5 DATE : Sep 22/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Mar 03/05 Page : 1 of 

Printed in FRANCE © AIRBUS, 2005 All rights reserved

MANDATORY MANDATORY MAND

ATA SYSTEM : 27

TITLE : FLIGHT CONTROLS - ELEVATOR SERVOCONTROLS - INSPECTION AND 

THE SOLENOID VALVES O-RING SEALS.

MODIFICATION No. : None

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

ADDITIONAL WORK

No additional work is required by this revision for aircraft m

previous issue.

REASON

Revision No. 01 issued to inform the operators that this Servi

rendered mandatory and to delete aircraft MSN 0643, 0646, 065

0797 and 0810.

CHANGES

SUMMARY :

— REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES

. Text modified. Compliance Recommended becomes Mandatory. 

TABLE updated.

— EFFECTIVITY

. Operator AIB deleted.

PLANNING INFORMATION :

— EFFECTIVITY

. Para. 1.A. Operator AIB, aircraft MSN 0796, 0797 and 0810 

Aircraft MSN 0643, 0646 and 0651 deleted for operator SAA

0668 deleted for operator THT. NOTE added.

— REASON

. Para. 1.C. Text modified.
DATE : Sep 22/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Mar 03/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

MATERIAL INFORMATION :

— MATERIAL - PRICE AND AVAILABILITY

. Para. 2.A. Sentence modified.

— INDUSTRIAL SUPPORT

. Para. 2.B. Sentence modified.

— LIST OF MATERIALS - OPERATOR SUPPLIED

. Para. 2.D.(1) PN NAS1611-011A, NAS1611-012A, NAS1611-013A 

NAS1611-112A added.

ACCOMPLISHMENT INSTRUCTIONS :

— Preparation

. Para. 3.A.(1) NOTE modified.

— REPAIR

. Para. 3.C. PN NAS1611-011A, NAS1611-012A, NAS1611-013A an

added.

— TESTS

. Para. 3.D. NOTE modified.

APPENDIX 1 :

— Text modified.

FILING INSTRUCTIONS

This Service Bulletin has been generated electronically and is 

complete document. Replace the complete document.

Put this Revision Transmittal Sheet in front of the Service B

HISTORY OF PREVIOUS REVISIONS

No previous revisions.

2
DATE : Sep 22/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Mar 03/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

3
5 DATE : Sep 22/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Mar 03/05 Page : 1 of 

Printed in FRANCE © AIRBUS, 2005 All rights reserved

This summary is for information only

and is not approved for modification of the aircraf

MANDATORY MANDATORY MAND

ATA SYSTEM : 27

TITLE : FLIGHT CONTROLS - ELEVATOR SERVOCONTROLS - INSPECTION AND 

THE SOLENOID VALVES O-RING SEALS.

MODIFICATION No. : None

REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES

Illustrated Parts Catalog (IPC) 27-34-51 Figure 1, applicable to 

servocontrols Part Number (PN) SC4800-2/-4/-7/-8 calls for instal

o-ring seals PN MS28775-XXX for items 130, 140 and 150, whereas I

Figure 1A applicable to elevator servocontrols PN SC 4800-7A/-9, 

installation of o-ring seals PN NAS1611-XXX.

The MS28775-XXX PNs are not qualified for phosphate ester based h

applications and must therefore not be used in elevator servocont

installation can lead to their complete degradation in a short ti

All elevator servocontrols delivered by GOODRICH actuation system

with the correct seals.

But, because the solenoid valves are Line Replaceable Units (LRUs

elevator servocontrols, the wrong o-ring seals MS28775-XXX might 

installed when performing the replacement of solenoid valves or se

aircraft or in shop.

This Service Bulletin requires within 1,400FH to :

— make sure checking in the maintenance and the results recorded i

data PN NAS1611-XXX or NAS1611-XXXA are installed on active and 

elevator servocontrols (FINs 2CS1, 2CS2, 3CS1, 3CS2),

— replace them when there is no evidence that the correct seals a

Accomplishment of this Service Bulletin will ensure that correct 

installed on all A340 aircraft elevator servocontrols.
DATE : Sep 22/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Mar 03/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

EFFECTIVITY

This Service Bulletin is applicable to these operators :

39Z 50Z ACA AFR AJM ALK ARG AUA B3R BUB BWA CAL CES CPA CRX CXN D

KAC LAN M3R MAU MSR OAL PAL QAF R3L RJA SAA SAS TAP THT THY UAE V

CONCURRENT REQUIREMENTS

None

REFERENCES/REPERCUSSIONS

TFU : 27.34.00.012

OEB : None

AOT : None

SIL : None

LIFE LIMIT : None

LINE MAINTENANCE AFFECTED : No

OTHERS : None

NATURE OF THE WORK

AIRCRAFT : NO

EQUIPMENT : YES

HARD : NO

SOFT : NO

OBRM : NO

MANPOWER

INSPECTION

REPAIR

COST SAVING No LROPS AFFECTED 

STRUCTURAL LIFE EXTN No VENDOR SB INVOLVED 

KIT PRICE (USD) No Kit

TOTAL MANHOURS 

ELAPSED TIME (HOURS) 

2
DATE : Sep 22/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Mar 03/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

Seals

APPENDICES

Refer to Appendix 01 : Inspection report.

3
DATE : Sep 22/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Mar 03/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

4
5 DATE : Sep 22/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Mar 03/05 Page : 1 of 

Printed in FRANCE © AIRBUS, 2005 All rights reserved

MANDATORY MANDATORY MAND

ATA SYSTEM : 27

TITLE : FLIGHT CONTROLS - ELEVATOR SERVOCONTROLS - INSPECTION AND 

THE SOLENOID VALVES O-RING SEALS.

MODIFICATION No. : None

This document contains AIRBUS PROPRIETARY INFORMATION and shall a

remain the property of AIRBUS; no intellectual property right or 

granted by AIRBUS in connection with any information contained in 

delivered on the express condition that said document and the inf

contained in it shall be treated as confidential, shall not be us

purpose other than that for which it is hereby delivered. It shal

disclosed in whole or in part to third parties and shall not be d

any manner (except for the purposes of performing the tasks descr

and provided that any recipient of such document shall comply wit

conditions herein), without AIRBUS' prior written consent.

1. PLANNING INFORMATION

A. EFFECTIVITY

(1) Models

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

(2) Aircraft

(a) Effectivity by MSN

The Operator/MSN relationship is provided for in

and is correct at the time of issue in accordan

information available to AIRBUS. Any future cha

from transfer of an aircraft from one operator t

not be reflected in this list unless the Service 

revised for another reason.

0002-0009 0011 0013-0016 0018-0029 0031-0035 00

0044 0046-0049 0051-0053 0056-0058 0061 0063 00

0078-0081 0084 0085 0088-0091 0093 0094 0097 010

0114 0115 0117 0123 0125 0126 0128 0129 0131 01

0141 0142 0145-0147 0149-0152 0154 0156-0161 01

0166-0170 0173-0176 0178-0180 0182 0185-0187 019

0196 0197 0199 0201 0202 0204 0207 0208 0210 02
DATE : Sep 22/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Mar 03/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

(b) Effectivity by Operator

The Operator/MSN relationship is provided for in

and is correct at the time of issue in accordan

information available to AIRBUS. Any future cha

from transfer of an aircraft from one operator t

not be reflected in this list unless the Service 

revised for another reason.

OPERATOR MSN

39Z 0151

50Z 0009

ACA 0088 0150 0154 0167 0170 0175 0179 0

AFR 0005 0007 0029 0049 0078 0084 0168 0

0210 0237 0245 0246 0260 0289 0307 0

0377 0399

AJM 0048 0216 0257

ALK 0032 0033 0034 0367 0374

ARG 0063 0074 0080 0085

AUA 0075 0081 0169 0263

B3R 0046 0204

BUB 0031

BWA 0016 0093

CAL 0402 0406 0411 0415 0433 0528 0541

CES 0129 0131 0141 0161 0182

CPA 0123 0126 0128 0136 0137 0142 0147 0

0218 0220 0227 0228 0381

CRX 0538 0545 0546 0556 0559 0561 0562 0

CXN 0192 0199 0201 0242 0243 0264

DLH 0020 0024 0027 0028 0035 0047 0051 0

0135 0158 0213 0233 0252 0274 0297 0

0327 0335 0347 0352 0354 0355 0379 0

ETD 0117

GFA 0039 0040 0097 0103 0133 0212 0215 0

IBE 0125 0134 0145 0146 0193 0197 0217 0

0329 0332 0378 0387 0414 0459 0474 0

2
DATE : Sep 22/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Mar 03/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

(c) Effectivity by MSN and Kit/Configuration

No AIRBUS kit is required for the accomplishment 

Service Bulletin.

(3) Spares

Servo-control SC4800-2

or

Servo-control SC4800-4

or

Servo-control SC4800-7

or

Servo-control SC4800-7A

or

Servo-control SC4800-8

or

Servo-control SC4800-9

MSR 0156 0159 0178

OAL 0235 0239 0280 0292

PAL 0173 0176 0187 0196

QAF 0026

R3L 0004

RJA 0014 0022 0038 0043

SAA 0006 0008 0011 0018 0019 0021 0544 0

SAS 0413 0424 0430 0435 0450 0467 0470

TAP 0041 0044 0079 0091

THT 0385 0395 0438 0446

THY 0023 0025 0057 0115 0180 0270 0331

UAE 0139 0149 0163 0166 0185 0190 0202 0

VIR 0002 0003 0013 0015 0058 0114 0164 0

3
DATE : Sep 22/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Mar 03/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

B. CONCURRENT REQUIREMENTS

None

C. REASON

(1) History

Illustrated Parts Catalog (IPC) 27-34-51 Figure 1, a

elevator servocontrols Part Number (PN) SC4800-2/-4/-

installation of o-ring seals PN MS28775-XXX for item

150, whereas IPC 27-34-51 Figure 1A applicable to el

servocontrols PN SC 4800-7A/-9, calls for installatio

seals PN NAS1611-XXX.

The MS28775-XXX PNs are not qualified for phosphate 

hydraulic fluid applications and must therefore not 

elevator servocontrols. Their installation can lead t

complete degradation in a short time.

All elevator servocontrols delivered by GOODRICH act

are fitted with the correct seals.

But, because the solenoid valves are Line Replaceabl

on the elevator servocontrols, the wrong o-ring seal

might have been installed when performing the replac

solenoid valves or seals change, on aircraft or in s

(2) Objective/Action

This Service Bulletin requires within 1,400FH to :

— make sure checking in the maintenance and the resul

the aircraft data PN NAS1611-XXX or NAS1611-XXXA ar

active and damping elevator servocontrols (FINs 2CS

3CS2),

— replace them when there is no evidence that the cor

installed.

Accomplishment of this Service Bulletin will ensure t

seals are installed on all A340 aircraft elevator se

(3) Advantages

Accomplishment of this Service Bulletin will ensure t

seals are installed on all A340 aircraft elevator se

4
DATE : Sep 22/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Mar 03/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

(1) Make sure that the correct o-ring seals are installed 

solenoid valves of the elevator servocontrols PN SC4

2CS2, 3CS1 and 3CS2 (refer to the maintenance and th

recorded in the aircraft data).

(2) In accordance with the results of the inspection, re

o-ring seals of the solenoid valves of the elevator 

PN SC4800 FINs 2CS1, 2CS2, 3CS1 and 3CS2.

E. COMPLIANCE

(1) Classification

Mandatory

(2) Accomplishment Timescale

Accomplishment of this Service Bulletin is required w

after receipt of this Service Bulletin.

European Aviation Safety Agency (EASA) regulatory act

expected for this Service Bulletin by the issue of a 

Navigabilite (CN) (Airworthiness Directive (AD)). It 

that the CN will confirm the thresholds given above 

should be made to the CN for confirmation of the mand

accomplishment timescale.

F. APPROVAL

Approved under EASA Design Organisation Approval No. EASA

If an aircraft listed in the effectivity has a modificatio

embodied that is not of AIRBUS origin, and which affects 

this Service Bulletin, the operator is responsible for ob

approval by its airworthiness authority for any adaptatio

before incorporation of the Service Bulletin.

G. MANPOWER

The manpower estimates given in this Service Bulletin are 

direct labor cost to do the work. These estimates assume 

will be done by experienced personnel, and may need to be 

upwards to suit operator's circumstances. The estimates do 

the time to prepare, plan or inspect the work. Manufactur

procurement of parts and tools, drying times for paints, 

and general administration work are also not included.

5
DATE : Sep 22/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Mar 03/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

REPAIR

H. WEIGHT AND BALANCE

Not changed

I. ELECTRICAL LOAD DATA

Not changed

J. REFERENCES

Appendix 1

K. PUBLICATIONS AFFECTED

L. INTERCHANGEABILITY/MIXABILITY

Not applicable

Get access 

Replacement of the o-ring

seals

Test 

Close-up 

TOTAL MANHOURS 

ELAPSED TIME (HOURS) 

Aircraft Maintenance Manual (AMM) : 06-41-55 12-34-24 

27-34-51 27-96-00

Consumable Material List (CML)

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

Illustrated Parts Catalog (IPC) : 27-34-51

6
DATE : Sep 22/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Mar 03/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

HONEYWELL INC

5575 WAYZATA BLVD

PO BOX 889

MINNEAPOLIS, MN 55440

USA

(2) Price and Availability

Sales terms for the equipment must be negotiated with 

vendor (See MATERIAL INFORMATION).

B. INDUSTRY SUPPORT INFORMATION

Refer to paragraph 2.A.(2): Price and Availability.

For those aircraft with finding (the incorrect seal refer

to inspection as per this Service Bulletin, AIRBUS will c

manhours for the correction at the operator's agreed in-ho

labor rate upon receipt of a warranty claim.

C. LIST OF COMPONENTS

None

D. LIST OF MATERIALS — OPERATOR SUPPLIED

(1) Consumable Materials

NOTE (01) The operators must get it from :

DESCRIPTION REFERENCE TO CML

MAT. No.

QTY PER A/C 

Solvent General Purpose 11-026 As required

Seal NAS1611-011 None 8 

Seal NAS1611-011A None 8 

Seal NAS1611-012 None 8 

Seal NAS1611-012A None 8 

Seal NAS1611-013 None 8 

Seal NAS1611-013A None 8 

Seal NAS1611-112 None 8 

Seal NAS1611-112A None 8 

7
DATE : Sep 22/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Mar 03/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

None

E. PARTS TO BE RE—IDENTIFIED BY THE OPERATOR

None

F. TOOLING — PRICE AND AVAILABILITY

None

G. SPECIAL TOOLS

None

8
DATE : Sep 22/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Mar 03/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY 

MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENAN

REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICA

COMPONENTS AND THE WORK AREA AS CLEAN AS POSSIB

:

— PUT PROTECTION, SUCH AS PLASTIC SHEETING, CLOT

NECESSARY ON WIRING AND COMPONENTS.

— REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATER

CONTAMINATION.

THESE PRECAUTIONS WILL DECREASE THE RISK OF CONT

DAMAGE TO THE ELECTRICAL WIRING INSTALLATION.

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

(1) Preparation

(a) For the inspection :

1 None

(b) For the repair :

1 Make sure that the aircraft is grounded (Refe

12-34-24 Page block 201).

2 Put the access platform(s) in position.

3 Open the Trailing Edge access panels 334CB, 

344CB, 344DB and 344BB (Refer to AMM 06-41-5

001).

4 Open, safety and tag these circuit breakers 

PANEL DESIGNATION FIN LOCA

721VU FCPC3 STBY COM 7CE6 20 R

721VU FCPC3 STBY MON 7CE5 19 R

722VU FCSC 2 10CE2 37 T

722VU FCSC 2 10CE2 39 T

722VU FCPC 3 7CE3 42 V

722VU FCPC 2 NORM 7CE2 41 V

722VU FCPC 3 7CE4 38 V

9
DATE : Sep 22/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Mar 03/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

NOTE : Open, safety and tag the circuit brea

and 7CE5 only if installed.

(2) Standard Practices

(a) For the inspection :

1 None

(b) For the repair :

1 For the specification of the material number

refer to the CML.

2 Clean the surfaces with Solvent General Purpo

11-026) .

B. INSPECTION

(1) Make sure that the correct o-ring seals are installed 

solenoid valves of the elevator servocontrols PN SC4

2CS2, 3CS1 and 3CS2, Refer to figure 2 .

NOTE : For the location of the solenoid valves, Refe

(2) For the inspection report, Refer to Appendix 01 .

C. REPAIR

(1) In accordance with the results of the inspection, re

o-ring seals of the solenoid valves of the elevator 

PN SC4800, FINs 2CS1, 2CS2, 3CS1 and 3CS2.

Refer to figure 3

(a) Remove the solenoid valves of the elevator servo

(Refer to AMM 27-34-51 Page block 401).

(b) Remove :

Refer to figure 3

742VU FCSC 1 STBY 9CE 75 G

742VU FCSC 1 STBY 9CE 77 G

742VU FCPC 1 STBY 11CE 67 K

742VU FCPC 1 STBY 11CE 69 K

10
DATE : Sep 22/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Mar 03/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

Refer to figure 3

1 Install the Seal NAS1611-011 Item 130 or the 

NAS1611-011A Item 130.

2 Install the Seal NAS1611-012 Item 140 or the 

NAS1611-012A Item 140.

3 Install the Seal NAS1611-013 Item 150 or the 

NAS1611-013A Item 150.

4 Install the Seal NAS1611-112 Item 80 or the 

NAS1611-112A Item 80.

(d) Install the solenoid valves of the elevator serv

(Refer to AMM 27-34-51 Page block 401).

D. TEST

(1) For the inspection :

(a) None

(2) For the repair :

(a) Remove the safety clips and tags and close these 

breakers :

PANEL DESIGNATION FIN LOCA

721VU FCPC3 STBY COM 7CE6 20 R

721VU FCPC3 STBY MON 7CE5 19 R

722VU FCSC 2 10CE2 37 T

722VU FCSC 2 10CE2 39 T

722VU FCPC 3 7CE3 42 V

722VU FCPC 2 NORM 7CE2 41 V

722VU FCPC 3 7CE4 38 V

742VU FCSC 1 NORM 10CE1 67 C

742VU FCSC 1 NORM 10CE1 70 C

742VU FCPC 1 NORM 7CE1 66 C

742VU FCPC 1 NORM 7CE1 69 C

742VU FCSC2 STBY SPLY 41CE 66 D

11
DATE : Sep 22/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Mar 03/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

NOTE : Remove the safety clips and tags and clo

circuit breakers FINs 7CE6 and 7CE5 only 

(b) Do an operational test of the elevator servocont

hydraulic actuation (Refer to AMM 27-34-00 Page 

(c) Do an operational test of the Flight Control Pri

(FCPCs) and the Flight Control Secondary Compute

standby servo loops on pitch control (Refer to A

Page block 501).

E. CLOSE UP

(1) For the inspection

(a) None

(2) For the repair :

(a) Make sure that the work areas are clean and clea

other items of equipment.

(b) Close the Trailing Edge access panels 334CB, 334

344CB, 344DB and 344BB (Refer to AMM 06-41-55 Pa

(c) Remove the access platform(s).

(d) Restore the systems and the aircraft to normal o

condition.

F. DOCUMENTATION

Write in the applicable aircraft records that you have don

given in the Service Bulletin.

12
DATE : Sep 22/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Mar 03/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

Figure 1 Sheet 1

Area to be Inspected

13
DATE : Sep 22/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Mar 03/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

Figure 2 Sheet 1

Flow Chart

14
DATE : Sep 22/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Mar 03/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

Figure 3 Sheet 1

Removal/Installation of the O-Ring Seals of the Solenoid 

15
5 DATE : Sep 22/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Mar 03/05 Page : 1 of 

Printed in FRANCE © AIRBUS, 2005 All rights reserved
DATE : Sep 22/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Mar 03/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

Figure 1 Sheet 1

Inspection Report

2
5 DATE : Sep 22/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Mar 03/05 Page : 1 of 

Printed in FRANCE © AIRBUS, 2005 All rights reserved

A - SB WILL BE embodied............. YES/NO (if NO p

If YES, aircraft concerned (as per SB effectivity by default) and 

(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 th

information is needed prior to next normal revision or prior to S

please indicate required service(s):

Either: Advance Data..................... YE

Or : Intermediate/Temporary revision............ YE

Important Information: This SB will only be incorporated in your m

operational documentation if this sheet is returned to Airbus and 

duly authorised representative. With the next feasible revision, 

result in

- updating of maintenance documentation to show pre and post S

- updating of maintenance and operational documentation to show 

after embodiment.

If this SB requires previous or simultaneous accomplishment of ot

Airbus shall automatically include them in the manual revisions. 

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

 or via your Resident Customer Support Office.

 Alternatively, SB lists via letters or fax are also accepted.
5 DATE : Sep 22/04 SERVICE BULLETIN No. : A340

REVISION No. : 01 — Mar 03/05 Page : 1 of 

Printed in FRANCE © AIRBUS, 2005 All rights reserved

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

- Quality rating of this SB 

- Quality rating of the Accomplishment Instructions 

- Quality rating of the Illustrations 

- Is this SB easy to understand ? 

If you have had difficulties in the accomplishment of this SB plea

the area(s) and give a short description of the issue.

Planning Material Instruct

X Effectivity X Kit content X Preparat

X Reason X List of Materials X Mod/Insp

X Manpower Operator Supplied X Test

X References X Re-identification X Close-Up

X Publication X Tooling X Illustra

Comments :

Operator : Date:

Name/Title :

Please return this form to :

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC

Attn : SET1 Service Bulletins Management

FAX : (33) 5 61 93 42 51

Or via your Resident Customer Support Office.