# @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: 34 

### TITLE: NAVIGATION - AOA - INSTALL AOA PROBES IN MIXED CONFIGURATION - THALES FOR CAPT AND FIRST OFFICER AND UTAS ON STANDBY **CONF ALL MODIFICATIONS MODIFICATION CLASSIFICATION MAJOR None MINOR 204937S33428 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 The aim of this modification is to allow the airlines to fly in a mixed Angle of Attack (AOA) configuration. This Service Bulletin requires the replacement of two UTAS AoA probes (FINs 3FP1 and 3FP2) PN 0861ED (installed by Mod. No. 46921S14694) or PN 0861ED2 (installed by Mod. No. 204294S33100 or Service Bulletin No. A340-34-5102) by two THALES AoA probes PN C16291AB. The accomplishment of this Service Bulletin will allow the airlines to fly in mixed AoA configurations. 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: Mar 26/15 SERVICE BULLETIN No.: A340-34-5105 REVISION No.: 00 - Mar 26/15 Page: 1 5

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# @A340-500/600 SERVICE BULLETIN SUMMARY MATERIAL PRICE INFORMATION **CONF 001 MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Equipment BFEA01 1 See SB AOA Probes **CONF 002 MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Equipment BFEA02 1 See SB AOA Probes EFFECTIVITY **CONF ALL This Service Bulletin is applicable to this (these) operator(s) :

16R 25R 31V 32P 81Q AIB CES HFM I2L MHK THA VIR CONCURRENT REQUIREMENTS **CONF 001 None **CONF 002 None REFERENCES / REPERCUSSIONS **CONF ALL TFU None OEB None AOT None SIL None LINE MAINTENANCE AFFECTED No LIFE LIMIT None OTHER Operator Information Transmission (OIT) No. 999.0017/15 NATURE OF THE WORK AIRCRAFT NO EQUIPMENT YES HARD NO
DATE: Mar 26/15 SERVICE BULLETIN No.: A340-34-5105 REVISION No.: 00 - Mar 26/15 Page: 2 5

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# @A340-500/600 SERVICE BULLETIN SUMMARY SOFT NO OBRM NO MANPOWER **CONF 001 Task 345105-831-801-001: Modification by Replacement of the two AOA Probes (FINs 3FP1 and 3FP2) on Aircraft TOTAL MANHOURS 4.50 ELAPSED TIME (HOURS) 3.50 **CONF 002 Task 345105-831-801-001: Modification by Replacement of the two AOA Probes (FINs 3FP1 and 3FP2) on Aircraft TOTAL MANHOURS 4.50 ELAPSED TIME (HOURS) 3.50 APPENDICES **CONF ALL Appendix 01 - Elapsed Time Assumptions

DATE: Mar 26/15 SERVICE BULLETIN No.: A340-34-5105 REVISION No.: 00 - Mar 26/15 Page: 3 5

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# @A340-500/600 SERVICE BULLETIN SUMMARY

**CONF ALL

FR1 FR20
Z120 

### A

FR19 FR18



## A 3FP2

3FP1



### A

TYPICAL INSTALLATION

F_SB_345105_5_SAAA_01_00 Figure A-FSAAA - Sheet 01

DATE: Mar 26/15 SERVICE BULLETIN No.: A340-34-5105 REVISION No.: 00 - Mar 26/15 Page: 4 5

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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



# MANDATORY MANDATORY MANDATORY
ATA SYSTEM: 34 

### TITLE: NAVIGATION - AOA - INSTALL AOA PROBES IN MIXED CONFIGURATION - THALES FOR CAPT AND FIRST OFFICER AND UTAS ON STANDBY MODIFICATION No.: 204937S33428 This document contains AIRBUS PROPRIETARY INFORMATION and shall at all times remain the property of AIRBUS; no intellectual property right or licence is granted by AIRBUS in connection with any information contained in it. It is delivered on the express condition that said document and the information contained in it shall be treated as confidential, shall not be used for any purpose other than that for which it is hereby delivered. It shall not be disclosed in whole or in part to third parties and shall not be duplicated in any manner (except for the purposes of performing the tasks described hereunder and provided that any recipient of such document shall comply with the conditions herein), without AIRBUS prior written consent. 1. PLANNING INFORMATION **CONF ALL A. EFFECTIVITY NOTE: This modification is applicable by Service Bulletin only. NOTE: This Service Bulletin is only applicable to aircraft equipped with UTAS AOA PN 0861ED or PN 0861ED2. NOTE: This Service Bulletin is only applicable to aircraft on which Mod. No. 46921S14694 (INSTALL ANGLE OF ATTACK SENSORS ROSEMOUNT) is embodied. (1) Models 340-541 340-642 (2) Effectivity by MSN 0371 0376 0383 0391 0416 0436 0449 0453 0468 0475 0478 0488 0492 0499 0514 0560 0563 0575 0577 0586 0615 0622 0624 0628 0639 0677 0681 0689 0698 0706 0710 0719 0723 0736 0753 0764-0765 0768 0775 0787 0804 0924 0953

DATE: Mar 26/15 SERVICE BULLETIN No.: A340-34-5105 REVISION No.: 00 - Mar 26/15 Page: 1 5

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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 16R 0615 0622 25R 0924 31V 0436 32P 0560 81Q 0563 AIB 0478 0492 0499 CES 0468 0488 0514 0577 0586 HFM 0391 I2L 0453 0475 MHK 0371 0376 0383 0416 0449 THA 0624 0628 0677 0681 0689 0698 0710 0719 0775 0953 VIR 0575 0639 0706 0723 0736 0753 0764 0765 0768 0787 0804 (4) Configuration by MSN MSN CONFIGURATION 0371 0376 0383 0391 0416 0436 0449 0453 0468 0475 0478 0488 0492 0499 0514 0560 0563 0575 0577 0586 0615 0622 0624 0628 0639 0677 0681 0689 0698 0706 0710 0719 0723 0736 0753 0764 0765 0768 0775 0787 0804 0924 0953 001 002

(5) Configuration definition **CONF 001 Config. 001 is valid for aircraft on which Mod. No. 204294S33100 (Service Bulletin No. A340-34-5102) is not embodied. **CONF 002 Config. 002 is valid for aircraft on which Mod. No. 204294S33100 (Service Bulletin No. A340-34-5102) is embodied. (6) Material Effectivity **CONF 001 MATERIAL QTY PER A/C SEE NOTES Equipment BFEA01 1 **CONF 002 MATERIAL QTY PER A/C SEE NOTES Equipment BFEA02 1

DATE: Mar 26/15 SERVICE BULLETIN No.: A340-34-5105 REVISION No.: 00 - Mar 26/15 Page: 2 5

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# @A340-500/600 SERVICE BULLETIN
**CONF ALL B. CONCURRENT REQUIREMENTS **CONF 001 None **CONF 002 None **CONF ALL C. REASON (1) History The aim of this modification is to allow the airlines to fly in a mixed Angle of Attack (AOA) configuration. (2) Objective/Action This Service Bulletin requires the replacement of two UTAS AoA probes (FINs 3FP1 and 3FP2) PN 0861ED (installed by Mod. No. 46921S14694) or PN 0861ED2 (installed by Mod. No. 204294S33100 or Service Bulletin No. A340-34-5102) by two THALES AoA probes PN C16291AB. (3) Advantages The accomplishment of this Service Bulletin will allow the airlines to fly in mixed AoA configurations. (4) Operational/Maintenance Consequences None D. DESCRIPTION To accomplish this Service Bulletin it is necessary to : **CONF 001 Task 345105-831-801-001: Modification by Replacement of the two AOA Probes (FINs 3FP1 and 3FP2) on Aircraft (1) Replace the AOA Probe 1 (FIN 3FP1) (2) Replace the AOA Probe 2 (FIN 3FP2) **CONF 002 Task 345105-831-801-001: Modification by Replacement of the two AOA Probes (FINs 3FP1

DATE: Mar 26/15 SERVICE BULLETIN No.: A340-34-5105 REVISION No.: 00 - Mar 26/15 Page: 3 5

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# @A340-500/600 SERVICE BULLETIN and 3FP2) on Aircraft (1) Replace the AOA Probe 1 (FIN 3FP1) (2) Replace the AOA Probe 2 (FIN 3FP2) **CONF ALL E. COMPLIANCE (1) Classification MANDATORY: Service Bulletin must be accomplished. (2) Accomplishment Timescale This Service Bulletin has been classified Mandatory. It is expected that an Airworthiness Directive (AD) published by the European Aviation Safety Agency (EASA) will be issued to confirm this classification. It is anticipated that this Service Bulletin must be done before Mar 31/17, the AD will confirm it but reference should be made to the AD for confirmation of the mandated accomplishment timescale. F. APPROVAL The technical content of this document is approved under the authority of Design Organization 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. **CONF 001 Task 345105-831-801-001: Modification by Replacement of the two AOA Probes (FINs 3FP1 and 3FP2) on Aircraft Get Access 1.00 On Aircraft Replace the AOA Probe 1 (FIN 3FP1) 1.00 Replace the AOA Probe 2 (FIN 3FP2) 1.00 Tests 0.50 Close-Up 1.00 TOTAL MANHOURS 4.50 DATE: Mar 26/15 SERVICE BULLETIN No.: A340-34-5105 REVISION No.: 00 - Mar 26/15 Page: 4 5

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# @A340-500/600 SERVICE BULLETIN
Task 345105-831-801-001: Modification by Replacement of the two AOA Probes (FINs 3FP1 and 3FP2) on Aircraft ELAPSED TIME (HOURS) 3.50 NOTE: For an explanation of the manhours and elapsed time, refer to the Gantt Chart, Fig. A-FAAAA given in Appendix 01 - Elapsed Time Assumptions . **CONF 002 Task 345105-831-801-001: Modification by Replacement of the two AOA Probes (FINs 3FP1 and 3FP2) on Aircraft Get Access 1.00 On Aircraft Replace the AOA Probe 1 (FIN 3FP1) 1.00 Replace the AOA Probe 2 (FIN 3FP2) 1.00 Tests 0.50 Close-Up 1.00 TOTAL MANHOURS 4.50 ELAPSED TIME (HOURS) 3.50 NOTE: For an explanation of the manhours and elapsed time, refer to the Gantt Chart, Fig. A-FAAAA given in Appendix 01 - Elapsed Time Assumptions . **CONF ALL H. WEIGHT AND BALANCE Not Changed I. ELECTRICAL LOAD DATA Not Changed J. REFERENCES **CONF 001 Aircraft Maintenance Manual (AMM) 06-20-00 06-31-53 06-41-53 12-34-24 34-11-19 ATA Common Support Data Dictionary (CSDD), Chapter 2 Elec. Std. Practices Manual (ESPM) 20-55-00 **CONF 002 Aircraft Maintenance Manual (AMM) 06-20-00 06-31-53 06-41-53 12-34-24 34-11-19 ATA Common Support Data Dictionary (CSDD), Chapter 2 Elec. Std. Practices Manual (ESPM) 20-55-00

DATE: Mar 26/15 SERVICE BULLETIN No.: A340-34-5105 REVISION No.: 00 - Mar 26/15 Page: 5 5

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# @A340-500/600 SERVICE BULLETIN
**CONF ALL K. PUBLICATION AFFECTED

Aircraft Wiring List (AWL) Illustrated Parts Catalog (IPC) 34-11-01 34-11-19 L. INTERCHANGEABILITY/MIXABILITY The interchangeability/mixability possibilities are for new or modified parts introduced by the accomplishment of this Service Bulletin. **CONF 001 DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE NOTES AOA Probe 0861ED C16291AB 03 NO (1) NOTE : For definitions of interchangeability codes in column INT., refer to ATA Common Support Data Dictionary (CSDD), Chapter 2. NOTE: Only the mixability configuration(s) and condition(s) stated in this Service Bulletin are approved. NOTE (1) : When AOA PN 0861ED is removed, it may be replaced: - with the AOA PN 0861ED, - with the AOA PN C16291AB only if both AOA probes (FINs 3FP1 and 3FP2) are replaced simultaneously. When the new PN is removed, it must be replaced by the new PN. **CONF 002 DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE NOTES AOA Probe 0861ED2 C16291AB 03 NO (1) NOTE: For definitions of interchangeability codes in column INT., refer to ATA Common Support Data Dictionary (CSDD), Chapter 2. NOTE: Only the mixability configuration(s) and condition(s) stated in this Service Bulletin are approved. NOTE (1) : When AOA PN 0861ED2 is removed, it may be replaced: - with the AOA PN 0861ED2, - with the AOA PN C16291AB only if both AOA probes (FINs 3FP1 and 3FP2) are replaced simultaneously. When the new PN is removed, it must be replaced by the new PN.
DATE: Mar 26/15 SERVICE BULLETIN No.: A340-34-5105 REVISION No.: 00 - Mar 26/15 Page: 6 5

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# @A340-500/600 SERVICE BULLETIN
**CONF ALL M. SPARES AOA Probe 0861ED AOA Probe 0861ED2

DATE: Mar 26/15 SERVICE BULLETIN No.: A340-34-5105 REVISION No.: 00 - Mar 26/15 Page: 7 5

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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 Vendor parts are to be procured from: Equipment BFEA01 Equipment BFEA02 THALES AVIONICS S.A.S. 105, avenue du General Eisenhower BP 63647 TOULOUSE CEDEX 1 FRANCE Attn: Retrofit Manager Tel: +33 5 61 19 76 95 Fax: +33 5 61 19 68 20 e-mail: retrofit@fr.thalesgroup.com (2) Price and Availability From Equipment BFEA01 to Equipment BFEA02 No AIRBUS kit will be provided. Procurement terms for the equipment must be negotiated with the equipment supplier. B. INDUSTRY SUPPORT INFORMATION From Equipment BFEA01 to Equipment BFEA02 Industry support terms for the equipment must be negotiated with the equipment supplier. This Service Bulletin is the subject of an AIRBUS monitored retrofit campaign. For the organization of this retrofit, you are kindly requested to contact AIRBUS retrofit management department. AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX France E-mail: monitored.retrofit@airbus.com Tel: (33) 5 67 19 06 22 Fax: (33) 5 61 93 27 45 C. LIST OF COMPONENTS No Kit

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# @A340-500/600 SERVICE BULLETIN
D. LIST OF MATERIALS - OPERATOR SUPPLIED (1) Consumable Materials None (2) Components NOTE: To accomplish this Service Bulletin it is necessary to use the expendable parts listed in the subsequent referenced AMM task: - AMM Task 34-11-19-400-801. (3) Equipment Equipment BFEA01 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES C16291AB 2 SENSOR 0861ED 03 NOTE: For definitions of interchangeability codes in column INT., refer to ATA Common Support Data Dictionary (CSDD), Chapter 2. NOTE: The above list of components is not an AIRBUS Kit, the required parts shall be ordered as necessary through the given channel. Equipment BFEA02 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES C16291AB 2 SENSOR 0861ED2 03 NOTE: For definitions of interchangeability codes in column INT., refer to ATA Common Support Data Dictionary (CSDD), Chapter 2. NOTE: The above list of components is not an AIRBUS Kit, the required parts shall be ordered as necessary through the given channel. E. PARTS TO BE RE-IDENTIFIED BY OPERATOR None F. TOOLING None

DATE: Mar 26/15 SERVICE BULLETIN No.: A340-34-5105 REVISION No.: 00 - Mar 26/15 Page: 10 5

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# @A340-500/600 SERVICE BULLETIN
3. ACCOMPLISHMENT INSTRUCTIONS Task 345105-831-801-001 - Modification by Replacement of the two AOA Probes (FINs 3FP1 and 3FP2) on Aircraft WARNING : MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONS INCLUDED IN THE REFERENCED PROCEDURES. CAUTION : ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY AND MECHANICALLY SERVICEABLE) . WHEN YOU DO MAINTENANCE WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING, COMPONENTS AND THE WORK AREA AS CLEAN AS POSSIBLE. TO DO THIS: - PUT PROTECTION, SUCH AS PLASTIC SHEETING, CLOTHS, ETC. AS NECESSARY ON WIRING AND COMPONENTS. - REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND OTHER CONTAMINATION. THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION. IF THERE IS CONTAMINATION, REFER TO ESPM 20-55-00. NOTE: The accomplishment instructions of this Service Bulletin include procedures given in other documents or in other sections of the Service Bulletin. When the words "refer to" are used and the operator has a procedure accepted by the local authority he belongs to, the accepted alternative procedure can be used. When the words "in accordance with" are used then the given procedure must be followed. NOTE: The access and close-up instructions, not comprising return to service tests, in this Service Bulletin do not constitute or affect the technical intent of the Service Bulletin. Operators can therefore, as deemed necessary, omit or add access and/or close-up steps to add flexibility to their maintenance operations as long as the technical intent of the Service Bulletin is met within the set parameters. NOTE: Manual titles given in the accomplishment instructions are referred to by acronyms. Refer to paragraph 1.J., References, for the definition of acronyms. NOTE: This Service Bulletin is classified mandatory or expected to be classified mandatory by an Airworthiness Directive (AD). The paragraphs 3.C. and 3.D. in these accomplishment instructions are Required for Compliance (RC) and must be done to comply with the AD. Other paragraphs are recommended and may be deviated from, done as part of other actions or done with accepted methods different from those given in the Service Bulletin, as long as the RC paragraphs can be done and the aircraft can be put back into a serviceable condition.

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# @A340-500/600 SERVICE BULLETIN
Task Associated Data **CONF 001 Zone 121 122 Modified FIN 3FP1 3FP2 Access Door 811 Manpower TOTAL MANHOURS 4.50 ELAPSED TIME (HOURS) 3.50 **CONF 002 Zone 121 122 Modified FIN 3FP1 3FP2 Access Door 811 Manpower TOTAL MANHOURS 4.50 ELAPSED TIME (HOURS) 3.50 **CONF ALL A. GENERAL **CONF 001 (1) Subtask 345105-910-001-001 - Standard Practices Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-20-00, Page Block 001 06-31-53, Page Block 001 06-41-53, Page Block 001 (a) For the Frame (FR) identification, refer to AMM 06-31-53, Page Block 001. (b) For the identification of zones, refer to AMM 06-20-00, Page Block 001. (c) For the identification of access panels, refer to AMM 06-41-53, Page Block 001.

DATE: Mar 26/15 SERVICE BULLETIN No.: A340-34-5105 REVISION No.: 00 - Mar 26/15 Page: 12 5

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# @A340-500/600 SERVICE BULLETIN (2) Subtask 345105-839-001-001 - Administrative Manpower Resources Skills NON SPECIFIC Write in the applicable aircraft records that you have done all the work given in this Service Bulletin. **CONF 002 (1) Subtask 345105-910-001-001 - Standard Practices Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-20-00, Page Block 001 06-31-53, Page Block 001 06-41-53, Page Block 001 (a) For the Frame (FR) identification, refer to AMM 06-31-53, Page Block 001. (b) For the identification of zones, refer to AMM 06-20-00, Page Block 001. (c) For the identification of access panels, refer to AMM 06-41-53, Page Block 001. (2) Subtask 345105-839-001-001 - Administrative Manpower Resources Skills NON SPECIFIC Write in the applicable aircraft records that you have done all the work given in this Service Bulletin. **CONF ALL B. PREPARATION **CONF 001 (1) Subtask 345105-941-001-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802 Task 34-11-19-000-801 NOTE: The items given in this note shall be considered as the basic Aircraft configuration before you start a maintenance task: - Aircraft on the ground resting on landing gear (the ground safety DATE: Mar 26/15 SERVICE BULLETIN No.: A340-34-5105 REVISION No.: 00 - Mar 26/15 Page: 13 5

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# @A340-500/600 SERVICE BULLETIN locks and the wheel chocks are in position on the landing gear) - Engine shut down, thrust reversers closed and locked - Aircraft in clean configuration - Parking brake applied - Aircraft electrical network de-energized - Hydraulic systems depressurized - Access to the cockpit and cabin is available - All circuit breakers are in closed position - All controls in NORM, AUTO or OFF position (a) Make sure that the aircraft is electrically grounded, refer to AMM Task 12-34-24-860-802. (b) Do the Job Set-up procedure as specified in the removal of the AOA Probes (FINs 3FP1 and 3FP2), refer to AMM Task 34-11-19-000-801. **CONF 002 (1) Subtask 345105-941-001-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802 Task 34-11-19-000-801 NOTE: The items given in this note shall be considered as the basic Aircraft configuration before you start a maintenance task: - Aircraft on the ground resting on landing gear (the ground safety locks and the wheel chocks are in position on the landing gear) - Engine shut down, thrust reversers closed and locked - Aircraft in clean configuration - Parking brake applied - Aircraft electrical network de-energized - Hydraulic systems depressurized - Access to the cockpit and cabin is available - All circuit breakers are in closed position DATE: Mar 26/15 SERVICE BULLETIN No.: A340-34-5105 REVISION No.: 00 - Mar 26/15 Page: 14 5

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# @A340-500/600 SERVICE BULLETIN - All controls in NORM, AUTO or OFF position (a) Make sure that the aircraft is electrically grounded, refer to AMM Task 12-34-24-860-802. (b) Do the Job Set-up procedure as specified in the removal of the AOA Probes (FINs 3FP1 and 3FP2), refer to AMM Task 34-11-19-000-801. **CONF ALL C. PROCEDURE **CONF 001 (1) Subtask 345105-831-001-001 - Replace the AOA Probe 1 (FIN 3FP1) Work Zones and Access Panels Zone Access/Work location 121 Access Door 811 Work location from Frame 18 to Frame 19 Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills NON SPECIFIC Material necessary to do the job Equipment BFEA01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES C16291AB 1 SENSOR NOTE: The above list of components is not an AIRBUS Kit, the required parts shall be ordered as necessary through the given channel. References Aircraft Maintenance Manual (AMM) Task 34-11-19-000-801 Task 34-11-19-400-801 (a) Remove: Refer to AMM Task 34-11-19-000-801 FIN 3FP1 1 AOA Probe 0861ED (b) Install: Refer to AMM Task 34-11-19-400-801
DATE: Mar 26/15 SERVICE BULLETIN No.: A340-34-5105 REVISION No.: 00 - Mar 26/15 Page: 15 5

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# @A340-500/600 SERVICE BULLETIN

FIN 3FP1 1 AOA Probe C16291AB

(2) Subtask 345105-831-002-001 - Replace the AOA Probe 2 (FIN 3FP2) Work Zones and Access Panels Zone Access/Work location 122 Access Door 811 Work location from Frame 18 to Frame 19 Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills NON SPECIFIC Material necessary to do the job Equipment BFEA01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES C16291AB 1 SENSOR NOTE: The above list of components is not an AIRBUS Kit, the required parts shall be ordered as necessary through the given channel. References Aircraft Maintenance Manual (AMM) Task 34-11-19-000-801 Task 34-11-19-400-801 (a) Remove: Refer to AMM Task 34-11-19-000-801 FIN 3FP2 1 AOA Probe 0861ED (b) Install: Refer to AMM Task 34-11-19-400-801 FIN 3FP2 1 AOA Probe C16291AB

DATE: Mar 26/15 SERVICE BULLETIN No.: A340-34-5105 REVISION No.: 00 - Mar 26/15 Page: 16 5

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# @A340-500/600 SERVICE BULLETIN
**CONF 002 (1) Subtask 345105-831-001-002 - Replace the AOA Probe 1 (FIN 3FP1) Work Zones and Access Panels Zone Access/Work location 121 Access Door 811 Work location from Frame 18 to Frame 19 Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills NON SPECIFIC Material necessary to do the job Equipment BFEA02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES C16291AB 1 SENSOR NOTE: The above list of components is not an AIRBUS Kit, the required parts shall be ordered as necessary through the given channel. References Aircraft Maintenance Manual (AMM) Task 34-11-19-000-801 Task 34-11-19-400-801 (a) Remove: Refer to AMM Task 34-11-19-000-801 FIN 3FP1 1 AOA Probe 0861ED2 (b) Install: Refer to AMM Task 34-11-19-400-801 FIN 3FP1 1 AOA Probe C16291AB

(2) Subtask 345105-831-002-002 - Replace the AOA Probe 2 (FIN 3FP2) Work Zones and Access Panels Zone Access/Work location 122 Access Door 811 Work location from Frame 18 to Frame 19

DATE: Mar 26/15 SERVICE BULLETIN No.: A340-34-5105 REVISION No.: 00 - Mar 26/15 Page: 17 5

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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 NON SPECIFIC Material necessary to do the job Equipment BFEA02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES C16291AB 1 SENSOR NOTE: The above list of components is not an AIRBUS Kit, the required parts shall be ordered as necessary through the given channel. References Aircraft Maintenance Manual (AMM) Task 34-11-19-000-801 Task 34-11-19-400-801 (a) Remove: Refer to AMM Task 34-11-19-000-801 FIN 3FP2 1 AOA Probe 0861ED2 (b) Install: Refer to AMM Task 34-11-19-400-801 FIN 3FP2 1 AOA Probe C16291AB **CONF ALL D. TEST **CONF 001 (1) Subtask 345105-700-001-001 - Testing Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 34-11-19-400-801

DATE: Mar 26/15 SERVICE BULLETIN No.: A340-34-5105 REVISION No.: 00 - Mar 26/15 Page: 18 5

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# @A340-500/600 SERVICE BULLETIN (a) Job Set-up: 1 Remove the safety clip(s) and/or tag(s) and close/unlock the circuit breaker(s) as specified after the installation of the AOA Probes (FINs 3FP1 and 3FP2), refer to AMM Task 34-11-19-400-801. (b) Procedure: 1 Do the test procedure as specified after the installation of the AOA Probes (FINs 3FP1 and 3FP2), refer to AMM Task 34-11-19-400-801. **CONF 002 (1) Subtask 345105-700-001-001 - Testing Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 34-11-19-400-801 (a) Job Set-up: 1 Remove the safety clip(s) and/or tag(s) and close/unlock the circuit breaker(s) as specified after the installation of the AOA Probes (FINs 3FP1 and 3FP2), refer to AMM Task 34-11-19-400-801. (b) Procedure: 1 Do the test procedure as specified after the installation of the AOA Probes (FINs 3FP1 and 3FP2), refer to AMM Task 34-11-19-400-801. **CONF ALL E. CLOSE-UP **CONF 001 (1) Subtask 345105-942-001-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 34-11-19-400-801 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Do the Close-up procedure as specified after the installation of the AOA Probes (FINs 3FP1 and 3FP2), refer to AMM Task 34-11-19-400-801. (c) Put the aircraft back to its initial configuration. DATE: Mar 26/15 SERVICE BULLETIN No.: A340-34-5105 REVISION No.: 00 - Mar 26/15 Page: 19 5

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# @A340-500/600 SERVICE BULLETIN
**CONF 002 (1) Subtask 345105-942-001-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 34-11-19-400-801 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Do the Close-up procedure as specified after the installation of the AOA Probes (FINs 3FP1 and 3FP2), refer to AMM Task 34-11-19-400-801. (c) Put the aircraft back to its initial configuration.

DATE: Mar 26/15 SERVICE BULLETIN No.: A340-34-5105 REVISION No.: 00 - Mar 26/15 Page: 20 5

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# @A340-500/600 SERVICE BULLETIN Appendix 01 - Elapsed Time Assumptions **CONF ALL (1) For an explanation of the manhours and elapsed time, refer to the following Gantt Chart.

DATE: Mar 26/15 SERVICE BULLETIN No.: A340-34-5105 REVISION No.: 00 - Mar 26/15 Page: 1 5

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# @A340-500/600 SERVICE BULLETIN Appendix 01 - Elapsed Time Assumptions

**CONF ALL

ELAPSED TIME ASSUMPTION SERVICE BULLETIN No A340−34−5105

GET ACCESS MH ET/S

SB ELAPSED TIME 4.50 3.50 STEPS

1.00 1.00

0

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

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

1

: : SB ELAPSED TIME (HOURS) 2 4 1 3

IF A VSB IS INVOLVED, THE ASSOCIATED MANHOURS ARE NOT REFLECTED IN THIS GANTT CHART. REPLACEMENT OF THE AOA PROBE 1.00 1.00 1

CLOSE

−UP 1.00 1.00 1

TOTAL MANHOURS 1.00 1.00 1

TEST 0.50 0.50 1 FIN 3FP1

REPLACEMENT OF THE AOA PROBE FIN 3FP2

F_SB_345105_5_AAAA_01_00 Figure A-FAAAA - Sheet 01 Gantt Chart
DATE: Mar 26/15 SERVICE BULLETIN No.: A340-34-5105 REVISION No.: 00 - Mar 26/15 Page: 2 5

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# @A340-500/600 SERVICE BULLETIN REPORTING SHEET 

### TITLE: NAVIGATION - AOA - INSTALL AOA PROBES IN MIXED CONFIGURATION - THALES FOR CAPT AND FIRST OFFICER AND UTAS ON STANDBY MODIFICATION No.: 204937S33428 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: Mar 26/15 SERVICE BULLETIN No.: A340-34-5105 REVISION No.: 00 - Mar 26/15 Page: 1 5

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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: Mar 26/15 SERVICE BULLETIN No.: A340-34-5105 REVISION No.: 00 - Mar 26/15 Page: 1 5

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