@A340

SERVICE BULLETIN

SUMMARY

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

This summary is for information only and is not approved for modification of the aircraft.

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 27

TITLE: FLIGHT CONTROLS - FCPC - INTRODUCE FCPC L22A 2K1 OR FCPC

L22A 2K0 FOR A340-200/300 BASIC A/C WITH MECHANICAL RUDDER

**CONF ALL

MODIFICATIONS

MODIFICATION CLASSIFICATION

MAJOR 55437S18647 55438S18648 201689S31875 201690S31876

MINOR None

NOTE: As per EASA IR 21, a minor change is one that has no appreciable effect on the

mass, balance, structural strength, reliability, operational characteristics affecting the

airworthiness of the product. All other changes are major changes.

REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES

New Flight Control Primary Computer (FCPC) standards L22A 2K0 and L22A 2K1 are developed to

cover the improvement of Flight Guidance and Envelope (FGE) behaviour in some conditions of FCPC

in alternate law.

It implies to replace the current FCPC standard L20 2K1 PN LA2K1A100290000 by new ones, FCPC

standard L22A 2K1 PN LA2K1A1002B0000, electrically and mechanically interchangeable and to

replace the current FCPC standard L20 2K0 PN LA2K01500290000 by new ones, FCPC standard L22A

2K0 PN LA2K015002B0000, electrically and mechanically interchangeable.

Replace associated OBRM PN LA2K01500290400 by new one PN LA2K015002B0400.

Replace associated OBRM PN LA2K1A100290400 by new one PN LA2K1A1002B0400.

Main improvements introduced by L22A 2K0 and L22A 2K1 Standard :

- Reduction of High Vertical Speed (VZ) at touchdown with new parameters recording in the DFDR

(Digital Flight Data Recorder),

- Improvement of aircraft behaviour in case of erratic Air Data/Inertial Reference Unit (ADIRU)

outputs,

DATE: Nov 21/11 SERVICE BULLETIN No.: A340-27-4174

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SERVICE BULLETIN

SUMMARY

- Improvement of the reconfiguration logics in case of electrical transients during rotation at Take Off

(TFU 27.90.00.035),

- Improvement of the GS and PLD logics (ground spoiler and partial lift damping),

- Improvement of aircraft behaviour in case of two consistently erroneous AOA (Angle Of Attack)

information : limitation of Trimmable Horizontal Stabilizer (THS) at pitch up,

- Maximum Operating Speed/Maximum Operating Mach (VMO/MMO) and autopilot disconnection

logic (A340-300 only),

- Autopilot inhibition engagement under unreliable airspeed condition.

Accomplishment of this Service Bulletin will cancel the OEB 35 (formerly OEB 95 up until 2011) and the

Airplane Flight Manual (AFM) TR 150 according to Airworthiness Directive No. 2010-0271.

Accomplishment of this Service Bulletin will also cancel the OEB 40 (formerly OEB 88 up until 2011).

GENERAL EVALUATION

EVALUATION TABLE

COMPLIANCE MANDATORY (1) CANCELS INSPECTION SB NO

POTENTIAL AD YES A/C OPERATION AFFECTED YES

RELIABILITY AFFECTED NO PAX COMFORT AFFECTED NO

COST SAVING NO LROPS AFFECTED NO

STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED YES

NOTE (1): Service Bulletin must be accomplished.

MATERIAL PRICE INFORMATION

**CONF 001

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Equipment BFEA01 1 See SB FCPCs

**CONF 002

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Equipment BFEA02 1 See SB FCPCs

**CONF 003

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Equipment BFEA03 1 See SB FCPCs

DATE: Nov 21/11 SERVICE BULLETIN No.: A340-27-4174

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@A340

SERVICE BULLETIN

SUMMARY

**CONF 004

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Equipment BFEA04 1 See SB FCPCs

EFFECTIVITY

**CONF ALL

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

47W 56W AAW AFR ALK ARG B3R CAL CCA CES CPA DGA DLH

FIN GAF GFA HFY I2L IBE KAC KNE LAN M3R MAU MSR NMB

OAL PAL QAF RJA S3R SAA SAS SLM SWR TAP THT THY UAE

VCV VIR XAX

CONCURRENT REQUIREMENTS

Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishment of the

following Service Bulletin or the equivalent production modification(s):

Service Bulletin No. A340-27-4131 Mod. No. 48753S14988

48754S14989

51340S16797

51356S16796

53501S18049

53502S18050

A340-31-4067 49633S16355

REFERENCES / REPERCUSSIONS

TFU 27.90.00.035

OEB 35

40

AOT None

SIL 00-022

LINE MAINTENANCE AFFECTED No

LIFE LIMIT None

OTHER FOT Ref. 999.0112/10 dated 20 December 2010

OTHER OIT SE 999.0035/11 dated 28 April 2011

NATURE OF THE WORK

AIRCRAFT NO

EQUIPMENT YES

HARD YES

SOFT NO

OBRM YES

DATE: Nov 21/11 SERVICE BULLETIN No.: A340-27-4174

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@A340

SERVICE BULLETIN

SUMMARY

MANPOWER

**CONF 001

Task 274174-831-801-001: Modification of the three FCPCs by replacement or reprogramming

of their OBRMs.

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

Additional manhours related to Vendor SB; refer to:

In the Main Rack 800VU and on the FWD Shelf 915VU

modify the three FCPCs (FINs 2CE1, 2CE2 and 2CE3) by

replacement or reprogramming of their OBRMs.

AIRBUS OPERATION S.A.S.

Service Bulletin No. LA2K1-27-014

Task 274174-831-802-001: Modification by replacement of three FCPCs.

TOTAL MANHOURS 4.50

ELAPSED TIME (HOURS) 4.50

**CONF 002

Task 274174-831-801-001: Modification of the three FCPCs by replacement or reprogramming

of their OBRMs.

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

Additional manhours related to Vendor SB; refer to:

In the Main Rack 800VU and on the FWD Shelf 915VU

modify the three FCPCs (FINs 2CE1, 2CE2 and 2CE3) by

replacement or reprogramming of their OBRMs.

AIRBUS OPERATION S.A.S.

Service Bulletin No. LA2K1-27-014

Task 274174-831-802-001: Modification by replacement of three FCPCs.

TOTAL MANHOURS 4.50

ELAPSED TIME (HOURS) 4.50

**CONF 003

Task 274174-831-801-001: Modification of the three FCPCs by replacement or reprogramming

of their OBRMs.

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

Additional manhours related to Vendor SB; refer to:

In the Main Rack 800VU and on the FWD Shelf 915VU

modify the three FCPCs (FINs 2CE1, 2CE2 and 2CE3) by

replacement or reprogramming of their OBRMs.

AIRBUS OPERATION S.A.S.

Service Bulletin No. LA2K0-27-022

Task 274174-831-802-001: Modification by replacement of three FCPCs.

TOTAL MANHOURS 4.50

DATE: Nov 21/11 SERVICE BULLETIN No.: A340-27-4174

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@A340

SERVICE BULLETIN

SUMMARY

Task 274174-831-802-001: Modification by replacement of three FCPCs.

ELAPSED TIME (HOURS) 4.50

**CONF 004

Task 274174-831-801-001: Modification of the three FCPCs by replacement or reprogramming

of their OBRMs.

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

Additional manhours related to Vendor SB; refer to:

In the Main Rack 800VU and on the FWD Shelf 915VU

modify the three FCPCs (FINs 2CE1, 2CE2 and 2CE3) by

replacement or reprogramming of their OBRMs.

AIRBUS OPERATION S.A.S.

Service Bulletin No. LA2K0-27-022

Task 274174-831-802-001: Modification by replacement of three FCPCs.

TOTAL MANHOURS 4.50

ELAPSED TIME (HOURS) 4.50

APPENDICES

**CONF ALL

None

DATE: Nov 21/11 SERVICE BULLETIN No.: A340-27-4174

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@A340

SERVICE BULLETIN

SUMMARY

**CONF ALL

FR20

2CE1

2CE2

2CE3

A

B

A

B

Z120

F_SB_274174_5_SAAA_01_00

915VU

800VU

Figure A-FSAAA - Sheet 01

DATE: Nov 21/11 SERVICE BULLETIN No.: A340-27-4174

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@A340

SERVICE BULLETIN

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 27

TITLE: FLIGHT CONTROLS - FCPC - INTRODUCE FCPC L22A 2K1 OR FCPC

L22A 2K0 FOR A340-200/300 BASIC A/C WITH MECHANICAL RUDDER

MODIFICATION No.: 55437S18647 55438S18648 201689S31875 201690S31876

This document contains AIRBUS PROPRIETARY INFORMATION and shall at all times remain the

property of AIRBUS; no intellectual property right or licence is granted by AIRBUS in connection with

any information contained in it. It is delivered on the express condition that said document and the

information contained in it shall be treated as confidential, shall not be used for any purpose other than

that for which it is hereby delivered. It shall not be disclosed in whole or in part to third parties and shall

not be duplicated in any manner (except for the purposes of performing the tasks described hereunder

and provided that any recipient of such document shall comply with the conditions herein), without

AIRBUS prior written consent.

1. PLANNING INFORMATION

**CONF ALL

A. EFFECTIVITY

NOTE: These modifications are applicable by Service Bulletin only.

NOTE: This Service Bulletin is only applicable to aircraft on which Mod. No.

49144S16279 (INSTALL RUDDER FLY-BY WIRE ON A330/A340) is not

embodied.

(1) Models

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

(2) Effectivity by MSN

0002-0006 0008-0009 0011 0013-0015 0018-0029 0031-0035 0038 0041 0043-0044

0046-0049 0051-0053 0056-0058 0061 0063 0074-0076 0078-0081 0084-0085

0088-0091 0093-0094 0101 0104 0114-0115 0117 0123 0125-0126 0128-0129 0131

0133-0137 0139 0141-0142 0145-0147 0149-0152 0154 0156-0161 0163-0164

0166-0170 0173-0176 0178-0180 0182 0185-0187 0190 0192-0194 0196-0197 0199

0201-0202 0204 0207-0208 0210 0212-0218 0220-0221 0225 0227-0228 0233

0235-0237 0239 0242-0243 0245-0246 0252 0257 0260 0263-0264 0268 0270

0273-0274 0278 0280 0282 0292 0297 0302 0304 0307 0310 0318-0319 0321 0325

0327 0329 0331-0332 0335 0347 0352 0354-0355 0359 0363 0367 0373-0374

DATE: Nov 21/11 SERVICE BULLETIN No.: A340-27-4174

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@A340

SERVICE BULLETIN

0377-0379 0381 0385 0387 0390 0395 0399 0402 0406 0411 0413-0415 0424

0429-0430 0433-0435 0438 0442 0446-0447 0450 0459 0467 0470 0474 0483 0528

0538 0541 0545-0546 0554 0556 0559 0561-0562

(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

47W 0009

56W 0002 0003 0013 0015

AAW 0151

AFR 0029 0078 0084 0186 0207 0210 0237 0245 0246 0260 0307 0310

0319 0377 0399

ALK 0032 0033 0034 0367 0374 0381

ARG 0048 0063 0074 0080 0085 0093 0094 0123 0126

B3R 0046

CAL 0402 0406 0411 0415 0433 0541

CCA 0192 0199 0201 0242 0243 0264

CES 0129 0131 0141 0161 0182

CPA 0128 0136 0137 0142 0147 0157 0160 0208 0218 0220 0227 0228

DGA 0075 0081

DLH 0020 0024 0027 0028 0035 0052 0053 0056 0135 0158 0213 0233

0252 0297 0304 0321 0325 0327 0335 0347 0352 0354 0379 0390

0434 0447

FIN 0058 0168 0174

GAF 0274 0355

GFA 0212 0215 0282 0554

HFY 0117 0133 0450

I2L 0373

IBE 0005 0088 0125 0134 0145 0146 0170 0193 0217 0221 0302 0318

0329 0332 0387 0414 0459 0474 0483

KAC 0089 0090 0101 0104

KNE 0004

LAN 0167 0359 0363 0429 0442

M3R 0061

MAU 0076 0152 0194 0268

MSR 0156 0159 0178

NMB 0047 0051

OAL 0235 0239 0280 0292

PAL 0173 0176 0187 0196

QAF 0026 0528

RJA 0014 0022 0038 0043

S3R 0204

SAA 0006 0008 0011 0018 0019 0021 0197 0378

SAS 0413 0424 0430 0435 0467 0470

DATE: Nov 21/11 SERVICE BULLETIN No.: A340-27-4174

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@A340

SERVICE BULLETIN

OPERATOR MSN

SLM 0049

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

0562

TAP 0041 0044 0079 0091

THT 0385 0395 0438 0446

THY 0023 0025 0057 0115 0180 0216 0257 0270 0331

UAE 0139 0149 0163 0166 0185 0190 0202 0236

VCV 0031

VIR 0114 0164 0214 0225

XAX 0273 0278

(4) Configuration by MSN

MSN CONFIGURATION

0002 0003 0006 0008 0011 0018 0019 0020 0021 0024 0027

0028 0029 0032 0033 0034 0035 0038 0041 0044 0046 0047

0048 0051 0052 0053 0056 0058 0061 0063 0074 0075 0076

0078 0079 0080 0081 0084 0085 0089 0090 0091 0093 0094

0101 0104 0114 0117 0123 0126 0128 0129 0131 0135 0136

0137 0139 0141 0142 0147 0149 0150 0151 0152 0154 0156

0157 0158 0159 0160 0161 0163 0164 0166 0167 0168 0169

0173 0175 0176 0178 0179 0182 0185 0187 0190 0192 0194

0196 0197 0199 0201 0202 0207 0208 0210 0212 0213 0214

0215 0218 0220 0225 0227 0228 0233 0236 0237 0252

004

0004 0005 0009 0013 0014 0015 0022 0023 0025 0026 0031

0043 0049 0057 0088 0115 0125 0133 0134 0145 0146 0170

0174 0180 0186 0193 0204 0216 0217 0221 0235 0239

003 004

0242 0243 0245 0246 0260 0263 0264 0268 0273 0274 0278

0282 0297 0304 0307 0310 0321 0325 0327 0335 0347 0352

0354 0355 0359 0363 0367 0373 0374 0377 0378 0379 0381

0385 0390 0395 0399 0402 0406 0411 0413 0415 0424 0429

0430 0433 0434 0435 0438 0442 0446 0447 0450 0467 0470

0538 0541 0545 0546 0554 0556 0559 0561 0562

002

0257 0270 0280 0292 0302 0318 0319 0329 0331 0332 0387

0414 0459 0474 0483 0528

001 002

(5) Configuration definition

**CONF 001

Config. 001 is valid for aircraft on which Service Bulletin No. A340-27-4144 (Mod. No.

55438S18648) and Service Bulletin No. A340-27-4070 (Mod. No. 46627S14401) are not

embodied and on which Service Bulletin No. A340-27-4067 (Mod. No 46292S14150) is

embodied.

**CONF 002

Config. 002 is valid for aircraft on which Service Bulletin No. A340-27-4144 (Mod No.

55438S18648) and Service Bulletin No. A340-27-4067 (Mod. No 46292S14150) are

embodied and on which Service Bulletin No. A340-27-4070 (Mod. No. 46627S14401) is

not embodied.

DATE: Nov 21/11 SERVICE BULLETIN No.: A340-27-4174

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SERVICE BULLETIN

**CONF 003

Config. 003 is valid for aircraft on which Service Bulletin No. A340-27-4144 (Mod No.

55438S18648) and Service Bulletin No. A340-27-4067 (Mod. No 46292S14150) are not

embodied and on which Service Bulletin No. A340-27-4070 (Mod. No. 46627S14401) is

embodied.

**CONF 004

Config. 004 is valid for aircraft on which Service Bulletin No. A340-27-4144 (Mod No.

55438S18648) and Service Bulletin No. A340-27-4070 (Mod. No. 46627S14401) are

embodied and on which Service Bulletin No. A340-27-4067 (Mod. No 46292S14150) is

not embodied.

(6) Material Effectivity

**CONF 001

MATERIAL QTY PER A/C SEE NOTES

Equipment BFEA01 1

**CONF 002

MATERIAL QTY PER A/C SEE NOTES

Equipment BFEA02 1

**CONF 003

MATERIAL QTY PER A/C SEE NOTES

Equipment BFEA03 1

**CONF 004

MATERIAL QTY PER A/C SEE NOTES

Equipment BFEA04 1

**CONF ALL

B. CONCURRENT REQUIREMENTS

Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishment of

the following Service Bulletin or the equivalent production modification(s):

Service Bulletin No. A340-27-4131 Mod. No. 48753S14988

48754S14989

51340S16797

51356S16796

53501S18049

53502S18050

A340-31-4067 49633S16355

DATE: Nov 21/11 SERVICE BULLETIN No.: A340-27-4174

REVISION No.: 00 - Nov 21/11 Page: 4

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SERVICE BULLETIN

C. REASON

(1) History

New Flight Control Primary Computer (FCPC) standards L22A 2K0 and L22A 2K1 are

developed to cover the improvement of Flight Guidance and Envelope (FGE) behaviour

in some conditions of FCPC in alternate law.

(2) Objective/Action

It implies to replace the current FCPC standard L20 2K1 PN LA2K1A100290000

by new ones, FCPC standard L22A 2K1 PN LA2K1A1002B0000, electrically and

mechanically interchangeable and to replace the current FCPC standard L20 2K0 PN

LA2K01500290000 by new ones, FCPC standard L22A 2K0 PN LA2K015002B0000,

electrically and mechanically interchangeable.

Replace associated OBRM PN LA2K01500290400 by new one PN LA2K015002B0400.

Replace associated OBRM PN LA2K1A100290400 by new one PN LA2K1A1002B0400.

(3) Advantages

Main improvements introduced by L22A 2K0 and L22A 2K1 Standard :

- Reduction of High Vertical Speed (VZ) at touchdown with new parameters recording

in the DFDR (Digital Flight Data Recorder),

- Improvement of aircraft behaviour in case of erratic Air Data/Inertial Reference Unit

(ADIRU) outputs,

- Improvement of the reconfiguration logics in case of electrical transients during

rotation at Take Off (TFU 27.90.00.035),

- Improvement of the GS and PLD logics (ground spoiler and partial lift damping),

- Improvement of aircraft behaviour in case of two consistently erroneous AOA (Angle

Of Attack) information : limitation of Trimmable Horizontal Stabilizer (THS) at pitch

up,

- Maximum Operating Speed/Maximum Operating Mach (VMO/MMO) and autopilot

disconnection logic (A340-300 only),

- Autopilot inhibition engagement under unreliable airspeed condition.

(4) Operational/Maintenance Consequences

Accomplishment of this Service Bulletin will cancel the OEB 35 (formerly OEB 95 up

until 2011) and the Airplane Flight Manual (AFM) TR 150 according to Airworthiness

Directive No. 2010-0271.

Accomplishment of this Service Bulletin will also cancel the OEB 40 (formerly OEB 88

up until 2011).

DATE: Nov 21/11 SERVICE BULLETIN No.: A340-27-4174

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SERVICE BULLETIN

D. DESCRIPTION

NOTE: To accomplish this Service Bulletin, you have two possibilities :

- either you modify the three FCPCs by replacement or reprogramming of

their OBRMs as described in TASK 274174-831-801 001 Modification of

the three FCPCs by replacement or reprogramming of their OBRMs. ,

- or you replace them as described in TASK 274174-831-802 001

Modification by replacement of three FCPCs. .

To accomplish this Service Bulletin it is necessary to :

**CONF 001

Task 274174-831-801-001: Modification of the three FCPCs by replacement or

reprogramming of their OBRMs.

(1) In the Main Rack 800VU and on the FWD Shelf 915VU modify the three FCPCs

(FINs 2CE1, 2CE2 and 2CE3) by replacement or reprogramming of their OBRMs.

Task 274174-831-802-001: Modification by replacement of three FCPCs.

(1) In the Main Rack 800VU and on the FWD Shelf 915VU, replace the three FCPCs

(FINs 2CE1, 2CE2 and 2CE3).

**CONF 002

Task 274174-831-801-001: Modification of the three FCPCs by replacement or

reprogramming of their OBRMs.

(1) In the Main Rack 800VU and on the FWD Shelf 915VU modify the three FCPCs

(FINs 2CE1, 2CE2 and 2CE3) by replacement or reprogramming of their OBRMs.

Task 274174-831-802-001: Modification by replacement of three FCPCs.

(1) In the Main Rack 800VU and on the FWD Shelf 915VU, replace the three FCPCs

(FINs 2CE1, 2CE2 and 2CE3).

**CONF 003

Task 274174-831-801-001: Modification of the three FCPCs by replacement or

reprogramming of their OBRMs.

(1) In the Main Rack 800VU and on the FWD Shelf 915VU modify the three FCPCs

(FINs 2CE1, 2CE2 and 2CE3) by replacement or reprogramming of their OBRMs.

Task 274174-831-802-001: Modification by replacement of three FCPCs.

(1) In the Main Rack 800VU and on the FWD Shelf 915VU, replace the three FCPCs

(FINs 2CE1, 2CE2 and 2CE3).

DATE: Nov 21/11 SERVICE BULLETIN No.: A340-27-4174

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SERVICE BULLETIN

**CONF 004

Task 274174-831-801-001: Modification of the three FCPCs by replacement or

reprogramming of their OBRMs.

(1) In the Main Rack 800VU and on the FWD Shelf 915VU modify the three FCPCs

(FINs 2CE1, 2CE2 and 2CE3) by replacement or reprogramming of their OBRMs.

Task 274174-831-802-001: Modification by replacement of three FCPCs.

(1) In the Main Rack 800VU and on the FWD Shelf 915VU, replace the three FCPCs

(FINs 2CE1, 2CE2 and 2CE3).

**CONF ALL

E. COMPLIANCE

(1) Classification

MANDATORY: Service Bulletin must be accomplished.

(2) Accomplishment Timescale

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

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

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

F. APPROVAL

The technical content of this document is approved under the authority of Design

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 274174-831-801-001: Modification of the three FCPCs by replacement or reprogramming

of their OBRMs.

Get Access 1.00

Tests 0.50

Close-Up 1.00

DATE: Nov 21/11 SERVICE BULLETIN No.: A340-27-4174

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@A340

SERVICE BULLETIN

Task 274174-831-801-001: Modification of the three FCPCs by replacement or reprogramming

of their OBRMs.

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

Additional manhours related to Vendor SB; refer to:

In the Main Rack 800VU and on the FWD Shelf 915VU

modify the three FCPCs (FINs 2CE1, 2CE2 and 2CE3)

by replacement or reprogramming of their OBRMs.

AIRBUS OPERATION S.A.S.

Service Bulletin No. LA2K1-27-014

Task 274174-831-802-001: Modification by replacement of three FCPCs.

Get Access 1.00

On Aircraft

In the Main Rack 800VU and on the FWD Shelf

915VU, replace the three FCPCs (FINs 2CE1, 2CE2

and 2CE3).

1.50

Tests 1.00

Close-Up 1.00

TOTAL MANHOURS 4.50

ELAPSED TIME (HOURS) 4.50

**CONF 002

Task 274174-831-801-001: Modification of the three FCPCs by replacement or reprogramming

of their OBRMs.

Get Access 1.00

Tests 0.50

Close-Up 1.00

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

Additional manhours related to Vendor SB; refer to:

In the Main Rack 800VU and on the FWD Shelf 915VU

modify the three FCPCs (FINs 2CE1, 2CE2 and 2CE3)

by replacement or reprogramming of their OBRMs.

AIRBUS OPERATION S.A.S.

Service Bulletin No. LA2K1-27-014

Task 274174-831-802-001: Modification by replacement of three FCPCs.

Get Access 1.00

On Aircraft

In the Main Rack 800VU and on the FWD Shelf

915VU, replace the three FCPCs (FINs 2CE1, 2CE2

and 2CE3).

1.50

Tests 1.00

Close-Up 1.00

TOTAL MANHOURS 4.50

ELAPSED TIME (HOURS) 4.50

DATE: Nov 21/11 SERVICE BULLETIN No.: A340-27-4174

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**CONF 003

Task 274174-831-801-001: Modification of the three FCPCs by replacement or reprogramming

of their OBRMs.

Get Access 1.00

Tests 0.50

Close-Up 1.00

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

Additional manhours related to Vendor SB; refer to:

In the Main Rack 800VU and on the FWD Shelf 915VU

modify the three FCPCs (FINs 2CE1, 2CE2 and 2CE3)

by replacement or reprogramming of their OBRMs.

AIRBUS OPERATION S.A.S.

Service Bulletin No. LA2K0-27-022

Task 274174-831-802-001: Modification by replacement of three FCPCs.

Get Access 1.00

On Aircraft

In the Main Rack 800VU and on the FWD Shelf

915VU, replace the three FCPCs (FINs 2CE1, 2CE2

and 2CE3).

1.50

Tests 1.00

Close-Up 1.00

TOTAL MANHOURS 4.50

ELAPSED TIME (HOURS) 4.50

**CONF 004

Task 274174-831-801-001: Modification of the three FCPCs by replacement or reprogramming

of their OBRMs.

Get Access 1.00

Tests 0.50

Close-Up 1.00

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

Additional manhours related to Vendor SB; refer to:

In the Main Rack 800VU and on the FWD Shelf 915VU

modify the three FCPCs (FINs 2CE1, 2CE2 and 2CE3)

by replacement or reprogramming of their OBRMs.

AIRBUS OPERATION S.A.S.

Service Bulletin No. LA2K0-27-022

Task 274174-831-802-001: Modification by replacement of three FCPCs.

Get Access 1.00

On Aircraft

In the Main Rack 800VU and on the FWD Shelf

915VU, replace the three FCPCs (FINs 2CE1, 2CE2

and 2CE3).

1.50

DATE: Nov 21/11 SERVICE BULLETIN No.: A340-27-4174

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Task 274174-831-802-001: Modification by replacement of three FCPCs.

Tests 1.00

Close-Up 1.00

TOTAL MANHOURS 4.50

ELAPSED TIME (HOURS) 4.50

**CONF ALL

H. WEIGHT AND BALANCE

Not Changed

I. ELECTRICAL LOAD DATA

Not Changed

J. REFERENCES

**CONF 001

Airworthiness Directive (AD) Airworthiness Directive No.

2010-0271

Aircraft Maintenance Manual (AMM) 12-34-24 20-15-00 22-97-00

27-93-34 27-96-00 31-51-00

ATA Common Support Data Dictionary (CSDD),

Chapter 2

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

Service Bulletin (SB) A340-27-4067

A340-27-4070

A340-27-4131

A340-27-4144

A340-31-4067

Service Information Letter (SIL) SIL 00-022

Vendor Service Bulletin (VSB) AIRBUS OPERATION S.A.S.

Service Bulletin No. LA2K1-27-014

**CONF 002

Airworthiness Directive (AD) Airworthiness Directive No.

2010-0271

Aircraft Maintenance Manual (AMM) 12-34-24 20-15-00 22-97-00

27-93-34 27-96-00 31-51-00

DATE: Nov 21/11 SERVICE BULLETIN No.: A340-27-4174

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ATA Common Support Data Dictionary (CSDD),

Chapter 2

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

Service Bulletin (SB) A340-27-4067

A340-27-4070

A340-27-4131

A340-27-4144

A340-31-4067

Service Information Letter (SIL) SIL 00-022

Vendor Service Bulletin (VSB) AIRBUS OPERATION S.A.S.

Service Bulletin No. LA2K1-27-014

**CONF 003

Airworthiness Directive (AD) Airworthiness Directive No.

2010-0271

Aircraft Maintenance Manual (AMM) 12-34-24 20-15-00 22-97-00

27-93-34 27-96-00 31-51-00

ATA Common Support Data Dictionary (CSDD),

Chapter 2

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

Service Bulletin (SB) A340-27-4067

A340-27-4070

A340-27-4131

A340-27-4144

A340-31-4067

Service Information Letter (SIL) SIL 00-022

Vendor Service Bulletin (VSB) AIRBUS OPERATION S.A.S.

Service Bulletin No. LA2K0-27-022

**CONF 004

Airworthiness Directive (AD) Airworthiness Directive No.

2010-0271

Aircraft Maintenance Manual (AMM) 12-34-24 20-15-00 22-97-00

27-93-34 27-96-00 31-51-00

ATA Common Support Data Dictionary (CSDD),

Chapter 2

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

Service Bulletin (SB) A340-27-4067

A340-27-4070

A340-27-4131

A340-27-4144

A340-31-4067

Service Information Letter (SIL) SIL 00-022

Vendor Service Bulletin (VSB) AIRBUS OPERATION S.A.S.

Service Bulletin No. LA2K0-27-022

DATE: Nov 21/11 SERVICE BULLETIN No.: A340-27-4174

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**CONF ALL

K. PUBLICATION AFFECTED

Aircraft Maintenance Manual (AMM) 27-93-00

Aircraft Wiring List (AWL)

Flight Crew Operating Manuel (FCOM)

Flight Manual (FM)

Illustrated Parts Catalog (IPC) 27-93-08 27-93-34

Master Minimum Equipment List (MMEL)

This Service Bulletin has an operational impact. Please inform AIRBUS, at least four weeks in

advance, in case you need your operational documentation to be amended by a revision prior

to Service Bulletin embodiment. For this purpose, please request the revision by e-mail, online through the SB Reporting service or alternatively by fax to :

SEDOR4 - AIRBUS Customer Services Technical Data

Fax No.: (33) 5 61 93 28 06

E-mail: sb.reporting@airbus.com

SB Reporting service is accessible on-line through AIRBUSWorld from :

My on-line services’ section, available on all AIRBUSWorld pages.

The Maintenance and Engineering Community, in :

- Modify and Upgrade page,

- Access SB and VSB section.

These amendments will be confirmed by the next normal revision of operational

documentation, once your Service Bulletin accomplishment report has been sent, as usual, to

our Customer Services Aircraft In-Service Data (SEDOR4).

L. INTERCHANGEABILITY/MIXABILITY

**CONF 001

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE

NOTES

FCPC LA2K1A100270000 LA2K1A1002B0000 03 NO (1) (2)

NOTE: For definitions of interchangeability codes in column INT., refer to ATA

Common Support Data Dictionary (CSDD), Chapter 2.

NOTE: Only the mixability configuration(s) and condition(s) stated in this Service

Bulletin are approved.

NOTE (1): Interchangeability code 03 becomes 01 provided that the three FCPCs are

replaced at the same time. Mixability not authorized. Replacement of the

three FCPCs has to be done simultaneously as per ACCOMPLISHMENT

INSTRUCTIONS paragraph C. of this Service Bulletin.

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NOTE (2): On non-enhanced A340 aircraft model, FCPC standard L22A 2K1 (PN

LA2K1A1002B0000) is interchangeable and mixable with FCPC standard

L22A 2K0 (PN LA2K015002B0000).

**CONF 002

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE

NOTES

FCPC LA2K1A100290000 LA2K1A1002B0000 03 NO (1) (2)

NOTE: For definitions of interchangeability codes in column INT., refer to ATA

Common Support Data Dictionary (CSDD), Chapter 2.

NOTE: Only the mixability configuration(s) and condition(s) stated in this Service

Bulletin are approved.

NOTE (1): Interchangeability code 03 becomes 01 provided that the three FCPCs are

replaced at the same time. Mixability not authorized. Replacement of the

three FCPCs has to be done simultaneously as per ACCOMPLISHMENT

INSTRUCTIONS paragraph C. of this Service Bulletin.

NOTE (2): On non-enhanced A340 aircraft model, FCPC standard L22A 2K1 (PN

LA2K1A1002B0000) is interchangeable and mixable with FCPC standard

L22A 2K0 (PN LA2K015002B0000).

**CONF 003

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE

NOTES

FCPC LA2K01500270000 LA2K015002B0000 03 NO (1) (2)

NOTE: For definitions of interchangeability codes in column INT., refer to ATA

Common Support Data Dictionary (CSDD), Chapter 2.

NOTE: Only the mixability configuration(s) and condition(s) stated in this Service

Bulletin are approved.

NOTE (1): Interchangeability code 03 becomes 01 provided that the three FCPCs are

replaced at the same time. Mixability not authorized. Replacement of the

three FCPCs has to be done simultaneously as per ACCOMPLISHMENT

INSTRUCTIONS paragraph C. of this Service Bulletin.

NOTE (2): On non-enhanced A340 aircraft model, FCPC standard L22A 2K0 (PN

LA2K015002B0000) is interchangeable and mixable with FCPC standard

L22A 2K1 (PN LA2K1A1002B0000).

**CONF 004

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE

NOTES

FCPC LA2K01500290000 LA2K015002B0000 03 NO (1) (2)

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NOTE: For definitions of interchangeability codes in column INT., refer to ATA

Common Support Data Dictionary (CSDD), Chapter 2.

NOTE: Only the mixability configuration(s) and condition(s) stated in this Service

Bulletin are approved.

NOTE (1): Interchangeability code 03 becomes 01 provided that the three FCPCs are

replaced at the same time. Mixability not authorized. Replacement of the

three FCPCs has to be done simultaneously as per ACCOMPLISHMENT

INSTRUCTIONS paragraph C. of this Service Bulletin.

NOTE (2): On non-enhanced A340 aircraft model, FCPC standard L22A 2K0 (PN

LA2K015002B0000) is interchangeable and mixable with FCPC standard

L22A 2K1 (PN LA2K1A1002B0000).

**CONF ALL

M. SPARES

FCPC LA2K01500270000

FCPC LA2K01500290000

FCPC LA2K1A100270000

FCPC LA2K1A100290000

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2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

(1) Procurement Addresses

This Service Bulletin is the subject of an AIRBUS monitored retrofit campaign.

Equipment BFEA01

Equipment BFEA02

Modification of removed equipment should be

negotiated directly with AIRBUS OPERATION

S.A.S. as per instructions given in AIRBUS

OPERATION S.A.S. Service Bulletin No.

LA2K1-27-014.

Equipment BFEA03

Equipment BFEA04

Modification of removed equipment should be

negotiated directly with AIRBUS OPERATION

S.A.S. as per instructions given in AIRBUS

OPERATION S.A.S. Service Bulletin No.

LA2K0-27-022.

(2) Price and Availability

No AIRBUS kit will be provided.

Refer to the Vendor Service Bulletin No. LA2K0-27-014 or LA2K1-27-022 for the

equipment modification sales terms.

B. INDUSTRY SUPPORT INFORMATION

Refer to the Vendor Service Bulletin No. LA2K0-27-014 or LA2K1-27-022 for the industry

support terms of the Vendor Service Bulletin parts and labor.

For the organization of this retrofit, operators are kindly requested to contact AIRBUS retrofit

management department.

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

France

Tel : (33) 5 67 19 06 22

E-mail : monitored.retrofit@airbus.com

Fax : (33) 5 61 93 27 45

C. LIST OF COMPONENTS

No Kit

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D. LIST OF MATERIALS - OPERATOR SUPPLIED

(1) Consumable Materials

None

(2) Components

None

(3) Equipment

Equipment BFEA01

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

NOTES

LA2K1A1002B0000 3 FCPC LA2K1A100270000 03

NOTE: For definitions of interchangeability codes in column INT., refer to ATA

Common Support Data Dictionary (CSDD), Chapter 2.

NOTE: Modification of removed equipment should be negotiated directly with

AIRBUS OPERATION S.A.S. as per instructions given in Service Bulletin

No. LA2K1-27-014.

Equipment BFEA02

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

NOTES

LA2K1A1002B0000 3 FCPC LA2K1A100290000 03

NOTE: For definitions of interchangeability codes in column INT., refer to ATA

Common Support Data Dictionary (CSDD), Chapter 2.

NOTE: Modification of removed equipment should be negotiated directly with

AIRBUS OPERATION S.A.S. as per instructions given in Service Bulletin

No. LA2K1-27-014.

Equipment BFEA03

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

NOTES

LA2K015002B0000 3 FCPC LA2K01500270000 03

NOTE: For definitions of interchangeability codes in column INT., refer to ATA

Common Support Data Dictionary (CSDD), Chapter 2.

NOTE: Modification of removed equipment should be negotiated directly with

AIRBUS OPERATION S.A.S. as per instructions given in Service Bulletin

No. LA2K0-27-022.

DATE: Nov 21/11 SERVICE BULLETIN No.: A340-27-4174

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Equipment BFEA04

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

NOTES

LA2K015002B0000 3 FCPC LA2K01500290000 03

NOTE: For definitions of interchangeability codes in column INT., refer to ATA

Common Support Data Dictionary (CSDD), Chapter 2.

NOTE: Modification of removed equipment should be negotiated directly with

AIRBUS OPERATION S.A.S. as per instructions given in Service Bulletin

No. LA2K0-27-022.

E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

None

F. TOOLING

(1) Tooling - Price and Availability

None

(2) Tools

To accomplish this Service Bulletin it is necessary to use the tools defined in AIRBUS

OPERATION S.A.S. Service Bulletin No. LA2K0-27-014 or AIRBUS OPERATION S.A.S.

Service Bulletin No. LA2K1-27-022.

(3) Special Tools

None

DATE: Nov 21/11 SERVICE BULLETIN No.: A340-27-4174

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This Page Intentionally Left Blank

DATE: Nov 21/11 SERVICE BULLETIN No.: A340-27-4174

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3. ACCOMPLISHMENT INSTRUCTIONS

Task 274174-831-801-001 - Modification of the three FCPCs by replacement or

reprogramming of their OBRMs.

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.

CAUTION: REFER TO AMM 20-15-00, Page Block 201 AND AIRBUS SIL 00-022 FOR

ELECTROSTATIC DISCHARGE PRECAUTIONS.

NOTE: This Task concerns the modification of the FCPCs by replacement or by

reprogramming of theirs OBRMs.

Task Associated Data

**CONF 001

Zone

120

Modified FIN

2CE1 2CE2 2CE3

Manpower

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

Additional manhours related to Vendor SB; refer to:

AIRBUS OPERATION S.A.S. Service Bulletin No. LA2K1-27-014

**CONF 002

Zone

120

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Modified FIN

2CE1 2CE2 2CE3

Manpower

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

Additional manhours related to Vendor SB; refer to:

AIRBUS OPERATION S.A.S. Service Bulletin No. LA2K1-27-014

**CONF 003

Zone

120

Modified FIN

2CE1 2CE2 2CE3

Manpower

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

Additional manhours related to Vendor SB; refer to:

AIRBUS OPERATION S.A.S. Service Bulletin No. LA2K0-27-022

**CONF 004

Zone

120

Modified FIN

2CE1 2CE2 2CE3

Manpower

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

Additional manhours related to Vendor SB; refer to:

AIRBUS OPERATION S.A.S. Service Bulletin No. LA2K0-27-022

**CONF ALL

A. GENERAL

**CONF 001

(1) Subtask 274174-839-001-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

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**CONF 002

(1) Subtask 274174-839-001-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF 003

(1) Subtask 274174-839-001-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF 004

(1) Subtask 274174-839-001-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF ALL

B. PREPARATION

**CONF 001

(1) Subtask 274174-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

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

Task 27-93-34-000-801

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

12-34-24-860-802).

(b) Do the Job Set-up procedure as specified in the removal of the three FCPCs (FINs

2CE1, 2CE2 and 2CE3) (Refer to AMM Task 27-93-34-000-801).

DATE: Nov 21/11 SERVICE BULLETIN No.: A340-27-4174

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**CONF 002

(1) Subtask 274174-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

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

Task 27-93-34-000-801

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

12-34-24-860-802).

(b) Do the Job Set-up procedure as specified in the removal of the three FCPCs (FINs

2CE1, 2CE2 and 2CE3) (Refer to AMM Task 27-93-34-000-801).

**CONF 003

(1) Subtask 274174-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

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

Task 27-93-34-000-801

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

12-34-24-860-802).

(b) Do the Job Set-up procedure as specified in the removal of the three FCPCs (FINs

2CE1, 2CE2 and 2CE3) (Refer to AMM Task 27-93-34-000-801).

**CONF 004

(1) Subtask 274174-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

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

Task 27-93-34-000-801

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

12-34-24-860-802).

(b) Do the Job Set-up procedure as specified in the removal of the three FCPCs (FINs

2CE1, 2CE2 and 2CE3) (Refer to AMM Task 27-93-34-000-801).

DATE: Nov 21/11 SERVICE BULLETIN No.: A340-27-4174

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**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 274174-831-001-001 - In the Main Rack 800VU and on the FWD Shelf

915VU modify the three FCPCs (FINs 2CE1, 2CE2 and 2CE3) by replacement or

reprogramming of their OBRMs.

Work Zones and Access Panels

Zone Access/Work location

120

References

Aircraft Maintenance Manual (AMM) Task 27-93-34-000-801

Task 27-93-34-400-801

Task 27-96-00-740-807

Task 31-51-00-610-802

Vendor Service Bulletin (VSB) AIRBUS OPERATION S.A.S. LA2K1-27-014

(a) Before replacement or reprogramming of the OBRMs.

1 On the FLT CTL section of the overhead panel 241VU (212VU), make sure

that the PRIM 1 (PRIM 2) (PRIM 3) pushbutton switch(es) is (are) pushed (the

OFF and FAULT legends of this (these) pushbutton switch(es) is (are) off).

2 Do the BITE test of the EFCS (LRU IDENT), (Refer to AMM Task

27-96-00-740-807) and make sure that the old P/N of the FCPCs are correct,

(Refer to AIRBUS OPERATION S.A.S. Service Bulletin No. LA2K1-27-014).

NOTE: Print the LRU IDENTIFICATION page (if the printer is not

available, a visual check is acceptable).

3 Open, safety/lock and tag the circuit breakers specified as per removal

of the FCPCs (FINs 2CE1, 2CE2 and 2CE3) (Refer to AMM Task

27-93-34-000-801).

4 Replace or reprogram the OBRMs on the three FCPCs (FINs 2CE1,

2CE2 and 2CE3) as per AIRBUS OPERATION S.A.S. Service Bulletin No.

LA2K1-27-014.

5 Remove the safety clip(s) and/or tag(s) and close/unlock the circuit breakers

as per installation of the FCPCs (FINs 2CE1, 2CE2 and 2CE3) (Refer to AMM

Task 27-93-34-400-801).

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(b) OEB cancellation :

1 On aircraft equipped with OEB REMINDER function, if the ECAM warning has

been flagged as described in OEB 40 (formerly OEB 88 up until 2011), the

following codes should be deleted from the FWC database.

CODE WARN STS

34/10/050/061 YES NO

34/10/060/063 YES NO

34/10/070/065 YES NO

34/10/020/055 YES NO

34/10/030/057 YES NO

34/10/040/059 YES NO

NOTE: Refer to AMM Task 31-51-00-610-802 "Delete OEB

REMINDER data from FWCs using MCDUs".

2 On aircraft equipped with OEB REMINDER function, if the ECAM warning has

been flagged as described in OEB 08 (formerly OEB 54 up until 2011), the

following codes should be deleted from the FWC database.

CODE WARN STS

27/90/050/113 NO YES

27/90/200/109 NO YES

27/30/050/083 NO YES

29/11/060/091 NO YES

NOTE: Refer to AMM Task 31-51-00-610-802 "Delete OEB

REMINDER data from FWCs using MCDUs".

**CONF 002

(1) Subtask 274174-831-001-002 - In the Main Rack 800VU and on the FWD Shelf

915VU modify the three FCPCs (FINs 2CE1, 2CE2 and 2CE3) by replacement or

reprogramming of their OBRMs.

Work Zones and Access Panels

Zone Access/Work location

120

References

Aircraft Maintenance Manual (AMM) Task 27-93-34-000-801

Task 27-93-34-400-801

Task 27-96-00-740-807

Task 31-51-00-610-802

Vendor Service Bulletin (VSB) AIRBUS OPERATION S.A.S. LA2K1-27-014

(a) Before replacement or reprogramming of the OBRMs.

1 On the FLT CTL section of the overhead panel 241VU (212VU), make sure

that the PRIM 1 (PRIM 2) (PRIM 3) pushbutton switch(es) is (are) pushed (the

OFF and FAULT legends of this (these) pushbutton switch(es) is (are) off).

DATE: Nov 21/11 SERVICE BULLETIN No.: A340-27-4174

REVISION No.: 00 - Nov 21/11 Page: 24

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2 Do the BITE test of the EFCS (LRU IDENT), (Refer to AMM Task

27-96-00-740-807) and make sure that the old P/N of the FCPCs are correct,

(Refer to AIRBUS OPERATION S.A.S. Service Bulletin No. LA2K1-27-014).

NOTE: Print the LRU IDENTIFICATION page (if the printer is not

available, a visual check is acceptable).

3 Open, safety/lock and tag the circuit breakers specified as per removal

of the FCPCs (FINs 2CE1, 2CE2 and 2CE3) (Refer to AMM Task

27-93-34-000-801).

4 Replace or reprogram the OBRMs on the three FCPCs (FINs 2CE1,

2CE2 and 2CE3) as per AIRBUS OPERATION S.A.S. Service Bulletin No.

LA2K1-27-014.

5 Remove the safety clip(s) and/or tag(s) and close/unlock the circuit breakers

as per installation of the FCPCs (FINs 2CE1, 2CE2 and 2CE3) (Refer to AMM

Task 27-93-34-400-801).

(b) OEB cancellation :

1 On aircraft equipped with OEB REMINDER function, if the ECAM warning has

been flagged as described in OEB 40 (formerly OEB 88 up until 2011), the

following codes should be deleted from the FWC database.

CODE WARN STS

34/10/050/061 YES NO

34/10/060/063 YES NO

34/10/070/065 YES NO

34/10/020/055 YES NO

34/10/030/057 YES NO

34/10/040/059 YES NO

NOTE: Refer to AMM Task 31-51-00-610-802 "Delete OEB

REMINDER data from FWCs using MCDUs".

2 On aircraft equipped with OEB REMINDER function, if the ECAM warning has

been flagged as described in OEB 08 (formerly OEB 54 up until 2011), the

following codes should be deleted from the FWC database.

CODE WARN STS

27/90/050/113 NO YES

27/90/200/109 NO YES

27/30/050/083 NO YES

29/11/060/091 NO YES

NOTE: Refer to AMM Task 31-51-00-610-802 "Delete OEB

REMINDER data from FWCs using MCDUs".

DATE: Nov 21/11 SERVICE BULLETIN No.: A340-27-4174

REVISION No.: 00 - Nov 21/11 Page: 25

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SERVICE BULLETIN

**CONF 003

(1) Subtask 274174-831-001-003 - In the Main Rack 800VU and on the FWD Shelf

915VU modify the three FCPCs (FINs 2CE1, 2CE2 and 2CE3) by replacement or

reprogramming of their OBRMs.

Work Zones and Access Panels

Zone Access/Work location

120

References

Aircraft Maintenance Manual (AMM) Task 27-93-34-000-801

Task 27-93-34-400-801

Task 27-96-00-740-807

Task 31-51-00-610-802

Vendor Service Bulletin (VSB) AIRBUS OPERATION S.A.S. LA2K0-27-022

(a) Before replacement or reprogramming of the OBRMs.

1 On the FLT CTL section of the overhead panel 241VU (212VU), make sure

that the PRIM 1 (PRIM 2) (PRIM 3) pushbutton switch(es) is (are) pushed (the

OFF and FAULT legends of this (these) pushbutton switch(es) is (are) off).

2 Do the BITE test of the EFCS (LRU IDENT), (Refer to AMM Task

27-96-00-740-807) and make sure that the old P/N of the FCPCs are correct,

(Refer to AIRBUS OPERATION S.A.S. Service Bulletin No. LA2K0-27-022).

NOTE: Print the LRU IDENTIFICATION page (if the printer is not

available, a visual check is acceptable).

3 Open, safety/lock and tag the circuit breakers specified as per removal

of the FCPCs (FINs 2CE1, 2CE2 and 2CE3) (Refer to AMM Task

27-93-34-000-801).

4 Replace or reprogram the OBRMs on the three FCPCs (FINs 2CE1,

2CE2 and 2CE3) as per AIRBUS OPERATION S.A.S. Service Bulletin No.

LA2K0-27-022.

5 Remove the safety clip(s) and/or tag(s) and close/unlock the circuit breakers

as per installation of the FCPCs (FINs 2CE1, 2CE2 and 2CE3) (Refer to AMM

Task 27-93-34-400-801).

(b) OEB cancellation :

1 On aircraft equipped with OEB REMINDER function, if the ECAM warning has

been flagged as described in OEB 40 (formerly OEB 88 up until 2011), the

following codes should be deleted from the FWC database.

CODE WARN STS

34/10/050/061 YES NO

34/10/060/063 YES NO

34/10/070/065 YES NO

DATE: Nov 21/11 SERVICE BULLETIN No.: A340-27-4174

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SERVICE BULLETIN

CODE WARN STS

34/10/020/055 YES NO

34/10/030/057 YES NO

34/10/040/059 YES NO

NOTE: Refer to AMM Task 31-51-00-610-802 "Delete OEB

REMINDER data from FWCs using MCDUs".

2 On aircraft equipped with OEB REMINDER function, if the ECAM warning has

been flagged as described in OEB 08 (formerly OEB 54 up until 2011), the

following codes should be deleted from the FWC database.

CODE WARN STS

27/90/050/113 NO YES

27/90/200/109 NO YES

27/30/050/083 NO YES

29/11/060/091 NO YES

NOTE: Refer to AMM Task 31-51-00-610-802 "Delete OEB

REMINDER data from FWCs using MCDUs".

**CONF 004

(1) Subtask 274174-831-001-004 - In the Main Rack 800VU and on the FWD Shelf

915VU modify the three FCPCs (FINs 2CE1, 2CE2 and 2CE3) by replacement or

reprogramming of their OBRMs.

Work Zones and Access Panels

Zone Access/Work location

120

References

Aircraft Maintenance Manual (AMM) Task 27-93-34-000-801

Task 27-93-34-400-801

Task 27-96-00-740-807

Task 31-51-00-610-802

Vendor Service Bulletin (VSB) AIRBUS OPERATION S.A.S. LA2K0-27-022

(a) Before replacement or reprogramming of the OBRMs.

1 On the FLT CTL section of the overhead panel 241VU (212VU), make sure

that the PRIM 1 (PRIM 2) (PRIM 3) pushbutton switch(es) is (are) pushed (the

OFF and FAULT legends of this (these) pushbutton switch(es) is (are) off).

2 Do the BITE test of the EFCS (LRU IDENT), (Refer to AMM Task

27-96-00-740-807) and make sure that the old P/N of the FCPCs are correct,

(Refer to AIRBUS OPERATION S.A.S. Service Bulletin No. LA2K0-27-022).

NOTE: Print the LRU IDENTIFICATION page (if the printer is not

available, a visual check is acceptable).

DATE: Nov 21/11 SERVICE BULLETIN No.: A340-27-4174

REVISION No.: 00 - Nov 21/11 Page: 27

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SERVICE BULLETIN

3 Open, safety/lock and tag the circuit breakers specified as per removal

of the FCPCs (FINs 2CE1, 2CE2 and 2CE3) (Refer to AMM Task

27-93-34-000-801).

4 Replace or reprogram the OBRMs on the three FCPCs (FINs 2CE1,

2CE2 and 2CE3) as per AIRBUS OPERATION S.A.S. Service Bulletin No.

LA2K0-27-022.

5 Remove the safety clip(s) and/or tag(s) and close/unlock the circuit breakers

as per installation of the FCPCs (FINs 2CE1, 2CE2 and 2CE3) (Refer to AMM

Task 27-93-34-400-801).

(b) OEB cancellation :

1 On aircraft equipped with OEB REMINDER function, if the ECAM warning has

been flagged as described in OEB 40 (formerly OEB 88 up until 2011), the

following codes should be deleted from the FWC database.

CODE

WARN

STS

34/10/050/061 YES NO

34/10/060/063 YES NO

34/10/070/065 YES NO

34/10/020/055 YES NO

34/10/030/057 YES NO

34/10/040/059 YES NO

NOTE: Refer to AMM Task 31-51-00-610-802 "Delete OEB

REMINDER data from FWCs using MCDUs".

2 On aircraft equipped with OEB REMINDER function, if the ECAM warning has

been flagged as described in OEB 08 (formerly OEB 54 up until 2011), the

following codes should be deleted from the FWC database.

CODE WARN STS

27/90/050/113 NO YES

27/90/200/109 NO YES

27/30/050/083 NO YES

29/11/060/091 NO YES

NOTE: Refer to AMM Task 31-51-00-610-802 "Delete OEB

REMINDER data from FWCs using MCDUs".

DATE: Nov 21/11 SERVICE BULLETIN No.: A340-27-4174

REVISION No.: 00 - Nov 21/11 Page: 28

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SERVICE BULLETIN

**CONF ALL

D. TEST

**CONF 001

(1) Subtask 274174-700-001-001 - Test

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 22-97-00-740-801

Task 27-93-34-000-801

Task 27-93-34-400-801

Task 27-96-00-740-802

Task 27-96-00-740-807

Vendor Service Bulletin (VSB) AIRBUS OPERATION S.A.S. LA2K1-27-014

(a) After replacement or reprogramming of OBRMs.

1 After power-up, on the FLT CTL section of the overhead panel 241VU

(212VU), make sure that the PRIM 1 (PRIM 2) (PRIM 3) pushbutton switch(es)

is (are) pushed (the OFF and FAULT legends of this (these) pushbutton

switch(es) is (are) off).

NOTE: If a FAULT is present, do a reset with the concerned

pushbutton switch. If FAULT persists, replace the concerned

computer (Refer to AMM Task 27-93-34-000-801 and AMM

Task 27-93-34-400-801).

2 Do the BITE test of the Electrical Flight Control System (EFCS) (LRU IDENT)

(Refer to AMM Task 27-96-00-740-807) and make sure that the new P/N of

the FCPCs are correct, (Refer to AIRBUS OPERATION S.A.S. Service Bulletin

No. LA2K1-27-014).

NOTE: Print the LRU IDENTIFICATION page (if the printer is not

available, a visual check is acceptable).

3 Do the BITE test of the EFCS (SYSTEM TEST) (Refer to AMM Task

27-96-00-740-802).

4 If the airline operates the aircraft in CAT 3 conditions, do the LAND CAT III

capability test (Refer to AMM Task 22-97-00-740-801).

**CONF 002

(1) Subtask 274174-700-001-002 - Test

Manpower Resources

Skills NON SPECIFIC

DATE: Nov 21/11 SERVICE BULLETIN No.: A340-27-4174

REVISION No.: 00 - Nov 21/11 Page: 29

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SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) Task 22-97-00-740-801

Task 27-93-34-000-801

Task 27-93-34-400-801

Task 27-96-00-740-802

Task 27-96-00-740-807

Vendor Service Bulletin (VSB) AIRBUS OPERATION S.A.S. LA2K1-27-014

(a) After replacement or reprogramming of OBRMs.

1 After power-up, on the FLT CTL section of the overhead panel 241VU

(212VU), make sure that the PRIM 1 (PRIM 2) (PRIM 3) pushbutton switch(es)

is (are) pushed (the OFF and FAULT legends of this (these) pushbutton

switch(es) is (are) off).

NOTE: If a FAULT is present, do a reset with the concerned

pushbutton switch. If FAULT persists, replace the concerned

computer (Refer to AMM Task 27-93-34-000-801 and AMM

Task 27-93-34-400-801).

2 Do the BITE test of the Electrical Flight Control System (EFCS) (LRU IDENT)

(Refer to AMM Task 27-96-00-740-807) and make sure that the new P/N of

the FCPCs are correct, (Refer to AIRBUS OPERATION S.A.S. Service Bulletin

No. LA2K1-27-014).

NOTE: Print the LRU IDENTIFICATION page (if the printer is not

available, a visual check is acceptable).

3 Do the BITE test of the EFCS (SYSTEM TEST) (Refer to AMM Task

27-96-00-740-802).

4 If the airline operates the aircraft in CAT 3 conditions, do the LAND CAT III

capability test (Refer to AMM Task 22-97-00-740-801).

**CONF 003

(1) Subtask 274174-700-001-003 - Test

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 22-97-00-740-801

Task 27-93-34-000-801

Task 27-93-34-400-801

Task 27-96-00-740-802

Task 27-96-00-740-807

Vendor Service Bulletin (VSB) AIRBUS OPERATION S.A.S. LA2K0-27-022

DATE: Nov 21/11 SERVICE BULLETIN No.: A340-27-4174

REVISION No.: 00 - Nov 21/11 Page: 30

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SERVICE BULLETIN

(a) After replacement or reprogramming of OBRMs.

1 After power-up, on the FLT CTL section of the overhead panel 241VU

(212VU), make sure that the PRIM 1 (PRIM 2) (PRIM 3) pushbutton switch(es)

is (are) pushed (the OFF and FAULT legends of this (these) pushbutton

switch(es) is (are) off).

NOTE: If a FAULT is present, do a reset with the concerned

pushbutton switch. If FAULT persists, replace the concerned

computer (Refer to AMM Task 27-93-34-000-801 and AMM

Task 27-93-34-400-801).

2 Do the BITE test of the Electrical Flight Control System (EFCS) (LRU IDENT)

(Refer to AMM Task 27-96-00-740-807) and make sure that the new P/N of

the FCPCs are correct, (Refer to AIRBUS OPERATION S.A.S. Service Bulletin

No. LA2K0-27-022).

NOTE: Print the LRU IDENTIFICATION page (if the printer is not

available, a visual check is acceptable).

3 Do the BITE test of the EFCS (SYSTEM TEST) (Refer to AMM Task

27-96-00-740-802).

4 If the airline operates the aircraft in CAT 3 conditions, do the LAND CAT III

capability test (Refer to AMM Task 22-97-00-740-801).

**CONF 004

(1) Subtask 274174-700-001-004 - Test

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 22-97-00-740-801

Task 27-93-34-000-801

Task 27-93-34-400-801

Task 27-96-00-740-802

Task 27-96-00-740-807

Vendor Service Bulletin (VSB) AIRBUS OPERATION S.A.S. LA2K0-27-022

(a) After replacement or reprogramming of OBRMs.

1 After power-up, on the FLT CTL section of the overhead panel 241VU

(212VU), make sure that the PRIM 1 (PRIM 2) (PRIM 3) pushbutton switch(es)

is (are) pushed (the OFF and FAULT legends of this (these) pushbutton

switch(es) is (are) off).

NOTE: If a FAULT is present, do a reset with the concerned

pushbutton switch. If FAULT persists, replace the concerned

computer (Refer to AMM Task 27-93-34-000-801 and AMM

Task 27-93-34-400-801).

DATE: Nov 21/11 SERVICE BULLETIN No.: A340-27-4174

REVISION No.: 00 - Nov 21/11 Page: 31

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SERVICE BULLETIN

2 Do the BITE test of the Electrical Flight Control System (EFCS) (LRU IDENT)

(Refer to AMM Task 27-96-00-740-807) and make sure that the new P/N of

the FCPCs are correct, (Refer to AIRBUS OPERATION S.A.S. Service Bulletin

No. LA2K0-27-022).

NOTE: Print the LRU IDENTIFICATION page (if the printer is not

available, a visual check is acceptable).

3 Do the BITE test of the EFCS (SYSTEM TEST) (Refer to AMM Task

27-96-00-740-802).

4 If the airline operates the aircraft in CAT 3 conditions, do the LAND CAT III

capability test (Refer to AMM Task 22-97-00-740-801).

**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 274174-942-001-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 27-93-34-400-801

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

equipment.

(b) Do the close-up procedure as specified in installation of the three FCPCs (FINs

2CE1, 2CE2 and 2CE3) (Refer to AMM Task 27-93-34-400-801).

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

**CONF 002

(1) Subtask 274174-942-001-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 27-93-34-400-801

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

equipment.

(b) Do the close-up procedure as specified in installation of the three FCPCs (FINs

2CE1, 2CE2 and 2CE3) (Refer to AMM Task 27-93-34-400-801).

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

DATE: Nov 21/11 SERVICE BULLETIN No.: A340-27-4174

REVISION No.: 00 - Nov 21/11 Page: 32

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SERVICE BULLETIN

**CONF 003

(1) Subtask 274174-942-001-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 27-93-34-400-801

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

equipment.

(b) Do the close-up procedure as specified in installation of the three FCPCs (FINs

2CE1, 2CE2 and 2CE3) (Refer to AMM Task 27-93-34-400-801).

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

**CONF 004

(1) Subtask 274174-942-001-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 27-93-34-400-801

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

equipment.

(b) Do the close-up procedure as specified in installation of the three FCPCs (FINs

2CE1, 2CE2 and 2CE3) (Refer to AMM Task 27-93-34-400-801).

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

DATE: Nov 21/11 SERVICE BULLETIN No.: A340-27-4174

REVISION No.: 00 - Nov 21/11 Page: 33

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This Page Intentionally Left Blank

DATE: Nov 21/11 SERVICE BULLETIN No.: A340-27-4174

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SERVICE BULLETIN

Task 274174-831-802-001 - Modification by replacement of three FCPCs.

**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: This Task concerns the replacement of the three FCPCs.

Task Associated Data

**CONF 001

Zone

120

Modified FIN

2CE1 2CE2 2CE3

Manpower

TOTAL MANHOURS 4.50

ELAPSED TIME (HOURS) 4.50

**CONF 002

Zone

120

Modified FIN

2CE1 2CE2 2CE3

Manpower

TOTAL MANHOURS 4.50

ELAPSED TIME (HOURS) 4.50

DATE: Nov 21/11 SERVICE BULLETIN No.: A340-27-4174

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SERVICE BULLETIN

**CONF 003

Modified FIN

2CE1 2CE2 2CE3

Manpower

TOTAL MANHOURS 4.50

ELAPSED TIME (HOURS) 4.50

**CONF 004

Modified FIN

2CE1 2CE2 2CE3

Manpower

TOTAL MANHOURS 4.50

ELAPSED TIME (HOURS) 4.50

**CONF ALL

A. GENERAL

**CONF 001

(1) Subtask 274174-839-002-001 - 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 274174-839-002-001 - 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 003

(1) Subtask 274174-839-002-001 - 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: Nov 21/11 SERVICE BULLETIN No.: A340-27-4174

REVISION No.: 00 - Nov 21/11 Page: 36

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SERVICE BULLETIN

**CONF 004

(1) Subtask 274174-839-002-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF ALL

B. PREPARATION

**CONF 001

(1) Subtask 274174-941-002-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

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

Task 27-93-34-000-801

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

12-34-24-860-802).

(b) Do the Job Set-up procedure as specified in the removal of the three FCPCs (FINs

2CE1, 2CE2 and 2CE3) (Refer to AMM Task 27-93-34-000-801).

**CONF 002

(1) Subtask 274174-941-002-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

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

Task 27-93-34-000-801

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

12-34-24-860-802).

(b) Do the Job Set-up procedure as specified in the removal of the three FCPCs (FINs

2CE1, 2CE2 and 2CE3) (Refer to AMM Task 27-93-34-000-801).

DATE: Nov 21/11 SERVICE BULLETIN No.: A340-27-4174

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SERVICE BULLETIN

**CONF 003

(1) Subtask 274174-941-002-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

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

Task 27-93-34-000-801

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

12-34-24-860-802).

(b) Do the Job Set-up procedure as specified in the removal of the three FCPCs (FINs

2CE1, 2CE2 and 2CE3) (Refer to AMM Task 27-93-34-000-801).

**CONF 004

(1) Subtask 274174-941-002-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

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

Task 27-93-34-000-801

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

12-34-24-860-802).

(b) Do the Job Set-up procedure as specified in the removal of the three FCPCs (FINs

2CE1, 2CE2 and 2CE3) (Refer to AMM Task 27-93-34-000-801).

**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 274174-960-001-001 - In the Main Rack 800VU and on the FWD Shelf

915VU, replace the three FCPCs (FINs 2CE1, 2CE2 and 2CE3).

Work Zones and Access Panels

Zone Access/Work location

120

DATE: Nov 21/11 SERVICE BULLETIN No.: A340-27-4174

REVISION No.: 00 - Nov 21/11 Page: 38

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SERVICE BULLETIN

Manpower Resources

Manhours 1.50

Minimum number of person 1

Subtask elapsed time 1.50

Skills NON SPECIFIC

Material necessary to do the job

Equipment BFEA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

LA2K1A1002B0000 3 FCPC

NOTE: Modification of removed equipment should be negotiated directly with

AIRBUS OPERATION S.A.S. as per instructions given in Service Bulletin

No. LA2K1-27-014.

References

Aircraft Maintenance Manual (AMM) Task 27-93-34-000-801

Task 27-93-34-400-801

Task 31-51-00-610-802

(a) Replacement of the FCPCs :

1 On the FWD Shelf 915VU, remove the FCPC (FIN 2CE1) :

Refer to AMM Task 27-93-34-000-801

FIN 2CE1

1 FCPC LA2K1A100270000

2 In the FWD Shelf 915VU, install the FCPC (FIN 2CE1) :

Refer to AMM Task 27-93-34-400-801

FIN 2CE1

1 FCPC LA2K1A1002B0000

3 In the main rack 800VU, remove the two FCPCs (FINs 2CE2 and 2CE3) :

Refer to AMM Task 27-93-34-000-801

FIN 2CE2

1 FCPC LA2K1A100270000

and

FIN 2CE3

1 FCPC LA2K1A100270000

4 In the main rack 800VU, install the two FCPCs (FINs 2CE2 and 2CE3) :

Refer to AMM Task 27-93-34-400-801

DATE: Nov 21/11 SERVICE BULLETIN No.: A340-27-4174

REVISION No.: 00 - Nov 21/11 Page: 39

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SERVICE BULLETIN

FIN 2CE2

1 FCPC LA2K1A1002B0000

and

FIN 2CE3

1 FCPC LA2K1A1002B0000

(b) OEB cancellation :

1 On aircraft equipped with OEB REMINDER function, if the ECAM warning has

been flagged as described in OEB 40 (formerly OEB 88 up until 2011), the

following codes should be deleted from the FWC database.

CODE WARN STS

34/10/050/061 YES NO

34/10/060/063 YES NO

34/10/070/065 YES NO

34/10/020/055 YES NO

34/10/030/057 YES NO

34/10/040/059 YES NO

NOTE: Refer to AMM Task 31-51-00-610-802 "Delete OEB

REMINDER data from FWCs using MCDUs".

2 On aircraft equipped with OEB REMINDER function, if the ECAM warning has

been flagged as described in OEB 08 (formerly OEB 54 up until 2011), the

following codes should be deleted from the FWC database.

CODE WARN STS

27/90/050/113 NO YES

27/90/200/109 NO YES

27/30/050/083 NO YES

29/11/060/091 NO YES

NOTE: Refer to AMM Task 31-51-00-610-802 "Delete OEB

REMINDER data from FWCs using MCDUs".

**CONF 002

(1) Subtask 274174-960-001-002 - In the Main Rack 800VU and on the FWD Shelf

915VU, replace the three FCPCs (FINs 2CE1, 2CE2 and 2CE3).

Work Zones and Access Panels

Zone Access/Work location

120

DATE: Nov 21/11 SERVICE BULLETIN No.: A340-27-4174

REVISION No.: 00 - Nov 21/11 Page: 40

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SERVICE BULLETIN

Manpower Resources

Manhours 1.50

Minimum number of person 1

Subtask elapsed time 1.50

Skills NON SPECIFIC

Material necessary to do the job

Equipment BFEA02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

LA2K1A1002B0000 3 FCPC

NOTE: Modification of removed equipment should be negotiated directly with

AIRBUS OPERATION S.A.S. as per instructions given in Service Bulletin

No. LA2K1-27-014.

References

Aircraft Maintenance Manual (AMM) Task 27-93-34-000-801

Task 27-93-34-400-801

Task 31-51-00-610-802

(a) Replacement of the FCPCs :

1 On the FWD Shelf 915VU, remove the FCPC (FIN 2CE1) :

Refer to AMM Task 27-93-34-000-801

FIN 2CE1

1 FCPC LA2K1A100290000

2 In the FWD Shelf 915VU, install the FCPC (FIN 2CE1) :

Refer to AMM Task 27-93-34-400-801

FIN 2CE1

1 FCPC LA2K1A1002B0000

3 In the main rack 800VU, remove the two FCPCs (FINs 2CE2 and 2CE3) :

Refer to AMM Task 27-93-34-000-801

FIN 2CE2

1 FCPC LA2K1A100290000

and

FIN 2CE3

1 FCPC LA2K1A100290000

4 In the main rack 800VU, install the two FCPCs (FINs 2CE2 and 2CE3) :

Refer to AMM Task 27-93-34-400-801

DATE: Nov 21/11 SERVICE BULLETIN No.: A340-27-4174

REVISION No.: 00 - Nov 21/11 Page: 41

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SERVICE BULLETIN

FIN 2CE2

1 FCPC LA2K1A1002B0000

and

FIN 2CE3

1 FCPC LA2K1A1002B0000

(b) OEB cancellation :

1 On aircraft equipped with OEB REMINDER function, if the ECAM warning has

been flagged as described in OEB 40 (formerly OEB 88 up until 2011), the

following codes should be deleted from the FWC database.

CODE WARN STS

34/10/050/061 YES NO

34/10/060/063 YES NO

34/10/070/065 YES NO

34/10/020/055 YES NO

34/10/030/057 YES NO

34/10/040/059 YES NO

NOTE: Refer to AMM Task 31-51-00-610-802 "Delete OEB

REMINDER data from FWCs using MCDUs".

2 On aircraft equipped with OEB REMINDER function, if the ECAM warning has

been flagged as described in OEB 08 (formerly OEB 54 up until 2011), the

following codes should be deleted from the FWC database.

CODE WARN STS

27/90/050/113 NO YES

27/90/200/109 NO YES

27/30/050/083 NO YES

29/11/060/091 NO YES

NOTE: Refer to AMM Task 31-51-00-610-802 "Delete OEB

REMINDER data from FWCs using MCDUs".

**CONF 003

(1) Subtask 274174-960-001-003 - In the Main Rack 800VU and on the FWD Shelf

915VU, replace the three FCPCs (FINs 2CE1, 2CE2 and 2CE3).

Manpower Resources

Manhours 1.50

Minimum number of person 1

Subtask elapsed time 1.50

Skills NON SPECIFIC

DATE: Nov 21/11 SERVICE BULLETIN No.: A340-27-4174

REVISION No.: 00 - Nov 21/11 Page: 42

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SERVICE BULLETIN

Material necessary to do the job

Equipment BFEA03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

LA2K015002B0000 3 FCPC

NOTE: Modification of removed equipment should be negotiated directly with

AIRBUS OPERATION S.A.S. as per instructions given in Service Bulletin

No. LA2K0-27-022.

References

Aircraft Maintenance Manual (AMM) Task 27-93-34-000-801

Task 27-93-34-400-801

Task 31-51-00-610-802

(a) Replacement of the FCPCs :

1 On the FWD Shelf 915VU, remove the FCPC (FIN 2CE1) :

Refer to AMM Task 27-93-34-000-801

FIN 2CE1

1 FCPC LA2K01500270000

2 On the FWD Shelf 915VU, install the FCPC (FIN 2CE1) :

Refer to AMM Task 27-93-34-400-801

FIN 2CE1

1 FCPC LA2K015002B0000

3 In the main rack 800VU, remove the two FCPCs (FINs 2CE2 and 2CE3) :

Refer to AMM Task 27-93-34-000-801

FIN 2CE2

1 FCPC LA2K01500270000

and

FIN 2CE3

1 FCPC LA2K01500270000

4 In the main rack 800VU, install the two FCPCs (FINs 2CE2 and 2CE3) :

Refer to AMM Task 27-93-34-400-801

FIN 2CE2

1 FCPC LA2K015002B0000

and

DATE: Nov 21/11 SERVICE BULLETIN No.: A340-27-4174

REVISION No.: 00 - Nov 21/11 Page: 43

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SERVICE BULLETIN

FIN 2CE3

1 FCPC LA2K015002B0000

(b) OEB cancellation :

1 On aircraft equipped with OEB REMINDER function, if the ECAM warning has

been flagged as described in OEB 40 (formerly OEB 88 up until 2011), the

following codes should be deleted from the FWC database.

CODE WARN STS

34/10/050/061 YES NO

34/10/060/063 YES NO

34/10/070/065 YES NO

34/10/020/055 YES NO

34/10/030/057 YES NO

34/10/040/059 YES NO

NOTE: Refer to AMM Task 31-51-00-610-802 "Delete OEB

REMINDER data from FWCs using MCDUs".

2 On aircraft equipped with OEB REMINDER function, if the ECAM warning has

been flagged as described in OEB 08 (formerly OEB 54 up until 2011), the

following codes should be deleted from the FWC database.

CODE WARN STS

27/90/050/113 NO YES

27/90/200/109 NO YES

27/30/050/083 NO YES

29/11/060/091 NO YES

NOTE: Refer to AMM Task 31-51-00-610-802 "Delete OEB

REMINDER data from FWCs using MCDUs".

**CONF 004

(1) Subtask 274174-960-001-004 - In the Main Rack 800VU and on the FWD Shelf

915VU, replace the three FCPCs (FINs 2CE1, 2CE2 and 2CE3).

Manpower Resources

Manhours 1.50

Minimum number of person 1

Subtask elapsed time 1.50

Skills NON SPECIFIC

Material necessary to do the job

Equipment BFEA04

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

LA2K015002B0000 3 FCPC

DATE: Nov 21/11 SERVICE BULLETIN No.: A340-27-4174

REVISION No.: 00 - Nov 21/11 Page: 44

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SERVICE BULLETIN

NOTE: Modification of removed equipment should be negotiated directly with

AIRBUS OPERATION S.A.S. as per instructions given in Service Bulletin

No. LA2K0-27-022.

References

Aircraft Maintenance Manual (AMM) Task 27-93-34-000-801

Task 27-93-34-400-801

Task 31-51-00-610-802

(a) Replacement of the FCPCs :

1 On the FWD Shelf 915VU, remove the FCPC (FIN 2CE1) :

Refer to AMM Task 27-93-34-000-801

FIN 2CE1

1 FCPC LA2K01500290000

2 On the FWD Shelf 915VU, install the FCPC (FIN 2CE1) :

Refer to AMM Task 27-93-34-400-801

FIN 2CE1

1 FCPC LA2K015002B0000

3 In the main rack 800VU, remove the two FCPCs (FINs 2CE2 and 2CE3) :

Refer to AMM Task 27-93-34-000-801

FIN 2CE2

1 FCPC LA2K01500290000

and

FIN 2CE3

1 FCPC LA2K01500290000

4 In the main rack 800VU, install the two FCPCs (FINs 2CE2 and 2CE3) :

Refer to AMM Task 27-93-34-400-801

FIN 2CE2

1 FCPC LA2K015002B0000

and

FIN 2CE3

1 FCPC LA2K015002B0000

DATE: Nov 21/11 SERVICE BULLETIN No.: A340-27-4174

REVISION No.: 00 - Nov 21/11 Page: 45

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SERVICE BULLETIN

(b) OEB cancellation :

1 On aircraft equipped with OEB REMINDER function, if the ECAM warning has

been flagged as described in OEB 40 (formerly OEB 88 up until 2011), the

following codes should be deleted from the FWC database.

CODE WARN STS

34/10/050/061 YES NO

34/10/060/063 YES NO

34/10/070/065 YES NO

34/10/020/055 YES NO

34/10/030/057 YES NO

34/10/040/059 YES NO

NOTE: Refer to AMM Task 31-51-00-610-802 "Delete OEB

REMINDER data from FWCs using MCDUs".

2 On aircraft equipped with OEB REMINDER function, if the ECAM warning has

been flagged as described in OEB 08 (formerly OEB 54 up until 2011), the

following codes should be deleted from the FWC database.

CODE WARN STS

27/90/050/113 NO YES

27/90/200/109 NO YES

27/30/050/083 NO YES

29/11/060/091 NO YES

NOTE: Refer to AMM Task 31-51-00-610-802 "Delete OEB

REMINDER data from FWCs using MCDUs".

**CONF ALL

D. TEST

**CONF 001

(1) Subtask 274174-700-002-001 - Test

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 27-93-34-400-801

(a) Do the test procedure after installation of the FCPCs (FINs 2CE1, 2CE2 and 2CE3)

(Refer to AMM Task 27-93-34-400-801).

DATE: Nov 21/11 SERVICE BULLETIN No.: A340-27-4174

REVISION No.: 00 - Nov 21/11 Page: 46

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SERVICE BULLETIN

**CONF 002

(1) Subtask 274174-700-002-001 - Test

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 27-93-34-400-801

(a) Do the test procedure after installation of the FCPCs (FINs 2CE1, 2CE2 and 2CE3)

(Refer to AMM Task 27-93-34-400-801).

**CONF 003

(1) Subtask 274174-700-002-001 - Test

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 27-93-34-400-801

(a) Do the test procedure after installation of the FCPCs (FINs 2CE1, 2CE2 and 2CE3)

(Refer to AMM Task 27-93-34-400-801).

**CONF 004

(1) Subtask 274174-700-002-001 - Test

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 27-93-34-400-801

(a) Do the test procedure after installation of the FCPCs (FINs 2CE1, 2CE2 and 2CE3)

(Refer to AMM Task 27-93-34-400-801).

**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 274174-942-002-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 27-93-34-400-801

DATE: Nov 21/11 SERVICE BULLETIN No.: A340-27-4174

REVISION No.: 00 - Nov 21/11 Page: 47

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SERVICE BULLETIN

(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 installation of the three FCPCs (FINs

2CE1, 2CE2 and 2CE3) (Refer to AMM Task 27-93-34-400-801).

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

**CONF 002

(1) Subtask 274174-942-002-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 27-93-34-400-801

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

equipment.

(b) Do the close-up procedure as specified in installation of the three FCPCs (FINs

2CE1, 2CE2 and 2CE3) (Refer to AMM Task 27-93-34-400-801).

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

**CONF 003

(1) Subtask 274174-942-002-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 27-93-34-400-801

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

equipment.

(b) Do the close-up procedure as specified in installation of the three FCPCs (FINs

2CE1, 2CE2 and 2CE3) (Refer to AMM Task 27-93-34-400-801).

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

**CONF 004

(1) Subtask 274174-942-002-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

DATE: Nov 21/11 SERVICE BULLETIN No.: A340-27-4174

REVISION No.: 00 - Nov 21/11 Page: 48

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SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) Task 27-93-34-400-801

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

equipment.

(b) Do the close-up procedure as specified in installation of the three FCPCs (FINs

2CE1, 2CE2 and 2CE3) (Refer to AMM Task 27-93-34-400-801).

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

DATE: Nov 21/11 SERVICE BULLETIN No.: A340-27-4174

REVISION No.: 00 - Nov 21/11 Page: 49

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SERVICE BULLETIN

REPORTING SHEET

TITLE: FLIGHT CONTROLS - FCPC - INTRODUCE FCPC L22A 2K1 OR FCPC

L22A 2K0 FOR A340-200/300 BASIC A/C WITH MECHANICAL RUDDER

MODIFICATION No.: 55437S18647 55438S18648 201689S31875 201690S31876

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: Nov 21/11 SERVICE BULLETIN No.: A340-27-4174

REVISION No.: 00 - Nov 21/11 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: Nov 21/11 SERVICE BULLETIN No.: A340-27-4174

REVISION No.: 00 - Nov 21/11 Page: 1

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