# Airbus Service Bulletin A330-53-3297

Copy: No revision named ("A330-53-3297 R00"), 96 pages: PDF https://openairdocs.org/files/sha256/49/ba/49baa1a217896d7af0a44e61c84c2000bdbf752c68e504a6a05dfbeb0cfc0471; text https://openairdocs.org/service-documents/airbus/a330-53-3297/file/49baa1a21789.md. Rights: © Airbus S.A.S. Filed by the FAA in regulations.gov docket FAA-2020-1135, the docket of AD 2020-26-18. Not covered by OpenAirDocs’ CC0 dedication.

## Details

- Manufacturer: [Airbus](https://openairdocs.org/service-documents/airbus.md)
- Type: Service bulletin (Service Bulletin)
- Number: A330-53-3297
- Page: https://openairdocs.org/service-documents/airbus/a330-53-3297

## Text (96 pages)

Rights: © Airbus S.A.S. Filed by the FAA in regulations.gov docket FAA-2020-1135, the docket of AD 2020-26-18. 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
REV 00 Jul 21/20 A330-53-3297
Page 1
CONF ALL
AIRBUS
2, ROND POINT EMILE DEWOITINE
31700 BLAGNAC
FRANCE
 
The content of this document is the property of Airbus. All rights including copyrights are reserved.
It is supplied in confidence and commercial security on its contents must be maintained.
It must not be used for any purpose other than that for which it is supplied, nor may information
contained in it be disclosed to unauthorized persons.
It must not be reproduced in whole or in part without permission in writing from the owners of the
copyright. Requests for reproduction of any data in this document and the media authorized for it must
be addressed to Airbus.
MANDATORY MANDATORY MANDATORY
ATA SYSTEM: 53
TITLE: FUSELAGE - CENTER FUSELAGE - INSPECTION A330 ON FILLET
FAIRING RODS DUE TO CORROSION ISSUE
MODIFICATION No.:
None

### Page 2

A330
SERVICE BULLETIN
SUMMARY
REV 00 Jul 21/20 A330-53-3297
Page 2
ATA SYSTEM: 53
TITLE: FUSELAGE - CENTER FUSELAGE - INSPECTION A330 ON FILLET
FAIRING RODS DUE TO CORROSION ISSUE
SUMMARY
This summary is for information only and is not approved for modification of the aircraft.
A. MODIFICATIONS
CONF 001
MODIFICATION CLASSIFICATION
MAJOR None
MINOR None
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.
CONF 002
MODIFICATION CLASSIFICATION
MAJOR None
MINOR None
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.
CONF ALL
B. REASON
(1) History
During quality inspection in Final Assembly Line (FAL), at the Wing/Fuselage Fillet
interface, evidence of black stains and white oxidation was seen on several areas of
adjustable rods. These adjustable rods are used to tune and close the Fillet Fairing
panels which provides the aerodynamic fairing between the wing and the fuselage.
It has been reported that there is chemical contamination due to the oil used during
the machining followed by insufficient cleaning inside the clevis, allowing corrosion to
develop in normal environmental conditions.
(2) Objective/Action
This Inspection Service Bulletin (ISB) is issued to perform one time visual inspection
with replacement of the adjustable rods (X3 per side on A330 CEO and X2 per side on
A330 NEO).
(3) Advantages
Accomplishment of this ISB will install new adjustable rods.
(4) Operational/Maintenance Consequences
None
C. GENERAL EVALUATION

### Page 3

A330
SERVICE BULLETIN
SUMMARY
REV 00 Jul 21/20 A330-53-3297
Page 3
EVALUATION TABLE
COMPLIANCE MANDATORY COST SAVING NO
A/C OPERATION
AFFECTED
NO VENDOR SB NO
CANCELS INSPECTION SB NO ETOPS AFFECTED NO
PAX COMFORT AFFECTED NO POTENTIAL AD YES
RELIABILITY AFFECTED NO STRUCTURAL LIFE EXTENSION NO
LIFE LIMIT NO LINE MAINTENANCE AFFECTED NO
NOTE: Service Bulletin must be accomplished.
D. MAINTENANCE CONFIGURATION
CONF 001
No specific aircraft maintenance configuration required.
CONF 002
No specific aircraft maintenance configuration required.
CONF ALL
E. MATERIAL PRICE INFORMATION
CONF 001
(1) General Visual Inspection and Replacement of the Fillet Fairing Rods on LH
and RH Sides
(a) T ask set A330-A-53-XX-3297-01000-93BA-A General Visual Inspection and
Replacement of the Fillet Fairing Rods on LH and RH Sides
MATERIAL PRICE INFORMATION TABLE
MATERIAL SET QTYPER A/C PRICE PER A/C MAIN PARTS
Components See SB See Note Rods, nuts, pin-cotters, wire-
lock
NOTE: Price information to be obtained from the given supplier.
CONF 002
(1) General Visual Inspection and Replacement of the Fillet Fairing Rods on LH
and RH Sides
(a) T ask set A330-A-53-XX-3297-01000-93BA-A General Visual Inspection and
Replacement of the Fillet Fairing Rods on LH and RH Sides
MATERIAL PRICE INFORMATION TABLE
MATERIAL SET QTYPER A/C PRICE PER A/C MAIN PARTS
Components See SB See Note Rods, nuts, pin-cotters, wire-
lock
NOTE: Price information to be obtained from the given supplier.
CONF ALL
F. APPLICABILITY

### Page 4

A330
SERVICE BULLETIN
SUMMARY
REV 00 Jul 21/20 A330-53-3297
Page 4
This Service Bulletin is applicable to this (these) operator(s):
12P AZU CHH CSN CSZ TAP
G. CONCURRENT REQUIREMENTS
None
H. NATURE OF THE WORK
CONF 001
(1) General Visual Inspection and Replacement of the Fillet Fairing Rods on LH
and RH Sides
(a) T ask set A330-A-53-XX-3297-01000-93BA-A General Visual Inspection and
Replacement of the Fillet Fairing Rods on LH and RH Sides
AIRCRAFT YES
EQUIPMENT NO
CONF 002
(1) General Visual Inspection and Replacement of the Fillet Fairing Rods on LH
and RH Sides
(a) T ask set A330-A-53-XX-3297-01000-93BA-A General Visual Inspection and
Replacement of the Fillet Fairing Rods on LH and RH Sides
AIRCRAFT YES
EQUIPMENT NO
CONF ALL
I. MANPOWER
CONF 001
(1) General Visual Inspection and Replacement of the Fillet Fairing Rods on LH
and RH Sides
(a) T ask set A330-A-53-XX-3297-01000-93BA-A General Visual Inspection and
Replacement of the Fillet Fairing Rods on LH and RH Sides
MANPOWER
TOTAL MAN-HOURS 7.50 h
ELAPSED TIME (HOURS) 2.25 h
CONF 002
(1) General Visual Inspection and Replacement of the Fillet Fairing Rods on LH
and RH Sides
(a) T ask set A330-A-53-XX-3297-01000-93BA-A General Visual Inspection and
Replacement of the Fillet Fairing Rods on LH and RH Sides
MANPOWER
TOTAL MAN-HOURS 6.50 h
ELAPSED TIME (HOURS) 2.25 h

### Page 5

A330
SERVICE BULLETIN
SUMMARY
Figure ICN-A330-A-53XX3297-A-FAPE3-015EV-A-001-01 SHEET 1/1
REV 00 Jul 21/20 A330-53-3297General Overview
Page 5
CONF ALL
J. GENERAL OVERVIEW
CONF 001
B
FWD FILLET FAIRING
FR39
UPPER FILLET FAIRING ROD TO BE INSPECTED
MIDDLE FILLET FAIRING ROD
LOWER FILLET FAIRING ROD
A
B
LH SHOWN
RH SYMMETRICAL
TO BE INSPECTED
TO BE INSPECTED
(Z621)
A
Z521
ICN-A330-A-53XX3297-A-FAPE3-015EV-A-001-01

### Page 6

A330
SERVICE BULLETIN
SUMMARY
Figure ICN-A330-A-53XX3297-A-FAPE3-015EY-A-001-01 SHEET 1/1
REV 00 Jul 21/20 A330-53-3297General Overview
Page 6
CONF 002
B
(Z621)
FWD FILLET FAIRING
FR39
UPPER FILLET FAIRING ROD TO BE INSPECTED
LOWER FILLET FAIRING ROD
A
B
LH SHOWN
RH SYMMETRICAL
TO BE INSPECTED
A
Z521
ICN-A330-A-53XX3297-A-FAPE3-015EY-A-001-01

### Page 7

A330
SERVICE BULLETIN
REV 00 Jul 21/20 A330-53-3297
Page 7
ATA SYSTEM: 53
TITLE: FUSELAGE - CENTER FUSELAGE - INSPECTION A330 ON FILLET
FAIRING RODS DUE TO CORROSION ISSUE
CONF ALL
1. PLANNING INFORMATION
A. APPLICABILITY
(1) Models
ON A/C 1891
330-243
ON A/C 1889, 1893, 1894, 1896, 1898, 1899
330-343
ON A/C 1895, 1897
330-941
CONF ALL
(2) Applicability by MSN
1889 1891 1893-1899
(3) MSN by configuration
CONF 001
MSN CONFIGURATION
1889 1891 1893 1894 1896 1898 1899 001
CONF 002
MSN CONFIGURATION
1895 1897 002
CONF ALL
(4) Configuration definition
CONF 001
Configuration 001
CONF 001 is applicable for all A330 Current Engine Option (CEO) aircraft listed
above.
CONF 002
Configuration 002
CONF 002 is applicable for all A330 New Engine Option (NEO) aircraft listed
above.
CONF ALL
B. CONCURRENT REQUIREMENTS
None
C. REASON

### Page 8

A330
SERVICE BULLETIN
REV 00 Jul 21/20 A330-53-3297
Page 8
(1) History
During quality inspection in Final Assembly Line (FAL), at the Wing/Fuselage Fillet
interface, evidence of black stains and white oxidation was seen on several areas of
adjustable rods. These adjustable rods are used to tune and close the Fillet Fairing
panels which provides the aerodynamic fairing between the wing and the fuselage.
It has been reported that there is chemical contamination due to the oil used during
the machining followed by insufficient cleaning inside the clevis, allowing corrosion to
develop in normal environmental conditions.
(2) Objective/Action
This Inspection Service Bulletin (ISB) is issued to perform one time visual inspection
with replacement of the adjustable rods (X3 per side on A330 CEO and X2 per side on
A330 NEO).
(3) Advantages
Accomplishment of this ISB will install new adjustable rods.
(4) Operational/Maintenance Consequences
None
D. DESCRIPTION
T o accomplish this Service Bulletin it is necessary to:
(1) General Visual Inspection and Replacement of the Fillet Fairing Rods on LH
and RH Sides
(a) T ask set A330-A-53-XX-3297-01000-93BA-A General Visual Inspection and
Replacement of the Fillet Fairing Rods on LH and RH Sides
CONF 001
1 Inspect the Fillet Fairing Rods on the LH Side
CONF 002
1 Inspect the Fillet Fairing Rods on the LH Side
CONF 001
2 Inspect the Fillet Fairing Rods on the RH Side
CONF 002
2 Inspect the Fillet Fairing Rods on the RH Side
CONF 001
3 Replace the Upper Rod on the LH Side
CONF 002
3 Replace the Upper Rod on the LH Side
CONF 001
4 Replace the Middle Rod on the LH Side
5 Replace the Lower Rod on the LH Side
CONF 002
5 Replace the Lower Rod on the LH Side
CONF 001
6 Replace the Upper Rod on the RH Side
CONF 002
6 Replace the Upper Rod on the RH Side
CONF 001

### Page 9

A330
SERVICE BULLETIN
REV 00 Jul 21/20 A330-53-3297
Page 9
7 Replace the Middle Rod on the RH Side
8 Replace the Lower Rod on the RH Side
CONF 002
8 Replace the Lower Rod on the RH Side
CONF ALL
E. COMPLIANCE
(1) Classification
MANDATORY: Service Bulletin must be accomplished.
(2) Accomplishment Timescale
Accomplishment of this Service Bulletin must be done in accordance with the
threshold given in the table below.
This Service Bulletin has been classified Mandatory. It is expected that an
Airworthiness Directive (AD) published by the European Union Aviation Safety Agency
(EASA) will be issued to confirm this classification. It is anticipated that the AD will
confirm the (thresholds and/or intervals and/or date) given but reference should be
made to the AD for confirmation of the mandated accomplishment timescale.
COMPLIANCE TIME
CONDITIONS ACTION
THRESHOLD GRACE PERIOD
REPETITIVE
INTERVAL
All Aircraft Inspect the fillet
fairing rods
part numbers
Before exceeding
24 months since
the aircraft Date
of Manufacture
(DMF)
None None
The part
numbers
are affected
Replace the
fillet fairing rods
Before exceeding
24 months since
the aircraft DMF
None None
No further action None None None
The part
numbers are
not affected
Contact AIRBUS Before next flight None None
No further action None None None
F. APPROVAL
The technical content of this document is approved under the authority of the Design
Organisation Approval ref. EASA.21J.031.
If an aircraft listed in the applicability 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
CONF 001
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.

### Page 10

A330
SERVICE BULLETIN
REV 00 Jul 21/20 A330-53-3297
Page 10
(1) General Visual Inspection and Replacement of the Fillet Fairing Rods on LH
and RH Sides
(a) T ask set A330-A-53-XX-3297-01000-93BA-A General Visual Inspection and
Replacement of the Fillet Fairing Rods on LH and RH Sides
PREPARATION
Job Set-up for the LH Side 1.00 h
Job Set-up for the RH Side 1.00 h
PROCEDURE
Inspect the Fillet Fairing Rods on the LH Side 0.25 h
Inspect the Fillet Fairing Rods on the RH Side 0.25 h
Replace the Upper Rod on the LH Side 0.50 h
Replace the Middle Rod on the LH Side 0.50 h
Replace the Lower Rod on the LH Side 0.50 h
Replace the Upper Rod on the RH Side 0.50 h
Replace the Middle Rod on the RH Side 0.50 h
Replace the Lower Rod on the RH Side 0.50 h
PREPARATION FOR TEST
None
TEST
None
CLOSE-UP
Close-up for the LH Side 1.00 h
Close-up for the RH Side 1.00 h
TOTAL MAN-HOURS 7.50 h
ELAPSED TIME (HOURS) 2.25 h
NOTE: The minimum man-hours necessary to accomplish this Service Bulletin
are those for the Inspection. Depending on the inspection result,
additional man-hours can apply.
CONF 002
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.
(1) General Visual Inspection and Replacement of the Fillet Fairing Rods on LH
and RH Sides
(a) T ask set A330-A-53-XX-3297-01000-93BA-A General Visual Inspection and
Replacement of the Fillet Fairing Rods on LH and RH Sides
PREPARATION
Job Set-up for the LH Side 1.00 h
Job Set-up for the RH Side 1.00 h
PROCEDURE
Inspect the Fillet Fairing Rods on the LH Side 0.25 h

### Page 11

A330
SERVICE BULLETIN
REV 00 Jul 21/20 A330-53-3297
Page 11
Inspect the Fillet Fairing Rods on the RH Side 0.25 h
Replace the Upper Rod on the LH Side 0.50 h
Replace the Lower Rod on the LH Side 0.50 h
Replace the Upper Rod on the RH Side 0.50 h
Replace the Lower Rod on the RH Side 0.50 h
PREPARATION FOR TEST
None
TEST
None
CLOSE-UP
Close-up for the LH Side 1.00 h
Close-up for the RH Side 1.00 h
TOTAL MAN-HOURS 6.50 h
ELAPSED TIME (HOURS) 2.25 h
NOTE: The minimum man-hours necessary to accomplish this Service Bulletin
are those for the Inspection. Depending on the inspection result,
additional man-hours can apply.
CONF ALL
H. WEIGHT AND BALANCE
Not changed
I. ELECTRICAL LOAD DATA
Not changed
J. REFERENCES
CONF 001
(1) General Visual Inspection and Replacement of the Fillet Fairing Rods on LH
and RH Sides
(a) T ask set A330-A-53-XX-3297-01000-93BA-A General Visual Inspection and
Replacement of the Fillet Fairing Rods on LH and RH Sides
AIRCRAFT MAINTENANCE MANUAL (AMM)
06-20-00, Page Block 001 06-31-53, Page Block 001
T ask 12-34-24-860-802 20-11-11, Page Block 201
T ask 20-11-11-911-803
T ask 20-21-15-912-801 T ask 53-35-11-000-802
T ask 53-35-11-400-802
ELECTRICAL STANDARD PRACTICES MANUAL (ESPM)
20-55-00
STRUCTURAL REPAIR MANUAL (SRM)
51-24-00 51-40-00
51-42-00 51-43-00

### Page 12

A330
SERVICE BULLETIN
REV 00 Jul 21/20 A330-53-3297
Page 12
TECHNICAL FOLLOW UP (TFU)
53.35.00036
STANDARDS MANUAL (SM)
CONSUMABLE MATERIAL LIST (CML)
CONF 002
(1) General Visual Inspection and Replacement of the Fillet Fairing Rods on LH
and RH Sides
(a) T ask set A330-A-53-XX-3297-01000-93BA-A General Visual Inspection and
Replacement of the Fillet Fairing Rods on LH and RH Sides
AIRCRAFT MAINTENANCE MANUAL (AMM)
06-20-00, Page Block 001 06-31-53, Page Block 001
T ask 12-34-24-860-802 20-11-11, Page Block 201
T ask 20-11-11-911-803
T ask 20-21-15-912-801 T ask 53-35-11-000-802
T ask 53-35-11-400-802
ELECTRICAL STANDARD PRACTICES MANUAL (ESPM)
20-55-00
STRUCTURAL REPAIR MANUAL (SRM)
51-24-00 51-40-00
51-42-00 51-43-00
TECHNICAL FOLLOW UP (TFU)
53.35.00036
STANDARDS MANUAL (SM)
CONSUMABLE MATERIAL LIST (CML)
CONF ALL
K. PUBLICATION AFFECTED
None
L. INDUSTRY SUPPORT INFORMATION
AIRBUS will credit the man-hours indicated in this Service Bulletin for inspections that are
performed on aircraft in warranty at the time of such inspection. Credit will be at the agreed
in-house warranty labor rate. Claims for labor allowance should be received not later than
90 days after completion of the last affected warranted aircraft.
For those aircraft in warranty at the time of such inspection with findings further to
inspection as per this Service Bulletin, in case of findings, AIRBUS will share the costs of
accomplishment of this Service Bulletin by crediting the operator supplied AIRBUS parts for
orders placed within 24 months after the initial issue date of the Service Bulletin. Claims for
this allowance should be received no later than 90 days after completion of the last affected
aircraft of your fleet.
For those aircraft in warranty at the time of such inspection with findings further to
inspection as per this Service Bulletin, for the accomplishment of this Service Bulletin within
24 months after the initial issue date of the Service Bulletin, AIRBUS will share the costs by

### Page 13

A330
SERVICE BULLETIN
REV 00 Jul 21/20 A330-53-3297
Page 13
crediting the operator supplied standard hardware parts. Claims for this allowance should
be received no later than 90 days after completion of the last affected aircraft of your fleet.
For those aircraft in warranty at the time of such inspection with findings further to
inspection as per this Service Bulletin, AIRBUS will credit the man-hours indicated in this
Service Bulletin for corrections that are performed on aircraft in warranty at the time of
such correction. Credit will be at the agreed in-house warranty labor rate. Claims for labor
allowance should be received not later than 90 days after completion of the last affected
warranted aircraft.
This Service Bulletin is the subject of an AIRBUS monitored retrofit campaign.
For the organization of this retrofit, you are kindly requested to contact AIRBUS retrofit
management department: monitored.retrofit@airbus.com.

### Page 14

A330
SERVICE BULLETIN
REV 00 Jul 21/20 A330-53-3297
Page 14
2. MATERIAL INFORMATION
A. MATERIAL APPLICABILITY
CONF 001
Material for task set A330-A-53-XX-3297-01000-93BA-A General Visual Inspection
and Replacement of the Fillet Fairing Rods on LH and RH Sides
MATERIAL QTY SEE NOTES
Consumables See SB
Referenced consumables See SB
Components See SB
CONF 002
Material for task set A330-A-53-XX-3297-01000-93BA-A General Visual Inspection
and Replacement of the Fillet Fairing Rods on LH and RH Sides
MATERIAL QTY SEE NOTES
Consumables See SB
Referenced consumables See SB
Components See SB
CONF ALL
B. TOOLING
No tools
C. CONSUMABLES
CONF 001
Consumables for task set A330-A-53-XX-3297-01000-93BA-A General Visual
Inspection and Replacement of the Fillet Fairing Rods on LH and RH Sides
ITEM REFERENCE CML DESCRIPTION DRAWING SEE NOTES
06AAA1 Polysulfide Sealant -General Purpose Brushable
CONF 002
Consumables for task set A330-A-53-XX-3297-01000-93BA-A General Visual
Inspection and Replacement of the Fillet Fairing Rods on LH and RH Sides
ITEM REFERENCE CML DESCRIPTION DRAWING SEE NOTES
06AAA1 Polysulfide Sealant -General Purpose Brushable
CONF 001
Referenced consumables for task set A330-A-53-XX-3297-01000-93BA-A General
Visual Inspection and Replacement of the Fillet Fairing Rods on LH and RH Sides
T o accomplish this Service Bulletin it is necessary to use the consumables listed in:
Ref. AMM T ask 53-35-11-400-802
CONF 002
Referenced consumables for task set A330-A-53-XX-3297-01000-93BA-A General
Visual Inspection and Replacement of the Fillet Fairing Rods on LH and RH Sides
T o accomplish this Service Bulletin it is necessary to use the consumables listed in:
Ref. AMM T ask 53-35-11-400-802

### Page 15

A330
SERVICE BULLETIN
REV 00 Jul 21/20 A330-53-3297
Page 15
CONF ALL
D. LIST OF NEW PARTS
CONF 001
Components for task set A330-A-53-XX-3297-01000-93BA-A General Visual
Inspection and Replacement of the Fillet Fairing Rods on LH and RH Sides
Procurement address
D4296
AIRBUS Material, Logistics and Suppliers
Customer Order Fulfilment
Weg beim Jaeger 150
D-22335 HAMBURG
GERMANY
Phone: +49 (0) 40 50 76 40 02
E-mail: Please contact your Single Point Of Contact
(SPOC)
Internet: http://spares.airbus.com
D4296
AIRBUS Material, Logistics and Suppliers Standard
Parts
Customer Order Fulfilment
Phone: +49 (0) 40 50 76 40 02
E-mail: Please contact your Single Point Of Contact
(SPOC)
Internet: http://spares.airbus.com or via SPEC2000
NOTE(S)
Customers with aircraft shown in the applicability of this Service Bulletin should send
a purchase order to AIRBUS at the address given above and quote the number of this
Service Bulletin.
For standard hardware the purchase order must be addressed to AIRBUS at the
address given above. Quote the number of this Service Bulletin, the MSN and, if
applicable the Retrofit Information Letter (RIL) reference.
ITEM PART No. QTY (UM) KEYWORD DRAWING SEE NOTES
1 F5335002000000(D4296) 2 ROD (1) (2) (3)
2 F5335001900000(D4296) 2 ROD (1) (2) (3)
3 F5335001900200(D4296) 2 ROD (1) (2) (3)
6 NSA5060-6 (D4296) 12 NUT (1) (2) (4)
7 MS20995C32(D4296) 3 (m) WIRE (1) (2) (4)
11 MS24665-300(D4296) 12 PIN (1) (2) (4)
NOTE(S)
Refer to the AIRBUS Ref. SM if you find part numbers of hardware components which
you cannot identify. The SM will give you the correct part number to part number
relationship.
(1): The components listed above are not an AIRBUS Kit, the required parts must be
ordered as necessary through the given channel.
(2): The components listed above are only necessary if after the inspection the affected
rods part numbers are installed. The quantity of these items is to be ordered as
required.

### Page 16

A330
SERVICE BULLETIN
REV 00 Jul 21/20 A330-53-3297
Page 16
ITEM PART No. QTY (UM) KEYWORD DRAWING SEE NOTES
(3): Operator supplied AIRBUS parts required to accomplish this Service Bulletin are to be
purchased by a spares purchase order.
(4): Operator supplied standard hardware parts, required to accomplish this Service
Bulletin, are to be supplied from the operator's stock.
CONF 002
Components for task set A330-A-53-XX-3297-01000-93BA-A General Visual
Inspection and Replacement of the Fillet Fairing Rods on LH and RH Sides
Procurement address
D4296
AIRBUS Material, Logistics and Suppliers
Customer Order Fulfilment
Weg beim Jaeger 150
D-22335 HAMBURG
GERMANY
Phone: +49 (0) 40 50 76 40 02
E-mail: Please contact your Single Point Of Contact
(SPOC)
Internet: http://spares.airbus.com
D4296
AIRBUS Material, Logistics and Suppliers Standard
Parts
Customer Order Fulfilment
Phone: +49 (0) 40 50 76 40 02
E-mail: Please contact your Single Point Of Contact
(SPOC)
Internet: http://spares.airbus.com or via SPEC2000
NOTE(S)
Customers with aircraft shown in the applicability of this Service Bulletin should send
a purchase order to AIRBUS at the address given above and quote the number of this
Service Bulletin.
For standard hardware the purchase order must be addressed to AIRBUS at the
address given above. Quote the number of this Service Bulletin, the MSN and, if
applicable the Retrofit Information Letter (RIL) reference.
ITEM PART No. QTY (UM) KEYWORD DRAWING SEE NOTES
7 MS20995C32(D4296) 2 (m) WIRE (1) (2) (3)
11 MS24665-300(D4296) 8 PIN (1) (2) (3)
12 F0005579700400(D4296) 2 ROD (1) (2) (4)
13 F0005579700200(D4296) 2 ROD (1) (2) (4)
15 NSA5060E6 (D4296) 8 NUT (1) (2) (3)
NOTE(S)
Refer to the AIRBUS Ref. SM if you find part numbers of hardware components which
you cannot identify. The SM will give you the correct part number to part number
relationship.
(1): The components listed above are not an AIRBUS Kit, the required parts must be
ordered as necessary through the given channel.

### Page 17

A330
SERVICE BULLETIN
REV 00 Jul 21/20 A330-53-3297
Page 17
ITEM PART No. QTY (UM) KEYWORD DRAWING SEE NOTES
(2): The components listed above are only necessary if after the inspection the affected
rods part numbers are installed. The quantity of these items is to be ordered as
required.
(3): Operator supplied standard hardware parts, required to accomplish this Service
Bulletin, are to be supplied from the operator's stock.
(4): Operator supplied AIRBUS parts required to accomplish this Service Bulletin are to be
purchased by a spares purchase order.
CONF ALL
E. LIST OF EXISTING PARTS
No parts

### Page 18

A330
SERVICE BULLETIN
REV 00 Jul 21/20 A330-53-3297
Page 18
3. ACCOMPLISHMENT INSTRUCTIONS
Task set A330-A-53-XX-3297-01000-93BA-A
General Visual Inspection and Replacement of the Fillet Fairing Rods on LH and RH Sides
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 A 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.
IF THERE IS CONTAMINATION, REFER TO Ref. ESPM 20-55-00.
NOTE: The accomplishment instructions of this Service Bulletin include procedures given in
other documents or in other sections of the Service Bulletin. When the words “refer to”
are used and the operator has a procedure accepted by the local authority he belongs to,
the accepted alternative procedure can be used. When the words “in accordance with”
are used then the given procedure must be followed.
NOTE: The access and close-up instructions, not comprising return to service tests, in this
Service Bulletin do not constitute or affect the technical intent of the Service Bulletin.
Operators can therefore, as deemed necessary, omit or add access and/or close-up steps
to add flexibility to their maintenance operations as long as the technical intent of the
Service Bulletin is met within the set parameters.
NOTE: Manual titles given in the accomplishment instructions are referred to by acronyms. Refer
to paragraph 1.J., References, for the definition of acronyms.
NOTE: The purpose of flowcharts is to supplement the information given in the Procedure and
Compliance paragraphs and not to serve as the primary source for tasks or compliance
times given in this Service Bulletin.
NOTE: This Service Bulletin is classified mandatory or expected to be classified mandatory by
an Airworthiness Directive (AD). The paragraphs 3.C. and 3.E. in these accomplishment
instructions are Required for Compliance (RC) and must be done to comply with the AD.
T o allow more flexibility, the rule "refer to" and "in accordance with" will apply to these
paragraphs 3.C. and 3.E. Other paragraphs are recommended and may be deviated from,
done as part of other actions or done with accepted methods different from those given
in the Service Bulletin, as long as the RC paragraphs can be done and the aircraft can be
put back into a serviceable condition.
NOTE: This Service Bulletin contains the instructions for the on-aircraft maintenance necessary
to ensure the continued airworthiness of the aircraft.
For any deviations to the instructions, including Required for Compliance paragraph
contained herein, contact AIRBUS for further instructions and approval.
NOTE: Discarded parts must be managed at the operator's discretion.
A. TASK SET ASSOCIATED INFORMATION
Task Manpower

### Page 19

A330
SERVICE BULLETIN
REV 00 Jul 21/20 A330-53-3297
Page 19
CONF 001
TOTAL MAN-HOURS 7.50 h
CONF 002
TOTAL MAN-HOURS 6.50 h
CONF 001
ELAPSED TIME (HOURS) 2.25 h
CONF 002
ELAPSED TIME (HOURS) 2.25 h
CONF ALL
B. PREPARATION
(1) Task A330-A-53-XX-3297-01001-540A-A - Job Set-up for the LH Side
Job Set-Up Information
Manpower/Resources/Skills
Man-hours 1.00 h
Minimum Number of person 1
Elapsed Time 1.00 h
Skills Airframe
Referenced Information
Manuals/Drawings References/Sheets
AMM T ask 12-34-24-860-802T ask 53-35-11-000-802
Procedure
NOTE: For the basic Aircraft configuration, refer to AMM Chapter “Introduction -
Aircraft status for maintenance" in Manual Front Matter section.
(a) Make sure that the aircraft is electrically grounded, refer to Ref. AMM T ask 12-34-
24-860-802
(b) Put an access platform in position in zone 190.
(c) Remove the FWD fillet fairing for access on the LH side, refer to Ref. AMM T ask
53-35-11-000-802.
(2) Task A330-A-53-XX-3297-02001-540A-A - Job Set-up for the RH Side
Job Set-Up Information
Manpower/Resources/Skills
Man-hours 1.00 h
Minimum Number of person 1
Elapsed Time 1.00 h
Skills Airframe
Referenced Information
Manuals/Drawings References/Sheets
AMM T ask 12-34-24-860-802T ask 53-35-11-000-802
Procedure

### Page 20

A330
SERVICE BULLETIN
REV 00 Jul 21/20 A330-53-3297
Page 20
NOTE: For the basic Aircraft configuration, refer to AMM Chapter “Introduction -
Aircraft status for maintenance" in Manual Front Matter section.
(a) Make sure that the aircraft is electrically grounded, refer to Ref. AMM T ask 12-34-
24-860-802
(b) Put an access platform in position in zone 190.
(c) Remove the FWD fillet fairing for access on the RH side, refer to Ref. AMM T ask
53-35-11-000-802.
C. PROCEDURE
CONF 001
(1) Task A330-A-53-XX-3297-01001-311A-A - Inspect the Fillet Fairing Rods on
the LH Side
Job Set-Up Information
Working Area
Impacted Zone Access / Work Location
521
Manpower/Resources/Skills
Man-hours 0.25 h
Minimum Number of person 1
Elapsed Time 0.25 h
Skills Airframe
Referenced Information
Manuals/Drawings References/Sheets
AMM 06-20-00, Page Block 00106-31-53, Page Block 001
Procedure
(a) Standard practices:
1 For the identification of zones refer to Ref. AMM 06-20-00, Page Block 001.
2 For the identification of frames refer to Ref. AMM 06-31-53, Page Block 001.
(b) At the threshold given in the PLANNING INFORMATION paragraph E.(2):
Inspect the part numbers of the upper, middle and lower fillet fairing rods at
Frame 39, refer to Ref. Fig. Flow Chart and Ref. Fig. Inspection of the Fillet Fairing
Rods on the LH Side.
1 If the part numbers installed are F5335002000000, F5335001900000, and
F5335001900200:
a Replace the upper fillet fairing rod, refer to Ref. T ask A330-A-53-XX-
3297-01ZZZ-920Z-A.
b Replace the middle fillet fairing rod, refer to Ref. T ask A330-A-53-XX-
3297-02ZZZ-920Z-A.
c Replace the lower fillet fairing rod, refer to Ref. T ask A330-A-53-XX-
3297-03ZZZ-920Z-A.
NOTE: Make sure that all rods are inspected before the
replacement.

### Page 21

A330
SERVICE BULLETIN
REV 00 Jul 21/20 A330-53-3297
Page 21
CAUTION: RODS MUST BE REPLACED ONE AT A TIME.
d No further action.
2 If the part numbers installed are not F5335002000000, F5335001900000,
and/or F5335001900200:
a Contact AIRBUS.

### Page 22

A330
SERVICE BULLETIN
Figure ICN-A330-A-53XX3297-A-FAPE3-015EW-A-001-01 SHEET 1/1
REV 00 Jul 21/20 A330-53-3297Flow Chart
Page 22
CONF 001
MIDDLE AND LOWER FILLET FAIRING RODS
01
INSPECT THE PART NUMBERS OF THE UPPER,
NOTE:
THE PURPOSE OF FLOWCHARTS IS TO SUPPLEMENT THE INFORMATION GIVEN IN THE PROCEDURE
AND COMPLIANCE PARAGRAPHS AND NOT TO SERVE AS THE PRIMARY SOURCE FOR TASKS OR
COMPLIANCE TIMES GIVEN IN THE SERVICE BULLETIN.
FOR THE ACCOMPLISHMENT TIMESCALE, REFER TO PARAGRAPH 1.E.(2).01
YES NO
CONTACT AIRBUS
01
NO FURTHER ACTION
F5335002000000, F5335001900000
ARE THE PART NUMBERS
AND F5335001900200?
REPLACE THE THREE FILLET
01
NO FURTHER ACTION
FAIRING RODS
ICN-A330-A-53XX3297-A-FAPE3-015EW-A-001-01

### Page 23

A330
SERVICE BULLETIN
Figure ICN-A330-A-53XX3297-A-FAPE3-015EZ-A-001-01 SHEET 1/1
REV 00 Jul 21/20 A330-53-3297Inspection of the Fillet Fairing Rods on the LH Side
Page 23
CONF 001
B
FWD FILLET FAIRING
FR39
UPPER FILLET FAIRING ROD
MIDDLE FILLET FAIRING ROD
LOWER FILLET FAIRING ROD
A
B
AREA OF INSPECTION.
NOTE:
A
Z521
ICN-A330-A-53XX3297-A-FAPE3-015EZ-A-001-01

### Page 24

A330
SERVICE BULLETIN
REV 00 Jul 21/20 A330-53-3297
Page 24
CONF 002
(1) Task A330-A-53-XX-3297-01002-311A-A - Inspect the Fillet Fairing Rods on
the LH Side
Job Set-Up Information
Working Area
Impacted Zone Access / Work Location
521
Manpower/Resources/Skills
Man-hours 0.25 h
Minimum Number of person 1
Elapsed Time 0.25 h
Skills Airframe
Referenced Information
Manuals/Drawings References/Sheets
AMM 06-20-00, Page Block 00106-31-53, Page Block 001
Procedure
(a) Standard practices:
1 For the identification of zones refer to Ref. AMM 06-20-00, Page Block 001.
2 For the identification of frames refer to Ref. AMM 06-31-53, Page Block 001.
(b) At the threshold given in the PLANNING INFORMATION paragraph E.(2):
Inspect the part numbers of the upper and lower fillet fairing rods at Frame 39,
refer to Ref. Fig. Flow Chart and Ref. Fig. Inspection of the Fillet Fairing Rods on
the LH Side.
1 If the part numbers installed are F0005579700400 and F0005579700200:
a Replace the upper fillet fairing rod, refer to Ref. T ask A330-A-53-XX-
3297-01ZZZ-920Z-A.
b Replace the lower fillet fairing rod, refer to Ref. T ask A330-A-53-XX-
3297-03ZZZ-920Z-A.
NOTE: Make sure that all rods are inspected before the
replacement.
CAUTION: RODS MUST BE REPLACED ONE AT A TIME.
c No further action.
2 If the part numbers installed are not F0005579700400 and/or
F0005579700200:
a Contact AIRBUS.

### Page 25

A330
SERVICE BULLETIN
Figure ICN-A330-A-53XX3297-A-FAPE3-015EU-A-001-01 SHEET 1/1
REV 00 Jul 21/20 A330-53-3297Flow Chart
Page 25
CONF 002
AND LOWER FILLET FAIRING RODS
01
INSPECT THE PART NUMBERS OF THE UPPER,
NOTE:
THE PURPOSE OF FLOWCHARTS IS TO SUPPLEMENT THE INFORMATION GIVEN IN THE PROCEDURE
AND COMPLIANCE PARAGRAPHS AND NOT TO SERVE AS THE PRIMARY SOURCE FOR TASKS OR
COMPLIANCE TIMES GIVEN IN THE SERVICE BULLETIN.
FOR THE ACCOMPLISHMENT TIMESCALE, REFER TO PARAGRAPH 1.E.(2).01
YES NO
CONTACT AIRBUS
01
NO FURTHER ACTION
REPLACE THE TWO FILLET
01
NO FURTHER ACTION
FAIRING RODS
F0005579700400 AND
ARE THE PART NUMBERS
F0005579700200?
ICN-A330-A-53XX3297-A-FAPE3-015EU-A-001-01

### Page 26

A330
SERVICE BULLETIN
Figure ICN-A330-A-53XX3297-A-FAPE3-015EX-A-001-01 SHEET 1/1
REV 00 Jul 21/20 A330-53-3297Inspection of the Fillet Fairing Rods on the LH Side
Page 26
CONF 002
B
FWD FILLET FAIRING
FR39
UPPER FILLET FAIRING ROD
LOWER FILLET FAIRING ROD
A
B
AREA OF INSPECTION.
NOTE:
A
Z521
ICN-A330-A-53XX3297-A-FAPE3-015EX-A-001-01

### Page 27

A330
SERVICE BULLETIN
REV 00 Jul 21/20 A330-53-3297
Page 27
CONF 001
(2) Task A330-A-53-XX-3297-04001-311A-A - Inspect the Fillet Fairing Rods on
the RH Side
Job Set-Up Information
Working Area
Impacted Zone Access / Work Location
621
Manpower/Resources/Skills
Man-hours 0.25 h
Minimum Number of person 1
Elapsed Time 0.25 h
Skills Airframe
Referenced Information
Manuals/Drawings References/Sheets
AMM 06-20-00, Page Block 00106-31-53, Page Block 001
Procedure
(a) Standard practices:
1 For the identification of zones refer to Ref. AMM 06-20-00, Page Block 001.
2 For the identification of frames refer to Ref. AMM 06-31-53, Page Block 001.
(b) At the threshold given in the PLANNING INFORMATION paragraph E.(2):
Inspect the part numbers of the upper, middle and lower fillet fairing rods at
Frame 39, refer to Ref. Fig. Flow Chart and Ref. Fig. Inspection of the Fillet Fairing
Rods on the RH Side.
1 If the part numbers installed are F5335002000000, F5335001900000, and
F5335001900200:
a Replace the upper fillet fairing rod, refer to Ref. T ask A330-A-53-XX-
3297-04ZZZ-920Z-A.
b Replace the middle fillet fairing rod, refer to Ref. T ask A330-A-53-XX-
3297-05ZZZ-920Z-A.
c Replace the lower fillet fairing rod, refer to Ref. T ask A330-A-53-XX-
3297-06ZZZ-920Z-A.
NOTE: Make sure that all rods are inspected before the
replacement.
CAUTION: RODS MUST BE REPLACED ONE AT A TIME.
d No further action.
2 If the part numbers installed are not F5335002000000, F5335001900000,
and/or F5335001900200:
a Contact AIRBUS.

### Page 28

A330
SERVICE BULLETIN
Figure ICN-A330-A-53XX3297-A-FAPE3-015EW-A-001-01 SHEET 1/1
REV 00 Jul 21/20 A330-53-3297Flow Chart
Page 28
CONF 001
MIDDLE AND LOWER FILLET FAIRING RODS
01
INSPECT THE PART NUMBERS OF THE UPPER,
NOTE:
THE PURPOSE OF FLOWCHARTS IS TO SUPPLEMENT THE INFORMATION GIVEN IN THE PROCEDURE
AND COMPLIANCE PARAGRAPHS AND NOT TO SERVE AS THE PRIMARY SOURCE FOR TASKS OR
COMPLIANCE TIMES GIVEN IN THE SERVICE BULLETIN.
FOR THE ACCOMPLISHMENT TIMESCALE, REFER TO PARAGRAPH 1.E.(2).01
YES NO
CONTACT AIRBUS
01
NO FURTHER ACTION
F5335002000000, F5335001900000
ARE THE PART NUMBERS
AND F5335001900200?
REPLACE THE THREE FILLET
01
NO FURTHER ACTION
FAIRING RODS
ICN-A330-A-53XX3297-A-FAPE3-015EW-A-001-01

### Page 29

A330
SERVICE BULLETIN
Figure ICN-A330-A-53XX3297-A-FAPE3-015FB-A-001-01 SHEET 1/1
REV 00 Jul 21/20 A330-53-3297Inspection of the Fillet Fairing Rods on the RH Side
Page 29
CONF 001
AREA OF INSPECTION.
NOTE: FR39
UPPER FILLET FAIRING ROD
MIDDLE FILLET FAIRING ROD
LOWER FILLET FAIRING ROD
A
B
FWD FILLET FAIRING
Z621
A
B
ICN-A330-A-53XX3297-A-FAPE3-015FB-A-001-01

### Page 30

A330
SERVICE BULLETIN
REV 00 Jul 21/20 A330-53-3297
Page 30
CONF 002
(2) Task A330-A-53-XX-3297-04002-311A-A - Inspect the Fillet Fairing Rods on
the RH Side
Job Set-Up Information
Working Area
Impacted Zone Access / Work Location
621
Manpower/Resources/Skills
Man-hours 0.25 h
Minimum Number of person 1
Elapsed Time 0.25 h
Skills Airframe
Referenced Information
Manuals/Drawings References/Sheets
AMM 06-20-00, Page Block 00106-31-53, Page Block 001
Procedure
(a) Standard practices:
1 For the identification of zones refer to Ref. AMM 06-20-00, Page Block 001.
2 For the identification of frames refer to Ref. AMM 06-31-53, Page Block 001.
(b) At the threshold given in the PLANNING INFORMATION paragraph E.(2):
Inspect the part numbers of the upper and lower fillet fairing rods at Frame 39,
refer to Ref. Fig. Flow Chart and Ref. Fig. Inspection of the Fillet Fairing Rods on
the RH Side.
1 If the part numbers installed are F0005579700400 and F0005579700200:
a Replace the upper fillet fairing rod, refer to Ref. T ask A330-A-53-XX-
3297-04ZZZ-920Z-A.
b Replace the lower fillet fairing rod, refer to Ref. T ask A330-A-53-XX-
3297-06ZZZ-920Z-A.
NOTE: Make sure that all rods are inspected before the
replacement.
CAUTION: RODS MUST BE REPLACED ONE AT A TIME.
c No further action.
2 If the part numbers installed are not F0005579700400 and/or
F0005579700200:
a Contact AIRBUS.

### Page 31

A330
SERVICE BULLETIN
Figure ICN-A330-A-53XX3297-A-FAPE3-015EU-A-001-01 SHEET 1/1
REV 00 Jul 21/20 A330-53-3297Flow Chart
Page 31
CONF 002
AND LOWER FILLET FAIRING RODS
01
INSPECT THE PART NUMBERS OF THE UPPER,
NOTE:
THE PURPOSE OF FLOWCHARTS IS TO SUPPLEMENT THE INFORMATION GIVEN IN THE PROCEDURE
AND COMPLIANCE PARAGRAPHS AND NOT TO SERVE AS THE PRIMARY SOURCE FOR TASKS OR
COMPLIANCE TIMES GIVEN IN THE SERVICE BULLETIN.
FOR THE ACCOMPLISHMENT TIMESCALE, REFER TO PARAGRAPH 1.E.(2).01
YES NO
CONTACT AIRBUS
01
NO FURTHER ACTION
REPLACE THE TWO FILLET
01
NO FURTHER ACTION
FAIRING RODS
F0005579700400 AND
ARE THE PART NUMBERS
F0005579700200?
ICN-A330-A-53XX3297-A-FAPE3-015EU-A-001-01

### Page 32

A330
SERVICE BULLETIN
Figure ICN-A330-A-53XX3297-A-FAPE3-015FC-A-001-01 SHEET 1/1
REV 00 Jul 21/20 A330-53-3297Inspection of the Fillet Fairing Rods on the RH Side
Page 32
CONF 002
AREA OF INSPECTION.
NOTE:
FR39
UPPER FILLET FAIRING ROD
LOWER FILLET FAIRING ROD
A
B
FWD FILLET FAIRING
Z621
A
B
ICN-A330-A-53XX3297-A-FAPE3-015FC-A-001-01

### Page 33

A330
SERVICE BULLETIN
REV 00 Jul 21/20 A330-53-3297
Page 33
CONF 001
(3) Task A330-A-53-XX-3297-01001-920A-A - Replace the Upper Rod on the LH
Side
Job Set-Up Information
Working Area
Impacted Zone Access / Work Location
521
Manpower/Resources/Skills
Man-hours 0.50 h
Minimum Number of person 1
Elapsed Time 0.50 h
Skills Airframe
Material necessary to do the job
Consumables
ITEM REFERENCE CML DESCRIPTION DRAWING SEE NOTES
06AAA1 Polysulfide Sealant -General Purpose Brushable
Components
ITEM PART No. QTY (UM) KEYWORD DRAWING SEE NOTES
1 F5335002000000 1 ROD
6 NSA5060-6 2 NUT
7 MS20995C32 0.5 (m) WIRE
11 MS24665-300 2 PIN
Referenced Information
Manuals/Drawings References/Sheets
AMM
06-20-00, Page Block 001
06-31-53, Page Block 001
20-11-11, Page Block 201
T ask 20-11-11-911-803
T ask 20-21-15-912-801
CML CONSUMABLE MATERIAL LIST (CML)
SRM
51-24-00
51-40-00
51-42-00
51-43-00
Procedure
(a) Standard practices given in this procedure:
1 For the identification of zones refer to Ref. AMM 06-20-00, Page Block 001.
2 For the identification of frames refer to Ref. AMM 06-31-53, Page Block 001.
3 Remove and install fasteners in accordance with Ref. SRM 51-42-00.
4 Get alternative and substitute fastener data in accordance with Ref. SRM
51-43-00.

### Page 34

A330
SERVICE BULLETIN
REV 00 Jul 21/20 A330-53-3297
Page 34
5 If alternative and substitute fasteners have to be used, you must make
sure that the associated nut/collar are compatible in accordance with Ref.
SRM 51-40-00 ‘Mating Part’ column.
6 For the wirelocking, refer to Ref. AMM 20-11-11, Page Block 201.
7 For the specification of Material application codes given in this Service
Bulletin, refer to the Ref. CML.
8 T ag all the parts you must remove and retain to make the subsequent
installation easier.
9 Put all the retained hardware in identified plastic bags and attach the bags
to the related unit.
10 T o torque tighten the standard threaded fasteners, refer to Ref. AMM T ask
20-21-15-912-801.
11 Apply sealant in accordance with Ref. SRM 51-24-00.
(b) Remove the upper rod, item (1), refer to Ref. Fig. Replacement of the Upper Fillet
Fairing Rod on the LH Side:
1 ROD   Item (1) Discard
1 BOLT   Item (4) Retain
1 BOLT   Item (5) Retain
2 NUT   Item (6) Discard
1 BUSH   Item (8) Retain
2 WASHER   Item (9) Retain
2 PIN COTTER   Item (11) Discard
NOTE: Once item (1) is removed, it can not be used again.
(c) Record the measure of the dimension X of the removed rod, item (1), refer to
Ref. Fig. Replacement of the Upper Fillet Fairing Rod on the LH Side SHEET 3,view
D.
(d) Install the new upper rod, item 1, refer to Ref. Fig. Replacement of the Upper
Fillet Fairing Rod on the LH Side:
1 Set dimension X on the replaced rod with its corresponding tolerance
shown on Ref. Fig. Replacement of the Upper Fillet Fairing Rod on the LH
Side SHEET 3, view D.
2 Install the new upper rod:
1 ROD F5335002000000 Item 1
1 BOLT   Item (4) Retained
1 BOLT   Item (5) Retained
2 NUT NSA5060-6 Item 6
1 BUSH   Item (8) Retained
2 WASHER   Item (9) Retained
2 PIN-COTTER MS24665-300 Item 11

### Page 35

A330
SERVICE BULLETIN
REV 00 Jul 21/20 A330-53-3297
Page 35
Protect with:
  Polysulfide Sealant
- General Purpose
Brushable
06AAA1  
3 T orque tighten the jam nuts of the rod item 1, between 0.4 daNm (35.403
lbf.in) and 0.5 daNm (44.253 lbf.in).
4 Apply locking wire to secure jam nuts and locking devices, refer to Ref.
AMM T ask 20-11-11-911-803 and Ref. Fig. Replacement of the Upper Fillet
Fairing Rod on the LH Side SHEET 3, view D.
0.5(m) WIRE-LOCK MS20995C32 Item 7

### Page 36

A330
SERVICE BULLETIN
Figure ICN-A330-A-53XX3297-A-FAPE3-015F8-A-002-01 SHEET 1/3
REV 00 Jul 21/20 A330-53-3297Replacement of the Upper Fillet Fairing Rod on the LH Side
Page 36
CONF 001
B
FWD FILLET FAIRING
FR39
A
B
A
Z521
C D
ICN-A330-A-53XX3297-A-FAPE3-015F8-A-002-01

### Page 37

A330
SERVICE BULLETIN
Figure ICN-A330-A-53XX3297-A-FAPE3-015F9-A-002-01 SHEET 2/3
REV 00 Jul 21/20 A330-53-3297Replacement of the Upper Fillet Fairing Rod on the LH Side
Page 37
CONF 001
(1)
1
(11)
11
(4)
(9)
(9)
(11)
11
(6)
6(5)
(8)
03
03
01 02
01
(6)
601
01 02
C
01 APPLY PROTECTION WITH MATERIAL No 06AAA1.
02 TIGHTEN TO  A TORQUE VALUE BETWEEN 1.79 daNm (158.429 lbf.in) AND 2.24 daNm (198.256 lbf.in).
03 TIGHTEN THE LOCKING NUTS ON THE ROD TO A TORQUE VALUE BETWEEN 0.4 daNm (35.403 lbf.in) 
NOTE:
AND 0.5 daNm (44.253 lbf.in) AFTER ADJUSTMENT.
ICN-A330-A-53XX3297-A-FAPE3-015F9-A-002-01

### Page 38

A330
SERVICE BULLETIN
Figure ICN-A330-A-53XX3297-A-FAPE3-016LW-A-002-01 SHEET 3/3
REV 00 Jul 21/20 A330-53-3297Replacement of the Upper Fillet Fairing Rod on the LH Side
Page 38
CONF 001
FORK END EYE END
7
LOCKING DEVICE
JAM NUT
FORK/EYE END
D
DIM X ± 0.3 mm
(0.012 in)
ICN-A330-A-53XX3297-A-FAPE3-016LW-A-002-01

### Page 39

A330
SERVICE BULLETIN
REV 00 Jul 21/20 A330-53-3297
Page 39
CONF 002
(3) Task A330-A-53-XX-3297-01002-920A-A - Replace the Upper Rod on the LH
Side
Job Set-Up Information
Working Area
Impacted Zone Access / Work Location
521
Manpower/Resources/Skills
Man-hours 0.50 h
Minimum Number of person 1
Elapsed Time 0.50 h
Skills Airframe
Material necessary to do the job
Consumables
ITEM REFERENCE CML DESCRIPTION DRAWING SEE NOTES
06AAA1 Polysulfide Sealant -General Purpose Brushable
Components
ITEM PART No. QTY (UM) KEYWORD DRAWING SEE NOTES
7 MS20995C32 0.5 (m) WIRE
11 MS24665-300 2 PIN
12 F0005579700400 1 ROD
15 NSA5060E6 2 NUT
Referenced Information
Manuals/Drawings References/Sheets
AMM
06-20-00, Page Block 001
06-31-53, Page Block 001
20-11-11, Page Block 201
T ask 20-11-11-911-803
T ask 20-21-15-912-801
CML CONSUMABLE MATERIAL LIST (CML)
SRM
51-24-00
51-40-00
51-42-00
51-43-00
Procedure
(a) Standard practices given in this procedure:
1 For the identification of zones refer to Ref. AMM 06-20-00, Page Block 001.
2 For the identification of frames refer to Ref. AMM 06-31-53, Page Block 001.
3 Remove and install fasteners in accordance with Ref. SRM 51-42-00.
4 Get alternative and substitute fastener data in accordance with Ref. SRM
51-43-00.

### Page 40

A330
SERVICE BULLETIN
REV 00 Jul 21/20 A330-53-3297
Page 40
5 If alternative and substitute fasteners have to be used, you must make
sure that the associated nut/collar are compatible in accordance with Ref.
SRM 51-40-00 ‘Mating Part’ column.
6 For the wirelocking, refer to Ref. AMM 20-11-11, Page Block 201.
7 For the specification of Material application codes given in this Service
Bulletin, refer to the Ref. CML.
8 T ag all the parts you must remove and retain to make the subsequent
installation easier.
9 Put all the retained hardware in identified plastic bags and attach the bags
to the related unit.
10 T o torque tighten the standard threaded fasteners, refer to Ref. AMM T ask
20-21-15-912-801.
11 Apply sealant in accordance with Ref. SRM 51-24-00.
(b) Remove the upper rod, item (12), refer to Ref. Fig. Replacement of the Upper
Fillet Fairing Rod on the LH Side:
1 ROD   Item (12) Discard
1 BOLT   Item (4) Retain
1 BOLT   Item (14) Retain
2 NUT   Item (15) Discard
1 BUSH   Item (8) Retain
2 WASHER   Item (16) Retain
2 PIN COTTER   Item (11) Discard
NOTE: Once item (12) is removed, it can not be used again.
(c) Record the measure of the dimension X of the removed rod, item (12), refer to
Ref. Fig. Replacement of the Upper Fillet Fairing Rod on the LH Side SHEET 3,
view D.
(d) Install the new upper rod, item 12, refer to Ref. Fig. Replacement of the Upper
Fillet Fairing Rod on the LH Side:
1 Set dimension X on the replaced rod with its corresponding tolerance
shown on Ref. Fig. Replacement of the Upper Fillet Fairing Rod on the LH
Side SHEET 3, view D.
2 Install the new upper rod:
1 ROD F0005579700400 Item 12
1 BOLT   Item (4) Retained
1 BOLT   Item (14) Retained
2 NUT NSA5060E6 Item 15
2 PIN-COTTER MS24665-300 Item 11
1 BUSH   Item (8) Retained
2 WASHER   Item (16) Retained

### Page 41

A330
SERVICE BULLETIN
REV 00 Jul 21/20 A330-53-3297
Page 41
Protect with:
  Polysulfide Sealant
- General Purpose
Brushable
06AAA1  
3 T orque tighten the jam nuts of the rod item 12, between 1.03 daNm
(91.163 lbf.in) and 1.48 daNm (130.991 lbf.in).
4 Apply locking wire to secure jam nuts and locking devices, refer to Ref.
AMM T ask 20-11-11-911-803 and Ref. Fig. Replacement of the Upper Fillet
Fairing Rod on the LH Side SHEET 3, view D.
0.5(m) WIRE-LOCK MS20995C32 Item 7

### Page 42

A330
SERVICE BULLETIN
Figure ICN-A330-A-53XX3297-A-FAPE3-015F6-A-002-01 SHEET 1/3
REV 00 Jul 21/20 A330-53-3297Replacement of the Upper Fillet Fairing Rod on the LH Side
Page 42
CONF 002
B
FWD FILLET FAIRING
FR39
A
B
A
Z521
C D
ICN-A330-A-53XX3297-A-FAPE3-015F6-A-002-01

### Page 43

A330
SERVICE BULLETIN
Figure ICN-A330-A-53XX3297-A-FAPE3-015F7-A-002-01 SHEET 2/3
REV 00 Jul 21/20 A330-53-3297Replacement of the Upper Fillet Fairing Rod on the LH Side
Page 43
CONF 002
(12)
12
(11)
11
(4)
(16)
(16)
(11)
11
(15)
15(14)
(8)
03
03
01 02
01
(15)
1501
01 02
C
01 APPLY PROTECTION WITH MATERIAL No 06AAA1.
02 TIGHTEN TO  A TORQUE VALUE BETWEEN 1.9 daNm (168.165 lbf.in) AND 2.3 daNm (203.567 lbf.in).
03 TIGHTEN THE LOCKING NUTS ON THE ROD TO A TORQUE VALUE BETWEEN 1.03 daNm (91.163 lbf.in) 
NOTE:
AND 1.48 daNm (130.991 lbf.in) AFTER ADJUSTMENT.
ICN-A330-A-53XX3297-A-FAPE3-015F7-A-002-01

### Page 44

A330
SERVICE BULLETIN
Figure ICN-A330-A-53XX3297-A-FAPE3-016LV-A-002-01 SHEET 3/3
REV 00 Jul 21/20 A330-53-3297Replacement of the Upper Fillet Fairing Rod on the LH Side
Page 44
CONF 002
FORK END EYE END
7
LOCKING DEVICE
JAM NUT
FORK/EYE END
D
DIM X ± 0.3 mm
(0.012 in)
ICN-A330-A-53XX3297-A-FAPE3-016LV-A-002-01

### Page 45

A330
SERVICE BULLETIN
REV 00 Jul 21/20 A330-53-3297
Page 45
CONF 001
(4) Task A330-A-53-XX-3297-02001-920A-A - Replace the Middle Rod on the LH
Side
Job Set-Up Information
Working Area
Impacted Zone Access / Work Location
521
Manpower/Resources/Skills
Man-hours 0.50 h
Minimum Number of person 1
Elapsed Time 0.50 h
Skills Airframe
Material necessary to do the job
Consumables
ITEM REFERENCE CML DESCRIPTION DRAWING SEE NOTES
06AAA1 Polysulfide Sealant -General Purpose Brushable
Components
ITEM PART No. QTY (UM) KEYWORD DRAWING SEE NOTES
2 F5335001900000 1 ROD
6 NSA5060-6 2 NUT
7 MS20995C32 0.5 (m) WIRE
11 MS24665-300 2 PIN
Referenced Information
Manuals/Drawings References/Sheets
AMM
06-20-00, Page Block 001
06-31-53, Page Block 001
20-11-11, Page Block 201
T ask 20-11-11-911-803
T ask 20-21-15-912-801
CML CONSUMABLE MATERIAL LIST (CML)
SRM
51-24-00
51-40-00
51-42-00
51-43-00
Procedure
(a) Standard practices given in this procedure:
1 For the identification of zones refer to Ref. AMM 06-20-00, Page Block 001.
2 For the identification of frames refer to Ref. AMM 06-31-53, Page Block 001.
3 Remove and install fasteners in accordance with Ref. SRM 51-42-00.
4 Get alternative and substitute fastener data in accordance with Ref. SRM
51-43-00.

### Page 46

A330
SERVICE BULLETIN
REV 00 Jul 21/20 A330-53-3297
Page 46
5 If alternative and substitute fasteners have to be used, you must make
sure that the associated nut/collar are compatible in accordance with Ref.
SRM 51-40-00 ‘Mating Part’ column.
6 For the wirelocking, refer to Ref. AMM 20-11-11, Page Block 201.
7 For the specification of Material application codes given in this Service
Bulletin, refer to the Ref. CML.
8 T ag all the parts you must remove and retain to make the subsequent
installation easier.
9 Put all the retained hardware in identified plastic bags and attach the bags
to the related unit.
10 T o torque tighten the standard threaded fasteners, refer to Ref. AMM T ask
20-21-15-912-801.
11 Apply sealant in accordance with Ref. SRM 51-24-00.
(b) Remove the middle rod, item (2), refer to Ref. Fig. Replacement of the Middle
Fillet Fairing Rod on the LH Side:
1 ROD   Item (2) Discard
1 BOLT   Item (4) Retain
1 BOLT   Item (5) Retain
2 NUT   Item (6) Discard
1 BUSH   Item (8) Retain
2 WASHER   Item (9) Retain
2 PIN COTTER   Item (11) Discard
NOTE: Once item (2) is removed, it can not be used again.
(c) Record the measure of the dimension X of the removed rod, item (2), refer to
Ref. Fig. Replacement of the Middle Fillet Fairing Rod on the LH Side SHEET 3,
view D.
(d) Install the new middle rod, item 2, refer to Ref. Fig. Replacement of the Middle
Fillet Fairing Rod on the LH Side:
1 Set dimension X on the replaced rod with its corresponding tolerance
shown on Ref. Fig. Replacement of the Middle Fillet Fairing Rod on the LH
Side SHEET 3 , view D.
2 Install the new middle rod:
1 ROD F5335001900000 Item 2
1 BOLT   Item (4) Retained
1 BOLT   Item (5) Retained
2 NUT NSA5060-6 Item 6
1 BUSH   Item (8) Retained
2 WASHER   Item (9) Retained
2 PIN-COTTER MS24665-300 Item 11

### Page 47

A330
SERVICE BULLETIN
REV 00 Jul 21/20 A330-53-3297
Page 47
Protect with:
  Polysulfide Sealant
- General Purpose
Brushable
06AAA1  
3 T orque tighten the jam nuts of the rod item 2, between 0.4 daNm (35.403
lbf.in) and 0.5 daNm (44.253 lbf.in).
4 Apply locking wire to secure jam nuts and locking devices, refer to Ref.
AMM T ask 20-11-11-911-803 and Ref. Fig. Replacement of the Middle Fillet
Fairing Rod on the LH Side SHEET 3.
0.5(m) WIRE-LOCK MS20995C32 Item 7

### Page 48

A330
SERVICE BULLETIN
Figure ICN-A330-A-53XX3297-A-FAPE3-015F0-A-002-01 SHEET 1/3
REV 00 Jul 21/20 A330-53-3297Replacement of the Middle Fillet Fairing Rod on the LH Side
Page 48
CONF 001
A
B
Z521
FWD FILLET FAIRING
FR39
A
B
C D
ICN-A330-A-53XX3297-A-FAPE3-015F0-A-002-01

### Page 49

A330
SERVICE BULLETIN
Figure ICN-A330-A-53XX3297-A-FAPE3-015F1-A-003-01 SHEET 2/3
REV 00 Jul 21/20 A330-53-3297Replacement of the Middle Fillet Fairing Rod on the LH Side
Page 49
CONF 001
(2)
2
(11)
11
(4)
(9)
(9)
(11)
11
(6)
6(5)
(8)
03
03
01 02
01
(6)
601
01 02
C
NOTE:
APPLY PROTECTION WITH MATERIAL No 06AAA1.01
TIGHTEN TO  A TORQUE VALUE BETWEEN 1.79 daNm (158.429 lbf.in) AND 2.24 daNm (198.256 lbf.in).02
TIGHTEN THE LOCKING NUTS ON THE ROD TO A TORQUE VALUE BETWEEN 0.4 daNm (35.403 lbf.in) 03
AND 0.5 daNm (44.253 lbf.in) AFTER ADJUSTMENT.
ICN-A330-A-53XX3297-A-FAPE3-015F1-A-003-01

### Page 50

A330
SERVICE BULLETIN
Figure ICN-A330-A-53XX3297-A-FAPE3-016OU-A-002-01 SHEET 3/3
REV 00 Jul 21/20 A330-53-3297Replacement of the Middle Fillet Fairing Rod on the LH Side
Page 50
CONF 001
FORK END EYE END
7
LOCKING DEVICE
JAM NUT
FORK/EYE END
D
DIM X ± 0.3 mm
(0.012 in)
ICN-A330-A-53XX3297-A-FAPE3-016OU-A-002-01

### Page 51

A330
SERVICE BULLETIN
REV 00 Jul 21/20 A330-53-3297
Page 51
(5) Task A330-A-53-XX-3297-03001-920A-A - Replace the Lower Rod on the LH
Side
Job Set-Up Information
Working Area
Impacted Zone Access / Work Location
521
Manpower/Resources/Skills
Man-hours 0.50 h
Minimum Number of person 1
Elapsed Time 0.50 h
Skills Airframe
Material necessary to do the job
Consumables
ITEM REFERENCE CML DESCRIPTION DRAWING SEE NOTES
06AAA1 Polysulfide Sealant -General Purpose Brushable
Components
ITEM PART No. QTY (UM) KEYWORD DRAWING SEE NOTES
3 F5335001900200 1 ROD
6 NSA5060-6 2 NUT
7 MS20995C32 0.5 (m) WIRE
11 MS24665-300 2 PIN
Referenced Information
Manuals/Drawings References/Sheets
AMM
06-20-00, Page Block 001
06-31-53, Page Block 001
20-11-11, Page Block 201
T ask 20-11-11-911-803
T ask 20-21-15-912-801
CML CONSUMABLE MATERIAL LIST (CML)
SRM
51-24-00
51-40-00
51-42-00
51-43-00
Procedure
(a) Standard practices given in this procedure:
1 For the identification of zones refer to Ref. AMM 06-20-00, Page Block 001.
2 For the identification of frames refer to Ref. AMM 06-31-53, Page Block 001.
3 Remove and install fasteners in accordance with Ref. SRM 51-42-00.
4 Get alternative and substitute fastener data in accordance with Ref. SRM
51-43-00.

### Page 52

A330
SERVICE BULLETIN
REV 00 Jul 21/20 A330-53-3297
Page 52
5 If alternative and substitute fasteners have to be used, you must make
sure that the associated nut/collar are compatible in accordance with Ref.
SRM 51-40-00 ‘Mating Part’ column.
6 For the wirelocking, refer to Ref. AMM 20-11-11, Page Block 201.
7 For the specification of Material application codes given in this Service
Bulletin, refer to the Ref. CML.
8 T ag all the parts you must remove and retain to make the subsequent
installation easier.
9 Put all the retained hardware in identified plastic bags and attach the bags
to the related unit.
10 T o torque tighten the standard threaded fasteners, refer to Ref. AMM T ask
20-21-15-912-801.
11 Apply sealant in accordance with Ref. SRM 51-24-00.
(b) Remove the lower rod, item (3), refer to Ref. Fig. Replacement of the Lower Fillet
Fairing Rod on the LH Side:
1 ROD   Item (3) Discard
1 BOLT   Item (4) Retain
1 BOLT   Item (5) Retain
2 NUT   Item (6) Discard
1 BUSH   Item (8) Retain
2 WASHER   Item (9) Retain
2 PIN COTTER   Item (11) Discard
NOTE: Once item (3) is removed, it can not be used again.
(c) Record the measure of the dimension X of the removed rod, item (3), refer to
Ref. Fig. Replacement of the Lower Fillet Fairing Rod on the LH Side SHEET 3,
view D.
(d) Install the new lower rod, item 3, refer to Ref. Fig. Replacement of the Lower
Fillet Fairing Rod on the LH Side:
1 Set dimension X on the replaced rod with its corresponding tolerance
shown on Ref. Fig. Replacement of the Lower Fillet Fairing Rod on the LH
Side SHEET 3, view D.
2 Install the new lower rod:
1 ROD F5335001900200 Item 3
1 BOLT   Item (4) Retained
1 BOLT   Item (5) Retained
2 NUT NSA5060-6 Item 6
1 BUSH   Item (8) Retained
2 WASHER   Item (9) Retained
2 PIN-COTTER MS24665-300 Item 11

### Page 53

A330
SERVICE BULLETIN
REV 00 Jul 21/20 A330-53-3297
Page 53
Protect with:
  Polysulfide Sealant
- General Purpose
Brushable
06AAA1  
3 T orque tighten the jam nuts of the rod item 3, between 0.4 daNm (35.403
lbf.in) and 0.5 daNm (44.253 lbf.in).
4 Apply locking wire to secure jam nuts and locking devices, refer to Ref.
AMM T ask 20-11-11-911-803 and Ref. Fig. Replacement of the Lower Fillet
Fairing Rod on the LH Side SHEET 3, view D.
0.5(m) WIRE-LOCK MS20995C32 Item 7

### Page 54

A330
SERVICE BULLETIN
Figure ICN-A330-A-53XX3297-A-FAPE3-015F2-A-002-01 SHEET 1/3
REV 00 Jul 21/20 A330-53-3297Replacement of the Lower Fillet Fairing Rod on the LH Side
Page 54
CONF 001
A
B
Z521
FWD FILLET FAIRING
FR39
A
B
C D
ICN-A330-A-53XX3297-A-FAPE3-015F2-A-002-01

### Page 55

A330
SERVICE BULLETIN
Figure ICN-A330-A-53XX3297-A-FAPE3-015F3-A-002-01 SHEET 2/3
REV 00 Jul 21/20 A330-53-3297Replacement of the Lower Fillet Fairing Rod on the LH Side
Page 55
CONF 001
01 APPLY PROTECTION WITH MATERIAL No 06AAA1.
02
03
NOTE:
(3)
3
(11)
11
(4)
(9)
(9)
(11)
11
(6)
6(5)
(8)
03
03
01 02
01
(6)
601
01 02
C
TIGHTEN TO  A TORQUE VALUE BETWEEN 1.79 daNm (158.429 lbf.in) AND 2.24 daNm (198.256 lbf.in).
TIGHTEN THE LOCKING NUTS ON THE ROD TO A TORQUE VALUE BETWEEN 0.4 daNm (35.403 lbf.in) 
AND 0.5 daNm (44.253 lbf.in) AFTER ADJUSTMENT.
ICN-A330-A-53XX3297-A-FAPE3-015F3-A-002-01

### Page 56

A330
SERVICE BULLETIN
Figure ICN-A330-A-53XX3297-A-FAPE3-016OR-A-002-01 SHEET 3/3
REV 00 Jul 21/20 A330-53-3297Replacement of the Lower Fillet Fairing Rod on the LH Side
Page 56
CONF 001
FORK END EYE END
7
LOCKING DEVICE
JAM NUT
FORK/EYE END
D
DIM X ± 0.3 mm
(0.012 in)
ICN-A330-A-53XX3297-A-FAPE3-016OR-A-002-01

### Page 57

A330
SERVICE BULLETIN
REV 00 Jul 21/20 A330-53-3297
Page 57
CONF 002
(5) Task A330-A-53-XX-3297-03002-920A-A - Replace the Lower Rod on the LH
Side
Job Set-Up Information
Working Area
Impacted Zone Access / Work Location
521
Manpower/Resources/Skills
Man-hours 0.50 h
Minimum Number of person 1
Elapsed Time 0.50 h
Skills Airframe
Material necessary to do the job
Consumables
ITEM REFERENCE CML DESCRIPTION DRAWING SEE NOTES
06AAA1 Polysulfide Sealant -General Purpose Brushable
Components
ITEM PART No. QTY (UM) KEYWORD DRAWING SEE NOTES
7 MS20995C32 0.5 (m) WIRE
11 MS24665-300 2 PIN
13 F0005579700200 1 ROD
15 NSA5060E6 2 NUT
Referenced Information
Manuals/Drawings References/Sheets
AMM
06-20-00, Page Block 001
06-31-53, Page Block 001
20-11-11, Page Block 201
T ask 20-11-11-911-803
T ask 20-21-15-912-801
CML CONSUMABLE MATERIAL LIST (CML)
SRM
51-24-00
51-40-00
51-42-00
51-43-00
Procedure
(a) Standard practices given in this procedure:
1 For the identification of zones refer to Ref. AMM 06-20-00, Page Block 001.
2 For the identification of frames refer to Ref. AMM 06-31-53, Page Block 001.
3 Remove and install fasteners in accordance with Ref. SRM 51-42-00.
4 Get alternative and substitute fastener data in accordance with Ref. SRM
51-43-00.

### Page 58

A330
SERVICE BULLETIN
REV 00 Jul 21/20 A330-53-3297
Page 58
5 If alternative and substitute fasteners have to be used, you must make
sure that the associated nut/collar are compatible in accordance with Ref.
SRM 51-40-00 ‘Mating Part’ column.
6 For the wirelocking, refer to Ref. AMM 20-11-11, Page Block 201.
7 For the specification of Material application codes given in this Service
Bulletin, refer to the Ref. CML.
8 T ag all the parts you must remove and retain to make the subsequent
installation easier.
9 Put all the retained hardware in identified plastic bags and attach the bags
to the related unit.
10 T o torque tighten the standard threaded fasteners, refer to Ref. AMM T ask
20-21-15-912-801.
11 Apply sealant in accordance with Ref. SRM 51-24-00.
(b) Remove the lower rod, item (13), refer to Ref. Fig. Replacement of the Lower
Fillet Fairing Rod on the LH Side:
1 ROD   Item (13) Discard
1 BOLT   Item (4) Retain
1 BOLT   Item (14) Retain
2 NUT   Item (15) Discard
1 BUSH   Item (8) Retain
2 WASHER   Item (16) Retain
2 PIN COTTER   Item (11) Discard
NOTE: Once item (13) is removed, it can not be used again.
(c) Record the measure of the dimension X of the removed rod, item (13), refer to
Ref. Fig. Replacement of the Lower Fillet Fairing Rod on the LH Side SHEET 3,
view D.
(d) Install the new lower rod, item 13, refer to Ref. Fig. Replacement of the Lower
Fillet Fairing Rod on the LH Side:
1 Set dimension X on the replaced rod with its corresponding tolerance
shown on Ref. Fig. Replacement of the Lower Fillet Fairing Rod on the LH
Side SHEET 3, view D.
2 Install the new lower rod:
1 ROD F0005579700200 Item 13
1 BOLT   Item (4) Retained
1 BOLT   Item (14) Retained
2 NUT NSA5060E6 Item 15
2 PIN-COTTER MS24665-300 Item 11
1 BUSH   Item (8) Retained
2 WASHER   Item (16) Retained

### Page 59

A330
SERVICE BULLETIN
REV 00 Jul 21/20 A330-53-3297
Page 59
Protect with:
  Polysulfide Sealant
- General Purpose
Brushable
06AAA1  
3 T orque tighten the jam nuts of the rod item 13, between 1.03 daNm
(91.163 lbf.in) and 1.48 daNm (130.991 lbf.in).
4 Apply locking wire to secure jam nuts and locking devices, refer to Ref.
AMM T ask 20-11-11-911-803 and Ref. Fig. Replacement of the Lower Fillet
Fairing Rod on the LH Side SHEET 3, view D.
0.5(m) WIRE-LOCK MS20995C32 Item 7

### Page 60

A330
SERVICE BULLETIN
Figure ICN-A330-A-53XX3297-A-FAPE3-015F4-A-002-01 SHEET 1/3
REV 00 Jul 21/20 A330-53-3297Replacement of the Lower Fillet Fairing Rod on the LH Side
Page 60
CONF 002
A
B
Z521
FWD FILLET FAIRING
FR39
A
B
C D
ICN-A330-A-53XX3297-A-FAPE3-015F4-A-002-01

The text continues at https://openairdocs.org/service-documents/airbus/a330-53-3297/file/49baa1a21789.md?from=61

---
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