# @A340 SERVICE BULLETIN SUMMARY AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Tel : (33) 5 61 93 33 33 Telex : AIRBU 530526F Fax : (33) 5 61 93 42 51 This summary is for information only and is not approved for modification of the aircraft. ATA SYSTEM: 27 

### TITLE: FLIGHT CONTROLS - TRIMMABLE HORIZONTAL STABILIZER ACTUATOR - REPLACE THSA PN 47147-700 BY THSA PN 47172-530 **CONF ALL MODIFICATIONS MODIFICATION CLASSIFICATION MAJOR None MINOR 202802S32403 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 First delivered aircraft were equipped with Trimmable Horizontal Stabilizer Actuator (THSA) 47147 family which are no longer produced. THSA 47172 family is the current production standard. This Service Bulletin covers the introduction of THSA PN 47172-530 in replacement of THSA PN 47147-700. Accomplishment of this Service Bulletin allows: - Aircraft configuration evolution towards the current THSA family production standard, - Anticipation on obsolescence of THSA 47147 family, - Resolution of in-service issues encountered with THSA 47147 family (Technical Follow Up (TFU) 27.44.51.010). Accomplishment of this Service Bulletin cancels the inspection requirements of Service Bulletin No. A340-27-4175. GENERAL EVALUATION EVALUATION TABLE COMPLIANCE RECOMMENDED (1) CANCELS INSPECTION SB YES POTENTIAL AD NO A/C OPERATION AFFECTED NO

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# @A340 SERVICE BULLETIN SUMMARY EVALUATION TABLE 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 recommended to be accomplished to prevent significant operational disruptions. 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 THSA **CONF 002 MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Equipment BFEA01 1 See SB THSA EFFECTIVITY **CONF ALL This Service Bulletin is applicable to this (these) operator(s) :

47W 56W AAW AFR ALK ARG CCA CES CPA DGA DLH FIN GFA HFY I2L IBE IRC KAC KNE LAN M3R MAU MDG MSR NMB PAL QAF RJA S3R SAA SFB SLM SWR TAP THY UAE VCV VIR CONCURRENT REQUIREMENTS Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishment of the following Service Bulletin(s) or the equivalent production modification(s): Service Bulletin No. A340-27-4143 NOTE: Service Bulletin No.A340-27-4143 (FLIGHT CONTROLS - TRIMMABLE HORIZONTAL STABILIZER - INTRODUCE MODIFIED THSA (PN 47147-700)). REFERENCES / REPERCUSSIONS TFU 27.44.51.010 OEB None AOT None SIL None LINE MAINTENANCE AFFECTED No

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# @A340 SERVICE BULLETIN SUMMARY
LIFE LIMIT None OTHER None NATURE OF THE WORK AIRCRAFT NO EQUIPMENT YES HARD NO SOFT NO OBRM NO MANPOWER Task 274187-831-801-001: Modification TOTAL MANHOURS 19.00 ELAPSED TIME (HOURS) 19.00 APPENDICES None

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# @A340 SERVICE BULLETIN SUMMARY

**CONF ALL

FR87

FR80 − Z311 Z312 

### A **B**

1CS



## B 312AR



## A

F_SB_274187_5_SAAA_01_00 Figure A-FSAAA - Sheet 01

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# @A340 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 ATA SYSTEM: 27 

### TITLE: FLIGHT CONTROLS - TRIMMABLE HORIZONTAL STABILIZER ACTUATOR - REPLACE THSA PN 47147-700 BY THSA PN 47172-530 MODIFICATION No.: 202802S32403 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. (1) Models 340-211 340-212 340-213 340-311 340-312 340-313 (2) Effectivity by MSN 0002-0006 0009 0011 0013-0015 0018-0029 0031-0035 0038 0041 0043-0044 0046-0049 0051-0053 0056-0058 0061 0063 0074-0076 0078-0081 0084-0085 0088-0091 0093-0094 0101 0104 0114-0115 0117 0123 0125-0126 0128-0129 0131 0133-0137 0139 0141-0142 0145-0147 0149-0152 0154 0156-0161 0163-0164 0166-0170 0173-0176 0178-0180 0182 0185-0187 0190 0192-0194 0196-0197 0199 0201-0202 0204 0207-0208 0210 0212-0218 0220-0221 0225 0227-0228 (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.

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# @A340 SERVICE BULLETIN

OPERATOR MSN 47W 0009 56W 0003 0011 0013 0015 0018 0019 0021 AAW 0151 AFR 0029 0078 0084 0186 0207 ALK 0032 0033 0034 ARG 0048 0063 0074 0080 0085 0093 0094 0123 0126 0128 CCA 0192 0199 0201 CES 0129 0131 0141 0161 0182 CPA 0136 0137 0142 0147 0157 0160 0208 0218 0220 0227 0228 DGA 0075 0081 DLH 0020 0024 0027 0028 0035 0052 0053 0056 0135 0158 0213 FIN 0058 0168 0174 GFA 0212 0215 HFY 0117 0133 I2L 0216 IBE 0005 0088 0125 0134 0145 0146 0170 0193 0217 0221 IRC 0002 KAC 0089 0090 0101 0104 KNE 0004 LAN 0167 M3R 0061 MAU 0076 0152 0194 MDG 0210 MSR 0156 0159 0178 NMB 0047 0051 PAL 0173 0176 0187 0196 QAF 0026 RJA 0014 0022 0038 0043 S3R 0204 SAA 0006 0197 SFB 0046 SLM 0049 SWR 0150 0154 0169 0175 0179 TAP 0041 0044 0079 0091 THY 0023 0025 0057 0115 0180 UAE 0139 0149 0163 0166 0185 0190 0202 VCV 0031 VIR 0114 0164 0214 0225

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# @A340 SERVICE BULLETIN (4) Configuration by MSN MSN CONFIGURATION 0002 0003 0005 0013 0015 0020 0023 0024 0025 0027 0028 0029 0032 0033 0034 0035 0041 0044 0047 0048 0049 0051 0052 0053 0056 0057 0058 0076 0078 0079 0084 0088 0089 0090 0091 0093 0094 0101 0104 0114 0115 0117 0123 0125 0126 0128 0129 0131 0133 0134 0135 0136 0137 0139 0141 0142 0145 0146 0147 0149 0150 0152 0154 0157 0158 0160 0161 0163 0164 0166 0167 0168 0169 0170 0173 0174 0175 0176 0179 0180 0182 0185 0186 0187 0190 0192 0193 0194 0196 0197 0199 0201 0202 0207 0208 0210 0212 0213 0214 0215 0216 0217 0218 0220 0221 0225 0227 0228 002

0004 0006 0009 0011 0014 0018 0019 0021 0022 0026 0031 0038 0043 0046 0061 0063 0074 0075 0080 0081 0085 0151 0156 0159 0178 0204 001

(5) Configuration definition **CONF 001 Config. 001 is valid for Standard 2 (ST2) and Standard 5 (ST5) aircraft. **CONF 002 Config. 002 is valid for Standard 1 (ST1) and Standard 4 (ST4) aircraft. (6) Material Effectivity MATERIAL QTY PER A/C SEE NOTES Equipment BFEA01 1 B. CONCURRENT REQUIREMENTS Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishment of the following Service Bulletin(s) or the equivalent production modification(s): Service Bulletin No. A340-27-4143 NOTE: Service Bulletin No.A340-27-4143 (FLIGHT CONTROLS - TRIMMABLE HORIZONTAL STABILIZER - INTRODUCE MODIFIED THSA (PN 47147-700)). C. REASON (1) History First delivered aircraft were equipped with Trimmable Horizontal Stabilizer Actuator (THSA) 47147 family which are no longer produced. THSA 47172 family is the current production standard. (2) Objective/Action This Service Bulletin covers the introduction of THSA PN 47172-530 in replacement of THSA PN 47147-700.
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# @A340 SERVICE BULLETIN (3) Advantages Accomplishment of this Service Bulletin allows: - Aircraft configuration evolution towards the current THSA family production standard, - Anticipation on obsolescence of THSA 47147 family, - Resolution of in-service issues encountered with THSA 47147 family (Technical Follow Up (TFU) 27.44.51.010). Accomplishment of this Service Bulletin cancels the inspection requirements of Service Bulletin No. A340-27-4175. (4) Operational/Maintenance Consequences None D. DESCRIPTION To accomplish this Service Bulletin it is necessary to : **CONF 001 Task 274187-831-801-001: Modification (1) Remove the THSA. (2) Install the THSA. **CONF 002 Task 274187-831-801-001: Modification (1) Remove the THSA. (2) Install the THSA. **CONF ALL E. COMPLIANCE (1) Classification RECOMMENDED: Service Bulletin recommended to be accomplished to prevent significant operational disruptions. (2) Accomplishment Timescale Accomplishment of this Service Bulletin is recommended at the earliest opportunity where manpower and facilities are available.

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# @A340 SERVICE BULLETIN

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. Task 274187-831-801-001: Modification Get Access 1.00 On Aircraft Remove the THSA. 8.00 Install the THSA. 8.00 Tests 1.00 Close-Up 1.00 TOTAL MANHOURS 19.00 ELAPSED TIME (HOURS) 19.00 H. WEIGHT AND BALANCE **CONF 001 The weight and balance estimates given in this Service Bulletin are based on the Manufacturer’s Empty Weight (MEW) and do not include operator item’s. For the definition of MEW and operator’s items refer to Weight and Balance Manual (WBM) Chapter 1-00-07. Manufacturers Empty Weight +2.2 KG (+4.8501 LB) Effect on Balance +134.2 KGM (+970.668 LB.FT ) **CONF 002 The weight and balance estimates given in this Service Bulletin are based on the Manufacturer’s Empty Weight (MEW) and do not include operator item’s. For the definition of MEW and operator’s items refer to Weight and Balance Manual (WBM) Chapter 1-00-07. Manufacturers Empty Weight +2.2 KG (+4.8501 LB) Effect on Balance +143 KGM (+1034.319 LB.FT )

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# @A340 SERVICE BULLETIN

**CONF ALL I. ELECTRICAL LOAD DATA Not Changed J. REFERENCES **CONF 001 Aircraft Maintenance Manual (AMM) 12-34-24 27-44-51 ATA Common Support Data Dictionary (CSDD), Chapter 2 Elec. Std. Practices Manual (ESPM) 20-55-00 Service Bulletin (SB) A340-27-4143 Weight and Balance Manual (WBM) Weight and Balance Manual (WBM) Chapter 1-00-07 **CONF 002 Aircraft Maintenance Manual (AMM) 12-34-24 27-44-51 ATA Common Support Data Dictionary (CSDD), Chapter 2 Elec. Std. Practices Manual (ESPM) 20-55-00 Service Bulletin (SB) A340-27-4143 Weight and Balance Manual (WBM) Weight and Balance Manual (WBM) Chapter 1-00-07 **CONF ALL K. PUBLICATION AFFECTED

Aircraft Wiring List (AWL) Illustrated Parts Catalog (IPC) 27-44-04 L. INTERCHANGEABILITY/MIXABILITY **CONF 001 DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE NOTES THS Actuator 47147-700 47172-530 01 Not Applicable NOTE: For definitions of interchangeability codes in column INT., refer to ATA Common Support Data Dictionary (CSDD), Chapter 2.

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# @A340 SERVICE BULLETIN

**CONF 002 DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE NOTES THS Actuator 47147-700 47172-530 01 Not Applicable NOTE: For definitions of interchangeability codes in column INT., refer to ATA Common Support Data Dictionary (CSDD), Chapter 2. **CONF ALL M. SPARES THS Actuator 47147-700

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# @A340 SERVICE BULLETIN

This Page Intentionally Left Blank

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# @A340 SERVICE BULLETIN

2. MATERIAL INFORMATION **CONF ALL A. MATERIAL - PRICE AND AVAILABILITY (1) Procurement Addresses Vendor parts are to be procured from : Equipment BFEA01 UTC AEROSPACE 13 Avenue de l’eguillette ST-OUEN L’AUMONE 95310 FRANCE Tel: (33) 1 34 32 63 00 Fax: (33) 1 34 32 63 10 (2) Price and Availability No AIRBUS kit will be provided. Procurement terms for the equipment must be negotiated with the equipment supplier. B. INDUSTRY SUPPORT INFORMATION AIRBUS will not provide industry support for accomplishment of this Service Bulletin. C. LIST OF COMPONENTS No Kit D. LIST OF MATERIALS - OPERATOR SUPPLIED (1) Consumable Materials NOTE: To accomplish this Service Bulletin it is necessary to use the expendable parts listed in AMM Task 27-44-51-400-801. (2) Components None (3) Equipment Equipment BFEA01 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 47172-530 1 ACTUATOR 47147-700 01 (1) NOTE: For definitions of interchangeability codes in column INT., refer to ATA Common Support Data Dictionary (CSDD), Chapter 2.

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# @A340 SERVICE BULLETIN

NOTE (1): 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 (1) Tooling - Price and Availability None (2) Tools NOTE: To accomplish this Service Bulletin it is necessary to use the tools listed in AMM Task 27-44-51-000-801 and AMM Task 27-44-51-400-801. (3) Special Tools None

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# @A340 SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS Task 274187-831-801-001 - Modification WARNING: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONS INCLUDED IN THE REFERENCED PROCEDURES. CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY AND MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENANCE WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING, COMPONENTS AND THE WORK AREA AS CLEAN AS POSSIBLE. TO DO THIS: - PUT PROTECTION, SUCH AS PLASTIC SHEETING, CLOTHS, ETC; AS NECESSARY ON WIRING AND COMPONENTS. - REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND OTHER CONTAMINATION. THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION. IN CASE OF CONTAMINATION REFER TO ESPM 20-55-00. Task Associated Data **CONF 001 Zone From 311 to 312 Modified FIN 1CS Manpower TOTAL MANHOURS 19.00 ELAPSED TIME (HOURS) 19.00 **CONF 002 Zone From 311 to 312 Modified FIN 1CS Manpower TOTAL MANHOURS 19.00 ELAPSED TIME (HOURS) 19.00

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# @A340 SERVICE BULLETIN

**CONF ALL A. GENERAL **CONF 001 (1) Subtask 274187-839-001-001 - 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 274187-839-001-001 - 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 274187-941-001-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 12-34-24-860-002 Task 27-44-51-000-801 (a) Make sure that the aircraft is electrically grounded (Refer to AMM Task 12-34-24-860-002). (b) Do the Job Set-up procedure as described in the removal of the THSA (FIN 1CS), refer to AMM Task 27-44-51-000-801. **CONF 002 (1) Subtask 274187-941-001-001 - Job Set-up Manpower Resources Skills NON SPECIFIC

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# @A340 SERVICE BULLETIN

References Aircraft Maintenance Manual (AMM) Task 12-34-24-860-002 Task 27-44-51-000-801 (a) Make sure that the aircraft is electrically grounded (Refer to AMM Task 12-34-24-860-002). (b) Do the Job Set-up procedure as described in the removal of the THSA (FIN 1CS), refer to AMM Task 27-44-51-000-801. **CONF ALL C. PROCEDURE **CONF 001 (1) Subtask 274187-020-001-001 - Remove the THSA. Work Zones and Access Panels Zone Access/Work location From 311 To 312 Manpower Resources Manhours 8.00 Minimum number of person 2 Subtask elapsed time 8.00 Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 27-44-51-000-801 (a) Remove: Refer to AMM Task 27-44-51-000-801 FIN 1CS 1 THS Actuator 47147-700

(2) Subtask 274187-420-001-001 - Install the THSA. Work Zones and Access Panels Zone Access/Work location From 311 To 312 Manpower Resources Manhours 8.00 Minimum number of person 2 Subtask elapsed time 8.00 Skills NON SPECIFIC DATE: Oct 08/12 SERVICE BULLETIN No.: A340-27-4187 REVISION No.: 00 - Oct 08/12 Page: 13 5

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# @A340 SERVICE BULLETIN
Material necessary to do the job Equipment BFEA01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 47172-530 1 ACTUATOR (1) NOTE (1): 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 27-44-51-400-801 (a) Install: Refer to AMM Task 27-44-51-400-801 FIN 1CS 1 THS Actuator 47172-530 **CONF 002 (1) Subtask 274187-020-001-001 - Remove the THSA. Work Zones and Access Panels Zone Access/Work location From 311 To 312 Manpower Resources Manhours 8.00 Minimum number of person 2 Subtask elapsed time 8.00 Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 27-44-51-000-801 (a) Remove: Refer to AMM Task 27-44-51-000-801 FIN 1CS 1 THS Actuator 47147-700

(2) Subtask 274187-420-001-001 - Install the THSA. Work Zones and Access Panels Zone Access/Work location From 311 To 312 DATE: Oct 08/12 SERVICE BULLETIN No.: A340-27-4187 REVISION No.: 00 - Oct 08/12 Page: 14 5

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# @A340 SERVICE BULLETIN
Manpower Resources Manhours 8.00 Minimum number of person 2 Subtask elapsed time 8.00 Skills NON SPECIFIC Material necessary to do the job Equipment BFEA01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 47172-530 1 ACTUATOR (1) NOTE (1): 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 27-44-51-400-801 (a) Install: Refer to AMM Task 27-44-51-400-801 FIN 1CS 1 THS Actuator 47172-530 **CONF ALL D. TEST **CONF 001 (1) Subtask 274187-700-001-001 - Testing Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 27-44-51-400-801 (a) Remove the safety clips and/or tags and close/unlock the circuit breakers as specified after the installation of the THSA (FIN 1CS), refer to AMM Task 27-44-51-400-801. (b) Do the Test procedure as specified after the installation of the THSA (FIN 1CS), refer to AMM Task 27-44-51-400-801.

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# @A340 SERVICE BULLETIN

**CONF 002 (1) Subtask 274187-700-001-001 - Testing Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 27-44-51-400-801 (a) Remove the safety clips and/or tags and close/unlock the circuit breakers as specified after the installation of the THSA (FIN 1CS), refer to AMM Task 27-44-51-400-801. (b) Do the Test procedure as specified after the installation of the THSA (FIN 1CS), refer to AMM Task 27-44-51-400-801. **CONF ALL E. CLOSE-UP **CONF 001 (1) Subtask 274187-942-001-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 27-44-51-400-801 (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 described in the installation of the THSA (FIN 1CS), refer to AMM Task 27-44-51-400-801. (c) Restore the systems and the aircraft to normal operating condition. **CONF 002 (1) Subtask 274187-942-001-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 27-44-51-400-801 (a) Make sure that the work areas are clean and clear of tools and other items of equipment.

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# @A340 SERVICE BULLETIN (b) Do the Close-Up procedure as described in the installation of the THSA (FIN 1CS), refer to AMM Task 27-44-51-400-801. (c) Restore the systems and the aircraft to normal operating condition.

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# @A340 SERVICE BULLETIN REPORTING SHEET 

### TITLE: FLIGHT CONTROLS - TRIMMABLE HORIZONTAL STABILIZER ACTUATOR - REPLACE THSA PN 47147-700 BY THSA PN 47172-530 MODIFICATION No.: 202802S32403 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.

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# @A340 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.

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