5 DATE : Jan 12/06 SERVICE BULLETIN No. : A330

REVISION No. : 01 — Jul 19/06 Page : 1 of 

Printed in FRANCE © AIRBUS, 2006 All rights reserved

MANDATORY MANDATORY MAND

ATA SYSTEM : 27

TITLE : FLIGHT CONTROLS - ELEVATOR AND HYDRAULIC ACTUATION-INSTAL

SERVOCONTROL.

MODIFICATION No. : 54830S18488 54831S18489 54832S18490 54833S1849

This page transmits Revision No. 01 of Service Bulletin No. A330-

ADDITIONAL WORK

No additional work is required by this revision for aircraft m

previous issue.

REASON

This revision is issued to modify the effectivity.

CHANGES

SUMMARY :

— EFFECTIVITY

. Operator CES added. Operators updated.

PLANNING INFORMATION :

— EFFECTIVITY

. Para 1.A. Operator CES, aircraft MSN 713, 720, 728, and 7

aircraft MSN 708 added for operator AAR, aircraft MSN 714 

for operator CAL, aircraft MSN 717 added for operator ETD

716 added for operator HDA, aircraft MSN 709 and 726 adde

MSR, aircraft MSN 718 and 722 added for operator NWA, air

added for operator QFA, aircraft MSN 711 and 721 added fo

and aircraft MSN 704 added for operator THY. Effectivity 

ACCOMPLISHMENT INSTRUCTIONS :

— Preparation

. Para 3.A.(1) Text modified.
DATE : Jan 12/06 SERVICE BULLETIN No. : A330

REVISION No. : 01 — Jul 19/06 Page :

Printed in FRANCE © AIRBUS, 2006 All rights reserved

Put this Revision Transmittal Sheet in front of the Service B

HISTORY OF PREVIOUS REVISIONS

No previous revisions.

REVISION SEQUENCE

ORIGINAL : Jan 12/06

REVISION No. : 01 — Jul 19/06

2
5 DATE : Jan 12/06 SERVICE BULLETIN No. : A330

REVISION No. : 01 — Jul 19/06 Page : 1 of 

Printed in FRANCE © AIRBUS, 2006 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 AND HYDRAULIC ACTUATION-INSTAL

SERVOCONTROL.

MODIFICATION No. : 54830S18488 54831S18489 54832S18490 54833S1849

REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES

One operator reported several elevator servocontrols removals on 

aircraft. Following the shop repairs, GOODRICH noticed that most 

servocontrols were affected by the same anomaly, that is guide It

Illustrated Parts List (IPL) of the Component Maintenance Manual 

Figure 2, found broken. A review of the previous repairs performe

GOODRICH revealed that 10% of the servocontrols returned for repa

with the same broken guide.

The broken guides occurred on servocontrols removed from an activ

(left GREEN FIN 2CS1, right GREEN FIN 2CS2). Most of these remova

from messages focusing on the "MODE XDCR". Thus, it is suspected t

guide may affect the operation of the mode selector spool valve, 

the inability for the affected servocontrols to change their oper

(Active/Damping).

The root cause of the broken guides is an insufficient design rob

these guides. Consequently, the successive pressure cycles inside 

servocontrol result in cases of fatigue rupture. During the inves

was also noticed that the successive pressure cycles could result 

progressive decrease of the tightening torque of the plug Item 38

the CMM 27-34-51 Figure 2.

This Service Bulletin is published to advise all operators of A33

the issue of GOODRICH Service Bulletin No. SC4800-27-18.

This Service Bulletin requires modifying the affected servocontro

a new plug-guide assembly.

NOTE : If the existing guide is found broken, the elevator servoco

replaced.
DATE : Jan 12/06 SERVICE BULLETIN No. : A330

REVISION No. : 01 — Jul 19/06 Page :

Printed in FRANCE © AIRBUS, 2006 All rights reserved

As per EASA IR 21, a minor change is one that has no appreciable 

mass, balance, structural strength, reliability, operational char

affecting the airworthiness of the product. All other changes are 

EFFECTIVITY

This Service Bulletin is applicable to these operators :

AAR ACA ACI AFR ALK AUA BMA CAL CES CPA CRL CSN CYP DAH DAT DLH D

ETD EVA FWI GFA GIA GRL HDA IWD IYE KAL KLM LTU LVG LXR MAS MEA MO

NWA PAL QAF QFA QTR SAS SEU SSV SWR TAM TAP TCX THA THY TSC UAE U

CONCURRENT REQUIREMENTS

Accomplishment of this Service Bulletin requires the simultaneous 

of the following Service Bulletin(s) or the equivalent production

modification(s):

Service Bulletin No. A330-27-3134 Mod. No. 53969S18340

Mod. No. 53976S18343

Mod. No. 53977S18344

Mod. No. 53978S18345

Service Bulletin No. A330-27-3128 Mod. No. 52947S18075

Mod. No. 53386S18200

REFERENCES/REPERCUSSIONS

TFU : 27.34.00.014

OEB : None

COMPLIANCE Mandatory CANCELS INSPECTION S

AD Yes A/C OPERATION AFFECT

RELIABILITY AFFECTED No PAX COMFORT AFFECTED 

COST SAVING No ETOPS AFFECTED 

STRUCTURAL LIFE EXTN No VENDOR SB INVOLVED 

KIT PRICE No Kit

MODIFICATION CLASSIFICATION

MAJOR 54830S18488 54831S18489 54832S18490 54833S1849

MINOR None

2
DATE : Jan 12/06 SERVICE BULLETIN No. : A330

REVISION No. : 01 — Jul 19/06 Page :

Printed in FRANCE © AIRBUS, 2006 All rights reserved

AIRCRAFT : NO

EQUIPMENT : YES

HARD : NO

SOFT : NO

OBRM : NO

MANPOWER

Config. 01

Config. 01 On bench

MATERIAL INFORMATION

AIRCRAFT DATA

None

APPENDICES

None

TOTAL MANHOURS 

ELAPSED TIME (HOURS) 

TOTAL MANHOURS Refer to GOODRICH Service Bulleti

SC4800-27-18

ELAPSED TIME (HOURS) Refer to GOODRICH Service Bulleti

SC4800-27-18

3
5 DATE : Jan 12/06 SERVICE BULLETIN No. : A330

REVISION No. : 01 — Jul 19/06 Page : 1 of 

Printed in FRANCE © AIRBUS, 2006 All rights reserved

MANDATORY MANDATORY MAND

ATA SYSTEM : 27

TITLE : FLIGHT CONTROLS - ELEVATOR AND HYDRAULIC ACTUATION-INSTAL

SERVOCONTROL.

MODIFICATION No. : 54830S18488 54831S18489 54832S18490 54833S1849

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

330-201 330-202 330-203 330-223 330-243 330-301 330-

330-321 330-322 330-323 330-341 330-342 330-343

(2) Aircraft

(a) Effectivity by MSN

This Service Bulletin is applicable to aircraft 

0012 0017 0030 0037 0045 0050 0054 0055 0059 00

0064-0067 0069-0073 0077 0082 0083 0086 0087 009

0098-0100 0102 0106 0107 0109-0113 0116 0118-01

0138 0140 0143 0144 0148 0153 0155 0162 0165 01

0181 0183 0184 0188 0189 0191 0195 0198 0200 020

0209 0211 0219 0222-0224 0226 0229-0232 0234 02

0244 0247-0251 0253-0256 0258 0259 0261 0262 02

0271 0272 0275-0277 0279 0281 0283-0288 0290 029

0299-0301 0303 0305 0306 0308 0309 0311-0317 03

0326 0328 0330 0333 0334 0337-0340 0342-0346 034

0356-0358 0361 0362 0364-0366 0368-0370 0372 03
DATE : Jan 12/06 SERVICE BULLETIN No. : A330

REVISION No. : 01 — Jul 19/06 Page :

Printed in FRANCE © AIRBUS, 2006 All rights reserved

0605 0607 0609 0610 0612 0614 0616 0618 0620 06

0627 0629 0631-0638 0640-0642 0644 0645 0647-06

0669-0671 0673-0676 0678-0680 0682-0684 0686-06

0695-0697 0699-0701 0703-0705 0707-0709 0711-07

0720-0722 0725 0726 0728 0732

(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

AAR 0640 0676 0708

ACA 0277 0279 0284 0344 0400 0408 0412 0

ACI 0507 0510

AFR 0422 0443 0448 0458 0465 0481 0498 0

0516 0519 0567 0584 0657 0660

ALK 0303 0306 0311 0313

AUA 0181 0195 0223 0317

BMA 0398 0401 0404

CAL 0602 0607 0641 0671 0675 0691 0699 0

CES 0713 0720 0728 0732

CPA 0012 0017 0071 0083 0099 0102 0109 0

0155 0244 0386 0389 0393 0418 0420 0

0539 0548 0565 0669 0673 0679

CRL 0285 0320

CSN 0649 0652 0656 0664

CYP 0505 0526

DAH 0644 0647 0650 0653 0667

DAT 0030 0037 0045

DLH 0322 0324 0570 0576 0579 0629 0636 0

0687 0701

DRD 0054 0082 0205 0211 0362

EDW 0369

2
DATE : Jan 12/06 SERVICE BULLETIN No. : A330

REVISION No. : 01 — Jul 19/06 Page :

Printed in FRANCE © AIRBUS, 2006 All rights reserved

FWI 0240 0253

GFA 0276 0281 0286 0287 0334 0340

GIA 0138 0140 0144 0148 0153 0165

GRL 0230

HDA 0098 0106 0132 0177 0234 0405 0407 0

0654 0662 0692 0716

IWD 0072 0461 0670

IYE 0625 0632

KAL 0162 0172 0206 0219 0222 0226 0241 0

0338 0350 0351 0368 0425 0428 0484 0

KLM 0682 0686 0703

LTU 0120 0127 0171 0403 0432 0444 0454 0

LVG 0551 0597 0627

LXR 0087 0096

MAS 0067 0069 0073 0077 0095 0100 0107 0

0143 0255 0262 0290 0296 0300

MEA 0527 0529 0532

MON 0261 0265

MSR 0600 0610 0666 0683 0696 0709 0726

MYT 0254 0266 0301 0309

NVR 0353

NWA 0524 0533 0542 0549 0552 0578 0588 0

0618 0620 0621 0631 0633 0663 0674 0

PAL 0183 0184 0188 0189 0191 0198 0200 0

QAF 0487 0605

QFA 0506 0508 0513 0522 0553 0558 0564 0

0603 0695 0705 0712

QTR 0441 0463 0473 0489 0504 0511 0521 0

0623 0637 0638 0659 0680 0684 0711 0

SAS 0496 0497 0515 0568

SEU 0501 0635

SSV 0357

SWR 0229 0249 0275 0288 0291 0294 0299 0

TAM 0238 0247 0466 0472 0477 0486 0700

TAP 0305 0308 0312

3
DATE : Jan 12/06 SERVICE BULLETIN No. : A330

REVISION No. : 01 — Jul 19/06 Page :

Printed in FRANCE © AIRBUS, 2006 All rights reserved

(c) Effectivity by MSN and Kit/Configuration

The kits and configurations applicable to these 

at the end of this list:

0012 0017 0030 0037 0045 0050 0054-0055 0059-00

0064-0067 0069-0073 0077 0082-0083 0086-0087 009

0098-0100 0102 0106-0107 0109-0113 0116 0118-01

0138 0140 0143-0144 0148 0153 0155 0162 0165 01

0181 0183-0184 0188-0189 0191 0195 0198 0200 020

0209 0211 0219 0222-0224 0226 0229-0232 0234 02

0244 0247-0251 0253-0256 0258-0259 0261-0262 02

0271-0272 0275-0277 0279 0281 0283-0288 0290-029

0299-0301 0303 0305-0306 0308-0309 0311-0317 03

0326 0328 0330 0333-0334 0337-0340 0342-0346 034

0356-0358 0361-0362 0364-0366 0368-0370 0372 03

0384 0386 0388-0389 0392-0393 0396-0398 0400-040

0407-0409 0412 0418-0423 0425 0427-0428 0432 04

0443-0444 0448 0451-0452 0454-0456 0458 0461-04

0469 0472-0473 0476-0477 0479-0481 0484 0486-04

0493-0494 0496-0498 0500-0513 0515-0516 0518-05

0524-0527 0529-0530 0532-0533 0535-0536 0539 054

0555 0558 0564-0565 0567-0568 0570-0571 0573-05

0578-0579 0581 0584 0587-0588 0591 0593 0595 059

0602-0603 0605 0607 0609-0610 0612 0614 0616 06

0623 0625 0627 0629 0631-0638 0640-0642 0644-064

0652-0667 0669-0671 0673-0676 0678-0680 0682-06

0690-0693 0695-0697 0699-0701 0703-0705 0707-070

0716-0718 0720-0722 0725-0726 0728 0732

NOTE : Config. 01 is valid for all the aircraft 

effectivity.

TSC 0111 0250 0271 0480

UAE 0248 0251 0283 0293 0295 0314 0316 0

0348 0365 0372 0382 0384 0392 0396 0

0452 0455 0462 0491 0494 0509 0518 0

USA 0315 0323 0333 0337 0342 0370 0375 0

VKG 0349 0356

KIT No. QTY PER A/C CONFIGURATION

01

4
DATE : Jan 12/06 SERVICE BULLETIN No. : A330

REVISION No. : 01 — Jul 19/06 Page :

Printed in FRANCE © AIRBUS, 2006 All rights reserved

Accomplishment of this Service Bulletin requires the simu

accomplishment of the following Service Bulletin(s) or th

production modification(s):

Service Bulletin No. A330-27-3134 Mod. No. 53969S18340

Mod. No. 53976S18343

Mod. No. 53977S18344

Mod. No. 53978S18345

Service Bulletin No. A330-27-3128 Mod. No. 52947S18075

Mod. No. 53386S18200

C. REASON

(1) History

One operator reported several elevator servocontrols 

different aircraft. Following the shop repairs, GOOD

that most of these servocontrols were affected by the 

that is guide Item 450 from Illustrated Parts List (

Component Maintenance Manual (CMM) 27-35-51 Figure 2, 

A review of the previous repairs performed in 2004 by 

revealed that 10% of the servocontrols returned for 

found with the same broken guide.

The broken guides occurred on servocontrols removed 

position (left GREEN FIN 2CS1, right GREEN FIN 2CS2). 

removals resulted from messages focusing on the "MOD

it is suspected that the broken guide may affect the 

the mode selector spool valve, resulting in the inab

affected servocontrols to change their operating mod

(Active/Damping).

The root cause of the broken guides is an insufficie

robustness of these guides. Consequently, the succes

cycles inside the servocontrol result in cases of fat

During the investigations, it was also noticed that t

pressure cycles could result in a progressive decrea

tightening torque of the plug Item 380 from IPL of th

Figure 2.

(2) Objective/Action

This Service Bulletin is published to advise all ope

aircraft of the issue of GOODRICH Service Bulletin No

SC4800-27-18.

5
DATE : Jan 12/06 SERVICE BULLETIN No. : A330

REVISION No. : 01 — Jul 19/06 Page :

Printed in FRANCE © AIRBUS, 2006 All rights reserved

Accomplishment of this Service Bulletin will restore 

servocontrol reliability and will cancel the periodi

requirements introduced by All Operator Telex (AOT) 

A330-27A3138 Rev 01.

(4) Operational/Maintenance Consequences

None

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

(1) Config. 01

(a) Modify the elevator servocontrols FINs 2CS1, 2C

3CS2.

E. COMPLIANCE

(1) Classification

Mandatory

(2) Accomplishment Timescale

Accomplishment of this Service Bulletin is expected t

mandatory by the issue of a Consigne de Navigabilite 

(Airworthiness Directive (AD)) published by the DGAC 

the European Aviation Safety Agency (EASA). The accom

timescale, which has not yet been defined, will be g

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 

6
DATE : Jan 12/06 SERVICE BULLETIN No. : A330

REVISION No. : 01 — Jul 19/06 Page :

Printed in FRANCE © AIRBUS, 2006 All rights reserved

Config. 01 On bench

H. WEIGHT AND BALANCE

Not changed

I. ELECTRICAL LOAD DATA

Not changed

J. REFERENCES

GOODRICH Service Bulletin No. SC4800-27-18

K. PUBLICATIONS AFFECTED

Removal of the elevator

servocontrol

Installation of elevator

servocontrol

Test 

Close-up 

TOTAL MANHOURS 

ELAPSED TIME (HOURS) 

Modification of the

servocontrols

TOTAL MANHOURS Refer to GOODRICH Se

Bulletin No. SC4800-

ELAPSED TIME (HOURS) Refer to GOODRICH Se

Bulletin No. SC4800-

Aircraft Maintenance Manual (AMM) : 12-34-24 27-34-00 

27-96-00

Consumable Material List (CML)

Component Maintenance Manual (CMM) : 27-34-51 27-35-51

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

Service Bulletin No. : A330-27-3128 A330

Illustrated Parts Catalog (IPC) : 27-34-07 27-34-51

7
DATE : Jan 12/06 SERVICE BULLETIN No. : A330

REVISION No. : 01 — Jul 19/06 Page :

Printed in FRANCE © AIRBUS, 2006 All rights reserved

NOTE : For definitions of interchangeability codes in col

to ATA Common Support Data Dictionnary (CSDD), Cha

NOTE (01) Authorized without specific configuration/condit

possible to mix old and new P/N on a same aircra

NOTE (02) Only the mixability configuration(s) and condit

in this Service Bulletin are approved.

servocontrol

Elevator

servocontrol

SC4800-103 SC4800-104 01 

Elevator

servocontrol

SC4800-113 SC4800-114 01 

8
DATE : Jan 12/06 SERVICE BULLETIN No. : A330

REVISION No. : 01 — Jul 19/06 Page :

Printed in FRANCE © AIRBUS, 2006 All rights reserved

For the organisation of this retrofit, operators are kindl

contact :

GOODRICH Actuation Systems

Etb. de St. Ouen l'Aumone, BP 7186

13, avenue de l'Eguillette

95056 CERGY POINTOISE

FRANCE

As per Vendor Service Bulletin No. SC4800-27-18.

As Service Bulletin No. A330-27-3136 must be done simulta

Service Bulletins No. A330-27-3128 and A330-27-3134, AIRB

one time the labor for removal/installation of the elevato

servo-control, by crediting the man-hours indicated in th

Bulletin No. A330-27-3136 at the operator's agreed in-hou

labor rate upon receipt of warranty claim.

C. LIST OF COMPONENTS

None

D. LIST OF MATERIALS — OPERATOR SUPPLIED

(1) Consumable Materials

NOTE : To accomplish this Service Bulletin it is nece

the expendable parts listed in the AMM 27-34-

401.

(2) Components

DESCRIPTION REFERENCE TO CML

MAT. No.

QTY PER A/C 

Solvent General Purpose 11-026 As required

ITEM NEW PART No. QTY UM KEYWORD ITEM OLD PART No. 

SC4800-74 4 SRVCNTRL SC4800-73 

SC4800-94 4 SRVCNTRL SC4800-93 

SC4800-104 4 SRVCNTRL SC4800-103 

SC4800-114 4 SRVCNTRL SC4800-113 

9
DATE : Jan 12/06 SERVICE BULLETIN No. : A330

REVISION No. : 01 — Jul 19/06 Page :

Printed in FRANCE © AIRBUS, 2006 All rights reserved

E. PARTS TO BE RE—IDENTIFIED BY THE OPERATOR

None

F. TOOLING — PRICE AND AVAILABILITY

To accomplish this Service Bulletin it is necessary to us

listed in AMM 27-34-51 Page block 401.

G. SPECIAL TOOLS

None

10
DATE : Jan 12/06 SERVICE BULLETIN No. : A330

REVISION No. : 01 — Jul 19/06 Page :

Printed in FRANCE © AIRBUS, 2006 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 POSSIBL

— 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 20-55-0

(1) Preparation

(a) Config. 01

1 Make sure that the aircraft is grounded (Refe

12-34-24 Page block 201).

2 Put the access platform(s) in position.

3 Do the preparation procedure as specified in 

removal/installation of the elevator servoco

2CS1, 2CS2, 3CS1, 3CS2 (Refer to AMM 27-34-5

401).

(2) Standard Practices

(a) For the specification of the material numbers (M

refer to the CML.

(b) Clean the surfaces to seal with Solvent General 

No. 11-026) .

B. MODIFICATION

(1) Config. 01

(a) Modify the elevator servocontrols FINs 2CS1, 2C

3CS2.

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

11
DATE : Jan 12/06 SERVICE BULLETIN No. : A330

REVISION No. : 01 — Jul 19/06 Page :

Printed in FRANCE © AIRBUS, 2006 All rights reserved

CAUTION : SINCE THIS MODIFICATION INDUCE A SIMUL

ON ALL THE SERVOCONTROLS AND ALL HYDRA

AIRBUS HIGHLY RECOMMEND THAT :

— THE INSTALLATION OF THE SERVOCONTRO

TWO TEAMS, EACH TEAM DEDICATED TO ON

— THE CORRECT INSTALLATION OF THE SERV

CHECKED BY A PERSON WHO DID NOT DO T

INSTALLATION.

THESE RECOMMENDATIONS COMPLY WITH THE 

1 Remove:

or

or

or

2 Install:

or

or

4 Elevator

servocontrol

SC4800-73

4 Elevator

servocontrol

SC4800-93

4 Elevator

servocontrol

SC4800-103

4 Elevator

servocontrol

SC4800-113

4 Elevator

servocontrol

SC4800-74

4 Elevator

servocontrol

SC4800-94

4 Elevator

servocontrol

SC4800-104

12
DATE : Jan 12/06 SERVICE BULLETIN No. : A330

REVISION No. : 01 — Jul 19/06 Page :

Printed in FRANCE © AIRBUS, 2006 All rights reserved

hydraulic leaks the MVT200, the soleno

the plug installed on the servocontrol 

modifications. Leaks are not permitted

NOTE : The check for leaks of the plug shall 

using a sight glass (plug installed on 

the servocontrol).

C. TEST

(1) Config. 01

(a) Do the test after removal/installation of the e

control units (Refer to AMM 27-34-51 Page block 

(b) Do the operational test of the elevator and hyd

actuation (Refer to AMM 27-34-00 Page block 501)

NOTE : Refer to the task 27-34-00-710-801.

(c) Do the operational test of the FCPCs and the FC

servo-loops on pitch control (Refer to AMM 27-96

501).

NOTE : Refer to the task 27-96-00-710-803.

D. CLOSE UP

(1) Config. 01

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

other items of equipment.

(b) Do the close-up procedure as specified in the

removal/installation of the elevator servocontro

2CS2, 3CS1, 3CS2 (Refer to AMM 27-34-51 Page blo

(c) Remove the access platform(s).

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

condition.

E. DOCUMENTATION

Write in the applicable aircraft records that you have don

given in the Service Bulletin.

13
5 DATE : Jan 12/06 SERVICE BULLETIN No. : A330

REVISION No. : 01 — Jul 19/06 Page : 1 of 

Printed in FRANCE © AIRBUS, 2006 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:

Either: Modification Operational Impact (MOI), if available. . YE

Or : Intermediate 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

 e-mail: sb.reporting@airbus.com

 or via your Resident Customer Support Office.

 Alternatively, SB lists via letters or fax are also accepted.
5 DATE : Jan 12/06 SERVICE BULLETIN No. : A330

REVISION No. : 01 — Jul 19/06 Page : 1 of 

Printed in FRANCE © AIRBUS, 2006 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 : SEM4 Service Bulletins Management

FAX : (33) 5 61 93 42 51

Or via your Resident Customer Support Office.