# Airbus Service Bulletin A300-32-0468

Copy: No revision named ("A300-32-0468 R00"), 50 pages: PDF https://openairdocs.org/files/sha256/1b/cd/1bcd1dde087cd0af21266e1e0297c2acbbaa88afc47c02c2a5fdac1d9d3f0c07; text https://openairdocs.org/service-documents/airbus/a300-32-0468/file/1bcd1dde087c.md. Rights: © Airbus S.A.S. Filed by the FAA in regulations.gov docket FAA-2020-1113, the docket of AD 2021-11-18. Not covered by OpenAirDocs’ CC0 dedication.

## Details

- Manufacturer: [Airbus](https://openairdocs.org/service-documents/airbus.md)
- Type: Service bulletin (Service Bulletin)
- Number: A300-32-0468
- Page: https://openairdocs.org/service-documents/airbus/a300-32-0468

## Text (50 pages)

Rights: © Airbus S.A.S. Filed by the FAA in regulations.gov docket FAA-2020-1113, the docket of AD 2021-11-18. Not covered by OpenAirDocs’ CC0 dedication. Each page's text from the PDF; open the PDF at a page with #page=N.

### Page 1

@A300
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.
MANDATORY
 MANDATORY
 MANDATORY
ATA SYSTEM: 32
TITLE: MAIN LANDING GEAR - INSPECTION OF THE HINGE ARM/BARREL
PIN
**CONF ALL
MODIFICATIONS
None
REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES
Three cases of cracks on Main Landing Gear (MLG) Hinge Arm / Barrel Pin have been reported to
AIRBUS. These cracks initiated following an overload leading to the connecting rod bushings fracture.
Corrective actions are done in 2 steps:
- A clean-up of the fleet through MOD No. 13859S22952 (Service Bulletin No. A300-32-0469) for
used pins replacement by a brand new pin with primer paint.
- A new repetitive inspection described in this Inspection Service Bulletin (ISB) that will be performed
on the new pin with primer paint post MOD No. 13859S22952 (Service Bulletin No. A300-32-0469).
The aim of this procedure is to perform following inspection / maintenance actions on the aircraft on
which MOD No. 13859S22952 (Service Bulletin No. A300-32-0469) is embodied:
- Remove MLG Hinge Arm / Barrel Pin with dedicated tooling
- Visually inspect MLG Hinge Arm / Barrel Pin and associated connecting rod bushings
. In case connecting rod bushings are found cracked, distorted or fractured, or the MLG Hinge
Arm / Barrel Pin is found cracked, MLG Leg shall be removed and sent to MRO for inspection
with the MLG Hinge Arm / Barrel Pin, other side leg should be inspected before next flight (as
per this ISB)
. If MLG Hinge Arm / Barrel Pin is found with dam age (chrome damage, co rrosion, cracks), send
it to Safran landing Systems for investigation
. In case of nil findings, reinstall the same MLG Hinge Arm / Barrel Pin on aircraft.
DATE: Sep 24/19 SERVICE BULLETIN No.: A300-32-0468
REVISION No.: 00 - Sep 24/19 Page: 1
7
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

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SERVICE BULLETIN
SUMMARY
- Repeat inspection within the defined compliance time.
The accomplishment of this Service Bulletin will prevent failures on the MLG Hinge Arm / Barrel Pin.
The MLG Hinge Arm / Barrel Pin is a safe life item listed in ALS Part 1. Failure of the pin could result in
a MLG collapse.
GENERAL EVALUATION
EVALUATION TABLE
COMPLIANCE
 MANDATORY (1)
 CANCELS INSPECTION SB
 NO
POTENTIAL AD
 YES
 A/C OPERATION AFFECTED
 NO
RELIABILITY AFFECTED
 NO
 PAX COMFORT AFFECTED
 NO
COST SAVING
 NO
 ETOPS AFFECTED
 NO
STRUCTURAL LIFE EXTN
 NO
 VENDOR SB INVOLVED
 NO
AIRCRAFT JACKING
 YES
NOTE
 (1)
: Service Bulletin must be accomplished.
MATERIAL PRICE INFORMATION
MATERIAL PRICE INFORMATION TABLE
MATERIAL SET
 QTY PER
A/C
PRICE PER
A/C (USD)
MAIN PARTS
Equipment BFEB03
 See SB
 Pin, MLG Leg Assemblies
Equipment BFEB02
 See SB
 Pin, MLG Leg Assemblies
EFFECTIVITY
This Service Bulletin is applicable to this (these) operator(s) :
62N 81T A2S AFG F2I GLY IAW IRA IRM MIX MSB MSR RUN
STR TIW TNO
CONCURRENT REQUIREMENTS
Accomplishment of this Service Bulletin requires the prior accomplishment of the following Service
Bulletin:
Service Bulletin No. A300-32-0469
NOTE
: Service Bulletin No. A300-32-0469 LANDING GEAR - MAIN GEAR - CHANGE BARREL
/ HINGE ARM PIN WITH NEW WET PRIMER-IMPREGNATED PIN
REFERENCES / REPERCUSSIONS
TFU
 32.11.00.023
OEB
 None
AOT
 None
SIL
 None
ISI
 None
LINE MAINTENANCE AFFECTED
 No
LIFE LIMIT
 None
DATE: Sep 24/19 SERVICE BULLETIN No.: A300-32-0468
REVISION No.: 00 - Sep 24/19 Page: 2
7
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

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SERVICE BULLETIN
SUMMARY
OTHER
 None
NATURE OF THE WORK
AIRCRAFT
 YES
EQUIPMENT
 YES
MANPOWER
Task 320468-832-895-001: Inspect the RH / LH Hinge Arm / Barrel Pins and Connecting Rod
Bushings
TOTAL MANHOURS
 22.25
ELAPSED TIME (HOURS)
 9.75
Task 320468-831-895-001: Replace the RH / LH MLG Leg and Hinge Arm / Barrel Pin
(Depending on Inspection Result)
TOTAL MANHOURS
 89.25
ELAPSED TIME (HOURS)
 45.25
APPENDICES
Appendix 01 - Manpower Gantt Chart
Appendix 02 - Inspection Report
DATE: Sep 24/19 SERVICE BULLETIN No.: A300-32-0468
REVISION No.: 00 - Sep 24/19 Page: 3
7
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

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SERVICE BULLETIN
SUMMARY
**CONF ALL
LH SHOWN
RH SYMMETRICAL
Z731
Z741
A
A
B
LH SHOWN
RH SYMMETRICAL
INSPECTION AREA
NOTE:
B
A_SB_320468_7_SAAA_01_00
Figure A-USAAA - Sheet 01
DATE: Sep 24/19 SERVICE BULLETIN No.: A300-32-0468
REVISION No.: 00 - Sep 24/19 Page: 4
7
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

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@A300
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
MANDATORY
 MANDATORY
 MANDATORY
ATA SYSTEM: 32
TITLE: MAIN LANDING GEAR - INSPECTION OF THE HINGE ARM/BARREL
PIN
MODIFICATION No.: None
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
(1) Models
B4-103 B4-203 B4-2C C4-203 F4-203
(2) Effectivity by MSN
0075 0085 0107 0126 0139 0141 0151-0152 0154 0157 0173 0175 0180 0183 0203
0210 0212 0218 0220 0227 0234-0236 0239 0247 0255-0256 0259 0261 0274 0277
0292 0299 0302
(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
62N
 0183
81T
 0126 0141 0157 0277 0292
DATE: Sep 24/19 SERVICE BULLETIN No.: A300-32-0468
REVISION No.: 00 - Sep 24/19 Page: 1
7
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

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SERVICE BULLETIN
OPERATOR
 MSN
A2S
 0203
AFG
 0180
F2I
 0235
GLY
 0085
IAW
 0239
IRA
 0139 0151 0173 0256 0299 0302
IRM
 0175
MIX
 0218
MSB
 0212
MSR
 0255
RUN
 0075 0107 0154
STR
 0236
TIW
 0152 0220 0234 0259 0261 0274
TNO
 0210 0227 0247
(4) Configuration by MSN
MSN
 CONFIGURATION
0075 0085 0107 0126 0139 0141 0151 0152 0154 0157 0173
0175 0180 0183 0203 0210 0212 0218 0220 0227 0234 0235
0236 0239 0247 0255 0256 0259 0261 0274 0277 0292 0299
0302
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 BFEB03
 As required
Equipment BFEB02
 As required
Consumable CMLB01
 1
NOTE
: For Materials you cannot identify in the CML, please contact:
KLX Aerospace Solutions
10000 N.W. 15th Terrace
Miami, FL 33172
USA
Phone: +1.305.925.2600
Fax: +1.305.507.7191
Email: AOGdesk@KLX.com
Internet: http://www.klxaerospace.com
B. CONCURRENT REQUIREMENTS
Accomplishment of this Service Bulletin requires the prior accomplishment of the following
Service Bulletin:
DATE: Sep 24/19 SERVICE BULLETIN No.: A300-32-0468
REVISION No.: 00 - Sep 24/19 Page: 2
7
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

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SERVICE BULLETIN
Service Bulletin No. A300-32-0469
NOTE
: Service Bulletin No. A300-32-0469 LANDING GEAR - MAIN GEAR -
CHANGE BARREL / HINGE ARM PIN WITH NEW WET PRIMER-
IMPREGNATED PIN
C. REASON
(1) History
Three cases of cracks on Main Landing Gear (MLG) Hinge Arm / Barrel Pin have
been reported to AIRBUS. These cracks initiated following an overload leading to the
connecting rod bushings fracture.
Corrective actions are done in 2 steps:
- A clean-up of the fleet through MOD No. 13859S22952 (Service Bulletin No.
A300-32-0469) for used pins replacement by a brand new pin with primer paint.
- A new repetitive inspection described in this Inspection Service Bulletin (ISB) that
will be performed on the new pin with primer paint post MOD No. 13859S22952
(Service Bulletin No. A300-32-0469).
(2) Objective/Action
The aim of this procedure is to perform following inspection / maintenance actions on
the aircraft on which MOD No. 13859S22952 (Service Bulletin No. A300-32-0469) is
embodied:
- Remove MLG Hinge Arm / Barrel Pin with dedicated tooling
- Visually inspect MLG Hinge Arm / Barrel Pin and associated connecting rod
bushings
. In case connecting rod bushings are found cracked, distorted or fractured, or
the MLG Hinge Arm / Barrel Pin is found cracked, MLG Leg shall be removed
and sent to MRO for inspection with the MLG Hinge Arm / Barrel Pin, other side
leg should be inspected before next flight (as per this ISB)
. If MLG Hinge Arm / Barrel Pin is found with damage (chrome damage,
corrosion, cracks), send it to Safran l anding Systems for investigation
. In case of nil findings, reinstall the same MLG Hinge Arm / Barrel Pin on
aircraft.
- Repeat inspection within the defined compliance time.
(3) Advantages
The accomplishment of this Service Bulletin will prevent failures on the MLG Hinge Arm /
Barrel Pin. The MLG Hinge Arm / Barrel Pin is a safe life item listed in ALS Part 1.
Failure of the pin could result in a MLG collapse.
DATE: Sep 24/19 SERVICE BULLETIN No.: A300-32-0468
REVISION No.: 00 - Sep 24/19 Page: 3
7
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

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SERVICE BULLETIN
(4) Operational/Maintenance Consequences
None
D. DESCRIPTION
To accomplish this Service Bulletin it is necessary to :
Task 320468-832-895-001: Inspect the RH / LH Hinge Arm / Barrel Pins and Connecting Rod
Bushings
(1) Remove the RH Hinge Arm / Barrel Pin
(2) Inspect the RH Hinge Arm / Barrel Pin and Connecting Rod Bushings
(3) Install the RH Hinge Arm / Barrel Pin
(4) Remove the LH Hinge Arm / Barrel Pin
(5) Inspect the LH Hinge Arm / Barrel Pin and Connecting Rod Bushings
(6) Install the LH Hinge Arm / Barrel Pin
Task 320468-831-895-001: Replace the RH / LH MLG Leg and Hinge Arm / Barrel Pin
(Depending on Inspection Result)
(1) Replace the Existing RH MLG Leg and Hinge Arm / Barrel Pin (Depending on
Inspection Result)
(2) Replace the Existing LH MLG Leg and Hinge Arm / Barrel Pin (Depending on
Inspection Result)
E. COMPLIANCE
(1) Classification
MANDATORY: Service Bulletin must be accomplished.
(2) Accomplishment Timescale
- Accomplishment of this Service Bulletin must be done at the threshold and interval
given in the table below.
- This Service Bulletin has been classified Mandatory. It is expected that an
Airworthiness Directive (AD) published by the European Aviation Safety Agency
(EASA) will be issued to confirm this classification. It is anticipated that the AD will
confirm the thresholds and or intervals given but reference should be made to the
AD for confirmation of the mandated accomplishment timescale.
Table 1, Config. 001 - Special Detailed Inspection of Bushings
Compliance Time
Condition
 Action
Threshold
Repetitive Interval
DATE: Sep 24/19 SERVICE BULLETIN No.: A300-32-0468
REVISION No.: 00 - Sep 24/19 Page: 4
7
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

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SERVICE BULLETIN
All MLG on which MOD
13859S22952 has been
embodied
Remove the Hinge arm /
Barrel Pin from the MLG
and perform a Special
Detailed Inspection of
the MLG Connecting
Rod Bushings, refer to
TASK 320468-832-895
001 Inspect the RH / LH
Hinge Arm / Barrel Pins
and Connecting Rod
Bushings
30 Months following the
implementation of MOD
13859S22952
30 Months
Replace the affected
MLG Leg including the
Hinge Arm / Barrel Pin,
refer to TASK
320468-831-895 001
Replace the RH / LH
MLG Leg and Hinge Arm
/ Barrel Pin (Depending
on Inspection Result)
Before next flight
 None
AND
Send the removed Hinge
Arm / Barrel Pin to
Safran Landing Systems
for investigation
Upon completion of
removal
None
AND
Send the removed MLG
to the MRO for
inspection
Upon completion of
removal
None
AND
Inspect the opposite side
MLG, refer to TASK
320468-832-895 001
Inspect the RH / LH
Hinge Arm / Barrel Pins
and Connecting Rod
Bushings
Before next flight
 30 Months
AND
MLG with cracked,
distorted, or fractured
bushings
Report to AIRBUS
 Before next flight
 None
MLG with corroded
bushings or bushings
showing wear or
discoloration
Contact Safran Landing
Systems for instructions
Before next flight
 None
MLG without cracked,
distorted, or fractured
bushings that do not
show corrosion, wear,
or discoloration
Continue to Table 2
 Before next flight
 None
Table 2, Config. 001 - Detailed Visual Inspection of the MLG Hinge Arm / Barrel Pin
DATE: Sep 24/19 SERVICE BULLETIN No.: A300-32-0468
REVISION No.: 00 - Sep 24/19 Page: 5
7
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

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SERVICE BULLETIN
Compliance Time
Condition
 Action
Threshold
Repetitive Interval
MLG without cracked,
distorted, or fractured
bushings that do not
show corrosion, wear,
discoloration
Perform Detailed Visual
Inspection of the MLG
Hinge Arm / Barrel Pin,
refer to TASK
320468-832-895 001
Inspect the RH / LH
Hinge Arm / Barrel Pins
and Connecting Rod
Bushings
Before next flight
 None
Replace the affected
MLG Leg including the
Hinge Arm / Barrel Pin,
refer to TASK
320468-831-895 001
Replace the RH / LH
MLG Leg and Hinge Arm
/ Barrel Pin (Depending
on Inspection Result)
Before next flight
 None
AND
Send the removed Hinge
Arm / Barrel Pin to
Safran Landing Systems
for inspection
Upon completion of
removal
None
AND
Send the removed MLG
to the MRO for
investigation
Upon completion of
removal
None
AND
Inspect the opposite side
MLG, refer to TASK
320468-832-895 001
Inspect the RH / LH
Hinge Arm / Barrel Pins
and Connecting Rod
Bushings
Before next flight
 30 Months
AND
MLG with cracked
Hinge Arm / Barrel Pins
Report to AIRBUS
 Before next flight
 None
DATE: Sep 24/19 SERVICE BULLETIN No.: A300-32-0468
REVISION No.: 00 - Sep 24/19 Page: 6
7
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

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SERVICE BULLETIN
Install a serviceable
Hinge Arm / Barrel Pin,
refer to SUBTASK
320468-420-401 001
Install the RH Hinge Arm
/ Barrel Pin and / or
SUBTASK
320468-420-402 001
Install the LH Hinge Arm
/ Barrel Pin
Before next flight
 None
AND
Send the removed Hinge
Arm / Barrel Pin to
Safran Landing Systems
for inspection
Upon completion of
removal
None
AND
MLG with Hinge Arm /
Barrel Pins showing OD
Chrome Damage and /
or corrosion
Report to AIRBUS
 Before next flight
 None
MLG with Hinge Arm /
Barrel Pins with no
findings
Re-Install the removed
Hinge Arm / Barrel Pin,
refer to SUBTASK
320468-420-401 001
Install the RH Hinge Arm
/ Barrel Pin and / or
SUBTASK
320468-420-402 001
Install the LH Hinge Arm
/ Barrel Pin
Before next flight
 None
F. APPROVAL
The technical content of this document is approved under the authority of 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. 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 320468-832-895-001: Inspect the RH / LH Hinge Arm / Barrel Pins and Connecting Rod
Bushings
Get Access
 2.00
On Aircraft
DATE: Sep 24/19 SERVICE BULLETIN No.: A300-32-0468
REVISION No.: 00 - Sep 24/19 Page: 7
7
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

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SERVICE BULLETIN
Task 320468-832-895-001: Inspect the RH / LH Hinge Arm / Barrel Pins and Connecting Rod
Bushings
Remove the RH Hinge Arm / Barrel Pin
 5.75
Inspect the RH Hinge Arm / Barrel Pin and Connecting
Rod Bushings
0.50
Install the RH Hinge Arm / Barrel Pin
 2.25
Remove the LH Hinge Arm / Barrel Pin
 5.75
Inspect the LH Hinge Arm / Barrel Pin and Connecting
Rod Bushings
0.50
Install the LH Hinge Arm / Barrel Pin
 2.25
Close-Up
 3.25
TOTAL MANHOURS
 22.25
ELAPSED TIME (HOURS)
 9.75
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.
NOTE
: For an explanation of the man-hours and elapsed time, refer to the Gantt
Chart Fig. A-UAAAA
, given in Appendix 01.
Task 320468-831-895-001: Replace the RH / LH MLG Leg and Hinge Arm / Barrel Pin
(Depending on Inspection Result)
Get Access
 27.25
On Aircraft
Replace the Existing RH MLG Leg and Hinge Arm /
Barrel Pin (Depending on Inspection Result)
26.25
Replace the Existing LH MLG Leg and Hinge Arm /
Barrel Pin (Depending on Inspection Result)
26.25
Tests
 4.00
Close-Up
 5.50
TOTAL MANHOURS
 89.25
ELAPSED TIME (HOURS)
 45.25
H. WEIGHT AND BALANCE
Not Changed
I. ELECTRICAL LOAD DATA
Not Changed
J. REFERENCES
Aircraft Maintenance Manual (AMM)
 06-21-00 20-21-12 24-41-00
32-11-11 32-30-00
Elec. Std. Practices Manual (ESPM)
 20-55-00
In Service Information (ISI)
 00.00.00179
Service Bulletin (SB)
 A300-32-0469
DATE: Sep 24/19 SERVICE BULLETIN No.: A300-32-0468
REVISION No.: 00 - Sep 24/19 Page: 8
7
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SERVICE BULLETIN
K. PUBLICATION AFFECTED
None
L. INTERCHANGEABILITY/MIXABILITY
Not Applicable
M. SPARES
None
DATE: Sep 24/19 SERVICE BULLETIN No.: A300-32-0468
REVISION No.: 00 - Sep 24/19 Page: 9
7
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

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SERVICE BULLETIN
This Page Intentionally Left Blank
DATE: Sep 24/19 SERVICE BULLETIN No.: A300-32-0468
REVISION No.: 00 - Sep 24/19 Page: 10
7
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SERVICE BULLETIN
2. MATERIAL INFORMATION
**CONF ALL
A. MATERIAL - PRICE AND AVAILABILITY
(1) Procurement Addresses
Vendor parts are to be supplied from:
Equipment BFEB02
Equipment BFEB03
SAFRAN LANDING SYSTEMS
7 RUE DU GENERAL VALERIE ANDRE
78140 VELIZY-VILLACOUBLAY
FRANCE
T e l :+ 3 3( 0 ) 14 62 91 80 0
F a x :+ 3 3( 0 ) 14 62 98 77 0
(2) Price and Availability
Equipment BFEB03
Procurement terms for the equipment must be negotiated with the equipment supplier.
Equipment BFEB02
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.
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.
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
Consumable Materials listed i n the subsequent re ferenced tasks:
AMM 32-11-11, Page Block 401
AMM 32-11-11, Page Block 601
DATE: Sep 24/19 SERVICE BULLETIN No.: A300-32-0468
REVISION No.: 00 - Sep 24/19 Page: 11
7
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SERVICE BULLETIN
Consumable CMLB01
ITEM
 DESCRIPTION
 REFERENCE TO CML
MAT. No.
QTY PER A/C
 SEE
NOTES
Non Aqueous Cleaner-General
 08BAA9
 As required
Textile-Lint Free Cotton
 14SBA1
 As required
(2) Components
NOTE
: To accomplish this Service Bulletin it is necessary to use the expendable
parts listed in the subs equent referenced tasks:
AMM 32-11-11, Page Block 401
AMM 32-11-11, Page Block 601
(3) Equipment
Equipment BFEB02
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 ITEM
 OLD PART N˚
 INT
 SEE
NOTES
C23093-1010
 As
required
LEG
C23093-1115
 As
required
LEG
C23093-1216
 As
required
LEG
C23093-136
 As
required
LEG
C23093-1527
 As
required
LEG
C23093-1921
 As
required
LEG
C23093-224
 As
required
LEG
C23093-2529
 As
required
LEG
C23093-3529
 As
required
LEG
C23093-427
 As
required
LEG
C23093-527
 As
required
LEG
C23093-814
 As
required
LEG
C23093-921
 As
required
LEG
DATE: Sep 24/19 SERVICE BULLETIN No.: A300-32-0468
REVISION No.: 00 - Sep 24/19 Page: 12
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SERVICE BULLETIN
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 ITEM
 OLD PART N˚
 INT
 SEE
NOTES
C66441-200
 As
required
PIN
NOTE
: The above list of components is not an AIRBUS Kit, the required parts
shall be ordered as necessary through the given channel.
Equipment BFEB03
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 ITEM
 OLD PART N˚
 INT
 SEE
NOTES
C23094-1010
 As
required
LEG
C23094-1115
 As
required
LEG
C23094-1216
 As
required
LEG
C23094-136
 As
required
LEG
C23094-1527
 As
required
LEG
C23094-1921
 As
required
LEG
C23094-224
 As
required
LEG
C23094-2529
 As
required
LEG
C23094-3529
 As
required
LEG
C23094-427
 As
required
LEG
C23094-527
 As
required
LEG
C23094-814
 As
required
LEG
C23094-921
 As
required
LEG
C66441-200
 As
required
PIN
NOTE
: 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
DATE: Sep 24/19 SERVICE BULLETIN No.: A300-32-0468
REVISION No.: 00 - Sep 24/19 Page: 13
7
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SERVICE BULLETIN
F. TOOLING
(1) Tooling - Price and Availability
None
(2) Tools
To accomplish this Service Bulletin it is necessary to use the tools listed in the
subsequent referenced tasks:
AMM 32-11-11, Page Block 401
AMM 32-11-11, Page Block 601
AMM 32-30-00, Page Block 501
(3) Special Tools
None
DATE: Sep 24/19 SERVICE BULLETIN No.: A300-32-0468
REVISION No.: 00 - Sep 24/19 Page: 14
7
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SERVICE BULLETIN
3. ACCOMPLISHMENT INSTRUCTIONS
Task 320468-832-895-001 - Ins pect the RH / LH Hinge Arm / Barrel Pins and Connecting Rod
Bushings
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.
IF THERE IS CONTAMINATION, REFER TO 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
: 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 RC paragraph contained herein,
contact AIRBUS for further instructions and approval.
NOTE
: This Service Bulletin is classified mandatory or expected to be classified mandatory
by an Airworthiness Directive (AD). The paragraphs 3.C. and 3.D. in these
accomplishment instructions are Required for Compliance (RC) and must be done
to comply with the AD. To allow more flexibility, the rule "refer to" and "in
accordance with" will apply to these paragraphs 3.C. and 3.D. Other paragraphs
are recommended and may be deviated from, done as part of other actions or
DATE: Sep 24/19 SERVICE BULLETIN No.: A300-32-0468
REVISION No.: 00 - Sep 24/19 Page: 15
7
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SERVICE BULLETIN
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
: 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
: Discarded parts must be managed at the operator’s discretion.
Task Associated Data
Zone
731 741
Manpower
TOTAL MANHOURS
 22.25
ELAPSED TIME (HOURS)
 9.75
A. GENERAL
(1) Subtask 320468-910-401-001 - Standard Practices
Manpower Resources
Skills
 NON SPECIFIC
References
Aircraft Maintenance Manual (AMM)
 06-21-00, Page Block 001
20-21-12, Page Block 001
(a) To torque tighten the standard threaded fasteners, refer to AMM 20-21-12, Page
Block 001.
(b) For the identification of access panels, refer to AMM 06-21-00, Page Block 001.
(c) For the specification of materials (Mat. No.) given in this Service Bulletin, refer to
the Consumable Materials List (CML).
(d) For the identification of Zones, refer to AMM 06-21-00, Page Block 001.
(e) Put all the retained hardware in identified plastic bags and attach the bags to the
related unit.
(f) Tag all the parts you must remove and retain to make the subsequent installation
easier.
(2) Subtask 320468-839-401-001 - Administrative
Manpower Resources
Skills
 NON SPECIFIC
Write in the applicable aircraft records that you have done all the work given in the
Service Bulletin.
DATE: Sep 24/19 SERVICE BULLETIN No.: A300-32-0468
REVISION No.: 00 - Sep 24/19 Page: 16
7
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SERVICE BULLETIN
B. PREPARATION
(1) Subtask 320468-941-409-002 - Job Set-up
Work Zones and Access Panels
Zone
 Access/Work location
741
731
Manpower Resources
Skills
 NON SPECIFIC
References
Aircraft Maintenance Manual (AMM)
 24-41-00, Page Block 301
32-11-11, Page Block 601
NOTE
: For the basic Aircraft configuration, refer to AMM Chapter "Introduction -
Aircraft status for maintenance" in Manual Front Mater section.
(a) Make sure that the aircraft is electrically grounded, refer to AMM 24-41-00, Page
Block 301.
(b) Do the Job Set-up for the RH / LH MLG as specified in the LEG (Main Gear) -
Inspection/Check, refer to AMM 32-11-11, Page Block 601.
C. PROCEDURE
(1) Subtask 320468-020-401-001 - Remove the RH Hinge Arm / Barrel Pin
Work Zones and Access Panels
Zone
 Access/Work location
741
Manpower Resources
Manhours
 5.75
Minimum number of person
 5
Subtask elapsed time
 3.75
Skills
 AIRFRAME
References
Aircraft Maintenance Manual (AMM)
 32-11-11, Page Block 601
(a) Remove the RH MLG Hinge Arm / Barrel Pin, refer to AMM 32-11-11, Page Block
601:
As
required
Pin C66441-200 Retain
DATE: Sep 24/19 SERVICE BULLETIN No.: A300-32-0468
REVISION No.: 00 - Sep 24/19 Page: 17
7
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SERVICE BULLETIN
(2) Subtask 320468-832-401-001 - Inspect the RH Hinge Arm / Barrel Pin and
Connecting Rod Bushings
Work Zones and Access Panels
Zone
 Access/Work location
741
Manpower Resources
Manhours
 0.50
Minimum number of person
 1
Subtask elapsed time
 0.50
Skills
 AIRFRAME
Material necessary to do the job
Consumable CMLB01
ITEM
 DESCRIPTION
 REFERENCE TO
CML MAT. No.
QTY PER A/C
 SEE
NOTES
Non Aqueous Cleaner-
General
08BAA9
 As required
Textile-Lint Free Cotton
 14SBA1
 As required
References
Aircraft Maintenance Manual (AMM)
 32-11-11, Page Block 601
In Service Information (ISI)
 00.00.00179
Fig. A-UCAAA
Barrel / Hinge Arm Pin Inspection
Sheet 01
(a) Do a Special Detailed Inspection of the bushings of the connecting rod, using the
window in the dummy pin, refer to AMM 32-11-11, Page Block 601.
1
 If the bushings are found fractured, cracked, or distorted:
a
 Replace the associated MLG Leg and Hinge Arm / Barrel Pin. Proceed to
TASK 320468-831-895 001 Replace the RH / LH MLG Leg and Hinge
Arm / Barrel Pin (Depending on Inspection Result) .
b
 Upload the completed Inspection Report sheet given in Appendix 02 -
Inspection Report in accordance with ISI 00.00.00179.
c
 Inspect the opposite side MLG leg, refer to SUBTASK 320468-832-402
001 Inspect the LH Hinge Arm / Barrel Pin and Connecting Rod Bushings
, at the thresholds given in the accomplishment timescale paragraph
1.E.(2).
d
 Send the removed MLG Leg to MRO for inspection in accordance with
the thresholds given in the planning information paragraph 1.E.(2).
DATE: Sep 24/19 SERVICE BULLETIN No.: A300-32-0468
REVISION No.: 00 - Sep 24/19 Page: 18
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SERVICE BULLETIN
e
 Send the removed Hinge Arm / Barrel Pin to Safran Landing Systems for
investigation in accordance with the thresholds given in the planning
information paragraph 1.E.(2).
f
 Repeat the inspection within the required intervals in accordance with the
thresholds given in the planning information paragraph 1.E.(2).
2
 If the bushings are found with corrosion, wear, or discoloration on the inner
face of the bushings:
a
 Contact Safran Landing Systems for instructions.
3
 If no damage is found:
a
 Clean the inner and outer surfaces of the removed Hinge Arm / Barrel
Pin with:
Non Aqueous
Cleaner-General
08BAA9 As required
Textile-Lint Free
Cotton
14SBA1 As required
b
 Do a Detailed Visual Inspection of both inner and outer surfaces of the
removed Hinge Arm / Barrel Pin for presence of crack, chrome damage,
or corrosion, refer to AMM 32-11-11, Page Block 601.
<1> If a crack is found:
<a> Replace the associated MLG Leg. Proceed to TASK
320468-831-895 001 Replace the RH / LH MLG Leg and Hinge
Arm / Barrel Pin (Depending on Inspection Result) .
<b> Upload the completed Inspection Report sheet given in
Appendix 02 - Inspection Report in accordance with ISI
00.00.00179.
<c> Inspect the opposite side MLG leg, refer to SUBTASK
320468-832-402 001 Inspect the LH Hinge Arm / Barrel Pin
and Connecting Rod Bushings , at the thresholds given in the
accomplishment timescale paragraph 1.E.(2).
<d> Send the removed MLG Leg to MRO for inspection
in accordance with the thresholds given in the planning
information paragraph 1.E.(2).
<e> Send the removed Hinge Arm / Barrel Pin to Safran Landing
Systems for investigation in accordance with the thresholds
given in the planning information paragraph 1.E.(2).
<f> Repeat the inspection within the required intervals in
accordance with the thresholds given in the planning
information paragraph 1.E.(2).
DATE: Sep 24/19 SERVICE BULLETIN No.: A300-32-0468
REVISION No.: 00 - Sep 24/19 Page: 19
7
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SERVICE BULLETIN
<2> If no crack is found but outer surface has chrome damage and/or
corrosion:
<a> Install a serviceable Hinge Arm / Barrel Pin, refer to SUBTASK
320468-420-401 001 Install the RH Hinge Arm / Barrel Pin .
<b> Send the removed Hinge Arm / Barrel Pin to Safran Landing
Systems for investigation in accordance with the thresholds
given in the planning information paragraph 1.E.(2).
<c> Upload the completed Inspection Report sheet given in
Appendix 02 - Inspection Report in accordance with ISI
00.00.00179.
<d> Repeat the inspection within the required intervals in
accordance with the thresholds given in the planning
information paragraph 1.E.(2).
<3> If no crack is found and outer surface has no chrome damage or
corrosion:
<a> Install the retained Hinge Arm / Barrel Pin refer to SUBTASK
320468-420-401 001 Install the RH Hinge Arm / Barrel Pin .
<b> Repeat the inspection within the required intervals in
accordance with the thresholds given in the planning
information paragraph 1.E.(2).
(3) Subtask 320468-420-401-001 - Install the RH Hinge Arm / Barrel Pin
Work Zones and Access Panels
Zone
 Access/Work location
741
Manpower Resources
Manhours
 2.25
Minimum number of person
 1
Subtask elapsed time
 2.25
Skills
 AIRFRAME
Material necessary to do the job
Equipment BFEB03
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 SEE
NOTES
C66441-200
 As required
 PIN
NOTE
: The above list of components is not an AIRBUS Kit, the required parts
shall be ordered as necessary through the given channel.
DATE: Sep 24/19 SERVICE BULLETIN No.: A300-32-0468
REVISION No.: 00 - Sep 24/19 Page: 20
7
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SERVICE BULLETIN
References
Aircraft Maintenance Manual (AMM)
 32-11-11, Page Block 601
In Service Information (ISI)
 00.00.00179
(a) Refer to the RH Hinge Arm / Barrel Pin inspection results:
1
 If no crack was found but outer surface had chrome damage and/or corrosion:
a
 Install a serviceable Hinge Arm / Barrel Pin, refer to AMM 32-11-11,
Page Block 601:
As
required
Pin C66441-200
2
 If no crack was found and outer surface had no chrome damage or corrosion:
a
 Install the retained Hinge Arm / Barrel Pin, refer to AMM 32-11-11, Page
Block 601:
As
required
Pin C66441-200 Retained at
removal
(4) Subtask 320468-020-402-001 - Remove the LH Hinge Arm / Barrel Pin
Work Zones and Access Panels
Zone
 Access/Work location
731
Manpower Resources
Manhours
 5.75
Minimum number of person
 5
Subtask elapsed time
 3.75
Skills
 AIRFRAME
References
Aircraft Maintenance Manual (AMM)
 32-11-11, Page Block 601
(a) Remove the LH MLG Hinge Arm / Barrel Pin, refer to AMM 32-11-11, Page Block
601:
As
required
Pin C66441-200 Retain
(5) Subtask 320468-832-402-001 - Inspect the LH Hinge Arm / Barrel Pin and
Connecting Rod Bushings
Work Zones and Access Panels
Zone
 Access/Work location
731
DATE: Sep 24/19 SERVICE BULLETIN No.: A300-32-0468
REVISION No.: 00 - Sep 24/19 Page: 21
7
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SERVICE BULLETIN
Manpower Resources
Manhours
 0.50
Minimum number of person
 1
Subtask elapsed time
 0.50
Skills
 AIRFRAME
Material necessary to do the job
Consumable CMLB01
ITEM
 DESCRIPTION
 REFERENCE TO
CML MAT. No.
QTY PER A/C
 SEE
NOTES
Non Aqueous Cleaner-
General
08BAA9
 As required
Textile-Lint Free Cotton
 14SBA1
 As required
References
Aircraft Maintenance Manual (AMM)
 32-11-11, Page Block 601
In Service Information (ISI)
 00.00.00179
Fig. A-UCAAA
Barrel / Hinge Arm Pin Inspection
Sheet 01
(a) Do a Special Detailed Inspection of the bushings of the connecting rod, using the
window in the dummy pin, refer to AMM 32-11-11, Page Block 601.
1
 If the bushings are found fractured, cracked, or distorted:
a
 Replace the associated MLG Leg and Hinge Arm / Barrel Pin. Proceed to
TASK 320468-831-895 001 Replace the RH / LH MLG Leg and Hinge
Arm / Barrel Pin (Depending on Inspection Result) .
b
 Upload the completed Inspection Report sheet given in Appendix 02 -
Inspection Report in accordance with ISI 00.00.00179.
c
 Inspect the opposite side MLG leg, refer to SUBTASK 320468-832-401
001 Inspect the RH Hinge Arm / Barrel Pin and Connecting Rod
Bushings , at the thresholds given in the accomplishment timescale
paragraph 1.E.(2).
d
 Send the removed MLG Leg to MRO for inspection in accordance with
the thresholds given in the planning information paragraph 1.E.(2).
e
 Send the removed Hinge Arm / Barrel Pin to Safran Landing Systems for
investigation in accordance with the thresholds given in the planning
information paragraph 1.E.(2).
f
 Repeat the inspection within the required intervals in accordance with the
thresholds given in the planning information paragraph 1.E.(2).
DATE: Sep 24/19 SERVICE BULLETIN No.: A300-32-0468
REVISION No.: 00 - Sep 24/19 Page: 22
7
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SERVICE BULLETIN
2
 If the bushings are found with corrosion, wear, or discoloration on the inner
face of the bushings:
a
 Contact Safran Landing Systems for instructions.
3
 If no damage is found:
a
 Clean the inner and outer diameter of the removed Hinge Arm / Barrel
Pin with:
Non Aqueous
Cleaner-General
08BAA9 As required
Textile-Lint Free
Cotton
14SBA1 As required
b
 Do a Detailed Visual Inspection of both inner and outer surfaces of the
removed Hinge Arm / Barrel Pin for presence of crack, chrome damage,
or corrosion, refer to AMM 32-11-11, Page Block 601.
<1> If a crack is found:
<a> Replace the associated MLG Leg. Proceed to TASK
320468-831-895 001 Replace the RH / LH MLG Leg and Hinge
Arm / Barrel Pin (Depending on Inspection Result) .
<b> Upload the completed Inspection Report sheet given in
Appendix 02 - Inspection Report in accordance with ISI
00.00.00179.
<c> Inspect the opposite side MLG leg, refer to SUBTASK
320468-832-401 001 Inspect the RH Hinge Arm / Barrel Pin
and Connecting Rod Bushings , at the thresholds given in the
accomplishment timescale paragraph 1.E.(2).
<d> Send the removed MLG Leg to MRO for inspection
in accordance with the thresholds given in the planning
information paragraph 1.E.(2).
<e> Send the removed Hinge Arm / Barrel Pin to Safran Landing
Systems for investigation in accordance with the thresholds
given in the planning information paragraph 1.E.(2).
<f> Repeat the inspection within the required intervals in
accordance with the thresholds given in the planning
information paragraph 1.E.(2).
<2> If no crack is found but outer surface has chrome damage and/or
corrosion:
<a> Install a serviceable Hinge Arm / Barrel Pin, refer to SUBTASK
320468-420-402 001 Install the LH Hinge Arm / Barrel Pin .
DATE: Sep 24/19 SERVICE BULLETIN No.: A300-32-0468
REVISION No.: 00 - Sep 24/19 Page: 23
7
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@A300
SERVICE BULLETIN
<b> Send the removed Hinge Arm / Barrel Pin to Safran Landing
Systems for investigation in accordance with the thresholds
given in the planning information paragraph 1.E.(2)..
<c> Upload the completed Inspection Report sheet given in
Appendix 02 - Inspection Report in accordance with ISI
00.00.00179.
<d> Repeat the inspection within the required intervals in
accordance with the thresholds given in the planning
information paragraph 1.E.(2).
<3> If no crack is found and outer surface has no chrome damage or
corrosion:
<a> Install the retained Hinge Arm / Barrel Pin, refer to SUBTASK
320468-420-402 001 Install the LH Hinge Arm / Barrel Pin .
<b> Repeat the inspection within the required intervals in
accordance with the thresholds given in the planning
information paragraph 1.E.(2).
(6) Subtask 320468-420-402-001 - Install the LH Hinge Arm / Barrel Pin
Work Zones and Access Panels
Zone
 Access/Work location
731
Manpower Resources
Manhours
 2.25
Minimum number of person
 1
Subtask elapsed time
 2.25
Skills
 AIRFRAME
Material necessary to do the job
Equipment BFEB02
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 SEE
NOTES
C66441-200
 As required
 PIN
NOTE
: 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)
 32-11-11, Page Block 601
In Service Information (ISI)
 00.00.00179
Fig. A-UCAAA
Barrel / Hinge Arm Pin Inspection
Sheet 01
DATE: Sep 24/19 SERVICE BULLETIN No.: A300-32-0468
REVISION No.: 00 - Sep 24/19 Page: 24
7
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SERVICE BULLETIN
(a) Refer to the RH Hinge Arm / Barrel Pin inspection results:
1
 If no crack was found but outer surface had chrome damage and/or corrosion:
a
 Install a serviceable Hinge Arm / Barrel Pin, refer to AMM 32-11-11,
Page Block 601:
As
required
Pin C66441-200
2
 If no crack was found and outer surface had no chrome damage or corrosion:
a
 Install the retained Hinge Arm / Barrel Pin, refer to AMM 32-11-11, Page
Block 601:
As
required
Pin C66441-200 Retained at
removal
D. TEST
None
E. CLOSE-UP
(1) Subtask 320468-942-401-001 - Close-up
Manpower Resources
Skills
 NON SPECIFIC
References
Aircraft Maintenance Manual (AMM)
 32-11-11, Page Block 601
NOTE
: If you intend to accomplish an associated Repair Task during the same
layover period, the subsequent Close-up procedure is not necessary.
(a) Make sure that the work areas are clean and clear of tools and other items of
equipment.
(b) Do the Close-up as specified in the LEG (Main Gear) - Inspection/Check, refer to
AMM 32-11-11, Page Block 601.
(c) Put the aircraft back to its initial configuration.
DATE: Sep 24/19 SERVICE BULLETIN No.: A300-32-0468
REVISION No.: 00 - Sep 24/19 Page: 25
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This Page Intentionally Left Blank
DATE: Sep 24/19 SERVICE BULLETIN No.: A300-32-0468
REVISION No.: 00 - Sep 24/19 Page: 26
7
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SERVICE BULLETIN
Task 320468-831-895-001 - Replace the RH / LH MLG Leg and Hinge Arm / Barrel Pin
(Depending on Inspection Result)
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.
IF THERE IS CONTAMINATION, REFER TO 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
: 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 RC paragraph contained herein,
contact AIRBUS for further instructions and approval.
NOTE
: This Service Bulletin is classified mandatory or expected to be classified mandatory
by an Airworthiness Directive (AD). The paragraphs 3.C. and 3.D. in these
accomplishment instructions are Required for Compliance (RC) and must be done
to comply with the AD. To allow more flexibility, the rule "refer to" and "in
accordance with" will apply to these paragraphs 3.C. and 3.D. 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
DATE: Sep 24/19 SERVICE BULLETIN No.: A300-32-0468
REVISION No.: 00 - Sep 24/19 Page: 27
7
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### Page 32

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SERVICE BULLETIN
serviceable condition.
NOTE
: Discarded parts must be managed at the operator’s discretion.
Task Associated Data
Zone
731 741
Manpower
TOTAL MANHOURS
 89.25
ELAPSED TIME (HOURS)
 45.25
A. GENERAL
(1) Subtask 320468-910-402-002 - Standard Practices
Manpower Resources
Skills
 NON SPECIFIC
References
Aircraft Maintenance Manual (AMM)
 06-21-00, Page Block 001
20-21-12, Page Block 001
(a) To torque tighten the standard threaded fasteners, refer to AMM 20-21-12, Page
Block 001.
(b) For the identification of access panels, refer to AMM 06-21-00, Page Block 001.
(c) For the specification of materials (Mat. No.) given in this Service Bulletin, refer to
the Consumable Materials List (CML).
(d) For the identification of Zones, refer to AMM 06-21-00, Page Block 001.
(e) Put all the retained hardware in identified plastic bags and attach the bags to the
related unit.
(f) Tag all the parts you must remove and retain to make the subsequent installation
easier.
(2) Subtask 320468-839-402-001 - Administrative
Manpower Resources
Skills
 NON SPECIFIC
Write in the applicable aircraft records that you have done all the work given in the
Service Bulletin.
DATE: Sep 24/19 SERVICE BULLETIN No.: A300-32-0468
REVISION No.: 00 - Sep 24/19 Page: 28
7
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@A300
SERVICE BULLETIN
B. PREPARATION
(1) Subtask 320468-941-407-001 - Job Set-up for the RH MLG
Work Zones and Access Panels
Zone
 Access/Work location
741
Manpower Resources
Skills
 NON SPECIFIC
References
Aircraft Maintenance Manual (AMM)
 32-11-11, Page Block 401
NOTE
: For the basic Aircraft configuration, refer to AMM Chapter "Introduction -
Aircraft status for maintenance" in Manual Front Matter section.
(a) Do the Job Set-up as specified in LEG (Main Gear) - Removal/Installation, refer to
AMM 32-11-11, Page Block 401.
(2) Subtask 320468-941-408-001 - Job Set-up for the LH MLG
Work Zones and Access Panels
Zone
 Access/Work location
731
Manpower Resources
Skills
 NON SPECIFIC
References
Aircraft Maintenance Manual (AMM)
 32-11-11, Page Block 401
NOTE
: For the basic Aircraft configuration, refer to AMM Chapter "Introduction -
Aircraft status for maintenance" in Manual Front Matter section.
(a) Do the Job Set-up as specified in LEG (Main Gear) - Removal/Installation, refer to
AMM 32-11-11, Page Block 401.
C. PROCEDURE
(1) Subtask 320468-960-401-001 - Replace the Existing RH MLG Leg and Hinge Arm /
Barrel Pin (Depending on Inspection Result)
Work Zones and Access Panels
Zone
 Access/Work location
741
DATE: Sep 24/19 SERVICE BULLETIN No.: A300-32-0468
REVISION No.: 00 - Sep 24/19 Page: 29
7
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@A300
SERVICE BULLETIN
Manpower Resources
Manhours
 26.25
Minimum number of person
 2
Subtask elapsed time
 23.25
Skills
 AIRFRAME
Material necessary to do the job
Equipment BFEB03
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 SEE
NOTES
C23094-1010
 As required
 LEG
C23094-1115
 As required
 LEG
C23094-1216
 As required
 LEG
C23094-136
 As required
 LEG
C23094-1527
 As required
 LEG
C23094-1921
 As required
 LEG
C23094-224
 As required
 LEG
C23094-2529
 As required
 LEG
C23094-3529
 As required
 LEG
C23094-427
 As required
 LEG
C23094-527
 As required
 LEG
C23094-814
 As required
 LEG
C23094-921
 As required
 LEG
NOTE
: 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)
 32-11-11, Page Block 401
(a) Replace existing RH MLG Leg with a serviceable one, refer to AMM 32-11-11,
Page Block 401.
Replace:
As
required
LEG ASSY-MLG C 23094-1010 Retain
WITH:
As
required
LEG ASSY-MLG C23094-1010
OR
As
required
LEG ASSY-MLG C 23094-1115 Retain
DATE: Sep 24/19 SERVICE BULLETIN No.: A300-32-0468
REVISION No.: 00 - Sep 24/19 Page: 30
7
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### Page 35

@A300
SERVICE BULLETIN
WITH:
As
required
LEG ASSY-MLG C23094-1115
OR
As
required
LEG ASSY-MLG C 23094-1216 Retain
WITH:
As
required
LEG ASSY-MLG C23094-1216
OR
As
required
LEG ASSY-MLG C 23094-136 Retain
WITH:
As
required
LEG ASSY-MLG C23094-136
OR
As
required
LEG ASSY-MLG C 23094-1527 Retain
WITH:
As
required
LEG ASSY-MLG C23094-1527
OR
As
required
LEG ASSY-MLG C 23094-1921 Retain
WITH:
As
required
LEG ASSY-MLG C23094-1921
OR
As
required
LEG ASSY-MLG C 23094-224 Retain
WITH:
As
required
LEG ASSY-MLG C23094-224
DATE: Sep 24/19 SERVICE BULLETIN No.: A300-32-0468
REVISION No.: 00 - Sep 24/19 Page: 31
7
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### Page 36

@A300
SERVICE BULLETIN
OR
As
required
LEG ASSY-MLG C 23094-2529 Retain
WITH:
As
required
LEG ASSY-MLG C23094-2529
OR
As
required
LEG ASSY-MLG C 23094-3529 Retain
WITH:
As
required
LEG ASSY-MLG C23094-3529
OR
As
required
LEG ASSY-MLG C 23094-427 Retain
WITH:
As
required
LEG ASSY-MLG C23094-427
OR
As
required
LEG ASSY-MLG C 23094-527 Retain
WITH:
As
required
LEG ASSY-MLG C23094-527
OR
As
required
LEG ASSY-MLG C 23094-814 Retain
WITH:
As
required
LEG ASSY-MLG C23094-814
OR
As
required
LEG ASSY-MLG C 23094-921 Retain
DATE: Sep 24/19 SERVICE BULLETIN No.: A300-32-0468
REVISION No.: 00 - Sep 24/19 Page: 32
7
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### Page 37

@A300
SERVICE BULLETIN
WITH:
As
required
LEG ASSY-MLG C23094-921
NOTE
: Retained MLG Leg to be sent to MRO for inspection.
NOTE
: Install the same MLG Leg part number that was removed.
(2) Subtask 320468-960-402-001 - Replace the Existing LH MLG Leg and Hinge Arm /
Barrel Pin (Depending on Inspection Result)
Work Zones and Access Panels
Zone
 Access/Work location
731
Manpower Resources
Manhours
 26.25
Minimum number of person
 4
Subtask elapsed time
 23.25
Skills
 AIRFRAME
Material necessary to do the job
Equipment BFEB02
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 SEE
NOTES
C23093-1010
 As required
 LEG
C23093-1115
 As required
 LEG
C23093-1216
 As required
 LEG
C23093-136
 As required
 LEG
C23093-1527
 As required
 LEG
C23093-1921
 As required
 LEG
C23093-224
 As required
 LEG
C23093-2529
 As required
 LEG
C23093-3529
 As required
 LEG
C23093-427
 As required
 LEG
C23093-527
 As required
 LEG
C23093-814
 As required
 LEG
C23093-921
 As required
 LEG
NOTE
: 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)
 32-11-11, Page Block 401
DATE: Sep 24/19 SERVICE BULLETIN No.: A300-32-0468
REVISION No.: 00 - Sep 24/19 Page: 33
7
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### Page 38

@A300
SERVICE BULLETIN
(a) Replace existing LH MLG Leg with a serviceable one, refer to AMM 32-11-11, Page
Block 401.
Replace:
As
required
LEG ASSY-MLG C 23093-1010 Retain
WITH:
As
required
LEG ASSY-MLG C23093-1010
OR
As
required
LEG ASSY-MLG C 23093-1115 Retain
WITH:
As
required
LEG ASSY-MLG C23093-1115
OR
As
required
LEG ASSY-MLG C 23093-1216 Retain
WITH:
As
required
LEG ASSY-MLG C23093-1216
OR
As
required
LEG ASSY-MLG C 23093-136 Retain
WITH:
As
required
LEG ASSY-MLG C23093-136
OR
As
required
LEG ASSY-MLG C 23093-1527 Retain
WITH:
As
required
LEG ASSY-MLG C23093-1527
OR
DATE: Sep 24/19 SERVICE BULLETIN No.: A300-32-0468
REVISION No.: 00 - Sep 24/19 Page: 34
7
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### Page 39

@A300
SERVICE BULLETIN
As
required
LEG ASSY-MLG C 23093-1921 Retain
WITH:
As
required
LEG ASSY-MLG C23093-1921
OR
As
required
LEG ASSY-MLG C 23093-224 Retain
WITH:
As
required
LEG ASSY-MLG C23093-224
OR
As
required
LEG ASSY-MLG C 23093-2529 Retain
WITH:
As
required
LEG ASSY-MLG C23093-2529
OR
As
required
LEG ASSY-MLG C 23093-3529 Retain
WITH:
As
required
LEG ASSY-MLG C23093-3529
OR
As
required
LEG ASSY-MLG C 23093-427 Retain
WITH:
As
required
LEG ASSY-MLG C23093-427
OR
As
required
LEG ASSY-MLG C 23093-527 Retain
WITH:
DATE: Sep 24/19 SERVICE BULLETIN No.: A300-32-0468
REVISION No.: 00 - Sep 24/19 Page: 35
7
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 40

@A300
SERVICE BULLETIN
As
required
LEG ASSY-MLG C23093-527
OR
As
required
LEG ASSY-MLG C 23093-814 Retain
WITH:
As
required
LEG ASSY-MLG C23093-814
OR
As
required
LEG ASSY-MLG C 23093-921 Retain
WITH:
As
required
LEG ASSY-MLG C23093-921
NOTE
: Retained MLG Leg to be sent to MRO for inspection.
NOTE
: Install the same MLG Leg part number that was removed.
D. TEST
(1) Subtask 320468-720-402-001 - Test
Manpower Resources
Skills
 NON SPECIFIC
References
Aircraft Maintenance Manual (AMM)
 32-11-11, Page Block 401
(a) Do the test procedure as specified after the installation of the MLG (LH and RH
sides), refer to AMM 32-11-11, Page Block 401.
E. CLOSE-UP
(1) Subtask 320468-942-402-001 - Close-up
Work Zones and Access Panels
Zone
 Access/Work location
741
731
Manpower Resources
Skills
 NON SPECIFIC
DATE: Sep 24/19 SERVICE BULLETIN No.: A300-32-0468
REVISION No.: 00 - Sep 24/19 Page: 36
7
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 41

@A300
SERVICE BULLETIN
References
Aircraft Maintenance Manual (AMM)
 32-11-11, Page Block 401
(a) Make sure that the work areas are clean and clear of tools and other items of
equipment.
(b) Do the Close-Up as specified in the LEG (Main Gear) - Removal/Installation, refer
to AMM 32-11-11, Page Block 401.
(c) Put the aircraft back to its initial configuration.
DATE: Sep 24/19 SERVICE BULLETIN No.: A300-32-0468
REVISION No.: 00 - Sep 24/19 Page: 37
7
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### Page 42

@A300
SERVICE BULLETIN
**CONF ALL
B
LH SHOWN
RH SYMMETRICAL
Z731
Z741
A
A
B
LH SHOWN
RH SYMMETRICAL
A A
LH SHOWN
RH SYMMETRICAL
INSPECT THE INNER AND OUTER
SURFACES OF THE PIN
A
A
A_SB_320468_7_CAAA_01_04
Figure A-UCAAA - Sheet 01
Barrel / Hinge Arm Pin Inspection
DATE: Sep 24/19 SERVICE BULLETIN No.: A300-32-0468
REVISION No.: 00 - Sep 24/19 Page: 38
7
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### Page 43

@A300
SERVICE BULLETIN
**CONF ALL
NOYES
ARE THE
BUSHINGS CRACKED,
DISTORTED, OR
FRACTURED?
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.
REMOVE THE HINGE ARM / BARREL PIN FROM THE MAIN LANDING GEAR
DO A SPECIAL DETAILED INSPECTION OF THE CONNECTING ROD BUSHINGS
DO A DETAILED VISUAL
INSPECTION OF THE
HINGE ARM / BARREL PIN
IS THE
HINGE ARM /
BARREL PIN
CRACKED?
NO
YES
INSTALL A SERVICEABLE
HINGE ARM / BARREL PIN
DO THE
BUSHINGS SHOW SIGNS
OF CORROSION, WEAR, OR
DISCOLORATION?
NO
YES
CONTACT SAFRAN LANDING
SYSTEMS FOR
FURTHER INSTRUCTION
DOES THE
HINGE ARM / BARREL PIN
SHOW OD CHROME DAMAGE
AND OR CORROSION?
YES
RE−INSTALL THE HINGE
ARM / BARREL PIN
NO
REPEAT INSPECTION WITHIN
THE REQUIRED INTERVALS
IN ACCORDANCE WITH
THRESHOLDS GIVEN IN
PLANNING INFORMATION
PARAGRAPH 1.E.(2)
SEND THE REMOVED HINGE ARM / BARREL PIN TO
SAFRAN LANDING SYSTEMS FOR INVESTIGATION
IF APPLICABLE, SEND THE REMOVED MAIN
LANDING GEAR TO THE MRO FOR INSPECTION
INSPECT THE
OPPOSITE SIDE LEG
IN ACCORDANCE WITH
THRESHOLDS GIVEN
IN PLANNING
INFORMATION
PARAGRAPH 1.E.(2)
REPLACE THE MAIN LANDING GEAR LEG
INCLUDING THE HINGE ARM / BARREL PIN
IN ACCORDANCE WITH THRESHOLDS GIVEN
IN PLANNING INFORMATION PARAGRAPH 1.E.(2)
REPORT TO
AIRBUS
AND REPORT TO AIRBUS
A_SB_320468_7_FAAA_01_08
Figure A-UFAAA - Sheet 01
Flowchart
DATE: Sep 24/19 SERVICE BULLETIN No.: A300-32-0468
REVISION No.: 00 - Sep 24/19 Page: 39
7
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### Page 44

@A300
SERVICE BULLETIN
This Page Intentionally Left Blank
DATE: Sep 24/19 SERVICE BULLETIN No.: A300-32-0468
REVISION No.: 00 - Sep 24/19 Page: 40
7
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### Page 45

@A300
SERVICE BULLETIN
Appendix 01 - Manpower Gantt Chart
**CONF ALL
For an explanation of the man-hours and elapsed time, refer to the next page.
DATE: Sep 24/19 SERVICE BULLETIN No.: A300-32-0468
REVISION No.: 00 - Sep 24/19 Page: 1
7
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### Page 46

@A300
SERVICE BULLETIN
Appendix 01 - Manpower Gantt Chart
**CONF ALL
ELAPSED TIME ASSUMPTION SERVICE BULLETIN No A300−32−0468
SB ELAPSED TIME
(HOURS)
MH ET/S
TOTAL MANHOURS
SB ELAPSED TIME
22.25
9.75
STEPS
10
INSPECT THE RH HINGE ARM / BARREL PIN 0.50 0.50
0.50 0.50
CLOSE−UP 3.25 1.25
MH
ET/S:
PER
MANHOURS
ELAPSED TIME PER STEP
NUMBER OF PERSONS
01
02
THIS CHART IS ONLY A PROPOSAL.
OPERATORS MAY DETERMINE THAT ANOTHER WAY
TO DO THE WORK IS MORE SUITABLE FOR THEM.
01
02
NOTE:
PER
1
1
5
:
:
IF A VSB IS INVOLVED, THE ASSOCIATED MANHOURS
ARE NOT REFLECTED IN THIS GANTT CHART.
2 3 4 5 6 7 8 9 10
INSPECT THE LH HINGE ARM / BARREL PIN
JOB SET−UP 2.00 2.001
REMOVE THE RH HINGE ARM / BARREL PIN 5.75 3.755
REMOVE THE LH HINGE ARM / BARREL PIN 5.75 3.755
AND CONNECTING ROD BUSHINGS
AND CONNECTING ROD BUSHINGS
INSTALL THE RH HINGE ARM / BARREL PIN 2.25 2.251
2.25 2.251INSTALL THE LH HINGE ARM / BARREL PIN
A_SB_320468_7_AAAA_01_05
Figure A-UAAAA - Sheet 01
Appendix 01 - Manpower Gantt Chart
DATE: Sep 24/19 SERVICE BULLETIN No.: A300-32-0468
REVISION No.: 00 - Sep 24/19 Page: 2
7
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### Page 47

@A300
SERVICE BULLETIN
Appendix 02 - Inspection Report
**CONF ALL
The results of the inspection, including no findings, replacement or actions to be done, must be
uploaded in accordance with ISI 00.00.00179 using the on-line reporting application in AIRBUSworld.
DATE: Sep 24/19 SERVICE BULLETIN No.: A300-32-0468
REVISION No.: 00 - Sep 24/19 Page: 1
7
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### Page 48

@A300
SERVICE BULLETIN
Appendix 02 - Inspection Report
**CONF ALL
INSPECTION REPORT
SERVICE BULLETIN No :
A/C MSN :
FLIGHT CYCLES :
FLIGHT HOURS :
A300−32−0468
DATE OF INSPECTION :
INSPECTION METHOD : SPECIAL DETAILED
INSPECTION
UPLOAD THE COMPLETED INSPECTION REPORT
SHEET IN ACCORDANCE WITH ISI 00.00.00179
INSPECTED MLG LEG LOCATION:
INSPECTED MLG ASSEMBLY NUMBER:
INSPECTED MLG LEG SERIAL NUMBER:
RH LH
CRACK
DISTORTION
BROKEN INTO PARTS
CORROSION
WEAR
DISCOLORATION
NO DAMAGE
NOYES
BUSHING INSPECTION RESULTS:
PIN INSPECTION RESULTS:
N/A (BUSHING INSPECTION LED TO MLG REPLACEMENT)
CRACK ON EXTERNAL DIAMETER
CRACK ON INTERNAL DIAMETER
CHROME DAMAGE / CORROSION
DISCOLORATION
NO DAMAGE
NOYES
MLG LEG REPLACEMENT:
REPLACEMENT NOT NECESSARY:
REPLACEMENT NECESSARY:
NEW MLG LEG LOCATION:
INSTALLED MLG LEG ASSEMBLY NUMBER:
INSTALLED MLG LEG SERIAL NUMBER:
RH LH
A_SB_320468_7_AEAA_01_01
Figure A-UAEAA - Sheet 01
Appendix 02 - Inspection Report
DATE: Sep 24/19 SERVICE BULLETIN No.: A300-32-0468
REVISION No.: 00 - Sep 24/19 Page: 2
7
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### Page 49

@A300
SERVICE BULLETIN
Service Bulletin REPORTING
TITLE: MAIN LANDING GEAR - INSPECTION OF THE HINGE ARM/BARREL
PIN
MODIFICATION No.: None
SB Reporting status
This Service Bulletin will only be incorporated into affected customized Maintenance and Flight
Operations Products if it is duly reported to Airbus.
General information
The SB Reporting policy is published in ISI 00.00.00135. This document provides information regarding:
the SB Reporting means and benefits, the update of customized Maintenance Products and customized
Flight Operations Products.
If this Service Bulletin has an operational impact, refer to paragraph "Flight Operations Products" for
further information on the update of affected Flight Operations Products.
SB Reporting procedure
Standard practice to report SB is to use the online reporting application on AirbusWorld.
Refer to ISI 00.00.00179:
- For complete information on reporting means to Airbus. Question 2 "What are the standard
practices for SB reporting?"
- If this SB requires previous or simultaneous accomplishment of other SBs, Question 3 "What about
the reporting of prerequisite Service Bulletin?"
NOTE:
 ISI 00.00.00179 covers all the frequently asked questions about SB Reporting. It is revised on a
regular basis.
DATE: Sep 24/19 SERVICE BULLETIN No.: A300-32-0468
REVISION No.: 00 - Sep 24/19 Page: 1
7
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

### Page 50

@A300
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: Sep 24/19 SERVICE BULLETIN No.: A300-32-0468
REVISION No.: 00 - Sep 24/19 Page: 1
7
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

---
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