# @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. 

# MANDATORYMANDATORYMANDATORY 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 REVISION No.: 00 - Jan 03/12 Page: 1 6

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# @A340-500/600 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 REVISION No.: 00 - Jan 03/12 Page: 2 6

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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 6

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# @A340-500/600 SERVICE BULLETIN SUMMARY

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# @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



# MANDATORYMANDATORYMANDATORY 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 REVISION No.: 00 - Jan 03/12 Page: 1 6

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# @A340-500/600 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 REVISION No.: 00 - Jan 03/12 Page: 2 6

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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 REVISION No.: 00 - Jan 03/12 Page: 3 6

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# @A340-500/600 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 6

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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 REVISION No.: 00 - Jan 03/12 Page: 5 6

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# @A340-500/600 SERVICE BULLETIN

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# @A340-500/600 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 REVISION No.: 00 - Jan 03/12 Page: 7 6

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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 REVISION No.: 00 - Jan 03/12 Page: 8 6

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# @A340-500/600 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 REVISION No.: 00 - Jan 03/12 Page: 9 6

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# @A340-500/600 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
DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-5006 REVISION No.: 00 - Jan 03/12 Page: 10 6

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# @A340-500/600 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

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-5006 REVISION No.: 00 - Jan 03/12 Page: 11 6

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# @A340-500/600 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 REVISION No.: 00 - Jan 03/12 Page: 12 6

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# @A340-500/600 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 6

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# @A340-500/600 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 6

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# @A340-500/600 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 6

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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 6

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# @A340-500/600 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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# @A340-500/600 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 6

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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 6

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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:** SAFETY THE CLIP WITH LOCKWIRE (MAT. NO. 19−018) 01 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 FR85FR87

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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# @A340-500/600 SERVICE BULLETIN

**CONF ALL



## B (14) (15) (11) (12) (13) (4 POS) (4 POS)

5872VB /2M FR83 FR85FR87

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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# @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 

## BEFORE

5003

**NOTE:** F G H J K B C A D E 1 2 4LJ 312 5005 5006 5007 5008 6LJ 3125014

8LJ 3125015 2 1 2 1

1 2 1 2 5012VN DC2 5420VN DC250165017

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 6

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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 6

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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 

## 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 6

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# @A340-500/600 SERVICE BULLETIN

**CONF ALL

L I N E ZONE OR PANEL TERM. TERMINAL P/N WIRE IDENT C0L ROUTE GAUGE LENGTH MM INCH ZONE OR PANEL ELEC. IDENT TERM. TERMINAL P/N INSTRUCTIONS 

## END 2 LEAD END 1

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 4LJ 312 312 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 6

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# @A340-500/600 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

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# @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

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