXA 11WX 11WXA 12WX 12WXA 13WX 13WXA

Access

Door 132AZ 821 831 841

Panel 131AW 131BA 131BW 132CW 132NM 132PM 132RM 211EW

Manpower

TOTAL MANHOURS 166.50

ELAPSED TIME (HOURS) 89.00

**CONF 004

Zone

120 121 122 131 132 200 210 212 800

From 121 to 211

From 212 to 121

From 212 to 122

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 46

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

Modified FIN

212LF 582VT 582VT2 582VT3 703VT 703VT20 1712VT 1712VT17 2900VT 2900VT50

5WX 5WX1 5WXA 10WX 10WXA 11WX 11WXA 12WX 12WXA 13WX 13WXA

Access

Door 132AZ 821 831 841

Panel 131AW 131BA 131BW 132CW 132NM 132PM 132RM 211EW

Manpower

TOTAL MANHOURS 166.50

ELAPSED TIME (HOURS) 89.00

**CONF 005

Zone

120 121 122 131 132 200 210 212 800

From 121 to 211

From 212 to 121

From 212 to 122

Modified FIN

212LF 582VT 582VT2 582VT3 703VT 703VT20 1712VT 1712VT17 2900VT 2900VT50

5WX 5WX1 5WXA 10WX 10WXA 11WX 11WXA 12WX 12WXA 13WX 13WXA

Access

Door 132AZ 821 831 841

Panel 131AW 131BA 131BW 132CW 132NM 132PM 132RM 211EW

Manpower

TOTAL MANHOURS 166.50

ELAPSED TIME (HOURS) 89.00

**CONF 006

Zone

120 121 122 131 132 200 210 212 800

From 121 to 211

From 212 to 121

From 212 to 122

Modified FIN

212LF 582VT 582VT2 582VT3 703VT 703VT20 1712VT 1712VT17 2900VT 2900VT50

5WX 5WX1 5WXA 10WX 10WXA 11WX 11WXA 12WX 12WXA 13WX 13WXA

Access

Door 132AZ 821 831 841

Panel 131AW 131BA 131BW 132CW 132NM 132PM 132RM 211EW

Manpower

TOTAL MANHOURS 166.50

ELAPSED TIME (HOURS) 89.00

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 47

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF ALL

A. GENERAL

**CONF 001

(1) Subtask 265020-910-001-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-31-53

06-41-53

20-21-15, Page Block 201

Elec. Std. Practices Manual (ESPM) 20-25-51

20-33-00

20-33-34

20-52-21

Standards Manual (SM)

(a) For the frame identification, refer to AMM 06-31-53.

(b) For the identification of the access panels, refer to AMM 06-41-53.

(c) Tag all the parts you must remove and retain to make the subsequent installation

easier.

(d) Put all the retained hardware in identified plastic bags and attach the bags to the

related unit.

(e) 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.

(f) To torque tighten the electrical component fasteners, refer to AMM 20-21-15, Page

Block 201.

(g) Obey the instructions for the general wiring installation (Refer to ESPM 20-33-00).

(h) Put blanking caps on the disconnected electrical connectors.

(i) To install new wires, cut them to the necessary length, crimp the terminals and

connect them.

(j) When you install modified electrical connectors, do a visual check of each

connector which was disconnected to make sure that :

- All the electrical connectors are serviceable before you connect them,

- The label of the connector is the same as the label on the receptacle.

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 48

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

(k) Route the new wires with the wires that are in the aircraft.

(l) Use existing spare conduits to route new wires in location with difficult access.

(m) Do a continuity test of the new and the modified wires (Refer to ESPM 20-52-21).

(n) For the cable-ties application and tooling, refer to ESPM 20-33-34 and ESPM

20-25-51.

(2) Subtask 265020-910-201-001 - Standard Practices

Work Zones and Access Panels

Zone Access/Work location

120

132 Work location from Frame 35 to Frame 37.1

Manpower Resources

Skills NON SPECIFIC

Material necessary to do the job

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Oil, Hydraulic Petroleum

Fluid

02-001 As required

Silicone Grease Pneumatic

Syst And Seals

04-011 As required

Electrical Bonding Coating

(blue Color)

07-001D As required

Corrosion Inhibiting Fillet

Consistency

09-016 As required

Solvent General Purpose 11-026 As required

Lint-Free Cotton Cloth 19-003 As required

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

11-00-00, Page Block 201

20-21-00, Page Block 001

20-21-12, Page Block 201

20-23-11, Page Block 201

Consumable Material List (CML)

Process and Material Specification

(PMS)

Process and Material Specification (PMS)

01-07-06

Structural Repair Manual (SRM) 51-42-11

51-43-00

51-44-11

51-47-00

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 49

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

(a) Consumable Materials List (CML) for the specification of materials (Mat. No.) you

must use in this Service Bulletin.

(b) For the location of the sidewall panel (Refer to AMM 06-41-53, Page Block 001).

(c) Torque the pipe unions (Refer to AMM 20-21-12, Page Block 201).

(d) For standard torque values of nuts and screws (Refer to AMM 20-21-00, Page

Block 001).

(e) Clean the contact areas of bonding surfaces with :

Solvent General

Purpose

11-026 As required

and

Lint-Free Cotton

Cloth

19-003 As required

(f) Seal the bonding areas with :

Corrosion Inhibiting

Fillet Consistency

09-016 As required

(g) For protective coating of bonding connection use :

Electrical Bonding

Coating (blue Color)

07-001D As required

(h) Close all open tubes with blanking caps.

(i) For connecting of hydraulic tubes with PERMASWAGE fittings (Refer to AMM

20-23-11, Page Block 201).

(j) Apply hydraulic fluid to the packings before installation, use :

Oil, Hydraulic

Petroleum Fluid

02-001 As required

(k) The plumbing parts should be "dry" and shall be installed with care. Anti fretting

material is to be applied in very limited quantity (only with a drop of lubricant) and

only on the threads, use :

Silicone Grease

Pneumatic Syst

And Seals

04-011 As required

NOTE: Take care that no lubricant or other contamination residues remain

on inner surface of the pipes.

(l) For the installation of self-adhesive placards, (Refer to AMM 11-00-00, Page Block

201).

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 50

6

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SERVICE BULLETIN

(m) For fastener installation and removal (Refer to SRM 51-42-11).

(n) For fastener hole and drill data (Refer to SRM 51-44-11).

(o) For oversize and alternate fastener installation (Refer to SRM 51-43-00).

(p) For fastener spacing and margin data (Refer to SRM 51-47-00).

(q) Cut the rivets to the required length, if necessary.

(r) For the installation of heat shrinkable sleeves (Refer to Process and Material

Specification (PMS) 01-07-06).

(3) Subtask 265020-839-001-001 - 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 265020-910-001-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-31-53

06-41-53

20-21-15, Page Block 201

Elec. Std. Practices Manual (ESPM) 20-25-51

20-33-00

20-33-34

20-52-21

Standards Manual (SM)

(a) For the frame identification, refer to AMM 06-31-53.

(b) For the identification of the access panels, refer to AMM 06-41-53.

(c) Tag all the parts you must remove and retain to make the subsequent installation

easier.

(d) Put all the retained hardware in identified plastic bags and attach the bags to the

related unit.

(e) 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.

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 51

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

(f) To torque tighten the electrical component fasteners, refer to AMM 20-21-15, Page

Block 201.

(g) Obey the instructions for the general wiring installation (Refer to ESPM 20-33-00).

(h) Put blanking caps on the disconnected electrical connectors.

(i) To install new wires, cut them to the necessary length, crimp the terminals and

connect them.

(j) When you install modified electrical connectors, do a visual check of each

connector which was disconnected to make sure that :

- All the electrical connectors are serviceable before you connect them,

- The label of the connector is the same as the label on the receptacle.

(k) Route the new wires with the wires that are in the aircraft.

(l) Use existing spare conduits to route new wires in location with difficult access.

(m) Do a continuity test of the new and the modified wires (Refer to ESPM 20-52-21).

(n) For the cable-ties application and tooling, refer to ESPM 20-33-34 and ESPM

20-25-51.

(2) Subtask 265020-910-201-001 - Standard Practices

Work Zones and Access Panels

Zone Access/Work location

120

132 Work location from Frame 35 to Frame 37.1

Manpower Resources

Skills NON SPECIFIC

Material necessary to do the job

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Oil, Hydraulic Petroleum

Fluid

02-001 As required

Silicone Grease Pneumatic

Syst And Seals

04-011 As required

Electrical Bonding Coating

(blue Color)

07-001D As required

Corrosion Inhibiting Fillet

Consistency

09-016 As required

Solvent General Purpose 11-026 As required

Lint-Free Cotton Cloth 19-003 As required

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 52

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

11-00-00, Page Block 201

20-21-00, Page Block 001

20-21-12, Page Block 201

20-23-11, Page Block 201

Consumable Material List (CML)

Process and Material Specification

(PMS)

Process and Material Specification (PMS)

01-07-06

Structural Repair Manual (SRM) 51-42-11

51-43-00

51-44-11

51-47-00

(a) Consumable Materials List (CML) for the specification of materials (Mat. No.) you

must use in this Service Bulletin.

(b) For the location of the sidewall panel (Refer to AMM 06-41-53, Page Block 001).

(c) Torque the pipe unions (Refer to AMM 20-21-12, Page Block 201).

(d) For standard torque values of nuts and screws (Refer to AMM 20-21-00, Page

Block 001).

(e) Clean the contact areas of bonding surfaces with :

Solvent General

Purpose

11-026 As required

and

Lint-Free Cotton

Cloth

19-003 As required

(f) Seal the bonding areas with :

Corrosion Inhibiting

Fillet Consistency

09-016 As required

(g) For protective coating of bonding connection use :

Electrical Bonding

Coating (blue Color)

07-001D As required

(h) Close all open tubes with blanking caps.

(i) For connecting of hydraulic tubes with PERMASWAGE fittings (Refer to AMM

20-23-11, Page Block 201).

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 53

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

(j) Apply hydraulic fluid to the packings before installation, use :

Oil, Hydraulic

Petroleum Fluid

02-001 As required

(k) The plumbing parts should be "dry" and shall be installed with care. Anti fretting

material is to be applied in very limited quantity (only with a drop of lubricant) and

only on the threads, use :

Silicone Grease

Pneumatic Syst

And Seals

04-011 As required

NOTE: Take care that no lubricant or other contamination residues remain

on inner surface of the pipes.

(l) For the installation of self-adhesive placards, (Refer to AMM 11-00-00, Page Block

201).

(m) For fastener installation and removal (Refer to SRM 51-42-11).

(n) For fastener hole and drill data (Refer to SRM 51-44-11).

(o) For oversize and alternate fastener installation (Refer to SRM 51-43-00).

(p) For fastener spacing and margin data (Refer to SRM 51-47-00).

(q) Cut the rivets to the required length, if necessary.

(r) For the installation of heat shrinkable sleeves (Refer to Process and Material

Specification (PMS) 01-07-06).

(3) Subtask 265020-839-001-001 - 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 003

(1) Subtask 265020-910-001-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-31-53

06-41-53

20-21-15, Page Block 201

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 54

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

References

Elec. Std. Practices Manual (ESPM) 20-25-51

20-33-00

20-33-34

20-52-21

Standards Manual (SM)

(a) For the frame identification, refer to AMM 06-31-53.

(b) For the identification of the access panels, refer to AMM 06-41-53.

(c) Tag all the parts you must remove and retain to make the subsequent installation

easier.

(d) Put all the retained hardware in identified plastic bags and attach the bags to the

related unit.

(e) 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.

(f) To torque tighten the electrical component fasteners, refer to AMM 20-21-15, Page

Block 201.

(g) Obey the instructions for the general wiring installation (Refer to ESPM 20-33-00).

(h) Put blanking caps on the disconnected electrical connectors.

(i) To install new wires, cut them to the necessary length, crimp the terminals and

connect them.

(j) When you install modified electrical connectors, do a visual check of each

connector which was disconnected to make sure that :

- All the electrical connectors are serviceable before you connect them,

- The label of the connector is the same as the label on the receptacle.

(k) Route the new wires with the wires that are in the aircraft.

(l) Use existing spare conduits to route new wires in location with difficult access.

(m) Do a continuity test of the new and the modified wires (Refer to ESPM 20-52-21).

(n) For the cable-ties application and tooling, refer to ESPM 20-33-34 and ESPM

20-25-51.

(2) Subtask 265020-910-201-001 - Standard Practices

Work Zones and Access Panels

Zone Access/Work location

120

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 55

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

132 Work location from Frame 35 to Frame 37.1

Manpower Resources

Skills NON SPECIFIC

Material necessary to do the job

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Oil, Hydraulic Petroleum

Fluid

02-001 As required

Silicone Grease Pneumatic

Syst And Seals

04-011 As required

Electrical Bonding Coating

(blue Color)

07-001D As required

Corrosion Inhibiting Fillet

Consistency

09-016 As required

Solvent General Purpose 11-026 As required

Lint-Free Cotton Cloth 19-003 As required

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

11-00-00, Page Block 201

20-21-00, Page Block 001

20-21-12, Page Block 201

20-23-11, Page Block 201

Consumable Material List (CML)

Process and Material Specification

(PMS)

Process and Material Specification (PMS)

01-07-06

Structural Repair Manual (SRM) 51-42-11

51-43-00

51-44-11

51-47-00

(a) Consumable Materials List (CML) for the specification of materials (Mat. No.) you

must use in this Service Bulletin.

(b) For the location of the sidewall panel (Refer to AMM 06-41-53, Page Block 001).

(c) Torque the pipe unions (Refer to AMM 20-21-12, Page Block 201).

(d) For standard torque values of nuts and screws (Refer to AMM 20-21-00, Page

Block 001).

(e) Clean the contact areas of bonding surfaces with :

Solvent General

Purpose

11-026 As required

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 56

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

and

Lint-Free Cotton

Cloth

19-003 As required

(f) Seal the bonding areas with :

Corrosion Inhibiting

Fillet Consistency

09-016 As required

(g) For protective coating of bonding connection use :

Electrical Bonding

Coating (blue Color)

07-001D As required

(h) Close all open tubes with blanking caps.

(i) For connecting of hydraulic tubes with PERMASWAGE fittings (Refer to AMM

20-23-11, Page Block 201).

(j) Apply hydraulic fluid to the packings before installation, use :

Oil, Hydraulic

Petroleum Fluid

02-001 As required

(k) The plumbing parts should be "dry" and shall be installed with care. Anti fretting

material is to be applied in very limited quantity (only with a drop of lubricant) and

only on the threads, use :

Silicone Grease

Pneumatic Syst

And Seals

04-011 As required

NOTE: Take care that no lubricant or other contamination residues remain

on inner surface of the pipes.

(l) For the installation of self-adhesive placards, (Refer to AMM 11-00-00, Page Block

201).

(m) For fastener installation and removal (Refer to SRM 51-42-11).

(n) For fastener hole and drill data (Refer to SRM 51-44-11).

(o) For oversize and alternate fastener installation (Refer to SRM 51-43-00).

(p) For fastener spacing and margin data (Refer to SRM 51-47-00).

(q) Cut the rivets to the required length, if necessary.

(r) For the installation of heat shrinkable sleeves (Refer to Process and Material

Specification (PMS) 01-07-06).

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 57

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

(3) Subtask 265020-839-001-001 - 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 004

(1) Subtask 265020-910-001-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-31-53

06-41-53

20-21-15, Page Block 201

Elec. Std. Practices Manual (ESPM) 20-25-51

20-33-00

20-33-34

20-52-21

Standards Manual (SM)

(a) For the frame identification, refer to AMM 06-31-53.

(b) For the identification of the access panels, refer to AMM 06-41-53.

(c) Tag all the parts you must remove and retain to make the subsequent installation

easier.

(d) Put all the retained hardware in identified plastic bags and attach the bags to the

related unit.

(e) 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.

(f) To torque tighten the electrical component fasteners, refer to AMM 20-21-15, Page

Block 201.

(g) Obey the instructions for the general wiring installation (Refer to ESPM 20-33-00).

(h) Put blanking caps on the disconnected electrical connectors.

(i) To install new wires, cut them to the necessary length, crimp the terminals and

connect them.

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 58

6

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@A340-500/600

SERVICE BULLETIN

(j) When you install modified electrical connectors, do a visual check of each

connector which was disconnected to make sure that :

- All the electrical connectors are serviceable before you connect them,

- The label of the connector is the same as the label on the receptacle.

(k) Route the new wires with the wires that are in the aircraft.

(l) Use existing spare conduits to route new wires in location with difficult access.

(m) Do a continuity test of the new and the modified wires (Refer to ESPM 20-52-21).

(n) For the cable-ties application and tooling, refer to ESPM 20-33-34 and ESPM

20-25-51.

(2) Subtask 265020-910-201-001 - Standard Practices

Work Zones and Access Panels

Zone Access/Work location

120

132 Work location from Frame 35 to Frame 37.1

Manpower Resources

Skills NON SPECIFIC

Material necessary to do the job

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Oil, Hydraulic Petroleum

Fluid

02-001 As required

Silicone Grease Pneumatic

Syst And Seals

04-011 As required

Electrical Bonding Coating

(blue Color)

07-001D As required

Corrosion Inhibiting Fillet

Consistency

09-016 As required

Solvent General Purpose 11-026 As required

Lint-Free Cotton Cloth 19-003 As required

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

11-00-00, Page Block 201

20-21-00, Page Block 001

20-21-12, Page Block 201

20-23-11, Page Block 201

Consumable Material List (CML)

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 59

6

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@A340-500/600

SERVICE BULLETIN

References

Process and Material Specification

(PMS)

Process and Material Specification (PMS)

01-07-06

Structural Repair Manual (SRM) 51-42-11

51-43-00

51-44-11

51-47-00

(a) Consumable Materials List (CML) for the specification of materials (Mat. No.) you

must use in this Service Bulletin.

(b) For the location of the sidewall panel (Refer to AMM 06-41-53, Page Block 001).

(c) Torque the pipe unions (Refer to AMM 20-21-12, Page Block 201).

(d) For standard torque values of nuts and screws (Refer to AMM 20-21-00, Page

Block 001).

(e) Clean the contact areas of bonding surfaces with :

Solvent General

Purpose

11-026 As required

and

Lint-Free Cotton

Cloth

19-003 As required

(f) Seal the bonding areas with :

Corrosion Inhibiting

Fillet Consistency

09-016 As required

(g) For protective coating of bonding connection use :

Electrical Bonding

Coating (blue Color)

07-001D As required

(h) Close all open tubes with blanking caps.

(i) For connecting of hydraulic tubes with PERMASWAGE fittings (Refer to AMM

20-23-11, Page Block 201).

(j) Apply hydraulic fluid to the packings before installation, use :

Oil, Hydraulic

Petroleum Fluid

02-001 As required

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 60

6

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@A340-500/600

SERVICE BULLETIN

(k) The plumbing parts should be "dry" and shall be installed with care. Anti fretting

material is to be applied in very limited quantity (only with a drop of lubricant) and

only on the threads, use :

Silicone Grease

Pneumatic Syst

And Seals

04-011 As required

NOTE: Take care that no lubricant or other contamination residues remain

on inner surface of the pipes.

(l) For the installation of self-adhesive placards, (Refer to AMM 11-00-00, Page Block

201).

(m) For fastener installation and removal (Refer to SRM 51-42-11).

(n) For fastener hole and drill data (Refer to SRM 51-44-11).

(o) For oversize and alternate fastener installation (Refer to SRM 51-43-00).

(p) For fastener spacing and margin data (Refer to SRM 51-47-00).

(q) Cut the rivets to the required length, if necessary.

(r) For the installation of heat shrinkable sleeves (Refer to Process and Material

Specification (PMS) 01-07-06).

(3) Subtask 265020-839-001-001 - 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 005

(1) Subtask 265020-910-001-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-31-53

06-41-53

20-21-15, Page Block 201

Elec. Std. Practices Manual (ESPM) 20-25-51

20-33-00

20-33-34

20-52-21

Standards Manual (SM)

(a) For the frame identification, refer to AMM 06-31-53.

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 61

6

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@A340-500/600

SERVICE BULLETIN

(b) For the identification of the access panels, refer to AMM 06-41-53.

(c) Tag all the parts you must remove and retain to make the subsequent installation

easier.

(d) Put all the retained hardware in identified plastic bags and attach the bags to the

related unit.

(e) 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.

(f) To torque tighten the electrical component fasteners, refer to AMM 20-21-15, Page

Block 201.

(g) Obey the instructions for the general wiring installation (Refer to ESPM 20-33-00).

(h) Put blanking caps on the disconnected electrical connectors.

(i) To install new wires, cut them to the necessary length, crimp the terminals and

connect them.

(j) When you install modified electrical connectors, do a visual check of each

connector which was disconnected to make sure that :

- All the electrical connectors are serviceable before you connect them,

- The label of the connector is the same as the label on the receptacle.

(k) Route the new wires with the wires that are in the aircraft.

(l) Use existing spare conduits to route new wires in location with difficult access.

(m) Do a continuity test of the new and the modified wires (Refer to ESPM 20-52-21).

(n) For the cable-ties application and tooling, refer to ESPM 20-33-34 and ESPM

20-25-51.

(2) Subtask 265020-910-201-001 - Standard Practices

Work Zones and Access Panels

Zone Access/Work location

120

132 Work location from Frame 35 to Frame 37.1

Manpower Resources

Skills NON SPECIFIC

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 62

6

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@A340-500/600

SERVICE BULLETIN

Material necessary to do the job

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Oil, Hydraulic Petroleum

Fluid

02-001 As required

Silicone Grease Pneumatic

Syst And Seals

04-011 As required

Electrical Bonding Coating

(blue Color)

07-001D As required

Corrosion Inhibiting Fillet

Consistency

09-016 As required

Solvent General Purpose 11-026 As required

Lint-Free Cotton Cloth 19-003 As required

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

11-00-00, Page Block 201

20-21-00, Page Block 001

20-21-12, Page Block 201

20-23-11, Page Block 201

Consumable Material List (CML)

Process and Material Specification

(PMS)

Process and Material Specification (PMS)

01-07-06

Structural Repair Manual (SRM) 51-42-11

51-43-00

51-44-11

51-47-00

(a) Consumable Materials List (CML) for the specification of materials (Mat. No.) you

must use in this Service Bulletin.

(b) For the location of the sidewall panel (Refer to AMM 06-41-53, Page Block 001).

(c) Torque the pipe unions (Refer to AMM 20-21-12, Page Block 201).

(d) For standard torque values of nuts and screws (Refer to AMM 20-21-00, Page

Block 001).

(e) Clean the contact areas of bonding surfaces with :

Solvent General

Purpose

11-026 As required

and

Lint-Free Cotton

Cloth

19-003 As required

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 63

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

(f) Seal the bonding areas with :

Corrosion Inhibiting

Fillet Consistency

09-016 As required

(g) For protective coating of bonding connection use :

Electrical Bonding

Coating (blue Color)

07-001D As required

(h) Close all open tubes with blanking caps.

(i) For connecting of hydraulic tubes with PERMASWAGE fittings (Refer to AMM

20-23-11, Page Block 201).

(j) Apply hydraulic fluid to the packings before installation, use :

Oil, Hydraulic

Petroleum Fluid

02-001 As required

(k) The plumbing parts should be "dry" and shall be installed with care. Anti fretting

material is to be applied in very limited quantity (only with a drop of lubricant) and

only on the threads, use :

Silicone Grease

Pneumatic Syst

And Seals

04-011 As required

NOTE: Take care that no lubricant or other contamination residues remain

on inner surface of the pipes.

(l) For the installation of self-adhesive placards, (Refer to AMM 11-00-00, Page Block

201).

(m) For fastener installation and removal (Refer to SRM 51-42-11).

(n) For fastener hole and drill data (Refer to SRM 51-44-11).

(o) For oversize and alternate fastener installation (Refer to SRM 51-43-00).

(p) For fastener spacing and margin data (Refer to SRM 51-47-00).

(q) Cut the rivets to the required length, if necessary.

(r) For the installation of heat shrinkable sleeves (Refer to Process and Material

Specification (PMS) 01-07-06).

(3) Subtask 265020-839-001-001 - Documentation

Manpower Resources

Skills NON SPECIFIC

Write in the applicable aircraft records that you have done all the work given in this

Service Bulletin.

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 64

6

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@A340-500/600

SERVICE BULLETIN

**CONF 006

(1) Subtask 265020-910-001-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-31-53

06-41-53

20-21-15, Page Block 201

Elec. Std. Practices Manual (ESPM) 20-25-51

20-33-00

20-33-34

20-52-21

Standards Manual (SM)

(a) For the frame identification, refer to AMM 06-31-53.

(b) For the identification of the access panels, refer to AMM 06-41-53.

(c) Tag all the parts you must remove and retain to make the subsequent installation

easier.

(d) Put all the retained hardware in identified plastic bags and attach the bags to the

related unit.

(e) 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.

(f) To torque tighten the electrical component fasteners, refer to AMM 20-21-15, Page

Block 201.

(g) Obey the instructions for the general wiring installation (Refer to ESPM 20-33-00).

(h) Put blanking caps on the disconnected electrical connectors.

(i) To install new wires, cut them to the necessary length, crimp the terminals and

connect them.

(j) When you install modified electrical connectors, do a visual check of each

connector which was disconnected to make sure that :

- All the electrical connectors are serviceable before you connect them,

- The label of the connector is the same as the label on the receptacle.

(k) Route the new wires with the wires that are in the aircraft.

(l) Use existing spare conduits to route new wires in location with difficult access.

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 65

6

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@A340-500/600

SERVICE BULLETIN

(m) Do a continuity test of the new and the modified wires (Refer to ESPM 20-52-21).

(n) For the cable-ties application and tooling, refer to ESPM 20-33-34 and ESPM

20-25-51.

(2) Subtask 265020-910-201-001 - Standard Practices

Work Zones and Access Panels

Zone Access/Work location

120

132 Work location from Frame 35 to Frame 37.1

Manpower Resources

Skills NON SPECIFIC

Material necessary to do the job

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Oil, Hydraulic Petroleum

Fluid

02-001 As required

Silicone Grease Pneumatic

Syst And Seals

04-011 As required

Electrical Bonding Coating

(blue Color)

07-001D As required

Corrosion Inhibiting Fillet

Consistency

09-016 As required

Solvent General Purpose 11-026 As required

Lint-Free Cotton Cloth 19-003 As required

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

11-00-00, Page Block 201

20-21-00, Page Block 001

20-21-12, Page Block 201

20-23-11, Page Block 201

Consumable Material List (CML)

Process and Material Specification

(PMS)

Process and Material Specification (PMS)

01-07-06

Structural Repair Manual (SRM) 51-42-11

51-43-00

51-44-11

51-47-00

(a) Consumable Materials List (CML) for the specification of materials (Mat. No.) you

must use in this Service Bulletin.

(b) For the location of the sidewall panel (Refer to AMM 06-41-53, Page Block 001).

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 66

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

(c) Torque the pipe unions (Refer to AMM 20-21-12, Page Block 201).

(d) For standard torque values of nuts and screws (Refer to AMM 20-21-00, Page

Block 001).

(e) Clean the contact areas of bonding surfaces with :

Solvent General

Purpose

11-026 As required

and

Lint-Free Cotton

Cloth

19-003 As required

(f) Seal the bonding areas with :

Corrosion Inhibiting

Fillet Consistency

09-016 As required

(g) For protective coating of bonding connection use :

Electrical Bonding

Coating (blue Color)

07-001D As required

(h) Close all open tubes with blanking caps.

(i) For connecting of hydraulic tubes with PERMASWAGE fittings (Refer to AMM

20-23-11, Page Block 201).

(j) Apply hydraulic fluid to the packings before installation, use :

Oil, Hydraulic

Petroleum Fluid

02-001 As required

(k) The plumbing parts should be "dry" and shall be installed with care. Anti fretting

material is to be applied in very limited quantity (only with a drop of lubricant) and

only on the threads, use :

Silicone Grease

Pneumatic Syst

And Seals

04-011 As required

NOTE: Take care that no lubricant or other contamination residues remain

on inner surface of the pipes.

(l) For the installation of self-adhesive placards, (Refer to AMM 11-00-00, Page Block

201).

(m) For fastener installation and removal (Refer to SRM 51-42-11).

(n) For fastener hole and drill data (Refer to SRM 51-44-11).

(o) For oversize and alternate fastener installation (Refer to SRM 51-43-00).

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 67

6

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@A340-500/600

SERVICE BULLETIN

(p) For fastener spacing and margin data (Refer to SRM 51-47-00).

(q) Cut the rivets to the required length, if necessary.

(r) For the installation of heat shrinkable sleeves (Refer to Process and Material

Specification (PMS) 01-07-06).

(3) Subtask 265020-839-001-001 - 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 265020-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802

Task 26-16-34-000-801

(a) Make sure that the aircraft is electrically grounded (Refer to AMM Task

12-34-24-860-802).

(b) Put the access platform(s) in position.

(c) Do the preparation procedure as specified in the removal of the Smoke Detection

Control Unit (SDCU) (20WH) (Refer to AMM Task 26-16-34-000-801).

(2) Subtask 265020-941-201-001 - Job Set-up

Work Zones and Access Panels

Zone Access/Work location

210

800 Access Door 821

132 Access Panel 132PM, Panel 132NM, Panel 132RM

Work location from Frame 35 to Frame 37.1

120

131 Access Panel 131AW, Panel 131BW, Panel 132CW,

Panel 131BA

Work location from Frame 35 to Frame 37.1

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 68

6

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@A340-500/600

SERVICE BULLETIN

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 21-20-00-010-801

24-41-00, Page Block 201

25-52-00, Page Block 201

Task 25-52-00-000-801

Task 52-30-00-010-801

Task 52-30-00-010-802

(a) Open the FWD cargo-compartment door 821 (Refer to AMM Task

52-30-00-010-801) or (Refer to AMM Task 52-30-00-010-802).

(b) In the FWD cargo-compartment, remove the sidewall panels 131PM, 132NM and

132RM(Refer to AMM 25-52-00, Page Block 201).

(c) In the FWD cargo-compartment, remove the partition panels 131AW, 131BW,

132CW and the ceiling panels 131BA, 131PA and 131NA (Refer to AMM Task

25-52-00-000-801).

(d) Remove the air-conditioning distribution ducts in the affected area (Refer to AMM

Task 21-20-00-010-801).

(e) Open the avionics compartment door 132AZ.

(f) Energize the aircraft electrical circuits (Refer to AMM 24-41-00, Page Block 201).

(g) Open, safety and tag this(these) circuit breaker(s) :

PANEL DESIGNATION FIN LOCATION SEE

NOTES

722 EXTC FAN FWD CARGO 11HN 34 A

722 SDCU CHAN 2 12WH 36 T

722 CRG FIRE EXTNG/B 2WX 44 W

742 CRG FIRE EXTNG/A 1WX 68 J

742 SDCU CHAN 1 11WH 75 L

(3) Subtask 265020-010-002-001 - Remove/Open for Access (Upper Half of Fuselage)

Work Zones and Access Panels

Zone Access/Work location

200

Manpower Resources

Skills NON SPECIFIC

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 69

6

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@A340-500/600

SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) Task 23-51-12-000-801

Task 23-71-34-000-801

Task 23-81-13-000-801

Task 25-11-51-000-801

Task 25-13-44-000-801

Task 25-13-44-000-802

Task 45-22-21-000-801

Task 52-10-00-010-801

(a) Open the FWD passenger/crew door(s) 831 or 841 (Refer to AMM Task

52-10-00-010-801).

(b) In the cockpit, remove the ceiling panels 211LC, 211MC, 212NC and the strips

211KC and 212CC (Refer to AMM Task 25-13-44-000-801).

(c) From the overhead panel, remove and disconnect (if installed) :

- Reset C/B panel 262VU

- External View Camera Panel 272VU

- Reading Light Panel 252VU2

- AIREADOR panel

- Audio Control Panel (2RN3) (Refer to AMM Task 23-51-12-000-801)

- Data Loader Selector (101TD) (Refer to AMM Task 45-22-21-000-801)

- Cockpit Voice Recorder (CVR) Control Unit (1RK) (Refer to AMM Task

23-71-34-000-801)

- Radio Management Panel (1RG3) (Refer to AMM Task 23-81-13-000-801).

(d) Remove the captain seat (Refer to AMM Task 25-11-51-000-801).

(e) Remove the panel (211EW) (Refer to AMM Task 25-13-44-000-802).

(4) Subtask 265020-862-001-001 - De-energize Electrical Network

Manpower Resources

Skills NON SPECIFIC

(a) In the cockpit, on the panel 235VU, make sure that these pushbutton switches are

released :

- BAT 1, BAT 2, APU BAT,

- GEN 1 (2,3, 4), APU GEN,

- EXT A(B).

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 70

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@A340-500/600

SERVICE BULLETIN

(b) Open, safety and tag these circuit breakers :

PANEL DESIGNATION FIN LOCATION SEE

NOTES

742VU 701PP 10PB1 72 S

742VU 702PP 10PB2 71 S

(c) Make sure that there are warning notices in the cockpit to tell persons not to

operate the pushbutton switches on the overhead panel :

- 211VU (EMER ELEC PWR)

- 235VU (ELEC).

(d) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not

start the Auxiliary Power Unit (APU).

(e) Make sure that the external connector(s) is (are) not connected to the aircraft

receptacle(s) EXT PWR A (B).

(f) Make sure that there is a warning notice at the access door 121EL to tell persons

not to connect the external power connector(s).

**CONF 002

(1) Subtask 265020-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802

Task 26-16-34-000-801

(a) Make sure that the aircraft is electrically grounded (Refer to AMM Task

12-34-24-860-802).

(b) Put the access platform(s) in position.

(c) Do the preparation procedure as specified in the removal of the Smoke Detection

Control Unit (SDCU) (20WH) (Refer to AMM Task 26-16-34-000-801).

(2) Subtask 265020-941-201-001 - Job Set-up

Work Zones and Access Panels

Zone Access/Work location

210

800 Access Door 821

132 Access Panel 132PM, Panel 132NM, Panel 132RM

Work location from Frame 35 to Frame 37.1

120

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 71

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@A340-500/600

SERVICE BULLETIN

131 Access Panel 131AW, Panel 131BW, Panel 132CW,

Panel 131BA

Work location from Frame 35 to Frame 37.1

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 21-20-00-010-801

24-41-00, Page Block 201

25-52-00, Page Block 201

Task 25-52-00-000-801

Task 52-30-00-010-801

Task 52-30-00-010-802

(a) Open the FWD cargo-compartment door 821 (Refer to AMM Task

52-30-00-010-801) or (Refer to AMM Task 52-30-00-010-802).

(b) In the FWD cargo-compartment, remove the sidewall panels 131PM, 132NM and

132RM(Refer to AMM 25-52-00, Page Block 201).

(c) In the FWD cargo-compartment, remove the partition panels 131AW, 131BW,

132CW and the ceiling panels 131BA, 131PA and 131NA (Refer to AMM Task

25-52-00-000-801).

(d) Remove the air-conditioning distribution ducts in the affected area (Refer to AMM

Task 21-20-00-010-801).

(e) Open the avionics compartment door 132AZ.

(f) Energize the aircraft electrical circuits (Refer to AMM 24-41-00, Page Block 201).

(g) Open, safety and tag this(these) circuit breaker(s) :

PANEL DESIGNATION FIN LOCATION SEE

NOTES

722 EXTC FAN FWD CARGO 11HN 34 A

722 SDCU CHAN 2 12WH 36 T

722 CRG FIRE EXTNG/B 2WX 44 W

742 CRG FIRE EXTNG/A 1WX 68 J

742 SDCU CHAN 1 11WH 75 L

(3) Subtask 265020-010-002-001 - Remove/Open for Access (Upper Half of Fuselage)

Work Zones and Access Panels

Zone Access/Work location

200

Manpower Resources

Skills NON SPECIFIC

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 72

6

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@A340-500/600

SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) Task 23-51-12-000-801

Task 23-71-34-000-801

Task 23-81-13-000-801

Task 25-11-51-000-801

Task 25-13-44-000-801

Task 25-13-44-000-802

Task 45-22-21-000-801

Task 52-10-00-010-801

(a) Open the FWD passenger/crew door(s) 831 or 841 (Refer to AMM Task

52-10-00-010-801).

(b) In the cockpit, remove the ceiling panels 211LC, 211MC, 212NC and the strips

211KC and 212CC (Refer to AMM Task 25-13-44-000-801).

(c) From the overhead panel, remove and disconnect (if installed) :

- Reset C/B panel 262VU

- External View Camera Panel 272VU

- Reading Light Panel 252VU2

- AIREADOR panel

- Audio Control Panel (2RN3) (Refer to AMM Task 23-51-12-000-801)

- Data Loader Selector (101TD) (Refer to AMM Task 45-22-21-000-801)

- Cockpit Voice Recorder (CVR) Control Unit (1RK) (Refer to AMM Task

23-71-34-000-801)

- Radio Management Panel (1RG3) (Refer to AMM Task 23-81-13-000-801).

(d) Remove the captain seat (Refer to AMM Task 25-11-51-000-801).

(e) Remove the panel (211EW) (Refer to AMM Task 25-13-44-000-802).

(4) Subtask 265020-862-001-001 - De-energize Electrical Network

Manpower Resources

Skills NON SPECIFIC

(a) In the cockpit, on the panel 235VU, make sure that these pushbutton switches are

released :

- BAT 1, BAT 2, APU BAT,

- GEN 1 (2,3, 4), APU GEN,

- EXT A(B).

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 73

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@A340-500/600

SERVICE BULLETIN

(b) Open, safety and tag these circuit breakers :

PANEL DESIGNATION FIN LOCATION SEE

NOTES

742VU 701PP 10PB1 72 S

742VU 702PP 10PB2 71 S

(c) Make sure that there are warning notices in the cockpit to tell persons not to

operate the pushbutton switches on the overhead panel :

- 211VU (EMER ELEC PWR)

- 235VU (ELEC).

(d) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not

start the Auxiliary Power Unit (APU).

(e) Make sure that the external connector(s) is (are) not connected to the aircraft

receptacle(s) EXT PWR A (B).

(f) Make sure that there is a warning notice at the access door 121EL to tell persons

not to connect the external power connector(s).

**CONF 003

(1) Subtask 265020-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802

Task 26-16-34-000-801

(a) Make sure that the aircraft is electrically grounded (Refer to AMM Task

12-34-24-860-802).

(b) Put the access platform(s) in position.

(c) Do the preparation procedure as specified in the removal of the Smoke Detection

Control Unit (SDCU) (20WH) (Refer to AMM Task 26-16-34-000-801).

(2) Subtask 265020-941-201-001 - Job Set-up

Work Zones and Access Panels

Zone Access/Work location

210

800 Access Door 821

132 Access Panel 132PM, Panel 132NM, Panel 132RM

Work location from Frame 35 to Frame 37.1

120

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 74

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@A340-500/600

SERVICE BULLETIN

131 Access Panel 131AW, Panel 131BW, Panel 132CW,

Panel 131BA

Work location from Frame 35 to Frame 37.1

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 21-20-00-010-801

24-41-00, Page Block 201

25-52-00, Page Block 201

Task 25-52-00-000-801

Task 52-30-00-010-801

Task 52-30-00-010-802

(a) Open the FWD cargo-compartment door 821 (Refer to AMM Task

52-30-00-010-801) or (Refer to AMM Task 52-30-00-010-802).

(b) In the FWD cargo-compartment, remove the sidewall panels 131PM, 132NM and

132RM(Refer to AMM 25-52-00, Page Block 201).

(c) In the FWD cargo-compartment, remove the partition panels 131AW, 131BW,

132CW and the ceiling panels 131BA, 131PA and 131NA (Refer to AMM Task

25-52-00-000-801).

(d) Remove the air-conditioning distribution ducts in the affected area (Refer to AMM

Task 21-20-00-010-801).

(e) Open the avionics compartment door 132AZ.

(f) Energize the aircraft electrical circuits (Refer to AMM 24-41-00, Page Block 201).

(g) Open, safety and tag this(these) circuit breaker(s) :

PANEL DESIGNATION FIN LOCATION SEE

NOTES

722 EXTC FAN FWD CARGO 11HN 34 A

722 SDCU CHAN 2 12WH 36 T

722 CRG FIRE EXTNG/B 2WX 44 W

742 CRG FIRE EXTNG/A 1WX 68 J

742 SDCU CHAN 1 11WH 75 L

(3) Subtask 265020-010-002-001 - Remove/Open for Access (Upper Half of Fuselage)

Work Zones and Access Panels

Zone Access/Work location

200

Manpower Resources

Skills NON SPECIFIC

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 75

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@A340-500/600

SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) Task 23-51-12-000-801

Task 23-71-34-000-801

Task 23-81-13-000-801

Task 25-11-51-000-801

Task 25-13-44-000-801

Task 25-13-44-000-802

Task 45-22-21-000-801

Task 52-10-00-010-801

(a) Open the FWD passenger/crew door(s) 831 or 841 (Refer to AMM Task

52-10-00-010-801).

(b) In the cockpit, remove the ceiling panels 211LC, 211MC, 212NC and the strips

211KC and 212CC (Refer to AMM Task 25-13-44-000-801).

(c) From the overhead panel, remove and disconnect (if installed) :

- Reset C/B panel 262VU

- External View Camera Panel 272VU

- Reading Light Panel 252VU2

- AIREADOR panel

- Audio Control Panel (2RN3) (Refer to AMM Task 23-51-12-000-801)

- Data Loader Selector (101TD) (Refer to AMM Task 45-22-21-000-801)

- Cockpit Voice Recorder (CVR) Control Unit (1RK) (Refer to AMM Task

23-71-34-000-801)

- Radio Management Panel (1RG3) (Refer to AMM Task 23-81-13-000-801).

(d) Remove the captain seat (Refer to AMM Task 25-11-51-000-801).

(e) Remove the panel (211EW) (Refer to AMM Task 25-13-44-000-802).

(4) Subtask 265020-862-001-001 - De-energize Electrical Network

Manpower Resources

Skills NON SPECIFIC

(a) In the cockpit, on the panel 235VU, make sure that these pushbutton switches are

released :

- BAT 1, BAT 2, APU BAT,

- GEN 1 (2,3, 4), APU GEN,

- EXT A(B).

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 76

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@A340-500/600

SERVICE BULLETIN

(b) Open, safety and tag these circuit breakers :

PANEL DESIGNATION FIN LOCATION SEE

NOTES

742VU 701PP 10PB1 72 S

742VU 702PP 10PB2 71 S

(c) Make sure that there are warning notices in the cockpit to tell persons not to

operate the pushbutton switches on the overhead panel :

- 211VU (EMER ELEC PWR)

- 235VU (ELEC).

(d) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not

start the Auxiliary Power Unit (APU).

(e) Make sure that the external connector(s) is (are) not connected to the aircraft

receptacle(s) EXT PWR A (B).

(f) Make sure that there is a warning notice at the access door 121EL to tell persons

not to connect the external power connector(s).

**CONF 004

(1) Subtask 265020-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802

Task 26-16-34-000-801

(a) Make sure that the aircraft is electrically grounded (Refer to AMM Task

12-34-24-860-802).

(b) Put the access platform(s) in position.

(c) Do the preparation procedure as specified in the removal of the Smoke Detection

Control Unit (SDCU) (20WH) (Refer to AMM Task 26-16-34-000-801).

(2) Subtask 265020-941-201-001 - Job Set-up

Work Zones and Access Panels

Zone Access/Work location

210

800 Access Door 821

132 Access Panel 132PM, Panel 132NM, Panel 132RM

Work location from Frame 35 to Frame 37.1

120

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 77

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@A340-500/600

SERVICE BULLETIN

131 Access Panel 131AW, Panel 131BW, Panel 132CW,

Panel 131BA

Work location from Frame 35 to Frame 37.1

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 21-20-00-010-801

24-41-00, Page Block 201

25-52-00, Page Block 201

Task 25-52-00-000-801

Task 52-30-00-010-801

Task 52-30-00-010-802

(a) Open the FWD cargo-compartment door 821 (Refer to AMM Task

52-30-00-010-801) or (Refer to AMM Task 52-30-00-010-802).

(b) In the FWD cargo-compartment, remove the sidewall panels 131PM, 132NM and

132RM(Refer to AMM 25-52-00, Page Block 201).

(c) In the FWD cargo-compartment, remove the partition panels 131AW, 131BW,

132CW and the ceiling panels 131BA, 131PA and 131NA (Refer to AMM Task

25-52-00-000-801).

(d) Remove the air-conditioning distribution ducts in the affected area (Refer to AMM

Task 21-20-00-010-801).

(e) Open the avionics compartment door 132AZ.

(f) Energize the aircraft electrical circuits (Refer to AMM 24-41-00, Page Block 201).

(g) Open, safety and tag this(these) circuit breaker(s) :

PANEL DESIGNATION FIN LOCATION SEE

NOTES

722 EXTC FAN FWD CARGO 11HN 34 A

722 SDCU CHAN 2 12WH 36 T

722 CRG FIRE EXTNG/B 2WX 44 W

742 CRG FIRE EXTNG/A 1WX 68 J

742 SDCU CHAN 1 11WH 75 L

(3) Subtask 265020-010-002-001 - Remove/Open for Access (Upper Half of Fuselage)

Work Zones and Access Panels

Zone Access/Work location

200

Manpower Resources

Skills NON SPECIFIC

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 78

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@A340-500/600

SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) Task 23-51-12-000-801

Task 23-71-34-000-801

Task 23-81-13-000-801

Task 25-11-51-000-801

Task 25-13-44-000-801

Task 25-13-44-000-802

Task 45-22-21-000-801

Task 52-10-00-010-801

(a) Open the FWD passenger/crew door(s) 831 or 841 (Refer to AMM Task

52-10-00-010-801).

(b) In the cockpit, remove the ceiling panels 211LC, 211MC, 212NC and the strips

211KC and 212CC (Refer to AMM Task 25-13-44-000-801).

(c) From the overhead panel, remove and disconnect (if installed) :

- Reset C/B panel 262VU

- External View Camera Panel 272VU

- Reading Light Panel 252VU2

- AIREADOR panel

- Audio Control Panel (2RN3) (Refer to AMM Task 23-51-12-000-801)

- Data Loader Selector (101TD) (Refer to AMM Task 45-22-21-000-801)

- Cockpit Voice Recorder (CVR) Control Unit (1RK) (Refer to AMM Task

23-71-34-000-801)

- Radio Management Panel (1RG3) (Refer to AMM Task 23-81-13-000-801).

(d) Remove the captain seat (Refer to AMM Task 25-11-51-000-801).

(e) Remove the panel (211EW) (Refer to AMM Task 25-13-44-000-802).

(4) Subtask 265020-862-001-001 - De-energize Electrical Network

Manpower Resources

Skills NON SPECIFIC

(a) In the cockpit, on the panel 235VU, make sure that these pushbutton switches are

released :

- BAT 1, BAT 2, APU BAT,

- GEN 1 (2,3, 4), APU GEN,

- EXT A(B).

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 79

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SERVICE BULLETIN

(b) Open, safety and tag these circuit breakers :

PANEL DESIGNATION FIN LOCATION SEE

NOTES

742VU 701PP 10PB1 72 S

742VU 702PP 10PB2 71 S

(c) Make sure that there are warning notices in the cockpit to tell persons not to

operate the pushbutton switches on the overhead panel :

- 211VU (EMER ELEC PWR)

- 235VU (ELEC).

(d) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not

start the Auxiliary Power Unit (APU).

(e) Make sure that the external connector(s) is (are) not connected to the aircraft

receptacle(s) EXT PWR A (B).

(f) Make sure that there is a warning notice at the access door 121EL to tell persons

not to connect the external power connector(s).

**CONF 005

(1) Subtask 265020-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802

Task 26-16-34-000-801

(a) Make sure that the aircraft is electrically grounded (Refer to AMM Task

12-34-24-860-802).

(b) Put the access platform(s) in position.

(c) Do the preparation procedure as specified in the removal of the Smoke Detection

Control Unit (SDCU) (20WH) (Refer to AMM Task 26-16-34-000-801).

(2) Subtask 265020-941-201-001 - Job Set-up

Work Zones and Access Panels

Zone Access/Work location

210

800 Access Door 821

132 Access Panel 132PM, Panel 132NM, Panel 132RM

Work location from Frame 35 to Frame 37.1

120

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 80

6

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@A340-500/600

SERVICE BULLETIN

131 Access Panel 131AW, Panel 131BW, Panel 132CW,

Panel 131BA

Work location from Frame 35 to Frame 37.1

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 21-20-00-010-801

24-41-00, Page Block 201

25-52-00, Page Block 201

Task 25-52-00-000-801

Task 52-30-00-010-801

Task 52-30-00-010-802

(a) Open the FWD cargo-compartment door 821 (Refer to AMM Task

52-30-00-010-801) or (Refer to AMM Task 52-30-00-010-802).

(b) In the FWD cargo-compartment, remove the sidewall panels 131PM, 132NM and

132RM(Refer to AMM 25-52-00, Page Block 201).

(c) In the FWD cargo-compartment, remove the partition panels 131AW, 131BW,

132CW and the ceiling panels 131BA, 131PA and 131NA (Refer to AMM Task

25-52-00-000-801).

(d) Remove the air-conditioning distribution ducts in the affected area (Refer to AMM

Task 21-20-00-010-801).

(e) Open the avionics compartment door 132AZ.

(f) Energize the aircraft electrical circuits (Refer to AMM 24-41-00, Page Block 201).

(g) Open, safety and tag this(these) circuit breaker(s) :

PANEL DESIGNATION FIN LOCATION SEE

NOTES

722 EXTC FAN FWD CARGO 11HN 34 A

722 SDCU CHAN 2 12WH 36 T

722 CRG FIRE EXTNG/B 2WX 44 W

742 CRG FIRE EXTNG/A 1WX 68 J

742 SDCU CHAN 1 11WH 75 L

(3) Subtask 265020-010-002-001 - Remove/Open for Access (Upper Half of Fuselage)

Work Zones and Access Panels

Zone Access/Work location

200

Manpower Resources

Skills NON SPECIFIC

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 81

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@A340-500/600

SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) Task 23-51-12-000-801

Task 23-71-34-000-801

Task 23-81-13-000-801

Task 25-11-51-000-801

Task 25-13-44-000-801

Task 25-13-44-000-802

Task 45-22-21-000-801

Task 52-10-00-010-801

(a) Open the FWD passenger/crew door(s) 831 or 841 (Refer to AMM Task

52-10-00-010-801).

(b) In the cockpit, remove the ceiling panels 211LC, 211MC, 212NC and the strips

211KC and 212CC (Refer to AMM Task 25-13-44-000-801).

(c) From the overhead panel, remove and disconnect (if installed) :

- Reset C/B panel 262VU

- External View Camera Panel 272VU

- Reading Light Panel 252VU2

- AIREADOR panel

- Audio Control Panel (2RN3) (Refer to AMM Task 23-51-12-000-801)

- Data Loader Selector (101TD) (Refer to AMM Task 45-22-21-000-801)

- Cockpit Voice Recorder (CVR) Control Unit (1RK) (Refer to AMM Task

23-71-34-000-801)

- Radio Management Panel (1RG3) (Refer to AMM Task 23-81-13-000-801).

(d) Remove the captain seat (Refer to AMM Task 25-11-51-000-801).

(e) Remove the panel (211EW) (Refer to AMM Task 25-13-44-000-802).

(4) Subtask 265020-862-001-001 - De-energize Electrical Network

Manpower Resources

Skills NON SPECIFIC

(a) In the cockpit, on the panel 235VU, make sure that these pushbutton switches are

released :

- BAT 1, BAT 2, APU BAT,

- GEN 1 (2,3, 4), APU GEN,

- EXT A(B).

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 82

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@A340-500/600

SERVICE BULLETIN

(b) Open, safety and tag these circuit breakers :

PANEL DESIGNATION FIN LOCATION SEE

NOTES

742VU 701PP 10PB1 72 S

742VU 702PP 10PB2 71 S

(c) Make sure that there are warning notices in the cockpit to tell persons not to

operate the pushbutton switches on the overhead panel :

- 211VU (EMER ELEC PWR)

- 235VU (ELEC).

(d) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not

start the Auxiliary Power Unit (APU).

(e) Make sure that the external connector(s) is (are) not connected to the aircraft

receptacle(s) EXT PWR A (B).

(f) Make sure that there is a warning notice at the access door 121EL to tell persons

not to connect the external power connector(s).

**CONF 006

(1) Subtask 265020-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802

Task 26-16-34-000-801

(a) Make sure that the aircraft is electrically grounded (Refer to AMM Task

12-34-24-860-802).

(b) Put the access platform(s) in position.

(c) Do the preparation procedure as specified in the removal of the Smoke Detection

Control Unit (SDCU) (20WH) (Refer to AMM Task 26-16-34-000-801).

(2) Subtask 265020-941-201-001 - Job Set-up

Work Zones and Access Panels

Zone Access/Work location

210

800 Access Door 821

132 Access Panel 132PM, Panel 132NM, Panel 132RM

Work location from Frame 35 to Frame 37.1

120

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 83

6

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@A340-500/600

SERVICE BULLETIN

131 Access Panel 131AW, Panel 131BW, Panel 132CW,

Panel 131BA

Work location from Frame 35 to Frame 37.1

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 21-20-00-010-801

24-41-00, Page Block 201

25-52-00, Page Block 201

Task 25-52-00-000-801

Task 52-30-00-010-801

Task 52-30-00-010-802

(a) Open the FWD cargo-compartment door 821 (Refer to AMM Task

52-30-00-010-801) or (Refer to AMM Task 52-30-00-010-802).

(b) In the FWD cargo-compartment, remove the sidewall panels 131PM, 132NM and

132RM(Refer to AMM 25-52-00, Page Block 201).

(c) In the FWD cargo-compartment, remove the partition panels 131AW, 131BW,

132CW and the ceiling panels 131BA, 131PA and 131NA (Refer to AMM Task

25-52-00-000-801).

(d) Remove the air-conditioning distribution ducts in the affected area (Refer to AMM

Task 21-20-00-010-801).

(e) Open the avionics compartment door 132AZ.

(f) Energize the aircraft electrical circuits (Refer to AMM 24-41-00, Page Block 201).

(g) Open, safety and tag this(these) circuit breaker(s) :

PANEL DESIGNATION FIN LOCATION SEE

NOTES

722 EXTC FAN FWD CARGO 11HN 34 A

722 SDCU CHAN 2 12WH 36 T

722 CRG FIRE EXTNG/B 2WX 44 W

742 CRG FIRE EXTNG/A 1WX 68 J

742 SDCU CHAN 1 11WH 75 L

(3) Subtask 265020-010-002-001 - Remove/Open for Access (Upper Half of Fuselage)

Work Zones and Access Panels

Zone Access/Work location

200

Manpower Resources

Skills NON SPECIFIC

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 84

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) Task 23-51-12-000-801

Task 23-71-34-000-801

Task 23-81-13-000-801

Task 25-11-51-000-801

Task 25-13-44-000-801

Task 25-13-44-000-802

Task 45-22-21-000-801

Task 52-10-00-010-801

(a) Open the FWD passenger/crew door(s) 831 or 841 (Refer to AMM Task

52-10-00-010-801).

(b) In the cockpit, remove the ceiling panels 211LC, 211MC, 212NC and the strips

211KC and 212CC (Refer to AMM Task 25-13-44-000-801).

(c) From the overhead panel, remove and disconnect (if installed) :

- Reset C/B panel 262VU

- External View Camera Panel 272VU

- Reading Light Panel 252VU2

- AIREADOR panel

- Audio Control Panel (2RN3) (Refer to AMM Task 23-51-12-000-801)

- Data Loader Selector (101TD) (Refer to AMM Task 45-22-21-000-801)

- Cockpit Voice Recorder (CVR) Control Unit (1RK) (Refer to AMM Task

23-71-34-000-801)

- Radio Management Panel (1RG3) (Refer to AMM Task 23-81-13-000-801).

(d) Remove the captain seat (Refer to AMM Task 25-11-51-000-801).

(e) Remove the panel (211EW) (Refer to AMM Task 25-13-44-000-802).

(4) Subtask 265020-862-001-001 - De-energize Electrical Network

Manpower Resources

Skills NON SPECIFIC

(a) In the cockpit, on the panel 235VU, make sure that these pushbutton switches are

released :

- BAT 1, BAT 2, APU BAT,

- GEN 1 (2,3, 4), APU GEN,

- EXT A(B).

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 85

6

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@A340-500/600

SERVICE BULLETIN

(b) Open, safety and tag these circuit breakers :

PANEL DESIGNATION FIN LOCATION SEE

NOTES

742VU 701PP 10PB1 72 S

742VU 702PP 10PB2 71 S

(c) Make sure that there are warning notices in the cockpit to tell persons not to

operate the pushbutton switches on the overhead panel :

- 211VU (EMER ELEC PWR)

- 235VU (ELEC).

(d) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not

start the Auxiliary Power Unit (APU).

(e) Make sure that the external connector(s) is (are) not connected to the aircraft

receptacle(s) EXT PWR A (B).

(f) Make sure that there is a warning notice at the access door 121EL to tell persons

not to connect the external power connector(s).

**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 265020-831-001-001 - Modify the Equipment and the Wiring in the RH

Overhead Panel 212VU.

Work Zones and Access Panels

Zone Access/Work location

212 Access Door 831, Door 841

Work location Electrical panel 212VU

Manpower Resources

Manhours 12.00

Minimum number of person 1

Subtask elapsed time 12.00

Skills ELECTRICAL

Material necessary to do the job

Kit 265020A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

2 ASNA2083BG2-10 7 Screw

6 NSA937901MA2206 1 Module

7 NSA937901FM 1 Module

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 86

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@A340-500/600

SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

10 F9251088400000 1 Plate

F1131101500000 Placard

F9000095226495 Bundle

NAS1102-04-5 44 Screw

NSA935401-03 50 TIE

NSA937901E2 1 Label

Kit 265020A02R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 F33110238A00 1 Plate

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Pure Mineral Vaseline Or

Petro-Latum

04-012 As required

Electrical Bond Varnish 07-001B As required

Sealant, High Temperature 08-007C

References

Aircraft Maintenance Manual (AMM) Task 11-00-00-400-802

Task 20-28-00-912-802

Fig. A-FBBAA

Modification of the Equipment in the RH

Overhead Panel 212VU

Sheet 01

Sheet 02

Sheet 03

Fig. A-FCAAA

Modification of the Wiring in the RH

Overhead Panel 212VU

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

(a) Remove and disconnect the RH overhead panel 212VU.

NOTE: Retain it.

(b) Modify the equipment in the RH overhead panel 212VU.

1 Remove the integrally lighted plate (212LF).

a Remove as shown in Fig. A-FBBAA Sheet 01 :

FIN 212LF

1 Plate-Integrally Lighted F33110259A00 Item (1) Discard

attached with :

7 Screw ASNA2083BG2-10 Item (2) Discard

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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SERVICE BULLETIN

2 Remove the indicator light BTL3 (5WX).

a Remove as shown in Fig. A-FBBAA Sheet 01 and Fig. A-FBBAA Sheet

02, Detail B :

FIN 5WX

1 Light-Indicator ABS0951A0LP110 Item (3) Discard

FIN 5WX1

1 Sleeve E0416-02 Item (4) Discard

FIN 5WXA

1 Connector E0417A01S Item (5) Discard

NOTE: Remove and discard the attachment hardware.

3 Replace the 212VU front plate.

a Remove and retain all the items of equipment that are installed on the

front plate.

b Remove as shown in Fig. A-FBBAA Sheet 01 :

1 Plate Assy- Front

212VU

F9251602100000 Item (10) Discard

attached with :

8 Screw NAS1102-06-5 Item (11) Retain

c On the new front plate, bond the placards (Refer to AMM Task

11-00-00-400-802) supplied in :

Placard Set-212VU F1131101500000

NOTE: Bond the applicable placards at the same locations as on

the old front plate. Discard the unused placards.

d Install as shown in Fig. A-FBBAA Sheet 03 :

1 Plate Assy- Front

212VU

F9251088400000 Item 10

attach with :

8 Screw NAS1102-06-5 Item (11)

NOTE: The screws Item (11) were retained at the removal.

e Install again all the items of equipment that you removed and retained

before the replacement of the front plate and attach with :

44 Screw NAS1102-04-5

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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SERVICE BULLETIN

Safety the screws with :

Sealant, High

Temperature

08-007C As required

NOTE: Replace the screws if they are damaged during the

removal. The quantity of screws to be replaced depends

on aircraft configuration (44 is the maximum).

f Do the electrical bonding (Refer to AMM Task 20-28-00-912-802) with :

Pure Mineral

Vaseline Or PetroLatum

04-012 As required

and

Electrical Bond

Varnish

07-001B As required

4 Modify the terminal block (582VT) as shown in Fig. A-FBBAA Sheet 01 and

Fig. A-FBBAA Sheet 02, Detail C.

a Remove from position 2 :

FIN 582VT2

1 Module-False NSA937901FM Item (6) Discard

b Remove from position 3 :

FIN 582VT3

1 Module NSA937901MA2204 Item (7) Discard

c Install at position 2 as shown in :

FIN 582VT2

1 Module NSA937901MA2206 Item 6

with

1 Label-Identification NSA937901E2

d Install at position 3 as shown in :

FIN 582VT3

1 Module-False NSA937901FM Item 7

5 Install the new integrally lighted plate (212LF).

a Install as shown in Fig. A-FBBAA Sheet 03 :

FIN 212LF

1 Plate-Integrally Lighted F33110238A00 Item 1

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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@A340-500/600

SERVICE BULLETIN

attach with :

7 Screw ASNA2083BG2-10 Item 2

(c) Modify the wiring in the RH overhead panel 212VU.

1 Remove the wires as shown in the wiring diagrams Fig. A-FCAAA Sheet 01,

Fig. A-FCAAA Sheet 02 and as given in the hook-up chart lines :

- 1 thru 13 (Refer to Fig. A-FCAAA Sheet 04).

2 Modify the connections of the wires as shown in the wiring diagrams Fig. AFCAAA Sheet 02, Fig. A-FCAAA Sheet 03 and as given in the hook-up chart

lines :

- 17 thru 24 (Refer to Fig. A-FCAAA Sheet 04)

- 1 and 2 (Refer to Fig. A-FCAAA Sheet 05).

3 Install the wires as shown in the wiring diagram Fig. A-FCAAA Sheet 03 and

as given in the hook-up chart lines :

- 6 thru 12 (Refer to Fig. A-FCAAA Sheet 05), supplied in :

Bundle F9000095226495

4 Attach the wires with :

50 Tie-Cable NSA935401-03

(d) Install the RH overhead panel 212VU.

(2) Subtask 265020-831-002-001 - Modify the Equipment and the Wiring in the

Emergency Power Center 740VU.

Work Zones and Access Panels

Zone Access/Work location

121 Access Door 821, Door 132AZ

Work location Electrical panel 740VU

Manpower Resources

Manhours 3.50

Minimum number of person 1

Subtask elapsed time 3.50

Skills ELECTRICAL

Material necessary to do the job

Kit 265020A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

F9000095226495 Bundle

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 90

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@A340-500/600

SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

NSA935401-03 50 TIE

NSA935401-05 50 TIE

References

Fig. A-FBCAA

Modification of the Equipment in the

Emergency Power Center 740VU

Sheet 01

Fig. A-FCBAA

Modification of the Wiring in the

Emergency Power Center 740VU

Sheet 01

Sheet 02

(a) Open the emergency power center 740VU.

(b) Remove the wires as shown in the wiring diagram Fig. A-FCBAA Sheet 01 and as

given in the hook-up chart lines :

- 1 thru 8 (Refer to Fig. A-FCBAA Sheet 02).

(c) Modify the terminal block (703VT) as shown in Fig. A-FBCAA Sheet 01.

1 Remove from position 21 :

1 Clamp-End NSA937901S Retain

2 Remove from position 20 :

FIN 703VT20

1 Module NSA937901MA2004 Item (7) Discard

3 Install at position 20 :

1 Clamp-End NSA937901S

NOTE: The end clamp was retained at the removal.

(d) Install the wire as shown in the wiring diagram Fig. A-FCBAA Sheet 01 and as

given in the hook-up chart line :

- 12 (Refer to Fig. A-FCBAA Sheet 02), supplied in :

Bundle F9000095226495

(e) Attach the wire with :

50 Tie-Cable NSA935401-03

50 Tie-Cable NSA935401-05

(f) Close the emergency power center 740VU.

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 91

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SERVICE BULLETIN

(3) Subtask 265020-831-003-001 - Modify the Equipment and the Wiring in the AC/DC

Main Power Center 710VU.

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 821, Door 132AZ

Work location Electrical panel 710VU

Manpower Resources

Manhours 3.50

Minimum number of person 1

Subtask elapsed time 3.50

Skills ELECTRICAL

Material necessary to do the job

Kit 265020A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

F9000095226495 Bundle

NSA935401-03 50 TIE

NSA935401-05 50 TIE

References

Fig. A-FBDAA

Modification of the Equipment in the

AC/DC Main Power Center 710VU

Sheet 01

Fig. A-FCCAA

Modification of the Wiring in the AC/DC

Main Power Center 710VU

Sheet 01

Sheet 02

(a) Open the AC/DC main power center 710VU.

(b) Remove the wires as shown in the wiring diagram Fig. A-FCCAA Sheet 01 and as

given in the hook-up chart lines :

- 1 thru 8 (Refer to Fig. A-FCCAA Sheet 02).

(c) Modify the terminal block (1712VT) as shown in Fig. A-FBDAA Sheet 01.

1 Remove from position 18 :

1 Clamp-End NSA937901S Retain

2 Remove from position 17 :

FIN 1712VT17

1 Module NSA937901MA2004 Item (7) Discard

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 92

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@A340-500/600

SERVICE BULLETIN

3 Install at position 17 :

1 Clamp-End NSA937901S

NOTE: The end clamp was retained at the removal.

(d) Install the wire as shown in the wiring diagram Fig. A-FCCAA Sheet 01 and as

given in the hook-up chart line :

- 12 (Refer to Fig. A-FCCAA Sheet 02), supplied in :

Bundle F9000095226495

(e) Attach the wire with :

50 Tie-Cable NSA935401-03

50 Tie-Cable NSA935401-05

(f) CLose the AC/DC main power center 710VU.

(4) Subtask 265020-831-004-001 - Modify the Equipment and the Wiring in the LH

Relay Box 751VU.

Work Zones and Access Panels

Zone Access/Work location

121 Access Door 821, Door 132AZ

Work location Electrical panel 751VU

Manpower Resources

Manhours 3.50

Minimum number of person 1

Subtask elapsed time 3.50

Skills ELECTRICAL

References

Fig. A-FBEAA

Modification of the Equipment in the LH

Relay Box 751VU

Sheet 01

Fig. A-FCDAA

Modification of the Wiring in the LH

Relay Box 751VU

Sheet 01

Sheet 02

(a) Open the LH relay box 751VU.

(b) Remove the wires as shown in the wiring diagram Fig. A-FCDAA Sheet 01 and as

given in the hook-up chart lines :

- 1 thru 12 (Refer to Fig. A-FCDAA Sheet 02).

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 93

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@A340-500/600

SERVICE BULLETIN

(c) Remove from position E93, as shown in Fig. A-FBEAA Sheet 01 :

FIN 10WX

1 Relay E0245-28A0 Item (8) Discard

FIN 10WXA

1 Base E0250A0S Item (9) Discard

NOTE: Remove and discard the attachment hardware and the related

placard(s).

(d) Remove from position E89, as shown in Fig. A-FBEAA Sheet 01 :

FIN 11WX

1 Relay E0245-28A0 Item (8) Discard

FIN 11WXA

1 Base E0250A0S Item (9) Discard

NOTE: Remove and discard the attachment hardware and the related

placard(s).

(e) Close the LH relay box 751VU.

(5) Subtask 265020-831-005-001 - Modify the Equipment and the Wiring in the RH

Relay Box 752VU.

Work Zones and Access Panels

Zone Access/Work location

122 Access Door 821, Door 132AZ

Work location Electrical panel 752VU

Manpower Resources

Manhours 3.50

Minimum number of person 1

Subtask elapsed time 3.50

Skills ELECTRICAL

References

Fig. A-FBFAA

Modification of the Equipment in the RH

Relay Box 752VU

Sheet 01

Fig. A-FCEAA

Modification of the Wiring in the RH

Relay Box 752VU

Sheet 01

Sheet 02

(a) Open the RH relay box 752VU.

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 94

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@A340-500/600

SERVICE BULLETIN

(b) Remove the wires as shown in the wiring diagram Fig. A-FCEAA Sheet 01 and as

given in the hook-up chart lines :

- 1 thru 12 (Refer to Fig. A-FCEAA Sheet 02).

(c) Remove from position B37, as shown in Fig. A-FBFAA Sheet 01 :

FIN 12WX

1 Relay E0245-28A0 Item (8) Discard

FIN 12WXA

1 Base E0250A0S Item (9) Discard

NOTE: Remove and discard the attachment hardware and the related

placard(s).

(d) Remove from position B33, as shown in Fig. A-FBFAA Sheet 01 :

FIN 13WX

1 Relay E0245-28A0 Item (8) Discard

FIN 13WXA

1 Base E0250A0S Item (9) Discard

NOTE: Remove and discard the attachment hardware and the related

placard(s).

(e) Close the RH relay box 752VU.

(6) Subtask 265020-831-006-001 - Modify the Equipment and the Wiring in the Main

Rack 800VU.

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 821, Door 132AZ

Work location Electrical panel 800VU

Manpower Resources

Manhours 8.00

Minimum number of person 2

Subtask elapsed time 4.00

Skills ELECTRICAL

Material necessary to do the job

Kit 265020A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

7 NSA937901FM 1 Module

F9000095226495 Bundle

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 95

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@A340-500/600

SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

NSA935401-03 200 TIE

NSA935401-05 200 TIE

NSA935401-08 200 Tie

References

Aircraft Maintenance Manual (AMM) Task 26-16-34-000-801

Task 26-16-34-400-801

Fig. A-FBGAA

Modification of the Equipment in the

Main Rack 800VU

Sheet 01

Fig. A-FCFAA

Modification of the Wiring in the Main

Rack 800VU

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

Fig. A-FCGAA

Modification of the Pin Programming in

the Main Rack 800VU

Sheet 01

Sheet 02

(a) Remove and retain the SDCU (20WH) (Refer to AMM Task 26-16-34-000-801).

(b) Remove the wires as shown in the wiring diagrams Fig. A-FCFAA Sheet 01, Fig. AFCFAA Sheet 02, Fig. A-FCFAA Sheet 03, and as given in the hook-up chart lines :

- 1 thru 25 (Refer to Fig. A-FCFAA Sheet 05)

- 1 thru 3 (Refer to Fig. A-FCFAA Sheet 06).

(c) Modify the terminal block (2900VT) as shown in Fig. A-FBGAA Sheet 01.

1 Remove from position 50 :

FIN 2900VT50

1 Module NSA937901MA2011 Item (7) Discard

2 Install at position 50 :

FIN 2900VT50

1 Module-False NSA937901FM Item 7

(d) Install the wires as shown in the wiring diagram Fig. A-FCFAA Sheet 04 and as

given in the hook-up chart lines :

- 7 thru 18 (Refer to Fig. A-FCFAA Sheet 06), supplied in :

Bundle F9000095226495

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 96

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SERVICE BULLETIN

(e) Modify the connection of the wires as shown in the wiring diagram Fig. A-FCGAA

Sheet 01 and as given in the hook-up chart lines :

- 1 thru 4 (Refer to Fig. A-FCGAA Sheet 02).

(f) Attach the wires with :

200 Tie-Cable NSA935401-03

200 Tie-Cable NSA935401-05

200 Tie-Cable NSA935401-08

(g) Install the SDCU (20WH) (Refer to AMM Task 26-16-34-400-801).

(7) Subtask 265020-831-007-001 - Modify the Wiring between the Main Rack Shelf

801VU and the LH Relay Box 751VU.

Work Zones and Access Panels

Zone Access/Work location

121 Access Door 821, Door 132AZ

Work location from Electrical panel 801VU to Electrical panel

751VU

Manpower Resources

Manhours 3.50

Minimum number of person 1

Subtask elapsed time 3.50

Skills ELECTRICAL

Material necessary to do the job

Kit 265020A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

NSA936604CA0931 8 Cap

References

Fig. A-FBAAA

Location of the Working Areas

Sheet 01

Fig. A-FCHAA

Modification of the Wiring between the

Main Rack Shelf 801VU and the LH

Relay Box 751VU

Sheet 01

Sheet 02

(a) Modify the connections of the wires as shown in the wiring diagram Fig. A-FCHAA

Sheet 01 and as given in the hook-up chart lines :

- 1 thru 8 (Refer to Fig. A-FCHAA Sheet 02).

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 97

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@A340-500/600

SERVICE BULLETIN

(b) Install on the stowed wires ends :

8 Cap-Sealing NSA936604CA0931

(8) Subtask 265020-831-008-001 - Modify the Wiring between the Main Rack Shelf

802VU and the RH Relay Box 752VU.

Work Zones and Access Panels

Zone Access/Work location

122 Access Door 821, Door 132AZ

Work location from Electrical panel 802VU to Electrical panel

752VU

Manpower Resources

Manhours 3.50

Minimum number of person 1

Subtask elapsed time 3.50

Skills ELECTRICAL

References

Fig. A-FBAAA

Location of the Working Areas

Sheet 01

Fig. A-FCJAA

Modification of the Wiring between the

Main Rack Shelf 802VU and the RH

Relay Box 752VU

Sheet 01

Sheet 02

(a) Remove the wires as shown in the wiring diagram Fig. A-FCJAA Sheet 01 and as

given in the hook-up chart lines :

- 1 thru 4 (Refer to Fig. A-FCJAA Sheet 02).

(9) Subtask 265020-831-009-001 - Modify the Wiring between the Emergency Power

Center 740VU and the LH Relay Box 751VU.

Work Zones and Access Panels

Zone Access/Work location

121 Access Door 821, Door 132AZ

Work location from Electrical panel 740VU to Electrical panel

751VU

Manpower Resources

Manhours 3.50

Minimum number of person 1

Subtask elapsed time 3.50

Skills ELECTRICAL

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 98

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@A340-500/600

SERVICE BULLETIN

References

Fig. A-FBAAA

Location of the Working Areas

Sheet 01

Fig. A-FCKAA

Modification of the Wiring between the

Emergency Power Center 740VU and

the LH Relay Box 751VU

Sheet 01

Sheet 02

(a) Remove the wires as shown in the wiring diagram Fig. A-FCKAA Sheet 01 and as

given in the hook-up chart lines :

- 1 thru 4 (Refer to Fig. A-FCKAA Sheet 02).

(10) Subtask 265020-831-010-001 - Modify the Wiring between the AC/DC Main Power

Center 715VU and the RH Relay Box 752VU.

Work Zones and Access Panels

Zone Access/Work location

122 Access Door 821, Door 132AZ

Work location from Electrical panel 715VU to Electrical panel

752VU

Manpower Resources

Manhours 3.50

Minimum number of person 1

Subtask elapsed time 3.50

Skills ELECTRICAL

References

Fig. A-FBAAA

Location of the Working Areas

Sheet 01

Fig. A-FCLAA

Modification of the Wiring between the

AC/DC Main Power Center 715VU and

the RH Relay Box 752VU

Sheet 01

Sheet 02

(a) Remove the wires as shown in the wiring diagram Fig. A-FCLAA Sheet 01 and as

given in the hook-up chart lines :

- 1 thru 4 (Refer to Fig. A-FCLAA Sheet 02).

(11) Subtask 265020-831-011-001 - Modify the Wiring between the Main Rack Shelf

801VU and the Avionics Compartment at FR2.

Work Zones and Access Panels

Zone Access/Work location

From 121 Access Door 821, Door 132AZ

Work location Electrical panel 801VU

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 99

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To 211 Access Door 831, Door 841

Panel 211EW

Work location Frame 2

Manpower Resources

Manhours 3.50

Minimum number of person 1

Subtask elapsed time 3.50

Skills ELECTRICAL

Material necessary to do the job

Kit 265020A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

NSA936604CA0931 2 Cap

References

Fig. A-FBAAA

Location of the Working Areas

Sheet 01

Fig. A-FCMAA

Modification of the Wiring between the

Main Rack Shelf 801VU and the

Avionics Compartment at FR2

Sheet 01

Sheet 02

(a) Modify the connections of the wire as shown in the wiring diagram Fig. A-FCMAA

Sheet 01 and as given in the hook-up chart lines :

- 1 and 2 (Refer to Fig. A-FCMAA Sheet 02).

(b) Install on the stowed wire ends :

2 Cap-Sealing NSA936604CA0931

(12) Subtask 265020-831-012-001 - Modify the Wiring between the RH Overhead Panel

212VU and the Avionics Compartment (LH Side).

Work Zones and Access Panels

Zone Access/Work location

From 212 Access Door 831, Door 841

Work location Electrical panel 212VU

To 121 Access Door 821, Door 132AZ

Work location Electrical panel 751VU

Electrical panel 740VU

Frame 2

Electrical panel 801VU

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 100

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@A340-500/600

SERVICE BULLETIN

Manpower Resources

Manhours 10.00

Minimum number of person 2

Subtask elapsed time 5.00

Skills ELECTRICAL

Material necessary to do the job

Kit 265020A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

F9000095226495 Bundle

NSA935401-05 200 TIE

NSA935401-08 200 Tie

NSA936604CA0931 8 Cap

References

Fig. A-FBAAA

Location of the Working Areas

Sheet 01

Fig. A-FCNAA

Modification of the Wiring between the

RH Overhead Panel 212VU and the

Avionics Compartment (LH Side)

Sheet 01

Sheet 02

Sheet 03

(a) Modify the connections of the wires as shown in the wiring diagrams Fig. A-FCNAA

Sheet 01, Fig. A-FCNAA Sheet 02 and as given in the hook-up chart lines :

- 1 thru 8 (Refer to Fig. A-FCNAA Sheet 03).

(b) Install on the stowed wires ends :

8 Cap-Sealing NSA936604CA0931

(c) Install the wires as shown in the wiring diagram Fig. A-FCNAA Sheet 01 and as

given in the hook-up chart lines :

- 12 and 13 (Refer to Fig. A-FCNAA Sheet 02), supplied in :

Bundle F9000095226495

(d) Attach the wires with :

200 Tie-Cable NSA935401-05

200 Tie-Cable NSA935401-08

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 101

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SERVICE BULLETIN

(13) Subtask 265020-831-013-001 - Modify the Wiring between the RH Overhead Panel

212VU and the Avionics Compartment (RH Side).

Work Zones and Access Panels

Zone Access/Work location

From 212 Access Door 831, Door 841

Work location Electrical panel 212VU

To 122 Access Door 821, Door 132AZ

Panel 131BA

Work location Electrical panel 752VU

Electrical panel 715VU

Electrical panel 802VU

Frame 20

Manpower Resources

Manhours 10.00

Minimum number of person 2

Subtask elapsed time 5.00

Skills ELECTRICAL

Material necessary to do the job

Kit 265020A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

F9000095226495 Bundle

NSA935401-05 200 TIE

NSA935401-08 200 Tie

NSA936604CA0931 10 Cap

References

Fig. A-FBAAA

Location of the Working Areas

Sheet 01

Fig. A-FCPAA

Modification of the Wiring between the

RH Overhead Panel 212VU and the

Avionics Compartment (RH Side)

Sheet 01

Sheet 02

Sheet 03

(a) Modify the connections of the wires as shown in the wiring diagram Fig. A-FCPAA

Sheet 01, Fig. A-FCPAA Sheet 02 and as given in the hook-up chart lines :

- 1 thru 12 (Refer to Fig. A-FCPAA Sheet 03).

(b) Install on the stowed wires ends :

10 Cap-Sealing NSA936604CA0931

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 102

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SERVICE BULLETIN

(c) Install the wires as shown in the wiring diagram Fig. A-FCPAA Sheet 01 and as

given in the hook-up chart lines :

- 9 and 10 (Refer to Fig. A-FCPAA Sheet 02), supplied in :

Bundle F9000095226495

(d) Attach the wires with :

200 Tie-Cable NSA935401-05

200 Tie-Cable NSA935401-08

(14) Subtask 265020-831-201-001 - Remove the Fire Extinguishing Bottles, 4010WX,

4005WX and 4020WX.

Work Zones and Access Panels

Zone Access/Work location

132 Access Panel 132PM

Work location from Frame 35 to Frame 37.1

Manpower Resources

Manhours 3.00

Minimum number of person 2

Subtask elapsed time 1.50

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 26-23-41, Page Block 401

Fig. A-GBAAA

Removal of Fire Extinguishing Bottles

4005WX, 4010WX and 4020WX with

Cartridges.

Sheet 01

Sheet 02

Sheet 03

(a) Remove the Fire Extinguishing Bottle 2 (FWD), 4010WX.

Refer to Fig. A-GBAAA

1 Between FR35RH and FR36RH, remove the fire extinguishing bottle 4010WX

(Refer to AMM 26-23-41, Page Block 401) :

Refer to Fig. A-GBAAA Sheet 01, Fig. A-GBAAA Sheet 02 and Fig. A-GBAAA

Sheet 03, Detail D :

1 Extinguisher-Fire 35200003-2 Item (200) Retain

with :

4 Nut NAS1726-5E Item (100) Discard

4 Bolt NAS1305-2 Item (101) Discard

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 103

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@A340-500/600

SERVICE BULLETIN

1 Bolt NAS1304-9 Item (103) Discard

1 Nut NAS1726-4E Item (104) Discard

2 Screw Item (260)

2 Washer Item (261)

2 Nut Item (262)

NOTE: Retain the Items (260), (261) and (262).

(b) Remove the Fire Extinguishing Bottle 1 (MID), 4005WX.

Refer to Fig. A-GBAAA

1 Between FR36RH and FR37RH, remove the fire extinguishing bottle 4005WX

(Refer to AMM 26-23-41, Page Block 401) :

Refer to Fig. A-GBAAA Sheet 01 and Fig. A-GBAAA Sheet 03 :

1 Extinguisher-Fire 34900008-2 Item (201) Retain

with :

4 Nut NAS1726-5E Item (100) Discard

4 Bolt NAS1305-2 Item (101) Discard

1 Bolt NAS1304-9 Item (103) Discard

1 Nut NAS1726-4E Item (104) Discard

2 Screw Item (260)

2 Washer Item (261)

2 Nut Item (262)

NOTE: Discard the Items (260), (261) and (262).

(c) Remove the Fire Extinguishing Bottle 3 (AFT), 4020WX.

Refer to Fig. A-GBAAA

1 Between FR37RH and FR37.1RH, remove the fire extinguishing bottle

4020WX (Refer to AMM 26-23-41, Page Block 401) :

Refer to Fig. A-GBAAA Sheet 01, Fig. A-GBAAA Sheet 02 and Fig. A-GBAAA

Sheet 03, Detail D :

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 104

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SERVICE BULLETIN

1 Extinguisher-Fire 35200003-2 Item (200) Discard

with :

4 Nut NAS1726-5E Item (100) Discard

4 Bolt NAS1305-2 Item (101) Discard

1 Bolt NAS1304-9 Item (103) Discard

1 Nut NAS1726-4E Item (104) Discard

2 Screw Item (260)

2 Washer Item (261)

2 Nut Item (262)

NOTE: Retain the Items (260), (261) and (262).

(15) Subtask 265020-831-202-001 - Remove the 4 Flow Metering Compact Units (FMCU),

FIN 4031WX, 4032WX, 4033WX and 4034WX.

Work Zones and Access Panels

Zone Access/Work location

132 Access Panel 132PM

Work location from Frame 35 to Frame 37.1

Manpower Resources

Manhours 4.00

Minimum number of person 2

Subtask elapsed time 2.00

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 26-23-43, Page Block 401

Fig. A-GBCAA

Removal of the 4 Flow Metering

Compact Units (FMCU), FIN 4031WX,

4032WX, 4033WX and 4034WX, the

related Plumbing Installations and

Placards

Sheet 01

Sheet 02

Sheet 03

(a) Remove the Flow Metering Compact Unit (FMCU), FIN 4031WX.

Refer to Fig. A-GBCAA

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 105

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SERVICE BULLETIN

1 From FR35RH, remove the FMCU, FIN 4031WX (Refer to AMM 26-23-43,

Page Block 401) :

Refer to Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet 02 and Fig. A-GBCAA

Sheet 03

1 Meter-Flow, Compact

Unit

QA07907-01 Item (205) Discard

and

1 Hose Assy G2627007000000 Item (107) Discard

1 Tube Assy G2627006000000 Item (109) Discard

with :

1 Washer NAS1149F0332P Item (106) Discard

1 Clamp NSA5516-06NJ Item (111) Discard

1 Screw NAS1096-3-10 Item (112) Discard

1 Nut NAS1726-3E Item (113) Discard

3 Screw NAS1100E4-36 Item (130) Discard

3 Washer NAS1149C0432R Item (131) Discard

1 Fitting A2627048220400 Item (132) Discard

2 O-Ring NSA8202-6 Item (133) Discard

1 Fitting A2627048221600 Item (134) Discard

(b) Remove the Flow Metering Compact Unit (FMCU), FIN 4032WX.

Refer to Fig. A-GBCAA

1 From FR36RH, remove the FMCU, FIN 4032WX (Refer to AMM 26-23-43,

Page Block 401) :

Refer to Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet 02 and Fig. A-GBCAA

Sheet 03

1 Meter-Flow, Compact

Unit

QA07907-01 Item (205) Discard

and

1 Hose Assy G2627007000200 Item (108) Discard

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 106

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@A340-500/600

SERVICE BULLETIN

1 Tube Assy G2627006000200 Item (110) Discard

with :

1 Washer NAS1149F0332P Item (106) Discard

1 Clamp NSA5516-06NJ Item (111) Discard

1 Screw NAS1096-3-10 Item (112) Discard

1 Nut NAS1726-3E Item (113) Discard

3 Screw NAS1100E4-36 Item (130) Discard

3 Washer NAS1149C0432R Item (131) Discard

1 Fitting A2627048220400 Item (132) Discard

2 O-Ring NSA8202-6 Item (133) Discard

1 Fitting A2627048221600 Item (134) Discard

(c) Remove the Flow Metering Compact Unit (FMCU), FIN 4033WX.

Refer to Fig. A-GBCAA

1 From FR37RH, remove the FMCU, FIN 4033WX (Refer to AMM 26-23-43,

Page Block 401) :

Refer to Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet 02 and Fig. A-GBCAA

Sheet 03

1 Meter-Flow, Compact

Unit

QA07907-01 Item (205) Discard

and

1 Hose Assy G2627007000000 Item (107) Discard

1 Tube Assy G2627006000000 Item (109) Discard

with :

1 Washer NAS1149F0332P Item (106) Discard

1 Clamp NSA5516-06NJ Item (111) Discard

1 Screw NAS1096-3-10 Item (112) Discard

1 Nut NAS1726-3E Item (113) Discard

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 107

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Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

3 Screw NAS1100E4-36 Item (130) Discard

3 Washer NAS1149C0432R Item (131) Discard

1 Fitting A2627048220400 Item (132) Discard

2 O-Ring NSA8202-6 Item (133) Discard

1 Fitting A2627048221600 Item (134) Discard

(d) Remove the Flow Metering Compact Unit (FMCU), FIN 4034WX.

Refer to Fig. A-GBCAA

1 From FR37.1RH, remove the FMCU, FIN 4034WX (Refer to AMM 26-23-43,

Page Block 401) :

Refer to Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet 02 and Fig. A-GBCAA

Sheet 03

1 Meter-Flow, Compact

Unit

QA07907-01 Item (205) Discard

and

1 Hose Assy G2627007000200 Item (108) Discard

1 Tube Assy G2627006000200 Item (110) Discard

with :

1 Washer NAS1149F0332P Item (106) Discard

1 Clamp NSA5516-06NJ Item (111) Discard

1 Screw NAS1096-3-10 Item (112) Discard

1 Nut NAS1726-3E Item (113) Discard

3 Screw NAS1100E4-36 Item (130) Discard

3 Washer NAS1149C0432R Item (131) Discard

1 Fitting A2627048220400 Item (132) Discard

2 O-Ring NSA8202-6 Item (133) Discard

1 Fitting A2627048221600 Item (134) Discard

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 108

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SERVICE BULLETIN

(16) Subtask 265020-831-203-001 - Remove the plumbing installations and placards.

Work Zones and Access Panels

Zone Access/Work location

132 Access Panel 132PM

Work location from Frame 35 to Frame 37.1

Manpower Resources

Manhours 2.50

Minimum number of person 2

Subtask elapsed time 1.25

Skills NON SPECIFIC

References

Fig. A-GBCAA

Removal of the 4 Flow Metering

Compact Units (FMCU), FIN 4031WX,

4032WX, 4033WX and 4034WX, the

related Plumbing Installations and

Placards

Sheet 01

Sheet 02

Sheet 03

(a) Remove the plumbing installations between FR35RH thru FR37.1RH.

Refer to Fig. A-GBCAA

1 Between FR35RH and FR36RH, remove :

Refer to Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet 02 and Fig. A-GBCAA

Sheet 03

2 Reducer MS21916D10-4 Item (115) Discard

1 Tube Assy G2627005004400 Item (116) Discard

1 Tee NSA855113-34D Item (117) Discard

1 Tube Assy G2627005004200 Item (118) Discard

1 Hose A2627045200400 Item (209) Discard

with :

2 Washer NAS1149F0332P Item (106) Discard

2 Screw NAS1096-3-10 Item (112) Discard

2 Nut NAS1726-3E Item (113) Discard

2 Clamp NSA5516-18NJ Item (121) Discard

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 109

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@A340-500/600

SERVICE BULLETIN

1 Rod End NSA8141-04R Item (135) Discard

1 Nut NAS509-5 Item (136) Discard

1 Rod End NSA8140-04RK Item (137) Discard

2 Lead-Bonding E0090-41-320 Item (138) Discard

1 Bolt NAS1304-12 Item (139) Discard

1 Nut NAS1726-4E Item (104) Discard

1 Washer NAS1149D0432K Item (140) Discard

1 Washer-Lock NSA5355-5CA Item (141) Discard

2 Between FR36RH and FR37RH, remove :

Refer to Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet 02 and Fig. A-GBCAA

Sheet 03

2 Washer NAS1149F0332P Item (106) Discard

2 Screw NAS1096-3-10 Item (112) Discard

2 Nut NAS1726-3E Item (113) Discard

1 Tube Assy G2627005004000 Item (120) Discard

2 Clamp NSA5516-18NJ Item (121) Discard

1 Cross NSA855140-22D Item (122) Discard

1 Union MS21902D10 Item (123) Discard

1 Tube Assy G2627005003800 Item (124) Discard

2 Tee NSA855008D10 Item (125) Discard

1 Rod End NSA8141-04R Item (135) Retain

1 Nut NAS509-5 Item (136) Retain

1 Rod End NSA8140-04RK Item (137) Retain

2 Lead-Bonding E0090-41-320 Item (138) Discard

1 Bolt NAS1304-12 Item (139) Discard

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 110

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

1 Nut NAS1726-4E Item (104) Discard

1 Washer NAS1149D0432K Item (140) Discard

1 Washer-Lock NSA5355-5CA Item (141) Discard

1 Tube Assy G2627005006400 Item (142) Discard

1 Hose A2627045200400 Item (209) Retain

2 Hose Assy F2627007100200 Item (210) Retain

3 Between FR37RH and FR37.1RH, remove :

Refer to Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet 02 and Fig. A-GBCAA

Sheet 03

2 Reducer MS21916D10-4 Item (115) Discard

1 Tube Assy G2627005004400 Item (116) Discard

1 Tee NSA855113-34D Item (117) Discard

1 Tube Assy G2627005003400 Item (119) Discard

1 Tee NSA855008D10 Item (125) Discard

1 Tube Assy G2627005003600 Item (129) Discard

1 Rod End NSA8141-04R Item (135) Retain

1 Nut NAS509-5 Item (136) Retain

1 Rod End NSA8140-04RK Item (137) Retain

2 Lead-Bonding E0090-41-320 Item (138) Discard

1 Bolt NAS1304-12 Item (139) Discard

1 Nut NAS1726-4E Item (104) Discard

1 Washer NAS1149D0432K Item (140) Discard

1 Washer-Lock NSA5355-5CA Item (141) Discard

1 Hose A2627045200400 Item (209) Retain

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 111

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@A340-500/600

SERVICE BULLETIN

(b) Remove the placards between FR35RH thru FR37.1RH.

Refer to Fig. A-GBCAA

1 Between FR35RH and FR36RH, remove the placards 4010WX, 4031WX and

4032WX :

2 Label NSA931025-02F Item (126) Discard

1 Placard G2627004020200 Item (127) Discard

2 Between FR37RH and FR37.1RH, remove the placards 4020WX, 4033WX

and 4034WX :

2 Label NSA931025-02F Item (126) Discard

1 Placard G2627004020400 Item (128) Discard

(17) Subtask 265020-831-204-001 - Remove the brackets and the insulation blankets

between FR35RH thru FR37.1RH.

Work Zones and Access Panels

Zone Access/Work location

132 Work location from Frame 35 to Frame 37.1

Manpower Resources

Manhours 3.50

Minimum number of person 2

Subtask elapsed time 1.75

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 25-80-00-000-801

Fig. A-GBDAA

Removal of the Brackets

Sheet 01

Sheet 02

Sheet 03

(a) Remove the insulation blankets in the affected area (Refer to AMM Task

25-80-00-000-801).

(b) Remove the brackets between FR35RH thru FR37.1RH.

Refer to Fig. A-GBDAA

1 Between FR35 and FR36, STGR 29RH, remove :

Refer to Fig. A-GBDAA Sheet 01 and Fig. A-GBDAA Sheet 03

1 Section-T F5397460021800 Item (161) Discard

1 Bracket Assy F5397484500200 Item (162) Discard

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 112

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@A340-500/600

SERVICE BULLETIN

2 From FR35RH, STGR31, remove :

Refer to Fig. A-GBDAA Sheet 01 and Fig. A-GBDAA Sheet 03

1 Bracket F5397463611000 Item (163) Discard

3 From FR36RH, STGR31, remove :

Refer to Fig. A-GBDAA Sheet 01 and Fig. A-GBDAA Sheet 03

1 Bracket F5397463610800 Item (164) Discard

4 From FR37RH, STGR31, remove :

Refer to Fig. A-GBDAA Sheet 01 and Fig. A-GBDAA Sheet 03

1 Bracket F5397463611000 Item (163) Discard

5 From FR37.1RH, STGR31, remove :

Refer to Fig. A-GBDAA Sheet 01 and Fig. A-GBDAA Sheet 03

1 Bracket F5397463610800 Item (164) Discard

6 From the crossbeam at FR35 at -Y2462, remove :

Refer to Fig. A-GBDAA Sheet 01 and Fig. A-GBDAA Sheet 02

1 Bracket Assy F5397800200000 Item (165) Discard

1 Bracket F5397461823000 Item (166) Discard

7 From the crossbeam at FR36 at -Y2462, remove :

Refer to Fig. A-GBDAA Sheet 01 and Fig. A-GBDAA Sheet 02

1 Bracket Assy F5397800200000 Item (165) Discard

1 Bracket F5397469928000 Item (167) Discard

8 Between FR35RH and FR36RH, remove :

Refer to Fig. A-GBDAA Sheet 01 and Fig. A-GBDAA Sheet 02

1 Strut Assy F5397883300000 Item (168) Discard

(18) Subtask 265020-831-213-001 - Install the brackets, modify the insulation blankets

and close the rivet holes between FR35RH thru FR37.1RH.

Work Zones and Access Panels

Zone Access/Work location

132 Work location from Frame 35 to Frame 37.1

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 113

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@A340-500/600

SERVICE BULLETIN

Manpower Resources

Manhours 7.00

Minimum number of person 2

Subtask elapsed time 3.50

Skills NON SPECIFIC

Material necessary to do the job

Kit 265020D02R04

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

170 EN6081D4-09 28 RIVET

171 EN6081D6-14 30 RIVET

252 F5397757020200 2 ANGLE

253 F5397462009600 1 BRACKET

254 F5397462009800 1 BRACKET

281 ABS1577A05 1 BRACKET

282 ABS0787B05B 1 BRACKET

References

Aircraft Maintenance Manual (AMM) Task 20-28-00-912-802

Task 25-80-00-200-801

Task 25-80-00-400-801

Fig. A-GBGAA

Installation of the Brackets

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Fig. A-GBDAA

Removal of the Brackets

Sheet 01

Sheet 02

Sheet 03

(a) Install the brackets and close the existing rivet holes.

Refer to Fig. A-GBDAA and Fig. A-GBGAA

1 Between FR35 and FR36, on STGR29RH and STGR30RH, close the rivet

holes in the stringers with :

Refer to Fig. A-GBDAA Sheet 01, Fig. A-GBDAA Sheet 02 and Fig. A-GBDAA

Sheet 03

4 Rivet EN6081D6-14 Item 171

2 On FR35 and FR36, STGR31RH, close the rivet holes in the frames with :

Refer to Fig. A-GBDAA Sheet 01, Fig. A-GBDAA Sheet 02 and Fig. A-GBDAA

Sheet 03

8 Rivet EN6081D6-14 Item 171

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 114

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SERVICE BULLETIN

3 Between FR36 and FR37, on STGR30RH, install this bracket on the stringer :

Refer to Fig. A-GBGAA Sheet 01 and Fig. A-GBGAA Sheet 02

1 Angle-Bonding F5397757020200 Item 252

with :

3 Rivet EN6081D4-09 Item 170

NOTE: Do the electrical bonding (Refer to AMM Task

20-28-00-912-802)

4 On FR37 and FR37.1, STGR31RH, close the rivet holes in the frames with :

Refer to Fig. A-GBDAA Sheet 01,Fig. A-GBDAA Sheet 02 and Fig. A-GBDAA

Sheet 03

8 Rivet EN6081D6-14 Item 171

5 On FR37, between STGR31RH and STGR32RH, install this bracket :

Refer to Fig. A-GBGAA Sheet 01 and Fig. A-GBGAA Sheet 02

1 Bracket Assy F5397462009600 Item 253

with :

4 Rivet EN6081D6-14 Item 171

NOTE: Do the electrical bonding (Refer to AMM Task

20-28-00-912-802)

NOTE: Existing rivet spacing must be used.

6 Between FR37 and FR37.1, on STGR30RH, install this bracket :

Refer to Fig. A-GBGAA Sheet 01 and Fig. A-GBGAA Sheet 02

1 Angle-Bonding F5397757020200 Item 252

with :

3 Rivet EN6081D4-09 Item 170

7 Between FR37 and FR37.1, on STGR30RH, install this bracket :

Refer to Fig. A-GBGAA Sheet 01 and Fig. A-GBGAA Sheet 03

1 Bracket ABS1577A05 Item 281

with :

3 Rivet EN6081D4-09 Item 170

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 115

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SERVICE BULLETIN

NOTE: Do the electrical bonding (Refer to AMM Task

20-28-00-912-802)

8 On FR37.1, between STGR31RH and STGR32RH, install this bracket :

Refer to Fig. A-GBGAA Sheet 01 and Fig. A-GBGAA Sheet 02

1 Bracket Assy F5397462009800 Item 254

with :

4 Rivet EN6081D6-14 Item 171

NOTE: Do the electrical bonding (Refer to AMM Task

20-28-00-912-802)

NOTE: Existing rivet spacing must be used.

9 On the crossbeam at FR35, between -Y1959 and -Y2462, close the rivet holes

in the crossbeam with :

Refer to Fig. A-GBDAA Sheet 01, Fig. A-GBDAA Sheet 02 and Fig. A-GBDAA

Sheet 03

10 Rivet EN6081D4-09 Item 170

10 On the crossbeam at FR36, outboard of -Y2462, close the rivet holes in the

crossbeam with :

Refer to Fig. A-GBDAA Sheet 01, Fig. A-GBDAA Sheet 02 and Fig. A-GBDAA

Sheet 03

9 Rivet EN6081D4-09 Item 170

11 On the crossbeam at FR36, outboard of -Y2462, install this bracket :

Refer to Fig. A-GBGAA Sheet 01 and Fig. A-GBGAA Sheet 03

1 Bracket-Z ABS0787B05B Item 282

with :

2 Rivet EN6081D6-14 Item 171

NOTE: Do the electrical bonding (Refer to AMM Task

20-28-00-912-802)

(b) Between FR36 thru FR37.1RH modify the insulation blankets in the affected area.

1 Adapt the insulation blankets for the new locations of brackets (Refer to AMM

Task 25-80-00-200-801).

(c) Install the modified insulation in the affected area (Refer to AMM Task

25-80-00-400-801).

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 116

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SERVICE BULLETIN

(19) Subtask 265020-831-216-001 - Modify the equipment and the wiring of the

FMCU/FMS outlet pressure switches 4031WX, 4032WX, 4033WX, 4034WX, 4016WX

and 4018WX of the fire extinguishing bottles Nos. 2 and 3.

Work Zones and Access Panels

Zone Access/Work location

132 Work location from Frame 35 to Frame 37.1

200 Work location Electrical panel 801VU

Manpower Resources

Manhours 1.50

Minimum number of person 2

Subtask elapsed time 0.75

Skills ELECTRICAL

Material necessary to do the job

Kit 265020D03R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

173 G9237018016600 1 PLCRDSET

174 NSA935401-04 8 TIE

175 NSA935401-05 15 TIE

References

Process and Material Specification

(PMS)

Process and Material Specification (PMS)

01-07-10

Fig. A-GWAAA

Modification of the Wiring of the

FMCU/FMS Outlet Pressure Switches

4031WX, 4032WX, 4033WX, 4034WX,

4016WX and 4018WX

Sheet 01

Sheet 02

Fig. A-GHAAA

Hook-up Chart

Sheet 01

Fig. A-GBLAA

Stowage of the Electrical Wires of the

Connectors 4031WX-A, 4032WX-A

4011WX-A, 4012WX-A and 4013WX-A

Sheet 01

Sheet 02

Sheet 03

Sheet 04

(a) Modify the wiring of the FMCU/FMS outlet pressure switches.

1 Disconnect these electrical wires from the connectors 4031WX-A and

4032WX-A.

Refer to Fig. A-GWAAA Sheet 01 (Wiring)

Refer to Fig. A-GHAAA Sheet 01 (Hook-up Chart), LINES 1, 2, 3 and 4

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 117

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SERVICE BULLETIN

2 Remove the connectors 4031WX-A and 4032WX-A and discard.

Refer to Fig. A-GBLAA Sheet 01

Remove :

2 Connector-Plug EN2997KE60803BN Item (265) Discard

and remove the following attachment parts :

4 Screw NAS1801-08-7 Item (267) Discard

2 Nut MS21042-08 Item (268) Discard

4 Washer NAS1149CN816R Item (269) Discard

2 Clamp MS21919WCH8 Item (270) Retain

2 Screw NAS1801-08-23 Item (271) Discard

2 Lanyard DAN80-3-150 Item (273) Discard

2 Sleeve-Protective NSA935809-09 Item (274) Discard

5 Cable Mount Item (277) Retain

3 Disconnect these electrical wires from the connectors 4033WX-A and

4034WX-A.

Refer to Fig. A-GWAAA Sheet 01 (Wiring)

Refer to Fig. A-GHAAA Sheet 01 (Hook-up Chart), LINES 5, 6, 7 and 8

4 Reroute and install the electrical wires :

Refer to Fig. A-GWAAA Sheet 02 (Wiring)

Refer to Fig. A-GHAAA Sheet 01 (Hook-up Chart), LINES 13, 14, 15 and 16

with :

15 Tie-Cable NSA935401-05 Item 175

and attach the placards, identified 4016WX-A, 4018WX-A and the SB/MOD

placards :

1 Placardset G9237018016600 Item 173

with :

8 Tie-Cable NSA935401-04 Item 174

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 118

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(20) Subtask 265020-831-209-001 - Modify the equipment and the wiring of the fire

extinguishing bottle No. 3 (AFT), 4020WX, and relocated fire extinguishing bottle

No. 2 (AFT), 4010WX.

Work Zones and Access Panels

Zone Access/Work location

132 Work location from Frame 35 to Frame 37.1

200 Work location Electrical panel 801VU

Electrical panel 802VU

Manpower Resources

Manhours 1.00

Minimum number of person 2

Subtask elapsed time 1.00

Skills ELECTRICAL

Material necessary to do the job

Kit 265020D03R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

173 G9237018016600 1 PLCRDSET

174 NSA935401-04 12 TIE

175 NSA935401-05 15 TIE

176 EN3155-003F1614 2 CONTACT

References

Fig. A-GWBAA

Modification of the Wiring of the Fire

Extinguishing Bottle No. 3 (previously

AFT), 4020WX, and relocated Fire

Extinguishing Bottle No. 2 (now AFT),

4010WX

Sheet 01

Sheet 02

Fig. A-GHBAA

Hook-up Chart

Sheet 01

(a) Modify the wiring of the cartridges and the pressure switch of the fire extinguishing

bottle (AFT), 4020WX (4010WX)

1 Disconnect these electrical wires from the connector 2625VC-A.

Refer to Fig. A-GWBAA Sheet 01 (Wiring)

Refer to Fig. A-GHBAA Sheet 01 (Hook-up Chart), LINES 1 and 11, END 2

2 Reroute and install the electrical wires on the connector 2511VC-A.

Refer to Fig. A-GWBAA Sheet 02 (Wiring)

Refer to Fig. A-GHBAA Sheet 01 (Hook-up Chart), LINES 2 and 12, END 2

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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3 Disconnect these electrical wires from the connector 2636VC-A.

Refer to Fig. A-GWBAA Sheet 01 (Wiring)

Refer to Fig. A-GHBAA Sheet 01 (Hook-up Chart), LINES 5 and 15, END 2

NOTE: Cut off the contacts directly behind the contacts.

4 Reroute and install the electrical wires on the connector 2508VC-A.

Refer to Fig. A-GWBAA Sheet 02 (Wiring)

Refer to Fig. A-GHBAA Sheet 01 (Hook-up Chart), LINES 6 and 16, END 2

with :

2 Contact-Socket EN3155-003F1614 Item 176

5 Disconnect the electrical wire from the connector 2044VC-A.

Refer to Fig. A-GWBAA Sheet 01 (Wiring)

Refer to Fig. A-GHBAA Sheet 01 (Hook-up Chart), LINE 23, END 2

6 Reroute and install the electrical wire on the connector 2016VC-A.

Refer to Fig. A-GWBAA Sheet 02 (Wiring)

Refer to Fig. A-GHBAA Sheet 01 (Hook-up Chart), LINE 24, END 2

7 Attach the placards, identified 4011WX-A, 4012WX-A, 4013WX-A and the

SB/MOD placards :

1 Placardset G9237018016600 Item 173

with :

12 Tie-Cable NSA935401-04 Item 174

8 Install the tie-cables on the wire harnesses :

15 Tie-Cable NSA935401-05 Item 175

NOTE: For the stowage position of the connectors 4011WX-A,

4012WX-A, 4013WX-A, 4031WX-A and 4032WX-A, refer to

(22) Subtask 265020-831-218-001.

(21) Subtask 265020-831-210-001 - Modify the Equipment and the Wiring of the

previous Fire Extinguishing Bottle No. 2 (FWD), 4010WX.

Work Zones and Access Panels

Zone Access/Work location

132 Work location from Frame 35 to Frame 36

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 120

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200 Work location Electrical panel 801VU

Electrical panel 802VU

Manpower Resources

Manhours 1.50

Minimum number of person 1

Subtask elapsed time 1.50

Skills ELECTRICAL

References

Fig. A-GWCAA

Modification of the Wiring of the Fire

Extinguishing Bottle No. 2 (FWD),

4010WX

Sheet 01

Sheet 02

Fig. A-GHCAA

Hook-up Chart

Sheet 01

Fig. A-GBLAA

Stowage of the Electrical Wires of the

Connectors 4031WX-A, 4032WX-A

4011WX-A, 4012WX-A and 4013WX-A

Sheet 01

Sheet 02

Sheet 03

Sheet 04

(a) Modify the wiring of the previous fire extinguishing bottle No. 2 (FWD), 4010WX.

1 Disconnect these electrical wires from the connectors 4011WX-A, 4012WX-A

and 4013WX-A.

Refer to Fig. A-GWCAA Sheet 01 (Wiring)

Refer to Fig. A-GHCAA Sheet 01 (Hook-up Chart), LINES 1, 5, 11, 15 and 23

Refer to Fig. A-GHCAA Sheet 01 (Hook-up Chart), LINES 3, 7, 9, 13, 17, 19,

21, END 1

2 Remove the connectors 4011WX-A, 4012WX-A and 4013WX-A and discard.

Refer to Fig. A-GBLAA Sheet 01

Remove :

2 Connector EN2997KE61005BN Item (264) Discard

1 Connector-Plug EN2997KE60803BN Item (265) Discard

and remove the following attachment parts :

1 Tie-Cable NSA935401-03 Item (266) Discard

5 Screw NAS1801-08-7 Item (267) Discard

2 Nut MS21042-08 Item (268) Discard

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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4 Washer NAS1149CN816R Item (269) Discard

2 Clamp MS21919WCH8 Item (270) Discard

1 Screw NAS1801-08-29 Item (272) Discard

2 Lanyard DAN80-3-150 Item (273) Discard

2 Sleeve-Protective NSA935809-09 Item (274) Discard

2 Cable Mount Item (277) Retain

NOTE: For the stowage position of the connectors 4011WX-A,

4012WX-A, 4013WX-A, 4031WX-A and 4032WX-A, refer to

(22) Subtask 265020-831-218-001.

(22) Subtask 265020-831-218-001 - Put the electrical wires of the connectors 4031WX-A,

4032WX-A 4011WX-A, 4012WX-A and 4013WX-A in a stowage position.

Work Zones and Access Panels

Zone Access/Work location

132 Work location from Frame 35 to Frame 37.1

Manpower Resources

Manhours 2.50

Minimum number of person 1

Subtask elapsed time 2.50

Skills ELECTRICAL

Material necessary to do the job

Kit 265020D03R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

173 G9237018016600 1 PLCRDSET

177 NSA936603CC0100 23 CAP

Kit 265020D05R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

266 NSA935401-03 25 TIE

269 NAS1149CN816R 4 WASHER

270 MS21919WCH8 4 CLAMP

271 NAS1801-08-23 2 SCREW

272 NAS1801-08-29 1 SCREW

274 NSA935809-09 4 SLEEVE

275 NAS1801-08-25 1 SCREW

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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References

Fig. A-GBLAA

Stowage of the Electrical Wires of the

Connectors 4031WX-A, 4032WX-A

4011WX-A, 4012WX-A and 4013WX-A

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Fig. A-GHAAA

Hook-up Chart

Sheet 01

Fig. A-GHCAA

Hook-up Chart

Sheet 01

Fig. A-GWAAA

Modification of the Wiring of the

FMCU/FMS Outlet Pressure Switches

4031WX, 4032WX, 4033WX, 4034WX,

4016WX and 4018WX

Sheet 01

Sheet 02

Fig. A-GWCAA

Modification of the Wiring of the Fire

Extinguishing Bottle No. 2 (FWD),

4010WX

Sheet 01

Sheet 02

(a) Put the electrical wires of the connectors 4031WX-A and 4032WX-A in a stowage

position.

1 Put the electrical wires in a stowage position.

Refer to Fig. A-GBLAA Sheet 01, Fig. A-GBLAA Sheet 02, Fig. A-GBLAA

Sheet 03 and Fig. A-GBLAA Sheet 04

Refer to Fig. A-GWAAA Sheet 02 (Wiring)

Refer toFig. A-GHAAA Sheet 01 (Hook-up Chart), LINES 9, 10, 11 and 12

with :

6 Cap NSA936603CC0100 Item 177

NOTE: Do not cut off the contacts.

Attach the electrical wires in a stowage position.

with :

2 Washer NAS1149CN816R Item 269

2 Clamp MS21919WCH8 Item 270

2 Clamp MS21919WCH8 Item (270) Retained at

removal

1 Screw NAS1801-08-23 Item 271

2 Sleeve-Protective NSA935809-09 Item 274

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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1 Screw NAS1801-08-25 Item 275

5 Cable Mount Item (277) Retained at

removal

20 Tie-Cable NSA935401-03 Item 266

(b) Put the electrical wires of the connectors 4011WX-A, 4012WX-A and 4013WX-A in

a stowage position.

1 Put the electrical wires in a stowage position.

Refer to Fig. A-GBLAA Sheet 01, Fig. A-GBLAA Sheet 02, Fig. A-GBLAA

Sheet 03 and Fig. A-GBLAA Sheet 04

Refer to Fig. A-GWCAA Sheet 02 (Wiring)

Refer to Fig. A-GHCAA Sheet 01 (Hook-up Chart), LINES 2, 6, 12, 16 and 24

Refer to Fig. A-GHCAA Sheet 01 (Hook-up Chart), LINES 4, 8, 10, 14, 18, 20

and 22, END 1

with :

17 Cap NSA936603CC0100 Item 177

NOTE: Do not cut off the contacts.

Attach the electrical wires in a stowage position.

with :

2 Washer NAS1149CN816R Item 269

2 Clamp MS21919WCH8 Item 270

1 Screw NAS1801-08-23 Item 271

1 Screw NAS1801-08-29 Item 272

2 Sleeve-Protective NSA935809-09 Item 274

2 Cable Mount Item (277) Retained at

removal

and attach the SB/MOD placards :

1 Placardset G9237018016600 Item 173

with :

5 Tie-Cable NSA935401-03 Item 266

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 124

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(23) Subtask 265020-831-205-001 - Adapt the plumbing installation.

Work Zones and Access Panels

Zone Access/Work location

132 Work location from Frame 36 to Frame 37

Manpower Resources

Manhours 3.00

Minimum number of person 2

Subtask elapsed time 1.50

Skills NON SPECIFIC

Material necessary to do the job

Kit 265020D01R03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

113 NAS1726-3E 2 NUT

121 NSA5516A18NJ 2 CLAMP

125 NSA855008D10 1 TEE

144 NAS1149C0332R 2 WASHER

155 NSA5527-03-03 2 SPACER

157 NAS1801-3-12 2 SCREW

158 NSA855006D10 2 UNION

251 G2627005013000 1 TUBE

253 G2627005002000 1 TUBE

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Internal Polyurethane

Varnish

07-017 As required

Solvent General Purpose 11-026 As required

Low Voc Anti-Corrosion

Primer

16-006F As required

Lint-Free Cotton Cloth 19-003 As required

Standard tool TOOLD01

ITEM TOOL N ̊ TOOL NAME QTY SEE

NOTES

D12102C07-02 PERMASWAGE Repair

Kit D12000 Series

1

References

Aircraft Maintenance Manual (AMM) 20-23-11, Page Block 201

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 125

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References

Fig. A-GBEAA

Adaption of the Plumbing Installation

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Fig. A-GBFAA

Installation of the U-Section and the

Flow Metering System (FMS)

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

(a) Remove the fire extinguishing tubes from FR36 and FR37.

Refer to Fig. A-GBEAA

1 Remove and discard these items from FR36RH :

Refer to Fig. A-GBEAA Sheet 01, Fig. A-GBEAA Sheet 02 and Fig. A-GBEAA

Sheet 04

1 Nut NAS1726-3E Item (113) Discard

1 Clamp NSA5516-18NJ Item (121) Discard

1 Washer NAS1149C0332R Item (144) Discard

1 Spacer NSA5527-03-03 Item (155) Discard

1 Screw NAS1096-3-14 Item (157) Discard

2 Cut the fire extinguishing tube, Item (250), at the position shown in Fig. AGBEAA Sheet 02 (Refer to AMM 20-23-11, Page Block 201).

3 Remove the fire extinguishing tube, Item (250), partly between the cut and the

outboard X-connection fitting :

1 Tube Assy, partly G2627005013000 Item (250) Discard

4 Deburr the remaining tube, Item (250), (Refer to AMM 20-23-11, Page Block

201).

5 Clean the remaining tube, Item (250), with :

Solvent General

Purpose

11-026 As required

and

Lint-Free Cotton

Cloth

19-003 As required

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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6 Remove and discard these items from FR37RH :

Refer to Fig. A-GBEAA Sheet 01, Fig. A-GBEAA Sheet 02 and Fig. A-GBEAA

Sheet 04

1 Nut NAS1726-3E Item (113) Discard

1 Clamp NSA5516-18NJ Item (121) Discard

1 Washer NAS1149C0332R Item (144) Discard

1 Spacer NSA5527-03-03 Item (155) Discard

1 Screw NAS1096-3-14 Item (157) Discard

7 Cut the fire extinguishing tube, Item (252), at the position shown in Fig. AGBEAA Sheet 02 (Refer to AMM 20-23-11, Page Block 201).

8 Remove the fire extinguishing tube, Item (252), partly between the cut and the

outboard T-connection fitting :

1 Tube Assy, partly G2627005002000 Item (252) Discard

1 Tee NSA855008D10 Item (125) Discard

9 Deburr the remaining tube, Item (252), (Refer to AMM 20-23-11, Page Block

201).

10 Clean the remaining tube, Item (252), with :

Solvent General

Purpose

11-026 As required

and

Lint-Free Cotton

Cloth

19-003 As required

(b) Install the fire extinguishing tubes on FR36 and FR37.

CAUTION: BEFORE YOU CONNECT THE FIRE EXTINGUISHING TUBES

WITH THE PERMASWAGE TOOL, MAKE SURE THAT THE FIRE

EXTINGUISHING TUBES ARE INSTALLED STRESS-FREE IN

THEIR CLAMPS.

CAUTION: DO NOT BEND THE TUBE WHEN YOU INSTALL IT. IF THE

TUBE IS BENT, IT CAN BECOME DAMAGED.

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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CAUTION: IF YOU USE DUST CAPS FOR THE CONTAMINATION

PROTECTION OF OPEN LINES, ALWAYS BE SURE TO

INSTALL THE CAPS AROUND THE TUBE ENDS AND NOT IN

THE TUBE ENDS. THERE CAN BE BLOCKAGE OF THE FLOW

THROUGH THE TUBES IF THESE TUBES ARE INSTALLED

ACCIDENTALLY WITH DUST CAPS IN THE TUBE ENDS.

NOTE: The fire extinguishing tubes must be installed with their related

clamps.

Refer to Fig. A-GBEAA

1 Install temporarily, Item 233, before install the other tubes.

Refer to Fig. A-GBFAA Sheet 01

2 Install the tube, Item 251, at FR36RH.

Refer to Fig. A-GBEAA Sheet 01, Fig. A-GBEAA Sheet 02 and Fig. A-GBEAA

Sheet 03

1 Tube Assy G2627005013000 Item 251

with :

1 Union NSA855006D10 Item 158

3 Connect the fire extinguishing tubes, Item (250), and Item 251, with the union,

Item 158, (Refer to AMM 20-23-11, Page Block 201).

D12102C07-02 PERMASWAGE

Repair Kit D12000

Series

1

NOTE: Use these swaging tools of the D12000 series :

- Head assembly D12210-56 with power unit D12010-52.

NOTE: The surface protection on both ends of the pipes must be

removed on a length of 43mm (1.692in.).

4 After the installation of the union, Item 158, perform surface protection with :

Low Voc AntiCorrosion Primer16-006F As required

and

Internal

Polyurethane

Varnish

07-017 As required

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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5 Install the clamp, Item 121, at FR36RH.

Fig. A-GBEAA Sheet 01, Fig. A-GBEAA Sheet 02 and Fig. A-GBEAA Sheet

03

1 Clamp NSA5516A18NJ Item 121

with :

1 Nut NAS1726-3E Item 113

1 Washer NAS1149C0332R Item 144

1 Spacer NSA5527-03-03 Item 155

1 Screw NAS1801-3-12 Item 157

6 Install temporarily, Item 234 and 238, before install the other tubes.

Refer to Fig. A-GBFAA Sheet 01

7 Install the tube, Item 253 at FR37RH.

Refer to Fig. A-GBEAA Sheet 01, Fig. A-GBEAA Sheet 02 and Fig. A-GBEAA

Sheet 03

1 Tube Assy G2627005002000 Item 253

with :

1 Tee NSA855008D10 Item 125

1 Union NSA855006D10 Item 158

8 Connect the fire extinguishing tubes, Item (252), and Item 253, with the union,

Item 158, and on the other end with the T-fitting, Item 125 (Refer to AMM

20-23-11, Page Block 201).

NOTE: Use these swaging tools of the D12000 series :

- Head assembly D12210-56 with power unit D12010-52.

NOTE: The surface protection on the ends of the pipes must be

removed on a length of 43mm (1.692in.).

9 After the installation of the tee-fitting, Item 125, and the union, Item 158,

perform surface protection with :

Low Voc AntiCorrosion Primer16-006F As required

and

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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Internal

Polyurethane

Varnish

07-017 As required

10 Install the clamp, Item 121, at FR37RH.

Fig. A-GBEAA Sheet 01, Fig. A-GBEAA Sheet 02 and Fig. A-GBEAA Sheet

03

1 Clamp NSA5516A18NJ Item 121

with :

1 Nut NAS1726-3E Item 113

1 Washer NAS1149C0332R Item 144

1 Spacer NSA5527-03-03 Item 155

1 Screw NAS1801-3-12 Item 157

11 Tighten all connections of the installed fire extinguishing tubes.

(24) Subtask 265020-831-206-001 - Install the U-section.

Work Zones and Access Panels

Zone Access/Work location

132 Work location from Frame 37 to Frame 37.1

Manpower Resources

Manhours 1.00

Minimum number of person 2

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 265020D01R03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

106 NAS1149F0332P 2 WASHER

143 NAS1801-3-8 4 SCREW

144 NAS1149C0332R 5 WASHER

145 NAS1801-3-7 3 SCREW

212 G2627008001400 1 SECTION

213 F2627008100000 1 BRACKET

220 E0090-10-135NN 1 LEAD

References

Aircraft Maintenance Manual (AMM) 20-28-00, Page Block 201

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 130

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References

Fig. A-GBFAA

Installation of the U-Section and the

Flow Metering System (FMS)

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

(a) Install the U-section between FR37RH and FR37.1.

Refer to Fig. A-GBFAA

1 Between FR37RH and FR37.1RH, install :

Refer to Fig. A-GBFAA Sheet 03, Fig. A-GBFAA Sheet 05 and Fig. A-GBFAA

Sheet 06

1 U-section G2627008001400 Item 212

1 Bracket F2627008100000 Item 213

1 Lead-Bonding E0090-10-135NN Item 220

with :

2 Washer NAS1149F0332P Item 106

4 Screw NAS1801-3-8 Item 143

5 Washer NAS1149C0332R Item 144

3 Screw NAS1801-3-7 Item 145

NOTE: For the installation of the bolt (Refer to AMM 20-28-00, Page

Block 201).

NOTE: Seal the bonding connection by overlapping application and

identify the bonding connection by overlapping application with

blue dyed protective coating.

(25) Subtask 265020-831-207-001 - Install the Flow Metering Systems (FMS) for the Fire

Ext. Bottles No. 1 and No. 2 on the U-section.

Work Zones and Access Panels

Zone Access/Work location

132 Work location from Frame 37 to Frame 37.1

Manpower Resources

Manhours 4.00

Minimum number of person 2

Subtask elapsed time 2.00

Skills NON SPECIFIC

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 131

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Material necessary to do the job

Kit 265020D01R03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

104 NAS1726-4E 2 NUT

106 NAS1149F0332P 6 WASHER

113 NAS1726-3E 3 NUT

121 NSA5516A18NJ 2 CLAMP

132 A2627048220400 6 FITTING

133 NSA8202-6 8 ORING

134 A2627048221600 2 FITTING

139 NAS1304-12 2 BOLT

140 NAS1149D0432K 10 WASHER

141 NSA5355-5CA 2 WASHER

143 NAS1801-3-8 6 SCREW

144 NAS1149C0332R 6 WASHER

145 NAS1801-3-7 4 SCREW

146 NAS1100E4-34 6 SCREW

147 A2627048920000 2 WASHER

148 NSA5516A06NJ 4 CLAMP

152 E0090-10-320NN 2 LEAD

153 E0090-10-350NN 2 LEAD

159 NAS1801-3-10 2 SCREW

160 MS21103-4 2 CLAMP

219 G2627006001000 1 TUBE

221 G2627006000800 1 TUBE

222 G2627006001800 1 TUBE

223 F2627006003600 1 TUBE

224 A2627048220200 2 RESTRCTR

225 F2627006001400 1 TUBE

226 F2627006000000 1 TUBE

227 F2627007200000 1 HOSE

228 F2627007200200 1 HOSE

229 G2627006002000 1 TUBE

230 G2627006001200 1 TUBE

231 G2627006001400 1 TUBE

232 G2627006001600 1 TUBE

233 NSA855140-22D 1 CROSS

234 G2627005013200 1 TUBE

235 MS21902W10 1 UNION

236 A2627045107800 1 TUBE

237 NSA855113-34D 1 TEE

238 G2627005003400 1 TUBE

239 MS21916W10-4 2 REDUCER

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 132

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Component COMPD01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

LN9424A100 As required WIRE

Equipment BFEZ01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

214 QA06753-03 2 FILTER

215 E61751-00-0001 2 REDUCER

216 TP0714033 2 SWITCH

217 HTE400115 2 VALVE

References

Aircraft Maintenance Manual (AMM) Task 20-28-00-912-802

Fig. A-GBFAA

Installation of the U-Section and the

Flow Metering System (FMS)

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

(a) Install the Halon Filter, FIN 5010WE, for Fire Ext. Bottle No. 1.

Refer to Fig. A-GBFAA

1 On the U-section, between FR37RH and FR37.1RH, install :

Refer to Fig. A-GBFAA Sheet 01, Fig. A-GBFAA Sheet 03 and Fig. A-GBFAA

Sheet 04

1 Filter-Halon QA06753-03 Item 214

NOTE: See NOTE 03

with :

3 Washer NAS1149D0432K Item 140

3 Screw NAS1100E4-34 Item 146

and

2 O-Ring NSA8202-6 Item 133

1 Fitting A2627048221600 Item 134

NOTE: See NOTE 03

1 Fitting A2627048220400 Item 132

NOTE: See NOTE 03

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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2 Secure the fittings, Items 132 and 134, with :

As

required

Wire-Lock LN9424A100

3 On the fitting, Item 134, install :

1 Hose Assy F2627007200000 Item 227

NOTE: See NOTE 03

NOTE (03): No lubrication on this item.

(b) Install the Pressure Reducer, FIN 5014WE, for Fire Ext. Bottle No. 1.

1 On the U-section, between FR37RH and FR37.1RH, install :

Refer to Fig. A-GBFAA Sheet 01, Fig. A-GBFAA Sheet 03 and Fig. A-GBFAA

Sheet 04

1 Reducer-Pressure E61751-00-0001 Item 215

NOTE: See NOTE 03

with :

1 Washer-Tab A2627048920000 Item 147

2 Fitting A2627048220400 Item 132

NOTE: See NOTE 03

2 O-Ring NSA8202-6 Item 133

NOTE (03): No lubrication on this item.

2 Secure the fittings, Item 132, with :

As

required

Wire-Lock LN9424A100

(c) Install the Pressure Switch, FIN 4016WX, for Fire Ext. Bottle No. 1.

1 On the pressure reducer 5014WE, between FR37RH and FR37.1RH, install :

Refer to Fig. A-GBFAA Sheet 01, Fig. A-GBFAA Sheet 03, Fig. A-GBFAA

Sheet 04 and Fig. A-GBFAA Sheet 05

1 Tube Assy G2627006000800 Item 221

with :

1 Washer NAS1149C0332R Item 144

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 134

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1 Screw NAS1801-3-7 Item 145

1 Clamp NSA5516A06NJ Item 148

and

1 Switch-Pressure TP0714033 Item 216

NOTE: See NOTE 03

2 On the pressure switch, Item 216, install :

1 Tube Assy G2627006001800 Item 222

with :

1 Washer NAS1149F0332P Item 106

1 SCREW NAS1801-3-10 Item 159

1 CLAMP MS21103-4 Item 160

NOTE (03): No lubrication on this item.

(d) Install the Check Valve, FIN 5016WE, for Fire Ext. Bottle No. 1.

1 On the pressure reducer 5014WE, between FR37RH and FR37.1RH, install :

Refer to Fig. A-GBFAA Sheet 01, Fig. A-GBFAA Sheet 03 and Fig. A-GBFAA

Sheet 05

1 Tube Assy F2627006003600 Item 223

1 Restrictor A2627048220200 Item 224

1 Tube Assy F2627006001400 Item 225

and

1 Valve-Nonreturn HTE400115 Item 217

NOTE: See NOTE 03

2 On the check valve, Item 217, install :

1 Tube Assy F2627006000000 Item 226

with :

1 Washer NAS1149C0332R Item 144

1 Screw NAS1801-3-7 Item 145

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 135

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1 Clamp NSA5516A06NJ Item 148

NOTE (03): No lubrication on this item.

(e) Install the Halon Filter, FIN 5011WE, for Fire Ext. Bottle No. 2.

Refer to Fig. A-GBFAA

1 On the U-section, between FR37RH and FR37.1RH, install :

Refer to Fig. A-GBFAA Sheet 01, Fig. A-GBFAA Sheet 03 and Fig. A-GBFAA

Sheet 04

1 Filter-Halon QA06753-03 Item 214

NOTE: See NOTE 03

with :

3 Washer NAS1149D0432K Item 140

3 Screw NAS1100E4-34 Item 146

and

2 O-Ring NSA8202-6 Item 133

1 Fitting A2627048221600 Item 134

NOTE: See NOTE 03

1 Fitting A2627048220400 Item 132

NOTE: See NOTE 03

2 Secure the fittings, Items 132 and 134, with :

As

required

Wire-Lock LN9424A100

3 On the fitting, Item 134, install :

1 Hose Assy F2627007200200 Item 228

NOTE: See NOTE 03

NOTE (03): No lubrication on this item.

(f) Install the Pressure Reducer, FIN 5015WE, for Fire Ext. Bottle No. 2.

1 On the U-section, between FR37RH and FR37.1RH, install :

Refer to Fig. A-GBFAA Sheet 01, Fig. A-GBFAA Sheet 03 and Fig. A-GBFAA

Sheet 04

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 136

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1 Reducer-Pressure E61751-00-0001 Item 215

NOTE: See NOTE 03

with :

1 Washer-Tab A2627048920000 Item 147

2 Fitting A2627048220400 Item 132

NOTE: See NOTE 03

2 O-Ring NSA8202-6 Item 133

2 Secure the fittings, Item 132, with :

As

required

Wire-Lock LN9424A100

NOTE (03): No lubrication on this item.

(g) Install the Pressure Switch, FIN 4018WX, for Fire Ext. Bottle No. 2

1 On the pressure reducer 5015WE, between FR37RH and FR37.1RH, install :

Refer to Fig. A-GBFAA Sheet 01, Fig. A-GBFAA Sheet 03 and Fig. A-GBFAA

Sheet 04

1 Tube Assy G2627006001000 Item 219

with :

1 Washer NAS1149C0332R Item 144

1 Screw NAS1801-3-7 Item 145

1 Clamp NSA5516A06NJ Item 148

and

1 Switch-Pressure TP0714033 Item 216

NOTE: See NOTE 03

2 On the pressure switch, Item 216, install :

1 Tube Assy G2627006002000 Item 229

with :

1 Washer NAS1149F0332P Item 106

1 SCREW NAS1801-3-10 Item 159

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 137

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1 CLAMP MS21103-4 Item 160

NOTE (03): No lubrication on this item.

(h) Install the Check Valve, FIN 5017WE, for Fire Ext. Bottle No. 2

1 On the pressure reducer 5015WE, between FR37RH and FR37.1RH, install :

Refer to Fig. A-GBFAA Sheet 01, Fig. A-GBFAA Sheet 03 and Fig. A-GBFAA

Sheet 05

1 Tube Assy G2627006001200 Item 230

1 Restrictor A2627048220200 Item 224

1 Tube Assy G2627006001400 Item 231

and

1 Valve-Nonreturn HTE400115 Item 217

NOTE: See NOTE 03

2 On the check valve, Item 217, install :

1 Tube Assy G2627006001600 Item 232

with :

1 Washer NAS1149C0332R Item 144

1 Screw NAS1801-3-7 Item 145

1 Clamp NSA5516A06NJ Item 148

1 Nut NAS1726-3E Item 113

NOTE (03): No lubrication on this item.

(i) Install the new plumbing and rod ends between FR36RH and FR37.1

1 Between FR36RH and FR37.1, install the rod ends :

Refer to Fig. A-GBFAA Sheet 01 and Fig. A-GBFAA Sheet 02

2 Rod End NSA8141-04R Item (135) Retained at

removal

2 Rod End NSA8140-04RK Item (137) Retained at

removal

with :

2 Nut NAS1726-4E Item 104

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 138

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2 BOLT NAS1304-12 Item 139

4 Washer NAS1149D0432K Item 140

2 Nut NAS509-5 Item (136) Retained at

removal

2 Washer-Lock NSA5355-5CA Item 141

and

2 Lead-Bonding E0090-10-320NN Item 152

2 Lead-Bonding E0090-10-350NN Item 153

with :

4 Washer NAS1149F0332P Item 106

4 Screw NAS1801-3-8 Item 143

NOTE: Do the electrical bonding (Refer to AMM Task

20-28-00-912-802)

2 Between FR36RH and FR37.1, install the plumbing :

Refer to Fig. A-GBFAA Sheet 01 and Fig. A-GBFAA Sheet 03

2 Hose A2627045200400 Item (209) Retained at

removal

2 Hose Assy F2627007100200 Item (210) Retained at

removal

1 Cross NSA855140-22D Item 233

1 Tube Assy G2627005013200 Item 234

1 Union MS21902W10 Item 235

with :

2 Screw NAS1801-3-8 Item 143

2 Washer NAS1149C0332R Item 144

2 Nut NAS1726-3E Item 113

2 Clamp NSA5516A18NJ Item 121

and

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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1 Tube Assy A2627045107800 Item 236

1 Tee NSA855113-34D Item 237

1 Tube Assy G2627005003400 Item 238

2 Reducer MS21916W10-4 Item 239

(26) Subtask 265020-831-211-001 - Install the Fire Extinguishing Bottles 4005WX and

4010WX.

Work Zones and Access Panels

Zone Access/Work location

132 Access Panel 132PM

Work location from Frame 35 to Frame 37.1

Manpower Resources

Manhours 2.00

Minimum number of person 2

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 265020D01R03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

100 NAS1726-5E 8 NUT

101 NAS1305-2 8 BOLT

103 NAS1304-9 2 BOLT

104 NAS1726-4E 2 NUT

Component COMPD01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

LN9424A100 As required WIRE

References

Aircraft Maintenance Manual (AMM) 26-23-41, Page Block 401

Fig. A-GBHAA

Installation of Fire Extinguishing Bottles

4005WX and 4010WX with Cartridges.

Sheet 01

Sheet 02

Sheet 03

Refer to Fig. A-GBHAA

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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(a) Install the fire extinguishing bottle 1 (FWD) 4005WX.

1 Between FR36RH and FR37RH, install the fire extinguishing bottle 4005WX

(Refer to AMM 26-23-41, Page Block 401) :

Refer to Fig. A-GBHAA Sheet 01, Fig. A-GBHAA Sheet 02and Fig. A-GBHAA

Sheet 03, Detail D :

1 Extinguisher-Fire 34900008-2 Item (201) Retained at

removal

with :

4 Nut NAS1726-5E Item 100

4 Bolt NAS1305-2 Item 101

1 Bolt NAS1304-9 Item 103

1 Nut NAS1726-4E Item 104

2 Screw Item (260)

2 Washer Item (261)

2 Nut Item (262)

NOTE: Item (260), (261) and (262) are retained parts.

2 Secure the coupling nuts of the fire extinguishing discharge heads with :

As

required

Wire-Lock LN9424A100

(b) Install the fire extinguishing bottle 2 (AFT) 4010WX.

1 Between FR37RH and FR37.1RH, install the fire extinguishing bottle 4010WX

(Refer to AMM 26-23-41, Page Block 401) :

Refer to Fig. A-GBHAA Sheet 01 and Fig. A-GBHAA Sheet 03 :

1 Extinguisher-Fire 35200003-2 Item (200) Retained at

removal

with :

4 Nut NAS1726-5E Item 100

4 Bolt NAS1305-2 Item 101

1 Bolt NAS1304-9 Item 103

1 Nut NAS1726-4E Item 104

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 141

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2 Screw Item (260)

2 Washer Item (261)

2 Nut Item (262)

NOTE: Item (260), (261) and (262) are retained parts.

2 Secure the coupling nuts of the fire extinguishing discharge heads with :

As

required

Wire-Lock LN9424A100

(27) Subtask 265020-831-212-001 - Install the new identification placards.

Work Zones and Access Panels

Zone Access/Work location

132 Work location from Frame 37 to Frame 37.1

Manpower Resources

Manhours 1.50

Minimum number of person 2

Subtask elapsed time 0.75

Skills NON SPECIFIC

Material necessary to do the job

Kit 265020D01R03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

240 F2627004120800 1 PLACARD

241 F2627004121400 1 PLACARD

242 F2627004121200 1 PLACARD

243 F2627004120400 1 PLACARD

244 F2627004120600 1 PLACARD

245 F2627004121600 1 PLACARD

246 F2627004121800 1 PLACARD

247 F2627004121000 1 PLACARD

248 G2627004020200 1 PLACARD

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Abrasion Resistant Coating

(Teflon Polyuret)

07-003 As required

General Purpose Adhesive

Honeycomb Filler

08-554 As required

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 142

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References

Fig. A-GBFAA

Installation of the U-Section and the

Flow Metering System (FMS)

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

(a) Install the identification placards 4010WX, 4016WX, 4018WX, 5010WE, 5011WE,

5014WE, 5015WE, 5016WE, 5017WE, between FR37 and FR37.1.

Refer to Fig. A-GBFAA

1 Between FR37RH and FR37.1RH, install :

Refer to Fig. A-GBFAA Sheet 01, Fig. A-GBFAA Sheet 03 and Fig. A-GBFAA

Sheet 06

1 Placard F2627004120800 Item 240

1 Placard F2627004121400 Item 241

1 Placard F2627004121200 Item 242

1 Placard F2627004120400 Item 243

1 Placard F2627004120600 Item 244

1 Placard F2627004121600 Item 245

1 Placard F2627004121800 Item 246

1 Placard F2627004121000 Item 247

1 Placard G2627004020200 Item 248

Bond the placard, Item 248, with :

General Purpose

Adhesive

Honeycomb Filler

08-554 As required

Protect the placard, Item 248, with :

Abrasion Resistant

Coating (Teflon

Polyuret)

07-003 As required

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 143

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**CONF 002

(1) Subtask 265020-831-001-003 - Modify the Equipment and the Wiring in the RH

Overhead Panel 212VU.

Work Zones and Access Panels

Zone Access/Work location

212 Work location Electrical panel 212VU

Manpower Resources

Manhours 12.00

Minimum number of person 1

Subtask elapsed time 12.00

Skills ELECTRICAL

Material necessary to do the job

Kit 265020A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

2 ASNA2083BG2-10 7 Screw

6 NSA937901MA2206 1 Module

7 NSA937901FM 1 Module

10 F9251088400000 1 Plate

F1131101500000 Placard

F9000095226495 Bundle

NAS1102-04-5 44 Screw

NSA935401-03 50 TIE

NSA937901E2 1 Label

Kit 265020A03R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 F33110263A00 1 Plate

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Pure Mineral Vaseline Or

Petro-Latum

04-012 As required

Electrical Bond Varnish 07-001B As required

Sealant, High Temperature 08-007C As required

References

Aircraft Maintenance Manual (AMM) Task 11-00-00-400-802

Task 20-28-00-912-802

Fig. A-FBBAA

Modification of the Equipment in the RH

Overhead Panel 212VU

Sheet 01

Sheet 02

Sheet 03

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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References

Fig. A-FCAAA

Modification of the Wiring in the RH

Overhead Panel 212VU

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

(a) Remove and disconnect the RH overhead panel 212VU.

NOTE: Retain it.

(b) Modify the equipment in the RH overhead panel 212VU.

1 Remove the integrally lighted plate (212LF).

a Remove as shown in Fig. A-FBBAA Sheet 01 :

FIN 212LF

1 Plate-Integrally Lighted F33110261A00 Item (1) Discard

attached with :

7 Screw ASNA2083BG2-10 Item (2) Discard

2 Remove the indicator light BTL3 (5WX).

a Remove as shown in Fig. A-FBBAA Sheet 01 and Fig. A-FBBAA Sheet

02, Detail B :

FIN 5WX

1 Light-Indicator ABS0951A0LP110 Item (3) Discard

FIN 5WX1

1 Sleeve E0416-02 Item (4) Discard

FIN 5WXA

1 Connector E0417A01S Item (5) Discard

NOTE: Remove and discard the attachment hardware.

3 Replace the 212VU front plate.

a Remove and retain all the items of equipment that are installed on the

front plate.

b Remove as shown in Fig. A-FBBAA Sheet 01 :

1 Plate Assy- Front

212VU

F9251602100000 Item (10) Discard

attached with :

8 Screw NAS1102-06-5 Item (11) Retain

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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c On the new front plate, bond the placards (Refer to AMM Task

11-00-00-400-802) supplied in :

Placard Set-212VU F1131101500000

NOTE: Bond the applicable placards at the same locations as on

the old front plate. Discard the unused placards.

d Install as shown in Fig. A-FBBAA Sheet 03 :

1 Plate Assy- Front

212VU

F9251088400000 Item 10

attach with :

8 Screw NAS1102-06-5 Item (11)

NOTE: The screws Item (11) were retained at the removal.

e Install again all the items of equipment that you removed and retained

before the replacement of the front plate and attach with :

44 Screw NAS1102-04-5

Safety the screws with :

Sealant, High

Temperature

08-007C As required

NOTE: Replace the screws if they are damaged during the

removal. The quantity of screws to be replaced depends

on aircraft configuration (44 is the maximum).

f Do the electrical bonding (Refer to AMM Task 20-28-00-912-802) with :

Pure Mineral

Vaseline Or PetroLatum

04-012 As required

and

Electrical Bond

Varnish

07-001B As required

4 Modify the terminal block (582VT) as shown in Fig. A-FBBAA Sheet 01 and

Fig. A-FBBAA Sheet 02, Detail C.

a Remove from position 2 :

FIN 582VT2

1 Module-False NSA937901FM Item (6) Discard

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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b Remove from position 3 :

FIN 582VT3

1 Module NSA937901MA2204 Item (7) Discard

c Install at position 2 as shown in :

FIN 582VT2

1 Module NSA937901MA2206 Item 6

with

1 Label-Identification NSA937901E2

d Install at position 3 as shown in :

FIN 582VT3

1 Module-False NSA937901FM Item 7

5 Install the new integrally lighted plate (212LF).

a Install as shown in Fig. A-FBBAA Sheet 03 :

FIN 212LF

1 Plate-Integrally Lighted F33110263A00 Item 1

attach with :

7 Screw ASNA2083BG2-10 Item 2

(c) Modify the wiring in the RH overhead panel 212VU.

1 Remove the wires as shown in the wiring diagrams Fig. A-FCAAA Sheet 01,

Fig. A-FCAAA Sheet 02 and as given in the hook-up chart lines :

- 1 thru 13 (Refer to Fig. A-FCAAA Sheet 04).

2 Modify the connections of the wires as shown in the wiring diagrams Fig. AFCAAA Sheet 02, Fig. A-FCAAA Sheet 03 and as given in the hook-up chart

lines :

- 17 thru 24 (Refer to Fig. A-FCAAA Sheet 04)

- 1 and 2 (Refer to Fig. A-FCAAA Sheet 05).

3 Install the wires as shown in the wiring diagram Fig. A-FCAAA Sheet 03 and

as given in the hook-up chart lines :

- 6 thru 12 (Refer to Fig. A-FCAAA Sheet 05), supplied in :

Bundle F9000095226495

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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4 Attach the wires with :

50 Tie-Cable NSA935401-03

(d) Install the RH overhead panel 212VU.

(2) Subtask 265020-831-002-001 - Modify the Equipment and the Wiring in the

Emergency Power Center 740VU.

Work Zones and Access Panels

Zone Access/Work location

121 Access Door 821, Door 132AZ

Work location Electrical panel 740VU

Manpower Resources

Manhours 3.50

Minimum number of person 1

Subtask elapsed time 3.50

Skills ELECTRICAL

Material necessary to do the job

Kit 265020A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

F9000095226495 Bundle

NSA935401-03 50 TIE

NSA935401-05 50 TIE

References

Fig. A-FBCAA

Modification of the Equipment in the

Emergency Power Center 740VU

Sheet 01

Fig. A-FCBAA

Modification of the Wiring in the

Emergency Power Center 740VU

Sheet 01

Sheet 02

(a) Open the emergency power center 740VU.

(b) Remove the wires as shown in the wiring diagram Fig. A-FCBAA Sheet 01 and as

given in the hook-up chart lines :

- 1 thru 8 (Refer to Fig. A-FCBAA Sheet 02).

(c) Modify the terminal block (703VT) as shown in Fig. A-FBCAA Sheet 01.

1 Remove from position 21 :

1 Clamp-End NSA937901S Retain

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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2 Remove from position 20 :

FIN 703VT20

1 Module NSA937901MA2004 Item (7) Discard

3 Install at position 20 :

1 Clamp-End NSA937901S

NOTE: The end clamp was retained at the removal.

(d) Install the wire as shown in the wiring diagram Fig. A-FCBAA Sheet 01 and as

given in the hook-up chart line :

- 12 (Refer to Fig. A-FCBAA Sheet 02), supplied in :

Bundle F9000095226495

(e) Attach the wire with :

50 Tie-Cable NSA935401-03

50 Tie-Cable NSA935401-05

(f) Close the emergency power center 740VU.

(3) Subtask 265020-831-003-001 - Modify the Equipment and the Wiring in the AC/DC

Main Power Center 710VU.

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 821, Door 132AZ

Work location Electrical panel 710VU

Manpower Resources

Manhours 3.50

Minimum number of person 1

Subtask elapsed time 3.50

Skills ELECTRICAL

Material necessary to do the job

Kit 265020A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

F9000095226495 Bundle

NSA935401-03 50 TIE

NSA935401-05 50 TIE

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 149

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References

Fig. A-FBDAA

Modification of the Equipment in the

AC/DC Main Power Center 710VU

Sheet 01

Fig. A-FCCAA

Modification of the Wiring in the AC/DC

Main Power Center 710VU

Sheet 01

Sheet 02

(a) Open the AC/DC main power center 710VU.

(b) Remove the wires as shown in the wiring diagram Fig. A-FCCAA Sheet 01 and as

given in the hook-up chart lines :

- 1 thru 8 (Refer to Fig. A-FCCAA Sheet 02).

(c) Modify the terminal block (1712VT) as shown in Fig. A-FBDAA Sheet 01.

1 Remove from position 18 :

1 Clamp-End NSA937901S Retain

2 Remove from position 17 :

FIN 1712VT17

1 Module NSA937901MA2004 Item (7) Discard

3 Install at position 17 :

1 Clamp-End NSA937901S

NOTE: The end clamp was retained at the removal.

(d) Install the wire as shown in the wiring diagram Fig. A-FCCAA Sheet 01 and as

given in the hook-up chart line :

- 12 (Refer to Fig. A-FCCAA Sheet 02), supplied in :

Bundle F9000095226495

(e) Attach the wire with :

50 Tie-Cable NSA935401-03

50 Tie-Cable NSA935401-05

(f) CLose the AC/DC main power center 710VU.

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 150

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SERVICE BULLETIN

(4) Subtask 265020-831-004-001 - Modify the Equipment and the Wiring in the LH

Relay Box 751VU.

Work Zones and Access Panels

Zone Access/Work location

121 Access Door 821, Door 132AZ

Work location Electrical panel 751VU

Manpower Resources

Manhours 3.50

Minimum number of person 1

Subtask elapsed time 3.50

Skills ELECTRICAL

References

Fig. A-FBEAA

Modification of the Equipment in the LH

Relay Box 751VU

Sheet 01

Fig. A-FCDAA

Modification of the Wiring in the LH

Relay Box 751VU

Sheet 01

Sheet 02

(a) Open the LH relay box 751VU.

(b) Remove the wires as shown in the wiring diagram Fig. A-FCDAA Sheet 01 and as

given in the hook-up chart lines :

- 1 thru 12 (Refer to Fig. A-FCDAA Sheet 02).

(c) Remove from position E93, as shown in Fig. A-FBEAA Sheet 01 :

FIN 10WX

1 Relay E0245-28A0 Item (8) Discard

FIN 10WXA

1 Base E0250A0S Item (9) Discard

NOTE: Remove and discard the attachment hardware and the related

placard(s).

(d) Remove from position E89, as shown in Fig. A-FBEAA Sheet 01 :

FIN 11WX

1 Relay E0245-28A0 Item (8) Discard

FIN 11WXA

1 Base E0250A0S Item (9) Discard

NOTE: Remove and discard the attachment hardware and the related

placard(s).

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 151

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SERVICE BULLETIN

(e) Close the LH relay box 751VU.

(5) Subtask 265020-831-005-001 - Modify the Equipment and the Wiring in the RH

Relay Box 752VU.

Work Zones and Access Panels

Zone Access/Work location

122 Access Door 821, Door 132AZ

Work location Electrical panel 752VU

Manpower Resources

Manhours 3.50

Minimum number of person 1

Subtask elapsed time 3.50

Skills ELECTRICAL

References

Fig. A-FBFAA

Modification of the Equipment in the RH

Relay Box 752VU

Sheet 01

Fig. A-FCEAA

Modification of the Wiring in the RH

Relay Box 752VU

Sheet 01

Sheet 02

(a) Open the RH relay box 752VU.

(b) Remove the wires as shown in the wiring diagram Fig. A-FCEAA Sheet 01 and as

given in the hook-up chart lines :

- 1 thru 12 (Refer to Fig. A-FCEAA Sheet 02).

(c) Remove from position B37, as shown in Fig. A-FBFAA Sheet 01 :

FIN 12WX

1 Relay E0245-28A0 Item (8) Discard

FIN 12WXA

1 Base E0250A0S Item (9) Discard

NOTE: Remove and discard the attachment hardware and the related

placard(s).

(d) Remove from position B33, as shown in Fig. A-FBFAA Sheet 01 :

FIN 13WX

1 Relay E0245-28A0 Item (8) Discard

FIN 13WXA

1 Base E0250A0S Item (9) Discard

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 152

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SERVICE BULLETIN

NOTE: Remove and discard the attachment hardware and the related

placard(s).

(e) Close the RH relay box 752VU.

(6) Subtask 265020-831-006-001 - Modify the Equipment and the Wiring in the Main

Rack 800VU.

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 821, Door 132AZ

Work location Electrical panel 800VU

Manpower Resources

Manhours 8.00

Minimum number of person 2

Subtask elapsed time 4.00

Skills ELECTRICAL

Material necessary to do the job

Kit 265020A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

7 NSA937901FM 1 Module

F9000095226495 Bundle

NSA935401-03 200 TIE

NSA935401-05 200 TIE

NSA935401-08 200 Tie

References

Aircraft Maintenance Manual (AMM) Task 26-16-34-000-801

Task 26-16-34-400-801

Fig. A-FBGAA

Modification of the Equipment in the

Main Rack 800VU

Sheet 01

Fig. A-FCFAA

Modification of the Wiring in the Main

Rack 800VU

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

Fig. A-FCGAA

Modification of the Pin Programming in

the Main Rack 800VU

Sheet 01

Sheet 02

(a) Remove and retain the SDCU (20WH) (Refer to AMM Task 26-16-34-000-801).

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 153

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SERVICE BULLETIN

(b) Remove the wires as shown in the wiring diagrams Fig. A-FCFAA Sheet 01, Fig. AFCFAA Sheet 02, Fig. A-FCFAA Sheet 03, and as given in the hook-up chart lines :

- 1 thru 25 (Refer to Fig. A-FCFAA Sheet 05)

- 1 thru 3 (Refer to Fig. A-FCFAA Sheet 06).

(c) Modify the terminal block (2900VT) as shown in Fig. A-FBGAA Sheet 01.

1 Remove from position 50 :

FIN 2900VT50

1 Module NSA937901MA2011 Item (7) Discard

2 Install at position 50 :

FIN 2900VT50

1 Module-False NSA937901FM Item 7

(d) Install the wires as shown in the wiring diagram Fig. A-FCFAA Sheet 04 and as

given in the hook-up chart lines :

- 7 thru 18 (Refer to Fig. A-FCFAA Sheet 06), supplied in :

Bundle F9000095226495

(e) Modify the connection of the wires as shown in the wiring diagram Fig. A-FCGAA

Sheet 01 and as given in the hook-up chart lines :

- 1 thru 4 (Refer to Fig. A-FCGAA Sheet 02).

(f) Attach the wires with :

200 Tie-Cable NSA935401-03

200 Tie-Cable NSA935401-05

200 Tie-Cable NSA935401-08

(g) Install the SDCU (20WH) (Refer to AMM Task 26-16-34-400-801).

(7) Subtask 265020-831-007-001 - Modify the Wiring between the Main Rack Shelf

801VU and the LH Relay Box 751VU.

Work Zones and Access Panels

Zone Access/Work location

121 Access Door 821, Door 132AZ

Work location from Electrical panel 801VU to Electrical panel

751VU

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 154

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@A340-500/600

SERVICE BULLETIN

Manpower Resources

Manhours 3.50

Minimum number of person 1

Subtask elapsed time 3.50

Skills ELECTRICAL

Material necessary to do the job

Kit 265020A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

NSA936604CA0931 8 Cap

References

Fig. A-FBAAA

Location of the Working Areas

Sheet 01

Fig. A-FCHAA

Modification of the Wiring between the

Main Rack Shelf 801VU and the LH

Relay Box 751VU

Sheet 01

Sheet 02

(a) Modify the connections of the wires as shown in the wiring diagram Fig. A-FCHAA

Sheet 01 and as given in the hook-up chart lines :

- 1 thru 8 (Refer to Fig. A-FCHAA Sheet 02).

(b) Install on the stowed wires ends :

8 Cap-Sealing NSA936604CA0931

(8) Subtask 265020-831-008-001 - Modify the Wiring between the Main Rack Shelf

802VU and the RH Relay Box 752VU.

Work Zones and Access Panels

Zone Access/Work location

122 Access Door 821, Door 132AZ

Work location from Electrical panel 802VU to Electrical panel

752VU

Manpower Resources

Manhours 3.50

Minimum number of person 1

Subtask elapsed time 3.50

Skills ELECTRICAL

References

Fig. A-FBAAA

Location of the Working Areas

Sheet 01

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 155

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SERVICE BULLETIN

References

Fig. A-FCJAA

Modification of the Wiring between the

Main Rack Shelf 802VU and the RH

Relay Box 752VU

Sheet 01

Sheet 02

(a) Remove the wires as shown in the wiring diagram Fig. A-FCJAA Sheet 01 and as

given in the hook-up chart lines :

- 1 thru 4 (Refer to Fig. A-FCJAA Sheet 02).

(9) Subtask 265020-831-009-001 - Modify the Wiring between the Emergency Power

Center 740VU and the LH Relay Box 751VU.

Work Zones and Access Panels

Zone Access/Work location

121 Access Door 821, Door 132AZ

Work location from Electrical panel 740VU to Electrical panel

751VU

Manpower Resources

Manhours 3.50

Minimum number of person 1

Subtask elapsed time 3.50

Skills ELECTRICAL

References

Fig. A-FBAAA

Location of the Working Areas

Sheet 01

Fig. A-FCKAA

Modification of the Wiring between the

Emergency Power Center 740VU and

the LH Relay Box 751VU

Sheet 01

Sheet 02

(a) Remove the wires as shown in the wiring diagram Fig. A-FCKAA Sheet 01 and as

given in the hook-up chart lines :

- 1 thru 4 (Refer to Fig. A-FCKAA Sheet 02).

(10) Subtask 265020-831-010-001 - Modify the Wiring between the AC/DC Main Power

Center 715VU and the RH Relay Box 752VU.

Work Zones and Access Panels

Zone Access/Work location

122 Access Door 821, Door 132AZ

Work location from Electrical panel 715VU to Electrical panel

752VU

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 156

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@A340-500/600

SERVICE BULLETIN

Manpower Resources

Manhours 3.50

Minimum number of person 1

Subtask elapsed time 3.50

Skills ELECTRICAL

References

Fig. A-FBAAA

Location of the Working Areas

Sheet 01

Fig. A-FCLAA

Modification of the Wiring between the

AC/DC Main Power Center 715VU and

the RH Relay Box 752VU

Sheet 01

Sheet 02

(a) Remove the wires as shown in the wiring diagram Fig. A-FCLAA Sheet 01 and as

given in the hook-up chart lines :

- 1 thru 4 (Refer to Fig. A-FCLAA Sheet 02).

(11) Subtask 265020-831-011-001 - Modify the Wiring between the Main Rack Shelf

801VU and the Avionics Compartment at FR2.

Work Zones and Access Panels

Zone Access/Work location

From 121 Access Door 821, Door 132AZ

Work location Electrical panel 801VU

To 211 Access Door 831, Door 841

Panel 211EW

Work location Frame 2

Manpower Resources

Manhours 3.50

Minimum number of person 1

Subtask elapsed time 3.50

Skills ELECTRICAL

Material necessary to do the job

Kit 265020A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

NSA936604CA0931 2 Cap

References

Fig. A-FBAAA

Location of the Working Areas

Sheet 01

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 157

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SERVICE BULLETIN

References

Fig. A-FCMAA

Modification of the Wiring between the

Main Rack Shelf 801VU and the

Avionics Compartment at FR2

Sheet 01

Sheet 02

(a) Modify the connections of the wire as shown in the wiring diagram Fig. A-FCMAA

Sheet 01 and as given in the hook-up chart lines :

- 1 and 2 (Refer to Fig. A-FCMAA Sheet 02).

(b) Install on the stowed wire ends :

2 Cap-Sealing NSA936604CA0931

(12) Subtask 265020-831-012-001 - Modify the Wiring between the RH Overhead Panel

212VU and the Avionics Compartment (LH Side).

Work Zones and Access Panels

Zone Access/Work location

From 212 Access Door 831, Door 841

Work location Electrical panel 212VU

To 121 Access Door 821, Door 132AZ

Work location Electrical panel 751VU

Electrical panel 740VU

Frame 2

Electrical panel 801VU

Manpower Resources

Manhours 10.00

Minimum number of person 2

Subtask elapsed time 5.00

Skills ELECTRICAL

Material necessary to do the job

Kit 265020A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

F9000095226495 Bundle

NSA935401-05 200 TIE

NSA935401-08 200 Tie

NSA936604CA0931 8 Cap

References

Fig. A-FBAAA

Location of the Working Areas

Sheet 01

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 158

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SERVICE BULLETIN

References

Fig. A-FCNAA

Modification of the Wiring between the

RH Overhead Panel 212VU and the

Avionics Compartment (LH Side)

Sheet 01

Sheet 02

Sheet 03

(a) Modify the connections of the wires as shown in the wiring diagrams Fig. A-FCNAA

Sheet 01, Fig. A-FCNAA Sheet 02 and as given in the hook-up chart lines :

- 1 thru 8 (Refer to Fig. A-FCNAA Sheet 03).

(b) Install on the stowed wires ends :

8 Cap-Sealing NSA936604CA0931

(c) Install the wires as shown in the wiring diagram Fig. A-FCNAA Sheet 01 and as

given in the hook-up chart lines :

- 12 and 13 (Refer to Fig. A-FCNAA Sheet 02), supplied in :

Bundle F9000095226495

(d) Attach the wires with :

200 Tie-Cable NSA935401-05

200 Tie-Cable NSA935401-08

(13) Subtask 265020-831-013-001 - Modify the Wiring between the RH Overhead Panel

212VU and the Avionics Compartment (RH Side).

Work Zones and Access Panels

Zone Access/Work location

From 212 Access Door 831, Door 841

Work location Electrical panel 212VU

To 122 Access Door 821, Door 132AZ

Panel 131BA

Work location Electrical panel 752VU

Electrical panel 715VU

Electrical panel 802VU

Frame 20

Manpower Resources

Manhours 10.00

Minimum number of person 2

Subtask elapsed time 5.00

Skills ELECTRICAL

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 159

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SERVICE BULLETIN

Material necessary to do the job

Kit 265020A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

F9000095226495 Bundle

NSA935401-05 200 TIE

NSA935401-08 200 Tie

NSA936604CA0931 10 Cap

References

Fig. A-FBAAA

Location of the Working Areas

Sheet 01

Fig. A-FCPAA

Modification of the Wiring between the

RH Overhead Panel 212VU and the

Avionics Compartment (RH Side)

Sheet 01

Sheet 02

Sheet 03

(a) Modify the connections of the wires as shown in the wiring diagram Fig. A-FCPAA

Sheet 01, Fig. A-FCPAA Sheet 02 and as given in the hook-up chart lines :

- 1 thru 12 (Refer to Fig. A-FCPAA Sheet 03).

(b) Install on the stowed wires ends :

10 Cap-Sealing NSA936604CA0931

(c) Install the wires as shown in the wiring diagram Fig. A-FCPAA Sheet 01 and as

given in the hook-up chart lines :

- 9 and 10 (Refer to Fig. A-FCPAA Sheet 02), supplied in :

Bundle F9000095226495

(d) Attach the wires with :

200 Tie-Cable NSA935401-05

200 Tie-Cable NSA935401-08

(14) Subtask 265020-831-201-002 - Remove the Fire Extinguishing Bottles, 4010WX,

4005WX and 4020WX.

Work Zones and Access Panels

Zone Access/Work location

132 Access Panel 132PM

Work location from Frame 35 to Frame 37.1

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 160

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@A340-500/600

SERVICE BULLETIN

Manpower Resources

Manhours 3.00

Minimum number of person 2

Subtask elapsed time 1.50

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 26-23-41, Page Block 401

Fig. A-GBBAA

Removal of Fire Extinguishing Bottles

4005WX, 4010WX and 4020WX with

Cartridges.

Sheet 01

Sheet 02

Sheet 03

(a) Remove the Fire Extinguishing Bottle 2 (FWD), 4010WX.

Refer to Fig. A-GBBAA

1 Between FR35RH and FR36RH, remove the fire extinguishing bottle 4010WX

(Refer to AMM 26-23-41, Page Block 401) :

Refer to Fig. A-GBBAA Sheet 01 and Fig. A-GBBAA Sheet 02 :

1 Extinguisher-Fire 472625-3 Item (203) Retain

with :

4 Nut NAS1726-5E Item (100) Discard

4 Bolt NAS1305-2 Item (101) Discard

1 Bolt NAS1304-9 Item (103) Discard

1 Nut NAS1726-4E Item (104) Discard

2 Bolt NAS563-11 Item (105) Discard

2 Washer NAS1149F0332P Item (106) Discard

(b) Remove the Fire Extinguishing Bottle 1 (MID), 4005WX.

Refer to Fig. A-GBBAA

1 Between FR36RH and FR37RH, remove the fire extinguishing bottle 4005WX

(Refer to AMM 26-23-41, Page Block 401) :

Refer to Fig. A-GBBAA Sheet 01 and Fig. A-GBBAA Sheet 03 :

1 Extinguisher-Fire 472931-3 Item (204) Retain

with :

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 161

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@A340-500/600

SERVICE BULLETIN

4 Nut NAS1726-5E Item (100) Discard

4 Bolt NAS1305-2 Item (101) Discard

1 Bolt NAS1304-9 Item (103) Discard

1 Nut NAS1726-4E Item (104) Discard

2 Bolt NAS563-11 Item (105) Discard

2 Washer NAS1149F0332P Item (106) Discard

(c) Remove the Fire Extinguishing Bottle 3 (AFT), 4020WX.

Refer to Fig. A-GBBAA

1 Between FR37RH and FR37.1RH, remove the fire extinguishing bottle

4020WX (Refer to AMM 26-23-41, Page Block 401) :

Refer to Fig. A-GBBAA Sheet 01 and Fig. A-GBBAA Sheet 02 :

1 Extinguisher-Fire 472625-3 Item (203) Discard

with :

4 Nut NAS1726-5E Item (100) Discard

4 Bolt NAS1305-2 Item (101) Discard

1 Bolt NAS1304-9 Item (103) Discard

1 Nut NAS1726-4E Item (104) Discard

2 Bolt NAS563-11 Item (105) Discard

2 Washer NAS1149F0332P Item (106) Discard

(15) Subtask 265020-831-202-001 - Remove the 4 Flow Metering Compact Units (FMCU),

FIN 4031WX, 4032WX, 4033WX and 4034WX.

Work Zones and Access Panels

Zone Access/Work location

132 Access Panel 132PM

Work location from Frame 35 to Frame 37.1

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 162

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@A340-500/600

SERVICE BULLETIN

Manpower Resources

Manhours 4.00

Minimum number of person 2

Subtask elapsed time 2.00

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 26-23-43, Page Block 401

Fig. A-GBCAA

Removal of the 4 Flow Metering

Compact Units (FMCU), FIN 4031WX,

4032WX, 4033WX and 4034WX, the

related Plumbing Installations and

Placards

Sheet 01

Sheet 02

Sheet 03

(a) Remove the Flow Metering Compact Unit (FMCU), FIN 4031WX.

Refer to Fig. A-GBCAA

1 From FR35RH, remove the FMCU, FIN 4031WX (Refer to AMM 26-23-43,

Page Block 401) :

Refer to Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet 02 and Fig. A-GBCAA

Sheet 03

1 Meter-Flow, Compact

Unit

QA07907-01 Item (205) Discard

and

1 Hose Assy G2627007000000 Item (107) Discard

1 Tube Assy G2627006000000 Item (109) Discard

with :

1 Washer NAS1149F0332P Item (106) Discard

1 Clamp NSA5516-06NJ Item (111) Discard

1 Screw NAS1096-3-10 Item (112) Discard

1 Nut NAS1726-3E Item (113) Discard

3 Screw NAS1100E4-36 Item (130) Discard

3 Washer NAS1149C0432R Item (131) Discard

1 Fitting A2627048220400 Item (132) Discard

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 163

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@A340-500/600

SERVICE BULLETIN

2 O-Ring NSA8202-6 Item (133) Discard

1 Fitting A2627048221600 Item (134) Discard

(b) Remove the Flow Metering Compact Unit (FMCU), FIN 4032WX.

Refer to Fig. A-GBCAA

1 From FR36RH, remove the FMCU, FIN 4032WX (Refer to AMM 26-23-43,

Page Block 401) :

Refer to Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet 02 and Fig. A-GBCAA

Sheet 03

1 Meter-Flow, Compact

Unit

QA07907-01 Item (205) Discard

and

1 Hose Assy G2627007000200 Item (108) Discard

1 Tube Assy G2627006000200 Item (110) Discard

with :

1 Washer NAS1149F0332P Item (106) Discard

1 Clamp NSA5516-06NJ Item (111) Discard

1 Screw NAS1096-3-10 Item (112) Discard

1 Nut NAS1726-3E Item (113) Discard

3 Screw NAS1100E4-36 Item (130) Discard

3 Washer NAS1149C0432R Item (131) Discard

1 Fitting A2627048220400 Item (132) Discard

2 O-Ring NSA8202-6 Item (133) Discard

1 Fitting A2627048221600 Item (134) Discard

(c) Remove the Flow Metering Compact Unit (FMCU), FIN 4033WX.

Refer to Fig. A-GBCAA

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 164

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@A340-500/600

SERVICE BULLETIN

1 From FR37RH, remove the FMCU, FIN 4033WX (Refer to AMM 26-23-43,

Page Block 401) :

Refer to Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet 02 and Fig. A-GBCAA

Sheet 03

1 Meter-Flow, Compact

Unit

QA07907-01 Item (205) Discard

and

1 Hose Assy G2627007000000 Item (107) Discard

1 Tube Assy G2627006000000 Item (109) Discard

with :

1 Washer NAS1149F0332P Item (106) Discard

1 Clamp NSA5516-06NJ Item (111) Discard

1 Screw NAS1096-3-10 Item (112) Discard

1 Nut NAS1726-3E Item (113) Discard

3 Screw NAS1100E4-36 Item (130) Discard

3 Washer NAS1149C0432R Item (131) Discard

1 Fitting A2627048220400 Item (132) Discard

2 O-Ring NSA8202-6 Item (133) Discard

1 Fitting A2627048221600 Item (134) Discard

(d) Remove the Flow Metering Compact Unit (FMCU), FIN 4034WX.

Refer to Fig. A-GBCAA

1 From FR37.1RH, remove the FMCU, FIN 4034WX (Refer to AMM 26-23-43,

Page Block 401) :

Refer to Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet 02 and Fig. A-GBCAA

Sheet 03

1 Meter-Flow, Compact

Unit

QA07907-01 Item (205) Discard

and

1 Hose Assy G2627007000200 Item (108) Discard

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 165

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@A340-500/600

SERVICE BULLETIN

1 Tube Assy G2627006000200 Item (110) Discard

with :

1 Washer NAS1149F0332P Item (106) Discard

1 Clamp NSA5516-06NJ Item (111) Discard

1 Screw NAS1096-3-10 Item (112) Discard

1 Nut NAS1726-3E Item (113) Discard

3 Screw NAS1100E4-36 Item (130) Discard

3 Washer NAS1149C0432R Item (131) Discard

1 Fitting A2627048220400 Item (132) Discard

2 O-Ring NSA8202-6 Item (133) Discard

1 Fitting A2627048221600 Item (134) Discard

(16) Subtask 265020-831-203-001 - Remove the plumbing installations and placards.

Work Zones and Access Panels

Zone Access/Work location

132 Access Panel 132PM

Work location from Frame 35 to Frame 37.1

Manpower Resources

Manhours 2.50

Minimum number of person 2

Subtask elapsed time 1.25

Skills NON SPECIFIC

References

Fig. A-GBCAA

Removal of the 4 Flow Metering

Compact Units (FMCU), FIN 4031WX,

4032WX, 4033WX and 4034WX, the

related Plumbing Installations and

Placards

Sheet 01

Sheet 02

Sheet 03

(a) Remove the plumbing installations between FR35RH thru FR37.1RH.

Refer to Fig. A-GBCAA

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 166

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1 Between FR35RH and FR36RH, remove :

Refer to Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet 02 and Fig. A-GBCAA

Sheet 03

2 Reducer MS21916D10-4 Item (115) Discard

1 Tube Assy G2627005004400 Item (116) Discard

1 Tee NSA855113-34D Item (117) Discard

1 Tube Assy G2627005004200 Item (118) Discard

1 Hose A2627045200400 Item (209) Discard

with :

2 Washer NAS1149F0332P Item (106) Discard

2 Screw NAS1096-3-10 Item (112) Discard

2 Nut NAS1726-3E Item (113) Discard

2 Clamp NSA5516-18NJ Item (121) Discard

1 Rod End NSA8141-04R Item (135) Discard

1 Nut NAS509-5 Item (136) Discard

1 Rod End NSA8140-04RK Item (137) Discard

2 Lead-Bonding E0090-41-320 Item (138) Discard

1 Bolt NAS1304-12 Item (139) Discard

1 Nut NAS1726-4E Item (104) Discard

1 Washer NAS1149D0432K Item (140) Discard

1 Washer-Lock NSA5355-5CA Item (141) Discard

2 Between FR36RH and FR37RH, remove :

Refer to Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet 02 and Fig. A-GBCAA

Sheet 03

2 Washer NAS1149F0332P Item (106) Discard

2 Screw NAS1096-3-10 Item (112) Discard

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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2 Nut NAS1726-3E Item (113) Discard

1 Tube Assy G2627005004000 Item (120) Discard

2 Clamp NSA5516-18NJ Item (121) Discard

1 Cross NSA855140-22D Item (122) Discard

1 Union MS21902D10 Item (123) Discard

1 Tube Assy G2627005003800 Item (124) Discard

2 Tee NSA855008D10 Item (125) Discard

1 Rod End NSA8141-04R Item (135) Retain

1 Nut NAS509-5 Item (136) Retain

1 Rod End NSA8140-04RK Item (137) Retain

2 Lead-Bonding E0090-41-320 Item (138) Discard

1 Bolt NAS1304-12 Item (139) Discard

1 Nut NAS1726-4E Item (104) Discard

1 Washer NAS1149D0432K Item (140) Discard

1 Washer-Lock NSA5355-5CA Item (141) Discard

1 Tube Assy G2627005006400 Item (142) Discard

1 Hose A2627045200400 Item (209) Retain

2 Hose Assy F2627007100200 Item (210) Retain

3 Between FR37RH and FR37.1RH, remove :

Refer to Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet 02 and Fig. A-GBCAA

Sheet 03

2 Reducer MS21916D10-4 Item (115) Discard

1 Tube Assy G2627005004400 Item (116) Discard

1 Tee NSA855113-34D Item (117) Discard

1 Tube Assy G2627005003400 Item (119) Discard

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 168

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SERVICE BULLETIN

1 Tee NSA855008D10 Item (125) Discard

1 Tube Assy G2627005003600 Item (129) Discard

1 Rod End NSA8141-04R Item (135) Retain

1 Nut NAS509-5 Item (136) Retain

1 Rod End NSA8140-04RK Item (137) Retain

2 Lead-Bonding E0090-41-320 Item (138) Discard

1 Bolt NAS1304-12 Item (139) Discard

1 Nut NAS1726-4E Item (104) Discard

1 Washer NAS1149D0432K Item (140) Discard

1 Washer-Lock NSA5355-5CA Item (141) Discard

1 Hose A2627045200400 Item (209) Retain

(b) Remove the placards between FR35RH thru FR37.1RH.

Refer to Fig. A-GBCAA

1 Between FR35RH and FR36RH, remove the placards 4010WX, 4031WX and

4032WX :

2 Label NSA931025-02F Item (126) Discard

1 Placard G2627004020200 Item (127) Discard

2 Between FR37RH and FR37.1RH, remove the placards 4020WX, 4033WX

and 4034WX :

2 Label NSA931025-02F Item (126) Discard

1 Placard G2627004020400 Item (128) Discard

(17) Subtask 265020-831-204-001 - Remove the brackets and the insulation blankets

between FR35RH thru FR37.1RH.

Work Zones and Access Panels

Zone Access/Work location

132 Work location from Frame 35 to Frame 37.1

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 169

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SERVICE BULLETIN

Manpower Resources

Manhours 3.50

Minimum number of person 2

Subtask elapsed time 1.75

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 25-80-00-000-801

Fig. A-GBDAA

Removal of the Brackets

Sheet 01

Sheet 02

Sheet 03

(a) Remove the insulation blankets in the affected area (Refer to AMM Task

25-80-00-000-801).

(b) Remove the brackets between FR35RH thru FR37.1RH.

Refer to Fig. A-GBDAA

1 Between FR35 and FR36, STGR 29RH, remove :

Refer to Fig. A-GBDAA Sheet 01 and Fig. A-GBDAA Sheet 03

1 Section-T F5397460021800 Item (161) Discard

1 Bracket Assy F5397484500200 Item (162) Discard

2 From FR35RH, STGR31, remove :

Refer to Fig. A-GBDAA Sheet 01 and Fig. A-GBDAA Sheet 03

1 Bracket F5397463611000 Item (163) Discard

3 From FR36RH, STGR31, remove :

Refer to Fig. A-GBDAA Sheet 01 and Fig. A-GBDAA Sheet 03

1 Bracket F5397463610800 Item (164) Discard

4 From FR37RH, STGR31, remove :

Refer to Fig. A-GBDAA Sheet 01 and Fig. A-GBDAA Sheet 03

1 Bracket F5397463611000 Item (163) Discard

5 From FR37.1RH, STGR31, remove :

Refer to Fig. A-GBDAA Sheet 01 and Fig. A-GBDAA Sheet 03

1 Bracket F5397463610800 Item (164) Discard

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 170

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SERVICE BULLETIN

6 From the crossbeam at FR35 at -Y2462, remove :

Refer to Fig. A-GBDAA Sheet 01 and Fig. A-GBDAA Sheet 02

1 Bracket Assy F5397800200000 Item (165) Discard

1 Bracket F5397461823000 Item (166) Discard

7 From the crossbeam at FR36 at -Y2462, remove :

Refer to Fig. A-GBDAA Sheet 01 and Fig. A-GBDAA Sheet 02

1 Bracket Assy F5397800200000 Item (165) Discard

1 Bracket F5397469928000 Item (167) Discard

8 Between FR35RH and FR36RH, remove :

Refer to Fig. A-GBDAA Sheet 01 and Fig. A-GBDAA Sheet 02

1 Strut Assy F5397883300000 Item (168) Discard

(18) Subtask 265020-831-213-001 - Install the brackets, modify the insulation blankets

and close the rivet holes between FR35RH thru FR37.1RH.

Work Zones and Access Panels

Zone Access/Work location

132 Work location from Frame 35 to Frame 37.1

Manpower Resources

Manhours 7.00

Minimum number of person 2

Subtask elapsed time 3.50

Skills NON SPECIFIC

Material necessary to do the job

Kit 265020D02R04

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

170 EN6081D4-09 28 RIVET

171 EN6081D6-14 30 RIVET

252 F5397757020200 2 ANGLE

253 F5397462009600 1 BRACKET

254 F5397462009800 1 BRACKET

281 ABS1577A05 1 BRACKET

282 ABS0787B05B 1 BRACKET

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 171

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References

Aircraft Maintenance Manual (AMM) Task 20-28-00-912-802

Task 25-80-00-200-801

Task 25-80-00-400-801

Fig. A-GBGAA

Installation of the Brackets

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Fig. A-GBDAA

Removal of the Brackets

Sheet 01

Sheet 02

Sheet 03

(a) Install the brackets and close the existing rivet holes.

Refer to Fig. A-GBDAA and Fig. A-GBGAA

1 Between FR35 and FR36, on STGR29RH and STGR30RH, close the rivet

holes in the stringers with :

Refer to Fig. A-GBDAA Sheet 01, Fig. A-GBDAA Sheet 02 and Fig. A-GBDAA

Sheet 03

4 Rivet EN6081D6-14 Item 171

2 On FR35 and FR36, STGR31RH, close the rivet holes in the frames with :

Refer to Fig. A-GBDAA Sheet 01, Fig. A-GBDAA Sheet 02 and Fig. A-GBDAA

Sheet 03

8 Rivet EN6081D6-14 Item 171

3 Between FR36 and FR37, on STGR30RH, install this bracket on the stringer :

Refer to Fig. A-GBGAA Sheet 01 and Fig. A-GBGAA Sheet 02

1 Angle-Bonding F5397757020200 Item 252

with :

3 Rivet EN6081D4-09 Item 170

NOTE: Do the electrical bonding (Refer to AMM Task

20-28-00-912-802)

4 On FR37 and FR37.1, STGR31RH, close the rivet holes in the frames with :

Refer to Fig. A-GBDAA Sheet 01,Fig. A-GBDAA Sheet 02 and Fig. A-GBDAA

Sheet 03

8 Rivet EN6081D6-14 Item 171

5 On FR37, between STGR31RH and STGR32RH, install this bracket :

Refer to Fig. A-GBGAA Sheet 01 and Fig. A-GBGAA Sheet 02

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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1 Bracket Assy F5397462009600 Item 253

with :

4 Rivet EN6081D6-14 Item 171

NOTE: Do the electrical bonding (Refer to AMM Task

20-28-00-912-802)

NOTE: Existing rivet spacing must be used.

6 Between FR37 and FR37.1, on STGR30RH, install this bracket :

Refer to Fig. A-GBGAA Sheet 01 and Fig. A-GBGAA Sheet 02

1 Angle-Bonding F5397757020200 Item 252

with :

3 Rivet EN6081D4-09 Item 170

7 Between FR37 and FR37.1, on STGR30RH, install this bracket :

Refer to Fig. A-GBGAA Sheet 01 and Fig. A-GBGAA Sheet 03

1 Bracket ABS1577A05 Item 281

with :

3 Rivet EN6081D4-09 Item 170

NOTE: Do the electrical bonding (Refer to AMM Task

20-28-00-912-802)

8 On FR37.1, between STGR31RH and STGR32RH, install this bracket :

Refer to Fig. A-GBGAA Sheet 01 and Fig. A-GBGAA Sheet 02

1 Bracket Assy F5397462009800 Item 254

with :

4 Rivet EN6081D6-14 Item 171

NOTE: Do the electrical bonding (Refer to AMM Task

20-28-00-912-802)

NOTE: Existing rivet spacing must be used.

9 On the crossbeam at FR35, between -Y1959 and -Y2462, close the rivet holes

in the crossbeam with :

Refer to Fig. A-GBDAA Sheet 01, Fig. A-GBDAA Sheet 02 and Fig. A-GBDAA

Sheet 03

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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10 Rivet EN6081D4-09 Item 170

10 On the crossbeam at FR36, outboard of -Y2462, close the rivet holes in the

crossbeam with :

Refer to Fig. A-GBDAA Sheet 01, Fig. A-GBDAA Sheet 02 and Fig. A-GBDAA

Sheet 03

9 Rivet EN6081D4-09 Item 170

11 On the crossbeam at FR36, outboard of -Y2462, install this bracket :

Refer to Fig. A-GBGAA Sheet 01 and Fig. A-GBGAA Sheet 03

1 Bracket-Z ABS0787B05B Item 282

with :

2 Rivet EN6081D6-14 Item 171

NOTE: Do the electrical bonding (Refer to AMM Task

20-28-00-912-802)

(b) Between FR36 thru FR37.1RH modify the insulation blankets in the affected area.

1 Adapt the insulation blankets for the new locations of brackets (Refer to AMM

Task 25-80-00-200-801).

(c) Install the modified insulation in the affected area (Refer to AMM Task

25-80-00-400-801).

(19) Subtask 265020-831-216-001 - Modify the equipment and the wiring of the

FMCU/FMS outlet pressure switches 4031WX, 4032WX, 4033WX, 4034WX, 4016WX

and 4018WX of the fire extinguishing bottles Nos. 2 and 3.

Work Zones and Access Panels

Zone Access/Work location

132 Work location from Frame 35 to Frame 37.1

200 Work location Electrical panel 801VU

Manpower Resources

Manhours 1.50

Minimum number of person 2

Subtask elapsed time 0.75

Skills ELECTRICAL

Material necessary to do the job

Kit 265020D03R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

173 G9237018016600 1 PLCRDSET

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

174 NSA935401-04 8 TIE

175 NSA935401-05 15 TIE

References

Process and Material Specification

(PMS)

Process and Material Specification (PMS)

01-07-10

Fig. A-GWAAA

Modification of the Wiring of the

FMCU/FMS Outlet Pressure Switches

4031WX, 4032WX, 4033WX, 4034WX,

4016WX and 4018WX

Sheet 01

Sheet 02

Fig. A-GHAAA

Hook-up Chart

Sheet 01

Fig. A-GBLAA

Stowage of the Electrical Wires of the

Connectors 4031WX-A, 4032WX-A

4011WX-A, 4012WX-A and 4013WX-A

Sheet 01

Sheet 02

Sheet 03

Sheet 04

(a) Modify the wiring of the FMCU/FMS outlet pressure switches.

1 Disconnect these electrical wires from the connectors 4031WX-A and

4032WX-A.

Refer to Fig. A-GWAAA Sheet 01 (Wiring)

Refer to Fig. A-GHAAA Sheet 01 (Hook-up Chart), LINES 1, 2, 3 and 4

2 Remove the connectors 4031WX-A and 4032WX-A and discard.

Refer to Fig. A-GBLAA Sheet 01

Remove :

2 Connector-Plug EN2997KE60803BN Item (265) Discard

and remove the following attachment parts :

4 Screw NAS1801-08-7 Item (267) Discard

2 Nut MS21042-08 Item (268) Discard

4 Washer NAS1149CN816R Item (269) Discard

2 Clamp MS21919WCH8 Item (270) Retain

2 Screw NAS1801-08-23 Item (271) Discard

2 Lanyard DAN80-3-150 Item (273) Discard

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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2 Sleeve-Protective NSA935809-09 Item (274) Discard

5 Cable Mount Item (277) Retain

3 Disconnect these electrical wires from the connectors 4033WX-A and

4034WX-A.

Refer to Fig. A-GWAAA Sheet 01 (Wiring)

Refer to Fig. A-GHAAA Sheet 01 (Hook-up Chart), LINES 5, 6, 7 and 8

4 Reroute and install the electrical wires :

Refer to Fig. A-GWAAA Sheet 02 (Wiring)

Refer to Fig. A-GHAAA Sheet 01 (Hook-up Chart), LINES 13, 14, 15 and 16

with :

15 Tie-Cable NSA935401-05 Item 175

and attach the placards, identified 4016WX-A, 4018WX-A and the SB/MOD

placards :

1 Placardset G9237018016600 Item 173

with :

8 Tie-Cable NSA935401-04 Item 174

(20) Subtask 265020-831-209-001 - Modify the equipment and the wiring of the fire

extinguishing bottle No. 3 (AFT), 4020WX, and relocated fire extinguishing bottle

No. 2 (AFT), 4010WX.

Work Zones and Access Panels

Zone Access/Work location

132 Work location from Frame 35 to Frame 37.1

200 Work location Electrical panel 801VU

Electrical panel 802VU

Manpower Resources

Manhours 1.00

Minimum number of person 2

Subtask elapsed time 1.00

Skills ELECTRICAL

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 176

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Material necessary to do the job

Kit 265020D03R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

173 G9237018016600 1 PLCRDSET

174 NSA935401-04 12 TIE

175 NSA935401-05 15 TIE

176 EN3155-003F1614 2 CONTACT

References

Fig. A-GWBAA

Modification of the Wiring of the Fire

Extinguishing Bottle No. 3 (previously

AFT), 4020WX, and relocated Fire

Extinguishing Bottle No. 2 (now AFT),

4010WX

Sheet 01

Sheet 02

Fig. A-GHBAA

Hook-up Chart

Sheet 01

(a) Modify the wiring of the cartridges and the pressure switch of the fire extinguishing

bottle (AFT), 4020WX (4010WX)

1 Disconnect these electrical wires from the connector 2625VC-A.

Refer to Fig. A-GWBAA Sheet 01 (Wiring)

Refer to Fig. A-GHBAA Sheet 01 (Hook-up Chart), LINES 1 and 11, END 2

2 Reroute and install the electrical wires on the connector 2511VC-A.

Refer to Fig. A-GWBAA Sheet 02 (Wiring)

Refer to Fig. A-GHBAA Sheet 01 (Hook-up Chart), LINES 2 and 12, END 2

3 Disconnect these electrical wires from the connector 2636VC-A.

Refer to Fig. A-GWBAA Sheet 01 (Wiring)

Refer to Fig. A-GHBAA Sheet 01 (Hook-up Chart), LINES 5 and 15, END 2

NOTE: Cut off the contacts directly behind the contacts.

4 Reroute and install the electrical wires on the connector 2508VC-A.

Refer to Fig. A-GWBAA Sheet 02 (Wiring)

Refer to Fig. A-GHBAA Sheet 01 (Hook-up Chart), LINES 6 and 16, END 2

with :

2 Contact-Socket EN3155-003F1614 Item 176

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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5 Disconnect the electrical wire from the connector 2044VC-A.

Refer to Fig. A-GWBAA Sheet 01 (Wiring)

Refer to Fig. A-GHBAA Sheet 01 (Hook-up Chart), LINE 23, END 2

6 Reroute and install the electrical wire on the connector 2016VC-A.

Refer to Fig. A-GWBAA Sheet 02 (Wiring)

Refer to Fig. A-GHBAA Sheet 01 (Hook-up Chart), LINE 24, END 2

7 Attach the placards, identified 4011WX-A, 4012WX-A, 4013WX-A and the

SB/MOD placards :

1 Placardset G9237018016600 Item 173

with :

12 Tie-Cable NSA935401-04 Item 174

8 Install the tie-cables on the wire harnesses :

15 Tie-Cable NSA935401-05 Item 175

NOTE: For the stowage position of the connectors 4011WX-A,

4012WX-A, 4013WX-A, 4031WX-A and 4032WX-A, refer to

(22) Subtask 265020-831-218-001.

(21) Subtask 265020-831-210-001 - Modify the Equipment and the Wiring of the

previous Fire Extinguishing Bottle No. 2 (FWD), 4010WX.

Work Zones and Access Panels

Zone Access/Work location

132 Work location from Frame 35 to Frame 36

200 Work location Electrical panel 801VU

Electrical panel 802VU

Manpower Resources

Manhours 1.50

Minimum number of person 1

Subtask elapsed time 1.50

Skills ELECTRICAL

References

Fig. A-GWCAA

Modification of the Wiring of the Fire

Extinguishing Bottle No. 2 (FWD),

4010WX

Sheet 01

Sheet 02

Fig. A-GHCAA

Hook-up Chart

Sheet 01

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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References

Fig. A-GBLAA

Stowage of the Electrical Wires of the

Connectors 4031WX-A, 4032WX-A

4011WX-A, 4012WX-A and 4013WX-A

Sheet 01

Sheet 02

Sheet 03

Sheet 04

(a) Modify the wiring of the previous fire extinguishing bottle No. 2 (FWD), 4010WX.

1 Disconnect these electrical wires from the connectors 4011WX-A, 4012WX-A

and 4013WX-A.

Refer to Fig. A-GWCAA Sheet 01 (Wiring)

Refer to Fig. A-GHCAA Sheet 01 (Hook-up Chart), LINES 1, 5, 11, 15 and 23

Refer to Fig. A-GHCAA Sheet 01 (Hook-up Chart), LINES 3, 7, 9, 13, 17, 19,

21, END 1

2 Remove the connectors 4011WX-A, 4012WX-A and 4013WX-A and discard.

Refer to Fig. A-GBLAA Sheet 01

Remove :

2 Connector EN2997KE61005BN Item (264) Discard

1 Connector-Plug EN2997KE60803BN Item (265) Discard

and remove the following attachment parts :

1 Tie-Cable NSA935401-03 Item (266) Discard

5 Screw NAS1801-08-7 Item (267) Discard

2 Nut MS21042-08 Item (268) Discard

4 Washer NAS1149CN816R Item (269) Discard

2 Clamp MS21919WCH8 Item (270) Discard

1 Screw NAS1801-08-29 Item (272) Discard

2 Lanyard DAN80-3-150 Item (273) Discard

2 Sleeve-Protective NSA935809-09 Item (274) Discard

2 Cable Mount Item (277) Retain

NOTE: For the stowage position of the connectors 4011WX-A,

4012WX-A, 4013WX-A, 4031WX-A and 4032WX-A, refer to

(22) Subtask 265020-831-218-001.

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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(22) Subtask 265020-831-218-001 - Put the electrical wires of the connectors 4031WX-A,

4032WX-A 4011WX-A, 4012WX-A and 4013WX-A in a stowage position.

Work Zones and Access Panels

Zone Access/Work location

132 Work location from Frame 35 to Frame 37.1

Manpower Resources

Manhours 2.50

Minimum number of person 1

Subtask elapsed time 2.50

Skills ELECTRICAL

Material necessary to do the job

Kit 265020D03R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

173 G9237018016600 1 PLCRDSET

177 NSA936603CC0100 23 CAP

Kit 265020D05R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

266 NSA935401-03 25 TIE

269 NAS1149CN816R 4 WASHER

270 MS21919WCH8 4 CLAMP

271 NAS1801-08-23 2 SCREW

272 NAS1801-08-29 1 SCREW

274 NSA935809-09 4 SLEEVE

275 NAS1801-08-25 1 SCREW

References

Fig. A-GBLAA

Stowage of the Electrical Wires of the

Connectors 4031WX-A, 4032WX-A

4011WX-A, 4012WX-A and 4013WX-A

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Fig. A-GHAAA

Hook-up Chart

Sheet 01

Fig. A-GHCAA

Hook-up Chart

Sheet 01

Fig. A-GWAAA

Modification of the Wiring of the

FMCU/FMS Outlet Pressure Switches

4031WX, 4032WX, 4033WX, 4034WX,

4016WX and 4018WX

Sheet 01

Sheet 02

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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References

Fig. A-GWCAA

Modification of the Wiring of the Fire

Extinguishing Bottle No. 2 (FWD),

4010WX

Sheet 01

Sheet 02

(a) Put the electrical wires of the connectors 4031WX-A and 4032WX-A in a stowage

position.

1 Put the electrical wires in a stowage position.

Refer to Fig. A-GBLAA Sheet 01, Fig. A-GBLAA Sheet 02, Fig. A-GBLAA

Sheet 03 and Fig. A-GBLAA Sheet 04

Refer to Fig. A-GWAAA Sheet 02 (Wiring)

Refer toFig. A-GHAAA Sheet 01 (Hook-up Chart), LINES 9, 10, 11 and 12

with :

6 Cap NSA936603CC0100 Item 177

NOTE: Do not cut off the contacts.

Attach the electrical wires in a stowage position.

with :

2 Washer NAS1149CN816R Item 269

2 Clamp MS21919WCH8 Item 270

2 Clamp MS21919WCH8 Item (270) Retained at

removal

1 Screw NAS1801-08-23 Item 271

2 Sleeve-Protective NSA935809-09 Item 274

1 Screw NAS1801-08-25 Item 275

5 Cable Mount Item (277) Retained at

removal

20 Tie-Cable NSA935401-03 Item 266

(b) Put the electrical wires of the connectors 4011WX-A, 4012WX-A and 4013WX-A in

a stowage position.

1 Put the electrical wires in a stowage position.

Refer to Fig. A-GBLAA Sheet 01, Fig. A-GBLAA Sheet 02, Fig. A-GBLAA

Sheet 03 and Fig. A-GBLAA Sheet 04

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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SERVICE BULLETIN

Refer to Fig. A-GWCAA Sheet 02 (Wiring)

Refer to Fig. A-GHCAA Sheet 01 (Hook-up Chart), LINES 2, 6, 12, 16 and 24

Refer to Fig. A-GHCAA Sheet 01 (Hook-up Chart), LINES 4, 8, 10, 14, 18, 20

and 22, END 1

with :

17 Cap NSA936603CC0100 Item 177

NOTE: Do not cut off the contacts.

Attach the electrical wires in a stowage position.

with :

2 Washer NAS1149CN816R Item 269

2 Clamp MS21919WCH8 Item 270

1 Screw NAS1801-08-23 Item 271

1 Screw NAS1801-08-29 Item 272

2 Sleeve-Protective NSA935809-09 Item 274

2 Cable Mount Item (277) Retained at

removal

and attach the SB/MOD placards :

1 Placardset G9237018016600 Item 173

with :

5 Tie-Cable NSA935401-03 Item 266

(23) Subtask 265020-831-208-001 - Adapt the plumbing installation.

Work Zones and Access Panels

Zone Access/Work location

132 Work location from Frame 36 to Frame 37

Manpower Resources

Manhours 3.00

Minimum number of person 2

Subtask elapsed time 1.50

Skills NON SPECIFIC

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 182

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SERVICE BULLETIN

Material necessary to do the job

Kit 265020D04R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

113 NAS1726-3E 2 NUT

121 NSA5516A18NJ 2 CLAMP

125 NSA855008D10 1 TEE

144 NAS1149C0332R 2 WASHER

155 NSA5527-03-03 2 SPACER

157 NAS1801-3-12 2 SCREW

158 NSA855006D10 2 UNION

251 G2627005013000 1 TUBE

253 G2627005002000 1 TUBE

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Internal Polyurethane

Varnish

07-017 As required

Solvent General Purpose 11-026 As required

Low Voc Anti-Corrosion

Primer

16-006F As required

Lint-Free Cotton Cloth 19-003 As required

Standard tool TOOLD01

ITEM TOOL N ̊ TOOL NAME QTY SEE

NOTES

D12102C07-02 PERMASWAGE Repair

Kit D12000 Series

1

References

Aircraft Maintenance Manual (AMM) 20-23-11, Page Block 201

Fig. A-GBEAA

Adaption of the Plumbing Installation

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Fig. A-GBFAA

Installation of the U-Section and the

Flow Metering System (FMS)

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

(a) Remove the fire extinguishing tubes from FR36 and FR37.

Refer to Fig. A-GBEAA

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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SERVICE BULLETIN

1 Remove and discard these items from FR36RH :

Refer to Fig. A-GBEAA Sheet 01, Fig. A-GBEAA Sheet 02 and Fig. A-GBEAA

Sheet 04

1 Nut NAS1726-3E Item (113) Discard

1 Clamp NSA5516-18NJ Item (121) Discard

1 Washer NAS1149C0332R Item (144) Discard

1 Spacer NSA5527-03-03 Item (155) Discard

1 Screw NAS1096-3-14 Item (157) Discard

2 Cut the fire extinguishing tube, Item (250), at the position shown in Fig. AGBEAA Sheet 02 (Refer to AMM 20-23-11, Page Block 201).

3 Remove the fire extinguishing tube, Item (250), partly between the cut and the

outboard X-connection fitting :

1 Tube Assy, partly G2627005013000 Item (250) Discard

4 Deburr the remaining tube, Item (250), (Refer to AMM 20-23-11, Page Block

201).

5 Clean the remaining tube, Item (250), with :

Solvent General

Purpose

11-026 As required

and

Lint-Free Cotton

Cloth

19-003 As required

6 Remove and discard these items from FR37RH :

Refer to Fig. A-GBEAA Sheet 01, Fig. A-GBEAA Sheet 02 and Fig. A-GBEAA

Sheet 04

1 Nut NAS1726-3E Item (113) Discard

1 Clamp NSA5516-18NJ Item (121) Discard

1 Washer NAS1149C0332R Item (144) Discard

1 Spacer NSA5527-03-03 Item (155) Discard

1 Screw NAS1096-3-14 Item (157) Discard

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 184

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SERVICE BULLETIN

7 Cut the fire extinguishing tube, Item (252), at the position shown in Fig. AGBEAA Sheet 02 (Refer to AMM 20-23-11, Page Block 201).

8 Remove the fire extinguishing tube, Item (252), partly between the cut and the

outboard T-connection fitting :

1 Tube Assy, partly G2627005002000 Item (252) Discard

1 Tee NSA855008D10 Item (125) Discard

9 Deburr the remaining tube, Item (252), (Refer to AMM 20-23-11, Page Block

201).

10 Clean the remaining tube, Item (252), with :

Solvent General

Purpose

11-026 As required

and

Lint-Free Cotton

Cloth

19-003 As required

(b) Install the fire extinguishing tubes on FR36 and FR37.

CAUTION: BEFORE YOU CONNECT THE FIRE EXTINGUISHING TUBES

WITH THE PERMASWAGE TOOL, MAKE SURE THAT THE FIRE

EXTINGUISHING TUBES ARE INSTALLED STRESS-FREE IN

THEIR CLAMPS.

CAUTION: DO NOT BEND THE TUBE WHEN YOU INSTALL IT. IF THE

TUBE IS BENT, IT CAN BECOME DAMAGED.

CAUTION: IF YOU USE DUST CAPS FOR THE CONTAMINATION

PROTECTION OF OPEN LINES, ALWAYS BE SURE TO

INSTALL THE CAPS AROUND THE TUBE ENDS AND NOT IN

THE TUBE ENDS. THERE CAN BE BLOCKAGE OF THE FLOW

THROUGH THE TUBES IF THESE TUBES ARE INSTALLED

ACCIDENTALLY WITH DUST CAPS IN THE TUBE ENDS.

NOTE: The fire extinguishing tubes must be installed with their related

clamps.

Refer to Fig. A-GBEAA

1 Install temporarily, Item 233, before install the other tubes.

Refer to Fig. A-GBFAA Sheet 01

2 Install the tube, Item 251, at FR36RH.

Refer to Fig. A-GBEAA Sheet 01, Fig. A-GBEAA Sheet 02 and Fig. A-GBEAA

Sheet 03

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 185

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SERVICE BULLETIN

1 Tube Assy G2627005013000 Item 251

with :

1 Union NSA855006D10 Item 158

3 Connect the fire extinguishing tubes, Item (250), and Item 251, with the union,

Item 158, (Refer to AMM 20-23-11, Page Block 201).

D12102C07-02 PERMASWAGE

Repair Kit D12000

Series

1

NOTE: Use these swaging tools of the D12000 series :

- Head assembly D12210-56 with power unit D12010-52.

NOTE: The surface protection on both ends of the pipes must be

removed on a length of 43mm (1.692in.).

4 After the installation of the union, Item 158, perform surface protection with :

Low Voc AntiCorrosion Primer16-006F As required

and

Internal

Polyurethane

Varnish

07-017 As required

5 Install the clamp, Item 121, at FR36RH.

Fig. A-GBEAA Sheet 01, Fig. A-GBEAA Sheet 02 and Fig. A-GBEAA Sheet

03

1 Clamp NSA5516A18NJ Item 121

with :

1 Nut NAS1726-3E Item 113

1 Washer NAS1149C0332R Item 144

1 Spacer NSA5527-03-03 Item 155

1 Screw NAS1801-3-12 Item 157

6 Install temporarily, Item 234 and 238, before install the other tubes.

Refer to Fig. A-GBFAA Sheet 01

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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SERVICE BULLETIN

7 Install the tube, Item 253, at FR37RH.

Refer to Fig. A-GBEAA Sheet 01, Fig. A-GBEAA Sheet 02 and Fig. A-GBEAA

Sheet 03

1 Tube Assy G2627005002000 Item 253

with :

1 Tee NSA855008D10 Item 125

1 Union NSA855006D10 Item 158

8 Connect the fire extinguishing tubes, Item (252), and Item 253, with the union,

Item 158, and on the other end with the T-fitting, Item 125 (Refer to AMM

20-23-11, Page Block 201).

NOTE: Use these swaging tools of the D12000 series :

- Head assembly D12210-56 with power unit D12010-52.

NOTE: The surface protection on the ends of the pipes must be

removed on a length of 43mm (1.692in.).

9 After the installation of the tee-fitting, Item 125, and the union, Item 158,

perform surface protection with :

Low Voc AntiCorrosion Primer16-006F As required

and

Internal

Polyurethane

Varnish

07-017 As required

10 Install the clamp, Item 121, at FR37RH.

Fig. A-GBEAA Sheet 01, Fig. A-GBEAA Sheet 02 and Fig. A-GBEAA Sheet

03

1 Clamp NSA5516A18NJ Item 121

with :

1 Nut NAS1726-3E Item 113

1 Washer NAS1149C0332R Item 144

1 Spacer NSA5527-03-03 Item 155

1 Screw NAS1801-3-12 Item 157

11 Tighten all connections of the installed fire extinguishing tubes.

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 187

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SERVICE BULLETIN

(24) Subtask 265020-831-215-001 - Install the U-section.

Work Zones and Access Panels

Zone Access/Work location

132 Work location from Frame 37 to Frame 37.1

Manpower Resources

Manhours 1.00

Minimum number of person 2

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 265020D04R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

106 NAS1149F0332P 2 WASHER

143 NAS1801-3-8 4 SCREW

144 NAS1149C0332R 5 WASHER

145 NAS1801-3-7 3 SCREW

212 G2627008001400 1 SECTION

213 F2627008100000 1 BRACKET

220 E0090-10-135NN 1 LEAD

References

Aircraft Maintenance Manual (AMM) 20-28-00, Page Block 201

Fig. A-GBFAA

Installation of the U-Section and the

Flow Metering System (FMS)

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

(a) Install the U-section between FR37RH and FR37.1.

Refer to Fig. A-GBFAA

1 Between FR37RH and FR37.1RH, install :

Refer to Fig. A-GBFAA Sheet 03, Fig. A-GBFAA Sheet 05 and Fig. A-GBFAA

Sheet 06

1 U-section G2627008001400 Item 212

1 Bracket F2627008100000 Item 213

1 Lead-Bonding E0090-10-135NN Item 220

with :

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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SERVICE BULLETIN

2 Washer NAS1149F0332P Item 106

4 Screw NAS1801-3-8 Item 143

5 Washer NAS1149C0332R Item 144

3 Screw NAS1801-3-7 Item 145

NOTE (01): For the installation of the bolt (Refer to AMM 20-28-00, Page

Block 201).

NOTE (02): Seal the bonding connection by overlapping application and

identify the bonding connection by overlapping application with

blue dyed protective coating.

(25) Subtask 265020-831-217-001 - Install the Flow Metering Systems (FMS) for the Fire

Ext. Bottles No. 1 and No. 2 on the U-section.

Work Zones and Access Panels

Zone Access/Work location

132 Work location from Frame 37 to Frame 37.1

Manpower Resources

Manhours 4.00

Minimum number of person 2

Subtask elapsed time 2.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 265020D04R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

104 NAS1726-4E 2 NUT

106 NAS1149F0332P 6 WASHER

113 NAS1726-3E 3 NUT

121 NSA5516A18NJ 2 CLAMP

132 A2627048220400 6 FITTING

133 NSA8202-6 8 ORING

134 A2627048221600 2 FITTING

139 NAS1304-12 2 BOLT

140 NAS1149D0432K 10 WASHER

141 NSA5355-5CA 2 WASHER

143 NAS1801-3-8 6 SCREW

144 NAS1149C0332R 6 WASHER

145 NAS1801-3-7 4 SCREW

146 NAS1100E4-34 6 SCREW

147 A2627048920000 2 WASHER

148 NSA5516A06NJ 4 CLAMP

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

152 E0090-10-320NN 2 LEAD

153 E0090-10-350NN 2 LEAD

159 NAS1801-3-10 2 SCREW

160 MS21103-4 2 CLAMP

219 G2627006001000 1 TUBE

221 G2627006000800 1 TUBE

222 G2627006001800 1 TUBE

223 F2627006003600 1 TUBE

224 A2627048220200 2 RESTRCTR

225 F2627006001400 1 TUBE

226 F2627006000000 1 TUBE

227 F2627007200000 1 HOSE

228 F2627007200200 1 HOSE

229 G2627006002000 1 TUBE

230 G2627006001200 1 TUBE

231 G2627006001400 1 TUBE

232 G2627006001600 1 TUBE

233 NSA855140-22D 1 CROSS

234 G2627005013200 1 TUBE

235 MS21902W10 1 UNION

236 A2627045107800 1 TUBE

237 NSA855113-34D 1 TEE

238 G2627005003400 1 TUBE

239 MS21916W10-4 2 REDUCER

Component COMPD01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

LN9424A100 As required WIRE

Equipment BFEZ04

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

214 QA06753-03 2 FILTER

215 E61751-00-0001 2 REDUCER

216 TP0714033 2 SWITCH

217 HTE400115 2 VALVE

References

Aircraft Maintenance Manual (AMM) Task 20-28-00-912-802

Fig. A-GBFAA

Installation of the U-Section and the

Flow Metering System (FMS)

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 190

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SERVICE BULLETIN

(a) Install the Halon Filter, FIN 5010WE, for Fire Ext. Bottle No. 1.

Refer to Fig. A-GBFAA

1 On the U-section, between FR37RH and FR37.1RH, install :

Refer to Fig. A-GBFAA Sheet 01, Fig. A-GBFAA Sheet 03 and Fig. A-GBFAA

Sheet 04

1 Filter-Halon QA06753-03 Item 214

NOTE: See NOTE 03

with :

3 Washer NAS1149D0432K Item 140

3 Screw NAS1100E4-34 Item 146

and

2 O-Ring NSA8202-6 Item 133

1 Fitting A2627048221600 Item 134

NOTE: See NOTE 03

1 Fitting A2627048220400 Item 132

NOTE: See NOTE 03

2 Secure the fittings, Items 132 and 134, with :

As

required

Wire-Lock LN9424A100

3 On the fitting, Item 132, install :

1 Hose Assy F2627007200000 Item 227

NOTE (03): No lubrication on this item.

(b) Install the Pressure Reducer, FIN 5014WE, for Fire Ext. Bottle No. 1.

1 On the U-section, between FR37RH and FR37.1RH, install :

Refer to Fig. A-GBFAA Sheet 01, Fig. A-GBFAA Sheet 03 and Fig. A-GBFAA

Sheet 04

1 Reducer-Pressure E61751-00-0001 Item 215

NOTE: See NOTE 03

with :

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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SERVICE BULLETIN

1 Washer-Tab A2627048920000 Item 147

2 Fitting A2627048220400 Item 132

NOTE: See NOTE 03

2 O-Ring NSA8202-6 Item 133

2 Secure the fittings, Item 132, with :

As

required

Wire-Lock LN9424A100

NOTE (03): No lubrication on this item.

(c) Install the Pressure Switch, FIN 4016WX, for Fire Ext. Bottle No. 1.

1 On the pressure reducer 5014WE, between FR37RH and FR37.1RH, install :

Refer to Fig. A-GBFAA Sheet 01, Fig. A-GBFAA Sheet 03, Fig. A-GBFAA

Sheet 04 and Fig. A-GBFAA Sheet 05

1 Tube Assy G2627006000800 Item 221

with :

1 Washer NAS1149C0332R Item 144

1 Screw NAS1801-3-7 Item 145

1 Clamp NSA5516A06NJ Item 148

and

1 Switch-Pressure TP0714033 Item 216

NOTE: See NOTE 03

2 On the pressure switch, Item 216, install :

1 Tube Assy G2627006001800 Item 222

with :

1 Washer NAS1149F0332P Item 106

1 SCREW NAS1801-3-10 Item 159

1 CLAMP MS21103-4 Item 160

NOTE (03): No lubrication on this item.

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 192

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SERVICE BULLETIN

(d) Install the Check Valve, FIN 5016WE, for Fire Ext. Bottle No. 1.

1 On the pressure reducer 5014WE, between FR37RH and FR37.1RH, install :

Refer to Fig. A-GBFAA Sheet 01, Fig. A-GBFAA Sheet 03 and Fig. A-GBFAA

Sheet 05

1 Tube Assy F2627006003600 Item 223

1 Restrictor A2627048220200 Item 224

1 Tube Assy F2627006001400 Item 225

and

1 Valve-Nonreturn HTE400115 Item 217

NOTE: See NOTE 03

2 On the check valve, Item 217, install :

1 Tube Assy F2627006000000 Item 226

with :

1 Washer NAS1149C0332R Item 144

1 Screw NAS1801-3-7 Item 145

1 Clamp NSA5516A06NJ Item 148

NOTE (03): No lubrication on this item.

(e) Install the Halon Filter, FIN 5011WE, for Fire Ext. Bottle No. 2.

Refer to Fig. A-GBFAA

1 On the U-section, between FR37RH and FR37.1RH, install :

Refer to Fig. A-GBFAA Sheet 01, Fig. A-GBFAA Sheet 03 and Fig. A-GBFAA

Sheet 04

1 Filter-Halon QA06753-03 Item 214

NOTE: See NOTE 03

with :

3 Washer NAS1149D0432K Item 140

3 Screw NAS1100E4-34 Item 146

and

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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SERVICE BULLETIN

2 O-Ring NSA8202-6 Item 133

1 Fitting A2627048221600 Item 134

NOTE: See NOTE 03

1 Fitting A2627048220400 Item 132

NOTE: See NOTE 03

2 Secure the fittings, Items 132 and 134, with :

As

required

Wire-Lock LN9424A100

3 On the fitting, Item 132, install :

1 Hose Assy F2627007200200 Item 228

NOTE: See NOTE 03

NOTE (03): No lubrication on this item.

(f) Install the Pressure Reducer, FIN 5015WE, for Fire Ext. Bottle No. 2.

1 On the U-section, between FR37RH and FR37.1RH, install :

Refer to Fig. A-GBFAA Sheet 01, Fig. A-GBFAA Sheet 03 and Fig. A-GBFAA

Sheet 04

1 Reducer-Pressure E61751-00-0001 Item 215

NOTE: See NOTE 03

with :

1 Washer-Tab A2627048920000 Item 147

2 Fitting A2627048220400 Item 132

NOTE: See NOTE 03

2 O-Ring NSA8202-6 Item 133

2 Secure the fittings, Item 132, with :

As

required

Wire-Lock LN9424A100

NOTE (03): No lubrication on this item.

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 194

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SERVICE BULLETIN

(g) Install the Pressure Switch, FIN 4018WX, for Fire Ext. Bottle No. 2

1 On the pressure reducer 5015WE, between FR37RH and FR37.1RH, install :

Refer to Fig. A-GBFAA Sheet 01, Fig. A-GBFAA Sheet 03 and Fig. A-GBFAA

Sheet 04

1 Tube Assy G2627006001000 Item 219

with :

1 Washer NAS1149C0332R Item 144

1 Screw NAS1801-3-7 Item 145

1 Clamp NSA5516A06NJ Item 148

and

1 Switch-Pressure TP0714033 Item 216

NOTE: See NOTE 03

2 On the pressure switch, Item 216, install :

1 Tube Assy G2627006002000 Item 229

with :

1 Washer NAS1149F0332P Item 106

1 SCREW NAS1801-3-10 Item 159

1 CLAMP MS21103-4 Item 160

NOTE (03): No lubrication on this item.

(h) Install the Check Valve, FIN 5017WE, for Fire Ext. Bottle No. 2

1 On the pressure reducer 5015WE, between FR37RH and FR37.1RH, install :

Refer to Fig. A-GBFAA Sheet 01, Fig. A-GBFAA Sheet 03 and Fig. A-GBFAA

Sheet 05

1 Tube Assy G2627006001200 Item 230

1 Restrictor A2627048220200 Item 224

1 Tube Assy G2627006001400 Item 231

and

1 Valve-Nonreturn HTE400115 Item 217

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 195

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SERVICE BULLETIN

NOTE: See NOTE 03

2 On the check valve, Item 217, install :

1 Tube Assy G2627006001600 Item 232

with :

1 Washer NAS1149C0332R Item 144

1 Screw NAS1801-3-7 Item 145

1 Clamp NSA5516A06NJ Item 148

1 Nut NAS1726-3E Item 113

NOTE (03): No lubrication on this item.

(i) Install the new plumbing and rod ends between FR36RH and FR37.1

1 Between FR36RH and FR37.1, install the rod ends :

Refer to Fig. A-GBFAA Sheet 01 and Fig. A-GBFAA Sheet 02

2 Rod End NSA8141-04R Item (135) Retained at

removal

2 Rod End NSA8140-04RK Item (137) Retained at

removal

with :

2 Nut NAS1726-4E Item 104

2 BOLT NAS1304-12 Item 139

4 Washer NAS1149D0432K Item 140

2 Nut NAS509-5 Item (136) Retained at

removal

2 Washer-Lock NSA5355-5CA Item 141

and

2 Lead-Bonding E0090-10-320NN Item 152

2 Lead-Bonding E0090-10-350NN Item 153

with :

4 Washer NAS1149F0332P Item 106

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 196

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SERVICE BULLETIN

4 Screw NAS1801-3-8 Item 143

NOTE: Do the electrical bonding (Refer to AMM Task

20-28-00-912-802)

2 Between FR36RH and FR37.1, install the plumbing :

Refer to Fig. A-GBFAA Sheet 01, Fig. A-GBFAA Sheet 02 and Fig. A-GBFAA

Sheet 03

2 Hose A2627045200400 Item (209) Retained at

removal

2 Hose Assy F2627007100200 Item (210) Retained at

removal

1 Cross NSA855140-22D Item 233

1 Tube Assy G2627005013200 Item 234

1 Union MS21902W10 Item 235

with :

2 Screw NAS1801-3-8 Item 143

2 Washer NAS1149C0332R Item 144

2 Nut NAS1726-3E Item 113

2 Clamp NSA5516A18NJ Item 121

and

1 Tube Assy A2627045107800 Item 236

1 Tee NSA855113-34D Item 237

1 Tube Assy G2627005003400 Item 238

2 Reducer MS21916W10-4 Item 239

(26) Subtask 265020-831-211-002 - Install the Fire Extinguishing Bottles 4005WX and

4010WX.

Work Zones and Access Panels

Zone Access/Work location

132 Access Panel 132PM

Work location from Frame 35 to Frame 37.1

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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Manpower Resources

Manhours 2.00

Minimum number of person 2

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 265020D04R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

100 NAS1726-5E 8 NUT

101 NAS1305-2 8 BOLT

103 NAS1304-9 2 BOLT

104 NAS1726-4E 2 NUT

105 NAS563-11 4 BOLT

106 NAS1149F0332P 4 WASHER

Component COMPD01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

LN9424A100 As required WIRE

References

Aircraft Maintenance Manual (AMM) 20-28-00, Page Block 201

26-23-41, Page Block 401

Fig. A-GBJAA

Installation of Fire Extinguishing Bottles

FIN 4005WX and FIN 4010WX with

Cartridges.

Sheet 01

Sheet 02

Sheet 03

Refer to Fig. A-GBJAA

(a) Install the fire extinguishing bottle 1 (FWD) 4005WX.

1 Between FR36RH and FR37RH, install the fire extinguishing bottle 4005WX

(Refer to AMM 26-23-41, Page Block 401) :

Refer to Fig. A-GBJAA Sheet 01 and Fig. A-GBJAA Sheet 02 :

1 Extinguisher-Fire 472931-3 Item (204) Retained at

removal

with :

4 Nut NAS1726-5E Item 100

4 Bolt NAS1305-2 Item 101

1 Bolt NAS1304-9 Item 103

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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1 Nut NAS1726-4E Item 104

2 Bolt NAS563-11 Item 105

NOTE: See NOTE 01, 02, 03.

2 Washer NAS1149F0332P Item 106

2 Secure the coupling nuts of the fire extinguishing discharge heads and the

bolts, Item 105, with :

As

required

Wire-Lock LN9424A100

NOTE (01): Torque tighten the bolt to between 0.30da.Nm (26.552lbf.in)

and 0.35da.Nm (30.977lbf.in).

NOTE (02): For the installation of the bolt refer to the electrical bonding of

components with conductive screws and bolts and bonding

straps according toAMM 20-28-00, Page Block 201.

NOTE (03): Seal the bonding connection by overlapping application and

identify the bonding connection by overlapping application with

blue dyed protective coating.

(b) Install the fire extinguishing bottle 2 (AFT) 4010WX.

1 Between FR37RH and FR37.1RH, install the fire extinguishing bottle 4010WX

(Refer to AMM 26-23-41, Page Block 401) :

Refer to Fig. A-GBJAA Sheet 01 and Fig. A-GBJAA Sheet 03 :

1 Extinguisher-Fire 472625-3 Item (203)

with :

4 Nut NAS1726-5E Item 100

4 Bolt NAS1305-2 Item 101

1 Bolt NAS1304-9 Item 103

1 Nut NAS1726-4E Item 104

2 Bolt NAS563-11 Item 105

NOTE: See NOTE 01, 02, 03.

2 Washer NAS1149F0332P Item 106

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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2 Secure the coupling nuts of the fire extinguishing discharge heads and the

bolts, Item 105, with :

As

required

Wire-Lock LN9424A100

NOTE (01): Torque tighten the bolt to between 0.30da.Nm (26.552lbf.in)

and 0.35da.Nm (30.977lbf.in).

NOTE (02): For the installation of the bolt refer to the electrical bonding of

components with conductive screws and bolts and bonding

straps according toAMM 20-28-00, Page Block 201.

NOTE (03): Seal the bonding connection by overlapping application and

identify the bonding connection by overlapping application with

blue dyed protective coating.

(27) Subtask 265020-831-214-001 - Install the new identification placards.

Work Zones and Access Panels

Zone Access/Work location

132 Work location from Frame 37 to Frame 37.1

Manpower Resources

Manhours 1.50

Minimum number of person 2

Subtask elapsed time 0.75

Skills NON SPECIFIC

Material necessary to do the job

Kit 265020D04R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

240 F2627004120800 1 PLACARD

241 F2627004121400 1 PLACARD

242 F2627004121200 1 PLACARD

243 F2627004120400 1 PLACARD

244 F2627004120600 1 PLACARD

245 F2627004121600 1 PLACARD

246 F2627004121800 1 PLACARD

247 F2627004121000 1 PLACARD

248 G2627004020200 1 PLACARD

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Abrasion Resistant Coating

(Teflon Polyuret)

07-003 As required

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

General Purpose Adhesive

Honeycomb Filler

08-554 As required

References

Fig. A-GBFAA

Installation of the U-Section and the

Flow Metering System (FMS)

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

(a) Install the identification placards 4010WX, 4016WX, 4018WX, 5010WE, 5011WE,

5014WE, 5015WE, 5016WE, 5017WE, between FR37 and FR37.1.

Refer to Fig. A-GBFAA

1 Between FR37RH and FR37.1RH, install :

Refer to Fig. A-GBFAA Sheet 01, Fig. A-GBFAA Sheet 03 and Fig. A-GBFAA

Sheet 06

1 Placard F2627004120800 Item 240

1 Placard F2627004121400 Item 241

1 Placard F2627004121200 Item 242

1 Placard F2627004120400 Item 243

1 Placard F2627004120600 Item 244

1 Placard F2627004121600 Item 245

1 Placard F2627004121800 Item 246

1 Placard F2627004121000 Item 247

1 Placard G2627004020200 Item 248

Bond the placard, Item 248, with :

General Purpose

Adhesive

Honeycomb Filler

08-554 As required

Protect the placard, Item 248, with :

Abrasion Resistant

Coating (Teflon

Polyuret)

07-003 As required

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 201

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SERVICE BULLETIN

**CONF 003

(1) Subtask 265020-831-001-004 - Modify the Equipment and the Wiring in the RH

Overhead Panel 212VU.

Work Zones and Access Panels

Zone Access/Work location

212 Work location Electrical panel 212VU

Manpower Resources

Manhours 12.00

Minimum number of person 1

Subtask elapsed time 12.00

Skills ELECTRICAL

Material necessary to do the job

Kit 265020A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

2 ASNA2083BG2-10 7 Screw

6 NSA937901MA2206 1 Module

7 NSA937901FM 1 Module

10 F9251088400000 1 Plate

F1131101500000 Placard

F9000095226495 Bundle

NAS1102-04-5 44 Screw

NSA935401-03 50 TIE

NSA937901E2 1 Label

Kit 265020A04R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 F33110427A00 1 Plate

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Pure Mineral Vaseline Or

Petro-Latum

04-012 As required

Electrical Bond Varnish 07-001B As required

Sealant, High Temperature 08-007C As required

References

Aircraft Maintenance Manual (AMM) Task 11-00-00-400-802

Task 20-28-00-912-802

Fig. A-FBBAA

Modification of the Equipment in the RH

Overhead Panel 212VU

Sheet 01

Sheet 02

Sheet 03

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References

Fig. A-FCAAA

Modification of the Wiring in the RH

Overhead Panel 212VU

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

(a) Remove and disconnect the RH overhead panel 212VU.

NOTE: Retain it.

(b) Modify the equipment in the RH overhead panel 212VU.

1 Remove the integrally lighted plate (212LF).

a Remove as shown in Fig. A-FBBAA Sheet 01 :

FIN 212LF

1 Plate-Integrally Lighted F33110330A00 Item (1) Discard

attached with :

7 Screw ASNA2083BG2-10 Item (2) Discard

2 Remove the indicator light BTL3 (5WX).

a Remove as shown in Fig. A-FBBAA Sheet 01 and Fig. A-FBBAA Sheet

02, Detail B :

FIN 5WX

1 Light-Indicator ABS0951A0LP110 Item (3) Discard

FIN 5WX1

1 Sleeve E0416-02 Item (4) Discard

FIN 5WXA

1 Connector E0417A01S Item (5) Discard

NOTE: Remove and discard the attachment hardware.

3 Replace the 212VU front plate.

a Remove and retain all the items of equipment that are installed on the

front plate.

b Remove as shown in Fig. A-FBBAA Sheet 01 :

1 Plate Assy- Front

212VU

F9251602100000 Item (10) Discard

attached with :

8 Screw NAS1102-06-5 Item (11) Retain

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c On the new front plate, bond the placards (Refer to AMM Task

11-00-00-400-802) supplied in :

Placard Set-212VU F1131101500000

NOTE: Bond the applicable placards at the same locations as on

the old front plate. Discard the unused placards.

d Install as shown in Fig. A-FBBAA Sheet 03 :

1 Plate Assy- Front

212VU

F9251088400000 Item 10

attach with :

8 Screw NAS1102-06-5 Item (11)

NOTE: The screws Item (11) were retained at the removal.

e Install again all the items of equipment that you removed and retained

before the replacement of the front plate and attach with :

44 Screw NAS1102-04-5

Safety the screws with :

Sealant, High

Temperature

08-007C As required

NOTE: Replace the screws if they are damaged during the

removal. The quantity of screws to be replaced depends

on aircraft configuration (44 is the maximum).

f Do the electrical bonding (Refer to AMM Task 20-28-00-912-802) with :

Pure Mineral

Vaseline Or PetroLatum

04-012 As required

and

Electrical Bond

Varnish

07-001B As required

4 Modify the terminal block (582VT) as shown in Fig. A-FBBAA Sheet 01 and

Fig. A-FBBAA Sheet 02, Detail C.

a Remove from position 2 :

FIN 582VT2

1 Module-False NSA937901FM Item (6) Discard

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b Remove from position 3 :

FIN 582VT3

1 Module NSA937901MA2204 Item (7) Discard

c Install at position 2 as shown in :

FIN 582VT2

1 Module NSA937901MA2206 Item 6

with

1 Label-Identification NSA937901E2

d Install at position 3 as shown in :

FIN 582VT3

1 Module-False NSA937901FM Item 7

5 Install the new integrally lighted plate (212LF).

a Install as shown in Fig. A-FBBAA Sheet 03 :

FIN 212LF

1 Plate-Integrally Lighted F33110427A00 Item 1

attach with :

7 Screw ASNA2083BG2-10 Item 2

(c) Modify the wiring in the RH overhead panel 212VU.

1 Remove the wires as shown in the wiring diagrams Fig. A-FCAAA Sheet 01,

Fig. A-FCAAA Sheet 02 and as given in the hook-up chart lines :

- 1 thru 13 (Refer to Fig. A-FCAAA Sheet 04).

2 Modify the connections of the wires as shown in the wiring diagrams Fig. AFCAAA Sheet 02, Fig. A-FCAAA Sheet 03 and as given in the hook-up chart

lines :

- 17 thru 24 (Refer to Fig. A-FCAAA Sheet 04)

- 1 and 2 (Refer to Fig. A-FCAAA Sheet 05).

3 Install the wires as shown in the wiring diagram Fig. A-FCAAA Sheet 03 and

as given in the hook-up chart lines :

- 6 thru 12 (Refer to Fig. A-FCAAA Sheet 05), supplied in :

Bundle F9000095226495

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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4 Attach the wires with :

50 Tie-Cable NSA935401-03

(d) Install the RH overhead panel 212VU.

(2) Subtask 265020-831-002-001 - Modify the Equipment and the Wiring in the

Emergency Power Center 740VU.

Work Zones and Access Panels

Zone Access/Work location

121 Access Door 821, Door 132AZ

Work location Electrical panel 740VU

Manpower Resources

Manhours 3.50

Minimum number of person 1

Subtask elapsed time 3.50

Skills ELECTRICAL

Material necessary to do the job

Kit 265020A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

F9000095226495 Bundle

NSA935401-03 50 TIE

NSA935401-05 50 TIE

References

Fig. A-FBCAA

Modification of the Equipment in the

Emergency Power Center 740VU

Sheet 01

Fig. A-FCBAA

Modification of the Wiring in the

Emergency Power Center 740VU

Sheet 01

Sheet 02

(a) Open the emergency power center 740VU.

(b) Remove the wires as shown in the wiring diagram Fig. A-FCBAA Sheet 01 and as

given in the hook-up chart lines :

- 1 thru 8 (Refer to Fig. A-FCBAA Sheet 02).

(c) Modify the terminal block (703VT) as shown in Fig. A-FBCAA Sheet 01.

1 Remove from position 21 :

1 Clamp-End NSA937901S Retain

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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2 Remove from position 20 :

FIN 703VT20

1 Module NSA937901MA2004 Item (7) Discard

3 Install at position 20 :

1 Clamp-End NSA937901S

NOTE: The end clamp was retained at the removal.

(d) Install the wire as shown in the wiring diagram Fig. A-FCBAA Sheet 01 and as

given in the hook-up chart line :

- 12 (Refer to Fig. A-FCBAA Sheet 02), supplied in :

Bundle F9000095226495

(e) Attach the wire with :

50 Tie-Cable NSA935401-03

50 Tie-Cable NSA935401-05

(f) Close the emergency power center 740VU.

(3) Subtask 265020-831-003-001 - Modify the Equipment and the Wiring in the AC/DC

Main Power Center 710VU.

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 821, Door 132AZ

Work location Electrical panel 710VU

Manpower Resources

Manhours 3.50

Minimum number of person 1

Subtask elapsed time 3.50

Skills ELECTRICAL

Material necessary to do the job

Kit 265020A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

F9000095226495 Bundle

NSA935401-03 50 TIE

NSA935401-05 50 TIE

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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References

Fig. A-FBDAA

Modification of the Equipment in the

AC/DC Main Power Center 710VU

Sheet 01

Fig. A-FCCAA

Modification of the Wiring in the AC/DC

Main Power Center 710VU

Sheet 01

Sheet 02

(a) Open the AC/DC main power center 710VU.

(b) Remove the wires as shown in the wiring diagram Fig. A-FCCAA Sheet 01 and as

given in the hook-up chart lines :

- 1 thru 8 (Refer to Fig. A-FCCAA Sheet 02).

(c) Modify the terminal block (1712VT) as shown in Fig. A-FBDAA Sheet 01.

1 Remove from position 18 :

1 Clamp-End NSA937901S Retain

2 Remove from position 17 :

FIN 1712VT17

1 Module NSA937901MA2004 Item (7) Discard

3 Install at position 17 :

1 Clamp-End NSA937901S

NOTE: The end clamp was retained at the removal.

(d) Install the wire as shown in the wiring diagram Fig. A-FCCAA Sheet 01 and as

given in the hook-up chart line :

- 12 (Refer to Fig. A-FCCAA Sheet 02), supplied in :

Bundle F9000095226495

(e) Attach the wire with :

50 Tie-Cable NSA935401-03

50 Tie-Cable NSA935401-05

(f) CLose the AC/DC main power center 710VU.

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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(4) Subtask 265020-831-004-001 - Modify the Equipment and the Wiring in the LH

Relay Box 751VU.

Work Zones and Access Panels

Zone Access/Work location

121 Access Door 821, Door 132AZ

Work location Electrical panel 751VU

Manpower Resources

Manhours 3.50

Minimum number of person 1

Subtask elapsed time 3.50

Skills ELECTRICAL

References

Fig. A-FBEAA

Modification of the Equipment in the LH

Relay Box 751VU

Sheet 01

Fig. A-FCDAA

Modification of the Wiring in the LH

Relay Box 751VU

Sheet 01

Sheet 02

(a) Open the LH relay box 751VU.

(b) Remove the wires as shown in the wiring diagram Fig. A-FCDAA Sheet 01 and as

given in the hook-up chart lines :

- 1 thru 12 (Refer to Fig. A-FCDAA Sheet 02).

(c) Remove from position E93, as shown in Fig. A-FBEAA Sheet 01 :

FIN 10WX

1 Relay E0245-28A0 Item (8) Discard

FIN 10WXA

1 Base E0250A0S Item (9) Discard

NOTE: Remove and discard the attachment hardware and the related

placard(s).

(d) Remove from position E89, as shown in Fig. A-FBEAA Sheet 01 :

FIN 11WX

1 Relay E0245-28A0 Item (8) Discard

FIN 11WXA

1 Base E0250A0S Item (9) Discard

NOTE: Remove and discard the attachment hardware and the related

placard(s).

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 209

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(e) Close the LH relay box 751VU.

(5) Subtask 265020-831-005-001 - Modify the Equipment and the Wiring in the RH

Relay Box 752VU.

Work Zones and Access Panels

Zone Access/Work location

122 Access Door 821, Door 132AZ

Work location Electrical panel 752VU

Manpower Resources

Manhours 3.50

Minimum number of person 1

Subtask elapsed time 3.50

Skills ELECTRICAL

References

Fig. A-FBFAA

Modification of the Equipment in the RH

Relay Box 752VU

Sheet 01

Fig. A-FCEAA

Modification of the Wiring in the RH

Relay Box 752VU

Sheet 01

Sheet 02

(a) Open the RH relay box 752VU.

(b) Remove the wires as shown in the wiring diagram Fig. A-FCEAA Sheet 01 and as

given in the hook-up chart lines :

- 1 thru 12 (Refer to Fig. A-FCEAA Sheet 02).

(c) Remove from position B37, as shown in Fig. A-FBFAA Sheet 01 :

FIN 12WX

1 Relay E0245-28A0 Item (8) Discard

FIN 12WXA

1 Base E0250A0S Item (9) Discard

NOTE: Remove and discard the attachment hardware and the related

placard(s).

(d) Remove from position B33, as shown in Fig. A-FBFAA Sheet 01 :

FIN 13WX

1 Relay E0245-28A0 Item (8) Discard

FIN 13WXA

1 Base E0250A0S Item (9) Discard

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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NOTE: Remove and discard the attachment hardware and the related

placard(s).

(e) Close the RH relay box 752VU.

(6) Subtask 265020-831-006-001 - Modify the Equipment and the Wiring in the Main

Rack 800VU.

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 821, Door 132AZ

Work location Electrical panel 800VU

Manpower Resources

Manhours 8.00

Minimum number of person 2

Subtask elapsed time 4.00

Skills ELECTRICAL

Material necessary to do the job

Kit 265020A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

7 NSA937901FM 1 Module

F9000095226495 Bundle

NSA935401-03 200 TIE

NSA935401-05 200 TIE

NSA935401-08 200 Tie

References

Aircraft Maintenance Manual (AMM) Task 26-16-34-000-801

Task 26-16-34-400-801

Fig. A-FBGAA

Modification of the Equipment in the

Main Rack 800VU

Sheet 01

Fig. A-FCFAA

Modification of the Wiring in the Main

Rack 800VU

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

Fig. A-FCGAA

Modification of the Pin Programming in

the Main Rack 800VU

Sheet 01

Sheet 02

(a) Remove and retain the SDCU (20WH) (Refer to AMM Task 26-16-34-000-801).

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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(b) Remove the wires as shown in the wiring diagrams Fig. A-FCFAA Sheet 01, Fig. AFCFAA Sheet 02, Fig. A-FCFAA Sheet 03, and as given in the hook-up chart lines :

- 1 thru 25 (Refer to Fig. A-FCFAA Sheet 05)

- 1 thru 3 (Refer to Fig. A-FCFAA Sheet 06).

(c) Modify the terminal block (2900VT) as shown in Fig. A-FBGAA Sheet 01.

1 Remove from position 50 :

FIN 2900VT50

1 Module NSA937901MA2011 Item (7) Discard

2 Install at position 50 :

FIN 2900VT50

1 Module-False NSA937901FM Item 7

(d) Install the wires as shown in the wiring diagram Fig. A-FCFAA Sheet 04 and as

given in the hook-up chart lines :

- 7 thru 18 (Refer to Fig. A-FCFAA Sheet 06), supplied in :

Bundle F9000095226495

(e) Modify the connection of the wires as shown in the wiring diagram Fig. A-FCGAA

Sheet 01 and as given in the hook-up chart lines :

- 1 thru 4 (Refer to Fig. A-FCGAA Sheet 02).

(f) Attach the wires with :

200 Tie-Cable NSA935401-03

200 Tie-Cable NSA935401-05

200 Tie-Cable NSA935401-08

(g) Install the SDCU (20WH) (Refer to AMM Task 26-16-34-400-801).

(7) Subtask 265020-831-007-001 - Modify the Wiring between the Main Rack Shelf

801VU and the LH Relay Box 751VU.

Work Zones and Access Panels

Zone Access/Work location

121 Access Door 821, Door 132AZ

Work location from Electrical panel 801VU to Electrical panel

751VU

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 212

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SERVICE BULLETIN

Manpower Resources

Manhours 3.50

Minimum number of person 1

Subtask elapsed time 3.50

Skills ELECTRICAL

Material necessary to do the job

Kit 265020A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

NSA936604CA0931 8 Cap

References

Fig. A-FBAAA

Location of the Working Areas

Sheet 01

Fig. A-FCHAA

Modification of the Wiring between the

Main Rack Shelf 801VU and the LH

Relay Box 751VU

Sheet 01

Sheet 02

(a) Modify the connections of the wires as shown in the wiring diagram Fig. A-FCHAA

Sheet 01 and as given in the hook-up chart lines :

- 1 thru 8 (Refer to Fig. A-FCHAA Sheet 02).

(b) Install on the stowed wires ends :

8 Cap-Sealing NSA936604CA0931

(8) Subtask 265020-831-008-001 - Modify the Wiring between the Main Rack Shelf

802VU and the RH Relay Box 752VU.

Work Zones and Access Panels

Zone Access/Work location

122 Access Door 821, Door 132AZ

Work location from Electrical panel 802VU to Electrical panel

752VU

Manpower Resources

Manhours 3.50

Minimum number of person 1

Subtask elapsed time 3.50

Skills ELECTRICAL

References

Fig. A-FBAAA

Location of the Working Areas

Sheet 01

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 213

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SERVICE BULLETIN

References

Fig. A-FCJAA

Modification of the Wiring between the

Main Rack Shelf 802VU and the RH

Relay Box 752VU

Sheet 01

Sheet 02

(a) Remove the wires as shown in the wiring diagram Fig. A-FCJAA Sheet 01 and as

given in the hook-up chart lines :

- 1 thru 4 (Refer to Fig. A-FCJAA Sheet 02).

(9) Subtask 265020-831-009-001 - Modify the Wiring between the Emergency Power

Center 740VU and the LH Relay Box 751VU.

Work Zones and Access Panels

Zone Access/Work location

121 Access Door 821, Door 132AZ

Work location from Electrical panel 740VU to Electrical panel

751VU

Manpower Resources

Manhours 3.50

Minimum number of person 1

Subtask elapsed time 3.50

Skills ELECTRICAL

References

Fig. A-FBAAA

Location of the Working Areas

Sheet 01

Fig. A-FCKAA

Modification of the Wiring between the

Emergency Power Center 740VU and

the LH Relay Box 751VU

Sheet 01

Sheet 02

(a) Remove the wires as shown in the wiring diagram Fig. A-FCKAA Sheet 01 and as

given in the hook-up chart lines :

- 1 thru 4 (Refer to Fig. A-FCKAA Sheet 02).

(10) Subtask 265020-831-010-001 - Modify the Wiring between the AC/DC Main Power

Center 715VU and the RH Relay Box 752VU.

Work Zones and Access Panels

Zone Access/Work location

122 Access Door 821, Door 132AZ

Work location from Electrical panel 715VU to Electrical panel

752VU

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 214

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

Manpower Resources

Manhours 3.50

Minimum number of person 1

Subtask elapsed time 3.50

Skills ELECTRICAL

References

Fig. A-FBAAA

Location of the Working Areas

Sheet 01

Fig. A-FCLAA

Modification of the Wiring between the

AC/DC Main Power Center 715VU and

the RH Relay Box 752VU

Sheet 01

Sheet 02

(a) Remove the wires as shown in the wiring diagram Fig. A-FCLAA Sheet 01 and as

given in the hook-up chart lines :

- 1 thru 4 (Refer to Fig. A-FCLAA Sheet 02).

(11) Subtask 265020-831-011-001 - Modify the Wiring between the Main Rack Shelf

801VU and the Avionics Compartment at FR2.

Work Zones and Access Panels

Zone Access/Work location

From 121 Access Door 821, Door 132AZ

Work location Electrical panel 801VU

To 211 Access Door 831, Door 841

Panel 211EW

Work location Frame 2

Manpower Resources

Manhours 3.50

Minimum number of person 1

Subtask elapsed time 3.50

Skills ELECTRICAL

Material necessary to do the job

Kit 265020A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

NSA936604CA0931 2 Cap

References

Fig. A-FBAAA

Location of the Working Areas

Sheet 01

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 215

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

References

Fig. A-FCMAA

Modification of the Wiring between the

Main Rack Shelf 801VU and the

Avionics Compartment at FR2

Sheet 01

Sheet 02

(a) Modify the connections of the wire as shown in the wiring diagram Fig. A-FCMAA

Sheet 01 and as given in the hook-up chart lines :

- 1 and 2 (Refer to Fig. A-FCMAA Sheet 02).

(b) Install on the stowed wire ends :

2 Cap-Sealing NSA936604CA0931

(12) Subtask 265020-831-012-001 - Modify the Wiring between the RH Overhead Panel

212VU and the Avionics Compartment (LH Side).

Work Zones and Access Panels

Zone Access/Work location

From 212 Access Door 831, Door 841

Work location Electrical panel 212VU

To 121 Access Door 821, Door 132AZ

Work location Electrical panel 751VU

Electrical panel 740VU

Frame 2

Electrical panel 801VU

Manpower Resources

Manhours 10.00

Minimum number of person 2

Subtask elapsed time 5.00

Skills ELECTRICAL

Material necessary to do the job

Kit 265020A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

F9000095226495 Bundle

NSA935401-05 200 TIE

NSA935401-08 200 Tie

NSA936604CA0931 8 Cap

References

Fig. A-FBAAA

Location of the Working Areas

Sheet 01

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 216

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

References

Fig. A-FCNAA

Modification of the Wiring between the

RH Overhead Panel 212VU and the

Avionics Compartment (LH Side)

Sheet 01

Sheet 02

Sheet 03

(a) Modify the connections of the wires as shown in the wiring diagrams Fig. A-FCNAA

Sheet 01, Fig. A-FCNAA Sheet 02 and as given in the hook-up chart lines :

- 1 thru 8 (Refer to Fig. A-FCNAA Sheet 03).

(b) Install on the stowed wires ends :

8 Cap-Sealing NSA936604CA0931

(c) Install the wires as shown in the wiring diagram Fig. A-FCNAA Sheet 01 and as

given in the hook-up chart lines :

- 12 and 13 (Refer to Fig. A-FCNAA Sheet 02), supplied in :

Bundle F9000095226495

(d) Attach the wires with :

200 Tie-Cable NSA935401-05

200 Tie-Cable NSA935401-08

(13) Subtask 265020-831-013-001 - Modify the Wiring between the RH Overhead Panel

212VU and the Avionics Compartment (RH Side).

Work Zones and Access Panels

Zone Access/Work location

From 212 Access Door 831, Door 841

Work location Electrical panel 212VU

To 122 Access Door 821, Door 132AZ

Panel 131BA

Work location Electrical panel 752VU

Electrical panel 715VU

Electrical panel 802VU

Frame 20

Manpower Resources

Manhours 10.00

Minimum number of person 2

Subtask elapsed time 5.00

Skills ELECTRICAL

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 217

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

Material necessary to do the job

Kit 265020A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

F9000095226495 Bundle

NSA935401-05 200 TIE

NSA935401-08 200 Tie

NSA936604CA0931 10 Cap

References

Fig. A-FBAAA

Location of the Working Areas

Sheet 01

Fig. A-FCPAA

Modification of the Wiring between the

RH Overhead Panel 212VU and the

Avionics Compartment (RH Side)

Sheet 01

Sheet 02

Sheet 03

(a) Modify the connections of the wires as shown in the wiring diagram Fig. A-FCPAA

Sheet 01, Fig. A-FCPAA Sheet 02 and as given in the hook-up chart lines :

- 1 thru 12 (Refer to Fig. A-FCPAA Sheet 03).

(b) Install on the stowed wires ends :

10 Cap-Sealing NSA936604CA0931

(c) Install the wires as shown in the wiring diagram Fig. A-FCPAA Sheet 01 and as

given in the hook-up chart lines :

- 9 and 10 (Refer to Fig. A-FCPAA Sheet 02), supplied in :

Bundle F9000095226495

(d) Attach the wires with :

200 Tie-Cable NSA935401-05

200 Tie-Cable NSA935401-08

(14) Subtask 265020-831-201-002 - Remove the Fire Extinguishing Bottles, 4010WX,

4005WX and 4020WX.

Work Zones and Access Panels

Zone Access/Work location

132 Access Panel 132PM

Work location from Frame 35 to Frame 37.1

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 218

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

Manpower Resources

Manhours 3.00

Minimum number of person 2

Subtask elapsed time 1.50

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 26-23-41, Page Block 401

Fig. A-GBBAA

Removal of Fire Extinguishing Bottles

4005WX, 4010WX and 4020WX with

Cartridges.

Sheet 01

Sheet 02

Sheet 03

(a) Remove the Fire Extinguishing Bottle 2 (FWD), 4010WX.

Refer to Fig. A-GBBAA

1 Between FR35RH and FR36RH, remove the fire extinguishing bottle 4010WX

(Refer to AMM 26-23-41, Page Block 401) :

Refer to Fig. A-GBBAA Sheet 01 and Fig. A-GBBAA Sheet 02 :

1 Extinguisher-Fire 472625-3 Item (203) Retain

with :

4 Nut NAS1726-5E Item (100) Discard

4 Bolt NAS1305-2 Item (101) Discard

1 Bolt NAS1304-9 Item (103) Discard

1 Nut NAS1726-4E Item (104) Discard

2 Bolt NAS563-11 Item (105) Discard

2 Washer NAS1149F0332P Item (106) Discard

(b) Remove the Fire Extinguishing Bottle 1 (MID), 4005WX.

Refer to Fig. A-GBBAA

1 Between FR36RH and FR37RH, remove the fire extinguishing bottle 4005WX

(Refer to AMM 26-23-41, Page Block 401) :

Refer to Fig. A-GBBAA Sheet 01 and Fig. A-GBBAA Sheet 03 :

1 Extinguisher-Fire 472931-3 Item (204) Retain

with :

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 219

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

4 Nut NAS1726-5E Item (100) Discard

4 Bolt NAS1305-2 Item (101) Discard

1 Bolt NAS1304-9 Item (103) Discard

1 Nut NAS1726-4E Item (104) Discard

2 Bolt NAS563-11 Item (105) Discard

2 Washer NAS1149F0332P Item (106) Discard

(c) Remove the Fire Extinguishing Bottle 3 (AFT), 4020WX.

Refer to Fig. A-GBBAA

1 Between FR37RH and FR37.1RH, remove the fire extinguishing bottle

4020WX (Refer to AMM 26-23-41, Page Block 401) :

Refer to Fig. A-GBBAA Sheet 01 and Fig. A-GBBAA Sheet 02 :

1 Extinguisher-Fire 472625-3 Item (203) Discard

with :

4 Nut NAS1726-5E Item (100) Discard

4 Bolt NAS1305-2 Item (101) Discard

1 Bolt NAS1304-9 Item (103) Discard

1 Nut NAS1726-4E Item (104) Discard

2 Bolt NAS563-11 Item (105) Discard

2 Washer NAS1149F0332P Item (106) Discard

(15) Subtask 265020-831-202-001 - Remove the 4 Flow Metering Compact Units (FMCU),

FIN 4031WX, 4032WX, 4033WX and 4034WX.

Work Zones and Access Panels

Zone Access/Work location

132 Access Panel 132PM

Work location from Frame 35 to Frame 37.1

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 220

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

Manpower Resources

Manhours 4.00

Minimum number of person 2

Subtask elapsed time 2.00

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 26-23-43, Page Block 401

Fig. A-GBCAA

Removal of the 4 Flow Metering

Compact Units (FMCU), FIN 4031WX,

4032WX, 4033WX and 4034WX, the

related Plumbing Installations and

Placards

Sheet 01

Sheet 02

Sheet 03

(a) Remove the Flow Metering Compact Unit (FMCU), FIN 4031WX.

Refer to Fig. A-GBCAA

1 From FR35RH, remove the FMCU, FIN 4031WX (Refer to AMM 26-23-43,

Page Block 401) :

Refer to Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet 02 and Fig. A-GBCAA

Sheet 03

1 Meter-Flow, Compact

Unit

QA07907-01 Item (205) Discard

and

1 Hose Assy G2627007000000 Item (107) Discard

1 Tube Assy G2627006000000 Item (109) Discard

with :

1 Washer NAS1149F0332P Item (106) Discard

1 Clamp NSA5516-06NJ Item (111) Discard

1 Screw NAS1096-3-10 Item (112) Discard

1 Nut NAS1726-3E Item (113) Discard

3 Screw NAS1100E4-36 Item (130) Discard

3 Washer NAS1149C0432R Item (131) Discard

1 Fitting A2627048220400 Item (132) Discard

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 221

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Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

2 O-Ring NSA8202-6 Item (133) Discard

1 Fitting A2627048221600 Item (134) Discard

(b) Remove the Flow Metering Compact Unit (FMCU), FIN 4032WX.

Refer to Fig. A-GBCAA

1 From FR36RH, remove the FMCU, FIN 4032WX (Refer to AMM 26-23-43,

Page Block 401) :

Refer to Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet 02 and Fig. A-GBCAA

Sheet 03

1 Meter-Flow, Compact

Unit

QA07907-01 Item (205) Discard

and

1 Hose Assy G2627007000200 Item (108) Discard

1 Tube Assy G2627006000200 Item (110) Discard

with :

1 Washer NAS1149F0332P Item (106) Discard

1 Clamp NSA5516-06NJ Item (111) Discard

1 Screw NAS1096-3-10 Item (112) Discard

1 Nut NAS1726-3E Item (113) Discard

3 Screw NAS1100E4-36 Item (130) Discard

3 Washer NAS1149C0432R Item (131) Discard

1 Fitting A2627048220400 Item (132) Discard

2 O-Ring NSA8202-6 Item (133) Discard

1 Fitting A2627048221600 Item (134) Discard

(c) Remove the Flow Metering Compact Unit (FMCU), FIN 4033WX.

Refer to Fig. A-GBCAA

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 222

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

1 From FR37RH, remove the FMCU, FIN 4033WX (Refer to AMM 26-23-43,

Page Block 401) :

Refer to Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet 02 and Fig. A-GBCAA

Sheet 03

1 Meter-Flow, Compact

Unit

QA07907-01 Item (205) Discard

and

1 Hose Assy G2627007000000 Item (107) Discard

1 Tube Assy G2627006000000 Item (109) Discard

with :

1 Washer NAS1149F0332P Item (106) Discard

1 Clamp NSA5516-06NJ Item (111) Discard

1 Screw NAS1096-3-10 Item (112) Discard

1 Nut NAS1726-3E Item (113) Discard

3 Screw NAS1100E4-36 Item (130) Discard

3 Washer NAS1149C0432R Item (131) Discard

1 Fitting A2627048220400 Item (132) Discard

2 O-Ring NSA8202-6 Item (133) Discard

1 Fitting A2627048221600 Item (134) Discard

(d) Remove the Flow Metering Compact Unit (FMCU), FIN 4034WX.

Refer to Fig. A-GBCAA

1 From FR37.1RH, remove the FMCU, FIN 4034WX (Refer to AMM 26-23-43,

Page Block 401) :

Refer to Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet 02 and Fig. A-GBCAA

Sheet 03

1 Meter-Flow, Compact

Unit

QA07907-01 Item (205) Discard

and

1 Hose Assy G2627007000200 Item (108) Discard

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 223

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

1 Tube Assy G2627006000200 Item (110) Discard

with :

1 Washer NAS1149F0332P Item (106) Discard

1 Clamp NSA5516-06NJ Item (111) Discard

1 Screw NAS1096-3-10 Item (112) Discard

1 Nut NAS1726-3E Item (113) Discard

3 Screw NAS1100E4-36 Item (130) Discard

3 Washer NAS1149C0432R Item (131) Discard

1 Fitting A2627048220400 Item (132) Discard

2 O-Ring NSA8202-6 Item (133) Discard

1 Fitting A2627048221600 Item (134) Discard

(16) Subtask 265020-831-203-001 - Remove the plumbing installations and placards.

Work Zones and Access Panels

Zone Access/Work location

132 Access Panel 132PM

Work location from Frame 35 to Frame 37.1

Manpower Resources

Manhours 2.50

Minimum number of person 2

Subtask elapsed time 1.25

Skills NON SPECIFIC

References

Fig. A-GBCAA

Removal of the 4 Flow Metering

Compact Units (FMCU), FIN 4031WX,

4032WX, 4033WX and 4034WX, the

related Plumbing Installations and

Placards

Sheet 01

Sheet 02

Sheet 03

(a) Remove the plumbing installations between FR35RH thru FR37.1RH.

Refer to Fig. A-GBCAA

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 224

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

1 Between FR35RH and FR36RH, remove :

Refer to Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet 02 and Fig. A-GBCAA

Sheet 03

2 Reducer MS21916D10-4 Item (115) Discard

1 Tube Assy G2627005004400 Item (116) Discard

1 Tee NSA855113-34D Item (117) Discard

1 Tube Assy G2627005004200 Item (118) Discard

1 Hose A2627045200400 Item (209) Discard

with :

2 Washer NAS1149F0332P Item (106) Discard

2 Screw NAS1096-3-10 Item (112) Discard

2 Nut NAS1726-3E Item (113) Discard

2 Clamp NSA5516-18NJ Item (121) Discard

1 Rod End NSA8141-04R Item (135) Discard

1 Nut NAS509-5 Item (136) Discard

1 Rod End NSA8140-04RK Item (137) Discard

2 Lead-Bonding E0090-41-320 Item (138) Discard

1 Bolt NAS1304-12 Item (139) Discard

1 Nut NAS1726-4E Item (104) Discard

1 Washer NAS1149D0432K Item (140) Discard

1 Washer-Lock NSA5355-5CA Item (141) Discard

2 Between FR36RH and FR37RH, remove :

Refer to Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet 02 and Fig. A-GBCAA

Sheet 03

2 Washer NAS1149F0332P Item (106) Discard

2 Screw NAS1096-3-10 Item (112) Discard

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 225

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

2 Nut NAS1726-3E Item (113) Discard

1 Tube Assy G2627005004000 Item (120) Discard

2 Clamp NSA5516-18NJ Item (121) Discard

1 Cross NSA855140-22D Item (122) Discard

1 Union MS21902D10 Item (123) Discard

1 Tube Assy G2627005003800 Item (124) Discard

2 Tee NSA855008D10 Item (125) Discard

1 Rod End NSA8141-04R Item (135) Retain

1 Nut NAS509-5 Item (136) Retain

1 Rod End NSA8140-04RK Item (137) Retain

2 Lead-Bonding E0090-41-320 Item (138) Discard

1 Bolt NAS1304-12 Item (139) Discard

1 Nut NAS1726-4E Item (104) Discard

1 Washer NAS1149D0432K Item (140) Discard

1 Washer-Lock NSA5355-5CA Item (141) Discard

1 Tube Assy G2627005006400 Item (142) Discard

1 Hose A2627045200400 Item (209) Retain

2 Hose Assy F2627007100200 Item (210) Retain

3 Between FR37RH and FR37.1RH, remove :

Refer to Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet 02 and Fig. A-GBCAA

Sheet 03

2 Reducer MS21916D10-4 Item (115) Discard

1 Tube Assy G2627005004400 Item (116) Discard

1 Tee NSA855113-34D Item (117) Discard

1 Tube Assy G2627005003400 Item (119) Discard

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 226

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

1 Tee NSA855008D10 Item (125) Discard

1 Tube Assy G2627005003600 Item (129) Discard

1 Rod End NSA8141-04R Item (135) Retain

1 Nut NAS509-5 Item (136) Retain

1 Rod End NSA8140-04RK Item (137) Retain

2 Lead-Bonding E0090-41-320 Item (138) Discard

1 Bolt NAS1304-12 Item (139) Discard

1 Nut NAS1726-4E Item (104) Discard

1 Washer NAS1149D0432K Item (140) Discard

1 Washer-Lock NSA5355-5CA Item (141) Discard

1 Hose A2627045200400 Item (209) Retain

(b) Remove the placards between FR35RH thru FR37.1RH.

Refer to Fig. A-GBCAA

1 Between FR35RH and FR36RH, remove the placards 4010WX, 4031WX and

4032WX :

2 Label NSA931025-02F Item (126) Discard

1 Placard G2627004020200 Item (127) Discard

2 Between FR37RH and FR37.1RH, remove the placards 4020WX, 4033WX

and 4034WX :

2 Label NSA931025-02F Item (126) Discard

1 Placard G2627004020400 Item (128) Discard

(17) Subtask 265020-831-204-001 - Remove the brackets and the insulation blankets

between FR35RH thru FR37.1RH.

Work Zones and Access Panels

Zone Access/Work location

132 Work location from Frame 35 to Frame 37.1

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 227

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

Manpower Resources

Manhours 3.50

Minimum number of person 2

Subtask elapsed time 1.75

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 25-80-00-000-801

Fig. A-GBDAA

Removal of the Brackets

Sheet 01

Sheet 02

Sheet 03

(a) Remove the insulation blankets in the affected area (Refer to AMM Task

25-80-00-000-801).

(b) Remove the brackets between FR35RH thru FR37.1RH.

Refer to Fig. A-GBDAA

1 Between FR35 and FR36, STGR 29RH, remove :

Refer to Fig. A-GBDAA Sheet 01 and Fig. A-GBDAA Sheet 03

1 Section-T F5397460021800 Item (161) Discard

1 Bracket Assy F5397484500200 Item (162) Discard

2 From FR35RH, STGR31, remove :

Refer to Fig. A-GBDAA Sheet 01 and Fig. A-GBDAA Sheet 03

1 Bracket F5397463611000 Item (163) Discard

3 From FR36RH, STGR31, remove :

Refer to Fig. A-GBDAA Sheet 01 and Fig. A-GBDAA Sheet 03

1 Bracket F5397463610800 Item (164) Discard

4 From FR37RH, STGR31, remove :

Refer to Fig. A-GBDAA Sheet 01 and Fig. A-GBDAA Sheet 03

1 Bracket F5397463611000 Item (163) Discard

5 From FR37.1RH, STGR31, remove :

Refer to Fig. A-GBDAA Sheet 01 and Fig. A-GBDAA Sheet 03

1 Bracket F5397463610800 Item (164) Discard

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 228

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

6 From the crossbeam at FR35 at -Y2462, remove :

Refer to Fig. A-GBDAA Sheet 01 and Fig. A-GBDAA Sheet 02

1 Bracket Assy F5397800200000 Item (165) Discard

1 Bracket F5397461823000 Item (166) Discard

7 From the crossbeam at FR36 at -Y2462, remove :

Refer to Fig. A-GBDAA Sheet 01 and Fig. A-GBDAA Sheet 02

1 Bracket Assy F5397800200000 Item (165) Discard

1 Bracket F5397469928000 Item (167) Discard

8 Between FR35RH and FR36RH, remove :

Refer to Fig. A-GBDAA Sheet 01 and Fig. A-GBDAA Sheet 02

1 Strut Assy F5397883300000 Item (168) Discard

(18) Subtask 265020-831-213-001 - Install the brackets, modify the insulation blankets

and close the rivet holes between FR35RH thru FR37.1RH.

Work Zones and Access Panels

Zone Access/Work location

132 Work location from Frame 35 to Frame 37.1

Manpower Resources

Manhours 7.00

Minimum number of person 2

Subtask elapsed time 3.50

Skills NON SPECIFIC

Material necessary to do the job

Kit 265020D02R04

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

170 EN6081D4-09 28 RIVET

171 EN6081D6-14 30 RIVET

252 F5397757020200 2 ANGLE

253 F5397462009600 1 BRACKET

254 F5397462009800 1 BRACKET

281 ABS1577A05 1 BRACKET

282 ABS0787B05B 1 BRACKET

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 229

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SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) Task 20-28-00-912-802

Task 25-80-00-200-801

Task 25-80-00-400-801

Fig. A-GBGAA

Installation of the Brackets

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Fig. A-GBDAA

Removal of the Brackets

Sheet 01

Sheet 02

Sheet 03

(a) Install the brackets and close the existing rivet holes.

Refer to Fig. A-GBDAA and Fig. A-GBGAA

1 Between FR35 and FR36, on STGR29RH and STGR30RH, close the rivet

holes in the stringers with :

Refer to Fig. A-GBDAA Sheet 01, Fig. A-GBDAA Sheet 02 and Fig. A-GBDAA

Sheet 03

4 Rivet EN6081D6-14 Item 171

2 On FR35 and FR36, STGR31RH, close the rivet holes in the frames with :

Refer to Fig. A-GBDAA Sheet 01, Fig. A-GBDAA Sheet 02 and Fig. A-GBDAA

Sheet 03

8 Rivet EN6081D6-14 Item 171

3 Between FR36 and FR37, on STGR30RH, install this bracket on the stringer :

Refer to Fig. A-GBGAA Sheet 01 and Fig. A-GBGAA Sheet 02

1 Angle-Bonding F5397757020200 Item 252

with :

3 Rivet EN6081D4-09 Item 170

NOTE: Do the electrical bonding (Refer to AMM Task

20-28-00-912-802)

4 On FR37 and FR37.1, STGR31RH, close the rivet holes in the frames with :

Refer to Fig. A-GBDAA Sheet 01,Fig. A-GBDAA Sheet 02 and Fig. A-GBDAA

Sheet 03

8 Rivet EN6081D6-14 Item 171

5 On FR37, between STGR31RH and STGR32RH, install this bracket :

Refer to Fig. A-GBGAA Sheet 01 and Fig. A-GBGAA Sheet 02

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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SERVICE BULLETIN

1 Bracket Assy F5397462009600 Item 253

with :

4 Rivet EN6081D6-14 Item 171

NOTE: Do the electrical bonding (Refer to AMM Task

20-28-00-912-802)

NOTE: Existing rivet spacing must be used.

6 Between FR37 and FR37.1, on STGR30RH, install this bracket :

Refer to Fig. A-GBGAA Sheet 01 and Fig. A-GBGAA Sheet 02

1 Angle-Bonding F5397757020200 Item 252

with :

3 Rivet EN6081D4-09 Item 170

7 Between FR37 and FR37.1, on STGR30RH, install this bracket :

Refer to Fig. A-GBGAA Sheet 01 and Fig. A-GBGAA Sheet 03

1 Bracket ABS1577A05 Item 281

with :

3 Rivet EN6081D4-09 Item 170

NOTE: Do the electrical bonding (Refer to AMM Task

20-28-00-912-802)

8 On FR37.1, between STGR31RH and STGR32RH, install this bracket :

Refer to Fig. A-GBGAA Sheet 01 and Fig. A-GBGAA Sheet 02

1 Bracket Assy F5397462009800 Item 254

with :

4 Rivet EN6081D6-14 Item 171

NOTE: Do the electrical bonding (Refer to AMM Task

20-28-00-912-802)

NOTE: Existing rivet spacing must be used.

9 On the crossbeam at FR35, between -Y1959 and -Y2462, close the rivet holes

in the crossbeam with :

Refer to Fig. A-GBDAA Sheet 01, Fig. A-GBDAA Sheet 02 and Fig. A-GBDAA

Sheet 03

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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SERVICE BULLETIN

10 Rivet EN6081D4-09 Item 170

10 On the crossbeam at FR36, outboard of -Y2462, close the rivet holes in the

crossbeam with :

Refer to Fig. A-GBDAA Sheet 01, Fig. A-GBDAA Sheet 02 and Fig. A-GBDAA

Sheet 03

9 Rivet EN6081D4-09 Item 170

11 On the crossbeam at FR36, outboard of -Y2462, install this bracket :

Refer to Fig. A-GBGAA Sheet 01 and Fig. A-GBGAA Sheet 03

1 Bracket-Z ABS0787B05B Item 282

with :

2 Rivet EN6081D6-14 Item 171

NOTE: Do the electrical bonding (Refer to AMM Task

20-28-00-912-802)

(b) Between FR36 thru FR37.1RH modify the insulation blankets in the affected area.

1 Adapt the insulation blankets for the new locations of brackets (Refer to AMM

Task 25-80-00-200-801).

(c) Install the modified insulation in the affected area (Refer to AMM Task

25-80-00-400-801).

(19) Subtask 265020-831-216-001 - Modify the equipment and the wiring of the

FMCU/FMS outlet pressure switches 4031WX, 4032WX, 4033WX, 4034WX, 4016WX

and 4018WX of the fire extinguishing bottles Nos. 2 and 3.

Work Zones and Access Panels

Zone Access/Work location

132 Work location from Frame 35 to Frame 37.1

200 Work location Electrical panel 801VU

Manpower Resources

Manhours 1.50

Minimum number of person 2

Subtask elapsed time 0.75

Skills ELECTRICAL

Material necessary to do the job

Kit 265020D03R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

173 G9237018016600 1 PLCRDSET

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 232

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ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

174 NSA935401-04 8 TIE

175 NSA935401-05 15 TIE

References

Process and Material Specification

(PMS)

Process and Material Specification (PMS)

01-07-10

Fig. A-GWAAA

Modification of the Wiring of the

FMCU/FMS Outlet Pressure Switches

4031WX, 4032WX, 4033WX, 4034WX,

4016WX and 4018WX

Sheet 01

Sheet 02

Fig. A-GHAAA

Hook-up Chart

Sheet 01

Fig. A-GBLAA

Stowage of the Electrical Wires of the

Connectors 4031WX-A, 4032WX-A

4011WX-A, 4012WX-A and 4013WX-A

Sheet 01

Sheet 02

Sheet 03

Sheet 04

(a) Modify the wiring of the FMCU/FMS outlet pressure switches.

1 Disconnect these electrical wires from the connectors 4031WX-A and

4032WX-A.

Refer to Fig. A-GWAAA Sheet 01 (Wiring)

Refer to Fig. A-GHAAA Sheet 01 (Hook-up Chart), LINES 1, 2, 3 and 4

2 Remove the connectors 4031WX-A and 4032WX-A and discard.

Refer to Fig. A-GBLAA Sheet 01

Remove :

2 Connector-Plug EN2997KE60803BN Item (265) Discard

and remove the following attachment parts :

4 Screw NAS1801-08-7 Item (267) Discard

2 Nut MS21042-08 Item (268) Discard

4 Washer NAS1149CN816R Item (269) Discard

2 Clamp MS21919WCH8 Item (270) Retain

2 Screw NAS1801-08-23 Item (271) Discard

2 Lanyard DAN80-3-150 Item (273) Discard

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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SERVICE BULLETIN

2 Sleeve-Protective NSA935809-09 Item (274) Discard

5 Cable Mount Item (277) Retain

3 Disconnect these electrical wires from the connectors 4033WX-A and

4034WX-A.

Refer to Fig. A-GWAAA Sheet 01 (Wiring)

Refer to Fig. A-GHAAA Sheet 01 (Hook-up Chart), LINES 5, 6, 7 and 8

4 Reroute and install the electrical wires :

Refer to Fig. A-GWAAA Sheet 02 (Wiring)

Refer to Fig. A-GHAAA Sheet 01 (Hook-up Chart), LINES 13, 14, 15 and 16

with :

15 Tie-Cable NSA935401-05 Item 175

and attach the placards, identified 4016WX-A, 4018WX-A and the SB/MOD

placards :

1 Placardset G9237018016600 Item 173

with :

8 Tie-Cable NSA935401-04 Item 174

(20) Subtask 265020-831-209-001 - Modify the equipment and the wiring of the fire

extinguishing bottle No. 3 (AFT), 4020WX, and relocated fire extinguishing bottle

No. 2 (AFT), 4010WX.

Work Zones and Access Panels

Zone Access/Work location

132 Work location from Frame 35 to Frame 37.1

200 Work location Electrical panel 801VU

Electrical panel 802VU

Manpower Resources

Manhours 1.00

Minimum number of person 2

Subtask elapsed time 1.00

Skills ELECTRICAL

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 234

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SERVICE BULLETIN

Material necessary to do the job

Kit 265020D03R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

173 G9237018016600 1 PLCRDSET

174 NSA935401-04 12 TIE

175 NSA935401-05 15 TIE

176 EN3155-003F1614 2 CONTACT

References

Fig. A-GWBAA

Modification of the Wiring of the Fire

Extinguishing Bottle No. 3 (previously

AFT), 4020WX, and relocated Fire

Extinguishing Bottle No. 2 (now AFT),

4010WX

Sheet 01

Sheet 02

Fig. A-GHBAA

Hook-up Chart

Sheet 01

(a) Modify the wiring of the cartridges and the pressure switch of the fire extinguishing

bottle (AFT), 4020WX (4010WX)

1 Disconnect these electrical wires from the connector 2625VC-A.

Refer to Fig. A-GWBAA Sheet 01 (Wiring)

Refer to Fig. A-GHBAA Sheet 01 (Hook-up Chart), LINES 1 and 11, END 2

2 Reroute and install the electrical wires on the connector 2511VC-A.

Refer to Fig. A-GWBAA Sheet 02 (Wiring)

Refer to Fig. A-GHBAA Sheet 01 (Hook-up Chart), LINES 2 and 12, END 2

3 Disconnect these electrical wires from the connector 2636VC-A.

Refer to Fig. A-GWBAA Sheet 01 (Wiring)

Refer to Fig. A-GHBAA Sheet 01 (Hook-up Chart), LINES 5 and 15, END 2

NOTE: Cut off the contacts directly behind the contacts.

4 Reroute and install the electrical wires on the connector 2508VC-A.

Refer to Fig. A-GWBAA Sheet 02 (Wiring)

Refer to Fig. A-GHBAA Sheet 01 (Hook-up Chart), LINES 6 and 16, END 2

with :

2 Contact-Socket EN3155-003F1614 Item 176

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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5 Disconnect the electrical wire from the connector 2044VC-A.

Refer to Fig. A-GWBAA Sheet 01 (Wiring)

Refer to Fig. A-GHBAA Sheet 01 (Hook-up Chart), LINE 23, END 2

6 Reroute and install the electrical wire on the connector 2016VC-A.

Refer to Fig. A-GWBAA Sheet 02 (Wiring)

Refer to Fig. A-GHBAA Sheet 01 (Hook-up Chart), LINE 24, END 2

7 Attach the placards, identified 4011WX-A, 4012WX-A, 4013WX-A and the

SB/MOD placards :

1 Placardset G9237018016600 Item 173

with :

12 Tie-Cable NSA935401-04 Item 174

8 Install the tie-cables on the wire harnesses :

15 Tie-Cable NSA935401-05 Item 175

NOTE: For the stowage position of the connectors 4011WX-A,

4012WX-A, 4013WX-A, 4031WX-A and 4032WX-A, refer to

(22) Subtask 265020-831-218-001.

(21) Subtask 265020-831-210-001 - Modify the Equipment and the Wiring of the

previous Fire Extinguishing Bottle No. 2 (FWD), 4010WX.

Work Zones and Access Panels

Zone Access/Work location

132 Work location from Frame 35 to Frame 36

200 Work location Electrical panel 801VU

Electrical panel 802VU

Manpower Resources

Manhours 1.50

Minimum number of person 1

Subtask elapsed time 1.50

Skills ELECTRICAL

References

Fig. A-GWCAA

Modification of the Wiring of the Fire

Extinguishing Bottle No. 2 (FWD),

4010WX

Sheet 01

Sheet 02

Fig. A-GHCAA

Hook-up Chart

Sheet 01

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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SERVICE BULLETIN

References

Fig. A-GBLAA

Stowage of the Electrical Wires of the

Connectors 4031WX-A, 4032WX-A

4011WX-A, 4012WX-A and 4013WX-A

Sheet 01

Sheet 02

Sheet 03

Sheet 04

(a) Modify the wiring of the previous fire extinguishing bottle No. 2 (FWD), 4010WX.

1 Disconnect these electrical wires from the connectors 4011WX-A, 4012WX-A

and 4013WX-A.

Refer to Fig. A-GWCAA Sheet 01 (Wiring)

Refer to Fig. A-GHCAA Sheet 01 (Hook-up Chart), LINES 1, 5, 11, 15 and 23

Refer to Fig. A-GHCAA Sheet 01 (Hook-up Chart), LINES 3, 7, 9, 13, 17, 19,

21, END 1

2 Remove the connectors 4011WX-A, 4012WX-A and 4013WX-A and discard.

Refer to Fig. A-GBLAA Sheet 01

Remove :

2 Connector EN2997KE61005BN Item (264) Discard

1 Connector-Plug EN2997KE60803BN Item (265) Discard

and remove the following attachment parts :

1 Tie-Cable NSA935401-03 Item (266) Discard

5 Screw NAS1801-08-7 Item (267) Discard

2 Nut MS21042-08 Item (268) Discard

4 Washer NAS1149CN816R Item (269) Discard

2 Clamp MS21919WCH8 Item (270) Discard

1 Screw NAS1801-08-29 Item (272) Discard

2 Lanyard DAN80-3-150 Item (273) Discard

2 Sleeve-Protective NSA935809-09 Item (274) Discard

2 Cable Mount Item (277) Retain

NOTE: For the stowage position of the connectors 4011WX-A,

4012WX-A, 4013WX-A, 4031WX-A and 4032WX-A, refer to

(22) Subtask 265020-831-218-001.

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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(22) Subtask 265020-831-218-001 - Put the electrical wires of the connectors 4031WX-A,

4032WX-A 4011WX-A, 4012WX-A and 4013WX-A in a stowage position.

Work Zones and Access Panels

Zone Access/Work location

132 Work location from Frame 35 to Frame 37.1

Manpower Resources

Manhours 2.50

Minimum number of person 1

Subtask elapsed time 2.50

Skills ELECTRICAL

Material necessary to do the job

Kit 265020D03R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

173 G9237018016600 1 PLCRDSET

177 NSA936603CC0100 23 CAP

Kit 265020D05R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

266 NSA935401-03 25 TIE

269 NAS1149CN816R 4 WASHER

270 MS21919WCH8 4 CLAMP

271 NAS1801-08-23 2 SCREW

272 NAS1801-08-29 1 SCREW

274 NSA935809-09 4 SLEEVE

275 NAS1801-08-25 1 SCREW

References

Fig. A-GBLAA

Stowage of the Electrical Wires of the

Connectors 4031WX-A, 4032WX-A

4011WX-A, 4012WX-A and 4013WX-A

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Fig. A-GHAAA

Hook-up Chart

Sheet 01

Fig. A-GHCAA

Hook-up Chart

Sheet 01

Fig. A-GWAAA

Modification of the Wiring of the

FMCU/FMS Outlet Pressure Switches

4031WX, 4032WX, 4033WX, 4034WX,

4016WX and 4018WX

Sheet 01

Sheet 02

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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SERVICE BULLETIN

References

Fig. A-GWCAA

Modification of the Wiring of the Fire

Extinguishing Bottle No. 2 (FWD),

4010WX

Sheet 01

Sheet 02

(a) Put the electrical wires of the connectors 4031WX-A and 4032WX-A in a stowage

position.

1 Put the electrical wires in a stowage position.

Refer to Fig. A-GBLAA Sheet 01, Fig. A-GBLAA Sheet 02, Fig. A-GBLAA

Sheet 03 and Fig. A-GBLAA Sheet 04

Refer to Fig. A-GWAAA Sheet 02 (Wiring)

Refer toFig. A-GHAAA Sheet 01 (Hook-up Chart), LINES 9, 10, 11 and 12

with :

6 Cap NSA936603CC0100 Item 177

NOTE: Do not cut off the contacts.

Attach the electrical wires in a stowage position.

with :

2 Washer NAS1149CN816R Item 269

2 Clamp MS21919WCH8 Item 270

2 Clamp MS21919WCH8 Item (270) Retained at

removal

1 Screw NAS1801-08-23 Item 271

2 Sleeve-Protective NSA935809-09 Item 274

1 Screw NAS1801-08-25 Item 275

5 Cable Mount Item (277) Retained at

removal

20 Tie-Cable NSA935401-03 Item 266

(b) Put the electrical wires of the connectors 4011WX-A, 4012WX-A and 4013WX-A in

a stowage position.

1 Put the electrical wires in a stowage position.

Refer to Fig. A-GBLAA Sheet 01, Fig. A-GBLAA Sheet 02, Fig. A-GBLAA

Sheet 03 and Fig. A-GBLAA Sheet 04

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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Refer to Fig. A-GWCAA Sheet 02 (Wiring)

Refer to Fig. A-GHCAA Sheet 01 (Hook-up Chart), LINES 2, 6, 12, 16 and 24

Refer to Fig. A-GHCAA Sheet 01 (Hook-up Chart), LINES 4, 8, 10, 14, 18, 20

and 22, END 1

with :

17 Cap NSA936603CC0100 Item 177

NOTE: Do not cut off the contacts.

Attach the electrical wires in a stowage position.

with :

2 Washer NAS1149CN816R Item 269

2 Clamp MS21919WCH8 Item 270

1 Screw NAS1801-08-23 Item 271

1 Screw NAS1801-08-29 Item 272

2 Sleeve-Protective NSA935809-09 Item 274

2 Cable Mount Item (277) Retained at

removal

and attach the SB/MOD placards :

1 Placardset G9237018016600 Item 173

with :

5 Tie-Cable NSA935401-03 Item 266

(23) Subtask 265020-831-208-001 - Adapt the plumbing installation.

Work Zones and Access Panels

Zone Access/Work location

132 Work location from Frame 36 to Frame 37

Manpower Resources

Manhours 3.00

Minimum number of person 2

Subtask elapsed time 1.50

Skills NON SPECIFIC

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 240

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SERVICE BULLETIN

Material necessary to do the job

Kit 265020D04R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

113 NAS1726-3E 2 NUT

121 NSA5516A18NJ 2 CLAMP

125 NSA855008D10 1 TEE

144 NAS1149C0332R 2 WASHER

155 NSA5527-03-03 2 SPACER

157 NAS1801-3-12 2 SCREW

158 NSA855006D10 2 UNION

251 G2627005013000 1 TUBE

253 G2627005002000 1 TUBE

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Internal Polyurethane

Varnish

07-017 As required

Solvent General Purpose 11-026 As required

Low Voc Anti-Corrosion

Primer

16-006F As required

Lint-Free Cotton Cloth 19-003 As required

Standard tool TOOLD01

ITEM TOOL N ̊ TOOL NAME QTY SEE

NOTES

D12102C07-02 PERMASWAGE Repair

Kit D12000 Series

1

References

Aircraft Maintenance Manual (AMM) 20-23-11, Page Block 201

Fig. A-GBEAA

Adaption of the Plumbing Installation

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Fig. A-GBFAA

Installation of the U-Section and the

Flow Metering System (FMS)

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

(a) Remove the fire extinguishing tubes from FR36 and FR37.

Refer to Fig. A-GBEAA

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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1 Remove and discard these items from FR36RH :

Refer to Fig. A-GBEAA Sheet 01, Fig. A-GBEAA Sheet 02 and Fig. A-GBEAA

Sheet 04

1 Nut NAS1726-3E Item (113) Discard

1 Clamp NSA5516-18NJ Item (121) Discard

1 Washer NAS1149C0332R Item (144) Discard

1 Spacer NSA5527-03-03 Item (155) Discard

1 Screw NAS1096-3-14 Item (157) Discard

2 Cut the fire extinguishing tube, Item (250), at the position shown in Fig. AGBEAA Sheet 02 (Refer to AMM 20-23-11, Page Block 201).

3 Remove the fire extinguishing tube, Item (250), partly between the cut and the

outboard X-connection fitting :

1 Tube Assy, partly G2627005013000 Item (250) Discard

4 Deburr the remaining tube, Item (250), (Refer to AMM 20-23-11, Page Block

201).

5 Clean the remaining tube, Item (250), with :

Solvent General

Purpose

11-026 As required

and

Lint-Free Cotton

Cloth

19-003 As required

6 Remove and discard these items from FR37RH :

Refer to Fig. A-GBEAA Sheet 01, Fig. A-GBEAA Sheet 02 and Fig. A-GBEAA

Sheet 04

1 Nut NAS1726-3E Item (113) Discard

1 Clamp NSA5516-18NJ Item (121) Discard

1 Washer NAS1149C0332R Item (144) Discard

1 Spacer NSA5527-03-03 Item (155) Discard

1 Screw NAS1096-3-14 Item (157) Discard

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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7 Cut the fire extinguishing tube, Item (252), at the position shown in Fig. AGBEAA Sheet 02 (Refer to AMM 20-23-11, Page Block 201).

8 Remove the fire extinguishing tube, Item (252), partly between the cut and the

outboard T-connection fitting :

1 Tube Assy, partly G2627005002000 Item (252) Discard

1 Tee NSA855008D10 Item (125) Discard

9 Deburr the remaining tube, Item (252), (Refer to AMM 20-23-11, Page Block

201).

10 Clean the remaining tube, Item (252), with :

Solvent General

Purpose

11-026 As required

and

Lint-Free Cotton

Cloth

19-003 As required

(b) Install the fire extinguishing tubes on FR36 and FR37.

CAUTION: BEFORE YOU CONNECT THE FIRE EXTINGUISHING TUBES

WITH THE PERMASWAGE TOOL, MAKE SURE THAT THE FIRE

EXTINGUISHING TUBES ARE INSTALLED STRESS-FREE IN

THEIR CLAMPS.

CAUTION: DO NOT BEND THE TUBE WHEN YOU INSTALL IT. IF THE

TUBE IS BENT, IT CAN BECOME DAMAGED.

CAUTION: IF YOU USE DUST CAPS FOR THE CONTAMINATION

PROTECTION OF OPEN LINES, ALWAYS BE SURE TO

INSTALL THE CAPS AROUND THE TUBE ENDS AND NOT IN

THE TUBE ENDS. THERE CAN BE BLOCKAGE OF THE FLOW

THROUGH THE TUBES IF THESE TUBES ARE INSTALLED

ACCIDENTALLY WITH DUST CAPS IN THE TUBE ENDS.

NOTE: The fire extinguishing tubes must be installed with their related

clamps.

Refer to Fig. A-GBEAA

1 Install temporarily, Item 233, before install the other tubes.

Refer to Fig. A-GBFAA Sheet 01

2 Install the tube, Item 251, at FR36RH.

Refer to Fig. A-GBEAA Sheet 01, Fig. A-GBEAA Sheet 02 and Fig. A-GBEAA

Sheet 03

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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SERVICE BULLETIN

1 Tube Assy G2627005013000 Item 251

with :

1 Union NSA855006D10 Item 158

3 Connect the fire extinguishing tubes, Item (250), and Item 251, with the union,

Item 158, (Refer to AMM 20-23-11, Page Block 201).

D12102C07-02 PERMASWAGE

Repair Kit D12000

Series

1

NOTE: Use these swaging tools of the D12000 series :

- Head assembly D12210-56 with power unit D12010-52.

NOTE: The surface protection on both ends of the pipes must be

removed on a length of 43mm (1.692in.).

4 After the installation of the union, Item 158, perform surface protection with :

Low Voc AntiCorrosion Primer16-006F As required

and

Internal

Polyurethane

Varnish

07-017 As required

5 Install the clamp, Item 121, at FR36RH.

Fig. A-GBEAA Sheet 01, Fig. A-GBEAA Sheet 02 and Fig. A-GBEAA Sheet

03

1 Clamp NSA5516A18NJ Item 121

with :

1 Nut NAS1726-3E Item 113

1 Washer NAS1149C0332R Item 144

1 Spacer NSA5527-03-03 Item 155

1 Screw NAS1801-3-12 Item 157

6 Install temporarily, Item 234 and 238, before install the other tubes.

Refer to Fig. A-GBFAA Sheet 01

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 244

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SERVICE BULLETIN

7 Install the tube, Item 253, at FR37RH.

Refer to Fig. A-GBEAA Sheet 01, Fig. A-GBEAA Sheet 02 and Fig. A-GBEAA

Sheet 03

1 Tube Assy G2627005002000 Item 253

with :

1 Tee NSA855008D10 Item 125

1 Union NSA855006D10 Item 158

8 Connect the fire extinguishing tubes, Item (252), and Item 253, with the union,

Item 158, and on the other end with the T-fitting, Item 125 (Refer to AMM

20-23-11, Page Block 201).

NOTE: Use these swaging tools of the D12000 series :

- Head assembly D12210-56 with power unit D12010-52.

NOTE: The surface protection on the ends of the pipes must be

removed on a length of 43mm (1.692in.).

9 After the installation of the tee-fitting, Item 125, and the union, Item 158,

perform surface protection with :

Low Voc AntiCorrosion Primer16-006F As required

and

Internal

Polyurethane

Varnish

07-017 As required

10 Install the clamp, Item 121, at FR37RH.

Fig. A-GBEAA Sheet 01, Fig. A-GBEAA Sheet 02 and Fig. A-GBEAA Sheet

03

1 Clamp NSA5516A18NJ Item 121

with :

1 Nut NAS1726-3E Item 113

1 Washer NAS1149C0332R Item 144

1 Spacer NSA5527-03-03 Item 155

1 Screw NAS1801-3-12 Item 157

11 Tighten all connections of the installed fire extinguishing tubes.

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 245

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SERVICE BULLETIN

(24) Subtask 265020-831-215-001 - Install the U-section.

Work Zones and Access Panels

Zone Access/Work location

132 Work location from Frame 37 to Frame 37.1

Manpower Resources

Manhours 1.00

Minimum number of person 2

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 265020D04R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

106 NAS1149F0332P 2 WASHER

143 NAS1801-3-8 4 SCREW

144 NAS1149C0332R 5 WASHER

145 NAS1801-3-7 3 SCREW

212 G2627008001400 1 SECTION

213 F2627008100000 1 BRACKET

220 E0090-10-135NN 1 LEAD

References

Aircraft Maintenance Manual (AMM) 20-28-00, Page Block 201

Fig. A-GBFAA

Installation of the U-Section and the

Flow Metering System (FMS)

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

(a) Install the U-section between FR37RH and FR37.1.

Refer to Fig. A-GBFAA

1 Between FR37RH and FR37.1RH, install :

Refer to Fig. A-GBFAA Sheet 03, Fig. A-GBFAA Sheet 05 and Fig. A-GBFAA

Sheet 06

1 U-section G2627008001400 Item 212

1 Bracket F2627008100000 Item 213

1 Lead-Bonding E0090-10-135NN Item 220

with :

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 246

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SERVICE BULLETIN

2 Washer NAS1149F0332P Item 106

4 Screw NAS1801-3-8 Item 143

5 Washer NAS1149C0332R Item 144

3 Screw NAS1801-3-7 Item 145

NOTE (01): For the installation of the bolt (Refer to AMM 20-28-00, Page

Block 201).

NOTE (02): Seal the bonding connection by overlapping application and

identify the bonding connection by overlapping application with

blue dyed protective coating.

(25) Subtask 265020-831-217-001 - Install the Flow Metering Systems (FMS) for the Fire

Ext. Bottles No. 1 and No. 2 on the U-section.

Work Zones and Access Panels

Zone Access/Work location

132 Work location from Frame 37 to Frame 37.1

Manpower Resources

Manhours 4.00

Minimum number of person 2

Subtask elapsed time 2.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 265020D04R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

104 NAS1726-4E 2 NUT

106 NAS1149F0332P 6 WASHER

113 NAS1726-3E 3 NUT

121 NSA5516A18NJ 2 CLAMP

132 A2627048220400 6 FITTING

133 NSA8202-6 8 ORING

134 A2627048221600 2 FITTING

139 NAS1304-12 2 BOLT

140 NAS1149D0432K 10 WASHER

141 NSA5355-5CA 2 WASHER

143 NAS1801-3-8 6 SCREW

144 NAS1149C0332R 6 WASHER

145 NAS1801-3-7 4 SCREW

146 NAS1100E4-34 6 SCREW

147 A2627048920000 2 WASHER

148 NSA5516A06NJ 4 CLAMP

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 247

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@A340-500/600

SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

152 E0090-10-320NN 2 LEAD

153 E0090-10-350NN 2 LEAD

159 NAS1801-3-10 2 SCREW

160 MS21103-4 2 CLAMP

219 G2627006001000 1 TUBE

221 G2627006000800 1 TUBE

222 G2627006001800 1 TUBE

223 F2627006003600 1 TUBE

224 A2627048220200 2 RESTRCTR

225 F2627006001400 1 TUBE

226 F2627006000000 1 TUBE

227 F2627007200000 1 HOSE

228 F2627007200200 1 HOSE

229 G2627006002000 1 TUBE

230 G2627006001200 1 TUBE

231 G2627006001400 1 TUBE

232 G2627006001600 1 TUBE

233 NSA855140-22D 1 CROSS

234 G2627005013200 1 TUBE

235 MS21902W10 1 UNION

236 A2627045107800 1 TUBE

237 NSA855113-34D 1 TEE

238 G2627005003400 1 TUBE

239 MS21916W10-4 2 REDUCER

Component COMPD01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

LN9424A100 As required WIRE

Equipment BFEZ04

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

214 QA06753-03 2 FILTER

215 E61751-00-0001 2 REDUCER

216 TP0714033 2 SWITCH

217 HTE400115 2 VALVE

References

Aircraft Maintenance Manual (AMM) Task 20-28-00-912-802

Fig. A-GBFAA

Installation of the U-Section and the

Flow Metering System (FMS)

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 248

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@A340-500/600

SERVICE BULLETIN

(a) Install the Halon Filter, FIN 5010WE, for Fire Ext. Bottle No. 1.

Refer to Fig. A-GBFAA

1 On the U-section, between FR37RH and FR37.1RH, install :

Refer to Fig. A-GBFAA Sheet 01, Fig. A-GBFAA Sheet 03 and Fig. A-GBFAA

Sheet 04

1 Filter-Halon QA06753-03 Item 214

NOTE: See NOTE 03

with :

3 Washer NAS1149D0432K Item 140

3 Screw NAS1100E4-34 Item 146

and

2 O-Ring NSA8202-6 Item 133

1 Fitting A2627048221600 Item 134

NOTE: See NOTE 03

1 Fitting A2627048220400 Item 132

NOTE: See NOTE 03

2 Secure the fittings, Items 132 and 134, with :

As

required

Wire-Lock LN9424A100

3 On the fitting, Item 132, install :

1 Hose Assy F2627007200000 Item 227

NOTE (03): No lubrication on this item.

(b) Install the Pressure Reducer, FIN 5014WE, for Fire Ext. Bottle No. 1.

1 On the U-section, between FR37RH and FR37.1RH, install :

Refer to Fig. A-GBFAA Sheet 01, Fig. A-GBFAA Sheet 03 and Fig. A-GBFAA

Sheet 04

1 Reducer-Pressure E61751-00-0001 Item 215

NOTE: See NOTE 03

with :

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 249

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SERVICE BULLETIN

1 Washer-Tab A2627048920000 Item 147

2 Fitting A2627048220400 Item 132

NOTE: See NOTE 03

2 O-Ring NSA8202-6 Item 133

2 Secure the fittings, Item 132, with :

As

required

Wire-Lock LN9424A100

NOTE (03): No lubrication on this item.

(c) Install the Pressure Switch, FIN 4016WX, for Fire Ext. Bottle No. 1.

1 On the pressure reducer 5014WE, between FR37RH and FR37.1RH, install :

Refer to Fig. A-GBFAA Sheet 01, Fig. A-GBFAA Sheet 03, Fig. A-GBFAA

Sheet 04 and Fig. A-GBFAA Sheet 05

1 Tube Assy G2627006000800 Item 221

with :

1 Washer NAS1149C0332R Item 144

1 Screw NAS1801-3-7 Item 145

1 Clamp NSA5516A06NJ Item 148

and

1 Switch-Pressure TP0714033 Item 216

NOTE: See NOTE 03

2 On the pressure switch, Item 216, install :

1 Tube Assy G2627006001800 Item 222

with :

1 Washer NAS1149F0332P Item 106

1 SCREW NAS1801-3-10 Item 159

1 CLAMP MS21103-4 Item 160

NOTE (03): No lubrication on this item.

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 250

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SERVICE BULLETIN

(d) Install the Check Valve, FIN 5016WE, for Fire Ext. Bottle No. 1.

1 On the pressure reducer 5014WE, between FR37RH and FR37.1RH, install :

Refer to Fig. A-GBFAA Sheet 01, Fig. A-GBFAA Sheet 03 and Fig. A-GBFAA

Sheet 05

1 Tube Assy F2627006003600 Item 223

1 Restrictor A2627048220200 Item 224

1 Tube Assy F2627006001400 Item 225

and

1 Valve-Nonreturn HTE400115 Item 217

NOTE: See NOTE 03

2 On the check valve, Item 217, install :

1 Tube Assy F2627006000000 Item 226

with :

1 Washer NAS1149C0332R Item 144

1 Screw NAS1801-3-7 Item 145

1 Clamp NSA5516A06NJ Item 148

NOTE (03): No lubrication on this item.

(e) Install the Halon Filter, FIN 5011WE, for Fire Ext. Bottle No. 2.

Refer to Fig. A-GBFAA

1 On the U-section, between FR37RH and FR37.1RH, install :

Refer to Fig. A-GBFAA Sheet 01, Fig. A-GBFAA Sheet 03 and Fig. A-GBFAA

Sheet 04

1 Filter-Halon QA06753-03 Item 214

NOTE: See NOTE 03

with :

3 Washer NAS1149D0432K Item 140

3 Screw NAS1100E4-34 Item 146

and

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 251

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SERVICE BULLETIN

2 O-Ring NSA8202-6 Item 133

1 Fitting A2627048221600 Item 134

NOTE: See NOTE 03

1 Fitting A2627048220400 Item 132

NOTE: See NOTE 03

2 Secure the fittings, Items 132 and 134, with :

As

required

Wire-Lock LN9424A100

3 On the fitting, Item 132, install :

1 Hose Assy F2627007200200 Item 228

NOTE: See NOTE 03

NOTE (03): No lubrication on this item.

(f) Install the Pressure Reducer, FIN 5015WE, for Fire Ext. Bottle No. 2.

1 On the U-section, between FR37RH and FR37.1RH, install :

Refer to Fig. A-GBFAA Sheet 01, Fig. A-GBFAA Sheet 03 and Fig. A-GBFAA

Sheet 04

1 Reducer-Pressure E61751-00-0001 Item 215

NOTE: See NOTE 03

with :

1 Washer-Tab A2627048920000 Item 147

2 Fitting A2627048220400 Item 132

NOTE: See NOTE 03

2 O-Ring NSA8202-6 Item 133

2 Secure the fittings, Item 132, with :

As

required

Wire-Lock LN9424A100

NOTE (03): No lubrication on this item.

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 252

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SERVICE BULLETIN

(g) Install the Pressure Switch, FIN 4018WX, for Fire Ext. Bottle No. 2

1 On the pressure reducer 5015WE, between FR37RH and FR37.1RH, install :

Refer to Fig. A-GBFAA Sheet 01, Fig. A-GBFAA Sheet 03 and Fig. A-GBFAA

Sheet 04

1 Tube Assy G2627006001000 Item 219

with :

1 Washer NAS1149C0332R Item 144

1 Screw NAS1801-3-7 Item 145

1 Clamp NSA5516A06NJ Item 148

and

1 Switch-Pressure TP0714033 Item 216

NOTE: See NOTE 03

2 On the pressure switch, Item 216, install :

1 Tube Assy G2627006002000 Item 229

with :

1 Washer NAS1149F0332P Item 106

1 SCREW NAS1801-3-10 Item 159

1 CLAMP MS21103-4 Item 160

NOTE (03): No lubrication on this item.

(h) Install the Check Valve, FIN 5017WE, for Fire Ext. Bottle No. 2

1 On the pressure reducer 5015WE, between FR37RH and FR37.1RH, install :

Refer to Fig. A-GBFAA Sheet 01, Fig. A-GBFAA Sheet 03 and Fig. A-GBFAA

Sheet 05

1 Tube Assy G2627006001200 Item 230

1 Restrictor A2627048220200 Item 224

1 Tube Assy G2627006001400 Item 231

and

1 Valve-Nonreturn HTE400115 Item 217

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 253

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@A340-500/600

SERVICE BULLETIN

NOTE: See NOTE 03

2 On the check valve, Item 217, install :

1 Tube Assy G2627006001600 Item 232

with :

1 Washer NAS1149C0332R Item 144

1 Screw NAS1801-3-7 Item 145

1 Clamp NSA5516A06NJ Item 148

1 Nut NAS1726-3E Item 113

NOTE (03): No lubrication on this item.

(i) Install the new plumbing and rod ends between FR36RH and FR37.1

1 Between FR36RH and FR37.1, install the rod ends :

Refer to Fig. A-GBFAA Sheet 01 and Fig. A-GBFAA Sheet 02

2 Rod End NSA8141-04R Item (135) Retained at

removal

2 Rod End NSA8140-04RK Item (137) Retained at

removal

with :

2 Nut NAS1726-4E Item 104

2 BOLT NAS1304-12 Item 139

4 Washer NAS1149D0432K Item 140

2 Nut NAS509-5 Item (136) Retained at

removal

2 Washer-Lock NSA5355-5CA Item 141

and

2 Lead-Bonding E0090-10-320NN Item 152

2 Lead-Bonding E0090-10-350NN Item 153

with :

4 Washer NAS1149F0332P Item 106

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 254

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SERVICE BULLETIN

4 Screw NAS1801-3-8 Item 143

NOTE: Do the electrical bonding (Refer to AMM Task

20-28-00-912-802)

2 Between FR36RH and FR37.1, install the plumbing :

Refer to Fig. A-GBFAA Sheet 01, Fig. A-GBFAA Sheet 02 and Fig. A-GBFAA

Sheet 03

2 Hose A2627045200400 Item (209) Retained at

removal

2 Hose Assy F2627007100200 Item (210) Retained at

removal

1 Cross NSA855140-22D Item 233

1 Tube Assy G2627005013200 Item 234

1 Union MS21902W10 Item 235

with :

2 Screw NAS1801-3-8 Item 143

2 Washer NAS1149C0332R Item 144

2 Nut NAS1726-3E Item 113

2 Clamp NSA5516A18NJ Item 121

and

1 Tube Assy A2627045107800 Item 236

1 Tee NSA855113-34D Item 237

1 Tube Assy G2627005003400 Item 238

2 Reducer MS21916W10-4 Item 239

(26) Subtask 265020-831-211-002 - Install the Fire Extinguishing Bottles 4005WX and

4010WX.

Work Zones and Access Panels

Zone Access/Work location

132 Access Panel 132PM

Work location from Frame 35 to Frame 37.1

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 255

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@A340-500/600

SERVICE BULLETIN

Manpower Resources

Manhours 2.00

Minimum number of person 2

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 265020D04R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

100 NAS1726-5E 8 NUT

101 NAS1305-2 8 BOLT

103 NAS1304-9 2 BOLT

104 NAS1726-4E 2 NUT

105 NAS563-11 4 BOLT

106 NAS1149F0332P 4 WASHER

Component COMPD01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

LN9424A100 As required WIRE

References

Aircraft Maintenance Manual (AMM) 20-28-00, Page Block 201

26-23-41, Page Block 401

Fig. A-GBJAA

Installation of Fire Extinguishing Bottles

FIN 4005WX and FIN 4010WX with

Cartridges.

Sheet 01

Sheet 02

Sheet 03

Refer to Fig. A-GBJAA

(a) Install the fire extinguishing bottle 1 (FWD) 4005WX.

1 Between FR36RH and FR37RH, install the fire extinguishing bottle 4005WX

(Refer to AMM 26-23-41, Page Block 401) :

Refer to Fig. A-GBJAA Sheet 01 and Fig. A-GBJAA Sheet 02 :

1 Extinguisher-Fire 472931-3 Item (204) Retained at

removal

with :

4 Nut NAS1726-5E Item 100

4 Bolt NAS1305-2 Item 101

1 Bolt NAS1304-9 Item 103

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 256

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SERVICE BULLETIN

1 Nut NAS1726-4E Item 104

2 Bolt NAS563-11 Item 105

NOTE: See NOTE 01, 02, 03.

2 Washer NAS1149F0332P Item 106

2 Secure the coupling nuts of the fire extinguishing discharge heads and the

bolts, Item 105, with :

As

required

Wire-Lock LN9424A100

NOTE (01): Torque tighten the bolt to between 0.30da.Nm (26.552lbf.in)

and 0.35da.Nm (30.977lbf.in).

NOTE (02): For the installation of the bolt refer to the electrical bonding of

components with conductive screws and bolts and bonding

straps according toAMM 20-28-00, Page Block 201.

NOTE (03): Seal the bonding connection by overlapping application and

identify the bonding connection by overlapping application with

blue dyed protective coating.

(b) Install the fire extinguishing bottle 2 (AFT) 4010WX.

1 Between FR37RH and FR37.1RH, install the fire extinguishing bottle 4010WX

(Refer to AMM 26-23-41, Page Block 401) :

Refer to Fig. A-GBJAA Sheet 01 and Fig. A-GBJAA Sheet 03 :

1 Extinguisher-Fire 472625-3 Item (203)

with :

4 Nut NAS1726-5E Item 100

4 Bolt NAS1305-2 Item 101

1 Bolt NAS1304-9 Item 103

1 Nut NAS1726-4E Item 104

2 Bolt NAS563-11 Item 105

NOTE: See NOTE 01, 02, 03.

2 Washer NAS1149F0332P Item 106

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 257

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SERVICE BULLETIN

2 Secure the coupling nuts of the fire extinguishing discharge heads and the

bolts, Item 105, with :

As

required

Wire-Lock LN9424A100

NOTE (01): Torque tighten the bolt to between 0.30da.Nm (26.552lbf.in)

and 0.35da.Nm (30.977lbf.in).

NOTE (02): For the installation of the bolt refer to the electrical bonding of

components with conductive screws and bolts and bonding

straps according toAMM 20-28-00, Page Block 201.

NOTE (03): Seal the bonding connection by overlapping application and

identify the bonding connection by overlapping application with

blue dyed protective coating.

(27) Subtask 265020-831-214-001 - Install the new identification placards.

Work Zones and Access Panels

Zone Access/Work location

132 Work location from Frame 37 to Frame 37.1

Manpower Resources

Manhours 1.50

Minimum number of person 2

Subtask elapsed time 0.75

Skills NON SPECIFIC

Material necessary to do the job

Kit 265020D04R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

240 F2627004120800 1 PLACARD

241 F2627004121400 1 PLACARD

242 F2627004121200 1 PLACARD

243 F2627004120400 1 PLACARD

244 F2627004120600 1 PLACARD

245 F2627004121600 1 PLACARD

246 F2627004121800 1 PLACARD

247 F2627004121000 1 PLACARD

248 G2627004020200 1 PLACARD

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Abrasion Resistant Coating

(Teflon Polyuret)

07-003 As required

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 258

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SERVICE BULLETIN

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

General Purpose Adhesive

Honeycomb Filler

08-554 As required

References

Fig. A-GBFAA

Installation of the U-Section and the

Flow Metering System (FMS)

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

(a) Install the identification placards 4010WX, 4016WX, 4018WX, 5010WE, 5011WE,

5014WE, 5015WE, 5016WE, 5017WE, between FR37 and FR37.1.

Refer to Fig. A-GBFAA

1 Between FR37RH and FR37.1RH, install :

Refer to Fig. A-GBFAA Sheet 01, Fig. A-GBFAA Sheet 03 and Fig. A-GBFAA

Sheet 06

1 Placard F2627004120800 Item 240

1 Placard F2627004121400 Item 241

1 Placard F2627004121200 Item 242

1 Placard F2627004120400 Item 243

1 Placard F2627004120600 Item 244

1 Placard F2627004121600 Item 245

1 Placard F2627004121800 Item 246

1 Placard F2627004121000 Item 247

1 Placard G2627004020200 Item 248

Bond the placard, Item 248, with :

General Purpose

Adhesive

Honeycomb Filler

08-554 As required

Protect the placard, Item 248, with :

Abrasion Resistant

Coating (Teflon

Polyuret)

07-003 As required

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 259

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SERVICE BULLETIN

**CONF 004

(1) Subtask 265020-831-001-005 - Modify the Equipment and the Wiring in the RH

Overhead Panel 212VU.

Work Zones and Access Panels

Zone Access/Work location

212 Work location Electrical panel 212VU

Manpower Resources

Manhours 12.00

Minimum number of person 1

Subtask elapsed time 12.00

Skills ELECTRICAL

Material necessary to do the job

Kit 265020A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

2 ASNA2083BG2-10 7 Screw

6 NSA937901MA2206 1 Module

7 NSA937901FM 1 Module

10 F9251088400000 1 Plate

F1131101500000 Placard

F9000095226495 Bundle

NAS1102-04-5 44 Screw

NSA935401-03 50 TIE

NSA937901E2 1 Label

Kit 265020A05R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 F33110381A00 1 Plate

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Pure Mineral Vaseline Or

Petro-Latum

04-012 As required

Electrical Bond Varnish 07-001B As required

Sealant, High Temperature 08-007C As required

References

Aircraft Maintenance Manual (AMM) Task 11-00-00-400-802

Task 20-28-00-912-802

Fig. A-FBBAA

Modification of the Equipment in the RH

Overhead Panel 212VU

Sheet 01

Sheet 02

Sheet 03

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 260

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References

Fig. A-FCAAA

Modification of the Wiring in the RH

Overhead Panel 212VU

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

(a) Remove and disconnect the RH overhead panel 212VU.

NOTE: Retain it.

(b) Modify the equipment in the RH overhead panel 212VU.

1 Remove the integrally lighted plate (212LF).

a Remove as shown in Fig. A-FBBAA Sheet 01 :

FIN 212LF

1 Plate-Integrally Lighted F33110321A00 Item (1) Discard

attached with :

7 Screw ASNA2083BG2-10 Item (2) Discard

2 Remove the indicator light BTL3 (5WX).

a Remove as shown in Fig. A-FBBAA Sheet 01 and Fig. A-FBBAA Sheet

02, Detail B :

FIN 5WX

1 Light-Indicator ABS0951A0LP110 Item (3) Discard

FIN 5WX1

1 Sleeve E0416-02 Item (4) Discard

FIN 5WXA

1 Connector E0417A01S Item (5) Discard

NOTE: Remove and discard the attachment hardware.

3 Replace the 212VU front plate.

a Remove and retain all the items of equipment that are installed on the

front plate.

b Remove as shown in Fig. A-FBBAA Sheet 01 :

1 Plate Assy- Front

212VU

F9251602100000 Item (10) Discard

attached with :

8 Screw NAS1102-06-5 Item (11) Retain

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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SERVICE BULLETIN

c On the new front plate, bond the placards (Refer to AMM Task

11-00-00-400-802) supplied in :

Placard Set-212VU F1131101500000

NOTE: Bond the applicable placards at the same locations as on

the old front plate. Discard the unused placards.

d Install as shown in Fig. A-FBBAA Sheet 03 :

1 Plate Assy- Front

212VU

F9251088400000 Item 10

attach with :

8 Screw NAS1102-06-5 Item (11)

NOTE: The screws Item (11) were retained at the removal.

e Install again all the items of equipment that you removed and retained

before the replacement of the front plate and attach with :

44 Screw NAS1102-04-5

Safety the screws with :

Sealant, High

Temperature

08-007C As required

NOTE: Replace the screws if they are damaged during the

removal. The quantity of screws to be replaced depends

on aircraft configuration (44 is the maximum).

f Do the electrical bonding (Refer to AMM Task 20-28-00-912-802) with :

Pure Mineral

Vaseline Or PetroLatum

04-012 As required

and

Electrical Bond

Varnish

07-001B As required

4 Modify the terminal block (582VT) as shown in Fig. A-FBBAA Sheet 01 and

Fig. A-FBBAA Sheet 02, Detail C.

a Remove from position 2 :

FIN 582VT2

1 Module-False NSA937901FM Item (6) Discard

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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b Remove from position 3 :

FIN 582VT3

1 Module NSA937901MA2204 Item (7) Discard

c Install at position 2 as shown in :

FIN 582VT2

1 Module NSA937901MA2206 Item 6

with

1 Label-Identification NSA937901E2

d Install at position 3 as shown in :

FIN 582VT3

1 Module-False NSA937901FM Item 7

5 Install the new integrally lighted plate (212LF).

a Install as shown in Fig. A-FBBAA Sheet 03 :

FIN 212LF

1 Plate-Integrally Lighted F33110381A00 Item 1

attach with :

7 Screw ASNA2083BG2-10 Item 2

(c) Modify the wiring in the RH overhead panel 212VU.

1 Remove the wires as shown in the wiring diagrams Fig. A-FCAAA Sheet 01,

Fig. A-FCAAA Sheet 02 and as given in the hook-up chart lines :

- 1 thru 13 (Refer to Fig. A-FCAAA Sheet 04).

2 Modify the connections of the wires as shown in the wiring diagrams Fig. AFCAAA Sheet 02, Fig. A-FCAAA Sheet 03 and as given in the hook-up chart

lines :

- 17 thru 24 (Refer to Fig. A-FCAAA Sheet 04)

- 1 and 2 (Refer to Fig. A-FCAAA Sheet 05).

3 Install the wires as shown in the wiring diagram Fig. A-FCAAA Sheet 03 and

as given in the hook-up chart lines :

- 6 thru 12 (Refer to Fig. A-FCAAA Sheet 05), supplied in :

Bundle F9000095226495

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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4 Attach the wires with :

50 Tie-Cable NSA935401-03

(d) Install the RH overhead panel 212VU.

(2) Subtask 265020-831-002-001 - Modify the Equipment and the Wiring in the

Emergency Power Center 740VU.

Work Zones and Access Panels

Zone Access/Work location

121 Access Door 821, Door 132AZ

Work location Electrical panel 740VU

Manpower Resources

Manhours 3.50

Minimum number of person 1

Subtask elapsed time 3.50

Skills ELECTRICAL

Material necessary to do the job

Kit 265020A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

F9000095226495 Bundle

NSA935401-03 50 TIE

NSA935401-05 50 TIE

References

Fig. A-FBCAA

Modification of the Equipment in the

Emergency Power Center 740VU

Sheet 01

Fig. A-FCBAA

Modification of the Wiring in the

Emergency Power Center 740VU

Sheet 01

Sheet 02

(a) Open the emergency power center 740VU.

(b) Remove the wires as shown in the wiring diagram Fig. A-FCBAA Sheet 01 and as

given in the hook-up chart lines :

- 1 thru 8 (Refer to Fig. A-FCBAA Sheet 02).

(c) Modify the terminal block (703VT) as shown in Fig. A-FBCAA Sheet 01.

1 Remove from position 21 :

1 Clamp-End NSA937901S Retain

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 264

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@A340-500/600

SERVICE BULLETIN

2 Remove from position 20 :

FIN 703VT20

1 Module NSA937901MA2004 Item (7) Discard

3 Install at position 20 :

1 Clamp-End NSA937901S

NOTE: The end clamp was retained at the removal.

(d) Install the wire as shown in the wiring diagram Fig. A-FCBAA Sheet 01 and as

given in the hook-up chart line :

- 12 (Refer to Fig. A-FCBAA Sheet 02), supplied in :

Bundle F9000095226495

(e) Attach the wire with :

50 Tie-Cable NSA935401-03

50 Tie-Cable NSA935401-05

(f) Close the emergency power center 740VU.

(3) Subtask 265020-831-003-001 - Modify the Equipment and the Wiring in the AC/DC

Main Power Center 710VU.

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 821, Door 132AZ

Work location Electrical panel 710VU

Manpower Resources

Manhours 3.50

Minimum number of person 1

Subtask elapsed time 3.50

Skills ELECTRICAL

Material necessary to do the job

Kit 265020A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

F9000095226495 Bundle

NSA935401-03 50 TIE

NSA935401-05 50 TIE

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 265

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SERVICE BULLETIN

References

Fig. A-FBDAA

Modification of the Equipment in the

AC/DC Main Power Center 710VU

Sheet 01

Fig. A-FCCAA

Modification of the Wiring in the AC/DC

Main Power Center 710VU

Sheet 01

Sheet 02

(a) Open the AC/DC main power center 710VU.

(b) Remove the wires as shown in the wiring diagram Fig. A-FCCAA Sheet 01 and as

given in the hook-up chart lines :

- 1 thru 8 (Refer to Fig. A-FCCAA Sheet 02).

(c) Modify the terminal block (1712VT) as shown in Fig. A-FBDAA Sheet 01.

1 Remove from position 18 :

1 Clamp-End NSA937901S Retain

2 Remove from position 17 :

FIN 1712VT17

1 Module NSA937901MA2004 Item (7) Discard

3 Install at position 17 :

1 Clamp-End NSA937901S

NOTE: The end clamp was retained at the removal.

(d) Install the wire as shown in the wiring diagram Fig. A-FCCAA Sheet 01 and as

given in the hook-up chart line :

- 12 (Refer to Fig. A-FCCAA Sheet 02), supplied in :

Bundle F9000095226495

(e) Attach the wire with :

50 Tie-Cable NSA935401-03

50 Tie-Cable NSA935401-05

(f) CLose the AC/DC main power center 710VU.

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 266

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SERVICE BULLETIN

(4) Subtask 265020-831-004-001 - Modify the Equipment and the Wiring in the LH

Relay Box 751VU.

Work Zones and Access Panels

Zone Access/Work location

121 Access Door 821, Door 132AZ

Work location Electrical panel 751VU

Manpower Resources

Manhours 3.50

Minimum number of person 1

Subtask elapsed time 3.50

Skills ELECTRICAL

References

Fig. A-FBEAA

Modification of the Equipment in the LH

Relay Box 751VU

Sheet 01

Fig. A-FCDAA

Modification of the Wiring in the LH

Relay Box 751VU

Sheet 01

Sheet 02

(a) Open the LH relay box 751VU.

(b) Remove the wires as shown in the wiring diagram Fig. A-FCDAA Sheet 01 and as

given in the hook-up chart lines :

- 1 thru 12 (Refer to Fig. A-FCDAA Sheet 02).

(c) Remove from position E93, as shown in Fig. A-FBEAA Sheet 01 :

FIN 10WX

1 Relay E0245-28A0 Item (8) Discard

FIN 10WXA

1 Base E0250A0S Item (9) Discard

NOTE: Remove and discard the attachment hardware and the related

placard(s).

(d) Remove from position E89, as shown in Fig. A-FBEAA Sheet 01 :

FIN 11WX

1 Relay E0245-28A0 Item (8) Discard

FIN 11WXA

1 Base E0250A0S Item (9) Discard

NOTE: Remove and discard the attachment hardware and the related

placard(s).

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 267

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SERVICE BULLETIN

(e) Close the LH relay box 751VU.

(5) Subtask 265020-831-005-001 - Modify the Equipment and the Wiring in the RH

Relay Box 752VU.

Work Zones and Access Panels

Zone Access/Work location

122 Access Door 821, Door 132AZ

Work location Electrical panel 752VU

Manpower Resources

Manhours 3.50

Minimum number of person 1

Subtask elapsed time 3.50

Skills ELECTRICAL

References

Fig. A-FBFAA

Modification of the Equipment in the RH

Relay Box 752VU

Sheet 01

Fig. A-FCEAA

Modification of the Wiring in the RH

Relay Box 752VU

Sheet 01

Sheet 02

(a) Open the RH relay box 752VU.

(b) Remove the wires as shown in the wiring diagram Fig. A-FCEAA Sheet 01 and as

given in the hook-up chart lines :

- 1 thru 12 (Refer to Fig. A-FCEAA Sheet 02).

(c) Remove from position B37, as shown in Fig. A-FBFAA Sheet 01 :

FIN 12WX

1 Relay E0245-28A0 Item (8) Discard

FIN 12WXA

1 Base E0250A0S Item (9) Discard

NOTE: Remove and discard the attachment hardware and the related

placard(s).

(d) Remove from position B33, as shown in Fig. A-FBFAA Sheet 01 :

FIN 13WX

1 Relay E0245-28A0 Item (8) Discard

FIN 13WXA

1 Base E0250A0S Item (9) Discard

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 268

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SERVICE BULLETIN

NOTE: Remove and discard the attachment hardware and the related

placard(s).

(e) Close the RH relay box 752VU.

(6) Subtask 265020-831-006-001 - Modify the Equipment and the Wiring in the Main

Rack 800VU.

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 821, Door 132AZ

Work location Electrical panel 800VU

Manpower Resources

Manhours 8.00

Minimum number of person 2

Subtask elapsed time 4.00

Skills ELECTRICAL

Material necessary to do the job

Kit 265020A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

7 NSA937901FM 1 Module

F9000095226495 Bundle

NSA935401-03 200 TIE

NSA935401-05 200 TIE

NSA935401-08 200 Tie

References

Aircraft Maintenance Manual (AMM) Task 26-16-34-000-801

Task 26-16-34-400-801

Fig. A-FBGAA

Modification of the Equipment in the

Main Rack 800VU

Sheet 01

Fig. A-FCFAA

Modification of the Wiring in the Main

Rack 800VU

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

Fig. A-FCGAA

Modification of the Pin Programming in

the Main Rack 800VU

Sheet 01

Sheet 02

(a) Remove and retain the SDCU (20WH) (Refer to AMM Task 26-16-34-000-801).

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 269

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SERVICE BULLETIN

(b) Remove the wires as shown in the wiring diagrams Fig. A-FCFAA Sheet 01, Fig. AFCFAA Sheet 02, Fig. A-FCFAA Sheet 03, and as given in the hook-up chart lines :

- 1 thru 25 (Refer to Fig. A-FCFAA Sheet 05)

- 1 thru 3 (Refer to Fig. A-FCFAA Sheet 06).

(c) Modify the terminal block (2900VT) as shown in Fig. A-FBGAA Sheet 01.

1 Remove from position 50 :

FIN 2900VT50

1 Module NSA937901MA2011 Item (7) Discard

2 Install at position 50 :

FIN 2900VT50

1 Module-False NSA937901FM Item 7

(d) Install the wires as shown in the wiring diagram Fig. A-FCFAA Sheet 04 and as

given in the hook-up chart lines :

- 7 thru 18 (Refer to Fig. A-FCFAA Sheet 06), supplied in :

Bundle F9000095226495

(e) Modify the connection of the wires as shown in the wiring diagram Fig. A-FCGAA

Sheet 01 and as given in the hook-up chart lines :

- 1 thru 4 (Refer to Fig. A-FCGAA Sheet 02).

(f) Attach the wires with :

200 Tie-Cable NSA935401-03

200 Tie-Cable NSA935401-05

200 Tie-Cable NSA935401-08

(g) Install the SDCU (20WH) (Refer to AMM Task 26-16-34-400-801).

(7) Subtask 265020-831-007-001 - Modify the Wiring between the Main Rack Shelf

801VU and the LH Relay Box 751VU.

Work Zones and Access Panels

Zone Access/Work location

121 Access Door 821, Door 132AZ

Work location from Electrical panel 801VU to Electrical panel

751VU

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 270

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SERVICE BULLETIN

Manpower Resources

Manhours 3.50

Minimum number of person 1

Subtask elapsed time 3.50

Skills ELECTRICAL

Material necessary to do the job

Kit 265020A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

NSA936604CA0931 8 Cap

References

Fig. A-FBAAA

Location of the Working Areas

Sheet 01

Fig. A-FCHAA

Modification of the Wiring between the

Main Rack Shelf 801VU and the LH

Relay Box 751VU

Sheet 01

Sheet 02

(a) Modify the connections of the wires as shown in the wiring diagram Fig. A-FCHAA

Sheet 01 and as given in the hook-up chart lines :

- 1 thru 8 (Refer to Fig. A-FCHAA Sheet 02).

(b) Install on the stowed wires ends :

8 Cap-Sealing NSA936604CA0931

(8) Subtask 265020-831-008-001 - Modify the Wiring between the Main Rack Shelf

802VU and the RH Relay Box 752VU.

Work Zones and Access Panels

Zone Access/Work location

122 Access Door 821, Door 132AZ

Work location from Electrical panel 802VU to Electrical panel

752VU

Manpower Resources

Manhours 3.50

Minimum number of person 1

Subtask elapsed time 3.50

Skills ELECTRICAL

References

Fig. A-FBAAA

Location of the Working Areas

Sheet 01

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 271

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SERVICE BULLETIN

References

Fig. A-FCJAA

Modification of the Wiring between the

Main Rack Shelf 802VU and the RH

Relay Box 752VU

Sheet 01

Sheet 02

(a) Remove the wires as shown in the wiring diagram Fig. A-FCJAA Sheet 01 and as

given in the hook-up chart lines :

- 1 thru 4 (Refer to Fig. A-FCJAA Sheet 02).

(9) Subtask 265020-831-009-001 - Modify the Wiring between the Emergency Power

Center 740VU and the LH Relay Box 751VU.

Work Zones and Access Panels

Zone Access/Work location

121 Access Door 821, Door 132AZ

Work location from Electrical panel 740VU to Electrical panel

751VU

Manpower Resources

Manhours 3.50

Minimum number of person 1

Subtask elapsed time 3.50

Skills ELECTRICAL

References

Fig. A-FBAAA

Location of the Working Areas

Sheet 01

Fig. A-FCKAA

Modification of the Wiring between the

Emergency Power Center 740VU and

the LH Relay Box 751VU

Sheet 01

Sheet 02

(a) Remove the wires as shown in the wiring diagram Fig. A-FCKAA Sheet 01 and as

given in the hook-up chart lines :

- 1 thru 4 (Refer to Fig. A-FCKAA Sheet 02).

(10) Subtask 265020-831-010-001 - Modify the Wiring between the AC/DC Main Power

Center 715VU and the RH Relay Box 752VU.

Work Zones and Access Panels

Zone Access/Work location

122 Access Door 821, Door 132AZ

Work location from Electrical panel 715VU to Electrical panel

752VU

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 272

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Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

Manpower Resources

Manhours 3.50

Minimum number of person 1

Subtask elapsed time 3.50

Skills ELECTRICAL

References

Fig. A-FBAAA

Location of the Working Areas

Sheet 01

Fig. A-FCLAA

Modification of the Wiring between the

AC/DC Main Power Center 715VU and

the RH Relay Box 752VU

Sheet 01

Sheet 02

(a) Remove the wires as shown in the wiring diagram Fig. A-FCLAA Sheet 01 and as

given in the hook-up chart lines :

- 1 thru 4 (Refer to Fig. A-FCLAA Sheet 02).

(11) Subtask 265020-831-011-001 - Modify the Wiring between the Main Rack Shelf

801VU and the Avionics Compartment at FR2.

Work Zones and Access Panels

Zone Access/Work location

From 121 Access Door 821, Door 132AZ

Work location Electrical panel 801VU

To 211 Access Door 831, Door 841

Panel 211EW

Work location Frame 2

Manpower Resources

Manhours 3.50

Minimum number of person 1

Subtask elapsed time 3.50

Skills ELECTRICAL

Material necessary to do the job

Kit 265020A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

NSA936604CA0931 2 Cap

References

Fig. A-FBAAA

Location of the Working Areas

Sheet 01

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 273

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@A340-500/600

SERVICE BULLETIN

References

Fig. A-FCMAA

Modification of the Wiring between the

Main Rack Shelf 801VU and the

Avionics Compartment at FR2

Sheet 01

Sheet 02

(a) Modify the connections of the wire as shown in the wiring diagram Fig. A-FCMAA

Sheet 01 and as given in the hook-up chart lines :

- 1 and 2 (Refer to Fig. A-FCMAA Sheet 02).

(b) Install on the stowed wire ends :

2 Cap-Sealing NSA936604CA0931

(12) Subtask 265020-831-012-001 - Modify the Wiring between the RH Overhead Panel

212VU and the Avionics Compartment (LH Side).

Work Zones and Access Panels

Zone Access/Work location

From 212 Access Door 831, Door 841

Work location Electrical panel 212VU

To 121 Access Door 821, Door 132AZ

Work location Electrical panel 751VU

Electrical panel 740VU

Frame 2

Electrical panel 801VU

Manpower Resources

Manhours 10.00

Minimum number of person 2

Subtask elapsed time 5.00

Skills ELECTRICAL

Material necessary to do the job

Kit 265020A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

F9000095226495 Bundle

NSA935401-05 200 TIE

NSA935401-08 200 Tie

NSA936604CA0931 8 Cap

References

Fig. A-FBAAA

Location of the Working Areas

Sheet 01

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 274

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SERVICE BULLETIN

References

Fig. A-FCNAA

Modification of the Wiring between the

RH Overhead Panel 212VU and the

Avionics Compartment (LH Side)

Sheet 01

Sheet 02

Sheet 03

(a) Modify the connections of the wires as shown in the wiring diagrams Fig. A-FCNAA

Sheet 01, Fig. A-FCNAA Sheet 02 and as given in the hook-up chart lines :

- 1 thru 8 (Refer to Fig. A-FCNAA Sheet 03).

(b) Install on the stowed wires ends :

8 Cap-Sealing NSA936604CA0931

(c) Install the wires as shown in the wiring diagram Fig. A-FCNAA Sheet 01 and as

given in the hook-up chart lines :

- 12 and 13 (Refer to Fig. A-FCNAA Sheet 02), supplied in :

Bundle F9000095226495

(d) Attach the wires with :

200 Tie-Cable NSA935401-05

200 Tie-Cable NSA935401-08

(13) Subtask 265020-831-013-001 - Modify the Wiring between the RH Overhead Panel

212VU and the Avionics Compartment (RH Side).

Work Zones and Access Panels

Zone Access/Work location

From 212 Access Door 831, Door 841

Work location Electrical panel 212VU

To 122 Access Door 821, Door 132AZ

Panel 131BA

Work location Electrical panel 752VU

Electrical panel 715VU

Electrical panel 802VU

Frame 20

Manpower Resources

Manhours 10.00

Minimum number of person 2

Subtask elapsed time 5.00

Skills ELECTRICAL

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 275

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@A340-500/600

SERVICE BULLETIN

Material necessary to do the job

Kit 265020A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

F9000095226495 Bundle

NSA935401-05 200 TIE

NSA935401-08 200 Tie

NSA936604CA0931 10 Cap

References

Fig. A-FBAAA

Location of the Working Areas

Sheet 01

Fig. A-FCPAA

Modification of the Wiring between the

RH Overhead Panel 212VU and the

Avionics Compartment (RH Side)

Sheet 01

Sheet 02

Sheet 03

(a) Modify the connections of the wires as shown in the wiring diagram Fig. A-FCPAA

Sheet 01, Fig. A-FCPAA Sheet 02 and as given in the hook-up chart lines :

- 1 thru 12 (Refer to Fig. A-FCPAA Sheet 03).

(b) Install on the stowed wires ends :

10 Cap-Sealing NSA936604CA0931

(c) Install the wires as shown in the wiring diagram Fig. A-FCPAA Sheet 01 and as

given in the hook-up chart lines :

- 9 and 10 (Refer to Fig. A-FCPAA Sheet 02), supplied in :

Bundle F9000095226495

(d) Attach the wires with :

200 Tie-Cable NSA935401-05

200 Tie-Cable NSA935401-08

(14) Subtask 265020-831-201-001 - Remove the Fire Extinguishing Bottles, 4010WX,

4005WX and 4020WX.

Work Zones and Access Panels

Zone Access/Work location

132 Access Panel 132PM

Work location from Frame 35 to Frame 37.1

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 276

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@A340-500/600

SERVICE BULLETIN

Manpower Resources

Manhours 3.00

Minimum number of person 2

Subtask elapsed time 1.50

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 26-23-41, Page Block 401

Fig. A-GBAAA

Removal of Fire Extinguishing Bottles

4005WX, 4010WX and 4020WX with

Cartridges.

Sheet 01

Sheet 02

Sheet 03

(a) Remove the Fire Extinguishing Bottle 2 (FWD), 4010WX.

Refer to Fig. A-GBAAA

1 Between FR35RH and FR36RH, remove the fire extinguishing bottle 4010WX

(Refer to AMM 26-23-41, Page Block 401) :

Refer to Fig. A-GBAAA Sheet 01, Fig. A-GBAAA Sheet 02 and Fig. A-GBAAA

Sheet 03, Detail D :

1 Extinguisher-Fire 35200003-2 Item (200) Retain

with :

4 Nut NAS1726-5E Item (100) Discard

4 Bolt NAS1305-2 Item (101) Discard

1 Bolt NAS1304-9 Item (103) Discard

1 Nut NAS1726-4E Item (104) Discard

2 Screw Item (260)

2 Washer Item (261)

2 Nut Item (262)

NOTE: Retain the Items (260), (261) and (262).

(b) Remove the Fire Extinguishing Bottle 1 (MID), 4005WX.

Refer to Fig. A-GBAAA

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 277

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@A340-500/600

SERVICE BULLETIN

1 Between FR36RH and FR37RH, remove the fire extinguishing bottle 4005WX

(Refer to AMM 26-23-41, Page Block 401) :

Refer to Fig. A-GBAAA Sheet 01 and Fig. A-GBAAA Sheet 03 :

1 Extinguisher-Fire 34900008-2 Item (201) Retain

with :

4 Nut NAS1726-5E Item (100) Discard

4 Bolt NAS1305-2 Item (101) Discard

1 Bolt NAS1304-9 Item (103) Discard

1 Nut NAS1726-4E Item (104) Discard

2 Screw Item (260)

2 Washer Item (261)

2 Nut Item (262)

NOTE: Discard the Items (260), (261) and (262).

(c) Remove the Fire Extinguishing Bottle 3 (AFT), 4020WX.

Refer to Fig. A-GBAAA

1 Between FR37RH and FR37.1RH, remove the fire extinguishing bottle

4020WX (Refer to AMM 26-23-41, Page Block 401) :

Refer to Fig. A-GBAAA Sheet 01, Fig. A-GBAAA Sheet 02 and Fig. A-GBAAA

Sheet 03, Detail D :

1 Extinguisher-Fire 35200003-2 Item (200) Discard

with :

4 Nut NAS1726-5E Item (100) Discard

4 Bolt NAS1305-2 Item (101) Discard

1 Bolt NAS1304-9 Item (103) Discard

1 Nut NAS1726-4E Item (104) Discard

2 Screw Item (260)

2 Washer Item (261)

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 278

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@A340-500/600

SERVICE BULLETIN

2 Nut Item (262)

NOTE: Retain the Items (260), (261) and (262).

(15) Subtask 265020-831-202-001 - Remove the 4 Flow Metering Compact Units (FMCU),

FIN 4031WX, 4032WX, 4033WX and 4034WX.

Work Zones and Access Panels

Zone Access/Work location

132 Access Panel 132PM

Work location from Frame 35 to Frame 37.1

Manpower Resources

Manhours 4.00

Minimum number of person 2

Subtask elapsed time 2.00

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 26-23-43, Page Block 401

Fig. A-GBCAA

Removal of the 4 Flow Metering

Compact Units (FMCU), FIN 4031WX,

4032WX, 4033WX and 4034WX, the

related Plumbing Installations and

Placards

Sheet 01

Sheet 02

Sheet 03

(a) Remove the Flow Metering Compact Unit (FMCU), FIN 4031WX.

Refer to Fig. A-GBCAA

1 From FR35RH, remove the FMCU, FIN 4031WX (Refer to AMM 26-23-43,

Page Block 401) :

Refer to Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet 02 and Fig. A-GBCAA

Sheet 03

1 Meter-Flow, Compact

Unit

QA07907-01 Item (205) Discard

and

1 Hose Assy G2627007000000 Item (107) Discard

1 Tube Assy G2627006000000 Item (109) Discard

with :

1 Washer NAS1149F0332P Item (106) Discard

1 Clamp NSA5516-06NJ Item (111) Discard

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 279

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@A340-500/600

SERVICE BULLETIN

1 Screw NAS1096-3-10 Item (112) Discard

1 Nut NAS1726-3E Item (113) Discard

3 Screw NAS1100E4-36 Item (130) Discard

3 Washer NAS1149C0432R Item (131) Discard

1 Fitting A2627048220400 Item (132) Discard

2 O-Ring NSA8202-6 Item (133) Discard

1 Fitting A2627048221600 Item (134) Discard

(b) Remove the Flow Metering Compact Unit (FMCU), FIN 4032WX.

Refer to Fig. A-GBCAA

1 From FR36RH, remove the FMCU, FIN 4032WX (Refer to AMM 26-23-43,

Page Block 401) :

Refer to Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet 02 and Fig. A-GBCAA

Sheet 03

1 Meter-Flow, Compact

Unit

QA07907-01 Item (205) Discard

and

1 Hose Assy G2627007000200 Item (108) Discard

1 Tube Assy G2627006000200 Item (110) Discard

with :

1 Washer NAS1149F0332P Item (106) Discard

1 Clamp NSA5516-06NJ Item (111) Discard

1 Screw NAS1096-3-10 Item (112) Discard

1 Nut NAS1726-3E Item (113) Discard

3 Screw NAS1100E4-36 Item (130) Discard

3 Washer NAS1149C0432R Item (131) Discard

1 Fitting A2627048220400 Item (132) Discard

2 O-Ring NSA8202-6 Item (133) Discard

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 280

6

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@A340-500/600

SERVICE BULLETIN

1 Fitting A2627048221600 Item (134) Discard

(c) Remove the Flow Metering Compact Unit (FMCU), FIN 4033WX.

Refer to Fig. A-GBCAA

1 From FR37RH, remove the FMCU, FIN 4033WX (Refer to AMM 26-23-43,

Page Block 401) :

Refer to Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet 02 and Fig. A-GBCAA

Sheet 03

1 Meter-Flow, Compact

Unit

QA07907-01 Item (205) Discard

and

1 Hose Assy G2627007000000 Item (107) Discard

1 Tube Assy G2627006000000 Item (109) Discard

with :

1 Washer NAS1149F0332P Item (106) Discard

1 Clamp NSA5516-06NJ Item (111) Discard

1 Screw NAS1096-3-10 Item (112) Discard

1 Nut NAS1726-3E Item (113) Discard

3 Screw NAS1100E4-36 Item (130) Discard

3 Washer NAS1149C0432R Item (131) Discard

1 Fitting A2627048220400 Item (132) Discard

2 O-Ring NSA8202-6 Item (133) Discard

1 Fitting A2627048221600 Item (134) Discard

(d) Remove the Flow Metering Compact Unit (FMCU), FIN 4034WX.

Refer to Fig. A-GBCAA

1 From FR37.1RH, remove the FMCU, FIN 4034WX (Refer to AMM 26-23-43,

Page Block 401) :

Refer to Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet 02 and Fig. A-GBCAA

Sheet 03

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 281

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

1 Meter-Flow, Compact

Unit

QA07907-01 Item (205) Discard

and

1 Hose Assy G2627007000200 Item (108) Discard

1 Tube Assy G2627006000200 Item (110) Discard

with :

1 Washer NAS1149F0332P Item (106) Discard

1 Clamp NSA5516-06NJ Item (111) Discard

1 Screw NAS1096-3-10 Item (112) Discard

1 Nut NAS1726-3E Item (113) Discard

3 Screw NAS1100E4-36 Item (130) Discard

3 Washer NAS1149C0432R Item (131) Discard

1 Fitting A2627048220400 Item (132) Discard

2 O-Ring NSA8202-6 Item (133) Discard

1 Fitting A2627048221600 Item (134) Discard

(16) Subtask 265020-831-203-001 - Remove the plumbing installations and placards.

Work Zones and Access Panels

Zone Access/Work location

132 Access Panel 132PM

Work location from Frame 35 to Frame 37.1

Manpower Resources

Manhours 2.50

Minimum number of person 2

Subtask elapsed time 1.25

Skills NON SPECIFIC

References

Fig. A-GBCAA

Removal of the 4 Flow Metering

Compact Units (FMCU), FIN 4031WX,

4032WX, 4033WX and 4034WX, the

related Plumbing Installations and

Placards

Sheet 01

Sheet 02

Sheet 03

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 282

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@A340-500/600

SERVICE BULLETIN

(a) Remove the plumbing installations between FR35RH thru FR37.1RH.

Refer to Fig. A-GBCAA

1 Between FR35RH and FR36RH, remove :

Refer to Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet 02 and Fig. A-GBCAA

Sheet 03

2 Reducer MS21916D10-4 Item (115) Discard

1 Tube Assy G2627005004400 Item (116) Discard

1 Tee NSA855113-34D Item (117) Discard

1 Tube Assy G2627005004200 Item (118) Discard

1 Hose A2627045200400 Item (209) Discard

with :

2 Washer NAS1149F0332P Item (106) Discard

2 Screw NAS1096-3-10 Item (112) Discard

2 Nut NAS1726-3E Item (113) Discard

2 Clamp NSA5516-18NJ Item (121) Discard

1 Rod End NSA8141-04R Item (135) Discard

1 Nut NAS509-5 Item (136) Discard

1 Rod End NSA8140-04RK Item (137) Discard

2 Lead-Bonding E0090-41-320 Item (138) Discard

1 Bolt NAS1304-12 Item (139) Discard

1 Nut NAS1726-4E Item (104) Discard

1 Washer NAS1149D0432K Item (140) Discard

1 Washer-Lock NSA5355-5CA Item (141) Discard

2 Between FR36RH and FR37RH, remove :

Refer to Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet 02 and Fig. A-GBCAA

Sheet 03

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 283

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@A340-500/600

SERVICE BULLETIN

2 Washer NAS1149F0332P Item (106) Discard

2 Screw NAS1096-3-10 Item (112) Discard

2 Nut NAS1726-3E Item (113) Discard

1 Tube Assy G2627005004000 Item (120) Discard

2 Clamp NSA5516-18NJ Item (121) Discard

1 Cross NSA855140-22D Item (122) Discard

1 Union MS21902D10 Item (123) Discard

1 Tube Assy G2627005003800 Item (124) Discard

2 Tee NSA855008D10 Item (125) Discard

1 Rod End NSA8141-04R Item (135) Retain

1 Nut NAS509-5 Item (136) Retain

1 Rod End NSA8140-04RK Item (137) Retain

2 Lead-Bonding E0090-41-320 Item (138) Discard

1 Bolt NAS1304-12 Item (139) Discard

1 Nut NAS1726-4E Item (104) Discard

1 Washer NAS1149D0432K Item (140) Discard

1 Washer-Lock NSA5355-5CA Item (141) Discard

1 Tube Assy G2627005006400 Item (142) Discard

1 Hose A2627045200400 Item (209) Retain

2 Hose Assy F2627007100200 Item (210) Retain

3 Between FR37RH and FR37.1RH, remove :

Refer to Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet 02 and Fig. A-GBCAA

Sheet 03

2 Reducer MS21916D10-4 Item (115) Discard

1 Tube Assy G2627005004400 Item (116) Discard

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 284

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@A340-500/600

SERVICE BULLETIN

1 Tee NSA855113-34D Item (117) Discard

1 Tube Assy G2627005003400 Item (119) Discard

1 Tee NSA855008D10 Item (125) Discard

1 Tube Assy G2627005003600 Item (129) Discard

1 Rod End NSA8141-04R Item (135) Retain

1 Nut NAS509-5 Item (136) Retain

1 Rod End NSA8140-04RK Item (137) Retain

2 Lead-Bonding E0090-41-320 Item (138) Discard

1 Bolt NAS1304-12 Item (139) Discard

1 Nut NAS1726-4E Item (104) Discard

1 Washer NAS1149D0432K Item (140) Discard

1 Washer-Lock NSA5355-5CA Item (141) Discard

1 Hose A2627045200400 Item (209) Retain

(b) Remove the placards between FR35RH thru FR37.1RH.

Refer to Fig. A-GBCAA

1 Between FR35RH and FR36RH, remove the placards 4010WX, 4031WX and

4032WX :

2 Label NSA931025-02F Item (126) Discard

1 Placard G2627004020200 Item (127) Discard

2 Between FR37RH and FR37.1RH, remove the placards 4020WX, 4033WX

and 4034WX :

2 Label NSA931025-02F Item (126) Discard

1 Placard G2627004020400 Item (128) Discard

(17) Subtask 265020-831-204-001 - Remove the brackets and the insulation blankets

between FR35RH thru FR37.1RH.

Work Zones and Access Panels

Zone Access/Work location

132 Work location from Frame 35 to Frame 37.1

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 285

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@A340-500/600

SERVICE BULLETIN

Manpower Resources

Manhours 3.50

Minimum number of person 2

Subtask elapsed time 1.75

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 25-80-00-000-801

Fig. A-GBDAA

Removal of the Brackets

Sheet 01

Sheet 02

Sheet 03

(a) Remove the insulation blankets in the affected area (Refer to AMM Task

25-80-00-000-801).

(b) Remove the brackets between FR35RH thru FR37.1RH.

Refer to Fig. A-GBDAA

1 Between FR35 and FR36, STGR 29RH, remove :

Refer to Fig. A-GBDAA Sheet 01 and Fig. A-GBDAA Sheet 03

1 Section-T F5397460021800 Item (161) Discard

1 Bracket Assy F5397484500200 Item (162) Discard

2 From FR35RH, STGR31, remove :

Refer to Fig. A-GBDAA Sheet 01 and Fig. A-GBDAA Sheet 03

1 Bracket F5397463611000 Item (163) Discard

3 From FR36RH, STGR31, remove :

Refer to Fig. A-GBDAA Sheet 01 and Fig. A-GBDAA Sheet 03

1 Bracket F5397463610800 Item (164) Discard

4 From FR37RH, STGR31, remove :

Refer to Fig. A-GBDAA Sheet 01 and Fig. A-GBDAA Sheet 03

1 Bracket F5397463611000 Item (163) Discard

5 From FR37.1RH, STGR31, remove :

Refer to Fig. A-GBDAA Sheet 01 and Fig. A-GBDAA Sheet 03

1 Bracket F5397463610800 Item (164) Discard

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 286

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@A340-500/600

SERVICE BULLETIN

6 From the crossbeam at FR35 at -Y2462, remove :

Refer to Fig. A-GBDAA Sheet 01 and Fig. A-GBDAA Sheet 02

1 Bracket Assy F5397800200000 Item (165) Discard

1 Bracket F5397461823000 Item (166) Discard

7 From the crossbeam at FR36 at -Y2462, remove :

Refer to Fig. A-GBDAA Sheet 01 and Fig. A-GBDAA Sheet 02

1 Bracket Assy F5397800200000 Item (165) Discard

1 Bracket F5397469928000 Item (167) Discard

8 Between FR35RH and FR36RH, remove :

Refer to Fig. A-GBDAA Sheet 01 and Fig. A-GBDAA Sheet 02

1 Strut Assy F5397883300000 Item (168) Discard

(18) Subtask 265020-831-213-001 - Install the brackets, modify the insulation blankets

and close the rivet holes between FR35RH thru FR37.1RH.

Work Zones and Access Panels

Zone Access/Work location

132 Work location from Frame 35 to Frame 37.1

Manpower Resources

Manhours 7.00

Minimum number of person 2

Subtask elapsed time 3.50

Skills NON SPECIFIC

Material necessary to do the job

Kit 265020D02R04

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

170 EN6081D4-09 28 RIVET

171 EN6081D6-14 30 RIVET

252 F5397757020200 2 ANGLE

253 F5397462009600 1 BRACKET

254 F5397462009800 1 BRACKET

281 ABS1577A05 1 BRACKET

282 ABS0787B05B 1 BRACKET

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 287

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@A340-500/600

SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) Task 20-28-00-912-802

Task 25-80-00-200-801

Task 25-80-00-400-801

Fig. A-GBGAA

Installation of the Brackets

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Fig. A-GBDAA

Removal of the Brackets

Sheet 01

Sheet 02

Sheet 03

(a) Install the brackets and close the existing rivet holes.

Refer to Fig. A-GBDAA and Fig. A-GBGAA

1 Between FR35 and FR36, on STGR29RH and STGR30RH, close the rivet

holes in the stringers with :

Refer to Fig. A-GBDAA Sheet 01, Fig. A-GBDAA Sheet 02 and Fig. A-GBDAA

Sheet 03

4 Rivet EN6081D6-14 Item 171

2 On FR35 and FR36, STGR31RH, close the rivet holes in the frames with :

Refer to Fig. A-GBDAA Sheet 01, Fig. A-GBDAA Sheet 02 and Fig. A-GBDAA

Sheet 03

8 Rivet EN6081D6-14 Item 171

3 Between FR36 and FR37, on STGR30RH, install this bracket on the stringer :

Refer to Fig. A-GBGAA Sheet 01 and Fig. A-GBGAA Sheet 02

1 Angle-Bonding F5397757020200 Item 252

with :

3 Rivet EN6081D4-09 Item 170

NOTE: Do the electrical bonding (Refer to AMM Task

20-28-00-912-802)

4 On FR37 and FR37.1, STGR31RH, close the rivet holes in the frames with :

Refer to Fig. A-GBDAA Sheet 01,Fig. A-GBDAA Sheet 02 and Fig. A-GBDAA

Sheet 03

8 Rivet EN6081D6-14 Item 171

5 On FR37, between STGR31RH and STGR32RH, install this bracket :

Refer to Fig. A-GBGAA Sheet 01 and Fig. A-GBGAA Sheet 02

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 288

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@A340-500/600

SERVICE BULLETIN

1 Bracket Assy F5397462009600 Item 253

with :

4 Rivet EN6081D6-14 Item 171

NOTE: Do the electrical bonding (Refer to AMM Task

20-28-00-912-802)

NOTE: Existing rivet spacing must be used.

6 Between FR37 and FR37.1, on STGR30RH, install this bracket :

Refer to Fig. A-GBGAA Sheet 01 and Fig. A-GBGAA Sheet 02

1 Angle-Bonding F5397757020200 Item 252

with :

3 Rivet EN6081D4-09 Item 170

7 Between FR37 and FR37.1, on STGR30RH, install this bracket :

Refer to Fig. A-GBGAA Sheet 01 and Fig. A-GBGAA Sheet 03

1 Bracket ABS1577A05 Item 281

with :

3 Rivet EN6081D4-09 Item 170

NOTE: Do the electrical bonding (Refer to AMM Task

20-28-00-912-802)

8 On FR37.1, between STGR31RH and STGR32RH, install this bracket :

Refer to Fig. A-GBGAA Sheet 01 and Fig. A-GBGAA Sheet 02

1 Bracket Assy F5397462009800 Item 254

with :

4 Rivet EN6081D6-14 Item 171

NOTE: Do the electrical bonding (Refer to AMM Task

20-28-00-912-802)

NOTE: Existing rivet spacing must be used.

9 On the crossbeam at FR35, between -Y1959 and -Y2462, close the rivet holes

in the crossbeam with :

Refer to Fig. A-GBDAA Sheet 01, Fig. A-GBDAA Sheet 02 and Fig. A-GBDAA

Sheet 03

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 289

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@A340-500/600

SERVICE BULLETIN

10 Rivet EN6081D4-09 Item 170

10 On the crossbeam at FR36, outboard of -Y2462, close the rivet holes in the

crossbeam with :

Refer to Fig. A-GBDAA Sheet 01, Fig. A-GBDAA Sheet 02 and Fig. A-GBDAA

Sheet 03

9 Rivet EN6081D4-09 Item 170

11 On the crossbeam at FR36, outboard of -Y2462, install this bracket :

Refer to Fig. A-GBGAA Sheet 01 and Fig. A-GBGAA Sheet 03

1 Bracket-Z ABS0787B05B Item 282

with :

2 Rivet EN6081D6-14 Item 171

NOTE: Do the electrical bonding (Refer to AMM Task

20-28-00-912-802)

(b) Between FR36 thru FR37.1RH modify the insulation blankets in the affected area.

1 Adapt the insulation blankets for the new locations of brackets (Refer to AMM

Task 25-80-00-200-801).

(c) Install the modified insulation in the affected area (Refer to AMM Task

25-80-00-400-801).

(19) Subtask 265020-831-216-001 - Modify the equipment and the wiring of the

FMCU/FMS outlet pressure switches 4031WX, 4032WX, 4033WX, 4034WX, 4016WX

and 4018WX of the fire extinguishing bottles Nos. 2 and 3.

Work Zones and Access Panels

Zone Access/Work location

132 Work location from Frame 35 to Frame 37.1

200 Work location Electrical panel 801VU

Manpower Resources

Manhours 1.50

Minimum number of person 2

Subtask elapsed time 0.75

Skills ELECTRICAL

Material necessary to do the job

Kit 265020D03R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

173 G9237018016600 1 PLCRDSET

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 290

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@A340-500/600

SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

174 NSA935401-04 8 TIE

175 NSA935401-05 15 TIE

References

Process and Material Specification

(PMS)

Process and Material Specification (PMS)

01-07-10

Fig. A-GWAAA

Modification of the Wiring of the

FMCU/FMS Outlet Pressure Switches

4031WX, 4032WX, 4033WX, 4034WX,

4016WX and 4018WX

Sheet 01

Sheet 02

Fig. A-GHAAA

Hook-up Chart

Sheet 01

Fig. A-GBLAA

Stowage of the Electrical Wires of the

Connectors 4031WX-A, 4032WX-A

4011WX-A, 4012WX-A and 4013WX-A

Sheet 01

Sheet 02

Sheet 03

Sheet 04

(a) Modify the wiring of the FMCU/FMS outlet pressure switches.

1 Disconnect these electrical wires from the connectors 4031WX-A and

4032WX-A.

Refer to Fig. A-GWAAA Sheet 01 (Wiring)

Refer to Fig. A-GHAAA Sheet 01 (Hook-up Chart), LINES 1, 2, 3 and 4

2 Remove the connectors 4031WX-A and 4032WX-A and discard.

Refer to Fig. A-GBLAA Sheet 01

Remove :

2 Connector-Plug EN2997KE60803BN Item (265) Discard

and remove the following attachment parts :

4 Screw NAS1801-08-7 Item (267) Discard

2 Nut MS21042-08 Item (268) Discard

4 Washer NAS1149CN816R Item (269) Discard

2 Clamp MS21919WCH8 Item (270) Retain

2 Screw NAS1801-08-23 Item (271) Discard

2 Lanyard DAN80-3-150 Item (273) Discard

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 291

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@A340-500/600

SERVICE BULLETIN

2 Sleeve-Protective NSA935809-09 Item (274) Discard

5 Cable Mount Item (277) Retain

3 Disconnect these electrical wires from the connectors 4033WX-A and

4034WX-A.

Refer to Fig. A-GWAAA Sheet 01 (Wiring)

Refer to Fig. A-GHAAA Sheet 01 (Hook-up Chart), LINES 5, 6, 7 and 8

4 Reroute and install the electrical wires :

Refer to Fig. A-GWAAA Sheet 02 (Wiring)

Refer to Fig. A-GHAAA Sheet 01 (Hook-up Chart), LINES 13, 14, 15 and 16

with :

15 Tie-Cable NSA935401-05 Item 175

and attach the placards, identified 4016WX-A, 4018WX-A and the SB/MOD

placards :

1 Placardset G9237018016600 Item 173

with :

8 Tie-Cable NSA935401-04 Item 174

(20) Subtask 265020-831-209-001 - Modify the equipment and the wiring of the fire

extinguishing bottle No. 3 (AFT), 4020WX, and relocated fire extinguishing bottle

No. 2 (AFT), 4010WX.

Work Zones and Access Panels

Zone Access/Work location

132 Work location from Frame 35 to Frame 37.1

200 Work location Electrical panel 801VU

Electrical panel 802VU

Manpower Resources

Manhours 1.00

Minimum number of person 2

Subtask elapsed time 1.00

Skills ELECTRICAL

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 292

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SERVICE BULLETIN

Material necessary to do the job

Kit 265020D03R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

173 G9237018016600 1 PLCRDSET

174 NSA935401-04 12 TIE

175 NSA935401-05 15 TIE

176 EN3155-003F1614 2 CONTACT

References

Fig. A-GWBAA

Modification of the Wiring of the Fire

Extinguishing Bottle No. 3 (previously

AFT), 4020WX, and relocated Fire

Extinguishing Bottle No. 2 (now AFT),

4010WX

Sheet 01

Sheet 02

Fig. A-GHBAA

Hook-up Chart

Sheet 01

(a) Modify the wiring of the cartridges and the pressure switch of the fire extinguishing

bottle (AFT), 4020WX (4010WX)

1 Disconnect these electrical wires from the connector 2625VC-A.

Refer to Fig. A-GWBAA Sheet 01 (Wiring)

Refer to Fig. A-GHBAA Sheet 01 (Hook-up Chart), LINES 1 and 11, END 2

2 Reroute and install the electrical wires on the connector 2511VC-A.

Refer to Fig. A-GWBAA Sheet 02 (Wiring)

Refer to Fig. A-GHBAA Sheet 01 (Hook-up Chart), LINES 2 and 12, END 2

3 Disconnect these electrical wires from the connector 2636VC-A.

Refer to Fig. A-GWBAA Sheet 01 (Wiring)

Refer to Fig. A-GHBAA Sheet 01 (Hook-up Chart), LINES 5 and 15, END 2

NOTE: Cut off the contacts directly behind the contacts.

4 Reroute and install the electrical wires on the connector 2508VC-A.

Refer to Fig. A-GWBAA Sheet 02 (Wiring)

Refer to Fig. A-GHBAA Sheet 01 (Hook-up Chart), LINES 6 and 16, END 2

with :

2 Contact-Socket EN3155-003F1614 Item 176

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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5 Disconnect the electrical wire from the connector 2044VC-A.

Refer to Fig. A-GWBAA Sheet 01 (Wiring)

Refer to Fig. A-GHBAA Sheet 01 (Hook-up Chart), LINE 23, END 2

6 Reroute and install the electrical wire on the connector 2016VC-A.

Refer to Fig. A-GWBAA Sheet 02 (Wiring)

Refer to Fig. A-GHBAA Sheet 01 (Hook-up Chart), LINE 24, END 2

7 Attach the placards, identified 4011WX-A, 4012WX-A, 4013WX-A and the

SB/MOD placards :

1 Placardset G9237018016600 Item 173

with :

12 Tie-Cable NSA935401-04 Item 174

8 Install the tie-cables on the wire harnesses :

15 Tie-Cable NSA935401-05 Item 175

NOTE: For the stowage position of the connectors 4011WX-A,

4012WX-A, 4013WX-A, 4031WX-A and 4032WX-A, refer to

(22) Subtask 265020-831-218-001.

(21) Subtask 265020-831-210-001 - Modify the Equipment and the Wiring of the

previous Fire Extinguishing Bottle No. 2 (FWD), 4010WX.

Work Zones and Access Panels

Zone Access/Work location

132 Work location from Frame 35 to Frame 36

200 Work location Electrical panel 801VU

Electrical panel 802VU

Manpower Resources

Manhours 1.50

Minimum number of person 1

Subtask elapsed time 1.50

Skills ELECTRICAL

References

Fig. A-GWCAA

Modification of the Wiring of the Fire

Extinguishing Bottle No. 2 (FWD),

4010WX

Sheet 01

Sheet 02

Fig. A-GHCAA

Hook-up Chart

Sheet 01

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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References

Fig. A-GBLAA

Stowage of the Electrical Wires of the

Connectors 4031WX-A, 4032WX-A

4011WX-A, 4012WX-A and 4013WX-A

Sheet 01

Sheet 02

Sheet 03

Sheet 04

(a) Modify the wiring of the previous fire extinguishing bottle No. 2 (FWD), 4010WX.

1 Disconnect these electrical wires from the connectors 4011WX-A, 4012WX-A

and 4013WX-A.

Refer to Fig. A-GWCAA Sheet 01 (Wiring)

Refer to Fig. A-GHCAA Sheet 01 (Hook-up Chart), LINES 1, 5, 11, 15 and 23

Refer to Fig. A-GHCAA Sheet 01 (Hook-up Chart), LINES 3, 7, 9, 13, 17, 19,

21, END 1

2 Remove the connectors 4011WX-A, 4012WX-A and 4013WX-A and discard.

Refer to Fig. A-GBLAA Sheet 01

Remove :

2 Connector EN2997KE61005BN Item (264) Discard

1 Connector-Plug EN2997KE60803BN Item (265) Discard

and remove the following attachment parts :

1 Tie-Cable NSA935401-03 Item (266) Discard

5 Screw NAS1801-08-7 Item (267) Discard

2 Nut MS21042-08 Item (268) Discard

4 Washer NAS1149CN816R Item (269) Discard

2 Clamp MS21919WCH8 Item (270) Discard

1 Screw NAS1801-08-29 Item (272) Discard

2 Lanyard DAN80-3-150 Item (273) Discard

2 Sleeve-Protective NSA935809-09 Item (274) Discard

2 Cable Mount Item (277) Retain

NOTE: For the stowage position of the connectors 4011WX-A,

4012WX-A, 4013WX-A, 4031WX-A and 4032WX-A, refer to

(22) Subtask 265020-831-218-001.

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 295

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(22) Subtask 265020-831-218-001 - Put the electrical wires of the connectors 4031WX-A,

4032WX-A 4011WX-A, 4012WX-A and 4013WX-A in a stowage position.

Work Zones and Access Panels

Zone Access/Work location

132 Work location from Frame 35 to Frame 37.1

Manpower Resources

Manhours 2.50

Minimum number of person 1

Subtask elapsed time 2.50

Skills ELECTRICAL

Material necessary to do the job

Kit 265020D03R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

173 G9237018016600 1 PLCRDSET

177 NSA936603CC0100 23 CAP

Kit 265020D05R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

266 NSA935401-03 25 TIE

269 NAS1149CN816R 4 WASHER

270 MS21919WCH8 4 CLAMP

271 NAS1801-08-23 2 SCREW

272 NAS1801-08-29 1 SCREW

274 NSA935809-09 4 SLEEVE

275 NAS1801-08-25 1 SCREW

References

Fig. A-GBLAA

Stowage of the Electrical Wires of the

Connectors 4031WX-A, 4032WX-A

4011WX-A, 4012WX-A and 4013WX-A

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Fig. A-GHAAA

Hook-up Chart

Sheet 01

Fig. A-GHCAA

Hook-up Chart

Sheet 01

Fig. A-GWAAA

Modification of the Wiring of the

FMCU/FMS Outlet Pressure Switches

4031WX, 4032WX, 4033WX, 4034WX,

4016WX and 4018WX

Sheet 01

Sheet 02

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 296

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SERVICE BULLETIN

References

Fig. A-GWCAA

Modification of the Wiring of the Fire

Extinguishing Bottle No. 2 (FWD),

4010WX

Sheet 01

Sheet 02

(a) Put the electrical wires of the connectors 4031WX-A and 4032WX-A in a stowage

position.

1 Put the electrical wires in a stowage position.

Refer to Fig. A-GBLAA Sheet 01, Fig. A-GBLAA Sheet 02, Fig. A-GBLAA

Sheet 03 and Fig. A-GBLAA Sheet 04

Refer to Fig. A-GWAAA Sheet 02 (Wiring)

Refer toFig. A-GHAAA Sheet 01 (Hook-up Chart), LINES 9, 10, 11 and 12

with :

6 Cap NSA936603CC0100 Item 177

NOTE: Do not cut off the contacts.

Attach the electrical wires in a stowage position.

with :

2 Washer NAS1149CN816R Item 269

2 Clamp MS21919WCH8 Item 270

2 Clamp MS21919WCH8 Item (270) Retained at

removal

1 Screw NAS1801-08-23 Item 271

2 Sleeve-Protective NSA935809-09 Item 274

1 Screw NAS1801-08-25 Item 275

5 Cable Mount Item (277) Retained at

removal

20 Tie-Cable NSA935401-03 Item 266

(b) Put the electrical wires of the connectors 4011WX-A, 4012WX-A and 4013WX-A in

a stowage position.

1 Put the electrical wires in a stowage position.

Refer to Fig. A-GBLAA Sheet 01, Fig. A-GBLAA Sheet 02, Fig. A-GBLAA

Sheet 03 and Fig. A-GBLAA Sheet 04

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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Refer to Fig. A-GWCAA Sheet 02 (Wiring)

Refer to Fig. A-GHCAA Sheet 01 (Hook-up Chart), LINES 2, 6, 12, 16 and 24

Refer to Fig. A-GHCAA Sheet 01 (Hook-up Chart), LINES 4, 8, 10, 14, 18, 20

and 22, END 1

with :

17 Cap NSA936603CC0100 Item 177

NOTE: Do not cut off the contacts.

Attach the electrical wires in a stowage position.

with :

2 Washer NAS1149CN816R Item 269

2 Clamp MS21919WCH8 Item 270

1 Screw NAS1801-08-23 Item 271

1 Screw NAS1801-08-29 Item 272

2 Sleeve-Protective NSA935809-09 Item 274

2 Cable Mount Item (277) Retained at

removal

and attach the SB/MOD placards :

1 Placardset G9237018016600 Item 173

with :

5 Tie-Cable NSA935401-03 Item 266

(23) Subtask 265020-831-205-001 - Adapt the plumbing installation.

Work Zones and Access Panels

Zone Access/Work location

132 Work location from Frame 36 to Frame 37

Manpower Resources

Manhours 3.00

Minimum number of person 2

Subtask elapsed time 1.50

Skills NON SPECIFIC

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 298

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SERVICE BULLETIN

Material necessary to do the job

Kit 265020D01R03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

113 NAS1726-3E 2 NUT

121 NSA5516A18NJ 2 CLAMP

125 NSA855008D10 1 TEE

144 NAS1149C0332R 2 WASHER

155 NSA5527-03-03 2 SPACER

157 NAS1801-3-12 2 SCREW

158 NSA855006D10 2 UNION

251 G2627005013000 1 TUBE

253 G2627005002000 1 TUBE

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Internal Polyurethane

Varnish

07-017 As required

Solvent General Purpose 11-026 As required

Low Voc Anti-Corrosion

Primer

16-006F As required

Lint-Free Cotton Cloth 19-003 As required

Standard tool TOOLD01

ITEM TOOL N ̊ TOOL NAME QTY SEE

NOTES

D12102C07-02 PERMASWAGE Repair

Kit D12000 Series

1

References

Aircraft Maintenance Manual (AMM) 20-23-11, Page Block 201

Fig. A-GBEAA

Adaption of the Plumbing Installation

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Fig. A-GBFAA

Installation of the U-Section and the

Flow Metering System (FMS)

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

(a) Remove the fire extinguishing tubes from FR36 and FR37.

Refer to Fig. A-GBEAA

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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SERVICE BULLETIN

1 Remove and discard these items from FR36RH :

Refer to Fig. A-GBEAA Sheet 01, Fig. A-GBEAA Sheet 02 and Fig. A-GBEAA

Sheet 04

1 Nut NAS1726-3E Item (113) Discard

1 Clamp NSA5516-18NJ Item (121) Discard

1 Washer NAS1149C0332R Item (144) Discard

1 Spacer NSA5527-03-03 Item (155) Discard

1 Screw NAS1096-3-14 Item (157) Discard

2 Cut the fire extinguishing tube, Item (250), at the position shown in Fig. AGBEAA Sheet 02 (Refer to AMM 20-23-11, Page Block 201).

3 Remove the fire extinguishing tube, Item (250), partly between the cut and the

outboard X-connection fitting :

1 Tube Assy, partly G2627005013000 Item (250) Discard

4 Deburr the remaining tube, Item (250), (Refer to AMM 20-23-11, Page Block

201).

5 Clean the remaining tube, Item (250), with :

Solvent General

Purpose

11-026 As required

and

Lint-Free Cotton

Cloth

19-003 As required

6 Remove and discard these items from FR37RH :

Refer to Fig. A-GBEAA Sheet 01, Fig. A-GBEAA Sheet 02 and Fig. A-GBEAA

Sheet 04

1 Nut NAS1726-3E Item (113) Discard

1 Clamp NSA5516-18NJ Item (121) Discard

1 Washer NAS1149C0332R Item (144) Discard

1 Spacer NSA5527-03-03 Item (155) Discard

1 Screw NAS1096-3-14 Item (157) Discard

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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7 Cut the fire extinguishing tube, Item (252), at the position shown in Fig. AGBEAA Sheet 02 (Refer to AMM 20-23-11, Page Block 201).

8 Remove the fire extinguishing tube, Item (252), partly between the cut and the

outboard T-connection fitting :

1 Tube Assy, partly G2627005002000 Item (252) Discard

1 Tee NSA855008D10 Item (125) Discard

9 Deburr the remaining tube, Item (252), (Refer to AMM 20-23-11, Page Block

201).

10 Clean the remaining tube, Item (252), with :

Solvent General

Purpose

11-026 As required

and

Lint-Free Cotton

Cloth

19-003 As required

(b) Install the fire extinguishing tubes on FR36 and FR37.

CAUTION: BEFORE YOU CONNECT THE FIRE EXTINGUISHING TUBES

WITH THE PERMASWAGE TOOL, MAKE SURE THAT THE FIRE

EXTINGUISHING TUBES ARE INSTALLED STRESS-FREE IN

THEIR CLAMPS.

CAUTION: DO NOT BEND THE TUBE WHEN YOU INSTALL IT. IF THE

TUBE IS BENT, IT CAN BECOME DAMAGED.

CAUTION: IF YOU USE DUST CAPS FOR THE CONTAMINATION

PROTECTION OF OPEN LINES, ALWAYS BE SURE TO

INSTALL THE CAPS AROUND THE TUBE ENDS AND NOT IN

THE TUBE ENDS. THERE CAN BE BLOCKAGE OF THE FLOW

THROUGH THE TUBES IF THESE TUBES ARE INSTALLED

ACCIDENTALLY WITH DUST CAPS IN THE TUBE ENDS.

NOTE: The fire extinguishing tubes must be installed with their related

clamps.

Refer to Fig. A-GBEAA

1 Install temporarily, Item 233, before install the other tubes.

Refer to Fig. A-GBFAA Sheet 01

2 Install the tube, Item 251, at FR36RH.

Refer to Fig. A-GBEAA Sheet 01, Fig. A-GBEAA Sheet 02 and Fig. A-GBEAA

Sheet 03

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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1 Tube Assy G2627005013000 Item 251

with :

1 Union NSA855006D10 Item 158

3 Connect the fire extinguishing tubes, Item (250), and Item 251, with the union,

Item 158, (Refer to AMM 20-23-11, Page Block 201).

D12102C07-02 PERMASWAGE

Repair Kit D12000

Series

1

NOTE: Use these swaging tools of the D12000 series :

- Head assembly D12210-56 with power unit D12010-52.

NOTE: The surface protection on both ends of the pipes must be

removed on a length of 43mm (1.692in.).

4 After the installation of the union, Item 158, perform surface protection with :

Low Voc AntiCorrosion Primer16-006F As required

and

Internal

Polyurethane

Varnish

07-017 As required

5 Install the clamp, Item 121, at FR36RH.

Fig. A-GBEAA Sheet 01, Fig. A-GBEAA Sheet 02 and Fig. A-GBEAA Sheet

03

1 Clamp NSA5516A18NJ Item 121

with :

1 Nut NAS1726-3E Item 113

1 Washer NAS1149C0332R Item 144

1 Spacer NSA5527-03-03 Item 155

1 Screw NAS1801-3-12 Item 157

6 Install temporarily, Item 234 and 238, before install the other tubes.

Refer to Fig. A-GBFAA Sheet 01

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7 Install the tube, Item 253 at FR37RH.

Refer to Fig. A-GBEAA Sheet 01, Fig. A-GBEAA Sheet 02 and Fig. A-GBEAA

Sheet 03

1 Tube Assy G2627005002000 Item 253

with :

1 Tee NSA855008D10 Item 125

1 Union NSA855006D10 Item 158

8 Connect the fire extinguishing tubes, Item (252), and Item 253, with the union,

Item 158, and on the other end with the T-fitting, Item 125 (Refer to AMM

20-23-11, Page Block 201).

NOTE: Use these swaging tools of the D12000 series :

- Head assembly D12210-56 with power unit D12010-52.

NOTE: The surface protection on the ends of the pipes must be

removed on a length of 43mm (1.692in.).

9 After the installation of the tee-fitting, Item 125, and the union, Item 158,

perform surface protection with :

Low Voc AntiCorrosion Primer16-006F As required

and

Internal

Polyurethane

Varnish

07-017 As required

10 Install the clamp, Item 121, at FR37RH.

Fig. A-GBEAA Sheet 01, Fig. A-GBEAA Sheet 02 and Fig. A-GBEAA Sheet

03

1 Clamp NSA5516A18NJ Item 121

with :

1 Nut NAS1726-3E Item 113

1 Washer NAS1149C0332R Item 144

1 Spacer NSA5527-03-03 Item 155

1 Screw NAS1801-3-12 Item 157

11 Tighten all connections of the installed fire extinguishing tubes.

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 303

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SERVICE BULLETIN

(24) Subtask 265020-831-206-001 - Install the U-section.

Work Zones and Access Panels

Zone Access/Work location

132 Work location from Frame 37 to Frame 37.1

Manpower Resources

Manhours 1.00

Minimum number of person 2

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 265020D01R03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

106 NAS1149F0332P 2 WASHER

143 NAS1801-3-8 4 SCREW

144 NAS1149C0332R 5 WASHER

145 NAS1801-3-7 3 SCREW

212 G2627008001400 1 SECTION

213 F2627008100000 1 BRACKET

220 E0090-10-135NN 1 LEAD

References

Aircraft Maintenance Manual (AMM) 20-28-00, Page Block 201

Fig. A-GBFAA

Installation of the U-Section and the

Flow Metering System (FMS)

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

(a) Install the U-section between FR37RH and FR37.1.

Refer to Fig. A-GBFAA

1 Between FR37RH and FR37.1RH, install :

Refer to Fig. A-GBFAA Sheet 03, Fig. A-GBFAA Sheet 05 and Fig. A-GBFAA

Sheet 06

1 U-section G2627008001400 Item 212

1 Bracket F2627008100000 Item 213

1 Lead-Bonding E0090-10-135NN Item 220

with :

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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2 Washer NAS1149F0332P Item 106

4 Screw NAS1801-3-8 Item 143

5 Washer NAS1149C0332R Item 144

3 Screw NAS1801-3-7 Item 145

NOTE: For the installation of the bolt (Refer to AMM 20-28-00, Page

Block 201).

NOTE: Seal the bonding connection by overlapping application and

identify the bonding connection by overlapping application with

blue dyed protective coating.

(25) Subtask 265020-831-207-001 - Install the Flow Metering Systems (FMS) for the Fire

Ext. Bottles No. 1 and No. 2 on the U-section.

Work Zones and Access Panels

Zone Access/Work location

132 Work location from Frame 37 to Frame 37.1

Manpower Resources

Manhours 4.00

Minimum number of person 2

Subtask elapsed time 2.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 265020D01R03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

104 NAS1726-4E 2 NUT

106 NAS1149F0332P 6 WASHER

113 NAS1726-3E 3 NUT

121 NSA5516A18NJ 2 CLAMP

132 A2627048220400 6 FITTING

133 NSA8202-6 8 ORING

134 A2627048221600 2 FITTING

139 NAS1304-12 2 BOLT

140 NAS1149D0432K 10 WASHER

141 NSA5355-5CA 2 WASHER

143 NAS1801-3-8 6 SCREW

144 NAS1149C0332R 6 WASHER

145 NAS1801-3-7 4 SCREW

146 NAS1100E4-34 6 SCREW

147 A2627048920000 2 WASHER

148 NSA5516A06NJ 4 CLAMP

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

152 E0090-10-320NN 2 LEAD

153 E0090-10-350NN 2 LEAD

159 NAS1801-3-10 2 SCREW

160 MS21103-4 2 CLAMP

219 G2627006001000 1 TUBE

221 G2627006000800 1 TUBE

222 G2627006001800 1 TUBE

223 F2627006003600 1 TUBE

224 A2627048220200 2 RESTRCTR

225 F2627006001400 1 TUBE

226 F2627006000000 1 TUBE

227 F2627007200000 1 HOSE

228 F2627007200200 1 HOSE

229 G2627006002000 1 TUBE

230 G2627006001200 1 TUBE

231 G2627006001400 1 TUBE

232 G2627006001600 1 TUBE

233 NSA855140-22D 1 CROSS

234 G2627005013200 1 TUBE

235 MS21902W10 1 UNION

236 A2627045107800 1 TUBE

237 NSA855113-34D 1 TEE

238 G2627005003400 1 TUBE

239 MS21916W10-4 2 REDUCER

Component COMPD01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

LN9424A100 As required WIRE

Equipment BFEZ01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

214 QA06753-03 2 FILTER

215 E61751-00-0001 2 REDUCER

216 TP0714033 2 SWITCH

217 HTE400115 2 VALVE

References

Aircraft Maintenance Manual (AMM) Task 20-28-00-912-802

Fig. A-GBFAA

Installation of the U-Section and the

Flow Metering System (FMS)

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 306

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SERVICE BULLETIN

(a) Install the Halon Filter, FIN 5010WE, for Fire Ext. Bottle No. 1.

Refer to Fig. A-GBFAA

1 On the U-section, between FR37RH and FR37.1RH, install :

Refer to Fig. A-GBFAA Sheet 01, Fig. A-GBFAA Sheet 03 and Fig. A-GBFAA

Sheet 04

1 Filter-Halon QA06753-03 Item 214

NOTE: See NOTE 03

with :

3 Washer NAS1149D0432K Item 140

3 Screw NAS1100E4-34 Item 146

and

2 O-Ring NSA8202-6 Item 133

1 Fitting A2627048221600 Item 134

NOTE: See NOTE 03

1 Fitting A2627048220400 Item 132

NOTE: See NOTE 03

2 Secure the fittings, Items 132 and 134, with :

As

required

Wire-Lock LN9424A100

3 On the fitting, Item 134, install :

1 Hose Assy F2627007200000 Item 227

NOTE: See NOTE 03

NOTE (03): No lubrication on this item.

(b) Install the Pressure Reducer, FIN 5014WE, for Fire Ext. Bottle No. 1.

1 On the U-section, between FR37RH and FR37.1RH, install :

Refer to Fig. A-GBFAA Sheet 01, Fig. A-GBFAA Sheet 03 and Fig. A-GBFAA

Sheet 04

1 Reducer-Pressure E61751-00-0001 Item 215

NOTE: See NOTE 03

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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with :

1 Washer-Tab A2627048920000 Item 147

2 Fitting A2627048220400 Item 132

NOTE: See NOTE 03

2 O-Ring NSA8202-6 Item 133

NOTE (03): No lubrication on this item.

2 Secure the fittings, Item 132, with :

As

required

Wire-Lock LN9424A100

(c) Install the Pressure Switch, FIN 4016WX, for Fire Ext. Bottle No. 1.

1 On the pressure reducer 5014WE, between FR37RH and FR37.1RH, install :

Refer to Fig. A-GBFAA Sheet 01, Fig. A-GBFAA Sheet 03, Fig. A-GBFAA

Sheet 04 and Fig. A-GBFAA Sheet 05

1 Tube Assy G2627006000800 Item 221

with :

1 Washer NAS1149C0332R Item 144

1 Screw NAS1801-3-7 Item 145

1 Clamp NSA5516A06NJ Item 148

and

1 Switch-Pressure TP0714033 Item 216

NOTE: See NOTE 03

2 On the pressure switch, Item 216, install :

1 Tube Assy G2627006001800 Item 222

with :

1 Washer NAS1149F0332P Item 106

1 SCREW NAS1801-3-10 Item 159

1 CLAMP MS21103-4 Item 160

NOTE (03): No lubrication on this item.

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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(d) Install the Check Valve, FIN 5016WE, for Fire Ext. Bottle No. 1.

1 On the pressure reducer 5014WE, between FR37RH and FR37.1RH, install :

Refer to Fig. A-GBFAA Sheet 01, Fig. A-GBFAA Sheet 03 and Fig. A-GBFAA

Sheet 05

1 Tube Assy F2627006003600 Item 223

1 Restrictor A2627048220200 Item 224

1 Tube Assy F2627006001400 Item 225

and

1 Valve-Nonreturn HTE400115 Item 217

NOTE: See NOTE 03

2 On the check valve, Item 217, install :

1 Tube Assy F2627006000000 Item 226

with :

1 Washer NAS1149C0332R Item 144

1 Screw NAS1801-3-7 Item 145

1 Clamp NSA5516A06NJ Item 148

NOTE (03): No lubrication on this item.

(e) Install the Halon Filter, FIN 5011WE, for Fire Ext. Bottle No. 2.

Refer to Fig. A-GBFAA

1 On the U-section, between FR37RH and FR37.1RH, install :

Refer to Fig. A-GBFAA Sheet 01, Fig. A-GBFAA Sheet 03 and Fig. A-GBFAA

Sheet 04

1 Filter-Halon QA06753-03 Item 214

NOTE: See NOTE 03

with :

3 Washer NAS1149D0432K Item 140

3 Screw NAS1100E4-34 Item 146

and

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SERVICE BULLETIN

2 O-Ring NSA8202-6 Item 133

1 Fitting A2627048221600 Item 134

NOTE: See NOTE 03

1 Fitting A2627048220400 Item 132

NOTE: See NOTE 03

2 Secure the fittings, Items 132 and 134, with :

As

required

Wire-Lock LN9424A100

3 On the fitting, Item 134, install :

1 Hose Assy F2627007200200 Item 228

NOTE: See NOTE 03

NOTE (03): No lubrication on this item.

(f) Install the Pressure Reducer, FIN 5015WE, for Fire Ext. Bottle No. 2.

1 On the U-section, between FR37RH and FR37.1RH, install :

Refer to Fig. A-GBFAA Sheet 01, Fig. A-GBFAA Sheet 03 and Fig. A-GBFAA

Sheet 04

1 Reducer-Pressure E61751-00-0001 Item 215

NOTE: See NOTE 03

with :

1 Washer-Tab A2627048920000 Item 147

2 Fitting A2627048220400 Item 132

NOTE: See NOTE 03

2 O-Ring NSA8202-6 Item 133

2 Secure the fittings, Item 132, with :

As

required

Wire-Lock LN9424A100

NOTE (03): No lubrication on this item.

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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(g) Install the Pressure Switch, FIN 4018WX, for Fire Ext. Bottle No. 2

1 On the pressure reducer 5015WE, between FR37RH and FR37.1RH, install :

Refer to Fig. A-GBFAA Sheet 01, Fig. A-GBFAA Sheet 03 and Fig. A-GBFAA

Sheet 04

1 Tube Assy G2627006001000 Item 219

with :

1 Washer NAS1149C0332R Item 144

1 Screw NAS1801-3-7 Item 145

1 Clamp NSA5516A06NJ Item 148

and

1 Switch-Pressure TP0714033 Item 216

NOTE: See NOTE 03

2 On the pressure switch, Item 216, install :

1 Tube Assy G2627006002000 Item 229

with :

1 Washer NAS1149F0332P Item 106

1 SCREW NAS1801-3-10 Item 159

1 CLAMP MS21103-4 Item 160

NOTE (03): No lubrication on this item.

(h) Install the Check Valve, FIN 5017WE, for Fire Ext. Bottle No. 2

1 On the pressure reducer 5015WE, between FR37RH and FR37.1RH, install :

Refer to Fig. A-GBFAA Sheet 01, Fig. A-GBFAA Sheet 03 and Fig. A-GBFAA

Sheet 05

1 Tube Assy G2627006001200 Item 230

1 Restrictor A2627048220200 Item 224

1 Tube Assy G2627006001400 Item 231

and

1 Valve-Nonreturn HTE400115 Item 217

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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NOTE: See NOTE 03

2 On the check valve, Item 217, install :

1 Tube Assy G2627006001600 Item 232

with :

1 Washer NAS1149C0332R Item 144

1 Screw NAS1801-3-7 Item 145

1 Clamp NSA5516A06NJ Item 148

1 Nut NAS1726-3E Item 113

NOTE (03): No lubrication on this item.

(i) Install the new plumbing and rod ends between FR36RH and FR37.1

1 Between FR36RH and FR37.1, install the rod ends :

Refer to Fig. A-GBFAA Sheet 01 and Fig. A-GBFAA Sheet 02

2 Rod End NSA8141-04R Item (135) Retained at

removal

2 Rod End NSA8140-04RK Item (137) Retained at

removal

with :

2 Nut NAS1726-4E Item 104

2 BOLT NAS1304-12 Item 139

4 Washer NAS1149D0432K Item 140

2 Nut NAS509-5 Item (136) Retained at

removal

2 Washer-Lock NSA5355-5CA Item 141

and

2 Lead-Bonding E0090-10-320NN Item 152

2 Lead-Bonding E0090-10-350NN Item 153

with :

4 Washer NAS1149F0332P Item 106

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4 Screw NAS1801-3-8 Item 143

NOTE: Do the electrical bonding (Refer to AMM Task

20-28-00-912-802)

2 Between FR36RH and FR37.1, install the plumbing :

Refer to Fig. A-GBFAA Sheet 01 and Fig. A-GBFAA Sheet 03

2 Hose A2627045200400 Item (209) Retained at

removal

2 Hose Assy F2627007100200 Item (210) Retained at

removal

1 Cross NSA855140-22D Item 233

1 Tube Assy G2627005013200 Item 234

1 Union MS21902W10 Item 235

with :

2 Screw NAS1801-3-8 Item 143

2 Washer NAS1149C0332R Item 144

2 Nut NAS1726-3E Item 113

2 Clamp NSA5516A18NJ Item 121

and

1 Tube Assy A2627045107800 Item 236

1 Tee NSA855113-34D Item 237

1 Tube Assy G2627005003400 Item 238

2 Reducer MS21916W10-4 Item 239

(26) Subtask 265020-831-211-001 - Install the Fire Extinguishing Bottles 4005WX and

4010WX.

Work Zones and Access Panels

Zone Access/Work location

132 Access Panel 132PM

Work location from Frame 35 to Frame 37.1

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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SERVICE BULLETIN

Manpower Resources

Manhours 2.00

Minimum number of person 2

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 265020D01R03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

100 NAS1726-5E 8 NUT

101 NAS1305-2 8 BOLT

103 NAS1304-9 2 BOLT

104 NAS1726-4E 2 NUT

Component COMPD01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

LN9424A100 As required WIRE

References

Aircraft Maintenance Manual (AMM) 26-23-41, Page Block 401

Fig. A-GBHAA

Installation of Fire Extinguishing Bottles

4005WX and 4010WX with Cartridges.

Sheet 01

Sheet 02

Sheet 03

Refer to Fig. A-GBHAA

(a) Install the fire extinguishing bottle 1 (FWD) 4005WX.

1 Between FR36RH and FR37RH, install the fire extinguishing bottle 4005WX

(Refer to AMM 26-23-41, Page Block 401) :

Refer to Fig. A-GBHAA Sheet 01, Fig. A-GBHAA Sheet 02and Fig. A-GBHAA

Sheet 03, Detail D :

1 Extinguisher-Fire 34900008-2 Item (201) Retained at

removal

with :

4 Nut NAS1726-5E Item 100

4 Bolt NAS1305-2 Item 101

1 Bolt NAS1304-9 Item 103

1 Nut NAS1726-4E Item 104

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2 Screw Item (260)

2 Washer Item (261)

2 Nut Item (262)

NOTE: Item (260), (261) and (262) are retained parts.

2 Secure the coupling nuts of the fire extinguishing discharge heads with :

As

required

Wire-Lock LN9424A100

(b) Install the fire extinguishing bottle 2 (AFT) 4010WX.

1 Between FR37RH and FR37.1RH, install the fire extinguishing bottle 4010WX

(Refer to AMM 26-23-41, Page Block 401) :

Refer to Fig. A-GBHAA Sheet 01 and Fig. A-GBHAA Sheet 03 :

1 Extinguisher-Fire 35200003-2 Item (200) Retained at

removal

with :

4 Nut NAS1726-5E Item 100

4 Bolt NAS1305-2 Item 101

1 Bolt NAS1304-9 Item 103

1 Nut NAS1726-4E Item 104

2 Screw Item (260)

2 Washer Item (261)

2 Nut Item (262)

NOTE: Item (260), (261) and (262) are retained parts.

2 Secure the coupling nuts of the fire extinguishing discharge heads with :

As

required

Wire-Lock LN9424A100

(27) Subtask 265020-831-212-001 - Install the new identification placards.

Work Zones and Access Panels

Zone Access/Work location

132 Work location from Frame 37 to Frame 37.1

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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SERVICE BULLETIN

Manpower Resources

Manhours 1.50

Minimum number of person 2

Subtask elapsed time 0.75

Skills NON SPECIFIC

Material necessary to do the job

Kit 265020D01R03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

240 F2627004120800 1 PLACARD

241 F2627004121400 1 PLACARD

242 F2627004121200 1 PLACARD

243 F2627004120400 1 PLACARD

244 F2627004120600 1 PLACARD

245 F2627004121600 1 PLACARD

246 F2627004121800 1 PLACARD

247 F2627004121000 1 PLACARD

248 G2627004020200 1 PLACARD

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Abrasion Resistant Coating

(Teflon Polyuret)

07-003 As required

General Purpose Adhesive

Honeycomb Filler

08-554 As required

References

Fig. A-GBFAA

Installation of the U-Section and the

Flow Metering System (FMS)

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

(a) Install the identification placards 4010WX, 4016WX, 4018WX, 5010WE, 5011WE,

5014WE, 5015WE, 5016WE, 5017WE, between FR37 and FR37.1.

Refer to Fig. A-GBFAA

1 Between FR37RH and FR37.1RH, install :

Refer to Fig. A-GBFAA Sheet 01, Fig. A-GBFAA Sheet 03 and Fig. A-GBFAA

Sheet 06

1 Placard F2627004120800 Item 240

1 Placard F2627004121400 Item 241

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1 Placard F2627004121200 Item 242

1 Placard F2627004120400 Item 243

1 Placard F2627004120600 Item 244

1 Placard F2627004121600 Item 245

1 Placard F2627004121800 Item 246

1 Placard F2627004121000 Item 247

1 Placard G2627004020200 Item 248

Bond the placard, Item 248, with :

General Purpose

Adhesive

Honeycomb Filler

08-554 As required

Protect the placard, Item 248, with :

Abrasion Resistant

Coating (Teflon

Polyuret)

07-003 As required

**CONF 005

(1) Subtask 265020-831-001-006 - Modify the Equipment and the Wiring in the RH

Overhead Panel 212VU.

Work Zones and Access Panels

Zone Access/Work location

212 Work location Electrical panel 212VU

Manpower Resources

Manhours 12.00

Minimum number of person 1

Subtask elapsed time 12.00

Skills ELECTRICAL

Material necessary to do the job

Kit 265020A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

2 ASNA2083BG2-10 7 Screw

6 NSA937901MA2206 1 Module

7 NSA937901FM 1 Module

10 F9251088400000 1 Plate

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

F1131101500000 Placard

F9000095226495 Bundle

NAS1102-04-5 44 Screw

NSA935401-03 50 TIE

NSA937901E2 1 Label

Kit 265020A06R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 F33110354A00 1 Plate

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Pure Mineral Vaseline Or

Petro-Latum

04-012 As required

Electrical Bond Varnish 07-001B As required

Sealant, High Temperature 08-007C As required

References

Aircraft Maintenance Manual (AMM) Task 11-00-00-400-802

Task 20-28-00-912-802

Fig. A-FBBAA

Modification of the Equipment in the RH

Overhead Panel 212VU

Sheet 01

Sheet 02

Sheet 03

Fig. A-FCAAA

Modification of the Wiring in the RH

Overhead Panel 212VU

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

(a) Remove and disconnect the RH overhead panel 212VU.

NOTE: Retain it.

(b) Modify the equipment in the RH overhead panel 212VU.

1 Remove the integrally lighted plate (212LF).

a Remove as shown in Fig. A-FBBAA Sheet 01 :

FIN 212LF

1 Plate-Integrally Lighted F33110359A00 Item (1) Discard

attached with :

7 Screw ASNA2083BG2-10 Item (2) Discard

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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2 Remove the indicator light BTL3 (5WX).

a Remove as shown in Fig. A-FBBAA Sheet 01 and Fig. A-FBBAA Sheet

02, Detail B :

FIN 5WX

1 Light-Indicator ABS0951A0LP110 Item (3) Discard

FIN 5WX1

1 Sleeve E0416-02 Item (4) Discard

FIN 5WXA

1 Connector E0417A01S Item (5) Discard

NOTE: Remove and discard the attachment hardware.

3 Replace the 212VU front plate.

a Remove and retain all the items of equipment that are installed on the

front plate.

b Remove as shown in Fig. A-FBBAA Sheet 01 :

1 Plate Assy- Front

212VU

F9251602100000 Item (10) Discard

attached with :

8 Screw NAS1102-06-5 Item (11) Retain

c On the new front plate, bond the placards (Refer to AMM Task

11-00-00-400-802) supplied in :

Placard Set-212VU F1131101500000

NOTE: Bond the applicable placards at the same locations as on

the old front plate. Discard the unused placards.

d Install as shown in Fig. A-FBBAA Sheet 03 :

1 Plate Assy- Front

212VU

F9251088400000 Item 10

attach with :

8 Screw NAS1102-06-5 Item (11)

NOTE: The screws Item (11) were retained at the removal.

e Install again all the items of equipment that you removed and retained

before the replacement of the front plate and attach with :

44 Screw NAS1102-04-5

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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Safety the screws with :

Sealant, High

Temperature

08-007C As required

NOTE: Replace the screws if they are damaged during the

removal. The quantity of screws to be replaced depends

on aircraft configuration (44 is the maximum).

f Do the electrical bonding (Refer to AMM Task 20-28-00-912-802) with :

Pure Mineral

Vaseline Or PetroLatum

04-012 As required

and

Electrical Bond

Varnish

07-001B As required

4 Modify the terminal block (582VT) as shown in Fig. A-FBBAA Sheet 01 and

Fig. A-FBBAA Sheet 02, Detail C.

a Remove from position 2 :

FIN 582VT2

1 Module-False NSA937901FM Item (6) Discard

b Remove from position 3 :

FIN 582VT3

1 Module NSA937901MA2204 Item (7) Discard

c Install at position 2 as shown in :

FIN 582VT2

1 Module NSA937901MA2206 Item 6

with

1 Label-Identification NSA937901E2

d Install at position 3 as shown in :

FIN 582VT3

1 Module-False NSA937901FM Item 7

5 Install the new integrally lighted plate (212LF).

a Install as shown in Fig. A-FBBAA Sheet 03 :

FIN 212LF

1 Plate-Integrally Lighted F33110354A00 Item 1

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attach with :

7 Screw ASNA2083BG2-10 Item 2

(c) Modify the wiring in the RH overhead panel 212VU.

1 Remove the wires as shown in the wiring diagrams Fig. A-FCAAA Sheet 01,

Fig. A-FCAAA Sheet 02 and as given in the hook-up chart lines :

- 1 thru 13 (Refer to Fig. A-FCAAA Sheet 04).

2 Modify the connections of the wires as shown in the wiring diagrams Fig. AFCAAA Sheet 02, Fig. A-FCAAA Sheet 03 and as given in the hook-up chart

lines :

- 17 thru 24 (Refer to Fig. A-FCAAA Sheet 04)

- 1 and 2 (Refer to Fig. A-FCAAA Sheet 05).

3 Install the wires as shown in the wiring diagram Fig. A-FCAAA Sheet 03 and

as given in the hook-up chart lines :

- 6 thru 12 (Refer to Fig. A-FCAAA Sheet 05), supplied in :

Bundle F9000095226495

4 Attach the wires with :

50 Tie-Cable NSA935401-03

(d) Install the RH overhead panel 212VU.

(2) Subtask 265020-831-002-001 - Modify the Equipment and the Wiring in the

Emergency Power Center 740VU.

Work Zones and Access Panels

Zone Access/Work location

121 Access Door 821, Door 132AZ

Work location Electrical panel 740VU

Manpower Resources

Manhours 3.50

Minimum number of person 1

Subtask elapsed time 3.50

Skills ELECTRICAL

Material necessary to do the job

Kit 265020A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

F9000095226495 Bundle

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

NSA935401-03 50 TIE

NSA935401-05 50 TIE

References

Fig. A-FBCAA

Modification of the Equipment in the

Emergency Power Center 740VU

Sheet 01

Fig. A-FCBAA

Modification of the Wiring in the

Emergency Power Center 740VU

Sheet 01

Sheet 02

(a) Open the emergency power center 740VU.

(b) Remove the wires as shown in the wiring diagram Fig. A-FCBAA Sheet 01 and as

given in the hook-up chart lines :

- 1 thru 8 (Refer to Fig. A-FCBAA Sheet 02).

(c) Modify the terminal block (703VT) as shown in Fig. A-FBCAA Sheet 01.

1 Remove from position 21 :

1 Clamp-End NSA937901S Retain

2 Remove from position 20 :

FIN 703VT20

1 Module NSA937901MA2004 Item (7) Discard

3 Install at position 20 :

1 Clamp-End NSA937901S

NOTE: The end clamp was retained at the removal.

(d) Install the wire as shown in the wiring diagram Fig. A-FCBAA Sheet 01 and as

given in the hook-up chart line :

- 12 (Refer to Fig. A-FCBAA Sheet 02), supplied in :

Bundle F9000095226495

(e) Attach the wire with :

50 Tie-Cable NSA935401-03

50 Tie-Cable NSA935401-05

(f) Close the emergency power center 740VU.

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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(3) Subtask 265020-831-003-001 - Modify the Equipment and the Wiring in the AC/DC

Main Power Center 710VU.

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 821, Door 132AZ

Work location Electrical panel 710VU

Manpower Resources

Manhours 3.50

Minimum number of person 1

Subtask elapsed time 3.50

Skills ELECTRICAL

Material necessary to do the job

Kit 265020A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

F9000095226495 Bundle

NSA935401-03 50 TIE

NSA935401-05 50 TIE

References

Fig. A-FBDAA

Modification of the Equipment in the

AC/DC Main Power Center 710VU

Sheet 01

Fig. A-FCCAA

Modification of the Wiring in the AC/DC

Main Power Center 710VU

Sheet 01

Sheet 02

(a) Open the AC/DC main power center 710VU.

(b) Remove the wires as shown in the wiring diagram Fig. A-FCCAA Sheet 01 and as

given in the hook-up chart lines :

- 1 thru 8 (Refer to Fig. A-FCCAA Sheet 02).

(c) Modify the terminal block (1712VT) as shown in Fig. A-FBDAA Sheet 01.

1 Remove from position 18 :

1 Clamp-End NSA937901S Retain

2 Remove from position 17 :

FIN 1712VT17

1 Module NSA937901MA2004 Item (7) Discard

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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3 Install at position 17 :

1 Clamp-End NSA937901S

NOTE: The end clamp was retained at the removal.

(d) Install the wire as shown in the wiring diagram Fig. A-FCCAA Sheet 01 and as

given in the hook-up chart line :

- 12 (Refer to Fig. A-FCCAA Sheet 02), supplied in :

Bundle F9000095226495

(e) Attach the wire with :

50 Tie-Cable NSA935401-03

50 Tie-Cable NSA935401-05

(f) CLose the AC/DC main power center 710VU.

(4) Subtask 265020-831-004-001 - Modify the Equipment and the Wiring in the LH

Relay Box 751VU.

Work Zones and Access Panels

Zone Access/Work location

121 Access Door 821, Door 132AZ

Work location Electrical panel 751VU

Manpower Resources

Manhours 3.50

Minimum number of person 1

Subtask elapsed time 3.50

Skills ELECTRICAL

References

Fig. A-FBEAA

Modification of the Equipment in the LH

Relay Box 751VU

Sheet 01

Fig. A-FCDAA

Modification of the Wiring in the LH

Relay Box 751VU

Sheet 01

Sheet 02

(a) Open the LH relay box 751VU.

(b) Remove the wires as shown in the wiring diagram Fig. A-FCDAA Sheet 01 and as

given in the hook-up chart lines :

- 1 thru 12 (Refer to Fig. A-FCDAA Sheet 02).

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 324

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SERVICE BULLETIN

(c) Remove from position E93, as shown in Fig. A-FBEAA Sheet 01 :

FIN 10WX

1 Relay E0245-28A0 Item (8) Discard

FIN 10WXA

1 Base E0250A0S Item (9) Discard

NOTE: Remove and discard the attachment hardware and the related

placard(s).

(d) Remove from position E89, as shown in Fig. A-FBEAA Sheet 01 :

FIN 11WX

1 Relay E0245-28A0 Item (8) Discard

FIN 11WXA

1 Base E0250A0S Item (9) Discard

NOTE: Remove and discard the attachment hardware and the related

placard(s).

(e) Close the LH relay box 751VU.

(5) Subtask 265020-831-005-001 - Modify the Equipment and the Wiring in the RH

Relay Box 752VU.

Work Zones and Access Panels

Zone Access/Work location

122 Access Door 821, Door 132AZ

Work location Electrical panel 752VU

Manpower Resources

Manhours 3.50

Minimum number of person 1

Subtask elapsed time 3.50

Skills ELECTRICAL

References

Fig. A-FBFAA

Modification of the Equipment in the RH

Relay Box 752VU

Sheet 01

Fig. A-FCEAA

Modification of the Wiring in the RH

Relay Box 752VU

Sheet 01

Sheet 02

(a) Open the RH relay box 752VU.

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 325

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SERVICE BULLETIN

(b) Remove the wires as shown in the wiring diagram Fig. A-FCEAA Sheet 01 and as

given in the hook-up chart lines :

- 1 thru 12 (Refer to Fig. A-FCEAA Sheet 02).

(c) Remove from position B37, as shown in Fig. A-FBFAA Sheet 01 :

FIN 12WX

1 Relay E0245-28A0 Item (8) Discard

FIN 12WXA

1 Base E0250A0S Item (9) Discard

NOTE: Remove and discard the attachment hardware and the related

placard(s).

(d) Remove from position B33, as shown in Fig. A-FBFAA Sheet 01 :

FIN 13WX

1 Relay E0245-28A0 Item (8) Discard

FIN 13WXA

1 Base E0250A0S Item (9) Discard

NOTE: Remove and discard the attachment hardware and the related

placard(s).

(e) Close the RH relay box 752VU.

(6) Subtask 265020-831-006-001 - Modify the Equipment and the Wiring in the Main

Rack 800VU.

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 821, Door 132AZ

Work location Electrical panel 800VU

Manpower Resources

Manhours 8.00

Minimum number of person 2

Subtask elapsed time 4.00

Skills ELECTRICAL

Material necessary to do the job

Kit 265020A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

7 NSA937901FM 1 Module

F9000095226495 Bundle

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 326

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ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

NSA935401-03 200 TIE

NSA935401-05 200 TIE

NSA935401-08 200 Tie

References

Aircraft Maintenance Manual (AMM) Task 26-16-34-000-801

Task 26-16-34-400-801

Fig. A-FBGAA

Modification of the Equipment in the

Main Rack 800VU

Sheet 01

Fig. A-FCFAA

Modification of the Wiring in the Main

Rack 800VU

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

Fig. A-FCGAA

Modification of the Pin Programming in

the Main Rack 800VU

Sheet 01

Sheet 02

(a) Remove and retain the SDCU (20WH) (Refer to AMM Task 26-16-34-000-801).

(b) Remove the wires as shown in the wiring diagrams Fig. A-FCFAA Sheet 01, Fig. AFCFAA Sheet 02, Fig. A-FCFAA Sheet 03, and as given in the hook-up chart lines :

- 1 thru 25 (Refer to Fig. A-FCFAA Sheet 05)

- 1 thru 3 (Refer to Fig. A-FCFAA Sheet 06).

(c) Modify the terminal block (2900VT) as shown in Fig. A-FBGAA Sheet 01.

1 Remove from position 50 :

FIN 2900VT50

1 Module NSA937901MA2011 Item (7) Discard

2 Install at position 50 :

FIN 2900VT50

1 Module-False NSA937901FM Item 7

(d) Install the wires as shown in the wiring diagram Fig. A-FCFAA Sheet 04 and as

given in the hook-up chart lines :

- 7 thru 18 (Refer to Fig. A-FCFAA Sheet 06), supplied in :

Bundle F9000095226495

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 327

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@A340-500/600

SERVICE BULLETIN

(e) Modify the connection of the wires as shown in the wiring diagram Fig. A-FCGAA

Sheet 01 and as given in the hook-up chart lines :

- 1 thru 4 (Refer to Fig. A-FCGAA Sheet 02).

(f) Attach the wires with :

200 Tie-Cable NSA935401-03

200 Tie-Cable NSA935401-05

200 Tie-Cable NSA935401-08

(g) Install the SDCU (20WH) (Refer to AMM Task 26-16-34-400-801).

(7) Subtask 265020-831-007-001 - Modify the Wiring between the Main Rack Shelf

801VU and the LH Relay Box 751VU.

Work Zones and Access Panels

Zone Access/Work location

121 Access Door 821, Door 132AZ

Work location from Electrical panel 801VU to Electrical panel

751VU

Manpower Resources

Manhours 3.50

Minimum number of person 1

Subtask elapsed time 3.50

Skills ELECTRICAL

Material necessary to do the job

Kit 265020A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

NSA936604CA0931 8 Cap

References

Fig. A-FBAAA

Location of the Working Areas

Sheet 01

Fig. A-FCHAA

Modification of the Wiring between the

Main Rack Shelf 801VU and the LH

Relay Box 751VU

Sheet 01

Sheet 02

(a) Modify the connections of the wires as shown in the wiring diagram Fig. A-FCHAA

Sheet 01 and as given in the hook-up chart lines :

- 1 thru 8 (Refer to Fig. A-FCHAA Sheet 02).

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 328

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@A340-500/600

SERVICE BULLETIN

(b) Install on the stowed wires ends :

8 Cap-Sealing NSA936604CA0931

(8) Subtask 265020-831-008-001 - Modify the Wiring between the Main Rack Shelf

802VU and the RH Relay Box 752VU.

Work Zones and Access Panels

Zone Access/Work location

122 Access Door 821, Door 132AZ

Work location from Electrical panel 802VU to Electrical panel

752VU

Manpower Resources

Manhours 3.50

Minimum number of person 1

Subtask elapsed time 3.50

Skills ELECTRICAL

References

Fig. A-FBAAA

Location of the Working Areas

Sheet 01

Fig. A-FCJAA

Modification of the Wiring between the

Main Rack Shelf 802VU and the RH

Relay Box 752VU

Sheet 01

Sheet 02

(a) Remove the wires as shown in the wiring diagram Fig. A-FCJAA Sheet 01 and as

given in the hook-up chart lines :

- 1 thru 4 (Refer to Fig. A-FCJAA Sheet 02).

(9) Subtask 265020-831-009-001 - Modify the Wiring between the Emergency Power

Center 740VU and the LH Relay Box 751VU.

Work Zones and Access Panels

Zone Access/Work location

121 Access Door 821, Door 132AZ

Work location from Electrical panel 740VU to Electrical panel

751VU

Manpower Resources

Manhours 3.50

Minimum number of person 1

Subtask elapsed time 3.50

Skills ELECTRICAL

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 329

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@A340-500/600

SERVICE BULLETIN

References

Fig. A-FBAAA

Location of the Working Areas

Sheet 01

Fig. A-FCKAA

Modification of the Wiring between the

Emergency Power Center 740VU and

the LH Relay Box 751VU

Sheet 01

Sheet 02

(a) Remove the wires as shown in the wiring diagram Fig. A-FCKAA Sheet 01 and as

given in the hook-up chart lines :

- 1 thru 4 (Refer to Fig. A-FCKAA Sheet 02).

(10) Subtask 265020-831-010-001 - Modify the Wiring between the AC/DC Main Power

Center 715VU and the RH Relay Box 752VU.

Work Zones and Access Panels

Zone Access/Work location

122 Access Door 821, Door 132AZ

Work location from Electrical panel 715VU to Electrical panel

752VU

Manpower Resources

Manhours 3.50

Minimum number of person 1

Subtask elapsed time 3.50

Skills ELECTRICAL

References

Fig. A-FBAAA

Location of the Working Areas

Sheet 01

Fig. A-FCLAA

Modification of the Wiring between the

AC/DC Main Power Center 715VU and

the RH Relay Box 752VU

Sheet 01

Sheet 02

(a) Remove the wires as shown in the wiring diagram Fig. A-FCLAA Sheet 01 and as

given in the hook-up chart lines :

- 1 thru 4 (Refer to Fig. A-FCLAA Sheet 02).

(11) Subtask 265020-831-011-001 - Modify the Wiring between the Main Rack Shelf

801VU and the Avionics Compartment at FR2.

Work Zones and Access Panels

Zone Access/Work location

From 121 Access Door 821, Door 132AZ

Work location Electrical panel 801VU

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 330

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SERVICE BULLETIN

To 211 Access Door 831, Door 841

Panel 211EW

Work location Frame 2

Manpower Resources

Manhours 3.50

Minimum number of person 1

Subtask elapsed time 3.50

Skills ELECTRICAL

Material necessary to do the job

Kit 265020A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

NSA936604CA0931 2 Cap

References

Fig. A-FBAAA

Location of the Working Areas

Sheet 01

Fig. A-FCMAA

Modification of the Wiring between the

Main Rack Shelf 801VU and the

Avionics Compartment at FR2

Sheet 01

Sheet 02

(a) Modify the connections of the wire as shown in the wiring diagram Fig. A-FCMAA

Sheet 01 and as given in the hook-up chart lines :

- 1 and 2 (Refer to Fig. A-FCMAA Sheet 02).

(b) Install on the stowed wire ends :

2 Cap-Sealing NSA936604CA0931

(12) Subtask 265020-831-012-001 - Modify the Wiring between the RH Overhead Panel

212VU and the Avionics Compartment (LH Side).

Work Zones and Access Panels

Zone Access/Work location

From 212 Access Door 831, Door 841

Work location Electrical panel 212VU

To 121 Access Door 821, Door 132AZ

Work location Electrical panel 751VU

Electrical panel 740VU

Frame 2

Electrical panel 801VU

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 331

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@A340-500/600

SERVICE BULLETIN

Manpower Resources

Manhours 10.00

Minimum number of person 2

Subtask elapsed time 5.00

Skills ELECTRICAL

Material necessary to do the job

Kit 265020A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

F9000095226495 Bundle

NSA935401-05 200 TIE

NSA935401-08 200 Tie

NSA936604CA0931 8 Cap

References

Fig. A-FBAAA

Location of the Working Areas

Sheet 01

Fig. A-FCNAA

Modification of the Wiring between the

RH Overhead Panel 212VU and the

Avionics Compartment (LH Side)

Sheet 01

Sheet 02

Sheet 03

(a) Modify the connections of the wires as shown in the wiring diagrams Fig. A-FCNAA

Sheet 01, Fig. A-FCNAA Sheet 02 and as given in the hook-up chart lines :

- 1 thru 8 (Refer to Fig. A-FCNAA Sheet 03).

(b) Install on the stowed wires ends :

8 Cap-Sealing NSA936604CA0931

(c) Install the wires as shown in the wiring diagram Fig. A-FCNAA Sheet 01 and as

given in the hook-up chart lines :

- 12 and 13 (Refer to Fig. A-FCNAA Sheet 02), supplied in :

Bundle F9000095226495

(d) Attach the wires with :

200 Tie-Cable NSA935401-05

200 Tie-Cable NSA935401-08

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 332

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SERVICE BULLETIN

(13) Subtask 265020-831-013-001 - Modify the Wiring between the RH Overhead Panel

212VU and the Avionics Compartment (RH Side).

Work Zones and Access Panels

Zone Access/Work location

From 212 Access Door 831, Door 841

Work location Electrical panel 212VU

To 122 Access Door 821, Door 132AZ

Panel 131BA

Work location Electrical panel 752VU

Electrical panel 715VU

Electrical panel 802VU

Frame 20

Manpower Resources

Manhours 10.00

Minimum number of person 2

Subtask elapsed time 5.00

Skills ELECTRICAL

Material necessary to do the job

Kit 265020A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

F9000095226495 Bundle

NSA935401-05 200 TIE

NSA935401-08 200 Tie

NSA936604CA0931 10 Cap

References

Fig. A-FBAAA

Location of the Working Areas

Sheet 01

Fig. A-FCPAA

Modification of the Wiring between the

RH Overhead Panel 212VU and the

Avionics Compartment (RH Side)

Sheet 01

Sheet 02

Sheet 03

(a) Modify the connections of the wires as shown in the wiring diagram Fig. A-FCPAA

Sheet 01, Fig. A-FCPAA Sheet 02 and as given in the hook-up chart lines :

- 1 thru 12 (Refer to Fig. A-FCPAA Sheet 03).

(b) Install on the stowed wires ends :

10 Cap-Sealing NSA936604CA0931

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 333

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@A340-500/600

SERVICE BULLETIN

(c) Install the wires as shown in the wiring diagram Fig. A-FCPAA Sheet 01 and as

given in the hook-up chart lines :

- 9 and 10 (Refer to Fig. A-FCPAA Sheet 02), supplied in :

Bundle F9000095226495

(d) Attach the wires with :

200 Tie-Cable NSA935401-05

200 Tie-Cable NSA935401-08

(14) Subtask 265020-831-201-002 - Remove the Fire Extinguishing Bottles, 4010WX,

4005WX and 4020WX.

Work Zones and Access Panels

Zone Access/Work location

132 Access Panel 132PM

Work location from Frame 35 to Frame 37.1

Manpower Resources

Manhours 3.00

Minimum number of person 2

Subtask elapsed time 1.50

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 26-23-41, Page Block 401

Fig. A-GBBAA

Removal of Fire Extinguishing Bottles

4005WX, 4010WX and 4020WX with

Cartridges.

Sheet 01

Sheet 02

Sheet 03

(a) Remove the Fire Extinguishing Bottle 2 (FWD), 4010WX.

Refer to Fig. A-GBBAA

1 Between FR35RH and FR36RH, remove the fire extinguishing bottle 4010WX

(Refer to AMM 26-23-41, Page Block 401) :

Refer to Fig. A-GBBAA Sheet 01 and Fig. A-GBBAA Sheet 02 :

1 Extinguisher-Fire 472625-3 Item (203) Retain

with :

4 Nut NAS1726-5E Item (100) Discard

4 Bolt NAS1305-2 Item (101) Discard

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 334

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@A340-500/600

SERVICE BULLETIN

1 Bolt NAS1304-9 Item (103) Discard

1 Nut NAS1726-4E Item (104) Discard

2 Bolt NAS563-11 Item (105) Discard

2 Washer NAS1149F0332P Item (106) Discard

(b) Remove the Fire Extinguishing Bottle 1 (MID), 4005WX.

Refer to Fig. A-GBBAA

1 Between FR36RH and FR37RH, remove the fire extinguishing bottle 4005WX

(Refer to AMM 26-23-41, Page Block 401) :

Refer to Fig. A-GBBAA Sheet 01 and Fig. A-GBBAA Sheet 03 :

1 Extinguisher-Fire 472931-3 Item (204) Retain

with :

4 Nut NAS1726-5E Item (100) Discard

4 Bolt NAS1305-2 Item (101) Discard

1 Bolt NAS1304-9 Item (103) Discard

1 Nut NAS1726-4E Item (104) Discard

2 Bolt NAS563-11 Item (105) Discard

2 Washer NAS1149F0332P Item (106) Discard

(c) Remove the Fire Extinguishing Bottle 3 (AFT), 4020WX.

Refer to Fig. A-GBBAA

1 Between FR37RH and FR37.1RH, remove the fire extinguishing bottle

4020WX (Refer to AMM 26-23-41, Page Block 401) :

Refer to Fig. A-GBBAA Sheet 01 and Fig. A-GBBAA Sheet 02 :

1 Extinguisher-Fire 472625-3 Item (203) Discard

with :

4 Nut NAS1726-5E Item (100) Discard

4 Bolt NAS1305-2 Item (101) Discard

1 Bolt NAS1304-9 Item (103) Discard

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 335

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@A340-500/600

SERVICE BULLETIN

1 Nut NAS1726-4E Item (104) Discard

2 Bolt NAS563-11 Item (105) Discard

2 Washer NAS1149F0332P Item (106) Discard

(15) Subtask 265020-831-202-001 - Remove the 4 Flow Metering Compact Units (FMCU),

FIN 4031WX, 4032WX, 4033WX and 4034WX.

Work Zones and Access Panels

Zone Access/Work location

132 Access Panel 132PM

Work location from Frame 35 to Frame 37.1

Manpower Resources

Manhours 4.00

Minimum number of person 2

Subtask elapsed time 2.00

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 26-23-43, Page Block 401

Fig. A-GBCAA

Removal of the 4 Flow Metering

Compact Units (FMCU), FIN 4031WX,

4032WX, 4033WX and 4034WX, the

related Plumbing Installations and

Placards

Sheet 01

Sheet 02

Sheet 03

(a) Remove the Flow Metering Compact Unit (FMCU), FIN 4031WX.

Refer to Fig. A-GBCAA

1 From FR35RH, remove the FMCU, FIN 4031WX (Refer to AMM 26-23-43,

Page Block 401) :

Refer to Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet 02 and Fig. A-GBCAA

Sheet 03

1 Meter-Flow, Compact

Unit

QA07907-01 Item (205) Discard

and

1 Hose Assy G2627007000000 Item (107) Discard

1 Tube Assy G2627006000000 Item (109) Discard

with :

1 Washer NAS1149F0332P Item (106) Discard

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 336

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@A340-500/600

SERVICE BULLETIN

1 Clamp NSA5516-06NJ Item (111) Discard

1 Screw NAS1096-3-10 Item (112) Discard

1 Nut NAS1726-3E Item (113) Discard

3 Screw NAS1100E4-36 Item (130) Discard

3 Washer NAS1149C0432R Item (131) Discard

1 Fitting A2627048220400 Item (132) Discard

2 O-Ring NSA8202-6 Item (133) Discard

1 Fitting A2627048221600 Item (134) Discard

(b) Remove the Flow Metering Compact Unit (FMCU), FIN 4032WX.

Refer to Fig. A-GBCAA

1 From FR36RH, remove the FMCU, FIN 4032WX (Refer to AMM 26-23-43,

Page Block 401) :

Refer to Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet 02 and Fig. A-GBCAA

Sheet 03

1 Meter-Flow, Compact

Unit

QA07907-01 Item (205) Discard

and

1 Hose Assy G2627007000200 Item (108) Discard

1 Tube Assy G2627006000200 Item (110) Discard

with :

1 Washer NAS1149F0332P Item (106) Discard

1 Clamp NSA5516-06NJ Item (111) Discard

1 Screw NAS1096-3-10 Item (112) Discard

1 Nut NAS1726-3E Item (113) Discard

3 Screw NAS1100E4-36 Item (130) Discard

3 Washer NAS1149C0432R Item (131) Discard

1 Fitting A2627048220400 Item (132) Discard

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 337

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@A340-500/600

SERVICE BULLETIN

2 O-Ring NSA8202-6 Item (133) Discard

1 Fitting A2627048221600 Item (134) Discard

(c) Remove the Flow Metering Compact Unit (FMCU), FIN 4033WX.

Refer to Fig. A-GBCAA

1 From FR37RH, remove the FMCU, FIN 4033WX (Refer to AMM 26-23-43,

Page Block 401) :

Refer to Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet 02 and Fig. A-GBCAA

Sheet 03

1 Meter-Flow, Compact

Unit

QA07907-01 Item (205) Discard

and

1 Hose Assy G2627007000000 Item (107) Discard

1 Tube Assy G2627006000000 Item (109) Discard

with :

1 Washer NAS1149F0332P Item (106) Discard

1 Clamp NSA5516-06NJ Item (111) Discard

1 Screw NAS1096-3-10 Item (112) Discard

1 Nut NAS1726-3E Item (113) Discard

3 Screw NAS1100E4-36 Item (130) Discard

3 Washer NAS1149C0432R Item (131) Discard

1 Fitting A2627048220400 Item (132) Discard

2 O-Ring NSA8202-6 Item (133) Discard

1 Fitting A2627048221600 Item (134) Discard

(d) Remove the Flow Metering Compact Unit (FMCU), FIN 4034WX.

Refer to Fig. A-GBCAA

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 338

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@A340-500/600

SERVICE BULLETIN

1 From FR37.1RH, remove the FMCU, FIN 4034WX (Refer to AMM 26-23-43,

Page Block 401) :

Refer to Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet 02 and Fig. A-GBCAA

Sheet 03

1 Meter-Flow, Compact

Unit

QA07907-01 Item (205) Discard

and

1 Hose Assy G2627007000200 Item (108) Discard

1 Tube Assy G2627006000200 Item (110) Discard

with :

1 Washer NAS1149F0332P Item (106) Discard

1 Clamp NSA5516-06NJ Item (111) Discard

1 Screw NAS1096-3-10 Item (112) Discard

1 Nut NAS1726-3E Item (113) Discard

3 Screw NAS1100E4-36 Item (130) Discard

3 Washer NAS1149C0432R Item (131) Discard

1 Fitting A2627048220400 Item (132) Discard

2 O-Ring NSA8202-6 Item (133) Discard

1 Fitting A2627048221600 Item (134) Discard

(16) Subtask 265020-831-203-001 - Remove the plumbing installations and placards.

Work Zones and Access Panels

Zone Access/Work location

132 Access Panel 132PM

Work location from Frame 35 to Frame 37.1

Manpower Resources

Manhours 2.50

Minimum number of person 2

Subtask elapsed time 1.25

Skills NON SPECIFIC

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 339

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@A340-500/600

SERVICE BULLETIN

References

Fig. A-GBCAA

Removal of the 4 Flow Metering

Compact Units (FMCU), FIN 4031WX,

4032WX, 4033WX and 4034WX, the

related Plumbing Installations and

Placards

Sheet 01

Sheet 02

Sheet 03

(a) Remove the plumbing installations between FR35RH thru FR37.1RH.

Refer to Fig. A-GBCAA

1 Between FR35RH and FR36RH, remove :

Refer to Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet 02 and Fig. A-GBCAA

Sheet 03

2 Reducer MS21916D10-4 Item (115) Discard

1 Tube Assy G2627005004400 Item (116) Discard

1 Tee NSA855113-34D Item (117) Discard

1 Tube Assy G2627005004200 Item (118) Discard

1 Hose A2627045200400 Item (209) Discard

with :

2 Washer NAS1149F0332P Item (106) Discard

2 Screw NAS1096-3-10 Item (112) Discard

2 Nut NAS1726-3E Item (113) Discard

2 Clamp NSA5516-18NJ Item (121) Discard

1 Rod End NSA8141-04R Item (135) Discard

1 Nut NAS509-5 Item (136) Discard

1 Rod End NSA8140-04RK Item (137) Discard

2 Lead-Bonding E0090-41-320 Item (138) Discard

1 Bolt NAS1304-12 Item (139) Discard

1 Nut NAS1726-4E Item (104) Discard

1 Washer NAS1149D0432K Item (140) Discard

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 340

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SERVICE BULLETIN

1 Washer-Lock NSA5355-5CA Item (141) Discard

2 Between FR36RH and FR37RH, remove :

Refer to Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet 02 and Fig. A-GBCAA

Sheet 03

2 Washer NAS1149F0332P Item (106) Discard

2 Screw NAS1096-3-10 Item (112) Discard

2 Nut NAS1726-3E Item (113) Discard

1 Tube Assy G2627005004000 Item (120) Discard

2 Clamp NSA5516-18NJ Item (121) Discard

1 Cross NSA855140-22D Item (122) Discard

1 Union MS21902D10 Item (123) Discard

1 Tube Assy G2627005003800 Item (124) Discard

2 Tee NSA855008D10 Item (125) Discard

1 Rod End NSA8141-04R Item (135) Retain

1 Nut NAS509-5 Item (136) Retain

1 Rod End NSA8140-04RK Item (137) Retain

2 Lead-Bonding E0090-41-320 Item (138) Discard

1 Bolt NAS1304-12 Item (139) Discard

1 Nut NAS1726-4E Item (104) Discard

1 Washer NAS1149D0432K Item (140) Discard

1 Washer-Lock NSA5355-5CA Item (141) Discard

1 Tube Assy G2627005006400 Item (142) Discard

1 Hose A2627045200400 Item (209) Retain

2 Hose Assy F2627007100200 Item (210) Retain

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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SERVICE BULLETIN

3 Between FR37RH and FR37.1RH, remove :

Refer to Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet 02 and Fig. A-GBCAA

Sheet 03

2 Reducer MS21916D10-4 Item (115) Discard

1 Tube Assy G2627005004400 Item (116) Discard

1 Tee NSA855113-34D Item (117) Discard

1 Tube Assy G2627005003400 Item (119) Discard

1 Tee NSA855008D10 Item (125) Discard

1 Tube Assy G2627005003600 Item (129) Discard

1 Rod End NSA8141-04R Item (135) Retain

1 Nut NAS509-5 Item (136) Retain

1 Rod End NSA8140-04RK Item (137) Retain

2 Lead-Bonding E0090-41-320 Item (138) Discard

1 Bolt NAS1304-12 Item (139) Discard

1 Nut NAS1726-4E Item (104) Discard

1 Washer NAS1149D0432K Item (140) Discard

1 Washer-Lock NSA5355-5CA Item (141) Discard

1 Hose A2627045200400 Item (209) Retain

(b) Remove the placards between FR35RH thru FR37.1RH.

Refer to Fig. A-GBCAA

1 Between FR35RH and FR36RH, remove the placards 4010WX, 4031WX and

4032WX :

2 Label NSA931025-02F Item (126) Discard

1 Placard G2627004020200 Item (127) Discard

2 Between FR37RH and FR37.1RH, remove the placards 4020WX, 4033WX

and 4034WX :

2 Label NSA931025-02F Item (126) Discard

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 342

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@A340-500/600

SERVICE BULLETIN

1 Placard G2627004020400 Item (128) Discard

(17) Subtask 265020-831-204-001 - Remove the brackets and the insulation blankets

between FR35RH thru FR37.1RH.

Work Zones and Access Panels

Zone Access/Work location

132 Work location from Frame 35 to Frame 37.1

Manpower Resources

Manhours 3.50

Minimum number of person 2

Subtask elapsed time 1.75

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 25-80-00-000-801

Fig. A-GBDAA

Removal of the Brackets

Sheet 01

Sheet 02

Sheet 03

(a) Remove the insulation blankets in the affected area (Refer to AMM Task

25-80-00-000-801).

(b) Remove the brackets between FR35RH thru FR37.1RH.

Refer to Fig. A-GBDAA

1 Between FR35 and FR36, STGR 29RH, remove :

Refer to Fig. A-GBDAA Sheet 01 and Fig. A-GBDAA Sheet 03

1 Section-T F5397460021800 Item (161) Discard

1 Bracket Assy F5397484500200 Item (162) Discard

2 From FR35RH, STGR31, remove :

Refer to Fig. A-GBDAA Sheet 01 and Fig. A-GBDAA Sheet 03

1 Bracket F5397463611000 Item (163) Discard

3 From FR36RH, STGR31, remove :

Refer to Fig. A-GBDAA Sheet 01 and Fig. A-GBDAA Sheet 03

1 Bracket F5397463610800 Item (164) Discard

4 From FR37RH, STGR31, remove :

Refer to Fig. A-GBDAA Sheet 01 and Fig. A-GBDAA Sheet 03

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 343

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@A340-500/600

SERVICE BULLETIN

1 Bracket F5397463611000 Item (163) Discard

5 From FR37.1RH, STGR31, remove :

Refer to Fig. A-GBDAA Sheet 01 and Fig. A-GBDAA Sheet 03

1 Bracket F5397463610800 Item (164) Discard

6 From the crossbeam at FR35 at -Y2462, remove :

Refer to Fig. A-GBDAA Sheet 01 and Fig. A-GBDAA Sheet 02

1 Bracket Assy F5397800200000 Item (165) Discard

1 Bracket F5397461823000 Item (166) Discard

7 From the crossbeam at FR36 at -Y2462, remove :

Refer to Fig. A-GBDAA Sheet 01 and Fig. A-GBDAA Sheet 02

1 Bracket Assy F5397800200000 Item (165) Discard

1 Bracket F5397469928000 Item (167) Discard

8 Between FR35RH and FR36RH, remove :

Refer to Fig. A-GBDAA Sheet 01 and Fig. A-GBDAA Sheet 02

1 Strut Assy F5397883300000 Item (168) Discard

(18) Subtask 265020-831-213-001 - Install the brackets, modify the insulation blankets

and close the rivet holes between FR35RH thru FR37.1RH.

Work Zones and Access Panels

Zone Access/Work location

132 Work location from Frame 35 to Frame 37.1

Manpower Resources

Manhours 7.00

Minimum number of person 2

Subtask elapsed time 3.50

Skills NON SPECIFIC

Material necessary to do the job

Kit 265020D02R04

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

170 EN6081D4-09 28 RIVET

171 EN6081D6-14 30 RIVET

252 F5397757020200 2 ANGLE

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 344

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@A340-500/600

SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

253 F5397462009600 1 BRACKET

254 F5397462009800 1 BRACKET

281 ABS1577A05 1 BRACKET

282 ABS0787B05B 1 BRACKET

References

Aircraft Maintenance Manual (AMM) Task 20-28-00-912-802

Task 25-80-00-200-801

Task 25-80-00-400-801

Fig. A-GBGAA

Installation of the Brackets

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Fig. A-GBDAA

Removal of the Brackets

Sheet 01

Sheet 02

Sheet 03

(a) Install the brackets and close the existing rivet holes.

Refer to Fig. A-GBDAA and Fig. A-GBGAA

1 Between FR35 and FR36, on STGR29RH and STGR30RH, close the rivet

holes in the stringers with :

Refer to Fig. A-GBDAA Sheet 01, Fig. A-GBDAA Sheet 02 and Fig. A-GBDAA

Sheet 03

4 Rivet EN6081D6-14 Item 171

2 On FR35 and FR36, STGR31RH, close the rivet holes in the frames with :

Refer to Fig. A-GBDAA Sheet 01, Fig. A-GBDAA Sheet 02 and Fig. A-GBDAA

Sheet 03

8 Rivet EN6081D6-14 Item 171

3 Between FR36 and FR37, on STGR30RH, install this bracket on the stringer :

Refer to Fig. A-GBGAA Sheet 01 and Fig. A-GBGAA Sheet 02

1 Angle-Bonding F5397757020200 Item 252

with :

3 Rivet EN6081D4-09 Item 170

NOTE: Do the electrical bonding (Refer to AMM Task

20-28-00-912-802)

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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SERVICE BULLETIN

4 On FR37 and FR37.1, STGR31RH, close the rivet holes in the frames with :

Refer to Fig. A-GBDAA Sheet 01,Fig. A-GBDAA Sheet 02 and Fig. A-GBDAA

Sheet 03

8 Rivet EN6081D6-14 Item 171

5 On FR37, between STGR31RH and STGR32RH, install this bracket :

Refer to Fig. A-GBGAA Sheet 01 and Fig. A-GBGAA Sheet 02

1 Bracket Assy F5397462009600 Item 253

with :

4 Rivet EN6081D6-14 Item 171

NOTE: Do the electrical bonding (Refer to AMM Task

20-28-00-912-802)

NOTE: Existing rivet spacing must be used.

6 Between FR37 and FR37.1, on STGR30RH, install this bracket :

Refer to Fig. A-GBGAA Sheet 01 and Fig. A-GBGAA Sheet 02

1 Angle-Bonding F5397757020200 Item 252

with :

3 Rivet EN6081D4-09 Item 170

7 Between FR37 and FR37.1, on STGR30RH, install this bracket :

Refer to Fig. A-GBGAA Sheet 01 and Fig. A-GBGAA Sheet 03

1 Bracket ABS1577A05 Item 281

with :

3 Rivet EN6081D4-09 Item 170

NOTE: Do the electrical bonding (Refer to AMM Task

20-28-00-912-802)

8 On FR37.1, between STGR31RH and STGR32RH, install this bracket :

Refer to Fig. A-GBGAA Sheet 01 and Fig. A-GBGAA Sheet 02

1 Bracket Assy F5397462009800 Item 254

with :

4 Rivet EN6081D6-14 Item 171

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 346

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SERVICE BULLETIN

NOTE: Do the electrical bonding (Refer to AMM Task

20-28-00-912-802)

NOTE: Existing rivet spacing must be used.

9 On the crossbeam at FR35, between -Y1959 and -Y2462, close the rivet holes

in the crossbeam with :

Refer to Fig. A-GBDAA Sheet 01, Fig. A-GBDAA Sheet 02 and Fig. A-GBDAA

Sheet 03

10 Rivet EN6081D4-09 Item 170

10 On the crossbeam at FR36, outboard of -Y2462, close the rivet holes in the

crossbeam with :

Refer to Fig. A-GBDAA Sheet 01, Fig. A-GBDAA Sheet 02 and Fig. A-GBDAA

Sheet 03

9 Rivet EN6081D4-09 Item 170

11 On the crossbeam at FR36, outboard of -Y2462, install this bracket :

Refer to Fig. A-GBGAA Sheet 01 and Fig. A-GBGAA Sheet 03

1 Bracket-Z ABS0787B05B Item 282

with :

2 Rivet EN6081D6-14 Item 171

NOTE: Do the electrical bonding (Refer to AMM Task

20-28-00-912-802)

(b) Between FR36 thru FR37.1RH modify the insulation blankets in the affected area.

1 Adapt the insulation blankets for the new locations of brackets (Refer to AMM

Task 25-80-00-200-801).

(c) Install the modified insulation in the affected area (Refer to AMM Task

25-80-00-400-801).

(19) Subtask 265020-831-216-001 - Modify the equipment and the wiring of the

FMCU/FMS outlet pressure switches 4031WX, 4032WX, 4033WX, 4034WX, 4016WX

and 4018WX of the fire extinguishing bottles Nos. 2 and 3.

Work Zones and Access Panels

Zone Access/Work location

132 Work location from Frame 35 to Frame 37.1

200 Work location Electrical panel 801VU

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 347

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@A340-500/600

SERVICE BULLETIN

Manpower Resources

Manhours 1.50

Minimum number of person 2

Subtask elapsed time 0.75

Skills ELECTRICAL

Material necessary to do the job

Kit 265020D03R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

173 G9237018016600 1 PLCRDSET

174 NSA935401-04 8 TIE

175 NSA935401-05 15 TIE

References

Process and Material Specification

(PMS)

Process and Material Specification (PMS)

01-07-10

Fig. A-GWAAA

Modification of the Wiring of the

FMCU/FMS Outlet Pressure Switches

4031WX, 4032WX, 4033WX, 4034WX,

4016WX and 4018WX

Sheet 01

Sheet 02

Fig. A-GHAAA

Hook-up Chart

Sheet 01

Fig. A-GBLAA

Stowage of the Electrical Wires of the

Connectors 4031WX-A, 4032WX-A

4011WX-A, 4012WX-A and 4013WX-A

Sheet 01

Sheet 02

Sheet 03

Sheet 04

(a) Modify the wiring of the FMCU/FMS outlet pressure switches.

1 Disconnect these electrical wires from the connectors 4031WX-A and

4032WX-A.

Refer to Fig. A-GWAAA Sheet 01 (Wiring)

Refer to Fig. A-GHAAA Sheet 01 (Hook-up Chart), LINES 1, 2, 3 and 4

2 Remove the connectors 4031WX-A and 4032WX-A and discard.

Refer to Fig. A-GBLAA Sheet 01

Remove :

2 Connector-Plug EN2997KE60803BN Item (265) Discard

and remove the following attachment parts :

4 Screw NAS1801-08-7 Item (267) Discard

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 348

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@A340-500/600

SERVICE BULLETIN

2 Nut MS21042-08 Item (268) Discard

4 Washer NAS1149CN816R Item (269) Discard

2 Clamp MS21919WCH8 Item (270) Retain

2 Screw NAS1801-08-23 Item (271) Discard

2 Lanyard DAN80-3-150 Item (273) Discard

2 Sleeve-Protective NSA935809-09 Item (274) Discard

5 Cable Mount Item (277) Retain

3 Disconnect these electrical wires from the connectors 4033WX-A and

4034WX-A.

Refer to Fig. A-GWAAA Sheet 01 (Wiring)

Refer to Fig. A-GHAAA Sheet 01 (Hook-up Chart), LINES 5, 6, 7 and 8

4 Reroute and install the electrical wires :

Refer to Fig. A-GWAAA Sheet 02 (Wiring)

Refer to Fig. A-GHAAA Sheet 01 (Hook-up Chart), LINES 13, 14, 15 and 16

with :

15 Tie-Cable NSA935401-05 Item 175

and attach the placards, identified 4016WX-A, 4018WX-A and the SB/MOD

placards :

1 Placardset G9237018016600 Item 173

with :

8 Tie-Cable NSA935401-04 Item 174

(20) Subtask 265020-831-209-001 - Modify the equipment and the wiring of the fire

extinguishing bottle No. 3 (AFT), 4020WX, and relocated fire extinguishing bottle

No. 2 (AFT), 4010WX.

Work Zones and Access Panels

Zone Access/Work location

132 Work location from Frame 35 to Frame 37.1

200 Work location Electrical panel 801VU

Electrical panel 802VU

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 349

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@A340-500/600

SERVICE BULLETIN

Manpower Resources

Manhours 1.00

Minimum number of person 2

Subtask elapsed time 1.00

Skills ELECTRICAL

Material necessary to do the job

Kit 265020D03R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

173 G9237018016600 1 PLCRDSET

174 NSA935401-04 12 TIE

175 NSA935401-05 15 TIE

176 EN3155-003F1614 2 CONTACT

References

Fig. A-GWBAA

Modification of the Wiring of the Fire

Extinguishing Bottle No. 3 (previously

AFT), 4020WX, and relocated Fire

Extinguishing Bottle No. 2 (now AFT),

4010WX

Sheet 01

Sheet 02

Fig. A-GHBAA

Hook-up Chart

Sheet 01

(a) Modify the wiring of the cartridges and the pressure switch of the fire extinguishing

bottle (AFT), 4020WX (4010WX)

1 Disconnect these electrical wires from the connector 2625VC-A.

Refer to Fig. A-GWBAA Sheet 01 (Wiring)

Refer to Fig. A-GHBAA Sheet 01 (Hook-up Chart), LINES 1 and 11, END 2

2 Reroute and install the electrical wires on the connector 2511VC-A.

Refer to Fig. A-GWBAA Sheet 02 (Wiring)

Refer to Fig. A-GHBAA Sheet 01 (Hook-up Chart), LINES 2 and 12, END 2

3 Disconnect these electrical wires from the connector 2636VC-A.

Refer to Fig. A-GWBAA Sheet 01 (Wiring)

Refer to Fig. A-GHBAA Sheet 01 (Hook-up Chart), LINES 5 and 15, END 2

NOTE: Cut off the contacts directly behind the contacts.

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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SERVICE BULLETIN

4 Reroute and install the electrical wires on the connector 2508VC-A.

Refer to Fig. A-GWBAA Sheet 02 (Wiring)

Refer to Fig. A-GHBAA Sheet 01 (Hook-up Chart), LINES 6 and 16, END 2

with :

2 Contact-Socket EN3155-003F1614 Item 176

5 Disconnect the electrical wire from the connector 2044VC-A.

Refer to Fig. A-GWBAA Sheet 01 (Wiring)

Refer to Fig. A-GHBAA Sheet 01 (Hook-up Chart), LINE 23, END 2

6 Reroute and install the electrical wire on the connector 2016VC-A.

Refer to Fig. A-GWBAA Sheet 02 (Wiring)

Refer to Fig. A-GHBAA Sheet 01 (Hook-up Chart), LINE 24, END 2

7 Attach the placards, identified 4011WX-A, 4012WX-A, 4013WX-A and the

SB/MOD placards :

1 Placardset G9237018016600 Item 173

with :

12 Tie-Cable NSA935401-04 Item 174

8 Install the tie-cables on the wire harnesses :

15 Tie-Cable NSA935401-05 Item 175

NOTE: For the stowage position of the connectors 4011WX-A,

4012WX-A, 4013WX-A, 4031WX-A and 4032WX-A, refer to

(22) Subtask 265020-831-218-001.

(21) Subtask 265020-831-210-001 - Modify the Equipment and the Wiring of the

previous Fire Extinguishing Bottle No. 2 (FWD), 4010WX.

Work Zones and Access Panels

Zone Access/Work location

132 Work location from Frame 35 to Frame 36

200 Work location Electrical panel 801VU

Electrical panel 802VU

Manpower Resources

Manhours 1.50

Minimum number of person 1

Subtask elapsed time 1.50

Skills ELECTRICAL

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 351

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SERVICE BULLETIN

References

Fig. A-GWCAA

Modification of the Wiring of the Fire

Extinguishing Bottle No. 2 (FWD),

4010WX

Sheet 01

Sheet 02

Fig. A-GHCAA

Hook-up Chart

Sheet 01

Fig. A-GBLAA

Stowage of the Electrical Wires of the

Connectors 4031WX-A, 4032WX-A

4011WX-A, 4012WX-A and 4013WX-A

Sheet 01

Sheet 02

Sheet 03

Sheet 04

(a) Modify the wiring of the previous fire extinguishing bottle No. 2 (FWD), 4010WX.

1 Disconnect these electrical wires from the connectors 4011WX-A, 4012WX-A

and 4013WX-A.

Refer to Fig. A-GWCAA Sheet 01 (Wiring)

Refer to Fig. A-GHCAA Sheet 01 (Hook-up Chart), LINES 1, 5, 11, 15 and 23

Refer to Fig. A-GHCAA Sheet 01 (Hook-up Chart), LINES 3, 7, 9, 13, 17, 19,

21, END 1

2 Remove the connectors 4011WX-A, 4012WX-A and 4013WX-A and discard.

Refer to Fig. A-GBLAA Sheet 01

Remove :

2 Connector EN2997KE61005BN Item (264) Discard

1 Connector-Plug EN2997KE60803BN Item (265) Discard

and remove the following attachment parts :

1 Tie-Cable NSA935401-03 Item (266) Discard

5 Screw NAS1801-08-7 Item (267) Discard

2 Nut MS21042-08 Item (268) Discard

4 Washer NAS1149CN816R Item (269) Discard

2 Clamp MS21919WCH8 Item (270) Discard

1 Screw NAS1801-08-29 Item (272) Discard

2 Lanyard DAN80-3-150 Item (273) Discard

2 Sleeve-Protective NSA935809-09 Item (274) Discard

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 352

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@A340-500/600

SERVICE BULLETIN

2 Cable Mount Item (277) Retain

NOTE: For the stowage position of the connectors 4011WX-A,

4012WX-A, 4013WX-A, 4031WX-A and 4032WX-A, refer to

(22) Subtask 265020-831-218-001.

(22) Subtask 265020-831-218-001 - Put the electrical wires of the connectors 4031WX-A,

4032WX-A 4011WX-A, 4012WX-A and 4013WX-A in a stowage position.

Work Zones and Access Panels

Zone Access/Work location

132 Work location from Frame 35 to Frame 37.1

Manpower Resources

Manhours 2.50

Minimum number of person 1

Subtask elapsed time 2.50

Skills ELECTRICAL

Material necessary to do the job

Kit 265020D03R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

173 G9237018016600 1 PLCRDSET

177 NSA936603CC0100 23 CAP

Kit 265020D05R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

266 NSA935401-03 25 TIE

269 NAS1149CN816R 4 WASHER

270 MS21919WCH8 4 CLAMP

271 NAS1801-08-23 2 SCREW

272 NAS1801-08-29 1 SCREW

274 NSA935809-09 4 SLEEVE

275 NAS1801-08-25 1 SCREW

References

Fig. A-GBLAA

Stowage of the Electrical Wires of the

Connectors 4031WX-A, 4032WX-A

4011WX-A, 4012WX-A and 4013WX-A

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Fig. A-GHAAA

Hook-up Chart

Sheet 01

Fig. A-GHCAA

Hook-up Chart

Sheet 01

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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SERVICE BULLETIN

References

Fig. A-GWAAA

Modification of the Wiring of the

FMCU/FMS Outlet Pressure Switches

4031WX, 4032WX, 4033WX, 4034WX,

4016WX and 4018WX

Sheet 01

Sheet 02

Fig. A-GWCAA

Modification of the Wiring of the Fire

Extinguishing Bottle No. 2 (FWD),

4010WX

Sheet 01

Sheet 02

(a) Put the electrical wires of the connectors 4031WX-A and 4032WX-A in a stowage

position.

1 Put the electrical wires in a stowage position.

Refer to Fig. A-GBLAA Sheet 01, Fig. A-GBLAA Sheet 02, Fig. A-GBLAA

Sheet 03 and Fig. A-GBLAA Sheet 04

Refer to Fig. A-GWAAA Sheet 02 (Wiring)

Refer toFig. A-GHAAA Sheet 01 (Hook-up Chart), LINES 9, 10, 11 and 12

with :

6 Cap NSA936603CC0100 Item 177

NOTE: Do not cut off the contacts.

Attach the electrical wires in a stowage position.

with :

2 Washer NAS1149CN816R Item 269

2 Clamp MS21919WCH8 Item 270

2 Clamp MS21919WCH8 Item (270) Retained at

removal

1 Screw NAS1801-08-23 Item 271

2 Sleeve-Protective NSA935809-09 Item 274

1 Screw NAS1801-08-25 Item 275

5 Cable Mount Item (277) Retained at

removal

20 Tie-Cable NSA935401-03 Item 266

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 354

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SERVICE BULLETIN

(b) Put the electrical wires of the connectors 4011WX-A, 4012WX-A and 4013WX-A in

a stowage position.

1 Put the electrical wires in a stowage position.

Refer to Fig. A-GBLAA Sheet 01, Fig. A-GBLAA Sheet 02, Fig. A-GBLAA

Sheet 03 and Fig. A-GBLAA Sheet 04

Refer to Fig. A-GWCAA Sheet 02 (Wiring)

Refer to Fig. A-GHCAA Sheet 01 (Hook-up Chart), LINES 2, 6, 12, 16 and 24

Refer to Fig. A-GHCAA Sheet 01 (Hook-up Chart), LINES 4, 8, 10, 14, 18, 20

and 22, END 1

with :

17 Cap NSA936603CC0100 Item 177

NOTE: Do not cut off the contacts.

Attach the electrical wires in a stowage position.

with :

2 Washer NAS1149CN816R Item 269

2 Clamp MS21919WCH8 Item 270

1 Screw NAS1801-08-23 Item 271

1 Screw NAS1801-08-29 Item 272

2 Sleeve-Protective NSA935809-09 Item 274

2 Cable Mount Item (277) Retained at

removal

and attach the SB/MOD placards :

1 Placardset G9237018016600 Item 173

with :

5 Tie-Cable NSA935401-03 Item 266

(23) Subtask 265020-831-208-001 - Adapt the plumbing installation.

Work Zones and Access Panels

Zone Access/Work location

132 Work location from Frame 36 to Frame 37

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 355

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SERVICE BULLETIN

Manpower Resources

Manhours 3.00

Minimum number of person 2

Subtask elapsed time 1.50

Skills NON SPECIFIC

Material necessary to do the job

Kit 265020D04R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

113 NAS1726-3E 2 NUT

121 NSA5516A18NJ 2 CLAMP

125 NSA855008D10 1 TEE

144 NAS1149C0332R 2 WASHER

155 NSA5527-03-03 2 SPACER

157 NAS1801-3-12 2 SCREW

158 NSA855006D10 2 UNION

251 G2627005013000 1 TUBE

253 G2627005002000 1 TUBE

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Internal Polyurethane

Varnish

07-017 As required

Solvent General Purpose 11-026 As required

Low Voc Anti-Corrosion

Primer

16-006F As required

Lint-Free Cotton Cloth 19-003 As required

Standard tool TOOLD01

ITEM TOOL N ̊ TOOL NAME QTY SEE

NOTES

D12102C07-02 PERMASWAGE Repair

Kit D12000 Series

1

References

Aircraft Maintenance Manual (AMM) 20-23-11, Page Block 201

Fig. A-GBEAA

Adaption of the Plumbing Installation

Sheet 01

Sheet 02

Sheet 03

Sheet 04

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 356

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SERVICE BULLETIN

References

Fig. A-GBFAA

Installation of the U-Section and the

Flow Metering System (FMS)

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

(a) Remove the fire extinguishing tubes from FR36 and FR37.

Refer to Fig. A-GBEAA

1 Remove and discard these items from FR36RH :

Refer to Fig. A-GBEAA Sheet 01, Fig. A-GBEAA Sheet 02 and Fig. A-GBEAA

Sheet 04

1 Nut NAS1726-3E Item (113) Discard

1 Clamp NSA5516-18NJ Item (121) Discard

1 Washer NAS1149C0332R Item (144) Discard

1 Spacer NSA5527-03-03 Item (155) Discard

1 Screw NAS1096-3-14 Item (157) Discard

2 Cut the fire extinguishing tube, Item (250), at the position shown in Fig. AGBEAA Sheet 02 (Refer to AMM 20-23-11, Page Block 201).

3 Remove the fire extinguishing tube, Item (250), partly between the cut and the

outboard X-connection fitting :

1 Tube Assy, partly G2627005013000 Item (250) Discard

4 Deburr the remaining tube, Item (250), (Refer to AMM 20-23-11, Page Block

201).

5 Clean the remaining tube, Item (250), with :

Solvent General

Purpose

11-026 As required

and

Lint-Free Cotton

Cloth

19-003 As required

6 Remove and discard these items from FR37RH :

Refer to Fig. A-GBEAA Sheet 01, Fig. A-GBEAA Sheet 02 and Fig. A-GBEAA

Sheet 04

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 357

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SERVICE BULLETIN

1 Nut NAS1726-3E Item (113) Discard

1 Clamp NSA5516-18NJ Item (121) Discard

1 Washer NAS1149C0332R Item (144) Discard

1 Spacer NSA5527-03-03 Item (155) Discard

1 Screw NAS1096-3-14 Item (157) Discard

7 Cut the fire extinguishing tube, Item (252), at the position shown in Fig. AGBEAA Sheet 02 (Refer to AMM 20-23-11, Page Block 201).

8 Remove the fire extinguishing tube, Item (252), partly between the cut and the

outboard T-connection fitting :

1 Tube Assy, partly G2627005002000 Item (252) Discard

1 Tee NSA855008D10 Item (125) Discard

9 Deburr the remaining tube, Item (252), (Refer to AMM 20-23-11, Page Block

201).

10 Clean the remaining tube, Item (252), with :

Solvent General

Purpose

11-026 As required

and

Lint-Free Cotton

Cloth

19-003 As required

(b) Install the fire extinguishing tubes on FR36 and FR37.

CAUTION: BEFORE YOU CONNECT THE FIRE EXTINGUISHING TUBES

WITH THE PERMASWAGE TOOL, MAKE SURE THAT THE FIRE

EXTINGUISHING TUBES ARE INSTALLED STRESS-FREE IN

THEIR CLAMPS.

CAUTION: DO NOT BEND THE TUBE WHEN YOU INSTALL IT. IF THE

TUBE IS BENT, IT CAN BECOME DAMAGED.

CAUTION: IF YOU USE DUST CAPS FOR THE CONTAMINATION

PROTECTION OF OPEN LINES, ALWAYS BE SURE TO

INSTALL THE CAPS AROUND THE TUBE ENDS AND NOT IN

THE TUBE ENDS. THERE CAN BE BLOCKAGE OF THE FLOW

THROUGH THE TUBES IF THESE TUBES ARE INSTALLED

ACCIDENTALLY WITH DUST CAPS IN THE TUBE ENDS.

NOTE: The fire extinguishing tubes must be installed with their related

clamps.

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 358

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SERVICE BULLETIN

Refer to Fig. A-GBEAA

1 Install temporarily, Item 233, before install the other tubes.

Refer to Fig. A-GBFAA Sheet 01

2 Install the tube, Item 251, at FR36RH.

Refer to Fig. A-GBEAA Sheet 01, Fig. A-GBEAA Sheet 02 and Fig. A-GBEAA

Sheet 03

1 Tube Assy G2627005013000 Item 251

with :

1 Union NSA855006D10 Item 158

3 Connect the fire extinguishing tubes, Item (250), and Item 251, with the union,

Item 158, (Refer to AMM 20-23-11, Page Block 201).

D12102C07-02 PERMASWAGE

Repair Kit D12000

Series

1

NOTE: Use these swaging tools of the D12000 series :

- Head assembly D12210-56 with power unit D12010-52.

NOTE: The surface protection on both ends of the pipes must be

removed on a length of 43mm (1.692in.).

4 After the installation of the union, Item 158, perform surface protection with :

Low Voc AntiCorrosion Primer16-006F As required

and

Internal

Polyurethane

Varnish

07-017 As required

5 Install the clamp, Item 121, at FR36RH.

Fig. A-GBEAA Sheet 01, Fig. A-GBEAA Sheet 02 and Fig. A-GBEAA Sheet

03

1 Clamp NSA5516A18NJ Item 121

with :

1 Nut NAS1726-3E Item 113

1 Washer NAS1149C0332R Item 144

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 359

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SERVICE BULLETIN

1 Spacer NSA5527-03-03 Item 155

1 Screw NAS1801-3-12 Item 157

6 Install temporarily, Item 234 and 238, before install the other tubes.

Refer to Fig. A-GBFAA Sheet 01

7 Install the tube, Item 253, at FR37RH.

Refer to Fig. A-GBEAA Sheet 01, Fig. A-GBEAA Sheet 02 and Fig. A-GBEAA

Sheet 03

1 Tube Assy G2627005002000 Item 253

with :

1 Tee NSA855008D10 Item 125

1 Union NSA855006D10 Item 158

8 Connect the fire extinguishing tubes, Item (252), and Item 253, with the union,

Item 158, and on the other end with the T-fitting, Item 125 (Refer to AMM

20-23-11, Page Block 201).

NOTE: Use these swaging tools of the D12000 series :

- Head assembly D12210-56 with power unit D12010-52.

NOTE: The surface protection on the ends of the pipes must be

removed on a length of 43mm (1.692in.).

9 After the installation of the tee-fitting, Item 125, and the union, Item 158,

perform surface protection with :

Low Voc AntiCorrosion Primer16-006F As required

and

Internal

Polyurethane

Varnish

07-017 As required

10 Install the clamp, Item 121, at FR37RH.

Fig. A-GBEAA Sheet 01, Fig. A-GBEAA Sheet 02 and Fig. A-GBEAA Sheet

03

1 Clamp NSA5516A18NJ Item 121

with :

1 Nut NAS1726-3E Item 113

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 360

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@A340-500/600

SERVICE BULLETIN

1 Washer NAS1149C0332R Item 144

1 Spacer NSA5527-03-03 Item 155

1 Screw NAS1801-3-12 Item 157

11 Tighten all connections of the installed fire extinguishing tubes.

(24) Subtask 265020-831-215-001 - Install the U-section.

Work Zones and Access Panels

Zone Access/Work location

132 Work location from Frame 37 to Frame 37.1

Manpower Resources

Manhours 1.00

Minimum number of person 2

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 265020D04R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

106 NAS1149F0332P 2 WASHER

143 NAS1801-3-8 4 SCREW

144 NAS1149C0332R 5 WASHER

145 NAS1801-3-7 3 SCREW

212 G2627008001400 1 SECTION

213 F2627008100000 1 BRACKET

220 E0090-10-135NN 1 LEAD

References

Aircraft Maintenance Manual (AMM) 20-28-00, Page Block 201

Fig. A-GBFAA

Installation of the U-Section and the

Flow Metering System (FMS)

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

(a) Install the U-section between FR37RH and FR37.1.

Refer to Fig. A-GBFAA

1 Between FR37RH and FR37.1RH, install :

Refer to Fig. A-GBFAA Sheet 03, Fig. A-GBFAA Sheet 05 and Fig. A-GBFAA

Sheet 06

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 361

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@A340-500/600

SERVICE BULLETIN

1 U-section G2627008001400 Item 212

1 Bracket F2627008100000 Item 213

1 Lead-Bonding E0090-10-135NN Item 220

with :

2 Washer NAS1149F0332P Item 106

4 Screw NAS1801-3-8 Item 143

5 Washer NAS1149C0332R Item 144

3 Screw NAS1801-3-7 Item 145

NOTE (01): For the installation of the bolt (Refer to AMM 20-28-00, Page

Block 201).

NOTE (02): Seal the bonding connection by overlapping application and

identify the bonding connection by overlapping application with

blue dyed protective coating.

(25) Subtask 265020-831-217-001 - Install the Flow Metering Systems (FMS) for the Fire

Ext. Bottles No. 1 and No. 2 on the U-section.

Work Zones and Access Panels

Zone Access/Work location

132 Work location from Frame 37 to Frame 37.1

Manpower Resources

Manhours 4.00

Minimum number of person 2

Subtask elapsed time 2.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 265020D04R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

104 NAS1726-4E 2 NUT

106 NAS1149F0332P 6 WASHER

113 NAS1726-3E 3 NUT

121 NSA5516A18NJ 2 CLAMP

132 A2627048220400 6 FITTING

133 NSA8202-6 8 ORING

134 A2627048221600 2 FITTING

139 NAS1304-12 2 BOLT

140 NAS1149D0432K 10 WASHER

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 362

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ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

141 NSA5355-5CA 2 WASHER

143 NAS1801-3-8 6 SCREW

144 NAS1149C0332R 6 WASHER

145 NAS1801-3-7 4 SCREW

146 NAS1100E4-34 6 SCREW

147 A2627048920000 2 WASHER

148 NSA5516A06NJ 4 CLAMP

152 E0090-10-320NN 2 LEAD

153 E0090-10-350NN 2 LEAD

159 NAS1801-3-10 2 SCREW

160 MS21103-4 2 CLAMP

219 G2627006001000 1 TUBE

221 G2627006000800 1 TUBE

222 G2627006001800 1 TUBE

223 F2627006003600 1 TUBE

224 A2627048220200 2 RESTRCTR

225 F2627006001400 1 TUBE

226 F2627006000000 1 TUBE

227 F2627007200000 1 HOSE

228 F2627007200200 1 HOSE

229 G2627006002000 1 TUBE

230 G2627006001200 1 TUBE

231 G2627006001400 1 TUBE

232 G2627006001600 1 TUBE

233 NSA855140-22D 1 CROSS

234 G2627005013200 1 TUBE

235 MS21902W10 1 UNION

236 A2627045107800 1 TUBE

237 NSA855113-34D 1 TEE

238 G2627005003400 1 TUBE

239 MS21916W10-4 2 REDUCER

Component COMPD01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

LN9424A100 As required WIRE

Equipment BFEZ04

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

214 QA06753-03 2 FILTER

215 E61751-00-0001 2 REDUCER

216 TP0714033 2 SWITCH

217 HTE400115 2 VALVE

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 363

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@A340-500/600

SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) Task 20-28-00-912-802

Fig. A-GBFAA

Installation of the U-Section and the

Flow Metering System (FMS)

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

(a) Install the Halon Filter, FIN 5010WE, for Fire Ext. Bottle No. 1.

Refer to Fig. A-GBFAA

1 On the U-section, between FR37RH and FR37.1RH, install :

Refer to Fig. A-GBFAA Sheet 01, Fig. A-GBFAA Sheet 03 and Fig. A-GBFAA

Sheet 04

1 Filter-Halon QA06753-03 Item 214

NOTE: See NOTE 03

with :

3 Washer NAS1149D0432K Item 140

3 Screw NAS1100E4-34 Item 146

and

2 O-Ring NSA8202-6 Item 133

1 Fitting A2627048221600 Item 134

NOTE: See NOTE 03

1 Fitting A2627048220400 Item 132

NOTE: See NOTE 03

2 Secure the fittings, Items 132 and 134, with :

As

required

Wire-Lock LN9424A100

3 On the fitting, Item 132, install :

1 Hose Assy F2627007200000 Item 227

NOTE (03): No lubrication on this item.

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 364

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SERVICE BULLETIN

(b) Install the Pressure Reducer, FIN 5014WE, for Fire Ext. Bottle No. 1.

1 On the U-section, between FR37RH and FR37.1RH, install :

Refer to Fig. A-GBFAA Sheet 01, Fig. A-GBFAA Sheet 03 and Fig. A-GBFAA

Sheet 04

1 Reducer-Pressure E61751-00-0001 Item 215

NOTE: See NOTE 03

with :

1 Washer-Tab A2627048920000 Item 147

2 Fitting A2627048220400 Item 132

NOTE: See NOTE 03

2 O-Ring NSA8202-6 Item 133

2 Secure the fittings, Item 132, with :

As

required

Wire-Lock LN9424A100

NOTE (03): No lubrication on this item.

(c) Install the Pressure Switch, FIN 4016WX, for Fire Ext. Bottle No. 1.

1 On the pressure reducer 5014WE, between FR37RH and FR37.1RH, install :

Refer to Fig. A-GBFAA Sheet 01, Fig. A-GBFAA Sheet 03, Fig. A-GBFAA

Sheet 04 and Fig. A-GBFAA Sheet 05

1 Tube Assy G2627006000800 Item 221

with :

1 Washer NAS1149C0332R Item 144

1 Screw NAS1801-3-7 Item 145

1 Clamp NSA5516A06NJ Item 148

and

1 Switch-Pressure TP0714033 Item 216

NOTE: See NOTE 03

2 On the pressure switch, Item 216, install :

1 Tube Assy G2627006001800 Item 222

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 365

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SERVICE BULLETIN

with :

1 Washer NAS1149F0332P Item 106

1 SCREW NAS1801-3-10 Item 159

1 CLAMP MS21103-4 Item 160

NOTE (03): No lubrication on this item.

(d) Install the Check Valve, FIN 5016WE, for Fire Ext. Bottle No. 1.

1 On the pressure reducer 5014WE, between FR37RH and FR37.1RH, install :

Refer to Fig. A-GBFAA Sheet 01, Fig. A-GBFAA Sheet 03 and Fig. A-GBFAA

Sheet 05

1 Tube Assy F2627006003600 Item 223

1 Restrictor A2627048220200 Item 224

1 Tube Assy F2627006001400 Item 225

and

1 Valve-Nonreturn HTE400115 Item 217

NOTE: See NOTE 03

2 On the check valve, Item 217, install :

1 Tube Assy F2627006000000 Item 226

with :

1 Washer NAS1149C0332R Item 144

1 Screw NAS1801-3-7 Item 145

1 Clamp NSA5516A06NJ Item 148

NOTE (03): No lubrication on this item.

(e) Install the Halon Filter, FIN 5011WE, for Fire Ext. Bottle No. 2.

Refer to Fig. A-GBFAA

1 On the U-section, between FR37RH and FR37.1RH, install :

Refer to Fig. A-GBFAA Sheet 01, Fig. A-GBFAA Sheet 03 and Fig. A-GBFAA

Sheet 04

1 Filter-Halon QA06753-03 Item 214

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 366

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SERVICE BULLETIN

NOTE: See NOTE 03

with :

3 Washer NAS1149D0432K Item 140

3 Screw NAS1100E4-34 Item 146

and

2 O-Ring NSA8202-6 Item 133

1 Fitting A2627048221600 Item 134

NOTE: See NOTE 03

1 Fitting A2627048220400 Item 132

NOTE: See NOTE 03

2 Secure the fittings, Items 132 and 134, with :

As

required

Wire-Lock LN9424A100

3 On the fitting, Item 132, install :

1 Hose Assy F2627007200200 Item 228

NOTE: See NOTE 03

NOTE (03): No lubrication on this item.

(f) Install the Pressure Reducer, FIN 5015WE, for Fire Ext. Bottle No. 2.

1 On the U-section, between FR37RH and FR37.1RH, install :

Refer to Fig. A-GBFAA Sheet 01, Fig. A-GBFAA Sheet 03 and Fig. A-GBFAA

Sheet 04

1 Reducer-Pressure E61751-00-0001 Item 215

NOTE: See NOTE 03

with :

1 Washer-Tab A2627048920000 Item 147

2 Fitting A2627048220400 Item 132

NOTE: See NOTE 03

2 O-Ring NSA8202-6 Item 133

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 367

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SERVICE BULLETIN

2 Secure the fittings, Item 132, with :

As

required

Wire-Lock LN9424A100

NOTE (03): No lubrication on this item.

(g) Install the Pressure Switch, FIN 4018WX, for Fire Ext. Bottle No. 2

1 On the pressure reducer 5015WE, between FR37RH and FR37.1RH, install :

Refer to Fig. A-GBFAA Sheet 01, Fig. A-GBFAA Sheet 03 and Fig. A-GBFAA

Sheet 04

1 Tube Assy G2627006001000 Item 219

with :

1 Washer NAS1149C0332R Item 144

1 Screw NAS1801-3-7 Item 145

1 Clamp NSA5516A06NJ Item 148

and

1 Switch-Pressure TP0714033 Item 216

NOTE: See NOTE 03

2 On the pressure switch, Item 216, install :

1 Tube Assy G2627006002000 Item 229

with :

1 Washer NAS1149F0332P Item 106

1 SCREW NAS1801-3-10 Item 159

1 CLAMP MS21103-4 Item 160

NOTE (03): No lubrication on this item.

(h) Install the Check Valve, FIN 5017WE, for Fire Ext. Bottle No. 2

1 On the pressure reducer 5015WE, between FR37RH and FR37.1RH, install :

Refer to Fig. A-GBFAA Sheet 01, Fig. A-GBFAA Sheet 03 and Fig. A-GBFAA

Sheet 05

1 Tube Assy G2627006001200 Item 230

1 Restrictor A2627048220200 Item 224

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 368

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SERVICE BULLETIN

1 Tube Assy G2627006001400 Item 231

and

1 Valve-Nonreturn HTE400115 Item 217

NOTE: See NOTE 03

2 On the check valve, Item 217, install :

1 Tube Assy G2627006001600 Item 232

with :

1 Washer NAS1149C0332R Item 144

1 Screw NAS1801-3-7 Item 145

1 Clamp NSA5516A06NJ Item 148

1 Nut NAS1726-3E Item 113

NOTE (03): No lubrication on this item.

(i) Install the new plumbing and rod ends between FR36RH and FR37.1

1 Between FR36RH and FR37.1, install the rod ends :

Refer to Fig. A-GBFAA Sheet 01 and Fig. A-GBFAA Sheet 02

2 Rod End NSA8141-04R Item (135) Retained at

removal

2 Rod End NSA8140-04RK Item (137) Retained at

removal

with :

2 Nut NAS1726-4E Item 104

2 BOLT NAS1304-12 Item 139

4 Washer NAS1149D0432K Item 140

2 Nut NAS509-5 Item (136) Retained at

removal

2 Washer-Lock NSA5355-5CA Item 141

and

2 Lead-Bonding E0090-10-320NN Item 152

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 369

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SERVICE BULLETIN

2 Lead-Bonding E0090-10-350NN Item 153

with :

4 Washer NAS1149F0332P Item 106

4 Screw NAS1801-3-8 Item 143

NOTE: Do the electrical bonding (Refer to AMM Task

20-28-00-912-802)

2 Between FR36RH and FR37.1, install the plumbing :

Refer to Fig. A-GBFAA Sheet 01, Fig. A-GBFAA Sheet 02 and Fig. A-GBFAA

Sheet 03

2 Hose A2627045200400 Item (209) Retained at

removal

2 Hose Assy F2627007100200 Item (210) Retained at

removal

1 Cross NSA855140-22D Item 233

1 Tube Assy G2627005013200 Item 234

1 Union MS21902W10 Item 235

with :

2 Screw NAS1801-3-8 Item 143

2 Washer NAS1149C0332R Item 144

2 Nut NAS1726-3E Item 113

2 Clamp NSA5516A18NJ Item 121

and

1 Tube Assy A2627045107800 Item 236

1 Tee NSA855113-34D Item 237

1 Tube Assy G2627005003400 Item 238

2 Reducer MS21916W10-4 Item 239

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 370

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SERVICE BULLETIN

(26) Subtask 265020-831-211-002 - Install the Fire Extinguishing Bottles 4005WX and

4010WX.

Work Zones and Access Panels

Zone Access/Work location

132 Access Panel 132PM

Work location from Frame 35 to Frame 37.1

Manpower Resources

Manhours 2.00

Minimum number of person 2

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 265020D04R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

100 NAS1726-5E 8 NUT

101 NAS1305-2 8 BOLT

103 NAS1304-9 2 BOLT

104 NAS1726-4E 2 NUT

105 NAS563-11 4 BOLT

106 NAS1149F0332P 4 WASHER

Component COMPD01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

LN9424A100 As required WIRE

References

Aircraft Maintenance Manual (AMM) 20-28-00, Page Block 201

26-23-41, Page Block 401

Fig. A-GBJAA

Installation of Fire Extinguishing Bottles

FIN 4005WX and FIN 4010WX with

Cartridges.

Sheet 01

Sheet 02

Sheet 03

Refer to Fig. A-GBJAA

(a) Install the fire extinguishing bottle 1 (FWD) 4005WX.

1 Between FR36RH and FR37RH, install the fire extinguishing bottle 4005WX

(Refer to AMM 26-23-41, Page Block 401) :

Refer to Fig. A-GBJAA Sheet 01 and Fig. A-GBJAA Sheet 02 :

1 Extinguisher-Fire 472931-3 Item (204) Retained at

removal

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with :

4 Nut NAS1726-5E Item 100

4 Bolt NAS1305-2 Item 101

1 Bolt NAS1304-9 Item 103

1 Nut NAS1726-4E Item 104

2 Bolt NAS563-11 Item 105

NOTE: See NOTE 01, 02, 03.

2 Washer NAS1149F0332P Item 106

2 Secure the coupling nuts of the fire extinguishing discharge heads and the

bolts, Item 105, with :

As

required

Wire-Lock LN9424A100

NOTE (01): Torque tighten the bolt to between 0.30da.Nm (26.552lbf.in)

and 0.35da.Nm (30.977lbf.in).

NOTE (02): For the installation of the bolt refer to the electrical bonding of

components with conductive screws and bolts and bonding

straps according toAMM 20-28-00, Page Block 201.

NOTE (03): Seal the bonding connection by overlapping application and

identify the bonding connection by overlapping application with

blue dyed protective coating.

(b) Install the fire extinguishing bottle 2 (AFT) 4010WX.

1 Between FR37RH and FR37.1RH, install the fire extinguishing bottle 4010WX

(Refer to AMM 26-23-41, Page Block 401) :

Refer to Fig. A-GBJAA Sheet 01 and Fig. A-GBJAA Sheet 03 :

1 Extinguisher-Fire 472625-3 Item (203)

with :

4 Nut NAS1726-5E Item 100

4 Bolt NAS1305-2 Item 101

1 Bolt NAS1304-9 Item 103

1 Nut NAS1726-4E Item 104

2 Bolt NAS563-11 Item 105

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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NOTE: See NOTE 01, 02, 03.

2 Washer NAS1149F0332P Item 106

2 Secure the coupling nuts of the fire extinguishing discharge heads and the

bolts, Item 105, with :

As

required

Wire-Lock LN9424A100

NOTE (01): Torque tighten the bolt to between 0.30da.Nm (26.552lbf.in)

and 0.35da.Nm (30.977lbf.in).

NOTE (02): For the installation of the bolt refer to the electrical bonding of

components with conductive screws and bolts and bonding

straps according toAMM 20-28-00, Page Block 201.

NOTE (03): Seal the bonding connection by overlapping application and

identify the bonding connection by overlapping application with

blue dyed protective coating.

(27) Subtask 265020-831-214-001 - Install the new identification placards.

Work Zones and Access Panels

Zone Access/Work location

132 Work location from Frame 37 to Frame 37.1

Manpower Resources

Manhours 1.50

Minimum number of person 2

Subtask elapsed time 0.75

Skills NON SPECIFIC

Material necessary to do the job

Kit 265020D04R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

240 F2627004120800 1 PLACARD

241 F2627004121400 1 PLACARD

242 F2627004121200 1 PLACARD

243 F2627004120400 1 PLACARD

244 F2627004120600 1 PLACARD

245 F2627004121600 1 PLACARD

246 F2627004121800 1 PLACARD

247 F2627004121000 1 PLACARD

248 G2627004020200 1 PLACARD

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Abrasion Resistant Coating

(Teflon Polyuret)

07-003 As required

General Purpose Adhesive

Honeycomb Filler

08-554 As required

References

Fig. A-GBFAA

Installation of the U-Section and the

Flow Metering System (FMS)

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

(a) Install the identification placards 4010WX, 4016WX, 4018WX, 5010WE, 5011WE,

5014WE, 5015WE, 5016WE, 5017WE, between FR37 and FR37.1.

Refer to Fig. A-GBFAA

1 Between FR37RH and FR37.1RH, install :

Refer to Fig. A-GBFAA Sheet 01, Fig. A-GBFAA Sheet 03 and Fig. A-GBFAA

Sheet 06

1 Placard F2627004120800 Item 240

1 Placard F2627004121400 Item 241

1 Placard F2627004121200 Item 242

1 Placard F2627004120400 Item 243

1 Placard F2627004120600 Item 244

1 Placard F2627004121600 Item 245

1 Placard F2627004121800 Item 246

1 Placard F2627004121000 Item 247

1 Placard G2627004020200 Item 248

Bond the placard, Item 248, with :

General Purpose

Adhesive

Honeycomb Filler

08-554 As required

Protect the placard, Item 248, with :

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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SERVICE BULLETIN

Abrasion Resistant

Coating (Teflon

Polyuret)

07-003 As required

**CONF 006

(1) Subtask 265020-831-001-007 - Modify the Equipment and the Wiring in the RH

Overhead Panel 212VU.

Work Zones and Access Panels

Zone Access/Work location

212 Work location Electrical panel 212VU

Manpower Resources

Manhours 12.00

Minimum number of person 1

Subtask elapsed time 12.00

Skills ELECTRICAL

Material necessary to do the job

Kit 265020A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

2 ASNA2083BG2-10 7 Screw

6 NSA937901MA2206 1 Module

7 NSA937901FM 1 Module

10 F9251088400000 1 Plate

F1131101500000 Placard

F9000095226495 Bundle

NAS1102-04-5 44 Screw

NSA935401-03 50 TIE

NSA937901E2 1 Label

Kit 265020A07R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 F33110444A00 1 Plate

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Pure Mineral Vaseline Or

Petro-Latum

04-012 As required

Electrical Bond Varnish 07-001B As required

Sealant, High Temperature 08-007C As required

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) Task 11-00-00-400-802

Task 20-28-00-912-802

Fig. A-FBBAA

Modification of the Equipment in the RH

Overhead Panel 212VU

Sheet 01

Sheet 02

Sheet 03

Fig. A-FCAAA

Modification of the Wiring in the RH

Overhead Panel 212VU

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

(a) Remove and disconnect the RH overhead panel 212VU.

NOTE: Retain it.

(b) Modify the equipment in the RH overhead panel 212VU.

1 Remove the integrally lighted plate (212LF).

a Remove as shown in Fig. A-FBBAA Sheet 01 :

FIN 212LF

1 Plate-Integrally Lighted F33110305A00 Item (1) Discard

attached with :

7 Screw ASNA2083BG2-10 Item (2) Discard

2 Remove the indicator light BTL3 (5WX).

a Remove as shown in Fig. A-FBBAA Sheet 01 and Fig. A-FBBAA Sheet

02, Detail B :

FIN 5WX

1 Light-Indicator ABS0951A0LP110 Item (3) Discard

FIN 5WX1

1 Sleeve E0416-02 Item (4) Discard

FIN 5WXA

1 Connector E0417A01S Item (5) Discard

NOTE: Remove and discard the attachment hardware.

3 Replace the 212VU front plate.

a Remove and retain all the items of equipment that are installed on the

front plate.

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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b Remove as shown in Fig. A-FBBAA Sheet 01 :

1 Plate Assy- Front

212VU

F9251602100000 Item (10) Discard

attached with :

8 Screw NAS1102-06-5 Item (11) Retain

c On the new front plate, bond the placards (Refer to AMM Task

11-00-00-400-802) supplied in :

Placard Set-212VU F1131101500000

NOTE: Bond the applicable placards at the same locations as on

the old front plate. Discard the unused placards.

d Install as shown in Fig. A-FBBAA Sheet 03 :

1 Plate Assy- Front

212VU

F9251088400000 Item 10

attach with :

8 Screw NAS1102-06-5 Item (11)

NOTE: The screws Item (11) were retained at the removal.

e Install again all the items of equipment that you removed and retained

before the replacement of the front plate and attach with :

44 Screw NAS1102-04-5

Safety the screws with :

Sealant, High

Temperature

08-007C As required

NOTE: Replace the screws if they are damaged during the

removal. The quantity of screws to be replaced depends

on aircraft configuration (44 is the maximum).

f Do the electrical bonding (Refer to AMM Task 20-28-00-912-802) with :

Pure Mineral

Vaseline Or PetroLatum

04-012 As required

and

Electrical Bond

Varnish

07-001B As required

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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4 Modify the terminal block (582VT) as shown in Fig. A-FBBAA Sheet 01 and

Fig. A-FBBAA Sheet 02, Detail C.

a Remove from position 2 :

FIN 582VT2

1 Module-False NSA937901FM Item (6) Discard

b Remove from position 3 :

FIN 582VT3

1 Module NSA937901MA2204 Item (7) Discard

c Install at position 2 as shown in :

FIN 582VT2

1 Module NSA937901MA2206 Item 6

with

1 Label-Identification NSA937901E2

d Install at position 3 as shown in :

FIN 582VT3

1 Module-False NSA937901FM Item 7

5 Install the new integrally lighted plate (212LF).

a Install as shown in Fig. A-FBBAA Sheet 03 :

FIN 212LF

1 Plate-Integrally Lighted F33110444A00 Item 1

attach with :

7 Screw ASNA2083BG2-10 Item 2

(c) Modify the wiring in the RH overhead panel 212VU.

1 Remove the wires as shown in the wiring diagrams Fig. A-FCAAA Sheet 01,

Fig. A-FCAAA Sheet 02 and as given in the hook-up chart lines :

- 1 thru 13 (Refer to Fig. A-FCAAA Sheet 04).

2 Modify the connections of the wires as shown in the wiring diagrams Fig. AFCAAA Sheet 02, Fig. A-FCAAA Sheet 03 and as given in the hook-up chart

lines :

- 17 thru 24 (Refer to Fig. A-FCAAA Sheet 04)

- 1 and 2 (Refer to Fig. A-FCAAA Sheet 05).

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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3 Install the wires as shown in the wiring diagram Fig. A-FCAAA Sheet 03 and

as given in the hook-up chart lines :

- 6 thru 12 (Refer to Fig. A-FCAAA Sheet 05), supplied in :

Bundle F9000095226495

4 Attach the wires with :

50 Tie-Cable NSA935401-03

(d) Install the RH overhead panel 212VU.

(2) Subtask 265020-831-002-001 - Modify the Equipment and the Wiring in the

Emergency Power Center 740VU.

Work Zones and Access Panels

Zone Access/Work location

121 Access Door 821, Door 132AZ

Work location Electrical panel 740VU

Manpower Resources

Manhours 3.50

Minimum number of person 1

Subtask elapsed time 3.50

Skills ELECTRICAL

Material necessary to do the job

Kit 265020A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

F9000095226495 Bundle

NSA935401-03 50 TIE

NSA935401-05 50 TIE

References

Fig. A-FBCAA

Modification of the Equipment in the

Emergency Power Center 740VU

Sheet 01

Fig. A-FCBAA

Modification of the Wiring in the

Emergency Power Center 740VU

Sheet 01

Sheet 02

(a) Open the emergency power center 740VU.

(b) Remove the wires as shown in the wiring diagram Fig. A-FCBAA Sheet 01 and as

given in the hook-up chart lines :

- 1 thru 8 (Refer to Fig. A-FCBAA Sheet 02).

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 379

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(c) Modify the terminal block (703VT) as shown in Fig. A-FBCAA Sheet 01.

1 Remove from position 21 :

1 Clamp-End NSA937901S Retain

2 Remove from position 20 :

FIN 703VT20

1 Module NSA937901MA2004 Item (7) Discard

3 Install at position 20 :

1 Clamp-End NSA937901S

NOTE: The end clamp was retained at the removal.

(d) Install the wire as shown in the wiring diagram Fig. A-FCBAA Sheet 01 and as

given in the hook-up chart line :

- 12 (Refer to Fig. A-FCBAA Sheet 02), supplied in :

Bundle F9000095226495

(e) Attach the wire with :

50 Tie-Cable NSA935401-03

50 Tie-Cable NSA935401-05

(f) Close the emergency power center 740VU.

(3) Subtask 265020-831-003-001 - Modify the Equipment and the Wiring in the AC/DC

Main Power Center 710VU.

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 821, Door 132AZ

Work location Electrical panel 710VU

Manpower Resources

Manhours 3.50

Minimum number of person 1

Subtask elapsed time 3.50

Skills ELECTRICAL

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 380

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Material necessary to do the job

Kit 265020A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

F9000095226495 Bundle

NSA935401-03 50 TIE

NSA935401-05 50 TIE

References

Fig. A-FBDAA

Modification of the Equipment in the

AC/DC Main Power Center 710VU

Sheet 01

Fig. A-FCCAA

Modification of the Wiring in the AC/DC

Main Power Center 710VU

Sheet 01

Sheet 02

(a) Open the AC/DC main power center 710VU.

(b) Remove the wires as shown in the wiring diagram Fig. A-FCCAA Sheet 01 and as

given in the hook-up chart lines :

- 1 thru 8 (Refer to Fig. A-FCCAA Sheet 02).

(c) Modify the terminal block (1712VT) as shown in Fig. A-FBDAA Sheet 01.

1 Remove from position 18 :

1 Clamp-End NSA937901S Retain

2 Remove from position 17 :

FIN 1712VT17

1 Module NSA937901MA2004 Item (7) Discard

3 Install at position 17 :

1 Clamp-End NSA937901S

NOTE: The end clamp was retained at the removal.

(d) Install the wire as shown in the wiring diagram Fig. A-FCCAA Sheet 01 and as

given in the hook-up chart line :

- 12 (Refer to Fig. A-FCCAA Sheet 02), supplied in :

Bundle F9000095226495

(e) Attach the wire with :

50 Tie-Cable NSA935401-03

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 381

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50 Tie-Cable NSA935401-05

(f) CLose the AC/DC main power center 710VU.

(4) Subtask 265020-831-004-001 - Modify the Equipment and the Wiring in the LH

Relay Box 751VU.

Work Zones and Access Panels

Zone Access/Work location

121 Access Door 821, Door 132AZ

Work location Electrical panel 751VU

Manpower Resources

Manhours 3.50

Minimum number of person 1

Subtask elapsed time 3.50

Skills ELECTRICAL

References

Fig. A-FBEAA

Modification of the Equipment in the LH

Relay Box 751VU

Sheet 01

Fig. A-FCDAA

Modification of the Wiring in the LH

Relay Box 751VU

Sheet 01

Sheet 02

(a) Open the LH relay box 751VU.

(b) Remove the wires as shown in the wiring diagram Fig. A-FCDAA Sheet 01 and as

given in the hook-up chart lines :

- 1 thru 12 (Refer to Fig. A-FCDAA Sheet 02).

(c) Remove from position E93, as shown in Fig. A-FBEAA Sheet 01 :

FIN 10WX

1 Relay E0245-28A0 Item (8) Discard

FIN 10WXA

1 Base E0250A0S Item (9) Discard

NOTE: Remove and discard the attachment hardware and the related

placard(s).

(d) Remove from position E89, as shown in Fig. A-FBEAA Sheet 01 :

FIN 11WX

1 Relay E0245-28A0 Item (8) Discard

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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FIN 11WXA

1 Base E0250A0S Item (9) Discard

NOTE: Remove and discard the attachment hardware and the related

placard(s).

(e) Close the LH relay box 751VU.

(5) Subtask 265020-831-005-001 - Modify the Equipment and the Wiring in the RH

Relay Box 752VU.

Work Zones and Access Panels

Zone Access/Work location

122 Access Door 821, Door 132AZ

Work location Electrical panel 752VU

Manpower Resources

Manhours 3.50

Minimum number of person 1

Subtask elapsed time 3.50

Skills ELECTRICAL

References

Fig. A-FBFAA

Modification of the Equipment in the RH

Relay Box 752VU

Sheet 01

Fig. A-FCEAA

Modification of the Wiring in the RH

Relay Box 752VU

Sheet 01

Sheet 02

(a) Open the RH relay box 752VU.

(b) Remove the wires as shown in the wiring diagram Fig. A-FCEAA Sheet 01 and as

given in the hook-up chart lines :

- 1 thru 12 (Refer to Fig. A-FCEAA Sheet 02).

(c) Remove from position B37, as shown in Fig. A-FBFAA Sheet 01 :

FIN 12WX

1 Relay E0245-28A0 Item (8) Discard

FIN 12WXA

1 Base E0250A0S Item (9) Discard

NOTE: Remove and discard the attachment hardware and the related

placard(s).

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 383

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SERVICE BULLETIN

(d) Remove from position B33, as shown in Fig. A-FBFAA Sheet 01 :

FIN 13WX

1 Relay E0245-28A0 Item (8) Discard

FIN 13WXA

1 Base E0250A0S Item (9) Discard

NOTE: Remove and discard the attachment hardware and the related

placard(s).

(e) Close the RH relay box 752VU.

(6) Subtask 265020-831-006-001 - Modify the Equipment and the Wiring in the Main

Rack 800VU.

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 821, Door 132AZ

Work location Electrical panel 800VU

Manpower Resources

Manhours 8.00

Minimum number of person 2

Subtask elapsed time 4.00

Skills ELECTRICAL

Material necessary to do the job

Kit 265020A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

7 NSA937901FM 1 Module

F9000095226495 Bundle

NSA935401-03 200 TIE

NSA935401-05 200 TIE

NSA935401-08 200 Tie

References

Aircraft Maintenance Manual (AMM) Task 26-16-34-000-801

Task 26-16-34-400-801

Fig. A-FBGAA

Modification of the Equipment in the

Main Rack 800VU

Sheet 01

Fig. A-FCFAA

Modification of the Wiring in the Main

Rack 800VU

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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SERVICE BULLETIN

References

Fig. A-FCGAA

Modification of the Pin Programming in

the Main Rack 800VU

Sheet 01

Sheet 02

(a) Remove and retain the SDCU (20WH) (Refer to AMM Task 26-16-34-000-801).

(b) Remove the wires as shown in the wiring diagrams Fig. A-FCFAA Sheet 01, Fig. AFCFAA Sheet 02, Fig. A-FCFAA Sheet 03, and as given in the hook-up chart lines :

- 1 thru 25 (Refer to Fig. A-FCFAA Sheet 05)

- 1 thru 3 (Refer to Fig. A-FCFAA Sheet 06).

(c) Modify the terminal block (2900VT) as shown in Fig. A-FBGAA Sheet 01.

1 Remove from position 50 :

FIN 2900VT50

1 Module NSA937901MA2011 Item (7) Discard

2 Install at position 50 :

FIN 2900VT50

1 Module-False NSA937901FM Item 7

(d) Install the wires as shown in the wiring diagram Fig. A-FCFAA Sheet 04 and as

given in the hook-up chart lines :

- 7 thru 18 (Refer to Fig. A-FCFAA Sheet 06), supplied in :

Bundle F9000095226495

(e) Modify the connection of the wires as shown in the wiring diagram Fig. A-FCGAA

Sheet 01 and as given in the hook-up chart lines :

- 1 thru 4 (Refer to Fig. A-FCGAA Sheet 02).

(f) Attach the wires with :

200 Tie-Cable NSA935401-03

200 Tie-Cable NSA935401-05

200 Tie-Cable NSA935401-08

(g) Install the SDCU (20WH) (Refer to AMM Task 26-16-34-400-801).

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 385

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SERVICE BULLETIN

(7) Subtask 265020-831-007-001 - Modify the Wiring between the Main Rack Shelf

801VU and the LH Relay Box 751VU.

Work Zones and Access Panels

Zone Access/Work location

121 Access Door 821, Door 132AZ

Work location from Electrical panel 801VU to Electrical panel

751VU

Manpower Resources

Manhours 3.50

Minimum number of person 1

Subtask elapsed time 3.50

Skills ELECTRICAL

Material necessary to do the job

Kit 265020A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

NSA936604CA0931 8 Cap

References

Fig. A-FBAAA

Location of the Working Areas

Sheet 01

Fig. A-FCHAA

Modification of the Wiring between the

Main Rack Shelf 801VU and the LH

Relay Box 751VU

Sheet 01

Sheet 02

(a) Modify the connections of the wires as shown in the wiring diagram Fig. A-FCHAA

Sheet 01 and as given in the hook-up chart lines :

- 1 thru 8 (Refer to Fig. A-FCHAA Sheet 02).

(b) Install on the stowed wires ends :

8 Cap-Sealing NSA936604CA0931

(8) Subtask 265020-831-008-001 - Modify the Wiring between the Main Rack Shelf

802VU and the RH Relay Box 752VU.

Work Zones and Access Panels

Zone Access/Work location

122 Access Door 821, Door 132AZ

Work location from Electrical panel 802VU to Electrical panel

752VU

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 386

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SERVICE BULLETIN

Manpower Resources

Manhours 3.50

Minimum number of person 1

Subtask elapsed time 3.50

Skills ELECTRICAL

References

Fig. A-FBAAA

Location of the Working Areas

Sheet 01

Fig. A-FCJAA

Modification of the Wiring between the

Main Rack Shelf 802VU and the RH

Relay Box 752VU

Sheet 01

Sheet 02

(a) Remove the wires as shown in the wiring diagram Fig. A-FCJAA Sheet 01 and as

given in the hook-up chart lines :

- 1 thru 4 (Refer to Fig. A-FCJAA Sheet 02).

(9) Subtask 265020-831-009-001 - Modify the Wiring between the Emergency Power

Center 740VU and the LH Relay Box 751VU.

Work Zones and Access Panels

Zone Access/Work location

121 Access Door 821, Door 132AZ

Work location from Electrical panel 740VU to Electrical panel

751VU

Manpower Resources

Manhours 3.50

Minimum number of person 1

Subtask elapsed time 3.50

Skills ELECTRICAL

References

Fig. A-FBAAA

Location of the Working Areas

Sheet 01

Fig. A-FCKAA

Modification of the Wiring between the

Emergency Power Center 740VU and

the LH Relay Box 751VU

Sheet 01

Sheet 02

(a) Remove the wires as shown in the wiring diagram Fig. A-FCKAA Sheet 01 and as

given in the hook-up chart lines :

- 1 thru 4 (Refer to Fig. A-FCKAA Sheet 02).

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 387

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SERVICE BULLETIN

(10) Subtask 265020-831-010-001 - Modify the Wiring between the AC/DC Main Power

Center 715VU and the RH Relay Box 752VU.

Work Zones and Access Panels

Zone Access/Work location

122 Access Door 821, Door 132AZ

Work location from Electrical panel 715VU to Electrical panel

752VU

Manpower Resources

Manhours 3.50

Minimum number of person 1

Subtask elapsed time 3.50

Skills ELECTRICAL

References

Fig. A-FBAAA

Location of the Working Areas

Sheet 01

Fig. A-FCLAA

Modification of the Wiring between the

AC/DC Main Power Center 715VU and

the RH Relay Box 752VU

Sheet 01

Sheet 02

(a) Remove the wires as shown in the wiring diagram Fig. A-FCLAA Sheet 01 and as

given in the hook-up chart lines :

- 1 thru 4 (Refer to Fig. A-FCLAA Sheet 02).

(11) Subtask 265020-831-011-001 - Modify the Wiring between the Main Rack Shelf

801VU and the Avionics Compartment at FR2.

Work Zones and Access Panels

Zone Access/Work location

From 121 Access Door 821, Door 132AZ

Work location Electrical panel 801VU

To 211 Access Door 831, Door 841

Panel 211EW

Work location Frame 2

Manpower Resources

Manhours 3.50

Minimum number of person 1

Subtask elapsed time 3.50

Skills ELECTRICAL

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 388

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@A340-500/600

SERVICE BULLETIN

Material necessary to do the job

Kit 265020A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

NSA936604CA0931 2 Cap

References

Fig. A-FBAAA

Location of the Working Areas

Sheet 01

Fig. A-FCMAA

Modification of the Wiring between the

Main Rack Shelf 801VU and the

Avionics Compartment at FR2

Sheet 01

Sheet 02

(a) Modify the connections of the wire as shown in the wiring diagram Fig. A-FCMAA

Sheet 01 and as given in the hook-up chart lines :

- 1 and 2 (Refer to Fig. A-FCMAA Sheet 02).

(b) Install on the stowed wire ends :

2 Cap-Sealing NSA936604CA0931

(12) Subtask 265020-831-012-001 - Modify the Wiring between the RH Overhead Panel

212VU and the Avionics Compartment (LH Side).

Work Zones and Access Panels

Zone Access/Work location

From 212 Access Door 831, Door 841

Work location Electrical panel 212VU

To 121 Access Door 821, Door 132AZ

Work location Electrical panel 751VU

Electrical panel 740VU

Frame 2

Electrical panel 801VU

Manpower Resources

Manhours 10.00

Minimum number of person 2

Subtask elapsed time 5.00

Skills ELECTRICAL

Material necessary to do the job

Kit 265020A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

F9000095226495 Bundle

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 389

6

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@A340-500/600

SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

NSA935401-05 200 TIE

NSA935401-08 200 Tie

NSA936604CA0931 8 Cap

References

Fig. A-FBAAA

Location of the Working Areas

Sheet 01

Fig. A-FCNAA

Modification of the Wiring between the

RH Overhead Panel 212VU and the

Avionics Compartment (LH Side)

Sheet 01

Sheet 02

Sheet 03

(a) Modify the connections of the wires as shown in the wiring diagrams Fig. A-FCNAA

Sheet 01, Fig. A-FCNAA Sheet 02 and as given in the hook-up chart lines :

- 1 thru 8 (Refer to Fig. A-FCNAA Sheet 03).

(b) Install on the stowed wires ends :

8 Cap-Sealing NSA936604CA0931

(c) Install the wires as shown in the wiring diagram Fig. A-FCNAA Sheet 01 and as

given in the hook-up chart lines :

- 12 and 13 (Refer to Fig. A-FCNAA Sheet 02), supplied in :

Bundle F9000095226495

(d) Attach the wires with :

200 Tie-Cable NSA935401-05

200 Tie-Cable NSA935401-08

(13) Subtask 265020-831-013-001 - Modify the Wiring between the RH Overhead Panel

212VU and the Avionics Compartment (RH Side).

Work Zones and Access Panels

Zone Access/Work location

From 212 Access Door 831, Door 841

Work location Electrical panel 212VU

To 122 Access Door 821, Door 132AZ

Panel 131BA

Work location Electrical panel 752VU

Electrical panel 715VU

Electrical panel 802VU

Frame 20

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 390

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@A340-500/600

SERVICE BULLETIN

Manpower Resources

Manhours 10.00

Minimum number of person 2

Subtask elapsed time 5.00

Skills ELECTRICAL

Material necessary to do the job

Kit 265020A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

F9000095226495 Bundle

NSA935401-05 200 TIE

NSA935401-08 200 Tie

NSA936604CA0931 10 Cap

References

Fig. A-FBAAA

Location of the Working Areas

Sheet 01

Fig. A-FCPAA

Modification of the Wiring between the

RH Overhead Panel 212VU and the

Avionics Compartment (RH Side)

Sheet 01

Sheet 02

Sheet 03

(a) Modify the connections of the wires as shown in the wiring diagram Fig. A-FCPAA

Sheet 01, Fig. A-FCPAA Sheet 02 and as given in the hook-up chart lines :

- 1 thru 12 (Refer to Fig. A-FCPAA Sheet 03).

(b) Install on the stowed wires ends :

10 Cap-Sealing NSA936604CA0931

(c) Install the wires as shown in the wiring diagram Fig. A-FCPAA Sheet 01 and as

given in the hook-up chart lines :

- 9 and 10 (Refer to Fig. A-FCPAA Sheet 02), supplied in :

Bundle F9000095226495

(d) Attach the wires with :

200 Tie-Cable NSA935401-05

200 Tie-Cable NSA935401-08

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 391

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

(14) Subtask 265020-831-201-001 - Remove the Fire Extinguishing Bottles, 4010WX,

4005WX and 4020WX.

Work Zones and Access Panels

Zone Access/Work location

132 Access Panel 132PM

Work location from Frame 35 to Frame 37.1

Manpower Resources

Manhours 3.00

Minimum number of person 2

Subtask elapsed time 1.50

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 26-23-41, Page Block 401

Fig. A-GBAAA

Removal of Fire Extinguishing Bottles

4005WX, 4010WX and 4020WX with

Cartridges.

Sheet 01

Sheet 02

Sheet 03

(a) Remove the Fire Extinguishing Bottle 2 (FWD), 4010WX.

Refer to Fig. A-GBAAA

1 Between FR35RH and FR36RH, remove the fire extinguishing bottle 4010WX

(Refer to AMM 26-23-41, Page Block 401) :

Refer to Fig. A-GBAAA Sheet 01, Fig. A-GBAAA Sheet 02 and Fig. A-GBAAA

Sheet 03, Detail D :

1 Extinguisher-Fire 35200003-2 Item (200) Retain

with :

4 Nut NAS1726-5E Item (100) Discard

4 Bolt NAS1305-2 Item (101) Discard

1 Bolt NAS1304-9 Item (103) Discard

1 Nut NAS1726-4E Item (104) Discard

2 Screw Item (260)

2 Washer Item (261)

2 Nut Item (262)

NOTE: Retain the Items (260), (261) and (262).

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 392

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SERVICE BULLETIN

(b) Remove the Fire Extinguishing Bottle 1 (MID), 4005WX.

Refer to Fig. A-GBAAA

1 Between FR36RH and FR37RH, remove the fire extinguishing bottle 4005WX

(Refer to AMM 26-23-41, Page Block 401) :

Refer to Fig. A-GBAAA Sheet 01 and Fig. A-GBAAA Sheet 03 :

1 Extinguisher-Fire 34900008-2 Item (201) Retain

with :

4 Nut NAS1726-5E Item (100) Discard

4 Bolt NAS1305-2 Item (101) Discard

1 Bolt NAS1304-9 Item (103) Discard

1 Nut NAS1726-4E Item (104) Discard

2 Screw Item (260)

2 Washer Item (261)

2 Nut Item (262)

NOTE: Discard the Items (260), (261) and (262).

(c) Remove the Fire Extinguishing Bottle 3 (AFT), 4020WX.

Refer to Fig. A-GBAAA

1 Between FR37RH and FR37.1RH, remove the fire extinguishing bottle

4020WX (Refer to AMM 26-23-41, Page Block 401) :

Refer to Fig. A-GBAAA Sheet 01, Fig. A-GBAAA Sheet 02 and Fig. A-GBAAA

Sheet 03, Detail D :

1 Extinguisher-Fire 35200003-2 Item (200) Discard

with :

4 Nut NAS1726-5E Item (100) Discard

4 Bolt NAS1305-2 Item (101) Discard

1 Bolt NAS1304-9 Item (103) Discard

1 Nut NAS1726-4E Item (104) Discard

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 393

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

2 Screw Item (260)

2 Washer Item (261)

2 Nut Item (262)

NOTE: Retain the Items (260), (261) and (262).

(15) Subtask 265020-831-202-001 - Remove the 4 Flow Metering Compact Units (FMCU),

FIN 4031WX, 4032WX, 4033WX and 4034WX.

Work Zones and Access Panels

Zone Access/Work location

132 Access Panel 132PM

Work location from Frame 35 to Frame 37.1

Manpower Resources

Manhours 4.00

Minimum number of person 2

Subtask elapsed time 2.00

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 26-23-43, Page Block 401

Fig. A-GBCAA

Removal of the 4 Flow Metering

Compact Units (FMCU), FIN 4031WX,

4032WX, 4033WX and 4034WX, the

related Plumbing Installations and

Placards

Sheet 01

Sheet 02

Sheet 03

(a) Remove the Flow Metering Compact Unit (FMCU), FIN 4031WX.

Refer to Fig. A-GBCAA

1 From FR35RH, remove the FMCU, FIN 4031WX (Refer to AMM 26-23-43,

Page Block 401) :

Refer to Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet 02 and Fig. A-GBCAA

Sheet 03

1 Meter-Flow, Compact

Unit

QA07907-01 Item (205) Discard

and

1 Hose Assy G2627007000000 Item (107) Discard

1 Tube Assy G2627006000000 Item (109) Discard

with :

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 394

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

1 Washer NAS1149F0332P Item (106) Discard

1 Clamp NSA5516-06NJ Item (111) Discard

1 Screw NAS1096-3-10 Item (112) Discard

1 Nut NAS1726-3E Item (113) Discard

3 Screw NAS1100E4-36 Item (130) Discard

3 Washer NAS1149C0432R Item (131) Discard

1 Fitting A2627048220400 Item (132) Discard

2 O-Ring NSA8202-6 Item (133) Discard

1 Fitting A2627048221600 Item (134) Discard

(b) Remove the Flow Metering Compact Unit (FMCU), FIN 4032WX.

Refer to Fig. A-GBCAA

1 From FR36RH, remove the FMCU, FIN 4032WX (Refer to AMM 26-23-43,

Page Block 401) :

Refer to Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet 02 and Fig. A-GBCAA

Sheet 03

1 Meter-Flow, Compact

Unit

QA07907-01 Item (205) Discard

and

1 Hose Assy G2627007000200 Item (108) Discard

1 Tube Assy G2627006000200 Item (110) Discard

with :

1 Washer NAS1149F0332P Item (106) Discard

1 Clamp NSA5516-06NJ Item (111) Discard

1 Screw NAS1096-3-10 Item (112) Discard

1 Nut NAS1726-3E Item (113) Discard

3 Screw NAS1100E4-36 Item (130) Discard

3 Washer NAS1149C0432R Item (131) Discard

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 395

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

1 Fitting A2627048220400 Item (132) Discard

2 O-Ring NSA8202-6 Item (133) Discard

1 Fitting A2627048221600 Item (134) Discard

(c) Remove the Flow Metering Compact Unit (FMCU), FIN 4033WX.

Refer to Fig. A-GBCAA

1 From FR37RH, remove the FMCU, FIN 4033WX (Refer to AMM 26-23-43,

Page Block 401) :

Refer to Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet 02 and Fig. A-GBCAA

Sheet 03

1 Meter-Flow, Compact

Unit

QA07907-01 Item (205) Discard

and

1 Hose Assy G2627007000000 Item (107) Discard

1 Tube Assy G2627006000000 Item (109) Discard

with :

1 Washer NAS1149F0332P Item (106) Discard

1 Clamp NSA5516-06NJ Item (111) Discard

1 Screw NAS1096-3-10 Item (112) Discard

1 Nut NAS1726-3E Item (113) Discard

3 Screw NAS1100E4-36 Item (130) Discard

3 Washer NAS1149C0432R Item (131) Discard

1 Fitting A2627048220400 Item (132) Discard

2 O-Ring NSA8202-6 Item (133) Discard

1 Fitting A2627048221600 Item (134) Discard

(d) Remove the Flow Metering Compact Unit (FMCU), FIN 4034WX.

Refer to Fig. A-GBCAA

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 396

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Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

1 From FR37.1RH, remove the FMCU, FIN 4034WX (Refer to AMM 26-23-43,

Page Block 401) :

Refer to Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet 02 and Fig. A-GBCAA

Sheet 03

1 Meter-Flow, Compact

Unit

QA07907-01 Item (205) Discard

and

1 Hose Assy G2627007000200 Item (108) Discard

1 Tube Assy G2627006000200 Item (110) Discard

with :

1 Washer NAS1149F0332P Item (106) Discard

1 Clamp NSA5516-06NJ Item (111) Discard

1 Screw NAS1096-3-10 Item (112) Discard

1 Nut NAS1726-3E Item (113) Discard

3 Screw NAS1100E4-36 Item (130) Discard

3 Washer NAS1149C0432R Item (131) Discard

1 Fitting A2627048220400 Item (132) Discard

2 O-Ring NSA8202-6 Item (133) Discard

1 Fitting A2627048221600 Item (134) Discard

(16) Subtask 265020-831-203-001 - Remove the plumbing installations and placards.

Work Zones and Access Panels

Zone Access/Work location

132 Access Panel 132PM

Work location from Frame 35 to Frame 37.1

Manpower Resources

Manhours 2.50

Minimum number of person 2

Subtask elapsed time 1.25

Skills NON SPECIFIC

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 397

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@A340-500/600

SERVICE BULLETIN

References

Fig. A-GBCAA

Removal of the 4 Flow Metering

Compact Units (FMCU), FIN 4031WX,

4032WX, 4033WX and 4034WX, the

related Plumbing Installations and

Placards

Sheet 01

Sheet 02

Sheet 03

(a) Remove the plumbing installations between FR35RH thru FR37.1RH.

Refer to Fig. A-GBCAA

1 Between FR35RH and FR36RH, remove :

Refer to Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet 02 and Fig. A-GBCAA

Sheet 03

2 Reducer MS21916D10-4 Item (115) Discard

1 Tube Assy G2627005004400 Item (116) Discard

1 Tee NSA855113-34D Item (117) Discard

1 Tube Assy G2627005004200 Item (118) Discard

1 Hose A2627045200400 Item (209) Discard

with :

2 Washer NAS1149F0332P Item (106) Discard

2 Screw NAS1096-3-10 Item (112) Discard

2 Nut NAS1726-3E Item (113) Discard

2 Clamp NSA5516-18NJ Item (121) Discard

1 Rod End NSA8141-04R Item (135) Discard

1 Nut NAS509-5 Item (136) Discard

1 Rod End NSA8140-04RK Item (137) Discard

2 Lead-Bonding E0090-41-320 Item (138) Discard

1 Bolt NAS1304-12 Item (139) Discard

1 Nut NAS1726-4E Item (104) Discard

1 Washer NAS1149D0432K Item (140) Discard

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 398

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

1 Washer-Lock NSA5355-5CA Item (141) Discard

2 Between FR36RH and FR37RH, remove :

Refer to Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet 02 and Fig. A-GBCAA

Sheet 03

2 Washer NAS1149F0332P Item (106) Discard

2 Screw NAS1096-3-10 Item (112) Discard

2 Nut NAS1726-3E Item (113) Discard

1 Tube Assy G2627005004000 Item (120) Discard

2 Clamp NSA5516-18NJ Item (121) Discard

1 Cross NSA855140-22D Item (122) Discard

1 Union MS21902D10 Item (123) Discard

1 Tube Assy G2627005003800 Item (124) Discard

2 Tee NSA855008D10 Item (125) Discard

1 Rod End NSA8141-04R Item (135) Retain

1 Nut NAS509-5 Item (136) Retain

1 Rod End NSA8140-04RK Item (137) Retain

2 Lead-Bonding E0090-41-320 Item (138) Discard

1 Bolt NAS1304-12 Item (139) Discard

1 Nut NAS1726-4E Item (104) Discard

1 Washer NAS1149D0432K Item (140) Discard

1 Washer-Lock NSA5355-5CA Item (141) Discard

1 Tube Assy G2627005006400 Item (142) Discard

1 Hose A2627045200400 Item (209) Retain

2 Hose Assy F2627007100200 Item (210) Retain

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 399

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@A340-500/600

SERVICE BULLETIN

3 Between FR37RH and FR37.1RH, remove :

Refer to Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet 02 and Fig. A-GBCAA

Sheet 03

2 Reducer MS21916D10-4 Item (115) Discard

1 Tube Assy G2627005004400 Item (116) Discard

1 Tee NSA855113-34D Item (117) Discard

1 Tube Assy G2627005003400 Item (119) Discard

1 Tee NSA855008D10 Item (125) Discard

1 Tube Assy G2627005003600 Item (129) Discard

1 Rod End NSA8141-04R Item (135) Retain

1 Nut NAS509-5 Item (136) Retain

1 Rod End NSA8140-04RK Item (137) Retain

2 Lead-Bonding E0090-41-320 Item (138) Discard

1 Bolt NAS1304-12 Item (139) Discard

1 Nut NAS1726-4E Item (104) Discard

1 Washer NAS1149D0432K Item (140) Discard

1 Washer-Lock NSA5355-5CA Item (141) Discard

1 Hose A2627045200400 Item (209) Retain

(b) Remove the placards between FR35RH thru FR37.1RH.

Refer to Fig. A-GBCAA

1 Between FR35RH and FR36RH, remove the placards 4010WX, 4031WX and

4032WX :

2 Label NSA931025-02F Item (126) Discard

1 Placard G2627004020200 Item (127) Discard

2 Between FR37RH and FR37.1RH, remove the placards 4020WX, 4033WX

and 4034WX :

2 Label NSA931025-02F Item (126) Discard

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 400

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Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

1 Placard G2627004020400 Item (128) Discard

(17) Subtask 265020-831-204-001 - Remove the brackets and the insulation blankets

between FR35RH thru FR37.1RH.

Work Zones and Access Panels

Zone Access/Work location

132 Work location from Frame 35 to Frame 37.1

Manpower Resources

Manhours 3.50

Minimum number of person 2

Subtask elapsed time 1.75

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 25-80-00-000-801

Fig. A-GBDAA

Removal of the Brackets

Sheet 01

Sheet 02

Sheet 03

(a) Remove the insulation blankets in the affected area (Refer to AMM Task

25-80-00-000-801).

(b) Remove the brackets between FR35RH thru FR37.1RH.

Refer to Fig. A-GBDAA

1 Between FR35 and FR36, STGR 29RH, remove :

Refer to Fig. A-GBDAA Sheet 01 and Fig. A-GBDAA Sheet 03

1 Section-T F5397460021800 Item (161) Discard

1 Bracket Assy F5397484500200 Item (162) Discard

2 From FR35RH, STGR31, remove :

Refer to Fig. A-GBDAA Sheet 01 and Fig. A-GBDAA Sheet 03

1 Bracket F5397463611000 Item (163) Discard

3 From FR36RH, STGR31, remove :

Refer to Fig. A-GBDAA Sheet 01 and Fig. A-GBDAA Sheet 03

1 Bracket F5397463610800 Item (164) Discard

4 From FR37RH, STGR31, remove :

Refer to Fig. A-GBDAA Sheet 01 and Fig. A-GBDAA Sheet 03

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 401

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@A340-500/600

SERVICE BULLETIN

1 Bracket F5397463611000 Item (163) Discard

5 From FR37.1RH, STGR31, remove :

Refer to Fig. A-GBDAA Sheet 01 and Fig. A-GBDAA Sheet 03

1 Bracket F5397463610800 Item (164) Discard

6 From the crossbeam at FR35 at -Y2462, remove :

Refer to Fig. A-GBDAA Sheet 01 and Fig. A-GBDAA Sheet 02

1 Bracket Assy F5397800200000 Item (165) Discard

1 Bracket F5397461823000 Item (166) Discard

7 From the crossbeam at FR36 at -Y2462, remove :

Refer to Fig. A-GBDAA Sheet 01 and Fig. A-GBDAA Sheet 02

1 Bracket Assy F5397800200000 Item (165) Discard

1 Bracket F5397469928000 Item (167) Discard

8 Between FR35RH and FR36RH, remove :

Refer to Fig. A-GBDAA Sheet 01 and Fig. A-GBDAA Sheet 02

1 Strut Assy F5397883300000 Item (168) Discard

(18) Subtask 265020-831-213-001 - Install the brackets, modify the insulation blankets

and close the rivet holes between FR35RH thru FR37.1RH.

Work Zones and Access Panels

Zone Access/Work location

132 Work location from Frame 35 to Frame 37.1

Manpower Resources

Manhours 7.00

Minimum number of person 2

Subtask elapsed time 3.50

Skills NON SPECIFIC

Material necessary to do the job

Kit 265020D02R04

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

170 EN6081D4-09 28 RIVET

171 EN6081D6-14 30 RIVET

252 F5397757020200 2 ANGLE

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 402

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@A340-500/600

SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

253 F5397462009600 1 BRACKET

254 F5397462009800 1 BRACKET

281 ABS1577A05 1 BRACKET

282 ABS0787B05B 1 BRACKET

References

Aircraft Maintenance Manual (AMM) Task 20-28-00-912-802

Task 25-80-00-200-801

Task 25-80-00-400-801

Fig. A-GBGAA

Installation of the Brackets

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Fig. A-GBDAA

Removal of the Brackets

Sheet 01

Sheet 02

Sheet 03

(a) Install the brackets and close the existing rivet holes.

Refer to Fig. A-GBDAA and Fig. A-GBGAA

1 Between FR35 and FR36, on STGR29RH and STGR30RH, close the rivet

holes in the stringers with :

Refer to Fig. A-GBDAA Sheet 01, Fig. A-GBDAA Sheet 02 and Fig. A-GBDAA

Sheet 03

4 Rivet EN6081D6-14 Item 171

2 On FR35 and FR36, STGR31RH, close the rivet holes in the frames with :

Refer to Fig. A-GBDAA Sheet 01, Fig. A-GBDAA Sheet 02 and Fig. A-GBDAA

Sheet 03

8 Rivet EN6081D6-14 Item 171

3 Between FR36 and FR37, on STGR30RH, install this bracket on the stringer :

Refer to Fig. A-GBGAA Sheet 01 and Fig. A-GBGAA Sheet 02

1 Angle-Bonding F5397757020200 Item 252

with :

3 Rivet EN6081D4-09 Item 170

NOTE: Do the electrical bonding (Refer to AMM Task

20-28-00-912-802)

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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SERVICE BULLETIN

4 On FR37 and FR37.1, STGR31RH, close the rivet holes in the frames with :

Refer to Fig. A-GBDAA Sheet 01,Fig. A-GBDAA Sheet 02 and Fig. A-GBDAA

Sheet 03

8 Rivet EN6081D6-14 Item 171

5 On FR37, between STGR31RH and STGR32RH, install this bracket :

Refer to Fig. A-GBGAA Sheet 01 and Fig. A-GBGAA Sheet 02

1 Bracket Assy F5397462009600 Item 253

with :

4 Rivet EN6081D6-14 Item 171

NOTE: Do the electrical bonding (Refer to AMM Task

20-28-00-912-802)

NOTE: Existing rivet spacing must be used.

6 Between FR37 and FR37.1, on STGR30RH, install this bracket :

Refer to Fig. A-GBGAA Sheet 01 and Fig. A-GBGAA Sheet 02

1 Angle-Bonding F5397757020200 Item 252

with :

3 Rivet EN6081D4-09 Item 170

7 Between FR37 and FR37.1, on STGR30RH, install this bracket :

Refer to Fig. A-GBGAA Sheet 01 and Fig. A-GBGAA Sheet 03

1 Bracket ABS1577A05 Item 281

with :

3 Rivet EN6081D4-09 Item 170

NOTE: Do the electrical bonding (Refer to AMM Task

20-28-00-912-802)

8 On FR37.1, between STGR31RH and STGR32RH, install this bracket :

Refer to Fig. A-GBGAA Sheet 01 and Fig. A-GBGAA Sheet 02

1 Bracket Assy F5397462009800 Item 254

with :

4 Rivet EN6081D6-14 Item 171

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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SERVICE BULLETIN

NOTE: Do the electrical bonding (Refer to AMM Task

20-28-00-912-802)

NOTE: Existing rivet spacing must be used.

9 On the crossbeam at FR35, between -Y1959 and -Y2462, close the rivet holes

in the crossbeam with :

Refer to Fig. A-GBDAA Sheet 01, Fig. A-GBDAA Sheet 02 and Fig. A-GBDAA

Sheet 03

10 Rivet EN6081D4-09 Item 170

10 On the crossbeam at FR36, outboard of -Y2462, close the rivet holes in the

crossbeam with :

Refer to Fig. A-GBDAA Sheet 01, Fig. A-GBDAA Sheet 02 and Fig. A-GBDAA

Sheet 03

9 Rivet EN6081D4-09 Item 170

11 On the crossbeam at FR36, outboard of -Y2462, install this bracket :

Refer to Fig. A-GBGAA Sheet 01 and Fig. A-GBGAA Sheet 03

1 Bracket-Z ABS0787B05B Item 282

with :

2 Rivet EN6081D6-14 Item 171

NOTE: Do the electrical bonding (Refer to AMM Task

20-28-00-912-802)

(b) Between FR36 thru FR37.1RH modify the insulation blankets in the affected area.

1 Adapt the insulation blankets for the new locations of brackets (Refer to AMM

Task 25-80-00-200-801).

(c) Install the modified insulation in the affected area (Refer to AMM Task

25-80-00-400-801).

(19) Subtask 265020-831-216-001 - Modify the equipment and the wiring of the

FMCU/FMS outlet pressure switches 4031WX, 4032WX, 4033WX, 4034WX, 4016WX

and 4018WX of the fire extinguishing bottles Nos. 2 and 3.

Work Zones and Access Panels

Zone Access/Work location

132 Work location from Frame 35 to Frame 37.1

200 Work location Electrical panel 801VU

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 405

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SERVICE BULLETIN

Manpower Resources

Manhours 1.50

Minimum number of person 2

Subtask elapsed time 0.75

Skills ELECTRICAL

Material necessary to do the job

Kit 265020D03R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

173 G9237018016600 1 PLCRDSET

174 NSA935401-04 8 TIE

175 NSA935401-05 15 TIE

References

Process and Material Specification

(PMS)

Process and Material Specification (PMS)

01-07-10

Fig. A-GWAAA

Modification of the Wiring of the

FMCU/FMS Outlet Pressure Switches

4031WX, 4032WX, 4033WX, 4034WX,

4016WX and 4018WX

Sheet 01

Sheet 02

Fig. A-GHAAA

Hook-up Chart

Sheet 01

Fig. A-GBLAA

Stowage of the Electrical Wires of the

Connectors 4031WX-A, 4032WX-A

4011WX-A, 4012WX-A and 4013WX-A

Sheet 01

Sheet 02

Sheet 03

Sheet 04

(a) Modify the wiring of the FMCU/FMS outlet pressure switches.

1 Disconnect these electrical wires from the connectors 4031WX-A and

4032WX-A.

Refer to Fig. A-GWAAA Sheet 01 (Wiring)

Refer to Fig. A-GHAAA Sheet 01 (Hook-up Chart), LINES 1, 2, 3 and 4

2 Remove the connectors 4031WX-A and 4032WX-A and discard.

Refer to Fig. A-GBLAA Sheet 01

Remove :

2 Connector-Plug EN2997KE60803BN Item (265) Discard

and remove the following attachment parts :

4 Screw NAS1801-08-7 Item (267) Discard

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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SERVICE BULLETIN

2 Nut MS21042-08 Item (268) Discard

4 Washer NAS1149CN816R Item (269) Discard

2 Clamp MS21919WCH8 Item (270) Retain

2 Screw NAS1801-08-23 Item (271) Discard

2 Lanyard DAN80-3-150 Item (273) Discard

2 Sleeve-Protective NSA935809-09 Item (274) Discard

5 Cable Mount Item (277) Retain

3 Disconnect these electrical wires from the connectors 4033WX-A and

4034WX-A.

Refer to Fig. A-GWAAA Sheet 01 (Wiring)

Refer to Fig. A-GHAAA Sheet 01 (Hook-up Chart), LINES 5, 6, 7 and 8

4 Reroute and install the electrical wires :

Refer to Fig. A-GWAAA Sheet 02 (Wiring)

Refer to Fig. A-GHAAA Sheet 01 (Hook-up Chart), LINES 13, 14, 15 and 16

with :

15 Tie-Cable NSA935401-05 Item 175

and attach the placards, identified 4016WX-A, 4018WX-A and the SB/MOD

placards :

1 Placardset G9237018016600 Item 173

with :

8 Tie-Cable NSA935401-04 Item 174

(20) Subtask 265020-831-209-001 - Modify the equipment and the wiring of the fire

extinguishing bottle No. 3 (AFT), 4020WX, and relocated fire extinguishing bottle

No. 2 (AFT), 4010WX.

Work Zones and Access Panels

Zone Access/Work location

132 Work location from Frame 35 to Frame 37.1

200 Work location Electrical panel 801VU

Electrical panel 802VU

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 407

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SERVICE BULLETIN

Manpower Resources

Manhours 1.00

Minimum number of person 2

Subtask elapsed time 1.00

Skills ELECTRICAL

Material necessary to do the job

Kit 265020D03R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

173 G9237018016600 1 PLCRDSET

174 NSA935401-04 12 TIE

175 NSA935401-05 15 TIE

176 EN3155-003F1614 2 CONTACT

References

Fig. A-GWBAA

Modification of the Wiring of the Fire

Extinguishing Bottle No. 3 (previously

AFT), 4020WX, and relocated Fire

Extinguishing Bottle No. 2 (now AFT),

4010WX

Sheet 01

Sheet 02

Fig. A-GHBAA

Hook-up Chart

Sheet 01

(a) Modify the wiring of the cartridges and the pressure switch of the fire extinguishing

bottle (AFT), 4020WX (4010WX)

1 Disconnect these electrical wires from the connector 2625VC-A.

Refer to Fig. A-GWBAA Sheet 01 (Wiring)

Refer to Fig. A-GHBAA Sheet 01 (Hook-up Chart), LINES 1 and 11, END 2

2 Reroute and install the electrical wires on the connector 2511VC-A.

Refer to Fig. A-GWBAA Sheet 02 (Wiring)

Refer to Fig. A-GHBAA Sheet 01 (Hook-up Chart), LINES 2 and 12, END 2

3 Disconnect these electrical wires from the connector 2636VC-A.

Refer to Fig. A-GWBAA Sheet 01 (Wiring)

Refer to Fig. A-GHBAA Sheet 01 (Hook-up Chart), LINES 5 and 15, END 2

NOTE: Cut off the contacts directly behind the contacts.

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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4 Reroute and install the electrical wires on the connector 2508VC-A.

Refer to Fig. A-GWBAA Sheet 02 (Wiring)

Refer to Fig. A-GHBAA Sheet 01 (Hook-up Chart), LINES 6 and 16, END 2

with :

2 Contact-Socket EN3155-003F1614 Item 176

5 Disconnect the electrical wire from the connector 2044VC-A.

Refer to Fig. A-GWBAA Sheet 01 (Wiring)

Refer to Fig. A-GHBAA Sheet 01 (Hook-up Chart), LINE 23, END 2

6 Reroute and install the electrical wire on the connector 2016VC-A.

Refer to Fig. A-GWBAA Sheet 02 (Wiring)

Refer to Fig. A-GHBAA Sheet 01 (Hook-up Chart), LINE 24, END 2

7 Attach the placards, identified 4011WX-A, 4012WX-A, 4013WX-A and the

SB/MOD placards :

1 Placardset G9237018016600 Item 173

with :

12 Tie-Cable NSA935401-04 Item 174

8 Install the tie-cables on the wire harnesses :

15 Tie-Cable NSA935401-05 Item 175

NOTE: For the stowage position of the connectors 4011WX-A,

4012WX-A, 4013WX-A, 4031WX-A and 4032WX-A, refer to

(22) Subtask 265020-831-218-001.

(21) Subtask 265020-831-210-001 - Modify the Equipment and the Wiring of the

previous Fire Extinguishing Bottle No. 2 (FWD), 4010WX.

Work Zones and Access Panels

Zone Access/Work location

132 Work location from Frame 35 to Frame 36

200 Work location Electrical panel 801VU

Electrical panel 802VU

Manpower Resources

Manhours 1.50

Minimum number of person 1

Subtask elapsed time 1.50

Skills ELECTRICAL

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 409

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SERVICE BULLETIN

References

Fig. A-GWCAA

Modification of the Wiring of the Fire

Extinguishing Bottle No. 2 (FWD),

4010WX

Sheet 01

Sheet 02

Fig. A-GHCAA

Hook-up Chart

Sheet 01

Fig. A-GBLAA

Stowage of the Electrical Wires of the

Connectors 4031WX-A, 4032WX-A

4011WX-A, 4012WX-A and 4013WX-A

Sheet 01

Sheet 02

Sheet 03

Sheet 04

(a) Modify the wiring of the previous fire extinguishing bottle No. 2 (FWD), 4010WX.

1 Disconnect these electrical wires from the connectors 4011WX-A, 4012WX-A

and 4013WX-A.

Refer to Fig. A-GWCAA Sheet 01 (Wiring)

Refer to Fig. A-GHCAA Sheet 01 (Hook-up Chart), LINES 1, 5, 11, 15 and 23

Refer to Fig. A-GHCAA Sheet 01 (Hook-up Chart), LINES 3, 7, 9, 13, 17, 19,

21, END 1

2 Remove the connectors 4011WX-A, 4012WX-A and 4013WX-A and discard.

Refer to Fig. A-GBLAA Sheet 01

Remove :

2 Connector EN2997KE61005BN Item (264) Discard

1 Connector-Plug EN2997KE60803BN Item (265) Discard

and remove the following attachment parts :

1 Tie-Cable NSA935401-03 Item (266) Discard

5 Screw NAS1801-08-7 Item (267) Discard

2 Nut MS21042-08 Item (268) Discard

4 Washer NAS1149CN816R Item (269) Discard

2 Clamp MS21919WCH8 Item (270) Discard

1 Screw NAS1801-08-29 Item (272) Discard

2 Lanyard DAN80-3-150 Item (273) Discard

2 Sleeve-Protective NSA935809-09 Item (274) Discard

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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SERVICE BULLETIN

2 Cable Mount Item (277) Retain

NOTE: For the stowage position of the connectors 4011WX-A,

4012WX-A, 4013WX-A, 4031WX-A and 4032WX-A, refer to

(22) Subtask 265020-831-218-001.

(22) Subtask 265020-831-218-001 - Put the electrical wires of the connectors 4031WX-A,

4032WX-A 4011WX-A, 4012WX-A and 4013WX-A in a stowage position.

Work Zones and Access Panels

Zone Access/Work location

132 Work location from Frame 35 to Frame 37.1

Manpower Resources

Manhours 2.50

Minimum number of person 1

Subtask elapsed time 2.50

Skills ELECTRICAL

Material necessary to do the job

Kit 265020D03R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

173 G9237018016600 1 PLCRDSET

177 NSA936603CC0100 23 CAP

Kit 265020D05R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

266 NSA935401-03 25 TIE

269 NAS1149CN816R 4 WASHER

270 MS21919WCH8 4 CLAMP

271 NAS1801-08-23 2 SCREW

272 NAS1801-08-29 1 SCREW

274 NSA935809-09 4 SLEEVE

275 NAS1801-08-25 1 SCREW

References

Fig. A-GBLAA

Stowage of the Electrical Wires of the

Connectors 4031WX-A, 4032WX-A

4011WX-A, 4012WX-A and 4013WX-A

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Fig. A-GHAAA

Hook-up Chart

Sheet 01

Fig. A-GHCAA

Hook-up Chart

Sheet 01

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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SERVICE BULLETIN

References

Fig. A-GWAAA

Modification of the Wiring of the

FMCU/FMS Outlet Pressure Switches

4031WX, 4032WX, 4033WX, 4034WX,

4016WX and 4018WX

Sheet 01

Sheet 02

Fig. A-GWCAA

Modification of the Wiring of the Fire

Extinguishing Bottle No. 2 (FWD),

4010WX

Sheet 01

Sheet 02

(a) Put the electrical wires of the connectors 4031WX-A and 4032WX-A in a stowage

position.

1 Put the electrical wires in a stowage position.

Refer to Fig. A-GBLAA Sheet 01, Fig. A-GBLAA Sheet 02, Fig. A-GBLAA

Sheet 03 and Fig. A-GBLAA Sheet 04

Refer to Fig. A-GWAAA Sheet 02 (Wiring)

Refer toFig. A-GHAAA Sheet 01 (Hook-up Chart), LINES 9, 10, 11 and 12

with :

6 Cap NSA936603CC0100 Item 177

NOTE: Do not cut off the contacts.

Attach the electrical wires in a stowage position.

with :

2 Washer NAS1149CN816R Item 269

2 Clamp MS21919WCH8 Item 270

2 Clamp MS21919WCH8 Item (270) Retained at

removal

1 Screw NAS1801-08-23 Item 271

2 Sleeve-Protective NSA935809-09 Item 274

1 Screw NAS1801-08-25 Item 275

5 Cable Mount Item (277) Retained at

removal

20 Tie-Cable NSA935401-03 Item 266

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 412

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SERVICE BULLETIN

(b) Put the electrical wires of the connectors 4011WX-A, 4012WX-A and 4013WX-A in

a stowage position.

1 Put the electrical wires in a stowage position.

Refer to Fig. A-GBLAA Sheet 01, Fig. A-GBLAA Sheet 02, Fig. A-GBLAA

Sheet 03 and Fig. A-GBLAA Sheet 04

Refer to Fig. A-GWCAA Sheet 02 (Wiring)

Refer to Fig. A-GHCAA Sheet 01 (Hook-up Chart), LINES 2, 6, 12, 16 and 24

Refer to Fig. A-GHCAA Sheet 01 (Hook-up Chart), LINES 4, 8, 10, 14, 18, 20

and 22, END 1

with :

17 Cap NSA936603CC0100 Item 177

NOTE: Do not cut off the contacts.

Attach the electrical wires in a stowage position.

with :

2 Washer NAS1149CN816R Item 269

2 Clamp MS21919WCH8 Item 270

1 Screw NAS1801-08-23 Item 271

1 Screw NAS1801-08-29 Item 272

2 Sleeve-Protective NSA935809-09 Item 274

2 Cable Mount Item (277) Retained at

removal

and attach the SB/MOD placards :

1 Placardset G9237018016600 Item 173

with :

5 Tie-Cable NSA935401-03 Item 266

(23) Subtask 265020-831-205-001 - Adapt the plumbing installation.

Work Zones and Access Panels

Zone Access/Work location

132 Work location from Frame 36 to Frame 37

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 413

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@A340-500/600

SERVICE BULLETIN

Manpower Resources

Manhours 3.00

Minimum number of person 2

Subtask elapsed time 1.50

Skills NON SPECIFIC

Material necessary to do the job

Kit 265020D01R03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

113 NAS1726-3E 2 NUT

121 NSA5516A18NJ 2 CLAMP

125 NSA855008D10 1 TEE

144 NAS1149C0332R 2 WASHER

155 NSA5527-03-03 2 SPACER

157 NAS1801-3-12 2 SCREW

158 NSA855006D10 2 UNION

251 G2627005013000 1 TUBE

253 G2627005002000 1 TUBE

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Internal Polyurethane

Varnish

07-017 As required

Solvent General Purpose 11-026 As required

Low Voc Anti-Corrosion

Primer

16-006F As required

Lint-Free Cotton Cloth 19-003 As required

Standard tool TOOLD01

ITEM TOOL N ̊ TOOL NAME QTY SEE

NOTES

D12102C07-02 PERMASWAGE Repair

Kit D12000 Series

1

References

Aircraft Maintenance Manual (AMM) 20-23-11, Page Block 201

Fig. A-GBEAA

Adaption of the Plumbing Installation

Sheet 01

Sheet 02

Sheet 03

Sheet 04

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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SERVICE BULLETIN

References

Fig. A-GBFAA

Installation of the U-Section and the

Flow Metering System (FMS)

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

(a) Remove the fire extinguishing tubes from FR36 and FR37.

Refer to Fig. A-GBEAA

1 Remove and discard these items from FR36RH :

Refer to Fig. A-GBEAA Sheet 01, Fig. A-GBEAA Sheet 02 and Fig. A-GBEAA

Sheet 04

1 Nut NAS1726-3E Item (113) Discard

1 Clamp NSA5516-18NJ Item (121) Discard

1 Washer NAS1149C0332R Item (144) Discard

1 Spacer NSA5527-03-03 Item (155) Discard

1 Screw NAS1096-3-14 Item (157) Discard

2 Cut the fire extinguishing tube, Item (250), at the position shown in Fig. AGBEAA Sheet 02 (Refer to AMM 20-23-11, Page Block 201).

3 Remove the fire extinguishing tube, Item (250), partly between the cut and the

outboard X-connection fitting :

1 Tube Assy, partly G2627005013000 Item (250) Discard

4 Deburr the remaining tube, Item (250), (Refer to AMM 20-23-11, Page Block

201).

5 Clean the remaining tube, Item (250), with :

Solvent General

Purpose

11-026 As required

and

Lint-Free Cotton

Cloth

19-003 As required

6 Remove and discard these items from FR37RH :

Refer to Fig. A-GBEAA Sheet 01, Fig. A-GBEAA Sheet 02 and Fig. A-GBEAA

Sheet 04

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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SERVICE BULLETIN

1 Nut NAS1726-3E Item (113) Discard

1 Clamp NSA5516-18NJ Item (121) Discard

1 Washer NAS1149C0332R Item (144) Discard

1 Spacer NSA5527-03-03 Item (155) Discard

1 Screw NAS1096-3-14 Item (157) Discard

7 Cut the fire extinguishing tube, Item (252), at the position shown in Fig. AGBEAA Sheet 02 (Refer to AMM 20-23-11, Page Block 201).

8 Remove the fire extinguishing tube, Item (252), partly between the cut and the

outboard T-connection fitting :

1 Tube Assy, partly G2627005002000 Item (252) Discard

1 Tee NSA855008D10 Item (125) Discard

9 Deburr the remaining tube, Item (252), (Refer to AMM 20-23-11, Page Block

201).

10 Clean the remaining tube, Item (252), with :

Solvent General

Purpose

11-026 As required

and

Lint-Free Cotton

Cloth

19-003 As required

(b) Install the fire extinguishing tubes on FR36 and FR37.

CAUTION: BEFORE YOU CONNECT THE FIRE EXTINGUISHING TUBES

WITH THE PERMASWAGE TOOL, MAKE SURE THAT THE FIRE

EXTINGUISHING TUBES ARE INSTALLED STRESS-FREE IN

THEIR CLAMPS.

CAUTION: DO NOT BEND THE TUBE WHEN YOU INSTALL IT. IF THE

TUBE IS BENT, IT CAN BECOME DAMAGED.

CAUTION: IF YOU USE DUST CAPS FOR THE CONTAMINATION

PROTECTION OF OPEN LINES, ALWAYS BE SURE TO

INSTALL THE CAPS AROUND THE TUBE ENDS AND NOT IN

THE TUBE ENDS. THERE CAN BE BLOCKAGE OF THE FLOW

THROUGH THE TUBES IF THESE TUBES ARE INSTALLED

ACCIDENTALLY WITH DUST CAPS IN THE TUBE ENDS.

NOTE: The fire extinguishing tubes must be installed with their related

clamps.

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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SERVICE BULLETIN

Refer to Fig. A-GBEAA

1 Install temporarily, Item 233, before install the other tubes.

Refer to Fig. A-GBFAA Sheet 01

2 Install the tube, Item 251, at FR36RH.

Refer to Fig. A-GBEAA Sheet 01, Fig. A-GBEAA Sheet 02 and Fig. A-GBEAA

Sheet 03

1 Tube Assy G2627005013000 Item 251

with :

1 Union NSA855006D10 Item 158

3 Connect the fire extinguishing tubes, Item (250), and Item 251, with the union,

Item 158, (Refer to AMM 20-23-11, Page Block 201).

D12102C07-02 PERMASWAGE

Repair Kit D12000

Series

1

NOTE: Use these swaging tools of the D12000 series :

- Head assembly D12210-56 with power unit D12010-52.

NOTE: The surface protection on both ends of the pipes must be

removed on a length of 43mm (1.692in.).

4 After the installation of the union, Item 158, perform surface protection with :

Low Voc AntiCorrosion Primer16-006F As required

and

Internal

Polyurethane

Varnish

07-017 As required

5 Install the clamp, Item 121, at FR36RH.

Fig. A-GBEAA Sheet 01, Fig. A-GBEAA Sheet 02 and Fig. A-GBEAA Sheet

03

1 Clamp NSA5516A18NJ Item 121

with :

1 Nut NAS1726-3E Item 113

1 Washer NAS1149C0332R Item 144

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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SERVICE BULLETIN

1 Spacer NSA5527-03-03 Item 155

1 Screw NAS1801-3-12 Item 157

6 Install temporarily, Item 234 and 238, before install the other tubes.

Refer to Fig. A-GBFAA Sheet 01

7 Install the tube, Item 253 at FR37RH.

Refer to Fig. A-GBEAA Sheet 01, Fig. A-GBEAA Sheet 02 and Fig. A-GBEAA

Sheet 03

1 Tube Assy G2627005002000 Item 253

with :

1 Tee NSA855008D10 Item 125

1 Union NSA855006D10 Item 158

8 Connect the fire extinguishing tubes, Item (252), and Item 253, with the union,

Item 158, and on the other end with the T-fitting, Item 125 (Refer to AMM

20-23-11, Page Block 201).

NOTE: Use these swaging tools of the D12000 series :

- Head assembly D12210-56 with power unit D12010-52.

NOTE: The surface protection on the ends of the pipes must be

removed on a length of 43mm (1.692in.).

9 After the installation of the tee-fitting, Item 125, and the union, Item 158,

perform surface protection with :

Low Voc AntiCorrosion Primer16-006F As required

and

Internal

Polyurethane

Varnish

07-017 As required

10 Install the clamp, Item 121, at FR37RH.

Fig. A-GBEAA Sheet 01, Fig. A-GBEAA Sheet 02 and Fig. A-GBEAA Sheet

03

1 Clamp NSA5516A18NJ Item 121

with :

1 Nut NAS1726-3E Item 113

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 418

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SERVICE BULLETIN

1 Washer NAS1149C0332R Item 144

1 Spacer NSA5527-03-03 Item 155

1 Screw NAS1801-3-12 Item 157

11 Tighten all connections of the installed fire extinguishing tubes.

(24) Subtask 265020-831-206-001 - Install the U-section.

Work Zones and Access Panels

Zone Access/Work location

132 Work location from Frame 37 to Frame 37.1

Manpower Resources

Manhours 1.00

Minimum number of person 2

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 265020D01R03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

106 NAS1149F0332P 2 WASHER

143 NAS1801-3-8 4 SCREW

144 NAS1149C0332R 5 WASHER

145 NAS1801-3-7 3 SCREW

212 G2627008001400 1 SECTION

213 F2627008100000 1 BRACKET

220 E0090-10-135NN 1 LEAD

References

Aircraft Maintenance Manual (AMM) 20-28-00, Page Block 201

Fig. A-GBFAA

Installation of the U-Section and the

Flow Metering System (FMS)

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

(a) Install the U-section between FR37RH and FR37.1.

Refer to Fig. A-GBFAA

1 Between FR37RH and FR37.1RH, install :

Refer to Fig. A-GBFAA Sheet 03, Fig. A-GBFAA Sheet 05 and Fig. A-GBFAA

Sheet 06

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 419

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SERVICE BULLETIN

1 U-section G2627008001400 Item 212

1 Bracket F2627008100000 Item 213

1 Lead-Bonding E0090-10-135NN Item 220

with :

2 Washer NAS1149F0332P Item 106

4 Screw NAS1801-3-8 Item 143

5 Washer NAS1149C0332R Item 144

3 Screw NAS1801-3-7 Item 145

NOTE: For the installation of the bolt (Refer to AMM 20-28-00, Page

Block 201).

NOTE: Seal the bonding connection by overlapping application and

identify the bonding connection by overlapping application with

blue dyed protective coating.

(25) Subtask 265020-831-207-001 - Install the Flow Metering Systems (FMS) for the Fire

Ext. Bottles No. 1 and No. 2 on the U-section.

Work Zones and Access Panels

Zone Access/Work location

132 Work location from Frame 37 to Frame 37.1

Manpower Resources

Manhours 4.00

Minimum number of person 2

Subtask elapsed time 2.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 265020D01R03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

104 NAS1726-4E 2 NUT

106 NAS1149F0332P 6 WASHER

113 NAS1726-3E 3 NUT

121 NSA5516A18NJ 2 CLAMP

132 A2627048220400 6 FITTING

133 NSA8202-6 8 ORING

134 A2627048221600 2 FITTING

139 NAS1304-12 2 BOLT

140 NAS1149D0432K 10 WASHER

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

141 NSA5355-5CA 2 WASHER

143 NAS1801-3-8 6 SCREW

144 NAS1149C0332R 6 WASHER

145 NAS1801-3-7 4 SCREW

146 NAS1100E4-34 6 SCREW

147 A2627048920000 2 WASHER

148 NSA5516A06NJ 4 CLAMP

152 E0090-10-320NN 2 LEAD

153 E0090-10-350NN 2 LEAD

159 NAS1801-3-10 2 SCREW

160 MS21103-4 2 CLAMP

219 G2627006001000 1 TUBE

221 G2627006000800 1 TUBE

222 G2627006001800 1 TUBE

223 F2627006003600 1 TUBE

224 A2627048220200 2 RESTRCTR

225 F2627006001400 1 TUBE

226 F2627006000000 1 TUBE

227 F2627007200000 1 HOSE

228 F2627007200200 1 HOSE

229 G2627006002000 1 TUBE

230 G2627006001200 1 TUBE

231 G2627006001400 1 TUBE

232 G2627006001600 1 TUBE

233 NSA855140-22D 1 CROSS

234 G2627005013200 1 TUBE

235 MS21902W10 1 UNION

236 A2627045107800 1 TUBE

237 NSA855113-34D 1 TEE

238 G2627005003400 1 TUBE

239 MS21916W10-4 2 REDUCER

Component COMPD01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

LN9424A100 As required WIRE

Equipment BFEZ01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

214 QA06753-03 2 FILTER

215 E61751-00-0001 2 REDUCER

216 TP0714033 2 SWITCH

217 HTE400115 2 VALVE

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) Task 20-28-00-912-802

Fig. A-GBFAA

Installation of the U-Section and the

Flow Metering System (FMS)

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

(a) Install the Halon Filter, FIN 5010WE, for Fire Ext. Bottle No. 1.

Refer to Fig. A-GBFAA

1 On the U-section, between FR37RH and FR37.1RH, install :

Refer to Fig. A-GBFAA Sheet 01, Fig. A-GBFAA Sheet 03 and Fig. A-GBFAA

Sheet 04

1 Filter-Halon QA06753-03 Item 214

NOTE: See NOTE 03

with :

3 Washer NAS1149D0432K Item 140

3 Screw NAS1100E4-34 Item 146

and

2 O-Ring NSA8202-6 Item 133

1 Fitting A2627048221600 Item 134

NOTE: See NOTE 03

1 Fitting A2627048220400 Item 132

NOTE: See NOTE 03

2 Secure the fittings, Items 132 and 134, with :

As

required

Wire-Lock LN9424A100

3 On the fitting, Item 134, install :

1 Hose Assy F2627007200000 Item 227

NOTE: See NOTE 03

NOTE (03): No lubrication on this item.

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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(b) Install the Pressure Reducer, FIN 5014WE, for Fire Ext. Bottle No. 1.

1 On the U-section, between FR37RH and FR37.1RH, install :

Refer to Fig. A-GBFAA Sheet 01, Fig. A-GBFAA Sheet 03 and Fig. A-GBFAA

Sheet 04

1 Reducer-Pressure E61751-00-0001 Item 215

NOTE: See NOTE 03

with :

1 Washer-Tab A2627048920000 Item 147

2 Fitting A2627048220400 Item 132

NOTE: See NOTE 03

2 O-Ring NSA8202-6 Item 133

NOTE (03): No lubrication on this item.

2 Secure the fittings, Item 132, with :

As

required

Wire-Lock LN9424A100

(c) Install the Pressure Switch, FIN 4016WX, for Fire Ext. Bottle No. 1.

1 On the pressure reducer 5014WE, between FR37RH and FR37.1RH, install :

Refer to Fig. A-GBFAA Sheet 01, Fig. A-GBFAA Sheet 03, Fig. A-GBFAA

Sheet 04 and Fig. A-GBFAA Sheet 05

1 Tube Assy G2627006000800 Item 221

with :

1 Washer NAS1149C0332R Item 144

1 Screw NAS1801-3-7 Item 145

1 Clamp NSA5516A06NJ Item 148

and

1 Switch-Pressure TP0714033 Item 216

NOTE: See NOTE 03

2 On the pressure switch, Item 216, install :

1 Tube Assy G2627006001800 Item 222

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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SERVICE BULLETIN

with :

1 Washer NAS1149F0332P Item 106

1 SCREW NAS1801-3-10 Item 159

1 CLAMP MS21103-4 Item 160

NOTE (03): No lubrication on this item.

(d) Install the Check Valve, FIN 5016WE, for Fire Ext. Bottle No. 1.

1 On the pressure reducer 5014WE, between FR37RH and FR37.1RH, install :

Refer to Fig. A-GBFAA Sheet 01, Fig. A-GBFAA Sheet 03 and Fig. A-GBFAA

Sheet 05

1 Tube Assy F2627006003600 Item 223

1 Restrictor A2627048220200 Item 224

1 Tube Assy F2627006001400 Item 225

and

1 Valve-Nonreturn HTE400115 Item 217

NOTE: See NOTE 03

2 On the check valve, Item 217, install :

1 Tube Assy F2627006000000 Item 226

with :

1 Washer NAS1149C0332R Item 144

1 Screw NAS1801-3-7 Item 145

1 Clamp NSA5516A06NJ Item 148

NOTE (03): No lubrication on this item.

(e) Install the Halon Filter, FIN 5011WE, for Fire Ext. Bottle No. 2.

Refer to Fig. A-GBFAA

1 On the U-section, between FR37RH and FR37.1RH, install :

Refer to Fig. A-GBFAA Sheet 01, Fig. A-GBFAA Sheet 03 and Fig. A-GBFAA

Sheet 04

1 Filter-Halon QA06753-03 Item 214

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 424

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NOTE: See NOTE 03

with :

3 Washer NAS1149D0432K Item 140

3 Screw NAS1100E4-34 Item 146

and

2 O-Ring NSA8202-6 Item 133

1 Fitting A2627048221600 Item 134

NOTE: See NOTE 03

1 Fitting A2627048220400 Item 132

NOTE: See NOTE 03

2 Secure the fittings, Items 132 and 134, with :

As

required

Wire-Lock LN9424A100

3 On the fitting, Item 134, install :

1 Hose Assy F2627007200200 Item 228

NOTE: See NOTE 03

NOTE (03): No lubrication on this item.

(f) Install the Pressure Reducer, FIN 5015WE, for Fire Ext. Bottle No. 2.

1 On the U-section, between FR37RH and FR37.1RH, install :

Refer to Fig. A-GBFAA Sheet 01, Fig. A-GBFAA Sheet 03 and Fig. A-GBFAA

Sheet 04

1 Reducer-Pressure E61751-00-0001 Item 215

NOTE: See NOTE 03

with :

1 Washer-Tab A2627048920000 Item 147

2 Fitting A2627048220400 Item 132

NOTE: See NOTE 03

2 O-Ring NSA8202-6 Item 133

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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SERVICE BULLETIN

2 Secure the fittings, Item 132, with :

As

required

Wire-Lock LN9424A100

NOTE (03): No lubrication on this item.

(g) Install the Pressure Switch, FIN 4018WX, for Fire Ext. Bottle No. 2

1 On the pressure reducer 5015WE, between FR37RH and FR37.1RH, install :

Refer to Fig. A-GBFAA Sheet 01, Fig. A-GBFAA Sheet 03 and Fig. A-GBFAA

Sheet 04

1 Tube Assy G2627006001000 Item 219

with :

1 Washer NAS1149C0332R Item 144

1 Screw NAS1801-3-7 Item 145

1 Clamp NSA5516A06NJ Item 148

and

1 Switch-Pressure TP0714033 Item 216

NOTE: See NOTE 03

2 On the pressure switch, Item 216, install :

1 Tube Assy G2627006002000 Item 229

with :

1 Washer NAS1149F0332P Item 106

1 SCREW NAS1801-3-10 Item 159

1 CLAMP MS21103-4 Item 160

NOTE (03): No lubrication on this item.

(h) Install the Check Valve, FIN 5017WE, for Fire Ext. Bottle No. 2

1 On the pressure reducer 5015WE, between FR37RH and FR37.1RH, install :

Refer to Fig. A-GBFAA Sheet 01, Fig. A-GBFAA Sheet 03 and Fig. A-GBFAA

Sheet 05

1 Tube Assy G2627006001200 Item 230

1 Restrictor A2627048220200 Item 224

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 426

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SERVICE BULLETIN

1 Tube Assy G2627006001400 Item 231

and

1 Valve-Nonreturn HTE400115 Item 217

NOTE: See NOTE 03

2 On the check valve, Item 217, install :

1 Tube Assy G2627006001600 Item 232

with :

1 Washer NAS1149C0332R Item 144

1 Screw NAS1801-3-7 Item 145

1 Clamp NSA5516A06NJ Item 148

1 Nut NAS1726-3E Item 113

NOTE (03): No lubrication on this item.

(i) Install the new plumbing and rod ends between FR36RH and FR37.1

1 Between FR36RH and FR37.1, install the rod ends :

Refer to Fig. A-GBFAA Sheet 01 and Fig. A-GBFAA Sheet 02

2 Rod End NSA8141-04R Item (135) Retained at

removal

2 Rod End NSA8140-04RK Item (137) Retained at

removal

with :

2 Nut NAS1726-4E Item 104

2 BOLT NAS1304-12 Item 139

4 Washer NAS1149D0432K Item 140

2 Nut NAS509-5 Item (136) Retained at

removal

2 Washer-Lock NSA5355-5CA Item 141

and

2 Lead-Bonding E0090-10-320NN Item 152

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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2 Lead-Bonding E0090-10-350NN Item 153

with :

4 Washer NAS1149F0332P Item 106

4 Screw NAS1801-3-8 Item 143

NOTE: Do the electrical bonding (Refer to AMM Task

20-28-00-912-802)

2 Between FR36RH and FR37.1, install the plumbing :

Refer to Fig. A-GBFAA Sheet 01 and Fig. A-GBFAA Sheet 03

2 Hose A2627045200400 Item (209) Retained at

removal

2 Hose Assy F2627007100200 Item (210) Retained at

removal

1 Cross NSA855140-22D Item 233

1 Tube Assy G2627005013200 Item 234

1 Union MS21902W10 Item 235

with :

2 Screw NAS1801-3-8 Item 143

2 Washer NAS1149C0332R Item 144

2 Nut NAS1726-3E Item 113

2 Clamp NSA5516A18NJ Item 121

and

1 Tube Assy A2627045107800 Item 236

1 Tee NSA855113-34D Item 237

1 Tube Assy G2627005003400 Item 238

2 Reducer MS21916W10-4 Item 239

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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(26) Subtask 265020-831-211-001 - Install the Fire Extinguishing Bottles 4005WX and

4010WX.

Work Zones and Access Panels

Zone Access/Work location

132 Access Panel 132PM

Work location from Frame 35 to Frame 37.1

Manpower Resources

Manhours 2.00

Minimum number of person 2

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 265020D01R03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

100 NAS1726-5E 8 NUT

101 NAS1305-2 8 BOLT

103 NAS1304-9 2 BOLT

104 NAS1726-4E 2 NUT

Component COMPD01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

LN9424A100 As required WIRE

References

Aircraft Maintenance Manual (AMM) 26-23-41, Page Block 401

Fig. A-GBHAA

Installation of Fire Extinguishing Bottles

4005WX and 4010WX with Cartridges.

Sheet 01

Sheet 02

Sheet 03

Refer to Fig. A-GBHAA

(a) Install the fire extinguishing bottle 1 (FWD) 4005WX.

1 Between FR36RH and FR37RH, install the fire extinguishing bottle 4005WX

(Refer to AMM 26-23-41, Page Block 401) :

Refer to Fig. A-GBHAA Sheet 01, Fig. A-GBHAA Sheet 02and Fig. A-GBHAA

Sheet 03, Detail D :

1 Extinguisher-Fire 34900008-2 Item (201) Retained at

removal

with :

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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4 Nut NAS1726-5E Item 100

4 Bolt NAS1305-2 Item 101

1 Bolt NAS1304-9 Item 103

1 Nut NAS1726-4E Item 104

2 Screw Item (260)

2 Washer Item (261)

2 Nut Item (262)

NOTE: Item (260), (261) and (262) are retained parts.

2 Secure the coupling nuts of the fire extinguishing discharge heads with :

As

required

Wire-Lock LN9424A100

(b) Install the fire extinguishing bottle 2 (AFT) 4010WX.

1 Between FR37RH and FR37.1RH, install the fire extinguishing bottle 4010WX

(Refer to AMM 26-23-41, Page Block 401) :

Refer to Fig. A-GBHAA Sheet 01 and Fig. A-GBHAA Sheet 03 :

1 Extinguisher-Fire 35200003-2 Item (200) Retained at

removal

with :

4 Nut NAS1726-5E Item 100

4 Bolt NAS1305-2 Item 101

1 Bolt NAS1304-9 Item 103

1 Nut NAS1726-4E Item 104

2 Screw Item (260)

2 Washer Item (261)

2 Nut Item (262)

NOTE: Item (260), (261) and (262) are retained parts.

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 430

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2 Secure the coupling nuts of the fire extinguishing discharge heads with :

As

required

Wire-Lock LN9424A100

(27) Subtask 265020-831-212-001 - Install the new identification placards.

Work Zones and Access Panels

Zone Access/Work location

132 Work location from Frame 37 to Frame 37.1

Manpower Resources

Manhours 1.50

Minimum number of person 2

Subtask elapsed time 0.75

Skills NON SPECIFIC

Material necessary to do the job

Kit 265020D01R03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

240 F2627004120800 1 PLACARD

241 F2627004121400 1 PLACARD

242 F2627004121200 1 PLACARD

243 F2627004120400 1 PLACARD

244 F2627004120600 1 PLACARD

245 F2627004121600 1 PLACARD

246 F2627004121800 1 PLACARD

247 F2627004121000 1 PLACARD

248 G2627004020200 1 PLACARD

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Abrasion Resistant Coating

(Teflon Polyuret)

07-003 As required

General Purpose Adhesive

Honeycomb Filler

08-554 As required

References

Fig. A-GBFAA

Installation of the U-Section and the

Flow Metering System (FMS)

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 431

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(a) Install the identification placards 4010WX, 4016WX, 4018WX, 5010WE, 5011WE,

5014WE, 5015WE, 5016WE, 5017WE, between FR37 and FR37.1.

Refer to Fig. A-GBFAA

1 Between FR37RH and FR37.1RH, install :

Refer to Fig. A-GBFAA Sheet 01, Fig. A-GBFAA Sheet 03 and Fig. A-GBFAA

Sheet 06

1 Placard F2627004120800 Item 240

1 Placard F2627004121400 Item 241

1 Placard F2627004121200 Item 242

1 Placard F2627004120400 Item 243

1 Placard F2627004120600 Item 244

1 Placard F2627004121600 Item 245

1 Placard F2627004121800 Item 246

1 Placard F2627004121000 Item 247

1 Placard G2627004020200 Item 248

Bond the placard, Item 248, with :

General Purpose

Adhesive

Honeycomb Filler

08-554 As required

Protect the placard, Item 248, with :

Abrasion Resistant

Coating (Teflon

Polyuret)

07-003 As required

**CONF ALL

D. TEST

**CONF 001

(1) Subtask 265020-861-001-001 - Energize Electrical Network

Manpower Resources

Skills NON SPECIFIC

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 432

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SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) Task 24-41-00-861-801

(a) In the cockpit, on the panel 235VU, push these pushbutton switches :

- BAT 1, BAT 2, APU BAT,

- GEN 1 (2,3, 4), APU GEN,

- EXT A(B).

(b) Remove the warning notices.

(c) Energize the aircraft electrical circuits (Refer to AMM Task 24-41-00-861-801).

(d) Remove the safety clips and tags and close these circuit breakers :

PANEL DESIGNATION FIN LOCATION SEE

NOTES

742VU 701PP 10PB1 72 S

742VU 702PP 10PB2 71 S

(2) Subtask 265020-700-001-001 - Preliminary Tests

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 21-26-00-710-803

Task 22-96-00-740-801

Task 22-97-00-740-801

Task 31-50-00-710-803

Task 31-50-00-740-801

Task 31-60-00-710-802

Task 33-13-00-710-801

Task 33-14-00-710-801

Elec. Std. Practices Manual (ESPM) 20-52-10

NOTE: If the aircraft is operated in CAT III conditions, you must also do the

LAND CAT III capability test (Refer to AMM Task 22-97-00-740-801).

(a) On each connector which was disconnected, do the checks as defined in ESPM

20-52-10.

NOTE: The functional test or operational test requested by this ESPM

procedure is given hereafter.

(b) Do an operational test of the instrument and panel integral lighting (Refer to AMM

Task 33-13-00-710-801).

(c) Do an operational test of the lights (Refer to AMM Task 33-14-00-710-801).

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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(d) Do an operational test of the avionics equipment ventilation system (Refer to AMM

Task 21-26-00-710-803).

(e) Do a BITE test of the Automatic Flight System (AFS) (SYSTEM TEST) (Refer to

AMM Task 22-96-00-740-801).

(f) Do an operational test of the Electronic Centralized Aircraft Monitoring (ECAM)

control panel (Refer to AMM Task 31-50-00-710-803).

(g) Do the test of the Flight Warning System (FWS) (Refer to AMM Task

31-50-00-740-801).

(h) Do an operational test of the Electronic Instrument System (EIS) (Refer to AMM

Task 31-60-00-710-802).

(3) Subtask 265020-700-002-001 - Testing

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 21-28-00-710-802

Task 21-28-00-710-803

Task 21-31-00-710-801

Task 21-63-00-730-801

Task 23-36-00-710-808

Task 23-51-00-740-801

Task 23-71-00-710-801

Task 23-73-00-710-814

Task 23-81-00-740-801

Task 25-11-00-710-801

Task 26-16-00-740-801

Task 27-51-00-740-801

Task 27-81-00-740-801

Task 27-96-00-710-816

Task 28-24-00-710-801

Task 28-51-00-740-801

Task 29-13-00-710-803

Task 30-21-00-710-807

Task 30-45-00-720-801

Task 32-31-00-740-801

Task 33-44-00-710-801

Task 36-11-00-740-805

Task 52-71-00-740-801

Task 71-00-00-720-802

(a) Tests after removal/installation of the RH overhead panel 212VU

1 Do an operational test of the flight control computers

engagement/disengagement (Refer to AMM Task 27-96-00-710-816).

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 434

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2 Do an operational test of the hard wired backup of ventilation controller to

make sure that the isolation valves and cold air valve close correctly (if

installed) (Refer to AMM Task 21-28-00-710-803).

3 Do the dry motoring check (Refer to AMM Task 71-00-00-720-802).

4 Do a functional test of the windshield rain protection (Refer to AMM Task

30-45-00-720-801).

(b) Tests after removal/installation of the captain seat

1 Do an operational test of the seat of the captain (Refer to AMM Task

25-11-00-710-801).

(c) Tests after removal/installation of the Reset CBs Panel 262VU

1 Do the BITE test of the normal extension and retraction system (Refer to AMM

Task 32-31-00-740-801).

2 Do the Fuel Control Monitoring System (FCMS) BITE test (Refer to AMM Task

28-51-00-740-801).

3 Do an operational test of the pressure control and monitoring (Refer to AMM

Task 21-31-00-710-801).

4 Do the system test of the cockpit and cabin temperature-control (Refer to

AMM Task 21-63-00-730-801).

5 Do the manual RESET of the Cabin Intercommunication Data System (CIDS)

(Refer to AMM Task 23-73-00-710-814).

6 Do an operational test of the Lower Deck Cargo-Compartment (LDCC)

ventilation system (SYSTEM) (Refer to AMM Task 21-28-00-710-802).

7 Do the BITE test of the smoke detection system through the Multipurpose

Control and Display Unit (MCDU) (Refer to AMM Task 26-16-00-740-801).

8 Do the SYSTEM TEST of the Slat/Flap Control Computer (SFCC) (Refer to

AMM Task 27-51-00-740-801).

9 Do the SYSTEM TEST of the SFCC (Refer to AMM Task 27-81-00-740-801).

10 Do the BITE test of the Proximity Switch Control Unit (PSCU) (5MJ) (Refer to

AMM Task 52-71-00-740-801).

(d) Tests after removal/installation of the Audio Control Panel 2RN3

1 Do the BITE test of the audio system (Refer to AMM Task 23-51-00-740-801).

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 435

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(e) Tests after removal/installation of the Data Loader Selector 101TD

1 Make sure that this C/B is closed :

PANEL DESIGNATION FIN LOCATION SEE

NOTES

721 DATA LOADER 3TD 12 L

721 DATA LOADER 3TD 13 L

721 DATA LOADER 3TD 18 L

NOTE: The location of the C/B depends on aircraft configuration.

2 On the overhead panel Data Loading Selector 101TD, put the data loading

selector ON/OFF switch to the ON position.

3 On the overhead panel data loading selector display, make sure that the

messages "DB/N:XXXXXXX" and "PUSH NEXT/PREV" come into view.

4 On the overhead panel Data Loading Selector 101TD, put the data loading

selector ON/OFF switch to the OFF position.

(f) Tests after removal/installation of the CVR Control Unit 1RK

1 Do an operational test of the CVR and of the recording on all four channels

(Refer to AMM Task 23-71-00-710-801).

(g) Tests after removal/installation of the Radio Management Panel 1RG3

1 Do the BITE test of the radio management (Refer to AMM Task

23-81-00-740-801).

(h) Tests after removal/installation of the panel 272VU

1 Do the operational test of the landscape-camera system (Refer to AMM Task

23-36-00-710-808).

(i) Tests after removal/installation of the panel 252VU2

1 Included in the preliminary test.

(j) Tests of the connectors

1 2539VC and 2636VC :

a Do a BITE test of the Bleed Monitoring Computer (BMC) 1 (2) (Refer to

AMM Task 36-11-00-740-805).

2 2625VC :

a Do an operational test of the Low Pressure (LP) fuel valve using

individual motors to make sure that the actuator moves correctly and the

cockpit indication is correct (Refer to AMM Task 28-24-00-710-801).

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 436

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3 1449VC, 1518VC and 2044VC :

a Do an operational test of the taxi camera lighting (Refer to AMM Task

33-44-00-710-801).

4 580VC and 2618VC :

a Do an operational test of the LDCC ventilation system (SYSTEM TEST)

(Refer to AMM Task 21-28-00-710-802).

5 1728VC :

a Do an operational test of the engine air intake ice protection (Refer to

AMM Task 30-21-00-710-807).

6 1037VC :

a Do an operational test of the YELLOW hydraulic fire shut-off valve (4JY)

(Refer to AMM Task 29-13-00-710-803).

(4) Subtask 265020-700-201-001 - Testing

Work Zones and Access Panels

Zone Access/Work location

132 Work location from Frame 36 to Frame 37.1

210

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 21-28-00-710-801

Task 26-16-34-400-801

26-23-00, Page Block 601

26-23-00, Page Block 501

26-23-00, Page Block 501

(a) Preparation

1 In the avionic compartment, remove the safety clip(s) and tag(s) and open

this(these) circuit breaker(s) :

PANEL DESIGNATION FIN LOCATION SEE

NOTES

722 EXTC FAN FWD CARGO 11HN 34 A

722 SDCU CHAN 2 12WH 36 T

722 CRG FIRE EXTNG/B 2WX 44 W

742 CRG FIRE EXTNG/A 1WX 68 J

742 SDCU CHAN 1 11WH 75 L

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 437

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SERVICE BULLETIN

(b) Procedure

1 Do the test after removal/installation of the SDCU (20WH) (Refer to AMM

Task 26-16-34-400-801).

2 Do the test after disconnection/reconnection of the connectors 582VC, 584VC,

1007VC, 1704VC, 2508VC, 2511VC, 2614VC, 2629VC, 3027VC and 3029VC

and the terminal blocks 580VT and 582VT.

For the test procedure, refer to Appendix 01.

3 Do a "Check of the Lower-Deck Cargo-Compartment (LDCC) FireExtinguishing Distribution-Piping for Obstruction and Leaks" for the fire

extinguishing bottles 4005WX and 4010WX (Refer to AMM 26-23-00, Page

Block 601).

a If the pressure test is not OK, detect and eliminate the leakage.

b If the pressure test is OK, proceed with the next workstep.

4 Do the "Check of the LDCC Fire-Extinguisher Firing-Circuit Continuity" (Refer

to AMM 26-23-00, Page Block 501).

5 Do the "Operational Check of Fire-Extinguishing Bottle Low Pressure

Indication Circuit by PTT" (Refer to AMM 26-23-00, Page Block 501).

6 Do the "Operational test of the LDCC ventilation system (POWER SUPPLY

TEST)" (Refer to AMM Task 21-28-00-710-801).

**CONF 002

(1) Subtask 265020-861-001-001 - Energize Electrical Network

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 24-41-00-861-801

(a) In the cockpit, on the panel 235VU, push these pushbutton switches :

- BAT 1, BAT 2, APU BAT,

- GEN 1 (2,3, 4), APU GEN,

- EXT A(B).

(b) Remove the warning notices.

(c) Energize the aircraft electrical circuits (Refer to AMM Task 24-41-00-861-801).

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 438

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SERVICE BULLETIN

(d) Remove the safety clips and tags and close these circuit breakers :

PANEL DESIGNATION FIN LOCATION SEE

NOTES

742VU 701PP 10PB1 72 S

742VU 702PP 10PB2 71 S

(2) Subtask 265020-700-001-001 - Preliminary Tests

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 21-26-00-710-803

Task 22-96-00-740-801

Task 22-97-00-740-801

Task 31-50-00-710-803

Task 31-50-00-740-801

Task 31-60-00-710-802

Task 33-13-00-710-801

Task 33-14-00-710-801

Elec. Std. Practices Manual (ESPM) 20-52-10

NOTE: If the aircraft is operated in CAT III conditions, you must also do the

LAND CAT III capability test (Refer to AMM Task 22-97-00-740-801).

(a) On each connector which was disconnected, do the checks as defined in ESPM

20-52-10.

NOTE: The functional test or operational test requested by this ESPM

procedure is given hereafter.

(b) Do an operational test of the instrument and panel integral lighting (Refer to AMM

Task 33-13-00-710-801).

(c) Do an operational test of the lights (Refer to AMM Task 33-14-00-710-801).

(d) Do an operational test of the avionics equipment ventilation system (Refer to AMM

Task 21-26-00-710-803).

(e) Do a BITE test of the Automatic Flight System (AFS) (SYSTEM TEST) (Refer to

AMM Task 22-96-00-740-801).

(f) Do an operational test of the Electronic Centralized Aircraft Monitoring (ECAM)

control panel (Refer to AMM Task 31-50-00-710-803).

(g) Do the test of the Flight Warning System (FWS) (Refer to AMM Task

31-50-00-740-801).

(h) Do an operational test of the Electronic Instrument System (EIS) (Refer to AMM

Task 31-60-00-710-802).

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 439

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SERVICE BULLETIN

(3) Subtask 265020-700-002-001 - Testing

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 21-28-00-710-802

Task 21-28-00-710-803

Task 21-31-00-710-801

Task 21-63-00-730-801

Task 23-36-00-710-808

Task 23-51-00-740-801

Task 23-71-00-710-801

Task 23-73-00-710-814

Task 23-81-00-740-801

Task 25-11-00-710-801

Task 26-16-00-740-801

Task 27-51-00-740-801

Task 27-81-00-740-801

Task 27-96-00-710-816

Task 28-24-00-710-801

Task 28-51-00-740-801

Task 29-13-00-710-803

Task 30-21-00-710-807

Task 30-45-00-720-801

Task 32-31-00-740-801

Task 33-44-00-710-801

Task 36-11-00-740-805

Task 52-71-00-740-801

Task 71-00-00-720-802

(a) Tests after removal/installation of the RH overhead panel 212VU

1 Do an operational test of the flight control computers

engagement/disengagement (Refer to AMM Task 27-96-00-710-816).

2 Do an operational test of the hard wired backup of ventilation controller to

make sure that the isolation valves and cold air valve close correctly (if

installed) (Refer to AMM Task 21-28-00-710-803).

3 Do the dry motoring check (Refer to AMM Task 71-00-00-720-802).

4 Do a functional test of the windshield rain protection (Refer to AMM Task

30-45-00-720-801).

(b) Tests after removal/installation of the captain seat

1 Do an operational test of the seat of the captain (Refer to AMM Task

25-11-00-710-801).

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 440

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(c) Tests after removal/installation of the Reset CBs Panel 262VU

1 Do the BITE test of the normal extension and retraction system (Refer to AMM

Task 32-31-00-740-801).

2 Do the Fuel Control Monitoring System (FCMS) BITE test (Refer to AMM Task

28-51-00-740-801).

3 Do an operational test of the pressure control and monitoring (Refer to AMM

Task 21-31-00-710-801).

4 Do the system test of the cockpit and cabin temperature-control (Refer to

AMM Task 21-63-00-730-801).

5 Do the manual RESET of the Cabin Intercommunication Data System (CIDS)

(Refer to AMM Task 23-73-00-710-814).

6 Do an operational test of the Lower Deck Cargo-Compartment (LDCC)

ventilation system (SYSTEM) (Refer to AMM Task 21-28-00-710-802).

7 Do the BITE test of the smoke detection system through the Multipurpose

Control and Display Unit (MCDU) (Refer to AMM Task 26-16-00-740-801).

8 Do the SYSTEM TEST of the Slat/Flap Control Computer (SFCC) (Refer to

AMM Task 27-51-00-740-801).

9 Do the SYSTEM TEST of the SFCC (Refer to AMM Task 27-81-00-740-801).

10 Do the BITE test of the Proximity Switch Control Unit (PSCU) (5MJ) (Refer to

AMM Task 52-71-00-740-801).

(d) Tests after removal/installation of the Audio Control Panel 2RN3

1 Do the BITE test of the audio system (Refer to AMM Task 23-51-00-740-801).

(e) Tests after removal/installation of the Data Loader Selector 101TD

1 Make sure that this C/B is closed :

PANEL DESIGNATION FIN LOCATION SEE

NOTES

721 DATA LOADER 3TD 12 L

721 DATA LOADER 3TD 13 L

721 DATA LOADER 3TD 18 L

NOTE: The location of the C/B depends on aircraft configuration.

2 On the overhead panel Data Loading Selector 101TD, put the data loading

selector ON/OFF switch to the ON position.

3 On the overhead panel data loading selector display, make sure that the

messages "DB/N:XXXXXXX" and "PUSH NEXT/PREV" come into view.

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 441

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SERVICE BULLETIN

4 On the overhead panel Data Loading Selector 101TD, put the data loading

selector ON/OFF switch to the OFF position.

(f) Tests after removal/installation of the CVR Control Unit 1RK

1 Do an operational test of the CVR and of the recording on all four channels

(Refer to AMM Task 23-71-00-710-801).

(g) Tests after removal/installation of the Radio Management Panel 1RG3

1 Do the BITE test of the radio management (Refer to AMM Task

23-81-00-740-801).

(h) Tests after removal/installation of the panel 272VU

1 Do the operational test of the landscape-camera system (Refer to AMM Task

23-36-00-710-808).

(i) Tests after removal/installation of the panel 252VU2

1 Included in the preliminary test.

(j) Tests of the connectors

1 2539VC and 2636VC :

a Do a BITE test of the Bleed Monitoring Computer (BMC) 1 (2) (Refer to

AMM Task 36-11-00-740-805).

2 2625VC :

a Do an operational test of the Low Pressure (LP) fuel valve using

individual motors to make sure that the actuator moves correctly and the

cockpit indication is correct (Refer to AMM Task 28-24-00-710-801).

3 1449VC, 1518VC and 2044VC :

a Do an operational test of the taxi camera lighting (Refer to AMM Task

33-44-00-710-801).

4 580VC and 2618VC :

a Do an operational test of the LDCC ventilation system (SYSTEM TEST)

(Refer to AMM Task 21-28-00-710-802).

5 1728VC :

a Do an operational test of the engine air intake ice protection (Refer to

AMM Task 30-21-00-710-807).

6 1037VC :

a Do an operational test of the YELLOW hydraulic fire shut-off valve (4JY)

(Refer to AMM Task 29-13-00-710-803).

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 442

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SERVICE BULLETIN

(4) Subtask 265020-700-201-001 - Testing

Work Zones and Access Panels

Zone Access/Work location

132 Work location from Frame 36 to Frame 37.1

210

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 21-28-00-710-801

Task 26-16-34-400-801

26-23-00, Page Block 601

26-23-00, Page Block 501

26-23-00, Page Block 501

(a) Preparation

1 In the avionic compartment, remove the safety clip(s) and tag(s) and open

this(these) circuit breaker(s) :

PANEL DESIGNATION FIN LOCATION SEE

NOTES

722 EXTC FAN FWD CARGO 11HN 34 A

722 SDCU CHAN 2 12WH 36 T

722 CRG FIRE EXTNG/B 2WX 44 W

742 CRG FIRE EXTNG/A 1WX 68 J

742 SDCU CHAN 1 11WH 75 L

(b) Procedure

1 Do the test after removal/installation of the SDCU (20WH) (Refer to AMM

Task 26-16-34-400-801).

2 Do the test after disconnection/reconnection of the connectors 582VC, 584VC,

1007VC, 1704VC, 2508VC, 2511VC, 2614VC, 2629VC, 3027VC and 3029VC

and the terminal blocks 580VT and 582VT.

For the test procedure, refer to Appendix 01.

3 Do a "Check of the Lower-Deck Cargo-Compartment (LDCC) FireExtinguishing Distribution-Piping for Obstruction and Leaks" for the fire

extinguishing bottles 4005WX and 4010WX (Refer to AMM 26-23-00, Page

Block 601).

a If the pressure test is not OK, detect and eliminate the leakage.

b If the pressure test is OK, proceed with the next workstep.

4 Do the "Check of the LDCC Fire-Extinguisher Firing-Circuit Continuity" (Refer

to AMM 26-23-00, Page Block 501).

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 443

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5 Do the "Operational Check of Fire-Extinguishing Bottle Low Pressure

Indication Circuit by PTT" (Refer to AMM 26-23-00, Page Block 501).

6 Do the "Operational test of the LDCC ventilation system (POWER SUPPLY

TEST)" (Refer to AMM Task 21-28-00-710-801).

**CONF 003

(1) Subtask 265020-861-001-001 - Energize Electrical Network

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 24-41-00-861-801

(a) In the cockpit, on the panel 235VU, push these pushbutton switches :

- BAT 1, BAT 2, APU BAT,

- GEN 1 (2,3, 4), APU GEN,

- EXT A(B).

(b) Remove the warning notices.

(c) Energize the aircraft electrical circuits (Refer to AMM Task 24-41-00-861-801).

(d) Remove the safety clips and tags and close these circuit breakers :

PANEL DESIGNATION FIN LOCATION SEE

NOTES

742VU 701PP 10PB1 72 S

742VU 702PP 10PB2 71 S

(2) Subtask 265020-700-001-001 - Preliminary Tests

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 21-26-00-710-803

Task 22-96-00-740-801

Task 22-97-00-740-801

Task 31-50-00-710-803

Task 31-50-00-740-801

Task 31-60-00-710-802

Task 33-13-00-710-801

Task 33-14-00-710-801

Elec. Std. Practices Manual (ESPM) 20-52-10

NOTE: If the aircraft is operated in CAT III conditions, you must also do the

LAND CAT III capability test (Refer to AMM Task 22-97-00-740-801).

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 444

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@A340-500/600

SERVICE BULLETIN

(a) On each connector which was disconnected, do the checks as defined in ESPM

20-52-10.

NOTE: The functional test or operational test requested by this ESPM

procedure is given hereafter.

(b) Do an operational test of the instrument and panel integral lighting (Refer to AMM

Task 33-13-00-710-801).

(c) Do an operational test of the lights (Refer to AMM Task 33-14-00-710-801).

(d) Do an operational test of the avionics equipment ventilation system (Refer to AMM

Task 21-26-00-710-803).

(e) Do a BITE test of the Automatic Flight System (AFS) (SYSTEM TEST) (Refer to

AMM Task 22-96-00-740-801).

(f) Do an operational test of the Electronic Centralized Aircraft Monitoring (ECAM)

control panel (Refer to AMM Task 31-50-00-710-803).

(g) Do the test of the Flight Warning System (FWS) (Refer to AMM Task

31-50-00-740-801).

(h) Do an operational test of the Electronic Instrument System (EIS) (Refer to AMM

Task 31-60-00-710-802).

(3) Subtask 265020-700-002-001 - Testing

Manpower Resources

Skills NON SPECIFIC

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 445

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@A340-500/600

SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) Task 21-28-00-710-802

Task 21-28-00-710-803

Task 21-31-00-710-801

Task 21-63-00-730-801

Task 23-36-00-710-808

Task 23-51-00-740-801

Task 23-71-00-710-801

Task 23-73-00-710-814

Task 23-81-00-740-801

Task 25-11-00-710-801

Task 26-16-00-740-801

Task 27-51-00-740-801

Task 27-81-00-740-801

Task 27-96-00-710-816

Task 28-24-00-710-801

Task 28-51-00-740-801

Task 29-13-00-710-803

Task 30-21-00-710-807

Task 30-45-00-720-801

Task 32-31-00-740-801

Task 33-44-00-710-801

Task 36-11-00-740-805

Task 52-71-00-740-801

Task 71-00-00-720-802

(a) Tests after removal/installation of the RH overhead panel 212VU

1 Do an operational test of the flight control computers

engagement/disengagement (Refer to AMM Task 27-96-00-710-816).

2 Do an operational test of the hard wired backup of ventilation controller to

make sure that the isolation valves and cold air valve close correctly (if

installed) (Refer to AMM Task 21-28-00-710-803).

3 Do the dry motoring check (Refer to AMM Task 71-00-00-720-802).

4 Do a functional test of the windshield rain protection (Refer to AMM Task

30-45-00-720-801).

(b) Tests after removal/installation of the captain seat

1 Do an operational test of the seat of the captain (Refer to AMM Task

25-11-00-710-801).

(c) Tests after removal/installation of the Reset CBs Panel 262VU

1 Do the BITE test of the normal extension and retraction system (Refer to AMM

Task 32-31-00-740-801).

2 Do the Fuel Control Monitoring System (FCMS) BITE test (Refer to AMM Task

28-51-00-740-801).

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 446

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@A340-500/600

SERVICE BULLETIN

3 Do an operational test of the pressure control and monitoring (Refer to AMM

Task 21-31-00-710-801).

4 Do the system test of the cockpit and cabin temperature-control (Refer to

AMM Task 21-63-00-730-801).

5 Do the manual RESET of the Cabin Intercommunication Data System (CIDS)

(Refer to AMM Task 23-73-00-710-814).

6 Do an operational test of the Lower Deck Cargo-Compartment (LDCC)

ventilation system (SYSTEM) (Refer to AMM Task 21-28-00-710-802).

7 Do the BITE test of the smoke detection system through the Multipurpose

Control and Display Unit (MCDU) (Refer to AMM Task 26-16-00-740-801).

8 Do the SYSTEM TEST of the Slat/Flap Control Computer (SFCC) (Refer to

AMM Task 27-51-00-740-801).

9 Do the SYSTEM TEST of the SFCC (Refer to AMM Task 27-81-00-740-801).

10 Do the BITE test of the Proximity Switch Control Unit (PSCU) (5MJ) (Refer to

AMM Task 52-71-00-740-801).

(d) Tests after removal/installation of the Audio Control Panel 2RN3

1 Do the BITE test of the audio system (Refer to AMM Task 23-51-00-740-801).

(e) Tests after removal/installation of the Data Loader Selector 101TD

1 Make sure that this C/B is closed :

PANEL DESIGNATION FIN LOCATION SEE

NOTES

721 DATA LOADER 3TD 12 L

721 DATA LOADER 3TD 13 L

721 DATA LOADER 3TD 18 L

NOTE: The location of the C/B depends on aircraft configuration.

2 On the overhead panel Data Loading Selector 101TD, put the data loading

selector ON/OFF switch to the ON position.

3 On the overhead panel data loading selector display, make sure that the

messages "DB/N:XXXXXXX" and "PUSH NEXT/PREV" come into view.

4 On the overhead panel Data Loading Selector 101TD, put the data loading

selector ON/OFF switch to the OFF position.

(f) Tests after removal/installation of the CVR Control Unit 1RK

1 Do an operational test of the CVR and of the recording on all four channels

(Refer to AMM Task 23-71-00-710-801).

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 447

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(g) Tests after removal/installation of the Radio Management Panel 1RG3

1 Do the BITE test of the radio management (Refer to AMM Task

23-81-00-740-801).

(h) Tests after removal/installation of the panel 272VU

1 Do the operational test of the landscape-camera system (Refer to AMM Task

23-36-00-710-808).

(i) Tests after removal/installation of the panel 252VU2

1 Included in the preliminary test.

(j) Tests of the connectors

1 2539VC and 2636VC :

a Do a BITE test of the Bleed Monitoring Computer (BMC) 1 (2) (Refer to

AMM Task 36-11-00-740-805).

2 2625VC :

a Do an operational test of the Low Pressure (LP) fuel valve using

individual motors to make sure that the actuator moves correctly and the

cockpit indication is correct (Refer to AMM Task 28-24-00-710-801).

3 1449VC, 1518VC and 2044VC :

a Do an operational test of the taxi camera lighting (Refer to AMM Task

33-44-00-710-801).

4 580VC and 2618VC :

a Do an operational test of the LDCC ventilation system (SYSTEM TEST)

(Refer to AMM Task 21-28-00-710-802).

5 1728VC :

a Do an operational test of the engine air intake ice protection (Refer to

AMM Task 30-21-00-710-807).

6 1037VC :

a Do an operational test of the YELLOW hydraulic fire shut-off valve (4JY)

(Refer to AMM Task 29-13-00-710-803).

(4) Subtask 265020-700-201-001 - Testing

Work Zones and Access Panels

Zone Access/Work location

132 Work location from Frame 36 to Frame 37.1

210

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 448

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SERVICE BULLETIN

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 21-28-00-710-801

Task 26-16-34-400-801

26-23-00, Page Block 601

26-23-00, Page Block 501

26-23-00, Page Block 501

(a) Preparation

1 In the avionic compartment, remove the safety clip(s) and tag(s) and open

this(these) circuit breaker(s) :

PANEL DESIGNATION FIN LOCATION SEE

NOTES

722 EXTC FAN FWD CARGO 11HN 34 A

722 SDCU CHAN 2 12WH 36 T

722 CRG FIRE EXTNG/B 2WX 44 W

742 CRG FIRE EXTNG/A 1WX 68 J

742 SDCU CHAN 1 11WH 75 L

(b) Procedure

1 Do the test after removal/installation of the SDCU (20WH) (Refer to AMM

Task 26-16-34-400-801).

2 Do the test after disconnection/reconnection of the connectors 582VC, 584VC,

1007VC, 1704VC, 2508VC, 2511VC, 2614VC, 2629VC, 3027VC and 3029VC

and the terminal blocks 580VT and 582VT.

For the test procedure, refer to Appendix 01.

3 Do a "Check of the Lower-Deck Cargo-Compartment (LDCC) FireExtinguishing Distribution-Piping for Obstruction and Leaks" for the fire

extinguishing bottles 4005WX and 4010WX (Refer to AMM 26-23-00, Page

Block 601).

a If the pressure test is not OK, detect and eliminate the leakage.

b If the pressure test is OK, proceed with the next workstep.

4 Do the "Check of the LDCC Fire-Extinguisher Firing-Circuit Continuity" (Refer

to AMM 26-23-00, Page Block 501).

5 Do the "Operational Check of Fire-Extinguishing Bottle Low Pressure

Indication Circuit by PTT" (Refer to AMM 26-23-00, Page Block 501).

6 Do the "Operational test of the LDCC ventilation system (POWER SUPPLY

TEST)" (Refer to AMM Task 21-28-00-710-801).

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 449

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**CONF 004

(1) Subtask 265020-861-001-001 - Energize Electrical Network

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 24-41-00-861-801

(a) In the cockpit, on the panel 235VU, push these pushbutton switches :

- BAT 1, BAT 2, APU BAT,

- GEN 1 (2,3, 4), APU GEN,

- EXT A(B).

(b) Remove the warning notices.

(c) Energize the aircraft electrical circuits (Refer to AMM Task 24-41-00-861-801).

(d) Remove the safety clips and tags and close these circuit breakers :

PANEL DESIGNATION FIN LOCATION SEE

NOTES

742VU 701PP 10PB1 72 S

742VU 702PP 10PB2 71 S

(2) Subtask 265020-700-001-001 - Preliminary Tests

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 21-26-00-710-803

Task 22-96-00-740-801

Task 22-97-00-740-801

Task 31-50-00-710-803

Task 31-50-00-740-801

Task 31-60-00-710-802

Task 33-13-00-710-801

Task 33-14-00-710-801

Elec. Std. Practices Manual (ESPM) 20-52-10

NOTE: If the aircraft is operated in CAT III conditions, you must also do the

LAND CAT III capability test (Refer to AMM Task 22-97-00-740-801).

(a) On each connector which was disconnected, do the checks as defined in ESPM

20-52-10.

NOTE: The functional test or operational test requested by this ESPM

procedure is given hereafter.

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 450

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SERVICE BULLETIN

(b) Do an operational test of the instrument and panel integral lighting (Refer to AMM

Task 33-13-00-710-801).

(c) Do an operational test of the lights (Refer to AMM Task 33-14-00-710-801).

(d) Do an operational test of the avionics equipment ventilation system (Refer to AMM

Task 21-26-00-710-803).

(e) Do a BITE test of the Automatic Flight System (AFS) (SYSTEM TEST) (Refer to

AMM Task 22-96-00-740-801).

(f) Do an operational test of the Electronic Centralized Aircraft Monitoring (ECAM)

control panel (Refer to AMM Task 31-50-00-710-803).

(g) Do the test of the Flight Warning System (FWS) (Refer to AMM Task

31-50-00-740-801).

(h) Do an operational test of the Electronic Instrument System (EIS) (Refer to AMM

Task 31-60-00-710-802).

(3) Subtask 265020-700-002-001 - Testing

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 21-28-00-710-802

Task 21-28-00-710-803

Task 21-31-00-710-801

Task 21-63-00-730-801

Task 23-36-00-710-808

Task 23-51-00-740-801

Task 23-71-00-710-801

Task 23-73-00-710-814

Task 23-81-00-740-801

Task 25-11-00-710-801

Task 26-16-00-740-801

Task 27-51-00-740-801

Task 27-81-00-740-801

Task 27-96-00-710-816

Task 28-24-00-710-801

Task 28-51-00-740-801

Task 29-13-00-710-803

Task 30-21-00-710-807

Task 30-45-00-720-801

Task 32-31-00-740-801

Task 33-44-00-710-801

Task 36-11-00-740-805

Task 52-71-00-740-801

Task 71-00-00-720-802

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 451

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(a) Tests after removal/installation of the RH overhead panel 212VU

1 Do an operational test of the flight control computers

engagement/disengagement (Refer to AMM Task 27-96-00-710-816).

2 Do an operational test of the hard wired backup of ventilation controller to

make sure that the isolation valves and cold air valve close correctly (if

installed) (Refer to AMM Task 21-28-00-710-803).

3 Do the dry motoring check (Refer to AMM Task 71-00-00-720-802).

4 Do a functional test of the windshield rain protection (Refer to AMM Task

30-45-00-720-801).

(b) Tests after removal/installation of the captain seat

1 Do an operational test of the seat of the captain (Refer to AMM Task

25-11-00-710-801).

(c) Tests after removal/installation of the Reset CBs Panel 262VU

1 Do the BITE test of the normal extension and retraction system (Refer to AMM

Task 32-31-00-740-801).

2 Do the Fuel Control Monitoring System (FCMS) BITE test (Refer to AMM Task

28-51-00-740-801).

3 Do an operational test of the pressure control and monitoring (Refer to AMM

Task 21-31-00-710-801).

4 Do the system test of the cockpit and cabin temperature-control (Refer to

AMM Task 21-63-00-730-801).

5 Do the manual RESET of the Cabin Intercommunication Data System (CIDS)

(Refer to AMM Task 23-73-00-710-814).

6 Do an operational test of the Lower Deck Cargo-Compartment (LDCC)

ventilation system (SYSTEM) (Refer to AMM Task 21-28-00-710-802).

7 Do the BITE test of the smoke detection system through the Multipurpose

Control and Display Unit (MCDU) (Refer to AMM Task 26-16-00-740-801).

8 Do the SYSTEM TEST of the Slat/Flap Control Computer (SFCC) (Refer to

AMM Task 27-51-00-740-801).

9 Do the SYSTEM TEST of the SFCC (Refer to AMM Task 27-81-00-740-801).

10 Do the BITE test of the Proximity Switch Control Unit (PSCU) (5MJ) (Refer to

AMM Task 52-71-00-740-801).

(d) Tests after removal/installation of the Audio Control Panel 2RN3

1 Do the BITE test of the audio system (Refer to AMM Task 23-51-00-740-801).

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 452

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(e) Tests after removal/installation of the Data Loader Selector 101TD

1 Make sure that this C/B is closed :

PANEL DESIGNATION FIN LOCATION SEE

NOTES

721 DATA LOADER 3TD 12 L

721 DATA LOADER 3TD 13 L

721 DATA LOADER 3TD 18 L

NOTE: The location of the C/B depends on aircraft configuration.

2 On the overhead panel Data Loading Selector 101TD, put the data loading

selector ON/OFF switch to the ON position.

3 On the overhead panel data loading selector display, make sure that the

messages "DB/N:XXXXXXX" and "PUSH NEXT/PREV" come into view.

4 On the overhead panel Data Loading Selector 101TD, put the data loading

selector ON/OFF switch to the OFF position.

(f) Tests after removal/installation of the CVR Control Unit 1RK

1 Do an operational test of the CVR and of the recording on all four channels

(Refer to AMM Task 23-71-00-710-801).

(g) Tests after removal/installation of the Radio Management Panel 1RG3

1 Do the BITE test of the radio management (Refer to AMM Task

23-81-00-740-801).

(h) Tests after removal/installation of the panel 272VU

1 Do the operational test of the landscape-camera system (Refer to AMM Task

23-36-00-710-808).

(i) Tests after removal/installation of the panel 252VU2

1 Included in the preliminary test.

(j) Tests of the connectors

1 2539VC and 2636VC :

a Do a BITE test of the Bleed Monitoring Computer (BMC) 1 (2) (Refer to

AMM Task 36-11-00-740-805).

2 2625VC :

a Do an operational test of the Low Pressure (LP) fuel valve using

individual motors to make sure that the actuator moves correctly and the

cockpit indication is correct (Refer to AMM Task 28-24-00-710-801).

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 453

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3 1449VC, 1518VC and 2044VC :

a Do an operational test of the taxi camera lighting (Refer to AMM Task

33-44-00-710-801).

4 580VC and 2618VC :

a Do an operational test of the LDCC ventilation system (SYSTEM TEST)

(Refer to AMM Task 21-28-00-710-802).

5 1728VC :

a Do an operational test of the engine air intake ice protection (Refer to

AMM Task 30-21-00-710-807).

6 1037VC :

a Do an operational test of the YELLOW hydraulic fire shut-off valve (4JY)

(Refer to AMM Task 29-13-00-710-803).

(4) Subtask 265020-700-201-001 - Testing

Work Zones and Access Panels

Zone Access/Work location

132 Work location from Frame 36 to Frame 37.1

210

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 21-28-00-710-801

Task 26-16-34-400-801

26-23-00, Page Block 601

26-23-00, Page Block 501

26-23-00, Page Block 501

(a) Preparation

1 In the avionic compartment, remove the safety clip(s) and tag(s) and open

this(these) circuit breaker(s) :

PANEL DESIGNATION FIN LOCATION SEE

NOTES

722 EXTC FAN FWD CARGO 11HN 34 A

722 SDCU CHAN 2 12WH 36 T

722 CRG FIRE EXTNG/B 2WX 44 W

742 CRG FIRE EXTNG/A 1WX 68 J

742 SDCU CHAN 1 11WH 75 L

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 454

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SERVICE BULLETIN

(b) Procedure

1 Do the test after removal/installation of the SDCU (20WH) (Refer to AMM

Task 26-16-34-400-801).

2 Do the test after disconnection/reconnection of the connectors 582VC, 584VC,

1007VC, 1704VC, 2508VC, 2511VC, 2614VC, 2629VC, 3027VC and 3029VC

and the terminal blocks 580VT and 582VT.

For the test procedure, refer to Appendix 01.

3 Do a "Check of the Lower-Deck Cargo-Compartment (LDCC) FireExtinguishing Distribution-Piping for Obstruction and Leaks" for the fire

extinguishing bottles 4005WX and 4010WX (Refer to AMM 26-23-00, Page

Block 601).

a If the pressure test is not OK, detect and eliminate the leakage.

b If the pressure test is OK, proceed with the next workstep.

4 Do the "Check of the LDCC Fire-Extinguisher Firing-Circuit Continuity" (Refer

to AMM 26-23-00, Page Block 501).

5 Do the "Operational Check of Fire-Extinguishing Bottle Low Pressure

Indication Circuit by PTT" (Refer to AMM 26-23-00, Page Block 501).

6 Do the "Operational test of the LDCC ventilation system (POWER SUPPLY

TEST)" (Refer to AMM Task 21-28-00-710-801).

**CONF 005

(1) Subtask 265020-861-001-001 - Energize Electrical Network

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 24-41-00-861-801

(a) In the cockpit, on the panel 235VU, push these pushbutton switches :

- BAT 1, BAT 2, APU BAT,

- GEN 1 (2,3, 4), APU GEN,

- EXT A(B).

(b) Remove the warning notices.

(c) Energize the aircraft electrical circuits (Refer to AMM Task 24-41-00-861-801).

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 455

6

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SERVICE BULLETIN

(d) Remove the safety clips and tags and close these circuit breakers :

PANEL DESIGNATION FIN LOCATION SEE

NOTES

742VU 701PP 10PB1 72 S

742VU 702PP 10PB2 71 S

(2) Subtask 265020-700-001-001 - Preliminary Tests

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 21-26-00-710-803

Task 22-96-00-740-801

Task 22-97-00-740-801

Task 31-50-00-710-803

Task 31-50-00-740-801

Task 31-60-00-710-802

Task 33-13-00-710-801

Task 33-14-00-710-801

Elec. Std. Practices Manual (ESPM) 20-52-10

NOTE: If the aircraft is operated in CAT III conditions, you must also do the

LAND CAT III capability test (Refer to AMM Task 22-97-00-740-801).

(a) On each connector which was disconnected, do the checks as defined in ESPM

20-52-10.

NOTE: The functional test or operational test requested by this ESPM

procedure is given hereafter.

(b) Do an operational test of the instrument and panel integral lighting (Refer to AMM

Task 33-13-00-710-801).

(c) Do an operational test of the lights (Refer to AMM Task 33-14-00-710-801).

(d) Do an operational test of the avionics equipment ventilation system (Refer to AMM

Task 21-26-00-710-803).

(e) Do a BITE test of the Automatic Flight System (AFS) (SYSTEM TEST) (Refer to

AMM Task 22-96-00-740-801).

(f) Do an operational test of the Electronic Centralized Aircraft Monitoring (ECAM)

control panel (Refer to AMM Task 31-50-00-710-803).

(g) Do the test of the Flight Warning System (FWS) (Refer to AMM Task

31-50-00-740-801).

(h) Do an operational test of the Electronic Instrument System (EIS) (Refer to AMM

Task 31-60-00-710-802).

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 456

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SERVICE BULLETIN

(3) Subtask 265020-700-002-001 - Testing

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 21-28-00-710-802

Task 21-28-00-710-803

Task 21-31-00-710-801

Task 21-63-00-730-801

Task 23-36-00-710-808

Task 23-51-00-740-801

Task 23-71-00-710-801

Task 23-73-00-710-814

Task 23-81-00-740-801

Task 25-11-00-710-801

Task 26-16-00-740-801

Task 27-51-00-740-801

Task 27-81-00-740-801

Task 27-96-00-710-816

Task 28-24-00-710-801

Task 28-51-00-740-801

Task 29-13-00-710-803

Task 30-21-00-710-807

Task 30-45-00-720-801

Task 32-31-00-740-801

Task 33-44-00-710-801

Task 36-11-00-740-805

Task 52-71-00-740-801

Task 71-00-00-720-802

(a) Tests after removal/installation of the RH overhead panel 212VU

1 Do an operational test of the flight control computers

engagement/disengagement (Refer to AMM Task 27-96-00-710-816).

2 Do an operational test of the hard wired backup of ventilation controller to

make sure that the isolation valves and cold air valve close correctly (if

installed) (Refer to AMM Task 21-28-00-710-803).

3 Do the dry motoring check (Refer to AMM Task 71-00-00-720-802).

4 Do a functional test of the windshield rain protection (Refer to AMM Task

30-45-00-720-801).

(b) Tests after removal/installation of the captain seat

1 Do an operational test of the seat of the captain (Refer to AMM Task

25-11-00-710-801).

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 457

6

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(c) Tests after removal/installation of the Reset CBs Panel 262VU

1 Do the BITE test of the normal extension and retraction system (Refer to AMM

Task 32-31-00-740-801).

2 Do the Fuel Control Monitoring System (FCMS) BITE test (Refer to AMM Task

28-51-00-740-801).

3 Do an operational test of the pressure control and monitoring (Refer to AMM

Task 21-31-00-710-801).

4 Do the system test of the cockpit and cabin temperature-control (Refer to

AMM Task 21-63-00-730-801).

5 Do the manual RESET of the Cabin Intercommunication Data System (CIDS)

(Refer to AMM Task 23-73-00-710-814).

6 Do an operational test of the Lower Deck Cargo-Compartment (LDCC)

ventilation system (SYSTEM) (Refer to AMM Task 21-28-00-710-802).

7 Do the BITE test of the smoke detection system through the Multipurpose

Control and Display Unit (MCDU) (Refer to AMM Task 26-16-00-740-801).

8 Do the SYSTEM TEST of the Slat/Flap Control Computer (SFCC) (Refer to

AMM Task 27-51-00-740-801).

9 Do the SYSTEM TEST of the SFCC (Refer to AMM Task 27-81-00-740-801).

10 Do the BITE test of the Proximity Switch Control Unit (PSCU) (5MJ) (Refer to

AMM Task 52-71-00-740-801).

(d) Tests after removal/installation of the Audio Control Panel 2RN3

1 Do the BITE test of the audio system (Refer to AMM Task 23-51-00-740-801).

(e) Tests after removal/installation of the Data Loader Selector 101TD

1 Make sure that this C/B is closed :

PANEL DESIGNATION FIN LOCATION SEE

NOTES

721 DATA LOADER 3TD 12 L

721 DATA LOADER 3TD 13 L

721 DATA LOADER 3TD 18 L

NOTE: The location of the C/B depends on aircraft configuration.

2 On the overhead panel Data Loading Selector 101TD, put the data loading

selector ON/OFF switch to the ON position.

3 On the overhead panel data loading selector display, make sure that the

messages "DB/N:XXXXXXX" and "PUSH NEXT/PREV" come into view.

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 458

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SERVICE BULLETIN

4 On the overhead panel Data Loading Selector 101TD, put the data loading

selector ON/OFF switch to the OFF position.

(f) Tests after removal/installation of the CVR Control Unit 1RK

1 Do an operational test of the CVR and of the recording on all four channels

(Refer to AMM Task 23-71-00-710-801).

(g) Tests after removal/installation of the Radio Management Panel 1RG3

1 Do the BITE test of the radio management (Refer to AMM Task

23-81-00-740-801).

(h) Tests after removal/installation of the panel 272VU

1 Do the operational test of the landscape-camera system (Refer to AMM Task

23-36-00-710-808).

(i) Tests after removal/installation of the panel 252VU2

1 Included in the preliminary test.

(j) Tests of the connectors

1 2539VC and 2636VC :

a Do a BITE test of the Bleed Monitoring Computer (BMC) 1 (2) (Refer to

AMM Task 36-11-00-740-805).

2 2625VC :

a Do an operational test of the Low Pressure (LP) fuel valve using

individual motors to make sure that the actuator moves correctly and the

cockpit indication is correct (Refer to AMM Task 28-24-00-710-801).

3 1449VC, 1518VC and 2044VC :

a Do an operational test of the taxi camera lighting (Refer to AMM Task

33-44-00-710-801).

4 580VC and 2618VC :

a Do an operational test of the LDCC ventilation system (SYSTEM TEST)

(Refer to AMM Task 21-28-00-710-802).

5 1728VC :

a Do an operational test of the engine air intake ice protection (Refer to

AMM Task 30-21-00-710-807).

6 1037VC :

a Do an operational test of the YELLOW hydraulic fire shut-off valve (4JY)

(Refer to AMM Task 29-13-00-710-803).

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 459

6

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SERVICE BULLETIN

(4) Subtask 265020-700-201-001 - Testing

Work Zones and Access Panels

Zone Access/Work location

132 Work location from Frame 36 to Frame 37.1

210

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 21-28-00-710-801

Task 26-16-34-400-801

26-23-00, Page Block 601

26-23-00, Page Block 501

26-23-00, Page Block 501

(a) Preparation

1 In the avionic compartment, remove the safety clip(s) and tag(s) and open

this(these) circuit breaker(s) :

PANEL DESIGNATION FIN LOCATION SEE

NOTES

722 EXTC FAN FWD CARGO 11HN 34 A

722 SDCU CHAN 2 12WH 36 T

722 CRG FIRE EXTNG/B 2WX 44 W

742 CRG FIRE EXTNG/A 1WX 68 J

742 SDCU CHAN 1 11WH 75 L

(b) Procedure

1 Do the test after removal/installation of the SDCU (20WH) (Refer to AMM

Task 26-16-34-400-801).

2 Do the test after disconnection/reconnection of the connectors 582VC, 584VC,

1007VC, 1704VC, 2508VC, 2511VC, 2614VC, 2629VC, 3027VC and 3029VC

and the terminal blocks 580VT and 582VT.

For the test procedure, refer to Appendix 01.

3 Do a "Check of the Lower-Deck Cargo-Compartment (LDCC) FireExtinguishing Distribution-Piping for Obstruction and Leaks" for the fire

extinguishing bottles 4005WX and 4010WX (Refer to AMM 26-23-00, Page

Block 601).

a If the pressure test is not OK, detect and eliminate the leakage.

b If the pressure test is OK, proceed with the next workstep.

4 Do the "Check of the LDCC Fire-Extinguisher Firing-Circuit Continuity" (Refer

to AMM 26-23-00, Page Block 501).

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 460

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5 Do the "Operational Check of Fire-Extinguishing Bottle Low Pressure

Indication Circuit by PTT" (Refer to AMM 26-23-00, Page Block 501).

6 Do the "Operational test of the LDCC ventilation system (POWER SUPPLY

TEST)" (Refer to AMM Task 21-28-00-710-801).

**CONF 006

(1) Subtask 265020-861-001-001 - Energize Electrical Network

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 24-41-00-861-801

(a) In the cockpit, on the panel 235VU, push these pushbutton switches :

- BAT 1, BAT 2, APU BAT,

- GEN 1 (2,3, 4), APU GEN,

- EXT A(B).

(b) Remove the warning notices.

(c) Energize the aircraft electrical circuits (Refer to AMM Task 24-41-00-861-801).

(d) Remove the safety clips and tags and close these circuit breakers :

PANEL DESIGNATION FIN LOCATION SEE

NOTES

742VU 701PP 10PB1 72 S

742VU 702PP 10PB2 71 S

(2) Subtask 265020-700-001-001 - Preliminary Tests

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 21-26-00-710-803

Task 22-96-00-740-801

Task 22-97-00-740-801

Task 31-50-00-710-803

Task 31-50-00-740-801

Task 31-60-00-710-802

Task 33-13-00-710-801

Task 33-14-00-710-801

Elec. Std. Practices Manual (ESPM) 20-52-10

NOTE: If the aircraft is operated in CAT III conditions, you must also do the

LAND CAT III capability test (Refer to AMM Task 22-97-00-740-801).

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(a) On each connector which was disconnected, do the checks as defined in ESPM

20-52-10.

NOTE: The functional test or operational test requested by this ESPM

procedure is given hereafter.

(b) Do an operational test of the instrument and panel integral lighting (Refer to AMM

Task 33-13-00-710-801).

(c) Do an operational test of the lights (Refer to AMM Task 33-14-00-710-801).

(d) Do an operational test of the avionics equipment ventilation system (Refer to AMM

Task 21-26-00-710-803).

(e) Do a BITE test of the Automatic Flight System (AFS) (SYSTEM TEST) (Refer to

AMM Task 22-96-00-740-801).

(f) Do an operational test of the Electronic Centralized Aircraft Monitoring (ECAM)

control panel (Refer to AMM Task 31-50-00-710-803).

(g) Do the test of the Flight Warning System (FWS) (Refer to AMM Task

31-50-00-740-801).

(h) Do an operational test of the Electronic Instrument System (EIS) (Refer to AMM

Task 31-60-00-710-802).

(3) Subtask 265020-700-002-001 - Testing

Manpower Resources

Skills NON SPECIFIC

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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References

Aircraft Maintenance Manual (AMM) Task 21-28-00-710-802

Task 21-28-00-710-803

Task 21-31-00-710-801

Task 21-63-00-730-801

Task 23-36-00-710-808

Task 23-51-00-740-801

Task 23-71-00-710-801

Task 23-73-00-710-814

Task 23-81-00-740-801

Task 25-11-00-710-801

Task 26-16-00-740-801

Task 27-51-00-740-801

Task 27-81-00-740-801

Task 27-96-00-710-816

Task 28-24-00-710-801

Task 28-51-00-740-801

Task 29-13-00-710-803

Task 30-21-00-710-807

Task 30-45-00-720-801

Task 32-31-00-740-801

Task 33-44-00-710-801

Task 36-11-00-740-805

Task 52-71-00-740-801

Task 71-00-00-720-802

(a) Tests after removal/installation of the RH overhead panel 212VU

1 Do an operational test of the flight control computers

engagement/disengagement (Refer to AMM Task 27-96-00-710-816).

2 Do an operational test of the hard wired backup of ventilation controller to

make sure that the isolation valves and cold air valve close correctly (if

installed) (Refer to AMM Task 21-28-00-710-803).

3 Do the dry motoring check (Refer to AMM Task 71-00-00-720-802).

4 Do a functional test of the windshield rain protection (Refer to AMM Task

30-45-00-720-801).

(b) Tests after removal/installation of the captain seat

1 Do an operational test of the seat of the captain (Refer to AMM Task

25-11-00-710-801).

(c) Tests after removal/installation of the Reset CBs Panel 262VU

1 Do the BITE test of the normal extension and retraction system (Refer to AMM

Task 32-31-00-740-801).

2 Do the Fuel Control Monitoring System (FCMS) BITE test (Refer to AMM Task

28-51-00-740-801).

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3 Do an operational test of the pressure control and monitoring (Refer to AMM

Task 21-31-00-710-801).

4 Do the system test of the cockpit and cabin temperature-control (Refer to

AMM Task 21-63-00-730-801).

5 Do the manual RESET of the Cabin Intercommunication Data System (CIDS)

(Refer to AMM Task 23-73-00-710-814).

6 Do an operational test of the Lower Deck Cargo-Compartment (LDCC)

ventilation system (SYSTEM) (Refer to AMM Task 21-28-00-710-802).

7 Do the BITE test of the smoke detection system through the Multipurpose

Control and Display Unit (MCDU) (Refer to AMM Task 26-16-00-740-801).

8 Do the SYSTEM TEST of the Slat/Flap Control Computer (SFCC) (Refer to

AMM Task 27-51-00-740-801).

9 Do the SYSTEM TEST of the SFCC (Refer to AMM Task 27-81-00-740-801).

10 Do the BITE test of the Proximity Switch Control Unit (PSCU) (5MJ) (Refer to

AMM Task 52-71-00-740-801).

(d) Tests after removal/installation of the Audio Control Panel 2RN3

1 Do the BITE test of the audio system (Refer to AMM Task 23-51-00-740-801).

(e) Tests after removal/installation of the Data Loader Selector 101TD

1 Make sure that this C/B is closed :

PANEL DESIGNATION FIN LOCATION SEE

NOTES

721 DATA LOADER 3TD 12 L

721 DATA LOADER 3TD 13 L

721 DATA LOADER 3TD 18 L

NOTE: The location of the C/B depends on aircraft configuration.

2 On the overhead panel Data Loading Selector 101TD, put the data loading

selector ON/OFF switch to the ON position.

3 On the overhead panel data loading selector display, make sure that the

messages "DB/N:XXXXXXX" and "PUSH NEXT/PREV" come into view.

4 On the overhead panel Data Loading Selector 101TD, put the data loading

selector ON/OFF switch to the OFF position.

(f) Tests after removal/installation of the CVR Control Unit 1RK

1 Do an operational test of the CVR and of the recording on all four channels

(Refer to AMM Task 23-71-00-710-801).

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(g) Tests after removal/installation of the Radio Management Panel 1RG3

1 Do the BITE test of the radio management (Refer to AMM Task

23-81-00-740-801).

(h) Tests after removal/installation of the panel 272VU

1 Do the operational test of the landscape-camera system (Refer to AMM Task

23-36-00-710-808).

(i) Tests after removal/installation of the panel 252VU2

1 Included in the preliminary test.

(j) Tests of the connectors

1 2539VC and 2636VC :

a Do a BITE test of the Bleed Monitoring Computer (BMC) 1 (2) (Refer to

AMM Task 36-11-00-740-805).

2 2625VC :

a Do an operational test of the Low Pressure (LP) fuel valve using

individual motors to make sure that the actuator moves correctly and the

cockpit indication is correct (Refer to AMM Task 28-24-00-710-801).

3 1449VC, 1518VC and 2044VC :

a Do an operational test of the taxi camera lighting (Refer to AMM Task

33-44-00-710-801).

4 580VC and 2618VC :

a Do an operational test of the LDCC ventilation system (SYSTEM TEST)

(Refer to AMM Task 21-28-00-710-802).

5 1728VC :

a Do an operational test of the engine air intake ice protection (Refer to

AMM Task 30-21-00-710-807).

6 1037VC :

a Do an operational test of the YELLOW hydraulic fire shut-off valve (4JY)

(Refer to AMM Task 29-13-00-710-803).

(4) Subtask 265020-700-201-001 - Testing

Work Zones and Access Panels

Zone Access/Work location

132 Work location from Frame 36 to Frame 37.1

210

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Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 21-28-00-710-801

Task 26-16-34-400-801

26-23-00, Page Block 601

26-23-00, Page Block 501

26-23-00, Page Block 501

(a) Preparation

1 In the avionic compartment, remove the safety clip(s) and tag(s) and open

this(these) circuit breaker(s) :

PANEL DESIGNATION FIN LOCATION SEE

NOTES

722 EXTC FAN FWD CARGO 11HN 34 A

722 SDCU CHAN 2 12WH 36 T

722 CRG FIRE EXTNG/B 2WX 44 W

742 CRG FIRE EXTNG/A 1WX 68 J

742 SDCU CHAN 1 11WH 75 L

(b) Procedure

1 Do the test after removal/installation of the SDCU (20WH) (Refer to AMM

Task 26-16-34-400-801).

2 Do the test after disconnection/reconnection of the connectors 582VC, 584VC,

1007VC, 1704VC, 2508VC, 2511VC, 2614VC, 2629VC, 3027VC and 3029VC

and the terminal blocks 580VT and 582VT.

For the test procedure, refer to Appendix 01.

3 Do a "Check of the Lower-Deck Cargo-Compartment (LDCC) FireExtinguishing Distribution-Piping for Obstruction and Leaks" for the fire

extinguishing bottles 4005WX and 4010WX (Refer to AMM 26-23-00, Page

Block 601).

a If the pressure test is not OK, detect and eliminate the leakage.

b If the pressure test is OK, proceed with the next workstep.

4 Do the "Check of the LDCC Fire-Extinguisher Firing-Circuit Continuity" (Refer

to AMM 26-23-00, Page Block 501).

5 Do the "Operational Check of Fire-Extinguishing Bottle Low Pressure

Indication Circuit by PTT" (Refer to AMM 26-23-00, Page Block 501).

6 Do the "Operational test of the LDCC ventilation system (POWER SUPPLY

TEST)" (Refer to AMM Task 21-28-00-710-801).

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 265020-942-201-001 - Close-up

Work Zones and Access Panels

Zone Access/Work location

132 Access Panel 132PM, Panel 132NM, Panel 132RM

Work location from Frame 35 to Frame 37.1

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 21-20-00-410-801

25-52-00, Page Block 201

Task 25-52-00-400-801

Task 52-30-00-410-801

Task 52-30-00-410-802

(a) Make sure that the work areas are clean and clear of tools and other item of

equipment.

(b) In the FWD cargo-compartment, install the sidewall panels 131PM, 132NM and

132RM(Refer to AMM 25-52-00, Page Block 201).

(c) In the FWD cargo-compartment, install the partition panels 131AW, 131BW,

132CW and the ceiling panels 131BA, 131PA and 131NA(Refer to AMM Task

25-52-00-400-801).

(d) Close the avionics compartment door 132AZ.

(e) Close the FWD cargo-compartment door 821 (Refer to AMM Task

52-30-00-410-801 or AMM Task 52-30-00-410-802).

(f) Install the air-conditioning distribution ducts in the affected area (Refer to AMM

Task 21-20-00-410-801).

(2) Subtask 265020-410-002-001 - Install/Close Items Removed/Opened for access

(Upper Half of Fuselage)

Work Zones and Access Panels

Zone Access/Work location

200

Manpower Resources

Skills NON SPECIFIC

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 467

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References

Aircraft Maintenance Manual (AMM) Task 23-51-12-400-801

Task 23-71-34-400-801

Task 23-81-13-400-801

Task 25-11-51-400-801

Task 25-13-44-400-801

Task 25-13-44-400-802

Task 45-22-21-400-801

Task 52-10-00-410-801

(a) Make sure that the work areas are clean and clear of tools and other item of

equipment.

(b) In the cockpit, install the ceiling panels 211LC, 211MC, 212NC and the strips

211KC and 212CC (Refer to AMM Task 25-13-44-400-801).

(c) On the overhead panel, install and connect (if removed) :

- Reset C/B panel 262VU

- External View Camera Panel 272VU

- Reading Light Panel 252VU2

- AIREADOR panel

- Audio Control Panel (2RN3) (Refer to AMM Task 23-51-12-400-801)

- Data Loader Selector (101TD) (Refer to AMM Task 45-22-21-400-801)

- Cockpit Voice Recorder (CVR) Control Unit (1RK) (Refer to AMM Task

23-71-34-400-801)

- Radio Management Panel (1RG3) (Refer to AMM Task 23-81-13-400-801).

(d) Install the panel (211EW) (Refer to AMM Task 25-13-44-400-802).

(e) Install the captain seat (Refer to AMM Task 25-11-51-400-801).

(f) Close the FWD passenger/crew door(s) 831 or 841 (Refer to AMM Task

52-10-00-410-801).

(3) Subtask 265020-942-001-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 26-16-34-400-801

(a) Do the close-up procedure as specified in the installation of the SDCU (20WH)

(Refer to AMM Task 26-16-34-400-801).

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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(b) Remove the access platforms.

(c) Restore the systems and the aircraft to normal operating condition.

**CONF 002

(1) Subtask 265020-942-201-001 - Close-up

Work Zones and Access Panels

Zone Access/Work location

132 Access Panel 132PM, Panel 132NM, Panel 132RM

Work location from Frame 35 to Frame 37.1

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 21-20-00-410-801

25-52-00, Page Block 201

Task 25-52-00-400-801

Task 52-30-00-410-801

Task 52-30-00-410-802

(a) Make sure that the work areas are clean and clear of tools and other item of

equipment.

(b) In the FWD cargo-compartment, install the sidewall panels 131PM, 132NM and

132RM(Refer to AMM 25-52-00, Page Block 201).

(c) In the FWD cargo-compartment, install the partition panels 131AW, 131BW,

132CW and the ceiling panels 131BA, 131PA and 131NA(Refer to AMM Task

25-52-00-400-801).

(d) Close the avionics compartment door 132AZ.

(e) Close the FWD cargo-compartment door 821 (Refer to AMM Task

52-30-00-410-801 or AMM Task 52-30-00-410-802).

(f) Install the air-conditioning distribution ducts in the affected area (Refer to AMM

Task 21-20-00-410-801).

(2) Subtask 265020-410-002-001 - Install/Close Items Removed/Opened for access

(Upper Half of Fuselage)

Work Zones and Access Panels

Zone Access/Work location

200

Manpower Resources

Skills NON SPECIFIC

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 469

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References

Aircraft Maintenance Manual (AMM) Task 23-51-12-400-801

Task 23-71-34-400-801

Task 23-81-13-400-801

Task 25-11-51-400-801

Task 25-13-44-400-801

Task 25-13-44-400-802

Task 45-22-21-400-801

Task 52-10-00-410-801

(a) Make sure that the work areas are clean and clear of tools and other item of

equipment.

(b) In the cockpit, install the ceiling panels 211LC, 211MC, 212NC and the strips

211KC and 212CC (Refer to AMM Task 25-13-44-400-801).

(c) On the overhead panel, install and connect (if removed) :

- Reset C/B panel 262VU

- External View Camera Panel 272VU

- Reading Light Panel 252VU2

- AIREADOR panel

- Audio Control Panel (2RN3) (Refer to AMM Task 23-51-12-400-801)

- Data Loader Selector (101TD) (Refer to AMM Task 45-22-21-400-801)

- Cockpit Voice Recorder (CVR) Control Unit (1RK) (Refer to AMM Task

23-71-34-400-801)

- Radio Management Panel (1RG3) (Refer to AMM Task 23-81-13-400-801).

(d) Install the panel (211EW) (Refer to AMM Task 25-13-44-400-802).

(e) Install the captain seat (Refer to AMM Task 25-11-51-400-801).

(f) Close the FWD passenger/crew door(s) 831 or 841 (Refer to AMM Task

52-10-00-410-801).

(3) Subtask 265020-942-001-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 26-16-34-400-801

(a) Do the close-up procedure as specified in the installation of the SDCU (20WH)

(Refer to AMM Task 26-16-34-400-801).

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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(b) Remove the access platforms.

(c) Restore the systems and the aircraft to normal operating condition.

**CONF 003

(1) Subtask 265020-942-201-001 - Close-up

Work Zones and Access Panels

Zone Access/Work location

132 Access Panel 132PM, Panel 132NM, Panel 132RM

Work location from Frame 35 to Frame 37.1

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 21-20-00-410-801

25-52-00, Page Block 201

Task 25-52-00-400-801

Task 52-30-00-410-801

Task 52-30-00-410-802

(a) Make sure that the work areas are clean and clear of tools and other item of

equipment.

(b) In the FWD cargo-compartment, install the sidewall panels 131PM, 132NM and

132RM(Refer to AMM 25-52-00, Page Block 201).

(c) In the FWD cargo-compartment, install the partition panels 131AW, 131BW,

132CW and the ceiling panels 131BA, 131PA and 131NA(Refer to AMM Task

25-52-00-400-801).

(d) Close the avionics compartment door 132AZ.

(e) Close the FWD cargo-compartment door 821 (Refer to AMM Task

52-30-00-410-801 or AMM Task 52-30-00-410-802).

(f) Install the air-conditioning distribution ducts in the affected area (Refer to AMM

Task 21-20-00-410-801).

(2) Subtask 265020-410-002-001 - Install/Close Items Removed/Opened for access

(Upper Half of Fuselage)

Work Zones and Access Panels

Zone Access/Work location

200

Manpower Resources

Skills NON SPECIFIC

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 471

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SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) Task 23-51-12-400-801

Task 23-71-34-400-801

Task 23-81-13-400-801

Task 25-11-51-400-801

Task 25-13-44-400-801

Task 25-13-44-400-802

Task 45-22-21-400-801

Task 52-10-00-410-801

(a) Make sure that the work areas are clean and clear of tools and other item of

equipment.

(b) In the cockpit, install the ceiling panels 211LC, 211MC, 212NC and the strips

211KC and 212CC (Refer to AMM Task 25-13-44-400-801).

(c) On the overhead panel, install and connect (if removed) :

- Reset C/B panel 262VU

- External View Camera Panel 272VU

- Reading Light Panel 252VU2

- AIREADOR panel

- Audio Control Panel (2RN3) (Refer to AMM Task 23-51-12-400-801)

- Data Loader Selector (101TD) (Refer to AMM Task 45-22-21-400-801)

- Cockpit Voice Recorder (CVR) Control Unit (1RK) (Refer to AMM Task

23-71-34-400-801)

- Radio Management Panel (1RG3) (Refer to AMM Task 23-81-13-400-801).

(d) Install the panel (211EW) (Refer to AMM Task 25-13-44-400-802).

(e) Install the captain seat (Refer to AMM Task 25-11-51-400-801).

(f) Close the FWD passenger/crew door(s) 831 or 841 (Refer to AMM Task

52-10-00-410-801).

(3) Subtask 265020-942-001-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 26-16-34-400-801

(a) Do the close-up procedure as specified in the installation of the SDCU (20WH)

(Refer to AMM Task 26-16-34-400-801).

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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(b) Remove the access platforms.

(c) Restore the systems and the aircraft to normal operating condition.

**CONF 004

(1) Subtask 265020-942-201-001 - Close-up

Work Zones and Access Panels

Zone Access/Work location

132 Access Panel 132PM, Panel 132NM, Panel 132RM

Work location from Frame 35 to Frame 37.1

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 21-20-00-410-801

25-52-00, Page Block 201

Task 25-52-00-400-801

Task 52-30-00-410-801

Task 52-30-00-410-802

(a) Make sure that the work areas are clean and clear of tools and other item of

equipment.

(b) In the FWD cargo-compartment, install the sidewall panels 131PM, 132NM and

132RM(Refer to AMM 25-52-00, Page Block 201).

(c) In the FWD cargo-compartment, install the partition panels 131AW, 131BW,

132CW and the ceiling panels 131BA, 131PA and 131NA(Refer to AMM Task

25-52-00-400-801).

(d) Close the avionics compartment door 132AZ.

(e) Close the FWD cargo-compartment door 821 (Refer to AMM Task

52-30-00-410-801 or AMM Task 52-30-00-410-802).

(f) Install the air-conditioning distribution ducts in the affected area (Refer to AMM

Task 21-20-00-410-801).

(2) Subtask 265020-410-002-001 - Install/Close Items Removed/Opened for access

(Upper Half of Fuselage)

Work Zones and Access Panels

Zone Access/Work location

200

Manpower Resources

Skills NON SPECIFIC

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 473

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SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) Task 23-51-12-400-801

Task 23-71-34-400-801

Task 23-81-13-400-801

Task 25-11-51-400-801

Task 25-13-44-400-801

Task 25-13-44-400-802

Task 45-22-21-400-801

Task 52-10-00-410-801

(a) Make sure that the work areas are clean and clear of tools and other item of

equipment.

(b) In the cockpit, install the ceiling panels 211LC, 211MC, 212NC and the strips

211KC and 212CC (Refer to AMM Task 25-13-44-400-801).

(c) On the overhead panel, install and connect (if removed) :

- Reset C/B panel 262VU

- External View Camera Panel 272VU

- Reading Light Panel 252VU2

- AIREADOR panel

- Audio Control Panel (2RN3) (Refer to AMM Task 23-51-12-400-801)

- Data Loader Selector (101TD) (Refer to AMM Task 45-22-21-400-801)

- Cockpit Voice Recorder (CVR) Control Unit (1RK) (Refer to AMM Task

23-71-34-400-801)

- Radio Management Panel (1RG3) (Refer to AMM Task 23-81-13-400-801).

(d) Install the panel (211EW) (Refer to AMM Task 25-13-44-400-802).

(e) Install the captain seat (Refer to AMM Task 25-11-51-400-801).

(f) Close the FWD passenger/crew door(s) 831 or 841 (Refer to AMM Task

52-10-00-410-801).

(3) Subtask 265020-942-001-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 26-16-34-400-801

(a) Do the close-up procedure as specified in the installation of the SDCU (20WH)

(Refer to AMM Task 26-16-34-400-801).

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 474

6

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@A340-500/600

SERVICE BULLETIN

(b) Remove the access platforms.

(c) Restore the systems and the aircraft to normal operating condition.

**CONF 005

(1) Subtask 265020-942-201-001 - Close-up

Work Zones and Access Panels

Zone Access/Work location

132 Access Panel 132PM, Panel 132NM, Panel 132RM

Work location from Frame 35 to Frame 37.1

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 21-20-00-410-801

25-52-00, Page Block 201

Task 25-52-00-400-801

Task 52-30-00-410-801

Task 52-30-00-410-802

(a) Make sure that the work areas are clean and clear of tools and other item of

equipment.

(b) In the FWD cargo-compartment, install the sidewall panels 131PM, 132NM and

132RM(Refer to AMM 25-52-00, Page Block 201).

(c) In the FWD cargo-compartment, install the partition panels 131AW, 131BW,

132CW and the ceiling panels 131BA, 131PA and 131NA(Refer to AMM Task

25-52-00-400-801).

(d) Close the avionics compartment door 132AZ.

(e) Close the FWD cargo-compartment door 821 (Refer to AMM Task

52-30-00-410-801 or AMM Task 52-30-00-410-802).

(f) Install the air-conditioning distribution ducts in the affected area (Refer to AMM

Task 21-20-00-410-801).

(2) Subtask 265020-410-002-001 - Install/Close Items Removed/Opened for access

(Upper Half of Fuselage)

Work Zones and Access Panels

Zone Access/Work location

200

Manpower Resources

Skills NON SPECIFIC

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 475

6

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@A340-500/600

SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) Task 23-51-12-400-801

Task 23-71-34-400-801

Task 23-81-13-400-801

Task 25-11-51-400-801

Task 25-13-44-400-801

Task 25-13-44-400-802

Task 45-22-21-400-801

Task 52-10-00-410-801

(a) Make sure that the work areas are clean and clear of tools and other item of

equipment.

(b) In the cockpit, install the ceiling panels 211LC, 211MC, 212NC and the strips

211KC and 212CC (Refer to AMM Task 25-13-44-400-801).

(c) On the overhead panel, install and connect (if removed) :

- Reset C/B panel 262VU

- External View Camera Panel 272VU

- Reading Light Panel 252VU2

- AIREADOR panel

- Audio Control Panel (2RN3) (Refer to AMM Task 23-51-12-400-801)

- Data Loader Selector (101TD) (Refer to AMM Task 45-22-21-400-801)

- Cockpit Voice Recorder (CVR) Control Unit (1RK) (Refer to AMM Task

23-71-34-400-801)

- Radio Management Panel (1RG3) (Refer to AMM Task 23-81-13-400-801).

(d) Install the panel (211EW) (Refer to AMM Task 25-13-44-400-802).

(e) Install the captain seat (Refer to AMM Task 25-11-51-400-801).

(f) Close the FWD passenger/crew door(s) 831 or 841 (Refer to AMM Task

52-10-00-410-801).

(3) Subtask 265020-942-001-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 26-16-34-400-801

(a) Do the close-up procedure as specified in the installation of the SDCU (20WH)

(Refer to AMM Task 26-16-34-400-801).

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 476

6

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@A340-500/600

SERVICE BULLETIN

(b) Remove the access platforms.

(c) Restore the systems and the aircraft to normal operating condition.

**CONF 006

(1) Subtask 265020-942-201-001 - Close-up

Work Zones and Access Panels

Zone Access/Work location

132 Access Panel 132PM, Panel 132NM, Panel 132RM

Work location from Frame 35 to Frame 37.1

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 21-20-00-410-801

25-52-00, Page Block 201

Task 25-52-00-400-801

Task 52-30-00-410-801

Task 52-30-00-410-802

(a) Make sure that the work areas are clean and clear of tools and other item of

equipment.

(b) In the FWD cargo-compartment, install the sidewall panels 131PM, 132NM and

132RM(Refer to AMM 25-52-00, Page Block 201).

(c) In the FWD cargo-compartment, install the partition panels 131AW, 131BW,

132CW and the ceiling panels 131BA, 131PA and 131NA(Refer to AMM Task

25-52-00-400-801).

(d) Close the avionics compartment door 132AZ.

(e) Close the FWD cargo-compartment door 821 (Refer to AMM Task

52-30-00-410-801 or AMM Task 52-30-00-410-802).

(f) Install the air-conditioning distribution ducts in the affected area (Refer to AMM

Task 21-20-00-410-801).

(2) Subtask 265020-410-002-001 - Install/Close Items Removed/Opened for access

(Upper Half of Fuselage)

Work Zones and Access Panels

Zone Access/Work location

200

Manpower Resources

Skills NON SPECIFIC

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 477

6

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@A340-500/600

SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) Task 23-51-12-400-801

Task 23-71-34-400-801

Task 23-81-13-400-801

Task 25-11-51-400-801

Task 25-13-44-400-801

Task 25-13-44-400-802

Task 45-22-21-400-801

Task 52-10-00-410-801

(a) Make sure that the work areas are clean and clear of tools and other item of

equipment.

(b) In the cockpit, install the ceiling panels 211LC, 211MC, 212NC and the strips

211KC and 212CC (Refer to AMM Task 25-13-44-400-801).

(c) On the overhead panel, install and connect (if removed) :

- Reset C/B panel 262VU

- External View Camera Panel 272VU

- Reading Light Panel 252VU2

- AIREADOR panel

- Audio Control Panel (2RN3) (Refer to AMM Task 23-51-12-400-801)

- Data Loader Selector (101TD) (Refer to AMM Task 45-22-21-400-801)

- Cockpit Voice Recorder (CVR) Control Unit (1RK) (Refer to AMM Task

23-71-34-400-801)

- Radio Management Panel (1RG3) (Refer to AMM Task 23-81-13-400-801).

(d) Install the panel (211EW) (Refer to AMM Task 25-13-44-400-802).

(e) Install the captain seat (Refer to AMM Task 25-11-51-400-801).

(f) Close the FWD passenger/crew door(s) 831 or 841 (Refer to AMM Task

52-10-00-410-801).

(3) Subtask 265020-942-001-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 26-16-34-400-801

(a) Do the close-up procedure as specified in the installation of the SDCU (20WH)

(Refer to AMM Task 26-16-34-400-801).

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 478

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

(b) Remove the access platforms.

(c) Restore the systems and the aircraft to normal operating condition.

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 479

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF ALL

800VU

710VU

752VU

1LP9

2044VC

FR2

FR1

FR14

FR18

FR20

2M

1M

751VU

740VU

212VU

FR10.A

2016VC

F_SB_265020_5_BAAA_01_01

Figure A-FBAAA - Sheet 01

Location of the Working Areas

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 480

6

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@A340-500/600

SERVICE BULLETIN

**CONF ALL

BEFORE

(8 POS.)

(7 POS.)

212VU

D

C

B

A

(10)

NOTE:

ONLY ONE CONFIGURATION SHOWN.

EQUIPMENT IN THE PANEL 212VU MAY

DIFFER DEPENDING ON AIRCRAFT CONFIGURATION.

ELECTRICAL BONDING

(1)

(11)

(2)

F_SB_265020_5_BBAA_01_02

A

Figure A-FBBAA - Sheet 01

Modification of the Equipment in the RH Overhead Panel 212VU

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 481

6

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@A340-500/600

SERVICE BULLETIN

**CONF ALL

F_SB_265020_5_BBAA_02_00

7

6

(7)

(6)

582VT

5WX

(5)

(4)

(3)

B

C

4

1

Figure A-FBBAA - Sheet 02

Modification of the Equipment in the RH Overhead Panel 212VU

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 482

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF ALL

AFTER

(8 POS.)

(7 POS.)

212VU

NOTE:

ONLY ONE CONFIGURATION SHOWN.

EQUIPMENT IN THE PANEL 212VU MAY

DIFFER DEPENDING ON AIRCRAFT CONFIGURATION.

ELECTRICAL BONDING

(11)

10 1

2

D

F_SB_265020_5_BBAA_03_01

Figure A-FBBAA - Sheet 03

Modification of the Equipment in the RH Overhead Panel 212VU

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 483

6

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@A340-500/600

SERVICE BULLETIN

**CONF ALL

FR7

FR10

Z121

740VU

703VT

(7)

A

B

A

B

F_SB_265020_5_BCAA_01_00

20

Figure A-FBCAA - Sheet 01

Modification of the Equipment in the Emergency Power Center 740VU

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 484

6

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@A340-500/600

SERVICE BULLETIN

**CONF ALL

1712VT

1713VT

B

B

FR17

FR16A

Z121 Z122 − 

710VU

A

(7)

F_SB_265020_5_BDAA_01_01

A

17

Figure A-FBDAA - Sheet 01

Modification of the Equipment in the AC/DC Main Power Center 710VU

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 485

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF ALL

F_SB_265020_5_BEAA_01_00

FR14

FR15A

751VU

B

B

10WX

11WX

(9)

(8)

C

93

89

C

E

A

A

FWD

F_SB_265020_5_BEAA_01_00

Figure A-FBEAA - Sheet 01

Modification of the Equipment in the LH Relay Box 751VU

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 486

6

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@A340-500/600

SERVICE BULLETIN

**CONF ALL

FR14

FR15A

B

B

(9)

(8)

C

A

3733

12WX

13WX

752VU

A

FWD

F_SB_265020_5_BFAA_01_00

C B

Figure A-FBFAA - Sheet 01

Modification of the Equipment in the RH Relay Box 752VU

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 487

6

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@A340-500/600

SERVICE BULLETIN

**CONF ALL

A

B

800VU

2900VT

7

(7)

B

A

FR20

FR18

Z122

50

F_SB_265020_5_BGAA_01_00

Figure A-FBGAA - Sheet 01

Modification of the Equipment in the Main Rack 800VU

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 488

6

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@A340-500/600

SERVICE BULLETIN

**CONF ALL

Figure A-FCAAA - Sheet 01

Modification of the Wiring in the RH Overhead Panel 212VU

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 489

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF ALL

Figure A-FCAAA - Sheet 02

Modification of the Wiring in the RH Overhead Panel 212VU

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 490

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF ALL

Figure A-FCAAA - Sheet 03

Modification of the Wiring in the RH Overhead Panel 212VU

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 491

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF ALL

END1 LEAD END2

Instructions Zone or

Panel Elec.Ident. Term Terminal P/N

Wire

Ident. Co Rte Gauge

Lenght

mm Inch

Zone or

Panel Elec.Ident. Term Terminal P/N

L

i

n

e

 1 212VU 580VT 5R 2623−0005 1M BF22 212VU 582VC <I D

 2 212VU 580VT 5S 2623−0008 1M BF22 212VU 4WX−A A1 D

 3 212VU 580VT 5T 2623−0012 1M BF22 212VU 4WX−A C1 D

 4 212VU 580VT 1A 2623−0032 1M BF22 212VU 6WX−A A1 D

 5 212VU 580VT 1H 2623−0036 1M BF22 212VU 6WX−A C1 D

 6 212VU 580VT 8T 2623−0066 1M BF22 212VU 4WX−A 6 D

 7 212VU 580VT 1R 2623−0128 1M BF22 212VU 580VC J D

 8 212VU 5WX−A 8 2623−0068 1M BF22 212VU 3WX−A 6 D

 9 212VU 5WX−A 7 2623−0118 1M BF22 212VU 580VC <Y D

10 212VU 5WX−A 9 2623−0144 1M BF22 212VU 6WX−A 8 D

11 212VU 584VC <T 2623−0115 2M BF22 212VU 13WH 1G D

12 212VU 584VC <S 2623−0123 2M BF22 212VU 13WH 2G D

13 212VU 584VC <U 2623−0129 2M BF22 212VU 582VT 3Y D

14

15

16

17 212VU 582VT 3T 2623−0006 2M BF22 212VU 584VC <J M1O

18 212VU 582VT 2H EN3155−016M2222 2623−0006 2M BF22 212VU 584VC <J M1N

19 212VU 582VT 3R 2623−0010 2M BF22 212VU 4WX−A B1 M1O

20 212VU 582VT 2M EN3155−016M2222 2623−0010 2M BF22 212VU 4WX−A B1 M1N

21 212VU 582VT 3S 2623−0014 2M BF22 212VU 4WX−A D1 M1O

22 212VU 582VT 2L EN3155−016M2222 2623−0014 2M BF22 212VU 4WX−A D1 M1N

23 212VU 582VT 3G 2623−0034 2M BF22 212VU 6WX−A B1 M1O

24 212VU 582VT 2J EN3155−016M2222 2623−0034 2M BF22 212VU 6WX−A B1 M1N

25

 M1O = OLD HOOK−UP ON END 1

 M1N = NEW HOOK−UP ON END 1

 D = DELETED WIRE

Figure A-FCAAA - Sheet 04

Modification of the Wiring in the RH Overhead Panel 212VU

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 492

6

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@A340-500/600

SERVICE BULLETIN

**CONF ALL

END1 LEAD END2

Instructions Zone or

Panel Elec.Ident. Term Terminal P/N

Wire

Ident. Co Rte Gauge

Lenght

mm Inch

Zone or

Panel Elec.Ident. Term Terminal P/N

L

i

n

e

 1 212VU 582VT 3P 2623−0038 2M BF22 212VU 6WX−A D1 M1O

 2 212VU 582VT 2K EN3155−016M2222 2623−0038 2M BF22 212VU 6WX−A D1 M1N

 3

 4

 5

 6 212VU 580VT 3A EN3155−016M2222 2623−0005 1M BF22 1000 40 212VU 582VC <I EN3155−018M2018 (a) A

 7 212VU 580VT 3D EN3155−016M2222 2623−0008 1M BF22 1000 40 212VU 4WX−A A1 EN3155−003F2222 (a) A

 8 212VU 580VT 3E EN3155−016M2222 2623−0012 1M BF22 1000 40 212VU 4WX−A C1 EN3155−003F2222 (a) A

 9 212VU 580VT 3B EN3155−016M2222 2623−0032 1M BF22 1000 40 212VU 6WX−A A1 EN3155−003F2222 (a) A

10 212VU 580VT 3C EN3155−016M2222 2623−0036 1M BF22 1000 40 212VU 6WX−A C1 EN3155−003F2222 (a) A

11 212VU 4WX−A 6 EN3155−003F2222 2623−0066 1M BF22 1000 40 212VU 3WX−A 8 EN3155−003F2222 (a) A

12 212VU 6WX−A 8 EN3155−003F2222 2623−0068 1M BF22 1000 40 212VU 3WX−A 6 EN3155−003F2222 (a) A

13

14

15

16

17

18

19

20

21

22

23

24

25

 (a) = BUNDLE F9000095226495 M1N = NEW HOOK−UP ON END 1

 A = ADDED WIRE

 M1O = OLD HOOK−UP ON END 1

Figure A-FCAAA - Sheet 05

Modification of the Wiring in the RH Overhead Panel 212VU

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 493

6

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@A340-500/600

SERVICE BULLETIN

**CONF ALL

Figure A-FCBAA - Sheet 01

Modification of the Wiring in the Emergency Power Center 740VU

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 494

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF ALL

END1 LEAD END2

Instructions Zone or

Panel Elec.Ident. Term Terminal P/N

Wire

Ident. Co Rte Gauge

Lenght

mm Inch

Zone or

Panel Elec.Ident. Term Terminal P/N

L

i

n

e

 1 740VU 703VT 20B 2623−0124 1M DK20 740VU 1037VC 4 D

 2 740VU 703VT 20F 2623−0136 1M DK20 740VU 1007VC 21 D

 3 740VU 703VT 20C 2623−0149 1M DK20 740VU 1037VC 5 D

 4 740VU 703VT 20E 2623−0150 1M DK20 740VU 1037VC 6 D

 5 740VU 703VT 20H 2623−0179 1M DK20 740VU 1037VC 7 D

 6 740VU 703VT 20J 2623−0180 1M DK20 740VU 1037VC 8 D

 7 740VU 703VT 20G 2623−0001 1M DK20 742VU 1WX 2 D

 8 740VU 703VT 20D 2623−0145 1M DK20 742VU 1WX 2 D

 9

10

11

12 740VU 1007VC 21 EN3155−015F2018 2623−0001 1M DK20 3000 120 742VU 1WX 2 NSA936501TA2003 (a) A

13

14

15

16

17

18

19

20

21

22

23

24

25

 (a) = BUNDLE F9000095226495

 A = ADDED WIRE

 D = DELETED WIRE

Figure A-FCBAA - Sheet 02

Modification of the Wiring in the Emergency Power Center 740VU

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 495

6

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@A340-500/600

SERVICE BULLETIN

**CONF ALL

Figure A-FCCAA - Sheet 01

Modification of the Wiring in the AC/DC Main Power Center 710VU

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 496

6

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@A340-500/600

SERVICE BULLETIN

**CONF ALL

END1 LEAD END2

Instructions Zone or

Panel Elec.Ident. Term Terminal P/N

Wire

Ident. Co Rte Gauge

Lenght

mm Inch

Zone or

Panel Elec.Ident. Term Terminal P/N

L

i

n

e

 1 715VU 1712VT 17B 2623−0125 2M DK20 715VU 1728VC 16 D

 2 715VU 1712VT 17F 2623−0137 2M DK20 715VU 1704VC 21 D

 3 715VU 1712VT 17C 2623−0151 2M DK20 715VU 1728VC 17 D

 4 715VU 1712VT 17E 2623−0152 2M DK20 715VU 1728VC 18 D

 5 715VU 1712VT 17H 2623−0181 2M DK20 715VU 1728VC 19 D

 6 715VU 1712VT 17J 2623−0182 2M DK20 715VU 1728VC 20 D

 7 715VU 1712VT 17G 2623−0002 2M DK20 722VU 2WX 2 D

 8 715VU 1712VT 17D 2623−0146 2M DK20 722VU 2WX 2 D

 9

10

11

12 715VU 1704VC 21 EN3155−015F2018 2623−0002 2M DK20 5000 200 722VU 2WX 2 NSA936501TA2003 (a) A

13

14

15

16

17

18

19

20

21

22

23

24

25

 (a) = BUNDLE F9000095226495

 A = ADDED WIRE

 D = DELETED WIRE

Figure A-FCCAA - Sheet 02

Modification of the Wiring in the AC/DC Main Power Center 710VU

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 497

6

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@A340-500/600

SERVICE BULLETIN

**CONF ALL

Figure A-FCDAA - Sheet 01

Modification of the Wiring in the LH Relay Box 751VU

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 498

6

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@A340-500/600

SERVICE BULLETIN

**CONF ALL

END1 LEAD END2

Instructions Zone or

Panel Elec.Ident. Term Terminal P/N

Wire

Ident. Co Rte Gauge

Lenght

mm Inch

Zone or

Panel Elec.Ident. Term Terminal P/N

L

i

n

e

 1 751VU 1449VC 15 2623−0133 1M DK20 751VU 11WX−A X1 D

 2 751VU 1449VC 16 2623−0141 1M DK20 751VU 10WX−A X1 D

 3 751VU 1449VC 7 2623−0169 1M DK20 751VU 10WX−A B2 D

 4 751VU 1449VC 8 2623−0170 1M DK20 751VU 10WX−A A2 D

 5 751VU 1449VC 9 2623−0175 1M DK20 751VU 10WX−A A1 D

 6 751VU 1449VC 10 2623−0176 1M DK20 751VU 10WX−A B1 D

 7 751VU 1449VC 11 2623−0199 1M DK20 751VU 11WX−A B2 D

 8 751VU 1449VC 12 2623−0200 1M DK20 751VU 11WX−A A2 D

 9 751VU 1449VC 13 2623−0205 1M DK20 751VU 11WX−A A1 D

10 751VU 1449VC 14 2623−0206 1M DK20 751VU 11WX−A B1 D

11 751VU 10WX−A X2 2623−0139 1M DK20 751VU 1541VG GND D

12 751VU 11WX−A X2 2623−0131 1M DK20 751VU 1541VG GND D

13

14

15

16

17

18

19

20

21

22

23

24

25

 D = DELETED WIRE

 GND = GROUND

Figure A-FCDAA - Sheet 02

Modification of the Wiring in the LH Relay Box 751VU

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 499

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF ALL

Figure A-FCEAA - Sheet 01

Modification of the Wiring in the RH Relay Box 752VU

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 500

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF ALL

END1 LEAD END2

Instructions Zone or

Panel Elec.Ident. Term Terminal P/N

Wire

Ident. Co Rte Gauge

Lenght

mm Inch

Zone or

Panel Elec.Ident. Term Terminal P/N

L

i

n

e

 1 752VU 1518VC 44 2623−0132 2M DK20 752VU 13WX−A X1 D

 2 752VU 1518VC 43 2623−0140 2M DK20 752VU 12WX−A X1 D

 3 752VU 1518VC 35 2623−0171 2M DK20 752VU 12WX−A B2 D

 4 752VU 1518VC 36 2623−0172 2M DK20 752VU 12WX−A A2 D

 5 752VU 1518VC 37 2623−0173 2M DK20 752VU 12WX−A A1 D

 6 752VU 1518VC 38 2623−0174 2M DK20 752VU 12WX−A B1 D

 7 752VU 1518VC 39 2623−0201 2M DK20 752VU 13WX−A B2 D

 8 752VU 1518VC 40 2623−0202 2M DK20 752VU 13WX−A A2 D

 9 752VU 1518VC 41 2623−0203 2M DK20 752VU 13WX−A A1 D

10 752VU 1518VC 42 2623−0204 2M DK20 752VU 13WX−A B1 D

11 752VU 12WX−A X2 2623−0138 2M DK20 752VU 1414VG GND D

12 752VU 13WX−A X2 2623−0130 2M DK20 752VU 1414VG GND D

13

14

15

16

17

18

19

20

21

22

23

24

25

 D = DELETED WIRE

 GND = GROUND

Figure A-FCEAA - Sheet 02

Modification of the Wiring in the RH Relay Box 752VU

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 501

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF ALL

Figure A-FCFAA - Sheet 01

Modification of the Wiring in the Main Rack 800VU

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 502

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF ALL

Figure A-FCFAA - Sheet 02

Modification of the Wiring in the Main Rack 800VU

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 503

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF ALL

Figure A-FCFAA - Sheet 03

Modification of the Wiring in the Main Rack 800VU

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 504

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF ALL

Figure A-FCFAA - Sheet 04

Modification of the Wiring in the Main Rack 800VU

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 505

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF ALL

END1 LEAD END2

Instructions Zone or

Panel Elec.Ident. Term Terminal P/N

Wire

Ident. Co Rte Gauge

Lenght

mm Inch

Zone or

Panel Elec.Ident. Term Terminal P/N

L

i

n

e

 1 852VU 2900VT 50F 2623−0147 2M CF22 852VU 20WH−AB 12B D

 2 852VU 2900VT 47J 2623−0148 1M CF22 852VU 20WH−AA 5A D

 3 852VU 2900VT 50D 2623−0177 2M CF22 852VU 20WH−AB 12C D

 4 852VU 2900VT 50H 2623−0178 1M CF22 852VU 20WH−AA 5B D

 5 852VU 2900VT 47D 2623−0207 2M CF22 852VU 20WH−AB 12F D

 6 852VU 2900VT 52G 2623−0208 1M CF22 852VU 20WH−AA 5E D

 7 852VU 2900VT 98B 2623−0209 2M CF22 852VU 20WH−AB 12G D

 8 852VU 2900VT C 2623−0210 1M CF22 852VU 20WH−AA 5F D

 9 852VU 2900VT 47C 2623−0153 2M CF20 802VU 2614VC 37 D

10 852VU 2900VT 50B 2623−0154 2M CF20 802VU 2614VC 6 D

11 852VU 2900VT 52B 2623−0155 1M CF20 801VU 2629VC 44 D

12 852VU 2900VT 47H 2623−0156 1M CF20 801VU 2629VC 48 D

13 852VU 2900VT 47E 2623−0157 2M CF20 802VU 2508VC 46 D

14 852VU 2900VT 50G 2623−0158 2M CF20 802VU 2636VC 40 D

15 852VU 2900VT 52F 2623−0159 1M CF20 801VU 2511VC 36 D

16 852VU 2900VT 47K 2623−0160 1M CF20 801VU 2625VC 3 D

17 852VU 2900VT 98A 2623−0183 2M CF20 802VU 2614VC 38 D

18 852VU 2900VT 50C 2623−0184 2M CF20 802VU 2614VC 28 D

19 852VU 2900VT D 2623−0185 1M CF20 801VU 2629VC 46 D

20 852VU 2900VT 50J 2623−0186 1M CF20 801VU 2629VC 49 D

21 852VU 2900VT 98F 2623−0187 2M CF20 802VU 2508VC 47 D

22 852VU 2900VT 50E 2623−0188 2M CF20 802VU 2636VC 41 D

23 852VU 2900VT E 2623−0189 1M CF20 801VU 2511VC 38 D

24 852VU 2900VT 50K 2623−0190 1M CF20 801VU 2625VC 4 D

25 852VU 20WH−AA 3A 2623−0119 1M CF22 801VU 2539VC 47 D

 D = DELETED WIRE

Figure A-FCFAA - Sheet 05

Modification of the Wiring in the Main Rack 800VU

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 506

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF ALL

END1 LEAD END2

Instructions Zone or

Panel Elec.Ident. Term Terminal P/N

Wire

Ident. Co Rte Gauge

Lenght

mm Inch

Zone or

Panel Elec.Ident. Term Terminal P/N

L

i

n

e

 1 852VU 20WH−AA 3B 2623−0120 1M CF22 801VU 2539VC 48 D

 2 852VU 20WH−AB 13E 2623−0113 2M CF22 802VU 2618VC 31 D

 3 852VU 20WH−AB 1D 2623−0121 1M CF22 801VU 2629VC 23 D

 4

 5

 6

 7 852VU 2900VT 52A EN3155−016M2018 2623−0016 1M CF22 1000 40 852VU 20WH−AA 5E E0170FA2200 (a) A

 8 852VU 2900VT 47C EN3155−016M2018 2623−0018 2M CF22 1000 40 852VU 20WH−AB 12F E0170FA2200 (a) A

 9 852VU 2900VT E EN3155−016M2018 2623−0044 1M CF22 550 22 852VU 20WH−AA 5F E0170FA2200 (a) A

10 852VU 2900VT 98A EN3155−016M2018 2623−0046 2M CF22 1000 40 852VU 20WH−AB 12G E0170FA2200 (a) A

11 852VU 2900VT 52F EN3155−016M2018 2623−0092 1M CF20 3000 120 801VU 2629VC 44 EN3155−008M1614 (a) A

12 852VU 2900VT 47D EN3155−016M2018 2623−0094 2M CF20 1500 60 802VU 2614VC 37 EN3155−014M2018 (a) A

13 852VU 2900VT 52B EN3155−016M2018 2623−0096 1M CF20 4500 180 801VU 2511VC 36 EN3155−014M2018 (a) A

14 852VU 2900VT 47E EN3155−016M2018 2623−0098 2M CF20 3000 120 802VU 2508VC 46 EN3155−008M1614 (a) A

15 852VU 2900VT D EN3155−016M2018 2623−0100 1M CF20 3520 141 801VU 2511VC 38 EN3155−014M2018 (a) A

16 852VU 2900VT C EN3155−016M2018 2623−0102 1M CF20 2550 102 801VU 2629VC 46 EN3155−008M1614 (a) A

17 852VU 2900VT 98B EN3155−016M2018 2623−0104 2M CF20 1000 40 802VU 2614VC 38 EN3155−014M2018 (a) A

18 852VU 2900VT 98F EN3155−016M2018 2623−0106 2M CF20 2000 80 802VU 2508VC 47 EN3155−008M1614 (a) A

19

20

21

22

23

24

25

 (a) = BUNDLE F9000095226495

 A = ADDED WIRE

 D = DELETED WIRE

Figure A-FCFAA - Sheet 06

Modification of the Wiring in the Main Rack 800VU

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 507

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF ALL

Figure A-FCGAA - Sheet 01

Modification of the Pin Programming in the Main Rack 800VU

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 508

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF ALL

END1 LEAD END2

Instructions Zone or

Panel Elec.Ident. Term Terminal P/N

Wire

Ident. Co Rte Gauge

Lenght

mm Inch

Zone or

Panel Elec.Ident. Term Terminal P/N

L

i

n

e

 1 809VU 3027VC−A 64 2616−0170 1M CF24 852VU 20WH−AA 6G M1O

 2 809VU 3029VC−A 64 EN3155−003F2222 2616−0170 1M CF24 852VU 20WH−AA 6G M1N

 3 809VU 3027VC−A 40 2616−0267 1M CF24 852VU 20WH−AA 6J M1O

 4 809VU 3029VC−A 40 EN3155−003F2222 2616−0267 1M CF24 852VU 20WH−AA 6J M1N

 5

 6

 7

 8

 9

10

11

12

13

14

15

16

17

18

19

20

21

22

23

24

25

 M1O = OLD HOOK−UP ON END 1

 M1N = NEW HOOK−UP ON END 1

Figure A-FCGAA - Sheet 02

Modification of the Pin Programming in the Main Rack 800VU

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 509

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF ALL

Figure A-FCHAA - Sheet 01

Modification of the Wiring between the Main Rack Shelf 801VU and the LH Relay Box 751VU

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 510

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF ALL

END1 LEAD END2

Instructions Zone or

Panel Elec.Ident. Term Terminal P/N

Wire

Ident. Co Rte Gauge

Lenght

mm Inch

Zone or

Panel Elec.Ident. Term Terminal P/N

L

i

n

e

 1 801VU 2629VC−A 44 2623−0167 1M CF20 751VU 1449VC−A 9 M1O+M2O

 2 801VU 2629VC−A WS NSA936604CA0931 2623−0167 1M CF20 751VU 1449VC−A WS NSA936604CA0931 M1N+M2N

 3 801VU 2629VC−A 48 2623−0168 1M CF20 751VU 1449VC−A 10 M1O+M2O

 4 801VU 2629VC−A WS NSA936604CA0931 2623−0168 1M CF20 751VU 1449VC−A WS NSA936604CA0931 M1N+M2N

 5 801VU 2629VC−A 46 2623−0197 1M CF20 751VU 1449VC−A 13 M1O+M2O

 6 801VU 2629VC−A WS NSA936604CA0931 2623−0197 1M CF20 751VU 1449VC−A WS NSA936604CA0931 M1N+M2N

 7 801VU 2629VC−A 49 2623−0198 1M CF20 751VU 1449VC−A 14 M1O+M2O

 8 801VU 2629VC−A WS NSA936604CA0931 2623−0198 1M CF20 751VU 1449VC−A WS NSA936604CA0931 M1N+M2N

 9

10

11

12

13

14

15

16

17

18

19

20

21

22

23

24

25

 M1O+M2O= OLD HOOK−UP ON END 1 AND 2

 M1N+M2N= NEW HOOK−UP ON END 1 AND 2

 WS = WIRE STOWED

Figure A-FCHAA - Sheet 02

Modification of the Wiring between the Main Rack Shelf 801VU and the LH Relay Box 751VU

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 511

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF ALL

Figure A-FCJAA - Sheet 01

Modification of the Wiring between the Main Rack Shelf 802VU and the RH Relay Box 752VU

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 512

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF ALL

END1 LEAD END2

Instructions Zone or

Panel Elec.Ident. Term Terminal P/N

Wire

Ident. Co Rte Gauge

Lenght

mm Inch

Zone or

Panel Elec.Ident. Term Terminal P/N

L

i

n

e

 1 752VU 1518VC−A 37 2623−0165 2M CF20 802VU 2614VC−A 37 D

 2 752VU 1518VC−A 38 2623−0166 2M CF20 802VU 2614VC−A 6 D

 3 752VU 1518VC−A 41 2623−0195 2M CF20 802VU 2614VC−A 38 D

 4 752VU 1518VC−A 42 2623−0196 2M CF20 802VU 2614VC−A 28 D

 5

 6

 7

 8

 9

10

11

12

13

14

15

16

17

18

19

20

21

22

23

24

25

 D = DELETED WIRE

Figure A-FCJAA - Sheet 02

Modification of the Wiring between the Main Rack Shelf 802VU and the RH Relay Box 752VU

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 513

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF ALL

Figure A-FCKAA - Sheet 01

Modification of the Wiring between the Emergency Power Center 740VU and the LH Relay Box 751VU

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 514

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF ALL

END1 LEAD END2

Instructions Zone or

Panel Elec.Ident. Term Terminal P/N

Wire

Ident. Co Rte Gauge

Lenght

mm Inch

Zone or

Panel Elec.Ident. Term Terminal P/N

L

i

n

e

 1 740VU 1037VC−A 5 2623−0161 1M CF20 751VU 1449VC−A 7 D

 2 740VU 1037VC−A 6 2623−0162 1M CF20 751VU 1449VC−A 8 D

 3 740VU 1037VC−A 7 2623−0191 1M CF20 751VU 1449VC−A 11 D

 4 740VU 1037VC−A 8 2623−0192 1M CF20 751VU 1449VC−A 12 D

 5

 6

 7

 8

 9

10

11

12

13

14

15

16

17

18

19

20

21

22

23

24

25

 D = DELETED WIRE

Figure A-FCKAA - Sheet 02

Modification of the Wiring between the Emergency Power Center 740VU and the LH Relay Box

751VU

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 515

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF ALL

Figure A-FCLAA - Sheet 01

Modification of the Wiring between the AC/DC Main Power Center 715VU and the RH Relay Box

752VU

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 516

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF ALL

END1 LEAD END2

Instructions Zone or

Panel Elec.Ident. Term Terminal P/N

Wire

Ident. Co Rte Gauge

Lenght

mm Inch

Zone or

Panel Elec.Ident. Term Terminal P/N

L

i

n

e

 1 715VU 1728VC−A 17 2623−0163 2M CF20 752VU 1518VC−A 35 D

 2 715VU 1728VC−A 18 2623−0164 2M CF20 752VU 1518VC−A 36 D

 3 715VU 1728VC−A 19 2623−0193 2M CF20 752VU 1518VC−A 39 D

 4 715VU 1728VC−A 20 2623−0194 2M CF20 752VU 1518VC−A 40 D

 5

 6

 7

 8

 9

10

11

12

13

14

15

16

17

18

19

20

21

22

23

24

25

 D = DELETED WIRE

Figure A-FCLAA - Sheet 02

Modification of the Wiring between the AC/DC Main Power Center 715VU and the RH Relay Box

752VU

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 517

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF ALL

Figure A-FCMAA - Sheet 01

Modification of the Wiring between the Main Rack Shelf 801VU and the Avionics Compartment at FR2

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 518

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF ALL

END1 LEAD END2

Instructions Zone or

Panel Elec.Ident. Term Terminal P/N

Wire

Ident. Co Rte Gauge

Lenght

mm Inch

Zone or

Panel Elec.Ident. Term Terminal P/N

L

i

n

e

 1 801VU 2629VC−A 23 2623−0122 1M CF20 211 1LP9−A 39 M1O+M2O

 2 801VU 2629VC−A WS NSA936604CA0931 2623−0122 1M CF20 211 1LP9−A WS NSA936604CA0931 M1N+M2N

 3

 4

 5

 6

 7

 8

 9

10

11

12

13

14

15

16

17

18

19

20

21

22

23

24

25

 M1O+M2O= OLD HOOK−UP ON END 1 AND 2

 M1N+M2N= NEW HOOK−UP ON END 1 AND 2

 WS = WIRE STOWED

Figure A-FCMAA - Sheet 02

Modification of the Wiring between the Main Rack Shelf 801VU and the Avionics Compartment

at FR2

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 519

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF ALL

Figure A-FCNAA - Sheet 01

Modification of the Wiring between the RH Overhead Panel 212VU and the Avionics Compartment (LH

Side)

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 520

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF ALL

Figure A-FCNAA - Sheet 02

Modification of the Wiring between the RH Overhead Panel 212VU and the Avionics Compartment (LH

Side)

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 521

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF ALL

END1 LEAD END2

Instructions Zone or

Panel Elec.Ident. Term Terminal P/N

Wire

Ident. Co Rte Gauge

Lenght

mm Inch

Zone or

Panel Elec.Ident. Term Terminal P/N

L

i

n

e

 1 212VU 580VC−A <Y 2623−0117 1M CF22 211 1LP9−A 10 M1O+M2O

 2 212VU 580VC−A WS NSA936604CA0931 2623−0117 1M CF22 211 1LP9−A WS NSA936604CA0931 M1N+M2N

 3 212VU 580VC−A J 2623−0126 1M CF20 740VU 1037VC−A 4 M1O+M2O

 4 212VU 580VC−A WS NSA936604CA0931 2623−0126 1M CF20 740VU 1037VC−A WS NSA936604CA0931 M1N+M2N

 5 212VU 582VC−A V 2623−0135 1M CF20 751VU 1449VC−A 15 M1O+M2O

 6 212VU 582VC−A WS NSA936604CA0931 2623−0135 1M CF20 751VU 1449VC−A WS NSA936604CA0931 M1N+M2N

 7 212VU 582VC−A <H 2623−0143 1M CF20 751VU 1449VC−A 16 M1O+M2O

 8 212VU 582VC−A WS NSA936604CA0931 2623−0143 1M CF20 751VU 1449VC−A WS NSA936604CA0931 M1N+M2N

 9

10

11

12 212VU 582VC−A <H EN3155−019F2018 2623−0088 1M CF20 17000 680 801VU 2629VC−A 44 EN3155−003F1614 (a) A

13 212VU 582VC−A V EN3155−019F2018 2623−0108 1M CF20 17000 680 801VU 2629VC−A 46 EN3155−003F1614 (a) A

14

15

16

17

18

19

20

21

22

23

24

25

 (a) = BUNDLE F9000095226495 M1N+M2N= NEW HOOK−UP ON END 1 AND 2

 A = ADDED WIRE WS = WIRE STOWED

 M1O+M2O= OLD HOOK−UP ON END 1 AND 2

Figure A-FCNAA - Sheet 03

Modification of the Wiring between the RH Overhead Panel 212VU and the Avionics

Compartment (LH Side)

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 522

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF ALL

Figure A-FCPAA - Sheet 01

Modification of the Wiring between the RH Overhead Panel 212VU and the Avionics Compartment (RH

Side)

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 523

6

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@A340-500/600

SERVICE BULLETIN

**CONF ALL

Figure A-FCPAA - Sheet 02

Modification of the Wiring between the RH Overhead Panel 212VU and the Avionics Compartment (RH

Side)

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 524

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF ALL

END1 LEAD END2

Instructions Zone or

Panel Elec.Ident. Term Terminal P/N

Wire

Ident. Co Rte Gauge

Lenght

mm Inch

Zone or

Panel Elec.Ident. Term Terminal P/N

L

i

n

e

 1 212VU 584VC−A <K 2623−0077 2M CF20 132 2016VC−A 17 M2O

 2 212VU 584VC−A <K 2623−0077 2M CF20 132 2044VC−A 18 EN3155−015F2018 M2N

 3 212VU 584VC−A <S 2623−0114 2M CF20 802VU 2618VC−A 31 M1O+M2O

 4 212VU 584VC−A WS NSA936604CA0931 2623−0114 2M CF20 802VU 2618VC−A WS NSA936604CA0931 M1N+M2N

 5 212VU 584VC−A <T 2623−0116 2M CF20 132 2044VC−A 18 M1O+M2O

 6 212VU 584VC−A WS NSA936604CA0931 2623−0116 2M CF20 132 2044VC−A WS NSA936604CA0931 M1N+M2N

 7 212VU 584VC−A <U 2623−0127 2M CF20 715VU 1728VC−A 16 M1O+M2O

 8 212VU 584VC−A WS NSA936604CA0931 2623−0127 2M CF20 715VU 1728VC−A WS NSA936604CA0931 M1N+M2N

 9 212VU 584VC−A <B 2623−0134 2M CF20 752VU 1518VC−A 44 M1O+M2O

10 212VU 584VC−A WS NSA936604CA0931 2623−0134 2M CF20 752VU 1518VC−A WS NSA936604CA0931 M1N+M2N

11 212VU 584VC−A <G 2623−0142 2M CF20 752VU 1518VC−A 43 M1O+M2O

12 212VU 584VC−A WS NSA936604CA0931 2623−0142 2M CF20 752VU 1518VC−A WS NSA936604CA0931 M1N+M2N

13

14

15

16 212VU 584VC−A <G EN3155−019F2018 2623−0090 2M CF20 15500 620 802VU 2614VC−A 37 EN3155−015F2018 (a) A

17 212VU 584VC−A <B EN3155−019F2018 2623−0110 2M CF20 15500 620 802VU 2614VC−A 38 EN3155−015F2018 (a) A

18

19

20

21

22

23

24

25

 (a) = BUNDLE F9000095226495 M2N = NEW HOOK−UP ON END 2 WS = WIRE STOWED

 A = ADDED WIRE M1O+M2O= OLD HOOK−UP ON END 1 AND 2

 M2O = OLD HOOK−UP ON END 2 M1N+M2N= NEW HOOK−UP ON END 1 AND 2

Figure A-FCPAA - Sheet 03

Modification of the Wiring between the RH Overhead Panel 212VU and the Avionics

Compartment (RH Side)

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 525

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF 001, 004, 006

F_SB_265020_6_BAAA_01_00

4010WX

4005WX

4020WX

A

Z130

FR35

FR36

FR37

FR37.1

B A

B

C

Figure A-GBAAA - Sheet 01

Removal of Fire Extinguishing Bottles 4005WX, 4010WX and 4020WX with Cartridges.

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 526

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF 001, 004, 006

4010WX

4020WX

(4 POS)

(4 POS)

TYPICAL

(100)

(101)

(200)

(103)

(104) (2 POS)

B

D

D

F_SB_265020_6_BAAA_02_02

Figure A-GBAAA - Sheet 02

Removal of Fire Extinguishing Bottles 4005WX, 4010WX and 4020WX with Cartridges.

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 527

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF 001, 004, 006

(4 POS)

(4 POS)

4005WX

(100)

(101)

(103)

(104)

(201)

TYPICAL

(260)

(261)

D (262)

D C

D

F_SB_265020_6_BAAA_03_02

Figure A-GBAAA - Sheet 03

Removal of Fire Extinguishing Bottles 4005WX, 4010WX and 4020WX with Cartridges.

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 528

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF 002 thru 003, 005

4010WX

4005WX

4020WX

A

Z130

FR35

FR36

FR37

FR37.1

A

F_SB_265020_6_BBAA_01_00

B

B

D

Figure A-GBBAA - Sheet 01

Removal of Fire Extinguishing Bottles 4005WX, 4010WX and 4020WX with Cartridges.

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 529

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF 002 thru 003, 005

4010WX

4020WX

(4 POS)

(4 POS)

TYPICAL

F_SB_265020_6_BBAA_02_00

C

C

C

TYPICAL

B

(100)

(101)

(104)

(103)

(203)

(106)

(105)

Figure A-GBBAA - Sheet 02

Removal of Fire Extinguishing Bottles 4005WX, 4010WX and 4020WX with Cartridges.

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 530

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF 002 thru 003, 005

(4 POS)

(4 POS)

4005WX

F_SB_265020_6_BBAA_03_00

D TYPICAL

E

E

E

(100)

(101)

(106)

(105)

(103)

(104)

(204)

Figure A-GBBAA - Sheet 03

Removal of Fire Extinguishing Bottles 4005WX, 4010WX and 4020WX with Cartridges.

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 531

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF ALL

A

Z130

FR35

FR36

FR37

FR37.1

A

B

B

4034WX

4031WX

4032WX

4033WX

G F

G

G

G

G

(115)

(128)

(126)

(126)

(126)

(126)

(127)

(122)

(125)

(116)

(117)

(209)

(119)

(125)

(129)

(125)

(124)

(120)

(115)

(209)

(118)

(117)

(116)

(115)

(209)

(123)

(210)

(115)

(142)

(210)

F_SB_265020_6_BCAA_01_01

Figure A-GBCAA - Sheet 01

Removal of the 4 Flow Metering Compact Units (FMCU), FIN 4031WX, 4032WX, 4033WX and

4034WX, the related Plumbing Installations and Placards

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 532

6

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@A340-500/600

SERVICE BULLETIN

**CONF ALL

B

D

D

E

H

H

TYPICAL

(110)

(108)

(107)

(109)

F_SB_265020_6_BCAA_02_01

Figure A-GBCAA - Sheet 02

Removal of the 4 Flow Metering Compact Units (FMCU), FIN 4031WX, 4032WX, 4033WX and

4034WX, the related Plumbing Installations and Placards

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 533

6

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@A340-500/600

SERVICE BULLETIN

**CONF ALL

F_SB_265020_6_BCAA_03_00

D

TYPICAL

4031WX

4032WX

4033WX

4034WX

( 3 POS)

( 3 POS)

G

TYPICAL

H

TYPICAL

(205)(4 POS)

(134)

(133)

(132)

(133)

(131)

(130)

(113)

(121)

(106)

(112)

(113)

(111)

(106)

(112)

(139)

(140)

(138)

(138)

(104)

(141)

(136)

(137) (135)

E F

Figure A-GBCAA - Sheet 03

Removal of the 4 Flow Metering Compact Units (FMCU), FIN 4031WX, 4032WX, 4033WX and

4034WX, the related Plumbing Installations and Placards

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 534

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF ALL

A

Z130

FR35

FR36

FR37

FR37.1

F_SB_265020_6_BDAA_01_00

STGR29RH

STGR30RH

B

C

D

E

F

F

G

G A

Figure A-GBDAA - Sheet 01

Removal of the Brackets

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 535

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF ALL

01

01 (6 POS)

(6 POS)

(3 POS)

(3 POS)

(3 POS)

(3 POS)

(2 POS) 01

01 (2 POS)

(165)

(172)

(172)

(166)

(167)

(172)

(172)

(165)

NOTE:

CLOSE WITH RIVET 01

(168)

170

170

170

170

F_SB_265020_6_BDAA_02_02

B

D

C

Figure A-GBDAA - Sheet 02

Removal of the Brackets

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 536

6

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@A340-500/600

SERVICE BULLETIN

**CONF ALL

NOTE:

01 CLOSE WITH RIVET

(2 POS)

(2 POS)

01

01

STGR29

STGR30

TYPICAL

TYPICAL

(4 POS)

01

(4 POS)

01

E

F

G

(161)

(162)

(163)

(164)

F_SB_265020_6_BDAA_03_01

171

171

171

171

Figure A-GBDAA - Sheet 03

Removal of the Brackets

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 537

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF ALL

Z130

A

FR35

FR36

FR37

FR37.1

AD

F_SB_265020_6_BEAA_01_01

B D

C E

A

Figure A-GBEAA - Sheet 01

Adaption of the Plumbing Installation

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 538

6

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@A340-500/600

SERVICE BULLETIN

**CONF ALL

F_SB_265020_6_BEAA_02_02 FR37 VIEW LOOKING FWD

200.0mm

(7.87 in.)

200.0mm

(7.87 in.)

01

01

CUT THE PIPE

NOTE:

01

(250)

(252)

LOOSEN THE CLAMP 02

02 02 0202 02 02

G

BEFOREBEFORE

FR36

VIEW LOOKING FWD

B

C

G

Figure A-GBEAA - Sheet 02

Adaption of the Plumbing Installation

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 539

6

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@A340-500/600

SERVICE BULLETIN

**CONF ALL

200.0mm

(7.87 in.)

200.0mm

(7.87 in.)

(250)

251

(252)

125 253

FR37

VIEW LOOKING FWD NOTE:

01

SAFETY THE CLAMP 02

AFTERAFTER

FR36

VIEW LOOKING FWD

01

02 02 02

G

01

02 02 02

F

TEMPORARILY INSTALL THE NEW PIPE,ITEM 251 AND 253, BEFORE CUTTING.

D

E

F_SB_265020_6_BEAA_03_02

F

G

Figure A-GBEAA - Sheet 03

Adaption of the Plumbing Installation

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 540

6

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@A340-500/600

SERVICE BULLETIN

**CONF ALL

TYPICAL

TYPICAL

4.0mm

(0.16 in.)

(113)

113

(144)

144

(157)

157

(121)

121

155

(155)

158

F_SB_265020_6_BEAA_04_00

F

G

H

H

Figure A-GBEAA - Sheet 04

Adaption of the Plumbing Installation

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 541

6

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@A340-500/600

SERVICE BULLETIN

**CONF ALL

FR36

FR37

FR37.1

A

Z130

B

B

C C

D

E

4010WX

A

238

248

237

233

235

236

(210)

(210)

(209)

(209)

234

F_SB_265020_6_BFAA_01_01

Figure A-GBFAA - Sheet 01

Installation of the U-Section and the Flow Metering System (FMS)

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 542

6

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@A340-500/600

SERVICE BULLETIN

**CONF ALL

B

TYPICAL

C

TYPICAL

TYPICAL

D

144

143

104

140

(136)

(137) (135)

106

143

153

152

141

F_SB_265020_6_BFAA_02_02

139

113

121

Figure A-GBFAA - Sheet 02

Installation of the U-Section and the Flow Metering System (FMS)

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 543

6

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@A340-500/600

SERVICE BULLETIN

**CONF ALL

E

J

J

L

N

Q

R G

P

N

H

239

228

232

212 214

217

231

215

215

227

239

214

226

213

223

217

225

221

216

222

229

230

216

F

G F

K

J

F_SB_265020_6_BFAA_03_02

219

Figure A-GBFAA - Sheet 03

Installation of the U-Section and the Flow Metering System (FMS)

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 544

6

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@A340-500/600

SERVICE BULLETIN

**CONF ALL

(3 POS)

(3 POS)

G

5014WE

5015WE

5011WE

5010WE

H

214

215

146

140

133

133

132

147

132

133

133

132

160

159

106

159

106

160

F_SB_265020_6_BFAA_04_01

134

TYPICAL

F

Figure A-GBFAA - Sheet 04

Installation of the U-Section and the Flow Metering System (FMS)

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 545

6

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@A340-500/600

SERVICE BULLETIN

**CONF ALL

N

TYPICAL

P

Q

148

144

145

145 143

144

224

148

144

145

144

145

144

J K L

TYPICAL

F_SB_265020_6_BFAA_05_02

113

Figure A-GBFAA - Sheet 05

Installation of the U-Section and the Flow Metering System (FMS)

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 546

6

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@A340-500/600

SERVICE BULLETIN

**CONF ALL

R

S

S

5011WE

5017WE

5010WE

5016WE

5014WE

4016WX

4018WX

5015WE

S

TYPICAL

247

246

240

220

242

244

241

243

F_SB_265020_6_BFAA_06_02

143

106

245

Figure A-GBFAA - Sheet 06

Installation of the U-Section and the Flow Metering System (FMS)

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 547

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF ALL

A

Z130

FR36

FR37

FR37.1

STGR30RH

B

C

D

E

F_SB_265020_6_BGAA_01_01

STGR31RH

G

F

A

Figure A-GBGAA - Sheet 01

Installation of the Brackets

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 548

6

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@A340-500/600

SERVICE BULLETIN

**CONF ALL

D

L

D

252 K

170

252

170

FOR DIMENSIONS, REFER TO SHEET 4 F_SB_265020_6_BGAA_02_01

STGR31RH

STGR32RH

B

H

171 (4 POS)

253

F

B

STGR31RH

C

171 (4 POS)

254

D

E

NOTE:

01 USE EXISTING RIVET HOLES

01

01

FR36RH FR37RH

STGR30RH

FR37RH

FR37.1RH

STGR30RH

B C

Figure A-GBGAA - Sheet 02

Installation of the Brackets

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 549

6

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@A340-500/600

SERVICE BULLETIN

**CONF ALL

F_SB_265020_6_BGAA_03_00

E

G

282 171

A

A

A A

A 170

J

281

B

B

STGR30RH

STGR31RH

STGR32RH

NOTE:

FOR DIMENSIONS, REFER TO SHEET 4

−Y2462

STGR31RH

F

G

B B

FR37RH

FR36RH

FR37RH

Figure A-GBGAA - Sheet 03

Installation of the Brackets

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 550

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF ALL

mm

DIMENSIONS

(in.)

A 1.0 0.04

B 10.0 0.39

C 12.0 0.47

D 12.3 0.48

E 18.0 0.70

F 21.7 0.85

G 65.0 2.56

H 68.0 2.68

J 125.0 4.92

K 126.5 4.98

L 147.5 5.81

F_SB_265020_6_BGAA_04_00

Figure A-GBGAA - Sheet 04

Installation of the Brackets

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 551

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF 001, 004, 006

FR36

FR37

FR37.1

A

Z130

A

F_SB_265020_6_BHAA_01_00

B

C

Figure A-GBHAA - Sheet 01

Installation of Fire Extinguishing Bottles 4005WX and 4010WX with Cartridges.

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 552

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF 001, 004, 006

(4 POS)

(4 POS)

4005WX

100

101

104

103

(201)

F_SB_265020_6_BHAA_02_01

D

B

D

Figure A-GBHAA - Sheet 02

Installation of Fire Extinguishing Bottles 4005WX and 4010WX with Cartridges.

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 553

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF 001, 004, 006

4010WX

(4 POS)

(4 POS)

100

101

103

104

(200)

F_SB_265020_6_BHAA_03_01

TYPICAL

(260)

(261)

(262)

D

C D

D

Figure A-GBHAA - Sheet 03

Installation of Fire Extinguishing Bottles 4005WX and 4010WX with Cartridges.

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 554

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF 002 thru 003, 005

FR36

FR37

FR37.1

A

Z130

A

B

F_SB_265020_6_BJAA_01_00

D

Figure A-GBJAA - Sheet 01

Installation of Fire Extinguishing Bottles FIN 4005WX and FIN 4010WX with Cartridges.

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 555

6

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@A340-500/600

SERVICE BULLETIN

**CONF 002 thru 003, 005

(4 POS)

(4 POS)

4005WX

B TYPICAL

C

C

C

100

101

104

103

105

106

(204)

F_SB_265020_6_BJAA_02_01

Figure A-GBJAA - Sheet 02

Installation of Fire Extinguishing Bottles FIN 4005WX and FIN 4010WX with Cartridges.

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 556

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF 002 thru 003, 005

4010WX

(4 POS)

(4 POS)

TYPICAL

D

E

E

E

100

101

106

105

103

104

(203)

F_SB_265020_6_BJAA_03_01

Figure A-GBJAA - Sheet 03

Installation of Fire Extinguishing Bottles FIN 4005WX and FIN 4010WX with Cartridges.

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 557

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF ALL

5053 28DC1

5351VN

5049−CF22

5054 28DC1

5351VN

5050−CF22

5055 28DC1

7985VN

5051−CF22

5656 28DC1

7985VN

5052−CF22

3

2

1

4

3

2

1

31

3

2

1

3

2

1

A

A

01

2509VC

801VU

2539VC

801VU

4031WX

FMCU BTL 2 FWD/OUTLET PRESS

132

02

47

48

4033WX

FMCU BTL 3 FWD/OUTLET PRESS

132

4032WX

FMCU BTL 2 AFT/OUTLET PRESS

132

4034WX

FMCU BTL 3 AFT/OUTLET PRESS

132

NOTE:

01 CONNECTOR REMOVE AND SCRAP

02 RENAME CONNECTOR

EXISTING WIRE

F_SB_265020_6_WAAA_01_00

A

A

A

A

UNLESS OTHERWISE SPECIFIED PREFIX ALL WIRE IDENTIFICATION

WITH ATA 2623

UNLESS OTHERWISE SPECIFIED ALL WIRES ARE CF20 GAUGE

UNLESS OTHERWISE SPECIFIED ALL ROUTES ARE 1M

Figure A-GWAAA - Sheet 01

Modification of the Wiring of the FMCU/FMS Outlet Pressure Switches 4031WX, 4032WX, 4033WX,

4034WX, 4016WX and 4018WX

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 558

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF ALL

5053 28DC1

5351VN

5049−CF22

5054 28DC1

5351VN

5050−CF22

5055 28DC1

7985VN

5051−CF22

5656 28DC1

7985VN

5052−CF22

4

31

3

2

1

3

2

1

A 2509VC

801VU

4016WX

FLOW MET/FWD BLT2 OUTLET PRESS

132

132

STOW

F_SB_265020_6_WAAA_02_00

4018WX

FLOW MET/AFT BLT2 OUTLET PRESS

REROUTED WIRE

A

A

EXISTING WIRE

UNLESS OTHERWISE SPECIFIED PREFIX ALL WIRE IDENTIFICATION

WITH ATA 2623

UNLESS OTHERWISE SPECIFIED ALL WIRES ARE CF20 GAUGE

UNLESS OTHERWISE SPECIFIED ALL ROUTES ARE 1M

NOTE:

Figure A-GWAAA - Sheet 02

Modification of the Wiring of the FMCU/FMS Outlet Pressure Switches 4031WX, 4032WX, 4033WX,

4034WX, 4016WX and 4018WX

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 559

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF ALL

132

132

132

4031WX−A

4031WX−A

1

3

1

3

EN3155−005F2018

2623− 5053

5049

5054

5050

1M

1M

1M

1M

5351VN 28DC1

2509VC−A 31

4

28DC1

23000 2509VC−A

5351VN

801VU

801VU

ELT.EQUIPMENT G9297006800000 "SHEET 02,ISSUE C"

5051 1M 801VU 2539VC−A 47

5052 1M 2539VC−A 48

EN3155−003F2222

BEFORE

BEFORE

2623−

2623−

2623−

2623−

2623−

132

132

132 3

4032WX−A

4032WX−A

4033WX−A

4034WX−A

CF20

CF22

CF20

CF22

CF22

CF22

AFTER

AFTER

AFTER

AFTER

1000

23000

23000

23000

EN3155−005F2018 1000

EN3155−005F2018

EN3155−005F2018

EN3155−005F2018

EN3155−005F2018

NSA936501TA2004

NSA936501TA2004

EN3155−003F2222

EN3155−003F2222

EN3155−003F2222

BEFORE

BEFORE

BEFORE

BEFORE

AFTER

132 AFTER

132

132

4031WX−A

4031WX−A

STOW

STOW

STOW

STOW

2623− 5053

5049

5054

5050

1M

1M

1M

1M

5351VN 28DC1

2509VC−A STOW

STOW

28DC1

23000 2509VC−A

5351VN

801VU

801VU

3 5051 1M 801VU 2509VC−A 4

5052 1M 2509VC−A 31

2623−

2623−

2623−

2623−

2623−

132

132

132 3

4032WX−A

4032WX−A

4016WX−A

4018WX−A

CF20

CF22

CF20

CF22

CF22

CF22

1000

23000

23000

23000

NSA936603CC0100 1000

EN3155−005F2018

EN3155−005F2018

NSA936501TA2004

NSA936501TA2004

EN3155−003F2222

EN3155−003F2222

801VU

NSA936603CC0100

NSA936603CC0100

NSA936603CC0100 NSA936603CC0100

NSA936603CC0100

1 CONTACTS DO NOT CUT OFF

2 MANUFACTURE LIKE AOPS07−04−007

1 2

1 2

1 2

1 2

40

906

40

906

906

906

40

906

40

906

906

906

3

132 4033WX−A 1 EN3155−005F2018 2623− 5055 1M CF20 1000 40 7985VN 28DC1 NSA936501TA2004 BEFORE

132 4034WX−A 1 EN3155−005F2018 2623− 5656 1M CF20 1000 40 7985VN 28DC1 NSA936501TA2004 BEFORE

132 4016WX−A 1 EN3155−005F2018 2623− 5055 1M CF20 1000 40 7985VN 28DC1 NSA936501TA2004 AFTER

132 4018WX−A 1 EN3155−005F2018 2623− 5656 1M CF20 1000 40 132 7985VN 28DC1 NSA936501TA2004 AFTER

801VU

132

132

132

132

132

132

132

L

I

N

E ZONE OR

PANEL TERM. TERMINAL P/N WIREIDENT C0L ROUTE GAUGE

LENGTH

MM INCH

ZONE OR

PANEL

ELEC.

IDENT TERM. TERMINAL P/N

INSTRUCTIONS

END 1 LEAD END 2

10

11

12

13

14

15

16

17

18

19

20

21

22

23

24

25

1

2

3

4

5

6

7

8

9

ELEC.

IDENT.

Figure A-GHAAA - Sheet 01

Hook-up Chart

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 560

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF ALL

NOTE:

02 RENAME CONNECTOR

3

A 2625VC

801VU

4

40

A 2636VC

802VU

41

A

2044VC

132

18

5041 28DC1

7978VN

5042−CF18 B1

7980VN

5043 28DC1

7981VN

5044 28DC1

7982VN

5045−CF18 B1

7983VN

5046 28DC2

7979VN

5047 28DC2

7984VN

5048−CF22

02 02

5040

5039

5038

5037

2M

4020WX

CARGO FIRE EXTINGUISHING BOTTLE 3

(FLOW METERING)

132

4023WX 4021WX 4022WX

CARTRIDGE CARTRIDGE PRESS

SWITCH

A

1

2

3

4

5

A

1

2

3

4

5

A

3

2

1

UNLESS OTHERWISE SPECIFIED PREFIX ALL WIRE IDENTIFICATION

WITH ATA 2623

UNLESS OTHERWISE SPECIFIED ALL WIRES ARE CF20 GAUGE

UNLESS OTHERWISE SPECIFIED ALL ROUTES ARE 1M

EXISTING WIRE

F_SB_265020_6_WBAA_01_01

Figure A-GWBAA - Sheet 01

Modification of the Wiring of the Fire Extinguishing Bottle No. 3 (previously AFT), 4020WX, and

relocated Fire Extinguishing Bottle No. 2 (now AFT), 4010WX

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 561

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF ALL

36

A 2511VC

801VU

38

46

A 2508VC

802VU

47

A

2044VC

132

18

5041 28DC1

7978VN

5042−CF18 B1

7980VN

5043 28DC1

7981VN

5044 28DC1

7982VN

5045−CF18 B1

7983VN

5046 28DC2

7979VN

5047 28DC2

7984VN

5048−CF22

5040

5039

5038

5037

2M

4010WX

CARGO FIRE EXTINGUISHING BOTTLE 2

(FLOW METERING)

132

4013WX 4011WX 4012WX

CARTRIDGE CARTRIDGE PRESS

SWITCH

A

1

2

3

4

5

A

1

2

3

4

5

A

3

2

1

REROUTED WIRE

NOTE:

UNLESS OTHERWISE SPECIFIED PREFIX ALL WIRE IDENTIFICATION

WITH ATA−NO. 2623

UNLESS OTHERWISE SPECIFIED ALL WIRES ARE CF20 GAUGE

UNLESS OTHERWISE SPECIFIED ALL ROUTES ARE 1M F_SB_265020_6_WBAA_02_03

Figure A-GWBAA - Sheet 02

Modification of the Wiring of the Fire Extinguishing Bottle No. 3 (previously AFT), 4020WX, and

relocated Fire Extinguishing Bottle No. 2 (now AFT), 4010WX

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 562

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF ALL

4020WX

4020WX

4010WX

4023WX−A

4013WX−A

1

1

2

2

3

EN3155−005F2018

2623− 5037

5037

5041

5041

5039

1M

1M

1M

1M

2M CF20

2625VC−A 3

7978VN 28DC1

36

40

28DC1

23000 2511VC−A

7978VN

2636VC−A

801VU

802VU

801VU

ELT.EQUIPMENT G9297006800000 "SHEET 03,ISSUE D"

3 5039 2M 802VU 2508VC−A 46

5046 2M 7979VN 28DC2

5046 2M 7979VN 28DC2

5042 7980VN B1

5042

1M

1M 7980VN B1

4021WX−A 5038 1M 801VU 2625VC−A 4

5038 1M 2511VC−A 38

EN3155−015F2018

EN3155−015F2018

5043 1M 7981VN 28DC1

5043 1M 7981VN 28DC1

2M 802VU 2636VC−A 41

EN3155−003F1614

5040

5040 2M 802VU 2508VC−A 47

5044 2M 7982VN 28DC2

BEFORE

BEFORE

BEFORE

BEFORE

BEFORE

2623−

2623−

2623−

2623−

2623−

2623−

2623−

2623−

2623−

2623−

2623−

2623−

2623−

2623−

2623−

2623−

4010WX

4020WX

4010WX

40200WX

4010WX

4020WX

4010WX

4010WX

4020WX

4020WX

4020WX

4010WX

4010WX

4020WX

4

4

5

5

4023WX−A

4013WX−A

4023WX−A

4013WX−A

4023WX−A

4013WX−A

4023WX−A

4013WX−A

CF20

CF20

CF20

CF20

CF20

CF20

CF20

CF18

CF18

CF20

CF20

CF20

CF20

CF20

1

1

2

2

3

3

4

4

5

5

4011WX−A

4021WX−A

4011WX−A

4011WX−A

4021WX−A

4011WX−A

4011WX−A

4021WX−A

4021WX−A

4010WX

4020WX

4010WX

4020WX

4010WX

2623− 5044 2M CF20 7982VN 28DC2

2623− 5045 1M CF18 7983VN B1

2623− 5045 1M CF18 7983VN B1

2623− 5047 2M CF20 7984VN 28DC2

2623− 5047 2M CF20 7984VN 28DC2

2

2

4022WX−A

4012WX−A

AFTER

BEFORE

AFTER

BEFORE

AFTER

AFTER

AFTER

AFTER

AFTER

BEFORE

AFTER

BEFORE

AFTER

BEFORE

AFTER

BEFORE

AFTER

CF20

CF20

801VU

1200

1200

16000

16000

1200

1200

1200

1200

23500

23500

1500

23000

1500

16500

16500

1500

1500

1500

1500

1200

1200

EN3155−005F2018

EN3155−005F2018

EN3155−005F2018

EN3155−005F2018

EN3155−005F2018

EN3155−005F2018

EN3155−005F2018

EN3155−005F2018

EN3155−005F2018

EN3155−005F2018

EN3155−005F2018

EN3155−005F2018

EN3155−005F2018

EN3155−005F2018

EN3155−005F2018

EN3155−005F2018

EN3155−005F2018

EN3155−005F2018

EN3155−005F2018

EN3155−005F2018

EN3155−005F2018

NSA936501TA2004

NSA936501TA2004

NSA936501TA1604

NSA936501TA1604

NSA936501TA2004

NSA936501TA2004

EN3155−003F2018

NSA936501TA2004

NSA936501TA2004

NSA936501TA1604

NSA936501TA1604

NSA936501TA2004

NSA936501TA2004

EN3155−003F2018

EN3155−003F1614

NSA936501TA2004

NSA936501TA2004

EN3155−015F2018

EN3155−015F2018

906

48

630

48

48

925

59

59

59

48

48

59

59

59

925

48

48

630

48

906

650

650

4 DIRECTLY BEHIND THE CONTACT CUT OFF

4

4

4020WX

4010WX

4022WX−A

4012WX−A

3

3

EN3155−005F2018

EN3155−005F2018

2623−

2623−

5048

5048

2M

2M

CF22

CF22

14000

14000

551

551

2044VC

2044VC

18

18

EN3155−014M2018

EN3155−014M2018

BEFORE

AFTER

132

132

L

I

N

E ZONE OR

PANEL TERM. TERMINAL P/N WIREIDENT C0L ROUTE GAUGE

LENGTH

MM INCH

ZONE OR

PANEL

ELEC.

IDENT TERM. TERMINAL P/N

INSTRUCTIONS

END 1 LEAD END 2

10

11

12

13

14

15

16

17

18

19

20

21

22

23

24

25

1

2

3

4

5

6

7

8

9

ELEC.

IDENT.

Figure A-GHBAA - Sheet 01

Hook-up Chart

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 563

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF ALL

NOTE:

36

A 2511VC

801VU

38

46

A 2508VC

802VU

47

A

2016VC

132

17

5015 28DC1

5062VN

5016−CF18 B1

5453VN

5017 28DC1

5351VN

5018 28DC1

5476VN

5019−CF18 B1

5453VN

5020 28DC2

5482VN

5021 28DC2

5478VN

5023−CF22

5014

5013

5012

5011

2M

4010WX

CARGO FIRE EXTINGUISHING BOTTLE 2

(FLOW METERING)

132

4013 WX 4011 WX 4012 WX

CARTRIDGE CARTRIDGE PRESS

SWITCH

A

1

2

3

4

5

A

1

2

3

4

5

A

3

2

1

F_SB_265020_6_WCAA_01_00

CONNECTOR REMOVE AND SCRAP

01

01

01

EXISTING WIRE

UNLESS OTHERWISE SPECIFIED PREFIX ALL WIRE IDENTIFICATION

WITH ATA 2623

UNLESS OTHERWISE SPECIFIED ALL WIRES ARE CF20 GAUGE

UNLESS OTHERWISE SPECIFIED ALL ROUTES ARE 1M

Figure A-GWCAA - Sheet 01

Modification of the Wiring of the Fire Extinguishing Bottle No. 2 (FWD), 4010WX

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 564

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF ALL

5015 28DC1

5062VN

5016−CF18 B1

5453VN

5017 28DC1

5351VN

5018 28DC1

5476VN

5019−CF18 B1

5453VN

5020 28DC2

5482VN

5021 28DC2

5478VN

5023−CF22

5014

5013

5012

5011

2M

F_SB_265020_6_WCAA_02_00

STOW

UNLESS OTHERWISE SPECIFIED PREFIX ALL WIRE IDENTIFICATION

WITH ATA 2623

UNLESS OTHERWISE SPECIFIED ALL WIRES ARE CF20 GAUGE

UNLESS OTHERWISE SPECIFIED ALL ROUTES ARE 1M

NOTE:

Figure A-GWCAA - Sheet 02

Modification of the Wiring of the Fire Extinguishing Bottle No. 2 (FWD), 4010WX

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 565

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF ALL

1

2

3

NSA936603CC0100

2623− 5011

5011

5015

5015

5013

1M

1M

1M

1M

2M CF20

2511VC−A 36

5062VN 28DC1

STOW

46

28DC1

23000 2511VC−A

5062VN

2508VC−A

801VU

802VU

801VU

ELT.EQUIPMENT G9297006800000 "SHEET 01,ISSUE C"

5013 2M 802VU 2508VC−A STOW

5020 2M 5482VN 28DC2

5020 2M 5482VN 28DC2

2623−

2623−

2623−

2623−

2623−

2623−

2623−

4

CF20

CF20

CF20

CF20

CF20

CF20

CF20

4010WX 4011WX−A STOW

4010WX

4010WX

4010WX

4010WX

2623− 5019 1M CF18 5453VN B1

2623− 5021 2M CF20 5478VN 28DC2

2623− 5021 2M CF20 5478VN 28DC2

2623− 5023 1M CF22 132 2016VC 17

2623− 5023 1M CF22 132 2016VC STOW

2

STOW

3

STOW

4012WX−A

4012WX−A

4012WX−A

4012WX−A AFTER

BEFORE

1000

1000

15500

15500

1000

1000

23000

1200

1200

1200

13000

13000

EN3155−005F2018

EN3155−005F2018

EN3155−005F2018

EN3155−005F2018

EN3155−005F2018

EN3155−005F2018 EN3155−014M2018

NSA936501TA2004

NSA936501TA2004

NSA936501TA1604

NSA936501TA2004

NSA936501TA2004

5

1

2

2623− 5016

5016

5012

5012

5017

1M

1M

1M

1M

1M CF20

5453VN B1

2511VC−A STOW

B1

28DC1

38

1500 5453VN

2511VC−A

5351VN

801VU

801VU

5017 1M 5351VN 28DC1

5614 2M 2508VC−A 47

5014 2M 2508VC−A STOW

2623−

2623−

2623−

2623−

2623−

2623−

2623−

3

CF18

CF18

CF20

CF20

CF20

CF20

CF20

23500

23500

1200

1200

15500

15500

EN3155−005F2018 1500

EN3155−005F2018

EN3155−005F2018

EN3155−005F2018

NSA936501TA2004

4010WX

4010WX

4010WX

4010WX

4010WX

4010WX

4010WX

4010WX

4010WX

4010WX

4010WX

4010WX

4010WX

4010WX

4010WX

4010WX

4010WX

4010WX

4010WX

4011WX−A

4011WX−A

4011WX−A

4011WX−A

4011WX−A

4011WX−A

4011WX−A

4011WX−A

4011WX−A

4013WX−A

4013WX−A

4013WX−A

4013WX−A

4013WX−A

4013WX−A

4013WX−A

4013WX−A

4013WX−A

4013WX−A

STOW

STOW

STOW

STOW

STOW

STOW

STOW

STOW

STOW

5

4

EN3155−005F2018

EN3155−005F2018 2623− 5018 2M CF20 1200 5476VN 28DC2

2623− 5018 2M CF20 1200 5476VN 28DC2

2623− 5019 1M CF18 1200 5453VN B1

802VU

802VU

AFTER

BEFORE

AFTER

BEFORE

AFTER

BEFORE

AFTER

BEFORE

AFTER

BEFORE

AFTER

BEFORE

AFTER

BEFORE

AFTER

BEFORE

AFTER

BEFORE

AFTER

BEFORE

AFTER

BEFORE

NSA936501TA1604

NSA936501TA1604

NSA936501TA1604

EN3155−015F2018

NSA936603CC0100

EN3155−015F2018

NSA936501TA2004

NSA936501TA2004

NSA936501TA2004

NSA936501TA2004

EN3155−003F1614

EN3155−003F1614

NSA936501TA2004

NSA936603CC0100

NSA936603CC0100

NSA936603CC0100

NSA936603CC0100

NSA936603CC0100

NSA936603CC0100

NSA936603CC0100

NSA936603CC0100

NSA936603CC0100

NSA936603CC0100

NSA936603CC0100

NSA936603CC0100

NSA936603CC0100

NSA936603CC0100

NSA936603CC0100

1 2

1

1

1

1

2

2

2

2

1 2

1 2

1 2

1 2

1 2

1 2

1 2

1 2

906

40

610

40

59

925

48

610

48

48

48

512

512

48

48

48

610

48

925

59

40

610

40

906

1 CONTACTS DO NOT CUT OFF 2 SHRINKING AS PER AIPS07−04−007 AND

TIED WIRES AS PER AIPS07−01−003

132

132

132

132

132

132

132

132

132

132

132

132

132

132

L

I

N

E ZONE OR

PANEL TERM. TERMINAL P/N WIREIDENT C0L ROUTE GAUGE

LENGTH

MM INCH

ZONE OR

PANEL

ELEC.

IDENT TERM. TERMINAL P/N

INSTRUCTIONS

END 1 LEAD END 2

10

11

12

13

14

15

16

17

18

19

20

21

22

23

24

25

1

2

3

4

5

6

7

8

9

ELEC.

IDENT.

Figure A-GHCAA - Sheet 01

Hook-up Chart

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 566

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SERVICE BULLETIN

**CONF ALL

F_SB_265020_6_BLAA_01_00

A

Z130

FR35

FR36

B C

A

Figure A-GBLAA - Sheet 01

Stowage of the Electrical Wires of the Connectors 4031WX-A, 4032WX-A 4011WX-A, 4012WX-A and

4013WX-A

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 567

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SERVICE BULLETIN

**CONF ALL

FR35 FR36

BEFORE

FWD

(266)

F_SB_265020_6_BLAA_02_00

B

(2 POS)

(2 POS)

(2 POS)

(265)

(267)

(268)

(269)

(270)

(274)

(267)

(269)

(273)

(267)

(265)

(267)

(268)

(269)

(270)

(274)

(267)

(269)

(273) (273)

(269)

(267)

(274)

(270)

(269)

(268)

(267)

(265)

(273)

(269)

(267)

(274)

(270)

(269)

(268)

(267)

(271) (277)

(277)

(271)

(277)

(271)

(277)

FR35

Figure A-GBLAA - Sheet 02

Stowage of the Electrical Wires of the Connectors 4031WX-A, 4032WX-A 4011WX-A, 4012WX-A and

4013WX-A

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 568

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SERVICE BULLETIN

**CONF ALL

FR35 FR36

AFTER

FWD

266

266

266 266

C

D

E

G F

H

F_SB_265020_6_BLAA_03_01

173

173

173 173

5716VB /2M

Figure A-GBLAA - Sheet 03

Stowage of the Electrical Wires of the Connectors 4031WX-A, 4032WX-A 4011WX-A, 4012WX-A and

4013WX-A

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 569

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SERVICE BULLETIN

**CONF ALL

266

272

269

266

270

(277)

274

(277)

274

266

D

271

269 266

(277)

270

274 266

(277)

271

269

270

266

274 (277)

275

269

266

266

(277)

274 270

G

F_SB_265020_6_BLAA_04_01

5717VB /1M

5716VB /2M

5716VB /2M

5717VB /1M

5717VB /1M

5716VB /2M

5717VB /1M

5717VB /1M

5717VB /1M

5716VB /2M

5717VB /1M

5717VB /1M

5716VB /2M

5717VB /1M

5717VB /1M

5716VB /2M

(270)

(270)

E

F

H

Figure A-GBLAA - Sheet 04

Stowage of the Electrical Wires of the Connectors 4031WX-A, 4032WX-A 4011WX-A, 4012WX-A and

4013WX-A

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 570

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SERVICE BULLETIN

Appendix 01

**CONF ALL

(1) Do the test of the modified cargo fire extinguisher circuitries ignition

(a) Test description

1 Check of the manual test circuit

a Energize the cargo compartment smoke detection system WH (ATA 26-16).

Push circuit breaker :

- 742VU : 11WH SDCU CHAN 1

- 722VU : 12WH SDCU CHAN 2

b Wait for 2 minutes :

- the SDCU performs the power up test

c On MDCU select :

- Maintenance system

- System Status test

- Fire Protection

- SDCU

d The SDCU Main Menu appears :

- Select "GROUND REPORT"

- Make sure that no "Cargo Fire Extinguishing Failure" is displayed

e On panel 212VU CARGO SMOKE (OVHD PNL) the following lights are off :

- FWD and AFT AGENT SQUIB

- DISCH BTL 1 and 2

f Push and hold the push button switch TEST (13WH) on OVHD PNL 212VU for a

short time (two seconds or more). The bottle squibs, pressure switches and the

indications on overhead panel as well as the smoke detection system in LDCC and

AVNCS compartment will be tested. As long as the push button is pressed :

- on push button switch/indicator FWD AGENT (4WX) and AFT AGENT (6WX)

the legends SQUIB must illuminate

- on indicators DISCH 3WX the legends BTL 1 and BTL 2 must illuminate

After approx. 10 seconds :

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 1

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Appendix 01

<1> the repetitive chime will be activated (can be cancelled on ECAM control

panel)

<2> on upper ECAM display the messages :

- SMOKE AVNCS VENT SMOKE

- SMOKE FWD CRG SMOKE

- SMOKE AFT CRG SMOKE

appear (in red color) with their associated procedures for a duration of approx.

30 seconds

<3> on overhead panel 212VU the lamps :

- SMOKE AVIONICS

- SMOKE FWD CARGO

- SMOKE AFT CARGO

comes on for a duration of approx. 30 seconds.

g 30 seconds after the smoke warnings disappeared on ECAM and OVHD panel :

<1> the repetitive chime will be activated again (can be cancelled on ECAM control

panel)

<2> on upper ECAM display the messages :

- SMOKE AVNCS VENT SMOKE

- SMOKE FWD CRG SMOKE

- SMOKE AFT CRG SMOKE

appear (in red color) again with their associated procedures for a duration of

approx. 30 seconds.

<3> on overhead panel 212VU the lamps :

- SMOKE AVIONICS

- SMOKE FWD CARGO

- SMOKE AFT CARGO

come on again for a duration of approx. 30 seconds.

h Verify that on ECAM no relevant fire extinguishing fault will be shown.

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 2

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Appendix 01

i With ARINC bus reader or dedicated means (e.g. ACMS) verify that the ARINC bus

information are as follows :

- Bit 21 to 29 of Label 061 shall be

- Bit 11 to 15 of Label 062 shall be "0"

- Bit 17 of Label 062 shall be "0"

- Bit 18 of Label 062 shall be "1"

- Bit 19 to 25 of Label 062 shall be "0"

j De-energize circuit WH (ATA 26-16) and circuit WX (ATA 26-23).

2 Check of the ignition circuitries

a Disconnect all cartridge connectors on bottle 1 (4001WX-A, 4003WX-A) and bottle

2 (4011WX-A, 4013WX-A)

b Energize the electrical circuit WH (ATA 26-16) and push in circuit breaker :

- 742VU : 11WH SDCU CHAN 1

- 722VU : 12WH SDCU CHAN 2

c Wait for 2 minutes :

- the SDCU performs the power up test

d On ECAM/ Warning display on SMOKE page appears the bottle fault warning for all

disconnected cartridge plugs :

- SMOKE FWD CRG BTL1 FAULT

- FWD CRG BTL2 FAULT

- AFT CRG BTL1 FAULT

- AFT CRG BTL2 FAULT

e Disconnect the pressure switch connectors of bottle 1 (4002WX-A) and bottle 2

(4012WX-A) :

- indication lights DISCH BTL 1 and DISCH BTL 2 (3WX) on panel 212VU come

on

f De-energize circuit WH (ATA 26-16) and pull circuit breaker :

- 742VU : 11WH SDCU CHAN 1

- 722VU : 12WH SDCU CHAN 2

<1> on ECAM/Warning display SMOKE DET FAULT appears

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 3

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Appendix 01

<2> indication lights DISCH BTL 1 and DISCH BTL 2 (3WX) on panel 212VU are

deactivated

g Energize the electrical circuit WX (ATA 26-23) and push in circuit breaker :

- 742VU : 1WX CRG FIRE EXTING/A

h On CARGO SMOKE panel 212VU (OVHD PNL) push in and hold the guarded push

button switch FWD AGENT (4WX). As long as the pushbutton switch is pressed :

- on the electrical connector 4003WX-A, between pin 1 and 2 the voltmeter

reads 28VDC

i Release push button switch FWD AGENT (4WX) :

- on the electrical connector 4003WX-A, between pin 1 and 2 the voltmeter

reads zero.

j On CARGO SMOKE panel 212VU (OVHD PNL) push in and hold the guarded push

button switch FWD AGENT (4WX). As long as the pushbutton switch is pressed :

- on the electrical connector 4013WX-A, between pin 1 and 2 the voltmeter

reads 28VDC.

k Release push button switch FWD AGENT (4WX) :

- on the electrical connector 4013WX-A, between pin 1 and 2 the voltmeter

reads zero.

l On CARGO SMOKE panel 212VU (OVHD PNL) push in and hold the guarded push

button switch AFT AGENT (6WX). As long as the pushbutton switch is pressed :

- on the electrical connector 4001WX-A, between pin 1 and 2 the voltmeter

reads 28VDC.

m Release push button switch AFT AGENT (6WX) :

- on the electrical connector 4001WX-A, between pin 1 and 2 the voltmeter

reads zero.

n On CARGO SMOKE panel 212VU (OVHD PNL) push in and hold the guarded push

button switch AFT AGENT (6WX). As long as the pushbutton switch is pressed :

- on the electrical connector 4011WX-A, between pin 1 and 2 the voltmeter

reads 28VDC.

o Release push button switch AFT AGENT (6WX) :

- on the electrical connector 4011WX-A, between pin 1 and 2 the voltmeter

reads zero.

p Change the energizing of the electrical circuit WX and :

pull circuit breaker :

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 4

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Appendix 01

- 742VU : 1WX CRG FIRE EXTING/A

push circuit breaker :

- 722VU : 2WX CRG FIRE EXTING/B

q On CARGO SMOKE panel 212VU (OVHD PNL) push in and hold the guarded push

button switch FWD AGENT (4WX). As long as the pushbutton switch is pressed :

- on the electrical connector 4003WX-A, between pin 3 and 4 the voltmeter

reads 28VDC.

r Release push button switch FWD AGENT (4WX) :

- on the electrical connector 4003WX-A, between pin 3 and 4 the voltmeter

reads zero.

s On CARGO SMOKE panel 212VU (OVHD PNL) push in and hold the guarded push

button switch FWD AGENT (4WX). As long as the pushbutton switch is pressed :

- on the electrical connector 4013WX-A, between pin 3 and 4 the voltmeter

reads 28VDC.

t Release push button switch FWD AGENT (4WX) :

- on the electrical connector 4013WX-A, between pin 3 and 4 the voltmeter

reads zero.

u On CARGO SMOKE panel 212VU (OVHD PNL) push in and hold the guarded push

button switch AFT AGENT (6WX). As long as the pushbutton switch is pressed :

- on the electrical connector 4001WX-A, between pin 3 and 4 the voltmeter

reads 28VDC.

v Release push button switch AFT AGENT (6WX) :

- on the electrical connector 4001WX-A, between pin 3 and 4 the voltmeter

reads zero.

w On CARGO SMOKE panel 212VU (OVHD PNL) push in and hold the guarded push

button switch AFT AGENT (6WX). As long as the pushbutton switch is pressed :

- on the electrical connector 4011WX-A, between pin 3 and 4 the voltmeter

reads 28VDC.

x Release push button switch AFT AGENT (6WX) :

- on the electrical connector 4011WX-A, between pin 3 and 4 the voltmeter

reads zero.

y De-energize the electrical circuit WX.

z Connect all cartridge plugs and pressure switch plugs to the associated bottle

cartridges and pressure switches.

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 5

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Appendix 01

3 Check of the FMS pressure switches

The pressure switches 4016WX and 4018WX of the flow metering system FMS at the

bottle 2 forward and aft outlet will be monitored but not indicated by the SDCU. The

information will be sent on the ARINC 429 bus to the FWC. With ARINC bus reader or

dedicated means (e.g. ACMS) verify the ARINC bus information.

a Preparation

<1> Energize the electrical circuits WH (ATA 26-16) and WX (ATA26-23).

Push circuit breaker :

- 742VU :

. 11WH SDCU CHAN 1

. 1WX CRG FIRE EXTING/A

- 722VU :

. 12WH SDCU CHAN 2

. 2WX CRG FIRE EXTING/B

<2> Wait for 2 minutes :

- The SDCU performs the power up test.

b Execution

<1> Verify the ARINC 429 bus information for the (pressure less) flow metering

system label 062/bit 24 and 25 :

- Status "0" (NO)

<2> Verify the ARINC 429 bus information for the (pressure less) flow metering

system label 062/bit 24 and 25 :

- Status "0" (NO)

<3> Disconnect the plug 4018WX-A of the FMS and verify the ARINC 429 bus

information: label 062/bit 24 and 25 :

- Status "1" (YES)

<4> Reconnect the plugs 4016WX-A and 4018WX-A.

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

REVISION No.: 00 - Jun 03/10 Page: 6

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SERVICE BULLETIN

REPORTING SHEET

TITLE: FIRE PROTECTION-LDCC FIRE EXTINGUISHING-REPLACE FMCU (3

BOTTLES) BY FMS (2 BOTTLES) FOR A340-600 A/C

MODIFICATION No.: 200000D46917

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: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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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 4 3 2 1

- Quality rating of the Accomplishment Instructions 4 3 2 1

- Quality rating of the Illustrations 4 3 2 1

- Is this SB easy to understand ? Y / N

If you have had difficulties in the accomplishment of this SB please quote below the area(s) and give a

short description of the issue.

Planning Material Instructions

X Effectivity X Kit content X Preparation

X Reason X List of Materials Operator Supplied X Mod/Inspection

X Manpower X Industry support X Test

X References X Re-identification X Close-Up

X Publication X Tooling X Illustrations

Comments:

Operator: Date:

Name/Title:

Please return this form to:

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX FRANCE

Attn : SEM4 Service Bulletins Management

FAX : (33) 5 61 93 42 51

Or via your Resident Customer Support Office.

DATE: Jun 03/10 SERVICE BULLETIN No.: A340-26-5020

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