# Airbus Service Bulletin A330-54-3022

Copy: No revision named ("A330-54-3022 R01"), 20 pages: PDF https://openairdocs.org/files/sha256/0b/cc/0bccdaefefef8ff91dc39e53a4b17cdd44cc79da5e06aeb0069bc169f1a58db0; text https://openairdocs.org/service-documents/airbus/a330-54-3022/file/0bccdaefefef.md. Rights: © Airbus S.A.S. Filed by the FAA in regulations.gov docket FAA-2023-0669, the docket of AD 2023-12-01. Not covered by OpenAirDocs’ CC0 dedication.

## Details

- Manufacturer: [Airbus](https://openairdocs.org/service-documents/airbus.md)
- Type: Service bulletin (Service Bulletin)
- Number: A330-54-3022
- Page: https://openairdocs.org/service-documents/airbus/a330-54-3022

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

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

- [AD 2006-10-13](https://openairdocs.org/ad/2006-10-13.md), effective Jun 20, 2006: No revision named

## Text (20 pages)

Rights: © Airbus S.A.S. Filed by the FAA in regulations.gov docket FAA-2023-0669, the docket of AD 2023-12-01. 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
A330
SERVICE BULLETIN
REVISION TRANSMITT AL SHEET
AIRBUS
CUSTOMER SERVICES DIRECTORA TE
1 Rond Point Maurice Bellonte
31707 BLAGNAC CEDEX FRANCE
Tel : (33) 5 61 93 33 33
Telex : AIRBU 530526F
Fax : (33) 5 61 93 42 51
A T A SYSTEM : 54
TITLE : NACELLES/PYLONS - LOWER FAIRING - MODIFY STRUCTURE A T LOWER AFT PYLON
FAIRING LEVEL FOR PW ENGINES
MODIFICA TION No. : 53623S18198
This page transmits Revision No. 01 of Service Bulletin No. A330-54-3022
ADDITIONAL WORK
No additional work is required by this revision for aircraft modified by any previous issue.
REASON
Revision No. 01 issued to add aircraft MSN 0663 for Operator NWA and aircraft MSN 0665 for
Operator EEZ.
CHANGES
SUMMARY :
- REASON/DESCRIPTION/OPERA TIONAL CONSEQUENCES
. Modification classification table added.
- EFFECTIVITY
. Operators updated.
- MANPOWER
. Notion of configuration added.
PLANNING INFORMA TION :
- DESCRIPTION
. 1.D. Notion of configuration added.
- MANPOWER
. 1.G. Notion of configuration added.
- SPECIAL TOOLS
DA TE : May 25/05 SERVICE BULLETIN No. : A330-54-3022
REVISION No. : 01 - Jan 09/08 Page : 1 of 2
Printed in France © AIRBUS 2007 All rights reserved

### Page 2

A330
A330
SERVICE BULLETIN
REVISION TRANSMITT AL SHEET
. 2.G. Mention to tools listed in the Vendor Service Bulletin added.
ACCOMPLISHMENT INSTRUCTIONS :
- Preparation
. 3.A.(1) Notion of configuration added.
- MODIFICA TION
. 3.B. Notion of configuration added.
- TESTS
. 3.C. Notion of configuration added.
- CLOSE-UP
. 3.D. Notion of configuration added.
FILING INSTRUCTIONS
This Service Bulletin has been generated electronically and is reissued as a complete document.
Replace the complete document.
Put this Revision T ransmittal Sheet in front of the Service Bulletin.
HISTORY OF PREVIOUS REVISIONS
No previous revisions.
REVISION SEQUENCE
ORIGINAL : May 25/05
REVISION No. : 01 - Jan 09/08
DA TE : May 25/05 SERVICE BULLETIN No. : A330-54-3022
REVISION No. : 01 - Jan 09/08 Page : 2
Printed in France © AIRBUS 2007 All rights reserved

### Page 3

A330
A330
SERVICE BULLETIN
SUMMARY
AIRBUS
CUSTOMER SERVICES DIRECTORA TE
1 Rond Point Maurice Bellonte
31707 BLAGNAC CEDEX FRANCE
Tel : (33) 5 61 93 33 33
Telex : AIRBU 530526F
Fax : (33) 5 61 93 42 51
This summary is for information only and is
not approved for modification of the aircraft
A T A SYSTEM : 54
TITLE : NACELLES/PYLONS - LOWER FAIRING - MODIFY STRUCTURE A T LOWER AFT PYLON
FAIRING LEVEL FOR PW ENGINES
MODIFICA TION No. : 53623S18198
REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES
This Service Bulletin is issued to advise all operators of A330 aircraft powered by PW4164 / PW4168 /
PW4168A engines, of the issue of PRA TT and WHITNEY Service Bulletin No. PW4G-100-54-7.
Some A330/PW operators are experiencing Lower Aft Pylon Fairing (LAPF) seals damage with cracking of
LAPF firewall, supports, frames, clips, spars, side skins, blade seals, nozzle seals and lower skin assembly .
Investigation identified seals failure due to fatigue and thermal distress. Damage of LAPF structure (cracks)
were also reported as a consequence of High Cycle Fatigue (HCF) and thermal stresses.
This Service Bulletin recommends to introduce a structural improvement at LAPF level by :
- Blade and nozzle seals re-design ;
- Structural modification on supports, firewall, heatshield, frames, spars and skins.
Accomplishment of this Service Bulletin will avoid any deterioration of the fairing and will protect surrounding
areas.
Accomplishment of this Service Bulletin cancels the inspection requirements of the mandatory Service
Bulletin No. A330-54-3021.
EVALUATION T ABLE
COMPLIANCE Recommended CANCELS INSPECTION SB YES
POTENTIAL AD No A/C OPERA TION AFFECTED No
RELIABILITY AFFECTED No P AX COMFORT AFFECTED No
DA TE : May 25/05 SERVICE BULLETIN No. : A330-54-3022
REVISION No. : 01 - Jan 09/08 Page : 1 of 3
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### Page 4

A330
A330
SERVICE BULLETIN
SUMMARY
EVALUATION T ABLE
COST SAVING No ETOPS AFFECTED No
STRUCTURAL LIFE EXTN YES VENDOR SB INVOL VED YES
KIT PRICE (USD) No Kit
MODIFICA TION CLASSIFICA TION
MAJOR 53623S18198
MINOR None
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.
EFFECTIVITY
This Service Bulletin is applicable to these operators :
AAR DA T EEZ FWI GRL HFY HVN IWD KAL L TU MAS NVR NWA SWR T AM T AP THA USA
This modification is embodied before delivery on aircraft 0674 and subsequent.
CONCURRENT REQUIREMENTS
None
REFERENCES/REPERCUSSIONS
TFU : 54.56.00.003
OEB : None
AOT : None
SIL : None
LIFE LIMIT : None
LINE MAINTENANCE AFFECTED : No
DA TE : May 25/05 SERVICE BULLETIN No. : A330-54-3022
REVISION No. : 01 - Jan 09/08 Page : 2
Printed in France © AIRBUS 2007 All rights reserved

### Page 5

A330
A330
SERVICE BULLETIN
SUMMARY
OTHERS : None
NATURE OF THE WORK
AIRCRAFT : YES
EQUIPMENT : NO
HARD : NO
SOFT : NO
OBRM : NO
MANPOWER
Config. 01, on aircraft for one pylon
TOT AL MANHOURS 5.0
ELAPSED TIME (HOURS) 4.5
Config. 01, on bench
TOT AL MANHOURS Refer to PRATT and WHITNEY Service
Bulletin No. PW4G-100-A54-7
ELAPSED TIME (HOURS) Refer to PRATT and WHITNEY Service
Bulletin No. PW4G-100-A54-7
MATERIAL INFORMATION
AIRCRAFT DA T A
None
APPENDICES
None
DA TE : May 25/05 SERVICE BULLETIN No. : A330-54-3022
REVISION No. : 01 - Jan 09/08 Page : 3
Printed in France © AIRBUS 2007 All rights reserved

### Page 6

(No text on this page.)

### Page 7

A330
A330
SERVICE BULLETIN
AIRBUS
CUSTOMER SERVICES DIRECTORA TE
1 Rond Point Maurice Bellonte
31707 BLAGNAC CEDEX FRANCE
Tel : (33) 5 61 93 33 33
Telex : AIRBU 530526F
Fax : (33) 5 61 93 42 51
A T A SYSTEM : 54
TITLE : NACELLES/PYLONS - LOWER FAIRING - MODIFY STRUCTURE A T LOWER AFT PYLON
FAIRING LEVEL FOR PW ENGINES
MODIFICA TION No. : 53623S18198
This document contains AIRBUS PROPRIET ARY INFORMA TION 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. P LANNING INFORMATION
A. E FFECTIVITY
(1) Models
330-223 330-321 330-322 330-323
(2) Aircraft
(a) Effectivity by MSN
This Service Bulletin is applicable to aircraft MSN :
0050 0060 0062 0064-0067 0069 0072 0073 0077 0082 0087 0095 0096 0100 0107
0110 0112 0116 0119 0120 0122 0127 0143 0162 0171 0172 0181 0195 0206 0209
0219 0222-0224 0226 0229-0232 0238 0240 0241 0247 0249 0253 0255 0256 0258
0259 0262 0267 0275 0288 0290 0291 0294 0296 0299 0300 0305 0308 0312 0315
0317 0322-0324 0333 0337 0338 0342 0343 0346 0350 0351 0353 0358 0361 0362
0364 0366 0368 0370 0375 0380 0388 0403 0425 0428 0432 0444 0454 0469 0476
0484 0490 0493 0524 0533 0542 0549 0550 0552 0578 0588 0591 0609 0614 0618
0620 0621 0631 0633 0640 0663 0665
(b) 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.
DA TE : May 25/05 SERVICE BULLETIN No. : A330-54-3022
REVISION No. : 01 - Jan 09/08 Page : 1 of 12
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### Page 8

A330
A330
SERVICE BULLETIN
OPERA TOR MSN
AAR 0640
DA T 0082
EEZ 0358 0364 0665
FWI 0240 0253
GRL 0230
HFY 0096
HVN 0087 0255 0262
IWD 0072
KAL 0162 0172 0206 0219 0222 0226 0241 0256 0258 0267 0338 0350
0351 0368 0425 0428 0484 0490 0550
L TU 0120 0127 0171 0403 0432 0444 0454 0469 0476 0493
MAS 0067 0069 0073 0077 0095 0100 0107 0110 0116 0119 0143
0290 0296 0300
NVR 0353 0362
NWA 0524 0533 0542 0549 0552 0578 0588 0591 0609 0614 0618
0620 0621 0631 0633 0663
SWR 0229 0249 0275 0288 0291 0294 0299 0322 0324 0343 0366
T AM 0232 0238 0247 0259 0361
T AP 0181 0195 0223 0305 0308 0312 0317
THA 0050 0060 0062 0064 0065 0066 0112 0122 0209 0224 0231 0346
USA 0315 0323 0333 0337 0342 0370 0375 0380 0388
(c) Effectivity by MSN and Kit/Configuration
The Kits and configurations applicable to these MSNs are given at the end of this list
0050 0060 0062 0064-0067 0069 0072-0073 0077 0082 0087 0095-0096 0100 0107
0110 0112 0116 0119-0120 0122 0127 0143 0162 0171-0172 0181 0195 0206 0209
0219 0222-0224 0226 0229-0232 0238 0240-0241 0247 0249 0253 0255-0256
0258-0259 0262 0267 0275 0288 0290-0291 0294 0296 0299-0300 0305 0308 0312
0315 0317 0322-0324 0333 0337-0338 0342-0343 0346 0350-0351 0353 0358
0361-0362 0364 0366 0368 0370 0375 0380 0388 0403 0425 0428 0432 0444 0454
0469 0476 0484 0490 0493 0524 0533 0542 0549-0550 0552 0578 0588 0591 0609
0614 0618 0620-0621 0631 0633 0640 0663 0665
DA TE : May 25/05 SERVICE BULLETIN No. : A330-54-3022
REVISION No. : 01 - Jan 09/08 Page : 2
Printed in France © AIRBUS 2007 All rights reserved

### Page 9

A330
A330
SERVICE BULLETIN
KIT No. QTY PER A/C CONFIGURA TION
None 01
NOTE : Config. 01 is valid for all the aircraft given in the effectivity of this Service
Bulletin as a standard configuration.
(3) Spares
Refer to PRA TT and WHITNEY Service Bulletin No. PW4G-100-54-7.
B. C ONCURRENT REQUIREMENTS
None
C. R EASON
(1) History
Some A330/PW operators are experiencing Lower Aft Pylon Fairing (LAPF) seals damage
with cracking of LAPF firewall, supports, frames, clips, spars, side skins, blade seals, nozzle
seals and lower skin assembly . Investigation identified seals failure due to fatigue and
thermal distress. Damage of LAPF structure (cracks) were also reported as a consequence
of High Cycle Fatigue (HCF) and thermal stresses.
(2) Objective/Action
This Service Bulletin is issued to advise all operators of A330 aircraft powered by PW4164 /
PW4168 / PW4168A engines, of the issue of PRA TT and WHITNEY Service Bulletin No.
PW4G-100-54-7.
This Service Bulletin recommends to introduce a structural improvement at LAPF level by :
- Blade and nozzle seals re-design ;
- Structural modification on supports, firewall, heatshield, frames, spars and skins.
(3) Advantages
Accomplishment of this Service Bulletin will avoid any deterioration of the fairing and
will protect surrounding areas.
Accomplishment of this Service Bulletin cancels the inspection requirements of the
mandatory Service Bulletin No. A330-54-3021.
(4) Operational/Maintenance Consequences
None
D. D ESCRIPTION
T o accomplish this Service Bulletin it is necessary to :
DA TE : May 25/05 SERVICE BULLETIN No. : A330-54-3022
REVISION No. : 01 - Jan 09/08 Page : 3
Printed in France © AIRBUS 2007 All rights reserved

### Page 10

A330
A330
SERVICE BULLETIN
(1) Config. 01
(a) Replace the Lower Aft Pylon Fairing Assies
E. C OMPLIANCE
(1) Classification
Recommended
(2) Accomplishment Timescale
Accomplishment of this Service Bulletin is recommended at the earliest opportunity where
manpower and facilities are available.
F. A PPROVAL
Approved under the EASA Design Organisation 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. M ANPOWER
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.
Config. 01 , on aircraft for one pylon
Get access 2.0
T est 0.5
Close-up 2.5
TOT AL MANHOURS 5.0
ELAPSED TIME (HOURS) 4.5
Config. 01 , on bench
Modification of LAPF Refer to PRA TT
and WHITNEY
Service Bulletin No.
PW4G-100-A54-7
TOT AL MANHOURS Refer to PRATT and WHITNEY Service
Bulletin No. PW4G-100-A54-7
DA TE : May 25/05 SERVICE BULLETIN No. : A330-54-3022
REVISION No. : 01 - Jan 09/08 Page : 4
Printed in France © AIRBUS 2007 All rights reserved

### Page 11

A330
A330
SERVICE BULLETIN
ELAPSED TIME (HOURS) Refer to PRATT and WHITNEY Service
Bulletin No. PW4G-100-A54-7
H. W EIGHT AND BALANCE
Manufacturers Empty Weight : 11.250 kg (+24.8017 lb)
Effect on Balance : + 371.475 kgm (+2686.878 lb.ft)
I. E LECTRICAL LOAD DATA
Not changed
J. R EFERENCES
Aircraft Maintenance Manual (AMM) : 12-34-24 54-56-11
Elec. Std. Practices Manual (ESPM) : 20-55-00
PRA TT and WHITNEY Service Bulletin No. PW4G-100-A54-7
Service Bulletin No. A330-54-3021
K. P UBLICATIONS AFFECTED
Illustrated Parts Catalog (IPC) : 54-56-11
L. I NTERCHANGEABILITY/MIXABILITY
DESCRIPTION OLD P ART No. NEW P ART No. INT MIXABILITY
Lower Aft Pylon Fairing
Assy
72A100-501
72A100-503
72A100-505
72A100-507
72A100-509
72A100-511
72A100-513
72A100-701
72A100-703
72A100-705 01 Not
applicable
NOTE : For definitions of interchangeability codes in column INT . refer to A T A Common
Support Data Dictionnary (CSDD), Chapter 2.
NOTE : Only the mixability configuration(s) and condition(s) stated in this Service Bulletin
are approved.
DA TE : May 25/05 SERVICE BULLETIN No. : A330-54-3022
REVISION No. : 01 - Jan 09/08 Page : 5
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### Page 12

A330
A330
SERVICE BULLETIN
This Page Intentionally Left Blank
DA TE : May 25/05 SERVICE BULLETIN No. : A330-54-3022
REVISION No. : 01 - Jan 09/08 Page : 6
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### Page 13

A330
A330
SERVICE BULLETIN
2. M ATERIAL INFORMATION
A. M ATERIAL - PRICE AND AVAILABILITY
(1) Material
Modification of removed equipment should be negotiated directly with PRA TT and
WHITNEY as per instructions given in Service Bulletin No. PW4G-100-A54-7.
(2) Price and Availability
Refer to the Vendor Service Bulletin No. PW4G-100-A54-7 for the equipment modification
sales terms.
B. I NDUSTRY SUPPORT INFORMATION
Refer to the Vendor Service Bulletin No. PW4G-100-A54-7 for the industry support terms.
C. L IST OF COMPONENTS
None
D. L IST OF MATERIALS - OPERATOR SUPPLIED
(1) Consumable Materials
None
(2) Components
ITEM NEW P ART No. QTY UM KEYWORD ITEM OLD P ART No. INT INST DISP
72A100-705 1 LAPF 72A100-501
72A100-503
72A100-505
72A100-507
72A100-509
72A100-511
72A100-513
72A100-701
72A100-703
01 (01)
NOTE : For definitions of interchangeability codes in column INT . refer to A T A Common
Support Data Dictionnary (CSDD), Chapter 2.
NOTE(01) Modification of removed equipment should be negotiated directly with PRA TT
and WHITNEY as per instructions given in Service Bulletin No. PW4G-100-A54-7
E. P ARTS TO BE RE-IDENTIFIED BY THE OPERATOR
None
DA TE : May 25/05 SERVICE BULLETIN No. : A330-54-3022
REVISION No. : 01 - Jan 09/08 Page : 7
Printed in France © AIRBUS 2007 All rights reserved

### Page 14

A330
A330
SERVICE BULLETIN
F. T OOLING - PRICE AND AVAILABILITY
None
G. S PECIAL TOOLS
T o accomplish this Service Bulletin it is necessary to use the tools listed in PRA TT and WHITNEY
Service Bulletin No. PW4G-100-A54-7.
DA TE : May 25/05 SERVICE BULLETIN No. : A330-54-3022
REVISION No. : 01 - Jan 09/08 Page : 8
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### Page 15

A330
A330
SERVICE BULLETIN
3. A CCOMPLISHMENT INSTRUCTIONS
A. G ENERAL
WARNING : MAKE SURE THA T Y OU OBEY ALL THE WARNINGS AND ALL THE CAUTIONS
INCLUDED IN THE REFERENCED PROCEDURES.
CAUTION : ALWA YS OBEY THE PRECAUTIONS THA T FOLLOW TO KEEP ELECTRICAL
WIRING IN A SA TISFACTORY CONDITION (ELECTRICALL Y AND MECHANICALL Y
SERVICEABLE). WHEN YOU DO MAINTENANCE WORK, REP AIRS OR
MODIFICA TIONS, 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.
- REGULARL Y REMOVE ALL SHAVINGS, UNWANTED MA TERIAL AND OTHER
CONT AMINA TION.
THESE PRECAUTIONS WILL DECREASE THE RISK OF CONT AMINA TION
AND DAMAGE TO THE ELECTRICAL WIRING INST ALLA TION.
IN CASE OF CONT AMINA TION REFER TO ESPM 20-55-00.
(1) Preparation
(a) Config. 01
1 Make sure that the aircraft is electrically grounded (Refer to AMM 12-34-24,
Page block 201).
2 Put the access platforms in position.
3 Do the preparation procedure as specified in the removal/installation of the lower
fairing (Refer to AMM 54-56-11, Page block 401).
(2) Standard Practices
None
B. M ODIFICATION
(1) Config. 01
NOTE : For LAPF modification, Refer to PRA TT and WHITNEY , Service Bulletin No.
PW4G-100-A54-7
NOTE : This paragraph describes the replacement of one LAPF . The job is identical
for both LAPF .
(a) Replace the Lower Aft Pylon Fairing Assies
(Refer to AMM 54-56-11, Page block 401)
1 Remove :
1 Lower Aft Pylon Fairing
Assy
72A100-501
DA TE : May 25/05 SERVICE BULLETIN No. : A330-54-3022
REVISION No. : 01 - Jan 09/08 Page : 9
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### Page 16

A330
A330
SERVICE BULLETIN
or
1 Lower Aft Pylon Fairing
Assy
72A100-503
or
1 Lower Aft Pylon Fairing
Assy
72A100-505
or
1 Lower Aft Pylon Fairing
Assy
72A100-507
or
1 Lower Aft Pylon Fairing
Assy
72A100-509
or
1 Lower Aft Pylon Fairing
Assy
72A100-511
or
1 Lower Aft Pylon Fairing
Assy
72A100-513
or
1 Lower Aft Pylon Fairing
Assy
72A100-701
or
1 Lower Aft Pylon Fairing
Assy
72A100-703
NOTE : The part number of the removed LAPF depends on the aircraft
configuration.
2 Install :
1 Lower Aft Pylon Fairing
Assy
72A100-705
C. T EST
(1) Config. 01
(a) Do the test procedure as specified in the removal/installation of the lower fairing
(Refer to AMM 54-56-11, Page block 401).
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REVISION No. : 01 - Jan 09/08 Page : 10
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### Page 17

A330
A330
SERVICE BULLETIN
D. C LOSE UP
(1) Config. 01
(a) Do the close-up procedure as specified in the removal/installation of the lower fairing
(Refer to AMM 54-56-11, Page block 401).
(b) Make sure that the work areas are clean and clear of tools and other items of
equipment.
(c) Restore the systems and the aircraft to normal operating conditions.
(d) Remove the access platforms.
(e) Disconnect the aircraft electrical ground-connection (Refer to AMM 12-34-24, Page
block 201).
E. D OCUMENTATION
Write in the applicable aircraft records that you have done all the work given in the Service Bulletin.
DA TE : May 25/05 SERVICE BULLETIN No. : A330-54-3022
REVISION No. : 01 - Jan 09/08 Page : 11
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A330
A330
SERVICE BULLETIN
This Page Intentionally Left Blank
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### Page 19

A330
A330
SERVICE BULLETIN
REPORTING SHEET
TITLE : NACELLES/PYLONS - LOWER FAIRING - MODIFY STRUCTURE A T LOWER AFT PYLON
FAIRING LEVEL FOR PW ENGINES
MODIFICA TION No. : 53623S18198
Please complete the appropriate item (A or B):
A - SB W ILL BE embodied .................................................................. YES/NO (if NO please comment)
If YES, aircraft concerned (as per SB effectivity by default) and planned dates (month/year) of embodiement:
.............................................................................................................................................................................
.............................................................................................................................................................................
B - SB H AS 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 : Advance data................................................................................... YES/NO
Or : Intermediate/T emporary 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 DIRECTORA TE
1 Rond Point Maurice Bellonte
31707 BLAGNAC CEDEX FRANCE
Attn: SDC32 T echnical 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.
DA TE : May 25/05 SERVICE BULLETIN No. : A330-54-3022
REVISION No. : 01 - Jan 09/08 Page : 1 of 1
Printed in France © AIRBUS 2007 All rights reserved

### Page 20

A330
A330
SERVICE BULLETIN
REPORTING QUALITY
TITLE : NACELLES/PYLONS - LOWER FAIRING - MODIFY STRUCTURE A T LOWER AFT PYLON
FAIRING LEVEL FOR PW ENGINES
MODIFICA TION No. : 53623S18198
Use this form to tell us what is your perception of the quality of this Service Bulletin.The reported data that you
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Planning Material Instructions
X Effectivity X Kit Content X Preparation
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DA TE : May 25/05 SERVICE BULLETIN No. : A330-54-3022
REVISION No. : 01 - Jan 09/08 Page : 1 of 1
Printed in France © AIRBUS 2007 All rights reserved

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