@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: 33

TITLE: LIGHTS - SERVICE AREA LIGHTING - REMOVE SERVICE AREA

LIGHTS IN SECTION 19 ACCORDING TO SFAR 88 REQUIREMENTS.

**CONF ALL

MODIFICATIONS

MODIFICATION CLASSIFICATION

MAJOR None

MINOR 201683D46730

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

To obey SFAR88 instructions for in-service aircraft, the maintenance lights in section 19 (5LJ, 6LJ, 7LJ

and 8LJ) are to be removed.

This Service Bulletin gives the procedure to remove the maintenance lights 5LJ, 6LJ, 7LJ and 8LJ.

The affected circuit breakers are to be opened and safetied. Related wires and connections that

are no longer used are to be stowed properly. Installation positions (for unit installation and ground

connections) must be protected with sealants and anti-corrosion treatments as applicable.

With the accomplishment of this Service Bulletin the applicable aircraft obey the instructions of SFAR88

for the de-activation of maintenance maintenance lights 5LJ, 6LJ, 7LJ and 8LJ.

GENERAL EVALUATION

EVALUATION TABLE

COMPLIANCE MANDATORY (1) CANCELS INSPECTION SB NO

POTENTIAL AD YES A/C OPERATION AFFECTED NO

RELIABILITY AFFECTED NO PAX COMFORT AFFECTED NO

COST SAVING NO LROPS AFFECTED NO

STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED NO

NOTE (1): Service Bulletin must be accomplished.

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-5006

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SERVICE BULLETIN

SUMMARY

MATERIAL PRICE INFORMATION

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 335006D01R02 1 224.00 Caps, clip, placard set and ties

EFFECTIVITY

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

62X 70U 72W 79W CES CHH DLH ETD HFY IBE QAF QTR SAA

SIA SOR TAM THA UAE 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 NO

EQUIPMENT YES

HARD NO

SOFT NO

OBRM NO

MANPOWER

Task 335006-831-848-001: Modification

TOTAL MANHOURS 5.75

ELAPSED TIME (HOURS) 5.75

APPENDICES

None

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-5006

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@A340-500/600

SERVICE BULLETIN

SUMMARY

**CONF ALL

Z270

A

Z310

FR83

FR87

4LJ

FR84

5872VB /2M

FR85

BEFORE

6LJ

5012VN /DC2 FR88

7LJ

8LJ

5315VN /DC2

5420VN /DC2

5LJ

5011VN /DC2

C

C

D

D

D

D

5LJ

6LJ

7LJ

8LJ

LH

RH

LH

RH

D

TYPICAL

AFTER

TYPICAL

E

E

5872VB /2M

A

B

FR67

FR66

FR68

FR65

B

5032VE

F_SB_335006_6_SAAA_01_01

Figure A-GSAAA - Sheet 01

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-5006

REVISION No.: 00 - Jan 03/12 Page: 3

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@A340-500/600

SERVICE BULLETIN

SUMMARY

This Page Intentionally Left Blank

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-5006

REVISION No.: 00 - Jan 03/12 Page: 4

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: 33

TITLE: LIGHTS - SERVICE AREA LIGHTING - REMOVE SERVICE AREA

LIGHTS IN SECTION 19 ACCORDING TO SFAR 88 REQUIREMENTS.

MODIFICATION No.: 201683D46730

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 modification is applicable by Service Bulletin only.

(1) Models

340-541 340-542 340-642

(2) Effectivity by MSN

0371 0376 0383 0391 0394 0410 0416-0417 0426 0431 0436 0440 0445 0449 0453

0457 0460 0464 0468 0471 0475 0478 0482 0485 0488 0492 0495 0499 0514 0517

0520 0523 0531 0534 0537 0540 0543 0547 0557 0560 0563 0566 0569 0572 0575

0577 0580 0583 0586 0601 0604 0606 0608 0611 0615 0617 0619 0622 0624 0626

0628 0630 0639 0672 0677 0681 0685 0689 0694 0698 0702 0706 0710 0715 0719

0723 0727 0736 0740 0744 0748 0753 0757 0761-0768 0771 0775 0779 0783 0787

0790 0794 0798 0804 0812 0829 0837 0846 0848 0870 0886 0894 0897 0902 0910

0912 0917 0924 0929 0933 0953 0960 0972 0981 0987

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-5006

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SERVICE BULLETIN

(3) Effectivity by Operator

The Operator/MSN relationship is provided for information only and is correct at the time

of issue in accordance with the information available to AIRBUS. Any future changes

resulting from transfer of an aircraft from one operator to another will not be reflected in

this list unless the Service Bulletin is revised for another reason.

OPERATOR MSN

62X 0779

70U 0902

72W 0917

79W 0924

CES 0468 0488 0514 0577 0586

CHH 0436 0453 0475

DLH 0482 0517 0523 0537 0540 0543 0566 0569 0580 0583 0762 0763

0767 0771 0790 0794 0812 0846 0848 0897 0972 0981 0987

ETD 0748 0757 0761 0783 0829 0837 0870 0929 0933

HFY 0910 0912

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

0960

QAF 0495

QTR 0715 0740 0766 0798

SAA 0410 0417 0426 0531 0534 0547 0557 0626 0630

SIA 0478 0492 0499 0560 0563

SOR 0886 0894

TAM 0445 0464

THA 0624 0628 0677 0681 0689 0698 0710 0719 0775 0953

UAE 0394 0457 0471 0485 0520 0572 0608 0611 0685 0694

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

0736 0753 0764 0765 0768 0787 0804

(4) Configuration by MSN

MSN CONFIGURATION

0371 0376 0383 0391 0394 0410 0416 0417 0426 0431 0436

0440 0445 0449 0453 0457 0460 0464 0468 0471 0475 0478

0482 0485 0488 0492 0495 0499 0514 0517 0520 0523 0531

0534 0537 0540 0543 0547 0557 0560 0563 0566 0569 0572

0575 0577 0580 0583 0586 0601 0604 0606 0608 0611 0615

0617 0619 0622 0624 0626 0628 0630 0639 0672 0677 0681

0685 0689 0694 0698 0702 0706 0710 0715 0719 0723 0727

0736 0740 0744 0748 0753 0757 0761 0762 0763 0764 0765

0766 0767 0768 0771 0775 0779 0783 0787 0790 0794 0798

0804 0812 0829 0837 0846 0848 0870 0886 0894 0897 0902

0910 0912 0917 0924 0929 0933 0953 0960 0972 0981 0987

001

(5) Configuration definition

**CONF 001

Config. 001 is valid for all the aircraft given in the effectivity of this Service Bulletin as a

standard configuration.

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-5006

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@A340-500/600

SERVICE BULLETIN

(6) Material Effectivity

NOTE: The Kit 335006D01R02 is not necessary, if Service Bulletin No.

A340-33-5007 will be embodied at the same time.

MATERIAL QTY PER A/C SEE NOTES

Kit 335006D01R02 1

Consumable CMLD01 1

B. CONCURRENT REQUIREMENTS

None

C. REASON

(1) History

To obey SFAR88 instructions for in-service aircraft, the maintenance lights in section 19

(5LJ, 6LJ, 7LJ and 8LJ) are to be removed.

(2) Objective/Action

This Service Bulletin gives the procedure to remove the maintenance lights 5LJ, 6LJ,

7LJ and 8LJ. The affected circuit breakers are to be opened and safetied. Related wires

and connections that are no longer used are to be stowed properly. Installation positions

(for unit installation and ground connections) must be protected with sealants and anticorrosion treatments as applicable.

(3) Advantages

With the accomplishment of this Service Bulletin the applicable aircraft obey the

instructions of SFAR88 for the de-activation of maintenance maintenance lights 5LJ, 6LJ,

7LJ and 8LJ.

(4) Operational/Maintenance Consequences

None

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

Task 335006-831-848-001: Modification

(1) Modify the circuit breaker panel 5032VE

(2) Modify the electrical wiring of the button toggle 4LJ

(3) Remove the maintenance light 5LJ and modify the electrical wire

(4) Remove the maintenance light 6LJ and modify the electrical wire

(5) Remove the maintenance lights 7LJ and 8LJ and modify the electrical wires

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-5006

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SERVICE BULLETIN

E. COMPLIANCE

(1) Classification

MANDATORY: Service Bulletin must be accomplished.

(2) Accomplishment Timescale

This Service Bulletin has been classified Mandatory by the issue of an Airworthiness

Directive (AD) published by the European Aviation Safety Agency (EASA). The AD must

be used as the reference document for the mandated accomplishment timescale.

F. APPROVAL

The technical content of this document is approved under the authority of Design

Organisation Approval No. EASA.21J.031.

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

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

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

before incorporation of the Service Bulletin.

G. MANPOWER

The manpower estimates given in this Service Bulletin are based on the direct labor cost to

do the work. These estimates assume that the work will be done by experienced personnel,

and may need to be revised upwards to suit operator’s circumstances. The estimates do not

include the time to prepare, plan or inspect the work. Manufacture and procurement of parts

and tools, drying times for paints, sealants, etc., and general administration work are also not

included.

Task 335006-831-848-001: Modification

Get Access 0.25

On Aircraft

Modify the circuit breaker panel 5032VE 0.25

Modify the electrical wiring of the button toggle 4LJ 0.50

Remove the maintenance light 5LJ and modify the

electrical wire

1.00

Remove the maintenance light 6LJ and modify the

electrical wire

1.00

Remove the maintenance lights 7LJ and 8LJ and

modify the electrical wires

2.00

Tests 0.50

Close-Up 0.25

TOTAL MANHOURS 5.75

ELAPSED TIME (HOURS) 5.75

H. WEIGHT AND BALANCE

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.

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-5006

REVISION No.: 00 - Jan 03/12 Page: 4

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@A340-500/600

SERVICE BULLETIN

Only for aircraft model A340-500

Manufactures Empty Weight -1.561 KG -3.4413 LB

Effect on Balance -102.024 KGM -737.939 LB.FT

Only for aircraft model A340-600

Manufactures Empty Weight -1.561 KG -3.4413 LB

Effect on Balance -113.628 KGM -821.871 LB.FT

I. ELECTRICAL LOAD DATA

Not Changed

J. REFERENCES

Aircraft Maintenance Manual (AMM) 06-20-00 06-31-53 06-41-53

12-34-24 20-16-00 20-28-00

24-41-00 31-18-00 33-31-00

33-31-11 52-10-00

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-25-51 20-33-00 20-33-44

20-42-13 20-51-21 20-51-22

20-54-55 20-55-00

Service Bulletin (SB) A340-33-5007

Standards Manual (SM)

Weight and Balance Manual (WBM) Weight and Balance Manual

(WBM) Chapter 1-00-07

K. PUBLICATION AFFECTED

Aircraft Maintenance Manual (AMM) 33-31-00 33-31-11

Aircraft Schematic Manual (ASM) 33-31-00

Illustrated Parts Catalog (IPC) 33-31-04

L. INTERCHANGEABILITY/MIXABILITY

Not Applicable

M. SPARES

None

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-5006

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SERVICE BULLETIN

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DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-5006

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SERVICE BULLETIN

2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

(1) Procurement Addresses

Consumable CMLD01

Kit 335006D01R02

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 ordering by fax : +49 40 50 76 25 90

For ordering by E-mail: airbus.kit@airbus.com

(2) Price and Availability

Kit 335006D01R02

Cost 224.00 USD

Availability 60 calendar days from receipt of order

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

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

your order so that we can try to comply with your requirements. The sales terms (costs

and availability) are estimated in relation to economic conditions at the issue date of

the Service Bulletin. The latest valid price and lead time for ordering purposes shall

be obtained through the AirbusSpares portal or through a request for quotation to

airbus.kit@airbus.com.

B. INDUSTRY SUPPORT INFORMATION

AIRBUS will not provide industry support for accomplishment of this Service Bulletin.

C. LIST OF COMPONENTS

Kit 335006D01R02

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

NOTES

1 NSA936603CC0100 5 CAP

2 NSA935401-03 15 TIE

3 ABS0772A01A 1 CLIP

10 F9239025710200 1 PLCRDSET

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-5006

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@A340-500/600

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.

D. LIST OF MATERIALS - OPERATOR SUPPLIED

(1) Consumable Materials

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO CML

MAT. No.

QTY PER A/C SEE

NOTES

Bonding Coating (Blue Color) 07-001 As required

Sealant 09-007 As required

Lockwire Stainlss Stl Or Nickel Alloy 19-018 As required

(2) Components

None

(3) Equipment

None

E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

None

F. TOOLING

None

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-5006

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SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS

Task 335006-831-848-001 - Modification

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

INCLUDED IN THE REFERENCED PROCEDURES

WARNING: MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE

LANDING GEAR.

WARNING: PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION

BEFORE YOU START A TASK ON OR NEAR :

- THE FLIGHT CONTROLS

- THE FLIGHT CONTROL SURFACES

- THE LANDING GEAR AND THE RELATED DOORS

- COMPONENTS THAT MOVE.

WARNING: LET THE LIGHT BECOME COOL BEFORE YOU TOUCH IT. THIS LIGHT

BECOMES VERY HOT WHEN IT IS ON, AND IT CAN BURN YOU IF YOU

TOUCH IT.

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

Zone

270 310

Modified FIN

4LJ 5LJ 6LJ 7LJ 8LJ

Manpower

TOTAL MANHOURS 5.75

ELAPSED TIME (HOURS) 5.75

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-5006

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SERVICE BULLETIN

A. GENERAL

(1) Subtask 335006-910-201-001 - Standard Practices

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) 06-20-00, Page Block 001

06-31-53, Page Block 001

06-41-53, Page Block 001

20-28-00, Page Block 201

Consumable Material List (CML)

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

20-33-00

20-33-44

20-51-21

Standards Manual (SM)

(a) For the specification of materials (Mat. No.) given in this Service Bulletin (Refer to

Consumable Materials List (CML)).

(b) For the identification of zones (Refer to AMM 06-20-00, Page Block 001).

(c) For the Frame (FR) identification (Refer to AMM 06-31-53, Page Block 001).

(d) For the identification of the access panels (Refer to AMM 06-41-53, Page Block

001).

(e) Do the electrical bonding (Refer to AMM 20-28-00, Page Block 201 and ESPM

20-51-21).

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

(g) For the cable tie application and tooling (Refer to ESPM 20-25-51 and ESPM

20-33-44).

(2) Subtask 335006-839-201-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

Write in the applicable aircraft records that you have done all the work given in this

Service Bulletin.

B. PREPARATION

(1) Subtask 335006-941-201-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

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SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802

Task 24-41-00-861-801

Task 52-10-00-010-801

(a) Make sure that the aircraft is electrically grounded (Refer to AMM Task

12-34-24-860-802).

(b) Energize the aircraft electrical circuits (Refer to AMM Task 24-41-00-861-801).

(c) Put access platform(s) in position below the access door 312AR.

(d) Open the access door 312AR.

(e) Put access platform(s) in position below the AFT passenger/crew door 833.

(f) Open the AFT passenger/crew door 833 (Refer to AMM Task 52-10-00-010-801).

C. PROCEDURE

(1) Subtask 335006-831-201-001 - Modify the circuit breaker panel 5032VE

Work Zones and Access Panels

Zone Access/Work location

270

Manpower Resources

Manhours 0.25

Minimum number of person 1

Subtask elapsed time 0.25

Skills ELECTRICAL

Material necessary to do the job

Kit 335006D01R02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

3 ABS0772A01A 1 CLIP

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Lockwire Stainlss Stl Or

Nickel Alloy

19-018 As required

References

Aircraft Maintenance Manual (AMM) Task 20-16-00-912-801

Task 31-18-00-010-801

Fig. A-GBAAA

Modification of the Circuit Breaker Panel

5032VE

Sheet 01

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SERVICE BULLETIN

References

Fig. A-GWCAA

Wiring 3

Sheet 01

(a) Modify the circuit breaker panel 5032VE:

WARNING: WEAR GOGGLES WHEN YOU REMOVE OR INSTALL

LOCKWIRE. CUT, REMOVE AND DISCARD THE LOCKWIRE AS

YOU DO THE TASK. LOOSE LOCKWIRE CAN CUT OR BLIND

YOU.

1 Open, safety/lock and tag this circuit breaker:

Refer to AMM Task 31-18-00-010-801.

Refer to AMM Task 20-16-00-912-801.

Refer to Fig. A-GBAAA Sheet 01, View C and D.

Refer to Fig. A-GWCAA Sheet 01.

PANEL DESIGNATION FIN LOCATION SEE

NOTES

5032VE LIGHT SEC19 1LJ D07

and install:

1 Clip-Locking ABS0772A01A Item 3

with:

Lockwire Stainlss

Stl Or Nickel Alloy

19-018 As required

(2) Subtask 335006-831-202-001 - Modify the electrical wiring of the button toggle 4LJ

Work Zones and Access Panels

Zone Access/Work location

310

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills ELECTRICAL

Material necessary to do the job

Kit 335006D01R02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 NSA936603CC0100 1 CAP

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-5006

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SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

2 NSA935401-03 3 TIE

10 F9239025710200 1 PLCRDSET

References

Elec. Std. Practices Manual (ESPM) 20-42-13

20-54-55

Fig. A-GBBAA

Modification of the Electrical Wiring of

the Button Toggle 4LJ

Sheet 01

Fig. A-GWAAA

Wiring 1

Sheet 01

Fig. A-GWBAA

Wiring 2

Sheet 01

Fig. A-GHAAA

Hookup Chart

Sheet 01

(a) Modify the electrical wire 5003 and the button toggle 4LJ:

Refer to ESPM 20-42-13 and ESPM 20-54-55.

Refer to Fig. A-GBBAA Sheet 01, View B to D.

Refer to Fig. A-GWAAA Sheet 01.

Refer to Fig. A-GWBAA Sheet 01.

Refer to Fig. A-GHAAA Sheet 01, Lines 1 and 2.

1 Remove the electrical wire 5003 from the button toggle 4LJ.

2 Stow the electrical wire 5003, install:

1 Cap NSA936603CC0100 Item 1

3 Tie-Cable NSA935401-03 Item 2

3 Install:

1 Placard set F9239025710200 Item 10

(3) Subtask 335006-831-203-001 - Remove the maintenance light 5LJ and modify the

electrical wire

Work Zones and Access Panels

Zone Access/Work location

310

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-5006

REVISION No.: 00 - Jan 03/12 Page: 13

6

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@A340-500/600

SERVICE BULLETIN

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

Material necessary to do the job

Kit 335006D01R02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 NSA936603CC0100 1 CAP

2 NSA935401-03 3 TIE

10 F9239025710200 1 PLCRDSET

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Electrical Coating (Blue

Color)

07-001 As required

Sealant 09-007 As required

References

Aircraft Maintenance Manual (AMM) Task 33-31-11-000-801

Elec. Std. Practices Manual (ESPM) 20-42-13

20-51-22

20-54-55

Fig. A-GBCAA

Removal of the Maintenance Light 5LJ

and Modification of the Electrical Wire

Sheet 01

Sheet 02

Fig. A-GWAAA

Wiring 1

Sheet 01

Fig. A-GWBAA

Wiring 2

Sheet 01

Fig. A-GHAAA

Hookup Chart

Sheet 01

WARNING: LET THE LIGHT BECOME COOL BEFORE YOU TOUCH IT. THIS

LIGHT BECOMES VERY HOT WHEN IT IS ON, AND IT CAN BURN

YOU IF YOU TOUCH IT.

(a) Remove the maintenance light 5LJ:

Refer to AMM Task 33-31-11-000-801.

Refer to Fig. A-GBCAA Sheet 01, View B.

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-5006

REVISION No.: 00 - Jan 03/12 Page: 14

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SERVICE BULLETIN

1 Remove:

FIN 5LJ

1 Light-Service Area 2LA002606-01 Item (11) Discard

4 Screw NAS1096-3-7 Item (12) Discard

4 Washer NAS1149DN816K Item (13) Discard

2 Nut Item (14) Discard

2 Washer Item (15) Discard

(b) Remove the electrical wire 5016.

Refer to Fig. A-GBCAA Sheet 02, View E to G.

Refer to Fig. A-GWAAA Sheet 01.

Refer to Fig. A-GWBAA Sheet 01.

Refer to Fig. A-GHAAA Sheet 01, Line 13.

1 Remove the bonding connection of the maintenance light 5LJ and the

maintenance socket 11LJ:

1 Nut MS21042-08 Item (17) Retain

1 Washer NAS1149C0332R Item (6) Retain

1 Screw NAS1096-3-8 Item (16) Retain

2 Remove the electrical wire 5016.

3 Re-install the bonding connection of the maintenance socket 11LJ:

1 Nut MS21042-08 Item (17) Retained at

removal

1 Washer NAS1149C0332R Item (6) Retained at

removal

1 Screw NAS1096-3-8 Item (16) Retained at

removal

4 Apply to the bonding connection 5011VN/DC2:

Refer to ESPM 20-51-22.

Sealant 09-007 As required

and

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-5006

REVISION No.: 00 - Jan 03/12 Page: 15

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SERVICE BULLETIN

Electrical Coating

(Blue Color)

07-001 As required

(c) Stow the electrical wire 5008, install:

Refer to ESPM 20-42-13 and ESPM 20-54-55.

Refer to Fig. A-GHAAA Sheet 01, Lines 9 and 10.

1 Cap NSA936603CC0100 Item 1

3 Tie-Cable NSA935401-03 Item 2

1 Install:

1 Placard set F9239025710200 Item 10

(4) Subtask 335006-831-204-001 - Remove the maintenance light 6LJ and modify the

electrical wire

Work Zones and Access Panels

Zone Access/Work location

310

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

Material necessary to do the job

Kit 335006D01R02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 NSA936603CC0100 1 CAP

2 NSA935401-03 3 TIE

10 F9239025710200 1 PLCRDSET

References

Aircraft Maintenance Manual (AMM) Task 33-31-11-000-801

Elec. Std. Practices Manual (ESPM) 20-42-13

20-54-55

Fig. A-GBDAA

Removal of the Maintenance Light 6LJ

and Modification of the Electrical Wiring

Sheet 01

Sheet 02

Fig. A-GHAAA

Hookup Chart

Sheet 01

Fig. A-GWAAA

Wiring 1

Sheet 01

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-5006

REVISION No.: 00 - Jan 03/12 Page: 16

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@A340-500/600

SERVICE BULLETIN

References

Fig. A-GWBAA

Wiring 2

Sheet 01

WARNING: LET THE LIGHT BECOME COOL BEFORE YOU TOUCH IT. THIS

LIGHT BECOMES VERY HOT WHEN IT IS ON, AND IT CAN BURN

YOU IF YOU TOUCH IT.

(a) Remove the maintenance light 6LJ.

Refer to AMM Task 33-31-11-000-801.

Refer to Fig. A-GBDAA Sheet 01, View B.

1 Remove:

FIN 6LJ

1 Light-Service Area 2LA002606-01 Item (11) Discard

4 Screw NAS1096-3-7 Item (12) Discard

4 Washer NAS1149DN816K Item (13) Discard

2 Nut Item (14) Discard

2 Washer Item (15) Discard

(b) Remove the electrical wire 5014.

Refer to Fig. A-GBDAA Sheet 02, View D.

Fig. A-GWAAA Sheet 01.

Refer to Fig. A-GWBAA Sheet 01.

Refer to Fig. A-GHAAA Sheet 01, Line 11.

1 Remove the bonding connection of the maintenance light 6LJ:

1 Nut MS21042-08 Item (17) Discard

1 Washer NAS1149C0332R Item (6) Discard

1 Screw NAS1096-3-8 Item (16) Discard

2 Remove the electrical wire 5014.

(c) Stow the electrical wire 5005, install:

Refer to ESPM 20-42-13 and ESPM 20-54-55.

Refer to Fig. A-GHAAA Sheet 01, Lines 3 and 4.

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-5006

REVISION No.: 00 - Jan 03/12 Page: 17

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SERVICE BULLETIN

1 Cap NSA936603CC0100 Item 1

3 Tie-Cable NSA935401-03 Item 2

1 Install:

1 Placard set F9239025710200 Item 10

(5) Subtask 335006-831-205-001 - Remove the maintenance lights 7LJ and 8LJ and

modify the electrical wires

Work Zones and Access Panels

Zone Access/Work location

310

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills ELECTRICAL

Material necessary to do the job

Kit 335006D01R02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 NSA936603CC0100 2 CAP

2 NSA935401-03 6 TIE

10 F9239025710200 2 PLCRDSET

References

Aircraft Maintenance Manual (AMM) Task 33-31-11-000-801

Elec. Std. Practices Manual (ESPM) 20-42-13

20-54-55

Fig. A-GBEAA

Removal of the Maintenance Light 7LJ

and 8LJ and Modification of the

Electrical Wiring

Sheet 01

Sheet 02

Sheet 03

Fig. A-GHAAA

Hookup Chart

Sheet 01

Fig. A-GWAAA

Wiring 1

Sheet 01

Fig. A-GWBAA

Wiring 2

Sheet 01

WARNING: LET THE LIGHT BECOME COOL BEFORE YOU TOUCH IT. THIS

LIGHT BECOMES VERY HOT WHEN IT IS ON, AND IT CAN BURN

YOU IF YOU TOUCH IT.

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-5006

REVISION No.: 00 - Jan 03/12 Page: 18

6

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SERVICE BULLETIN

(a) Remove the maintenance lights 7LJ and 8LJ:

Refer to AMM Task 33-31-11-000-801.

Refer to Fig. A-GBEAA Sheet 01, View B.

1 Remove:

FIN 7LJ

1 Light-Service Area 2LA002606-01 Item (11) Discard

FIN 8LJ

1 Light-Service Area 2LA002606-01 Item (11) Discard

8 Screw NAS1096-3-7 Item (12) Discard

8 Washer NAS1149DN816K Item (13) Discard

4 Nut Item (14) Discard

4 Washer Item (15) Discard

(b) Remove the electrical wires 5015 and 5017.

Refer to Fig. A-GBEAA Sheet 01, View E to G.

Refer to Fig. A-GWAAA Sheet 01.

Refer to Fig. A-GWBAA Sheet 01.

Refer to Fig. A-GHAAA Sheet 01, Lines 12 and 14.

1 Remove the bonding connection of the maintenance lights 7LJ and 8LJ:

2 Nut MS21042-08 Item (17) Discard

2 Washer NAS1149C0332R Item (6) Discard

2 Screw NAS1096-3-8 Item (16) Discard

2 Remove the electrical wires 5015 and 5017.

(c) Stow the electrical wires 5007 and 5006, install:

Refer to ESPM 20-42-13 and ESPM 20-54-55.

Refer to Fig. A-GHAAA Sheet 01, Lines 5, 6, 7 and 8.

2 Cap NSA936603CC0100 Item 1

6 Tie-Cable NSA935401-03 Item 2

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-5006

REVISION No.: 00 - Jan 03/12 Page: 19

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@A340-500/600

SERVICE BULLETIN

1 Install:

2 Placard set F9239025710200 Item 10

D. TEST

(1) Subtask 335006-700-201-001 - Test

Work Zones and Access Panels

Zone Access/Work location

310

Manpower Resources

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) Task 33-31-00-720-801

(a) Make sure that the resistance (ohmic) of the bonding connection 5011VN/DC2 of

the maintenance socket 11LJ is correct.

(b) Do the functional test of the maintenance socket 11LJ (Refer to AMM Task

33-31-00-720-801).

E. CLOSE-UP

(1) Subtask 335006-942-201-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 24-41-00-862-801

Task 52-10-00-410-801

(a) Make sure that the work areas are clean and clear of tools and other items of

equipment.

(b) Close the access door 312AR.

(c) De-energize the aircraft electrical circuits (Refer to AMM Task 24-41-00-862-801).

(d) Remove the access platform(s).

(e) Close the AFT passenger/crew door 833 (Refer to AMM Task 52-10-00-410-801).

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-5006

REVISION No.: 00 - Jan 03/12 Page: 20

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@A340-500/600

SERVICE BULLETIN

**CONF ALL

F_SB_335006_6_BAAA_01_00

Z160

A

A

B

FR67

FR66

FR68

FR65

B

C

5032VE

LIGHT

C

3 01

D

SEC19

1LJ

APU

D

NOTE:

01 SAFETY THE CLIP WITH LOCKWIRE (MAT. NO. 19−018)

Figure A-GBAAA - Sheet 01

Modification of the Circuit Breaker Panel 5032VE

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-5006

REVISION No.: 00 - Jan 03/12 Page: 21

6

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@A340-500/600

SERVICE BULLETIN

**CONF ALL

Z310

5872VB /2M

FR83

FR87

A

4LJ

FR84

B C

BEFORE

AFTER

5872VB /2M

FR84

4LJ

B

F

W

D

4LJ C F

W

D

FR84

D

A

2

1

10

D

AFTER

TO

4LJ

MOD. 201683

SB33−5006

F_SB_335006_6_BBAA_01_01

Figure A-GBBAA - Sheet 01

Modification of the Electrical Wiring of the Button Toggle 4LJ

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-5006

REVISION No.: 00 - Jan 03/12 Page: 22

6

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@A340-500/600

SERVICE BULLETIN

**CONF ALL

B

(14)

(15)

(11)

(12)

(13)

(4 POS)

(4 POS)

5872VB /2M

5LJ

11LJ

FR83

FR85

FR87

FR85

B

A

C E

5011VN /DC2

5LJ

Z310

A

F_SB_335006_6_BCAA_01_01

Figure A-GBCAA - Sheet 01

Removal of the Maintenance Light 5LJ and Modification of the Electrical Wire

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-5006

REVISION No.: 00 - Jan 03/12 Page: 23

6

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@A340-500/600

SERVICE BULLETIN

**CONF ALL

5872VB /2M 5LJ

BEFORE

AFTER

FR85

C F

W

D

D

5011VN /DC2

TO 5LJ

TO 11LJ

(16)

(6)

(17)

D

F

W

D

E

5872VB /2M

5011VN /DC2

BEFORE

TO 11LJ

AFTER

F

F

G

(16)

(6)

(17)

FR85

2

1

10

AFTER

MOD. 201683

SB33−5006

G

F_SB_335006_6_BCAA_02_02

Figure A-GBCAA - Sheet 02

Removal of the Maintenance Light 5LJ and Modification of the Electrical Wire

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-5006

REVISION No.: 00 - Jan 03/12 Page: 24

6

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SERVICE BULLETIN

**CONF ALL

(14) B (15)

(11)

(12)

(13)

(4 POS)

(4 POS)

5872VB /2M

FR83

FR85

FR87

FR85

A

6LJ

5012VN /DC2

B

C E

6LJ

Z310

A

F_SB_335006_6_BDAA_01_01

Figure A-GBDAA - Sheet 01

Removal of the Maintenance Light 6LJ and Modification of the Electrical Wiring

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-5006

REVISION No.: 00 - Jan 03/12 Page: 25

6

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@A340-500/600

SERVICE BULLETIN

**CONF ALL

5872VB /2M

BEFORE

AFTER

D

5872VB /2M

TO 6LJ (16)

(6)

(17) 6LJ

STGR18RH

STGR20RH

STGR20RH

STGR18RH

C

VIEW LOOKING FWD

5012VN /DC2

D

BEFORE

E

VIEW LOOKING FWD

F

FR83

FR83

2

1

10

AFTER

MOD. 201683

SB33−5006

F

F_SB_335006_6_BDAA_02_02

Figure A-GBDAA - Sheet 02

Removal of the Maintenance Light 6LJ and Modification of the Electrical Wiring

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-5006

REVISION No.: 00 - Jan 03/12 Page: 26

6

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@A340-500/600

SERVICE BULLETIN

**CONF ALL

B

(14)

(15)

(11)

(12)

(13)

(4 POS)

(4 POS)

5872VB /2M

7LJ

8LJ

LH

RH

TYPICAL

FR83

FR85

FR88

A

7LJ

8LJ

5315VN /DC2

5420VN /DC2

B

C E

Z310

A

F_SB_335006_6_BEAA_01_02

Figure A-GBEAA - Sheet 01

Removal of the Maintenance Light 7LJ and 8LJ and Modification of the Electrical Wiring

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-5006

REVISION No.: 00 - Jan 03/12 Page: 27

6

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@A340-500/600

SERVICE BULLETIN

**CONF ALL

5872VB /2M

C

(16)

(6)

(17)

BEFORE

D

5315VN /DC2

5420VN /DC2

7LJ

8LJ

LH

RH

TYPICAL

RH

LH

F

W

D

FR88

BEFORE

D

F_SB_335006_6_BEAA_02_01

TYPICAL

TO 7LJ LH

TO 8LJ RH

Figure A-GBEAA - Sheet 02

Removal of the Maintenance Light 7LJ and 8LJ and Modification of the Electrical Wiring

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-5006

REVISION No.: 00 - Jan 03/12 Page: 28

6

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@A340-500/600

SERVICE BULLETIN

**CONF ALL

TYPICAL

F

W

D

E

AFTER

F

FR80

5872VB /2M

F_SB_335006_6_BEAA_03_02

2

1

10

AFTER

MOD. 201683

SB33−5006

F

Figure A-GBEAA - Sheet 03

Removal of the Maintenance Light 7LJ and 8LJ and Modification of the Electrical Wiring

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-5006

REVISION No.: 00 - Jan 03/12 Page: 29

6

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SERVICE BULLETIN

**CONF ALL

UNLESS OTHERWISE SPECIFIED PREFIX ALL WIRE IDENTIFICATION WITH ATA−NO.3331

UNLESS OTHERWISE SPECIFIED ALL WIRES ARE CF18 GAUGE

UNLESS OTHERWISE SPECIFIED ALL ROUTES ARE 2M

1

5200VT

312

BEFORE

5003

NOTE:

F

G

H

J

K

B

C

A

D

E

1

2

4LJ

312

5005

5006

5007

5008

6LJ

312

5014

8LJ

312

5015

2

1

2

1

1

2

1

2

5012VN

DC2

5420VN

DC2

50165017

5011VN

DC2

5315VN

DC2

EXISTING WIRE

5LJ

311

7LJ

311

F_SB_335006_6_WAAA_01_00

Figure A-GWAAA - Sheet 01

Wiring 1

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-5006

REVISION No.: 00 - Jan 03/12 Page: 30

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@A340-500/600

SERVICE BULLETIN

**CONF ALL

UNLESS OTHERWISE SPECIFIED PREFIX ALL WIRE IDENTIFICATION WITH ATA−NO.3331

UNLESS OTHERWISE SPECIFIED ALL WIRES ARE CF18 GAUGE

UNLESS OTHERWISE SPECIFIED ALL ROUTES ARE 2M

1

5200VT

312

AFTER

5003

NOTE:

F

G

H

J

K

B

C

A

D

E

1

2

4LJ

312

5005

5006

5007

5008

EXISTING WIRE

REROUTED WIRE

STOWED WIRE

F_SB_335006_6_WBAA_01_00

Figure A-GWBAA - Sheet 01

Wiring 2

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-5006

REVISION No.: 00 - Jan 03/12 Page: 31

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SERVICE BULLETIN

**CONF ALL

UNLESS OTHERWISE SPECIFIED PREFIX ALL WIRE IDENTIFICATION WITH ATA−NO.3331

UNLESS OTHERWISE SPECIFIED ALL WIRES ARE CF18 GAUGE

UNLESS OTHERWISE SPECIFIED ALL ROUTES ARE 2M

BEFORE

NOTE:

EXISTING WIRE

1 2

7.5A

1LJ

1 2

4LJ

312

5002

5032VE

AFT CIRCUIT BREAKER PANEL

AFTER

1 2

7.5A

1LJ

1 2

4LJ

312

5002

5032VE

AFT CIRCUIT BREAKER PANEL

28V DC

GROUND

BUS

28V DC

GROUND

BUS

F_SB_335006_6_WCAA_01_01

Figure A-GWCAA - Sheet 01

Wiring 3

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-5006

REVISION No.: 00 - Jan 03/12 Page: 32

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@A340-500/600

SERVICE BULLETIN

**CONF ALL

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.

3331−5003

3331−5003

3331−5005

3331−5005

3331−5006

3331−5006

3331−5007

3331−5007

3331−5008

3331−5008

312 4LJ

312

2

STOW

2M CF18

2M

2M

2M

2M

2M

2M

2M

2M

2M

CF18

CF18

CF18

CF18

CF18

CF18

CF18

CF18

CF18

312

312

5200VT

5200VT

312

312

311

311

6LJ

8LJ

7LJ

5LJ

1A

1A

STOW

STOW

STOW

STOW

1

1

1

1

312

312

312

312

312

312

312

312

5200VT

5200VT

5200VT

5200VT

5200VT

5200VT

5200VT

5200VT

1B

1B

1C

1C

1D

1E

1D

1E

NSA936501TA1602

EN3155−016M2018

EN3155−016M2018

EN3155−016M2018

EN3155−016M2018

EN3155−016M2018

EN3155−016M2018

EN3155−016M2018

EN3155−016M2018

EN3155−016M2018

EN3155−016M2018

NSA936501TA1602

NSA936501TA1602

NSA936501TA1602

NSA936501TA1602

NSA936603CC0100

NSA936603CC0100

NSA936603CC0100

NSA936603CC0100

NSA936603CC0100

BEFORE

AFTER

BEFORE

BEFORE

BEFORE

BEFORE

AFTER

AFTER

AFTER

AFTER

312

312

311

311

6LJ

8LJ

5LJ

7LJ

2

2

2

2

NSA936501TA1602

NSA936501TA1602

NSA936501TA1602

NSA936501TA1602

3331−5014

3331−5015

3331−5016

3331−5017

2M

2M

2M

2M

CF18

CF18

CF18

CF18

312

312

311

311

5012VN

5420VN

5011VN

5315VN

DC2

DC2

DC2

DC2

DELETE

DELETE

DELETE

DELETE

F929−97007−000−00

NSA936501TA1604

NSA936501TA1604

NSA936501TA1604

NSA936501TA1604

312 6LJ

312 8LJ

311 7LJ

311 5LJ

Figure A-GHAAA - Sheet 01

Hookup Chart

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-5006

REVISION No.: 00 - Jan 03/12 Page: 33

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SERVICE BULLETIN

REPORTING SHEET

TITLE: LIGHTS - SERVICE AREA LIGHTING - REMOVE SERVICE AREA

LIGHTS IN SECTION 19 ACCORDING TO SFAR 88 REQUIREMENTS.

MODIFICATION No.: 201683D46730

Please complete the appropriate item (A or B):

A - SB WILL BE embodied YES/NO (if NO please comment)

If YES, aircraft concerned (as per SB effectivity by default) and planned dates (month/year) of

embodiment:

B - SB HAS BEEN embodied on aircraft:

Operator comments:

From Airline:

Name/Title:

Signature: Date:

If operational documentation is affected (see Paragraph 1.K of this SB): If information is needed prior to

next normal revision or prior to SB embodiment, please indicate required service(s):

Either: Modification Operational Impact (MOI), if available YES/NO

Or : Intermediate revision YES/NO

Important Information: This SB will only be incorporated in your maintenance and operational

documentation if this sheet is returned to Airbus and signed by a duly authorised representative. With

the next feasible revision, this will result in

- Updating of maintenance documentation to show pre and post SB data.

- Updating of maintenance and operational documentation to show post SB data after embodiment.

If this SB requires previous or simultaneous accomplishment of other SBs, Airbus shall automatically

include them in the manual revisions. Refer to SIL 00-037 for detailed information.

Please return this completed sheet to:

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX FRANCE

Attn: SDC32 Technical Data and Documentation Services

FAX: (+33) 5 61 93 28 06

e-mail: sb.reporting@airbus.com

or via your Resident Customer Support Office.

Alternatively, SB lists via letters or fax are also accepted.

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-5006

REVISION No.: 00 - Jan 03/12 Page: 1

6

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

SERVICE BULLETIN

QUALITY PERCEPTION FORM

Use this form to tell us what is your perception of the quality of this Service Bulletin. The reported data

that you provide us will be used to analyse areas of difficulties and to take corrective action to further

improve the quality of our Service Bulletins.

We thank you for the time you have taken in completing this form.

(Please rate on a scale of 1 to 4, with 4 being the highest score)

- Quality rating of this SB 4321

- Quality rating of the Accomplishment Instructions 4321

- Quality rating of the Illustrations 4321

- Is this SB easy to understand ? Y/N

If you have had difficulties in the accomplishment of this SB please quote below the area(s) and give a

short description of the issue.

Planning Material Instructions

X Effectivity X Kit content X Preparation

X Reason X List of Materials Operator Supplied X Mod/Inspection

X Manpower X Industry support X Test

X References X Re-identification X Close-Up

X Publication X Tooling X Illustrations

Comments:

Operator: Date:

Name/Title:

Please return this form to:

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX FRANCE

Attn : SEM4 Service Bulletins Management

FAX : (33) 5 61 93 42 51

Or via your Resident Customer Support Office.

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-5006

REVISION No.: 00 - Jan 03/12 Page: 1

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.