# Airbus Service Bulletin A330-27-3194

Copy: No revision named ("U.S. DOT/FAA - Service Bulletin - A330-27-3194 R00"), 18 pages: PDF https://openairdocs.org/files/sha256/14/c4/14c44df271aef83c158a814219935f1d79585f01eb0403a79ef36c010c831b8c; text https://openairdocs.org/service-documents/airbus/a330-27-3194/file/14c44df271ae.md. Rights: © Airbus S.A.S. Filed by the FAA in regulations.gov docket FAA-2013-0665; AD 2013-22-02 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication.

## Details

- Manufacturer: [Airbus](https://openairdocs.org/service-documents/airbus.md)
- Type: Service bulletin (Service Bulletin)
- Number: A330-27-3194
- Page: https://openairdocs.org/service-documents/airbus/a330-27-3194

## ADs that cite it (1) (OpenAirDocs)

Newest first, with the revision each names, as OpenAirDocs read it from the AD's text.

- [AD 2013-22-02](https://openairdocs.org/ad/2013-22-02.md), effective Dec 5, 2013: No revision named

Also cited in [1 proposed AD](https://openairdocs.org/service-documents/airbus/a330-27-3194/proposed.md).

## Text (18 pages)

Rights: © Airbus S.A.S. Filed by the FAA in regulations.gov docket FAA-2013-0665; AD 2013-22-02 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication. Each page's text from the PDF; open the PDF at a page with #page=N.

### Page 1

@A330
SERVICE BULLETIN
SUMMARY
AIRBUS
CUSTOMER SERVICES DIRECTORATE
1 Rond Point Maurice Bellonte
31707 BLAGNAC CEDEX
FRANCE
T e l:( 3 3 )56 19 33 33 3
Telex : AIRBU 530526F
F a x:( 3 3 )56 19 34 25 1
This summary is for information only and is not approved for modification of the aircraft.
ATA SYSTEM: 27
TITLE: FLIGHT CONTROLS - TRIMMABLE HORIZONTAL STABILIZER
ACTUATOR - REPLACE THSA PN 47147-700 BY THSA PN 47172-530
**CONF ALL
MODIFICATIONS
MODIFICATION CLASSIFICATION
MAJOR
 None
MINOR
 202802S32403
NOTE
: As per EASA IR 21, a minor change is one that has no appreciable effect on the
mass, balance, structural strength, reliability, operational characteristics affecting the
airworthiness of the product. All other changes are major changes.
REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES
First delivered aircraft were equipped with Trimmable Horizontal Stabilizer Actuator (THSA) 47147
family which are no longer produced. THSA 47172 family is the current production standard.
This Service Bulletin covers the introduction of THSA PN 47172-530 in replacement of THSA PN
47147-700.
Accomplishment of this Service Bulletin allows:
- Aircraft configuration evolution towards the current THSA family production standard,
- Anticipation on obsolescence of THSA 47147 family,
- Resolution of in-service issues encountered with THSA 47147 family (Technical Follow Up (TFU)
27.44.51.010).
Accomplishment of this Service Bulletin cancels the inspection requirements of Service Bulletin No.
A330-27-3179.
GENERAL EVALUATION
EVALUATION TABLE
COMPLIANCE
 RECOMMENDED (1)
 CANCELS INSPECTION SB
 YES
POTENTIAL AD
 NO
 A/C OPERATION AFFECTED
 NO
DATE: Oct 08/12 SERVICE BULLETIN No.: A330-27-3194
REVISION No.: 00 - Oct 08/12 Page: 1
5
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@A330
SERVICE BULLETIN
SUMMARY
EVALUATION TABLE
RELIABILITY AFFECTED
 NO
 PAX COMFORT AFFECTED
 NO
COST SAVING
 NO
 ETOPS AFFECTED
 NO
STRUCTURAL LIFE EXTN
 NO
 VENDOR SB INVOLVED
 NO
NOTE
 (1)
: Service Bulletin recommended to be accomplished to prevent significant operational
disruptions.
MATERIAL PRICE INFORMATION
MATERIAL PRICE INFORMATION TABLE
MATERIAL SET
 QTY PER
A/C
PRICE PER
A/C (USD)
MAIN PARTS
Equipment BFEA01
 1
 See SB
 THSA
EFFECTIVITY
This Service Bulletin is applicable to this (these) operator(s) :
BEL BER CPA GIA HDA HFY KAL MAS OHY PAL RSY SAI THA
TSC VLK XAX
CONCURRENT REQUIREMENTS
Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishment of the
following Service Bulletin(s) or the equivalent production modification(s):
Service Bulletin No. A330-27-3143
NOTE
: Service Bulletin No. A330-27-3143 (FLIGHT CONTROLS - TRIMMABLE HORIZONTAL
STABILIZER - INTRODUCE MODIFIED THSA (PN 47147-700)).
REFERENCES / REPERCUSSIONS
TFU
 27.44.51.010
OEB
 None
AOT
 None
SIL
 None
LINE MAINTENANCE AFFECTED
 No
LIFE LIMIT
 None
OTHER
 None
NATURE OF THE WORK
AIRCRAFT
 NO
EQUIPMENT
 YES
HARD
 NO
SOFT
 NO
OBRM
 NO
DATE: Oct 08/12 SERVICE BULLETIN No.: A330-27-3194
REVISION No.: 00 - Oct 08/12 Page: 2
5
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@A330
SERVICE BULLETIN
SUMMARY
MANPOWER
Task 273194-831-801-001: Modification
TOTAL MANHOURS
 19.00
ELAPSED TIME (HOURS)
 19.00
APPENDICES
None
DATE: Oct 08/12 SERVICE BULLETIN No.: A330-27-3194
REVISION No.: 00 - Oct 08/12 Page: 3
5
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@A330
SERVICE BULLETIN
SUMMARY
**CONF ALL
FR87
FR80
 − Z311 Z312
A
B
1CS
B
312AR
A
G_SB_273194_5_SAAA_01_00
Figure A-FSAAA - Sheet 01
DATE: Oct 08/12 SERVICE BULLETIN No.: A330-27-3194
REVISION No.: 00 - Oct 08/12 Page: 4
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 5

@A330
SERVICE BULLETIN
AIRBUS
CUSTOMER SERVICES DIRECTORATE
1 Rond Point Maurice Bellonte
31707 BLAGNAC CEDEX
FRANCE
T e l:( 3 3 )56 19 33 33 3
Telex : AIRBU 530526F
F a x:( 3 3 )56 19 34 25 1
ATA SYSTEM: 27
TITLE: FLIGHT CONTROLS - TRIMMABLE HORIZONTAL STABILIZER
ACTUATOR - REPLACE THSA PN 47147-700 BY THSA PN 47172-530
MODIFICATION No.: 202802S32403
This document contains AIRBUS PROPRIETARY INFORMATION and shall at all times remain the
property of AIRBUS; no intellectual property right or licence is granted by AIRBUS in connection with
any information contained in it. It is delivered on the express condition that said document and the
information contained in it shall be treated as confidential, shall not be used for any purpose other than
that for which it is hereby delivered. It shall not be disclosed in whole or in part to third parties and shall
not be duplicated in any manner (except for the purposes of performing the tasks described hereunder
and provided that any recipient of such document shall comply with the conditions herein), without
AIRBUS prior written consent.
1. PLANNING INFORMATION
**CONF ALL
A. EFFECTIVITY
NOTE
: This modification is applicable by Service Bulletin only.
(1) Models
330-301 330-321 330-322 330-341 330-342
(2) Effectivity by MSN
0012 0017 0030 0037 0045 0050 0054-0055 0060 0062 0064-0067 0069-0073 0077
0082-0083 0086-0087 0095-0096 0098-0100 0102 0106-0107 0109-0113 0116
0118-0122 0127 0132 0138 0140 0143-0144 0148 0153 0155 0162 0165 0171-0172
0177 0183-0184 0188-0189 0191 0198 0200 0203 0206 0209 0219 0224 0231
(3) Effectivity by Operator
The Operator/MSN relationship is provided for information only and is correct at the time
of issue in accordance with the information available to AIRBUS. Any future changes
resulting from transfer of an aircraft from one operator to another will not be reflected in
this list unless the Service Bulletin is revised for another reason.
OPERATOR
 MSN
BEL
 0030 0037 0045 0082 0095
BER
 0120 0127
DATE: Oct 08/12 SERVICE BULLETIN No.: A330-27-3194
REVISION No.: 00 - Oct 08/12 Page: 1
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SERVICE BULLETIN
OPERATOR
 MSN
CPA
 0012 0017 0071 0102 0113 0118 0121 0155
GIA
 0138 0140 0144 0148 0153 0165
HDA
 0083 0099 0106 0109
HFY
 0096
KAL
 0162 0172 0206 0219
MAS
 0067 0069 0073 0077 0100 0107 0110 0116 0119
OHY
 0072 0087 0098 0143
PAL
 0183 0184 0188 0189 0191 0198 0200 0203
RSY
 0171
SAI
 0055 0070
THA
 0050 0060 0062 0064 0065 0066 0112 0122 0209 0224 0231
TSC
 0111 0132 0177
VLK
 0086
XAX
 0054
(4) Configuration by MSN
MSN
 CONFIGURATION
0012 0017 0030 0037 0045 0050 0054 0055 0060 0062 0064
0065 0066 0067 0069 0070 0071 0072 0073 0077 0082 0083
0086 0087 0095 0096 0098 0099 0100 0102 0106 0107 0109
0110 0111 0112 0113 0116 0118 0119 0120 0121 0122 0127
0132 0138 0140 0143 0144 0148 0153 0155 0162 0165 0171
0172 0177 0183 0184 0188 0189 0191 0198 0200 0203 0206
0209 0219 0224 0231
001
(5) Configuration definition
**CONF 001
Config. 001 is valid for all the aircraft given in the effectivity of this Service Bulletin as a
standard configuration.
(6) Material Effectivity
MATERIAL
 QTY PER A/C
 SEE NOTES
Equipment BFEA01
 1
B. CONCURRENT REQUIREMENTS
Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishment of
the following Service Bulletin(s) or the equivalent production modification(s):
Service Bulletin No. A330-27-3143
NOTE
: Service Bulletin No. A330-27-3143 (FLIGHT CONTROLS - TRIMMABLE
HORIZONTAL STABILIZER - INTRODUCE MODIFIED THSA (PN
47147-700)).
DATE: Oct 08/12 SERVICE BULLETIN No.: A330-27-3194
REVISION No.: 00 - Oct 08/12 Page: 2
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

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@A330
SERVICE BULLETIN
C. REASON
(1) History
First delivered aircraft were equipped with Trimmable Horizontal Stabilizer Actuator
(THSA) 47147 family which are no longer produced. THSA 47172 family is the current
production standard.
(2) Objective/Action
This Service Bulletin covers the introduction of THSA PN 47172-530 in replacement of
THSA PN 47147-700.
(3) Advantages
Accomplishment of this Service Bulletin allows:
- Aircraft configuration evolution towards the current THSA family production
standard,
- Anticipation on obsolescence of THSA 47147 family,
- Resolution of in-service issues encountered with THSA 47147 family (Technical
Follow Up (TFU) 27.44.51.010).
Accomplishment of this Service Bulletin cancels the inspection requirements of Service
Bulletin No. A330-27-3179.
(4) Operational/Maintenance Consequences
None
D. DESCRIPTION
To accomplish this Service Bulletin it is necessary to :
Task 273194-831-801-001: Modification
(1) Remove the THSA.
(2) Install the THSA.
E. COMPLIANCE
(1) Classification
RECOMMENDED: Service Bulletin recommended to be accomplished to prevent
significant operational disruptions.
(2) Accomplishment Timescale
Accomplishment of this Service Bulletin is recommended at the earliest opportunity
where manpower and facilities are available.
DATE: Oct 08/12 SERVICE BULLETIN No.: A330-27-3194
REVISION No.: 00 - Oct 08/12 Page: 3
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

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@A330
SERVICE BULLETIN
F. APPROVAL
The technical content of this document is approved under the authority of Design
Organization Approval No. EASA.21J.031.
If an aircraft listed in the effectivity has a modification or repair embodied that is not of
AIRBUS origin, and which affects the content of this Service Bulletin, the operator is
responsible for obtaining approval by its airworthiness authority for any adaptation necessary
before incorporation of the Service Bulletin.
G. MANPOWER
The manpower estimates given in this Service Bulletin are based on the direct labor cost to
do the work. These estimates assume that the work will be done by experienced personnel,
and may need to be revised upwards to suit operator’s circumstances. The estimates do not
include the time to prepare, plan or inspect the work. Manufacture and procurement of parts
and tools, drying times for paints, sealants, etc., and general administration work are also not
included.
Task 273194-831-801-001: Modification
Get Access
 1.00
On Aircraft
Remove the THSA.
 8.00
Install the THSA.
 8.00
Tests
 1.00
Close-Up
 1.00
TOTAL MANHOURS
 19.00
ELAPSED TIME (HOURS)
 19.00
H. WEIGHT AND BALANCE
The weight and balance estimates given in this Service Bulletin are based on the
Manufacturer’s Empty Weight (MEW) and do not include operator item’s. For the definition of
MEW and operator’s items refer to Weight and Balance Manual (WBM) Chapter 1-00-07.
Manufacturers Empty Weight +2.2 KG (+4.8501 LB)
Effect on Balance +143 KGM (+1034.319 LB.FT )
I. ELECTRICAL LOAD DATA
Not Changed
J. REFERENCES
Aircraft Maintenance Manual (AMM)
 12-34-24 27-44-51
ATA Common Support Data Dictionary (CSDD),
Chapter 2
Elec. Std. Practices Manual (ESPM)
 20-55-00
Service Bulletin (SB)
 A330-27-3143
Weight and Balance Manual (WBM)
 Weight and Balance Manual
(WBM) Chapter 1-00-07
DATE: Oct 08/12 SERVICE BULLETIN No.: A330-27-3194
REVISION No.: 00 - Oct 08/12 Page: 4
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 9

@A330
SERVICE BULLETIN
K. PUBLICATION AFFECTED
Aircraft Wiring List (AWL)
Illustrated Parts Catalog (IPC)
 27-44-04
L. INTERCHANGEABILITY/MIXABILITY
DESCRIPTION
 OLD PART N˚
 NEW PART N˚
 INT
 MIXABILITY
 SEE
NOTES
THS Actuator
 47147-700
 47172-530
 01
 Not
Applicable
NOTE
: For definitions of interchangeability codes in column INT., refer to ATA
Common Support Data Dictionary (CSDD), Chapter 2.
M. SPARES
THS Actuator 47147-700
DATE: Oct 08/12 SERVICE BULLETIN No.: A330-27-3194
REVISION No.: 00 - Oct 08/12 Page: 5
5
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### Page 10

@A330
SERVICE BULLETIN
This Page Intentionally Left Blank
DATE: Oct 08/12 SERVICE BULLETIN No.: A330-27-3194
REVISION No.: 00 - Oct 08/12 Page: 6
5
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### Page 11

@A330
SERVICE BULLETIN
2. MATERIAL INFORMATION
**CONF ALL
A. MATERIAL - PRICE AND AVAILABILITY
(1) Procurement Addresses
Vendor parts are to be procured from :
Equipment BFEA01
 UTC AEROSPACE
13 Avenue de l’eguillette
ST-OUEN L’AUMONE
95310
FRANCE
T e l :( 3 3 )13 43 26 30 0
F a x :( 3 3 )13 43 26 31 0
(2) Price and Availability
No AIRBUS kit will be provided.
Procurement terms for the equipment must be negotiated with the equipment supplier.
B. INDUSTRY SUPPORT INFORMATION
AIRBUS will not provide industry support for accomplishment of this Service Bulletin.
C. LIST OF COMPONENTS
No Kit
D. LIST OF MATERIALS - OPERATOR SUPPLIED
(1) Consumable Materials
NOTE
: To accomplish this Service Bulletin it is necessary to use the expendable
parts listed in the AMM Task 27-44-51-400-801.
(2) Components
None
(3) Equipment
Equipment BFEA01
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 ITEM
 OLD PART N˚
 INT
 SEE
NOTES
47172-530
 1
 ACTUATOR
 47147-700
 01
 (1)
NOTE
: For definitions of interchangeability codes in column INT., refer to ATA
Common Support Data Dictionary (CSDD), Chapter 2.
DATE: Oct 08/12 SERVICE BULLETIN No.: A330-27-3194
REVISION No.: 00 - Oct 08/12 Page: 7
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 12

@A330
SERVICE BULLETIN
NOTE
 (1)
: The above list of components is not an AIRBUS Kit, the required parts
shall be ordered as necessary through the given channel.
E. PARTS TO BE RE-IDENTIFIED BY OPERATOR
None
F. TOOLING
(1) Tooling - Price and Availability
None
(2) Tools
NOTE
: To accomplish this Service Bulletin it is necessary to use the tools listed
in AMM Task 27-44-51-000-801 and AMM Task 27-44-51-400-801.
(3) Special Tools
None
DATE: Oct 08/12 SERVICE BULLETIN No.: A330-27-3194
REVISION No.: 00 - Oct 08/12 Page: 8
5
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### Page 13

@A330
SERVICE BULLETIN
3. ACCOMPLISHMENT INSTRUCTIONS
Task 273194-831-801-001 - Modification
WARNING
: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONS
INCLUDED IN THE REFERENCED PROCEDURES.
CAUTION
: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP
ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY
AND MECHANICALLY SERVICEABLE) . WHEN YOU DO MAINTENANCE
WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING,
COMPONENTS AND THE WORK AREA AS CLEAN AS POSSIBLE. TO DO
THIS:
- PUT PROTECTION, SUCH AS PLASTIC SHEETING, CLOTHS, ETC; AS
NECESSARY ON WIRING AND COMPONENTS.
- REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND
OTHER CONTAMINATION.
THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION
AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION.
IN CASE OF CONTAMINATION REFER TO ESPM 20-55-00.
Task Associated Data
Zone
From 311 to 312
Modified FIN
1CS
Manpower
TOTAL MANHOURS
 19.00
ELAPSED TIME (HOURS)
 19.00
A. GENERAL
(1) Subtask 273194-839-001-001 - Administrative
Manpower Resources
Skills
 NON SPECIFIC
Write in the applicable aircraft records that you have done all the work given in this
Service Bulletin.
B. PREPARATION
(1) Subtask 273194-941-001-001 - Job Set-up
Manpower Resources
Skills
 NON SPECIFIC
DATE: Oct 08/12 SERVICE BULLETIN No.: A330-27-3194
REVISION No.: 00 - Oct 08/12 Page: 9
5
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SERVICE BULLETIN
References
Aircraft Maintenance Manual (AMM)
 Task 12-34-24-860-002
Task 27-44-51-000-801
(a) Make sure that the aircraft is electrically grounded, refer to AMM Task
12-34-24-860-002.
(b) Do the Job Set-up procedure as described in the removal of the THSA (FIN 1CS),
refer to AMM Task 27-44-51-000-801.
C. PROCEDURE
(1) Subtask 273194-020-001-001 - Remove the THSA.
Work Zones and Access Panels
Zone
 Access/Work location
From
 311
To
 312
Manpower Resources
Manhours
 8.00
Minimum number of person
 2
Subtask elapsed time
 8.00
Skills
 NON SPECIFIC
References
Aircraft Maintenance Manual (AMM)
 Task 27-44-51-000-801
(a) Remove:
Refer to AMM Task 27-44-51-000-801
FIN 1CS
1 THS Actuator 47147-700
(2) Subtask 273194-420-001-001 - Install the THSA.
Work Zones and Access Panels
Zone
 Access/Work location
From
 311
To
 312
Manpower Resources
Manhours
 8.00
Minimum number of person
 2
Subtask elapsed time
 8.00
Skills
 NON SPECIFIC
DATE: Oct 08/12 SERVICE BULLETIN No.: A330-27-3194
REVISION No.: 00 - Oct 08/12 Page: 10
5
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@A330
SERVICE BULLETIN
Material necessary to do the job
Equipment BFEA01
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 SEE
NOTES
47172-530
 1
 ACTUATOR
 (1)
NOTE
 (1)
: The above list of components is not an AIRBUS Kit, the required parts
shall be ordered as necessary through the given channel.
References
Aircraft Maintenance Manual (AMM)
 Task 27-44-51-400-801
(a) Install:
Refer to AMM Task 27-44-51-400-801
FIN 1CS
1 THS Actuator 47172-530
D. TEST
(1) Subtask 273194-700-001-001 - Testing
Manpower Resources
Skills
 NON SPECIFIC
References
Aircraft Maintenance Manual (AMM)
 Task 27-44-51-400-801
(a) Remove the safety clips and/or tags and close/unlock the circuit breakers as
specified after the installation of the THSA (FIN 1CS), refer to AMM Task
27-44-51-400-801.
(b) Do the Test procedure as specified after the installation of the THSA (FIN 1CS),
refer to AMM Task 27-44-51-400-801.
E. CLOSE-UP
(1) Subtask 273194-942-001-001 - Close-up
Manpower Resources
Skills
 NON SPECIFIC
References
Aircraft Maintenance Manual (AMM)
 Task 27-44-51-400-801
(a) Make sure that the work areas are clean and clear of tools and other items of
equipment.
(b) Do the Close-Up procedure as described in the installation of the THSA (FIN 1CS),
refer to AMM Task 27-44-51-400-801.
DATE: Oct 08/12 SERVICE BULLETIN No.: A330-27-3194
REVISION No.: 00 - Oct 08/12 Page: 11
5
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@A330
SERVICE BULLETIN
(c) Restore the systems and the air craft to normal operating condition.
DATE: Oct 08/12 SERVICE BULLETIN No.: A330-27-3194
REVISION No.: 00 - Oct 08/12 Page: 12
5
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SERVICE BULLETIN
REPORTING SHEET
TITLE: FLIGHT CONTROLS - TRIMMABLE HORIZONTAL STABILIZER
ACTUATOR - REPLACE THSA PN 47147-700 BY THSA PN 47172-530
MODIFICATION No.: 202802S32403
Please complete the appropriate item (A or B):
A - SB WILL BE
 embodied YES/NO (if NO please comment)
If YES, aircraft concer ned (as per SB effectivity by default) and planned dates (month/year) of
embodiment:
B - SB HAS BEEN
 embodied on aircraft:
Operator comments:
From Airline:
Name/Title:
Signature: Date:
If operational documentation is affected (see Paragraph 1.K of this SB): If information is needed prior to
next normal revision or prior to SB embodiment, please indicate required service(s):
Either: Modification Operational Impact (MOI), if available YES/NO
Or : Intermediate revision YES/NO
Important Information:
 This SB will only be incorporated in your maintenance and operational
documentation if this sheet is returned to Airbus and signed by a duly authorised representative. With
the next feasible revision, this will result in
- Updating of maintenance documentation to show pre and post SB data.
- Updating of maintenance and operational documentation to show post SB data after embodiment.
If this SB requires previous or simultaneous accomplishment of other SBs, Airbus shall automatically
include them in the manual revisions. Refer to SIL 00-037 for detailed information.
Please return this completed sheet to:
AIRBUS
CUSTOMER SERVICES DIRECTORATE
1 Rond Point Maurice Bellonte
31707 BLAGNAC CEDEX FRANCE
Attn: SDC32 Technical Data and Documentation Services
F A X :( + 3 3 )56 19 32 80 6
e-mail: sb.reporting@airbus.com
or via your Resident Customer Support Office.
Alternatively, SB lists via letters or fax are also accepted.
DATE: Oct 08/12 SERVICE BULLETIN No.: A330-27-3194
REVISION No.: 00 - Oct 08/12 Page: 1
5
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SERVICE BULLETIN
QUALITY PERCEPTION FORM
Use this form to tell us what is your perception of the quality of this Service Bulletin. The reported data
that you provide us will be used to analyse areas of difficulties and to take corrective action to further
improve the quality of our Service Bulletins.
We thank you for the time you have taken in completing this form.
(Please rate on a scale of 1 to 4, with 4 being the highest score)
- Quality rating of this SB 4321
- Quality rating of the Accomplishment Instructions 4321
- Quality rating of the Illustrations 4321
- Is this SB easy to understand ? Y/N
If you have had difficulties in the accomplishment of this SB please quote below the area(s) and give a
short description of the issue.
Planning Material Instructions
X Effectivity X Kit content X Preparation
X Reason X List of Materials Operator Supplied X Mod/Inspection
X Manpower X Industry support X Test
X References X Re-identification X Close-Up
X Publication X Tooling X Illustrations
Comments:
Operator: Date:
Name/Title:
Please return this form to:
AIRBUS
CUSTOMER SERVICES DIRECTORATE
1 Rond Point Maurice Bellonte
31707 BLAGNAC CEDEX FRANCE
Attn : SEM4 Service Bulletins Management
F A X:( 3 3 )56 19 34 25 1
Or via your Resident Customer Support Office.
DATE: Oct 08/12 SERVICE BULLETIN No.: A330-27-3194
REVISION No.: 00 - Oct 08/12 Page: 1
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

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