@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 - SENSORS, POWER SUPPLY AND SWITCHING -

INSPECTION OF THALES AOA PROBES

MODIFICATION No.: None

This page transmits Revision No.01 of Service Bulletin No.A340-34-4239

ADDITIONAL WORK

**CONF ALL

ADDITIONAL WORK is required by this revision for aircraft inspected by the original issue of this

Service Bulletin and with PN C16291AB installed.

The ADDITIONAL WORK is issued to ensure that the correct Serial Number (SN) of AOA Probe PN

C16291AB was installed.

No ADDITIONAL WORK is required for aircraft with PN C16291AA installed by the original issue of this

Service Bulletin.

REASON

Revision No. 01 issued to add Serial Number of Angle Of Attack PN C16291AB to be inspected.

NOTE: The original issue of this Inspection Service Bulletin was focusing on a batch of SN

having all the PN C16291AA. However, in the mean time, some units may have been

upgraded to PN C16291AB by THALES Service Bulletin C16291A-34-009 without fixing

the oil residue anomaly.

The ADDITIONAL WORK for this Service Bulletin is issue to also inspect PN

C16291AB. The batch is unchanged in terms of SN.

CHANGES

The main changes of the Revision No. 01 are:

- to add ADDITIONAL WORK for aircraft on which AOA Probes PN C16291AB are installed by the

original issue of this Service Bulletin,

- to add Config. 002 valid for aircraft on which AOA PN C16291AB is installed,

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

REVISION No.: 01 - Sep 17/13 Page: 1

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@A340

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

- to modify Fig. A-FFAAA,

- to add Fig. A-FFBAA and Fig. A-FFAAB,

- to modify REASON paragraph,

- to update the effectivity.

FRONT MATTER

NAVIGATION - SENSORS, POWER

SUPPLY AND SWITCHING -

INSPECTION OF THALES AOA PROBES

CONFIGURATION UPDATED R

SUMMARY

REASON/DESCRIPTION/OPERATIONAL

CONSEQUENCES

REASON UPDATED R

GENERAL EVALUATION GENERAL EVALUATION TABLE UPDATED R

EFFECTIVITY OPERATOR LIST UPDATED R

MANPOWER MANPOWER UPDATED

CONFIGURATION UPDATED

R

MANPOWER ADDED N

APPENDICES APPENDICES UPDATED R

Fig. A-FSAAA FIGURE SOLUTION ADDED N

Fig. A-FSAAA Sheet 01 SHEET ADDED N

Fig. A-FSU FIGURE DELETED FOR APPLICABLE MSN D

PLANNING INFORMATION

EFFECTIVITY EFFECTIVITY RELATED INFORMATION

UPDATED

R

Configuration definition CONFIGURATION LIST UPDATED R

CONF 001 CONFIGURATION DEFINITION UPDATED

CONFIGURATION DESCRIPTION UPDATED

R

CONF 002 CONFIGURATION ADDED N

REASON

Objective/Action OBJECTIVE/ACTION UPDATED R

DESCRIPTION DESCRIPTION UPDATED R

COMPLIANCE

Classification CLASSIFICATION UPDATED R

Accomplishment Timescale ACCOMPLISHMENT TIMESCALE UPDATED

CONFIGURATION UPDATED

R

Accomplishment Timescale ACCOMPLISHMENT TIMESCALE ADDED N

APPROVAL APPROVAL UPDATED R

MANPOWER MANPOWER UPDATED

CONFIGURATION UPDATED

R

MANPOWER ADDED N

REFERENCES REFERENCED DOCUMENTATION UPDATED

CONFIGURATION UPDATED

R

REFERENCED DOCUMENTATION ADDED N

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

REVISION No.: 01 - Sep 17/13 Page: 2

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

MATERIAL INFORMATION

MATERIAL - PRICE AND AVAILABILITY

Procurement Addresses PROCUREMENT ADDRESSES UPDATED R

Price and Availability PRICE AND AVAILABILITY UPDATED R

INDUSTRY SUPPORT INFORMATION INDUSTRY SUPPORT INFORMATION UPDATED R

ACCOMPLISHMENT INSTRUCTIONS

TASK 344239- 832-801-001-Inspection TASK SOLUTION UPDATED

NOTE UPDATED

CONFIGURATION UPDATED

R

Task associated data - 001 CONFIGURATION UPDATED R

Task associated data - 002 TASK ASSOCIATED DATA ADDED N

Subtask 344239-839-001-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

R

Subtask 344239-839-001-001 SUBTASK SOLUTION ADDED N

Subtask 344239-941-001-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

REFERENCED DOCUMENTATION UPDATED

PANEL UPDATED

REFERENCES UPDATED

R

Subtask 344239-941-001-001 SUBTASK SOLUTION ADDED N

Subtask 344239-832-001-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

REFERENCED DOCUMENTATION UPDATED

FIGURE REFERENCE UPDATED

FIN UPDATED

PART NUMBER UPDATED

NOTE UPDATED

REFERENCES UPDATED

R

Subtask 344239-832-001-002 SUBTASK SOLUTION ADDED N

Subtask 344239-942-001-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

REFERENCED DOCUMENTATION UPDATED

NOTE UPDATED

REFERENCES UPDATED

R

Subtask 344239-942-001-001 SUBTASK SOLUTION ADDED N

TASK 344239- 831-801-001-Replacement

of the THALES AOA Probes by Part

Number C16291AB whose SN is not listed

in THALES AVIONICS Service Bulletin

No. C16291A-34-007 Revision No. 01 (or

any later revision).

TASK SOLUTION UPDATED

TASK TITLE UPDATED

NOTE UPDATED

CONFIGURATION UPDATED

R

Task associated data - 001 CONFIGURATION UPDATED R

Task associated data - 002 TASK ASSOCIATED DATA ADDED N

Subtask 344239-839-003-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

R

Subtask 344239-839-003-001 SUBTASK SOLUTION ADDED N

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

REVISION No.: 01 - Sep 17/13 Page: 3

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Subtask 344239-941-003-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

REFERENCED DOCUMENTATION UPDATED

NOTE UPDATED

PANEL UPDATED

REFERENCES UPDATED

R

Subtask 344239-941-003-001 SUBTASK SOLUTION ADDED N

Subtask 344239-960-002-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

REFERENCED DOCUMENTATION UPDATED

NOTE UPDATED

REFERENCES UPDATED

R

Subtask 344239-960-002-002 SUBTASK SOLUTION ADDED N

Subtask 344239-700-002-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

R

Subtask 344239-700-002-001 SUBTASK SOLUTION ADDED N

Subtask 344239-942-003-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

REFERENCED DOCUMENTATION UPDATED

PANEL UPDATED

REFERENCES UPDATED

R

Subtask 344239-942-003-001 SUBTASK SOLUTION ADDED N

TASK 344239- 831-802-001-Replacement

of the THALES AOA Probes by Part

Number C16291AA whose Serial Number

is not listed in the THALES VSB

C16291A-34-007 Revision No. 01 (or any

later revision).

TASK SOLUTION UPDATED

TASK TITLE UPDATED

NOTE UPDATED

CONFIGURATION UPDATED

R

Task associated data - 001 CONFIGURATION UPDATED R

Task associated data - 002 TASK ASSOCIATED DATA ADDED N

Subtask 344239-839-004-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

R

Subtask 344239-941-004-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

REFERENCED DOCUMENTATION UPDATED

NOTE UPDATED

PANEL UPDATED

REFERENCES UPDATED

R

Subtask 344239-960-003-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

R

Subtask 344239-700-003-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

R

Subtask 344239-942-004-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

REFERENCED DOCUMENTATION UPDATED

PANEL UPDATED

REFERENCES UPDATED

R

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

REVISION No.: 01 - Sep 17/13 Page: 4

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

TASK 344239- 831-803-001-Replacement

of the three THALES AOA Probes through

Airbus RFC/RMO Process.

TASK SOLUTION UPDATED

TASK TITLE UPDATED

NOTE UPDATED

CONFIGURATION UPDATED

R

Task associated data - 001 CONFIGURATION UPDATED R

Task associated data - 002 TASK ASSOCIATED DATA ADDED N

Subtask 344239-839-005-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

R

Subtask 344239-839-005-001 SUBTASK SOLUTION ADDED N

Subtask 344239-941-005-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

REFERENCED DOCUMENTATION UPDATED

NOTE UPDATED

PANEL UPDATED

REFERENCES UPDATED

R

Subtask 344239-941-005-001 SUBTASK SOLUTION ADDED N

Subtask 344239-960-004-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

NOTE UPDATED

R

Subtask 344239-960-004-002 SUBTASK SOLUTION ADDED N

Subtask 344239-700-004-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

R

Subtask 344239-700-004-001 SUBTASK SOLUTION ADDED N

Subtask 344239-942-006-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

REFERENCED DOCUMENTATION UPDATED

PANEL UPDATED

REFERENCES UPDATED

R

Subtask 344239-942-005-001 SUBTASK SOLUTION DELETED FOR

APPLICABLE MSN

D

Subtask 344239-942-006-001 SUBTASK SOLUTION ADDED N

TASK 344239- 831-804-001-Replacement

of the THALES AOA Probes by Part

Number post Vendor Service Bulletin

THALES AVIONICS C16291A-34-007

Revision No. 01 (or any later revision).

TASK SOLUTION UPDATED

TASK TITLE UPDATED

NOTE UPDATED

CONFIGURATION UPDATED

R

Task associated data - 001 CONFIGURATION UPDATED

REFERENCED DOCUMENTATION UPDATED

R

Task associated data - 002 TASK ASSOCIATED DATA ADDED N

Subtask 344239-839-006-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

R

Subtask 344239-839-006-001 SUBTASK SOLUTION ADDED N

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

REVISION No.: 01 - Sep 17/13 Page: 5

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Subtask 344239-941-006-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

REFERENCED DOCUMENTATION UPDATED

NOTE UPDATED

PANEL UPDATED

REFERENCES UPDATED

R

Subtask 344239-941-006-001 SUBTASK SOLUTION ADDED N

Subtask 344239-960-005-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

REFERENCED DOCUMENTATION UPDATED

NOTE UPDATED

PART NUMBER UPDATED

FIN UPDATED

MANPOWER RESSOURCE UPDATED

REFERENCES UPDATED

R

Subtask 344239-831-002-001 SUBTASK SOLUTION ADDED N

Subtask 344239-831-003-001 SUBTASK SOLUTION ADDED N

Subtask 344239-960-005-003 SUBTASK SOLUTION ADDED N

Subtask 344239-831-002-001 SUBTASK SOLUTION ADDED N

Subtask 344239-831-003-002 SUBTASK SOLUTION ADDED N

Subtask 344239-700-005-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

R

Subtask 344239-700-005-001 SUBTASK SOLUTION ADDED N

Subtask 344239-942-007-001 SUBTASK SOLUTION ADDED N

Subtask 344239-942-007-001 SUBTASK SOLUTION ADDED N

TASK 344239- 832-802-001-Inspection -

ADDITIONAL WORK for Aircraft modified

by Original Issue.

TASK SOLUTION ADDED N

Task associated data - 001 TASK ASSOCIATED DATA ADDED N

Task associated data - 002 TASK ASSOCIATED DATA ADDED N

Subtask 344239-839-007-001 SUBTASK SOLUTION ADDED N

Subtask 344239-941-007-001 SUBTASK SOLUTION ADDED N

Subtask 344239-832-002-001 SUBTASK SOLUTION ADDED N

Subtask 344239-942-005-001 SUBTASK SOLUTION ADDED N

Fig. A-FFAAA FIGURE SOLUTION ADDED N

Fig. A-FFAAA Sheet 01 SHEET ADDED N

Fig. A-FFAAB FIGURE SOLUTION ADDED N

Fig. A-FFAAB Sheet 01 SHEET ADDED N

Fig. A-FFBAA FIGURE SOLUTION ADDED N

Fig. A-FFBAA Sheet 01 SHEET ADDED N

Fig. A-FRAAA FIGURE SOLUTION ADDED N

Fig. A-FRAAA Sheet 01 SHEET ADDED N

Fig. A-FBB FIGURE DELETED FOR APPLICABLE MSN D

APPENDIX APPENDIX DELETED D

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

REVISION No.: 01 - Sep 17/13 Page: 6

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

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

No previous revision

REVISION SEQUENCE

ORIGINAL: Jan 20/10

REVISION No. : 01 - Sep 17/13

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

REVISION No.: 01 - Sep 17/13 Page: 7

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@A340

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

This Page Intentionally Left Blank

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

REVISION No.: 01 - Sep 17/13 Page: 8

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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 - SENSORS, POWER SUPPLY AND SWITCHING -

INSPECTION OF THALES AOA PROBES

**CONF ALL

MODIFICATIONS

None

REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES

During Airbus Final Assembly Line reception flight test, AOA (Angle of Attack) data from two aircraft

(one per A/C) were found inaccurate during the in-flight production tests and confirmed during DFDR

(Digital Flight Data Recorder) analysis.

Investigation of the removed probes revealed oil residue between the stator and the rotor parts of the

AOA vane position resolvers. The presence of this oil residue results from a quality escape during the

manufacturing process of the AOA resolvers, which led to a poor cleaning of machining oil.

The oil residue has been found to become viscous at low temperatures (typically in cruise) causing lag

of AOA vane movement.

This Inspection Service Bulletin requires the inspection of THALES AOA probes PN C16291AA and

PN C16291AB. For those AOA probes corresponding to the batch of serial numbers listed in VSB

C16291A-34-007 revision 01 or any later revision, replacement of the AOA probe is required.

Accomplishment of this Service Bulletin will ensure that AOA probes potentially affected by the oil

residue issue are replaced on aircraft.

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 YES

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

REVISION No.: 01 - Sep 17/13 Page: 1

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@A340

SERVICE BULLETIN

SUMMARY

NOTE (1): Service Bulletin must be accomplished.

MATERIAL PRICE INFORMATION

No Material

EFFECTIVITY

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

15R 15T 56W 58X 83V ABD ABQ ACA AFR ALK ARG CAL CCA

DGA DLH FIN GAF GFA HFY I2L IBE IRC IRM KAC LAN M3R

MAU MDG MSR NMB PAL QAF RJA S3R SAA SAS SFB SLM SVW

SWR TAP THT THY VCV VIR XAX

CONCURRENT REQUIREMENTS

None

REFERENCES / REPERCUSSIONS

TFU None

OEB None

AOT None

SIL None

LINE MAINTENANCE AFFECTED No

LIFE LIMIT None

OTHER OIT SE 999.065/09

NATURE OF THE WORK

AIRCRAFT NO

EQUIPMENT YES

HARD NO

SOFT NO

OBRM NO

MANPOWER

**CONF 001

Task 344239-832-801-001: Inspection

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

Task 344239-831-801-001: Replacement of the THALES AOA Probes by Part Number

C16291AB whose SN is not listed in THALES AVIONICS Service Bulletin No. C16291A-34-007

Revision No. 01 (or any later revision).

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

REVISION No.: 01 - Sep 17/13 Page: 2

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SERVICE BULLETIN

SUMMARY

Task 344239-831-802-001: Replacement of the THALES AOA Probes by Part Number

C16291AA whose Serial Number is not listed in the THALES VSB C16291A-34-007 Revision

No. 01 (or any later revision).

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

Task 344239-831-803-001: Replacement of the three THALES AOA Probes through Airbus

RFC/RMO Process.

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

Task 344239-831-804-001: Replacement of the THALES AOA Probes by Part Number post

Vendor Service Bulletin THALES AVIONICS C16291A-34-007 Revision No. 01 (or any later

revision).

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

Additional manhours related to Vendor SB; refer to:

Modify the AOA Probes. THALES AVIONICS Service Bulletin

No. C16291A-34-007

**CONF 002

Task 344239-832-801-001: Inspection

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

Task 344239-831-801-001: Replacement of the THALES AOA Probes by Part Number

C16291AB whose SN is not listed in THALES AVIONICS Service Bulletin No. C16291A-34-007

Revision No. 01 (or any later revision).

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

Task 344239-831-803-001: Replacement of the three THALES AOA Probes through Airbus

RFC/RMO Process.

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

Task 344239-831-804-001: Replacement of the THALES AOA Probes by Part Number post

Vendor Service Bulletin THALES AVIONICS C16291A-34-007 Revision No. 01 (or any later

revision).

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

Additional manhours related to Vendor SB; refer to:

Modify the AOA Probes. THALES AVIONICS Service Bulletin

No. C16291A-34-007

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

REVISION No.: 01 - Sep 17/13 Page: 3

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@A340

SERVICE BULLETIN

SUMMARY

Task 344239-832-802-001: Inspection - ADDITIONAL WORK for Aircraft modified by Original

Issue.

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

APPENDICES

**CONF ALL

None

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

REVISION No.: 01 - Sep 17/13 Page: 4

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@A340

SERVICE BULLETIN

SUMMARY

**CONF ALL

FR19

FR18

A

3FP1

3FP2

3FP3

A

A

AREA TO BE INSPECTED

TYPICAL INSTALLATION

A

F_SB_344239_5_SAAA_01_00

Figure A-FSAAA - Sheet 01

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

REVISION No.: 01 - Sep 17/13 Page: 5

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@A340

SERVICE BULLETIN

SUMMARY

This Page Intentionally Left Blank

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

REVISION No.: 01 - Sep 17/13 Page: 6

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 - SENSORS, POWER SUPPLY AND SWITCHING -

INSPECTION OF THALES AOA PROBES

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

(1) Models

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

(2) Effectivity by MSN

0002 0004-0006 0009 0011 0013-0014 0018-0020 0022-0029 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 0125 0133-0135 0145-0146

0150-0152 0154 0156 0158-0159 0164 0167-0170 0173-0176 0178-0180 0186-0187

0192-0194 0196-0197 0199 0201 0204 0207 0210 0213-0214 0216-0217 0221 0225

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 0414-0415 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: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

REVISION No.: 01 - Sep 17/13 Page: 1

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SERVICE BULLETIN

(3) Effectivity by Operator

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

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

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

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

OPERATOR MSN

15R 0151

15T 0009

56W 0011 0013 0018 0019

58X 0004

83V 0280 0292

ABD 0210

ABQ 0216 0257

ACA 0170

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

0399

ALK 0032 0033 0034 0367 0374

ARG 0048 0063 0074 0080 0085 0093 0094 0193 0373

CAL 0402 0406 0411 0415 0433 0541

CCA 0192 0199 0201 0242 0243 0264

DGA 0075 0081

DLH 0024 0027 0028 0035 0052 0053 0135 0158 0213 0233 0252 0297

0304 0321 0325 0327 0335 0347 0352 0354 0379 0390 0434 0447

FIN 0058 0168 0174

GAF 0274 0355

GFA 0554

HFY 0133

I2L 0005

IBE 0088 0125 0134 0145 0146 0217 0221 0329 0387 0414 0459 0474

0483

IRC 0002

IRM 0020 0056

KAC 0089 0090 0101 0104

LAN 0359 0363 0429 0442

M3R 0061

MAU 0076 0152 0194 0268 0793 0800

MDG 0319

MSR 0156 0159 0178

NMB 0047 0051

PAL 0173 0176 0187 0196 0302 0318 0332

QAF 0026 0528

RJA 0014 0022 0038 0043

S3R 0204

SAA 0006 0197 0378 0544 0582 0590 0643 0646 0651

SAS 0167

SFB 0046

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

REVISION No.: 01 - Sep 17/13 Page: 2

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@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 0164 0214 0225

XAX 0273 0278

(4) Configuration by MSN

MSN CONFIGURATION

0002 0004 0006 0011 0013 0018 0019 0020 0023 0024 0025

0027 0028 0031 0032 0033 0034 0035 0041 0044 0047 0048

0051 0052 0053 0056 0057 0058 0061 0063 0074 0075 0076

0079 0080 0081 0085 0088 0089 0090 0091 0093 0094 0101

0104 0114 0115 0125 0133 0134 0135 0146 0150 0152 0154

0156 0158 0159 0164 0167 0169 0175 0178 0179 0193 0194

0197 0204 0213 0214 0216 0225 0233 0252 0257 0263 0270

0280 0292 0297 0302 0304 0321 0325 0327 0329 0331 0335

0347 0352 0354 0359 0363 0367 0374 0378 0379 0385 0390

0395 0402 0406 0411 0415 0429 0433 0434 0438 0442 0446

0447 0459 0474 0538 0541 0544 0545 0546 0556 0559 0561

0562 0582 0585 0590 0598 0643 0646 0651 0793 0800

001 002

0005 0009 0014 0022 0026 0029 0038 0043 0046 0049 0078

0084 0145 0151 0168 0170 0173 0174 0176 0180 0186 0187

0192 0196 0199 0201 0207 0210 0217 0221 0237 0242 0243

0245 0246 0260 0264 0268 0273 0274 0278 0307 0310 0318

0319 0332 0355 0373 0377 0387 0399 0414 0483 0528 0554

0668 0955

002

(5) Configuration definition

**CONF 001

Config. 001 is valid for aircraft on which Mod. No. 58555S30640 (Service Bulletin No.

A340-34-4234) is not embodied.

**CONF 002

Config. 002 is valid for aircraft on which Mod. No. 58555S30640 (Service Bulletin No.

A340-34-4234) is embodied.

(6) Material Effectivity

No Material Set

B. CONCURRENT REQUIREMENTS

None

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

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SERVICE BULLETIN

C. REASON

(1) History

During Airbus Final Assembly Line reception flight test, AOA (Angle of Attack) data from

two aircraft (one per A/C) were found inaccurate during the in-flight production tests and

confirmed during DFDR (Digital Flight Data Recorder) analysis.

Investigation of the removed probes revealed oil residue between the stator and the

rotor parts of the AOA vane position resolvers. The presence of this oil residue results

from a quality escape during the manufacturing process of the AOA resolvers, which led

to a poor cleaning of machining oil.

The oil residue has been found to become viscous at low temperatures (typically in

cruise) causing lag of AOA vane movement.

(2) Objective/Action

This Inspection Service Bulletin requires the inspection of THALES AOA probes PN

C16291AA and PN C16291AB. For those AOA probes corresponding to the batch

of serial numbers listed in VSB C16291A-34-007 revision 01 or any later revision,

replacement of the AOA probe is required.

(3) Advantages

Accomplishment of this Service Bulletin will ensure that AOA probes potentially affected

by the oil residue issue are replaced on aircraft.

(4) Operational/Maintenance Consequences

None

D. DESCRIPTION

NOTE: For Config. 001, depending on the result of the inspection, four possibilities

are available:

- either replace the affected AOA probes as described in TASK

344239-831-801 001 Replacement of the THALES AOA Probes by Part

Number C16291AB whose SN is not listed in THALES AVIONICS Service

Bulletin No. C16291A-34-007 Revision No. 01 (or any later revision).

- or replace them as described in TASK 344239-831-802 001 Replacement

of the THALES AOA Probes by Part Number C16291AA whose Serial

Number is not listed in the THALES VSB C16291A-34-007 Revision No.

01 (or any later revision).

- or replace them as described in TASK 344239-831-804 001 Replacement

of the THALES AOA Probes by Part Number post Vendor Service Bulletin

THALES AVIONICS C16291A-34-007 Revision No. 01 (or any later

revision).

- or replace them as described in TASK 344239-831-803 001 Replacement

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

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SERVICE BULLETIN

of the three THALES AOA Probes through Airbus RFC/RMO Process.

NOTE: For Config. 002, depending on the result of the inspection, three possibilities

are available:

- either replace the affected AOA probes as described in TASK

344239-831-801 001 Replacement of the THALES AOA Probes by Part

Number C16291AB whose SN is not listed in THALES AVIONICS Service

Bulletin No. C16291A-34-007 Revision No. 01 (or any later revision).

- or replace them as described in TASK 344239-831-803 001 Replacement

of the three THALES AOA Probes through Airbus RFC/RMO Process.

- or replace them as described in TASK 344239-831-804 001 Replacement

of the THALES AOA Probes by Part Number post Vendor Service Bulletin

THALES AVIONICS C16291A-34-007 Revision No. 01 (or any later

revision).

To accomplish this Service Bulletin it is necessary to :

**CONF 001

Task 344239-832-801-001: Inspection

(1) Inspection of the three AOA probes (3FP1, 3FP2, 3FP3)

Task 344239-831-801-001: Replacement of the THALES AOA Probes by Part Number

C16291AB whose SN is not listed in THALES AVIONICS Service Bulletin No.

C16291A-34-007 Revision No. 01 (or any later revision).

(1) Replace the affected THALES AOA Probes by PN C16291AB whose SN is not listed

in THALES AVIONICS Service Bulletin No. C16291A-34-007 Revision No. 01 (or any

later revision).

Task 344239-831-802-001: Replacement of the THALES AOA Probes by Part Number

C16291AA whose Serial Number is not listed in the THALES VSB C16291A-34-007 Revision

No. 01 (or any later revision).

(1) Replace the affected THALES AOA Probes by PN whose Serial Number is not listed

in the THALES VSB C16291A-34-007 Rev. 01 or any later revision.

Task 344239-831-803-001: Replacement of the three THALES AOA Probes through Airbus

RFC/RMO Process.

(1) Replace the affected AOA Probes through Airbus RFC/RMO Process.

Task 344239-831-804-001: Replacement of the THALES AOA Probes by Part Number post

Vendor Service Bulletin THALES AVIONICS C16291A-34-007 Revision No. 01 (or any later

revision).

(1) Remove the affected AOA Probes.

(2) Modify the AOA Probes.

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

REVISION No.: 01 - Sep 17/13 Page: 5

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SERVICE BULLETIN

(3) Install the AOA Probes

**CONF 002

Task 344239-832-801-001: Inspection

(1) Inspection of the three AOA probes (3FP1, 3FP2, 3FP3)

Task 344239-831-801-001: Replacement of the THALES AOA Probes by Part Number

C16291AB whose SN is not listed in THALES AVIONICS Service Bulletin No.

C16291A-34-007 Revision No. 01 (or any later revision).

(1) Replace the affected THALES AOA Probes by PN C16291AB whose SN is not listed

in THALES AVIONICS Service Bulletin No. C16291A-34-007 Revision No. 01 (or any

later revision).

Task 344239-831-803-001: Replacement of the three THALES AOA Probes through Airbus

RFC/RMO Process.

(1) Replace the affected AOA Probes through Airbus RFC/RMO Process.

Task 344239-831-804-001: Replacement of the THALES AOA Probes by Part Number post

Vendor Service Bulletin THALES AVIONICS C16291A-34-007 Revision No. 01 (or any later

revision).

(1) Remove the affected AOA Probes.

(2) Modify the AOA Probes.

(3) Install the AOA Probes

Task 344239-832-802-001: Inspection - ADDITIONAL WORK for Aircraft modified by Original

Issue.

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

**CONF ALL

E. COMPLIANCE

(1) Classification

MANDATORY: Service Bulletin must be accomplished.

(2) Accomplishment Timescale

**CONF 001

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

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

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

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

REVISION No.: 01 - Sep 17/13 Page: 6

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SERVICE BULLETIN

Table 1, Config. 001 - Detailed Inspection of AOA Probes

Condition Action Compliance Time Repetitive Interval

All aircraft potentially

fitted with PN

C16291AA

Inspect in accordance

with TASK

344239-832-801 001

Inspection

NOTE*

At the earliest

maintenance opportunity

after ISB receipt and

before end of April 2010

None

Replace the affected

AOA probes as per

TASK 344239-831-801

001 Replacement of the

THALES AOA Probes

by Part Number

C16291AB whose SN is

not listed in THALES

AVIONICS Service

Bulletin No.

C16291A-34-007

Revision No. 01 (or any

later revision).

or TASK

344239-831-802 001

Replacement of the

THALES AOA Probes

by Part Number

C16291AA whose Serial

Number is not listed in

the THALES VSB

C16291A-34-007

Revision No. 01 (or any

later revision).

or TASK

344239-831-803 001

Replacement of the

three THALES AOA

Probes through Airbus

RFC/RMO Process.

or TASK

344239-831-804 001

Replacement of the

THALES AOA Probes

by Part Number post

Vendor Service Bulletin

THALES AVIONICS

C16291A-34-007

Revision No. 01 (or any

later revision).

Before end of April 2010 None

AND

Part Number C16291AA

installed with AOA Serial

Number listed in Vendor

SB C16291A-34-007

revision 01 (or any later

revision) and Mod

No.53368S18144 (or

Service Bulletin

A340-34-4213)

embodied

No further action None None

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

REVISION No.: 01 - Sep 17/13 Page: 7

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SERVICE BULLETIN

Table 1, Config. 001 - Detailed Inspection of AOA Probes

Condition Action Compliance Time Repetitive Interval

Replace the affected

AOA probes as per

TASK 344239-831-801

001 Replacement of the

THALES AOA Probes

by Part Number

C16291AB whose SN is

not listed in THALES

AVIONICS Service

Bulletin No.

C16291A-34-007

Revision No. 01 (or any

later revision).

or TASK

344239-831-802 001

Replacement of the

THALES AOA Probes

by Part Number

C16291AA whose Serial

Number is not listed in

the THALES VSB

C16291A-34-007

Revision No. 01 (or any

later revision).

or TASK

344239-831-803 001

Replacement of the

three THALES AOA

Probes through Airbus

RFC/RMO Process.

or TASK

344239-831-804 001

Replacement of the

THALES AOA Probes

by Part Number post

Vendor Service Bulletin

THALES AVIONICS

C16291A-34-007

Revision No. 01 (or any

later revision).

Before end of April 2011 None

AND

Part Number C16291AA

installed with AOA Serial

Number listed in VSB

C16291A-34-007

revision 01 (or any later

revision) and

53368S18144 (or

Service Bulletin

A340-34-4213) not

embodied

No further action None None

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

REVISION No.: 01 - Sep 17/13 Page: 8

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SERVICE BULLETIN

Table 1, Config. 001 - Detailed Inspection of AOA Probes

Condition Action Compliance Time Repetitive Interval

Part Number C16291AA

not installed or PN

C16291AA installed but

AOA Serial Number not

listed in VSB

C16291A-34-007

revision 01 (or any later

revision)

No further action None None

NOTE*: A review of aircraft maintenance records is acceptable to determine the SN of the AOA

Probes.

**CONF 002

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

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

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

Table 1, Config. 002 - Detailed Inspection of AOA Probes

Condition Action Compliance Time Repetitive Interval

All aircraft potentially

fitted with PN C16291AB

Inspect in accordance

with TASK

344239-832-801 001

Inspection

NOTE*

At the earliest

maintenance opportunity

after ISB receipt and

before end of

September 2013

None

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

REVISION No.: 01 - Sep 17/13 Page: 9

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SERVICE BULLETIN

Table 1, Config. 002 - Detailed Inspection of AOA Probes

Condition Action Compliance Time Repetitive Interval

Replace the affected

AOA probes as per

TASK 344239-831-801

001 Replacement of the

THALES AOA Probes

by Part Number

C16291AB whose SN is

not listed in THALES

AVIONICS Service

Bulletin No.

C16291A-34-007

Revision No. 01 (or any

later revision).

or

TASK 344239-831-803

001 Replacement of the

three THALES AOA

Probes through Airbus

RFC/RMO Process.

or

TASK 344239-831-804

001 Replacement of the

THALES AOA Probes

by Part Number post

Vendor Service Bulletin

THALES AVIONICS

C16291A-34-007

Revision No. 01 (or any

later revision).

Before end of

September 2013

None

AND

Part Number C16291AB

installed with AOA Serial

Number listed in Vendor

SB C16291A-34-007

revision 01 (or any later

revision)

No further action None None

Part Number C16291AB

not installed or PN

C16291AB installed but

AOA Serial Number not

listed in VSB

C16291A-34-007

revision 01 (or any later

revision)

No further action None None

NOTE*: A review of aircraft maintenance records is acceptable to determine the SN of the AOA

Probes.

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

REVISION No.: 01 - Sep 17/13 Page: 10

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SERVICE BULLETIN

Table 2, Config. 002 - ADDITIONAL WORK - Detailed Inspection of AOA Probes

Condition Action Compliance Time Repetitive Interval

All aircraft potentially

fitted with PN

C16291AB

Inspect in accordance

with TASK

344239-832-801 001

Inspection

NOTE*

At the earliest

maintenance opportunity

after ISB receipt and

before end of September

2013

None

Replace the affected

AOA probes as per

TASK 344239-831-801

001 Replacement of the

THALES AOA Probes

by Part Number

C16291AB whose SN is

not listed in THALES

AVIONICS Service

Bulletin No.

C16291A-34-007

Revision No. 01 (or any

later revision).

or

TASK 344239-831-803

001 Replacement of the

three THALES AOA

Probes through Airbus

RFC/RMO Process.

or

TASK 344239-831-804

001 Replacement of the

THALES AOA Probes

by Part Number post

Vendor Service Bulletin

THALES AVIONICS

C16291A-34-007

Revision No. 01 (or any

later revision).

Before end of September

2013

None

AND

Part Number C16291AB

installed with AOA Serial

Number listed in Vendor

SB C16291A-34-007

Revision No. 01 (or any

later revision)

No further action None None

Part Number C16291AB

not installed or PN

C16291AB installed but

AOA Serial Number not

listed in VSB

C16291A-34-007

Revision No. 01 (or any

later revision)

No further action None None

NOTE*: A review of aircraft maintenance records is acceptable to determine the SN of the AOA

Probes.

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

REVISION No.: 01 - Sep 17/13 Page: 11

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SERVICE BULLETIN

**CONF ALL

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 344239-832-801-001: Inspection

Get Access 0.50

On Aircraft

Inspection of the three AOA probes (3FP1, 3FP2,

3FP3)

1.50

Close-Up 0.50

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

Task 344239-831-801-001: Replacement of the THALES AOA Probes by Part Number

C16291AB whose SN is not listed in THALES AVIONICS Service Bulletin No. C16291A-34-007

Revision No. 01 (or any later revision).

Get Access 0.50

On Aircraft

Replace the affected THALES AOA Probes by PN

C16291AB whose SN is not listed in THALES

AVIONICS Service Bulletin No. C16291A-34-007

Revision No. 01 (or any later revision).

1.00

Tests 0.50

Close-Up 0.50

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

Task 344239-831-802-001: Replacement of the THALES AOA Probes by Part Number

C16291AA whose Serial Number is not listed in the THALES VSB C16291A-34-007 Revision

No. 01 (or any later revision).

Get Access 0.50

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

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Task 344239-831-802-001: Replacement of the THALES AOA Probes by Part Number

C16291AA whose Serial Number is not listed in the THALES VSB C16291A-34-007 Revision

No. 01 (or any later revision).

On Aircraft

Replace the affected THALES AOA Probes by PN

whose Serial Number is not listed in the THALES VSB

C16291A-34-007 Rev. 01 or any later revision.

1.00

Tests 0.50

Close-Up 0.50

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

Task 344239-831-803-001: Replacement of the three THALES AOA Probes through Airbus

RFC/RMO Process.

Get Access 0.50

On Aircraft

Replace the affected AOA Probes through Airbus

RFC/RMO Process.

1.00

Tests 0.50

Close-Up 0.50

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

Task 344239-831-804-001: Replacement of the THALES AOA Probes by Part Number post

Vendor Service Bulletin THALES AVIONICS C16291A-34-007 Revision No. 01 (or any later

revision).

Get Access 0.50

On Aircraft

Remove the affected AOA Probes. 0.50

Install the AOA Probes 0.50

Tests 0.50

Close-Up 0.50

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

Additional manhours related to Vendor SB; refer to:

Modify the AOA Probes. THALES AVIONICS Service Bulletin

No. C16291A-34-007

**CONF 002

Task 344239-832-801-001: Inspection

Get Access 0.50

On Aircraft

Inspection of the three AOA probes (3FP1, 3FP2,

3FP3)

1.50

Close-Up 0.50

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

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SERVICE BULLETIN

Task 344239-832-801-001: Inspection

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

Task 344239-831-801-001: Replacement of the THALES AOA Probes by Part Number

C16291AB whose SN is not listed in THALES AVIONICS Service Bulletin No. C16291A-34-007

Revision No. 01 (or any later revision).

Get Access 0.50

On Aircraft

Replace the affected THALES AOA Probes by PN

C16291AB whose SN is not listed in THALES

AVIONICS Service Bulletin No. C16291A-34-007

Revision No. 01 (or any later revision).

1.00

Tests 0.50

Close-Up 0.50

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

Task 344239-831-803-001: Replacement of the three THALES AOA Probes through Airbus

RFC/RMO Process.

Get Access 0.50

On Aircraft

Replace the affected AOA Probes through Airbus

RFC/RMO Process.

1.00

Tests 0.50

Close-Up 0.50

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

Task 344239-831-804-001: Replacement of the THALES AOA Probes by Part Number post

Vendor Service Bulletin THALES AVIONICS C16291A-34-007 Revision No. 01 (or any later

revision).

Get Access 0.50

On Aircraft

Remove the affected AOA Probes. 0.50

Install the AOA Probes 0.50

Tests 0.50

Close-Up 0.50

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

Additional manhours related to Vendor SB; refer to:

Modify the AOA Probes. THALES AVIONICS Service Bulletin

No. C16291A-34-007

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

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SERVICE BULLETIN

Task 344239-832-802-001: Inspection - ADDITIONAL WORK for Aircraft modified by Original

Issue.

Get Access 0.50

On Aircraft

Do a Detailed Inspection of the three AOA Probes

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

1.50

Close-Up 0.50

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

**CONF ALL

H. WEIGHT AND BALANCE

Not Changed

I. ELECTRICAL LOAD DATA

Not Changed

J. REFERENCES

**CONF 001

Aircraft Maintenance Manual (AMM) 06-41-53 12-34-24 34-11-19

52-10-00

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

Service Bulletin (SB) A340-34-4087

A340-34-4234

Vendor Service Bulletin (VSB) THALES AVIONICS Service

Bulletin No. C16291A-34-007

**CONF 002

Aircraft Maintenance Manual (AMM) 06-41-53 12-34-24 34-11-19

52-10-00

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

Service Bulletin (SB) A340-34-4087

Vendor Service Bulletin (VSB) THALES AVIONICS Service

Bulletin No. C16291A-34-007

**CONF ALL

K. PUBLICATION AFFECTED

None

L. INTERCHANGEABILITY/MIXABILITY

Not Applicable

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SERVICE BULLETIN

M. SPARES

None

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

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SERVICE BULLETIN

2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

(1) Procurement Addresses

Modification of removed equipment should be negotiated directly with THALES

AVIONICS as per instructions given in THALES AVIONICS Service Bulletin No.

C16291A-34-007.

(2) Price and Availability

No AIRBUS kit will be provided.

Refer to THALES AVIONICS Service Bulletin No. C16291A-34-007 for the equipment

modification sales terms.

B. INDUSTRY SUPPORT INFORMATION

Refer to THALES AVIONICS Service Bulletin No. C16291A-34-007 for the industry support

terms of the Vendor Service Bulletin parts and labor.

C. LIST OF COMPONENTS

No Kit

D. LIST OF MATERIALS - OPERATOR SUPPLIED

None

E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

None

F. TOOLING

None

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

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This Page Intentionally Left Blank

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

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SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS

Task 344239-832-801-001 - 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 CASE OF 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 or 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.

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

REVISION No.: 01 - Sep 17/13 Page: 19

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Task Associated Data

**CONF 001

Zone

121 122

Modified FIN

3FP1 3FP2 3FP3

Manpower

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

**CONF 002

Zone

121 122

Modified FIN

3FP1 3FP2 3FP3

Manpower

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

**CONF ALL

A. GENERAL

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.

**CONF 001

(1) Subtask 344239-839-001-001 - 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 344239-839-001-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

REVISION No.: 01 - Sep 17/13 Page: 20

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**CONF ALL

B. PREPARATION

**CONF 001

(1) Subtask 344239-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Task 12-34-24-860-802

Task 34-11-19-000-801

Task 52-10-00-010-801

(a) The following items 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.

- All controls in NORM, AUTO or OFF position.

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

12-34-24-860-802).

(c) Put an access platform(s) in position at the FWD passenger/crew door(s) 831 or

841.

(d) Open the FWD passenger/crew door(s) 831 or 841, refer to AMM 06-41-53, Page

Block 001 and AMM Task 52-10-00-010-801.

(e) Do the Job Set-up procedure as specified in the removal of the AOA Probes (FINs

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

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

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**CONF 002

(1) Subtask 344239-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Task 12-34-24-860-802

Task 34-11-19-000-801

Task 52-10-00-010-801

(a) The following items 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.

- All controls in NORM, AUTO or OFF position.

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

12-34-24-860-802).

(c) Put an access platform(s) in position at the FWD passenger/crew door(s) 831 or

841.

(d) Open the FWD passenger/crew door(s) 831 or 841, refer to AMM 06-41-53, Page

Block 001 and AMM Task 52-10-00-010-801.

(e) Do the Job Set-up procedure as specified in the removal of the AOA Probes (FINs

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

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

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**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 344239-832-001-001 - Inspection of the three AOA probes (3FP1, 3FP2,

3FP3)

Work Zones and Access Panels

Zone Access/Work location

121

122

Manpower Resources

Manhours 1.50

Minimum number of person 1

Subtask elapsed time 1.50

Skills NON SPECIFIC

References

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

Vendor Service Bulletin (VSB) THALES AVIONICS C16291A-34-007

Fig. A-FBAAA

Area to be inspected

Sheet 01

Fig. A-FFAAA

Flow Chart

Sheet 01

Fig. A-FRAAA

Inspection Report

Sheet 01

(a) At the threshold given in PLANNING INFORMATION paragraph E.(2):

Do a Detailed Inspection of the three AOA Probes (FINs 3FP1, 3FP2 and 3FP3).

Refer to Fig. A-FBAAA

Refer to Fig. A-FFAAA

1 Check the SN of the three AOA Probes (FINs 3FP1, 3FP2 and 3FP3), refer to

THALES AVIONICS Service Bulletin No. C16291A-34-007 Rev. 01 or any later

revision.

NOTE: If PN or/and SN are not clearly visible, remove the AOA

Probe, without disconnecting the connector, refer to AMM Task

34-11-19-000-801 to do the Inspection Requirements.

NOTE: A review of aircraft maintenance records is acceptable to

determine the SN of the AOA Probes.

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

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a If the AOA Probe is part of the affected SN:

<1> At the threshold given in PLANING INFORMATION paragraph E.(2),

do TASK 344239-831-801 001 Replacement of the THALES AOA

Probes by Part Number C16291AB whose SN is not listed in

THALES AVIONICS Service Bulletin No. C16291A-34-007 Revision

No. 01 (or any later revision).

or

Do TASK 344239-831-802 001 Replacement of the THALES AOA

Probes by Part Number C16291AA whose Serial Number is not

listed in the THALES VSB C16291A-34-007 Revision No. 01 (or any

later revision).

or

Do TASK 344239-831-803 001 Replacement of the three THALES

AOA Probes through Airbus RFC/RMO Process.

or

Do TASK 344239-831-804 001 Replacement of the THALES AOA

Probes by Part Number post Vendor Service Bulletin THALES

AVIONICS C16291A-34-007 Revision No. 01 (or any later revision).

<2> No further action is required.

b If the AOA Probe is not part of the affected SN:

<1> No further action is required.

(b) Send the Inspection Report to AIRBUS, refer to Fig. A-FRAAA.

**CONF 002

(1) Subtask 344239-832-001-002 - Inspection of the three AOA probes (3FP1, 3FP2,

3FP3)

Work Zones and Access Panels

Zone Access/Work location

121

122

Manpower Resources

Manhours 1.50

Minimum number of person 1

Subtask elapsed time 1.50

Skills NON SPECIFIC

References

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

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

REVISION No.: 01 - Sep 17/13 Page: 24

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References

Vendor Service Bulletin (VSB) THALES AVIONICS C16291A-34-007

Fig. A-FBAAA

Area to be inspected

Sheet 01

Fig. A-FRAAA

Inspection Report

Sheet 01

Fig. A-FFAAB

Flow Chart

Sheet 01

(a) At the threshold given in PLANNING INFORMATION paragraph E.(2):

Do a Detailed Inspection of the three AOA Probes (FINs 3FP1, 3FP2 and 3FP3).

Refer to Fig. A-FBAAA

Refer to Fig. A-FFAAB

1 Check the SN of the three AOA Probes (FINs 3FP1, 3FP2 and 3FP3), refer to

THALES AVIONICS Service Bulletin No. C16291A-34-007 Rev. 01 or any later

revision.

NOTE: If PN or/and SN are not clearly visible, remove the AOA

Probe, without disconnecting the connector, refer to AMM Task

34-11-19-000-801 to do the Inspection Requirements.

NOTE: A review of aircraft maintenance records is acceptable to

determine the SN of the AOA Probes.

a If the AOA Probe is part of the affected SN:

<1> At the threshold given in PLANING INFORMATION paragraph

E.(2)., do TASK 344239-831-801 001 Replacement of the THALES

AOA Probes by Part Number C16291AB whose SN is not listed in

THALES AVIONICS Service Bulletin No. C16291A-34-007 Revision

No. 01 (or any later revision).

or

Do TASK 344239-831-803 001 Replacement of the three THALES

AOA Probes through Airbus RFC/RMO Process.

or

Do TASK 344239-831-804 001 Replacement of the THALES AOA

Probes by Part Number post Vendor Service Bulletin THALES

AVIONICS C16291A-34-007 Revision No. 01 (or any later revision).

<2> No further action is required.

b If the AOA Probe is not part of the affected SN:

<1> No further action is required.

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

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(b) Send the Inspection Report to AIRBUS, refer to Fig. A-FRAAA.

**CONF ALL

D. TEST

**CONF 001

None

**CONF 002

None

**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 344239-942-001-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Task 34-11-19-400-801

Task 52-10-00-410-801

NOTE: If you intend to accomplish an associated Repair Task during the same

layover period, the subsequent Close-up procedure is not necessary.

(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 in the installation of the AOA probes, refer

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

(c) Close the FWD passenger/crew door(s) 831 or 841, refer to AMM 06-41-53, Page

Block 001 and AMM Task 52-10-00-410-801.

(d) Remove the access platform(s).

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

**CONF 002

(1) Subtask 344239-942-001-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

REVISION No.: 01 - Sep 17/13 Page: 26

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SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Task 34-11-19-400-801

Task 52-10-00-410-801

NOTE: If you intend to accomplish an associated Repair Task during the same

layover period, the subsequent Close-up procedure is not necessary.

(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 in the installation of the AOA probes, refer

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

(c) Close the FWD passenger/crew door(s) 831 or 841, refer to AMM 06-41-53, Page

Block 001 and AMM Task 52-10-00-410-801.

(d) Remove the access platform(s).

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

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

REVISION No.: 01 - Sep 17/13 Page: 27

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This Page Intentionally Left Blank

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

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Task 344239-831-801-001 - Replacement of the THALES AOA Probes by Part Number

C16291AB whose SN is not listed in THALES AVIONICS Service Bulletin No.

C16291A-34-007 Revision No. 01 (or any later revision).

**CONF ALL

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.

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 or 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.

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

REVISION No.: 01 - Sep 17/13 Page: 29

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SERVICE BULLETIN

Task Associated Data

**CONF 001

Zone

121 122

Modified FIN

3FP1 3FP2 3FP3

Manpower

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

**CONF 002

Zone

121 122

Modified FIN

3FP1 3FP2 3FP3

Manpower

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

**CONF ALL

A. GENERAL

**CONF 001

(1) Subtask 344239-839-003-001 - 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 344239-839-003-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

REVISION No.: 01 - Sep 17/13 Page: 30

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**CONF ALL

B. PREPARATION

**CONF 001

(1) Subtask 344239-941-003-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Task 12-34-24-860-802

Task 34-11-19-000-801

Task 52-10-00-010-801

NOTE: If you intend to accomplish this Repair Task during the same layover

period as the associated Inspection, the subsequent Preparation

procedure is not necessary.

(a) The following items 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.

- All controls in NORM, AUTO or OFF position.

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

12-34-24-860-802).

(c) Put an access platform(s) in position at the FWD passenger/crew door(s) 831 or

841.

(d) Open the FWD passenger/crew door(s) 831 or 841, refer to AMM 06-41-53, Page

Block 001 and AMM Task 52-10-00-010-801.

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REVISION No.: 01 - Sep 17/13 Page: 31

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(e) Do the Job Set-up procedure as specified in the removal of the AOA Probes (FINs

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

**CONF 002

(1) Subtask 344239-941-003-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Task 12-34-24-860-802

Task 34-11-19-000-801

Task 52-10-00-010-801

NOTE: If you intend to accomplish this Repair Task during the same layover

period as the associated Inspection, the subsequent Preparation

procedure is not necessary.

(a) The following items 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.

- All controls in NORM, AUTO or OFF position.

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

12-34-24-860-802).

(c) Put an access platform(s) in position at the FWD passenger/crew door(s) 831 or

841.

(d) Open the FWD passenger/crew door(s) 831 or 841, refer to AMM 06-41-53, Page

Block 001 and AMM Task 52-10-00-010-801.

(e) Do the Job Set-up procedure as specified in the removal of the AOA Probes (FINs

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

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

REVISION No.: 01 - Sep 17/13 Page: 32

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**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 344239-960-002-001 - Replace the affected THALES AOA Probes by PN

C16291AB whose SN is not listed in THALES AVIONICS Service Bulletin No.

C16291A-34-007 Revision No. 01 (or any later revision).

Work Zones and Access Panels

Zone Access/Work location

121

122

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

References

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

Task 34-11-19-400-801

Service Bulletin (SB) A340-34-4234

Vendor Service Bulletin (VSB) THALES AVIONICS C16291A-34-007

(a) Remove (Refer to AMM Task 34-11-19-000-801) :

1 3FP1, AOA probe, C16291AA.

- and/or

2 3FP2, AOA probe, C16291AA.

- and/or

3 3FP3, AOA probe, C16291AA.

(b) Install (Refer to AMM Task 34-11-19-400-801) :

NOTE: The replacement of the AOA probes is covered by Service Bulletin

No. A340-34-4234.

NOTE: Install AOA Probes whose Serial Number is not listed in THALES

AVIONICS Service Bulletin No. C16291A-34-007 Revision No. 01

(or any later revision).

1 3FP1, AOA probe, C16291AB.

- and/or

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

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2 3FP2, AOA probe, C16291AB.

- and/or

3 3FP3, AOA probe, C16291AB.

**CONF 002

(1) Subtask 344239-960-002-002 - Replace the affected THALES AOA Probes by PN

C16291AB whose SN is not listed in THALES AVIONICS Service Bulletin No.

C16291A-34-007 Revision No. 01 (or any later revision).

Work Zones and Access Panels

Zone Access/Work location

121

122

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

References

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

Task 34-11-19-400-801

Vendor Service Bulletin (VSB) THALES AVIONICS C16291A-34-007

(a) Remove:

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

1 3FP1, AOA probe, C16291AB.

and/or

2 3FP2, AOA probe, C16291AB.

and/or

3 3FP3, AOA probe, C16291AB.

(b) Install:

Refer to AMM Task 34-11-19-400-801

NOTE: Install AOA Probes whose Serial Number is not listed in THALES

AVIONICS Service Bulletin No. C16291A-34-007 Revision No. 01

(or any later revision).

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1 3FP1, AOA probe, C16291AB.

and/or

2 3FP2, AOA probe, C16291AB.

and/or

3 3FP3, AOA probe, C16291AB.

**CONF ALL

D. TEST

**CONF 001

(1) Subtask 344239-700-002-001 - Test

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, 3FP2 and

3FP3), refer to AMM Task 34-11-19-400-801.

(b) Test:

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

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

**CONF 002

(1) Subtask 344239-700-002-001 - Test

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, 3FP2 and

3FP3), refer to AMM Task 34-11-19-400-801.

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

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SERVICE BULLETIN

(b) Test:

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

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

**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 344239-942-003-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Task 34-11-19-400-801

Task 52-10-00-410-801

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

equipment.

(b) Do the Close-up procedure as specified in the installation of the AOA Probes (FINs

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

(c) Close the FWD passenger/crew door(s) 831 or 841, refer to AMM 06-41-53, Page

Block 001 and AMM Task 52-10-00-410-801.

(d) Remove the access platform(s).

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

**CONF 002

(1) Subtask 344239-942-003-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Task 34-11-19-400-801

Task 52-10-00-410-801

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

equipment.

(b) Do the Close-up procedure as specified in the installation of the AOA Probes (FINs

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

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

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SERVICE BULLETIN

(c) Close the FWD passenger/crew door(s) 831 or 841, refer to AMM 06-41-53, Page

Block 001 and AMM Task 52-10-00-410-801.

(d) Remove the access platform(s).

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

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

REVISION No.: 01 - Sep 17/13 Page: 37

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This Page Intentionally Left Blank

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

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SERVICE BULLETIN

Task 344239-831-802-001 - Replacement of the THALES AOA Probes by Part Number

C16291AA whose Serial Number is not listed in the THALES VSB C16291A-34-007 Revision

No. 01 (or any later revision).

**CONF ALL

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.

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 or 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.

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

REVISION No.: 01 - Sep 17/13 Page: 39

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SERVICE BULLETIN

Task Associated Data

**CONF 001

Zone

121 122

Modified FIN

3FP1 3FP2 3FP3

Manpower

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

**CONF 002

None

**CONF ALL

A. GENERAL

**CONF 001

(1) Subtask 344239-839-004-001 - 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

None

**CONF ALL

B. PREPARATION

**CONF 001

(1) Subtask 344239-941-004-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Task 12-34-24-860-802

Task 12-34-24-860-802

Task 34-11-19-000-801

Task 52-10-00-010-801

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

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SERVICE BULLETIN

NOTE: If you intend to accomplish this Repair Task during the same layover

period as the associated Inspection, the subsequent Preparation

procedure is not necessary.

(a) The following items 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.

- All controls in NORM, AUTO or OFF position.

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

12-34-24-860-802.

(c) Put an access platform(s) in position at the FWD passenger/crew door(s) 831 or

841.

(d) Open the FWD passenger/crew door(s) 831 or 841, refer to AMM 06-41-53, Page

Block 001 and AMM Task 52-10-00-010-801.

(e) Do the Job Set-up procedure as specified in the removal of the AOA Probes (FINs

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

**CONF 002

None

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

REVISION No.: 01 - Sep 17/13 Page: 41

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SERVICE BULLETIN

**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 344239-960-003-001 - Replace the affected THALES AOA Probes by PN

whose Serial Number is not listed in the THALES VSB C16291A-34-007 Rev. 01 or

any later revision.

Work Zones and Access Panels

Zone Access/Work location

121

122

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

References

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

Task 34-11-19-400-801

Vendor Service Bulletin (VSB) THALES AVIONICS C16291A-34-007

(a) Remove (Refer to AMM Task 34-11-19-000-801) :

1 3FP1, AOA probe, C16291AA.

- and/or

2 3FP2, AOA probe, C16291AA.

- and/or

3 3FP3, AOA probe, C16291AA.

(b) Install (Refer to AMM Task 34-11-19-400-801) :

NOTE: You must install AOA probes whose Serial Number is not listed in

THALES AVIONICS Service Bulletin No. C16291A-34-007 revision

01 or any later revision.

1 3FP1, AOA probe, C16291AA.

- and/or

2 3FP2, AOA probe, C16291AA.

- and/or

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

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SERVICE BULLETIN

3 3FP3, AOA probe, C16291AA.

**CONF 002

None

**CONF ALL

D. TEST

**CONF 001

(1) Subtask 344239-700-003-001 - Test

Manpower Resources

Skills NON SPECIFIC

References

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

(a) Job set-up :

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

after the installation of the AOA probes (3FP1, 3FP2, 3FP3) (Refer to AMM

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

(b) Test :

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

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

**CONF 002

None

**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 344239-942-004-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Task 34-11-19-400-801

Task 52-10-00-410-801

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

equipment.

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

REVISION No.: 01 - Sep 17/13 Page: 43

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SERVICE BULLETIN

(b) Do the Close-up procedure as specified in the installation of the AOA Probes (FINs

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

(c) Close the FWD passenger/crew door(s) 831 or 841, refer to AMM 06-41-53, Page

Block 001 and AMM Task 52-10-00-410-801.

(d) Remove the access platform(s).

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

**CONF 002

None

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

REVISION No.: 01 - Sep 17/13 Page: 44

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SERVICE BULLETIN

Task 344239-831-803-001 - Replacement of the three THALES AOA Probes through Airbus

RFC/RMO Process.

**CONF ALL

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.

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 or 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.

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

REVISION No.: 01 - Sep 17/13 Page: 45

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SERVICE BULLETIN

Task Associated Data

**CONF 001

Zone

121 122

Modified FIN

3FP1 3FP2 3FP3

Manpower

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

**CONF 002

Zone

121 122

Modified FIN

3FP1 3FP2 3FP3

Manpower

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

**CONF ALL

A. GENERAL

**CONF 001

(1) Subtask 344239-839-005-001 - 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 344239-839-005-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

REVISION No.: 01 - Sep 17/13 Page: 46

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SERVICE BULLETIN

**CONF ALL

B. PREPARATION

**CONF 001

(1) Subtask 344239-941-005-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Task 12-34-24-860-802

Task 34-11-19-000-801

Task 52-10-00-010-801

NOTE: If you intend to accomplish this Repair Task during the same layover

period as the associated Inspection, the subsequent Preparation

procedure is not necessary.

(a) The following items 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.

- All controls in NORM, AUTO or OFF position.

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

12-34-24-860-802.

(c) Put an access platform(s) in position at the FWD passenger/crew door(s) 831 or

841.

(d) Open the FWD passenger/crew door(s) 831 or 841, refer to AMM 06-41-53, Page

Block 001 and AMM Task 52-10-00-010-801.

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

REVISION No.: 01 - Sep 17/13 Page: 47

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SERVICE BULLETIN

(e) Do the Job Set-up procedure as specified in the removal of the AOA Probes (FINs

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

**CONF 002

(1) Subtask 344239-941-005-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Task 12-34-24-860-802

Task 34-11-19-000-801

Task 52-10-00-010-801

NOTE: If you intend to accomplish this Repair Task during the same layover

period as the associated Inspection, the subsequent Preparation

procedure is not necessary.

(a) The following items 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.

- All controls in NORM, AUTO or OFF position.

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

12-34-24-860-802.

(c) Put an access platform(s) in position at the FWD passenger/crew door(s) 831 or

841.

(d) Open the FWD passenger/crew door(s) 831 or 841, refer to AMM 06-41-53, Page

Block 001 and AMM Task 52-10-00-010-801.

(e) Do the Job Set-up procedure as specified in the removal of the AOA Probes (FINs

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

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

REVISION No.: 01 - Sep 17/13 Page: 48

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SERVICE BULLETIN

**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 344239-960-004-001 - Replace the affected AOA Probes through Airbus

RFC/RMO Process.

Work Zones and Access Panels

Zone Access/Work location

121

122

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

References

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

Task 34-11-19-400-801

Service Bulletin (SB) A340-34-4087

Vendor Service Bulletin (VSB) THALES AVIONICS C16291A-34-007

(a) Remove (Refer to AMM Task 34-11-19-000-801) :

1 3FP1, AOA probe, C16291AA.

- and

2 3FP2, AOA probe, C16291AA.

- and

3 3FP3, AOA probe, C16291AA.

(b) Install (Refer to AMM Task 34-11-19-400-801) :

NOTE: The replacement of the three THALES AOA probes by three

GOODRICH PN 0861ED is covered by Service Bulletin No.

A340-34-4087 or by RFC/RMO procedure.

1 3FP1, AOA probe, 0861ED.

- and

2 3FP2, AOA probe, 0861ED.

- and

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

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SERVICE BULLETIN

3 3FP3, AOA probe, 0861ED.

**CONF 002

(1) Subtask 344239-960-004-002 - Replace the affected AOA Probes through Airbus

RFC/RMO Process.

Work Zones and Access Panels

Zone Access/Work location

121

122

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

References

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

Task 34-11-19-400-801

Service Bulletin (SB) A340-34-4087

(a) Remove:

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

1 3FP1, AOA probe, C16291AB.

- and

2 3FP2, AOA probe, C16291AB.

- and

3 3FP3, AOA probe, C16291AB.

(b) Install:

Refer to AMM Task 34-11-19-400-801

NOTE: The replacement of the three THALES AOA probes by three

GOODRICH PN 0861ED is covered by Service Bulletin No.

A340-34-4087 or by RFC/RMO procedure.

1 3FP1, AOA probe, 0861ED.

- and

2 3FP2, AOA probe, 0861ED.

- and

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

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SERVICE BULLETIN

3 3FP3, AOA probe, 0861ED.

**CONF ALL

D. TEST

**CONF 001

(1) Subtask 344239-700-004-001 - Test

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, 3FP2 and

3FP3), refer to AMM Task 34-11-19-400-801.

(b) Test:

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

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

**CONF 002

(1) Subtask 344239-700-004-001 - Test

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, 3FP2 and

3FP3), refer to AMM Task 34-11-19-400-801.

(b) Test:

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

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

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

REVISION No.: 01 - Sep 17/13 Page: 51

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**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 344239-942-006-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Task 34-11-19-400-801

Task 52-10-00-410-801

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

equipment.

(b) Do the Close-up procedure as specified in the installation of the AOA Probes (FINs

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

(c) Close the FWD passenger/crew door(s) 831 or 841, refer to AMM 06-41-53, Page

Block 001 and AMM Task 52-10-00-410-801.

(d) Remove the access platform(s).

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

**CONF 002

(1) Subtask 344239-942-006-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Task 34-11-19-400-801

Task 52-10-00-410-801

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

equipment.

(b) Do the Close-up procedure as specified in the installation of the AOA Probes (FINs

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

(c) Close the FWD passenger/crew door(s) 831 or 841, refer to AMM 06-41-53, Page

Block 001 and AMM Task 52-10-00-410-801.

(d) Remove the access platform(s).

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

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

REVISION No.: 01 - Sep 17/13 Page: 52

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Task 344239-831-804-001 - Replacement of the THALES AOA Probes by Part Number post

Vendor Service Bulletin THALES AVIONICS C16291A-34-007 Revision No. 01 (or any later

revision).

**CONF ALL

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.

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 or 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.

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

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Task Associated Data

**CONF 001

Zone

121 122

Modified FIN

3FP1 3FP2 3FP3

Manpower

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

Additional manhours related to Vendor SB; refer to:

THALES AVIONICS Service Bulletin No. C16291A-34-007

**CONF 002

Zone

121 122

Modified FIN

3FP1 3FP2 3FP3

Manpower

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

Additional manhours related to Vendor SB; refer to:

THALES AVIONICS Service Bulletin No. C16291A-34-007

**CONF ALL

A. GENERAL

**CONF 001

(1) Subtask 344239-839-006-001 - 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 344239-839-006-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

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**CONF ALL

B. PREPARATION

**CONF 001

(1) Subtask 344239-941-006-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Task 12-34-24-860-802

Task 34-11-19-000-801

Task 52-10-00-010-801

NOTE: If you intend to accomplish this Repair Task during the same layover

period as the associated Inspection, the subsequent Preparation

procedure is not necessary.

(a) The following items 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.

- All controls in NORM, AUTO or OFF position.

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

12-34-24-860-802.

(c) Put an access platform(s) in position at the FWD passenger/crew door(s) 831 or

841.

(d) Open the FWD passenger/crew door(s) 831 or 841, refer to AMM 06-41-53, Page

Block 001 and AMM Task 52-10-00-010-801.

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

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(e) Do the Job Set-up procedure as specified in the removal of the AOA Probes (FINs

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

**CONF 002

(1) Subtask 344239-941-006-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Task 12-34-24-860-802

Task 34-11-19-000-801

Task 52-10-00-010-801

NOTE: If you intend to accomplish this Repair Task during the same layover

period as the associated Inspection, the subsequent Preparation

procedure is not necessary.

(a) The following items 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.

- All controls in NORM, AUTO or OFF position.

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

12-34-24-860-802.

(c) Put an access platform(s) in position at the FWD passenger/crew door(s) 831 or

841.

(d) Open the FWD passenger/crew door(s) 831 or 841, refer to AMM 06-41-53, Page

Block 001 and AMM Task 52-10-00-010-801.

(e) Do the Job Set-up procedure as specified in the removal of the AOA Probes (FINs

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

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

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**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 344239-960-005-001 - Remove the affected AOA Probes.

Work Zones and Access Panels

Zone Access/Work location

121

122

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills ELECTRICAL

References

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

(a) Remove:

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

1 3FP1, AOA probe, C16291AA.

- and/or

2 3FP2, AOA probe, C16291AA.

- and/or

3 3FP3, AOA probe, C16291AA.

(2) Subtask 344239-831-002-001 - Modify the AOA Probes.

References

Vendor Service Bulletin (VSB) THALES AVIONICS C16291A-34-007

(a) Modify the affected AOA Probes (FINs 3FP1 and/or 3FP2 and/or 3FP3) as per

instructions given in THALES AVIONICS Service Bulletin No. C16291A-34-007.

(3) Subtask 344239-831-003-001 - Install the AOA Probes

Work Zones and Access Panels

Zone Access/Work location

121

122

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Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills ELECTRICAL

References

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

(a) Install:

Refer to AMM Task 34-11-19-400-801

1 3FP1, AOA probe, C16291AA post THALES AVIONICS Service Bulletin

No.C16291A-34-007 Rev. 01 or any later revision.

- and/or

2 3FP2, AOA probe, C16291AA post THALES AVIONICS Service Bulletin

No.C16291A-34-007 Rev. 01 or any later revision.

- and/or

3 3FP3, AOA probe, C16291AA post THALES AVIONICS Service Bulletin

No.C16291A-34-007 Rev. 01 or any later revision.

**CONF 002

(1) Subtask 344239-960-005-003 - Remove the affected AOA Probes.

Work Zones and Access Panels

Zone Access/Work location

121

122

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills ELECTRICAL

References

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

(a) Remove:

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

1 3FP1, AOA probe, C16291AB.

- and/or

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2 3FP2, AOA probe, C16291AB.

- and/or

3 3FP3, AOA probe, C16291AB.

(2) Subtask 344239-831-002-001 - Modify the AOA Probes.

References

Vendor Service Bulletin (VSB) THALES AVIONICS C16291A-34-007

(a) Modify the affected AOA Probes (FINs 3FP1 and/or 3FP2 and/or 3FP3) as per

instructions given in THALES AVIONICS Service Bulletin No. C16291A-34-007.

(3) Subtask 344239-831-003-002 - Install the AOA Probes

Work Zones and Access Panels

Zone Access/Work location

121

122

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills ELECTRICAL

References

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

(a) Install:

Refer to AMM Task 34-11-19-400-801

1 3FP1, AOA probe, C16291AB post THALES AVIONICS Service Bulletin

No.C16291A-34-007 Rev. 01 or any later revision.

- and/or

2 3FP2, AOA probe, C16291AB post THALES AVIONICS Service Bulletin

No.C16291A-34-007 Rev. 01 or any later revision.

- and/or

3 3FP3, AOA probe, C16291AB post THALES AVIONICS Service Bulletin

No.C16291A-34-007 Rev. 01 or any later revision.

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**CONF ALL

D. TEST

**CONF 001

(1) Subtask 344239-700-005-001 - Test

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 (FINs3FP1, 3FP2 and

3FP3) refer to AMM Task 34-11-19-400-801.

(b) Test :

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

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

**CONF 002

(1) Subtask 344239-700-005-001 - Test

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 (FINs3FP1, 3FP2 and

3FP3) refer to AMM Task 34-11-19-400-801.

(b) Test :

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

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

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

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**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 344239-942-007-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Task 34-11-19-400-801

Task 52-10-00-410-801

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

equipment.

(b) Do the Close-up procedure as specified in the installation of the AOA Probes (FINs

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

(c) Close the FWD passenger/crew door(s) 831 or 841, refer to AMM 06-41-53, Page

Block 001 and AMM Task 52-10-00-410-801.

(d) Remove the access platform(s).

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

**CONF 002

(1) Subtask 344239-942-007-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Task 34-11-19-400-801

Task 52-10-00-410-801

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

equipment.

(b) Do the Close-up procedure as specified in the installation of the AOA Probes (FINs

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

(c) Close the FWD passenger/crew door(s) 831 or 841, refer to AMM 06-41-53, Page

Block 001 and AMM Task 52-10-00-410-801.

(d) Remove the access platform(s).

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

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

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This Page Intentionally Left Blank

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

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Task 344239-832-802-001 - Inspection - ADDITIONAL WORK for Aircraft modified by Original

Issue.

**CONF ALL

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.

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 or 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.

Task Associated Data

**CONF 001

None

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

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**CONF 002

Zone

121 122

Modified FIN

3FP1 3FP2 3FP3

Manpower

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

**CONF ALL

A. GENERAL

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.

**CONF 001

None

**CONF 002

(1) Subtask 344239-839-007-001 - 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

None

**CONF 002

(1) Subtask 344239-941-007-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Task 12-34-24-860-802

Task 34-11-19-000-801

Task 52-10-00-010-801

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(a) The following items 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.

- All controls in NORM, AUTO or OFF position.

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

12-34-24-860-802.

(c) Put an access platform(s) in position at the FWD passenger/crew door(s) 831 or

841.

(d) Open the FWD passenger/crew door(s) 831 or 841, refer to AMM 06-41-53, Page

Block 001 and AMM Task 52-10-00-010-801.

(e) Do the Job Set-up procedure as specified in the removal of the AOA Probes (FINs

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

**CONF ALL

C. PROCEDURE

**CONF 001

None

**CONF 002

(1) Subtask 344239-832-002-001 - Do a Detailed Inspection of the three AOA Probes

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

Work Zones and Access Panels

Zone Access/Work location

121

122

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

REVISION No.: 01 - Sep 17/13 Page: 65

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Manpower Resources

Manhours 1.50

Minimum number of person 1

Subtask elapsed time 1.50

Skills NON SPECIFIC

References

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

Vendor Service Bulletin (VSB) THALES AVIONICS C16291A-34-007

Fig. A-FBAAA

Area to be inspected

Sheet 01

Fig. A-FFBAA

Flow Chart (ADDITIONAL WORK)

Sheet 01

Fig. A-FRAAA

Inspection Report

Sheet 01

(a) At the threshold given in PLANNING INFORMATION paragraph E.(2):

Do a Detailed Inspection of the three AOA Probes (FINs 3FP1, 3FP2 and 3FP3).

Refer to Fig. A-FBAAA

Refer to Fig. A-FFBAA

1 Check the SN of the three AOA Probes (FINs 3FP1, 3FP2 and 3FP3), refer to

THALES AVIONICS Service Bulletin No. C16291A-34-007 Rev. 01 or any later

revision.

NOTE: If PN or/and SN are not clearly visible, remove the AOA

Probe, without disconnecting the connector, refer to AMM Task

34-11-19-000-801 to do the Inspection Requirements.

NOTE: A review of aircraft maintenance records is acceptable to

determine the SN of the AOA Probes.

a If the AOA Probe is part of the affected SN:

<1> At the threshold given in PLANNING INFORMATION paragraph

E.(2), do TASK 344239-831-801 001 Replacement of the THALES

AOA Probes by Part Number C16291AB whose SN is not listed in

THALES AVIONICS Service Bulletin No. C16291A-34-007 Revision

No. 01 (or any later revision).

or

Do TASK 344239-831-803 001 Replacement of the three THALES

AOA Probes through Airbus RFC/RMO Process.

or

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Do TASK 344239-831-804 001 Replacement of the THALES AOA

Probes by Part Number post Vendor Service Bulletin THALES

AVIONICS C16291A-34-007 Revision No. 01 (or any later revision).

<2> No further action is required.

b If the AOA Probe is not part of the affected SN:

<1> No further action is required.

(b) Send the Inspection Report to AIRBUS, refer to Fig. A-FRAAA.

**CONF ALL

D. TEST

**CONF 001

None

**CONF 002

None

**CONF ALL

E. CLOSE-UP

**CONF 001

None

**CONF 002

(1) Subtask 344239-942-005-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Task 34-11-19-400-801

Task 52-10-00-410-801

NOTE: If you intend to accomplish an associated Repair Task during the same

layover period, the subsequent Close-up procedure is not necessary.

(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 in the installation of the AOA Probes (FINs

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

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(c) Close the FWD passenger/crew door(s) 831 or 841, refer to AMM 06-41-53, Page

Block 001 and AMM Task 52-10-00-410-801.

(d) Remove the access platform(s).

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

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

REVISION No.: 01 - Sep 17/13 Page: 68

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**CONF ALL

FR19

FR18

A

3FP1

3FP2

3FP3

A

A

DETAILED VISUAL INSPECTION AREA

TYPICAL INSTALLATION

NOTE:

A

F_SB_344239_5_BAAA_01_03

Figure A-FBAAA - Sheet 01

Area to be inspected

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

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SERVICE BULLETIN

**CONF 001

REFER TO THALES VSB

NO

(OR ANY LATER

NO FURTHER ACTION

REPORT TO AIRBUS

QUESTION

ACTION

FINDING

LISTED IN TABLE,

SN

REVISION)

C16291A−34−007 REVISION 01

OR

NO

REMOVE AFFECTED AOA PROBES 

PN C16291AA REFER TO AMM 

34−11−19−000−801 BEFORE END APRIL 2010

OR

INSTALL AOA PROBES PN C16291AA WHOSE SN IS NOT LISTED IN

OR

INSTALL THREE GOODRICH AOA PROBES PN 0861ED

COVERED BY SB A340−34−4087 OR BY RFC/RMO PROCEDURE

INSTALL AOA PROBES PN C16291AA 

MODIFICATION

No. 53368S18144 OR

SB No A340−34−4213

EMBODIED

REMOVE AFFECTED AOA PROBES 

PN C16291AA REFER TO AMM 

34−11−19−000−801 BEFORE END APRIL 2011

POST THALES VSB C16291A−34−007 REVISION 01 (OR ANY LATER REVISION)

YES

YES

THALES VSB C16291A−34−007 REVISION 01 (OR ANY LATER REVISION)

REFER TO TASK 344239−831−802−001

REFER TO TASK 344239−831−803−001

REFER TO TASK 344239−831−804−001

REFER TO TASK 344239−832−801−001

IDENTIFY THE SERIAL NUMBER (SN) OF THE THREE AOA PROBES PART NUMBER (PN) C16291AA

(FINS 3FP1, 3FP2, 3FP3) THROUGH A DETAILED INSPECTION OR AS PER AIRCRAFT RECORDS DATA ANALYSIS

AT THE THRESHOLD GIVEN IN THE PLANNING INFORMATION PARAGRAPH E.(2)

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

INSTALL AOA PROBES PN C16291AB

WHOSE SN IS NOT LISTED IN THALES VSB C16291A−34−007 REVISION 01

(OR ANY LATER REVISION) COVERED BY SB A340−34−4234

REFER TO TASK 344239−831−801−001

F_SB_344239_5_FAAA_01_02

Figure A-FFAAA - Sheet 01

Flow Chart

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

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**CONF 002

REFER TO THALES VSB

NO

(OR ANY LATER

NO FURTHER ACTION

REPORT TO AIRBUS

QUESTION

ACTION

FINDING

LISTED IN TABLE,

SN

REVISION)

C16291A−34−007 REVISION 01

OR

REPLACEMENT OF THE AOA PROBES BY PN C16291AB

POST THALES VSB C16291A−34−007 REVISION 01 (OR ANY LATER REVISION)

YES

REFER TO TASK 344239−831−804−001

REFER TO TASK 344239−832−801−001

IDENTIFY THE SERIAL NUMBER (SN) OF THE THREE AOA PROBES PART NUMBER (PN) C16291AB

(FINS 3FP1, 3FP2, 3FP3) THROUGH A DETAILED INSPECTION OR AS PER AIRCRAFT RECORDS DATA ANALYSIS

AT THE THRESHOLD GIVEN IN THE PLANNING INFORMATION PARAGRAPH E.(2)

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

OR

INSTALL THREE GOODRICH AOA PROBES PN 0861ED

COVERED BY SB A340−34−4087 OR BY RFC/RMOPROCEDURE

REFER TO TASK 344239−831−803−001

REPLACEMENT OF THE AOA PROBES BY PN C16291AB

WHOSE SN IS NOT LISTED IN THALES VSB C16291A−34−007 REVISION 01

(OR ANY LATER REVISION)

REFER TO TASK 344239−831−801−001

F_SB_344239_5_FAAB_01_02

Figure A-FFAAB - Sheet 01

Flow Chart

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

REVISION No.: 01 - Sep 17/13 Page: 71

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@A340

SERVICE BULLETIN

**CONF 002

REFER TO THALES VSB

NO

(OR ANY LATER

NO FURTHER ACTION

REPORT TO AIRBUS

QUESTION

ACTION

FINDING

LISTED IN TABLE,

SN

REVISION)

C16291A−34−007 REVISION 01

OR

REPLACEMENT OF THE AOA PROBES BY PN C16291AB

POST THALES VSB C16291A−34−007 REVISION 01

YES

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

(OR ANY LATER REVISION)

REFER TO TASK 344239−831−804−001

OR

INSTALL THREE GOODRICH AOA PROBES PN 0861ED

COVERED BY SB A340−34−4087 OR BY RFC/RMO PROCEDURE

REFER TO TASK 344239−831−803−001

REFER TO TASK 344239−832−802−001

IDENTIFY THE SERIAL NUMBER (SN) OF THE THREE AOA PROBES PART NUMBER (PN) C16291AB

(FINS 3FP1, 3FP2, 3FP3) THROUGH A DETAILED INSPECTION OR AS PER AIRCRAFT RECORDS DATA ANALYSIS

AT THE THRESHOLD GIVEN IN THE PLANNING INFORMATION PARAGRAPH E.(2)

REPLACEMENT OF THE AOA PROBES BY PN C16291AB

WHOSE SN IS NOT LISTED IN THALES VSB C16291A−34−007 REVISION 01

REFER TO TASK 344239−831−801−001

(OR ANY LATER REVISION)

F_SB_344239_5_FBAA_01_02

Figure A-FFBAA - Sheet 01

Flow Chart (ADDITIONAL WORK)

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

REVISION No.: 01 - Sep 17/13 Page: 72

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SERVICE BULLETIN

**CONF ALL

PN IDENTIFICATION

3FP1

SN IDENTIFICATION

REPLACEMENT OF AOA YES

NO

FIN

PROBE

3FP2

YES

NO

3FP3

YES

NO

RETURN TO :

AIRBUS

CUSTOMER SERVICES ENGENEERING − SEEA3

NAVIGATION AND FLIGHT GUIDANCE/

1 ROND POINT MAURICE BELLONTE

31707 BLAGNAC CEDEX

FRANCE

FAX +33 (0)5 61 93 44 25

NEW AOA PROBE SN

INSTALLED

INSPECTION REPORT

SERVICE BULLETIN No. :

A/C MSN :

FLIGHT CYCLES :

FLIGHT HOURS :

A340−34−4239

DATE OF INSPECTION :

INSPECTION METHOD : DETAILED

INSPECTION

MANAGEMENT SYSTEMS

F_SB_344239_5_RAAA_01_00

Figure A-FRAAA - Sheet 01

Inspection Report

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

REVISION No.: 01 - Sep 17/13 Page: 73

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SERVICE BULLETIN

This Page Intentionally Left Blank

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

REVISION No.: 01 - Sep 17/13 Page: 74

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SERVICE BULLETIN

REPORTING SHEET

TITLE: NAVIGATION - SENSORS, POWER SUPPLY AND SWITCHING -

INSPECTION OF THALES AOA PROBES

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: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

REVISION No.: 01 - Sep 17/13 Page: 1

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SERVICE BULLETIN

QUALITY PERCEPTION FORM

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

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

improve the quality of our Service Bulletins.

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

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

- Quality rating of this SB 4321

- Quality rating of the Accomplishment Instructions 4321

- Quality rating of the Illustrations 4321

- Is this SB easy to understand ? Y/N

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

short description of the issue.

Planning Material Instructions

X Effectivity X Kit content X Preparation

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

X Manpower X Industry support X Test

X References X Re-identification X Close-Up

X Publication X Tooling X Illustrations

Comments:

Operator: Date:

Name/Title:

Please return this form to:

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX FRANCE

Attn : SEM4 Service Bulletins Management

FAX : (33) 5 61 93 42 51

Or via your Resident Customer Support Office.

DATE: Jan 20/10 SERVICE BULLETIN No.: A340-34-4239

REVISION No.: 01 - Sep 17/13 Page: 1

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