5 DATE : Sep 22/04 SERVICE BULLETIN No. : A330

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. A330-

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 0616, 0621, 062

0629, 0631 thru 0638, 0640 thru 0642, 0644, 0645, 0647 thru 0

0667, 0669 thru 0671, 0673 thru 0676, 0678 thru 0680, 0682 th

thru 0688, 0690 thru 0692, 0695, 0699 thru 0701, 0703, 0705, 0

0711, 0712, 0714, 0716 and 0741.

CHANGES

SUMMARY :

— REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES

. Text modified. Compliance Recommended becomes Mandatory.

— EFFECTIVITY

. Operators AAR, AIB, CSN, IYE and KLM deleted.

PLANNING INFORMATION :

— EFFECTIVITY

. Para. 1.A. Effectivity modified. NOTE added.

— REASON

. Para. 1.C. Text modified.
DATE : Sep 22/04 SERVICE BULLETIN No. : A330

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. PN NAS1611-011A, NAS1611-012A, NAS1611-013A an

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. : A330

REVISION No. : 01 — Mar 03/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

3
5 DATE : Sep 22/04 SERVICE BULLETIN No. : A330

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). For A330-

operators, only make sure checking in the maintenance and the re

in the aircraft data PN NAS1611-XXX or NAS1611-XXXA are install

elevator servocontrols (FINs 2CS1, 2CS2). The elevator servocont

in damping position (FINs 3CS1 and 3CS2) are already addressed 

Rev. 1 dated 16 July 2004 and further revisions).

— replace them when there is no evidence that the correct seals a
DATE : Sep 22/04 SERVICE BULLETIN No. : A330

REVISION No. : 01 — Mar 03/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

EFFECTIVITY

This Service Bulletin is applicable to these operators :

ACA ACI AFR ALK AUA BDY BMA CAL CPA CRL CRX CYP DAH DLH DRD EDW E

FWI GFA GIA GRL HDA IWD KAL LDI LTU LXR MAS MEA MON MSR MYT NVR NW

QTR SAS SEU SSV TAM TCX THA TSC UAE USA VKG VLE

CONCURRENT REQUIREMENTS

None

REFERENCES/REPERCUSSIONS

TFU : 27.34.00.012

OEB : None

AOT : A330-27A3129 (for A330-200 only)

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

COMPLIANCE Mandatory CANCELS INSPECTION S

AD Yes A/C OPERATION AFFECT

RELIABILITY AFFECTED No PAX COMFORT AFFECTED 

COST SAVING No LROPS AFFECTED 

STRUCTURAL LIFE EXTN No VENDOR SB INVOLVED 

KIT PRICE (USD) No Kit

2
DATE : Sep 22/04 SERVICE BULLETIN No. : A330

REVISION No. : 01 — Mar 03/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

MATERIAL INFORMATION

AIRCRAFT DATA

Seals

APPENDICES

Refer to Appendix 01 : Inspection report.

ELAPSED TIME (HOURS) 

3
DATE : Sep 22/04 SERVICE BULLETIN No. : A330

REVISION No. : 01 — Mar 03/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

4
5 DATE : Sep 22/04 SERVICE BULLETIN No. : A330

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

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 : Sep 22/04 SERVICE BULLETIN No. : A330

REVISION No. : 01 — Mar 03/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

0605 0607 0609 0610 0612 0614 0618 0620

(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

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

ALK 0303 0306 0311 0313

AUA 0181 0195 0223 0317

BDY 0030 0037 0045

BMA 0398 0401 0404

CAL 0602 0607

CPA 0012 0017 0071 0083 0099 0102 0109 0

0155 0244 0386 0389 0393 0418 0420 0

0539 0548 0565

CRL 0285 0320

CRX 0229 0249 0275 0288 0291 0294 0299 0

CYP 0505 0526

DAH 0054

DLH 0305 0308 0312 0322 0324 0570 0576 0

DRD 0205 0211

EDW 0369

EEZ 0358 0364

EIN 0055 0059 0070 0086 0269 0330 0397

ETD 0232 0238 0259 0361

EVA 0530 0535 0555 0573 0587

FWI 0240 0253

GFA 0276 0281 0286 0287 0334 0340

2
DATE : Sep 22/04 SERVICE BULLETIN No. : A330

REVISION No. : 01 — Mar 03/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

KAL 0162 0172 0206 0219 0222 0226 0241 0

0338 0350 0351 0368 0425 0428 0484 0

LDI 0551 0597

LTU 0082 0120 0127 0403 0432 0444 0454 0

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

MYT 0254 0266 0301 0309

NVR 0353 0362

NWA 0524 0533 0542 0549 0552 0578 0588 0

0618 0620

PAL 0183 0184 0188 0189 0191 0198 0200 0

QAF 0487 0605

QFA 0506 0508 0513 0522 0553 0558 0564 0

0603

QTR 0441 0463 0473 0489 0504 0511 0521 0

SAS 0496 0497 0515 0568

SEU 0501

SSV 0171

TAM 0247 0466 0472 0477 0486

TCX 0427 0456

THA 0050 0060 0062 0064 0065 0066 0112 0

0231 0346

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 0357

VLE 0272 0339

3
DATE : Sep 22/04 SERVICE BULLETIN No. : A330

REVISION No. : 01 — Mar 03/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

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

NOTE : For the spare elevator servocontrol SC4800-2/

SC4800-7A/-9 by embodiment in service of Serv

No. A330-27-3076 :

Before installation on aircraft, replace the o

installed on the spare servocontrol solenoid v

o-ring seals PN NAS1611-XXX or PN NAS1611-XXXA

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 

4
DATE : Sep 22/04 SERVICE BULLETIN No. : A330

REVISION No. : 01 — Mar 03/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

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). For A330-200 aircraft operators, only make 

in the maintenance and the results recorded in the 

PN NAS1611-XXX or NAS1611-XXXA are installed on act

servocontrols (FINs 2CS1, 2CS2). The elevator servo

installed in damping position (FINs 3CS1 and 3CS2) 

addressed by AOT 27A3129 Rev. 1 dated 16 July 2004 

revisions).

— replace them when there is no evidence that the cor

installed.

(3) Advantages

Accomplishment of this Service Bulletin will ensure t

seals are installed on all A330-200 aircraft elevator 

fitted in active positions and on all A330-300 aircr

servocontrols.

(4) Operational/Maintenance Consequences

None

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

(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.

5
DATE : Sep 22/04 SERVICE BULLETIN No. : A330

REVISION No. : 01 — Mar 03/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

Accomplishment of this Service Bulletin is required w

Flight Hours (FH) after receipt of this Service Bull

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.

INSPECTION

REPAIR

Inspection of the data

recording

TOTAL MANHOURS 

ELAPSED TIME (HOURS) 

Get access 

Replacement of the o-ring

seals

Test 

Close-up 

6
DATE : Sep 22/04 SERVICE BULLETIN No. : A330

REVISION No. : 01 — Mar 03/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

I. ELECTRICAL LOAD DATA

Not changed

J. REFERENCES

Appendix 1

K. PUBLICATIONS AFFECTED

L. INTERCHANGEABILITY/MIXABILITY

Not applicable

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

7
DATE : Sep 22/04 SERVICE BULLETIN No. : A330

REVISION No. : 01 — Mar 03/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

This Page Intentionally Left Blank

8
DATE : Sep 22/04 SERVICE BULLETIN No. : A330

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 

9
DATE : Sep 22/04 SERVICE BULLETIN No. : A330

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

10
DATE : Sep 22/04 SERVICE BULLETIN No. : A330

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

11
DATE : Sep 22/04 SERVICE BULLETIN No. : A330

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 A330-200 aircraft operators, only make su

o-ring seals are installed on the solenoid va

elevator servocontrols PN SC4800 FINs 2CS1 and 

position). The elevator servocontrols PN SC480

and 3CS2 (damping position) have been inspecte

A330-27A3129 Rev1, dated july 2004.

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

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

12
DATE : Sep 22/04 SERVICE BULLETIN No. : A330

REVISION No. : 01 — Mar 03/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

(c) Install the seals on the solenoid valves of the 

servocontrols.

Refer to figure 3

1 Install the Seal NAS1611-112 Item 80 or the 

NAS1611-112A Item 80.

2 Install the Seal NAS1611-011 Item 130 or the 

NAS1611-011A Item 130.

3 Install the Seal NAS1611-012 Item 140 or the 

NAS1611-012A Item 140.

4 Install the Seal NAS1611-013 Item 150 or the 

NAS1611-013A Item 150.

(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 :

8 Seal Item (1

8 Seal Item (1

8 Seal Item (1

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

13
DATE : Sep 22/04 SERVICE BULLETIN No. : A330

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 344BB (Refer to AMM 06-41-55 Page 

(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.

742VU FCSC 1 STBY 9CE 77 G

742VU FCPC 1 STBY 11CE 67 K

742VU FCPC 1 STBY 11CE 69 K

14
DATE : Sep 22/04 SERVICE BULLETIN No. : A330

REVISION No. : 01 — Mar 03/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

Figure 1 Sheet 1

Area to be Inspected

15
DATE : Sep 22/04 SERVICE BULLETIN No. : A330

REVISION No. : 01 — Mar 03/05 Page :

Printed in FRANCE © AIRBUS, 2005 All rights reserved

Figure 2 Sheet 1

Flow Chart

16
DATE : Sep 22/04 SERVICE BULLETIN No. : A330

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 

17
5 DATE : Sep 22/04 SERVICE BULLETIN No. : A330

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

Printed in FRANCE © AIRBUS, 2005 All rights reserved
DATE : Sep 22/04 SERVICE BULLETIN No. : A330

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. : A330

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. : A330

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.