5 DATE : Oct 13/05 SERVICE BULLETIN No. : A330

REVISION No. : 01 — May 12/06 Page : 1 of 

Printed in FRANCE © AIRBUS, 2006 All rights reserved

ATA SYSTEM : 27

TITLE : FLIGHT CONTROLS - ELEVATOR AND HYDRAULIC ACTUATION - INTRO

SOLENOID VALVE SEALS ON A330/A340 SERVOCONTROLS.

MODIFICATION No. : 53969S18340 53976S18343 53977S18344 53978S1834

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

Revision No. 01 issued to add aircraft MSN 0708 for operator A

0709 for operator MSR.

CHANGES

SUMMARY :

— REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES

. Text modified.

— EFFECTIVITY

. Operators updated. Sentence updated.

— MANPOWER

. 7.0 hours become 8.0 hours for the TOTAL MANHOURS. 7.0 ho

hours for the ELAPSED TIME hours.

PLANNING INFORMATION :

— EFFECTIVITY

. Para. 1.A. Aircraft MSN 0708 added for operator AAR. Airc

added for operator MSR. Effectivity updated. NOTE updated

— REASON

. Para. 1.C. Text modified.
DATE : Oct 13/05 SERVICE BULLETIN No. : A330

REVISION No. : 01 — May 12/06 Page :

Printed in FRANCE © AIRBUS, 2006 All rights reserved

. Para. 1.J. Reference to AD F-2004-158 added.

ACCOMPLISHMENT INSTRUCTIONS :

— GENERAL

. Para. 3.A. Preparation procedure modified.

— TESTS

. Para. 3.C. Test procedure modified.

— CLOSE-UP

. Para. 3.D. Close-up procedure modified.

NOTE : Layout changes due to computerization of this revision 

identified.

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.

REVISION SEQUENCE

ORIGINAL : Oct 13/05

REVISION No. : 01 — May 12/06

2
5 DATE : Oct 13/05 SERVICE BULLETIN No. : A330

REVISION No. : 01 — May 12/06 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

ATA SYSTEM : 27

TITLE : FLIGHT CONTROLS - ELEVATOR AND HYDRAULIC ACTUATION - INTRO

SOLENOID VALVE SEALS ON A330/A340 SERVOCONTROLS.

MODIFICATION No. : 53969S18340 53976S18343 53977S18344 53978S1834

REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES

Further to some reported cases of extrusion and damage of the sol

external preformed packings, a new elevator servocontrol with new 

standard has been developed.

This Service Bulletin is published to advise all operators of A33

the issue of GOODRICH Service Bulletin No. SC4800-27-17.

This Service Bulletin recommends modifying the affected servocont

— P/N SC4800-72 modified into P/N SC4800-73,

— P/N SC4800-92 modified into P/N SC4800-93,

— P/N SC4800-10 modified into P/N SC4800-103,

— P/N SC4800-11 modified into P/N SC4800-113.

Accomplishment of this Service Bulletin will reinforce the pressu

strength of external packings of the solenoid valves and cancels 

introduced by the paragraph 3.1 of the Airworthiness Directive (A

EVALUATION TABLE

COMPLIANCE Recommended CANCELS INSPECTION S

POTENTIAL AD No A/C OPERATION AFFECT

RELIABILITY AFFECTED No PAX COMFORT AFFECTED 

COST SAVING No ETOPS AFFECTED 

STRUCTURAL LIFE EXTN No VENDOR SB INVOLVED 

KIT PRICE (USD) No Kit
DATE : Oct 13/05 SERVICE BULLETIN No. : A330

REVISION No. : 01 — May 12/06 Page :

Printed in FRANCE © AIRBUS, 2006 All rights reserved

s peS, a ocage s oe tat as o appecabe 

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 :

79X AAR ACA ACI AFR ALK AUA BMA CAL 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 SWR TAM TAP TCX THA THY TSC UAE USA V

The modification No. 53969S18340 is embodied before delivery on A

MSN 0711 and subsequent.

The modifications No. 53976S18343, 53977S18344 and 53978S18345 are 

Service Bulletin only.

CONCURRENT REQUIREMENTS

If elevator servocontrols PN SC4800-9 are installed on aircraft :

accomplishment of this Service Bulletin requires the prior or sim

accomplishment of the following Service Bulletin or the equivalen

modification:

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

If elevator servocontrols PN SC4800-7A are installed on aircraft 

accomplishment of this Service Bulletin requires the prior or sim

accomplishment of the following Service Bulletin or the equivalen

modification:

Service Bulletin No. A330-27-3128 Mod. No. 53386S18200

REFERENCES/REPERCUSSIONS

TFU : 27.34.00.010

OEB : 50, 54

AOT : None

SIL : None

LIFE LIMIT : None

LINE MAINTENANCE AFFECTED : No

OTHERS : AD F-2004-158

2
DATE : Oct 13/05 SERVICE BULLETIN No. : A330

REVISION No. : 01 — May 12/06 Page :

Printed in FRANCE © AIRBUS, 2006 All rights reserved

MANPOWER

Config. 01 , on aircraft, modification of the four elevator servo

2CS1, 2CS2, 3CS1 and 3CS2

Config. 01 , on aircraft, replacement of the four elevator servoc

2CS1, 2CS2, 3CS1 and 3CS2

Config. 01 , on bench

MATERIAL INFORMATION

AIRCRAFT DATA

None

APPENDICES

None

TOTAL MANHOURS 

ELAPSED TIME (HOURS) 

TOTAL MANHOURS 

ELAPSED TIME (HOURS) 

TOTAL MANHOURS Refer to GOODRICH Service Bulletin 

SC4800-27-17

ELAPSED TIME (HOURS) Refer to GOODRICH Service Bulletin 

SC4800-27-17

3
5 DATE : Oct 13/05 SERVICE BULLETIN No. : A330

REVISION No. : 01 — May 12/06 Page : 1 of 

Printed in FRANCE © AIRBUS, 2006 All rights reserved

ATA SYSTEM : 27

TITLE : FLIGHT CONTROLS - ELEVATOR AND HYDRAULIC ACTUATION - INTRO

SOLENOID VALVE SEALS ON A330/A340 SERVOCONTROLS.

MODIFICATION No. : 53969S18340 53976S18343 53977S18344 53978S1834

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

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
DATE : Oct 13/05 SERVICE BULLETIN No. : A330

REVISION No. : 01 — May 12/06 Page :

Printed in FRANCE © AIRBUS, 2006 All rights reserved

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

NOTE : The modification No. 53969S18340 is embod

delivery on A330 aircraft MSN 0711 and 

NOTE (01) The modifications No. 53976S18343, 539

53978S18345 are applicable by Service 

(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

79X 0305 0312

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

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 0205 0211 0362

2
DATE : Oct 13/05 SERVICE BULLETIN No. : A330

REVISION No. : 01 — May 12/06 Page :

Printed in FRANCE © AIRBUS, 2006 All rights reserved

EVA 0530 0535 0555 0573 0587 0634 0655 0

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

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 0082 0120 0127 0171 0403 0432 0444 0

0493

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

MYT 0254 0266 0301

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

QTR 0441 0463 0473 0489 0504 0511 0521 0

0623 0637 0638 0659 0680 0684

SAS 0496 0497 0515 0568

SEU 0501 0635

SWR 0229 0249 0275 0288 0291 0294 0299 0

TAM 0238 0247 0466 0472 0477 0486 0700

3
DATE : Oct 13/05 SERVICE BULLETIN No. : A330

REVISION No. : 01 — May 12/06 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

NOTE : Config. 01 is valid for all the aircraft 

effectivity of this Service Bulletin.

THY 0697 0704

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 0309 0349 0356 0357

KIT No. QTY PER A/C CONFIGURATION

01

4
DATE : Oct 13/05 SERVICE BULLETIN No. : A330

REVISION No. : 01 — May 12/06 Page :

Printed in FRANCE © AIRBUS, 2006 All rights reserved

accomplishment of this Service Bulletin requires the prio

simultaneous accomplishment of the following Service Bull

equivalent production modification:

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

If elevator servocontrols PN SC4800-7A are installed on a

accomplishment of this Service Bulletin requires the prio

simultaneous accomplishment of the following Service Bull

equivalent production modification:

Service Bulletin No. A330-27-3128 Mod. No. 53386S18200

C. REASON

(1) History

Further to some reported cases of extrusion and damag

solenoid valves external preformed packings, a new e

servocontrol with new capped seals standard has been 

(2) Objective/Action

This Service Bulletin is published to advise all ope

aircraft of the issue of GOODRICH Service Bulletin No

SC4800-27-17.

This Service Bulletin recommends modifying the affect

servocontrols :

— P/N SC4800-72 modified into P/N SC4800-73,

— P/N SC4800-92 modified into P/N SC4800-93,

— P/N SC4800-10 modified into P/N SC4800-103,

— P/N SC4800-11 modified into P/N SC4800-113.

(3) Advantages

Accomplishment of this Service Bulletin will reinforc

fatigue strength of external packings of the solenoid 

cancels the action introduced by the paragraph 3.1 o

Airworthiness Directive (AD) F-2004-158.

5
DATE : Oct 13/05 SERVICE BULLETIN No. : A330

REVISION No. : 01 — May 12/06 Page :

Printed in FRANCE © AIRBUS, 2006 All rights reserved

(1) Config. 01

NOTE : To accomplish this Service Bulletin you have t

possibilities :

— either you modify on aircraft the four eleva

servocontrols FINs 2CS1, 2CS2, 3CS1 and 3CS2

in ACCOMPLISHMENT INSTRUCTIONS paragraph B.

— or you modify on bench them as described in 

INSTRUCTIONS paragraph B.(1) (b) below.

NOTE (01) For the modification of the four elevator 

FINs 2CS1, 2CS2, 3CS1 and 3CS2, refer to GO

Service Bulletin No. SC4800-27-17 .

(a) In the trimmable horizontal stabilizer trailing 

on aircraft the four elevator servocontrols FIN

3CS1 and 3CS2 by replacement of the solenoid va

seals.

(b) Modify on bench the four elevator servocontrols 

2CS2, 3CS1 and 3CS2.

E. COMPLIANCE

(1) Classification

Recommended

(2) Accomplishment Timescale

Accomplishment of this Service Bulletin is recommend

earliest opportunity where manpower and facilities a

F. APPROVAL

Approved under the EASA Design Organization Approval No. 

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.

6
DATE : Oct 13/05 SERVICE BULLETIN No. : A330

REVISION No. : 01 — May 12/06 Page :

Printed in FRANCE © AIRBUS, 2006 All rights reserved

and general administration work are also not included.

Config. 01 , on aircraft, modification of the four elevato

servocontrols FINs 2CS1, 2CS2, 3CS1 and 3CS2

Config. 01 , on aircraft, replacement of the four elevator 

FINs 2CS1, 2CS2, 3CS1 and 3CS2

Config. 01 , on bench

H. WEIGHT AND BALANCE

Not changed

I. ELECTRICAL LOAD DATA

Not changed

Get access 

Modification of

servocontrols

Test 

Close-up 

TOTAL MANHOURS 

ELAPSED TIME (HOURS) 

Get access 

Removal/installation of

servocontrols

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-

7
DATE : Oct 13/05 SERVICE BULLETIN No. : A330

REVISION No. : 01 — May 12/06 Page :

Printed in FRANCE © AIRBUS, 2006 All rights reserved

GOODRICH Service Bulletin No. SC4800-27-17

Airworthiness Directive (AD) F-2004-158

K. PUBLICATIONS AFFECTED

L. INTERCHANGEABILITY/MIXABILITY

NOTE : For definitions of interchangeability codes in col

to ATA Common Support Data Dictionary (CSDD), Chapt

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.

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

DESCRIPTION OLD PART No. NEW PART No. INT M

Elevator

servocontrol

SC4800-72 SC4800-73 01 

Elevator

servocontrol

SC4800-92 SC4800-93 01 

Elevator

servocontrol

SC4800-10 SC4800-103 01 

Elevator

servocontrol

SC4800-11 SC4800-113 01 

8
DATE : Oct 13/05 SERVICE BULLETIN No. : A330

REVISION No. : 01 — May 12/06 Page :

Printed in FRANCE © AIRBUS, 2006 All rights reserved

SC4800-27-17.

(2) Price and Availability

Refer to the Vendor Service Bulletin No. SC4800-27-1

equipment modification sales terms.

B. INDUSTRY SUPPORT INFORMATION

Refer to the Vendor Service Bulletin (VSB) for the indust

terms.

C. LIST OF COMPONENTS

None

D. LIST OF MATERIALS — OPERATOR SUPPLIED

(1) Consumable Materials

None

(2) Components

NOTE : For definitions of interchangeability codes i

refer to ATA Common Support Data Dictionary (C

2.

NOTE (01) Modification of removed equipment should be 

directly with GOODRICH as per instructions 

Service Bulletin No. SC4800-27-17.

E. PARTS TO BE RE—IDENTIFIED BY THE OPERATOR

None

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

SC4800-73 4 SRVCNTRL SC4800-72 

SC4800-93 4 SRVCNTRL SC4800-92 

SC4800-103 4 SRVCNTRL SC4800-10 

SC4800-113 4 SRVCNTRL SC4800-11 

9
DATE : Oct 13/05 SERVICE BULLETIN No. : A330

REVISION No. : 01 — May 12/06 Page :

Printed in FRANCE © AIRBUS, 2006 All rights reserved

G. SPECIAL TOOLS

None

10
DATE : Oct 13/05 SERVICE BULLETIN No. : A330

REVISION No. : 01 — May 12/06 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 electrically g

to AMM 12-34-24 Page block 201).

2 For the modification on aircraft of the four 

servocontrols FINs 2CS1, 2CS2, 3CS1 and 3CS2 

a Do the preparation procedure as specified 

removal/installation of the elevator servo

solenoid valves (Refer to AMM 27-34-51 Pag

3 For the modification on bench of the four ele

servocontrols FINs 2CS1, 2CS2, 3CS1 and 3CS2 

a Do the preparation procedure as specified 

removal/installation of the elevator servo

2CS1, 2CS2, 3CS1 and 3CS2 (Refer to AMM 2

block 401).

(2) Standard Practices

None

B. MODIFICATION

(1) Config. 01

11
DATE : Oct 13/05 SERVICE BULLETIN No. : A330

REVISION No. : 01 — May 12/06 Page :

Printed in FRANCE © AIRBUS, 2006 All rights reserved

INSTRUCTIONS paragraph B.(1) (b) below.

NOTE (01) For the modification of the four elevator 

FINs 2CS1, 2CS2, 3CS1 and 3CS2, refer to GO

Service Bulletin No. SC4800-27-17 .

(a) In the trimmable horizontal stabilizer trailing 

on aircraft the four elevator servocontrols FIN

3CS1 and 3CS2 by replacement of the solenoid va

seals.

NOTE : For the modification of the four elevator 

FINs 2CS1, 2CS2, 3CS1 and 3CS2, refer to 

Service Bulletin No. SC4800-27-17 .

1 Modify each servocontrol.

a Remove the two solenoid valves.

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

b Replace the seals on both solenoid valves

Refer to GOODRICH Service Bulletin No. SC

c Install the two solenoid valves.

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

(b) Modify on bench the four elevator servocontrols 

2CS2, 3CS1 and 3CS2.

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

NOTE : For the modification of the four elevator 

FINs 2CS1, 2CS2, 3CS1 and 3CS2, refer to 

Service Bulletin No. SC4800-27-17 .

1 Remove :

or

4 Elevator

servocontrol

SC4800-72

4 Elevator

servocontrol

SC4800-92

12
DATE : Oct 13/05 SERVICE BULLETIN No. : A330

REVISION No. : 01 — May 12/06 Page :

Printed in FRANCE © AIRBUS, 2006 All rights reserved

2 Install :

or

or

or

C. TEST

(1) Config. 01

(a) After modification on aircraft of the four eleva

servocontrols FINs 2CS1, 2CS2, 3CS1 and 3CS2 :

1 Do the tests after removal/installation of t

servocontrols unit solenoid valves (Refer to 

Page block 401).

(b) After modification on bench of the four elevato

servocontrols FINs 2CS1, 2CS2, 3CS1 and 3CS2 :

1 Do an operational test after removal/installa

elevator servocontrols FINs 2CS1, 2CS2, 3CS1 

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

D. CLOSE UP

(1) Config. 01

(a) After modification on aircraft of the four eleva

servocontrols FINs 2CS1, 2CS2, 3CS1 and 3CS2 :

servocontrol

4 Elevator

servocontrol

SC4800-73

4 Elevator

servocontrol

SC4800-93

4 Elevator

servocontrol

SC4800-103

4 Elevator

servocontrol

SC4800-113

13
DATE : Oct 13/05 SERVICE BULLETIN No. : A330

REVISION No. : 01 — May 12/06 Page :

Printed in FRANCE © AIRBUS, 2006 All rights reserved

removal/installation of the elevator servoco

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

401).

E. DOCUMENTATION

Write in the applicable aircraft records that you have don

given in the Service Bulletin.

14
5 DATE : Oct 13/05 SERVICE BULLETIN No. : A330

REVISION No. : 01 — May 12/06 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 : Oct 13/05 SERVICE BULLETIN No. : A330

REVISION No. : 01 — May 12/06 Page : 1 of 

Printed in FRANCE © AIRBUS, 2006 All rights reserved

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Planning Material Instruct

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