@A340

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

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 - ANGLE OF ATTACK - INSPECT THALES AOA PN

C16291AA.

MODIFICATION No.: None

This page transmits Revision No.03 of Service Bulletin No.A340-34-4215

ADDITIONAL WORK

**CONF ALL

No additional work is required by this revision for aircraft modified by any previous issue.

REASON

Revision No. 03 issued to inform the operators that this Service Bulletin is rendered mandatory and to

remove the terminating action option in accordance with SB A340-34-4087 (INSTALL ANGLE OF

ATTACK SENSORS ROSEMOUNT PN 0861ED).

CHANGES

SUMMARY

REASON/DESCRIPTION/OPERATIONAL

CONSEQUENCES

REASON UPDATED R

GENERAL EVALUATION GENERAL EVALUATION TABLE UPDATED R

EFFECTIVITY OPERATOR LIST UPDATED R

REFERENCES / REPERCUSSIONS REFERENCES/REPERCUSSIONS TABLE

UPDATED

R

MANPOWER MANPOWER UPDATED R

PLANNING INFORMATION

EFFECTIVITY EFFECTIVITY RELATED INFORMATION

UPDATED

R

Configuration definition

CONF 001 CONFIGURATION DEFINITION UPDATED R

REASON

History HISTORY UPDATED R

Objective/Action OBJECTIVE/ACTION UPDATED R

DATE: May 28/08 SERVICE BULLETIN No.: A340-34-4215

REVISION No.: 03 - Jul 27/15 Page: 1

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Advantages ADVANTAGES UPDATED R

Operational/Maintenance

Consequences

OPERATIONAL/MAINTENANCE CONSEQUENCES

UPDATED

R

DESCRIPTION DESCRIPTION UPDATED R

COMPLIANCE

Classification CLASSIFICATION UPDATED R

Accomplishment Timescale ACCOMPLISHMENT TIMESCALE UPDATED R

APPROVAL APPROVAL UPDATED R

MANPOWER MANPOWER UPDATED R

REFERENCES REFERENCED DOCUMENTATION UPDATED R

INTERCHANGEABILITY/MIXABILITY INTERCHANGEABILITY/MIXABILITY UPDATED R

SPARES SPARES UPDATED

PART NUMBER UPDATED

PART NUMBER DESCRIPTION UPDATED

R

MATERIAL INFORMATION

MATERIAL - PRICE AND AVAILABILITY

Procurement Addresses PROCUREMENT ADDRESSES UPDATED

MATERIAL SET UPDATED

R

Price and Availability PRICE AND AVAILABILITY UPDATED

MATERIAL SET UPDATED

R

INDUSTRY SUPPORT INFORMATION INDUSTRY SUPPORT INFORMATION UPDATED R

LIST OF MATERIALS - OPERATOR

SUPPLIED

Consumable Materials CONSUMABLE MATERIALS UPDATED R

Equipment EQUIPMENT UPDATED R

Equipement BFEA01 PART MATERIAL SET UPDATED

NOTE UPDATED

R

TOOLING

Tools TOOLS UPDATED R

ACCOMPLISHMENT INSTRUCTIONS

TASK 344215- 832-801-001-Inspection TASK SOLUTION UPDATED

NOTE UPDATED

CAUTION UPDATED

R

Subtask 344215-941-001-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

PANEL UPDATED

REFERENCES UPDATED

R

Subtask 344215-832-001-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

CONFIGURATION UPDATED

FIGURE REFERENCE UPDATED

PART NUMBER UPDATED

NOTE UPDATED

FIN UPDATED

REFERENCES UPDATED

R

Subtask 344215-700-001-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

DATE: May 28/08 SERVICE BULLETIN No.: A340-34-4215

REVISION No.: 03 - Jul 27/15 Page: 2

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Subtask 344215-942-001-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

PANEL UPDATED

REFERENCES UPDATED

R

TASK 344215- 833-801-001-Repair TASK SOLUTION UPDATED

CAUTION UPDATED

NOTE UPDATED

R

Task associated data - 001 Minor editorial or document structure change R

Subtask 344215-941-002-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

Subtask 344215-960-001-001 SUBTASK SOLUTION UPDATED

NOTE UPDATED

REFERENCED DOCUMENTATION UPDATED

MATERIAL LIST UPDATED

REFERENCES UPDATED

R

Subtask 344215-960-002-001 SUBTASK SOLUTION UPDATED

MANPOWER RESSOURCE UPDATED

REFERENCED DOCUMENTATION UPDATED

PART NUMBER UPDATED

NOTE UPDATED

REFERENCES UPDATED

R

Subtask 344215-700-002-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

Subtask 344215-942-002-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

Fig. A-FBBAA

Fig. A-FBBAA Sheet 01 SHEET UPDATED R

Appendix 1 : Inspection Report

APPENDIX CONTENT APPENDIX CONTENT UPDATED R

Fig. A-FAAAA

Fig. A-FAAAA Sheet 01 SHEET UPDATED R

FILLING INSTRUCTIONS

This Service Bulletin has been generated electronically and is reissued as a complete document.

Replace the complete document.

Put this Revision Transmittal Sheet in front of the Service Bulletin.

HISTORY OF PREVIOUS REVISIONS

Revision No. 01 issued to add aircraft which can be potentially fitted with the affected PN thanks to IPC

interchangeability conditions and to modify the flow chart accordingly.

Revision No. 02 issued to add Service Bulletin No. A340-34-4234 as terminating action.

DATE: May 28/08 SERVICE BULLETIN No.: A340-34-4215

REVISION No.: 03 - Jul 27/15 Page: 3

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

REVISION SEQUENCE

ORIGINAL: May 28/08

REVISION No.: 01 - Dec 03/08

REVISION No. : 02 - Mar 29/10

REVISION No. : 03 - Jul 27/15

DATE: May 28/08 SERVICE BULLETIN No.: A340-34-4215

REVISION No.: 03 - Jul 27/15 Page: 4

5

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

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 34

TITLE: NAVIGATION - ANGLE OF ATTACK - INSPECT THALES AOA PN

C16291AA.

**CONF ALL

MODIFICATIONS

None

REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES

The THALES Angle Of Attack (AOA) sensor Part Number (PN) C16291AA, basic standard fitted on SA

and LR aircraft, experience an ageing issue of the heating element, which means that after a given

number of Flight Hours (FH), the vane of the AOA sensor may not be able to de-ice properly in severe

icing conditions.

For aircraft on which one or more THALES PN C16291AA AOA sensors are installed, this Inspection

Service Bulletin mandates the periodic a functional test of the heating of the AOA sensor and replacing

the AOA sensor if the test fails.

Accomplishment of this Inspection Service Bulletin will allow the detection of any defective THALES PN

C16291AA AOA sensors, up to the embodiment of the terminating action.

The accomplishment of the Service Bulletin No. A340-34-4234 (Install THALES AOA sensors PN

C16291AB) cancels this inspection requirement and cancels the Maintenance Planning Document

(MPD) task 341300-02-1.

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

affected publications detailed in "PLANNING INFORMATION".

GENERAL EVALUATION

EVALUATION TABLE

COMPLIANCE MANDATORY (1) CANCELS INSPECTION SB NO

POTENTIAL AD YES A/C OPERATION AFFECTED NO

RELIABILITY AFFECTED NO PAX COMFORT AFFECTED NO

COST SAVING NO LROPS AFFECTED NO

DATE: May 28/08 SERVICE BULLETIN No.: A340-34-4215

REVISION No.: 03 - Jul 27/15 Page: 1

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

SUMMARY

EVALUATION TABLE

STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED NO

NOTE (1): Service Bulletin must be accomplished.

MATERIAL PRICE INFORMATION

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Equipment BFEA01 1 See SB AOA Sensor

EFFECTIVITY

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

15R 15T 22O 31V 56W 74W 83V 98W 98X ABD AFR AIB ALD

ALK ARG BOE CAL CCA DGA DLH F2I FIN G8E GAF IBE IRC

IRM KAC LAN M3R MAU MDG PAL QAF S3R SAA SAS SFB SLM

SVW SWR TAP THT THY VCV VIR XAX

CONCURRENT REQUIREMENTS

None

REFERENCES / REPERCUSSIONS

TFU 34.10.00.038

OEB None

AOT None

SIL None

ISI None

LINE MAINTENANCE AFFECTED No

LIFE LIMIT None

OTHERS Operator Information Transmission (OIT) No. 999.0036/08

NATURE OF THE WORK

AIRCRAFT NO

EQUIPMENT YES

HARD NO

SOFT NO

OBRM NO

MANPOWER

Task 344215-832-801-001: Inspection

TOTAL MANHOURS 3.00

ELAPSED TIME (HOURS) 3.00

DATE: May 28/08 SERVICE BULLETIN No.: A340-34-4215

REVISION No.: 03 - Jul 27/15 Page: 2

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

SUMMARY

Task 344215-833-801-001: Repair

TOTAL MANHOURS 5.00

ELAPSED TIME (HOURS) 5.00

APPENDICES

Appendix 1 : Inspection Report

DATE: May 28/08 SERVICE BULLETIN No.: A340-34-4215

REVISION No.: 03 - Jul 27/15 Page: 3

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

SUMMARY

**CONF ALL

FR19

FR18

A

A

A

3FP2

3FP3

A

3FP1

F_SB_344215_5_SUAA_01_00

Figure A-FSUAA - Sheet 01

DATE: May 28/08 SERVICE BULLETIN No.: A340-34-4215

REVISION No.: 03 - Jul 27/15 Page: 4

5

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

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 34

TITLE: NAVIGATION - ANGLE OF ATTACK - INSPECT THALES AOA PN

C16291AA.

MODIFICATION No.: None

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 Inspection Service Bulletin is only applicable to A340 aircraft on which

modification No. 58555S30640 (Service Bulletin No. A340-34-4234) is not

embodied.

(1) Models

340-211 340-212 340-213 340-311 340-312 340-313

(2) Effectivity by MSN

0002 0004 0006 0009 0014 0020 0022-0023 0025-0026 0029 0031-0034 0038 0041

0043-0044 0046-0047 0049 0051 0056-0058 0061 0063 0074-0076 0078-0081

0084-0085 0089-0091 0093-0094 0101 0104 0114-0115 0125 0134-0135 0145-0146

0150-0152 0154 0156 0158-0159 0164 0167-0170 0173-0175 0178-0180 0186-0187

0192-0194 0196-0197 0199 0201 0204 0207 0210 0213-0214 0216-0217 0221 0233

0237 0242-0243 0245-0246 0252 0257 0260 0263-0264 0268 0270 0273-0274 0278

0280 0292 0297 0302 0304 0307 0310 0318-0319 0321 0325 0327 0329 0331-0332

0335 0347 0352 0354-0355 0359 0363 0367 0373-0374 0377-0379 0385 0387 0390

0395 0399 0402 0406 0411 0415 0429 0433-0434 0438 0442 0446-0447 0459 0474

0483 0528 0538 0541 0544-0546 0554 0556 0559 0561-0562 0582 0585 0590 0598

0643 0646 0651 0668 0793 0800 0955

DATE: May 28/08 SERVICE BULLETIN No.: A340-34-4215

REVISION No.: 03 - Jul 27/15 Page: 1

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

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

15R 0151

15T 0009

22O 0257

31V 0093

56W 0006

74W 0047 0051

83V 0216 0280 0292

98W 0014 0022

98X 0429

ABD 0210

AFR 0029 0078 0084 0186 0207 0237 0245 0246 0260 0307 0310 0377

0399

AIB 0192 0199

ALD 0156 0159 0178

ALK 0032 0033 0034 0367 0374

ARG 0063 0074 0080 0085 0094 0170 0193 0373

BOE 0554

CAL 0402 0406 0411 0415 0433 0541

CCA 0201 0242 0243 0264

DGA 0075 0081

DLH 0135 0158 0213 0233 0252 0297 0304 0321 0325 0327 0335 0347

0352 0354 0379 0390 0434 0447

F2I 0038 0043

FIN 0058 0168 0174

G8E 0173 0187 0196

GAF 0274 0355

IBE 0125 0134 0145 0146 0217 0221 0329 0483

IRC 0002

IRM 0020 0056 0164

KAC 0089 0090 0101 0104

LAN 0359 0363 0442

M3R 0061

MAU 0076 0152 0194 0268 0793 0800

MDG 0319

PAL 0302 0318 0332 0387 0459 0474

QAF 0026 0528

S3R 0004 0204

SAA 0197 0378 0544 0582 0590 0643 0646 0651

SAS 0167

SFB 0046

DATE: May 28/08 SERVICE BULLETIN No.: A340-34-4215

REVISION No.: 03 - Jul 27/15 Page: 2

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

OPERATOR MSN

SLM 0049

SVW 0955

SWR 0150 0154 0169 0175 0179 0263 0538 0545 0546 0556 0559 0561

0562 0585 0598

TAP 0041 0044 0079 0091

THT 0385 0395 0438 0446 0668

THY 0023 0025 0057 0115 0180 0270 0331

VCV 0031

VIR 0114 0214

XAX 0273 0278

(4) Configuration by MSN

MSN CONFIGURATION

0002 0004 0006 0009 0014 0020 0022 0023 0025 0026 0029

0031 0032 0033 0034 0038 0041 0043 0044 0046 0047 0049

0051 0056 0057 0058 0061 0063 0074 0075 0076 0078 0079

0080 0081 0084 0085 0089 0090 0091 0093 0094 0101 0104

0114 0115 0125 0134 0135 0145 0146 0150 0151 0152 0154

0156 0158 0159 0164 0167 0168 0169 0170 0173 0174 0175

0178 0179 0180 0186 0187 0192 0193 0194 0196 0197 0199

0201 0204 0207 0210 0213 0214 0216 0217 0221 0233 0237

0242 0243 0245 0246 0252 0257 0260 0263 0264 0268 0270

0273 0274 0278 0280 0292 0297 0302 0304 0307 0310 0318

0319 0321 0325 0327 0329 0331 0332 0335 0347 0352 0354

0355 0359 0363 0367 0373 0374 0377 0378 0379 0385 0387

0390 0395 0399 0402 0406 0411 0415 0429 0433 0434 0438

0442 0446 0447 0459 0474 0483 0528 0538 0541 0544 0545

0546 0554 0556 0559 0561 0562 0582 0585 0590 0598 0643

0646 0651 0668 0793 0800 0955

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.

(6) Material Effectivity

MATERIAL QTY PER A/C SEE NOTES

Equipment BFEA01 1

B. CONCURRENT REQUIREMENTS

None

DATE: May 28/08 SERVICE BULLETIN No.: A340-34-4215

REVISION No.: 03 - Jul 27/15 Page: 3

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

C. REASON

(1) History

The THALES Angle Of Attack (AOA) sensor Part Number (PN) C16291AA, basic

standard fitted on SA and LR aircraft, experience an ageing issue of the heating

element, which means that after a given number of Flight Hours (FH), the vane of the

AOA sensor may not be able to de-ice properly in severe icing conditions.

(2) Objective/Action

For aircraft on which one or more THALES PN C16291AA AOA sensors are installed,

this Inspection Service Bulletin mandates the periodic a functional test of the heating of

the AOA sensor and replacing the AOA sensor if the test fails.

(3) Advantages

Accomplishment of this Inspection Service Bulletin will allow the detection of any

defective THALES PN C16291AA AOA sensors, up to the embodiment of the

terminating action.

The accomplishment of the Service Bulletin No. A340-34-4234 (Install THALES

AOA sensors PN C16291AB) cancels this inspection requirement and cancels the

Maintenance Planning Document (MPD) task 341300-02-1.

(4) Operational/Maintenance Consequences

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

update of the affected publications detailed in "PLANNING INFORMATION".

D. DESCRIPTION

NOTE: To accomplish the repair of the affected AOA sensor(s) you have two

possibilities :

- either you replace them as per AMM Task 34-11-19-000-801 and AMM

Task 34-11-19-400-801 in accordance with SUBTASK 344215-960-001

001 OPTION 1 - Replace the Affected AOA Sensor(s) ,

- or you replace them as per Service Bulletin in accordance with SUBTASK

344215-960-002 001 OPTION 2 - Replace the Affected AOA Sensors by

Another PN as Terminating Action .

To accomplish this Service Bulletin it is necessary to :

Task 344215-832-801-001: Inspection

(1) Do a Detailed Inspection of the Three AOA Sensors (FINs 3FP1, 3FP2 and 3FP3).

Task 344215-833-801-001: Repair

(1) OPTION 1 - Replace the Affected AOA Sensor(s)

(2) OPTION 2 - Replace the Affected AOA Sensors by Another PN as Terminating

DATE: May 28/08 SERVICE BULLETIN No.: A340-34-4215

REVISION No.: 03 - Jul 27/15 Page: 4

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

Action

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 Safety Agency (EASA). Tha AD must be used

as the reference document for the mandated accomplishment timescale.

Accomplishment of this Inspection Service Bulletin must be done before 17,000 Flight

Hours (FH), since the aircraft first flight.

For the aircraft which were added in the effectivity of this Service Bulletin at revision 01

and which have exceeded this threshold, a grace period of six months has been agreed

from the issue of this Inspection Service Bulletin at revision 01 for the first inspection.

Repeat the inspection of each THALES AOA sensor PN C16291AA at interval not

exceeding 3,800 FH.

NOTE: The accomplishment of the Service Bulletin No. A340-34-4234 as

terminating action cancels this inspection.

F. APPROVAL

The technical content of this document is approved under EASA Design Organisation

Approval No. EASA.21J.031.

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

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

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

before incorporation of the Service Bulletin.

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 344215-832-801-001: Inspection

Get Access 0.50

On Aircraft

Do a Detailed Inspection of the Three AOA Sensors

(FINs 3FP1, 3FP2 and 3FP3).

1.75

Tests 0.25

DATE: May 28/08 SERVICE BULLETIN No.: A340-34-4215

REVISION No.: 03 - Jul 27/15 Page: 5

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

Task 344215-832-801-001: Inspection

Close-Up 0.50

TOTAL MANHOURS 3.00

ELAPSED TIME (HOURS) 3.00

Task 344215-833-801-001: Repair

Get Access 0.50

On Aircraft

OPTION 1 - Replace the Affected AOA Sensor(s) 3.50

OPTION 2 - Replace the Affected AOA Sensors by

Another PN as Terminating Action

0.00

Tests 0.50

Close-Up 0.50

TOTAL MANHOURS 5.00

ELAPSED TIME (HOURS) 5.00

NOTE: The manpower in the TASK 344215-833-801 001 Repair is for the

replacement of one AOA sensor.

H. WEIGHT AND BALANCE

Not Changed

I. ELECTRICAL LOAD DATA

Not Changed

J. REFERENCES

Aircraft Maintenance Manual (AMM) 12-34-24 30-31-00 34-11-19

Elec. Std. Practices Manual (ESPM) 20-55-00

Service Bulletin (SB) A340-34-4234

K. PUBLICATION AFFECTED

A new Maintenance Planning Document (MPD) task 341300-02-1 has been created in A340

MPD to cover this repetitive inspection.

L. INTERCHANGEABILITY/MIXABILITY

Not Applicable

M. SPARES

None

DATE: May 28/08 SERVICE BULLETIN No.: A340-34-4215

REVISION No.: 03 - Jul 27/15 Page: 6

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

(1) Procurement Addresses

Vendor parts are to be purchased from :

Equipment BFEA01 THALES AVIONICS

AIR TRANSPORT AVIONICS

105 Avenue du general Eisenhower

BP 63647

31036 TOULOUSE CEDEX 1

FRANCE

(2) Price and Availability

Equipment BFEA01

No AIRBUS kit will be provided.

Procurement terms for the equipment must be negotiated with the equipment supplier.

B. INDUSTRY SUPPORT INFORMATION

Industry support terms for the equipment must be negotiated with the equipment supplier.

C. LIST OF COMPONENTS

No Kit

D. LIST OF MATERIALS - OPERATOR SUPPLIED

(1) Consumable Materials

To accomplish this Inspection Service Bulletin it is necessary to use the expendable

parts listed in the AMM Task 34-11-19-400-801.

(2) Components

None

(3) Equipment

For the replacement of the AOA sensors as described in SUBTASK 344215-960-001

001 OPTION 1 - Replace the Affected AOA Sensor(s) :

Equipment BFEA01

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

NOTES

C16291AA 3 SENSOR C16291AA

DATE: May 28/08 SERVICE BULLETIN No.: A340-34-4215

REVISION No.: 03 - Jul 27/15 Page: 7

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

NOTE: The components listed above are only necessary if found affected AOA

sensors. The quantity of these items are to be ordered as required.

E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

None

F. TOOLING

(1) Tooling - Price and Availability

None

(2) Tools

To accomplish this Inspection Service Bulletin it is necessary to use the tools listed in

AMM Task 30-31-00-720-801.

(3) Special Tools

None

DATE: May 28/08 SERVICE BULLETIN No.: A340-34-4215

REVISION No.: 03 - Jul 27/15 Page: 8

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS

Task 344215-832-801-001 - Inspection

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 THERE IS CONTAMINATION REFER TO ESPM 20-55-00.

NOTE: The accomplishment instructions of this Service Bulletin refer to procedures

included in other AIRBUS documents. When the words ’refer to’ are used and the

operator has an accepted alternative procedure, the accepted alternative procedure

can be used. When the words ’in accordance with’ are included in the instruction,

the procedure in the AIRBUS document must be used.

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: The purpose of flow charts is to supplement the information given in the Procedure

and Compliance paragraphs and not to serve as the primary source for tasks or

compliance times given in this Service Bulletin.

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.

DATE: May 28/08 SERVICE BULLETIN No.: A340-34-4215

REVISION No.: 03 - Jul 27/15 Page: 9

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

Task Associated Data

Modified FIN

3FP1 3FP2 3FP3

Manpower

TOTAL MANHOURS 3.00

ELAPSED TIME (HOURS) 3.00

A. GENERAL

(1) Subtask 344215-839-001-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

B. PREPARATION

(1) Subtask 344215-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

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

Task 30-31-00-720-801

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

12-34-24-860-802).

(b) Put access platform(s) in position.

(c) Open the Avionics Access Door 811.

(d) Open the passenger/crew door(s).

(e) Do the preparation procedure as specified in the functional test of the heating of the

AOA sensor, refer to AMM Task 30-31-00-720 801.

C. PROCEDURE

(1) Subtask 344215-832-001-001 - Do a Detailed Inspection of the Three AOA Sensors

(FINs 3FP1, 3FP2 and 3FP3).

Manpower Resources

Manhours 1.75

Minimum number of person 1

Subtask elapsed time 1.75

Skills NON SPECIFIC

DATE: May 28/08 SERVICE BULLETIN No.: A340-34-4215

REVISION No.: 03 - Jul 27/15 Page: 10

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) Task 30-31-00-720-801

Fig. A-FBAAA

Areas to be Inspected

Sheet 01

Fig. A-FBBAA

Flow Chart

Sheet 01

(a) Do a check of the part number of the three AOA sensors (FINs 3FP1, 3FP2 and

3FP3).

Refer to figure Fig. A-FBAAA Sheet 01

1 If the affected PN C16291AA is found installed on any of the three positions:

a Do the functional test of the heating of the AOA sensors PN C16291AA

(FINs 3FP1, 3FP2 and/or 3FP3).

Refer to AMM Task 30-31-00-720-801)

Refer to Figure Fig. A-FBBAA Sheet 01

NOTE: Refer to AMM Task 30-31-00-720-801 which requests to

perform three times the record of the maximum current

(Imax).

<1> If the maximun current (Imax) found is equal or less than 1.2A:

<a> Before next flight, replace the affected AOA sensor in

accordance with the SUBTASK 344215-960-001-001 Replace

the Affected AOA sensor(s) and

<b> Send the Inspection Report to Airbus and

<c> Repeat the Task 344215-832-801-001 at the interval given in

PLANNING INFORMATION paragraph 1.E.(2)

OR

<d> Do the SUBTASK 344215-960-002-001 Replace the Affected

AOA Sensors by Another PN as Terminating Action and

<e> Send the Inspection Report to Airbus

[1] If all AOA Sensors found upgraded to PN C16291AB

[a] No further action.

[2] If all AOA Sensors are not found upgraded to PN

C16291AB on the three positions (3FP1, 3FP2 and 3FP3):

[a] Repeat the Task 344215-832-801-001 at the interval

given in PLANING INFORMATION paragraph 1.E.(2)

DATE: May 28/08 SERVICE BULLETIN No.: A340-34-4215

REVISION No.: 03 - Jul 27/15 Page: 11

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

<2> If the maximun current (Imax) found is more than 1.2A:

<a> Send the Inspection Report to Airbus and

<b> Repeat the Task 344215-832-801-001 at the interval given in

PLANING INFORMATION paragraph 1.E.(2)

OR

<c> Do the SUBTASK 344215-960-002-001 Replace the Affected

AOA Sensors by Another PN as Terminating Action and

[1] Send the Inspection Report to Airbus and

[a] No further action.

[2] If all AOA Sensors are not found upgraded to PN

C16291AB on the three positions (3FP1, 3FP2 and 3FP3):

[a] Repeat the Task 344215-832-801-001 at the interval

given in PLANING INFORMATION paragraph 1.E.(2)

2 If the PN C16291AA is not found installed on the three positions (3FP1, 3FP2

and 3FP3)

a No further action

D. TEST

(1) Subtask 344215-700-001-001 - Test

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 30-31-00-720-801

(a) Job set-up :

1 Remove the safety clips and tags and close the circuit breakers as specified

after the functional test of heating of the AOA sensors (Refer to AMM Task

30-31-00-720-801).

(b) Procedure :

1 Do the operational test of the probe ice protection (Refer to AMM Task

30-31-00-720-801).

DATE: May 28/08 SERVICE BULLETIN No.: A340-34-4215

REVISION No.: 03 - Jul 27/15 Page: 12

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

E. CLOSE-UP

(1) Subtask 344215-942-001-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 34-11-19-400-801

(a) Do the close-up procedure after the functional test of the heating of the AOA

sensor (Refer to (Refer to AMM Task 34-11-19-400-801).

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

equipment.

(c) Close the passenger/crew door(s).

(d) Close the Avionics Access Door 811.

(e) Restore the systems and the aircraft to normal operating condition.

(f) Remove the access platform(s).

(g) Put the aircraft back to its initial configuration.

DATE: May 28/08 SERVICE BULLETIN No.: A340-34-4215

REVISION No.: 03 - Jul 27/15 Page: 13

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

This Page Intentionally Left Blank

DATE: May 28/08 SERVICE BULLETIN No.: A340-34-4215

REVISION No.: 03 - Jul 27/15 Page: 14

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

Task 344215-833-801-001 - Repair

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 THERE IS CONTAMINATION REFER TO ESPM 20-55-00.

Task Associated Data

Modified FIN

3FP1 3FP2 3FP3

Manpower

TOTAL MANHOURS 5.00

ELAPSED TIME (HOURS) 5.00

A. GENERAL

(1) Subtask 344215-839-002-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

B. PREPARATION

(1) Subtask 344215-941-002-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 34-11-19-000-801

Task 34-11-19-400-801

DATE: May 28/08 SERVICE BULLETIN No.: A340-34-4215

REVISION No.: 03 - Jul 27/15 Page: 15

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

(a) Do the preparation procedure as specified in the removal of the AOA sensors (FINs

3FP1, 3FP2 and 3FP3) (Refer to AMM Task 34-11-19-000-801).

C. PROCEDURE

NOTE: To accomplish the repair of the affected AOA sensor(s) you have two

possibilities :

- either you replace them as per AMM Task 34-11-19-000-801 and AMM

Task 34-11-19-400-801 in accordance with SUBTASK 344215-960-001

001 OPTION 1 - Replace the Affected AOA Sensor(s) ,

- or you replace them as per Service Bulletin in accordance with SUBTASK

344215-960-002 001 OPTION 2 - Replace the Affected AOA Sensors by

Another PN as Terminating Action .

(1) Subtask 344215-960-001-001 - OPTION 1 - Replace the Affected AOA Sensor(s)

Manpower Resources

Manhours 3.50

Minimum number of person 1

Subtask elapsed time 3.50

Skills NON SPECIFIC

Material necessary to do the job

Equipment BFEA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

C16291AA 3 SENSOR

NOTE: The components listed above are only necessary if found affected AOA

sensors. The quantity of these items are to be ordered as required.

References

Aircraft Maintenance Manual (AMM) Task 34-11-19-000-801

Fig. A-FBBAA

Flow Chart

Sheet 01

(a) Depending on the result of the inspection, replace the affected AOA sensor(s).

Refer to AMM Task 34-11-19-000-801

Refer to Figure Fig. A-FBBAA

1 Remove :

FIN 3FP1

1 AOA Sensor C16291AA

and/or

DATE: May 28/08 SERVICE BULLETIN No.: A340-34-4215

REVISION No.: 03 - Jul 27/15 Page: 16

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

FIN 3FP2

1 AOA Sensor C16291AA

and/or

FIN 3FP3

1 AOA Sensor C16291AA

2 Install :

FIN 3FP1

1 AOA Sensor C16291AA

and/or

FIN 3FP2

1 AOA Sensor C16291AA

and/or

FIN 3FP3

1 AOA Sensor C16291AA

(2) Subtask 344215-960-002-001 - OPTION 2 - Replace the Affected AOA Sensors by

Another PN as Terminating Action

Manpower Resources

Manhours 0.00

Minimum number of person 0

Subtask elapsed time 0.00

Skills NON SPECIFIC

References

Service Bulletin (SB) A340-34-4234

(a) Do the replacement of the three THALES AOA sensors PN C16291AA by PN

C16291AB as per Service Bulletin No. A340-34-4234.

D. TEST

(1) Subtask 344215-700-002-001 - Test

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 34-11-19-400-801

DATE: May 28/08 SERVICE BULLETIN No.: A340-34-4215

REVISION No.: 03 - Jul 27/15 Page: 17

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

(a) Job set-up :

1 Remove the safety clips and tags and close the circuit breakers as specified

after the installation of the AOA sensors (FINs 3FP1, 3FP2 and 3FP3) (Refer

to AMM Task 34-11-19-400-801).

(b) Procedure :

1 Do the test procedure as specified after the installation of the AOA sensors

(FINs 3FP1, 3FP2 and 3FP3) (Refer to AMM Task 34-11-19-400-801).

E. CLOSE-UP

(1) Subtask 344215-942-002-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 34-11-19-400-801

(a) Do the close-up procedure after the installation of the AOA sensors (FINs 3FP1,

3FP2 and 3FP3) (Refer to AMM Task 34-11-19-400-801).

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

equipment.

(c) Close the passenger/crew door(s).

(d) Restore the systems and the aircraft to normal operating condition.

(e) Remove the access platform(s).

(f) Put the aircraft back to its initial configuration.

DATE: May 28/08 SERVICE BULLETIN No.: A340-34-4215

REVISION No.: 03 - Jul 27/15 Page: 18

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

**CONF ALL

FR19

FR18

A

A

A

3FP2

3FP3

A

3FP1

AREA TO BE INSPECTED

F_SB_344215_5_BAAA_01_00

Figure A-FBAAA - Sheet 01

Areas to be Inspected

DATE: May 28/08 SERVICE BULLETIN No.: A340-34-4215

REVISION No.: 03 - Jul 27/15 Page: 19

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

**CONF ALL

YES

OR

SEND TO AIRBUS

INSPECTION REPORT

REFER TO APPENDIX 1

NO FURTHER ACTION

DO THE FUNCTIONAL TEST OF THE HEATING OF THE

AOA SENSOR(S) AT THE THRESHOLD GIVEN IN THE

PLANNING INFORMATION PARAGRAPH 1.E.(2) AS PER

SUBTASK 344215−832−001 001

I MAX CURRENT 1.2 A

DO A DETAILED VISUAL INSPECTION OF THE

THREE AOA SENSORS (FINS 3FP1, 3FP2 AND 3FP3).

DO A CHECK OF THE PART NUMBER

C16291AA OF THE THREE AOA SENSORS

YES PN C16291AA

INSTALLED

SEND TO AIRBUS

INSPECTION REPORT

REFER TO APPENDIX 1

NO FURTHER ACTION

NO

OR

SEND TO AIRBUS

INSPECTION REPORT

REFER TO APPENDIX 1

SEND TO AIRBUS

INSPECTION REPORT

REFER TO APPENDIX 1

REPEAT THE FUNCTIONAL

TEST AT INTERVAL GIVEN IN

THE PLANNING INFORMATION

PARAGRAPH 1.E.(2).

NO

REPLACE AFFECTED THALES

AOA SENSOR(S) PN C16291AA

BY THE NEW SAME PN AS PER

SUBTASK 344215−960−001 001

REPLACE THALES AOA

SENSOR(S) PN C16291AA BY

ANOTHER PN AS PER

SUBTASK 344215−960−002 001

NO

YES

NO

THE FUNCTIONAL TEST

 AT INTERVAL GIVEN IN THE

PLANNING INFORMATION

PARAGRAPH 1.E.(2).

REPEAT

AOA SENSORS

UPGRADED TO

PN C16291AB

ALL

F_SB_344215_5_BBAA_01_02

Figure A-FBBAA - Sheet 01

Flow Chart

DATE: May 28/08 SERVICE BULLETIN No.: A340-34-4215

REVISION No.: 03 - Jul 27/15 Page: 20

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

Appendix 1 : Inspection Report

**CONF ALL

The results of the inspection, including no findings, replacement or actions to be done, must be

forwarded to AIRBUS, on the attached inspection report sheet.

DATE: May 28/08 SERVICE BULLETIN No.: A340-34-4215

REVISION No.: 03 - Jul 27/15 Page: 1

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

Appendix 1 : Inspection Report

**CONF ALL

INSPECTION REPORT

SERVICE BULLETIN No. :

A/C MSN :

FLIGHT CYCLES :

FLIGHT HOURS :

A340−34−4215

DATE OF INSPECTION :

INSPECTION METHOD : DETAILED

INSPECTION

RETURN TO :

AIRBUS

CUSTOMER SERVICES ENGINEERING

AFS/NAV/COM SYSTEMS

1 ROND POINT MAURICE BELLONTE

31707 BLAGNAC CEDEX

FRANCE

E−mail: inspection.results@airbus.com

FAX +33 (0)5 61 93 44 25

I MAX CURRENT > 1.2A

3FP1 3FP2

REPLACEMENT OF AOA

FIN 3FP3

SENSOR

YES NO YES NO YES NO

YES NO YES NO YES NO

I MAX RECORDED

C16291AA

C16291AB AS PER

C16291AA C16291AA

SERVICE BULLETIN 

NEW AOA SENSOR PN

INSTALLED

No. A340−34−4234

C16291AB AS PER C16291AB AS PER

SERVICE BULLETIN 

No. A340−34−4234

SERVICE BULLETIN 

No. A340−34−4234

F_SB_344215_5_AAAA_01_05

Figure A-FAAAA - Sheet 01

Inspection Report

DATE: May 28/08 SERVICE BULLETIN No.: A340-34-4215

REVISION No.: 03 - Jul 27/15 Page: 2

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

REPORTING SHEET

TITLE: NAVIGATION - ANGLE OF ATTACK - INSPECT THALES AOA PN

C16291AA.

MODIFICATION No.: None

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: May 28/08 SERVICE BULLETIN No.: A340-34-4215

REVISION No.: 03 - Jul 27/15 Page: 1

5

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

DATE: May 28/08 SERVICE BULLETIN No.: A340-34-4215

REVISION No.: 03 - Jul 27/15 Page: 1

5

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